# STC SA00323WI

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Textron Aviation Inc
- Description: Increase seating capacity to four places.
- Status date: September 1, 2017
- Data sheets: A37CE
- Certificate PDF: https://openairdocs.org/files/sha256/9f/20/9f208475a467bdbc68e8d7114cbf59711860297fa4ba56a7c67c02ca718133c2
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E012F3DBA5A2E854862581CD0062BCE2.0001
- Page: https://openairdocs.org/stc/SA00323WI

## ADs that name it

None.

## Approved models (1)

- The Cessna Aircraft Company 208B (TCDS A37CE)

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

FAA Form 8110-2 (5/14) Page 1 of

Part of the

Signature

Title Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215 3 SA00323WI Federal Aviation Regulations.

23 A37CE Increase seating capacity to four places. The modification consists of the following:

a. Removal of the cargo barrier close-out nets (2613337-1, 1 each and 2613337-2, 2 each).

b. Removal of partition nets (9910573-16, 2 each).

(see continuation sheet 3 of 3) No cargo may be carried when either of the aft passenger seats are occupied. If cargo is to be carried, the barrier nets must be reinstalled and both aft passenger seats removed. It is the operator's responsibility to determine that the airplane remains within the safe weight and balance limits. Airplane Flight Manual supplement D1349-13 dated May 1, 1995, is required equipment for the 208B when this modification is installed. Compatibility of this design change with previously approved modifications must be determined by the installer.

Cessna 208B all serial numbers September 1, 2017 March 26, 1999 May 16, 1995 May 31, 1995 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: May 31, 1995 Date Amended: March 26, 1999 Date Reissued: September 1, 2017

Description of Type Design Change (continued):

c. Modify upper cargo door to remove cargo door handle spindle boss (2617000-1) and install inside door handle (5319026-1), lock plate (2617081-1), and attaching hardware.

d. Install upper door operation placards (2605013-1).

e. Install up to two aft single seat assembly (2614041-9 or 2614041-13).

All parts are Cessna Aircraft Company parts numbers.

-- END -- SA00323WI 3

## Every issue (2)

- September 1, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/9f/20/9f208475a467bdbc68e8d7114cbf59711860297fa4ba56a7c67c02ca718133c2)
- March 26, 1999: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/59/43/5943f7d889df21a159d55fac96fc537c94c735c0b70fb56a45545f8e4c0e63ea)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.