Pratt & Whitney JT8D-15A

Service difficulty reports · 538

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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 = 'JT8D15A'
  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 R342004F00000Valve · inoperativeNR 1 OIL TEMP CLIMBED INTO CAUTION RANGE DURING CLIMBOUT AND WOULD NOT RETURN BACK TO NORMAL OPERATING TEMP. SHUTDOWN NR 1 ENGINE AS PRECAUTIONARY MEASURE AND RETURNED TO BASE. REMOVED MAIN OIL FILTER AND INSPECTED NO CONTAMINATION ON FILTER. TROUBLESHOOT EApr 27, 2004 · N289MT · Boeing 727223 · Fuel HeaterSDR DHL2004755009O-Ring · leakingON CLIMBOUT NR 1 OIL TEMPERATURE EXCEEDED 120 DEGREES. ACCOMPLISHED ABNORMAL PROCEDURES. NR 1 FUEL HEAT WOULD NOT SHUT OFF. OIL QUANTITY BEGAN TO DECREASE. ALL ABNORMALS ACCOMPLISHED. SECURED NR 1 ENGINE PEAK TEMPERATURE 155 DEGREES FOR 5 MINUTES. FOUND Apr 9, 2004 · N755DH · Boeing 727225 · Fuel HeaterSDR 2820404Light · burnedDURING DESCENT, SOME SMOKE IN CABIN AT SEAT 15 ABC. THE "FASTEN SEAT BELT, NO SMOKING" CIRCUIT BREAKER POPPED. FOUND LIGHT BAR MELTED. DISCONNECTED AND STOWED WIRES. SEAT BELT, NO SMOKING SYSTEM PLACED ON MEL 33-3.Apr 7, 2004 · N282US · Boeing 727251 · Passenger Compartment LightingSDR 200405121Flap · bindingINBOARD FLAPS STUCK AT 2 DEGREES POSITION.Apr 5, 2004 · N86426 · Boeing 727251 · Trailing Edge FlapsSDR CA040329001Selector Panel · failed(CAN) DURING DESCENT, COMMUNICATIONS WERE LOST. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE FIRST OFFICER'S AUDIO SELECTOR PANEL WAS SUSPECT. A HOT MIKE SITUATION WAS APPARENT IN VHF 1 AND VHF 2. THE AUDIO SELECTOR PANEL WAS REPMar 27, 2004 · Boeing 727223 · Audio Integrating SystemSDR CA040319006Csd · failed(CAN) DURING TAKEOFF, IT WAS OBSERVED THAT ELECTRICAL POWER WAS LOST WITH NR 3 GENERATOR. A REJECTED TAKE-OFF WAS CARRIED OUT AND AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. NR 3 ENGINE CONSTANT SPEED DRIVE WAS DISCONNECTED AND SYSTEM WAS DEFERRED IAW MEL Mar 17, 2004 · Boeing 727225 · AC Generator-AlternatorSDR CA040312004Accessory Unit · faulty(CAN) DURING APPROACH AND LANDING GEAR HANDLE EXTENDED, IT WAS OBSERVED THAT THERE WAS AN UNSAFE LT LANDING GEAR LIGHT. IT WAS DECIDED THAT A MISSED APPROACH WOULD BE CARRIED OUT AND GO AROUND. EMERGENCY PROCEDURES WERE CARRIED OUT. TOWER WAS NOTIFIED OF THMar 11, 2004 · Boeing 727225 · Landing Gear Retraction/Extension SystemSDR DL73S040178Start Valve · contaminatedRIGHT ENGINE START VALVE OPEN LIGHT CAME ON DURING CLIMBOUT ISOLATION VALVE AND ENGINE BLEED VALVE WERE CLOSED. LIGHT WENT OUT AT LOW PWR SETTING. LIGHT STAYED OUT AT LOW PWR. FOUND F/F XMTR LEAKING AT HI PWR SETTING. REPLACED PACKING AND BACK UP RINGS. RFeb 20, 2004 · N334DL · Boeing 737232 · Engine Start Valves/ControlsSDR CA040219003Engine · failed(CAN) UPON THE TRANSITIONING FROM CLIMB TO CRUISE, A LOUD BANG WAS HEARD AND SUBSEQUENT VIBRATION FELT THROUGHOUT THE AIRFRAME. ALL NR 1 ENGINE PARAMETERS IMMEDIATELY BEGAN TO DETERIORATE RAPIDLY. AT FL280, ENGINE FAILURE DRILL INITIATED AND COMPLETED. ATC AFeb 18, 2004 · Boeing 727225 · Engine (Turbine/Turboprop)SDR CA040217008Control Cable · frayed(CAN) DURING SCHEDULED MAINTENANCE, IT WAS OBSERVED THAT THE LT IB FLAP ASSY WAS DROOPING. UPON FURTHER INVESTIGATION, THE CABLE ASSY WAS FOUND FRAYED AND BROKEN. A NEW CABLE ASSY WAS INSTALLED IAW MM 27-51-5 AND FUNCTIONED SERVICEABLE IAW MM 27-51-0. NO FURTFeb 13, 2004 · Boeing 727225 · Trailing Edge Flap Control SystemSDR DL73S040143Control Cable · stiffDURING CLIMB TO 370 FROM 330 NR 1 THROTTLE POPPED BACK AND FORTH. A/T DISCONNECTED AND THROTTLE STIFF. AFTER DESCENT BELOW 330 THROTTLE WORKED NORMAL AND NOT AS STIFF. REPLACED NR 1 ENGINE THROTTLE PUSH-PULL CABLE. RAN ENGINE PER PFHB. OPS GOOD.Feb 9, 2004 · N334DL · Boeing 737232 · Power LeverSDR CA040209003Target · misinstalled(CAN) DURING TAXI, THE RT MLG UNSAFE LIGHT ILLUMINATED AND GREEN SAFETY LIGHT WAS OUT. MAINTENANCE INSTALLED LANDING GEAR PINS AND THE AIRCRAFT TAXIED BACK TO THE RAMP. DURING INSPECTION OF THE PROXIMITY LANDING GEAR SWITCHES, IT WAS OBSERVED THE TARGETS WEREFeb 5, 2004 · Boeing 727225 · Landing Gear Position and WarningSDR 02240402WPDuct · brokenAFTER TAKEOFF THE RT ENGINE FIRE WARNING LOOP (A) LIGHT ILLUMINATED. SHORTLY, AFTER THE FIRE WARNING LOOP (B) ILLUMINATED WITH FULL ENGINE FIRE INDICATIONS. MAINTENANCE FOUND BROKEN COUPLING ON THE COWL ANTI-ICE DUCT, REMOVED AND REPLACED DUCT ASSEMBLY IAW MFeb 1, 2004 · N934LK · Doug DC9 · Air Intake Anti/De-Ice SystemSDR DL73S040087Blade · brokenAT TOP OF DESCENT UPON THROTTLE RETARD NR 2 ENGINE VIBRATION. ALL ENGINE PARAMETERS NORMAL. AT 75 PERCENT VIBRATION DISCONTINUED. LEFT ENGINE AT 75 PERCENT. FOUND TURBINE BLADE DAMAGE. REPLACED ENGINE.Jan 24, 2004 · N327DL · Boeing 737232 · Turbine SectionSDR CA040121001Transmitter · failed(CAN) DURING TAXI, IT WAS OBSERVED THAT THE NR 1 ENGINE EPR HAD NO INDICATION. THE AIRCRAFT WAS RETURNED TO THE RAMP. AFTER SOME TROUBLESHOOTING, MEL 77-01-01 WAS RAISED. THIS IS A 3 FLIGHT DAY, A CAT, MEL. THE AIRCRAFT WAS DISPATCHED.ON RETURN TO HOME BAJan 19, 2004 · Boeing 727225 · Engine Pressure Ratio (EPR)SDR DL73S040025Hose · leakingLOSS OF A-SYSTEM HYDRAULICS IN FLIGHT. FOUND NR 2 ENGINE HYDRAULIC PUMP PRESSURE HOSE LEAKING. REPLACED NR 2 ENG HYDRAULIC PRESSURE HOSE. HOSE LEAK CHECKS GOOD. SERVICED A-SYSTEM HYDRAULICS TO FULL. SPUN & RAN ENGINE PRESSURE AND LEAK CHECK GOOD.Jan 10, 2004 · N301DL · Boeing 737232 · Hydraulic System, MainSDR DL73S040012Engine · failedAT CRUISE FROM YYZ - ATL NR 02 ENGINE OIL PRESS DROPPED TO 28 PSI ALL OTHER INDICATIONS NORM. NR 02 OIL QTY ON MCO NO LOW OIL PRESS LIGHT. AFTER CONSULTING WITH ATL DIVERT TO CVG AND NR 02 ENGINE SHUTDOWN. ENGINE SHUTDOWN REPORT COMPLETED. CHECKED OIL QTY Jan 7, 2004 · N309DL · Boeing 737232 · Engine (Turbine/Turboprop)SDR CA040104002Flange · cracked(CAN) SCHEDULED MAINTENANCE WAS CARRIED OUT TO REPLACE THE FCU/FUEL PUMP QUAD RING. THE RUN OUT TORQUE INSPECTION WAS CARRIED OUT AND THE CLEARANCE FAILED. DISASSEMBLY OF THE AREA DETERMINED THAT THE QUAD RING NUT ATTACHMENT FLANGE WAS CRACKED. THE UNSERVICEAJan 1, 2004 · Boeing 727231 · Accessory GearboxesSDR DL73S031146Engine · malfunctionedAFTER T/O, NR 2 ENGINE WENT TO FULL THEN DROVE TO IDLE. ENGINE DATA READ ON FDR. REPLACED NR 2 ENGINE.Dec 28, 2003 · N310DA · Boeing 737232 · Engine (Turbine/Turboprop)SDR DL73S031115Wire Harness · shortedON APPROACH, THE LEFT GEN TRIPPED. RT BUS ATTEMPTED TO PICK UP AND TRIPPED ALSO. DOWN TO STBY POWER. CREW DECLARED EMERGENCY. FOUND LT GENERATOR CABLE SHORTED. REPLACED GENERATOR FEEDER HARNESS.Dec 20, 2003 · N243WA · Boeing 737247 · Electrical Power System WiringSDR CA031222002Skin · damaged(CAN) DURING LOADING OF CARGO, THE DOLLY AND CONTAINER UNLATCHED AND ROLLED UNDER THE LT WING SCORING THE PAINT AND CREASING THE LT OB AILERON LOWER SURFACE. THE RESULTING DAMAGE FOUND 2 CREASES ON THE AILERON WITH 1 AT 14 INCHES LONG AND THE OTHER AT 7 INCHEDec 19, 2003 · Boeing 727225 · Trailing Flap Position Indicating SystemSDR 251TR0005Transmitter · leakingNR 1 ENGINE LEAKING FUEL OUT OF FWD SIDE OF FUEL FLOW TRANSMITTER. REPLACED NR 1 ENGINE FUEL FLOW TRANSMITTER PER MM 73-31-12. LEAK AND OPS CHECK OK DURING ENGINE RUN PER MM 71-00.Dec 15, 2003 · N251TR · Boeing 737228 · Fuel Controlling SystemSDR Y1R2004F00000Oil Cooler · crackedCRACK DEVELOPED ON RT SEAM OP OIL COOLER, UNIT WAS REPAIRED AND ACCUMULATED 31.5 HOURS TSR. CRACKED AGAIN IN WELD AREA OF RT SEAM OF CSD OIL COOLER. (WP01200405240)Dec 12, 2003 · N289MT · Boeing 727223 · Engine Oil CoolerSDR C8GA20030027Wire · brokenFLT 800 FROM KMIA TO MMUN. AFTER TAKE-OFF CLIMBING THROUGH 1,000 FT AGL, THE NR 3 ENGINE OIL TEMPERATURE BEGAN TO FLUCTUATE BETWEEN 100 DEGREES AND OFF SCALE HIGH. AT APPROXIMATELY 15,000 FT, THE NR 3 ENGINE STAYED OFF SCALE HIGH. REFERENCE AOM CHECKLIST FOLLONov 19, 2003 · N715AA · Boeing 727223 · Engine Oil TemperatureSDR CA031023002Indicator · sticking(CAN) ON CLIMB, RT OB FLAP STOPPED AT 3 DEGREES. A FLAP ASYMMETRY CONDITION OBSERVED. AIRCRAFT RETURNED TO BASE WITHOUT INCIDENT. OB FLAP INDICATOR REPLACED IAW MM 27-52-21 AND FUNCTIONALLY TESTED SERVICEABLE. NO FURTHER INCIDENT ON SUBSEQUENT FLIGHT.Oct 22, 2003 · Boeing 727223 · Trailing Flap Position Indicating SystemSDR DL73S030910Autothrottle Sys · failedON T/O ROLL AFTER TOGA THROTTLES REQUIRED MANUAL SET WITH NORMAL FD/AP/AT. F/O TURNED THROTTLE OVER TO CAPT NR 1 AND 2 THROTTLES SPLIT WITH AN INCREASE ON 1. EGT WENT UP TO 630 ON NR 1 WITH A 2.12 SETTING 2.1 AT SET. NR 2 WAS AT 2.04. EVENED THROTTLES AT 2Oct 9, 2003 · N379DL · Boeing 737247 · Auto Throttle SystemSDR DL73S030899Duct · damagedRT ENGINE OVERHEAT LIGHT CAME ON DURING CLIMB, WENT OUT WITH THROTTLE AT IDLE. FOUND DAMAGED STARTER DUCT. REPLACED SAME.Oct 3, 2003 · N302DL · Boeing 737232 · Engine Start Valves/ControlsSDR DL73S030788Wire · shortedNR 2 ENG SHUTDOWN INFLT DUE TO OIL TEMP PEGGED HIGH. FOUND TO BE INDICATION PROBLEM (SHORTED WIRE). REPAIRED WIRE.Aug 27, 2003 · N374DL · Boeing 737247 · Engine Oil System WiringSDR CA030827008Nut Plate · missing(CAN) L-2 DOOR ESCAPE SLIDE GIRT BAR FORWARD FLOOR FITTING NUT PLATE ASSY MISSING, UNDER FLOOR PANEL. THIS NUT PLATE REENFORCED THE GIRT BAR FITTING ATTACHMENT TO THE FLOOR. IN CASE OF CHUTE DEPLOYEMENT, THE LOAD IN THE SLIDE WOULD PULL ON THE ATTACH FITTING AAug 13, 2003 · Boeing 727251 · Escape SlideSDR CA030827011Pulley · worn(CAN) WHILE INSPECTING THE TAIL AREA (C-CHECK), IT WAS NOTICED THAT THE RT STABILIZER TRIM CABLE WAS TRAVELLING VERY CLOSE TO THE PULLEY HOLDING BRACKET. FURTHER INVESTIGATION REVEALED ONE MORE RT CABLE PULLEY WORN AND TWO OTHERS WORN OUT ON THE LT CABLE. CABAug 13, 2003 · Boeing 727251 · Stabilizer Control SystemSDR CA030827012Bolt · missing(CAN) DURING INSPECTION FOUND RT INBOARD FLAP 2ND INBOARD TRACK, FORWARD ROLLER BOLTS (2) ASSY MISSING.Aug 13, 2003 · Boeing 727251 · Trailing Edge FlapsSDR CA030813003Transmission · damaged(CAN) ON APPROACH TO I/B T/E FLAPS WOULD NOT EXTEND IN NORMAL OR MANUAL MODE. POST LANDING INSPECTION DETERMINED NR 4 FLAP TRANSMISSION (I/B, I/B) WAS UNSERVICEABLE. THE UNIT WAS REPLACED THE FLAP SYSTEM RIG CHECKED AND FUNCTION TESTED. AIRCRAFT RETURNED TO SEAug 10, 2003 · Boeing 727233 · Trailing Edge Flap Control SystemSDR CA030813004Transmission · damaged(CAN) ON APPROACH TO I/B T/E FLAPS WOULD NOT EXTEND IN NORMAL OR MANUAL MODE. POST LANDING INSPECTION DETERMINED NR 4 FLAP TRANSMISSION (I/B, I/B) WAS UNSERVICEABLE. THE UNIT WAS REPLACED THE FLAP SYSTEM RIG CHECKED AND FUNCTION TESTED. AIRCRAFT RETURNED TO SEAug 10, 2003 · Boeing 727233 · Trailing Edge Flap Control SystemSDR 234TR0004Fuel Control · malfunctionedNR 1 ENGINE ROLLED BACK ON SHORT FINAL APPROACH. REPLACED IGNITION EXCITER BOX PER MM 74-11-11 AND REPLACED FUEL CONTROL UNIT PER MM 73-09-255. OPS CHECKS OK.Jul 19, 2003 · N234TR · Boeing 737228 · Fuel Control/Turbine EnginesSDR CA030718001Igniter · faulty(CAN) DURING START OF NR 3 ENGINE, IT WAS OBSERVED THERE WAS NO EGT. START WAS ABORTED & OBSERVED ALL PARAMETERS. MAINT INSPECTED AREA & REQUESTED ANOTHER START. NR 3 ENGINE STARTED & OBSERVED RAPID EGT RISE & ENG START ABORTED. MAINT INFORMED FLT DECK THAT Jul 15, 2003 · Boeing 727225 · Spark Plug/IgniterSDR DL73S030643Engine · bird ingestionIRREG: ON T/O DETECTED SMELL IN COCKPIT AND CABIN. RETURN TO CVG. FOUND EVIDENCE OF BIRD STRIKE NR 1 ENG. INSP ENG AND ENG BLEED DUCTS. PERFORMED DUCT BURNOUT AND REPLD. WATER SEPARATOR BAGS.Jul 14, 2003 · N304DL · Boeing 737232 · Engine (Turbine/Turboprop)SDR 2003F00542Hydraulic Line · damagedON TAKEOFF, OUT OF SDF AT GEAR ROTATION LOST SYS 'A' HYD FLUID, SHUT PUMPS OFF ACCOMPLISHED ABNORMAL CHECKLIST. REMOVED AND REPLACED HOSE ASSEMBLY NR 2 ENGINE P/N 10-60563-40, NO METAL FOUND IN CASE DRAIN FILTERS OR SUPPLY FILTERS REPLACED NR 1 AND NR 2 HYDRAJun 27, 2003 · N803MA · Boeing 727225 · Hydraulic System, MainSDR 03FDEA00974Engine · malfunctionedAT FL330, NR 2 ENGINE OIL TEMP ROSE TO HIGH IN THE YELLOW RANGE. ADDING FUEL FLOW BY INCREASING THROTTLE DID NOT HELP. AFTER 15 MINS IN YELLOW BAND, SHUTDOWN NR 2 ENGINE IAW ENGINE FAILURE/SHUTDOWN CHECKLIST. WHEN THROTTLE RETARDED TO IDLE, NR 2 ENG OIL Jun 26, 2003 · N236FE · Boeing 727200 · Engine Oil Indicating SystemSDR CA030627001Control Cable · chafed(CAN) DURING A ROUTINE MAINTENANCE INSPECTION, IT WAS OBSERVED THAT THE RT INBOARD AILERON CABLE ASSY WAS CHAFED AND WORN AT THE CABLE GUIDE. THE CABLE WAS REMOVED & NEW CABLE INSTALLED IAW MM 27-10-71. ADJUSTMENT AND FUNCTIONAL CHECK CARRIED OUT SERVICEABLE IJun 26, 2003 · Boeing 727225 · Aileron Control SystemSDR DHL2003755009Moisture Trap · contaminatedDURING T/O AND CLIMB NR 1 EPR AND FUEL FLOW CONTINUALLY FLUCTUATES .04 AND 400 LBS RESPECTIVELY. PERFORMED ABNORMAL PROCEDURES. FLUCTUATIONS STOPPED PRIOR TO PRECAUTIONARY ENGINE SHUT DOWN. FOUND MOISTURE IN THE NR 1 ENGINE FUEL CONTROL MOISTURE TRAP. DRAIJun 19, 2003 · N755DH · Boeing 727225 · Fuel Controlling SystemSDR SWAA031340Blade · bentDURING WALK AROUND INSP, FOUND BENT FAN BLADES (6 EA) ON NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENG PER MM.Jun 15, 2003 · Boeing 7372H4 · Turbine Engine Compressor SectionSDR CA030627012Line · ruptured(CAN) DURING TAXI, CREW APPLIED THE BRAKES AND OBSERVED LOSS OF 'B' SYSTEM HYDRAULIC PRESSURE AND HYD BRAKE PRESSURE. AIRCRAFT STOPPED AND MAINTENANCE TOWED AIRCRAFT BACK TO MAINTENANCE FACILITY. MAINTENANCE OBSERVED LEAKAGE FROM THE RT ELEVATOR PCU. THE Jun 10, 2003 · Boeing 727223 · Hydraulic System, MainSDR DL73S030488Bulb · malfunctionedNR 1 OIL TEMP ERRATIC FLUX PLUS OR MINUS 10 DEGREES UPPER GREEN BAND, THEN WENT INTO YELLOW BAND. ALL AREAS PLUS OR MINUS 10 DEGREES. FLUX STAYED IN YELLOW UP TO 15 MINUTES. PRECAUTIONARY SHUTDOWN PER POM. REPLACED OIL TEMP BULB.May 23, 2003 · N307DL · Boeing 737232 · Engine Oil TemperatureSDR DL73K030336Element · malfunctionedNR 1 ENGINE OVERHEAT ON CLIMBOUT.PERFORMED PROCEDURES IAW POM. LIGHT STAYED ON UNTIL AFTER SE LANDING - REPLACED LOWER LOOP AND FIRE DETECTOR ACCESSORY UNITApr 4, 2003 · N377DL · Boeing 737247 · Overheat DetectionSDR CA030327005Indicator · malfunctioned(CAN) DURING CLIMB, FLAPS WERE SELECTED TO THE 2 DEGREE POSITION. THE INBOARD FLAPS STAYED AT 5 DEGREE. AIRCRAFT RETURNED TO YYC AND LANDED WITHOUT INCIDENT. FLAP SYSTEM INSPECTED, LUBRICATED ANDCYCLED WITH SYSTEM OPERATING NORMALLY I.A.W. MM 27-51-0. FLAPMar 20, 2003 · Boeing 727225 · Trailing Flap Position Indicating SystemSDR DL72W030196O-Ring · leakingNR 1 ENG OIL LOSS. REPLACED FUEL PUMP SHAFT O-RING.Feb 25, 2003 · N297WA · Boeing 727247 · Turbine Engine Oil SystemSDR SQ7A242003Valve · inoperativeAT CURISE NR 1 ENGINE FUEL HEAT VALVE STUCK OPEN, ACCOMPLISHED ABNORMAL PROCEDURE 1-314-3, OIL TEMP REMIANED IN YELLOW BAND, ACCOMPLISHED ABNORMAL PROCEDURE 1-314-4, SHUT DOWN #1 ENGINE AS PERCAUTION. ADVISED ATC LANDING CVG UNEVENTFUL.Feb 24, 2003 · N282US · Boeing 727251 · Fuel HeaterSDR DL72W030192Pump · failedAIR TURNBACK, NR 1 ENGINE. REPLACED FUEL PUMP AND CONTROL.Feb 24, 2003 · N297WA · Boeing 727247 · Engine Fuel PumpSDR DL72S030110Warning Light · illuminatedNR 1 ENG OIL FILTER BYPASS LIGHT PER POM SHUT ENGINE DOWN. CLEANED CONNECTOR FOR MASTER DIM AND TEST MODULE AND PERFORMED ENGINE WINDMILL INSP PER M/M.Jan 29, 2003 · N523DA · Boeing 727232 · Engine (Turbine/Turboprop)SDR MYW2003F00001Regulator Valve · inoperativeON DEPARTURE, NR 1 ENGINE SUPPLY PRESSURE (DUCT PRESSURE) REACHED 95 PSI FOLLOWED BY STRUT OVERHEAT AND PACK TRIP. RETURN AIRCRAFT. AIRCRAFT PREPED FOR TWO ENGINE FERR. ACCOMPLISHED TWO ENGINE FERRY TO MIA IAW MM. REMOVED AND REPLACED 13 STAGE MODULATING RJan 18, 2003 · N804MA · Boeing 727225 · Pneumatic Distribution System
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