# STC SA2846SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Del-Air
- Description: Conversion from trigear to conventional gear configuration
- Status date: February 4, 2004
- Data sheets: 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, A13EU, A13EU, A13EU, A13EU, A13EU, A13EU, A13EU, A13EU, A13EU, A13EU, A13EU, A13EU
- Certificate PDF: https://openairdocs.org/files/sha256/31/be/31be93f498f6be765df04f21c77989431224bcb39f962bf50b75fdd74233d772
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E0B114EEE1501266862570CB0071AD62.0001
- Page: https://openairdocs.org/stc/SA2846SW

## ADs that name it

None.

## Approved models (30)

- Reims Aviation S.A. Cessna F150G (TCDS A13EU)
- Reims Aviation S.A. Cessna F150H (TCDS A13EU)
- Reims Aviation S.A. Cessna F150J (TCDS A13EU)
- Reims Aviation S.A. Cessna F150K (TCDS A13EU)
- Reims Aviation S.A. Cessna F150L (TCDS A13EU)
- Reims Aviation S.A. Cessna F150M (TCDS A13EU)
- Reims Aviation S.A. Cessna F152 (TCDS A13EU)
- Reims Aviation S.A. Cessna FA150K (TCDS A13EU)
- Reims Aviation S.A. Cessna FA150L (TCDS A13EU)
- Reims Aviation S.A. Cessna FA152 (TCDS A13EU)
- Reims Aviation S.A. Cessna FRA150L (TCDS A13EU)
- Reims Aviation S.A. Cessna FRA150M (TCDS A13EU)
- The Cessna Aircraft Company 150 (TCDS 3A19)
- The Cessna Aircraft Company 150A (TCDS 3A19)
- The Cessna Aircraft Company 150B (TCDS 3A19)
- The Cessna Aircraft Company 150C (TCDS 3A19)
- The Cessna Aircraft Company 150D (TCDS 3A19)
- The Cessna Aircraft Company 150E (TCDS 3A19)
- The Cessna Aircraft Company 150F (TCDS 3A19)
- The Cessna Aircraft Company 150G (TCDS 3A19)
- The Cessna Aircraft Company 150H (TCDS 3A19)
- The Cessna Aircraft Company 150J (TCDS 3A19)
- The Cessna Aircraft Company 150K (TCDS 3A19)
- The Cessna Aircraft Company 150L (TCDS 3A19)
- The Cessna Aircraft Company 150M (TCDS 3A19)
- The Cessna Aircraft Company 152 (TCDS 3A19)
- The Cessna Aircraft Company A150K (TCDS 3A19)
- The Cessna Aircraft Company A150L (TCDS 3A19)
- The Cessna Aircraft Company A150M (TCDS 3A19)
- The Cessna Aircraft Company A152 (TCDS 3A19)

## 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.

This Certificate issued to DEL-AIR 2121 South Wildcat Way Porterville, California 93257 Part 3 of the Civil Air Regulations.

3A19 CESSNA See Limitations and Conditions Description of Type Design Change: Conversion from trigear to conventional gear configuration in accordance with Drawing List No. CC150-0000, Revision D, dated 03/18/85 and Revision E dated 02/10/96;

No. CC150-0001 revised 12/17/81 and Revision C, dated 02/10/96; N o. C150-002 Revised 12/17/81 and Revision C, dated 02/10/96; No. ABC-000 revised 10/24/83 and, Revision B, dated 02/10/96; or No. ABC- 0000 revised 04/05/80 and Revision B, dated 02/10/96; as applicable for model, or later FAA-Approved Revisions.

Limitations and Conditions: 1. This modification is eligible on Cessna Models 150, 150A, 150B, 150C, 150D, 150E, 150F, 150G, 150H, 150J, 150K, A150K, 150L, A150L, A150M, 150M, 152, A152, F150G, F150H, F150J, F150K, F150L, F150M, F152, FA150K, 150L, FRA150L, FRA150M, FA152.

2. Aircraft Modified by STC SA750CE, or SA4795SW are eligible for modification according to this STC.

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.

Date of application : June 20, 1977

Date of issuance : September 8, 1978

Date reissued : Jan. 13, 1989; Jun. 28, 1996;

Mar. 1, 2000; Jun. 21, 2000; Feb. 4, 2004

Date amended : See page 3 for amendments

( Signature) Manager, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office ( Title)

(A) 06/20/77 (I) 09/08/78 (A) (See below)

(R) 01/13/1989; 06/28/1996; 03/01/2000; 06/21/2000; 02/04/2004

Limitations and Conditions: (Continued)

2. The conventional gear configuration may be reconverted to the trigear configuration in accordance with Custom Craft Installation Instructions, Report CC1105 dated 06/06/78.

3. The leaf spring type main landing gear, CC150-010, and tubular spring main landing gear TG150-100 or TG150-010, may be installed interchangeably.

4. Compatibility of this modification with other previously installed equipment must be determined by the installer.

Dates Amended:

1. May 07, 1979

2. May 30, 1979

3. July 30, 1979

4. April 23, 1980

5. February 18, 1981

6. January 06, 1982

7. February 03, 1983

8. November 01, 1983

9. March 26, 1985

10. June 14, 1996

## Every issue (2)

- February 4, 2004: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/31/be/31be93f498f6be765df04f21c77989431224bcb39f962bf50b75fdd74233d772)
- June 21, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/5b/34/5b34f3bba3bd9647ff7995dae818ca478a1e1e7cc0794d740de15741e05cc8a3)

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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.