# STC SA2700WE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Airborne Electronics, United States
- Description: Installation of Airborne Electronics solid state automatic propeller control Model 350A.
- Applied: July 5, 1972
- Status date: March 28, 1977
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A-777](https://openairdocs.org/tcds/A-777)
- Certificate PDF: https://openairdocs.org/files/sha256/36/94/3694684fa4ffba2a89cb6ddac71132741d7c7ef2d44e0ebbe6bb23c0560f3357
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/792D674746F2AF348625749C0066D0D2.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2700WE

## ADs that name it (0)

None.

## Approved models (8)

- Raytheon Aircraft Company 35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company A35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company B35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company C35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company D35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company E35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company F35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company G35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))

## What the certificate says

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

Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA2700WE This certificate issued to: Airborne Electronics 899 Haddock Street Foster City, C: 94404 Certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereen meets the airerhiness requirement's of Furt 3 If the Civil Air Regulations.

Original Product -Sype tertificate. Member: A-777 Make: Beech Medel A35, 35, B35, C35, D35, E35, F35, G35 Description of Type Design Change:

Installation of Airborne Electronics Solid State Automatic Propeller Control Model 350A in accordance with FAA sealed Airborne Electronics Top Drawing List No. 0350-0000, Revision El, dated April 27, 1976, or later FAA sealed revision, in place of Flight Research Engineering Corporation APC Model 31A installed in Beech airplane.

See Page 3 of this STC.

47 FAA FORM 8110-2 (10-68; Page 1 of 3 Pages

Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA2700WE March 28, 1977 Limitations and Conditions:

The approval of this change in type design applies basically to Beech Models 35, A35, B35, C35, D35, E35, and F35, with Continental Engine E185 and Beech Propeller Hub 215-107 with blades 215-207-88; and Beech Models 35, A35, B35, C35, D35, E35, F35, G35 with Continental Engine E225-8 and Beech Propeller Hub 215-107 with blades 215-213-84 only. This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane.

FAA approved Airborne Electronics Airplane Flight Manual Supplement No. 0350- 0004A, dated March 17, 1976, must be carried in aircraft.

**FAA FORM 8110-2-1 (10-59) PAGE 3 OF 3 PAGES FAA AC 73-2651**

## Every issue (1)

- March 28, 1977: Amended, Current. [certificate](https://openairdocs.org/files/sha256/36/94/3694684fa4ffba2a89cb6ddac71132741d7c7ef2d44e0ebbe6bb23c0560f3357)

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