- Effective
- July 31, 1990
- Models
- 727-100 Series, 727-100C Series, 727-200 Series, 727-200F Series, 727 Series, 727C Series and 13 more
- Registered aircraft
- 1,118 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-6683
- Docket
- 90-NM-86-AD
Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
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On this page
The airworthiness directive
90-12-11 R1 BOEING: Amendment 39-6626 as revised by Amendment 39-6683. Docket No. 90-NM-86-AD.
Applicability: Model 727, 737, and 757 series airplanes, equipped with escape slide release cables, certificated in any category.
Compliance: Required as indicated, unless previously accomplished.
To ensure proper escape slide release from the escape slide compartment, accomplish the following:
A. Within 45 days after the effective date of this AD, unless previously inspected within the last three months, perform a visual inspection of each escape slide release cable, if installed. Replace frayed (one or more broken strands) or broken cables prior to further flight.
B. Repeat the inspection for frayed or broken release cables required by paragraph A. of this AD, at intervals not to exceed 12 months.
C. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region.
NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either concur or comment, and then send it to the Manager, Seattle Aircraft Certification Office.
D. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD.
This AD revises AD 90-12-11, Amendment 39-6626.
The effective date for the requirements of this amendment remains June 25, 1990, as specified in Amendment 39-6626, AD 90-12-11. This amendment (39-6683, AD 90-12-11 R1) is effective on July 31, 1990.
Affected TCDS · 3
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 1,118
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1969 | 1 |
|---|---|
| 1971 | 1 |
| 1973 | 1 |
| 1975 | 3 |
| 1976 | 3 |
| 1977 | 2 |
| 1978 | 2 |
| 1979 | 2 |
| 1981 | 6 |
| 1982 | 4 |
| 1983 | 1 |
| 1985 | 2 |
| 1986 | 9 |
| 1987 | 5 |
| 1988 | 2 |
| 1989 | 9 |
| 1990 | 19 |
| 1991 | 27 |
| 1992 | 25 |
| 1993 | 21 |
| 1994 | 20 |
| 1995 | 10 |
| 1996 | 16 |
| 1997 | 17 |
| 1998 | 60 |
| 1999 | 105 |
| 2000 | 89 |
| 2001 | 90 |
| 2002 | 23 |
| 2003 | 16 |
| 2004 | 18 |
| 2005 | 14 |
| 2006 | 21 |
| 2007 | 21 |
| 2008 | 26 |
| 2009 | 38 |
| 2010 | 62 |
| 2011 | 21 |
| 2012 | 30 |
| 2013 | 31 |
| 2014 | 23 |
| 2015 | 20 |
| 2016 | 42 |
| 2017 | 72 |
| 2018 | 27 |
| 2025 | 2 |
59 with no year recorded