What it approves
Increase maximum ramp weight to 7610 pounds; maximum takeoff weight to7560 pounds; maximum landing weight is 7200 pounds; decrease zero fuel weight to 6533 pounds; install winglets
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; decrease zero fuel weight to 6533 pounds; install winglets in accordance with Drawing List No. 1133, Revision A dated 9/20/84, or later FAA approved revision.
Modification eligible on Cessna Model 421C, Serial Number 421C0001 thru 421C0800 only.
FAA Approved Airplane Flight Manual Supplement dated July 25, 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.
RAM Aircraft, Limited Partnership 7505 Karl May Drive Waco, TX 76708 A7CE M ake : Cessna M odel : 421C Date of application : November 08, 1983
Date of issu ance : September 24, 1984
Date reissued : October 8, 2001
Date amended : August 7, 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 SA5811SW Date of Issuance: September 24, 1984
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 |