Weight & Balance for Cessna 152
Cessna 152 · Weight And Balance
Overview
The Cessna Model 152 is a two-seat, single-engine aircraft that is widely used for flight training and personal flying. This section of the manual provides detailed procedures for establishing the aircraft's weight and balance, which are critical for safe operation. It includes guidelines for weighing the aircraft, calculating the center of gravity (C.G.), and understanding the implications of loading configurations. The manual emphasizes the importance of adhering to weight limits and C.G. specifications to ensure optimal performance and safety during flight operations.
- Ensure all pre-weighing procedures are followed to obtain accurate weight measurements.
- Calculate the C.G. using precise measurements and record keeping to maintain safety.
- Refer to the equipment list to understand how modifications may impact weight and balance.
Document
Source
Originally published by langleyflyingschool.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Weight And Balance
- Pages
- 10
- File size
- 2.6 MB
- Publisher
- langleyflyingschool.com
Specifications & performance
Extracted from this document.
Specifications
- Engine (hp)
- 110
- Length (ft)
- 27.2
- Propeller
- MCCAULEY FIXED PITCH
- Wingspan (ft)
- 36.1
- Engine model
- LYCOMING 0-235-L2C
- Empty weight (lb)
- 1,136
- Fuel capacity (gal)
- 24.5
- Max takeoff weight (lb)
- 1,670
Weight & balance
- Useful load (lb)
- 534
- Baggage allowance (lb)
- 120
- Basic empty weight (lb)
- 1,136
- Max takeoff weight (lb)
- 1,670
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In this document
Airplane Weighing Procedures
1. Preparation: Inflate tires to recommended pressures, drain fuel and oil, move seats forward, raise flaps, and set control surfaces to neutral. 2. Leveling: Place scales under each wheel and adjust the nose strut to center the bubble on the level. 3. Weighing: Record the weight on each scale and deduct any tare. 4. Measuring: Measure distances to determine the C.G. arm for calculations.
Weight and Balance Calculations
Use the basic empty weight and moment from the aircraft's records to calculate total weight and moment for various loading configurations. The moment must be divided by 1000 for use in calculations. The loading graph and C.G. moment envelope are tools to verify that the loading is within acceptable limits.
Equipment List
A comprehensive list of equipment available for the Cessna 152 is provided, detailing item numbers, descriptions, weights, and arms. This list is crucial for understanding how additional equipment affects the aircraft's weight and balance.
Safety notes
- Always verify the aircraft's weight and balance before flight to ensure compliance with safety regulations.
- Use the loading graph to confirm that the aircraft's loading configuration is within the C.G. envelope.
Full document text
CESSNA MODEL 152 SECTION 6 WEIGHT & BALANCE/ EQUIPMENT LIST SECTION 6 WEIGHT & BALANCE/ EQUIPMENT LIST TABLE OF CONTENTS Introduction Airplane Weighing Procedures Weight And Balance Equipment List Page 6-3 6-3 6-6 . 6-13 6-1/(6-2 blank) CESSNA MODEL 152 SECTION 6 WEIGHT & BALANCE/ EQUIPMENT LIST INTRODUCTION This section describes the procedure for establishing the basic empty weight and moment of the airplane. Sample forms are provided for reference. Procedures for calculating the weight and moment for various operations are also provided. A comprehensive list of all Cessna equip- ment available for this airplane is included at the back of this section. It should be noted that specific information regarding the weight, arm, moment and installed equipment list for this airplane can only be found in the appropriate weight and balance records carried in the airplane. AIRPLANE WEIGHING PROCEDURES 1. Preparation: a. b. Inflate tires to recommended operating pressures. Remove the fuel tank sump quick-drain fittings and fuel line drain plug to drain all fuel. Remove oil sump drain plug to drain all oil. C. d. Move sliding seats to the most forward position. e. Raise flaps to the fully retracted position. f. Place all control surfaces in neutral position. 2. 3. 4. 5. Leveling: a. b. Place scales under each wheel (500# minimum capacity for scales). Deflate nose tire and/or lower or raise the nose strut to center bubble on level (see figure 6-1). Weighing: a. With the airplane level and brakes released, record the weight shown on each scale. Deduct the tare, if any, from each reading. Measuring: a. b. Obtain measurement A by measuring horizontally (along the airplane center line) from a line stretched between the main wheel centers to a plumb bob dropped from the firewall. Obtain measurement B by measuring horizontally and paral- lel to the airplane center line, from center of nose wheel axle, left side, to a plumb bob dropped from the line between the main wheel centers. Repeat on right side and average the measure- ments. Using weights from item 3 and measurements from item 4, the 6-3 6-4 SECTION 6 WEIGHT & BALANCE/ EQUIPMENT LIST Datum (Firewall, Front Face) Sta. 0.0 N C.G. ரு B L & R CESSNA MODEL 152 CESSNA MODEL 152 · Level on Leveling Screws (Left Side of Tailcone) Scale Position Scale Reading Tare. Symbol Net Weight Left Wheel Right Wheel L R Nose Wheel N Sum of Net Weights (As Weighed) W X ARM (A) - (N) x (B); X = ( W Item Airplane Weight (From Item 5, page 6-3) Add Oil: No Oil Filter (6 Qts at 7.5 Lbs/Gal) With Oil Filter (7 Qts at 7.5 Lbs/Gal) Add Unusable Fuel: Std. Tanks (1.5 Gal at 6 Lbs/Gal) L.R. Tanks (1.5 Gal at 6 Lbs/Gal) Equipment Changes Airplane Basic Empty Weight )-( )x( } = ( IN. Weight (Lbs.) X C.G. Arm (In.) -14.7 -14.7 40.0 40.0 Figure 6-1. Sample Airplane Weighing = Moment/1000 (Lbs.-In.) SERIAL NUMBER PAGE NUMBER WEIGHT CHANGE ITEM NO. RUNNING BASIC EMPTY WEIGHT DATE DESCRIPTION ADDED (+) REMOVED (-) OF ARTICLE OR MODIFICATION In 1 Out Wt. (lb.) Arm (In.) Moment /1000 Wt. (lb.) Arm (in.) Moment /1000 Wt. (lb.) Moment /1000 AIRPLANE MODEL SAMPLE WEIGHT AND BALANCE RECORD (Continuous History of Changes in Structure or Equipment Affecting Weight and Balance} 6-5 SECTION 6 WEIGHT & BALANCE/ EQUIPMENT LIST Figure 6-2. Sample Weight and Balance Record SECTION 6 WEIGHT & BALANCE/ EQUIPMENT LIST airplane weight and C.G. can be determined. CESSNA MODEL 152 6. Basic Empty Weight may be determined by completing figure 6-1. WEIGHT AND BALANCE The following information will enable you to operate your Cessna within the prescribed weight and center of gravity limitations. To figure weight and balance, use the Sample Problem, Loading Graph, and Center of Gravity Moment Envelope as follows: Take the basic empty weight and moment from appropriate weight and balance records carried in your airplane, and enter them in the column titled YOUR AIRPLANE on the Sample Loading Problem. NOTE In addition to the basic empty weight and moment noted on these records, the C.G. arm (fuselage station) is also shown, but need not be used on the Sample Loading Problem. The moment which is shown must be divided by 1000 and this value used as the moment/1000 on the loading problem. Use the Loading Graph to determine the moment/1000 for each additional item to be carried; then list these on the loading problem. NOTE Loading Graph information for the pilot, passengers and baggage is based on seats positioned for average occu- pants and baggage loaded in the center of the baggage areas as shown on the Loading Arrangements diagram. For loadings which may differ from these, the Sample Loading Problem lists fuselage stations for these items to indicate their forward and aft C.G. range limitation (seat travel and baggage area limitation). Additional moment calculations, based on the actual weight and C.G. arm (fuselage station) of the item being loaded, must be made if the position of the load is different from that shown on the Loading Graph. Total the weights and moments/1000 and plot these values on the Center of Gravity Moment Envelope to determine whether the point falls within the envelope, and if the loading is acceptable. CESSNA MODEL 152 SECTION 6 WEIGHT & BALANCE/ EQUIPMENT LIST LOADING ARRANGEMENTS * Pilot or passenger center of gravity on adjustable seats positioned for average occu- pant. Numbers in parentheses indicate forward and aft limits. of occupant center of gravity range. **Arms measured to the center of the areas shown. NOTE STATION (C.G. ARM) *39 (33 TO 41) The aft baggage wall (approx- imate station 94) can be used as a convenient interior refer- ence point for determining the location of baggage area fuselage stations. **64 STATION (C.G. ARM) *39 (33 TO 41) CHILD SEAT AREA 1 64 ** 84 AREA 2 **84 AREA 2 94 94 STANDARD SEATING OPTIONAL SEATING Figure 6-3. Loading Arrangements BAGGAGE LOADING AND TIE-DOWN ① BAGGAGE AREA MAXIMUM ALLOWABLE LOADS AREAK CHCICE:CE: = 120 POUNDS
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AREA (2 = 40 POUNDS AREAS 1 + 2 = 120 POUNDS * TIE-DOWN NET ATTACH POINTS * A cargo tie-down net is provided to secure baggage in the baggage area. The net attaches to six tie-down rings. Two rings are located on the floor just aft of the seat backs and one ring is located two inches above the floor on each cabin wall at the aft end of area (①___ Two additional rings are located at the top, aft end of area ②①C:::: CACHE: least four rings should be used to restrain the maximum baggage load of 120". . Figure 6-4. Baggage Loading and Tie-Down 6-6 6-7 6-8 SECTION 6 WEIGHT & BALANCE/ EQUIPMENT LIST FIREWALL- CABIN HEIGHT MEASUREMENTS |37" 51 -56" FACE OF INSTRUMENT PANEL -38" 56.0 DOOR OPENING DIMENSIONS WIDTH (TOP) 31" 33¼" WIDTH (BOTTOM) (FRONT) 3112 HEIGHT 31" (REAR) HEIGHT 22" CESSNA SECTION 6 CESSNA MODEL 152 MODEL 152 WEIGHT & BALANCE/ EQUIPMENT LIST REAR WALL OF CABIN WIDTH * CABIN FLOOR LWR WINDOW LINE CABIN WIDTH MEASUREMENTS TIE DOWN RINGS (6) 35" 1 1 *20"| * 28" 11 *27" | 32½' 24"* 28" CABIN (C.G. ARMS) STATIONS 0.0 10 20 30 40 50 56.0 60 70 80 9094 Figure 6-5. Internal Cabin Dimensions SAMPLE AIRPLANE YOUR AIRPLANE SAMPLE LOADING PROBLEM Weight (lbs.) Moment (lb.-ins. /1000) Moment Weight (lbs.)' (lb.-ins. /1000) 1. Basic Empty Weight (Use the data pertaining to your airplane as it is presently equipped. Includes unusable fuel and full oil) 1136 34.0 2. Usable Fuel (At 6 Lbs./Gal.) Standard Tanks (24.5 Gal. Maximum) 147 6.2 Long Range Tanks (37.5 Gal. Maximum) Reduced Fuel (As limited by maximum weight) 3. Pilot and Passenger (Station 33 to 41) 340 13.3 4. Baggage Area 1 (Or passenger on child's seat) (Station 50 to 76, 120 Lbs. Max.). 47 3.0 5. Baggage Area 2 (Station 76 to 94, 40 Lbs. Max.) 6. TOTAL WEIGHT AND MOMENT 1670 56.5 7. Locate this point (1670 at 56.5) on the Center of Gravity Moment Envelope, and since this point falls within the envelope, the loading is acceptable. 6-9 Figure 8-6. Sample Loading Problem 6-10 6-11 LOAD WEIGHT (POUNDS) 0 25 2. 50 LOAD MOMENT/1000 (KILOGRAM-MILLIMETERS) CODE 400 PILOT, PASSENGER AND FUEL (LONG RANGE TANKS) @ 6#/GAL. (0,72 KG/LITRE) 350 FUEL (STANDARD TANKS) @ 6*/GAL. (0,72 KG/LITRE) 300 250 BAGGAGE IN AREA ① (OR PASSENGER ON CHILD'S SEAT) 120* MAX. (54,4 KG MAX) BAGGAGE IN AREA (2) 40# MAX. (18,1 KG MAX) 200 150 100 50 10 (37,9) 75 100 125 150 175 200 37.5 GAL. (141,9 LITRE) MAX: 175 150 125 100 30 (113,6) - 75 24.5 GAL. 20 (75,7) 11 (92,7 LITRE) MAX LOADING GRAPH 20 (75,7). 50 25 0 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 LOAD MOMENT/1000 (POUND-INCHES) LOADED AIRPLANE WEIGHT (POUNDS) NOTES: 1700 1600 1500 1400 1300 1200 1100 Line representing adjustable seats shows the pilot or passenger center of gravity on adjustable seats positioned for an average occupant. Refer to the Loading Arrangements Diagram for forward and aft limits of occupant C.G. range. Figure 6-7. Loading Graph 350 400 LOADED AIRPLANE MOMENT/1000 (KILOGRAM-MILLIMETERS) 450 500 CENTER OF GRAVITY MOMENT ENVELOPE 550 600 650 700 800 775 750 725 700 1000 30 35 40 45 50 55 60 60 LOADED AIRPLANE MOMENT/1000 (POUND-INCHES) Figure 6-8. Center of Gravity Moment Envelope T 675 650 625 600 575 550 525 500 475 65 LOAD WEIGHT (KILOGRAMS) LOADED AIRPLANE WEIGHT (KILOGRAMS) SECTION 6 EQUIPMENT LIST WEIGHT & BALANCE/ MODEL 152 CESSNA MODEL 152 CESSNA SECTION 6 WEIGHT & BALANCE/ EQUIPMENT LIST 6-12 775 875 900 AIRPLANE C.G. LOCATION-MILLIMETERS AFT OF DATUM (STA. 0.0) (SONNOD) LA CARTE PRO 800 1100 1000 30 825 31 098 CENTER OF GRAVITY LIMITS 33 34 925 35 SECTION 6 WEIGHT & BALANCE/ EQUIPMENT LIST 575 550 525 500 475 36 37 AIRPLANE C.G. LOCATION-INCHES AFT OF DATUM (STA. 0.0) Figure 6-9. Center of Gravity Limits 32 CESSNA MODEL 152 CESSNA MODEL 152 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. 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. 6-13 6-14 ITEM NO EQUIPMENT LIST DESCRIPTION REF DRAWING WT LBS ARM INS A . SECTION 6 EQUIPMENT LIST WEIGHT & BALANCE/ POWERPLANT & ACCESSORIES ENGINE, LYCOMING 0-235-L2C (INCLUDES STARTER, CARBURETOR, SPARK PLUGS AND ALTERNATOR BRACKETS) FILTER, CARBURETOR AIR ALTERNATOR, 60 AMP, 28 VOLT (BELT DRIVE) OIL COOLER INSTALLATION OIL COOLER (STEWART WARNER) OIL FILTER INSTALLATION (SPIN-ON ELEMENT) PROPELLER INSTALLATION PROPELLER, MCCAULEY FIXED PITCH 1A 103/TCM6958 SP INNER INSTALLATION, PROPELLER SPINNER DOME AFT BULKHEAD (BACK SIDE OF PROPI FWD BULKHEAD (FWD SIDE OF PROP) VACUUM SYSTEM INSTALLATION, ENGINE DRIVEN DRY VACUUM PUMP FILTER ASSEMBLY VACUUM GAUGE VACUUM RELIEF VALVE ENGINE PRIMING SYSTEM VAL VE, ENGINE OIL QUICK DRAIN (NET CHANGE) B. LANDING GEAR & ACCESSORIES WHEEL, BRAKE & TIRE ASSY, 6.00-6 MAIN (2) WHEEL ASSEMBLY, MCCAULEY (EACH) BRAKE ASSEMBLY, MCCAULEY (LEFT) BRAKE ASSEMBLY, MCCAULEY (RIGHT) TIRE, 4-PLY BLACKWALL (EACH) TUBE (EACH) WHEEL, BRAKE & TIRE ASSY, 6.00-6 MAIN (2) WHEEL ASSY, CLEVELAND BRAKE ASSY, CLEVELAND BRAKE ASSY, CLEVELAND 40-113 (EACH) 30-75A (LEFT) 30-75A (RIGHT) TIRE PLY BLACKWALL (EACH) TUBE (EACH) 2.5 24.9* 04500 71 243.5 -19.2 C294510-0201 0.5 0611503-0102 10.7 0450071 8406J 3.6* 2.0 0450412 0450077 C161001-0501 23.2 12221mm 27.5 -6.0* 5* 0450077 2.4* 0450073-1 0450072-1 0450076-1 1/11 36.5 38.6* 38.4 38.3 ·37.4 -1.5* -7.0 0413466-1 C431003-0101 120 10 75-2 C668509-0101 C48 2001-0401 17010 15-1 0.8 1.1 0.3 4.8* 2.8 18. C163018-0201 C163005-0101 40.3** 704 46.8* 47.1 C163032-0111 1.7 4307 C163032-0112 1.7 4307 C26 2003-0101 8.5 47.1 C262023-0102 1.8 47.1 1241156-40 37.6* 46.8* 0163001-0101 6.2 47.1 1.9 43.7 1.9 4307 47.1 47.1 C163030-0111 1630 30-112 C26 2003-0101 C262023-0102 A01-R A05-R A09-R A17-R A21-A A33-R A41-R A61-A A70-S A73-A B01-R-1 B01-R-2 CESSNA MODEL 152 MODEL 152 ARM INS CESSNA 18.0* 5.9 11111111 PrONTOO2819 8342834-8450 -10.8* 10.8 10.8 10.8 10.8* 10.8 10.8 -10.8 35.3* -9.5 49.5 ITEM NO EQUIPMENT LIST DESCRIPTION REF DRAWING WT LBS B04-R-1 WHEEL & TIRE ASSY, 5.00-5 NOSE WHEEL ASSY, MCCAULEY TIRE, 4 PLY BLACKWALL TUBE 804-R-2 B10-A WHEEL & TIRE ASSY, 5.00-5 NOSE WHEEL ASSY, CLEVELAND 40-77 TIRE, 4-PLY BLACKWALL TUBE WHEEL FAIRINGS (SET OF 3) C163018-0101 C163005-0201 C262003-0102 C262023-0101 1241156-2 1241156-12 C262003-0102 C262023-0101 0541225 NOSE WHEEL FAIRING MAIN WHEEL FAIRING BRAKE FAIRINGS (EACH) (EACH) C. ELECTRICAL SYSTEMS 0543079 0541223 0441227 185.5* 210.9 555505nnan 173.9 183.4 37.8* 35.5 39.5 C01-8-1 C01-R-2 C01-0 C04-R C07-A C16-A. BATTERY, 24 VOLT, 14 AMP HR BATTERY, 24 VOLT, 14 AMP HR BATTERY, 24 VOLT, 17 AMP HR REGULATOR, ALTERNATOR 60 AMP, 28 VOLT GROUND SERVICE RECEPTACLE PITOT HEATER 0870060-1 27.5 C6 14001-0101 22.8 C614001-0102 24.8 C611004-0101 0.6 0401021 C25-A C43-A 046-A C49-A-1 C49-A-2 LIGHT INSTALLATION, CONTROL WHEEL MAP LIGHT INSTALLATION, OMNIFLASH BEACON BEACON LIGHT IN FIN TIP FLASHER POWER SUPPLY IN AFT TAILCONE RESISTOR (MEMCOR) LIGHT INSTALLATION WING TIP STROBE STROBE LIGHTS IN WING TIP (SET OF 2) FLASHER POWER SUPPLIES IN TIPS (SET OF 21 LANDING LIGHT INSTALLATION--SINGLE BULB LANDING & TAXI LIGHT INSTL. DUAL BULB 0422355 0470117-3 0406003-1 0621001-0102 C594502-0102 0295-6 040 1009-1 C622006-0101 C622008-0102 0401022 0 40 10 22 00000NSTININM 1.0 6-15 0. INSTRUMENTS D01-R INDICATOR, AIRSPEED 001-0 D07-R INDICATOR, TRUE AIR SPEED ALTIMETER, SENSITIVE C661064-0107 0513279 C661071-0101 200 ..0 OP - 28.3 -28.3 EQUIPMENT LIST WEIGHT & BALANCE/ SECTION 6 17 18. 17.6 Now 6-16 SECTION 6 EQUIPMENT LIST WEIGHT & BALANCE/ CESSNA MODEL 152 MODEL 152 ITEM NO EQUIPMENT LIST DESCRIPTION REF DRAWING WT LBS ARM INS 007-0-1 007-0-2 D16-A-1 ALTIMETER SENSITIVE (20 FT MARKINGS) (FEET AND MILLIBARST C661025-0102 1.0 17.6 ALTIMETER, SENSITIVE (50 FT. MARKINGS) (FEET AND MILLIBARS) C661071-0102 1.0 17.6 016-A-2 ENCODING ALTIMETER (INCLUDES RELOCATION OF CONVENTIONAL ALTIMETER) ENCODING ALTIMETER, FEET & MILLIBARS (INCLUDES RELOCATION OF CONVENTIONAL ALTIMETER) 040 10 13 2.9 17.0 040 1013 2.9 17.0 D16-A-3 019-R D25-A D28-R D37-R D40-R 064-A 067-A 082-A D85-R 088-A 091-A E05-R E05-0 E07-S E07-0 E09-A E15-R ENCODING ALTIMETER, USE WITH TRANSPONDER (BLIND ENCODER-DOES NOT REQUIRE PANEL MOUNT) AMMETER CLOCK INSTALLATION CLOCK, ELECTRIC COMPASS INSTRUMENT CLUSTER (LH FUEL & RH FUEL) INSTRUMENT CLUSTER (OIL PRES. & OIL TEMP.) GYRO INSTALLATION (REQUIRES ITEM A61-A) DIRECTIONAL INDICATOR ATTITUDE INDICATOR RECORDER, ENGINE HOUR METER OUTSIDE AIR TEMPERATURE INDICATOR TACHOMETER INSTALLATION, ENGINE RECORDING TACH INDICATOR TACH FLEXIBLE SHAFT INDICATOR, TURN COORDINATOR INDICATOR, RATE OF CLIMB E. CABIN ACCOMMODATIONS SEAT, PILOT INDIVIDUAL SLIDING SEAT, VERTICALLY ADJUSTABLE, PILOT SEAT, CO-PILOT INDIVIDUAL SLIDING SEAT, VERTICALLY ADJUSTABLE, CO-PILOT SEAT INSTALLATION, AUXILIARY UPPER BACK REST CUSHION LOWER SEAT CUSHION ASSEMBLY LAP BELT ASSEMBLY BELT ASSY, PILOT LAP 0401019 1.5 2.0 S-1320-5 0400341 C664508-0101 C660501-0102 C669511-0101 C669512-0102 0413466-1 C661075 C661076 040 10 17 C668507-0101 1.0* 12.5* C668020-0119 0.6 17.0 S-1605-3 0.3 C661003-0505 2.0 17.2 C661080-0101 18.0 oooooo7NNOOLOOLI 18.0 14.4* 18.1 20.0 18.0 18.0 1* 14.8* 15.6 15.8 5.2 22.0 0414070 11.1 0414071 13.6 0414070 11.1 0414071 13.6 0400134-1 10.5* 66.5* 0711080-1 1.3 72.9 0400136-9 604 6405 S-1746-2 1.0 S-2275-104 1.0 39.0 0026ÜNNNN CESSNA ITEM NO EQUIPMENT LIST DESCRIPTION REF DRAWING WT LBS ARM INS E15-S E19-0 SHOULDER HARNESS ASSY, PILOT SHOULDER HARNESS INERTIA INSTL., CO-PILOT (NET CHANGE) PILOT & S-2275-202 040 10 12-1 1.0 om 39.0 71.1 E23-S E39-A E53-A BELT & SHOULDER HARNESS ASSY, CO-PILOT WINDOWS, OVERHEAD CABIN TOP (NET INCREASE) MIRROR, REAR VIEW S-2275-4 39.0 0413492 49.0 0400338 17.0 E55-A SUN VISORS (SET OF 2) 0413473-1 1.0 27.0 E57-A E65-S E85-A E93-R WINDOWS, TINTED ( SET OF 4, NET CHANGE) BAGGAGE NET DUAL CONTROLS (WHEEL, PEDALS & TOE BRAKES) HEATING SYSTEM, CABIN & CARBURETOR AIR (INCLUDES EXHAUST SYSTEM) F. PLACARDS & WARNING 0400324-1 0.0 2015009-2 0.5 84.0 0460118-2 0450071 14.0 F01-R FO1-0-1 OPERATIONAL LIMITATIONS PLACARD VFR-DAY OPERATIONAL LIMITATIONS PLACARD VFR-DAY NIGHT 0405058-1 NEGL 23.0 0405058-2 NEGL 23.0 F01-0-2 OPERATIONAL LIMITATIONS PLACARD IFR-DAY NIGHT F04-R INDICATOR, STALL WARNING AUDIBLE G. AUXILIARY EQUIPMENT 0405058-3 NEGL 23.0 0413029 0.5 21.5 SECTION 6 WEIGHT & BALANCE/ EQUIPMENT LIST GO4-A 607-A G13-A HOOK, TOW (NOT FACTORY INSTALLED) HOISTING RINGS, AIRCRAFT CABIN TOP CORROSION PROOFING, INTERNAL 0500228 0541115 0400027-2 405 200.0 42.0 68.0 G16-A STATIC DISCHARGERS (SET OF 10) 040 10 15 004 117.6 G19-A STABILIZER ABRASION BOOTS 0500041 2.5 179.4 G22-A TOW BAR, AIRCRAFT NOSE WHEEL (STOWED) 0501019-1 1.6 84.0 G25-S-1 PAINT, OVERALL EXTERIOR (ACRYLIC) 04040 30 8.5* 7901* OVERALL WHITE BASE 8.1 79.0 COLOR STRIPE 004 81.7 G25-S-2 PAINT, OVERALL EXTERIOR (MODIFIED POLY- URETHANE) 0404030 79.1* OVERALL BASE WHITE WASH PRIME COATING COLOR STRIPE Form5 °°° 79.0 79 81.7 6-17 6-18 SECTION 6 EQUIPMENT LIST WEIGHT & BALANCE/ ITEM NO 625-0 EQUIPMENT LIST DESCRIPTION PAINT, OVERALL EXTERIOR (MODIFIED POLY- URETHANE--USED WITH INTERNAL CORROSION PROOFING, ITEM G13-A) REF DRAWING WT LBS ARM INS 04040 30 9.5 79.1 G31-A 634-A G49-A G55-A G58-A 667-A 688-A CABLES, CORROSION RESISTANT CONTROL (NET CHANGE) 0400027 0.0 LIGHTER, CIGARETTE 0401023 18.0 WING TIPS, MODIFIED CONICAL (NET CHANGE} FIRE EXTINGUISHER, HAND TYPE 0523565 2.5 41.0 040 1001 3.0 9.5 G92-A STEPS & HANDLES, REFUELING ASSIST PEDAL EXTENSIONS, RUDDER, REMOVABLE - SET OF 2 (STOWABLE - INSTALLED ARM SHOWN) WINTERIZATION KIT INSTALLATION, ENGINE COVER PLATES, FWD COWL (SET OF 2 INSTALLED) COVER PLATES, FORWARD COWL (STOWED) CRANKCASE BREATHER TUBE INSULATION WINGS WITH 39 GALLON CAPACITY, EXTENDED RANGE FUEL TANKS (SET OF 2, NET CHANGE) Ho AVIONICS & AUTOPILOTS 0413456-2 2.1 9.9 0701048 2.3 8.0 1.2* == -24.2* 003 -37.0 0.3 84.0 0.3 - 24.0 04010 18 37.3 CESSNA MODEL 152 MODEL 152 REF DRAWING WT LBS ARM INS HO1-A CESSNA 300 ADF H07-A RECEIVER WITH BFO (R-546E) INDICATOR (IN-346A) ANTENNA INSTALLATION LOOP ANTENNA INSTALLATION CABLE INSTALLATION MISC. INSTALLATION COMPONENTS CESSNA 400 GLIDE SLOPE RECEIVER (R-443B) MOUNTING, RIGID ANTENNA RECEIVER (R-402A) ANTENNA, L SHAPED ROD BENDIX MARKER BEACON (EXPORT USE) H13-A-1 CESSNA 400 MARKER BEACON H13-A-2 RECEIVER ANTENNA, L SHAPED ROD H16-A-1 CESSNA 300 TRANSPONDER TRANSCEIVER (RT-359A) 3910159-11 18.2* 41240-0101 13.5 40980-1001 0.9 15.5 0470400-621 96.5 3960104-1 1.4 24.2 12.3 14.4 3950104-14 39 10157-10 42100-0000 36450-0000 1200098-2 3910142-1 8° 4.0* 80.4* 2.1 105.3 0.3 100.0 0.2 2004 2.2* 35.4* 42410-5114 0.8 11.7 0770681-1 0.6 86.0 39 10174-1 3.9* 85.7* GM-247A 1.5 0770681-1 0.6 99.8 86.0 3910127-1 3.6* 41420-1128 207 18.6* 13.0 EQUIPMENT LIST DESCRIPTION CESSNA SECTION 6 WEIGHT & BALANCE/ EQUIPMENT LIST ANTENNA (A-1098) H16-A-2 CESSNA 400 TRANSPONDER (EXPORT USE} TRANSCEIVER (RT-459A) ANTENNA (A-109B) H22-A-1 H22-A-2 H22-A-3 H22-A-4 H22-A-5 H22-A-6 H22-A-7 CESSNA 300 NAV/COM 160 CHANNEL TRANSMIT RECEIVER-TRANSCEIVER (RT-308C) VOR/LOC INDICATOR (IN-514B) H34-A BASIC AVIONICS KIT VOLTAGE CONVERTER INSTL. MOUNT, WIRING & MISC HARDWARE CESSNA 300 NAV/COM, 720 CHANNEL 1ST UNIT RECEIVER-TRANSCEIVER (RT-385A) VOR/LOC INDICATOR H34-A BASIC AVIONICS KIT MOUNT, WIRING & MI SC HARDWARE CESSNA 300 NAV/COM 720 CHANNEL 1ST UNIT WITH VOR/ILS RECEIVER TRANSCEIVER (RT-328T) VOR/ILS INDICATOR (IN-52581 INSTALLATION COMPONENTS ARE SIMILAR TO H22-A-1 CESSNA 300 NAV/COM, 720 CHANNEL, 1ST UNIT WITH VOR/ILS RECEIVER-TRANSCEIVER (RT-385A} VOR/ILS INDICATOR 1ST UNIT INSTL. COMPONENTS ARE SIMILAR TO H22-A-2 CESSNA 300 NAV/COM 720 CHANNEL 1ST UNIT RECEIVER-TRANSCEIVER (RT-328T) VOR/LOC INDICATOR (IN-514B) 1ST UNIT INSTL. COMPONANTS ARE SIMILAR TO H22-A-1 CESSNA 300 NAV/COM, 720 CH COM 1ST UNIT WITH VOR/LOC AUTOCOURSE INDICATOR RECEIVER-TRANSCEIVER (RT-385A) VOR/LOC INDICATOR (IN-385AC) (AUTOMATIC RADIAL CENTERING) BASIC AVIONICS KIT MOUNT, WIRING & MISC HARDWARE CESSNA 300 NAV/COM, 720 CH COM 1ST UNIT WITH VOR/ILS AUTOCOURSE INDICATOR RECEIVER-TRANSCEIVER (RT-385A) 3910184-4 42450-1114 450 10-1000 3910186-1 3940224 3930152-1 41530-0001 3910128-20 41470-1128 41530-0001 67.0 。6* 18.6* NOW 2.8 13.0 67.0 14.8* 29.2* 6.4 13.6 0.6 17.8 5.1 61.9 104 1.5 12.9 3910183 13.74 31.8* 46660-0000 5.4 13.6 46860-1000 2.2 15.5 3910186-1 5.1 61.9 12.9 3910184 28.6* 43340-1124 6.9 13.6 450 10-2000 0.7 17.8 7.8 42.9 39 10184-3 13.6* 32.1* 46660-0000 46660-2000 5.4 13.6 2.3 15.5 6.1 53.9 3900140 15.3* 28.7* 43340-1124 45010-1000 6.9 13.6 0.6 17.8 7.8 42.9 13.7* 31.8* 46660-0000 46860-1200 2:2 13.6 3910186-1 5.1 61.9 3910183 46660-0000 1.0 13.8* 504 12.9 31.7* 13.6 3910183 ITEM NO 6-19 6-20 SECTION 6 EQUIPMENT LIST WEIGHT & BALANCE/ CESSNA MODEL 152 MODEL 152 ITEM NO EQUIPMENT LIST DESCRIPTION VOR/ILS INDICATOR (IN-386AC) (AUTOMATIC RADIAL CENTERING } BASIC AVIONIC KIT MOUNT, WIRING & MI SC HARDWARE REF DRAWING WT LBS ARM INS 46860-2200 2.3 15.5 39 10186-1 5.1 61.9 1.0 12.9 H25-A-1 CESSNA 300 NAV/COM, 720 CHANNEL 2ND UNIT WITH VOR/LOC 3910184-5 10.6* 13.9* H25-A-2 H25-A-3 H25-A-4 (RT-328T) VOR/LOC INDICATOR (IN-514B) H37-A ANTENNA & COUPLER KIT VOLTAGE REGULATOR (41010) 2ND UNIT SWITCHING INSTL MOUNT, WIRING & MISC HARDWARE H28-A-1 EMERGENCY LOCATOR TRANSMITTER H28-A-2 TRANSMITTER (D & M DMELT-6) ANTENNA EMERGENCY LOCATOR TRANSMITTER (USED IN CANADA TRANSMITTER (D & M DMELT-60) ANTENNA H34-A BASIC AVIONICS KIT RADIO COOLING RECEIVER-TRANSCEIVER VOR/LOC INDICATOR (IN-5148) H37-A ANTENNA & COUPLER KIT VOLTAGE CONVERTER 2ND UNIT COM SWITCH INSTL MISC 2ND UNIT ITEMS CESSNA 300 NAV/COM, 720 CH, SECOND UNIT WITH VOR/LOC RECEIVER-TRANSCEIVER (RT-385A) VOR/LOC INDICATOR H37-A ANTENNA & COUPLER KIT 2ND UNIT COM SWITCHING INSTL MISC 2ND UNIT ITEMS 2ND UNIT CESSNA 300 NAV/COM 720 CH COM RECEIVER-TRANSCEIVER (RT-385A) VOR/LOC INDICATOR (IN-385AC) AUTOCOURSE (AUTOMATIC RADIAL CENTERING} H37-A ANTENNA & COUPLER KIT 2ND UNIT COM SWITCHING INSTL MOUNT, WIRING & MISC HARDWARE CESSNA 300 NAV/COM 720 CH COM 2ND UNIT RECEIVER-TRANSCEIVER 3940224 3970118-3 3910183 46660-0000 46860-1000 3910186 3970118-3 3910183 46660-0000 46860-1200 39 10186 (RT-328T) 42450-1114 13.6 450 10-1000 0.6 17.8 3910186 1.0 30.6 1.4 0.2 1.5 17.0 1.0 *8° 52102O5N 2.2 0 0 6 0 0 0 0 0 15.5 30.6 17.0 8* 13.3 15.8* 13.6 15.5 1.0 30.6 3970118-3 17.0 1.9 13.3 3910182 11.4* 13.9* 43340-1124 6.9 13.6 450 10-1000 17.8 3910186 1.0 30.6 3940224 .4 1.5 3970118-3 0.2 17.0 1.3 13.4 0470419-1 1.6* 102.4* C5895 11-0 101 1.4 102.6 C589511-0109 0.1 101.3 0470419-2 1.6* 102.4* C589511-0102 1.4 102.6 C589511-0109 3910186 0.1 101.3 5.1* 61.9* 3930152-1 1.0 15.6 13.0 15.8* 13.6 ITEM NO CESSNA REF DRAWING WT LBS ARM INS 3940148-1 3950104-3 3950104-4 3960102-9 3960113-1 3970117-1 3970118-2 0.2 3970123-6 3970125-1 0.2 17954321NŐ - 25. 20. 105.0 220.9 55.9 18.2 17.0 51.1 17.2 30.6* & CABLE S-2086-1 3970134 0000 +723 55.9 20.2 1.0 17.0 C59653-0101 1.1 EQUIPMENT LIST DESCRIPTION NOISE FILTER (AUDIO)(ON ALTERNATOR) LH COM ANTENNA CABLE OMNI ANTENNA CABLE OMNI ANTENNA INSTALLATION VHF L.H. COM ANTENNA MICROPHONE INSTALLATION COM SWITCHING INSTALLATION CABIN SPEAKER INSTL HEADPHONE INSTALLATION SECTION 6 WEIGHT & BALANCE/ EQUIPMENT LIST 36.7* 35.6* 23.9* 24.8* 0413466-1 4.8 0406003-1 1.4 185. 040 10 22 1.0 -28.3 0413466 7.1. 14.8 C668507-0101 0.1 22.0 C661003-0505 17.2 C661080-0101 1.0 18.0 0413473-1 1.0 27.0 0460118-2 401 12.1 9910220-1 0.1 18.0 14.6 29.5 13.7 31.8 14.7* 15.3* 13.1* 16.6* 3910127-1 3910182 3.6 18.6 10.6 13.9 -14.8 29.2 15.3 13.7 28.9 31.8 H37-A COM ANTENNA & OMNI COUPLER KIT (AVAILABLE ON 2ND UNIT NAV/COM FACTORY INSTL ONLY) RM COM ANTENNA INSTALLATION RH COM ANTENNA CABLE H55-A H56-A J01-A J04-A OMNI COUPLER (SIGNAL SPLITTER) MIKE-HEADSET COMBINATION (INCLUDES ALL- PURPOSE CONTROL WHEEL) PADDED HEADPHONE (STOWED) J. SPECIAL OPTION PACKAGES 152-II PACKAGE EQUIPMENT WITH RT-308C WITH RT-385A (AVAILABLE MID YEAR) A61-A VACUUM SYSTEM (FOR GYROS) C43-A OMNI FLASHING BEACON C49-A-1 LANDING LIGHT SINGLE BULB GYRO INSTALLATION OUTSIDE AIR TEMPERATURE IND 064-A D82-A D88-A TURN COORDINATOR 091-A E55-A SUN VISORS RATE OF CLIMB IND. E85-A DUAL CONTROLS 634-A CIGARETTE LIGHTER H22-A-1 CESSNA 300 NAV/COM RT-308C H22-A-2 CESSNA 300 NAV/COM RT-385 A 152 II NAV PAC WITH RT-328T 152 II NAV/PAC WITH RT-385A (MID-YEAR) H16-A-1 CESSNA 300 TRANSPONDER RT-359A H25-A-1 RT-308C NAV/COM 2ND UNIT ADDED H22-A-1 RT-308C 1ST UNIT DELETED H22-A-3 RT-328T NAV/COM 1ST UNIT ADDED H22-A-2 RT-385A 1ST UNIT ADDED MID-YEAR 3900140 6-21/(6-22 blank)
What's in the Cessna 152 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.
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