# STC SA1473SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Fly-A-Charter LLC d/b/a Avcon 2
- Description: Replace passenger entrance door with wide cargo door.
- Status date: June 10, 2021
- Data sheets: A7EU, A7EU, A7EU, A7EU, A7EU, A7EU, A7EU, A7EU, A7EU
- Certificate PDF: https://openairdocs.org/files/sha256/32/43/3243710cd9e68eb61c820cde58d770de3dbdfbd2f2c8ab5967de7d02047c25c5
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5814A5264ECCBAF086258717004BBE51.0001
- Page: https://openairdocs.org/stc/SA1473SW

## ADs that name it

None.

## Approved models (9)

- Dassault-Aviation Fan Jet Falcon Series C (TCDS A7EU)
- Dassault-Aviation Fan Jet Falcon Series D (TCDS A7EU)
- Dassault-Aviation Fan Jet Falcon Series E (TCDS A7EU)
- Dassault-Aviation Fan Jet Falcon Series F (TCDS A7EU)
- Dassault-Aviation Fan Jet Falcon Series G (TCDS A7EU)
- Dassault-Aviation Mystere-Falcon 20 - C5 (TCDS A7EU)
- Dassault-Aviation Mystere-Falcon 20 - D5 (TCDS A7EU)
- Dassault-Aviation Mystere-Falcon 20 - E5 (TCDS A7EU)
- Dassault-Aviation Mystere-Falcon 20 - F5 (TCDS A7EU)

## 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.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate SA1473SWNumber:

This certificate issued to: Fly-A-Charter, LLC d/b/a Avcon 2 843 Willow Run Airport Ypsilanti, MI 48198 BB__.

Make: Dassault AviationOriginal Product A7EU 7\SH&HUWLILFDWH1XPEHU Fan Jet Falcon Basic, Series C, D, E, F, GModel: Mystere-Falcon 20, Series C5, D5, E5, F5Description of Type Design Change:

Replacement of Passenger Entrance Door with Wide Cargo Door. Data required:

1. Basic Falcon series C/D/E/F/G only: FAA Approved Drawing List No. 2720, dated June 9, 1975, and 1a. Alternate net installation: FAA Approved Drawing List No. 2744, dated July 26, 1974, or later FAA Approved revision to both.

Continued on page 3.

1. The following STC must be installed: STC SA1468SW, for emergency exit requirements.

Continued on Page 3.

11/24/72, 10/9/74, 2/14/75, 7/6/87, 6/10/21August 10, 1971Date of Application: Date Reissued:

7/7/75, 3/23/88, 5/18/89, 12/7/04May 24, 1972Date of Issuance: Date Amended:

Grant Youngdahl Program Manager Title: Wichita ACO Branch $Q\DOWHUDWLRQRIWKLVFHUWLILFDWHLVSXQLVKDEOHE\DILQHRIQRWH[FHHGLQJRULPSULVRQPHQWQRWH[FHHGLQJ\HDUVRUERWK7KLVFHUWLILFDWHPD\EHWUDQVIHUUHGRUPDGH DYDLODEOHWRWKLUGSHUVRQVE\OLFHQVLQJDJUHHPHQWVLQDFFRUGDQFHZLWK&)53RVVHVVLRQRIWKLV6XSSOHPHQWDO7\SH&HUWLILFDWH 67& GRFXPHQWE\SHUVRQVRWKHUWKDQ WKH67&KROGHUGRHVQRWFRQVWLWXWHULJKWVWRWKHGHVLJQGDWDQRUWRDOWHUDQDLUFUDIWDLUFUDIWHQJLQHRUSURSHOOHU7KH67&¶VVXSSRUWLQJGRFXPHQWDWLRQ GUDZLQJVLQVWUXFWLRQV SURSHOOHUPXVWSURYLGHWKDWSHUVRQZLWKZULWWHQSHUPLVVLRQDFFHSWDEOHWRWKH)$$ 5HI&)5   )$$)RUP   3DJHRIBBB 3

I United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate SA1473SWNumber:

Date oI transfer:

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United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1473SW Date Reissued: June 10, 2021 Airworthiness requirements (*continued from page 1):

Effective December 31, 1953, Amendments 4b-1 through 4b-12, Special Regulations SR-422B plus applicable FAR 25 paragraphs listed on TCDS A7EU.

Type Design Change (continued from page 1):

2. Mystere-Falcon 20 series C5/D5/E5/F5 only: FAA Approved Drawing List, No. 2720, Revision A, dated August 20, 2004, and 2a. Alternate net installation: FAA Approved Drawing List, No. 2744, Revision A, dated August 20, 2004 or later FAA Approved revision to both.

Limitations and Conditions (continued from page 1):

2. This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of these other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane.

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

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## Every issue (2)

- June 10, 2021: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/32/43/3243710cd9e68eb61c820cde58d770de3dbdfbd2f2c8ab5967de7d02047c25c5)
- December 7, 2004: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/f5/f1/f5f1ebe0335fcac72c9ebe0b357d4a09e16c99a2a658e72b55858c43faa7a2ae)

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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.
