- Effective
- August 16, 1978
- Models
- 737-100 Series, 737-200 Series, 737-200C Series
- Data sheet
- TCDSA16WE
- Registered aircraft
- 10 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-3267
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.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| FAA DRS HTML | 24 KB | b2abb5f5…4335527 | FAA DRS (API key needed) |
On this page
The airworthiness directive
78-04-02 BOEING: Amendment 39-3140 as amended by Amendment 39-3267. Applies to all Boeing Model 737-100/200/200C/T43A series airplanes, listed in Boeing Service Bulletin No. 737-53-1048 which have not had the bolt replacement accomplished per figure 1 of that service bulletin, certificated in all categories. A. Within the next 75 flight hours time-in-service after January 16, 1978, unless accomplished within the last 3,000 flight hours time-in-service, accomplish paragraph B below. B. Remove panels 9126 L.H. and 9226 R.H. and check all attach bolts (16 per side) of the two horizontal stabilizer hinge outboard fittings for looseness. If found loose, before further flight, tighten bolt(s) to 65-80 in.-lbs. or accomplish the bolt replacement of figure 1 of Boeing Service Bulletin No. 737-53-1048, or later FAA approved revisions, or equivalent approved by the Chief, Engineering and Manufacturing Branch, FAA Northwest Region. In the event it is impracticable to perform the inspection within 75 flight hours time-in-service after January 16, 1978, permission to ferry an airplane to a location where the inspection can be accomplished, may be obtained by contacting the Chief, Engineering and Manufacturing Branch, FAA Northwest Region. C. Within the next 3,000 flight hours time-in-service after the inspection accomplished per paragraph A of this AD, and thereafter at intervals not to exceed 3,000 flight hours time-in- service, accomplish the inspection of paragraph B. D. Terminating action to this AD consists of replacement of the attach bolts of the horizontal stabilizer hinge outboard fittings in accordance with Figure 1 of Boeing Service Bulletin No. 737-53-1048, or later FAA approved revisions, or in a manner approved by the Chief, Engineering and Manufacturing Branch, FAA Northwest Region. The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1). All persons affected by this directive who have not already received these documents from the manufacturer, may obtain copies upon request to Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124. These documents may also be examined at FAA, Northwest Region, 9010 East Marginal Way South, Seattle, Washington 98108. Amendment 39-3140 became effective February 14, 1978. This amendment 39-3267 becomes effective August 16, 1978.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 10
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1969 | 1 |
|---|---|
| 1975 | 1 |
| 1979 | 1 |
| 1981 | 1 |
| 1986 | 1 |
| 1987 | 1 |
4 with no year recorded