What it approves
Installation of a door 5 overhead crew rest.
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 (8/13) Page 1
Part of the Federal A viation Regulations.
Original Product – Type Certificate Number: MDNH:
MRGHO:
Signature
Title
SA5957NM B/E Aerospace, Inc. - FSI 11404 Commando Road W, Suite C Everett, WA 98204 25 A20WE Boeing 747-200 Installation of a Door 5 Overhead Crew Rest in accordance with Flight Structures, Inc. Master Drawing List 92FS108-D01, Revision L, dated July 11, 1997, or later FAA approved revisions.
Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that 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.
(See Continuation Sheets Pages 3 through 3) 3/24/1993 5/13/1993 4/21/2016 12/18/1997 Lead Administrator ODA-635712-NM
FAA Form 8110-2 (8/13) Page 2
To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):
SA5957NM
FAA Form 8110-2 (8/13) Page 3
SA5957NM Limitations and Conditions, Continued:
This crew rest installation has not been evaluated for compliance with FAR 25.831(a); nor has it been found to be in compliance with the intent of FAR 121.485(a). A copy of this certificate and Flight Structures, Inc. Master Drawing List 92FS108-D01 must be maintained as part of the permanent records for the modified aircraft. The aircraft must be operated in accordance with the Flight Structures, Inc. FAA approved Airplane Flight Manual Supplement for Boeing 747-200, Boeing Document D6-13703.
The smoke detection system must be checked prior to the dispatch of the aircraft in accordance with Flight Structures documents 92FS108-D86 or 96FS642-D86 as applicable, Smoke Detection System - Continued Airworthiness Door 5 Crew Rest Area B747-200.
Certification Basis:
The certification basis for this modification is in accordance with Type Certificate Data Sheet, A20WE.
- END -
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 |
|---|---|---|
| The Boeing Company | 747-200 Series | A20WE |
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| April 21, 2016 | Reissued, current | Certificate |
| December 18, 1997 | Amended, earlier issue | Certificate |