# STC SA2532NM-D

- Type: Supplemental type certificate
- Status: Historical, Surrendered
- Holder: Hollingsead International, United States
- Description: Installation of Collins Model EFIS 85a, 4 Tube Electronic Flight Instrument System and dual Collins Model FD-109 Flight Director System. (1-11, Series 401AK)
- Applied: March 14, 1984
- Status date: March 19, 2009
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A5EU](https://openairdocs.org/tcds/A5EU)
- Certificate PDF: https://openairdocs.org/files/sha256/6e/4c/6e4cde70cac9d4c1145487349525d793d0f500cc0b86029c379e00537d27d7ae
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6F2033B3D9664106862575D000601E59.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA2532NM-D

## ADs that name it (0)

None.

## Approved models (1)

- British Aerospace Airbus Limited BAC 1-11 400 Series ([TCDS A5EU](https://openairdocs.org/tcds/A5EU))

## 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: SA2532NM-D Certificate This certificate issued to: Hollingsead International SURRENDERED 2226 Goodyear Avenue 3-19-09 Ventura, California 93003 on .

Certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requirement's of Part 40 of the Civil Air Regulations. (Effective December 31, 1953) Original Product Type Certificate Number: ASEU Make: British Aerospace Corporation Model: 1-11, Series 401AK Description of Type Design Change: Installation of Collins Model EFIS 85a, 4 Tube Electronic Flight Instrument System and dual Collins Model FD-109 Flight Director System in accordance with FAA sealed Tracor Aviation Index List IL-213-001, Revision B dated October 30, 1984 or later FAA sealed revision.

FAA approved Tracor Aviation Airplane Flight Manual Supplement required for this installation is listed on the sealed Tracor Aviation Index List.

Limitations and Conditions: The approval of this change in type design applies basically to the above listed BAC1-11 Model 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 by the installer that the interrelationship between this change and any of those previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. 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.

Date of Application: March 14, 1984 Date of Issuance: October 31, 1984

FEDERAL AVIATION Date Reissued: August 14, 1991; July 11, 1995;

March 15, 1996; April 1, 1998; August 1, 2005;

July 31, 2006 Date Amended:

By Direction of the Administrator lt K. Woo (Signature) TOMINISTRATO Manager, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office

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) from (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):

## Every issue (2)

- March 19, 2009: Surrendered, Historical. [certificate](https://openairdocs.org/files/sha256/6e/4c/6e4cde70cac9d4c1145487349525d793d0f500cc0b86029c379e00537d27d7ae)
- July 31, 2006: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/7a/68/7a687a07a2b6c8e7910785f50a029fc338e3c261d706d19ef554d658c2498dc6)

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