# STC SA5924NM

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Electronics International, United States
- Description: Installation of RPM instrument.
- Applied: November 10, 1992
- Status date: November 24, 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 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-796](https://openairdocs.org/tcds/A-796), [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 5A2](https://openairdocs.org/tcds/5A2), [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) and 78 more
- Certificate PDF: https://openairdocs.org/files/sha256/51/cd/51cd157ff31872fae9a5dc58c1187779798cbb4e5a8bc6323c827e2a0245b8f6
- Approved model list and other attachments: [AML SA5924NM.pdf](https://openairdocs.org/files/sha256/12/eb/12eb6b8dc55e495a04acd70598dad3b0d7eb42f87a3b87bf3d71533e367e0fca)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/BC871E7D597E1E75862579BC00607F61.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA5924NM

## ADs that name it (0)

None.

## Approved models (586, 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))
- 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. 11CC ([TCDS A-796](https://openairdocs.org/tcds/A-796))
- American Champion Aircraft Corp. 7AC ([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. 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. S11CC ([TCDS A-796](https://openairdocs.org/tcds/A-796))
- 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))
- Aviat Aircraft Inc S-2B ([TCDS A8SO](https://openairdocs.org/tcds/A8SO))
- Aviat Aircraft Inc S-2S ([TCDS A8SO](https://openairdocs.org/tcds/A8SO))
- Boeing Airplane Company Wichita Division A75J1 (Army PT-18) ([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))

All 586: https://openairdocs.org/stc/SA5924NM/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: SA59241M This certificate issued to: Electronics International, Inc.

Purt * off the * Regulations:

Original Product -Lype bertificate Number * See attached FAA Approved Model List (AML) Make: * No. SA5924NM for list of approved airplane Model: * models and applicable regulations.

Description of Type Design Change: Electronics International RPM instrument manufactured nd installed in accordance with the drawings and installation instructions specitle 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 Limitations and Conditions: 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. SA5924NM, dated February 17, 1993, or later FAA approved revision, must be maintained as part of the

FEDERA AVIATION By Direction of the Administrator (Signature ) TRAINIST RAIDS Acting Manager, Special Certification Branch Seattle Aircraft Certification Office (Title)

FAA FoL 8110-2 (10-68)

### AML SA5924NM.pdf

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

FAA Approved Model List (AML) SA5924NM for Electronics International RPM Instrument Issue Date: February 17, 1993 Original Cert. FAA Sealed Installation E.I. Instrument Type Basis Drawings Instructions Model Number AML Aircraft Aircraft Certificate for (See Note 1) Amended Item Make Model Number Alt. Number Rev Number Rev. ( ) = See Note Date No. No.

TD0326921 0I 0517911

1. Aeronca Inc. (Also see 50 - LA 65-LA, LB A -702 A-702 Car 4a R-1-4-G30R230 R -1-4-G30R255 6/3/94 American and 15AC, S15AC A -802 Car 3 R-1-4-G30R270 Bellanca)

2. Aerospatiale See Socata. 6/3/94

3. American Blimp A -60, A-60+ AS1NM FAR 21 R-1-4-G30Y260R300 10/30/97 American Champion 7AC, STAC A-759 CAR 4 4-G30R2300 6/3/94 (Also see Aeronca 78CM, 7DC, S70C 1-4-G3OR257 and Bellanca) 7CCM, S7CCM, 7JC, 7EC, S7EC, S7CF - 1-4-G30R247 S7GC, 7HC R-1-4-G30Y260R280 7GCA, 7GCB, 7KC, 7GCBA, 7GCAA - 1-4-G30R270 7GCBC, 7KCAB -4-G30R270 7ECA FAR 21 1-4 -G30R275 8KCAB A21CE Far 23 -4-G30Y255R270 10/30/97 8GCBC -4-G30Y240R270 11AC, S11AC A-761 CAR 4a 1-4-G3OR230 11BC, S11BC CAR 4a R -1-4-G30R2575 11C, S11C A -796 Car 3 R-1-4-G30R2575

5. Aviat Inc. (Pitts) A22NM ABSO FAR 23 21 =.==.= R-1-4-G30R270 R-1-4-G30R270 6/3/94 ==== R-1-4-G30Y200G236R270 R-1-4-G30Y215G236R270 R-1-4-G30Y200G236R270

- 28 R-1-6-G30R270 Page of 10

FAA Approved Model List (AML) SA5924NM Electronics International RPM Instrument Issue Date: February 17, 1993 Original Cert. FAA Sealed Installation E.1. Instrument Type Basis Drawings Instructions Model Number AML Aircraft Aircraft Certificate for (See Note 1) Amended Item Make Model Number Alt. Number Rev Number ( ) = See Note Date No.

TD0326921 01 0517911

6. Beech Aircraft 18D, A180, S180, DA18D A-684 Bul 7A 9-G30Y210R220 8/5/94 Corp. A18A, SA18A R-1-9-G30Y210R240 D18S A -675 R-1-9-G30Y220R230 C18S A -757 R-1-9-G30Y220R250 D18C, C45G E18C, G18S, H18 A -765 R-1-9-G30R230 - 1-9-GOR220 I9A, M19A, B19 A1CE 1-4-G30R270 A23, A23A, A23-19, A23-24 -4-G30R270 B23, C23 -4-G30R270 A24R, B24R, C24R 35 A- 777 CAR 3 1-6-G30Y205R230 -4-G3OR270 A35 w/ E-185-1 1-6-G30Y205R230 A35 w/ E-225-8 1-6-G30Y230R265 B35, 35R w/ E-185-8 R-1-6-G30Y205R245 B35, 35R w/ E-225-8 R-1-6-G30Y230R265 C35, D35, E35, F35 W/ E-185-11 C35, G35 D35, E35, F35 w/ E-185-11 R-1-6-G30Y230R260 R-1-6-G30Y230R265 R-1-6-G30Y230R265 H35, J35, K35, M35, 35-33 3A15 R-1-6-G3OR260 N52, P331 35-A33, 35-B33, 35-C33, E33, F33 G33 - 1-6-G30R262 - 1-6-G30R260 E33A, E33C S3S, V35, V35A, V358, 35-C33A F33A, F3SC 36, 36A, A6TC, B36TC R-1-6-G30R270 R-1-6-G30R270 R-1-6-G30R270 R-1-6-G30R270 45 (YT -34) R-1-4-G30Y245R260 10430/97 A45 (T-34A), D45 (T348) R-1-6-G3OR260 R-1-6-G30R300 8/5/94 B5O, C5O, D5O, D5OA, D50B, D5OC F50, G50, H50, J50 DSOE R-1-6-G30R310 R-1-6-G30R320 R-1-6-G30R310 D55, D55A, ESS, E55A 3A16 3 R-1-6-G3OR270 56TC, A56TC R-1-6-G30R290 58, 58A w/ 2 Blade Prop. R-1-6-G3OR255 58, 58A w/ 3 Blade Prop. 60, A60, B60 65, 65-80, 65-A80, 65-B80 A12CE 23 R-1-6-G30R270 R-1-6-G30R275 R-1-6-G30Y320R340 65-88, A65, A65-8200 R- 1-6-G30Y320R340 70 R-1-6-G30R320 76 A29CE R- 1-4-G30R270 77 95, 895 B95A, D95A, E95 95-55, * 5805, 5-85, 95-0559 3A16 R-1-4-G30R270 R-1-4-G30R270 R-1-4-G30R270 R-1-6-G30R262 95 - 8558 R-1-6-G30R262 95-C55, 95-C55A R-1-6-G30R270 Page of 10

FAA Approved Model List (AML) SA5924NM for Electronics International RPM Instrument Issue Date: February 17, 1993 Original Cert. FAA Sealed Installation E.I. Instrument Type Basis Drawings Instructions Model Number AML Aircraft Aircraft Certificate for (See Note 1) Amended Item Make Model Number Alt. Number Rev Number Rev. ( ) = See Note Date No. No.

TD0326921 0I 0517911

7. Bellanca Aircraft 14-19 1A3 Car 3 R-1-6-G30R255 613194 Corporation 17-30 R-1-6-G30R270 (Also, see 17-31 R-1-6-G30R257 American 17-31TC = R-1-6-G30Y240R257 Champion) 17-30A A18CE FAR 23 R-1-6-G30R270 17-31A R-1-6-G30R270 17-31ATC R-1-6-G30R2575

8. Boeing Aircraft A 75 J1 (Stearman) A-743 CAR 4a R-1-7-G30R200 10/30/97 1B75A R-1-9-G30Y195R230 Page of 10

FAA Approved Model List (AML) SA5924NM for Electronics International RPM Instrument Issue Date: February 17, 1993 Original Cert. FAA Sealed installatior E.I. Instrument Type Basis Drawings instructions Model Number AML Aircraft Aircraft Certificate for (See Note 1) Amended Item Make Model Number Alt. Number Rev Number Rev. ( ) = See Note Date No. No.

TD0326921 01 0517911 Cessna Aircraft 120, 140 м/ с-85 A- 768 CAR 4a R- 1-4-G30R257 8/5/94 Corp. 120, 140 w/ C-90 R-1-4-G30R247 120, 140 w/ C 0-235 R-1-4-G30R260 140A w/ C-85 5A2 CAR 3 R-1-4-G30R257 140A w/ C-90 R-1-4-G30R247 150, 150A, 150B, 150C, 150D 3A19 CAR 3 R-1-4-G30R275 150E, 150F, 150G, 150H, 150J R-1-4-G30R275 150K, A150K, 150L, A150L R-1-4-G30R275 50M, A150M R-1-4-G30R275 52, A152 R-1-4-G30R255 (2) 170 A - 799 R-1-4-G30R270 170A, 170B w/o Franklin Eng. R-1-4-G30R270

172. T286, T24, 12, 1720, 1722 R-1-4-G30Y215G225R280 3А12 R-1-4-G30R270 (5) R-1-4-G30R270 (5) 172K, 172M, 172N, 172P 172Q R-1-4-G30R270 (5) R172E, R172F, R172G, R172H, R172J 3A17 CAR 3 R-1-4-G30R280 (4) R172K R-1-4-G3OR260 (4) P1720 R-1-4-G30R320 (4) 172RG = = R-1-4-G30R270 (4) 175, 175A, 175B, 175C R-1-4-G30R320

177. 177A A13CE FAR 23 R-1-4-G30R270 177B w/ B2D34C206/78TA-0 Prop. -4-G30Y140G175R270 177B w/o B2D34C206/78TA-0 Prop. 177RG A20CE = = R-1-4-G30Y170G190R270 1-4-G30Y140G175R270 180 w/ 0-470-А 5A6 1-6-G30R260 (5) 180 / 0-470-J 1-6-G30R255 (5) 180w/ 0-470-K 180A, 180B, 180C, 180D, 180E 180J 180E 1-6-G30R260 (5) 1-6-G30R260 (5) 180F, 180G, 180H, 180J 1-6-G30R260 (5) 180K R-1-6-G30R240 (5) 182, 182A, 182B, 182C, 182D, 182E 3А13 R-1-6-G30R260 182F, 182G, 182H, 182J, 182K R-1-6-G30R260 1820 182R, R182, T182, TR182 182M, 182N, 182P R-1-6-G30R260 R-1-6-G30R240 185, 185A, 185B, 185C, 1850, 185E 3A24 R-1-6-G30R262 A185E, A185F 1-6-G30Y270R285 188, 188A, 1888 -6-G30R260 A188, A188A, A188B, T188C -6-G30R270 190, 1958 21 - 7-G3OR220 195 w/ R-755-A2 Eng. R-1-7-G30R220 195 w/ L-4MB Eng. R-1-7-G30Y200R220 195 w/ L-6MB Eng. R-1-7-G30Y210R220 195A R-1-7-G30Y200R220 Pagr of 10

FAA Approved Model List (AML) SA5924NM for Electronics International RPM Instrument Issue Date: February 17, 1993 Original Cert. FAA Sealed Installation E.I. Instrument Type Basis Drawings Instructions Model Number AML Aircraft Aircraft Certificate for (See Note 1) Amended Item Make Model Number Alt. Number Rev Number Rev. ( ) = See Note Date No. NO.

TD0326921 0I 0517911 Cessna Aircraft TU206C A4CE CAR 3 R-1-6-G30R270 8/5/94 Corp. (Cont.) 06A R-1-6-G30R270 060, TP206E R-1-6-G30R270 P206A, P206E R-1-6-G30R270 R-1-6-G30R270 02068, R- 1-6-G30Y270R285 A16CE FAR 23 R-1-6-G30Y270R285 R-1-6-G30Y260R270

- 5A 3A21 CAR 3 R-1-6-G30R262 210H, R-1-6-G30R270 R-1-6-G30Y270R285 10H, 1210J R-1-6-G30R270 OR, P210R R-1-6-G30R270 R-1-6-G30Y260R270 5A5 CAR 3 R-1-6-G30Y230R260 3058, 3A14 R- 1-6-G30Y230R260 3A10 CAR 3 R-1-6-G30R260 310G R-1-6-G30R262 310K R-1-6-G30R262 E310H, E310J R-1-6-G30R262 10R R-1-6-G30R270 310Q R-1-6-G30R262 oc 3A25 R-1-6-G30R260 R-1-6-G30R270 336 AZCE R-1-6-G30R280 A6CE R-1-6-G30R280 R-1-6-G30R280

- 1-6-G30R280 -6-G30R260 1-6-G30R280 3A25 1-6-G30R270 402A, 4028 A7CE R-1-6-G30R270 402C R-1-6-G30R270 404 A25CE FAR 23 R-1-6-G30R223 A7CE CAR 3 R- 1-6-G30R270 R-1-6-G30R227 421C R-1-6-G30R223

10. Commander 112, 1128 A12SO FAR 23 R-1-4-G30R270 6/3/94 Aircraft 114A, 114B, 114TC R-1-6-G30R270 9/26/97 100, - 1128CÙ R-1-4-G30R257 6/3/94 6A1 CAR 3 R-1-6-G30R257 10/30/97 560, 560A, R-1-6-Y300R340 680F, 680FC, 560F, 720 2A4 R-1-6-G30R320 A12SW R- 1-6-G30R250 Page - of 10

FAA Approved Model List (AML) SA5924NM Electronics International RPM Instrument Issue Date: February 17, 1993 Original Cert. FAA Sealed Installation E.I. Instrument Type Basis Drawings Instructions Model Number AML Aircraft Aircraft Certificate for (See Note 1) Amended Item Make Model Number Alt. Number Rev Number Rev. ( ) = See Note Date No. No.

TD0326921 01 0517911 C

11. DeHavil land DHC -2 A-806 CAR 10 = = R-1-6-G30Y200R220 6/3/94 Aircraft of DHC -3 A-815 CAR 10 R-1-6-G30Y200R220 6/3/94 Canada, Ltd.

12. Extra Flugzeugbau EA 300, - S A67EU FAR 23 R-1-6-G30Y240R270 10/30/97

13. Fairchild 24 C8C A -535 Bul 7a R-1-8-G30R205 10/30/97 24 R9 A - 706 Car 4a R-1-6-G30R245

14. Grumman F8F-2 AR - 32 CAR 8 R-1-18-G30R260 10/30/97 AF-2S w/R-2800-48 AR - 36 R-1-18-G30Y260R280 15 . Gulfstream AA-5, -5A, -5B ANẸN FAR 23 R-1-4-G30R2700 6/3/94 American Corp. AA - 1 - 1A, - 18 R-1-4-G30R2600 (Grumman AA - 1C R-1-4-G30R2700 Aircraft)

16. Helio Aircraft 15A ЗАЗ CAR 48 R-1-6-G30R2600 10/30/97 (Taylorcraft) 20 w/0-470-A R-1-6-G30R2450 20 w/0-470-J R-1-6-G30R2550

17. Helio Enterprise K-250 1A8 CAR 3 R-1-6-G30R257 10/30/97 H-295, HT-295, F-295 R- 1-6-G30Y300R340 Н-391, -3918, -395, -395А H-700 = = = = : R-1-6-G30Y300R340 R-1-6-G30R257 H-800 R-1-8-G30R265 18- Interceptor 200 ЗА18 car 3 R- 1-6-G30R260 10/30/97 (Aero Commander) 200A, 200B R-1-6-G30R262 (Meyers) 200D R-1-6-G30R270 19- Lake See Revo. 6/3/94

20. Luscombe 8 A-694 CAR 40 R-1-4-G30R190 6/3/94 BA R - 1-4-G30R235 8B R-1-4-G30R255 BE 8C, 8D R -1-4-G30R260 R-1-4-G30R257 8F, T-8F R-1-4-G30R247 Pagr of 10

FAA Approved Model List (AML) SA5924NM for Electronics International RPM Instrument Issue Date: February 17, 1993 Original Cert. FAA Sealed Installation E.I. Instrument Type Basis Drawings Instructions Model Number AML Aircraft Aircraft Certificate for (See Note 1) Amended Item Make Model Number Alt. Number Rev Number Rev. ( ) = See Note Date No. No.

TD0326921 01 0517911

21. Maule M-4, M-4C, M-4S, M-4T 3A23 CAR 3 R-1-4-G30R270 8/5/94 M-4-180C, M-4-180S, M-4-180T R-1-6-G30R280 M-4-210, -210C, -210S, -210T R-1-6-G30R280 M-4-220, -220c, -220S, -220T R-1-6-G30R280 1-5 - 180C R-1-4-G30R270 -5-210C, - 220c R-1-6-G30R280 1-5-235C -1-6-G30R240 M-5-210TC 1-4-G30R257 M-5-200 -4-G30R270 M-6-180 -4-G30R270 M-6-235 1-6-G30R240 M-7-180 1-6-G30R270 M-7-235 R-1-6-G30R240 MX - 7-180 R-1-4-G30R270 MX-7-235 R-1-6-G30R240

22. Mooney Aircraft M2O, A, B, C, D, G 2A3 Car 3 R - 1 -4-G30R200G225R270 8/5/94 Corp. M20J M20E, R-1-4-G30R200G235R270 R-1-4-G30R270 M20K R-1-6-G30R270 M20L R-1-6-G30R234 M20M R-1-6-G30R2575 M22 A6SW R-1-6-G30R257

23. Moravan zlin 526C A30EU PA 25 = R-1-4-G30R270 10430/97 Z-242L A76EU R-1-4-G30R270 2-143L R-1-6-G30R240

24. Navion See Thompson. 6/3/94 Page of 10

FAA Approved Model List (AML) SA5924NM for Electronics International RPM Instrument Issue Date: February 17, 1993 Original Cert. FAA Sealed Installation E.I. Instrument Type Basis Drawings Instructions Model Number AML Aircraft Aircraft Certificate for (See Note 1) Amended Item Make Model Number Alt. Number Rev Number Rev. ( ) = See Note Date No. No.

TD0326921 01 0517911

25. Piper Aircraft PA - 12, - 12S A-797 CAR 3 R-1-4-G30R260 10/30/97 Corp. PA - 14 A - 780 R-1-4-G30R280 PA - 15 A-800 CAR 3 1-4-G3OR255 8/5/94 PA - 16 A - 1A - 1-4-G30Y260R280 PA - 17 A-805 R-1-4-G30R230 PA - 18 1A2 CAR 3 • 1-4-G30Y235R247 PA-(18 or 18A or 18S) "125" 1-4-G30Y245R260 PA-(18 or 18A or 18S) "135" - 1-4-G30Y245R260 PA-(18 or 18A or 18S) "150" - 4-G30R270 PA - 19 4-G30R247 PA-20, -20S, -20-115, -20S-115 1A4 4-G30Y245R260 PA-20-135 4-G30Y245R260 PA -22, - 22-108, -22-135, - 22S- 135 1A6 -4-G30Y245R260 PA-22-150, -22S-150, -225-160 R-1-4-G30R270 PA-23 1A10 R-1-4-G30R270 PA -23-160 R-1-4-G30R270 PA-23-235 R-1-6-G30R257 PA-E23-250 R-1-6-G30R257 PA-24 1A15 R-1-4-G30R270 PA-24-250 R-1-6-G30R257 PA-24-260 R-1-6-G30R270 PA-24-400 R-1-8-G30R265 PA - 25 2A8 R-1-6-G30R270 PA- 25-235 R-1-6-G30R257 PA -25-260 R-1-6-G30R270 PA -28-140 2A13 R- 1-4-G30R270 PA -28-150 R-1-4-G30R270 PA-28-151 R-1-4-G30R270 PA- (28 or 28S)-160 R-1-4-G30R270 PA -28-161 R-1-4-G30R270 PA-28-180, PA-28S-180 R-1-4-G30R270 PA-28R - 180 R-1-4-G30Y200G220R270 PA-28-181 R-1-4-G30Y265R270 PA-28R-200 w/ Hart. Prop. R-1-4-G30Y210G235R270 A-28R-200 w/ McCauley Prop. R-1-4-G30Y150G195R270 PA-28-201T R-1-6-G30Y200G220R257 PA - 28R - 201 R-1-4-G30Y150G195R270 PA-28RT-201 N/ S/N => 8018001 R-1-4-G30Y265R270 PA-28RT-201 w/ S/N < 8018001 R-1-4-G30Y150G190R270 PA-28R-201T, PA-28-235 R-1-6-G30Y200G220R257 PA -28RT - 2011 R-1-6-G30Y200G220R257 PA -28-236 R-1-6-G30R240 PA -30 ATEA R-1-4-G30R270 PA -31 A20SO R-1-6-G30R257 PA -31-325 R-1-6-G30R257 PA-31-300 R-1-6-G30R270 Page of 10

FAA Approved Model List (AML) SA5924NM Electronics International RPM Instrument Issue Date: February 17, 1993 Original Cert. FAA Sealed Installation E.I. Instrument Type Basis Drawings Instructions Model Number AML Aircraft Aircraft Certificate for (See Note 1) Amended Item Make Model Number Alt. Number Rev Number Rev. ( ) = See Note Date No. No.

TD0326921 0I 0517911

25. Piper Aircraft PA-32-260, -32-300, - 32R -300 A3SO CAR 3 R-1-6-G30R270 8/5/94 Corp. (Cont.) PA-32S-300, - 32RT - 300 R-1-6-G30R270 PA- 32RT- 300T R-1-6-G30Y257R270 PA-32-3011, - 32R - 301T R-1-6-G30Y257R270 PR-32-301, - 32R -301 R-1-6-G30Y260R270 PA-34-200 AZSO FAR 23 R-1-4-G30R270 PA-34-200T R-1-6-G30R257 PA- 34-220T R-1-6-G30R260 PA-36-285 A9SO R-1-6-G30R400 PA-36-300 R-1-6-G30R270 PA-36-375 R-1-8-G30R250 PA-38-112 A 185O R-1-4-G30R260 PA-44-180 A19SO R-1-4-G30R270 PA-44-180T R-1-4-G30R257 PA -46-310P A25S0 R-1-6-G30R260 PA -46-350P R-1-6-G30R250

26. Pitts See Avait. 6/3/94

27. Revo Inc. C-1, -2 1A13 R- 1-4-G30R270 613194 (Lake) LA-4, -4A, -4P R-1-4-G30R270 LA-200 R- 1-4-G30Y200G236R270 250 R-1-6-G30R257

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

29. Schweizer G-164 w/W-670-6A 1A16 Car 8 R-1-7-G30R2075 10/30/97

30. Sky RC 2, 3, 4 A-769 Far 21 R- 1-6-G30R250 6/3/94

31. Socata Group TB9 AS1EU CAR 3 R-1-4-G30R270 613194 (Aerospatiale) TB10 R-1-4-G30Y200G226R270 TB20, TB21 R-1-6-G30R257 TB -200 R-1-6-G30R270

32. Stinson See Univair. 6/3/94

33. Swift GC - 1A 9-766 CAR 48 R-1-4-G30R2575 10/30/97 (Globe) GC - 1B R-1-6-G30R2550

34. Thompson, Jimmie, A -782 CAR 3 R-1 -4-G3OR230 6/3/94 Enterprise R-1-6-G30R300 (Navion) C, D, E R - 1-6-G30R260 F, G R-1-6-G30R262 R-1-6-G30R270 Page of 10

FAA Approved Model List (AML) SA5924NM for Electronics International RPM Instrument Issue Date: February 17, 1993 Original Cert. FAA Sealed Installation E.I. Instrument Type Basis Drawings Instructions Model Number AML Aircraft Aircraft Certificate for (See Note 1) Amended Item Make Model Number Alt. Number Rev Number Rev. ( ) = See Note Date No. No.

... TD0326921 0I 0517911

35. Univair Aircart 108, 108-1 A-767 CAR 3 R-1-4-G30R260 6/3/94 Corp. (Stinson) 108-2, -3, -5 R-1-4-G30R280

36. Zenair CH2000 TASCH FAR 21 R-1-4-G30R280 10/30/97 -- End of List • Mote 1: Electronics International Instrument Model Designation System.

A combination of letters and numbers defining the green, yellow and red RPM Arcs that the analog portion of the instrument was programned to.

A number corresponding to the number of cylinders the instrument was calibrated 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: R-1-4-G80Y210G235R260 indicates a 4 cylinder engine with the following markings and calibration: a green arc from 800 to 2090 RPM, a yellow arc from 2100 to 2340 RPM, a green arc from 2350 to 2590 and red from 2600 on up. Arc information is for reference only.

Note (2): For carbureted engines use the following placard, "Carb Ht Below 1900".

Note (3): For carbureted engines use the following placard, "Carb Ht Below 2000".

Note (4): For carbureted engines use the following placard, "Carb Ht Below 2100".

Note (5): For carbureted engines use the following placard, "Carb Ht Below 2200".

FAA Approved: Dote: Mov. 24, 1952 Acting Manager, Seattle Aircraft Certification Office Page of 10

## Every issue (1)

- November 24, 1997: Amended, Current. [certificate](https://openairdocs.org/files/sha256/51/cd/51cd157ff31872fae9a5dc58c1187779798cbb4e5a8bc6323c827e2a0245b8f6), [AML SA5924NM.pdf](https://openairdocs.org/files/sha256/12/eb/12eb6b8dc55e495a04acd70598dad3b0d7eb42f87a3b87bf3d71533e367e0fca)

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