STC SA2133NM

Supplemental type certificate · Raisbeck Engineering Inc.

Holder
Raisbeck Engineering Inc. · United States
Status
Current · Reissued
Status date
September 1, 2023
Applied
April 6, 1983
Product
Aircraft · Large Airplane
Data sheet
TCDS3A20

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of fully enclosed main landing gear doors

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 (11/20) SUPERSEDES PREVIOUS EDITION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

Page 1 of 2 SA2133NM Raisbeck Engineering Inc.

2811 South 102nd Street , Suite 100 Tukwila, WA 98168 Part 3 the Civil Air Regulations.

3A20 Beech 65-A90, 65-A90, B90, C90, E90 Installation of Fully Enclosed Main Landing Gear Doors in accordance with FAA sealed copies of Raisbeck Engineering Installation Instructions No. 83-1005, Revision B, dated August 1, 1983, and Sheets 1 through 4 of Raisbeck Engineering Installation Drawing No. 83-1701, Revision B, A, and NC, respectively, dated July 30, 1983, July 14, 1983, June 23, 1983, and July 14, 1983, respectively, or later FAA approved revision, and Fabrication of the Fully Enclosed Main Landing Gear Doors in accordance with an FAA sealed copy of Raisbeck Engineering Drawing List No. 83-1004, Revision B, dated August 1, 1983, or later FAA approved revision.

April 6, 1983 September 1, 2023 August 2, 1983 for Manager, West Certification Branch See TC Data Sheet 3A20 for additional requirements) Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate must be maintained as part of the permanent of records for 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.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

Page 2 of 2 SA2133NM

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 · 5

MakeModelData sheet
Hawker Beechcraft Corporation65-903A20
Hawker Beechcraft Corporation65-A903A20
Hawker Beechcraft CorporationB903A20
Hawker Beechcraft CorporationC903A20
Hawker Beechcraft CorporationE903A20

Every issue · 2

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
September 1, 2023Reissued, currentCertificate
August 2, 1983Issued, earlier issueCertificate