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Cessna 414 Maintenance Manual

CESSNA 414 · Maintenance Manual

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Overview

This document is the Maintenance Manual for the Cessna 414, providing essential information for maintenance personnel and technicians. It covers detailed procedures, specifications, and guidelines necessary for the proper upkeep and servicing of the aircraft. The manual is designed to ensure that maintenance is performed safely and effectively, adhering to the manufacturer's standards. Key topics include maintenance schedules, troubleshooting procedures, and component specifications, making it a vital resource for anyone involved in the maintenance of the Cessna 414.

  • Follow the maintenance schedule strictly to ensure aircraft safety and reliability.
  • Perform routine inspections at specified intervals: 50-hour, 100-hour, and annual checks.
  • Utilize the troubleshooting section for efficient problem diagnosis and resolution.
  • Refer to component specifications for accurate maintenance of engines and avionics.
  • Adhere to safety precautions outlined in the manual to prevent accidents during maintenance.

Document

Source

Originally published by www.aerolifeaviation.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Maintenance Manual
Pages
50
File size
5.7 MB
Publisher
www.aerolifeaviation.com
How rare is it?
306CESSNA 414 registered worldwide · 251 active

Common. One of the most common aircraft types we track.

Documentation completeness
7/7

Full essential library on file for the CESSNA 414.

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In this document

Introduction

The introduction outlines the purpose of the manual, which is to serve as a comprehensive guide for the maintenance of the Cessna 414. It emphasizes the importance of following the procedures outlined to ensure safety and reliability.

Maintenance Schedule

This section provides a detailed maintenance schedule, including routine inspections and required maintenance tasks. It specifies intervals for checks, such as 50-hour, 100-hour, and annual inspections, ensuring that all necessary maintenance is performed timely.

Troubleshooting

The troubleshooting section offers systematic approaches to diagnosing issues with the aircraft systems. It includes flowcharts and checklists to assist technicians in identifying and resolving problems efficiently.

Component Specifications

Detailed specifications for various aircraft components are provided, including engines, avionics, and landing gear. This section ensures that maintenance personnel have access to critical information regarding parts and their maintenance requirements.

Safety Precautions

Safety precautions are highlighted throughout the manual, emphasizing the importance of following safety protocols during maintenance activities to prevent accidents and ensure the safety of personnel.

Safety notes

  • Always wear appropriate personal protective equipment (PPE) when performing maintenance tasks.
  • Ensure the aircraft is properly secured before beginning any maintenance work.
  • Follow all safety protocols to mitigate risks associated with aircraft maintenance.

Full document text

ITEM ENGINE ENGINE PROPELLER PROPELLER INSTALLED EQUIPMENT AIRCRAFT MAINTENANCE SERVICES A Division of Ararat Management N. 4680N Tack 1858.9 Work Order SERIAL NO. Date 322-0 R 3015 L R L C/W AD2005-12-13 part (f) by visual and internal insp. Ref: ETI Job # 06-105 No defects Noted-Due each 100 HR. ENGINE ENGINE PROPELLER Retain as permanent aircraft record. alte Acrestod Mike Aarestad AP 22227281A PROPELLER ENGINE ENGINE PROPELLER PROPELLER ENGINE ENGINE PROPELLER PROPELLER HOBBS: 1860, 1 TTAF:9244.4 3-30-04 C/W AD 2001- 01-16 (D) leftright exhaust system. No defects found. All slip joints lubed w/comosion X. RA..PS04889AND HORDS: 1800. 1 TTAF: 9244,4 3-30-06 clw FAR 91,2071d) eltops check satisfactory. Batteryd July 2006, FAR 91.707(2) de next 3-2007. Rug My APSORSAID- 03-30-06 N4680N S/N 414A0070 TTAF: 9244.4. Hobbs: 1860.1 DATE ΤΙ IN IN NO - Clean aircraft, perform pre-inspection operational check. Change BA22 induction filters. Inspect/lube and check tensions of flight control cables. Lube flaps and flap mechanisms, lube gear and check through several retractions, C/W with gear blow down check satisfactory, service hydraulics and nitrogen- next due 03-07. Clean fuel filters, check tanks for contamination-none found. ELT Battery due 06-06, c/w 91.207(d), next due 03-07. A.D. 2005-18-20 (appliance) does not apply, no BFG "FASTprop" deicers installed. C/W AD 2001-01-16(b) by visual inspection, LH and RH exhaust system, lube slip joints and wastegate w/ Corrosion X. C/W AD 2004-21-05 by pressure decay test-satisfactory, next due @ heater Hobbs of 961.3 or 03-07. C/W A.D.2004-25-16 by visual inspection of shut-off valve per Kelly Aerospace SL A-107-A next due @heater Hobbs of 961.3. A.D.s checked current- see tech log and engine log books for complete list. Operational and leak checks satisfactory. I certify that this aircraft has been inspected in accordance with an Annual/100 hour inspection per Cessna 414 Maintenance Manual rev. 34/and found to be in airworthy condition this date: 04-07-01 2 Si CE S/ Duane Mader A&P 503880317 IA DATE -DESCRIPTION OF ALTERATION THE TRANSPONDER (S) IDENTIFIED BELOW HAVE BEEN INSPECTED AND MEET ALI. REQUIREMENTS CONTAINED IN FAR 91.413 AND FAR 43 APPENDIX F. GX320A NO. 1 ENCODER S/N 83800664 I CERTIFY THAT THE ALTIMETER (S), ALT. REPORTING AND STATIC SYSTEM TEST REQUIRED BY FAR PART 91.411 HAVE BEEN PERFORMED. THE ALTIMETER (S) WERE TESTED TO NO. 1 35009 FEET ON DATE 3-306 Pilo S/N NO. 2 35000 NO. 2 S/N NIA NA S/N DATE 3-30.06 S/N WORK ORDER# A1130 INPECTOR TE DATE 350-06 RETEST DUE 308 INSPECTOR TE RETEST DUE 3-08 FEET ON DATE 3-30-06 MAINTENANCE RELEASE THE AIRCRAFT AND/OR COMPONENT IDENTIFIED WAS REPAIRED AND INSPECTED IN ACCORDANCE WITH CURRENT FEDERAL AVIATION REGULATIONS AND IS APPROVED FOR RETURN TO SERVICE. DETAILS ON FILE AT THIS AGENCY JOB NO. A30 SIGNED Tri-State DATE 3-30 02 Tri-State Avionics Rapid City, SD 57703 FAA CRS#V5XR381Y HOBBS 1860.1 04-07-06 c/w 400 HOUR ITEM - TTAF 9244.4 CHANGE HYDRAULIC FILTERS LSR USING NEW AN6235-ZA ELEMENTS, ANG246-27 SEAL RINGS & MS28775-222 O-RING SEALS. LEAK CHECK & HYD FLUID LOVEY CK. SATISFACTORY - SEE 8130-3'5 AFP503880317 DATE MAJOR ALTERATIONS DESCRIPTION OF ALTERATION L&D Aero Service, Inc. Chadron, NE Reg: N4680N Make: Cessna Model: 414A SN: 414A0070 Hour Meter 1910.1 Total Time: 9294.4 Date: 5/22/06 CW AD 00-01-16 Inspection of LH and RH exhaust systems and mounts. (End) Lester Mittleider A&P 3120137 6/22/06 HOBBS READS 1923.4 πTAF 9307,7 INSTALLED NEW PILOTS A/C BLOWER FAN, PIN HE81293-1 SIN 111goll, ODS CIC GOOD. hell 1948- 49584389 L&D Aero Service, Inc. Chadron, NE Reg: N4680N Make: Cessna Model: 414A SN: 414A0070 Hour Meter: 1930.8 Total Time: 9294.4 Date: 7/29/06 Installed props after OH installed new batteries in ELT, Tested and inspected IAW 91.207d and found ok. New Expiration Date 7/08 Lester Mittlelder A&P 3120137 L&D Aero Service, Inc. Rapid City, SD Reg. N4680N Make Cessna Model 414A SN: 414A0070 Hour Meter: 2105.5 Total Time: 9469.4 Date: 4/10/07 CW AD 00-01-01 inspection of LH and RH exhaust systems and mounts, lubed joints and found ok. (End) Lester Mittielder A&P 3120137 UN/E 4124 Registration N4680N DATE 2106 8-15 4655334 CW Varia ight 9 740 19 Tape Cicar Instal 13. tal 1 Verit In sp Rapla Registration DATE 8-18-2006 23 су 13ldg 53 Bismarck, ND 58504 MOBLE 414A6020 TSO 1065.8 CYCLES HOUR METER 1956.8 • W50 Phillips TOTAL TIM 9340.2 in WA m. Ok this date 150 He CAD of his date (560 Hr Vondlechen thenal un! external (de cach 100 EF Ok this date. Ref. ETI Inspection report 06-276 insp per EAR 94.207(d)k this date. Duc vach 12 Months: CW A2M in of Ok this date Thie esch 100 Aircraft hours. Co weigh sight caugural. anonim for info Aircraft was weighed with all seats 6 seals installed and in beste adres. A Lli windshield folicate $9.5 1: Cleaned and renew 12 Installed new deposit. 13. states hivi ni 14 15. weked at a car operation leaks. No defects found. grief gear In Beglecod the larks were unpl 17 Replaced engine 437 Adjusted to MEG specs. AIRCRAFT MANAGEMENT SERVICES 8523 Briardale Drive Bismarck, North Dakota 58504 Office: (701) 223-4754 N4680N Date 8-18-04 Tack or Hobby 1956.8 TT 9340.2 I certify that this Aircraft has been inspected IAW a 100 HR Howard BURNS AP501908274 Hounda inspection and was determined to be in an airworthy condition. REFWO 3305 LIFE LIMITED PARTS OR OVERHAUL REQUIREMENTS AME OF PART PART NUMBER SERIAL NUMBER INSTALLATION DATE/HOURS TIME ON PART AT INSTALL LIFE LIMIT OR T.B.O. REMOVAL DATE/HOURS AGENCY CERT. NO. 8/23/06 HOBBS 1956.8 INStalled New CABIN Entry Step INSTALLEDS 3 New 08/29/04 INter Connect LINK & Spring. V6's ON LEFF 2326 • AP 501908279 HOBBS 1958.7 REM AND REP RIH ENC VACWMPMP PIN 44266 INSITATED Newly Overhauled Akpo Acessivrisine op ck good. PAP SIN 42194 WOFF 5060. Kelintensey AA 9460727 A8A246 SIN OFF 113251. L&D Aero Service, inc. Chadron, NE Reg N4680N Make: Cessna Model: 414A SN: 414A0070 Hour Meter: 2005.1 Total Time: 9389.4

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Date: 10/11/06 CW AD 00-01-01inspection of LH and RH exhaust systems and mounts, lubed joints and found ok. (End) Lester Mittleider A&P 3120137 L&D Aero Service, Inc. Chadron, NE Reg. N4680N Make Cessna Model: 414A SN: 414A0070 Hour Meter: 1920.1 Total Time: 9304.5 Date: 6/12/06 Replaced Flight Attitude Ind. SN 1084 with OH unit SN 1303 and tested ok. Le Lester Mittleider A&P 3120137 MAINT SERVIC A Den of Arcraft Ma awadi Current + eich 1001 Retain as perman aircraft record. MAINTENANCE SERVICES A Denon of Arora Management System Tack 2055-0 Date 1-24-07 Work Order 3559 2005-12-13-eff 6.2205 Part (f) by eddy Current + VISUAL INS- Ok this dot - Due euch 100162 Ret ETI WITH 07.033 HAUL REQUIREMENTS LIFE LIMIT OR T.B.O. REMOVAL DATE/HOURS AGENCY CERT. NO. Retain as permanent aircraft record. ulike arutad Mike Aarestad AP 22227281A Reg N4680N L&D Aero Service, Inc. Rapid City, SD Maks Cessna Model: 414A SN: 414A0076 Hour Meter 2055.8 Total Time: 9439.2 Date: 2/2/07 Checked controls. cables. pulleys and lubed Checked wing and tail neice systems ano found ok inspected wing and tail group fittings. Checked fuel and electrical systems Removed and replaced Static inverter PN 9910293-2RX with OH'd unil from Cessna SN 971. Tested ELT as per 91.20 d and found ok Exp. date 7/08 Jacked aircraft for retract inspected landing gear wheels and brakes. Packed wheel bearings and greased gear, Inctalied new hyd. filters on both sides. Performed yearly landing gear blow down and found ok Serviced blow down bottle and hyd. reservoir Replaced left hyd pump with like pump SN 061121. Inspected heater mounting and installation CWAD's 04-21- 15 am: 04-25-16 R1 for fuel regulator and found ok. Replaced heater assembly and regulator with OH unit from Aircraft Heating Heater PN 02E17-1 SN 1176118 Heater Hobbs 967.0 CW AD 00-01-16 part D of exhaust systems for both engines. CW 6 month fire extinguisher and found ok. I certify that this aircraft has been inspected IAW an annual inspection !AW Cessna 414 Service manual and determined airworthy Little Lester Mittleider IA 3120137 ( UNIT O# 3771 gistration ON AIRCRAFT MANAGEMENT SERVICES 2301 University Dr. Bldg 53 Bismarck, ND 58504 DATE une 05. 2007 MFG. Cessna MODEL 414A S/N 414A-0070 TSO CYCLES HOUR METER 2152.6 ΤΌΤΑΙ, ΤΙΜΕ A.D./BULL. NUMBER 1. Performed eddy current and visual inspection per Cessna Service Bulletin MEB00-7 revision 2 to c/w AD 2005-12-13. No defects noted. Inspection due each 100 hours. See ETI w/o 07-201. Howard Burns, Jr. A&P 501908279 IA H L&D Aero Service, Inc. Rapid City, SD Reg: N4680N Make: Cessna Model: 414A SN: 414A0070 Hour Meter: 2155.5 Total Time: 9538.9 Date: 6/20/07 Checked controls, cable tensions, pulleys and lubed. Checked wing and tail deice systems and installed patch on right inboard wing root. Inspected wing and tail group fittings. Replaced missing vg on left wing. Checked fuel and electrical systems. CW AD 95-09-13 fuel tank floats and tested of ok. Due in 600hrs. Tested ELT as per 91.207 d and found ok Exp. date 7/08. Jacked aircraft for retract, inspected landing gear, wheels and brakes. Replaced both main tires with tires form Wilkerson tire. Packed wheel bearings and greased gear. Installed new brake linings on right main Inspected heater mounting and installation. CW AD 00-01-16 part b of exhaust systems for both engines. CW 6 month fire extinguisher and found ok. Installed new air filters both engines. I certify that this aircraft has been inspected IAW an annual inspection IAW Cessna 414 Service manual and determined airworthy. X Lester Mittleider IA 3120137 UN WO# Registi N4680N DA September 1 2 3456 7 84 6 A.D./BULL. ITEM NUMBER AFFECTED DATE & HRS. AT COMP. METHOD OF COMPLIANCE TYPE OF A.D. NEXT COMP. 1 TIME/RECUR. DATE/HRS./CYCLE L&D Aero Service, Inc. Rapid City, SD Reg: N4680N Make: Cessna Model: 414A SN: 414A0070 Hour Meter: 2205.2 Total Time: 9569.1 AUTHORIZED SIGNATURE CERTIFICATE NO. Date: 8/23/07 CW AD 00-01-01 Inspection of LH and RH exhaust systems and mounts, lubed joints and found ok. (End) UNIT WO #3981 Registration N4680N Lester Mittleider A&P 3120137 L AIRCRAFT MANAGEMENT SERVICES 2301 University Dr. Bldg 53 Bismarck, ND 58504 DATE September 29, 2007 MFG. Cessna MODEL S/N 414A 414A0070 TSO 1360.2 CYCLES HOUR METER 2250.4 TOTAL TIME 9634.7 1. C/W 100 hr inspection of this aircraft this date using Cessna's 414 series maintenance manual 2. Installed aircraft on a pressurization cart and inspected general areas. Repositioned clamp on heater 3. to allow ram air dump valve to fully close. Installed small amount of sealant to middle door seal. Cleaned both outflow and safety valve with isopropyl. Installed both new brake discs. PN on 164-20306 4. C/W AD2001-01-16 part (b) by inspecting complete exhaust systems Ok this date. due each 50 hr. 5. C/W AD2001-01-16 part (c) by inspection of both tailpipes. Ok this date. Due each 12 months. 6. C/W AD2001-01-16 part (e) by pressure test of all exhaust systems. Ok this date. Due each 12 months. 7. Verified AD2001-01-16 part (d) 500 hr inspection on canted bulkhead is due by 2458.8 Hobbs. 8. C/W AD2004-25-16 R1 inspection of heater fuel regulator. Ok this date. This inspection is due each 100 hrs of aircraft time in service 9. C/W AD2005-12-13 by inspecting both internal and external wing insp items. Ok this date. Ref ETI testing Job # 07-369. 11. Cleaned, inspected and greased all wheel bearings. 12. Installed new brake cylinder on RH side using new orings, linings and shim, back plate bolts. PN of cylinder is 061-05400. 13. Installed new tube inside RH tire. 14. Installed new boits in wheel halves, RH side. PN AN5-32A 15. Installed new AM1034351A filter for central vacuum system. recruly mat uns AIRCRAFI nas veeh inspected IA'w a 100 nr inspection and was determined to be in an Airworthy condition. Mike Aarestad A&P 2222728 IA Date: 12/3/07 and found ok. L&D Aero Service, Inc. Rapid City, SD Reg: N4680N Make: Cessna Model, 414A SN: 414A0070 Hour Meter: 2304.7 Total Time: 9668.6 CW AD 00-01-01 Inspection of LH and RH exhaust systems and mounts, lubed joints (End) Lester Mittleider A&P 3120137 AIRWORTHINESS VIRCUTIVE/FACTURI DULLETIN CUMPLIANCE RECORD A.D./ NUA Aircraft Log Book Entry, by Yingling Aircraft, Inc. For: Cessna 414A-0070, N4680N Complied with Cessna Service Bulletin # MEB03-01, by completion of the inspection and modification of the lower forward wing spar cap using modification kit # SK402-47B. Reference the Weight and balance supplement dated 02-05-08. Completed By Yingling Aircraft, Inc. P.O. Box 9248, Wichita, KS 67277 FAA CRS #YN8R621X Signature: 8/2 THE TRANSPONDER (S) IDENTIFIED BELOW HAVE BEEN INSPECTED AND MEET ALL REQUIREMENTS CONTAINED IN FAR 91.413 AND FAR 43 APPENDIX F. NO. 1 S/N G7X3.04 NO. 2 S/N NIA 8330064 ENCODER 30120 S/N 530053 Date Completed Work Order Number Recorded Hours TTAF 9702-7 02-05-08 SVC7551 2318.4 (MX) I CERTIFY THAT THE ALTIMETER (S), ALT. REPORTING AND STATIC SYSTEM TEST REQUIRED BY FAR PART 91.411 HAVE BEEN PERFORMED. THE ALTIMETER (S) WERE TESTED TO NO. 1 FEET ON DATE 3-20 P S/N NO. 2 FEET ON DATE 3 2008 S/N 30000 66258 39000 WORK ORDER# 1715 INPECTOR DATE 3-2008 RETEST DUE 310 MAINTENANCE RELEASE THE AIRCRAFT AND/OR COMPONENT IDENTIFIED WAS REPAIRED AND INSPECTED IN ACCORDANCE WITH CURRENT FEDERAL AVIATION REGULATIONS AND IS APPROVED FOR RETURN TO SERVICE. DETAILS ON FILE AT THIS AGENCY JOB NO. A175 SIGNED DATE 3 20.08 Tri-State Avionics Rapid City, SD 57703 FAA CRS#V5XR381Y AIRWORTHINESS DIRECTIVE/FACTORY BULLETIN COMPLIANCE RECORD A.D./BULL. NUMBER ITEM AFFECTED DATE & HRS. AT COMP METHOD OF COMPLIANCE TYPE OF A.D. NEXT COMP. 1 TIME/RECUR. DATE/HRS./CYCLE L&D Aero Service, Inc. Rapid City, SD Reg: N4680N Make: Cessna Model. 414A SN: 414A0070 Hour Meter: 2344.1 Total Time: 9728.4 AUTHORIZED SIGNATURE CERTIFICATE NO. Date: 3/25/08 Checked controls, cable tensions, pulleys and lubed. Performed trim tab actuator inspection and replaced aileron trim tab actuator screw with new PN 0310362-5 and rigged. Inspected wing and tail group fittings. Checked fuel and electrical systems. Replaced deice light in left nacelle. Installed new circuit breaker PN 7277-5-10 for right landing light. Tested ELT as per 91.207d and found ok Exp. date 7/08. Jacked aircraft, replaced shims, bolts and bushing as required in all main gears as per service manual. Repaired minor crack on nose gear attach bracket as required. Performed gear retraction and blow down. Packed wheel bearings and greased gear. Inspected heater mounting and installation, CW AD 2004-25-16R1 inspection of regulator shutoff valve and found ok. Heater Hobbs 1104.1 CW AD 00-01-16 part b of exhaust systems for both engines. CW 6 year fire extinguisher recharge and weight. Installed new air filters both engines. Replaced vac pump on right engine with OH'd SN 55852 from Aero Accessories. I certify that this aircraft has been inspected IAW an annual inspection IAW Cessna 414 Service manual and determined airworthy. (END) Cessna 414A Hobbs 2361.3 N4680N Lester Mittleider IA 3120137 S/N 414A970 TT 97.15.2 6/9/08 Removed right hand wastegate controller and wastegate p/n 470908-13, s/n FF000192 and installed overhauled unit from Approved Turbo Components p/n 470908-13, s/n FCO111. Run up leak ck ok, Flight check ok. Josh Hartung AP2751095 Josh Carking TT 9758.8 8/13/08 Inspected aircraft and found to be in an airworthy state for ferry flight from Rapid City, SD (KRAP) to Greely, CO (KGXY) HODDS 2374.5 Josh Hartung AP2751095 Josh Hartung | || - A.D./B NUME Beegles Aircraft Service, Inc. Quality Service Since 1946 GREELEY, CO REPAIR STATION BX4R092M (970) 353-9200 09-12-08 Hobbs 2375.80 Tach 9760.1 N4680N sn 414A0070 Disassembled aircraft - removed: Rudder. Repaired LH wing: Replaced trailing edge rib pn 5122053-133 at Station 106.79. Repaired corrosion on trailing edge skin pn 5122053-93 at Station 106.00. Replaced corroded fasting rivets on lower nacelle fairing. Replaced working rivets at main landing gear hinge attach area. Repaired corrosion on trailing edge rib pn 5122053-35 at Station 87.29. Replaced working rivets on LH wing tip at Station 230.00. Replaced or re-shot miscellaneous working rivets. Repaired RH wing: Replaced working rivets on RH wing tip at Station 230.00. Replaced working rivets at main landing gear hinge attach area. Replaced or re-shot miscellaneous working rivets. Repaired rudder: Replaced rib pn 5133000-106. Replaced aft spar channel pn 5133000-20. Replaced LH lower side skin pn 5133000-64. Replaced RH lower side skin pn 5133000-22. Performed painted static balance check. Results: -2.4 inch lbs. Range is .75 to -3.75 inch lbs. Repaired landing gear: Replaced LH main landing gear door hinges pn's 5122115-27 and 5127050-15, pin pn S488570. Replaced RH main landing gear door hinges pn's 5122115-27 and 5127050-15, pin pn S488570. Performed retraction and extension cycle of landing gear system. Repainted repairs as required to match. Reassembled aircraft: Reinstalled rudder. Performed operational check. Replaced ELT battery pn BS2173, replacement battery due 09/2110. Performed operational check per FAR 91.207, Para d. Di Pe Sign 9/29/05 This aircraft was repaired and inspected in accordance with current regulations of the Federal Aviation Administration and is approved for return to service. LIMITED TO THE WORK PERFORMED Pertinent details on file at Beegles Aircraft Service, Inc., Greeley, CO. Work Order # 10,985 CRS# BX4R092M Signed Date 9-12-08 + Tach 2375.8 N 46800 Performed operational test flight in accordance with FAR 91.407 Paragraph (b). Signed Пат да 9/29/08/2885.1 Complied with AD 2000-01-06 para ( by removing & insp. tailpiper Complical with 6 month five extinguisher weighing, Josh Hastung AP275 1095

Type certificate, explained

What's in the CESSNA 414 TCDS

A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.

TCDS A7CERev 47· Issued 2007
Read the full TCDS

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