67-30-05 MCDONNELL DOUGLAS: Amdt. 39-505 Part 39 Federal Register November 9, 1967. Applies to Model DC-9 Series Airplanes. \n\n\tCompliance required as indicated. \n\n\tDue to at least three reports of malfunctions in the battery charger installed in DC-9 airplanes that have resulted in smoke and fire in the electrical compartment, accomplish the following: \n\n\t1.\tWithin 10 hours' time in service after the effective date of this AD: \n\n\t\tA.\tInspect the battery charger, P/N 263-40061-01 and inspect and service each battery in the electrical compartment in accordance with Paragraphs 1, 2 and 3 of the "Inspection Procedures for Aircraft" section of a wire dated 10-19-67, constituting McDonnell Douglas DC-9 Alert Service Bulletin A-24-26, or by a method approved by the Chief, Aircraft Engineering Division, FAA, Western Region: \n\n\t\tB.\tDeactivate circuit breakers normally coded K7, K8, and K9, titled battery charger and transfer relay (20 AMP, left bus) and secure in the open position, or remove and stow wires P32A14C, P33A14B, and P34A-14A at the circuit breaker: \n\n\t\tC.\tPlacard circuit breakers K7, K8, and K9 to indicate that they are deactivated: \n\n\t\tD.\tUnless already accomplished in accordance with Paragraph 5 of the "Inspection Procedures for Aircraft" section of the Service Bulletin referenced in this Paragraph, place an operating limitation in the form of a placard in the vicinity of the APU start switch stating: "Operating Limitation, Do not start APU electrically inflight": and \n\n\t\tE.\tUnless already accomplished in accordance with Paragraph 5 of the "Inspection Procedures for Aircraft" section of the Service Bulletin referenced in this Paragraph, place an operating limitation in the form of a placard in the cockpit in clear view of the pilot and copilot, stating: "Operating Limitation, Do not ground start APU after battery charger circuit breakers are opened (pulled) prior to takeoff." \n\n\t2.\tIf an inspection specified in Paragraph 1 of this AD reveals evidence of overheating, cracking, or other abnormal appearance of the battery charger (including the flag lugs and positive ceramic stud build-up and solder-joint on the inside and outside of the charger on the filter, and the solder-joints to chassis), replace before further flight. \n\n\t3.\tThe following operating limitations are prescribed for all affected airplanes: \n\n\t\tA.\tImmediately prior to start of each taxi: \n\n\t\t\ti.\tDetermine that the battery charger is operating in the pulsing mode. \n\n\t\t\tii.\tPull circuit breakers U21, W21, and X24 in immediate succession to deactivate the batter charger. \n\n\t\t\tiii.\tEnter the electrical compartment and inspect the battery charger and adjacent vicinity to determine that the charger has been operating satisfactorily as evidence by a lack of smoke. (May be accomplished by ground personnel.) \n\n\t\tB.\tAfter parking close (push in) circuit breakers U21, W21, and X21 in immediate succession. \n\n\tNOTE No. 1: The APU may be started after landing and during taxi to the ramp. \n\n\tNOTE No. 2: The APU may be windmill started in flight in the event of a complete in-flight loss of electrical power. \n\n\tThe operating limitations specified in Subparagraphs A and B of this Paragraph must be placed in the aircraft in the form of a placard in clear view of the pilot. For the purpose of this AD, any document (including a pilot check list) including these limitations constitutes a "placard" within the meaning of this Paragraph. \n\n\t4.\tCompliance with Paragraphs 1 and 3 of this AD is no longer required, and the operating limitations prescribed in those Paragraphs may be removed upon: \n\n\t\tA.\tAccomplishing the modifications specified in the "Accomplishment Instructions" sections of McDonnell Douglas DC-9 Service Bulletin Nos. 24-25 dated December 1, 1967 (or later FAA-approved revision), 24-27 dated December 1, 1967 (or later FAA-approved revision), 25-97 dated November 10, 1967 (or later FAA-approved revision); and \n\n\t\tB.Removing FAA-approved revisions dated May 3, 1967, and incorporating FAA-approved revisions dated December 1, 1967, to the Emergency Procedures Section of the FAA-approved DC-9 Series 10 Airplane Flight Manual (Douglas Report DAC-32999) or the FAA-approved DC-9 Series 30 Airplane Flight Manual (Douglas Report DAC-33530), as appropriate, under the heading of "Electrical Smoke of Unknown Origin" Phase III. \n\n\tThis amendment effective December 19, 1967.