What it approves
Conversion from trigear to conventional gear configuration
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may 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
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 30
| Make | Model | Data sheet |
|---|---|---|
| Reims Aviation S.A. | Cessna F150G | A13EU |
| Reims Aviation S.A. | Cessna F150H | A13EU |
| Reims Aviation S.A. | Cessna F150J | A13EU |
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| February 4, 2004 | Reissued, current | Certificate |
| June 21, 2000 | Reissued, earlier issue | Certificate |