# STC SA1220EA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: PATS Aircraft LLC, United States
- Description: Installation of a Garrett AiResearch GTCP 36-100(A) APU.
- Applied: November 13, 1980
- Status date: June 1, 2005
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A46EU](https://openairdocs.org/tcds/A46EU)
- Certificate PDF: https://openairdocs.org/files/sha256/ab/86/ab86cf3d030f1a1ecfa8e2b318b8f923cbfa40edd95caa53fbd20d9a72ba9143
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0E9DD3883028A7A3862570370063F494.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1220EA

## ADs that name it (0)

None.

## Approved models (1)

- Dassault-Aviation Mystere-Falcon 50 ([TCDS A46EU](https://openairdocs.org/tcds/A46EU))

## 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.

Number SA1220EA This certificate issued to PATS Aircraft, LLC 21652 Nanticoke Avenue Georgetown, DE 19947

Part 25 of the Federal Aviation Regulations.

Original Product -- Type Certificate Number : A46EU Make : Avions Marcel Dassault-Breguet Aviation

Model : Mystere-Falcon 50

Configuration 1: Installation of a Garrett AiResearch GTCP 36-100(A) APU in accordance with the data listed in PATS, Inc.

Report 162, Rev. A, dated February 10, 1981, and silencer mod. drawing SK50-232, dated December 20, 1989.

Configuration 1:

a) The above modification is limited to Aircraft S/N 14 only.

b) PATS, Inc. AFMS No. 2, FAA approved February 13, 1981, must accompany this modification.

Date reissued : June 29,1981, March 25, 1983, April 10, 2002, June 1, 2005

Date amended : September 14, 1981, April 8, 1982 April 14, 1993, Rev. 8

( Signature) Raymond H. Reinhardt Acting Manger New York Aircraft Certification Office

(Title) Date of application : November 13, 1980

Date of issuance : February 13, 1981

Number

FAA Form 8110-2-1(10-69) Page 2 of 2

SA1220EA Date of Reissuance: June 1, 2005

Description of Type Design Change: (Continued):

Configuration 2: Installation of a Garrett AiResearch GTCP 36-100(A) APU in accordance with the data listed in PATS, Inc.

Report 196, dated September 2, 1981, or later FAA approved revisions.

Configuration 3: Installation of a Garrett AiResearch GTCP 36-100(A) APU in accordance with the data listed in PATS, Inc.

Report 211 through Rev. G, dated May 18, 1992, or later FAA approved revisions.

Configuration 4: Installation of a Garrett AiResearch GTCP 36-100(A) APU in accordance with the data listed in PATS, Inc.

Report 211 through Rev. J, dated August 31, 1992, and Report 212, Rev. H, dated August 31, 1992 or later FAA approved revisions.

Configurations 2, 3 or 4:

a) PATS, Inc. Flight Manual Supplement No. 4, Revision B, dated August 25, 1989 must accompany configuration 2 or 3.

b) PATS, Inc. Flight Manual Supplement No. 4, Revision C, dated November 17, 1992 must accompany configuration 4.

Configurations 1, 2, 3 and 4:

a) This approval is limited to ground use only.

b) PATS, Inc. Report No. 222, “Maintenance Manual for th e Garrett GTCP 36-100(A) APU Installed in AMD-BA Falcon 50,” dated January 25, 1982, pertains to this installation. Configurations 1, 2 and 3 require that Service Bulletin FJC No.

50-32, dated May 17, 1989 be accomplished.

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.

Compatibility of this design change with previously approved modifications must be determined by the installer.

…. END….

FAA Form 8110-2-1(10-69) Page 3 of 2

## Every issue (1)

- June 1, 2005: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ab/86/ab86cf3d030f1a1ecfa8e2b318b8f923cbfa40edd95caa53fbd20d9a72ba9143)

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