# STC SA1173CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Textron Aviation Inc
- Description: Installation of thrust reverser system per Cessna ECO 1947 with the installation of additional devices to preclude
reverser operation per the STC Continuation Sheet 3.
- Status date: September 1, 2017
- Data sheets: A22CE
- Certificate PDF: https://openairdocs.org/files/sha256/ca/c1/cac14b28f6dacfabf383bcc52dc973f1dd9cbad872ed956c861c48283f9e8c4f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D54DB7EE7C407AB2862581CD00632FEF.0001
- Page: https://openairdocs.org/stc/SA1173CE

## ADs that name it

None.

## Approved models (1)

- Textron Aviation Inc. 500 (TCDS A22CE)

## 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 SA1173CE Federal Aviation Regulations.

25 Installation of thrust reverser system per Cessna ECO 1947 with the installation of additional devices to preclude reverser operation per the STC Continuation Sheet 3.

This approval is limited to Serial Number 500-0095 airplane.

(see continuation sheet 3 of 3) Cessna 500 March 3, 1986; September 1, 2017 October 2, 1975 October 24, 1975 A22CE 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: October 24, 1975 Date Reissued: September 1, 2017

The conditions and limitations of Aircraft Type Certification Data Sheet A22CE apply except as follows:

1. This aircraft modified in accordance with Cessna Engineering Change Order 1947 Thrust Reverser Kit definition and draft copy of Cessna Service Bulletin 78-1 Thrust Reverser Installation. Placard must be installed in view of the pilot to read, "AIRCRAFT NOT TO BE FLOWN WITH THRUST REVERSERS ACTIVATED. SEE AIRCRAFT LOG."

2. Aircraft must be configured as follows for purpose of flight:

A. Thrust Reversers must be in locked-stowed position.

B. Mechanical lockout devices must be installed per Rohr Drawing 202-0053, Tool Instl-Lockout Thrust Reverser.

C. Reverser control levers must be placarded "LOCKOUT TOOL INSTALLED - DO NOT OPERATE."

D. Electrical Connectors must be disconnected and stowed at connectors P215, P216, P213, and P214 on the two Isolation Valves and the two Thrust Reverser Control Valves respectively.

E. Aircraft Log Book entry to state: AIRCRAFT AIRWORTHY AS THRUST REVERSERS INACTIVATED PER STC SA1173CE.

3. Aircraft may be utilized for taxi demonstration of Thrust Reversers when configured as follows:

A. Mechanical Lockout devices installed per Rohr Drawing 202-0053 Tool Instl-Lockout Thrust Reverser must be removed.

B. Remove Placard "LOCKOUT TOOL INSTALLED - DO NOT OPERATE" from Thrust Reverser Levers.

C. Electrical connectors P215, P216, P213, and P214 on the two Isolation Valves and the two Thrust Reverser Control Valves must be connected.

D. Aircraft Log Book entry to state: "AIRCRAFT NOT TO BE FLOWN AS THRUST REVERSER SYSTEM IS ACTIVATED."

-- END -- SA1173CE 3

## Every issue (1)

- September 1, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ca/c1/cac14b28f6dacfabf383bcc52dc973f1dd9cbad872ed956c861c48283f9e8c4f)

---
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.