# STC SA2586NM

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: J P Instruments, United States
- Description: Installation of J.P. Instruments temperature monitoring systems.
- Applied: December 31, 1984
- Status date: September 20, 2017
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS A10EU](https://openairdocs.org/tcds/A10EU), [TCDS A17WE](https://openairdocs.org/tcds/A17WE), [TCDS 4A19](https://openairdocs.org/tcds/4A19), [TCDS A-773](https://openairdocs.org/tcds/A-773), [TCDS 1A3](https://openairdocs.org/tcds/1A3), [TCDS A18CE](https://openairdocs.org/tcds/A18CE), [TCDS A-743](https://openairdocs.org/tcds/A-743), [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 5A6](https://openairdocs.org/tcds/5A6), [TCDS 3A13](https://openairdocs.org/tcds/3A13), [TCDS 3A24](https://openairdocs.org/tcds/3A24), [TCDS A-790](https://openairdocs.org/tcds/A-790), [TCDS A16CE](https://openairdocs.org/tcds/A16CE), [TCDS 3A21](https://openairdocs.org/tcds/3A21), [TCDS 3A10](https://openairdocs.org/tcds/3A10), [TCDS 3A25](https://openairdocs.org/tcds/3A25) and 90 more
- Certificate PDF: https://openairdocs.org/files/sha256/5e/35/5e35eade56f2e2d0e4d5ad1e41b80bca2bc7679df0f34c1eb505cfcb384fb74c
- Approved model list and other attachments: [SA2586NM_AML.pdf](https://openairdocs.org/files/sha256/58/4a/584a4c680a7a273389914c9d9ea9b5fa9a8f72776ecd101f748fc6f1ffd32834)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C7F62E4C2D3B1A1A862581A60046CF99.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2586NM

## ADs that name it (0)

None.

## Approved models (911, 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))
- American General Aircraft Holding Co. Inc. AA-5 ([TCDS A16EA](https://openairdocs.org/tcds/A16EA))
- American General Aircraft Holding Co. Inc. AA-5A ([TCDS A16EA](https://openairdocs.org/tcds/A16EA))
- American General Aircraft Holding Co. Inc. AA-5B ([TCDS A16EA](https://openairdocs.org/tcds/A16EA))
- American General Aircraft Holding Co. Inc. AG-5B ([TCDS A16EA](https://openairdocs.org/tcds/A16EA))
- Augustair Inc. 2150 ([TCDS 4A19](https://openairdocs.org/tcds/4A19))
- Augustair Inc. 2150A ([TCDS 4A19](https://openairdocs.org/tcds/4A19))
- Augustair Inc. 2180 ([TCDS 4A19](https://openairdocs.org/tcds/4A19))
- 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))
- Bellanca Aircraft Corporation 14-19 ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- Bellanca Aircraft Corporation 14-19-2 ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- Bellanca Aircraft Corporation 14-19-3 ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- Bellanca Aircraft Corporation 14-19-3A ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- Bellanca Aircraft Corporation 17-30 ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- Bellanca Aircraft Corporation 17-30A ([TCDS A18CE](https://openairdocs.org/tcds/A18CE))
- Bellanca Aircraft Corporation 17-31 ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- Bellanca Aircraft Corporation 17-31A ([TCDS A18CE](https://openairdocs.org/tcds/A18CE))
- Bellanca Aircraft Corporation 17-31ATC ([TCDS A18CE](https://openairdocs.org/tcds/A18CE))
- Bellanca Aircraft Corporation 17-31TC ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- Boeing Airplane Company Wichita Division 75 (Army PT-13) ([TCDS A-743](https://openairdocs.org/tcds/A-743))
- Boeing Airplane Company Wichita Division A75 Series ([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 Series ([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 Series ([TCDS A-743](https://openairdocs.org/tcds/A-743))
- Boeing Airplane Company Wichita Division E75N1 ([TCDS A-743](https://openairdocs.org/tcds/A-743))

All 911: https://openairdocs.org/stc/SA2586NM/models.md

## What the certificate says

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

9103 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA2586NM This certificate issued to: J. P. INSTRUMENTS 9621 Bay Meadow Drive Huntington Beach, CA 92646 Part 3 of the Civil Aviation Regulations, including respective Amendment's as specified in the altached Approved Model List.

Original Product Type Certificate Number: * *See attached FAA Approved J.P. Instruments Make: * Master Eligibility List No. SA2586NM for list Model: * of approved aircraft models and applicable TCDS Description of Type Design Change:

Installation of J. P. Instruments temperature monitoring systems in accordance with FAA Approved J. P.

Instruments Drawing List Report No. 100, Revision D, dated December 19, 1996, or later FAA approved revisions. FAA Approved Airplane/Rotorcraft Flight Manual Supplement No. 1 for EGT-701 temperature indicator, Revision A, dated December 13, 1996, or later FAA approved revisions.

Limitations and Conditions: The approval of the change in type design applies to the basic airplane of the specific models that are otherwise unmodified. 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 installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of that airplane. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. (See continuation sheet) Date Reissued:

Date of Application: December 31, 1984 Date Amended: July 13, 1987, November 13, Date of Issuance: August 14, 1985 1992, December 19, 1996, May 15, 1998, June 17, 1999 FEDERAL AVIATION By Direction of the Administrator Ay son nur en (Signature) TOMINSTRATIO Los Angeles Aircraft Certification Office Manager, Propulsion Branch (Title)

TRANSFER ENDORSEMENT Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (Number and street) (City, State, and Zip code) trom (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and Zip code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA2586NM Limitations and Conditions: - continued Cylinder head, oil, turbine inlet and/or exhaust gas temperature, fuel flow equipment, tachometer instruments, and manifold pressure instruments required by the original type design, or if required by other FAA approval, must remain installed and operable.

Aircraft listed on the FAA approved Master Eligibility List SA2586NM and that have been previously modified with a fuel flow indication system that utilizes the Flowscan fuel flow transducer (P/N: 201-A, 201-B, 201-C, or 231 or equivalent as listed on page 4 of the FAA Approved Installation Instructions, Drawing 103) are eligible for installation of the EGT-701 fuel flow option.

This certificate does not constitute installation approval of the fuel flow transducer.

EGT-701 temperature indicator with tachometer (rpm) and manifold pressure options are eligible for the 4 cylinder and 6 cylinder engines listed on the Master Eligibility List (MEL) SA2586NM only.

FAA Approved Airplane/Rotorcraft Flight Manual Supplement No. 1, Revision A, dated December 13, 1996 or later FAA approved revision, is required with the installation of the EGT-701 system.

Eligible dash numbers for the EGT-701 are listed on MEL SA2586NM.

A copy of this certificate must be maintained as part of the permanent records of the modified aircraft.

-END-

### SA2586NM_AML.pdf

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

d ADD AP INSTRUMENTYS

MASTER ELIGIBILITY LIST NO. SA2586NM INSTALLATION OF THE EGT 100, 200 SERIES AND 701 SERIES TEMPERATURE

**INDICATORS, FOR EXHAUST GAS, CYLINDER HEAD TEMPERATURE MONITORING SYSTEM.**

STC NUMBER: SA2586NM REV 15 DATE: AUGUST 14,1985 DATE: Sept 20, 2017

FAA APPROVED Los Angeles INITIALS: 2 nice a nging once SEP 2 1 2017 RECEIVED Los Angeles Aircraft Certification Office CONTROL NO. 11-DOC - 2981 Action SEP 1 8 2017 10/3/17 Date Ans.

File Code:

**REVISION LOG**

TO FAA APPROVED MASTER ELIGIBILITY LIST NO. SA2586N REVISION DATE NO. REVISION DESCRIPTION APPROVED SHEET 2 NC - 1 9-23-85 8-14-85 Initial Release; Addition of; Cessna Models 320, 336, 340 and Piper Models PA-38, PA-44, PA-60 series; Sheet 6 Format Sheets 1 thru 5 -2 - 3 7-13-87 7-22-86 Addition of: Piper PA-46-310P (Malibu), PA-31P (Navajo) Suffix (O), added to instrument part number PA-32-301 Series ; Republic RC-3; Swift GC-1A and GC-1B Series; 14-13 and 14-19 Series; Cessna 185, 188, and 321 Series; Maule M-4, M-5 and M-6 Series; Piper PA-22, Addition of: Gulfstream American 112, 114, AA-5, 560 and 680; Beech 50, 60, 65, 76, Series ; Bellanca changes and typing corrections Omission of "Approval Date" column on sheet 6 and subsequent sheets Sheets 5,6 and 7 -4 5-23-90 Addition of: Enstrom Helicopter F-28,-28A,-28C,-28F, 280, 280C, 280F; Hughes Helicopter 269A, 269A-1, the options in parenthesis are applicable. Reorganized indicating Oil temperature PMA'd probe, P/N 400505,-L,-C. Applicable to all Lycoming and Continental direct drive piston engines. Suffix (T) added to instrument part number indicating turbine inlet temperature with probe P/N M-111 Parenthesis () added to any instrument part number, will indicate: None, Any or All" of Sheets ALL -9 -8 -7 12-19 -96 -5 -6 01-13-99 11-11-92 07-14-98 11-09-95 Beech Model D17S, SD17S, D17R, D17A. C17R, G17S. Piper PA-18 Series. Robinson R44 VARGA Series. Grumman G21. Corrected P/N. Was EGT-710 to EGT-701 De Havilland, DHC-2 Mk. series, North American T-28A series, WACO series and Beech 45 series. Addition of : Extra EA-300,S, L, EA-300/200. Maule MX-7-180C, MXT-7-180A, Addition of : Meyers (PROP-JETS, INC) 200, 200A, B, C, D. Gulfstream American GA-7 engines only". Added Cessna 170,A,B, 172R. Bellanca 17-30A series. AERO COMMANDER B-1, B-1A, . 269B, 269C; Robinson Helicopter R22, R22-Alpha, R22-Beta, R22-Mariner; Mooney Aircraft M20L, M20M; Addition of : GENERAL AVIA Construzioni Aeronautiche F22B, F22R, F22C & F20; Mooney M2OR ; Air Addition of : Added sheet 9 & 10 model designation system and Eligible Part Numbers. Revised all Part Numbers, all sheets. Added Fuel Flow suffix to P/N. Removed note "EGT-701 approved for 4 & 6 cylinder Siai-Marchetti S.205-18/F, -18/R, -20/F. -20/R, 22/R, S.208, S.208A, F.260, F.260B, F.260C ; S.O.C.A.T.A Addition of: EGT-701 (series) approved aircraft having for 4 or 6 cylinder engines only. Deleted aircraft model: Beech, all 90 series; Piper, PA-31T, -31T1,-31T2,-31T3. Sheets 2,3,7 TB10, TB20, TB21 ; Partenavia Costruzioni P68, P68B, P68C, P68C-TC, P68TC, AP68TP 300. Piper Tractor AT-300, -301; Ayres Corp. 600S-2D,S-2R, S2R-R1340; Avions Pierre Robin R2160 M-7-235, A, B, C, M-7-260, MT-7-260. Cessna 182S, 206H. Siai-Marchetti F.260D,E,F. Piper PA23-250 Sheets 2,5,6,8 -12 06-11-01 -13 04-18-03 H-295, HT-295, H-395, H-391, H-391B, H-700, H-800 Flugzeugbau EA-400 • Slingsby T67M260, T67M260-T3A • Wilga 80, Wilga 2000, •Helio (Alliance Aircraft) Mooney M-22., M20S, Jobmaster Comp DGA-15P. Weatherly 620, A, B. Thompson Navion C. Cessna U206A, B, C, D, E, F, G. (conv. Per STC 2123NM) 00472SE & STC SA 5691NM) M20K, M20J. Pitts (Aviat) S-1S, S-1T,S-2, S-2A. Christen (Avait) A-1, S-2B. Addition of : Beech 77 • Cirrus 22 • Cessna T303 • Diamond Aircraft DA20-A1, DA20-C1,DA40 • Extra T206H. Gulfstream American 114 B, TC. Maule MXT-7-180 ,A,B. Mooney (Rocket Conv. Per STC SA Addition of : RPM & MAP to identification list for EGT-701 Addition of : American Champ 8KCAB, 7GCBC, 7ECA, 7GCBA, 7GCAA, 7KCAB. Beech 95-58, Cessna Addition of : American General GA-7 • Beech V35, A, B (STC SA1035WE) • Beech, 58, 76 • Lance, LC40- 550FG • Cessna 140 (STC SA547EA) • 172,S, T• 182T, RS, T182T • 182E-Q (STC SA3825SW) • Cirrus SR-20 • Piper PA-18,18A-"150" (STC SA682AL, STC SA00035NY) • Piper PA-24-200 Sheets 3,5,6, 7, 8 Sheets 3,5,6,7,8 -14 07-20-08 1,2,3 • Cessna F182P, Q, FR182 • Chaparral Motors, 2T-1A,-1,-2 • Maule, MXT-7-160, MX-7-180AC, M-5- Addition of : American Champion Aircraft Corp., 8GCBC • Beagle (DeHavilland Support, Ltd.) B121 series Sheets 5, 6, 7, g -15 09-20-17 Added Robinson R-44 Il 22-150 • Univair Aircraft Corp, 108, 108-1,-2,-3, 5 • WACO YMF (F5,F5C) 200, M-7-260, M-4-220C, M-4-220S,T, MT-7-235, M5-235C • Micco Aircraft Co, MAC-145, 145A, B • Mooney M20TN • Moravan Inc. Z-242L,Z-143L • Pilatus Aircraft PC6/350, PC6/350-H1,-H2 • Piper, PA-12,-12S, PA- Sheet 9 Sheets 2, 3, 4, 5, 6, 7

FAA APPROVED MASTER ELIGIBILITY LIST J.P.INSTRUMENTS REPORT: SA 2586NM MAKE AIRCRAFT MODEL Part Number SHEET - 5 - T.C.D.S. (See Sheet. 11 for Series)

4. 3. 2. 1. Avions Pierre Robin AERO COMMANDER Ayres Corp Air Tractor S2R-R3S AT-300,AT-301 600 S-2D, S-2R, S2R-R1340 R2160 B-1, B-1A 100-180 Lycoming I0-720-A1A A8WE A48EU A9SW A3SW (8), (D) (9), (E) (9), (E) (4), (A) American Champion 8KCAB A8WE (4), (А) Aircraft Corp American Champion 8GCBC A21CE (4), (А) Aircraft Holdings, Grumman Aircraft Corp Aircraft Corp. American General American Champion 7GCBC, 7ECA, 7GCBA, 7GCAA, 7KCAB GA-7 Twin A17SO A21CE A-759 (6T*), (BT*) (4), (A) (4), (А) Aerospace) Support Ltd.) (British Beagle (DeHavilland B. 121 Series 1, 2, 3 A22EU (4), (A)

11. Beech Model D17S, SD17S, D17R, 45J or UC-45J (SNB-5), RC-45J (SNB-5P), E18S-9700, G18S, JRB-6, 3N, 3NM, 3TM, D18S, D18C, E18S, C-45G, TC-45G, C-45H, TC-45H, TC- P7W Wasps Jr. A-765 (9), (E)

14. 15. 12. 13. Beech Beech Beech Beech F35,G35,35R H35,J35,K35, M35, N35, P35,S35, (YT-34)45, (T-34A, B-45)A45, (T-34B) D45 A24,A24R, B24R, C24R 35,A35,B35,C35,D35,E35, G17S C17R (Army UC-43E) B19,M19A,A23-24,B23,C23, 23,A23,A23A,A23-19,19A Cont. E-225-8 ATC-779 ATC-604 ATC-713 A-777 A1CE A-649 5А3 (6), (B) (6), (B) (4), (A) (9), (E) (9), (E) (9), (E) (9), (E) V35, V35A, V35B, 35-33,35-A33, 35-B33,35-C33,35-C33А ЗА15 (6), (B)

17. 16. Beech Beech 50, B50; D50,A,B,C,E, G33,36,A36,A36TC,B36TC E33,33A, E33C,F33,F33A,F33C, V35, V35A, V35B with Optional engine TSI0-520 per STC SA1035WE ЗА15 (6), (B)

18. 19. 20. Beech Beech Beech 65, 65-80,65-A80,65-A80-8800, 60, A60, B60 E-5990; E50,F,G,H,J 58, 58P, 58PA, 58TC, 58TCА A12CE A23CE 5A4 (6T*), (BT*) (ST*), (BT*) (6T), (BT) 65-88,65-B80,A65 3A20 (6T), (BT) A65-8200,70,

21. Beech 76

23. 24. 22. Beech Beech Beech 95-55,-A55,-B55,-B55A 95,B95, B95A,D95A,E95 77 A3OCE A29CE 3A16 (4T), (AT) (4T), (AT) (4), (A) D55, D55A, E55, E55A,56TC, -C55,-C55A ЗА16 (6T*), (BT*) 26 25. Bellanca Bellanca А56TC, 58,58A, 95-58 14-19,19 -2, -3, -ЗА 14-13, 14-13-2,-3, -3W A773 (6), (B) FAA approved AFM Supplement is required with the EGT-701. The EGT-701 is applicable to all EGT-100/200 series. RPM and MAP applicable to the PIN EGT-701,4 and 6 cylinder engines only Revision 14 1A3 (6), (B)

FAA APPROVED MASTER ELIGIBILITY LIST J.P.INSTRUMENTS REPORT: SA 2586NM MAKE AIRCRAFT MODEL Part Number SHEET - 6 - 32 30. 31. 28. 27. 29. Cessna Cessna Cessna Boeing Cessna Boeing Cessna 172,172A,B,C,D,E,F,G,H, A150M, 152, A152 170. 170A, 170B A150K, 150L, A150L, 150M, 150, A,B, C,D,E,F,G,H,J,K IB75A, E75N1 A75J1, A75N1, B75N1, D75N1 B75, E75, A75, A75L300, (STEARMAN) A75L3,75,A75, 140A, with 0-200 Conversion per STC-SA547EA 140 17-30,-A, 17-31,-A, 17-31TC,-A 120, 140, with 0-200 Conversion per STC-SA547EA T.C.D.S. (See Sheet. 11 for Series) A-799 A-5A2 A-768 3А19 A-743 A-743 ЗА43 (6), (B) (4), (А) (4), (A) (4), (А) (7), (C) (4), (A) (9), (E) Cessna 1721, K,L,M,N,P, Q,R,S,T 3А12 (6), (B) Cessna 172RG, P172D 3А12 (4), (А)

33. Cessna Cessna 177,177A, 177B R172E,F,G,H,J,K, 175, 175A,B,C 3A17 ЗА17 (6), (B) (4), (A) Cessna 177RG A13CE (4), (A)

34. Cessna 180, 180A,B,C,D,E,F,G,H,J,K A20CE (4), (A)

35. 36. Cessna Cessna Cessna T182, TR182, 182RS, T182T, 182 Series STC SA00152WI 182, 182A,B,C,D,E,F,G,H,J,K, 182L,M,N,P,Q,R, S, T R182, ЗА13 5A6 (6), (B) (6), (B)

40. 38 39. 37 Cessna Cessna Cessna Cessna 195,195A, 195B 188, 188A, 188B,A188,A188A, 185, 185A,B,C,D,E,A185E,A185F A188B, T188C F182P, Q, FR182 182E,F,G,H,J,K, L, M, N, P, Q(Peterson, STC SA3825SW) A42EU A9CE 3A24 ЗА13 ЗА13 (6*), (В*) (6), (B) (6), (B) (6), (B) (6), (B)

41. Cessna U206,U206A,B,C,D,E,F,G, 206,H P206,P206A,B,C,D,E, H TP206A,B,C,D,E, 190 A-790 A4CE A-790 (6*), (B*) (9), (E) (7), (C)

43. 42. Cessna Cessna U206, U206A, B,C,D,E,F,G, (Conv. Per STC 2123 NM) T206H TU206A, B,C,D,E,F,G

44. Cessna 210-5,210-5A, T210F,210G, 207,207A, T207, T207A T210G,210H, T210H,210J, T210J, 210,210A,B,C,D,E,F A16CE A4CE 3A21 (6*), (B*) (6*), (В*) (6*), (B*) T210K,210K,210L, T210L,210M,

46. 45. Cessna Cessna 321 310J-1,310J, T310P, Q,R T310Q,310R, T310R 310,310A,B,C,D,E,F,G,H, T210M,210N, P210N, T210N,210R P210R, T210R E310H,3101,J,K,L,N,P, Q,R ЗА10 (6T*), (BT*)

48. 49. 47. Cessna Cessna Cessna 336 320,A,B,C,D,E,F,320-1,335, 340(,340A 3А25 3A11 (6T*), (BT*) (6T), (BT)

50. Cessna M337B,P337H,T337H-SP T337B,C,D,E,F, G,H 337, 337A,B,C,D,E,F,G,H T303 A34CE A6CE A2CE (6T*), (BT*) (6T*), (BT*) (6T), (BT) RPM and MAP applicable to the PIN EGT-701,4 and 6 cylinder engines only FAA approved AFM Supplement is required with the EGT-701. The EGT-701 is applicable to all EGT-100/200 series. Revision 14

FAA APPROVED MASTER ELIGIBILITY LIST J.P.INSTRUMENTS REPORT: SA 2586NM MAKE AIRCRAFT MODEL Part Number SHEET - 7 -

51. Cessna T.C.D.S. (See Sheet. 11 for Series) 401, 401A,B, 402,402A,B,C,

52. (Great Lakes) Chaparral Motors 2T-1A, 2T-1A-1, -2 421B,421C 411,411A, 414,414A 421,421A A7CE (6T*), (BT*) 53 Cirrus SR-20 A18EA (4), (А)

54. Cirrus

55. Aeronautical Consolidated LAKE 250 LAKE C-1,-2, LA-4, LA-4A, LA-4P, LA-4-200 SR-22 A00009CH A00009CH 1A13 (6), (B) (6), (B) (4), (А)

56. 57 58. Diamond Aircraft Ind Diamond Aircraft Ind. De Havilland DHC-3 DHC-2 Mk. I1 DA40, HK36, HK36TC, TS, TTC, TTC-ECO DA20-A1, DA20-C1 DHC-2 Mk. I TA4CH A47CE A-806 1A13 (6*), (B*) (9), (Е) (4), (A) (4), (A)

59. FLUGZEUGBAU EXTRA EA-300 EA-300S EA-300L EA-300/200 P&W Wasp. R-1340 A-805 (9), (E)

**60. FLUGZEUGBAU EXTRA EA-400 A67EU (6), (B)**

61. Enstrom Helicopter F-28,-28A, -28C, -28F, 280, 280C, 280F A43CE (6*), (B*) GENERAL AVIA Construzioni F22B, F22R, F22C H1CE (4*), (А*) Aeronautiche A75EU (4*), (А*) AA-5,-5A,-5B AG-5B AA-1, -1A, - 1B, - 1C A11EA A38EU (6T), (BT) (4), (А) Gulfstream American A16EA Gulfstream American Gulfstream American 112,112TC, 112B, 112TCA 114, 114A, B, TC A12SO 654 (9), (E) (4), (A) Aircraft Holding Co., American General A17SO A12SO (4T), (AT) (6), (B)

69. Gulfstream AA-5, AA-5A, AA-5B

76. 75. 71. 72. 70. 73. 74. Maule Maule Hughes Helicopter Helio (Alliance Aircraft) Jobmaster Company Lancair Gulfstream American American MXT-7-180, A, B MX-7-180,A,B, C 269A, 269A-1, 269B, 269C M-5-180C, -200, -210TC LC40-550FG H-800 M-6-180 680-FL(P), 685 Н-295, HТ-295, H-395, Н-391, H-391В, H-700 DGA-15P (Army UC-70; Navy GH-1, GH-2,GH-3, NH-1 560F, 680, 680-E, F, 680FL, 500, 500-A, B, U,S, 520, 560, 560A, -E, A00003SE A-717 3А23 4H12 A16EA 1A8 2A4 1A8 6A1 (6T*), (ВТ*) (4*), (А*) _(6*), (B*) (6*), (B*) (4*), (А*) (6T), (BT) (7), (E) (8), (D) (4), (А) Bee Dee M-4, M-4,-4C,-4S,-4T M-4-180C,S,T, M-4-220, M-4-210,C,S,T, M-4-220C,S,T ЗА23 (6*), (В*)

77. 78. Maule Maule MXT-7-160, MX-7-180AC, M-5-200 M-5-210C,-220C,-235C, M-6-235 MX-7-235,A,B,C M-7-235, A,B,C M-7-260, MT-7-260 RPM and MAP applicable to the PIN EGT-701,4 and 6 cylinder engines only FAA approved AFM Supplement is required with the EGT-701. The EGT-701 is applicable to all EGT-100/200 series. 79. Micco Aircraft Co MAC-145, 145A,B M-7-260, M-4-220C, M-4-220S,T, MT-7-235, M5-235C Revision 14 3А23 ЗА23 ЗА 1 (6*), (B*) (6), (B) (4), (A)

FAA APPROVED MASTER ELIGIBILITY LIST J.P.INSTRUMENTS REPORT: SA 2586NM MAKE AIRCRAFT MODEL Part Number SHEET - 8 -

80. Mooney T.C.D.S. (See Sheet. 11 for Series) M20, M20A, B,C,D,E,F, G,J M20K, L, M, R ,S 2A3 (4), (А)

81. Mooney

87. 86. 82. 84. 85. 83. North American Meyers PROP-JETS, INC. Moravan Inc. (ZLIN) Mooney Mooney Rocket Eng. Conv. Rocket Eng. Conv. Mooney AT-6 (SNJ-2,-7),-6A, B,C,D, E,F, T-6G 200, 200A, B, C, D Z-242L, Z-143L ( per STC SA 5691NM) M20J Missile M20TN M20K Rocket 305 (per STC SA 00472SE) M22 A76EU ЗА18 A6SW 2A3 2A3 2A3 2A3 (6T*), (BT*) (6T*), (BT*) (6T*), (BT*) (6*), (B*) (6*), (BT*) (6*), (B*) (4), (A) NA-260 (USAF T-28A) A-2-575 (9), (E) T-28A ,B,C,D Wright R-1300-1A 1A18 (9), (E)

88. Aeronautiche Partenavia Costruzioni P68, P68B, P68C, P68C-TC, P68TС, AP68TP 300 NA-260 (T-28A Conversion) AR-30 1A18 (9), (E) (9), (E A31EU (6T*), (BT*)

89. Pilatus Aircraft Limited PC6/350, PC6/350-H1, -H2

90. Piper (FS2003 Corp.) 7A15 (6*), (B*)

91. Piper PA-18, PA-18S, PA-18 "105" (Special), PA-18S "105" (Special) PA-18A, PA-18 "125" (Army L-21A) PA-18 "135" (Army L-21B), PA-12, -12S PA-18S "125", ", PA-18AS "125" A-780 1A2 (4), (А) (4), (A) PA-18A "135", PA-18S "135" PA-18AS "135", PA-18 "150"

92. Piper PA-18A "150", PA-18S "150" PA-18A-"150" ", PA-18AS "150"

94. 95. 93. Piper Piper Piper PA-22-150 PA-22, -22-108,-22-135, -22S-135, PA-22S-150,-22-160,-22S-160 PA-20,-20S,20-"115",20S-"115" PA-20-"135", SA00035NY) (Crosswinds STOL STC SA682AL) or (Penn-Yan, STC РА-18 -"150" , -20S-"135" 1A6 AR-7 1A4 1A2 (4), (А) (4), (A) (4), (A)

96. Piper PA-23,-23-160 1A6 (4), (A)

97. Piper Piper PA-23-235, PA-250, E23-250, 23-250 1A10 (4T), (AT)

98. Piper Piper Piper PA-25 PA -24-250, -24-260 PA-24-400 PA-24 1A15 1A15 1A15 1A10 (6T), (BT) (8), (D) (4), (A) (6), (B)

99. Piper Piper Piper PA-28RT-201,-28RT-201T,-28-201 PA-28S-180,-28R-180,-28-181, PA-28R-200, PA-28-236; -28-235 PA-28R-201,-28R-201T -28-201T, PA-25-235, -260 PA-28-140,-150,-151,-160,-161, PA-28-180,-28S-160 2A13 2A13 2A8 2A8 (6*), (B*) (4), (A) (6), (B) (4), (А) RPM and MAP applicable to the PIN EGT-701,4 and 6 cylinder engines only FAA approved AFM Supplement is required with the EGT-701. The EGT-701 is applicable to all EGT-100/200 series Revision 14

FAA APPROVED MASTER ELIGIBILITY LIST J.P.INSTRUMENTS REPORT: SA 2586NM SHEET - 9- MAKE AIRCRAFT MODEL Part Number

101. Piper 103. Piper 100. Piper 102. Piper PA-31P,31P-350 PA-32-260,-32-300,-32S-300 PA-30, PA-39, PA-40 PA-31,-31-300,-31-325,-31-350 T.C.D.S. (See Sheet. 11 for Series) A20SO ASEA A1EA (6T*), (BT*) (6T), (BT) (4T), (AT) PA-32-300, -32RT-300, -32RT-300T, A3SO (6"), (B*) PA-32R-301, -32R-301T,

104. Piper PA-32-301, -32-301T PA-34-200 Piper PA-34-200T,-220T A7SO (4T), (AT) 105, Piper PA-38-112 A7SO (6T*), (BT*) 107, Piper 108. Piper 106, Piper PA-60-600, -60-601, -60-700P, A, CR PA-46-310P,-350P PA-44-180, -44-180T A25SO A18SO A19SO (61*), (BT*) (4T*), (AT*) (4), (A) 109- Republic PA-60-601P, PA-60-602P, PA-60-650 A17WE (61*), (BT*)

110. Robinson Helicopter R22, R22 ALPHA, R22 BETA, R22 MARINER A-769 (6), (B)

111. Siai-Marchetti S.205-18/F, -18/R, -20/F, -20/R, R44, R441I H10WE H11NM (6), (B) (4), (A) -22/R, S.208, S208A AgEU (4), (A) 112, Slingsby 113. S.O.C.A.T.A Aerospatiale TB9,10, F.260, F.260B, F.260C, F.260D,, F.260E, , F.260F T67M260, T67M260-T3A A73EU A10EU (6), (B) (6*), (B*)

114. Univair Aircraft Corp, Stinson TB20, TB21,200 108,108-1, -2, -3, -5 A51EU A51EU (6*), (B*) (4), (A) 117, Thompson 116, Swift 115, Swift 118 VARGA Augustair, Inc. Navion, A ,B C, D,E,F,G ,H 2150, 2150A, 2180 GC-1A GC-1B A-767 A782 766 766 (6), (B) (G), (B) (6), (A) (4), (A) 119 WACO YMF, 4A19 (4), (A) 122 Christen (AVIAT) 121 PITTS (AVIAT) 120 WACO White Inter./ Sky Inter. White Inter. Ltd A-1, A, B YMF (F5, F5C modification per STC SA1000GL) S-1S, S-1T, S-2, S-2A, UPF-7 VPF-7 YKC, YKC-S, YKS-6, ZKS-6 S-2S, S-2B ATC 542 ATC542 A-642 A-533 A8SO (6), (B) (7), (C) (7), (C) (4), (A) (1, (C) (n. (C) 123 Weatherly A22NM (4), (A) 620, A, B 124 Wilga PZL-104 Wilga 80 A26WE (9), (E) PZL-104M Wilga 2000 A55EU (9), (E)

(6), (A) FAA approved AFM Supplement is required with the EGT-701. The EGT-701 is applicable to all EGT-100/200 series. RPM and MAP applicable to the PIN EGT-701,4 and 6 cylinder engines only Revision 14

FAA APPROVED MASTER ELIGIBILITY LIST J.P.INSTRUMENTS REPORT: SA 2586NM MAKE AIRCRAFT MODEL Part Number SHEET - 10 - T.C.D.S. (See Sheet. 11 for Series) Model designation system by part number for EGT-701 EGT-701- []C-OT []-OP []-A []-T [] -| []-F[] - R/M - L[] (L) TFT color display 730-830 (R/M L) RPM and MAP (F) Fuel Flow function (I) Induction Air Temperature (IAT) (T) Turbine Inlet Temperature (TIT) (A) Outside Air Temperature (OAT) (OP) Oil Pressure (OT) Oil temperature Number of Cylinders (4,6,7,8, & 9,) with EGT & CHT function Model designation system by part number for EGT-100 EGT-100- []C[]-O-T [] -A []-T[]-|[] Induction Air Temperature (IAT) Turbine inlet temperature (TIT) Oil temperature (Oil) Outside air temperature (OAT) Cylinder Head Temperature (CHT) Number of Cyl. with EGT only/and CHT (4,6,7,8,&9) Example: EGT-701 - (6C O-T A I R/M L) is indicated as such on the TSO label EGT 701 Model EDM 800 EGT-701 - 6C - OT [*] OP [] -A [*] -T [ ]-| [*] - F [*] -R/M L [*] -L[]

• 6 Cylinder

• Oil Temperature function

• OAT, Outside Air function

• IAT, Induction Air function RPM & MAP function Fuel Flow function RPM and MAP applicable to the PIN EGT-701,4 and 6 cylinder engines only FAA approved AFM Supplement is required with the EGT-701. The EGT-701 is applicable to all EGT-100/200 series. Revision 14

FAA APPROVED MASTER ELIGIBILITY LIST J.P.INSTRUMENTS REPORT: SA 2586NM MAKE AIRCRAFT MODEL Part Number SHEET - 11 - ELIGIBLE PART NUMBERS for EGT-701 (series ) T.C.D.S. (See Sheet. 11 for Series) Note (2) suffix" . " denotes turbocharged engines Note (1) suffix "T" designates twins, two instruments required 4COTOPATIF R/M L 4CIF R/M L 4CTF R/M L 4CTI R/M L 4CTIF R/M L 4CAIF R/M L 4CATI R/M L 4CATF R/M L 4CAI R/M L 4CAT R/M L 4CAF R/M L 4COTOPTIF R/M L 4COTOPAIF R/M L 4CATIF R/M L 4COTOPIT R/M L 4 COTOPTI RIM L 4COTOPTF R/M L 4COTOPAT R/M L 4COTOPATI R/M L 4COTOPAI R/M L 4COTOPAF R/M L 4COTOPATF R/M 4COTOPA R/M L 4COTOPI R/M L 4COTOPF R/M L 4COTOPT R/M L 4CF R/M L 4CA R/M L 4CT R/M L 4CI R/M L 4C0R/M L EGT-701-( ) 4C R/M L RPM & MAP 4 Cylinder with Note (2) suffix it denotes for turbocharged engines. Note (1) suffix "T" designates EGT-200 ( ) series for twins ELIGIBLE PART NUMBERS for EGT-100-( ) and EGT-200( ) A 4COTOPATIFL 4CTIL 4CTFL 4CIFL 4CTIFL 4CAIFL 4CATFL 4CATIFL 4CAFL 4CAIL 4CATIL 4CATL 4COTOPTIFL 4COTOPAIFL 4COTOPTIL 4COTOPTEL 4COTOPITL 4COTOPATFL 4COTOPATL 4COTOPAIL 4COTOPATIL 4COTOPAFL 4CIL 4COTOPLA 4COTOPFL 4COTOPTL 4COTOPL 4CTL 4CFL 4COTOPIL 4 Cylinder EGT-701-( ) 4CL 4CAL 4 B Part number Series Part number (Series) 6CIF R/M L 6COTOPATIF R/M L 6CTI R/M L 6CTF R/M L 6CATF R/M L 6CTIF R/M L 6CAIF R/M L 6CAF R/M L 6CAI R/M L 6CATIF R/M L 6CATI R/M L 6CAT R/M L 6COTOPIT R/M L 6COTOPTIF R/M L 6COTOPAIF R/M L 6COTOPTI R/M L 6COTOPATF R/M L 6COTOPAT R/M L 6COTOPATI R/M L 6COTOPAI R/M L 6COTOPAF R/M L 6COTOPF R/M L 6COTOPI R/M L 6COTOPT R/M L 6COTOP R/M L 6COTOPA R/M L 6C R/M L 6CA R/M L 6CI R/M L 6CF R/M L 6CT R/M L 6 Cylinder with RPM & MAP EGT-701-( ) 6 6COTOPATIFL 6CTFL 6CIFL 6CATIL 6CATFL 6CATIFL 6CATL 6CAIL 6COTOPTIFL 6COTOPITL 6CAFL 6COTOPAIFL 6COTOPTIL 6COTOPTFL 6COTOPFL 6COTOPATL 6COTOPAIL 6COTOPAFL 6COTOPATFL 6COTOPATIL 6CTL 6COTOPAL 6COTOPTL 6COTOPIL 6CIL 6CFL 6CAL 6CL 6COTOPL EGT-701-( ) 6 Cylinder 6 7COTOPATIFL 7CIFL 7CTIL 7CATFL 7CATIL 7CAFL 7CATL 7CAIL 7COTOPTIFL 7CATIFL 7COTOPITL 7COTOPATFL 7COTOPTIL 7COTOPAIFL 7COTOPTFL 7COTOPAFL 7COTOPATIL 7COTOPFL 7COTOPAIL 7COTOPATL 7COTOPTL 7COTOPAL 7COTOPIL 7CAL 7CTL 7CIL 7COTOPL 7CL 7CFL T Cylinder EGT-701-( ) SCOTOPATIFL 8CTFL 8CIFL 8CTIFL 8CTIL 8CATFL 8CAIFL 8CATIFL 8CAFL 8CATL 8CATIL 8CAIL 8COTOPITL 8COTOPTIFL 8COTOPAIFL 8COTOPATFL 8COTOPTIL 8COTOPTFL 8COTOPATL 8COTOPATIL 8COTOPFL 8COTOPAFL 8COTOPAIL 8COTOPIL 8CAL 8COTOPAL 8COTOPTL 8CTL 8CIL 8CFL 8COTOPL 8CL EGT-701-( ) 8 8 Cylinder Example: 9COTOPATIFL 9CTFL 9CTIL 9CIFL 9COTOPAIFL 9CATIFL 9CAIL 9CAFL 9COTOPTIFL 9COTOPTFL 9COTOPITL 9COTOPTIL 9COTOPAFL 9COTOPATIL 9COTOPATFL 9COTOPIL 9COTOPFL 9COTOPAIL 9COTOPATL 9CFL 9COTOPTL 9CTL 9COTOPL 9COTOPAL 9CL 9CIL 9 Cylinder EGT-701-( ) 9CAL 9 see page 5 TIT EGT-100-( ) 4C 4 cylinder EGT-100-( ) 6 cylinder EGT-100-( ) 7 7 cylinder EGT-100-( ) & cylinder EGT-100-() 9 cylinder TIT Cessna 310 (6T*) 6 = any PN in that column except * items in TIT column 4COIT 4COAI 4COATI 4COAT 4COT 4COA 4COI 4C0 4CA 4CT 4CI 6COIT 6COATI 6COAI 6CT 6COA 6COT 6COI 6COAT 6CI 6C 6C0 6CA 7CAI 7CAT 7CTI 7COA 7C 7CA 7CT 7COT 7COI 7C0 7CI 8C 9C 9 T = Requires two instruments * = Includes TIT (turbocharged a/c only) 4CAT 6CAT 4CAI 6CAI 4CATI 4CTI 6CATI 6CTI RPM and MAP applicable to the PIN EGT-701,4 and 6 cylinder engines only FAA approved AFM Supplement is required with the EGT-701. The EGT-701 is applicable to all EGT-100/200 series. Revision 14

## Every issue (6)

- September 20, 2017: Amended, Current. [certificate](https://openairdocs.org/files/sha256/5e/35/5e35eade56f2e2d0e4d5ad1e41b80bca2bc7679df0f34c1eb505cfcb384fb74c), [SA2586NM_AML.pdf](https://openairdocs.org/files/sha256/58/4a/584a4c680a7a273389914c9d9ea9b5fa9a8f72776ecd101f748fc6f1ffd32834)
- July 19, 2008: Amended, Current. [certificate](https://openairdocs.org/files/sha256/5e/35/5e35eade56f2e2d0e4d5ad1e41b80bca2bc7679df0f34c1eb505cfcb384fb74c), [MEL SA2586NM.pdf](https://openairdocs.org/files/sha256/dc/3b/dc3b0e83e2075b8451c17348c2f6ea2d088f0945292c3185ddd25b5df9644e78)
- July 19, 2008: Amended, Current. [certificate](https://openairdocs.org/files/sha256/5e/35/5e35eade56f2e2d0e4d5ad1e41b80bca2bc7679df0f34c1eb505cfcb384fb74c), [MEL SA2586NM.pdf](https://openairdocs.org/files/sha256/dc/3b/dc3b0e83e2075b8451c17348c2f6ea2d088f0945292c3185ddd25b5df9644e78)
- July 19, 2008: Amended, Current. [certificate](https://openairdocs.org/files/sha256/5e/35/5e35eade56f2e2d0e4d5ad1e41b80bca2bc7679df0f34c1eb505cfcb384fb74c), [MEL SA2586NM.pdf](https://openairdocs.org/files/sha256/dc/3b/dc3b0e83e2075b8451c17348c2f6ea2d088f0945292c3185ddd25b5df9644e78)
- July 20, 2008: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/5e/35/5e35eade56f2e2d0e4d5ad1e41b80bca2bc7679df0f34c1eb505cfcb384fb74c), [MEL SA2586NM.pdf](https://openairdocs.org/files/sha256/dc/3b/dc3b0e83e2075b8451c17348c2f6ea2d088f0945292c3185ddd25b5df9644e78)
- June 17, 1999: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/5e/35/5e35eade56f2e2d0e4d5ad1e41b80bca2bc7679df0f34c1eb505cfcb384fb74c), [MEL SA2586NM.pdf](https://openairdocs.org/files/sha256/dc/3b/dc3b0e83e2075b8451c17348c2f6ea2d088f0945292c3185ddd25b5df9644e78)

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