# STC SA00061LA

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: J P Instruments, United States
- Description: Installation of JPI digital tachometer.
- Applied: May 10, 1993
- Status date: January 12, 1996
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A10EU](https://openairdocs.org/tcds/A10EU), [TCDS A9EU](https://openairdocs.org/tcds/A9EU), [TCDS A17WE](https://openairdocs.org/tcds/A17WE), [TCDS A9SW](https://openairdocs.org/tcds/A9SW), [TCDS 1A3](https://openairdocs.org/tcds/1A3), [TCDS A18CE](https://openairdocs.org/tcds/A18CE), [TCDS A48EU](https://openairdocs.org/tcds/A48EU), [TCDS A-773](https://openairdocs.org/tcds/A-773), [TCDS A-743](https://openairdocs.org/tcds/A-743), [TCDS A-2-575](https://openairdocs.org/tcds/A-2-575), [TCDS 1A18](https://openairdocs.org/tcds/1A18), [TCDS A-768](https://openairdocs.org/tcds/A-768), [TCDS 3A19](https://openairdocs.org/tcds/3A19), [TCDS A-799](https://openairdocs.org/tcds/A-799), [TCDS 3A12](https://openairdocs.org/tcds/3A12), [TCDS 3A17](https://openairdocs.org/tcds/3A17), [TCDS A13CE](https://openairdocs.org/tcds/A13CE), [TCDS A20CE](https://openairdocs.org/tcds/A20CE), [TCDS 5A6](https://openairdocs.org/tcds/5A6), [TCDS 3A13](https://openairdocs.org/tcds/3A13) and 62 more
- Certificate PDF: https://openairdocs.org/files/sha256/5e/69/5e697e53a1e09bc4f70be0404b2f56d360d5111fa3a3115fe874b48d2df48d92
- Approved model list and other attachments: [SA00061LA.pdf](https://openairdocs.org/files/sha256/fd/45/fd45d81c1b3f8c05f9b3781c1af01d3bca0dd30d03540591af62b0489ce95f29)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/304B35E71AE2A9B985256CD400555195.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00061LA

## ADs that name it (0)

None.

## Approved models (687, first 50)

- Aermacchi S.p.A. F.260 ([TCDS A10EU](https://openairdocs.org/tcds/A10EU))
- Aermacchi S.p.A. F.260B ([TCDS A10EU](https://openairdocs.org/tcds/A10EU))
- Aermacchi S.p.A. F.260C ([TCDS A10EU](https://openairdocs.org/tcds/A10EU))
- Aermacchi S.p.A. F.260D ([TCDS A10EU](https://openairdocs.org/tcds/A10EU))
- Aermacchi S.p.A. F.260E ([TCDS A10EU](https://openairdocs.org/tcds/A10EU))
- Aermacchi S.p.A. F.260F ([TCDS A10EU](https://openairdocs.org/tcds/A10EU))
- Aermacchi S.p.A. S.205 - 18/F ([TCDS A9EU](https://openairdocs.org/tcds/A9EU))
- Aermacchi S.p.A. S.205 - 18/R ([TCDS A9EU](https://openairdocs.org/tcds/A9EU))
- Aermacchi S.p.A. S.205 - 20/F ([TCDS A9EU](https://openairdocs.org/tcds/A9EU))
- Aermacchi S.p.A. S.205 - 20/R ([TCDS A9EU](https://openairdocs.org/tcds/A9EU))
- Aermacchi S.p.A. S.205 - 22/R ([TCDS A9EU](https://openairdocs.org/tcds/A9EU))
- Aermacchi S.p.A. S.208 ([TCDS A9EU](https://openairdocs.org/tcds/A9EU))
- Aermacchi S.p.A. S.208A ([TCDS A9EU](https://openairdocs.org/tcds/A9EU))
- Aerostar Aircraft Corporation PA-60-600 (Aerostar 600) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))
- Aerostar Aircraft Corporation PA-60-601 (Aerostar 601) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))
- Aerostar Aircraft Corporation PA-60-601P (Aerostar 601P) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))
- Aerostar Aircraft Corporation PA-60-602P (Aerostar 602P) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))
- Aerostar Aircraft Corporation PA-60-700P (Aerostar 700P) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))
- Air Tractor Inc. AT-300 ([TCDS A9SW](https://openairdocs.org/tcds/A9SW))
- Air Tractor Inc. AT-301 ([TCDS A9SW](https://openairdocs.org/tcds/A9SW))
- Alexandria Aircraft LLC 14-19 ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- Alexandria Aircraft LLC 14-19-2 ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- Alexandria Aircraft LLC 14-19-3 ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- Alexandria Aircraft LLC 14-19-3A ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- Alexandria Aircraft LLC 17-30 ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- Alexandria Aircraft LLC 17-30A ([TCDS A18CE](https://openairdocs.org/tcds/A18CE))
- Alexandria Aircraft LLC 17-31 ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- Alexandria Aircraft LLC 17-31A ([TCDS A18CE](https://openairdocs.org/tcds/A18CE))
- Alexandria Aircraft LLC 17-31ATC ([TCDS A18CE](https://openairdocs.org/tcds/A18CE))
- Alexandria Aircraft LLC 17-31TC ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- Alpha Aviation Concept Limited R2160 ([TCDS A48EU](https://openairdocs.org/tcds/A48EU))
- Bellanca Aircraft Corporation 14-13 ([TCDS A-773](https://openairdocs.org/tcds/A-773))
- Bellanca Aircraft Corporation 14-13-2 ([TCDS A-773](https://openairdocs.org/tcds/A-773))
- Bellanca Aircraft Corporation 14-13-3 ([TCDS A-773](https://openairdocs.org/tcds/A-773))
- Bellanca Aircraft Corporation 14-13-3W ([TCDS A-773](https://openairdocs.org/tcds/A-773))
- Boeing Airplane Company Wichita Division 75 (Army PT-13) ([TCDS A-743](https://openairdocs.org/tcds/A-743))
- Boeing Airplane Company Wichita Division A75 (Army PT-13A; -13B; -13C) ([TCDS A-743](https://openairdocs.org/tcds/A-743))
- Boeing Airplane Company Wichita Division A75J1 (Army PT-18) ([TCDS A-743](https://openairdocs.org/tcds/A-743))
- Boeing Airplane Company Wichita Division A75L3 ([TCDS A-743](https://openairdocs.org/tcds/A-743))
- Boeing Airplane Company Wichita Division A75L300 ([TCDS A-743](https://openairdocs.org/tcds/A-743))
- Boeing Airplane Company Wichita Division A75N1 (Army PT-17; -17A; Navy N2S-1; -4) ([TCDS A-743](https://openairdocs.org/tcds/A-743))
- Boeing Airplane Company Wichita Division B75 (Navy N2S-5) ([TCDS A-743](https://openairdocs.org/tcds/A-743))
- Boeing Airplane Company Wichita Division B75N1 (Navy N2S-3) ([TCDS A-743](https://openairdocs.org/tcds/A-743))
- Boeing Airplane Company Wichita Division D75N1 (Army PT-27) ([TCDS A-743](https://openairdocs.org/tcds/A-743))
- Boeing Airplane Company Wichita Division E75 (Army PT-13D; Navy N2S-5; PT-13D/N2S-5) ([TCDS A-743](https://openairdocs.org/tcds/A-743))
- Boeing Airplane Company Wichita Division E75N1 (Army PT-13D; Navy N2S-5; PT-13D/N2S-5) ([TCDS A-743](https://openairdocs.org/tcds/A-743))
- Boeing Airplane Company Wichita Division IB75A ([TCDS A-743](https://openairdocs.org/tcds/A-743))
- CPAC Inc. 112 ([TCDS A12SO](https://openairdocs.org/tcds/A12SO))
- CPAC Inc. 112B ([TCDS A12SO](https://openairdocs.org/tcds/A12SO))
- CPAC Inc. 112TC ([TCDS A12SO](https://openairdocs.org/tcds/A12SO))

All 687: https://openairdocs.org/stc/SA00061LA/models.md

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

**FAA APPROVED**

**SPINSTRUMENTS**

MASTER ELIGIBILITY LIST NO. 410 INSTALLATION OF THE 400000 SERIES DIGITAL TACHOMETER With Range Lights

**FAA APPROVED JAN 1 2 1996**

ARCAT SECTIONS HOL LOS ANGELES , STC NUMBER: SA00061LA Make: March 20, 1995

**REVISION LOG SHEET NO. 2**

**TO FAA APPROVED MASTER ELIGIBILITY LIST REPORT 410**

REVISION DATE NO. APPROVED REVISION DESCRIPTION N/C 3-20-95 INITIAL RELEASE; SHEETS 1 THRU 8 A JAN 1 2 1996 ADD RANGE LIGHTS SHEETS 3 THRU 13, Revised part number Identification ( see sheet 13)

FAA APPROVED JAN 1 2 1996 AIRCRATS CENTICATION FACE INITIAS: Y

FAA APPROVED MASTER ELIGIBILITY LISTJ.P.INSTRUMENTS REPORT 410 SHEET NO. 3 MAKE AIRCRAFT MODE T.C.D.S P/N 400000 - XX-I) - (11*.

Air Tractor, AT-301 AT-300 A9SW 9-G300R2300 9-G300R2250 Avions Pierre R2160 A48EU 4-G300Y2600R2700 Robin Ayres Corp S2R-R3S 600 S-2D, S-2R, S2R-R1340 A3SW A4SW 9-G300Y2200R2250 9-G300Y2050R2200 Beech 23, A23-19, 19A), A23, A23A, B19, M19A A1CE 4-G300R2700 A23-24, B23,023 4-G300R2700 A23-24, A24, A24R C23 B24R,C24R A1CE 4-G300R2100G2250R2700 4-G300R2150G2350R2700 4-G300R2000G2150R2700 Beech 35, A35 A-777 6-G300R2050R2300 C35, E35, F35, D35 G35 B35, 35R, 6-G300R2050R2450 6-G300R2300R2600 6-G300R2300R2650 Beech H35,J35,K35, M35, 35-A33 G33, N35, P35 ЗА15 6-G300R2620 6-G300R2600 35-33, 35-B33, 35-C33, E33, F33 6-G300R2600 535, V35,V35A, V35B, 35-C33A, E33A, E33C, A36TC, B36TC 6-G300R2700 6-G300Y2550R2700 F33A, F33C, 36, A36 Beech 50 5A4 6-G300Y3000R3400 Twin D50, D50A, B, D50C, E, E-5990 B50, C50 E50, F50, G50, H50, J50 6-G300Y3100R3400 6-G300Y3200R3400 6-G300Y3100R3400 Beech 95, 895 ЗА16 4-G300R2700 Twin 95-8558 95-55, 95-A55, 95-B55, 95B55A B95A, D95A, E95 6-G300Y2550R2620 6-G300R2620 4-G300R2700 95-C55, 95-C55A, 95-D55, 95-D55A, E55, E55A (I0-520C, Below TE1171-2700RL, After sn: TE1171 2550-2700) 6-G300R2700 6-G300Y2550R2700 6-G300R2700 95-58, 58A (I0-520C, sn: TH1095, 2700RL, 6-G300Y2550R2700 sn: 1096 to TH1394, 2550-2700)

**FAA APPROVED JAN 1 2 1996**

**LOS ANGELES**

AIRCRAFT CERTIFICATION OFFIC * See Part Number Designation on Sheet 13 INITIAIS: SE ANM- 140L

FAA APPROVED MASTER ELIGIBILITY LISTJ.P.INSTRUMENTS REPORT 410 SHEET NO. 4 MAKE AIRCRAFT MODE T.C.D.S P/N 400000 - XX-[) - ()1* Beech 56TC, A56TC ЗА16 6-G300R2900 Twin Beech 58P, 58PA, 58TC, 38TCA A23CE 6-G300R2700 Twin Beech 60,60, B60 A12CE 6-G300Y2750R2900 Twin Beech 65-80, 65-A80,65-A80-3800, 65-88,65-880 3A20 6-G30Y3200R3400 Twin 65, A65,A65-8200,70 6-G30Y3200R3400 Beech 76 A29CE 4-G300R2700 Twin Beech 77 A30CE 4-G300R2700 Bellanca 14-13, 14-13-2, -3,-31 A773 6-G300R2600 Bellanca 14-19 1A3 6-G300R2550 14-19-2 6-G300R2600 14-19-3 6-G300R2620 Bellanca 17-30 1А3 6-G300Y2700R2850 Bellanca 17031 1A3 6-G300R2570 Bellanca 17-31 TC 1А3 6-G300Y2400R2570 Bellanca 17-30А, 17-31А A18CE (I0-540G1B5,-G1E5,-G1F5 2575RL) 6-G300R2570 (I0-540K1B5,-K1E5,-K1A5 2700RL) 6-G300R2700 Bellanca 17-31ATC, A18CE (I0-540G1B5,-G1E5,-G1F5 2575RL) 6-G300R2575 (I0-540K1B5,-K1E5,-K1A5 2700RL) 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, 875N1, D75N1 7-G300R2070 Cessna 120,140 A-768 4-G300R2570

FAA APPROVED JAN 1 2 1996 * See Part Number Designation on Sheet 13 AIRCRAFT CERTIFICATION OFFICI LOS ANGELES

FAR APPROVED MASTER ELIGIBILITY LISTJ.P.INSTRUMENTS. REPORT 410 SHEET NO. 5 MAKE AIRCRAFT MODE T.C.D.S _P/N 400000 - XX - [1 - (11* Cessna 140Д 5A2 4-G300R2470 Cessna 150,A,B,C,D,E,F,G,H,J,K A150K, 150L, A150L, 150M ЗА19 4-G300R2750 A150M Cessna 152, A152 ЗА 19 4-G300R2550 Cessna 170,170A, 1708 A-799 6-C300R2700 Cessna 172 ЗА12 6-G300R2700 172A, B,C, D,E,F,G,H Cessna 172, 1, K, L, M,N,P, Q ЗА 12 4-G300R2700 Cessna 172RG ЗА17 4-G300R2700 Cessna R172E, F, G, H, J, (I0-360-D,-H, 2800RL) K, (10-360K, 2600RL) ЗА17 6-G300R2800 6-G300R2600 Cessna P172D, 175,175A, B,C ЗА17 6-G300R3200 Cessna 177, 177А, 177฿ 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) 180A, B,C,D,E,F, G,H,J 180K 6-C300R2550 6-G300R2600 6-G300R2400 Cessna 182, 182A,B,C,D,E,F,G,H,J, K,L,M,N, P ЗА13 6-G300R2600 182, Q,R, R182, T182, TR182 6-G300R2400 Cessna 185,185A, B,C,D,E 3А24 6-G300R2620 Cessna A185E, A185F 3A24 6-G30Y2700R2850 Cessna 188,188A,1888 A188,A188A, A188B T188C ASCE 6-G300R2600 6-G300Y2700R2850 6-G300R2700 Cessna 190, 195,195B 195A A-790 7-G300Y2000R2200 7-G300R2200

FAA APPROVED JAN 1 2 1996 * See Part Number Designation on Sheet 13 AIRCRAFT CERTIFICATION OFFICE NITIMIS: IN ANM- 140L LOS ANGELES

FAA APPROVED MASTER ELIGIBILITY LISTJ.P.INSTRUMENTS REPORT 410 SHEET NO. 6 MAKE AIRCRAFT MODE T.C.D.SP/N 400000 - XX-[1-111 Cessna 206,P206, P206A,B, C,D,E A4CE 6-G300R2700 TP206A,B,C,D,E 6-G300R2700 Cessna U206,J206A U206B,C,D,E,F,G A4CE 6-G300R2700 6-G300Y2700R2850 TU206A,B,C,D,E,F,G 6-G300R2700 Cessna 207,207A A16CE 6-G300R2700 Cessna T207,T207A A16CE 6-G300Y2600R2700 Cessna 210,210A ЗА21 6-G300YR2620 Cessna 210B,C ЗА21 6-G300R2620 Cessna 210D, E,F ЗА21 6-G300R2700 Cessna 210-3,210-54 3А21 6-G300R2620 210G,, 210H, 210J T210F, T210G, T210H 6-G30R2700 6-G30R2700 Cessna T210J, T210K, T210L 3А21 6-G300R2700 210K, 210L, 210M,210N, 210R T210M, T210N, P210N 6-G300Y2700R2850 6-G300Y2600R2700 6-G30R2700 P210R, T210R Cessna 305A,C,D,F 5A5 6-G300Y2300R2600 Cessna 310,310Д,В ЗА10 6-G300R2600 Twin Cessna 310C, D,E,F,G,H,J, 310J-1, E310H, 3101, E310J ЗА10 6-G300R2620 Twin 310K, L,N,P,Q Cessna 310R, T310Q,T310P, T310R ЗА10 6-G300R2700 Twin Cessna 320,А,В,C, 320-1 3А25 6-G300R2600 Twin 320D, E, F,335, 340,340A 6-G300R2700 Cessna 321 ЗА11 6-G300R2600 Twin Cessna 336 A2CE 6-G300R2800 Twin

FAA APPROVED JAN 1 2 1996 * See Part Number Designation on Sheet 13 AIRCRAFT CERTIFICATION OF ICE LOS ANGELES ANS-140 L

FAA APPROVED MASTER ELIGIBILITY LISTJ.P.INSTRUMENTS REPORT 410 SHEET NO. 7 MAKE AIRCRAFT MODE T.C.D.S. P/N 400000 - XX-I) - () 1*.

Cessna 337, 337A,B, C,D,E,F,G,H A6CE 6-G300R2800 Twin T337B,C,D,E,F,G,H, M337B (MIL), P337H 6-G300R2800 T337H-SP, (TSIO-360-JB 2600-2800RL) 6-G300Y2600R2800 Cessna 401, 401A,B, 402,402A, B, C A7CE 6-G300R2700 Twin Cessna 404, 406 (GTSIO-520M, 3350RL, 2235PROP @ .667:1) A25CE 6-G300R3350 Twin Cessna 411,411A, (GTSIO-520C, 3200RL 2400Prop @.750:1) A7CE 6-G300R3200 Twin Cessna 414,4144 " A7CE 6-G300R2700 Twin Cessna 421,421A 421B, (GTSIO-520H, 3400RL 2275PROP @.667:1) A7CE 6-G300R3400 Twin Cessna 421C, (GTSIO-520H, 3350RL 2235PROP @.667:1) A7CE 6-G300R3350 Twin Consolidated C-1, C-2, LAKE LA-4, LA-4A, LA-4P 1A13 4-G300R2700 Aeronautical Consolidated LA-4-200 1A13 4-G300R2000G2350R2700 Aeronautical Consolidated LA-4-250 1A13 6-G300R2570 Aeronautical De Havilland DHC-2 Mk. I, DHC-2 Mk. II, DHC-2MK. III A-806 9-G300Y2200R2300 Enstrom F-28 H1CE 4-G300R2700 Helicopter F-28A,-28C, -28F, 280, 280C 4-G300R2900 280F, 280FX 4-G300R3050 AVIA GENERAL F22C F22B, F22R A75EU 4-G300R2700 4-G300R2000G2250R2700 Construzioni Aeronautiche GENERAL F20 (I0-520F, 2700-2850RL) twin A38EU 6-G300Y2700R2850 AVIA Construzioni Aeronautiche Twin FAA APPROVED JAN 1 2 1996 * See Part Number Designation on Sheet 13 IRATIS Z TOM POL LOS ANCELES

FAA APPROVED MASTER ELIGIBILITY LISTJ.P.INSTRUMENTS REPORT 410 SHEET NO. 8 MAKE AIRCRAFT MODE T.C.D.S P/N 400000 - XX-I) - (11* Grumman АД-1, -1А, -1В A11EA 4-G300R2600 Grumman АД-10 A11EA 4-G300R2700 Gulfstream AA-5, AA-SA, АД-5B A16EA 4-G300R2700 Commander 112,112B A12SO 4-G300R2700 Aircraft Commander 112TC, 112TCA A12SO 4-G300R2570 Aircraft Commander 114,114A, 8 A12SO 6-G300R2700 Aircraft Gulfstream 500 6A1 6-G300R2575 ( Twin Commander 500-A 6-G300R2620 Aircraft ) 500-B, U, S 6-G300R2620 520, 560,560A, -E 6-G300Y3000R3400 Gulfstream 560F 2A4 6-G300Y3000R3400 I Twin Aircraft ) Commander 680,E, 720 680-F, 680 FL, 680-FL(P) 6-G300Y3200R3400 6-G300Y3200R3400 685 6-G300R3400 Hughes 269A, (HO-360-B1A, 2900RL) 4H12 4-G300R2900 Helicopter (Schweizer) 269A (0-360-C2D, 2700-2900) 4-G300Y2700R2900 269A-1, (H10-360-BIA, 2900RL) 4-G300R2900 2698, 269C, (HIO-360-D1A,3200RL) 4-G300R3200 Maule Bee Dee M-4, M-4, 4C, 45, 4T 3А23 4-G300R2700 Maule M-4-210,C,S,T, M-4-220C,S,T, M-4-180C,S,T ЗА23 6-G300R2800 Maule M-5-180C, (Lyc 0-360-C1F,2000-2250, 2700RL) ЗА23 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

FAA APPROVED JAN 1 2 1996 * See Part Number Designation on Sheet 13 LOS ANGELES

AIRCRAFT CERFIFICATION OFFICI NITIAIS: 245 ANM-140L

FAA APPROVED MASTER ELIGIBILITY LISTJ.P.INSTRUMENTS REPORT 410 SHEET NO. 9 MAKE AIRCRAFT MODE T.C.D.S P/N 400000 - XX-I) - (11* Maule M-5-210C, M-5-220C ЗА23 6-G300R2800 M-5-210TC, (TO-360F1A6, 2575RL) 4-G300R2570 Maule M-5-235C, (0-540JI, I0-540W, 2400RL) ЗА23 6-G300R2400 M-5-235C with (0-540B, 2575RL) 6-G300R2570 Maule M-6-180 ЗА23 4-G300R2000G2250R2700 M-6-235 6-G300R2400 Maule M-7-235,A, B, MX-7-235, M-8235, (0-540JI,W, 2500RL) ЗА23 6-G300R2500 M-7-235,A, B, MX-7-235, M-8235, with (0-540B, 2575RL) 6-G300R2570 MXT-7-235, (I0-540W1A5, 2400RL) 6-G300R2400 Mooney M20 M20A, B,C,D,G (0-360 A1A, 2000-2250, 2700RL) 2A3 4-G300R2000G2250R2700 4-G300R2000G2250R2700 Mooney M20E, F (I0-360 A1A, 2000-2350 RED, 2700RL) 2A3 4-G300R2000G2350R2700 Mooney M20J 2A3 4-G300Y1600G1950R2700 Vooney M20K 2A3 6-G300R2700 Mooney M20L, (Porsche PFM3200N03, 2343RL) 2А3 6-G300R2340 M20M, (TSIO-540 AF1A, 2575RL) 6-G300R2570 Mooney M20R 2A3 6-G300R2570 North AT-6 (SNJ-2), 6A, B,C,D,E,F, (SNJ-3,4,5,6,7) A-2-575 9-G300Y2200R2250 American (P&W R-1340-47, 2200-2250RL) NOMAD NA-260 (USAF-28A) (Wright R1820-565,2500-2600) 1A18 9-G300Y2500R2600 Partenavia P68, P68B,P68C A31EU 4-G300R2700 Costruzioni P68C-TC, P68TC, (TIO 360-C 1 A6D, 2575RL) 4-G300R2570 Aeronautiche Twin Piper PA-20,-20S PA-2OS "115" PA-20 "135", PA-20S "135" 1A4 4-G300R2600 PA- 20-"115", (Ly 0-235C1,2600-2800RL) 4-G300Y2600Y2800 Piper PA-22,-22-108, PA-22-135, -22S,-135 1A6 4-G30R260 PA-22S-150, -22-160, -22S-160 (0-320-B2AB, 2700RL) 4-G300R2700 Piper РA-23,-23-160 1A10 4-G300R2700 TwIn

FAA APPROVED Piper РД-23-235 1A10 6-G300R2570 Twin PA-E23-250, PA-23-250 6-G300R2570 JAN 1 2 1996 * See Part Number Designation on Sheet 13

**ARCAT SEE TON OF CO**

FAA APPROVED MASTER ELIGIBILITY LISTJ.P.INSTRUMENTS REPORT 410 SHEET NO. 10 MAKE AIRCRAFT MODE T.C.D.S P/N 400000 - XX-I) - (11* Piper PA-24 1A15 4-G300R2700 Piper PA -24-250, Lycoming O-540-A1A, 2225-2275, 2575) 1A15 6-C300R2220G2280R2570 PA-24-260 (Lycoming O-540-E4A5, 2700RL) 6-G300R2700 Piper PA-24-400 1A15 8-G300R2650 Piper PA-25 2A8 4-G300R2700 2A10 Piper PA-25-235 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-G300R2700 4-G300Y2470R2700 PA-28R-180 4-G300R2000G2200R2700 4-G300R2700 PA-28-181 Piper PA-28R-200, PA-28R-201, (10-360-C1C, Hartzell Constant Speed Model HC-C2YK-1 2100-2350, / 6-G300Y2100G2350R2700 With McCauley Constant Speed Model B2D34C213, 6-G300Y1500G1950R2700 1500-1950YEL-2700RL) Piper PA-28R-201T, -28-201T, (Continental TSIO-360-F, 2000-2200YEL- 2A13 6-G900R2000G220R2570 2575RL) PA-28RT-201T 6-G900R2570 PA-28RT-201 6-G900Y2650R2700 Piper PA-28-235 2A13 6-G300R2570 PA-28-236 6-G900R2400 Piper Twin PA-39, PA-40 PA-30 A1EA 4-G300R2700 4-G300R2700 Piper Twin PA-31 PA-31-300, -31-325, 31-350 A20SO 6-G300R2570 6-G300R2570 Piper Twin PA-31P 31P-350 ASEA 6-G300R3200 6-G300R2600 Piper PA-32-260, PA-32-300, PA-325-300, -32R-300 A3SO 6-G300R2700

FAA APPROVED JAN 1 21996 * See Part Number Designation on Sheet 13 AIRCRAFT CERTIFICATION OFFICE LOS ANGELES NITIALS: MANM- 140L

FAA APPROVED MASTER ELIGIBILITY LISTJ.P.INSTRUMENTS REPORT 410 SHEET NO. 11 MAKE AIRCRAFT MODE T.C.D.S P/N 400000 - XX-I) - ()1* Piper PA-32RT-300 A3SO 6-G320Y2570R2700 Piper PA-32R-301, PA-32-301 PA-32R-301T, -32-3011 A3SO 6-G320Y2600R2700 6-G320Y2570R2700 Piper PA-34-200, (LIO-360-CIEG, 2200-2400 YEL-2700RL) Twin Aircraft equipped with Hartzell propellers damper.

A7SO 4-G300R2200G2400R2700 4-G300R2200G2400R2700 Piper PA-34-200T A7SO 6-G900R2000G2200R2570 Twin Piper PA-34-220T A7SO 6-G350R2000G2200R2570 Piper PA-36-285, (Cont 6-285-B, 4000RL, 2000 PROP) PA-36-300 A10SO 6-G300R2700 A9SO 6-G300R4000 Piper PA-36-375 A9SO 8-G300R2500 A10SO Piper PA-38-112 A18SO 4-G300R2600 Piper PA-44-180, PA-44-180T A19SO 4-G300R2700 Twin Piper РД-46-310Р A25SO 6-G300R2600 Piper РД-46-350Р A25SO 6-G300R2500 (Aerostar) Piper PA-60-600 60-601, -60-601Р A17WE 6-G300Y2520R2570 6-G300Y2470R2570 Twin Pipe PA-60-602P A17WE 6-G300R2420 (Aerostar) Twin Piper PA-60-700P A17VVE 6-G300R2500 Twin Republic RC-3 A-769 6-G300R2500 Robinson R22, R22 ALPHA, R22 BETA, R22 MARINER H10WE 4-G300R2650 Helicopter

**FAA APPROVED JAN 1 21996**

MRCRAFT CANSIHCAFION OF ICE * See Part Number Designation on Sheet 13 NITIALS. SU AUM-140 C

FAA APPROVED MASTER ELIGIBILITY LISTJ.P.INSTRUMENTS REPORT 410 SHEET NO. 12 MAKE AIRCRAFT MODE T.C.D.S P/N 400000 - XX -[() - ()]*.

Siai-Marchetti S.205-18/F,-205-18/R AGEU 4-G300R2000G2250R2700 (Agusta) S.205-20/F, S.205-20/R 4-G300R2100G2350R2700 S.205-22/R 6-G300R2800 6-G300R2100G2350R2700 S.208, S208A F.260, F.ZCOB, F.260C A10EU 6-G300R2700 S.O.C.A.T.A TB9 A51EU 4-G300R2700 Aerospatiale S.O.C.A.T.A TB10 A51EU 4-G300R2700 Aerospatiale S.O.C.A.T.A TB20 A51EU 6-G300R2570 Aerospatiale TB21 S.O.C.A.T.A TB-200 A51EU 6-G300R2700 Aerospatiale 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) A-782 6-G300R2300 Optional engines: (10-470H , 2625RL) 6-G300R2620 (0-470P ,2600RL) 6-G300R2600 (10-520, 2700KL) 6-G300R2700 Thompson Navion B A-782 6-G300Y3000R3400 Optional engines: (10-470-H, 2625RL) 6-G300R2620 (10-520, 2700RL) 6-G300R2700 Thompson Navion D,E A-782 6-G300R2600 Optional engine (10-520B, 2700RL) 6-G300R2700 Thompson Navion F,G A-782 6-G300R2620 Optional engine (10-520B, 2700RL) 6-G300R2700 Thompson Navion H A-782 6-G300R2700

**FAA APPROVED JAN 1 2 1996 LOS ANGELES .**

ARCRAFT CERTIFICATION OF IC NITIMIS:LE ANM-140L * See Part Number Designation on Sheet 13

FAA APPROVED MASTER ELIGIBILITY LISTJ.P.INSTRUMENTS REPORT 410 SHEET NO. 13 MAKE AIRCRAFT MODE T.C.D.S P/N 400000 - XX-I) - (11* Model designation system:

400000-XX-[()-()] A combination of letters and numbers defining the green, yellow and red rom arcs.

The number of cylinders the instrument was calibrated to .

Indicates type of sensor : -1 PN420807 Bendix ring -2 PN 420806 Bendix 20 PN 420815 Bendix Plug -4 PN 420100 Slick ring -5 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.

FAA APPROVED JAN 1 21996 * See Part Number Designation on Sheet 13

### SA00061LA.pdf

This is OCR from the scanned FAA attachment. OCR can misread letters and numbers.

8103 Minited States of Simerica Department of Cransportation -Federal Aviation Administration Supplemental Type Certificate Number SA00061LA This certificate, issued 10 J.P. INSTRUMENTS 9621 Bay Meadow Drive Huntington Beach, California 92646 certifies that the change in the type design for the foltowing product with the limitations and conditions herefor as specified hereon meets the airvorthiness requirements of Jar « See Applicable Type Certificate Data Sheet (T.C.D.S.) for certification basis Federal Aviation Regulations * See Attached FAA Approved J.P.

Originad Product Type Certificate Number: Matie: Instruments Master Eligibility List No. 410 Model: for list of approved aircraft models and applicable T.C.D.S.

Descriplion of hype Design Change: 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 banditions: 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 date which is the bas is fur approval shull remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrate r of the Federal Aviation Administration.

Date of application: May 10, 1993 Jute missued:

Date of issuance: March 29, 1995 Jate unended: January 12, 1996 FEDERAL AVIATION 'By direction of the Administrator Repon Alias ter *MINISTRATOR Los Angeles Aircraft Certification Office Manager, Propulsion Branch (Title) Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both This certificate may be transferred in accordance with FAR 21.47.

**FAA FORM 8110-2 (10-68)**

## Every issue (1)

- January 12, 1996: Amended, Current. [certificate](https://openairdocs.org/files/sha256/5e/69/5e697e53a1e09bc4f70be0404b2f56d360d5111fa3a3115fe874b48d2df48d92), [SA00061LA.pdf](https://openairdocs.org/files/sha256/fd/45/fd45d81c1b3f8c05f9b3781c1af01d3bca0dd30d03540591af62b0489ce95f29)

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