AD 85-04-02

Airworthiness directive · Fuel Boost Pump · Boeing 767-200 Series

Effective
March 28, 1985
Model
767-200 Series
Data sheet
TCDSA1NM
Registered aircraft
37 matched by model
Product
Aircraft · Large airplane
Amendment
39-5007

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.

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The airworthiness directive

85-04-02 BOEING: Amendment 39-5007. Applies to the Model 767-200 series airplanes certificated in all categories. Compliance is required as indicated unless previously accomplished. To prevent fuel boost pump seizures in flight, as a result of operation with cold fuel, accomplish the following:

A. Within 30 days after the effective date of this AD, install a cockpit placard which limits fuel tank temperature to -37 degrees C (-35 degrees F), in accordance with Boeing Service Bulletin 767-28-14 dated June 20, 1984, or later FAA approved revision.

B. Within one year after the effective date of this AD, replace at least one fuel boost pump in each main fuel tank and at least one fuel boost pump in each center auxiliary fuel tank (if activated) with an improved boost pump, in accordance with Boeing Service Bulletin 767-28-14 dated June 20, 1984, or later FAA approved revision.

C. Within two years after the effective date of this AD, replace all unimproved fuel boost pumps in each main tank and all unimproved fuel boost pumps in each center auxiliary tank (if activated) with improved fuel boost pumps, in accordance with Boeing Service Bulletin 767- 28-14 dated June 20, 1984, or later FAA approved revision.

D. The fuel temperature limitation and cockpit placard required by paragraph A., above, may be removed after at least one improved fuel boost pump is installed in each tank location required by paragraph B., above.

NOTE: The center auxiliary fuel tank boost pumps need not be replaced on airplanes with deactivated center auxiliary fuel tanks (i.e., those not able to be fueled); however, this deviation must be recorded in the permanent aircraft records. All center auxiliary fuel tank boost pumps must be replaced with the improved boost pumps identified in Boeing Service Bulletin 767-28-14 prior to activation of the center auxiliary fuel tank.

E. Alternate means of compliance which provide an equivalent level of safety may be used whenapproved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region.

F. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD.

This amendment becomes effective March 28, 1985.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 37

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Boeing37 aircraft
By year built
19822001
Registered aircraft by year built: 30 aircraft
19824
19837
19849
19854
19861
19871
19881
20013

7 with no year recorded

By model

Aircraft

See all 37 aircraft