STC SA02442LA

Supplemental type certificate · Peter Schiff Aero Inc.

Holder
Peter Schiff Aero Inc. · United States
Status
Current · Issued
Status date
June 5, 2015
Applied
August 26, 2010
Product
Aircraft · Small/Large Airplane
Certification basis
Part 21, Part 23
Data sheet
TCDSA24CE

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of Model 830 CCA Air Conditioning System

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.

This Certificate issued to Peter Schiff Aero, Inc.

4900 Forrest Hill Road Cookeville, TN 38506

Part 23* of the Federal Aviation Regulations.

*Certification basis is set forth in Type Certificate Data Sheet A24CE.

Original Product Type Certificate Number : A24CE Make Beechcraft Model 200 200C 200CT 200T 300 300LW B200 B200C B200CT B200GT B200T B300 B300C

Description of Type Design Change: Installation of Model 830 CCA Air Conditioning System in accordance with the FAA approved Peter Schiff Aero, Inc. Drawing List “PSA Model 830 CCA Air Conditioning System for Beechcraft Series 200 and 300 Aircraft” Document Number 8000, Revision F, dated July 22, 2014 or later FAA approved revision.

Limitations and Conditions: (Limitations and Conditions continued on page 3.)

Date of application : August 26, 2010

Date of issuance : June 5, 2015

(Signature) Manager, Cabin Safety, Mechanical and Environmental Systems Branch Los Angeles Aircraft Certification Office (Title)

Transfer the ownership of Supplemental Type Certificate Number

to (Name of transferee)

(Address of transferee) (Number and street)

(City, State, and ZIP Code)

from (Name of grantor) (Print or type)

(Address of grantor) (Number and street)

(City, State, and ZIP Code)

Signature of grantor (In ink):

U.S. GPO 1987-763-289

Number SA02442LA

Limitations and Conditions: (Continued)

The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. The approval of this modification applies to the above noted aircraft models and serial numbers listed in the Limitations and Conditions section only. A copy of this STC must be included in the permanent records of the modified aircraft. 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.

Peter Schiff Aero, Inc. Airplane Flight Manual Supplement “Beechcraft 200 and 300 Models Airplane Flight Manual Model 830 CCA Air Conditioning System” dated May 28, 2015 or later FAA approved revision and Peter Schiff Aero, Inc. Instructions for Continued Airworthiness document 9001a ICA, Revision “E”, dated February 20, 2015 or later FAA approved revision must be made available to the operator at the time of installation.

---END---

FAA Form 8110-2-1(10-69) Page 3 of 3

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 13

MakeModelData sheet
Beechcraft Corporation200A24CE
Beechcraft Corporation200CA24CE
Beechcraft Corporation200CTA24CE
Beechcraft Corporation200TA24CE
Beechcraft Corporation300A24CE
Beechcraft Corporation300LWA24CE
Beechcraft CorporationB200A24CE
Beechcraft CorporationB200CA24CE
Beechcraft CorporationB200CTA24CE
Beechcraft CorporationB200GTA24CE
Beechcraft CorporationB200TA24CE
Beechcraft CorporationB300A24CE
Beechcraft CorporationB300CA24CE