# STC SA2003SO

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Phoenix Air Group Inc.
- Description: Installation of certain External Under-Wing Military Stores designated as the HUTTS LTC-2 and LTC-6 target tow systems
- Status date: May 29, 2024
- Data sheets: A10CE, A10CE, A10CE, A10CE
- Certificate PDF: https://openairdocs.org/files/sha256/de/a2/dea2d6198e87f0e99fdbdb9db22e91d8d556c47bea0dfe1e37941f3605e4d7e1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172378996920240725214104.0001
- Page: https://openairdocs.org/stc/SA2003SO

## ADs that name it

None.

## Approved models (4)

- Learjet Inc. Learjet 35 (TCDS A10CE)
- Learjet Inc. Learjet 35A (C-21A) (TCDS A10CE)
- Learjet Inc. Learjet 36 (TCDS A10CE)
- Learjet Inc. Learjet 36A (TCDS A10CE)

## 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.

SA2003SO Phoenix Air Group, Inc.

100 Phoenix Air Drive, S.W.

Cartersville, GA 30120 Part 25 Title 14 Code of Federal Regulations A10CE Gates Learjet 35, 35A, 36, and 36A Installation of certain External Under-Wing Military Stores designated as the HUTTS LTC-2 and LTC-6 target tow systems in accordance with Flight International Report No. FI-83-6001, Rev. A, dated September 26, 1986, or later FAA approved revision.

This airplane must be operated in the Restricted Category with this STC installed. STC SA1604SO is required equipment for this installation. Airplane Flight Manual Supplement (Report No. FI-83-6001B), dated May 26, 1987, is a required part of this STC.

(See Limitations and Conditions continued on page 3 of 3) September 18, 1984 September 14, 1987, September 21, 2022, May 29, 2024 May 26, 1987 Christina M. Underwood Manager, East Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 3

SA2003SO 3

SA2003SO Date Reissued: May 29, 2024

2. This approval should not be incorporated in any aircraft of these specific models on which other approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those previously incorporated approved modifications will not introduce any adverse effect upon the airworthiness of the aircraft.

----------------------------END------------------------ 3 3

## Every issue (3)

- May 29, 2024: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/de/a2/dea2d6198e87f0e99fdbdb9db22e91d8d556c47bea0dfe1e37941f3605e4d7e1)
- September 21, 2022: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/27/0e/270e2998199d32aa02b56a4610afa06feaa2e6e8e1c4f4e3664b343137a438cb)
- September 14, 1987: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/6b/b4/6bb4779855d43caaa0b5715b6f6b7003e950c1679e1c894d5a17fd39afcd58b3)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.