Pratt & Whitney JT9D-7R4D

Service difficulty reports · 1,031

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Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE engine_model_key = 'JT9D7R4D'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR XV6A2014072700004Engine · fluctuatesAFTER LEVELING AT CRUISE ALTITUDE, LT ENGINE WOULD FLUCTUATE RAPIDLY. WITH NT TURNED OFF FOLLOWING WAS OBSI EPR 1.3 - 1.4, N1 80% TO 90%, N2 84% TO 93%, FUEL FLOW 4.6 TO 6.4 & 37,000 FT PRESS ALT. AT 3,000 FT LEVEL FLIGHT 250KTS N1 ON BOTH ENGS AT 61% LT ENGJul 27, 2014 · N769VA · Boeing 767222 · Powerplant SystemSDR XV6A2015071500001Engine · failedLEFT ENGINE COMPRESSOR STALLED DURING CLIMB OUT AT APPROXIMATELY 23000 FEET. EGT EXCEEDENCE 627 DEGREES. ENGINE FAILED ON APPROACH. PERFORMED OVERTEMP INSPECTION, ENGINE FAILED BORESCOPE AND VISUAL INSPECTIONS. METAL FOUND IN TAILPIPE, ALONG WITH MOLTEN METJul 15, 2014 · N769VA · Boeing 767222 · Engine (Turbine/Turboprop)SDR 2DYA20140708001Engine · power lossWE ENCOUNTERED AN AREA OF HI CLOUDS AS WE ENTERED THE AREA LIGHT TURBULENCE WAS ENCOUNTERED & A NOTED TEMP OF -51 SAT. LIGHT MOISTURE WAS OBSERVED & THE ENG ANTI-ICE WAS SELECTED ON. LIGHT ICING WAS OBSERVED INCREASING FROM MODERATE TO HEAVY & A TEMP OF -41 Jul 4, 2014 · N770JM · Boeing 767233 · Engine (Turbine/Turboprop)SDR UIEA2012080700347Target · out of adjustLEADING EDGE SLAT ASYMETRY WARNING, AFTER TAKEOFF. BITE CHECK PSEU, FOUND OTBD SLAT PROXIMITY SWITCH OUT OF LIMITS. ADJUSTED NR 4 OTBD TARGET, IAW AMM 27-88-00/201. RESET FSDU. CYCLED FLAPS OPS CHECKS GOOD.Aug 7, 2012 · N653GT · Boeing 767231 · Leading Edge Slat Position Indicating SystemSDR ABXR2012043000045Fitting · gougedDURING C-CHECK FOUND RT WING RIB 8 BACKUP FITTING HAS TOOLING MARKS AT WS 375. REPAIRED IAW WITH REA B657-59769-MR.Apr 30, 2012 · N713AX · Boeing 767205 · Wing Miscellaneous StructureSDR CTASRD2011001Sleeve · deformedRIGHT ENGINE NR 2 INBOARD THRUST REVERSER SLEEVE HALF IS DEFORMED DUE TO RUBBING WITH THE THRUST REVERSER BLOCKER DOORS IN FOUR PLACES. DEFORMATION RANGES FROM ONE INCH, TO .375 OF AN INCH.Jan 4, 2011 · N606TW · Boeing 767231 · Engine Thrust ReverserSDR PI22010F00000Slide · partial deployCREW MEMBER DISCOVERED A DISLODGED ACTUATION CABLE ON THE AFT LT ENTRY DOOR SLIDE ASSY WHICH HAD DISENGAGED THE ENTIRE FWD SIDE OF THE SLIDE PACK BOARD ASSY. FURTHER INVESTIGATION WHILE MX WAS SAFING THE PRESSURE CYLINDER REVEALED THE CYLINDER ACTUATION MECHANov 24, 2010 · N606TW · Boeing 767231 · Escape SlideSDR ABXR2010111900053Floor Support · cracked(ABXR) DURING C-CHECK FOUND COCKPIT FLOOR SUPPORT BEAM CRACKED AT STA 246, LBL 25. R & R ANGLE IAW SRM.Nov 19, 2010 · N768VA · Boeing 767222 · Fuselage Miscellaneous StructureSDR ABXR2010111900054Skin · cracked(ABXR) SKIN CRACKED AT STA 1645, STRINGER 7L. REPAIRED SKIN IAW SRM.Nov 19, 2010 · N768VA · Boeing 767222 · Fuselage Main, Plate/SkinSDR 2PSASDR7671010O-Ring · failedDURING CRUISE FLIGHT, AT APPROX 3:22 AFTER TAKEOFF, OBSERVED NR2 ENGINE OIL QTY STARTED TO SHOW A POSSIBLE LOSS OF OIL AT A RATE OF 1 QT EVERY 3 MINUTES. WHEN QTY REACHED 3 QTS, ENGINE BROUGHT BACK TO IDLE & SHUTDOWN INITIATED. ACFT LANDED WITH A TOTAL FLIGHOct 10, 2010 · N673BF · Boeing 767238 · Turbine Engine Oil SystemSDR FDEA201006212463Skin · gougedLT WING - DETECTED NICK AT HOLE NR 63 -EO 6-5710-7-3322PT1. HOLE NR 63 REPAIRED IAW EA 6-5710-141544.Jun 21, 2010 · N447FE · Airbus A310222 · Wing, Plate/SkinSDR TIPR200900013Slide · malfunctionedLT OFF-WING ESCAPE SLIDE FAILED, OPS CHECK FAILED TO DELPOY INITIALLY.Jul 2, 2009 · N768VA · Boeing 767222 · Escape SlideSDR TIPR200900009Stringer · corrodedSTRINGER 38 RT CORRODED AND CRACKED AT STA 1580 (LAV SERVICE PAN CUT OUT AREA). REMOVED AND REPLACED CORRODED SECTION OF STRINGER IAW SRM 53-00-03,51-20-01 AND 53-00-03.Jun 19, 2009 · N767VA · Boeing 767222 · Fuselage Main, Longeron/StringerSDR 7A7B20091192Slide · unwanted deployUNCOMANDED DEPLOYMENT OF OFF WING EVACUATION SLIDE.Jan 18, 2009 · N673BF · Boeing 767238 · Escape SlideSDR 2009F00015Wire · misinstalledWHILE ACFT WAS ON GROUND, WITH JUST APU RUNNING, THE LT OVERWING SLIDE DEPLOYED. THE ESCAPE HATCH WAS NOT DISTURBED. THIS TOOK PLACE IN LFPB. THE ONLY THING DONE PRIOR TO DEPLOYMENT WAS THAT THE LEAD F/A PUSHED THE EMERGENCY LIGHTING TEST SWITCH AT THE L1 CONTJan 17, 2009 · N673BF · Boeing 767238 · Equipment/Furnishings WiringSDR 2008FA0000850Pin · installedA SLIDE DEPLOYMENT OF THE RT AFT ENTRY DOOR OF THE ACFT WAS ATTEMPTED IN CONJUNCTION WITH A DITCHING DEMONSTRATION IN SUPPORT OF OUR FAR PART 125 CONFORMITY ASSESSMENT BY FSDO - 25. THE SLIDE DID NOT EXTRACT FROM THE DOOR BUSTLE AS THE DOOR WAS OPENED. UPON Oct 24, 2008 · N673BF · Boeing 767238 · Escape SlideSDR ERKR200800311Skin · corrodedECRA 606TW-53-767-001 REPAIR OF CORROSION DAMAGE AT STA 285 STR 36L: TRIMMED OUT CORROSION DAMAGED AREA AND PERFORMED A HFEC SKIN AND OPEN HOLE INSPECTION REPAIR FILLERS, DOUBLER AND TRIPLER PER THIS ENGINEERING CHANGE/REPAIR AUTHORIZATION ( ECRA ). APPROVAL SMay 26, 2008 · N606TW · Boeing 767231 · Fuselage Main, Plate/SkinSDR L43A102207001Fseu · faultedAFTER TAKEOFF WHEN MLG SELECTED UP & MLG DOOR LIGHTS EXTINGUISHED A "GEAR NOT DOWN" EICAS MESSAGE DISPLAYED. AS FLAPS SELECTED FROM 5 TO 1 DEGREE A "T/E FLAP DISAGREE" MESSAGE DISPLAYED. ALTERNATE T/E SWITCH CYCLED & AS FLAPS WENT TO 1 DEGREE "T/E FLAP DISAOct 18, 2007 · N260MY · Boeing 767205 · Trailing Edge Flap Control SystemSDR CA070514031Transformer · open(CAN) DURING CRUISE, THE LT AC BUS FAILED WITH THE LOSS OF ASSOCIATED SYSTEMS. THE CONCERN WAS BEING ABLE TO START THE APU. FLIGHT DECLARED A PAN-PAN WITH ATC AND BEGAN DIVERSION. AT FL 350, 2 APU START ATTEMPTS, BUT START WAS ACHIEVED ONLY AT FL150. IAW CMay 12, 2007 · Boeing 767233 · AC Generation SystemSDR 07FDEA00604Lock · unknownDURING LANDING AT KBUR, THRUST REVERSER LEVERS EXTREMELY STIFF, F/O LOWERED REVERSER OR ATTEMPTED TO STOW AND LEVERS WERE SO STIFF COULD NOT STOW REVERSERS. ALL BETWEEN 80-60 KTS, AT ABOUT 65 KTS CAPT COMMANDED F/O TO MOVE HAND FROM THROTTLE AND POUNDED ANDFeb 27, 2007 · N450FE · Airbus A310 · Engine Thrust ReverserSDR ABXA070019Blade · damagedON TAKEOFF FROM ILN, DURING LANDING GEAR RETRACTION, GOT SUBSTANTIAL IMPACT SOUND FROM LEFT ENGINE AREA, AND BURNING SMELL AFTER SOUND. NO ENGINE ABNORMALITIES OR EXCEEDANCES. LANDED UNDER WEIGHT. C/W BIRD STRIKE INSPECTION BORESCOPE & BLADE REPLACEMENT ON Jan 24, 2007 · N708AX · Boeing 767231 · Turbine Engine Compressor SectionSDR CA061010004Skin · delaminated(CAN) LT HORIZONTAL STAB LEADING EDGE PANEL 332CL INNER SKIN COMPLETELY DELAMINATED. DELAMINATED SKIN WEARING INTO VERTICAL STIFFENERS LOCATED ALONG FRONT SPAR. (TC NR 20061010004)Sep 27, 2006 · Boeing 767233 · Horizontal Stabilizer, Plate/SkinSDR CA060816001Oil System · low pressure(CAN) ENGINE INFLIGHT SHUTDOWN DO TO OIL PRESSURE AND QUANTITY LOSS, ENROUTE, DIVERTED, SUSPECT NR 4 BEARING. (TC NR 20060816001)Aug 15, 2006 · Boeing 767233 · Turbine Engine Oil SystemSDR ABXA060158Engine · surgesRIGHT ENGINE SURGE AT CONSTANT THRUST. ENGINE WAS SHUTDOWN DUE TO UNRECOVERABLE SURGE. COMPLIED WITH/W NR 2 ENGINE INSPECTION IAW FIM 71-05-00. BOROSCOPED NR 2 ENGINE. NO DEFECTS FOUND. TURNED VSV SCHEDULE RATE SCREW ON TURN CLOCKWISE. OPS CHECK GOOD ON GROApr 3, 2006 · N702AX · Boeing 767231 · Engine (Turbine/Turboprop)SDR CA060228004Pseu · malfunctionedSELECTING LANDING GEAR DOWN, STATUS MSG 'LDG GEAR MONITOR' CAME ON AND REMAINED ON, DURING LANDING, TAXI, AND PARKING. PSEU CARD FAILED ILLUM. PSEU REPLACED PER AMM 32-09-04 PB 401. PSEU BITE TEST OKAY. MESSAGES CLEARED. OKAY TO PROCEED.Feb 26, 2006 · Boeing 767233 · Landing Gear Retraction/Extension SystemSDR 05FDEA04016Regulator · malfunctionedNR 2 ENGINE INDICATED HIGH OIL PRESSURE, THEN FOLLOWED QRH & MONITORED PARAMETERS. OIL PRESS. WENT TO 20-32 PSI (LOW) FOLLOWED QRH AND SHUTDOWN ENGINE. DECLARED EMERGENCY AND LANDED RWY 32L. HIGH OIL PRESS. WAS 100, LOW OIL PRESS. WAS 22. PRESSURE VARIED Nov 29, 2005 · N454FE · Airbus A310 · Engine Oil QuantitySDR CA050713004Actuator · malfunctioned(CAN) DURING CRUISE FWD CARGO DOOR LIGHT CAME ON. QRH FOLLOWED WITH A DESCENT AND DIVERSON TO YHZ. NO FLUCTUATION IN PRESSURIZATION. NO BUFFET. FWD CARGO LATCH/HOOK ACTUATOR REPLACED AS PER AMM52-33-0.Jul 13, 2005 · Boeing 767209 · Cargo/Baggage DoorsSDR CA050706004Window · arcedBURNING SMELL DETECTED IN COCKPIT. ACFT DIVERTED. OVERWEIGHT LANDING BY 10,600 KL AND SMOOTH LANDING. FOUND CAUSE OF BURNING SMELL AT GROUND CONN OF RT NR 3 WINDOW. DE-ACT RT NR 3 AS PROCEDURES C/B P36-H7 PULLED AND COLLARED NR3 RT WINDOW HEAT INOP.Jul 6, 2005 · Boeing 767209 · Flight Compartment WindowsSDR CA050614002Control Lever · failed(CAN) FAULT: EICAS MESSAGE (LDG GEAR MONITOR) LANDING GEAR IND 3 GREEN. ALSO RECEIVED A GRN PROX (TOO LOW GEAR) RECYCLED THE GEAR. LANDED WITH NORMAL INDICATIONS. REPLACED LDG GEAR CONTROL LEVER MODULE IAW AMM 32-31-01 PG 1-5. AND CABLE TENTION ADJUSTED IAW Jun 14, 2005 · Boeing 767209 · Landing Gear SelectorSDR CA050413001Duct · ruptured(CAN) FAULT: AFTER TAKEOFF, LEFT ENGINE DUCT LEAK TEMPERATURE CONTINUED TO CLIMB IN ALL CABIN. RETURNED TO CANCUN. FOUND DUCT ASSY 213T2109-5 RUPTURED. DUCT ASSY CHANGED, OPERATION CHECK CARRIED OUT, FOUND OK CONS SERVICEABLE AS PER AMM 36-11-01.Apr 13, 2005 · Boeing 767233 · Air Distribution SystemSDR CA050224003Sensor · broken(CAN) ON TOUCHDOWN, MASTER WARNING CONFIG LIGHT GEAR NOT DOWN CAUTION, LT SIDE BRACE LIGHT AND LT GEAR GREEN LIGHT EXTINGUISHED. AIRCRAFT STOPPED, GEAR PINS INSTALLED AND TAXIED IN. FOUND TOP OF SENSOR S258 SHEARED OFF. REPLACED SENSOR. S258 AND S236 ADJUSTEFeb 24, 2005 · Boeing 767233 · Landing Gear Position and WarningSDR CA050215002Ballscrew · corroded(CAN) INSP OF HORIZONTAL STABILIZER SCREWJACK DURING M01 CHECK REVEALED EVIDENCE OF INTERNAL CORROSION AS A RESULT OF DISCOLORATION IN LUBRICANT. TEARDOWN AND SHOP ANALYSIS REQUESTED WITH RESULTS TO BE FORWARDED TO AWC/YUL. NOTE: SDR ISSUED AGAINST (GDSP) REFFeb 15, 2005 · Boeing 767233 · Stabilizer ActuatorSDR CA050214006Ballscrew · corroded(CAN) FAULT: WHILE CARRYING OUT AN INSPECTION. FOUND RUSTY COLORED LUBRICANT AND REDDISH STAINING ON THE STAB. JACKSCREW GIMBAL. A PURGING OF THE LUBRICANT FROM THE GIMBAL ASSY WAS CARRIED OUT. THE RUST COLORING WAS CONFIRMED TO BE DUE TO IRON IN THE GREASFeb 14, 2005 · Boeing 767233 · Stabilizer ActuatorSDR CA041229001Ring Gear · corroded(CAN) RING WAS FOUND CORRODED AND GEAR BEARING SURFACES WERE PITTED. NR 6 FLAP ACTUATOR HAD CORROSION EMITTING FROM AFT SIDE OF MOUNT FLANGE. REMOVED ACTUATOR AND INVESTIGATED SOURCE. FOUND RING GEAR CORRODED. REACTION RING INSTALLED AND ACTUATOR REINSTALLEDDec 29, 2004 · Boeing 767233 · Trailing Edge Flap ActuatorSDR CA041129005Shaft · sheared(CAN) IMMEDIATELY AFTER 500FT, R PRIM PUMP EICAS MSG, STATUS QTY/PX NML. CLIMBING OUT, R QTY DECREASED STEADILY TO ZERO BUT PX NML W/DEMAND PUMP IN AUTO. CKD DEMAND PUMP OFF AND SYS PX WRNG LT DEMAND PUMP AUTO AND RETURNED TO DEPARTURE. FOUND RT EDP LEAKING Nov 29, 2004 · Boeing 767233 · Engine Fuel PumpSDR CA041129009Engine · surges(CAN) LOUD BANG AND YAW FELT AT CLIMB THRUST 7000 FT , RETURNED. ADDED MAINTENANCE INFO, LT ENG SURGE DET. MSG91827. LANDING SMOOTH. 91827.(SIC) ACTION: DFDR CHANGED. REPLACED EVBC IAW MM-75-31-01. ENG. BOROSCOPE CARRIED OUT. NO FAULTS. ENG. TEST 8, 9 AND 1Nov 29, 2004 · Boeing 767233 · Engine (Turbine/Turboprop)SDR CA041006006Actuator · corroded(CAN) INSPECTION OF HORIZONTAL STABILIZER SCREWJACK DURING M01CHECK REVEALED EVIDENCE OF INTERNAL CORROSION AS A RESULT OF DISCOLORATION IN LUBRICANT.Oct 5, 2004 · Boeing 767233 · Stabilizer ActuatorSDR ABXA040317Lamp · inoperativeLT MAIN GEAR DOWN (GREEN) INDICATION LIGHT INOPERATIVE. LIGHT INOPERATIVE WITH TEST BUTTON PUSHED. CREW PERFORMED A GO AROUND AT EWR. RELAMPED LT MAIN GEAR DOWN GREEN INDICATOR LIGHT AND RT MAIN GEAR DOWN GREEN INDICATOR LIGHT. OPS CHECKED OK.Sep 1, 2004 · N709AX · Boeing 767231 · Landing Gear Position and WarningSDR ABXA040297Seal · tornDURING R1 PREFLIGHT, DISCOVERED CAPTAINS NR 2 WINDOW CRANK BINDING TOWARDS CLOSE. FOUND L2 WINDOW SEAL TORN AND CATCHING ON WINDOW, REMOVED AND REPLACED L2 WINDOW SEAL IAW AMM 56-11-11-4.Aug 25, 2004 · N707AX · Boeing 767231 · Flight Compartment WindowsSDR 0401356631Manifold · brokenDURING TAKEOFF ROLL, THE CREW OBSERVED THE NR 3 ENGINE EPR INDICATION DECREASE WITH THE EGT INDICATION RISING INTO THE CAUTION RANGE. THE TAKEOFF WAS ABORTED AT 100 KTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE ENGINE IAW FIM AND FOUND TAug 17, 2004 · N631US · Boeing 747251B · Compressor Bleed ControlSDR ABXA040280Screw · defectiveDURING MAINTENANCE INSPECTION AT BFI, FOUND THE CAPTAIN'S SLIDING WINDOW WOULD NOT CLOSE. NR 2 L WINDOW. REPLACED NR 2 LT WINDOW BALL SCREW AND NUT ASSEMBLY IAW MM CHAP. 56-11-04-4.Aug 13, 2004 · N707AX · Boeing 767231 · Flight Compartment WindowsSDR 2004UALA00732Compressor · stalledRT ENG COMPRESSOR EXPERIENCED A COMPRESSOR STALL. STALL STOPPED WHEN RT THROTTLE RETARDED. RESET BLEED ALL INDICATIONS NORMAL. ALL POST-COMPRESSOR STALL TROUBLESHOOTING ACCOMPLISHED IMMEDIATELY AFTER EVENT, NO DEFECTS FOUND. DECIDED TO WATCH ENG FOR ANY REAug 7, 2004 · N604UA · Boeing 767222 · Turbine Engine Compressor SectionSDR 0401256745Engine · failedDURING INITIAL CLIMB AT APPROXIMATELY 300 FT AGL, A LOUD BANG WAS HEARD FROM THE NR 1 ENGINE ALONG WITH LOSS OF THRUST AND RISING EGT. THE CREW PERFORMED THE COM PROCEDURE FOR AN ENGINE FAILURE AND SHUT DOWN THE NR 1 ENGINE. THE FLIGHT RETURNED TO KIX AND LAJul 28, 2004 · N645NW · Boeing 747222B · Turbine SectionSDR 2004UALA00627Warning Light · illuminatedCABIN ALT WARNING & EXCESSIVE HOT AIR CAUSED DIVERSION OF FLIGHT. AT FLIGHT LEVEL 330 THE AIRCRAFT WAS UNABLE TO MAINTAIN CABIN PRESSURE. THE CARGO DOOR DEPRESSOR SEAL WAS FOUND DAMAGED CAUSING A LARGE AIR LEAK.Jun 29, 2004 · N620UA · Boeing 767222 · Cabin Pressure Control SystemSDR 04FDEA01815Engine · failedUNRECOVERABLE STALL ENG NR 2 DURING T/O AT 500 FT ATB. EGT WAS RAISING TO 670 DEG C, EGT LIGHT ON, PULLED BACK THE THROTTLE TO PREVENT FURTHER EGT INCREASE. FLAME NOTED BY ATC. AS PER MTSI 72-00/3790 REMOVED AND REPLACED NR 2 ENG VANE AND BLEED CONTROL PEJun 20, 2004 · N454FE · Airbus A310222 · Engine (Turbine/Turboprop)SDR CA040920001Actuator · corroded(CAN) WATER INGRESS INTO GEAR BOX CAUSED EXTENSIVE CORROSION, INVESTIGATION ON GOING WITH MFG (STAB TRIM ACTUATOR).Jun 17, 2004 · Boeing 767233 · Stabilizer ActuatorSDR 2004UALA00522Warning Light · illuminatedLANDED LAX UNDER AMBER ALERT DUE TO FLAP DISAGREE INDICATION. ACCOMPLISHED FLAP POSITION TRANSMITTER SYNCHRONIZATION CHECK ON 3, 4, AND 5 FLAP POSITION TRANSMITTERS. FOUND NR 4 OUT OF LIMITS. ADJUSTED TRANSMITTER.Jun 1, 2004 · N604UA · Boeing 767222 · Trailing Edge Flap Control SystemSDR ABXA040182Pressure Switch · defectiveLT ENGINE OIL FILTER MESSAGE DISPLAYED. MESSAGE REMAINED WHEN THRUST REDUCED & ENG SHUTDOWN. NR 1 ENG OIL PRESSURE LIGHT DID NOT COME ON. C/W FIM 79A-35-00-90, OIL FILTER EICAS MESSAGE WAS NOT DISPLAYED AT AIRCRAFT ARRIVAL THOUGH ENGINE WAS STILL WINDMILLINGMay 20, 2004 · N702AX · Boeing 767231 · Engine Oil Indicating SystemSDR 2004UALA00370Engine · malfunctionedDIVERTED DUE TO LOSS OF LT ENGINE POWER. ENGINE HUNG DURING ACCELERATION. TSI WAS 10 HRS. FOUND PCB 3.5, PTT2 TOTAL AIR TEMP AND PIR INTERSTAGE RETURN PSI TUBE FROM TT2 SENSOR LOOSE. ALL WERE SECURED AND SAFETIED.Apr 19, 2004 · N620UA · Boeing 767222 · Engine (Turbine/Turboprop)SDR 2004UALA00318Roller · sparksFWD CARGO PIT POWER DRIVE ROLLER SPARKING AND SMOKING. POWER DRIVE UNIT CABLE CHAFED AGAINST CLAMP ATTACH SCREW ON BOTTOM OF PDU, DUE TO BROKEN CABLE CLAMP. SCREW APPEARS TO HAVE BURN MARKS FROM ARCING. PDU REPLACED.Apr 8, 2004 · N603UA · Boeing 767222 · Cargo Compartments
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