# STC SA5215NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Learjet Inc, United States
- Description: Installation of Honeywell Mode S transponder
- Applied: January 9, 1991
- Status date: March 7, 2002
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A-817](https://openairdocs.org/tcds/A-817)
- Certificate PDF: https://openairdocs.org/files/sha256/81/f0/81f0264f9787bfa8fecf07edbbe58b6f6b76a1504a6eeb9cbd38f6f15384c1fc
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A578FAB502868C7885256CC200122795.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA5215NM

## ADs that name it (0)

None.

## Approved models (4)

- Fokker Services F.27 Mark 200 ([TCDS A-817](https://openairdocs.org/tcds/A-817))
- Fokker Services F.27 Mark 400 ([TCDS A-817](https://openairdocs.org/tcds/A-817))
- Fokker Services F.27 Mark 500 ([TCDS A-817](https://openairdocs.org/tcds/A-817))
- Fokker Services F.27 Mark 600 ([TCDS A-817](https://openairdocs.org/tcds/A-817))

## What the certificate says

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

Departm if Transportation-Federal Aviation ministration Supplemental Type Certificate Number: SA5215NM This certificate issued to: Learjet Inc.

One Learjet Way Wichita, KS 67209 Certifies that the change in the type design for the fellowing product with the limitations and conditions therefor as specified hereen meets the airworthiness requirement's of Part 10 of the Civil Air Poegulations.

Original Product -Type Certificato Number: A-817 Make: Fokker Aircraft B.V.

Model: F-27 Mark 200, 400, 500, 600 Description of Type Design Change:

Installation of Honeywell Mode S transponder in accordance with AMR Combs, Inc., Drawing No. DEN-28324-614, revision N/C, FAA approved May 31, 1991, or later approved revision.

1. STC SA4597NM-D for the installation of provisions is required.

2. Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to 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.

3. A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft.

Date of Application: January 9, 1991 Date Reissued: January 4, 1995, March 7, 2002 Date of Issuance: May 31, 1991 Dule umended: November 13, 1991 FEDERAL AVIATION By Direction of the Administrator Da T David T. Grossman (Signature) Acting Manager HOMINS TRATION Northwest Mountain Region, Denver, Colorado Denver Aircraft Certification Office.

(Title)

## Every issue (1)

- March 7, 2002: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/81/f0/81f0264f9787bfa8fecf07edbbe58b6f6b76a1504a6eeb9cbd38f6f15384c1fc)

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