What it approves
Increase maximum ramp weight to 7610 pounds, maximum takeoff weight to 7560 pounds, maximum landing weight is 7200 pounds, maximum zero fuel weight is 6533 pounds.
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 :
Increase maximum ramp weight to 7610 pounds; maximum takeoff weight to 7560 pounds; maximum landing weight is 7200 pounds; maximum zero fuel weight is 6533 pounds in accordance with Report 85-8 dated May 28, 1985, or later FAA approved revision.
FAA Approved Airplane Flight Manual Supplement dated July 11, 1985, or Supplement dated November 6, 1985, is required.
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.
This certificate and the supporting data which is the basis for a pproval shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the A dministrator of the F ederal A viation A dministration.
RAM Aircraft, Limited Partnership 7505 Karl May Drive Waco, TX 76708 A7CE M ake : Cessna M odel : 421C Date of application : May 29, 1985
Date of issuance : July 11, 1985
Date reissued : October 8, 2001
Date amended : November 6, 1985 Revision 1
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 2
Number SA5981SW Date of Issuance: July 11, 1985
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 | 421C | A7CE |