What it approves
Install vortex generators.
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.
Part 3 of the Civil Air R egulations.
Original Product Type Certificate N umber :
OPTION 1: Install vortex generators in accordance with RAM Aircraft Corp., drawing No. 1507, Rev. C dated March 11, 1992, or later FAA approved revision.
No change to the Airplane Flight Manual. OPTION 2: Install vortex generators in accordance with RAM Aircraft Corporation Drawing No. 1507, Rev. C dated March 11, 1992, or later FAA approved revision. See Option 2 in limitations for appropriate Flight Manual Supplement.
RAM Aircraft, Limited Partnership 7505 Karl May Drive Waco, TX 76708 A7CE M ake : Cessna M odel : 414A Date of application : September 05, 1991
Date of issuance : November 15, 1991
Date reissued : 10/8/01; 9/20/02
Date amended : 05/22/92, 12/07/93, 08/23/94 Revision 3
B y direction of the A dministrator
(Signature) S. Frances Cox, Manager Special Certification Office, Southwest Region
(Title)
FAA Form 8110-2-1(10-69) Page 2 of 3
FAA Form 8110-2-1(10-69) Page 3 of 3
N umber SA8125SW Date of Issuance: November 15, 1991 Amended Date: August 23, 1994 Reissuance Date: September 20, 2002
Compatibility of this design change with previously approved modifications must be determined by the installer. 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.
The following aircraft are approved for this modification:
Option 1:
(a) Cessna 414A modified per STC SA4943SW (Increased Gross Weight/Winglets).
(b) Cessna 414A modified per STC SA4943SW and SA7463SW (Increased Gross Weight/Winglets and Engine Modifications).
(c) Cessna 414A modified per STC SA4943SW and STC SA4546SW (Increased Gross Weight/Winglets, and Increased Horsepower).
(d) Cessna 414A unmodified.
(e) Cessna 414A modified per STC SA7463SW.
(f) Cessna 414A modified per STC SA4546SW.
Option 2:
(a) Cessna 414A modified per STC SA4943SW. Flight Manual Supplement FM1021 dated 11/15/91, or later FAA approved revision, is required.
(b) Cessna 414A modified per STC SA4943SW and SA7463SW. Flight Manual Supplement FM1022 dated 11/15/91, or later FAA approved revision is required.
(c) Cessna 414A modified per STC SA4943SW and SA4546SW. Flight Manual Supplement FM1023 dated 11/15/93, or later FAA revision is required.
(d) Cessna 414A unmodified. Flight Manual Supplement FM1027 dated 03/16/92, or later FAA approved revision is required.
(e) Cessna 414A modified per STC SA7463SW. Flight Manual Supplement FM1028 dated 03/16/93, or later FAA revision, is required.
(f) Cessna 414A modified per STC SA4546SW. Flight Manual Supplement FM1029 dated 03/16/92, or later FAA approved revision, is required.
-END-
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Cessna Aircraft Company | 414A | A7CE |