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Aircraft Accident Briefs - Brief Format U.S. Civil and Foreign Aviation

CESSNA P337 · Other Documents

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Overview

This document is a technical report published by the National Transportation Safety Board (NTSB) that provides a summary of aircraft accidents occurring in U.S. civil and foreign aviation during the calendar year 1986. It includes approximately 200 accident reports, detailing the facts, conditions, circumstances, and probable causes of each incident. The report is intended for aviation professionals, safety analysts, and enthusiasts interested in understanding the factors contributing to aviation accidents. The data is presented in a brief format, allowing for quick reference and analysis of trends in aviation safety.

  • The report covers approximately 200 aviation accidents from 1986.
  • Accidents are categorized by type of operation, such as general aviation or air carrier.
  • Definitions of key terms help clarify the nature and severity of accidents and injuries.
  • Probable causes are determined based on thorough investigations conducted by the NTSB.

Document

Source

Originally published by libraryonline.erau.edu. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Other Documents
Year
1986
Pages
428
File size
12 MB
Publisher
libraryonline.erau.edu
How rare is it?
2CESSNA P337 registered worldwide

Common. Rarer than 17% of the aircraft models we track.

Documentation completeness
3/7

Most owners only have the POH. Here's the essential set for the CESSNA P337.

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In this document

Definitions

The document defines key terms related to aviation accidents, including 'Aircraft Accidents', 'Fatal Injury', 'Serious Injury', and 'Substantial Damage'. These definitions help clarify the criteria for what constitutes an accident and the severity of injuries sustained.

File Order Listing

The report includes a file order listing of accidents, organized by issue number and date. Each entry provides details such as the aircraft registration, date, location, make and model, and the nature of injuries sustained.

Probable Causes

The NTSB determines the probable causes of each accident based on the findings from investigations. This section summarizes the factors that contributed to the accidents, which can include pilot error, mechanical failure, and environmental conditions.

Accident Reports

The main body of the document consists of individual accident reports. Each report includes basic information about the accident, aircraft details, environmental conditions, and a narrative describing the events leading to the accident.

Safety notes

  • Accident reports are subject to legal limitations and cannot be used as evidence in lawsuits.
  • Caution should be exercised when interpreting the data due to potential abbreviations and formatting issues.

Full document text

TECHNICAL REPORT DOCUMENTATION PAGE . Report No. NTSB/AAB-87/12 2.Government Accession No. 3.Recipient's Catalog No . PB87-916912 . Title and Subtitle 7. Aircraft Accident Briefs - Brief Format U.S. Civil and Foreign Aviation 9. Performing Organization Name and Address Bureau of Field Operations National Transportation Safety Board Washington, D.C. 20594 12.Sponsoring Agency Name and Address NATIONAL TRANSPORTATION SAFETY BOARD Washington, D. C. 20594 15.Supplementary Notes .Abstract 5.Report Date Organization 10.Work Unit No. 11 .Contract or Grant No. 13.Type of Report and Period Covered Approximately 200 General Aviation and Air Carrier Accidents Occurring in This publication contains selected aircraft accident reports in Brief Format occurring in U.S. civil and foreign aviation operations during Calendar Year 1986. Approximately 200 General Aviation and Air Carrier accidents contained in this publication represent a random selection. This publication is issued irregularly, normally eighteen times each year. The Brief Format represents the facts, conditions, circumstances and probable cause(s) for each accident. File Numbers: 1801 through 2000 17.Key Words Aviation accident, probable cause, findings, certificate/rating, injuries, type of accident, type operating certificate, flight conducted under, accident occurred during, aircraft damage, basic weather 19.Security Classification (of this report) UNCLASSIFIED NTSB Form 1765.2 (Rev. 9/74) 20.Security Classification (of this page) UNCLASSIFIED .Distribution Statement This document is available to the public through the National Technical Infor- mation Service, Spring- field, Virginia 22161 21 .No. of Pages 22.Price 421 FOREWORD The National Transportaqon Safety Board, in accordance with th.e provisions of Title VII of the Federal Aviation Act of 1958 (as amended) and Section 304(a) of the Independent Safety Board Act of 1974, has determined the probable cause(s) of the accidents reported herein. This publication is issued eighteen (18) times per year and contains approximately 200 U.S. and foreign aircraft accident/incident reports arranged in state and date order. The enclosed computer briefs are the reports of the National Transportation Safety Board and thereby subject to the limitations of 49 USC 144l(e) which states: "No part of any report or reports of the Board, relating to any accident or the investigation thereof, shall be admitted as evidence or used in any suit or action for damage growing out of any matter mentioned in such report or reports." In reading these reports, it shou 1d be borne in mind th at they are produced directly from records on magnetic disk by electronic data processing equipment. Due to spacing limitations a number of abbreviations are utilized in the- narrative section. Therefore, caution should be exercised in reading this section on the Briefs of Accidents. Collisions between aircraft are treated as one accident. An analysis is done on each aircraft involved in a collision. This produces two aircraft accident records per accident. Consequently, when compiling information on accidents involving collisions between aircraft, the number of accident records will exceed the number of accidents. The Briefs of Accidents contain the essential information which fulfill most requirements of persons using these reports. However, for those having a need for more detailed information, the original factual reports are on file in the Washington Office of the National Transportation Safety Board. Upon request, these reports will be produced-commercially for a fee to cover reproduction and postage. The cost will be assessed per printed page and photograph(s) reproduced. Copies of material ordered will be mailed from the Washington business firm that holds the current contract for commercial reproduction of the Board's public files. Billing is also direct to you by the same company. -II- Orders for this material will also involve a user service charge by the Board for special services. Thfs charge is in addition to the cost of commercial reproduction of material and will be included in the bill from the commercial reproduction firm. Requests for reproduction should be forwarded to the: National Transportation Safety Board Public Inquiries Section, AD-46 800 Independence Avenue, S. W. Washington, D. C. 20594 -III- TABLE OF CONTENTS Page Foreword. . . . . . . . . . . . . . . . . . . I I Table of Contents.......... IV Exp 1anatory Notes.......... V AIRCRAFT ACCIDENTS File Order Listing......... IX Briefs of Accidents ........ 1-403 -IV- DEFINITIONS The following definitions contained in CFR 49, Part 830, Paragraph 830.2 apply when used in this publication. Aircraft Accidents An occurrence associated with the operation of an aircraft which takes p1ace between the ti me any person boards the aircraft with the intention of flight until such time as all such persons have disembarked, and in which any person suffers qeath or serious injury as a result of being in or upon the aircraft or by direct contact with the aircraft or anything attached thereto, or in which the aircraft receives substantial damage. Fatal Injury Any injury which results in death within 30 days of the accident. Serious Injury Any injury which 1) requires hospitalization for more than 48 hours, commencing within 7 days from the date the injury was received; 2) results in a fracture of any bone (except simple fractures of fingers, toes, or nose);

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involves lacerations which cause severe hemorrhages, nerve, muscle, or tendon damage; 4) ·involves injur.Y to any internal organ; or 5) involves second or third degree burns affecting more than 5 percent of the body surface. Substantial Damage 1) Except as provided in subparagraph (2) of this paragraph, substantial damage means damage or structural failure which adversely affects the structural strength, performance, or flight characteristics of the aircraft, and which would normally require major repair or replacement of the affected component. 2) Engine failure, damage limited to an engine, bent fairings or cowling, dented skin, small punctured holes in the skin or fabric, ground damage to rotor or propeller blades, damage to landing gear, wheels, tires, flaps, engine accessories, brakes, or wingtips are not considered "Substantial Damage" for the purpose of this part. OCCURRENCE Occurrence re 1ates to the immediate circumstance of the event. Occurrences are numbered in descending order and directly relate to the phase of operation. Some examples of occurrences are as follows: -V- Gear Collapsed Collapse of the landing gear due to mechanical failure other than malfunction of the retracting mechanism. TYPE OF OPERATING CERTIFICATE/TYPE OF OPERATION ---- ------ The type of operating certificate/type of operation refers to the purpose for which the aircraft is being operated at the time of the accident. This type of operating certificate is broken into two categories. These categories are: 1. GENERAL AVIATION This operating certificate refers to operations involving U.S. and foreign aircraft owned and operated by persons, businesses, corporat i ans, et cetera. This category also includes public use aircraft. To further define General Aviation operations we have classified the following: Personal Flying by individuals in there own or rented aircraft for pleasure, or persona 1 transportation not in furtherance of their occupation or company business. Business The use of aircraft by pilots (not rece1v1ng direct salary or compensation for piloting) in connection with their occupation or in the furtherance of a private business. Corporate/Executive Operations The use of aircraft owned or 1eased, and operated by a corporation or business firm for the transportation of personnel or cargo in furtherance of the corporation's or firm's business, and which are flown by professional pilots receiving a direct salary or compensation for piloting. Instructional Flyinq Refers to flyfng accomplished in supervised training under the direction of an accredited instructor. Other Flyi.!!.9_ Includes other kinds of flying not covered under the other broad categories. In some instances the criterion of direct financial return may or may not be present. -VI- 2. AIR CARRIER This operating certificate refers to all operations conducted for direct financial return except instructional flying. It includes Domestic/Flag Air Carriers, Supplemental Air Carriers, All Cargo Air Service Air Carriers, Commercial Operators, Air Travel Club, and Corporate (14 CFR 125) operations. Also included in this category are Commuter Air Carrier and On-Demand Air Taxi operations. Airframe/Component/System Failure/Malfunction Occurrences resulting from failure of any part of the airframe/component/system while in flight or in motion on the ground. Excludes failure resulting from contact with another airplane or object, or impact with the ground, or damage from landing gear collapse or retraction. Powerp l ant - ~ of Power Occurrences of engine failure or malfunction for any reason. Includes engine stoppage, power interruption, or power loss, actual or simulated. PHASE OF OPERATION The phase of operation relates to the particular segment of the flight or occurrences during which the circumstances of the accident occur. CAUSES AND RELATED FACTORS In determining probable cause(s) of an accident, all facts, conditions and circumstances are considered. The object is to ascertain these cause-effect rel at i onsh i ps in the ace i dent sequence about which something can be done to prevent recurrence of the type of accident under consideration. Accordingly, for statistical purposes where two or more causes exist in an accident, each is recorded and no attempt is made to establish a primary cause. The term factor is used to denote those elements of an accident which further explain or supplement the probable cause(s). Additional items that are not categorized as cause or factors are indicated as findings. These items are of interest in the investigation, however, they do not relate directly to the cause of the accident. -VII- BASIC WEATHER CONDITIONS The types of weather conditions (VMC /IMC) are determined in accordance with the prescribed minima in Part 91 of the Federal Aviation Regulations. These minima pertain to the ceiling and visibility, in conjunction with the type of airspace at the accident site. Type of weather conditions are based on surface weather as determined from officially recognized sources. Weather conditions encountered in flight are not necessarily representative of the classifications VMC/IMC as carried under Weather Data. -VIII- FILE ORDER LISTING ISSUE NUMBER 10 CALENDAR YEAR 1986 File Order Listing - Issue No. 10, 1986 File Aircraft Aircraft Injury Number Regist. Date Location Make Model Index Page ------- -------- 1801 920X 072286 FRANKLIN, LA GRUMMAN G-164A NONE 150 1802 3605P 121486 CHANDLER, AZ CESSNA P210N NONE 26 1803 5407 052186 BRANCH, LA GRUMMAN G-164A NONE 146 1804 35250 081586 VALLEY CITY, OH SENIOR AERO D-260 FATAL 268 1805 37800 120686 ROANOKE RAPIDS, NC SIKORSKY UH-19D NONE 214 1806 8239E 051086 WEBSTER, WI PIPER PA-28-181 NONE 388 1807 48102 051086 PLAINWELL, MI TAYLORCRAFT DC-65 NONE 180 1808 6647F 051286 GAYLORD, MI CESSNA 150F NONE 182 1809 8HD 061586 ST. ELMO, IL GLASFLUGEL CLUB LIBEL NONE 96 1810 53700 082986 GRAYSLAKE, IL CESSNA 172P NONE 100 1811 3757Z 092586 YANTLEY, AL CESSNA A-37A FATAL 14 1812 548YA 090186 MT OLIVE, AL JOE ALMON FALCON XP NONE 10 1813 222DU 072186 CHAPEL HILL, NC BELL 222UT MINOR 210 1814 306MA 102886 HILO, HI MURRAY AIR MA-1 NONE 82 1815 8670F 112586 NEWARK, DE HUGHES 369D NONE 56 1816 48925 100186 LUMBERTON, NJ CESSNA 152 FATAL 248 1817 8140V 060286 BLAINE, KS CESSNA A188 NONE 132 1818 778L 102986 SAN JUAN, PR DEHAVILLAND DHC-3 FATAL 302 1819 3026G 080586 WAGONER, OK FOURNEY F-1A NONE 280 1820 6151J 072386 STEINHATCHEE, FL PIPER PA-28-181 FATAL 58 1821 4563N 090186 SWEETWATER, TX BOEING E75 NONE 344 1822 8002J 110486 JACKSONVILLE, FL TED SMITH 601P MINOR 62 1823 3241W 110886 FT. LAUDERDALE, FL FELIX RASCH! GLASAIR NONE 66 1824 6915K 070586 VEGA BAJA, PR GRUMMAN G-164B FATAL 300 1825 3742Z 100886 RICHEY, MT PIPER J3C-65 SERIOUS 206 x F i1 e Order Listing - Issue No. 10, 1986 File Aircraft Aircraft Injury Number Regist. Date Location Make Model Index Page ------- -------- 1826 48331 091986 KERRVILLE, TX RYAN PT-22 MINOR 348 1826 NONE 091986 KERRVILLE, TX EAGLE PERFORMANC MINOR 350 1827 706M 093086 LAREDO, TX BEECH TC-45J NONE 352 1828 25532 120486 DURANT, OK CESSNA 152 MINOR 282 1829 44WR 090186 LAPORTE, TX BOEING A75N1 NONE 342 1830 7711J 082986 ADDISON, TX BOEING A75N1 NONE 340 1831 92BT 080886 SLIDELL, LA CESSNA A185F MINOR 152 1832 54759 092686 LIVE OAK, FL CESSNA 172P NONE 60 1833 714KY 122086 CRESSON, TX CESSNA 150M NONE 358 1834 5753L 072986 ROANOKE, TX AMERICAN AA-1 NONE 336 1835 50101 073186 BARTLESVILLE, OK CESSNA 150H MINOR 278 1836 8602G 070486 MARION, IN CESSNA 150F SERIOUS 116 1837 24RP 080386 DANVILLE, IL PATE QUICKIE MINOR 98 1838 73NS 092186 LACON, IL NORD STAMPE SV4 NONE 104 1839 28KD 111986 WAYLAND, MI DEVRIES SONERAI II SERIOUS 194 1840 43775 050486 ANADARKO, OK NORTH AMER IC SNJ-5 FATAL 272 1841 27785 051286 PINE SPRING, TX BELL 206B FATAL 330 1842 1356J 050186 EL PASO, TX ROCKWELL 112A SERIOUS 328 1843 4431B 032886 MCKINNEY, TX CESSNA L-19E SERIOUS 320 1843 66D 032886 MCKINNEY, TX SPENCER PITTS S-1 SERIOUS 322 1844 2161B 112986 STUGIS, SD PIPER PA-28-181 FATAL 312 1845 4350K 091086 FREDERICKSBURG, VA PIPER PA-28-181 MINOR 370 1846 55297 080486 ALBUQUERQUE, NM CESSNA 172P NONE 254 1847 5324 080586 CENTER, co GRUMMAN G-164A NONE 42 1848 7681P 080786 ALBUQUERQUE, NM PIPER PA-24-250 NONE 256 XI File Order Listing - Issue No. 10, 1986 File Aircraft Aircraft Injury Number Regist. Date Location Make Model Index Page ------- -------- 1849 1387V 080786 TOOELE, UT BOEING E75 NONE 364 1850 8272Y 073086 MONUMENT VALLEY, UT PIPER PA-28-181 NONE 362 1851 89208 090586 FESTUS, MO CESSNA 140 SERIOUS 200 1852 45986 090386 ONAWA, IA CESSNA 152 MINOR 84 1853 1810S 091686 HORTON, KS BEECH A36 NONE 136 1854 90BK 090686 WICHITA, KS CESSNA P337 NONE 134 1855 1BL 090186 HOLLY, MI LAWRENCE BABY GREAT FATAL 190 1856 4463L 101986 LANSING, MI LEBLANC DRAGONFLY NONE 192 1857 371DT 110986 CRAWFORDSVILLE, IN TURNBLOOM KIT FOX NONE 122 1858 2433 112286 ELWOOD, IN ROHDECAP/THO T-18 MINOR 128 1859 123AE 041186 KENOSHA, WI STEINORTH EXTRA LONG MINOR 384 1860 23DA 042086 WISCONSIN RAPID, WI DAY SKYBOLT DB NONE 386 1861 4072U 072086 MUSKEGON, MI CESSNA 150E SERIOUS 186 1862 4702Y 050286 HAGERSTOWN, IN CONNER KR-2 MINOR 114 1863 6860G 120786 CULLOWHE.E, NC CESSNA 150L MINOR 216 1864 58188 121086 CHARLOTTE, NC HUGHES 269C NONE 218 1865 549H 090186 COSHOCTON, OH ENSTROM F-28C NONE 270 1866 3328F 062886 HARTFORD, AR CESSNA 182J FATAL 20 1867 60PB 042786 RIDGEFIELD PARK, NJ ENSTROM F-28C NONE 238 1868 4067U 062986 HAMMONDSPORT, NY CESSNA 150E NONE 260 1869 80282 092086 ARKANSAS CITY, KS CESSNA 172M NONE 138 1870 711WW 110586 ORLANDO, FL GRUMMAN G-164A FATAL 64 1871 64430 092886 LEESBURG, VA MOONEY M20F FATAL 374 1872 251CC 092386 GALAX, VA BELL 222UT FATAL 372 1873 369B 081086 NORWOOD, MA HUGHES 369HS NONE 170 XII File Order Listing - Issue No. 10, 1986 File Aircraft Aircraft Injury Number Regist. Date Location Make Model Index Page ------- -------- 1874 5629K 032286 LACONIA, NH BEECH 535 MINOR 230 1875 59400 072086 PORTLAND, CT BELL 47G-5A NONE 54 1876 55149 062986 ENDICOTT, NY PIPER PA-28-140 NONE 262 1877 91356 080586 GROVE CITY, PA PIPER PA-38-112 NONE 298 1878 757JC 062886 OXFORD, MA CESSNA 152 NONE 164 1879 7040V 072186 WEST MILFORD, NJ MOONEY M20F MINOR 246 1880 43010 071586 WESTERLY, RI CESSNA 172L SERIOUS 310 1881 5533J 070386 BLOCK ISLAND, RI PIPER PA-32 MINOR 308 1882 54946 071486 KINGSTON, NY CESSNA 172 MINOR 264 1883 9909L 081586 MOULTONBORO, NH GRUMMAN AA-18 NONE 234 1884 44DN 041486 NEWTON, NJ CESSNA 150J MINOR 236 1885 6264W 041486 HAMPDEN, ME PIPER PA-28-140 NONE 176 1886 3539E 083186 CLEAR, AK CESSNA 1808 NONE 4 1887 11864 061686 SETTLERS BAY, AK CHAMPION 7ECA SERIOUS 2 1888 2805F 080986 FORT COLLINS, co RAVEN AERO STAR NONE 44 1889 93454 080486 HARRISBURG, PA CESSNA 152 NONE 296 1890 65612 071886 PLAINVILLE, CT CESSNA 172P NONE 52 1891 2428P 070186 LINCOLN, RI PIPER PA-38-112 NONE 306 1892 5186X 070186 LAKEWOOD, NJ CHAMPION 7GCAA NONE 244 1893 33985 072286 PLYMOUTH, MA SCHWEIZER SGS-2-33A NONE 168 1894 396X 072886 WOLFEBORO, NH MAULE M-5-235 NONE 232 1895 8299N 063086 WELLSBORO, PA PIPER PA-28-140 NONE 290 1896 1RJ 072386 TUNKHANNOCK, PA BEECH A24R NONE 292 1897 130LJ 120586 MIAMI, FL CESSNA T210L MINOR 72 1898 36250 062886 MARSTONS MILLS, MA BEECH A23-19 NONE 166 XIII File Order Listing - Issue No. 10, 1986 Fi 1 e Aircraft Aircraft Injury Number Regist. Date Location Make Model Index Page ------- -------- 1899 8389C 122786 HIGH POINT, NC PIPER PA-28-181 NONE 222 1900 32106 112786 WAYNESBORO, GA PIPER PA-28-140 MINOR 80 1901 44501 091686 F9RISTELL, MO PIPER PA28-151 FATAL 202 1902 1140S 050486 MT. GRAY LOCK, MA SCHWEIZER SGS 1-26 SERIOUS 160 1903 2311 R 111686 LANSING, IL PIPER PA-28-180 MINOR 110 1904 1457A 111686 ROCKFORD, IL PIPER PA-22 MINOR 112 1905 3871L 112186 EVANSVILLE, IN CESSNA 172G MINOR 126 1906 41765 120686 MARQUETTE, MI PIPER PA28-151 NONE 196 1907 340CB 070486 HAMBURG, MI CAMERON BALL 77 SERIOUS 184 1908 3436T 102286 WAUKESHA, WI CESSNA 177 NONE 398 1909 6184A 061386 BRECKENRIDGE, MN PIPER PA-36-375 NONE 198 1910 6517R 073086 MANCHESTER, MI BEECHCRAFT B-19 NONE 188 1911 9427F 092686 BALDWIN, WI HUGHES 269B NONE 396 1912 2896N 102286 DECATUR, IL CESSNA 120 NONE 106 1913 6997Q 102186 LAKE VILLAGE, IN BEECHCRAFT BE-23 NONE 118 1914 38688 100386 HOLYOKE, MA PIPER PA-28-140 FATAL 172 1915 55MM 050386 LONG BEACH, CA CESSNA P210N SERIOUS 28 1916 6877 092086 TULLAHOMA, TN ALEXANDER AS-K13 NONE 314 1917 9517M 081486 QUINCEY, WA MOONEY M20 NONE 376 1918 3HW 072086 BIG CREEK, ID WEISS-HAYNES STITS SA6B FATAL 86 1919 4156X 083186 PRIEST RIVER, ID AERO COMMAND 100 NONE 92 1921 1RC 082286 SOLDIER BAR AIR, ID CESSNA A185E NONE 90 1922 9940Y 082086 STANLEY, ID AERONCA 7GCB FATAL 88 1923 66BW 090186 KENT, WA BEECH A24R MINOR 380 1924 18079 090286 KENT, WA CESSNA 150L NONE 382 XIV File Order Listing - Issue No_ 10, 1986 File Aircraft Aircraft Injury Number Regist_ Date Location Make Model Index Page ------- -------- 1925 6401L 090486 CHINOOK, MT GRUMMAN AA-1A MINOR 204 1926 150SG 091286 CHRISTIAN LAKE, AK PIPER PA-18 FATAL 6 1927 5713P 080286 OSHKOSH, WI PIPER PA-24-250 SERIOUS 394 1928 8112T 110286 LAFAYETTE, IN PIPER PA-28-181 NONE 120 1929 3667X 071686 CRIVITZ, WI AERO COMMAND 100 FATAL 392 1930 1835W 060486 MARIETTA, OK BEECH A36TC FATAL 276 1931 1634G 092486 HURRICANE, UT CHAMPION 7ECA NONE 366 1932 6337U 061486 LAMAR, co BEECH C23 SERIOUS 36 1933 3694D 092986 BOULDER, co BEECH 60 NONE 48 1934 90622 022086 AUSTIN, TX ROBINSON R-22 NONE 318 1935 4608V 052586 BRIDGEPORT, NJ CESSNA 172RG SERIOUS 242 1936 161JD 040886 CHENEY, KS GLASAIR 2 FATAL 130 1937 736XP 121486 EL RENO, OK CESSNA 172K FATAL 284 1938 24902 051786 TEMECULA, CA GENERAL BALL AX-6 FATAL 30 1939 5220M 062086 SHIOCTON, WI CESSNA 152 NONE 390 1940 49220 122886 FT.POLK, LA CESSNA A-188-B NONE 158 1941 201PJ 081886 AURORA, OR MOONEY M-20-J MINOR 286 1942 394SK 082386 ROCHE HARBOR, WA GLASAIR SH2 FATAL 378 1943 80004 052486 SANTA FE, TX AEROTEK PITTS S2A FATAL 332 1944 34397 053186 KRUM, TX MEYERS 200B FATAL 334 1945 9051H 102686 RICHARDTON, ND CESSNA 172M SERIOUS 226 1946 6728J 051686 LARAMIE, WY BEECH BE-99C NONE 400 1947 40443 062786 BUFFALO, WY MARTIN 404 FATAL 402 1948 5260F 102086 NASHVILLE, TN PIPER PA-32R-300 FATAL 316 1950 23DK 110286 MACON, GA KOONS-DONALD SONERAI II FATAL 78 xv File Order Listing - Issue No. 10, 1986 Fi le Aircraft Aircraft Injury Number Regist. Date Location Make Model Index Page ------- -------- 1951 71966 121286 MORGANTON, NC LUSCOMBE BA NONE 220 1952 711TJ 110186 LAKE TAHOE, CA LEAR JET 24 NONE 34 1953 44767 062686 MAMMOTH SPRING, AR PIPER PA-28R-200 NONE 18 1954 6041Y 092086 MONTGOMERY, AL PIPER PA-23-250 NONE 12 1955 67490 061886 JONESBORO, AR CESSNA 15211 NONE 16 1956 20TS 080486 UVALDE, TX SCHLEICHER ASW-20 SERIOUS 338 1957 7975M 121086 IVEL, KY BEECH C-55 FATAL 144 1958 91548 112886 SPRINGTOWN, TX NORTH AMER IC NAVION A FATAL 354 1959 2389B 050486 MARSHFIELD, MA PIPER PA-38 MINOR 162 1960 2945Y 112686 CHIEFLAND, FL CESSNA 182E NONE 68 1961 1FD 120186 PANAMA CITY, FL CESSNA 320 SERIOUS 70 1962 47042 111086 GOSHEN, UT BELL 47G-3B-1 NONE 368 1963 76541 072586 TAOS, NM CESSNA 140, SERIOUS 252 1964 6DW 062186 SILVER CITY, NM CESSNA A150K FATAL 250 1965 6829H 040686 SENECA, IL CESSNA 172M SERIOUS 94 1966 578PA 111086 SOUTH BEND, IN PIPER PA-28R-200 MINOR 124 1967 3289U 111586 SANDWICH, IL CESSNA 182F SERIOUS 108 1968 71650 091786 QUINCY, IL CESSNA 182M MINOR 102 1969 4211T 032286 SPRINGVALE, ME PIPER PA-28-140 NONE 174 1970 95310 080386 LANCASTER, PA PIPER PA-60-601P NONE 294 1971 1030V 050886 NEWBURG, PA CESSNA T337HPII MINOR 288 1972 5068F 090686 ABILENE, TX HILLER FH-1100 NONE 346 1973 4346L 072686 BOULDER, co PIPER PA-46-310P FATAL 38 1973 5113S 072686 BOULDER, co CESSNA TR-182 FATAL 40 1974 9109D 091386 UNKNOWN, AK PIPER PA-18 FATAL 8 XVI F i1 e Order Listing - Issue No. 10, 1986 File Aircraft Aircraft Injury Number Regist_ Date Location Make Model Index Page ------- -------- 1975 16GB 122086 EL PASO. TX BEGGS PITTS S-1 FATAL 360 1976 32190 110686 HENDERSON, NV CESSNA 401 FATAL 258 1977 22943 100586 FORT SCOTT, KS CESSNA 150 FATAL 140 1978 33808 101886 JAMESTOWN, NY PIPER PA-28-235 FATAL 266 1979 8340F 081086 DOUGLASVILLE, GA PIPER PA-28-161 MINOR 76 1980 9444Y 060386 SPERRY, OK CESSNA T210N FATAL 274 1981 2784E 061386 HOUMA, LA MB 105 FATAL 148 1982 8696H 041586 HANKAMER, TX GRUMMAN G164A FATAL 324 1982 8751H 041586 HANKAMER, TX GRUMMAN G164A FATAL 326 1983 8271P 102286 CROSBY, ND PIPER PA-24-250 FATAL 224 1984 1373P 050486 WARREN, MI PIPER PA-23-150 FATAL 178 1985 7087D 120686 HAVRE, MT PIPER PA-18-150 SERIOUS 208 1986 26DL 121186 OLATHE, KS CESSNA 180 NONE 142 1987 414NY 051786 ATLANTIC CITY, NJ CESSNA 414A FATAL 240 1989 9665F 111986 EDEN, NC HUGHES 269C NONE 212 1990 5980P 100586 SEWARD, NE PIPER PA-24-250 NONE 228 1991 888MD 112586 ISABELA, PR PIPER PA-34-200T FATAL 304 1992 3371V 081586 SUN CITY WEST, AZ BEECH 35R SERIOUS 24 1993 34180 080386 MARANA, AZ SCHWEIZER SGS-1-35 NONE 22 1994 757QR 080486 APPLE VALLEY, CA CESSNA 152 MINOR 32 1995 5211G 120986 MASON, TX CESSNA 305A NONE 356 1996 1SN 121686 VERO BEACH, FL CESSNA 336 NONE 74 1997 2710L 091586 MER ROUGE, LA WSK-PZL-MIEL PZL-M18 FATAL 156 1998 38092 090386 PORT ALLEN, LA TEXAS OH-13E/M74 NONE 154 1999 1691V 091686 BENNETT, co CESSNA 172M FATAL 46 XVII File Aircraft Number Regist. 2000 3MU Date 101286 File Order Listing - Issue No. 10, 1986 Location DENVER, CO XVIII Make Aircraft Model MITSUBISHI MU-28-20 Injury Index NONE Page 50 AIRCRAFT ACCIDENT REPORTS BRIEF FORMAT U.S. CIVIL AND FOREIGN AVIATION ISSUE NUMBER 10 OF 1986 ACCIDENTS National Transportation Safety Board Washington, D.C. 20594 Brief of Accident File No. - 1887 6/16/86 SETTLERS BAY.AK A/C Reg. No. N11864 Time (Lcl) - 1521 ADT ----Basic Information---- Type Operating Certificate-NONE (GENERAL AVIATION) Type of Operation Flight Conducted Under Accident Occurred During ----Aircraft Information---- - INSTRUCTIONAL -14 CFR 91 -APPROACH Aircraft Damage SUBSTANTIAL Fire NONE Crew Pass Fatal 0 0 Injuries Serious Minor 2 0 0 0 None 0 0 Make/Model - CHAMPION 7ECA Landing Gear - TAILWHEEL-ALL FIXED Eng Make/Model - LYCOMING 0-235-C1 Number Engines - 1 ELT Installed/Activated - YES/YES Stall Warning System - YES Max Gross Wt 1650 No. of Seats 2 ----Environment/Operations Information---- Weather Data Wx Briefing - NO RECORD OF BRIEFING Method - N/A Completeness - N/A Basic Weather - VMC Wind Dir/Speed- 300/010 KTS Visibility 30.0 SM Lowest Sky/Clouds UNK/NR Lowest Ceiling 9000 FT BROKEN Obstructions to Vision- NONE Precipitation - NONE Condition of Light - DAYLIGHT ----Personnel Information---- Engine Type - RECIPROCATING-CARBURETOR Rated Power 115 HP Itinerary Last Departure Point WASILLA.AK Destination ANCHORAGE.AK ATC/Airspace Type of Flight Plan - NONE Type of Clearance - NONE Type Apch/Lndg - FULL STOP SIMULATED Airport Proximity ON AIRSTRIP Airport Data SETTLERS BAY Runway !dent Runway Lth/Wid Runway Surface Runway Status FORCED LANDING - 02 2200/ - GRAVEL - DRY 50 Pi lot-In-Command Certificate(s)/Rating(s) PRIVATE Age - 31 Medical Certificate - VALID MEDICAL-WAIVERS/LIMIT Biennial Flight Review Flight Time (Hours) Current - UNK/NR Total 93 Last 24 Hrs - SE LAND Months Since - UNK/NR Make/Model- UNK/NR Last 30 Days- Aircraft Type - UNK/NR Instrument- 3 Last 90 Days- Instrument Rating(s) - NONE ----Narrative---- THE INSTRUCTOR (CFI) GAVE THE FRONT SEAT PLT A SIMULATED FORCED LNDG WHILE THE AIRPLANE WAS ALIGNED WITH RWY 20 & THE WIND. THE FRONT SEAT PLT ELECTED TO FLY A TRAFFIC PATTERN TO RWY 2. AS THE FRONT SEAT PLT MANEUVERED TO LINE UP WITH RWY 2, MUCH ALT WAS LOST & THE FINAL APCH WAS ABOUT 30 DEG OFF THE RWY HEADING. THE CFI APPLIED POWER FOR A GO- AROUND, BUT WAS TOO LATE TO AVOID HITTING TREE TOPS & THE GND NEAR THE RGT SIDE OF THE RWY. THE FRONT SEAT OCCUPANT WAS A RATED SINGLE-ENG PLT & WAS CONSIDERED THE PLT-IN-COMMAND ON THIS FLT. PAGE 2 UNK/NR UNK/NR UNK/NR Brief of Accident (Continued) Fi 1 e No. - 1887 Occurrence #1 Phase of Operation Finding(s) 6/16/86 SETTLERS BAY.AK IN FLIGHT COLLISION WITH OBJECT APPROACH - VFR PATTERN - FINAL APPROACH 1. PLANNED APPROACH - POOR - DUAL STUDENT 2. SUPERVISION - INADEQUATE - OTHER CREW MEMBER 3. GO-AROUND - DELAYED - 4. OBJECT - TREE(S) 5. PROPER ALTITUDE - NOT MAINTAINED - Occurrence #2 Phase of Operation ----Probable Cause---- IN FLIGHT COLLISION WITH TERRAIN APPROACH - VFR PATTERN - FINAL APPROACH A/C Reg. No_ N11864 The National Transportation Safety Board determines that the Probable Cause(s) of this accident is/are f inding(s) 2,3,5 Factor(s) relating to this accident is/are finding(s) 1.4 PAGE 3 Time (Lcl) - 1521 ADT National Transportation Safety Board Washington, D.C. 20594 Brief of Accident F i 1 e No. - 1886 8/31/86 CLEAR.AK A/C Reg. No. N3539E Time (Lcl) - 2120 ADT ----Basic Information---- Type Operating Certificate-NONE (GENERAL AVIATION) Type of Operation -PERSONAL Flight Conducted Under -14 CFR 91 Accident Occurred During -LANDING ----Aircraft lnformation---- Aircraft Damage SUBSTANTIAL Fire NONE Crew Pass Fatal 0 0 Injuries Serious Minor 0 0 0 0 None 1 1 Make/Model - CESSNA 180B Landing Gear - TAILWHEEL-ALL FIXED Eng Make/Model - CONTINENTAL 0-470-K Number Engines - 1 ELT Installed/Activated - YES/NO Stall Warning System - YES Max Gross Wt 2650 Engine Type - RECIPROCATING-CARBURETOR No. of Seats 4 ----Environment/Operations Information---- Weather Data Wx Briefing - NO RECORD OF BRIEFING Method - N/A Completeness - N/A Basic Weather - VMC Wind Dir/Speed- CALM Visibility 60.0 SM Rated Power 230 HP Itinerary Last Departure Point FAIRBANKS.AK Destination SAME AS ACC/INC ATC/Airspace Lowest Sky/Clouds 10000 Lowest Ceiling - NONE FT SCATTERED Type of Flight Plan - NONE Type of Clearance - NONE Obstructions to Vision- NONE Precipitation - NONE Condition of Light - DUSK ----Personnel Information---- Pi lot-In-Command Type Apch/Lndg - UNK/NR Age - 40 Medical Biennial Flight Review Airport Proximity OFF AIRPORT/STRIP Airport Data Certificate Flight - Runway !dent Runway Lth/Wid Runway Surface Runway Status EXPIRED Time (Hours) - N/A - N/A - N/A - DRY Certif icate(s)/Rating(s) COMMERCIAL Current - UNK/NR Total 1400 Last 24 Hrs - SE LAND,ME LAND.SE SEA Months Since - UNK/NR Make/Model- 600 Last 30 Days- Aircraft Type - UNK/NR Instrument- UNK/NR Last 90 Days- Multi-Eng - 20 Rotorcraft Instrument Rating(s) - NONE ----Narrative---- THE PLT & PASSENGER WERE ON A HUNTING TRIP & HAD SELECTED A CLEARING ON A BRUSH COVERED HILLSIDE FOR A LANDING. THE CLEARING HAD BEEN PREVIOUSLY USED AS AN AIRSTRIP. WHILE ON FINAL APCH TO LAND AT DUSK, THE PLT LOST SIGHT OF THE TOUCHDOWN AREA DUE TO DARKNESS & SHADOWS. DURING THE LANDING, HE OVERRAN THE LANDING ZONE. THE LEFT MAIN GEAR THEN ENCOUNTERED UNEVEN TERRAIN & COLLAPSED. PAGE 4 - 2 UNK/NR 28 UNK/NR Brief of Accident (Continued) File No. - 1886 Occurrence #1 Phase of Operation Finding(s) OVERRUN LANDING 8/31/86 CLEAR.AK 1. IN-FLIGHT PLANNING/DECISION - IMPROPER - PILOT IN COMMAND 2. LIGHT CONDITION - DUSK 3. PROPER TOUCHDOWN POINT - NOT ATTAINED - PILOT IN COMMAND A/C Reg. No. N3539E 4. IMPROPER DECISION,VISUAL/AURAL PERCEPTION - PILOT IN COMMAND 5. IMPROPER DECISION,OVER CONFIDENCE IN PERSONAL ABILITY - PILOT IN COMMAND Occurrence #2 Phase of Operation Finding(s) MAIN GEAR COLLAPSED LANDING 6. TERRAIN CONDITION - ROUGH/UNEVEN 7. LANDING GEAR.MAIN GEAR - OVERLOAD ----Probable Cause---- The National Transportation Safety Board determines that the Probable Cause(s) of this accident is/are finding(s) 1,3 Factor(s) relating to this accident is/are finding(s) 2,4,5,6 PAGE 5 Time (Lcl) - 2120 ADT National Transportation Safety Board Washington. D.C. 20594 Brief of Accident File No. - 1926 9/12/86 CHRISTIAN LAKE.AK A/C Reg. No. N150SG Time (Lcl) - 1545 ADT ----Basic Information---- Type Operating Certificate-NONE (GENERAL AVIATION) Aircraft Damage DESTROYED Injuries Type of Operation Flight Conducted Under Accident Occurred During ----Aircraft Information---- -PERSONAL -14 CFR 91 -DESCENT Make/Model - PIPER PA-18 Landing Gear - FLOAT Max Gross Wt 1760 No. of Seats 2 ----Environment/Operations Information---- Weather Data Wx Briefing - NO RECORD OF BRIEFING Method - N/A Completeness - N/A Basic Weather - VMC Wind Dir/Speed- 180/005 KTS Visibility 15.0 SM Lowest Sky/Clouds CLEAR Lowest Ceiling - NONE Obstructions to Vision- NONE Precipitation - NONE Condition of Light - DAYLIGHT ----Personnel Information---- Pi lot-In-Command Certif icate(s)/Rating(s) PRIVATE SE LAND.SE SEA Instrument Rating(s) - NONE --~-Narrative---- Age Fire ON GROUND Crew Pass Eng Make/Model - LYCOMING 0-320-A2A Number Engines - 1 Fatal 1 0 Serious Minor 0 0 0 None 0 0 ELT Installed/Activated - YES-UNK/NR Stall Warning System - NO Engine Type - RECIPROCATING-CARBURETOR Rated Power 150 HP Itinerary Last Departure Point SAME AS ACC/INC Destination KENAI.AK ATC/Airspace - Type of Flight Plan - NONE Type of Clearance - NONE Type Apch/Lndg - NONE 29 Medical Airport Proximity OFF AIRPORT/STRIP Airport Data Certificate - Runway !dent Runway Lth/Wid Runway Surface Runway Status - N/A - N/A - WATER - WATER-CALM VALID MEDICAL-NO WAIVERS/LIMIT Biennial Flight Review Flight Time (Hours) Current - UNK/NR Total 257 Last 24 Hrs - UNK/NR Months Since - UNK/NR Make/Model- UNK/NR Last 30 Days- UNK/NR Aircraft Type - UNK/NR Instrument- UNK/NR Last 90 Days- UNK/NR Multi-Eng - UNK/NR Rotorcraft - UNK/NR THE PILOT-IN-COMMAND OF THE FLOAT EQUIPPED AIRPLANE, OVERLOADED THE AIRPLANE BEYOND THE AFT LIMIT OF THE CENTER OF GRAVITY RANGE. HE TOOK OFF WITHOUT FLAPS AND ATTEMPTED TO TURN AWAY FROM RISING TERRAIN. THE AIRPLANE STALLED AND CRASHED. PAGE 6 Brief of Accident (Continued) F i le No. - 1926 Occurrence #1 Phase of Operation Finding(s) 9/12/86 CHRISTIAN LAKE.AK LOSS OF CONTROL - IN FLIGHT TAKEOFF - INITIAL CLIMB 1. FLIGHT CONTROL.FLAP - NOT ENGAGED A/C Reg. No. N150SG 2. PREFLIGHT PLANNING/PREPARATION - INADEQUATE - PILOT IN COMMAND 3. FUSELAGE.CARGO COMPARTMENT - OVERLOAD 4. PERFORMANCE DATA - DISREGARDED - PILOT IN COMMAND 5. AIRCRAFT WEIGHT AND BALANCE - IMPROPER - PILOT IN COMMAND Occurrence #2 Phase of Operation ----Probable Cause---- IN FLIGHT COLLISION WITH TERRAIN DESCENT - UNCONTROLLED The National Transportation Safety Board determines that the Probable Cause(s) of this accident is/are f inding(s) 5 Factor(s) relating to this accident is/are finding(s) 1,2,3,4 PAGE 7 Time (Lcl) - 1545 ADT F i l e No . - 19 7 4 9/13/86 ----Basic Information---- National Transportation Safety Board Washington, D.C. 20594 Brief of Accident UNKNOWN.AK A/C Reg. No. N9109D Type Operating Certificate-NONE (GE~ERAL AVIATION) Aircraft Damage DESTROYED Type of Operation Flight Conducted Under Accident Occurred During ----Aircraft Information---- -HUNTING Fire -14 CFR 91 UNK/NR -UNKNOWN Crew Pass Fatal 1 1 Time (Lcl) - UNK/NR Injuries Serious Minor 0 0 0 0 None 0 0 Make/Model - PIPER PA-18 Landing Gear - TAILWHEEL-ALL FIXED Eng Make/Model - LYCOMING 0-320 Number Engines - 1 ELT Installed/Activated - YES-UNK/NR Stall Warning System - NO Max Gross Wt 1750 No. of Seats 2 ----Environment/Operations Information---- Weather Data Wx Briefing - UNK/NR Method - UNK/NR Completeness - UNK/NR Basic Weather - UNK/NR Wind Dir/Speed- UNK/NR Visibility - UNK/NR Lowest Sky/Clouds UNK/NR Lowest Ceiling - UNK/NR Obstructions to Vision- UNK/NR Precipitation - UNK/NR Condition of Light - DUSK ----Personnel Information---- Pi lot-In-Command Certificate(s)/Rating(s) PRIVATE SE LAND Instrument Rating(s) - NONE ----Narrative---- Age Engine Type - RECIPROCATING-CARBURETOR Rated Power 150 HP Itinerary Last Departure Point ANCHORAGE.AK Destination ALASKA MOUNTAIN.AK ATC/Airspace - Type of Flight Plan - NONE Type of Clearance - NONE Type Apch/Lndg - UNK/NR 46 Medical Airport Proximity OFF AIRPORT/STRIP Airport Data Certificate - Runway !dent Runway Lth/Wid Runway Surf ace Runway Status NO MEDICAL - N/A - N/A - N/A - N/A Biennial Flight Review Flight Time (Hours) Current - UNK/NR Total 1200 Last 24 Hrs - Months Since - UNK/NR Make/Model- UNK/NR Last 30 Days- Aircraft Type - UNK/NR Instrument- 0 Last 90 Days- THE PRIVATE PILOT OPERATING FOR HIRE DEPARTED ANCHORAGE AND FLEW INTO AN AREA OF FORECASTED DETERIORATING WEATHER CONDITIONS. THE AIRPLANE HAS NOT BEEN LOCATED. AIRCRAFT DAMAGE AND INJURIES ARE PRESUMED. PAGE 8 UNK/NR UNK/NR UNK/NR Brief of Accident (Continued) File No. - 1974 Occurrence Phase of Operation Finding(s) 9/13/86 MISSING AIRCRAFT UNKNOWN UNKNOWN,AK 1. PLANNING-DECISION - INADEQUATE - PILOT IN COMMAND 2. TERRAIN CONDITION - MOUNTAINOUS/HILLY 3. WEATHER CONDITION - LOW CEILING 4. JUDGEMENT - POOR - PILOT IN COMMAND 5. UNDETERMINED ----Probable Cause---- A/C Reg. No. N9109D The National Transportation Safety Board determines that the Probable Cause(s) of this accident is/are finding(s) 5 Factor(s) relating to this accident is/are finding(s) 1,2,3,4 PAGE 9 Time (Lcl) - UNK/NR National Transportation Safety Board Washington, D.C. 20594 Brief of Accident F i l e No . - 18 1 2 9/01/86 MT OLIVE, AL A/C Reg. No. N548YA Ti me (Le l ) - 1730 CDT ----Basic Information---- Type Operating Certificate-NONE (GENERAL AVIATION) Type of Operation -PERSONAL Flight Conducted Under -14 CFR 91 Accident Occurred During -OTHER ----Aircraft Information---- Aircraft Damage SUBSTANTIAL Fire NONE Crew Pass Fatal 0 0 Injuries Serious Minor 0 0 0 0 None 1 0 Make/Model - JOE ALMON FALCON XP Landing Gear - UNK/NR Eng Make/Model - ROTEX 503 Number Engines - 1 ELT Installed/Activated - NO -N/A Stall Warning System - NO Max Gross Wt - UNK/NR No. of Seats 2 ----Environment/Operations Information---- Weather Data Wx Briefing - NO RECORD OF BRIEF ING Method - N/A Completeness - N/A Basic Weather - VMC Wind Dir/Speed- 130/005 Visibility 7.0 Engine Type - RECIPROCATING-CARBURETOR Rated Power 50 HP Itinerary Last Departure Point SAME AS ACC/INC Destination LOCAL ATC/Airspace Airport Proximity OFF AIRPORT/STRIP Airport Data PRIVATE - 18 2000 Lowest Sky/Clouds KTS SM 1900 1900 FT Type of Flight Plan - NONE Type of Clearance - NONE Runway !dent Runway Lth/Wid Runway Surface Runway Status - GRASS/TURF Lowest Ceiling Obstructions to Vision- NONE - NONE FT BROKEN Precipitation Condition of Light - DAYLIGHT - DRY Type Apch/Lndg - STRAIGHT-IN ----Personnel Information---- Pi lot-In-Command Age - 31 Medical Certificate - VALID MEDICAL-NO WAIVERS/LI MIT Certif icate(s)/Rating(s) PRIVATE SE LAND Instrument Rating(s) - NONE ----Narrative---- Biennial Flight Review Current - YES Months Since - 12 Aircraft Type - C-172 Flight Time (Hours) Total 125 Last 24 Hrs - Make/Model- 3 Last 30 Days- Instrument- UNK/NR Last 90 Days- Multi-Eng - UNK/NR Rotorcraft - WHILE APCHG TO LAND, THE REGISTERED ULTRALIGHT ACFT ENCOUNTERED A DOWNDRAFT WHICH EXCEEDED ITS CLIMB PERFORMANCE. THE ACFT WAS HEADED TWO POWER LINES, SO THE PLT ELECTED TO FLY UNDER THE LINES. AS THE ULTRALIGHT WAS CROSSING UNDER THE POWER LINES, ONE OF ITS VERTICAL FINS HIT THE BOTTOM CABLE WHICH DISABLED THE ACFT'S LEFT RUDDER CONTROL. THE ACFT TURNED TO THE RGT TWO A HILL & WOULD NOT CLIMB SUFFICIENTLY TO CLEAR OVER TREES. THE PLT INTENTIONALLY ALLOWED THE ACFT TO MUSH INTO THE TREES WHILE HE STILL HAD CONTROL. PAGE 10 2 UNK/NR 3 UNK/NR Brief of Accident (Continued) F i l e No . - 18 1 2 Occurrence #1 Phase of Operation Finding(s) 9/01/86 MT OLIVE, AL IN FLIGHT ENCOUNTER WITH WEATHER APPROACH - VFR PATTERN - FINAL APPROACH 1. WEATHER CONDITION - DOWNDRAFT Occurrence #2 Phase of Operation Finding(s) IN FLIGHT COLLISION WITH OBJECT APPROACH 2. OBJECT - WIRE,TRANSMISSION(MARKED) 3. CLEARANCE - MISJUDGED - PILOT IN COMMAND 4. VERTICAL STABILIZER ATTACHMENT - SEPARATION FORCED LANDING A/C Reg. No. N548YA Occurrence #3 Phase of Operation MANEUVERING - TURN TO LANDING AREA (EMERGENCY) Finding(s) 5. FLIGHT CONTROL.RUDDER - MOVEMENT RESTRICTED 6. DIRECTIONAL CONTROL - REDUCED - 7. CLIMB - NOT POSSIBLE - Occurrence #4 Phase of Operation Finding(s) 8. OBJECT - TREE(S) 9. STALL/MUSH ----Probable Cause---- IN FLIGHT COLLISION WITH OBJECT OTHER The National Transportation Safety Board determines tha~ the Probable Cause(s) of this accident is/are finding(s) 3 Factor(s) relating to this accident is/are finding(s) 1,2,8 PAGE 11 Time (Lcl) - 1730 CDT National Transportation Safety Board · , Washington, D.C. 20594 Brief of Accident Fi le No. - 1954 9/20/86 MONTGOMERY.AL A/C Reg. No. N6041Y Time (Lcl) - 1022 CDT ----Basic Information---- Type Operating Certificate-NONE (GENERAL AVIATION) Type of Operation Flight Conducted Under Accident Occurred During ----Aircraft Information---- -OTHER WORK USE -14 CFR 91 -LANDING Aircraft Damage SUBSTANTIAL Fire NONE Crew Pass Fatal 0 0 Injuries Serious Minor 0 0 0 0 None 2 0 Make/Model - PIPER PA-23-250 Landing Gear - TRICYCLE-RETRACTABLE Eng Make/Model - LYCOMING I0-540-C4B5 Number Engines - 2 ELT Installed/Activated - YES/NO Stall Warning System - YES Max Gross Wt 5200 No. of Seats 2 ----Environment/Operations Information---- Weather Data Wx Briefing - NO RECORD OF BRIEFING Method - N/A Completeness - N/A Basic Weather - VMC Wind Dir/Speed- 120/003 KTS Visibility 6.0 SM Engine Type - RECIP-FUEL INJECTED Rated Power 250 HP Itinerary Last Departure Point MONTGOMERY.AL Destination GREENSBORO.NC ATC/Airspace Airport Proximity OFF AIRPORT/STRIP Airport Data - N/A - N/A Lowest Sky/Clouds 15000 FT SCATTERED Type of Flight Plan - NONE FT BROKEN Type of Clearance - NONE Runway !dent Runway Lth/Wid Runway Surf ace Runway Status - CONCRETE Lowest Ceiling - 25000 Obstructions to Vision- NONE Type Apch/Lndg - NONE - DRY Precipitation - NONE Condition of Light - DAYLIGHT ----Personnel Information---- Pi lot-In-Command Age - 50 Medical Certificate - VALID MEDICAL-NO WAIVERS/LIMIT Certificate(s)/Rating(s) COMMERCIAL.CF! Biennial Flight Current Review - YES Total Fl ,ight Time (Hours) 8295 Last 24 Hrs - SE LAND.ME LAND GLIDER Months Since - 10 Make/Model- 100 Last 30 Days- Aircraft Type - UNK/NR Instrument- 127 Last 90 Days- Multi-Eng - 300 Rotorcraft Instrument Rating(s) - AIRPLANE ----Narrative---- DURING INITIAL CLIMB PHASE OF AN EXPERIMENTAL FLT FROM MGM, AL, THE PLT RPTED THAT THE LEFT ENGINE HAD FAILED AND AN ATTEMPT WAS MADE TO FEATHER THE PROP. THE PLT RADIOED DANNELLY TOWER THAT THE ACFT WAS RETURNING TO THE ARPT. THEN THE PLT RPTED THAT THE RIGHT ENGINE LOST THRUST, HOWEVER THE RIGHT PROP WAS NOT FEATHERED BECAUSE HE WAS NOT SURE IF THE ENGINE WAS PRODUCING POWER. A GEAR-UP FORCED LANDING WAS MADE ON A 4-LANE HIGHWAY. THE ACFT ENGINES WERE FUELED WITH ALCOHOL WITH APPROVAL OF THE FAA FOR RESEARCH AND DEVELOPMENT. THREE DAYS PRIOR TO THE ACCIDENT THE ACFT EXPERIENCED POWER SURGES AND MADE A PRECAUTIONARY LANDING. NO PROBLEMS WERE FOUND AND THE FLIGHT WAS CONTINUED. INSPECTION OF THE ACFT REVEALED THE RIGHT PROP FEATHERED AND THE LEFT PROP IN LOW PITCH. THE ACFT WGT AND BAL INDICATED APPROX. 400# OVER GROSS WEIGHT. THE ENGINES WERE SUCCESSFULLY TEST RUN. THERE HAS BEEN NO DETERMINATION AS TO THE CAUSE OF THE RPTED ENGINE FAILURES. PAGE 12 UNK/NR UNK/NR 100 2 Brief of Accident (Continued) File No. ~ 1954 Occurrence #1 Phase of Operati-0n Finding(s) 1. UNDETERMINED Occurrence #2 Phase of Operation Finding(s) 9/20/86 MONTGOMERY.AL LOSS OF POWER(PARTIAL) - NON-MECHANICAL TAKEOFF - INITIAL CLIMB FORCED LANDING DESCENT - EMERGENCY 2. PROPELLER SYSTEM/ACCESSORIES.FEATHERING SYSTEM - UNDETERMINED 3. EMERGENCY PROCEDURE - NOT FOLLOWED - PILOT IN COMMAND Occurrence #3 Phase of Operation Finding(s) IN FLIGHT COLLISION WITH TERRAIN LANDING - FLARE/TOUCHDOWN 4. WHEELS UP LANDING - PERFORMED - PILOT IN COMMAND ----Probable Cause---- A/C Reg. No. N6041Y The National Transportation Safety Board determines that the Probable Cause(s) of this accident is/are finding(s) 1,4 Factor(s) relating to this accident is/are f inding(s) 3 PAGE 13 Time (Lcl) - 1022 CDT National Transportation Safety Board Washington, D.C. 20594 Brief of Accident F i l e No . - 18 1 1 9/25/86 YANTLEY,AL A/C Reg. No. N3757Z ----Basic ~nformation---- Type Operating Certificate-NONE (GENERAL AVIATION) Type of Operation -FERRY Flight Conducted Under -14 CFR 91 Accident Occurred During -DESCENT ----Aircraft Information---- Aircraft Damage DESTROYED Fire ON GROUND Crew Pass Fatal 1 0 Time (Lcl) - 1810 CDT Injuries Serious Minor 0 0 0 0 None 0 0 Make/Model - CESSNA A-37A Landing Gear - TRICYCLE-RETRACTABLE Eng Make/Model - GE J-85-GE-5A Number Engines - 2 ELT Installed/Activated - UNK/NR Stall Warning System - UNK/NR Max Gross Wt 14000 No. of Seats 2 ----Environment/Operations Information---- Weather Data Wx Briefing - FSS Method - TELEPHONE Completeness - FULL Basic Weather - VMC Wind Dir/Speed- 140/005 KTS Visibility 7.0 SM Engine Type - TURBOJET Rated Power 2850 LBS THRUST Itinerary Last Departure Point TROY.AL Destination ADDISON, TX ATC/Airspace Airport Proximity OFF AIRPORT/STRIP Airport Data - N/A - N/A Lowest Sky/Clouds 3500 Lowest Ceiling - 25000 FT SCATTERED Type of Flight Plan - IFR FT BROKEN Type of Clearance - IFR Runway !dent Runway Lth/Wid Runway Surface Runway Status - N/A - N/A Obstructions to Vision- NONE Precipitation - NONE Condition of Light - DAYLIGHT ----Personnel Information---- Pi lot-In-C-0mmand Certif icate(s)/Rating(s) COMMERCIAL SE LAND.ME LAND Instrument Rating(s) - AIRPLANE ----Narrative---- Type Apch/Lndg - NONE Age - 49 Biennial Flight Review Current - UNK/NR Months Since - UNK/NR Aircraft Type - UNK/NR Medical Certificate - VALID MEDICAL-WAIVERS/LIMIT Flight Time (Hours) · Total 2400 Last 24 Hrs - UNK/NR Make/Model- UNK/NR Last 30 Days- UNK/NR Instrument- UNK/NR Last 90 Days- UNK/NR Multi-Eng - UNK/NR Rotorcraft - UNK/NR THE PLT HAD JUST PURCHASED THE ACFT WHICH HAD AN EXPERIMENTAL AIRWORTHINESS CERTIFICATE. DURING A PREFLT WX BRIEFING, HE WAS ADVISED OF TOWERING CUMULUS CLOUDS ALONG HIS ROUTE. AFTER TAKEOFF, HE INITIATED A CLIMB TO FL 240 & LEVELED OFF APRX 10 MIN LATER. AFTER ANOTHER 7 MIN, THE PLT TRANSMITTED "N3757Z, I'M IN TROUBLE!" SHORTLY THEREAFTER, RADIO & RADAR CONTACT WITH THE ACFT WERE LOST. A MILITARY ACFT WAS DIVERTED TO THE AREA & THE CRASH SITE WAS LOCATED. AN EXAM OF THE WRECKAGE REVEALED THE ACFT HAD IMPACTED IN A STEEP NOSE DOWN, WINGS LEVEL ATTITUDE. NO PREIMPACT PART FAILURE OR MALFUNCTION WAS FND. FLT CREWS OF OTHER ACFT RPRTD THERE WAS HEAVY WX ACTIVITY IN THE VICINITY OF THE ACDNT. PAGE 14 Brief of Accident (Continued) File No. - 1811 Occurrence #1 Phase of Operation Finding(s) 9/25/86 YANTLEY,AL IN FLIGHT ENCOUNTER WITH WEATHER CRUISE - NORMAL 1. IN-FLIGHT PLANNING/DECISION - IMPROPER - PILOT IN COMMAND 2. IN FLIGHT WEATHER ADVISORIES - NOT OBTAINED - PILOT IN COMMAND 3. WEATHER CONDITION - CLOUDS 4. WEATHER CONDITION - THUNDERSTORM 5. WEATHER CONDITION - TURBULENCE(THUNDERSTORMS) A/C Reg. No. N3757Z 6. FLIGHT INTO KNOWN ADVERSE WEATHER - CONTINUED - PILOT IN COMMAND Occurrence #2 Phase of Operation Finding(s) LOSS OF CONTROL - IN FLIGHT CRUISE 7. AIRCRAFT HANDLING - NOT MAINTAINED - PILOT IN COMMAND Occurrence #3 Phase of Operation ----Probable Cause---- IN FLIGHT COLLISION WITH TERRAIN DESCENT - UNCONTROLLED The National Transportation Safety Board determines that the Probable Cause(s) of this accident is/are finding(s) 1,6,7 Factor(s) relating to this accident is/are finding(s) 2,3,4,5 PAGE 15 Time (Lcl) - 1810 CDT National Transportation Safety Board Washington, D.C. 20594 Brief of Accident File No. - 1955 6/18/86 JONESBORO.AR A/C Reg. No. N67490 Time (Lcl) - 1340 CDT ----Basic Information---- Type Operating Certificate-NONE (GENERAL AVIATION) Type of Operation Flight Conducted Under Accident Occurred During ----Aircraft Information---- - INSTRUCTIONAL -14 CFR 91 -MANEUVERING Aircraft Damage DESTROYED Fire NONE Crew Pass Fatal 0 0 Injuries Serious Minor 0 0 0 0 None 1 0 Make/Model - CESSNA 15211 Landing Gear - TRICYCLE-FIXED Eng Make/Model - LYCOMING 0-235 L2C Number Engines - 1 ELT Installed/Activated - YES-UNK/NR Stall Warning System - YES Max Gross Wt 1670 No. of Seats 2 ----Environment/Operations Information---- Weather Data Wx Briefing - NO RECORD OF BRIEFING Method - N/A Completeness - N/A Basic Weather - VMC Wind Dir/Speed- 040/007 KTS Visibility 12.0 SM Lowest Sky/Clouds CLEAR Lowest Ceiling - NONE Obstructions to Vision- NONE Precipitation Condition of Light - NONE - DAYLIGHT Engine Type - RECIPROCATING-CARBURETOR Rated Power 110 HP Itinerary Last Departure Point SHERIDAN.AR Destination JONESBORO.AR ATC/Airspace Type of Flight Plan - VFR Type of Clearance - VFR Type Apch/Lndg - FORCED LANDING Airport Proximity OFF AIRPORT/STRIP Airport Data Runway !dent Runway Lth/Wid Runway Surf ace Runway Status - N/A - N/A - DIRT - ROUGH ----Personnel Information---- Pi lot-In-Command Certificate(s)/Rating(s) STUDENT Age - 17 Medical Certificate - VALID MEDICAL-NO WAIVERS/LIMIT Instrument Rating(s) ----Narr~tive---- - NONE Biennial Flight Review Current - N/A Months Since - N/A Aircraft Type - N/A Flight Total Make/Model- Instrument- Time (Hours) 36 Last 24 36 Last 30 0 Last 90 THE PILOT STATED THAT HE WAS LEVEL AT 3,000 FEET, AND HAD THE AIRPORT IN SIGHT WHEN HE EXPERIENCED A FLUCTUATION IN ENGINE RPM. THE PILOT FURTHER STATED THAT HE CONTINUED THE FLIGHT BUT THAT THE ENGINE QUIT WHEN THE AIRCRAFT WAS OVER THE AIRPORT. THE P.l.C. COULD NOT EXPALIN WHY HE CHOSE NOT TO LAND AT THE AIRPORT, AND ATTEMPTED INSTEAD AN OFF-AIRPORT LANDING. THE AIRCRAFT CLIPPED A TREE WITH ITS RIGHT WING AND IMPACTED THE GROUND NOSE FIRST. THERE WAS NO FIRE. ACCORDING TO THE PILOT, THE AIRCRAFT HAD TEN GALLONS OF FUEL ON BOARD WHEN THE FLl~HT ORIGINATED. HE MADE ONE STOP ENROUTE TO HIS DESTINATION AIRPORT, 120NM AWAY. PAGE 16 Hrs - UNK/NR Days- UNK/NR Days- 20 Brief of Accident (Continued) File No. - 1955 Occurrence #1 Phase of Operation Finding(s) 6/18/86 JONESBORO.AR LOSS OF POWER(TOTAL) - NON-MECHANICAL CRUISE 1. PREFLIGHT PLANNING/PREPARATION - INADEQUATE - PILOT IN COMMAND A/C Reg. No. N67490 2. IMPROPER USE OF PROCEDURE.LACK OF TOTAL EXPERIENCE IN TYPE OPERATION - PILOT IN COMMAND 3. FUEL CONSUMPTION CALCULATIONS - MISJUDGED - PILOT IN COMMAND 4. REFUELING - NOT PERFORMED - PILOT IN COMMAND Occurrence #2 Phase of Operation Occurrence #3 Phase of Operation Finding(s) FORCED LANDING DESCENT - EMERGENCY IN FLIGHT COLLISION WITH OBJECT MANEUVERING - TURN TO LANDING AREA (EMERGENCY) 5. IN-FLIGHT PLANNING/DECISION - IMPROPER - PILOT IN COMMAND 6. EMERGENCY PROCEDURE - NOT FOLLOWED - PILOT IN COMMAND Occurrence #4 Phase of Operation ----Probable Cause---- IN FLIGHT COLLISION WITH TERRAIN MANEUVERING - TURN TO LANDING AREA (EMERGENCY) The National Transportation Safety Board determines that the Probable Cause(s) of this accident is/are finding(s) 3,4,6 Factor(s) relating to this accident is/are finding(s) 1,2,5 PAGE 17 Time (Lcl) - 1340 CDT File No. - 1953 6/26/86 ----Basic Information---- National Transportation Safety Board Washington, D.C. 20594 Brief of Accident MAMMOTH SPRING.AR A/C Reg. No. N44767 Type Operating Certificate-NONE (GENERAL AVIATION) Time (Lcl) - 1315 CDT Injuries Type of Operation -PERSONAL Aircraft Damage SUBSTANTIAL Fire Crew Pass Fatal 0 0 Serious Minor 0 0 None 1 Flight Conducted Under Accident Occurred During ----Aircraft Information---- -14 CFR 91 -LANDING NONE 0 0 2 Make/Model - PIPER PA-28R-200 Landing Gear - TRICYCLE-RETRACTABLE Eng Make/Model - LYCOMING I0-360-CIC Number Engines - 1 ELT Installed/Activated - YES/NO Stall Warning System - YES Max Gross Wt 2900 No. of Seats 4 ----Environment/Operations Information---- Weather Data Wx Briefing - FSS Method - TELEPHONE Completeness - WEATHER NOT PERTINENT Basic Weather - VMC Wind Dir/Speed- 220/008 KTS Visibility 5.0 SM Engine Type - RECIP-FUEL INJECTED Rated Power 200 HP Itinerary Last Departure Point FLIPPIN.AR Destination POPLAR BLUFF.MO ATC/Airspace Airport Proximity OFF AIRPORT/STRIP Airport Data - N/A - N/A Lowest Sky/Clouds 3500 Lowest Ceiling - NONE FT SCATTERED Type of Flight Plan - NONE Type of Clearance - NONE Runway !dent Runway Lth/Wid Runway Surf ace Runway Status - DIRT - DRY Obstructions to Vision- HAZE Type Apch/Lndg - FORCED LANDING SNOW - DRY Precipitation - NONE Condition of Light - DAYLIGHT ----Personnel Information---- Pi lot-In-Command Certificate(s)/Rating(s) COMMERCIAL,CFI Age - 27 Medical Certificate - VALID MEDICAL-WAIVERS/LIMIT Biennial Flight Review Current - YES SE LAND Months Since 0 Aircraft Type - UNK/NR Instrument Rating(s) - AIRPLANE ----Narrative---- Flight Time (Hours) Total Make/Model- Instrument- Mul ti -Eng - 334 Last 24 Hrs - 2 18 Last 30 Days- UNK/NR 53 Last 90 Days- 17 9 THE PILOT STATED THAT THE AIRCRAFT HAD PLENTY OF OIL PRIOR TO DEPARTURE AND THAT THE FLIGHT WAS PROCEEDING NORMALLY WHEN, SUDDENLY, THE OIL PRESSURE DROPPED TO ZERO. WHILE SUBSEQUENTLY HEADING FOR A NEARBY AIRPORT, THE ENGINE LOST POWER AND SEIZED, FORCING AN OFF-AIRPORT EMERGENCY LANDING, ACCORDING TO THE PILOT. A POST-CRASH EXAMINATION OF THE ENGINE BY AN FAA AIRWORTHINESS INSPECTOR REVEALED THAT THE OIL PLUG WAS MISSING AND THERE WAS NO EVIDENCE OF SAFETY WIRING. THE AIRCRAFT HAD JUST BEEN RELEASED FROM MAINTENANCE, ACCORDING TO THE INSPECTOR. PAGE 18 File No_ - 1953 Occurrence #1 Phase of Operation Finding(s) Brief of Accident (Continued) 6/26/86 MAMMOTH SPRING.AR A/C Reg. No .. N44767 LOSS OF POWER(TOTAL) - MECH FAILURE/MALFUNCTION CRUISE 1. MAINTENANCE.SERVICE OF AIRCRAFT - IMPROPER - OTHER MAINTENANCE PSNL 2. PROCEDURE INADEQUATE,CONDITION(S)/STEP(S) IN ERROR - OTHER MAINTENANCE PSNL 3. FLUID.OIL - EXHAUSTION Occurrence #2 Phase of Operation Occurrence #3 Phase of Operation Finding(s) FORCED LANDING CRUISE ON GROUND COLLISION WITH TERRAIN LANDING 4. TERRAIN CONDITION - ROUGH/UNEVEN ----Probable Cause---- The National Transportation Safety Board determines that the Probable Cause(s) of this accident is/are finding(s) 1,3 Factor(s) relating to this accident is/are finding(s) 2,4 PAGE 19 Time (Lcl) - 1315 CDT National Transportation Safety Board Washington, D.C. 20594 Brief of Accident File No. - 1866 6/28/86 HARTFORD.AR A/C Reg. No. N3328F Time (Lcl) - 0945 CDT ----Basic Information---- Type Operating Certificate-NONE (GENERAL AVIATION) Type of Operation Flight Conducted Under Accident Occurred During ----Aircraft Information---- -PERSONAL -14 CFR 91 -DESCENT Aircraft Damage DESTROYED Fire ON GROUND Crew Pass Fatal 1 3 Injuries Serious Minor 0 0 0 0 None 0 0 Make/Mode l - CESSNA 182J Landing Gear - TRICYCLE-FIXED Eng Make/Model - CONTINENTAL 0-470-R Number Engines - 1 ELT Installed/Activated - UNK/NR Stall Warning System - UNK/NR Max Gross Wt 2800 No. of Seats 4 ----Environment/Operations Information---- Weather Data Wx Briefing - NO RECORD OF BRIEFING Method - N/A Completeness - N/A Basic Weather - IMC Wind Dir/Speed- 290/005 KTS Visibility - UNK/NR Lowest Sky/Clouds UNK/NR Lowest Ceiling - UNK/NR Obstructions to Vision- FOG Precipitation Condition of Light - RAIN - DAYLIGHT Engine Type - RECIPROCATING-CARBURETOR Rated Power 230 HP Itinerary Last Departure Point WINNSBORO, TX Destination POINT LOOKOUT.MO ATC/Airspace Type of Flight Plan - NONE Type of Clearance - NONE Type.Apch/Lndg - NONE Airport Proximity OFF AIRPORT/STRIP Airport Data Runway !dent Runway Lth/Wid Runway Surface Runway Status - N/A - N/A - N/A - N/A ----Personnel Information---- Pi lot-In-Command Age - 38 Medical Certificate - VALID MEDICAL-NO WAIVERS/LIMIT Certif icate(s)/Rating(s) PRIVATE Biennial Flight Current Review - YES Total Flight Time (Hours) 104 Last 24 Hrs - SE LAND Months Since 5 Make/Model- UNK/NR Last 30 Days- Aircraft Type - C-172 Instrument- 5 Last 90 Days- Instrument Rating(s) - NONE ----Narrative---- WHEN THE ACFT DID NOT ARRIVE AT ITS DESTN, A SEARCH WAS INITIATED. THE WRECKAGE WAS LOCATED 4 DAYS LATER WHERE THE ACFT CRASHED IN MOUNTAINOUS TERRAIN. AN INVESTIGATION REVEALED THERE WAS SEVERE THUNDERSTORM ACTIVITY IN THE AREA AT THE TIME OF THE ACCIDENT. NO RECORD WAS FOUND OF THE PLT RECEIVING A PREFLT WX BRIEFING. RADAR DATA SHOWED THAT AN ACFT (PRESUMABLY N3328F) HAD TRACKED NORTHBOUND TOWARD AN AREA OF RISING TERRAIN WITH THE TRANSPONDER SQUAWKING 1200 (VFR CODE), BUT WITH NO MODE "C" ALT REPORTING. THE ACFT THEN TURNED EASTBOUND FOR 5 TO 7 MI, THEN BEGAN CIRCLING FOR ABOUT 1 MIN UNTIL RADAR CONTACT WAS LOST. SUBSEQUENTLY, THE WRECKAGE WAS FOUND IN THE SAME VICINITY. AN EXAM REVEALED THE ACFT HAD CRASHED IN A STEEP NOSE DOWN, SLIGHTLY INVERTED ATTITUDE, AT HI SPEED. NO PREIMPACT MECHANICAL FAILURE OR MALFUNCTION WAS FOUND. PAGE 20 UNK/NR UNK/NR UNK/NR Brief of Accident (Continued) File No. - 1866 6/28/86 HARTFORD.AR Occurrence #1 Phase of Operation IN FLIGHT ENCOUNTER WITH WEATHER CRUISE - NORMAL Finding(s) 1. PREFLIGHT PLANNING/PREPARATION - INADEQUATE - PILOT IN COMMAND 2. TERRAIN CONDITION·- HIGH TERRAIN 3. WEATHER CONDITION - CLOUDS 4. WEATHER CONDITION - LOW CEILING 5. WEATHER CONDITION - FOG 6. WEATHER CONDITION - THUNDERSTORM 7. VFR FLIGHT INTO IMC - CONTINUED - PILOT IN COMMAND Occurrence #2 Phase of Operation Finding(s) LOSS OF CONTROL - IN FLIGHT UNKNOWN 8. AIRCRAFT HANDLING - NOT MAINTAINED - PILOT IN COMMAND A/C Reg. No. N3328F 9. IMPROPER USE OF EQUIPMENT/AIRCRAFT.SPATIAL DISORIENTATION - PILOT IN COMMAND 10. IMPROPER USE OF EQUIPMENT/AIRCRAFT.LACK OF TOTAL INSTRUMENT TIME - PILOT IN COMMAND Occurrence #3 Phase of Operation Finding(s) IN FLIGHT COLLISION WITH TERRAIN DESCENT - UNCONTROLLED 11. TERRAIN CONDITION - MOUNTAINOUS/HILLY ----Probable Cause---- The National Transportation Safety Board determines that the Probable Cause(s) of this accident is/are finding(s) 7,8,9 Factor(s) relating to this accident is/are finding(s) 1,2,3,4,5,6,10, 11 PAGE 21 Time (Lcl) - 0945 CDT National Transportation Safety Board Washington, D.C. 20594 Brief of Accident File No. - 1993 8/03/86 MARANA.AZ A/C Reg. No. N34180 ----Basic Information---- Type Operating Certificate-NONE (GENERAL AVIATION) Type of Operation Flight Conducted Under Accident Occurred During ----Aircraft Information---- -PERSONAL -14 CFR 91 -APPROACH Aircraft Damage SUBSTANTIAL Fire NONE Crew Pass Fatal 0 0 Time (Lcl) - 1330 MST Injuries Serious Minor 0 0 0 0 None 1 0 Make/Model - SCHWEIZER SGS-1-35 Landing Gear - TAILWHEEL-RETRACTABLE MAINS Eng Make/Model - N/A Number Engines - N/A ELT Installed/Activated - NO -N/A Stall Warning System - NO Max Gross Wt 930 No. of Seats 1 ~---Environment/Operations lnformation---- Weather Data Wx Briefing - NO RECORD OF BRIEFING Method - N/A Completeness - N/A Basic Weather - VMC Engine Type - N/A Rated Power - N/A Itinerary Last Departure Point MARANA.AZ Destination LOCAL Airport Proximity ON AIRSTRIP Wind Dir/Speed- 360/003 KTS Visibility 50.0 SM Lowest Sky/Clouds CLEAR ATC/Airspace Type of Flight Plan - NONE Type of Clearance - NONE Airport Data TAYLOR FIELD Runway !dent Runway Lth/Wid Runway Surf ace Runway Status - 36 3000/ - DIRT Lowest Ceiling - NONE - DRY Obstructions to Vision- NONE Precipitation - NONE Condition of Light - DAYLIGHT ----Personnel Information---- Pi lot-In-Command Certificate(s)/Rating(s) PRIVATE GLIDER Type Apch/Lndg - FULL STOP Age - 33 Medical Certificate Biennial Flight Review Flight Current - UNK/NR Total Months Since 9 Make/Model- Aircraft Type - 2-33 Instrument- - NO MEDICAL Time (Hours) 33 Last 24 Hrs - 1 Last 30 Days- 0 Last 90 Days- Rotorcraft Instrument Rating(s) - NONE ----Narrative---- A SCHWEIZER SGS 1-35, LANDED HARD AFTER A STEEP FINAL APPROACH. THE PILOT INDICATED THAT HE WAS HIGH ON FINAL APPROACH AND INITIALLY APPLIED 30 DEGREES OF FLAPS. HE WAS STILL TOO HIGH AND ELECTED TO USE 80 DEGREES (FULL) FLAPS. THE AIRCRAFT LANDED HARD NOSE DONW ON THE AIRCRAFT BELLY FORWARD OF LANDING GEAR. THE AIRCRAFT CANOPY WAS BROKEN IMMEDIATELY BY THE IMPACT. THE AIRCRAFT THEN OVERRAN THE DIRT RUNWAY AND CAME TO REST IN VEGETATION OFF THE END. THE PILOT ALSO INDICATED THAT THIS WAS HIS FIRST FLIGHT IN THIS MODEL GLIDER AND THAT THERE WERE NO MECHANICAL FAILURES OR MALFUNCTIONS WITH JHE AIRCRAFT PRIOR TO THE ACCIDENT. PAGE 22 150 1 1 7 33 Brief of Accident (Continued) File No. - 1993 Occurrence #1 Phase of Operation Finding(s) 8/03/86 MARANA.AZ IN FLIGHT COLLISION WITH TERRAIN LANDING - FLARE/TOUCHDOWN 1. LEVEL OFF - NOT PERFORMED - PILOT IN COMMAND A/C Reg. No. N34180 2. IMPROPER USE OF PROCEDURE, LACK OF TOTAL EXPERIENCE IN TYPE OF AIRCRAFT - PILOT IN COMMAND 3. PROPER DESCENT RATE - EXCEEDED - PILOT IN COMMAND 4. PLANNED APPROACH - POOR - PILOT IN COMMAND 5. IMPROPER USE OF PROCEDURE, LACK OF TOTAL EXPERIENCE IN TYPE OF AIRCRAFT - PILOT IN COMMAND 6. PROPER GLIDEPATH - NOT FOLLOWED - PILOT IN COMMAND ----Probable Cause-~-- The National Transportation Safety Board determines that the Probable Cause(s) of this accident is/are finding(s) 1,4,6 Factor(s) relating to this accident is/are finding(s) 2,3,5 PAGE 23 Time (Lcl) - 1330 MST File No. - 1992 8/15/86 SUN CITY WEST, AZ ----Basic Information---- Type Operating Certificate-NONE (GENERAL AVIATION) Type of Operation Flight Conducted Under Accident Occurred During ----Aircraft Information---- -PERSONAL -14 CFR 91 -DESCENT Brief of Accident A/C Reg. No. N3371V Aircraft Damage SUBSTANTIAL Fire NONE Crew Pass Fatal 0 0 Time (Lcl) - 1450 MST Injuries Serious Minor 1 0 0 0 None 0 3 Make/Model - BEECH 35R Landing Gear - TRICYCLE-FIXED Eng Make/Model - CONTINENTAL E185-1 Number Engines - 1 ELT Installed/Activated - YES/NO Stall Warning System - UNK/NR Max Gross Wt 2650 No. of Seats 4 ----Environment/Operations Information---- Weather Data Wx Briefing - NO RECORD OF BRIEFING Method - N/A Completeness - N/A Basic Weather - VMC Wind Dir/Speed- 290/005 KTS Vis i bi l i ty 45. 0 SM Lowest Sky/Clouds CLEAR Lowest Ceiling - NONE Obstructions to Vision- NONE Precipitation - NONE Condition of Light - DAYLIGHT ----Personnel Information---- Pi lot-In-Command Certificate(s)/Rating(s) PRIVATE SE LAND Instrument Rating(s) - NONE ----Narrative---- Engine Type - RECIPROCATING-CARBURETOR Rated Power 185 HP Itinerary Last Departure Point SUN CITY WEST, AZ Destination MESA.AZ ATC/Airspace Type of Flight Plan - NONE Type of Clearance - NONE Type Apch/Lndg - NONE Airport Proximity OFF AIRPORT/STRIP Airport Data HART Runway !dent Runway Lth/Wid Runway Surf ace Runway Status - 25 2600 - DIRT - DRY Age - 32 Medical Certificate - VALID MEDICAL-WAIVERS/LIMIT Biennial Flight Review Current - NO Months Since - UNK/NR Aircraft Type - UNK/NR Flight Time (Hours) Total Make/Model- Instrument- 754 Last 24 Hrs - 2 718 Last 30 Days- UNK/NR 0 Last 90 Days- 70 A BEECHCRAFT BE-35R LOST ALT DURING INITIAL CLIMB AND COLLIDED WITH THE GROUND AFTER TAKEOFF FROM A PRIVATE AIRSTRIP. THE PLT DESCRIBED THE TAKEOFF AS NORMAL UNTIL HE REACHED AN ALT OF 100 TO 125 FT AGL AND STARTED TO TURN LEFT. THE PL T STATED, "THE AIRCRAFT ACTED LIKE IT LOST ALL ITS LI FT. 11 INVESrrr-GATION REVEALED THAT THERE WAS NO WEIGHT AND BALANCE RECORDS ONBOARD THE ACFT AT THE TIME OF THE ACCIDENT. THE PLT WAS USING PERFORMANCE DATA FROM A "C" MODEL BONANZA FLIGHT MANUAL. THE "C" MODEL BONANZA IS EQUIPPED WITH A CONTINENTAL E-185-1 ENGINE THAT PRODUCES 205 HORSEPOWER WHERE AS THE CONTINENTAL E-185-1 INSTALLED IN THE ACFT ONLY PRODUCES 185 HORSEPOWER. THE PLT COMPUTED THE GROSS WEIGHT FOR TAKEOFF AS 2,683.4 LBS, 33 LBS OVER THE MAX GWT FOR THE ACFT. THE TEMP WAS REPORTED TO BE 106 DEGREES FAT THE TIME OF THE ACCIDENT AND THE DENSITY ALT FOR THE 1,313 FOOT ELEVATION WAS COMPUTED AT 4,400 FT. PAGE 24 Brief of Accident (Continued) File No. - 1992 Occurrence #1 Phase of Operation Finding(s) 8/15/86 SUN CITY WEST, AZ ALTITUDE DEVIATION.UNCONTROLLED TAKEOFF - INITIAL CLIMB 1. AIRCRAFT WEIGHT AND BALANCE - IMPROPER - PILOT IN COMMAND A/C Reg. No. N3371V 2. IMPROPER USE OF EQUIPMENT/AIRCRAFT.OVER CONFIDENCE IN PERSONAL ABILITY - PILOT IN COMMAND 3. WEATHER CONDITION - HIGH DENSITY ALTITUDE 4. FLIGHT MANUALS - IMPROPER - PILOT IN COMMAND 5. PERFORMANCE DATA - INACCURATE - PILOT IN COMMAND Occurrence #2 Phase of Operation Finding(s) IN FLIGHT COLLISION WITH TERRAIN DESCENT - UNCONTROLLED 6. STALL/MUSH - PERFORMED - PILOT IN COMMAND ----Probable Cause---- The National Transportation Safety Board determines that the Probable Cause(s) of this accident is/are finding(s) 1,2,4,6 Factor(s) relating to this accident is/are f inding(s) 3,5 PAGE 25 Time (Lcl) - 1450 MST National Transportation Safety Board Washington, D.C. 20594 Brief of Accident F i l e No. - 1802 12/14/86 CHANDLER.AZ A/C Reg. No. N3605P Ti me (Le l ) - 1715 MST ----Basic Information---- Type Operating Certificate-NONE (GENERAL AVIATION) Type of Operation Flight Conducted Under Accident Occurred During ----Aircraft Information---- -BUSINESS -14 CFR 91 -LANDING Aircraft Damage SUB ST ANTI AL Fire NONE Crew Pass Fatal 0 0 Injuries Serious Minor 0 0 0 0 None 1 0 Make/Mode l - CESSNA P210N Landing Gear - TRICYCLE-RETRACTABLE Eng Make/Model - CONTINENTAL TSI0-520-P Number Engines - 1 ELT Installed/Activated - UNK/NR Stall Warning System - UNK/NR Max Gross Wt 4000 No. of Seats 6 ----Environment/Opera~ions Information---- Weather Data Wx Briefing - NO RECORD OF BRIEFING Method - N/A Completeness - N/A Basic Weather - VMC Engine Type - RECIP-FUEL INJECTED Rated Power 310 HP Itinerary Last Departure Point DURANGO.CO Destination CHANDLER,AZ Airport Proximity OFF AIRPORT/STRIP Airport Data Wind Dir/Speed- 320/005 KTS Visibility 25.0 SM Lowest Sky/Clouds 12000 ATC/Airspace FT SCATTERED Type of Flight Plan - NONE FT OVERCAST Type of Clearance - NONE Runway !dent Runway Lth/Wid Runway Surf ace Runway Status - 04 4395/ - ASPHALT 75 Lowest Ceiling - 25000 Obstructions to Vision- NONE Precipitation Condition of Light ----Personnel Information---- Pi lot-In-Command - NONE - DAYLIGHT Certif icate(s)/Rating(s) COMMERCIAL SE LAND.ME LAND Instrument Rating(s) - NONE ----Narrative---- - DRY Type Apch/Lndg - FORCED LANDING Age - 42 Medical Certificate - NON-VALID MEDICAL Biennial Flight Review Flight Time (Hours) Current - UNK/NR Total - UNK/NR Last 24 Hrs - Months Since - UNK/NR Make/Model- UNK/NR Last 30 Days- Aircraft Type - UNK/NR Instrument- UNK/NR Last 90 Days- Multi-Eng - UNK/NR Rotorcraft - WHILE THE PLT WAS RECEIVING VECTORS FOR ARRIVAL AT CHANDLER, AZ, THE ENG LOST POWER. SUBSEQUENTLY, THE PLT MADE AN EMERGENCY LANDING ABOUT 1 MI NORTH OF THE ARPT. HE RPRTD THAT HE -HAD FILLED THE FUEL TANKS AT CHANDLER & HAD FLOWN TO DURANGO, CO ON 12/5/86. ON THE DAY OF THE ACCIDENT, HE HAD RETURNED TO CHANDLER WITHOUT REFUELING. AN EXAM OF THE ACFT REVEALED THE FUEL TANKS WERE EMPTY. NO MECHANICAL PART FAILURE OR MALFUNCTION WAS RPRTD. PAGE 26 UNK/NR UNK/NR UNK/NR UNK/NR Brief of Accident (Continued) Fi 1 e No. - 1802 Occurrence #1 Phase of Operation Finding(s) 12/ 14/86 CHANDLER.AZ LOSS OF POWER(TOTAL) - NON-MECHANICAL APPROACH 1. PREFLIGHT PLANNING/PREPARATION - INADEQUATE - PILOT IN COMMAND 2. REFUELING - NOT PERFORMED - 3. FLUID.FUEL - EXHAUSTION 4. FUEL SUPPLY - INADEQUATE - PILOT IN COMMAND Occurrence #2 Phase of Operation Occurrence #3 Phase of Operation Finding(s) FORCED LANDING DESCENT - EMERGENCY ON GROUND COLLISION WITH TERRAIN · LANDING - ROLL 5. TERRAIN CONDITION - ROUGH/UNEVEN ----Probable Cause---- A/C Reg. No. N3605P The National Transportation Safety Board determines that the Probable Cause(s) of this accident is/are finding(s) 1,3,4 Factor(s) relating to this accident is/are finding(s) 2,5 PAGE 27 Time (Lcl) - 1715 MST National Transportation Safety Board Washington, D.C. 20594 Brief of Accident F i l e No . - 19 15 5/03/86 LONG BEACH.CA A/C Reg. No. N55MM ----Basic Information---- Type Operating Certificate-NONE (GENERAL AVIATION) Type of Operation Flight Conducted Under Accident Occurred During ----Aircraft Information---- -PERSONAL -14 CFR 91 -LANDING Aircraft Damage SUB ST ANTI AL Fire NONE Crew Pass Fatal 0 0 Time (Lcl) - 1600 PDT Injuries Serious Minor 1 0 0 0 None 0 0 Make/Model - CESSNA P210N Landing Gear - TRICYCLE-RETRACTABLE Eng Make/Model - CONTINENTAL TSI0-520-P Number Engines - 1 ELT Installed/Activated - YES/YES Stall Warning System - YES Max Gross Wt 3400 No. of Seats 6 ----Environment/Operations Information---- Weather Data Wx Briefing - FSS Method - TELEPHONE Completeness - WEATHER NOT PERTINENT Basic Weather - VMC Wind Dir/Speed- 260/014 KTS Visibility 25.0 SM Engine Type - RECIP-FUEL INJECTED Rated Power 310 HP Itinerary Last Departure Point PAYSON.AZ Destination TORRANCE.CA ATC/Airspace Airport Proximity OFF AIRPORT/STRIP Airport Data - N/A - N/A Lowest Sky/Clouds 1300 Lowest Ceiling - NONE FT SCATTERED Type of Flight Plan - NONE Type of Clearance - NONE LONG BEACH Runway Ident Runway Lth/Wid Runway Surf ace Runway Status - GRASS/TURF - DRY Obstructions to Vision- NONE Precipitation Condition of Light - NONE - DAYLIGHT ----Personnel Information---- Pi lot-In-Command Certificate(s)/Rating(s) COMMERCIAL SE LAND,ME LAND Instrument Rating(s) - AIRPLANE ----Narrative---- Type Apch/Lndg - FORCED LANDING Age - 57 Biennial Flight Review Current - YES Months Since 1 Aircraft Type - P210N Medical Certificate - VALID MEDICAL-WAIVERS/LIMIT Flight Time (Hours) Total Make/Model- Instrument- Mul ti -Eng - 4500 Last 24 Hrs - 8 3600 Last 30 Days- UNK/NR 410 Last 90 Days- 66 242 Rotorcraft - UNK/NR WHILE ENROUTE FROM CINCINNATI, OH (LUK), TO TORRANCE, CA, THE AIRPLANE EXPERIENCED A TOTAL ENGINE POWER LOSS ABOUT 10 MILES SOUTH OF LONG BEACH AIRPORT (LGB), LONG BEACH, CA. THE PILOT ATTEMPTED TO LAND AT LGB BUT THE ACFT ALT WAS INSUFFICIENT. THE ACFT CRASHED ON A GOLF COURSE LOCATED ABT 1/4 MILE EAST OF THE ARPT. THE INVESTIGATION DISCLSD THE NO. 2 PISTON HAD MELTED DUE TO EXTREME HIGH TEMP DISTRESS AND THE CON ROD FRACTURED IN OVERLOAD. THE ENGINE WAS INSTALLED AT LUK ON MAY 2, 1986 AND HAD ACCUM 125 FLT HRS. METALLURGICAL EXAM DISCLSD MISALIGNMENT OF THE CON ROD AND PISTON/CYLINDER BARREL. PAGE 28 Brief of Accident (Continued) File No. - 1915 5/03/86 LONG BEACH.CA A/C Reg. No. N55MM Occurrence #1 Phase of Operation LOSS OF POWER(TOTAL) - MECH FAILURE/MALFUNCTION CRUISE - NORMAL Finding(s) 1. ENGINE ASSEMBLY.PISTON - BINDING(MECHANICAL) 2. ENGINE ASSEMBLY.PISTON - OVERTEMPERATURE 3. ENGINE ASSEMBLY.CONNECTING ROD - OVERLOAD 4. MAINTENANCE.ALIGNMENT - IMPROPER - OTHER MAINTENANCE PSNL Occurrence #2 Phase of Operation Occurrence #3 Phase of Operation Finding(s) 5. OBJECT - TREE(S) ----Probable Cause---- FORCED LANDING DESCENT - EMERGENCY ON GROUND COLLISION WITH OBJECT LANDING - ROLL The National Transportation Safety Board determines that the Probable Cause(s) of this accident is/are finding(s) 4 Factor(s) relating to this accident is/are finding(s) 1,2,3,5 PAGE 29 Time (Lcl) - 1600 PDT National Transportation Safety Board Washington, D.C. 20594 Brief of Accident Fi le No. - 1938 5/17/86 TEMECULA,CA A/C Reg. No. N2490Z ----Basic Information---- Type Operating Certificate-NONE (GENERAL AVIATION) Type of Operation Flight Conducted Under Accident Occurred During ----Aircraft Information---- -PERSONAL -14 CFR 91 -DESCENT Aircraft Damage SUBSTANTIAL Fire NONE Crew Pass Fatal 1 Time (Lcl) - 0845 PDT Injuries Serious Minor 0 0 1 0 None 0 0 Make/Mode l - GENERAL BALLOON AX-6 Landing Gear - N/A Eng Make/Model - N/A Number Engines - N/A ELT Installed/Activated - NO -N/A Stall Warning System - NO Max Gross Wt 1210 No. of Seats - UNK/NR ----Environment/Operations Information---- Weather Data Wx Briefing - NO RECORD OF BRIEFING Method - N/A Completeness - N/A Basic Weather - VMC Wind Dir/Speed- 360/005 KTS Visibility 10.0 SM Lowest Sky/Clouds CLEAR Lowest Ceiling - NONE Obstructions to Vision- NONE Precipitation - NONE Condition of Light - DAYLIGHT ----Personnel Information---- Pi lot-In-Command Certificate(s)/Rating(s) COMMERCIAL FREE BALLOON Instrument Rating(s) - NONE ----Narrative---- Engine Type - N/A Rated Power - N/A Itinerary Last Departure Point TEMECULA.CA Destination LOCAL ATC/Airspace Airport Proximity OFF AIRPORT/STRIP Airport Data RANCHO CALIFORNIA - N/A - N/A Type of Flight Plan - NONE Type of Clearance - NONE Runway !dent Runway Lth/Wid Runway Surface Runway Status - DIRT - DRY Type Apch/Lndg - FORCED LANDING Age - 51 Biennial Flight Review Current - YES Months Since 2 Aircraft Type - AX-6 Medical Certificate - NO Flight Time Total Make/Model- 126 126 Instrument- UNK/NR Multi-Eng - UNK/NR MEDICAL (Hours) Last 24 Hrs - Last 30 Days- 3 Last 90 Days- 4 Rotorcraft - UNK/NR THE BALLOON WAS GOING TO PARTICIPATE IN A "HARE AND HOUND" EVENT AND HAD DEPARTED A FESTIVAL STAGING AREA ON A POSITIONING FLIGHT. PRIOR TO DEPARTING THE AREA THE BALLOON HAD FLOWN FOR ABOUT 45 MINUTES. WHILE ENROUTE TO THE POSITIONING AREA THE BALLOON HAD EXHAUSTED ITS LIQUID PROPANE SUPPLY. ONE OCCUPANT IN THE BALLOON WAS ATTEMPTING TO THROW A ROPE TO GROUND WITNESSES BUT DURING THE DESCENT THE BASKET CONTACTED SOME 31 FT AGL HIGH TENSION WIRES. ALL 12 CABLES AND THE HEATER CONTROL PANEL DISPLAYED EXTENSIVE BURNING/ARCING SIGNATURES AND ALL OF THE 1/4 IN STAINLESS STEEL CABLES WERE BURNED THROUGH & SEPARATED FROM THEIR RESPECTIVE ATTACH POINTS. PAGE 30 Brief of Accident (Continued) File No_ - 1938 Occurrence #1 Phase of Operation Finding(s) 5/ 17 /86 TEMECULA.CA LOSS OF POWER(TOTAL) - NON-MECHANICAL CRUISE - NORMAL 1. FLUID.FUEL - EXHAUSTION 2. PREFLIGHT PLANNING/PREPARATION - POOR - PILOT IN COMMAND 3. REFUELING - NOT PERFORMED - PILOT IN COMMAND Occurrence #2 Phase of Operation Occurrence #3 Phase of Operation Finding(s) FORCED LANDING DESCENT - EMERGENCY IN FLIGHT COLLISION WITH OBJECT DESCENT - UNCONTROLLED 4. OBJECT - WIRE.TRANSMISSION ----Probable Cause---- A/C Reg_ No_ N2490Z The National Transportation Safety Board determines that the Probable Cause(s) of this accident is/are finding(s) 1,2,3 Factor(s) relating to this accident is/are finding(s) 4 PAGE 31 Time (Lcl) - 0845 PDT National Transportation Safety Board Washington, D.C. 20594 Brief of Accident F i l e No . - 1994 8/04/86 APPLE VALLEY.CA A/C Reg. No. N757QR ----Basic Information---- Type Operating Certificate-NONE (GENERAL AVIATION) Type of Operation Flight Conducted Under Accident Occurred During ----Aircraft Information---- - INSTRUCTIONAL -14 CFR 91 -LANDING Aircraft Damage SUBSTANTIAL Fire NONE Crew Pass Fatal 0 0 Time (Lcl) - 1800 PDT Injuries Serious Minor 0 1 0 0 None 0 0 Make/Model - CESSNA 152 Landing Gear - TRICYCLE-FIXED Eng Make/Model - LYCOMING 0-235-L2C Number Engines - 1 ELT Installed/Activated - YES/NO Stall Warning System - YES Max Gross Wt 1670 No. of Seats 2 ----Environment/Operations Information---- Weather Data Wx Briefing - FSS Method - TELEPHONE Completeness - FULL Basic Weather - VMC Wind Dir/Speed- 225/020 KTS Visibility 30.0 SM Lowest Sky/Clouds CLEAR Lowest Ceiling - NONE Obstructions to Vision- NONE Precipitation - NONE Condition of Light - DAYLIGHT ----Personnel Information---- Engine Type - RECIPROCATING-CARBURETOR Rated Power 110 HP Itinerary Last Departure Point APPLE VALLEY.CA Destination DAGGET,CA ATC/Airspace Type of Flight Plan - VFR Type of Clearance - NONE Type Apch/Lndg - NONE Airport Proximity ON AIRPORT Airport Data APPLE VALLEY Runway !dent Runway Lth/Wid Runway Surface Runway Status - 36 6500/ - ASPHALT - DRY 150 Pilot-In-Command Age - 24 Medical Certificate - VALID MEDICAL-NO WAIVERS/LIMIT Certificate(s)/Rating(s) Biennial Flight Review Fl i ght Time (Hours) STUDENT Current - N/A Total 50 Last 24 Months Since - N/A Make/Model- 50 Last 30 Aircraft Type - N/A Instrument- 1 Last 90 Instrument Rating(s) - NONE ----Narrative---- A CESSNA 152 OVERRAN RWY 36 AND NOSED OVER ON THE OVERRUN AREA. THE STUDENT PLT INDICATED THAT HE ATTEMPTED THE TAKEOFF FROM MID-FIELD ON RWY 36 WITHOUT TAKING INTO ACCOUNT THE DENSITY ALT. HE ALSO STATED THAT HE ATTEMPTED TO ABORT THE TAKEOFF AFTER REACHING 40 TO 45 KTS, BUT WAS UNABLE TO STOP THE ACFT BEFORE IT OVERRAN THE RWY. THE ACFT NOSE GEAR COLLAPSED WHEN IT COLLIDED WITH A DIRT BANK AND THEN THE ACFT CAME TO REST IN A NOSE DOWN ATTITUDE. THE STUDENT PLT THEN STATED, "THE PLANE STOPPED MOVING, BUT A STRONG TAILWIND PICKED UP THE TAIL, NOSING OVER THE PLANE, WHICH CAUSED MUCH OF THE DAMAGE." A FAA ACCIDENT PREVENTION COUNSELOR LOCATED AT THE AIRPORT STATED THE STUDENT PLT ATTEMPTED TO TAKEOFF DOWNWIND ON RWY 36 FROM MID-FIELD. THE WINDS WERE ESTIMATED Hrs - Days- Days- TO BE FROM THE S-SW AT 20 KTS AND THE TEMPERATURE APPROXIMATELY 90 DEG. RWY 36 IS 6,059 FT. THE COMPUTED DENSITY ALT IS APRX 5,500 FT. PAGE 32 1 6 22 Brief of Accident (Continued) File No. - 1994 Occurrence #1 Phase of Operation Finding(s) 8/04/86 APPLE VALLEY.CA OVERRUN TAKEOFF - GROUND RUN 1. WEATHER CONDITION - TAILWIND 2. PLANNING-DECISION - POOR - PILOT IN COMMAND 3. WRONG RUNWAY - SELECTED - PILOT IN COMMAND A/C Reg. No. N757QR 4. IMPROPER DECISION.LACK OF TOTAL EXPERIENCE - PILOT IN COMMAND 5. WIND INFORMATION - NOT UNDERSTOOD - PILOT IN COMMAND 6. WEATHER CONDITION - TAILWIND Occurrence #2 Phase of Operation Finding(s) NOSE OVER LANDING - ROLL 7. TERRAIN CONDITION - DIRT BANK 8. ABORTED TAKEOFF - DELAYED - PILOT IN COMMAND ----Probable Cause---- The National Transportation Safety Board determines that the Probable Cause(s) of this accident is/are finding(s) 2,3,5,8 Factor(s) relating to this accident is/are finding(s) 1,4,6,7 PAGE 33 Time (Lcl) - 1800 PDT National Transportation Safety Board Washington, D.C. 20594 Brief of Accident File No. - 1952 11/01/86 LAKE TAHOE.CA A/C Reg. No. N711TJ ----Basic Information---- Type Operating Certificate-COMMUTER Name of Carrier -JET CHARTER INTERNATIONAL Type of Operation -NON SCHED,DOMESTIC,PASSENGER Flight Conducted Under -14 CFR 135 Accident Occurred During -LANDING ----Aircraft lnformation---- Aircraft Damage SUBSTANTIAL Fire NONE Crew Pass Fatal 0 0 Time (Lcl) - 1830 PST Injuries Serious Minor 0 0 0 0 None 2 5 Make/Model - LEAR JET 24 Landing Gear - TRICYCLE-RETRACTABLE Eng Make/Model - GE CJ610-4 Number Engines - 2 ELT Installed/Activated - YES/NO Stall Warning System - YES Max Gross Wt 13300 No. of Seats 9 ----Environment/Operations Information---- Weather Data Wx Briefing - NO RECORD OF BRIEFING Method - N/A Completeness - N/A Basic Weather - VMC Wind Dir/Speed- 340/010 KTS Visibility 15.0 SM Lowest Sky/Clouds CLEAR Lowest Ceiling - NONE Obstructions to Vision- NONE Precipitation Condition of Light - NONE - NIGHT(DARK) Engine Type - TURBOJET Rated Power 2950 LBS THRUST Itinerary Last Departure Point SAN FRANCISCO,CA Destination LAKE TAHOE.CA ATC/Airspace Type of Flight Plan - IFR Type of Clearance - IFR Type Apch/Lndg - STRAIGHT-IN FULL STOP Airport Proximity ON AIRPORT Airport Data LAKE TAHOE Runway !dent Runway Lth/Wid Runway Surf ace Runway Status - 18 8544/ - ASPHALT - DRY 150 ----Personnel Information---- Pi lot-In-Command Certificate(s)/Rating(s) ATP,CFI Age - 41 Medical Certificate - VALID MEDICAL-NO WAIVERS/LIMIT Biennial Flight Review Current - YES SE LAND.ME LAND Months Since 2 Aircraft Type - 24 Instrument Rating(s) - AIRPLANE ----Narrative---- Flight Time (Hours) Total Make/Model- Instrument- Mul ti -Eng - 14000 Last 24 Hrs - 40 Last 30 Days- 1600 Last 90 Days- 7300 AT THE END OF A CROSS COUNTRY FLIGHT, THE PILOT EXPERIENCED LIGHT TO MODERATE TURBULENCE ON SHORT FINAL WHILE EXECUTING A DOWN WIND APPROACH TO THE LAKE TAHOE AIRPORT. APPROXIMATELY 50 FEET AGL OVER THE RUNWAY, THE AIRCRAFT EXITED THE TURBULENCE AND TOUCHED DOWN APPROXIMATELY MID FIELD. THE PILOT APPLIED MODERATE BRAKING THEN STATED THE BRAKES FAILED. THE PILOT THEN ELECTED TO EXIT THE RUNWAY TO THE RIGHT, 200 FEET FROM THE END OF THE RUNWAY WHERE THE AIRCRAFT CRASHED IN A DITCH. INSPECTION OF THE BRAKING SYSTEM REVEALED NO MECHANICAL FAILURE OR MALFUNCTION. PAGE 34 2 50 180 Brief of Accident (Continued) File No. - 1952 Occurrence #1 Phase of Operation Finding(s) 11/01/86 LAKE TAHOE.CA IN FLIGHT ENCOUNTER WITH WEATHER APPROACH - VFR PAT~ERN - FINAL APPROACH 1. WEATHER CONDITION - TURBULENCE 2. WEATHER EVALUATION - MISJUDGED - PILOT IN COMMAND Occurrence #2 Phase of Operation Finding(s) OVERRUN LANDING - ROLL 3. IN-FLIGHT PLANNING/DECISION - POOR - PILOT IN COMMAND 4. PROPER TOUCHDOWN POINT - NOT ATTAINED - PILOT IN COMMAND Occurrence #3 Phase of Operation Finding(s) ON GROUND COLLISION WITH TERRAIN LANDING - ROLL 5. TERRAIN CONDITION - DITCH ----Probable Cause---- A/C Reg. No. N711TJ The National Transportation Safety Board determines that the Probable Cause(s) of this accident is/are f inding(s) 4 Factor(s) relating to this accident is/are finding(s) 1,2,3,5 PAGE 35 Time (Lcl) - 1830 PST National Transportation Safety Board Washington, D.C. 20594 Brief of Accident File No. - 1932 6/14/86 LAMAR.CO A/C Reg. No. N6337U ----Basic Information---- Type Operating Certificate-NONE (GENERAL AVIATION) Type of Operation Flight Conducted Under Accident Occurred During ----Aircraft Information---- -PERSONAL -14 CFR 91 -DESCENT Aircraft Damage DESTROYED Fire ON GROUND Crew Pass Fatal 0 0 Time (Lcl) - 0820 MDT Injuries Serious Minor 1 0 2 0 None 0 0 Make/Model - BEECH C23 Landing Gear - TRICYCLE-FIXED Eng Make/Model - LYCOMING 0-360-A4K Number Engines - 1 ELT Installed/Activated - YES/NO Stall Warning System - YES Max Gross Wt 2450 No. of Seats 4 ----Environment/Operations Information---- Weather Data Wx Briefing - FSS Method - TELEPHONE Completeness - FULL Basic Weather - VMC Wind Dir/Speed- CALM Visibility 35.0 SM Lowest Sky/Clouds CLEAR Lowest Ceiling - NONE Obstructions to Vision- NONE Precipitation - NONE Condition of Light - DAYLIGHT Engine Type - RECIPROCATING-CARBURETOR Rated Power 180 HP Itinerary Last Departure Point SAME AS ACC/INC Destination COLORADO SPRING.CO ATC/Airspace Type of Flight Plan - NONE Type of Clearance - TRAFFIC ADVISORY Type Apch/Lndg - TRAFFIC PATTERN Airport Proximity OFF AIRPORT/STRIP Airport Data LAMAR MUNICIPAL Runway !dent Runway Lth/Wid Runway Surf ace Runway Status - 18 6304/ - ASPHALT - DRY PRECAUTIONARY LANDING 100 ----Personnel lnformation---- Pi lot-In-Command Age - 28 Medical Certificate - VALID MEDICAL-NO WAIVERS/LIMIT Certif icate(s)/Rating(s) PRIVATE SE LAND Instrument Rating(s) - NONE ----Narrative---- Biennial Flight Review Current - YES Months Since 2 Aircraft Type - UNK/NR Fl i ght Time (Hours) Total 65 Last 24 Make/Model- 5 Last 30 Instrument- 3 Last 90 DURING THE TAKEOFF CLIMB, THE PLT'S DOOR CAME OPEN. THE PVT PLT WITH 2 HOURS FLYING EXPERIENCE IN C-23 ACFT MADE A CLOSE IN TRAFFIC PATTERN TO RETURN FOR LANDING. DURING THE TURN FROM BASE LEG TO FINAL THE NOSE OF THE ACFT SUDDENLY DROPPED AND THE ACFT STARTED TO SINK RAPIDLY. THE ACFT IMPACTED THE GROUND BEFORE TOTAL RECOVERY COULD BE AFFECTED. PAGE 36 Hrs - 2 Days- UNK/NR Days- 12 Brief of Accident (Continued) Fi 1 e No. - 1932 Occurrence #1 Phase of Operation Finding(s) 6/14/86 LAMAR.CO AIRFRAME/COMPONENT/SYSTEM FAILURE/MALFUNCTION TAKEOFF - INITIAL CLIMB 1. DOOR.EXTERIOR CREW - UNLOCKED 2. AIRCRAFT PREFLIGHT - INADEQUATE - PILOT IN COMMAND Occurrence #2 Phase of Operation Finding(s) LOSS OF CONTROL - IN FLIGHT APPROACH - VFR PATTERN - BASE TO FINAL 3. AIRSPEED - UNCONTROLLED - PILOT IN COMMAND A/C Reg. No. N6337U 4. IMPROPER USE OF PROCEDURE,~NXIETY/APPREHENSION - PILOT IN COMMAND 5. ALTITUDE - UNCONTROLLED - PILOT IN COMMAND 6. IMPROPER USE OF PROCEDURE, LACK OF FAMILIARITY WITH AIRCRAFT - PILOT IN COMMAND Occurrence #3 Phase of Operation Finding(s) IN FLIGHT COLLISION WITH TERRAIN DESCENT - UNCONTROLLED 7. TERRAIN CONDITION - SOFT 8. TERRAIN CONDITION - OPEN FIELD ----Probable Cause---- The National Transportation Safety Board determines that the Probable Cause(s) of this accident is/are finding(s) 1,2,3,5 Factor(s) relating to this accident is/are finding(s) 4,6 PAGE 37 Time (Lcl) - 0820 MDT National Transportation Safety Board Washington, D.C. 20594 Brief of Accident File No. - 1973 7/26/86 BOULDER.CO A/C Reg. No. N4346L ----Basic Information---- Type Operating Certificate-NONE (GENERAL AVIATION) Type of Operation Flight Conducted Under Accident Occurred During ----Aircraft Information---- -AERIAL PHOTO -14 CFR 91 -MANEUVERING Aircraft Damage DESTROYED Fire NONE Fatal Crew 1 Pass 0 Other 0 Time (Lcl) - 0740 MDT Injuries Serious Minor 0 0 0 0 0 0 None 0 0 2 Make/Model - PIPER PA-46-310P Landing Gear - TRICYCLE-RETRACTABLE Eng Make/Model - CONTINENTAL TSI0-520-BE1 Number Engines - 1 ELT Installed/Activated - YES/NO Stall Warning System - YES Max Gross Wt 4100 No. of Seats 6 ----Environment/Operations Information---- Weather Data Wx Briefing - NO RECORD OF BRIEFING Method - N/A Completeness - N/A Basic Weather - VMC Wind Dir/Speed- 310/010 KTS Engine Type - RECIP-FUEL INJECTED Rated Power 310 HP Itinerary Last Departure Point SAME AS ACC/INC Destination LOCAL Visibility 75.0 SM ATC/Airspace Lowest Sky/Clouds 16000 FT SCATTERED Type of Flight Plan - NONE Lowest Ceiling - NONE Type of Clearance - NONE Obstructions to Vision- NONE Type Apch/Lndg - NONE Precipitation - NONE Condition Of Light - DAYLIGHT Airport Proximity OFF AIRPORT/STRIP Airport Data Runway !dent Runway Lth/Wid Runway Surface Runway Status - N/A - N/A - N/A - N/A ----Personnel Information---- Pi lot-In-Command Certificate(s)/Rating(s) COMMERCIAL Age - 41 Medical Certificate - VALID MEDICAL-WAIVERS/LIMIT SE LAND.ME LAND Instrument Rating(s) - AIRPLANE ---~Narrative---- Biennial Flight Review Current - YES Months Since - 12 Aircraft Type - PA-46 Flight Time (Hours) Total Make/Model- Instrument- Multi-Eng - 1255 Last 24 Hrs - UNK/NR 83 Last 30 Days- UNK/NR 213 Last 90 Days- 25 171 Rotorcraft - UNK/NR THE PURPOSE OF THE FLT FOR BOTH ACFT WAS AN AERIAL PHOTO MISSION. N5113S WAS USED AS THE CAMERA PLATFORM. THE PLTS OF N5113S AND N4346L DISCUSSED PRIOR TO TAKEOFF THE PROCEDURES OF THE FLT. BOTH ACFT DEPARTED AND FLEW A COURSE TO POSITION THE AIRPLANES ON A SOUTHERLY HEADING. N5113S WAS TO THE EAST AND SLIGHTLY ABOVE AND AHEAD OF N4346L. THE PHOTOGRAPHER SHOT ONE ROLL OF FILM AND RELOADED. HE WAS READY TO BEGIN SHOOTING WHEN N4346L BEGAN TO CLOSE IN ON N5113S. THE PLT OF N5113S FELT TWO "BUMPS" AS N4346L CLOSED, AND DID NOT SEE THE ACFT PASS UNDER. THE PLT OF N5113S MANEUVERED HIS ACFT TO DETERMINE CONTROLLABILITY AND SAW N4346L SPIRALLING TO THE GROUND. EXAM OF N4346L REVEALED THE VERT STAB AND RUDDER HAD SEPARATED IN-FLIGHT. THERE WERE NUMEROUS PAINT SMEARS FOUND ON THE RIGHT SIDE ON N5113S. PAGE 38 Brief of Accident (Continued) File No. - 1973 Occurrence #1 Phase of Operation Finding(s) 7/26/86 MIDAIR COLLISION MANEUVERING BOULDER.CO 1. IN-FLIGHT PLANNING/DECISION - INADEQUATE - PILOT IN COMMAND 2. ALTITUDE - MISJUDGED - PILOT IN COMMAND 3. DISTANCE - MISJUDGED - PILOT IN COMMAND 4. CLEARANCE - NOT MAINTAINED - PILOT IN COMMAND A/C Reg. No. N4346L 5. IMPROPER USE OF EQUIPMENT/AIRCRAFT.OVER CONFIDENCE IN PERSONAL ABILITY - PILOT IN COMMAND Occurrence #2 Phase of Operation AIRFRAME/COMPONENT/SYSTEM FAILURE/MALFUNCTION MANEUVERING Finding(s) 6. VERTICAL STABILIZER SURFACE - SEPARATION 7. FLIGHT CONTROL,.RUDDER - SEPARATION Occurrence #3 Phase of Operation Finding(s) 8. OBJECT - VEHICLE IN FLIGHT COLLISION WITH TERRAIN DESCENT - UNCONTROLLED 9. OBJECT - NONE SUITABLE ----Probable Cause---- The National Transportation Safety Board determines that the Probable Cause(s) of this accident is/are f inding(s) 2,3,4 Factor(s) relating to this accident is/are finding(s) 1,5 PAGE 39 Time (Lcl) - 0740 MDT File No. - 1973 7/26/86 ----Basic Information---- National Transportation Safety Board Washington, D.C. 20594 Brief of Accident BOULDER,CO A/C Reg. No. N5113S Type Operating Certificate-NONE (GENERAL AVIATION) Aircraft Damage Time (Lcl) - 0740 MDT Injuries MINOR Fatal Serious Minor None Type of Operation -AERIAL PHOTO Fire Crew 0 0 0 1 Flight Conducted Under -14 CFR 91 NONE Pass 0 0 0 1 Accident Occurred During -MANEUVERING Other 1 0 0 0 ----Aircraft Information---- Make/Model - CESSNA TR-182 Landing Gear - TRICYCLE-RETRACTABLE Eng Make/Model - LYCOMING 0-540-L3C5D Number Engines - 1 ELT Installed/Activated - YES/NO Stall Warning System - YES Max Gross Wt 3100 No. of Seats 4 ----Environment/Operations Information---- Weather Data Wx Briefing - NO RECORD OF BRIEFING Method - N/A Completeness - N/A Basic Weather - VMC Wind Dir/Speed- 310/010 KTS Visibility 75.0 SM Engine Type - RECIPROCATING-CARBURETOR Rated Power 235 HP Itinerary Last Departure Point SAME AS ACC/INC Destination LOCAL ATC/Airspace Airport Proximity OFF AIRPORT/STRIP Airport Data - N/A - N/A Lowest Sky/Clouds 16000 Lowest Ceiling - NONE Obstructions to Vision- NON.E FT SCATTERED Type of Flight Plan - NONE Type of Clearance - NONE Type Apch/Lndg - NONE Runway Ident Runway Lth/Wid Runway Surface Runway Status - N/A - N/A Precipitation - NONE Condition of Light - DAYLIGHT ----Personnel Information---- Pi lot-In-Command Certificate(s)/Rating(s) COMMERCIAL,CFI SE LAND Instrument Rating(s) - AIRPLANE ----Narrative---- Age - 41 Review - YES 6 Biennial Flight Current Months Since Aircraft Type - UNK/NR Medical Certificate - VALID MEDICAL-WAIVERS/LIMIT Flight Time (Hours) Total Make/Model- Instrument- Multi-Eng - 1343 Last 24 Hrs - UNK/NR 114 Last 30 Days- UNK/NR 45 Last 90 Days- 210 UNK/NR Rotorcraf t - UNK/NR THE PURPOSE OF THE FLT FOR BOTH ACFT WAS AN AERIAL PHOTO MISSION. N5113S WAS USED AS THE CAMERA PLATFORM. THE PLTS OF N5113S AND N4346L DISCUSSED PRIOR TO TAKEOFF THE PROCEDURES OF THE FLT. BOTH ACFT DEPARTED AND FLEW A COURSE TO POSITION THE AIRPLANES ON A SOUTHERLY HEADING. N5113S WAS TO THE EAST AND SLIGHTLY ABOVE AND AHEAD OF N4346L. THE PHOTOGRAPHER SHOT ONE ROLL OF FILM AND RELOADED. HE WAS READY TO BEGIN SHOOTING WHEN N4346L BEGAN TO CLOSE IN ON N5113S. THE PLT OF N5113S FELT TWO "BUMPS" AS N4346L CLOSED, AND DID NOT SEE THE ACFT PASS UNDER. THE PLT OF N5113S MANEUVERED HIS ACFT TO DETERMINE CONTROLLABILITY AND SAW N4346L SPIRALLING TO THE GROUND. EXAM OF N4346L REVEALED THE VERT STAB AND RUDDER HAD SEPARATED IN-FLIGHT. THERE WERE NUMEROUS PAINT SMEARS FOUND ON THE RIGHT SIDE OF N5113S. PAGE 40 Brief of Accident (Continued) File No. - 1973 Occurrence Phase of Operation Finding(s) 7/26/86 MIDAIR COLLISION MANEUVERING BOULDER.CO 1. DISTANCE - MISJUDGED - PILOT OF OTHER AIRCRAFT 2. CLEARANCE - NOT MAINTAINED - PILOT OF OTHER AIRCRAFT ----Probable Cause---- A/C Reg. No. N5113S The National Transportation Safety Board determines that the Probable Cause(s) of this accident is/are finding(s) 1,2 PAGE 41 Time (Lcl) - 0740 MDT National Transportation Safety Board Washington, D.C. 20594 F i l e No. - 184 7 8/05/86 CENTER,CO ----Basic Information---- Type Operating Certificate-NONE (GENERAL AVIATION) Type of Operation -AERIAL APPLICATION Flight Conducted Under -14 CFR 137 Accident Occurred During -LANDING ----Aircraft Information---- Brief of Accident A/C Reg. No. N5324 Aircraft Damage SUBSTANTIAL Fire NONE Crew Pass Fatal 0 0 Time (Lcl) - 0934 MDT Injuries Serious Minor 0 0 0 0 None 1 0 Make/Model - GRUMMAN G-164A Landing Gear - TAILWHEEL-ALL FIXED Eng Make/Model - P&W R-1340 Number Engines - 1 ELT Installed/Activated - NO -N/A Stall Warning System - YES Max Gross Wt 3750 No. of Seats 1 ----Environment/Operations Information---- Weather Data Wx Briefing - NO RECORD OF BRIEFING Method - N/A Completeness - N/A Basic Weather - VMC Wind Dir/Speed- CALM Visibility 75.0 SM Lowest Sky/Clouds CLEAR Lowest Ceiling - NONE Obstructions to Vision- NONE Precipitation - NONE Condition of Light - DAYLIGHT ----Personnel Information---- Pi lot-In-Command Certif icate(s)/Rating(s) COMMERCIAL SE LAND.ME LAND Instrument Rating(s) - AIRPLANE ----Narrative---- Engine Type - RECIPROCATING-CARBURETOR Rated Power 600 HP Itinerary Last Departure Point SAME AS ACC/INC Destination LOCAL ATC/Airspace Type of Flight Plan - NONE Type of Clearance - NONE Type Apch/Lndg - STRAIGHT-IN Airport Proximity ON AIRSTRIP Airport Data PRIVATE AG STRIP Runway ldent Runway Lth/Wid Runway Surface Runway Status - UNK/NR 4000/ - DIRT - DRY 50 Age - 55 Medical Certificate - VALID MEDICAL-WAIVERS/LIMIT Biennial Flight Review Current - YES Months Since - 17 Aircraft Type - BE-55 Flight Time (Hours) Total Make/Model- Instrument- Mul ti -Eng - 7800 Last 24 Hrs - 3 2950 Last 30 Days- UNK/NR 325 Last 90 Days- 125 800 THE PLT REPORTED THAT HE WAS LANDING ON A 50 FT WIDE DIRT STRIP AND ALLOWED THE ACFT TO DRIFT TO THE LEFT DURING THE LANDING ROLL. THE LEFT WING COLLIDED WITH WHEAT GROWING ALONG THE LEFT SIDE OF THE STRIP AND THE ACFT SWERVED FURTHER TO THE LEFT. DURING THE SWERVE, THE RIGHT MAIN LANDING GEAR FAILED & THE WINGS WERE DAMAGED. PAGE 42 Brief of Accident (Continued) File No. - 184 7 Occurrence #1 Phase of Operation Finding(s) 8/05/86 CENTER.CO ON GROUND COLLISION WITH TERRAIN LANDING - ROLL 1. TERRAIN CONDITION - CROP 2. PROPER ALIGNMENT - NOT MAINTAINED - PILOT IN COMMAND Occurrence #2 Phase of Operation Finding(s) LOSS OF CONTROL - ON GROUND LANDING - ROLL 3. DIRECTIONAL CONTROL - NOT POSSIBLE - 4. GROUND LOOP/SWERVE - UNCONTROLLED - Occurrence #3 Phase of Operation Finding(s) MAIN GEAR COLLAPSED LANDING 5. LANDING GEAR.MAIN GEAR - OVERLOAD ----Probable Cause---- A/C Reg. No. N5324 The National Transportation Safety Board determines that the Probable Cause(s) of this accident is/are f inding(s) 2 Factor(s) relating to this accident is/are finding(s) 1 PAGE 43 Time (Lcl) - 0934 MDT National Transportation Safety Board Washington, D.C. 20594 Brief of Accident File No_ - 1888 8/09/86 FORT COLLINS, CO A/C Reg. No. N2805F ----Basic Information---- Type Operating Certificate-NONE (GENERAL AVIATION) Type of Operation Flight Conducted Under Accident Occurred During ----Aircraft Information---- -PERSONAL -14 CFR 91 -LANDING Aircraft Damage SUBSTANTIAL Fire NONE Crew Pass Fatal 0 0 Time (Lcl) - 0745 MDT Injuries Serious Minor 0 0 0 0 None 1 0 Make/Model - RAVEN AERO STAR S-66A Landing Gear - N/A Eng Make/Model - N/A Number Engines - N/A ELT Installed/Activated - NO -N/A Stall Warning System - NO Max Gross Wt 750 No. of Seats - UNK/NR ----Environment/Operations Information---- Weather Data Wx Briefing - FSS Method - TELEPHONE Completeness - FULL Basic Weather - VMC Wind Dir/Speed- 270/005 KTS Visibility 15.0 SM Lowest Sky/Clouds CLEAR Lowest Ceiling - NONE Obstructions to Vision- NONE Precipitation - NONE Condition of Light - DAYLIGHT Engine Type - N/A Rated Power - N/A Itinerary Airport Proximity OFF AIRPORT/STRIP Last Departure Point FORT COLLINS, CO Destination Airport Data LOCAL ATC/Airspace Type of Flight Plan - NONE Type of Clearance - NONE Type Apch/Lndg - FULL STOP Age - 34 Medical Certificate Flight - Runway !dent Runway Lth/Wid Runway Surf ace Runway Status NO MEDICAL Time (Hours) - N/A - N/A - N/A - N/A ----Personnel Information---- Pi lot-In-Command Certificate(s)/Rating(s) COMMERCIAL Review - YES Biennial Flight Current Months Since Aircraft Type Total 83 Last 24 Hrs - UNK/NR - 11 Make/Model- 4 Last 30 Days- UNK/NR FREE BALLOON - UNK/NR Instrument- UNK/NR Last 90 Days- 21 Multi-Eng - UNK/NR Rotorcraft - UNK/NR Instrument Rating(s) - NONE ----Narrative---- THE PLT RPRTD HE BEGAN VENTING THE BALLOON IN PREPARATION FOR A LANDING IN A FIELD. THE BALLOON ENCOUNTERED A WIND SHIFT & STARTED DRIFTING TOWARD POWERLINES. THE PLT SAID THERE WAS NOT ENOUGH TIME TO ADD HEAT TO AVOID THE POWERLINES, SO HE HELD THE VENT OPEN AS WIDE AS POSSIBLE. HOWEVER, THE ENVELOPE CONTACTED THE WIRES, WHICH ARCED & DAMAGED THREE PANELS. PAGE 44 Brief of Accident (Continued) F i 1 e No . - 18 8 8 Occurrence Phase of Operation Finding(s) 8/09/86 FORT COLLINS, CO IN FLIGHT COLLISION WITH OBJECT LANDING - FLARE/TOUCHDOWN 1. WEATHER CONDITION - UNFAVORABLE WIND A/C Reg. No. N2805F 2. COMPENSATION FOR WIND CONDITIONS - IMPROPER - PILOT IN COMMAND 3. IMPROPER USE OF PROCEDURE.LACK OF TOTAL EXPERIENCE IN KIND OF AIRCRAFT - PILOT IN COMMAND 4. OBJECT - WIRE,TRANSMISSION 5. CLEARANCE - NOT MAINTAINED - PILOT IN COMMAND ----Probable Cause---- The National Transportation Safety Board determines that the Probable Cause(s) of this accident is/are f inding(s) 2,5 Factor(s) relating to this accident is/are finding(s) 1,3,4 PAGE 45 Time (Lcl) - 0745 MDT National Transportation Safety Board Washington, D.C. 20594 Brief of Accident F i l e No_ - 1999 9/16/86 BENNETT.CO A/C Reg. No. N1691V Time (Lcl) - 1633 MDT ----Basic Information---- Type Operating Certificate-NONE (GENERAL AVIATION) Type of Operation Flight Conducted Under Accident Occurred During ----Aircraft Information---- -BUSINESS -14 CFR 91 -DESCENT Aircraft Damage DESTROYED Fire NONE Crew Pass Fatal 1 0 Injuries Serious Minor 0 0 0 0 None 0 0 Make/Mode l - CESSNA 172M Landing Gear - TRICYCLE-FIXED Eng Make/Model - LYCOMING 0-320-E2D Number Engines - 1 ELT Installed/Activated - YES/YES Stall Warning System - YES Max Gross Wt 2300 Engine Type - RECIPROCATING-CARBURETOR No. of Seats 4 ----Environment/Operations Information---- Weather Data Wx Briefing - FSS Method - TELEPHONE Completeness - FULL Basic Weather - VMC Wind Dir/Speed- 350/012 KTS Visibility 70.0 SM Rated Power 150 HP Itinerary Last Departure Point GOODLAND.KS Destination BRIGHTON.CO ATC/Airspace Lowest Sky/Clouds 5000 FT SCATTERED Type of Flight Plan - VFR Lowest Ceiling - 25000 FT BROKEN Type of Clearance - NONE Obstructions to Vision- NONE Type Apch/Lndg - NONE Precipitation - NONE Condition of Light - DAYLIGHT Age - 41 Medical Biennial Flight Review Airport Proximity OFF AIRPORT/STRIP Airport Data Certificate Flight - Runway !dent Runway Lth/Wid Runway Surface Runway Status EXPIRED Time (Hours) - N/A - N/A - N/A - N/A ----Personnel Information---- Pi lot-In-Command Certificate(s)/Rating(s) PRIVATE Current - UNK/NR Total 1500 Last 24 Hrs - SE LAND Months Since - UNK/NR Make/Model- UNK/NR Last 30 Days- Aircraft Type - UNK/NR Instrument- 0 Last 90 Instrument Rating(s) - NONE ----N