# STC SA5925NM

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Electronics International, United States
- Description: Installation of oil pressure/temperature instrument.
- Applied: November 10, 1992
- Status date: December 8, 1997
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS AR-32](https://openairdocs.org/tcds/AR-32), [TCDS AR-36](https://openairdocs.org/tcds/AR-36), [TCDS A17WE](https://openairdocs.org/tcds/A17WE), [TCDS 1A3](https://openairdocs.org/tcds/1A3), [TCDS A18CE](https://openairdocs.org/tcds/A18CE), [TCDS 1A16](https://openairdocs.org/tcds/1A16), [TCDS AS1NM](https://openairdocs.org/tcds/AS1NM), [TCDS A-761](https://openairdocs.org/tcds/A-761), [TCDS A-759](https://openairdocs.org/tcds/A-759), [TCDS A21CE](https://openairdocs.org/tcds/A21CE), [TCDS A22NM](https://openairdocs.org/tcds/A22NM), [TCDS A8SO](https://openairdocs.org/tcds/A8SO), [TCDS A-743](https://openairdocs.org/tcds/A-743), [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) and 76 more
- Certificate PDF: https://openairdocs.org/files/sha256/cf/9b/cf9b90fde9bf868f8f87abade3bc8b122caa487ac8ae7154c39200f98cd492e0
- Approved model list and other attachments: [AML SA5925NM.pdf](https://openairdocs.org/files/sha256/b1/6d/b16d071b79957762c5706ae0e8ab373eef53f457d38f40cbacf7c44f7d452396)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C448506F64A4FF5B862579BC0075D95B.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA5925NM

## ADs that name it (0)

None.

## Approved models (585, first 50)

- Acme Aircraft Company F8F-2 ([TCDS AR-32](https://openairdocs.org/tcds/AR-32))
- Aero Union Corporation AF-2S ([TCDS AR-36](https://openairdocs.org/tcds/AR-36))
- 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))
- Alexandria Aircraft LLC 14-19 ([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))
- Allied Ag Cat Productions Inc. G-164 ([TCDS 1A16](https://openairdocs.org/tcds/1A16))
- American Blimp Corporation A-60 ([TCDS AS1NM](https://openairdocs.org/tcds/AS1NM))
- American Blimp Corporation A-60+ ([TCDS AS1NM](https://openairdocs.org/tcds/AS1NM))
- American Champion Aircraft Corp. 11AC ([TCDS A-761](https://openairdocs.org/tcds/A-761))
- American Champion Aircraft Corp. 11BC ([TCDS A-761](https://openairdocs.org/tcds/A-761))
- American Champion Aircraft Corp. 7AC ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 7ACA ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 7BCM (Army L-16A) ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 7CCM (Army L-16B) ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 7DC ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 7EC ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 7ECA ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 7FC ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 7GC ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 7GCA ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 7GCAA ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 7GCB ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 7GCBA ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 7GCBC ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 7HC ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 7JC ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 7KC ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 7KCAB ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 8GCBC ([TCDS A21CE](https://openairdocs.org/tcds/A21CE))
- American Champion Aircraft Corp. 8KCAB ([TCDS A21CE](https://openairdocs.org/tcds/A21CE))
- American Champion Aircraft Corp. S11AC ([TCDS A-761](https://openairdocs.org/tcds/A-761))
- American Champion Aircraft Corp. S11BC ([TCDS A-761](https://openairdocs.org/tcds/A-761))
- American Champion Aircraft Corp. S7AC ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. S7CCM ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. S7DC ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. S7EC ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- Aviat Aircraft Inc A-1 ([TCDS A22NM](https://openairdocs.org/tcds/A22NM))
- Aviat Aircraft Inc S-1S ([TCDS A8SO](https://openairdocs.org/tcds/A8SO))
- Aviat Aircraft Inc S-1T ([TCDS A8SO](https://openairdocs.org/tcds/A8SO))
- Aviat Aircraft Inc S-2 ([TCDS A8SO](https://openairdocs.org/tcds/A8SO))
- Aviat Aircraft Inc S-2A ([TCDS A8SO](https://openairdocs.org/tcds/A8SO))

All 585: https://openairdocs.org/stc/SA5925NM/models.md

## What the certificate says

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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA5925NM This certificate issued to: Electronics International, Inc.

Purt * ofithe * Regulations:

Original Product - Type berlificate Number: * See attached FAA Approved Model List (AML) Make: * No. SA5925NM for list of approved airplane Mertel: * models and applicable regulations.

stripien Type sign hange installed in accordance with the drawings and Electronics International oil pressure/temperature installation instructions specified on the FAA Approved Model List (AML) of this STC, or later FAA approved revisions.

Approval of this change in type design applies to the above forter aircraft of ft is determin wh model aircraft only. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this certificate and FAA Approved Model List (AML) No. SA5925NM, dated February 17, 1993, or later FAA approved revision, must be maintained as part of the permanent records for the modified aircraft.

Date of Application: November 10, 1992 Sule reissued:

Date of Issuance: February 17, 1993 Jole amer eded

FEDERAL AVIATION (Signature, TAINISTEAIO Seattle Aircraft Certification Office Acting Manager, Special Certification Branch (Title) 47 FAA FORM 8110-2 (10-68)

### AML SA5925NM.pdf

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

FAA Approved Model List (AML) SA5925NM For Electronics International Oil Pressure/Temperature Instrument Issue Date: February 17, 1993 Original Certification FAA Sealed Installation Type Basis Drawings Instructions AML Aircraft Aircraft Certificate for Instrument Model Number Amended Item Make Model Number Alteration Number Rev. Number Rev. No. (See Note 1) Date TD0327921 N/R 01 0520911 1- Aeronca Inc. SSAC,, SISALA, -LB A-702 Car 48 OPT - 1-ROG10R40/YOG90R220 6/3/94 (Also see 15AC, A-802 Car z OPT - 1-ROG10R40/YOG90R220 American, Bel (anca)

2. Aerospatiale See Socata. 6/3/94

3. American Blimp A-60, A-60+ AS1NM FAR 21 OPT -ROG15R59/YOG65R245 10/30/97

4. American 7AC, STAC A -759 Car 4a OPT - 1-ROG30R60/YOG65R220 6/3/94 Champion (Also see 7ECA OPT - 1-ROG30R60/YOG65R225 Aeronca, Bel (anca) 7CM, 7CCM, 70C, 7EC OPT - 1-ROG30R40/YOG65R225 S7DC,S7CCM, S7EC 7FC, 7JC 7GC, 7HC, 7GCA, 7GCB OPT - 1- 7KC, 7GCBA, 7GCAA ROY25G60Y 90R100/ YOG65R245 7GCBC 7KCАB OPT - 1- ROGY25G55Y95R115/Y0G65R245 7ACA OPT - 1 -ROGY25G55R95/YOG65R285 8KCAB A21CE OPT - 1- 10/30/97 ROY25G60Y9OR100/Y0G65R245 8GCBC OPT - 1- ROY25G55Y95R115/Y0G65R245 11AC, S11AC A-761 4a OPT - 1-ROG30R60/YOG65R220 11BC, S11BC OPT - 1-ROG30R40/YOG65R225

5. Aviat A - 1 A22NM Far 23 OPT - 1-ROG25R100/YOG65R240 6/3/94 S- 1S, -1T A8SO Far 21 OPT - 1-ROY25G60R 100/YOG100R245 s-2, - 2A = S-2S -28 + 10

FAA Approved Model List (AML) SA5925NM For Electronics Internat ional Oil Pressure/Temperature Instrument Issue Date: February 17, 1993 Original Certification FAA Sealed Installation Type Basis Drawings Instructions AML Aircraft Aircraft Certificate for Instrument Model Number Amended Item Make Model Number Alteration Number Rev. Number Rev. No. (See Note 1) Date TD0327921 N/R 01 0520911 Beech Aircraft 18A,D, S18A, D,A180 A -684 Bul 7A OPT -1-ROG25R100/YOG65R205 8/15/93 Corp. 19, B19, M19A A1CE CAR 3 OPT - 1-ROY25G60R85/YOG120245 OPT - 1-ROY25G60R100/Y0G120R245 c23, 023, 25, 82 A24 OPT -1-ROY10G30R100/YOG120R225 OPT - • ROY25G60R100/YOG120R245 A24R, B24R, C24R OPT - •ROY25G60R100/Y0G120R245 35, A35, B35, C35 A-777 OPT- -ROG30R80/Y0G100R225 D35, E35, F3S OPT- -ROG30R80/Y0G100R225 G35, 35R OPT-1-ROG30R80/YOG100R225 H35, J35, K35 3A15 OPT-1-ROG30R80/YOG100R225 M35, N35, P35, OPT- -ROG30R80/YOG100R225 S35 OPT￾ •ROG30R80/Y0G100R225 V35, V35A, V358 OPT ROG3OR100/Y0G100R240 35-33, 35-A33 OPT: ROG30R80/Y0G100R225 35-833, 35-C33 OPT -1 1-ROG30R80/YOG100R225 35-C3ЗА, Е33 OPT - 1-ROG30R100/YOG100R240 E33A, E33C, F33 OP T -ROG30R100/Y0G100R240 F33A, F33C OP T -ROG3OR100/Y0G100R240 G33 OPT 1-ROG3OR100/Y0G100R225 36, A36 OPT.￾ 1-ROG3OR100/Y0G100R240 A36TC, B36TC OPT ￾ -ROY10G30R100/Y0G100R240 45, A45, D45 5A3 OPT -ROG30R60/Y0G65R225 10/30/97 50,C,D,E,F,G,H,J 5A4 OPT. -ROG25R100/Y0G100R235 8/15/93 A55, B55, 855B, 3A16 OP T -ROG3OR100/YOG75R240 C55, C55A, D55 OPT •ROG30R 100/YOG75R240 DSSA, E55, E55A OPT-1-ROG30R100/Y0G75R240 56TC, A56TC OPT - 1-ROG25R100/YOG100R240 58, 58A A23CE 23 OPT - 1-ROY10G30R100/YOG75R240 58P, 58PA, 58TC OPT - 1-ROY10G30R100/YOG100R240 58TCA OPT - 1-ROY10G30R100/YOG100R240 60, A60, B60 A12CE OPT - 1-ROG25R100/YOG100R245 65,-80,-88,B,-90 ЗА20 3 OPT - 1-ROG25R85/YOG100R225 A65,-8200,70,A90 OPT - 1-ROG25R85/YOG100R235 70 3A20 OPT - 1-ROG25R85/Y0G100R235 76 OPT -1-ROG25R85/YOG100R235 77 A3OCE FAR 23 OPT - 1-ROG25R100/YOG120R245 Beech Aircraft 95, 895, 895A CAR 3 OPT - 1-ROG25R85/YOG140R245 8/15/93 Corp. (Cont) D95A, E95 OPT - 1-ROG25R85/YOG140R245 -855 OPT -1-ROG30R80/YOG75R225 95-B55A, -B55B OPT - 1-ROG30R80/YOG75R225 95-C55, - C55A OPT - 1-ROG30R80/YOG75R225

7. Bel lanca 14-19 1A3 CAR 3 OPT - 1-ROG10R35/YOG90R220 6/3/94 Aircraft 17-30, -31, -31TC OPT - 1-ROY25G60R100/YOG100R245 Corporation 17-30A A18CE FAR 23 OPT - 1-ROG10R100/YOG75R240 17-31A. 17-31ATC OPT - 1- ROY25G60Y90R100/Y0G75R245

• PE + 10

FAA Approved Model List (AML) SA5925NM For Electronics International Oil Pressure/Temperature Instrument Issue Date: February 17, 1993 Original Certification FAA Sealed Installation Type Basis Drawings Instructions AML Aircraft Aircraft Certificate for Instrument Model Number Amended Item Make Model Number Alteration Number Rev. Number Rev. No. (See Note 1) Date TD0327921 N/R 01 0520911

8. Boeing A75-L3, - L300 A -743 Car 4a OPT - 1-ROG50R100/YOG65R200 10/30/97 Aircraft A75N1 OPT-1-ROG50R100/Y0G65R210 (Stearman) A75J1 OPT-1-ROG60R90/Y0G65R200 1B75A OPT -1-ROG50R100/YOG65R200 f 10

FAA Approved Model List (AML) SA5925NM For Electronics International Oil Pressure/Temperature Instrument Issue Date: February 17, 1993 Original Certification FAA Sealed Installation Type Basis Drawings Instructions AML Aircraft Aircraft Certificate for Instrument Model Number Amended Item Make ModeL Number Alteration Number Rev. Number Rev. No. (See Note 1) Date TD0327921 H/R 0I 0520911 Cessna 120, 140, 140A A - 768 CAR 4a DPT-1-ROY10G30R100/GOR240 8/15/93 Aircraft 150, 150A, 150B 3A19 CAR 3 Corp. 150C, 1500 150E, 150F, 150G 150H, 150J. F150F 150J. 150K, A150K 150L, A150L 150M, A150M 152, A152 OPT - 1-ROG25R115/YOG100R245 170, 170A, 170B A- 799 OPT-1-ROG25R100/GOR245 172, 172A, 1728 3A12 OPT-1-ROY10G30R100/GOR240 172C, 1720, 172E 172F, 172G, 1721 172K, 172L, 172M OPT -1-ROY10G30R100/YOG100R240 172N, 172P OPT - 1-ROG25R100/YOG100R245 172RG, P1720 3A17 3 R172E, R172F, R172G R172H, R172J, R172K, 175, 175A,B,C 172Q ================ OPT - 1-ROG10R100/YOG100R245 6/3/94 177, 177A, 1778 A 13CE 23 OPT -1-ROG26R100/YOG100R245 8/15/93 177RG AZOCE 180, 180A, 180B 5A6 3 OPT - 1-ROY10G30R100/YOG100R240 180C, 180D, 180E 180J 182A. 1828 180F, 180G, 180H 180K 182, 3A13 182C, 182D, 182E * 182F. 182G, 182H 182J, 182K 182L, 182M, 182N, 182P, 182Q 182R, R182 OPT- 1-ROG25R100/YOG100R245 T182. TR182

185. 185A. 1858 3A24 OPT - 1-ROY10G30R100/GOR225 185C, 185D, 185E A185E, A185F OPT - 1-ROY10G30R100/GOR240 188, 188A, 1888 ASCE 21 A188, A188A T188C 190, 195, -A, -B A - 790 = = == OPT - 1-ROG30R90/ROG100R200 205, 3A21 OPT - 1-ROY10G30R100/GOR240 206 Series A4CE DPT - 1-ROY10G30R100/YOG100R240 U206 Series TU&TP206 Series 207, 207A A16CE FAR 23 OPT- 1-ROY10G30R100/GOR240 PE F 10

FAA Approved Model List (AML) SA5925NM For Electronics International Oil Pressure/Temperature Instrument Issue Date: February 17, 1993 Original Certification FAA Sealed Installation Type Basis Drawings Instructions AML Aircraft Aircraft Certificate for Instrument Model Number Amended Item Make Model Number Alteration Number Rev. Number Rev. No. (See Note 1) Date TD0327921 N/R 01 0520911

9. Cessna T207, T207A 3A21 CAR 3 OPT- 1-ROY10G30R100/GOR240 8/15/93 Aircraft 210, 210A Corp. (Cont.) 210B, 210C, 210D, 210F, A210 Series 210-5, 210-5A T210F, 210G, 210M, -210H, 210K. T210L: 210N. T210G, 210H, 210J T210F, 12K, 210L OPT - 1-ROY10G30R100/YOG100R240 T210M P210N, P210R T210N 3050, 305E 3108 305А, 3058, 305С 5A5 CAR 3 OPT -1-ROY10G40R100/YOG75R225 305F 310, 310A, 3А10 310C, 3100, 310E 310F, 310H, E310H 3101, 310J OPT - 1-ROY10G30R100/YOG75R225 5300, 330P 3300 310R I310P, T310R T3100 310Q 320, -A, -B, -C 3A25 520D, -E, - F 336 A2CE 337, 337A, 3378 A6CE OPT - 1-ROY10G30R100/YOG75R240 337E, 337C T3378, 1337E, 3А25 P33T0 з4DА 1337H 340, A7CE 401, 401A, 4018 402, 402A, 4028 402C 404 411, 411A 414, 414A 421, 421A, 4218 421C, 425 Pa : 10

FAA Approved Model List (AML) SA5925NM For Electronics International Oil Pressure/Temperature Instrument Issue Date: February 17, 1993 Original Certification FAA Sealed Installation Type Basis Drawings Instructions AML Aircraft Aircraft Certificate for Instrument Model Number Amended Item Make Model Number Alteration Number Rev. Number Rev. No. (See Note 1) Date TD0327921 N/R 0I 0520911 10- Commander 112, 112B A12SO Far 23 OPT- 1- 6/3/94 Aircraft ROY25G50Y90R100/Y0G160R245 114, 114А, В, с 112TC, 112TCA 500, -B, -S, -U 6A1 Саг OPT - 1- 10/30/97 ROY25G55Y95R115/Y0G65R245 500-A OPT - 1- ROY10G30Y60R100/Y0G65R225 520 OPT - 1-ROG60R85/YOG65R225 560, -A, -E OPT - 1-ROY25G65R85/YOG65R225 700 A12SU Far 23 OPT - 1- ROY25G55Y95R1150/YOG65R245

11. DeHavilland DHC-2 CAR 10 OPT - 1-ROG50R100/YOG100R190 6/3/94 Aircraft of DHC -3 OPT - 1-ROG50R100/YOG100R190 Canada, Ltd.

12. Extra Flugz. EA 300, S,L,/200 A67EU Far 21 OPT • 10/30/97 ROY25G55YR95R115/YOG65R245

13. Fairchild 24 C8C 1-535 OPT - 1-ROG25100/YOG65R200 10/30/97 24R9, 24R40 1-704

14. Grumman F8F -2 AR -32 OPT -1-ROG60R100/YOG65R200 10/30/97 AF-2S AR - 36

15.. Gulfstream AA-1, AA-1A, A16EA OPT -1-ROG25100/YOG75R245 6/3/94 American Corp. AA-18, AA-1C OPT- 1-ROG25R100/YOG75R245 (Grumman AA-5, AA-5A OPT - 1-ROG25R100/YOG75R245 Aircraft) AA -58 OPT- 1-ROG25100/YOG75245

16. Helio Aircraft 15A ЗАЗ OPT - 1-ROG30R60/YOG65R230 10/30/97 (Taylorcraft) 20 OPT - 1-ROY10G3060/YOG65R225

17. Helio H-250,H700 1A8 OPT - 1- 10/30/97 Enterprise ROY25G55Y95R115/Y0G65R245 H-295, HT295,F295 OPT -1-ROY25G65R85/YOG100R225 H-395 H-395А, H-391 OPT - 1-ROG60R85/YOG100R225 H-800 OPT -1- ROY25G50Y95R115/Y0G100R245

18. Interceptor 200 3А18 Car 3 OPT - 1-ROY10G30R60/YOG65R225 10/30/97 (Aero 200A, B,C,D OPT - 1.

Commander) ROY10G30Y60R100/Y0G65R240 (Meyers) € 10

FAA Approved Model List (AML) SA5925NM For Electronics International Oil Pressure/Temperature Instrument Issue Date: February 17, 1993 Original Certification FAA Sealed Installation Type Basis Drawings Instructions AML Aircraft Aircraft Certificate for Instrument Model Number Amended Item Make Model Number Alteration Number Rev. Number Rev. No. (See Note 1) Date TD0327921 N/R 01 0520911

19. Lake See Revo. 6/3/94

20. Luscombe 8,A,B,C,D,E, F, A-694 CAR 4a 6/3/94 T - 8F

21. Maule M-4,C,S, I. -210, C 3A23 CAR 3 OPT - 1-ROG25R100/YOG65R240 6/3/94 M-4S, T, -220,C,S, OPT -1-ROG25R100/YOG65R240 4-4T, -180C,S,T OPT - 1-ROG25R100/YOG65R240 1-5-180C, -210C OPT - 1-ROG25R100/YOG65R240 1-5TC, - 220C OPT - 1-ROG25R100/YOG65R240 M-5-235C M-6-180 MX - 7-235

22. Mooney M20 2A3 CAR 3 OPT - 1-ROY26G61R100/Y0G100R245 None Aircraft Corp. M20A M208 M20C M20D M20E M20F M20G M20J M20K M2OL M20M M22 A6SW = = = =

23. Moravan 2 - 526C A30FU Far 23 OPT - 1- 10/30/97 2-242L, Z-143L A76EU ROY25G55Y95R115/Y0G65R245

24. Navion See Thompson. .... 6/3/94 Pr

FAA Approved Model List (AML) SA5925NM For Electronics International Oil Pressure/Temperature Instrument Issue Date: February 17, 1993 Certification FAA Sealed Installation Basis Drawings Instructions AML Aircraft Aircraft for Instrument Model Number Amended Item Make Model Alteration Number Rev. Number Rev. No. (See Note 1) Date TD0327921 N/R 0I 0520911

25. Piper Aircraft A -12, -S. -14 A-797 CAR 3 OPT - 1-ROY25G60R90/Y0G65R245 10/30/97 Corp- PA-15, -16, -17 A-800 OPT- 1-ROG25R100/YOG65R245 PA -18 1A2 OPT-1-ROY10G31R40/Y0G91R225 5/10/93 PA- (18, 18A, 18S) OPT-1-ROY10G31R40/Y0G121R245 #125" PA- (18, 18A, 18S) OPT -1-ROY10G31R40/YOG121R245 PA- (18, 18A, 185) 1A4 OPT-1-ROY26G61Y85R100/ "150" YOG121R245 PA-20,S, 115, OPT-1-ROY26G61Y85R100/ S-115,135,S-135 YOG121R240 PA-22&S, 108, 1A10 OPT-1-ROY26G61Y85R100/ 135,150,160 YOG121R240 PA - 23 OPT - 1ROY26G61Y85100/ YOG121R240 PA -23-160 OPT -1-ROY26G61Y85R100/ YOG121R240 PA-23-250 OPT-1-ROY26G61R100/YOG121R245 PA -23-235 1A15 OPT- -ROY26G61Y85R100/ YOG121R245 PA - 24-180 OPT -ROY26G61R100/YOG121R245 PA -24-250 OPT-1-ROY26G61R100/YOG121R245 PA -24-260 2A8 OPT-1-ROY26G61R100/Y0G121R245 PA -24-400 OPT-1-ROY26G61R100/YOG121R245 PA -25-235 2A13 OPT- 1-ROY26G61R90/YOG121R245 PA -25-260 OPT -1-ROY26G61R90/YOG121R245 PA-28-140 OPT -1-ROY26G61R90/YOG75R245 PA -28-150 OPT-1-ROY26G61R90/Y0G75R245 PA-28-151 OPT -1-ROY26G61R90/YOG75R245 PA- 22-161 28S) - 160 OPT - 1-ROY26G61R100/YOG75R245 OPT-1-ROY26G61R100/Y0G75R245 PA- (28, 28R) - 180 OPT-1-ROY26G61R90/Y0G75R245 PA - 28-181 OPT - 1-ROY26G61R90/YOG75R245 PA - 28R -200 OPT- 1-ROY26G61R90/YOG75R245 PA- 28R - 201 OPT - 1-ROY26G61R90/YOG75R245 PA-28-201T OPT - 1-ROY11G31R100/YOG75R240 PA - 28R - 201T OPT - 1-ROY11G31R100/YOG101R240 PA-28RT - (201, A20SO OPT-1-ROY11G31R100/YOG101R240 2011) * PA-28-235 & 236 OPT-1-ROY26G61R100/YOG75R245 PA -31 OPT-1-ROY26G61R100/YOG121R245 PA-31P OPT - 1-ROY11G56R100/YOG121R245 PA-31-325 OPT- 1-ROY26G61100/YOG121R245 PA-31-350 OPT-1-ROY26G61R100/YOG121R245 10

FAA Approved Model List (AML) SA5925NM For Electronics International Oil Pressure/Temperature Instrument Issue Date: February 17, 1993 Original Certification FAA Sealed instruction Type Basis Drawings AML Aircraft Aircraft Certificate for Instrument Model Number Amended Item Make Model Number Alteration Number Rev. Number Rev. No. (See Note 1) Date TD0327921 N/R OI 0520911 C

25. Piper Aircraft PA-32-260 A3SO CAR 3 OPT - -ROY26G61R100/Y0G75R245 5/10/93 Corp. (Cont.) PA-32-300 OPT - 1-ROY26G61R100/YOG75R245 PA -32R -300 OPT-1-ROY26G56R100/YOG75R245 PA -32RT -300T OPT -1-ROY26G56R100/YOG75R245 PA-32-301 OPT- - ROY26G61R100/YOG75R245 PA -32-301T OPT- -ROY26G56R100/Y0G75R245 PA -32R -301 OPT- -ROY26G61R100/Y0G75R245 PA -32R -301T OPT- - ROY26G56R100/YOG75R245 PA-34-200 ATSO FAR 23 OPT - 1-ROY26G61R90/YOG75R245 PA-34-200T OPT - 1-ROY11G31Y81R100/ YOG75R240 PA-34-220T OPT-1-ROY11G31R100/YOG100R240 PA-36-285 A9SO OPT- 1-ROY26G61R100/YOG75R245 PA-36-300 OPT-1-ROY26G61R100/Y0G75R245 PA-36-375 OPT -1-ROY26G56R100/YOG75R245 PA -38-112 A18SO OPT-1-ROY26G61R100/YOG75R245 PA -39 ATEA CAR 3 OPT -1-ROY26G61R100/YOG121R245 PA-44-180 A19S0 FAR 23 OPT-1-ROY26G61R100/YOG75R245 PA-44-180T OPT -1-ROY16G61R115/YOG75R245 PA-46-310P A25S0 OPT-1-ROY11G31R100/YOG101R240 PA -46-350P OPT- 1-ROY26G56R115/YOG101R245 PA-60-600 A17WE OPT-1-ROG25R100/Y0G75R245 PA-60-601 OPT - 1-ROG25R100/YOG75R245 PA-60-601P OPT -1-ROG25R100/YOG75R245 PA-60-602P OPT - 1-ROG26R115/YOG75R245 PA-60-700P OPT- 1-ROG26R115/YOG75R245

26. Pitts See Avait. 6/3/94

27. Revo Inc. 2-1, -2 1A13 For 25 OPT - 1-ROY25G60R100/YOG65R245 6/3/94 (Lake) LA-4. -4A. -4P LA-200, -250

28. Rockwell Int. See Commander 6/3/94 Corp.

29. Scheizer G164 1A16 Car8 OPT -1-ROG50R100/Y0G65R210 10/30/97

30. Sky RC 2, 3, 4 A -769 FAR 21 OPT - 1-ROG30Y60R65/YOG65R260 6/3/94 Enterprises (SeeBee)

31. Socata Group TB9 A5 1EU CAR 3 OPT - 1- 6/3/94 (Aerospatiale) ROY25G55Y90R100/YOG100R245 TB10 = OPT-1- ROY25G55Y90R100/Y0G100R245 TB20, TB21, TB- OPT - 1- 200 ROY25G55Y90R100/YOG100R245 PE - 10.

FAA Approved Model List (AML) SA5925NM For Electronics International Oil Pressure/Temperature Instrument Issue Date: February 17, 1993 Original Certification FAA Sealed Installation Basis Drawings Instructions AML Aircraft Aircraft Certificate for Instrument Model Number Amended Item Make ModeL Number Alteration Number Rev. Number Rev. No. (See Note 1) Date TD0327921 N/R OI 0520911 C

32. Stinson See Univair. 6/3/94

33. Swift GC - 1A A-766 Car 4a OPT -1-ROG30R40/YOG65R225 10/30/97 (Globe) GC - 18 OPT - 1-ROG30R40/YOG65R220 34- Thompson, A, B, C, H A-782 CAR 3 OPT - 1-ROG30R90/YOG100R215 6/3194 Jimmie, OPT - 1-ROG30R90/YOG100R215 Enterprise (Navion)

35. Univair 108, 108-1 A -767 CAR 3 OPT - 1-ROG35R55/YOG80R230 6/3/94 Aircraft Corp. 108-2, -3, -5 OPT - 1-ROG35R55/YOG80R230 (Stinson)

36. Zenair CH2000 TASCH Far 21 OPT-1 10/30/97 ROY25G60Y9OR100/Y0G65R245

- End of List Mote 1: Electronics International Model Designation System.

2 / 82 A combination of letters and numbers defining the green, yellow and red oil Temperature arcs that the analog portion of the instrument was programmed to.

A combination of letters and numbers defining the green, yellow and red Oil Pressure arcs that the analog portion of the instrument was programmed to.

A Letter here indicates any major changes in the hardware and/or software of the instrument.

Indicates the base model number of the instrument.

Example: OPT-1-ROY26G56R100/Y0G66R240 indicates the following markings and calibration (arc information is for reference only):

Oil Pressure: A red arc from 0 to 25 PS1, a yellow arc from 26 to 55 PSI, a green arc from 56 to 99 PS1 and red from 100 PSI on up.

Oil Temperature: A yellow arc from O and below to 65'F, a green arc from 66 to 239'F and red from 240'F on up.

FAA Approved: Dore: Doc. 8, 1997 Acting Manager, Seattle Aircraft Certification Office Pag F 10

## Every issue (1)

- December 8, 1997: Amended, Current. [certificate](https://openairdocs.org/files/sha256/cf/9b/cf9b90fde9bf868f8f87abade3bc8b122caa487ac8ae7154c39200f98cd492e0), [AML SA5925NM.pdf](https://openairdocs.org/files/sha256/b1/6d/b16d071b79957762c5706ae0e8ab373eef53f457d38f40cbacf7c44f7d452396)

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