AIRWORTHINESS DIRECTIVE
CAA-AD-041/2001
Date of issue:
May 10, 2001
AIRCRAFT - CENTER FUEL TANK - INSPECTION
Applicability: All Model 737 series
airplanes, certificated in any category.
Effective date: May 10, 2001
Compliance: Required as indicated in FAA AD 2001-08-24.
Remarks: The compliance of
this AD must be recorded in Aircraft Logbook, where applicable the requirements
of this AD must be integrated into Aircraft Technical Documentation. Address
inquiries concerning this AD to: Civil Aviation Authority, Airworthiness
Division, Ruzyne Airport, 160 08 Prague 6, Czech Republic, tel: 420 2 33320922,
fax: 420 2 20562270.
Ing. Pavel MATOUŠEK
Director of
Airworthiness Division
CAA CZ
2001-08-24
BOEING:
Amendment 39-12201. Docket 2001-NM-94-AD.
Applicability: All
Model 737 series airplanes, certificated in any category.
Compliance:
Required as indicated, unless accomplished previously.
To prevent ignition
of fuel vapors due to the generation of sparks and a potential ignition source
inside the center tank caused by metal-to-metal contact during dry fuel pump
operation, which could result in a fire or explosion of the fuel tank,
accomplish the following:
Revision of
Airplane Flight Manual (AFM)
(a) Within 7 days
after the effective date of this AD, revise the Limitations Section of the
FAA-approved AFM to include the following information. This may be accomplished
by inserting a copy of this AD into the AFM.
"For ground
operation, center tank fuel pump switches must not be positioned to
"ON" unless the center tank fuel quantity exceeds 1,000 pounds (453
kilograms), except when defueling or transferring fuel.
Center tank fuel
pump switches must be positioned to "OFF" when both center tank fuel
pump low pressure lights illuminate.
Center tank fuel
pumps must not be "ON" unless personnel are available in the flight
deck to monitor low pressure lights."
Alternative
Methods of Compliance
(b) An alternative
method of compliance or adjustment of the compliance time that provides an
acceptable level of safety may be used if approved by the Manager, Seattle
Aircraft Certification Office (ACO), FAA. Operators shall submit their requests
through an appropriate FAA Principal Operations Inspector, who may add comments
and then send it to the Manager, Seattle ACO.
Note 1: Information
concerning the existence of approved alternative methods of compliance with
this AD, if any, may be obtained from the Seattle ACO.
Special Flight
Permits
(c) Special flight
permits may be issued in accordance with sections 21.197 and 21.199 of the
Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane
to a location where the requirements of this AD can be accomplished.
Effective Date
(d) This amendment
becomes effective on May 10, 2001.
FOR FURTHER
INFORMATION CONTACT: Sherry Vevea, Aerospace Engineer, Propulsion Branch,
ANM-140S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW.,
Renton, Washington 98055-4056; telephone (425) 227-1360; fax
(425) 227-1181.
Issued in Renton,
Washington, on April 18, 2001.
Donald L. Riggin,
Acting Manager, Transport Airplane Directorate, Aircraft Certification Service