Pratt & Whitney JT9D-7A

Service difficulty reports · 593

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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 = 'JT9D7A'
  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 P5CA0401221Stringer · corrodedAFT CARGO COMPT STRINGER 50L B/W STA 1680-1700 CORRODED. REMOVED LIGHT CORROSION, PRIMED & TREATED.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Main, Longeron/StringerSDR P5CA0401222Skin · corrodedLEFT MAIN LANDING GEAR FWD CUTOUT EXTERNAL PANEL SKIN FROM LBL 21 - LBL 10 HAS CORROSION. REMOVED CORROSION, CORROSION WITHIN LIMITS, PRIMED & TREATED.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Main, Plate/SkinSDR P5CA0401214Bulkhead · corrodedBULKHEAD EXIT SIDE UNDER RADOME LT SIDE 3RD BEAM DOWN FROM TOP HAS CORROSION. REMOVED CORROSION, TREATED & PRIMED.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Main, BulkheadSDR P5CA0401210Keelbeam · corrodedKEEL BEAM FROM STA 1075-1095 HAS CORROSION LEFT & RIGHT SIDE. REMOVED CORROSION & TREATED PER SRM 53-10-01.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Main, KeelSDR P5CA0401212Frame · puncturedBULK CARGO COMPT FUSELAGE FRAME WEB BELOW THE UPPER CHORD IS PUNCTURED. CUT OUT DAMAGED AREA, FABRICATED DOUBLER & FILLER, REINSTALLED, TREATED & PRIMED.Sep 14, 2004 · N858FT · Boeing 747123 · Fuselage Main, FrameSDR P5CA0401220Jackscrew · corrodedLEFT WING NR 2 TRACK JACKSCREW HAS PITTED CORROSION. REMOVED AND REPLACED LEFT WING JACKSCREW AS PER MM 27-51-41.Sep 14, 2004 · N858FT · Boeing 747123 · Trailing Edge Flap Control SystemSDR UPS04443073Battery Pack · inoperativeEMERGENCY LIGHT INOPERATIVE, PASSENGER AREA. REPLACED BATTERY PACK, OPS CHECK GOOD.Sep 6, 2004 · N680UP · Boeing 747SR46 · Emergency LightingSDR EIA2004079Frame · crackedSTA 1840 FRAME CRACKED AT STR 12R. FABBED AND INSTALLED REPAIR IAW SRM 51-40-03 FIG 2 1-6.Sep 6, 2004 · N480EV · Boeing 747121 · Fuselage Main, FrameSDR P5CA0401193Skin · corrodedRIGHT WING UPPER SKIN HAS SURFACE CORROSION. REMOVED LITE CORROSION, TREATED & PRIMED.Sep 4, 2004 · N858FT · Boeing 747123 · Wing, Plate/SkinSDR EIA2004076Stringer · crackedSTRINGER 14R CRACKED AT BS 2200. REMOVED DAMAGE, FABBED REPAIR IAW SRM 51-30-02.Sep 4, 2004 · N480EV · Boeing 747121 · Fuselage Main, Longeron/StringerSDR EIA2004078Structure · corrodedLT WING GEAR W/W STA. 1241 LBL 40-80 CORROSION BETWEEN CANTED WEB AND LWR CHORD. REMOVED CORROSION AND REPAIRED IAW ECRA 480-53-167-2Sep 4, 2004 · N480EV · Boeing 747121 · Wing Main, Frame StructureSDR EIA2004084Skin · corrodedMAIN CABIN WINDOW BELT CORRODED BETWEEN B.S. 680-700 LT. REMOVED CORROSION FOUND OUT OF LIMITS INSTALLED REPAIR IAW ECRA 480-53-171-2.Sep 3, 2004 · N480EV · Boeing 747121 · Fuselage Main, StructureSDR EIA2004081Frame · crackedFRAME STA. 380L CRACKED FLANGE AT STR 22 CUTOUT. REMOVED DAMAGED AND FABBED AND INSTALLED REPAIR IAW SRM 53-10-04 PG. 43-45 AND 53-10-02.Sep 3, 2004 · N480EV · Boeing 747121 · Fuselage Main, FrameSDR EIA2004088Floorbeam · corrodedMAIN DECK FLOORBEAM FWD SIDE (J) CHANNEL CORRODED BS 460 LBL 9. FABBED AND INSTALLED REPAIR PARTS, STA 460 LOWER CHORD LBL9 IAW SRM 51-40-04 FIG. 1 AND 51-30-02.Sep 2, 2004 · N480EV · Boeing 747121 · Fuselage Main, Floor BeamSDR EIA2004083Stringer · corrodedMAIN CABIN INTERIOR RT STRINGER 22 BS 160-220 CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS, REPLACED STRINGER 22R BS 140-220 IAW SRM 51-30-02 AND 53-10-01.Sep 2, 2004 · N480EV · Boeing 747121 · Fuselage Main, Longeron/StringerSDR EIA2004082Floorbeam · crackedMAIN DECK FLOOR BS 460 LBL 65 FLOORBEAM WEB CRACKED AT UPPER EDGE. REMOVED AND REPLACED STA 460 FLOORBEAM WEB IAW SRM 53-10-07 FIG 11 AND 51-30-02.Sep 2, 2004 · N480EV · Boeing 747121 · Fuselage Main, Floor BeamSDR 04017Engine · failedAT 100 FT AFTER TAKEOFF THE NR 2 ENGINE FAILED.Apr 26, 2004 · N712CK · Boeing 747122 · Engine (Turbine/Turboprop)SDR UPS04442243Engine · flamed outDURING CRUISE NR 2 ENG FLAMED OUT AT 37K DURING CROSSFEED FROM NR 3 TANK. OIL PRESS REMAINED 10PSI, N1 25 PERCENT, N2 28 PERCENT ENG WAS SHUTDOWN FOR APPROX 25MIN. CREW ATTEMPTED RESTART AT 33K PER QRH - NO JOY, CREW COMPLETED ENG SEVERE DAMAGE CHECKLIST. CApr 22, 2004 · N676UP · Boeing 747123 · Engine (Turbine/Turboprop)SDR 04013Engine · malfunctionedSHUTDOWN NR 2 ENGINE IN FLIGHT; AT APPROX. 4000 FT AGL NR 2 ENGINE SURGED AND BANGED FOLLOWED WITH HIGH EGT 1150 DEG.C. RETURNED TO VHHH AND ALL OTHER ENGINE PARMETERS NOT EXCEEDED.Mar 31, 2004 · N712CK · Boeing 747122 · Engine (Turbine/Turboprop)SDR P5CA0300993Fuel Control · leakingON ENG START NR 2 ENGINE ACCELERATED TO HIGH IDLE 75 PERCENT N2. REMOVED AND REPLACED NR 2 ENG FCU AND THE TT2 SENSOR UNIT IAW 73-21-01 AND AMM 73-21-04, OPS CK AND LEAK CHECK SATISFACTORY.Nov 23, 2003 · N921FT · Boeing 747283B · Fuel Control/Turbine EnginesSDR UPS03441156Engine · flamed outAT 1330Z INTO FLIGHT NR 4 ENG FLAMED OUT. COMPLY WITHIN FLIGHT ENGINE FAILURE/SHUTDOWN CK LIST. TRIED INFLIGHT START CK LIST AS THE ENG INDICATION WAS NORMAL WITH EXCEPTION OF NR 4 OIL TEMP BEING AROUND 100 DEG. REMOVED AND REPLACED MAIN FILTER, INSPECTED PAug 30, 2003 · N676UP · Boeing 747123 · Engine (Turbine/Turboprop)SDR P5CA03000885Warning Light · illuminatedON T/O NR 4 ENG FIRE DET A-LOOP ILLUMINATED FIRE LIGHT. B-LOOP NORMAL. ITEM WAS DEFERRED PER THE DDPG AFTER IT WAS DETERMINED THAT ONE LOOP WAS OPERATIONAL. DEFECTIVE A-LOOP.May 30, 2003 · N922FT · Boeing 7472U3B · Fire DetectionSDR UPS03440288Engine · failedDURING T/O AND CLIMB, TOWER NOTICED AND NOTIFIED FLT 6703 THAT SMOKE WAS TRAILING FROM NR 4 ENGINE. AT 6500 FEET CREW REPORTED A BANG AND ASSOCIATED ROLL BACK OF N1/N2. CREW FOLLOWED SEVERE ENGINE DAMAGE CKLIST. FUEL DUMPED AND AIRCRAFT 526 ON FLT 6703 RETUMar 13, 2003 · N526UP · Boeing 747212B · Engine (Turbine/Turboprop)SDR EIA2002098Engine · flamed outKJFK - FOUND ENGINE NR 4 FLAMED OUT DURING DESCENT. (M)Sep 11, 2002 · N481EV · Boeing 747132 · Engine (Turbine/Turboprop)SDR UPS02438564Engine · flamed outINSPECTION TYPE:N/A ENGINE NR 3 FLAME-OUT AT FL350 APPROXIMATELY 15 MINUTES AFTER LEVEL OFF, CAUSE UNKNOWN. AOM PROCEDURES ACCOMPLISHED AND ENGINE RESTARTED. AS PER MM T/S TREE 71-00-42 PG 219 AND 131 ACCOMPLISHED ALL CORRECTIVE ACTIONS FOR FLAME-OUT. NO DIJun 5, 2002 · N677UP · Boeing 747123F · Engine (Turbine/Turboprop)SDR UPS02438093Resistor · blownINSPECTION TYPE:N/A SMOKE IN THE C/P ON TOP OF DESCENT. COULD NOT LOCATE SOURCE. DID NOT SMELL ELECTRICAL. COMPLETED C/P SMOKE/FUME EVACUATION CHECKLIST. SMOKE WAS MODERATE TO HEAVY FROM GLARESHIELD-AREA THROUGH WHOLE UPPER DECK. ADJUSTED NR 1 & 4 ENG N2Apr 28, 2002 · N521UP · Boeing 747200 · Compressor Bleed ControlSDR UPS02438087Heat Exchanger · defectiveINSPECTION TYPE:N/A ENG NR 2 OIL TEMP CLIMBED INTO YELLOW RANGE THEN HIT RED RADIAL 8 MIN LATER. EXECUTED PRECAUTIONARY INFLIGHT SHUTDOWN AT 08H53Z. REMOVED AND REPLACED FUEL HEATER VALVE AND FUEL /OIL COOLER. ENG RUN AT EPR 1.18 FOR 32 MIN OIL TEMP 70 DEGRApr 21, 2002 · N675UP · Boeing 747123 · Engine Fuel/Oil CoolerSDR 200200245Vane · crackedLEFT HAND NR 4 CASCADE VANE WAS CRACKED AT AFT ATTACH AREA. REPLACED CASCADE VANE IN ACCORDANCE WITH B747 M/M 78-31-07.Apr 12, 2002 · N477EV · Boeing 747SR46 · Engine Thrust ReverserSDR KCS2003F00000Blade · damagedON POST FLIGHT INSPECTION, FOUND NR 1, NR 2, NR 3, AND NR 4 ENGINES HAD EVIDENCE OF C-1 BLADE DAMAGE. REMOVED ALL DAMAGED C-1 (N1) BLADES AND INSTALLED MATCHED SET OF C-1 BLADES ON ALL 4 ENGINES IAW MM AND ACCOMPLISHED FOD DAMAGE INSPECTION AND FOUND NO DEFECMar 26, 2002 · N702CK · Boeing 747146 · Turbine Engine Compressor SectionSDR 2003F00056Engine · flamed outNR 4 ENGINE FLAMED OUT AT FL 38 ALL PARAMETERS NORMAL, RESTARTED ENGINE WITH NO FURTHER MALFUNCTIONS. INSPECTED NR 4 ENGINE IAW B747 MM CH 71-00, NO DEFECTS NOTED. RAN NR 4 ENGINE AND LEAK CHECK IAW B747 MM CH 71-00. NO LEAKS NOTED. (M)Mar 26, 2002 · N709CK · Boeing 747132 · Engine (Turbine/Turboprop)SDR 2003F00057Blade · damagedON POST FLIGHT INSPECTION, FOUND NR 1, 2, 3 AND 4 ENGINES HAD EVIDENCE OF C-1 BLADE DAMAGE. REMOVED ALL DAMAGED C-1 (N1) BLADES AND INSTALLED MATCHED SET OF C-1 BLADES ON ALL 4 ENGINES IAW B747 MM 72-32-02/72-31-01 AND ACCOMPLISHED FOD DAMAGE INSPECTION AND FMar 26, 2002 · N702CK · Boeing 747146 · Turbine Engine Compressor SectionSDR KCS2003F00001Blade · damagedON POST FLIGHT INSPECTION, FOUND NR 1, 2, 3, AND 4 ENGINES HAD EVIDENCE OF C-1 BLADE DAMAGE. REMOVED ALL DAMAGED C-1 (N1) BLADES AND INSTALLED MATCHED SET OF C-1 BLADES ON ALL 4 ENGINES IAW MM AND ACCOMPLISHED FOD DAMAGE INSPECTION AND FOUND NO DEFECTS IAW MMMar 26, 2002 · N702CK · Boeing 747146 · Turbine Engine Compressor SectionSDR 200200184Flange · crackedCRACK FROM THE "R" FLANGE LIGHTNING HOLE TO THE FLANGE OUTER DIAMETER AT THE 12 O'CLOCK POSITION. RADIAL CRACK ( 1/2 INCH LONG) FROM THE "R" FLANGE LIGHTNING HOLE TO THE CASE WALL BUT NOT TO THE FILLET RADIUS AT THE 12:30 O'CLOCK POSITION. CRACK FROM THE "R" Mar 21, 2002 · N479EV · Boeing 747132 · Turbine SectionSDR S02232002Landing GearB18255 1.HYD #1 QTY LOSS AFTER T/O, A/C LANDING WITH ALT FLAP AND GEAR EXTEND, #1 EDP DEPRESSURIZED WHEN HYD #1 QTY DROPPED. 2.GRD VISUAL CHECK, LH MAIN GEAR RETRACT ACTUATOR PISTON ROD BROKEN, AND WHEEL WELL VISUAL CHECK NO RELATED COMPONENT DAMAGED.C/A:1.RPLFeb 19, 2002 · Boeing 747209B · Landing Gear SystemSDR S01271035Oil SystemB-18751 # 1 ENG BREATHER TEMP REACH 220 DEG C DURING CLB. OIL TEMP HIGH BUT OIL TEMP INCREASE GRADUALLY TO AMBER BAND. THEN OIL QTY DROP DOWN TO ZERO. ENG IN FLT S/D. C/A:1.REPLENISHED # 1 ENG OIL TO NORMAL LEVEL THEN MOTORING CK FOUND OIL LEAKING FROM LH # 3 Nov 11, 2001 · Boeing 747209B · Powerplant SystemSDR S01257039Jackscrew · damagedB-18751 GRD CHK FOUND NR 1 FLAPTRACK JACKSCREW FITTING BROKEN.C/A:1.ISSUED REVISION OF EO 740-57-50-0004 TO PERFORM THE REPLACEMENT/OVERHAUL IN LIEU OF INSPECTION. 2.REPLACED WITH NEW FITTING NR 1 THROUGH NR 8 PER 742-57-639359-001R1. 3.PROVIDE BROKEN FITTIOct 7, 2001 · Boeing 747209B · Trailing Edge Flap Control SystemSDR P5CA0100590Engine · malfunctionedDURING CLIMBOUT NR 3 ENGINE FIRE LIGHT CAME ON WITH FIRE LOOPS BOTH AT 9 ALSO STARTER VALVE OPEN LIGHT. ZERO OIL QTY CSD OIL AND RISE IN TEMP READING. ZERO N2 RPM AND N1 14 PERCENT. RAN ENG FIRE CHECK LIST BOTH LIGHTS STAYED ON. ENGINE REMOVED AND REPLACEDJul 29, 2001 · N850FT · Boeing 747122 · Engine (Turbine/Turboprop)SDR UPS01436215Engine · malfunctionedINSPECTION TYPE:N/A THRUST LEVERS CLOSED INSIDE BRUCK 1200 AGL. NR 3 ENG OIL PRESS LIGHT ON, EGT 952 GEN LIGHT ON AIRSPEED 165 KTS. FF 0 N2 & N1 LOW (NEAR 0). INSPECTED 3.5 BLEED VLVS FOR FOD, FUEL PUMP FP12 PRESSURE CHECKED AND REPLACED FUEL PUMP FILTER PEJun 30, 2001 · N677UP · Boeing 747123F · Engine (Turbine/Turboprop)SDR UPS01435269Engine · malfunctionedINSPECTION TYPE:PFLT DURING INITIAL ROTATION FOR T/O SMOKE (LITE SMOKE) ENTERED COCKPIT AND SPREAD INTO CABIN. PUT ON OXY MASKS, INCLUDING 1 ACM FOLLOWED SMOKE ELIMINATION CHECK LIST. SMOKE CLEARED IN SHORT TIME. ODOR, BUT NOT OF RUBBER OR ELEC WIRING. *S/Mar 13, 2001 · N691UP · Boeing 747121 · Engine (Turbine/Turboprop)SDR P5CA0100482Bearing · damagedDAMAGE FOUND ON NR 2 ENG LT TANGENTIAL BEARING. REPLACED TANGENTIAL LINK AND BEARING PER MM 71-21-04 ITEM 13.Feb 28, 2001 · N850FT · Boeing 747122 · Engine (Turbine/Turboprop)SDR EIA2001001Case · wornAIRCRAFT VIBRATES EXCESSIVELY AFTER TAKEOFF AND DURING INTITIAL CLIMB-OUT. STOPS WHEN ABOVE 210 KCAS AND FLAPS UP. INITIAL MAINTENANCE INSPECTION INDICATIONS OF SPOILER/AILERON CABLE SYSTEM BRACKET AND PULLEY DAMAGE. SUBSEQUENT MAINTENANCE CHECK AND INSPECTJan 1, 2001 · N478EV · Boeing 747SR46 · Turbine Engine Compressor SectionSDR 20010131SG006Case · wornAIRCRAFT VIBRATES EXCESSIVELY AFTER TAKEOFF AND DURING INTITIAL CLIMB-OUT. STOPS WHEN ABOVE 210 KCAS AND FLAPS UP. INITIAL MAINTENANCE INSPECTION INDICATIONS OF SPOILER/AILERON CABLE SYSTEM BRACKET AND PULLEY DAMAGE. SUBSEQUENT MAINTENANCE CHECK AND INSPECTJan 1, 2001 · N478EV · Boeing 747SR46 · Turbine Engine Compressor SectionSDR EIA2000020Engine · bird strikeKHV - ON TAKEOFF, NR 1 ENGINE COMPRESSOR STALLED AT 140K WITH ASSOCIATED RISE IN EGT TO PEAK OF 920 DEGREES AND DROP IN N1/EPR. REJECTED TAKEOFF. FOUND EVIDENCE OF BIRD INGESTION. PERFORMED INTAKE/EXHAUST INSPECTION, NIL DAMAGE NOTED. PERFORMED BORESCOPE IMay 28, 2000 · N480EV · Boeing 747121 · Engine (Turbine/Turboprop)SDR P5CA0000200Thrust Reverser · malfunctionedON TAKEOFF ROLL AT APPROX 25 KTS, NR 2 THRUST REVERSER UNLOCKED LIGHT ILLUMINATED. TAKEOFF ABORTED. TRANSFEREDTO MEL 78-2-A CAT C DMI NR 25184 AS PER MX CONTROL AXLE VERIFICATION INSPECTION C/W AS PER DDPG 78-2-A.May 20, 2000 · N858FT · Boeing 747123 · Engine Thrust ReverserSDR P5CA0000197Engine · stalledNR 2 ENGINE STALLED LOST POWER AND WAS SHUTDOWN PER IAW POLAR PROCEDURES. LOG PAGE NR 098103. REMOVED AND REPLACED NR 2 ENGINE AS PER POLAR W/C 7100-002, OPS CHECKS GOOD.May 14, 2000 · N858FT · Boeing 747123 · Engine (Turbine/Turboprop)SDR P5CA0000198Plug · damagedON PRE-DEPARTURE, NR 1 EXHAUST PLUG SUSTAINED DAMAGE. REMOVED EXHAUST PLUG ASSY, INSPECTED AREA, NO CRACKS NOTED ON FLANGE OR ANY DEFECTS. EXHAUST PLUG ASSY INSTALLED IAW MM 78-11-01-01.Apr 25, 2000 · N859FT · Boeing 747123 · Engine Thrust ReverserSDR UPS00432386Oil Cap · missingINSPECTION TYPE:N/A, ON CLIMBOUT NR 4 ENGINE OIL PRESSURE BEGAN TO FLUCTUATE BETWEEN 35 AND 45 PSI. ENGINE OIL PRESSURE 4 LIGHT ILLUMINATED TO CONFIRM, AT 0715Z , NR 4 ENGINE SHUT DOWN WHEN OIL PRESS BELOW RED ARE CONTINUOUSLY AND OIL PRESS LIGHT ON STEADY, WApr 18, 2000 · N683UP · Boeing 747121 · Turbine Engine Oil SystemSDR 0000806601Engine · bird strikeWHILE CLIMBING AT 2000 FT AGL, THE NR 1 ENGINE SUSTAINED A BIRSTRIKE. THE ENGINE COMPRESSOR STALLED AND WAS SHUT DOWN. THE FLIGHT DIVERTED TO MSP LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE AND FOUND EVIDENCE OF BIRD INGESTION. A BOROSCOPE IMar 4, 2000 · N601US · Boeing 747151 · Turbine Engine Compressor SectionSDR P5CA0000100Flange · crackedNR 2 ENG S FLANGE CRACKED AT 2 O'CLOCK POSITION. CRACKED WELDED AND CKD WITH FLOURSCENT LIGHT OK PER MM 72-53-11.Feb 7, 2000 · N853FT · Boeing 747122 · Turbine SectionSDR P5CA0000101Flange · brokenNR 2 ENG R FLANGE CRACKED AT 10 O'CLOCK POSITION. CRACKED WELDED CKD WITH FLOURESCENT LIGHT OK PER SRM 72-53-11.Feb 7, 2000 · N853FT · Boeing 747122 · Turbine Section
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