Weight & Balance for Cessna 172RG Cutlass
Cessna 172RG Cutlass · Weight And Balance
Overview
This document provides essential weight and balance information for the Cessna 172RG Cutlass. It is designed for pilots and aviation enthusiasts to ensure safe operation within the aircraft's weight limits. The document outlines the maximum weight capacities, loading configurations, and methods for calculating weight and balance to maintain aircraft performance and safety. Understanding these parameters is crucial for flight planning and compliance with regulatory standards.
- Maximum takeoff weight: 2,550 lbs
- CG limits: 34.0 to 40.0 inches from the datum
- Weight and balance calculations are essential for safe flight
- Proper loading and weight distribution are critical
- Use the provided sample form for documentation
Document
Source
Originally published by www.skyservices-flightacademy.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Weight And Balance
- Pages
- 14
- File size
- 1007 KB
- Publisher
- www.skyservices-flightacademy.com
Specifications & performance
Extracted from this document.
Specifications
- Engine (hp)
- 180
- Length (ft)
- 27
- Propeller
- CONSTANT SPEED
- Wingspan (ft)
- 36
- Engine model
- LYCOMING 0-360-F1A6
- Empty weight (lb)
- 1,490
- Max takeoff weight (lb)
- 2,550
Weight & balance
- Useful load (lb)
- 1,060
- Max ramp weight (lb)
- 2,550
- Basic empty weight (lb)
- 1,490
- Max landing weight (lb)
- 2,550
- Max takeoff weight (lb)
- 2,550
Common. Rarer than 2% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Cessna 172RG Cutlass.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the 172RG Cutlass RG to your watchlist and track it in one place.
More Cessna 172RG Cutlassmanuals & documents
See all 20 →- 180 HP STC Jan 31/22 UPDATEAirworthiness Directives
- NORMAL CHECK LIST C172RG NORMAL CHECK LIST C172RGChecklist
- Cessna 172RG Cutlass Standardization ManualPilot's Operating Handbook
- Garmin G1000 NXi Pilot’s Guide for the Cessna Nav IIIV Speeds Reference
- Garmin G1000 NXi Pilot’s Guide for the Cessna Nav IIIV Speeds Reference
- Ground handling accident involving Cessna 172RG, VH-MKGOther Documents
- Cessna 172RG CHECKLISTChecklist
- Supplemental Airplane Flight ManualOther Documents
- Garmin G1000 Pilot’s Guide for Cessna Nav IIISystems Description
- Data Sheet - Cessna 172RGType Certificate
- G1000 NAV III LINE MAINTENANCE MANUALMaintenance Manual
- Density Altitude and YouPerformance Data
If you fly the Cessna 172RG Cutlass, you may also be researching these.
In this document
Maximum Weight Limits
The maximum takeoff weight for the Cessna 172RG Cutlass is 2,550 lbs. This includes the weight of the aircraft, passengers, cargo, and fuel. Pilots must ensure that the total weight does not exceed this limit to maintain safe flight operations.
Center of Gravity (CG) Limits
The CG limits for the Cessna 172RG Cutlass are between 34.0 inches and 40.0 inches from the datum. Proper loading is essential to keep the CG within these limits for safe handling and performance.
Weight and Balance Calculation
To calculate weight and balance, pilots must record the weight of each item, including passengers and baggage, and their respective arm (distance from the datum). The total moment is calculated by multiplying the weight by the arm, and the CG is determined by dividing the total moment by the total weight.
Loading Instructions
The document provides detailed loading instructions to ensure that the aircraft is loaded correctly. It emphasizes the importance of distributing weight evenly and securing all cargo to prevent shifting during flight.
Sample Weight and Balance Form
A sample weight and balance form is included to assist pilots in documenting their calculations. This form should be filled out prior to each flight to ensure compliance with weight and balance requirements.
Safety notes
- Ensure total weight does not exceed maximum limits
- Maintain CG within specified limits for safe handling
Full document text
PILOT'S OPERATING HANDBOOK and FAA APPROVED AIRPLANE FLIGHT MANUAL 0 CESSNA AIRCRAFT COMPANY THIS DOCUMENT MUST BE CARRIED IN THE AIRPLANE AT ALL TIMES. 1980 MODEL 172RG Serial No. 172R60002 Registration No. 4/4597R Assegnato all'a/m 1-PVLB THIS HANDBOOK INCLUDES THE MATERIAL REQUIRED TO BES FURNISHED TO THE PILOT BY CAR PART 3 AND CONSTITUTES THE FAA APPROVED AIRPLANE FLIGHT MANUAL. 31/3/00 Member of GAMA COPYRIGHT © 1979 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA 1 JULY 1979 EQUIPMENT LIST WEIGHT & BALANCE/ 2 ENGINE INSTRUMENTS LIMITATIONS سسس IN: m IN: Kg/m 0,292 0,526 Vhf-Com/Nav KX155 by NL NORMAL 1,800 Vhf-Com/Nav KX165A TEMPORARY REVISIONS MODEL 1980 172RG U.S. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Model 1980 172RG Airplanes 172RG0001 thru 172RG0570 THIS IS A LIST OF ALL CURRENT FAA APPROVED TEMPORARY REVISIONS. The following list of temporary revisions must be incorporated into this basic U.S. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual until the removal instructions have been complied with. Insert this page opposite the Log of Effective Pages in the front of this basic U.S. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual. TEMPORARY REVISION NUMBER PAGE NUMBER ISSUE DATE D1174 2 TR01 D1174 2 TR02 2-5 2-6 D1174 2 TR03 7-19 SERVICE BULLETIN, MODIFICATION KIT (IF APPLICABLE) OR SERIAL EFFECTIVITY 10/8/09 Airplanes 172RG0001 thru 172RG0570. 10/8/09 Airplanes 172RG0001 thru 172RG0570. 10/8/09 Airplanes 172RG0001 thru 172RG0570. ENGINE INSTRUMENTS Vhf-Com/Nav KX165A SNOW 2 CAD3. TIMON SMOMENTO DENOMINAZIONE IN: Kg 1.800 IN: m 0,292 IN: Kg/m 0,526 IN: Kg Vhf-Com/Nav KX155 490. 0.292 -0,727 CESSNA IL 172RG NS CESSNA MODEL 172RG KNOTS KNOTS M RS M ជួន៥ន 'M FT COVERAGE/REVISIONS/ LOG OF EFFECTIVE PAGES COVERAGE The Pilot's Operating Handbook in the airplane at the time of delivery from Cessna Aircraft Company contains information applicable to the 1980 Model 172RG airplane designated by the serial number and registration number shown on the Title Page of this handbook. REVISIONS Changes and/or additions to this handbook will be covered by revisions published by Cessna Aircraft Company. These revisions are distributed to all Cessna Dealers and to owners of U. S. Registered aircraft according to FAA records at the time of revision issuance. Revisions should be examined immediately upon receipt and incorporated in this handbook. NOTE It is the responsibility of the owner to maintain this handbook in a current status when it is being used for operational purposes. Owners should contact their Cessna Dealer whenever the revision status of their handbook is in question. A revision bar will extend the full length of new or revised text and/or illustrations added on new or presently existing pages. This bar will be located adjacent to the applicable revised area on the outer margin of the page. All revised pages will carry the revision number and date on the applicable page. The following Log of Effective Pages provides the dates of issue for original and revised pages, and a listing of all pages in the handbook. Pages affected by the current revision are indicated by an asterisk (*) preceding the pages listed. LOG OF EFFECTIVE PAGES Dates of issue for original and revised pages are: Original Revision 1 Revision 2 1 July 1979 15 July 1983 1 December 1983 Page Date Page iv Title Assignment Record i thru ii 1-1 thru 1-9 1-10 Blank 2-1 2-2 Blank 2-3 thru 2-4 *2-5 thru 2-6 2-7 2-8 2-9 thru 2-11 2-12 Blank 3-1 thru 3-19 3-20 Blank 4-1 thru 4-11 1 December 1983 1 July 1979 6-1 1 July 1979 6-2 Blank.... 1 July 1979 1 December 1983 1 July 1979 1 July 1979 1 July 1979 1 July 1979 1 july 1979 1 July 1979 1 July 1979 15 July 1983 1 July 1979 1 July 1979 1 July 1979 1 July 1979 6-3 thru 6-13 6-14 Blank... 6-15 thru 6-17 *6-18.... 6-19 thru 6-23 6-24 Blank 7-1 thru 7-18 *7-19 7-20 thru 7-46 8-1 8-2 Blank 8-3 thru 8-13 8-14 8-15 thru 8-17 8-18 Blank Date 1 July 1979 1 July 1979 1 July 1979 1 july 1979 1 July 1979 1 December 1983 July 1979 1 July 1979 1 July 1979 December 1983 July 1979 1 July 1979 1 July 1979 1 July 1979 15 July 1983 1 July 1979 1 July 1979 1 July 1979 9-1 thru 9-2 1 July 1979 4-12 Blank 1 July 1979 4-13 thru 4-24 1 July 1979 NOTE 5-1..... 1 July 1979 5-2 Blank 1 July 1979 5-3 thru 5-27 July 1979 5-28 Blank 1 July 1979 Refer to Section 9 Table of Contents for supple- ments applicable to optional systems. 1 July 1979 Revision 21 December 1983/D1174-2-13PH-RPC-1000-5/84 iii NORMAL ENGINE INSTRUMENTS LIMITATIONS 2 EQUIPMENT LIST WEIGHT & BALANCE/ PESO DENOMINAZIONE Vhf-Com/Nav KX155 IN: Kg -2.490. 0.292 ACCIO | MOMENTO IN m IN: Kg/m 0,526 IN Kg 1,800 Vhf-Com/Nav KX165A ས་སྲསམསྐྱག་བརྫྙྰ་བས་ཞ་ ་ ས ས ག ཞ ། ་ CESSNA MODEL 172RG SECTION 6 WEIGHT & BALANCE/ EQUIPMENT LIST EQUIPMENT LIST The following equipment list is a comprehensive list of all Cessna equipment available for this airplane. A separate equipment list of items installed in your specific airplane is provided in your aircraft file. The following list and the specific list for your airplane have a similar order of listing. This equipment list provides the following information: An item number gives the identification number for the item. Each number is prefixed with a letter which identifies the descriptive grouping (exam- ple: A. Powerplant & Accessories) under which it is listed. Suffix letters identify the equipment as a required item, a standard item or an optional item. Suffix letters are as follows: -R = required items of equipment for FAA certification -S = standard equipment items -O= optional equipment items replacing required or standard items -A = optional equipment items which are in addition to required or standard items A reference drawing column provides the drawing number for the item. NOTE If additional equipment is to be installed, it must be done in accordance with the reference drawing, accessory kit instruc- tions, or a separate FAA approval.
Show full textShow less
Columns showing weight (in pounds) and arm (in inches) provide the weight and center of gravity location for the equipment. NOTE Unless otherwise indicated, true values (not net change values) for the weight and arm are shown. Positive arms are distances aft of the airplane datum; negative arms are distan- ces forward of the datum. NOTE Asterisks (*) after the item weight and arm indicate complete assembly installations. Some major components of the assem- bly are listed on the lines immediately following. The summa- tion of these major components does not necessarily equal the complete assembly installation. о 1 July 1979 6-15 6-16 ITEM NO SECTION 6 EQUIPMENT LIST WEIGHT & BALANCE/ 302.5 -22.5 EQUIPMENT LIST DESCRIPTION REF DRAWING WT LBS ARM INS A. C294510-0501 1.0 -11.0 C611503-0102 10.7 -32.0 C161008-0111 55.8 -43.7 C161031-0112 3.0 -32.5 2450002 3.4* -43.8* 2.3 -46.4 2406001 4.3* C431003-0101 1.8 1201075 0.2 -2.3* -10.7 4.7 C668509-0101 0.1 16.2 C482001-0401 4.5 -12.0 A01-R ▼A05-R ☑A09-R A33-R A37-R VA41-R A61-S VATO-S VA73-0 B01-R ENGINE, POWERPLANT & ACCESSORIES LYCOMING 0-360-F1A6 (INCLUDES ELECTRIC STARTER, VACUUM PAD AND OIL FILTER FILTER, INDUCTION AIR ALTERNATOR, 28 VOLT 60 AMP PROPELLER, CONSTANT SPEED GOVERNOR, PROPELLER SPINNER INSTALLATION SPINNER DOME VACUUM SYSTEM INSTALLATION VACUUM PUMP FILTER GAUGE RELIEF VALVE & REGULATOR PRIMER SYSTEM, ENGINE (3 CYLINDER) DIL QUICK DRAIN VALVE (NET CHANGE) 8. LANDING GEAR & ACCESSORIES WHEEL, BRAKE & TIRE ASSEMBLY, 15X6.00X6 MAIN (SET OF 2) WHEEL ASSEMBLY (EACH) 2450000 2450000 1701015 C16301980203 36.4* 58.5* BRAKE ASSEMBLY (LEFT) BRAKE ASSEMBLY (RIGHT) TIRE, 6-PLY BLACKWALL (EACH) TUBE (EACHI B04-R WHEEL & TIRE ASSEMBLY, NOSE 0163006-0101 C163032-0115 0163032-0116 C262006-0101 C262026-0101 C163018-0104 59.0 54.5 1.9 54.5 6.6 59.0 1.2 8.6* WHEEL ASSEMBLY, MCCAULEY $1 TIRE, 6 PLY BLACKWALL TUBE C163005-0201 C262003-0202 C262023-0101 2.4 1 July 1979 C. ELECTRICAL SYSTEMS COL-R BATTERY, 24 VOLT (STANDARD CAPACITY) 0614002-0101 23.2 130.0 MODEL 172RG CESSNA : MODEL 172RG CESSNA SECTION 6 WEIGHT & BALANCE/ EQUIPMENT LIST ITEM NO 001-0 ✓C04-R C07-A ✓016-0 022-A EQUIPMENT LIST DESCRIPTION BATTERY, 24 VOLT (HEAVY DUTY) ALTERNATOR CONTROL UNIT WITH LOW VOLTAGE SENSING HEATED PITOT SYSTEM (NET CHANGE) MAP (REQUIRES E89-11 C614002-0102 C611005-0101 2401005 0422355-7 2413120 REF DRAWING WT LBS ARM INS 25:2 25.2 GROUND SERVICE PLUG RECEPTACLE 2.7 0.6 130.0 3.4 126.0 24.4 C25-A LIGHTS, INSTRUMENT POST (REQUIRES E34-0). LIGHT INSTALLATION, CONTROL WHEEL MOUNTED. 0.5 0501068 0.1 17.3 21.5 LIGHT INSTALLATION. MAP & INSTRUMENT 0700149 0.3 32.0 31-A ☑C40-A 043-A 0521101 0.5 61.0 0701013 0.0 2406002 1.4* 204.7* C621001-0102 C594502-0102 0.4 242.5 0.6 205.1 0501027-1 0.2. 3.4* 208.3 43.3* C622008-0102 2.3 47.0 C622006-0107 0.2 40.8 0501032 -18.6 VC28-S 046-A C49-S 001-R ▼D04-A 1001-0 007-R 007-0-1 ✓ 007-0-2' D10-A 016-A-1 ✓ 016-A-2 022-A 025-S ✓025-0 FLOOD DOORPOST MOUNTED LIGHTS, COURTESY (SET OF TWO) DETECTORS NAVIGATION LIGHT (SET OF TWO) LIGHT INSTALLATION, OMNIFLASH BEACON BEACON LIGHT IN FIN TIP FLASHER POWER SUPPLY IN VERTICAL TAIL ☐ RESISTOR - MEMCOR (7174) LIGHT INSTALLATION, WING TIP STROBE FLASHER POWER SUPPLY, WING TIP RIB (2) STROBE LIGHT,WING TIP (SET OF TWO) LIGHTS, LANDING, COWL MOUNTED - DUAL BULB D. INSTRUMENTS INDICATOR, AIRSPEED INDICATOR, TRUE AIRSPEED STATIC AIR, ALTERNATE SOURCE ALTIMETER, SENSITIVE (INCHES OF MERCURY) ALTIMETER, SENSITIVE (FEET & MILLIBARS) (50 FT. MARKINGS) ALTIMETER, SENSITIVE (FEET & MILLIBARS) (20 FT. MARKINGS) ALTIMETER INSTALLATION - DUAL ALTIMETER, ENCODING (REQUIRES RELOCATION OF REGULAR TYPE ALTIMETER) ALTITUDE ENCODER (BLIND, DOES NOT REQUIRE INSTRUMENT PANEL MOUNTING) ENCODER GAGE, CARBURETOR AIR TEMPERATURE CLOCK, ELECTRIC (DIAL READOUT) CLOCK, ELECTRIC (DIGITAL READOUT OR95-6 C661064-0108 0.6 16.0 2401012 0.7 16.3 0501017 0.2 15.5 C661071-0101 C661071-0102 0.7 0.7 14.0 14.0 C661025-0102 0.7 14.0 2001015 0501049 9-8 1.5* 14.0 14.8 14.4* 14.6 14.0 16.3 2401009 C744001-0101 S-1311-4 C664508-0102 C664511-0101 1.3. 0.3 16.3 1 July 1979 6-17 6-18 t : C669560-0108 airplanes modified Service Kit SK172-85. ITEM NO 028-R ▼038-R 041-R 043-R ✓ 049-A * 055-R ▼064-S 064-0 №067-A ☑082-S D85-R ✓688-5-1 088-5-2 088-0 ✓ 091-A E05-R E05-0 E07-S ▼E07-0 ▼E09-S E09-0 E15-R E19-0 EQUIPMENT LIST DESCRIPTION COMPASS INSTALLATION, MAGNETIC INSTRUMENT CLUSTER, LH & RH FUEL INSTRUMENT CLUSTER, CYL HEAD TEMP OIL TEMP INSTRUMENT CLUSTER, AMMETER & OIL PRES INDICATOR, ECONOMY MIXTURE (E.G.T.) GAGE, MANIFOLD PRESSURE GYRO INSTALLATION, ATTITUDE & DIRECTIONAL (NON NAV-O-MATIC) DIRECTIONAL INDICATOR ATTITUDE INDICATOR GYRO INSTALLATION FOR 300 NAV-O-MATIC DIRECTIONAL INDICATOR ATTITUDE INDICATOR RECORDER, FLIGHT HOUR (ARC) GAGE, OUTSIDE AIR TEMP (C668507-0101) TACHOMETER INSTALLATION RECORDING TACH HEAD TURN COORDINATOR (28 VOLT OPERATION) TURN COORDINATOR (10 TO 30 VOLT) COORDINATOR (FOR AUTO-PILOT USE) TURN INDICATOR, VERTICAL SPEED REF DRAWING WT LBS ARM INS 0513262 26.0 C669562-0101 C669561-0101 16.2 0.4 16.2 *C669560-0101 0.5 16.2 2401008 0.6 7.8 C662035-0104 2406001 1.1 16.5 13.6* C661075-0104 C661076-0101 2406001 40760-0104 0501052 C661076-0101 0500221 2406000 0668020-0124 C661003-0505 C661003-0506 42320-0028 C661080-0101 NNOMNOOHI 13.4* 14.3 14.3 6.3 28. 1.0* 0.6 1.3 15.5 15.8 1.3 15.8 1.3 15.8 1.0 15.7 SECTION 6 EQUIPMENT LIST WEIGHT & BALANCE/ Optional litude ind. RCA 26-BKZ (murch 2005) removed Sept. 2009 E. CABIN ACCOMMODATIONS SEAT. ADJUSTABLE FORE & AFT, PILOT SEAT, INFINITE ADJUSTING, PILOT SEAT, ADJUSTABLE FORE & AFT, CO-PILOT SEAT, INFINITE ADJUSTING, CO-PILOT SEAT, REAR (ONE PIECE BACK CUSHION) SEAT, REAR (TWO PIECE BACK CUSHION) BELT ASSEMBLY, PILOT LAP SHOULDER HARNESS ASSEMBLY, PILOT 0514168 0514171 0514168 0514171 ++. 12.6 23.0 44.0 41.5 0514169 0514143 22.0 79.5 23.0 S-2275-103 1.0' 79.5 37.0 S-2275-201 0.6 37.0 €23-S E27-S E27-0 E33-0 E34-0 E35-A-1 INERTIA REEL-SEAT BELT INSTALLATION, PILOT & CO-PILOT (NET CHANGE) BELT & SHOULDER HARNESS ASSY. CO-PILOT SEAT BELT ASSEMBLY, REAR (SET OF TWO) BELT & SHOULDER HARNESS ASSY, 2ND ROW (2) CARPETING, BLACK, NET CHANGE FOR STANDARD DELUXE GLARESHIELD (NET CHANGE) SEAT COVERING, VINYL, NET CHANGE 0501046-1 2.0 82.0 S-2275-3 1.6 37.0 S-1746-13 2.0 70.0 S-2275-8 3.2 70.0 0515034 0.0 1.0 21.0 MODEL 172RG CESSNA 1 July 1979 Revision 2 - 1 December 1983 1 July 1979 EQUIPMENT LIST DESCRIPTION 10 REF DRAWING WT LBS ARM INS CES-1151 ₤35-A-2 SEAT COVERING, LEATHER, NET CHANGE E37-A WINDOW, RIGHT DOOR HINGED (NET CHANGE) E39-A VE43-A WINDOWS, OVERHEAD CABIN TOP (NET INCREASE) VENTILATION SYSTEM, REAR SEAT E49-A -E50-A CUP HOLDER, RETRACTABLE (SET OF TWO HEADREST, FRONT (SET OF TWO HEADREST, REAR (SET OF TWO) ITEM NO MODEL 172RG CESSNA 0501075 0511800 0.9 47.9 0700322 1.7 50.9 0501023 0.1 15.5 1215073 1.5 47.0 1215073 86.0 0514166 0.9 32.8 0500267 0.0 2015009-8 95.0 2401010 2401007 12.4* 2.0 26.0 2467000-1 1.1 6.8 0513290 1.9 0501072 0501068 10.0 0.0 9.4 100.0 " 0005 0000 0505087 0505087 DAY- 0505087 0.0 1270733 0.5 E51-A E55-S VE57-0 E65-R E71-A E85-A SUN VISORS (SET OF 2) TINTED GLASS (ALL AROUND) (NET CHANGE} BAGGAGE TIE DOWN NET RINGS, CARGO TIE DOWN CONTROLS, DUAL (CO-PILOT'S WHEEL, PEDALS AND TOE BRAKES} CONTROL WHEEL WITH PROTECTIVE PADDING RUDDER PEDAL (SET OF TWO RUDDER TRIM SYSTEM CABIN AIR CIRCULATING FAN (CANNOT BE USED WITH E43-A) E87-S E88-A E89-A ALL PURPOSE CONTROL WHEEL NET CHANGE F01-R F01-0-1 ✓ 301-0-2 F07-R MF10-S P10-0-1 F10-0-2 16-R F. PLACARDS, WARNINGS & MANUALS PLACARD, OPERATIONAL LIMITATIONS VER DAY PLACARD, OPERATIONAL LIMITATIONS VFR DAY- PLACARD, OPERATIONAL LIMITATIONS NIGHT NIGHT STALL & GEAR WARNING BLACKBOX (REQUIRES ITEM H61-R FOR AUDIBLE OPERATION) PILOTS CHECK LIST (STANDARD A/C)(STOWED) PILOTS CHECK LIST (200A NAV-O-MATIC) PILOTS CHECK LIST (300A NAV-O-MATIC) PILOT'S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL G. AUXILIARY EQUIPMENT 6-19 G07-A RINGS, AIRPLANE HOISTING D1174-13PH SECTION 6 EQUIPMENT LIST WEIGHT & BALANCE/ HIF 111 0541115 1.1 49.1 ITEM NO EQUIPMENT LIST DESCRIPTION CORROSION PROOFING, INTERNAL STATIC DISCHARGER INSTALLATION (SET OF 101' STABILIZER ABRASION BOOTS Q13-A 16-A 619-A G22-S TOW BAR (STOWED) G25-$ G31-A 655-A-1 PAINT SCHEME, OVERALL EXTERIOR COVER OVERALL BASE WHITE STRIPE COLOR SCHEME CABLES, CORROSION RESISTANT CONTROL (NET CHANGE) FIRE EXTINGUISHER, STANDARD SEATING G55-A-2 FIRE EXTINGUISHER, VERTICAL ADJ SEAT STEPS AND HANDLE, REFUELING G58-A 667-A G88-A ☑HOI-A H04-A H05-A H07-A RUDDER PEDAL EXTENSIONS, REMOVABLE - SET OF 2 (STOWABLE - INSTALLED ARM SHOWN) (NOT FACTORY INSTALLED) WINTERIZATION KIT INSTALLATION, ENGINE COVER PLATE, FWD COWL (INSTALLED) COVER PLATE, FWD COWL (STOWED) H. AVIONICS & AUTOPILOTS CESSNA 300 ADF INSTALLATION CONSISTS OF-- RECEIVER WITH BFU (R-546E-1} INDICATOR LIN-346A) SENSE ANTENNA INSTALLATION LOOP ANTENNA INSTALLATION REF DRAWING WT LBS ARM INS 2401006 10.0 77.0 0501048 0.4 143.2 0500041 2.7 206.0 0501019 1.6 95.0 2404001 12.5* 90.4* 11.6 90.5 0.5 88. 0500036 0.0 2401011-1 2401011-2 2413123 0701048 Vedasi foto copia RECEIVER MOUNT, WIRES AND MISC ITEMS DME INSTALLATION, NARCO TRANSCEIVER COME-190) MOUNT ASSY ANTENNA FOSTER 511 R-NAV INSTALLATION RECEIVER & MOUNT CESSNA 400 GLIDESLOPE (INCLUDES VORTILS INDICATOR--NET CHANGE FOR VOR/LOC) RECEIVER (R-4438) ANTENNA (LOCATED UPPER WINDSHIELD) VOR/ILS INDICATOR (IN-386A)(INDICATOR WT NET CHANGE, ACTUAL WT IS 1.7 LBS) 3910159-25 41240-0001 8.0* 40980-1001 3.3 0.9 0570400-632 -- 3910166-14 3312-406 3910203-18 3910157-18 42100-0000 1200098 46860-2000 8.0 SECTION 6 EQUIPMENT LIST WEIGHT & BALANCE/ 1.0* 0.4 0.4 -24.3* -32.0 95.0 nuove configurazione 3.4* 4 9* DON 0-1 19.9* 12.1 14.0 108-6 39.3 13.7 18.5* 11.3 11.3 86.1 11.8* 14.5 105.6* 133.9 30.0 14.7 Висса 19.12.00 MQDEL 172RG CESSNA 6-20 1 July 1979 MODEL 172RG CESSNA SECTION 6 WEIGHT & BALANCE/ EQUIPMENT LIST ITEM NO M08-A-1 H08-A-2 EQUIPMENT LIST DESCRIPTION REMOTE RECEIVER SHELF INSTALLATION AUTO RADIAL CENTERING INDICATOR (ARC/LOC) EXCHANGE FOR VOR/LOC INDICATOR IN ITEM H22-A AND H25-AT NET CHANGE ARC/LOC INDICATOR ADDED VOR/LOC INDICATOR DELETED AUTO BADIAL CENTERING INDICATOR (ARC/ILS) EXCHANGE FOR VOR/ILS INDICATOR USED WITH H07-A ONLY (WT NET CHANGE) ARC/ILS INDICATOR ADDED VOR/ILS INDICATOR DELETED H11-A-1 RACK IS REQUIRED IF NOT PREVIOUSLY H11-A-2 VH13-A 416-A-1 416-A-2 VH22-A PANTRONICS PT10-A HF TRANSCEIVER REMOTE INSTALLED WITH REMOTE RACK REQUIRED WITH NO REMOTE RACK TINSTALLED W/H07-A. TRANSCEIVER (PANEL MOUNTED) ANTENNA LOAD BUX HF POWER SUPPLY (REMOTE) POWER SIGNAL CABLES ANTENNA INSTALLATION, 351 IN. LONG SUNAIR ASB-125 HF TRANSCEIVER, 2ND OR 3RD UNIT (REMOTE RACK IS REQUIRED IF NOT PREVIOUSLY INSTALLED WITH REMOTE UNIT RACK WITH NO REMOTE UNIT RACK ANTENNA LOAD BOX POWER SUPPLY (REMOTE) TRANSCEIVER (PANEL MOUNTED) ANTENNA INSTALLATION, 351 IN. LONG CESSNA 400 MARKER BEACON RECEIVER (R-402A) ANTENNA, L SHAPED ROD CESSNA 300 TRANSPONDER TRANSCEIVER (RT-359A) ANTENNA CESSNA 400 TRANSPONDER TRANSCEIVER (RT-459A) ANTENNA CESSNA 300 NAV/COM 720 CH COM 1ST UNIT (REQUIRES_H34-A TO BE OPERATIONAL). RECEIVER-TRANSCEIVER (RT-385A} 6:2 REF DRAWING WT LBS ARM INS 3940266-1 3910196-1 134.6. 14.7* 46860-1200 1.8 14.7 46860-1000 -1.6 14.7 3910196-2 0.1* 46860-2200 46860-2000 3910193-26 C582103-0102 C589502-0201 C582103-0301 3950149 3960117 3910158-43 99816 99683 99681 3960117 3910164-18 42410-5128. 0770681-1 3910127-29 41420-0028 42940-0000 3910128-28 41470-1028 281 22.8* 21.8* Vatromol ་་་་ 324840200420420® 14.7* مومو 97.0* 95.3* 10.4 131.9 139.5 62.0 137.5 0.3 2.3* 0.7. 99.7* 98.1* 132.0 139.5 10.4 137.5 34.5* 11.8 136.0 25.8* 11.1 127.0 25.1* 11.1 127.0 11.9* .0* 42940-0000 3910183 46660-1000 5.5 11.5 1 July 1979 6-21 SECTION 6 EQUIPMENT LIST WEIGHT & BALANCE/ MODEL 172RG CESSNA i ITEM NO #25-A EQUIPMENT LIST DESCRIPTION .95. VOR/LOC INDICATOR (IN-385A) MOUNT, WIRING & MISC ITEMS CESSNA 300 NAV/COM 720 CH COM ✰ REF DRAWING WT LBS ARM INS 3866 46860-1000 2ND UNIT 3910183 14.7 .2 8.3* (REQUIRES H37-A TO BE OPERATIONAL) RECEIVER-TRANSCEIVER (RT-385A) VOR/LOC INDICATOR LIN-385A) MOUNT, WIRING & MISC ITEMS VH28-A-1 EMERGENCY LOCATER TRANSMITTER 10.0 11.9* 11.5 14.7 10.0 116.5* H28-A-2 C589511-0109 0470419-4 TRANSMITTER (D & M DMELT-6-1) ANTENNA EMERGENCY LOCATOR TRANSMITTER (USED IN CANADA) TRANSMITTER (D & M DMELT-6-10) ANTENNA H31-A-1 NAV-O-MATIC 200A H31-A-2 №434-A H37-A CONTROLLER & MOUNT (CA-2958) TURN COORDINATOR (NET CHING) (G-300A) RELAY INSTALLATION WING INSTALLATION (SERVO IS 3.9 LBS AT 68.9 INCHEST(PA-495} NAV-O-MATIC 300A (AF395) CONTROLLER-AMPLIFIER & MOUNT (CA-395A) GYRO INSTALLATION (064-A-2) (NET CHNG) TURN COORDINATOR (NET CHANGE) RELAY INSTALLATION WING INSTALLATION (SERVO IS 3.9 LBS AT 68.9 INCHES) (PA-495) MISC WIRING & HARDWARE ITEMS BASIC AVIONICS KIT INSTALLATION RADIO COOLING NOISE FILTER INSTALLATION • COM ANTENNA CABLE, LH VHF OMNI ANTENNA CABLE OMNI ANTENNA COM ANTENNA, LH VHF MIKE INSTL, HAND HELD HEADPHONE, INST STOWED ARM SHOWN) AUDIO CONTROL PANEL INSTL. COM ANTENNA & OMNI COUPLER KIT COM ANTENNA CABLE, RH VHF OMNI ANTENNA COUPLER SIGNAL SPLITTER) COM ANTENNA, RH VHF 46660-1000 46860-1000 0470419-3 C58951 0117 C589511-0113 1.2 3.5* 3.3 116.4 0.1 122.0 116.5* 3.3 116.4 C589511-0109 0.1 122.0 3910162-25 9.2* 51.0* 3930144-2 1.6 13.1 42320-0028 0.0 2470009-4 0.4 350 0522632-4 6.1 68.1 3910163-25 46.4* 3930145-19 1.8 13.1 0513398 0.6 1.3 42320-0028 0.0 2470009-4 0.4 0522632-5 4.0 68.1 2730-4008 25. 3910186-17 55.6* 3930208 3940148-2. 0.1 10.2 -29.0 3950149-10 27.8 3950149-8 0.6 116.0 3960102-10 0.8 220.8 3960113-1 62.4 3970124-7 17.2 3970125-4 0.2 14.2 3970147-1 1.9. 12.5 3910185-15 1.0* 3950149-9 0.4 3960111-12 0.2 25.0* 27.8 7.0 3960113-2 0.4 62.4 6-22 1 July 1979 { MODEL 172RG CESSNA **REF DRAWING WT LBS ARM INS 0522632-2. 1.7 68.2 C596530-0101 13.0 C596531-0101 1.1 13.0 C596510-0101 1.9 38.5 ITEM NO H43-A H55-A VH56-A NHOL-R ☑01-A EQUIPMENT LIST DESCRIPTION AVIONICS OPTION D NAV-O-MATIC WING PROV. MIKE-HEADSET COMBO. INSTL (HEADSET STOWED) (REQUIRES ALL PURPOSE CONTROL WHEEL, VITEM E89 AT MICROPHONE/HEADSET, PADDED (STOWED) REQUIRES ALL PURPOSE CONTROL WHEEL, ITEM E89-A). CABIN SPEAKER AND GEAR WARNING HORN J. CUTLASS RG C16-0 C31-A SPECIAL OPTION PACKAGES II EQUIPMENT CONSISTS OF ITEMS HEATED PITOT SYSTEM 1 July 1979 0422355-7 37.3* 0.6 39.9* 24.4 COURTESY LIGHTS_ 0521101 0.5 61.0 C40-A NAV LIGHT DETECTORS 0701013 NEGE C43-A FLASHING BEACON LIGHT 2406002 204.7 001-0 TRUE AIRSPEED IND. (NET CHANGE) 2401012 004-A STATIC AIR, ALTERNATE SOURCE 0501017 E85-A DUAL CONTROLS 2401007 HO1-A CESSNA 300 ADF (R-543E) 3910159- 1434-A BASIC AVIONICS KIT 104-A ✓ NAV-PAC INSTALLATION H07-A H13-A H25-A GLIDESLOPE (R-4438} 300 NAV/COM, 2ND UNIT H16-A-1300 TRANSPONDER (RT-359A) H22-A NAV/COM 385 VOR/LOC H26-A-1 EMERGENCY LOCATER TRANSMITTER CESSNA 400 MARKER BEACON 3910183 0470419 3910157 3910127-17 3910127- 18.1 15.5 12.4 19.9 25.8 11.9 116.5 55.6 47.2* 105.6 34.5 11.9 6-23/(6-24 blank) ELT Dorneellarge in 3M6 Co nifice Segue a√lórica SECTION 6 EQUIPMENT LIST WEIGHT & BALANCE/ JAFT ofessione Volare. A/M: C-172RG A/C Inizio Lavori: 04/12/2000 S/N: Ore T.Time Fine Lavori: 19/12/2 Marc 1-PVLB Ident. Lavori Commissionati da: Sig. G. Ghetti "Professione Volare" DESCRIZIONE LAVORI 1) Applicato Bollettino TASS/19-99/RES "Riconfigurazione Apparati Avionici su a/m C172RG". Adeguamento alla raccomandazione ICAO Annex-10 e sostituzione Apparati Obsoleti. Rimossi i seguenti Apparati Avionici: #2 Sistemi COM/NAV Tipo RT385A; Sistema ADF Tipo R546E; G/S Tipo R443R; Sistema Marker Tipo R402A; Sistema Transponder Tipo RT359A. Effettuata installazione dei Seguenti Sistemi: COM/NAV/GS Indicatore VOR RIMOSSA IL COM/NAVIGS. ATAUNT Indicatore VOR Intercom/MKR ADF Rec. Antenna ADF Indicatore ADF Transponder DME #CHINAVIES. GRIFO Tipo KX-165 (p/n069-01033-0201 s/n 10070) Tipo Kl-209 (p/n066-03056-0001 s/n 77108) Tipo KX 155 (p/n069-01024 0043-s/n122207) Tipo KI-209 (p/n 066-03056-0001 s/n 77085) Tipo KMA-26 (p/n066-01155-0201 s/n 004543) Tipo KR-87 (p/n 066-01072-0004 s/n 74761) Tipo KA44B (p/n071-1234-0000 s/n 74958) Tipo K1227 (p/n066-03063-0001 s/n 47592) Tipo KT-76C (p/n066-01156-0101 s/n 11417) Tipo KN-62A (p/n 066-1068-0004 s/n 30126) Tipo kt 165A P.M. 063-1033-02015. M. 13978 30-633 S.R "New" "New" "New" "New" "New" "New" "New" S.R./ "New" "New" "New" NGW GRIFO Per l'installazione sono stati utilizzati i Breakers e le antenne della vecchia Installazione. I nuovi Apparati sono stati ubicati nel cruscotto nella stessa posizione dei vecchi. (nello spazio previsto dal Costruttore) L'installazione è conforme alla prima installazione effettuata su a/m I-AMDH (con la variente "installato un COM/ NAV KX165 in sostituzione di un KX155” Rev-1 Disegno TASS n° 172LB012000); al Manuale di Manutenzione dell'a/m; all' Installation Manuals Bendix/King 006-00179-0006,006-10544-0002,006-05184-0007,006-00143- 0006,066-10543-0000,066-10542-0001,066-00144-0006. A seguito annotazioni RAI (Forlì 10-04-2000): Effetuato sbarco A/P Tipo ARC 200AF295B. Completata installazione ELT come richiesto da C 39A (Installato interrutore per attivazione manuale su plancia di bordo) effettata prova funzionale con esito positivo.