# STC SA881EA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc., United States
- Description: Installation of Grimes 30-0437-1 anti-collision strobe light kit, P/N 34-0200-1.
- Applied: November 11, 1970
- Status date: June 4, 2007
- Product: Aircraft, Single-Engine
- Certification basis: Part 3, Part 21, Part 23
- Data sheets: [TCDS 1A15](https://openairdocs.org/tcds/1A15)
- Certificate PDF: https://openairdocs.org/files/sha256/53/18/5318b90b4bb6e1c97d94617788602b0b6c7089bb78f404a7fbbefb5083f60315
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F99357712E19E0C686257317004EB9CC.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA881EA

## ADs that name it (0)

None.

## Approved models (1)

- Piper Aircraft Inc. PA-24 ([TCDS 1A15](https://openairdocs.org/tcds/1A15))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

550 Route 55 Urbana, OH 43078

Part 3 of the Civil Air Regulations.

(See Type Certificate Data Sheet 1A15 for complete certification basis).

1A15 Original Product--Type Certificate Number :

Make : Piper Aircraft Corporation Model : PA-24

Installation of Grimes 30-0437-1 Anticollision Strobe Light Kit P/N 34-0200-1 in accordance with Grimes Manufacturing Co.

Specification Sheet P/N 34-0200-1 dated April 5, 1972, or later FAA approved revision.

1. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.

2. The Grimes 30-0437-1 Anticollision Light meets the requirements of FAR 23.1401(f) effective prior to August 11, 1971 (100 effective candles minimum). It also meets the requirements of FAR 23.1397, FAR 23.1401 ( c) and (d) effective August 11, 1971.

(See STC Continuation Sheet Page 3)

Date of application : November 11, 1970 Date reissued : May 5, 1988, November 5, 1991, June 4, 2007

Date of issuance : July 29, 1971

Date amended : May 2, 1972

( Signature) Charles L. Smalley Manager, Systems and Flight Test Branch Chicago Aircraft Certification Office

( Title)

FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES

Number SA881EA Date Reissued: June 4, 2007

Limitations and Conditions: Cont.

3. Although the requirements of FAR 23.1401 (b) are not met in the specific location, this installation is accepted as the aircraft was type certificated under airworthiness regulations that contained no anticollision light standards and the original issuance of this STC as a supplemental light was prior to August 11, 1971.

3. 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.

…END…

## Every issue (1)

- June 4, 2007: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/53/18/5318b90b4bb6e1c97d94617788602b0b6c7089bb78f404a7fbbefb5083f60315)

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