Pratt & Whitney JT8D-7A

Service difficulty reports · 262

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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 = 'JT8D7A'
  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 Y2PA2010102600027Battery Pack · unserviceableDURING PERFORMANCE OF A-1 CHECK, FOUND GALLEY SERVICE DOOR SLIDE EMERGENCY LIGHT INOPERATIVE. BATTERY PACK DISCHARGED. R & R EMERGENCY BATTERY PACK WITH SERVICEABLE. SYS OPERATIONALLY CHECKED GOOD.Oct 26, 2010 · N229DE · Doug DC915F · Emergency LightingSDR Y2PA2010051710008Circuit Breaker · arcedMULTIPLE ELEC FAILURES. A-OVERHEAD PANEL LIGHTS INOPERATIVE. B-MASTER CAUTION TRIGGERED BY PITOT/STALL AND RADIO FAN OFF ANNUN LIGHTS. CAUTION COULD NOT BE RESET AND DIMLY LIT. C-NUMEROUS FUEL BOOST PUMP C/B'S TRIPPED. D-RADAR INOP, BLACK SCREEN. E-GPS-1 INMay 15, 2010 · N166DE · Doug DC915F · AC Power Distribution SystemSDR ABXA060285Light · inoperativeDURING MAINTENANCE PRE-DEPARTURE CHECK, FOUND EMERGENCY LIGHTS WOULD NOT ILLUMINATE. RESET EMERGENCY ARM AND CHARGE 5 AMP CIRCUIT BREAKER ON OVERHEAD PANEL AND RESET EMERGENCY LIGHT CHARGING 5 AMP CIRCUIT BREAKER AT LOCATION Z32. EMERGENCY LIGHTS TEST GOOD IAOct 30, 2006 · N989AX · Doug DC932 · Emergency LightingSDR UPS06448619Floorbeam · corrodedINSPECTION TYPE-C M/D BS 2260 RBL13-20 FLOORBEAM FOUND CORRODED. CORROSION BLEND OUT 0.023 INCH X 2 INCHES X 2 INCHES EXCEED SRM LIMIT. M/D BS 2260 LBL 8 TO RBL 66 FLOORBEAM REPAIRED IAW SRM 51-40-04 FIG 1.Oct 20, 2006 · N677UP · Boeing 747123F · Fuselage Main, Floor BeamSDR UPS06448245Terminal · corrodedINSPECTION TYPE: N/A, SMOKE SMELLS, ABOUT 1:30 INTO FLIGHT. FOUND COPILOT WINDSCREEN CONNECTION AT LOWER RT SIDE SMOKING SECURED RT 1 OVERHEAD WINDOW HEAT, SMOKE STOPPED. FOUND R1 WINDOW HEAT POWER TERMINAL (A) LOOSE AT CORRODED. CLEANED, RETORQUED AT PERFORMOct 15, 2006 · N676UP · Boeing 747123 · Windshield/Door Rain/Ice RemovalSDR ABXA050242Battery · inoperativeOVERHEAD COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES IAW AMM 33-53-00-8.Oct 4, 2005 · N988AX · Doug DC932 · Emergency LightingSDR 2005FA0001197Rod End · brokenON AUGUST 5TH, DURING THE FLIGHT CONTROL RIGGING OPERATION, THE LT AILERON IB PCU ROD END WAS FOUND BROKEN. THIS ROD END IS PART OF THE BENDIX PCU PN 317012-1 ASSEMBLY. EVIDENCE OF CORROSION IS APPARENT AT CRACKED LOCATION. UNKNOWN TIME.Aug 5, 2005 · N145UA · Boeing 747SP21 · Aileron Control SystemSDR 72400003Seat Track · corroded1 X 1 AREA OF CORROSION SEAT TRACK.Jun 20, 2005 · N724CK · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 72400001Frame · cracked2 INCH CRACK ON FUSE FRAME CHORD REPLACEMENTJun 19, 2005 · N724CK · Boeing 727225 · Fuselage Main, FrameSDR 72400002Frame · cracked1 INCH CRACK ON FRAME REPLACEMENTJun 19, 2005 · N724CK · Boeing 727225 · Fuselage Main, FrameSDR P5CA0401239Beam · crackedBULK CARGO COMPT, LONGITUDNAL BEAM AT STA 2040-2060-2080 LBL 30 IS CRACKED. REMOVED DAMAGE SECTION, FABRICATED NEW PART & INSTALLED PER SRM 51-40-04.Oct 1, 2004 · N858FT · Boeing 747123 · Fuselage Main, Longeron/StringerSDR ABXA040292Longeron · corrodedLONGERON 24 RT END CAP AT STA 945 WAS CORRODED. REPLACED END CAP IAW SRM 51-30-2 AND 51-30-5.Aug 5, 2004 · N988AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA040287Pan · crackedFORWARD LOWER CARGO DOOR OUTER PAN CRACKED AT FASTENER HOLE AT UPPER FORWARD CORNER. REPLACED FORWARD LOWER CARGO DOOR ON N.R. 0399 IAW DC-9 SRM.Aug 4, 2004 · N988AX · Doug DC932 · Cargo/Baggage DoorsSDR ABXA040288Pan · crackedFORWARD LOWER CARGO DOORS OUTER PAN HAD CRACK INDICATION IN OUTER RADIUS OF FORWARD HINGE. REPLACED DOOR ON NR 0399 IAW SRM.Aug 4, 2004 · N988AX · Doug DC932 · Cargo/Baggage DoorsSDR ABXA040289Pan · defectiveFORWARD LOWER CARGO DOOR HAD DEFECT INDICATION IN OUTER PAN ALONG UPPER EDGE AT FORWARD STOP PAD AREA. REPLACED DOOR ON NR 0399 IAW SRM.Aug 4, 2004 · N988AX · Doug DC932 · Cargo/Baggage DoorsSDR ABXA040290Pan · crackedFORWARD LOWER CARGO DOORS OUTER PAN WAS CRACKED AT HI-LOCK ALONG AFT EDGE, CENTER STOP PAD AREA. REPLACED DOOR ON NR 0399 IAW SRM.Aug 4, 2004 · N988AX · Doug DC932 · Cargo/Baggage DoorsSDR ABXA040291Skin · corrodedFORWARD LOWER CARGO DOORS EXTERIOR SKIN HAD PITTING, CORROSION AT AFT LOWER CORNER. REPLACED DOOR ON NR 0399 IAW SRM.Aug 4, 2004 · N988AX · Doug DC932 · Cargo/Baggage DoorsSDR ABXA040284Frame · crackedRT MAIN FRAME STA 699 WAS CRACKED IN FORWARD UPPER FLANGE BETWEEN Z-CLIP FASTENERS. REPAIRED MAIN FRAME RT 699 IAW EA 53400120-001-1.Aug 3, 2004 · N988AX · Doug DC932 · Fuselage Main, FrameSDR ABXA040285Longeron · crackedLONGERON 4 LT CRACKED AT FS 160 SPLICED SECTION OF LONGERON IAW SRM 53-02.Aug 3, 2004 · N988AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA040286Beam · crackedAFT LOWER CARGO DOOR BEAM NR 1 BOTH FORWARD AND AFT END FITTINGS CRACKED. REPLACED FITTINGS S914025-501 AND 3914025-502 IAW SRM 51-30-1 AND 51-30-5.Aug 3, 2004 · N988AX · Doug DC932 · Fuselage Main, StructureSDR ABXA040283Skin · crackedFUSELAGE SKIN CRACKED AT RIVET ON LONGERON 22 LT BETWEEN FS 180-200. REPAIRED ON EA 53300031-001.Aug 3, 2004 · N988AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA040282Skin · corrodedBULGE IN FUSELAGE SKIN AT CABIN OUTFLOW NOZZLE. REPLACED SECTION OF LONGERON FROM APPROXIMATELY STA. 955-990 IAW SRM.Aug 2, 2004 · N988AX · Doug DC932 · Fuselage Main, Plate/SkinSDR CA040120008Rib · cracked(CAN) DURING C CHECK,THE INSPECTION OF THE HORIZONTAL STABILIZER, REVEALED A CRACK ON THE ELEVATOR HINGE SUPPORT RIB ON THE RT SIDE AT STATION 136.5.Jan 20, 2004 · Boeing 727171C · Horizontal Stabilizer, Spar/RibSDR CA040120009Block · worn(CAN) DURING C CHECK, ONE RUB BLOCK (P/N 69-31604-4) WAS FOUND LOOSE ON THE LOWER BEAM. AFTER REMOVAL OF THE BLOCK, IT WAS FOUND THAT THE LOWER BEAM WAS WORN OUT OF LIMIT AT THE PLACE WHERE THE RUB BLOCK WAS INSTALLED. THE LOWER BEAM HAS TO BE REPLACED.Jan 20, 2004 · Boeing 727171C · Horizontal Stabilizer StructureSDR CA030127006Rib · cracked(CAN) DURING INSPECTION OF THE HORIZONTAL STABILIZER TRAILING EDGE RIBS, IN ACCORDANCE WITH AD 2002-12-13 AND BOEING SB 727-55A0091 A CRACK WAS FOUND ON THE UPPER OUTBOARD FLANGE OF THE FITTING AT ELEVATOR STATION 66.50 RT. THE CRACK WAS REPORTED TO BOEING SERJan 17, 2003 · Boeing 727171C · Horizontal Stabilizer, Spar/RibSDR CA021217010Starter · making metal(CAN) DURING B CHECK INSPECTION OF ENGINE A METAL FRAGMENT WAS FOUND ON THE MAGNETIC CHIP PLUG OF THE NR 2 ENGINE STARTER. THE STARTER WAS CHANGED OUT AND THE AIRCRAFT RETURNED TO SERVICE. THE STARTER WILL BE SENT FOR EVALUATION.Nov 26, 2002 · Boeing 727171C · Engine StarterSDR CA020808004Csd · failed(CAN) DURING CRUISE NR 3 ENGINE GENERATOR TRIPPED - CSD OIL PRESSURE WAS LOW AND TEMP HIGH, DISCONNECT FAILED. ENGINE SHUTDOWN AS A PRECAUTION. AIRCRAFT LANDED WITHOUT INCIDENT, YEG AIRPORT RESCUE WAS IN ATTENDANCE BUT NO ACTION WAS TAKEN OR REQUIRED. CSD WASJul 29, 2002 · Boeing 727171C · AC Generator-AlternatorSDR MVI2001F00000Shaft · shearedAFTER NORMAL APPROACH WITH A GO AROUND FROM 501 AGL, FULL ENGINE POWER WAS ATTAINED ON ALL ENGINES. AT 700 FT, FE NOTED EPR ROLLBACK ON NR 3 ENGINE. ENGINE SUBSEQUENTLY WOULD NOT RESPOND TO POWER SETTINGS AND WAS SHUTDOWN. INSPECTION FOUND FUEL PUMP DRIVE SNov 28, 2001 · N40 · Boeing 72725C · Engine Fuel PumpSDR CA010529018Nut · cracked(CAN) LT MAIN GEAR OLEO WOULD NOT HOLD AIR CHARGE. OLEO FOUND LOW SEVERAL TIMES AND RECHARGED. UPON INVESTIGATION IT WAS FOUND THAT THE RETAINING NUT FOR THE UPPER OLEO SUPPORT TUBE WAS CRACKED, CAUSING AIR LEAKAGE. FURTHER INVESTIGATION ALSO REVEALED CORROSIOApr 29, 2001 · Boeing 72722C · Main Landing Gear Strut/Axle/TruckSDR EIA2001015Engine · failedKFAR - RIGHT ENGINE FAILED IN FLIGHT. (M)Mar 14, 2001 · N916F · Doug DC915F · Engine (Turbine/Turboprop)SDR CA010305022Engine · failed(CAN) CREW NOTICED THAT NR 3 ENGINE OIL PRESSURE AND QUANTITY WERE DECREASING. ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO YHM. UPON MAINTENANCE TROUBLESHOOTING IT WAS FOUND THAT ENGINE WOULD NOT CONTAIN ENGINE OIL. TAIL PIPE WAS WET AND UPON INVESTIGATION BFeb 21, 2001 · Boeing 727227 · Engine (Turbine/Turboprop)SDR CA001016005Shaft · failed(CAN) DURING CRUISE FLIGHT NR 3 ENGINE GENERATOR INDICATED UNDER EXCITATION FOLLOWED BY UNDER VOLTAGE THEN A FIELD TRIP. THE RESIDUAL VOLTAGE WAS BELOW MINIMUM AS SUCH THE CSD WAS DISCONNECTED AND THE ELECTRICAL BUSS LOADS WERE REDUCED. THE GENERATOR WAS FOUNDSep 15, 2000 · Boeing 727171C · AC Generator-AlternatorSDR AU000541Mount · failed(AUS) NR 2 SPOILER ACTUATOR MOUNT ASSEMBLY INBOARD LOWER MOUNT BOLT HOLE LUG CRACKED AND OUTBOARD LOWER MOUNT BOLT HOLE LUG BROKEN.INBOARD LOWER MOUNT BOLT SHEARED.Jul 13, 2000 · Boeing 72777C · Drag Control SystemSDR CA000427016Lock · galled(CAN) CARGO DOOR ACTUATOR FOUND TO HAVE HIGH RELEASE FORCES FROM INTERNAL LOCKS. TEARDOWN REPORT INDICATES LOCKING RING, KEYS WORN AND GALLED. LPCK POSITION TEFLON BACKUP RINGS TWISTED, DEFORMED, LOCKRAM ALSO WORN AND GALLED. REPLACED.Apr 18, 2000 · Boeing 727171C · Cargo/Baggage DoorsSDR CA000209047Panel · missing(CAN) ON ARRIVAL FOUND RT ENG UPPER COWL OVERPRESSURE RELIEF PANEL MISSING. INSTALLED.Jan 21, 2000 · Doug DC932 · Engine Cowling SystemSDR CA000209045Receptacle · failed(CAN) DURING TAXI BURNING SMELL NOTED AND TRACED TO GALLEY OVEN. A/C RETURNED. GALLEY OVEN RECEPTACLE AT FAULT REPLACED.Jan 13, 2000 · Doug DC932 · Buffet/GalleysSDR CA000209044Spacer · cracked(CAN) FRONT COMPRESSOR ROTOR THIRD TO FORTH STAGE SPACER WAS FOUND CRCKED, ONE CRACK EXTENDED FROM TIEROD SLEEVE HOLES TO INSIDE DIAMETER. REPORT TO FOLLOW. THE CRACK WAS VERY TIGHT WHICH HAD NOT TRAVELLED OUT OF THE TIE ROD HOLES WALL. THE ITEM WAS FOUND DURRJan 13, 2000 · Doug DC932 · Turbine Engine Compressor SectionSDR CA991231034Seat · damaged(CAN) CAPTAINS CHAIR FAILED TO LOCK FORE AND AFT. CHAIR REPLACED.Nov 30, 1999 · Doug DC932 · Flight Compartment EquipmentSDR CA991210062Outflow Valve · inoperative(CAN) CABIN AUTO PRESSURIZATION SYSTEM INOPERATIVE. REPLACED OUTFLOW VALVE.Nov 24, 1999 · Doug DC932 · Pressure Regulator/Outflow ValveSDR CA991210061Controller · failed(CAN) ON DESCENT AT 8,000 FEET, CABIN PRESSURE AUTO FAIL LIGHT CAME ON AND CABIN WAS CLIMBING AT 2,000 FEET PER MINUTE. REPLACED NR 2 CABIN PRESSURE CONTROLLER.Nov 22, 1999 · Doug DC932 · Cabin Pressure ControllerSDR CA991210063Duct · failed(CAN) CREW REPORTED LACK OF OXYGEN AND DIZZEYNESS. LT WATER SEPARATOR AFT DUCT REPLACED. SYSTEM SERVICEABLE.Nov 22, 1999 · Doug DC932 · Air Distribution SystemSDR CA991231032Windshield · arced(CAN) DURING RAMP CHECK OBSERVED ARCING AND SMOKE AT TOP OF CENTER OF FIRST OFFICERS WINDSCREEN. RT WINDOW AND HEAT CONTROLLER REPLACED.Nov 21, 1999 · Doug DC932 · Flight Compartment WindowsSDR CA990927085Panel · cracked(CAN) LEFT TRAPEZOIDAL PANEL FLANGE CRACKED ALONG FORWARD UPPER HORIZONTAL OUTER FLANGE. REPAIRED.Aug 19, 1999 · Doug DC932 · Fuselage Main, Plate/SkinSDR AU990778Skin · delaminated(AUS) LEFT ELEVATOR TRAILING EDGE INBOARD SKIN DELAMINATED FOR APPROXIMATELY 50.8 MM (2 INCHES).Aug 7, 1999 · Boeing 72777C · Elevator, Plate/SkinSDR CA990715042Thermovalve · failed(CAN) ON TAKEOFF, TEMP 8C UNABLE TO ACHIEVE TAKEOFF EPR OF 1.99 ON RT ENGINE EPR 1.94 WITH RT THROTTLE FIRE WALLED. ALL OTHER PARAMETERS MATCHED. EPR PROBLEMS SEEM ASSOCIATED WITH USE OF ENGINE ANTI-ICE. RT NOSE COWL THERMOSTAT VALVE REPLACED. EPR TP2 ANDJul 4, 1999 · Doug DC932 · Air Intake Anti/De-Ice SystemSDR CA990715040Rudder Peddle · cracked(CAN) CAPTAIN'S RUDDER PEDAL ATTACH BRACKET CRACKED. FAA AD 89-14-02 REPLACED.Jul 1, 1999 · Doug DC932 · Rudder Control SystemSDR CA990715036Connector · loose(CAN) AT FL 330 AFTER SELECTION OF AIRFOIL ANTI-ICE TAIL ANTI-ICE WITH ENG ANTI-ICE ON, CABIN ALT CLIMBED TO 10,000 FEET. AIRFOIL ANT-ICE SELECTED OFF AND DESCENT INITIATED. AT 29,000 FEET,CABIN STARTED A 500 FOOT CLIMB RATE. FOUND DUCT CONNECTOR ADRIFT AT Jun 25, 1999 · Doug DC932 · Air Distribution FanSDR CA990719034Bracket · cracked(CAN) FIRST OFFICER'S RUDDER PEDAL ATTACH BRACKET CRACKED. REPLACED. REFER TO FAA AD 89-14-02.Jun 23, 1999 · Doug DC932 · Aileron Control SystemSDR AU990736Wire · damaged(AUS) SEVEN ELECTRICAL CABLES DAMAGED AT THE OUTER INSULATION JACKET. NO EVIDENCE OF EXPOSED CONDUCTORS.Jun 18, 1999 · Boeing 72777C · Electrical Power System WiringSDR AU990774Skin · corroded(AUS) ELEVATOR SKIN CORRODED AT STN 40, STN 73, STN 84, STN 106 AND STN 166. RT STABILIZER UPPER SKIN ABOVE REAR SPAR CONTAINED FIVE AREAS OF REPAIR.May 26, 1999 · Boeing 72777C · Elevator, Plate/Skin
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