SA00061LA - J.P. Instruments
CESSNA 170B · Type Certificate
Overview
This document serves as the Type Certificate Data Sheet for the Robinson R22 Beta II helicopter. It provides essential information regarding the aircraft's specifications, limitations, and operating procedures. Designed for pilots, maintenance personnel, and aviation enthusiasts, the document outlines the aircraft's performance characteristics, weight and balance data, and safety information. It is a critical reference for understanding the operational capabilities and regulatory compliance of the R22 Beta II.
- Maximum gross weight: 1,370 lbs (622 kg)
- Maximum cruise speed: 102 knots (117 mph)
- Service ceiling: 14,000 feet
- Rate of climb: 1,200 feet per minute
- Maximum baggage weight: 50 lbs (23 kg)
Document
Source
Originally published by www.jpinstruments.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Type Certificate
- Pages
- 14
- File size
- 1.3 MB
- Publisher
- www.jpinstruments.com
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In this document
Aircraft Specifications
The Robinson R22 Beta II features a two-blade main rotor system and a two-blade tail rotor. It has a maximum gross weight of 1,370 lbs (622 kg) and a useful load of approximately 600 lbs (272 kg). The helicopter is powered by a Lycoming O-320 engine, providing a maximum continuous power output of 145 hp.
Performance Data
The R22 Beta II has a maximum cruise speed of 102 knots (117 mph) and a service ceiling of 14,000 feet. The rate of climb is approximately 1,200 feet per minute under standard conditions. The helicopter's range is about 300 nautical miles, depending on load and fuel consumption.
Weight and Balance
The document outlines the weight and balance limitations for the R22 Beta II, emphasizing the importance of adhering to the specified center of gravity limits for safe operation. The maximum baggage weight is limited to 50 lbs (23 kg).
Operating Limitations
The R22 Beta II has specific operating limitations, including a maximum airspeed of 102 knots and a maximum bank angle of 60 degrees. Pilots must also adhere to the specified limits for weight, balance, and fuel load.
Maintenance Requirements
Regular maintenance is essential for the safe operation of the R22 Beta II. The document details the required inspection intervals and maintenance procedures to ensure compliance with safety standards.
Safety notes
- Adhere to specified weight and balance limits for safe operation.
- Regular maintenance is critical to ensure safety and compliance.
Full document text
United States of America Department of Transportation-federal Aviation Administration Supplemental Type Certificate Number SA00061LA This certificate issued to J.P. INSTRUMENTS 9621 Bay Meadow Drive Huntington Beach, California 92646 cortifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requirements of Part of the Federal Aviation * See Applicable Type Certificate Data Sheet (T.C.D.S.) for certification basis Regulations Original Product Typs Cortificate Number: Make: Model: Description of Type Design Change: See Attached FAA Approved J.P. Instruments Master Eligibility List No. 410 for list of approved aircraft models and applicable T.C.D.S. Installation of JPI digital tachometer in accordance with FAA Approved J.P. Instruments Drawing List Report No. 400, Revision NC, dated March 20, 1995 or later FAA approved revision. Limitations and Conditions: This approval should not be extended to other specific airplanes of these models on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effects upon the airworthiness of that airplane The tachometer installed by the original aircraft manufacturer must remain installed and operable This certificate and the supporting dulu which is the basis for approval shall remain in effect until-sur rendered, suspended, rovoked,. (or a termination date is therwise istullished by the Administrator of the Federal Aviation Administration Date of application: May 10, 1993 Tute reissued Date of issuance March 29, 1995 Date amended FEDERAL AVIATION ONINISTRATION January 12, 1996 By direction of the Administrator (Signature) Manager, Propulsion Branch Los Angeles Aircraft Certification Office (Tille) This certificate may be transferred in accordance with FAR 21.47. Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA FORM 8110-2(10-68) REVISION LOG TO FAA APPROVED MASTER ELIGIBILITY LIST REPORT 410 REVISION NO. DATE APPROVED N/C 3-20-95 A REVISION DESCRIPTION INITIAL RELEASE; SHEETS 1 THRU 8 ADD RANGE LIGHTS SHEETS 3 THRU 13, Revised part number Identification (see sheet 13) SHEET NO. 2 FAA APPROVED J.P.INSTRUMENTS MASTER ELIGIBILITY LIST NO. 410 INSTALLATION OF THE 400000 SERIES DIGITAL TACHOMETER With Range Lights STC NUMBER: SA00061LA DATE: March 20, 1995 FAA APPROVED MAKE Air Tractor, AT-300 AT-301 MASTER ELIGIBILITY LIST J.P.INSTRUMENTS AIRCRAFT MODE Avions Pierre R2160 Robin Ayres Corp. 600 S-2D, S-2R, S2R-R1340 REPORT 410 SHEET NO. 3 T.C.D.S P/N 400000 - XX - [( ) - ( )] * A9SW 9-G300R2300 9-G300R2250 A48EU 4-G300Y2600R2700 A3SW 9-G300Y2200R2250 S2R-R3S A4SW 9-G300Y2050R2200 Beech 23, A23-19, 19A), A23, A23A, B19, M19A A23-24, B23,C23 A1CE 4-G300R2700 4-G300R2700 A23-24, A24, A24R C23 A1CE 4-G300R2000G2150R2700 4-G300R2150G2350R2700 B24R,C24R 4-G300R2100G2250R2700 Beech 35, A35 A-777 6-G300R2050R2300 B35, 35R, C35, E35, F35, D35 6-G300R2050R2450 6-G300R2300R2600 G35 Beech H35,J35,K35, M35, 35-A33 G33, N35, P35 35-33, 35-B33, 35-C33, E33, F33 S35, V35,V35A,V35B, 35-C33A, E33A, E33C, A36TC,B36TC F33A, F33C, 36, A36 6-G300R2300R2650 3A15 6-G300R2600 6-G300R2620 6-G300R2600 6-G300R2700 6-G300Y2550R2700 Beech 50 Twin B50, C50 E50, F50, G50, H50, J50 D50, D50A,B, D50C, E, E-5990 Beech Twin 95, B95 B95A, D95A, E95 95-55, 95-A55, 95-B55, 95B55A 95-B55B 95-C55, 95-C55A, 95-D55, 95-D55A,E55,E55A (10-520C, Below TE1171-2700RL. After sn: TE1171 2550-2700) 95-58, 58A (10-520C, sn: TH1095, 2700RL, sn: 1096 to TH1394, 2550-2700) See Part Number Designation on Sheet 13 5A4 6-G300Y3000R3400 6-G300Y3100R3400 6-G300Y3200R3400 6-G300Y3100R3400 3A16 4-G300R2700 4-G300R2700 6-G300Y2550R2620 6-G300R2620 6-G300R2700 6-G300Y2550R2700 6-G300R2700 6-G300Y2550R2700 FAA APPROVED MAKE MASTER ELIGIBILITY LIST J.P.INSTRUMENTS AIRCRAFT MODE REPORT 410 SHEET NO. 4 T.C.D.S PIN 400000 - XX -(()-(11* Beech 56TC,A56TC 3A16 6-G300R2900 Twin Beech 58P,58PA,58TC,58TCA A23CE 6-G300R2700 Twin Beech 60,A60,B60 A12CE 6-G300Y2750R2900 Twin Beech 65-80, 65-A80,65-A80-8800, 65-88,65-B80 3A20 Twin 65, A65,A65-8200,70 6-G30Y3200R3400 6-G30Y3200R3400 Beech Twin 76 A29CE 4-G300R2700 Beech 77 Bellanca 14-13, 14-13-2,-3,-3W Bellanca 14-19 14-19-2 14-19-3 Bellanca 17-30 Bellanca 17-31 Bellanca 17-31TC Bellanca 17-30A,17-31A Boeing (10-540G185,-G1E5,-G1F5 2575RL) (10-540K1B5,-K1E5,-K1A5 2700RL) Bellanca 17-31ATC, (10-540G1B5,-G1E5,-G1F5 2575RL) (10-540K185,-K1E5,-K1A5 2700RL) (STEARMAN) A75L3,75,A75, B75, E75 A75L3000 IB75A, E75N1 Boeing A75J1 A75N1, B75N1, D75N1 Cessna 120,140 A-743 9-G300R2100 9-G300Y2200R2300 9-G300Y1950R2300 A-743 7-G300R2000 7-G300R2070 A-768 4-G300R2570 A30CE 4-G300R2700 A773 6-G300R2600 1A3 6-G300R2550 6-G300R2600 6-G300R2620 1A3 6-G300Y2700R2850 1A3 6-G300R2570 1A3 6-G300Y2400R2570 A18CE 6-G300R2570 6-G300R2700 A18CE 6-G300R2575 6-G300R2700 See Part Number Designation on Sheet 13 FAA APPROVED MAKE MASTER ELIGIBILITY LIST J.P.INSTRUMENTS AIRCRAFT MODE REPORT 410 SHEET NO. 5 T.C.D.S PIN 400000 - XX -[( ) - ( )]* Cessna 140A 5A2 4-G300R2470 Cessna 150,A,B,C,D,E,F,G,H,J,K A150K, 150L, A150L, 150M 3A19 4-G300R2750 A150M Cessna 152, A152 Cessna 170,170A,170B Cessna 172 3A19 4-G300R2550 A-799 6-G300R2700 3A12 6-G300R2700 172A,B,C,D,E,F,G,H Cessna 172, I, K, L, M, N, P, Q 3A12 4-G300R2700 Cessna 172RG 3A17 4-G300R2700 Cessna R172E, F, G, H, J, (10-360-D,-H, 2800RL) K, (10-360K, 2600RL) 3A17 6-G300R2800 6-G300R2600 Cessna P172D,175,175A,B,C 3A17 6-G300R3200 Cessna 177, 177A, 177B A13CE 4-G300R2700 Cessna 177RG A20CE 4-G300R2700 Cessna 180, (0-470-A,-J.-K, A&K 2600RL, 5A6 6-G300R2600 180 (0-470-J 2550RL) 6-G300R2550 180A,B,C,D,E,F,G,H,J 6-G300R2600 180K 6-G300R2400 Cessna 182,182A,B,C,D,E,F,G,H,J,K,L,M,N,P 3A13 6-G300R2600
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182,Q,R, R182, T182, TR182 6-G300R2400 Cessna 185,185A,B,C,D,E 3A24 6-G300R2620 Cessna A185E,A185F 3A24 6-G30Y2700R2850 Cessna 188,188A,188B A9CE 6-G300R2600 A188,A188A, A188B T188C Cessna 190,195,195B 6-G300Y2700R2850 6-G300R2700 A-790 7-G300R2200 195A 7-G300Y2000R2200 See Part Number Designation on Sheet 13 FAA APPROVED MAKE MASTER ELIGIBILITY LIST J.P.INSTRUMENTS AIRCRAFT MODE Cessna 206,P206,P206A, B, C,D,E TP206A,B,C,D,E Cessna U206,U206A U206B,C,D,E,F,G TU206A,B,C,D,E,F,G REPORT 410 SHEET NO. 6 T.C.D.S P/N 400000 - XX - [ ( ) - ( )]* A4CE 6-G300R2700 6-G300R2700 A4CE 6-G300R2700 6-G300Y2700R2850 6-G300R2700 A16CE 6-G300R2700 Cessna 207,207A Cessna T207,T207A Cessna 210,210A Cessna 210B,C Cessna 210D,E,F Cessna 210-5,210-5A A16CE 6-G300Y2600R2700 3A21 6-G300YR2620 3A21 6-G300R2620 3A21 6-G300R2700 3A21 6-G300R2620 T210F,T210G,T210H 6-G30R2700 210G,,210H, 210J 6-G30R2700 Cessna T210J, T210K,T210L 3A21 6-G300R2700 210K, 210L, 210M,210N,210R 6-G300Y2700R2850 T210M,T210N, P210N 6-G300Y2600R2700 P210R, T210R 6-G30R2700 Cessna 305A,C,D,F Cessna Twin 310,310A,B 5A5 6-G300Y2300R2600 3A10 6-G300R2600 Cessna Twin 310C,D,E,F,G,H,J, 310J-1, E31OH, 3101, E31OJ 310K, L, N, P,Q 3A10 6-G300R2620 Cessna 310R, T310Q,T310P,T310R 3A10 6-G300R2700 Twin Cessna 320,A,B,C, 320-1 Twin 320D,E,F,335, 340,340A Cessna 321 3A25 6-G300R2600 6-G300R2700 3A11 6-G300R2600 Twin Cessna 336 A2CE 6-G300R2800 Twin See Part Number Designation on Sheet 13 FAA APPROVED MAKE MASTER ELIGIBILITY LIST J.P.INSTRUMENTS AIRCRAFT MODE REPORT 410 SHEET NO. 4 T.C.D.S P/N 400000 - XX -[()-()]* 3A16 6-G300R2900 Beech 56TC,A56TC Twin Beech 58P,58PA,58TC,58TCA Twin Beech 60,A60,B60 Twin Beech 65-80, 65-A80,65-A80-8800, 65-88,65-B80 Twin 65, A65,A65-8200,70 Beech 76 Twin Beech 77 Bellanca 14-13, 14-13-2,-3,-3W Bellanca 14-19 14-19-2 14-19-3 Bellanca 17-30 Bellanca 17-31 Bellanca 17-31TC Bellanca 17-30A,17-31A A23CE 6-G300R2700 A12CE 6-G300Y2750R2900 3A20 6-G30Y3200R3400 6-G30Y3200R3400 A29CE 4-G300R2700 A30CE 4-G300R2700 A773 6-G300R2600 1A3 6-G300R2550 6-G300R2600 6-G300R2620 1A3 6-G300Y2700R2850 1A3 6-G300R2570 1A3 6-G300Y2400R2570 A18CE (10-540G1B5,-G1E5,-G1F5 2575RL) (10-540K1B5,-K1E5,-K1A5 2700RL) 6-G300R2570 6-G300R2700 Bellanca 17-31ATC, A18CE (10-540G1B5,-G1E5,-G1F5 2575RL) (10-540K185,-K1E5,-K1A5 2700RL) 6-G300R2575 6-G300R2700 Boeing (STEARMAN) A75L3,75,A75, B75, E75 A-743 9-G300R2100 A75L3000 9-G300Y2200R2300 IB75A, E75N1 9-G300Y1950R2300 Boeing A75J1 A-743 7-G300R2000 A75N1, B75N1, D75N1 7-G300R2070 Cessna 120,140 A-768 4-G300R2570 See Part Number Designation on Sheet 13 FAA APPROVED MAKE MASTER ELIGIBILITY LIST J.P.INSTRUMENTS AIRCRAFT MODE Grumman AA-1, -1A, -1B Grumman AA-1C Gulfstream AA-5, AA-5A, AA-5B Commander 112,112B Aircraft REPORT 410 SHEET NO. 8 T.C.D.S P/N 400000 - XX -[()-()]* A11EA 4-G300R2600 A11EA 4-G300R2700 A16EA 4-G300R2700 A12SO 4-G300R2700 Commander 112TC, 112TCA Aircraft Commander 114,114A, B Aircraft Gulfstream 500 (Twin Commander 500-A A12SO 4-G300R2570 A12SO 6-G300R2700 6A1 6-G300R2575 6-G300R2620 Aircraft) 500-B, U, S 6-G300R2620 520, 560,560A, -E 6-G300Y3000R3400 Gulfstream 560F 2A4 6-G300Y3000R3400 (Twin Commander 680,E, 720 6-G300Y3200R3400 Aircraft) 680-F, 680FL, 680-FL(P) 6-G300Y3200R3400 685 6-G300R3400 Hughes 269A, (HO-360-B1A, 2900RL) 4H12 4-G300R2900 Helicopter 4-G300Y2700R2900 (Schweizer) 269A (O-360-C2D, 2700-2900) 269A-1,(HIO-360-B1A,2900RL) 269B, 269C,( HIO-360-DIA,3200RL) 4-G300R2900 4-G300R3200 Maule Bee Dee M-4, M-4,-4C, 4S,-4T 3A23 4-G300R2700 Maule M-4-210,C,S,T, M-4-220C,S,T, M-4-180C,S,T 3A23 6-G300R2800 Maule M-5-180C, (Lyc 0-360-C1F, 2000-2250, 2700RL) 3A23 4-G300R2000G2250R2700 M-5-200,) 4-G300R2700 MX-7-180, A, B, MXT-7-180, A, B, MXT-7-160, MX-7-160 4-G300R2700 See Part Number Designation on Sheet 13 FAA APPROVED MAKE MASTER ELIGIBILITY LIST J.P.INSTRUMENTS AIRCRAFT MODE REPORT 410 SHEET NO. 9 T.C.D.S PIN 400000 -xx-(()-(1)* Maule M-5-210C, M-5-220C 3A23 6-G300R2800 M-5-210TC, (TO-360F1A6, 2575RL) 4-G300R2570 Maule M-5-235C, (O-540JI, IO-540W, 2400RL) M-5-235C with (0-540B, 2575RL) 3A23 6-G300R2400 6-G300R2570 Maule M-6-180 3A23 4-G300R2000G2250R2700 M-6-235 6-G300R2400 Maule M-7-235,A, B, MX-7-235, M-8235, (0-540JI, W, 2500RL) 3A23 6-G300R2500 M-7-236,A, B, MX-7-235, M-8235, with (0-540B, 2575RL) MXT-7-235, (10-540W1A5, 2400RL) 6-G300R2570 6-G300R2400 Mooney M20 2A3 4-G300R2000G2250R2700 M20A,B,C,D,G (0-360 A1A, 2000-2250, 2700RL) 4-G300R2000G2250R2700 Mooney M20E,F (IO-360 A1A, 2000-2350 RED, 2700RL) 2A3 4-G300R2000G2350R2700 Mooney M20J 2A3 4-G300Y1600G1950R2700 Mooney M20K 2A3 6-G300R2700 Mooney M20L, (Porsche PFM3200N03, 2343RL) M20M, (TSIO-540 AF1A, 2575RL) 2A3 6-G300R2340 6-G300R2570 Mooney M20R North American AT-6 (SNJ-2),-6A,B,C,D,E,F, (SNJ-3,4,5,6,7) (P&W R-1340-47, 2200-2250RL) 2A3 6-G300R2570 A-2-575 9-G300Y2200R2250 NOMAD NA-260 (USA F-28A) (Wright R1820-56S,2500-2600) 1A18 9-G300Y2500R2600 Partenavia Costruzioni P68, P68B,P68C A31EU 4-G300R2700 P68C-TC, P68TC, ( TIO 360-CI A6D, 2575RL) 4-G300R2570 Aeronautiche Twin Piper PA-20,-20S PA-20S "115" PA-20 "135", PA-20S "135" PA-20-"115",(Ly 0-235C1,2600-2800RL) 1A4 4-G300R2600 4-G300Y2600Y2800 Piper PA-22,-22-108, PA-22-135, -22S,-135 1A6 PA-22S-150, -22-160, -22S-160 (0-320-B2AB, 2700RL) 4-G30R260 4-G300R2700 Piper PA-23,-23-160 1A10 4-G300R2700 Twin Piper PA-23-235 Twin PA-E23-250, PA-23-250 1A10 6-G300R2570 6-G300R2570 * See Part Number Designation on Sheet 13 FAA APPROVED MAKE Piper PA-24 Piper MASTER ELIGIBILITY LIST J.P.INSTRUMENTS AIRCRAFT MODE PA-24-250, Lycoming O-540-A1A, 2225-2275, 2575) PA-24-260 (Lycoming O-540-E4A5, 2700RL) Piper PA-24-400 Piper PA-25 Piper PA-25-235 REPORT 410 SHEET NO. 10 I.C.D.S P/N 400000 - XX -[( )-()]*. 1A15 4-G300R2700 1A15 6-G300R2220G2280R2570 6-G300R2700 1A15 8-G300R2650 2A8 4-G300R2700 2A10 2A8 6-G300R2570 2A10 Piper PA-25-260 2A8 6-G300R2700 2A10 Piper PA-28-140,-150,-151, -160, -161 2A13 4-G300R2700 PA-28-180, takeoff (A/C S/N 28-671 to 28-1760A), 2475-2700RL) PA-28S-180, PA-28S-160 4-G300Y2470R2700 4-G300R2700 PA-28R-180 4-G300R2000G2200R2700 PA-28-181 4-G300R2700 PA-28R-200, PA-28R-201, (IO-360-CIC, Hartzell Constant Speed 2A13 Piper Model HC-C2YK-1 2100-2350, / Piper With McCauley Constant Speed Model B2D34C213, 1500-1950YEL-2700RL) 6-G300Y2100G2350R2700 6-G300Y1500G1950R2700 PA-28R-201T, -28-201T, (Continental TSIO-360-F, 2000-2200YEL- 2A13 6-G900R2000G220R2570 2575RL) 6-G900R2570 6-G900Y2650R2700 PA-28RT-201T PA-28RT-201 Piper PA-28-235 PA-28-236 Piper PA-30 Twin PA-39, PA-40 Piper PA-31 Twin PA-31-300, -31-325, 31-350 Piper PA-31P Twin 31P-350 Piper PA-32-260, PA-32-300, PA-32S-300, -32R-300 See Part Number Designation on Sheet 13 2A13 6-G300R2570 6-G900R2400 A1EA 4-G300R2700 4-G300R2700 A20SO 6-G300R2570 6-G300R2570 A8EA 6-G300R3200 6-G300R2600 A3SO 6-G300R2700 FAA APPROVED MAKE MASTER ELIGIBILITY LIST J.P.INSTRUMENTS AIRCRAFT MODE Piper PA-32RT-300 Piper PA-32R-301, PA-32-301 PA-32R-301T, -32-301T Piper Twin PA-34-200, (LIO-360-C1E6, 2200-2400YEL-2700RL) Aircraft equipped with Hartzell propellers damper. Piper PA-34-200T Twin Piper PA-34-220T Piper PA-36-285,(Cont 6-285-B, 4000RL, 2000 PROP) PA-36-300 Piper PA-36-375 REPORT 410 SHEET NO. 11 T.C.D.S P/N 400000 -XX-(()-(1) A3SO 6-G320Y2570R2700 A3SO 6-G320Y2600R2700 6-G320Y2570R2700 A7SO 4-G300R2200G2400R2700 4-G300R2200G2400R2700 A7SO 6-G900R2000G2200R2570 A7SO 6-G350R2000G2200R2570 A9SO 6-G300R4000 A10SO 6-G300R2700 A9SO 8-G300R2500 A10SO Piper PA-38-112 A18SO 4-G300R2600 Piper PA-44-180, PA-44-180T A19SO 4-G300R2700 Twin Piper PA-46-310P A25SO 6-G300R2600 Piper PA-46-350P Piper PA-60-600 (Aerostar) -60-601, -60-601P A25SO 6-G300R2500 A17WE 6-G300Y2520R2570 6-G300Y2470R2570 Twin Pipe PA-60-602P A17WE 6-G300R2420 (Aerostar) Twin Piper PA-60-700P A17WE 6-G300R2500 Twin Republic RC-3 A-769 6-G300R2500 Robinson Helicopter R22, R22 ALPHA, R22 BETA, R22 MARINER H10WE 4-G300R2650 See Part Number Designation on Sheet 13 FAA APPROVED MAKE MASTER ELIGIBILITY LIST J.P.INSTRUMENTS AIRCRAFT MODE Sial-Marchetti S.205-18/F,.205-18/R (Agusta) S.205-20/F, S.205-20/R S.205-22/R S.208, S208A REPORT 410 SHEET NO. 12 T.C.D.S PIN 400000 - XX -[( ) - ( )]* A9EU 4-G300R2000G2250R2700 4-G300R2100G2350R2700 6-G300R2800 6-G300R2100G2350R2700 F.260, F.260B, F.260C A10EU 6-G300R2700 S.O.C.A.T.A TB9 Aerospatiale S.O.C.A.T.A TB10 Aerospatiale S.O.C.A.T.A TB20 Aerospatiale TB21 S.O.C.A.T.A TB-200 Aerospatiale A51EU 4-G300R2700 A51EU 4-G300R2700 A51EU 6-G300R2570 A51EU 6-G300R2700 Swift GC-1A A-766 4-G300R2570 Swift GC-1B A-766 4-G300R2550 Thompson Navion A, "(L-17A, L-17B, L-17C)" (E-185-3, 2300RL) Optional engines: (IO-470H 2625RL) A-782 6-G300R2300 6-G300R2620 (0-470P,2600RL) 6-G300R2600 (10-520, 2700RL) 6-G300R2700 Thompson Navion B A-782 6-G300Y3000R3400 Optional engines: (10-470-H, 2625RL) (10-520, 2700RL) 6-G300R2620 6-G300R2700 Thompson Navion D,E A-782 6-G300R2600 Optional engine (10-520B, 2700RL) 6-G300R2700 Thompson Navion F,G Optional engine (10-520B, 2700RL) Thompson Navion H A-782 6-G300R2620 6-G300R2700 A-782 6-G300R2700 See Part Number Designation on Sheet 13 FAA APPROVED MAKE MASTER ELIGIBILITY LIST J.P.INSTRUMENTS AIRCRAFT MODE Model designation system: 400000 -XX-- REPORT 410 SHEET NO. 13 T.C.D.S P/N 400000 - XX -(( )-(11* A combination of letters and numbers defining the green, yellow and red rpm arcs. The number of cylinders the instrument was calibrated to. Indicates type of sensor: -1 PN420807 Bendix ring -2 PN 420806 Bendix 20 -3 PN 420815 Bendix Plug PN 420100 Slick ring PN 420809 Slick Plug Indicates the base model number of the instruments Example: 400000-3-6-G800Y2100G2350R2700, Indicates a Bendix sensor on a 6 cylinder with the following ranges, green arc from 800 to 2090 rpm, yellow arc from 2100 to 2340 rpm, green arc from 2350 to 2690, red line 2700 rpm. All part numbers begin with 400000-(1-5). Basic Tachometer PN is 400000 and Sensor type of 1 through 5. * See Part Number Designation on Sheet 13
What's in the CESSNA 170B 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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