# STC SA2005WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Texas Airplane Mfg Co, Inc, United States
- Description: Installation of cabin air conditioning system
- Applied: February 26, 1969
- Status date: September 5, 1974
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A-807](https://openairdocs.org/tcds/A-807)
- Certificate PDF: https://openairdocs.org/files/sha256/39/28/39288f85d9606fe9de026b7bc5f3117ff7c29c33f4ca8a58cd58ddde951eb267
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2E2F7486769B7AC785256CC10083D51F.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA2005WE

## ADs that name it (0)

None.

## Approved models (2)

- The de Havilland Aircraft Co. Ltd. D.H. 104 Dove Series 7AXC ([TCDS A-807](https://openairdocs.org/tcds/A-807))
- The de Havilland Aircraft Co. Ltd. D.H. 104 Dove Series 8AXC ([TCDS A-807](https://openairdocs.org/tcds/A-807))

## 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.

mnM ^tatts of:

department of Importation -federal ablation administration Supplemental t^pe Certificate tyKwmv&t1- SA2005WE TwMa Airplane Mfg. Company, Inc.

P 0. Box 575 Add!son, Texas 75001 ,/' tiMr^'^afifm^n,-if t, tSl*atila£&n4r.

de HavilUnd .-D.H. 104 Dova SerUa 7AXC, 8AXC Installation of cabin air conditioning ayat«m la accordance wth FAA Sealed Ton Carstedt Master Drav;ing List No. CPD 9994.

Approved Von Carstedt Airplane Flight Manual Revision dated August 28, 1969, 1* required with this installation.

This installation is approved only on aircraft modified per STC SA1747WE.

v? ... ,. //' /... The approval of this change in type design applied basically^j*ti^a^nfia/nf/,'-Jariai:ftiA _ _ ^ *co theie above raoael aircraft only. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it la determined by the installer that the interrelationship between this change and any of those other previously approved modifications -111 introduce no adverse effect upon the airworthiness of that aircraft. This determination should include consideration of significant changes in weight distributed such as an Increase in the fixed disposable weight in the fuselage.

vf-^i^if<»'a^AfiMf/f/t^^^unln'Ji'Hf,^Xef/titi^ifi^Aa^- February 26, 1969 G/l f , 2/26/73» 9/5/74~£-*4ttf -pnAAstffff - August 28, 1969 ^ Don P Watson Acting Chief, Bnglneering and Manufacturing Branch

This ceitijicale may be Iransfeiied jn aicurdaact with FAR 2I.47, FAAFoiw 6110-5 (10-46)

INSTRUCTIONS: The transfer endorse merit below may ba used to notify tha appropriate FAA Regional Offica of the transfer of the Supplemental Type Certificate.

The FAA will raiasue the certificate in tha nane of the transferee and forward it to him.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) __ (Number and street) (City, State, and ZIP code) from (Name of" grantor) (Print or type) (Address of grantor) (Number s street) (City, State, and ZIP code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (1)

- September 5, 1974: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/39/28/39288f85d9606fe9de026b7bc5f3117ff7c29c33f4ca8a58cd58ddde951eb267)

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