What it approves
Increase seating capacity to five places. (208 WITH CARGOMASTER OPTION)
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.
FAA Form 8110-2 (5/14) Page 1 of
Part of the
Signature
Title effective February 1, 1965, plus amendments and special conditions listed in the type certificate data sheet.
SA2135CE Textron Aviation Inc.
One Cessna Boulevard Wichita, KS 67215 23 Federal Aviation Regulations Cessna 208 (with Cargomaster option) 208A and 208B 3 A37CE Increase seating capacity to five places. The modification consists of the following:
a. Removal of cargo barrier and closeout nets (2613334-1, -17, or -34; and 2613337-1, 2 each and 2613337-2, 2 each).
b. Removal of partition nets (2601174-1, 2 each or 9910573-1, 2 each).
1. Airplane Flight Manual Supplement (AFMS) dated August 15, 1985, is required equipment for the 208A when this modification is installed.
2. AFMS dated May 22, 1988, is required equipment for the 208B when this modification is installed.
(see continuation sheet 3 of 3) September 11, 1985; April 22, 1987;
April 27, 2017 May 22, 1988; March 18, 1992 August 8, 1985 August 15, 1985 Mark Fuller STC ODA administrator ODA-100129-CE
FAA Form 8110-2 (5/14) Page 2 of
To (Name and address of transferee)
From (Name and address of grantor)
FAA Form 8110-2 (5/14) Page 3 of
Date of Issuance: August 15, 1985 Date Amended: March 18, 1992 Date Reissued: April 27, 2017
Description of Type Design Change (continued):
c. Modify upper cargo door to remove cargo door handle spindle boss (2617100-2) and install inside door handle (5319026-1), lock plate (2617081-1), and attaching door hardware.
d. Install upper door operation placard (2605013-1).
e. Install aft single seat assembly (2614029-1).
f. Install aft bench seat assembly (2614028-1).
Note: All parts are Cessna Aircraft Company part numbers.
3. AFMS dated March 17, 1992, is required equipment for the 208 with the Cargomaster option when this modification is installed.
4. This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of these other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane.
-- END -- 3 SA2135CE
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