What it approves
Relocation of factory installed GPU outlet from the left main landing gear wheel well to the forward left nose in front of the left avionics bay door.
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 Textron Aviation Inc.
One Cessna Boulevard Wichita, KS 67215 2 SA00597WI Federal Aviation Regulations.
23 Relocation of factory installed GPU outlet from the left main landing gear wheel well to the forward left nose in front of the left avionics bay door. Data Required:
1. Raytheon Aircraft Services Master Drawing List No. CMA-136001, Revision (--), dated August 5, 1997, or later FAA approved revision.
Compatibility of this design change with previously approved modifications must be determined by the installer. 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.
Beech 1900D May 29, 2007; December 14, 2016 May 23, 1997 November 5, 1997 A24CE 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)
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Hawker Beechcraft Corporation | 1900D | A24CE |
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| December 14, 2016 | Reissued, current | Certificate |
| May 29, 2007 | Reissued, earlier issue | Certificate |