# STC ST00062SE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: B/E Aerospace Inc - FSI, United States
- Description: Installation of a lower lobe crew rest.
- Applied: March 12, 1992
- Status date: July 18, 2016
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 25, Part 121
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE)
- Certificate PDF: https://openairdocs.org/files/sha256/4d/e5/4de5c17e4771be567877d9f9bab6db381e737794ae2138890db5e8042f6a1458
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A55AF1498A94BF618625803D00679A39.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/ST00062SE

## ADs that name it (0)

None.

## Approved models (1)

- The Boeing Company MD-11 ([TCDS A22WE](https://openairdocs.org/tcds/A22WE))

## 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 (8/13) Page 1

Part of the Federal A viation Regulations.

Original Product – Type Certificate Number: MDNH:

MRGHO:

Signature

Title

ST00062SE B/E Aerospace, Inc. - FSI 11404 Commando Road W, Suite C Everett, WA 98204 25 A22WE McDonnell Douglas MD-11 Installation of a Lower Lobe Crew Rest in accordance with Flight Structures, Inc. Master Drawing List 91FS092-D01, revision D, dated February 3, 1994 or later FAA approved revision.

The approval of this change in type design applies to the above model aircraft only and only to those airplanes listed on the continuation sheet. 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 of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft.

(See Continuation Sheets Pages 3 through 3) 3/12/1992 3/1/1994 7/18/2016 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):

ST00062SE

FAA Form 8110-2 (8/13) Page 3

ST00062SE Limitations and Conditions, Continued:

All of the crew rest smoke detectors, the associated Engine Alert Display and System Display messages, aural alarms, and visual alarms must be tested once per day. The crew rest must be locked and placarded inoperative if any of the detectors or annunciators do not pass the test. 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 91FS092-D01 must be maintained as part of the permanent records for the modified aircraft. The airplane must be operated in accordance with Flight Structures, Inc. FAA approved Airplane Flight Manual Supplement for McDonnell Douglas MD-11 airplanes, McDonnell Douglas Document MDC-K0031.

Applicable serial numbers for the McDonnell Douglas MD-11 airplanes are as follows:

48555, 48556, 48557, 48558, 48559, 48560, 48561, 48562, 48563, 48564

Certification Basis:

The certification basis for this modification is in accordance with Type Certificate Data Sheet, A22WE.

- END -

## Every issue (2)

- July 18, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/4d/e5/4de5c17e4771be567877d9f9bab6db381e737794ae2138890db5e8042f6a1458)
- March 1, 1994: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/c8/db/c8dbf99caef22f3716c839f8980959e2dbb15e5b12368ee3e585a2d7bd39c165)

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