What it approves
Increase maximum ramp weight from 6750 to 7140 pounds and maximum takeoff weight to 7105 pounds, and addition of optional McCauley model 3AF32C515/82NLA-4.0 propellers.
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 from 6750 to 7140 pounds and maximum takeoff weight to 7105 pounds, and the addition of optional McCauley model 3AF32C515/82NLA-4.0 propellers in accordance with RAM Aircraft Corp. drawing number 1608, revision A, dated November 2, 1993, or later FAA approved revision.
FAA approved Flight Manual Supplement FM1050 dated December 6, 1993 or later FAA approved revision is required. Compatibility of this modification with previously installed equipment must be determined by 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 th e supporting data which is the basis for approval 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 : 414A Date of application : May 20, 1993
Date of issuance : December 06, 1993
Date reissued : October 8, 2001
Da te amended :
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 SA8726SW Date of Issuance: December 06, 1993
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 |