STC SA00061LA

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