Airworthiness Directive · Amendment 39-15415 · Boeing Model 737-600, -700, -700C, -800 and -900 Series Airplanes; and Model 757-200, -200PF, -200CB, and -300 Series Airplanes
Boeing Model 737-600, -700, -700C, -800 and -900 Series Airplanes; and Model 757-200, -200PF, -200CB, and -300 Series Airplanes
This AD applies to Boeing Model 737-600, -700, -700C, -800 and -900 series airplanes; and Boeing Model 757-200, -200PF, -200CB, and -300 series airplanes; certificated in any category; as identified in Boeing Alert Service Bulletins 737-28A1207, dated February 15, 2007, and 757-28A0088, dated January 25, 2007.
Note 1: This AD requires revisions to certain operator maintenance documents to include new inspections and maintenance actions. Compliance with these limitations is required by 14 CFR 43.16 and 91.403(c). For airplanes that have been previously modified, altered, or repaired in the areas addressed by these limitations, the operator may not be able to accomplish the actions described in the revisions. In this situation, to comply with 14 CFR 43.16 and 91.403(c), the operator must request approval for revision to the airworthiness limitations (AWLs) in the Boeing 737-600/700/700C/700IGW/800/900 Maintenance Planning Data (MPD) Document D626A001-CMR and the Boeing 757 MPD Document D622N001-9, as applicable, according to paragraph (i) of this AD.
The FAA is adopting a new airworthiness directive (AD) for certain Boeing airplanes, identified above. This AD requires inspecting to determine if certain motor-operated shutoff valve actuators for the fuel tanks are installed, and related investigative and corrective actions if necessary. This AD also requires revising the Airworthiness Limitations (AWLs) section of the Instructions for Continued Airworthiness to incorporate AWL No. 28-AWL-21, No. 28-AWL-22, and No. 28-AWL-24 (for Model 737-600, -700, -700C, -800 and -900 series airplanes); and No. 28-AWL-23, No. 28-AWL-24, and No. 28-AWL-25 (for Model 757-200, -200PF, -200CB, and -300 series airplanes). This AD results from a design review of the fuel tank systems. We are issuing this AD to prevent electrical energy from lightning, hot shorts, or fault current from entering the fuel tank through the actuator shaft, which could result in fuel tank explosions and consequent loss of the airplane.
You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done.
The term “service bulletin,” as used in this AD, means the Accomplishment Instructions of the following service bulletins, as applicable:
(1) For Model 737-600, -700, -700C, -800 and -900 series airplanes: Boeing Alert Service Bulletin 737-28A1207, dated February 15, 2007; and
(2) For Model 757-200, -200PF, -200CB, and -300 series airplanes: Boeing Alert Service Bulletin 757-28A0088, dated January 25, 2007.
Within 60 months after the effective date of this AD: Inspect the applicable motor-operated valves (MOVs) to determine whether an MOV with the affected part number identified in the Accomplishment Instructions of the applicable service bulletin is installed. A review of airplane maintenance records is acceptable in lieu of this inspection if the part number of the part can be conclusively determined from that review. Do all applicable related investigative and corrective actions before further flight. Do all actions in accordance with the Accomplishment Instructions of the applicable service bulletin.
Concurrently with the actions specified in paragraph (g) of this AD: Revise the AWLs section of the Instructions for Continued Airworthiness by incorporating the information specified in paragraphs (h)(1) and (h)(2) of this AD, as applicable. Accomplishing the revision in accordance with a later revision of the MPD document is an acceptable method of compliance if the revision is approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA.
(1) Section F., “AIRWORTHINESS LIMITATIONS—FUEL SYSTEM AWLs,” of Boeing 737-600/700/700C/700IGW/800/900 MPD Document D626A001-CMR, Section 9, Revision November 2006 R1, into the MPD to incorporate AWL No. 28-AWL-21, No. 28-AWL-22, and No. 28-AWL-24.
(2) Section G., “AIRWORTHINESS LIMITATIONS—FUEL SYSTEM AWLs,” of Boeing 757 MPD Document D622N001, Section 9, Revision January 2007, into the MPD Document to incorporate AWL No. 28-AWL-23, No. 28-AWL-24, and No. 28-AWL-25.
The aircraft, engines and makers this AD names, by the model designations in its text. A model listed here may still be outside the AD's serial ranges.
Aircraft
