Pratt & Whitney JT8D-7A
Service difficulty reports · 262
Newest first. General aviation reporting is voluntary.
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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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.SDR 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 INSDR 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 IASDR 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.SDR 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 PERFORMSDR ABXA050242Battery · inoperativeOVERHEAD COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES IAW AMM 33-53-00-8.SDR 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.SDR 72400003Seat Track · corroded1 X 1 AREA OF CORROSION SEAT TRACK.SDR 72400001Frame · cracked2 INCH CRACK ON FUSE FRAME CHORD REPLACEMENTSDR 72400002Frame · cracked1 INCH CRACK ON FRAME REPLACEMENTSDR 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.SDR ABXA040292Longeron · corrodedLONGERON 24 RT END CAP AT STA 945 WAS CORRODED. REPLACED END CAP IAW SRM 51-30-2 AND 51-30-5.SDR 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.SDR ABXA040288Pan · crackedFORWARD LOWER CARGO DOORS OUTER PAN HAD CRACK INDICATION IN OUTER RADIUS OF FORWARD HINGE. REPLACED DOOR ON NR 0399 IAW SRM.SDR 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.SDR 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.SDR ABXA040291Skin · corrodedFORWARD LOWER CARGO DOORS EXTERIOR SKIN HAD PITTING, CORROSION AT AFT LOWER CORNER. REPLACED DOOR ON NR 0399 IAW SRM.SDR 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.SDR ABXA040285Longeron · crackedLONGERON 4 LT CRACKED AT FS 160 SPLICED SECTION OF LONGERON IAW SRM 53-02.SDR 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.SDR ABXA040283Skin · crackedFUSELAGE SKIN CRACKED AT RIVET ON LONGERON 22 LT BETWEEN FS 180-200. REPAIRED ON EA 53300031-001.SDR ABXA040282Skin · corrodedBULGE IN FUSELAGE SKIN AT CABIN OUTFLOW NOZZLE. REPLACED SECTION OF LONGERON FROM APPROXIMATELY STA. 955-990 IAW SRM.SDR 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.SDR 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.SDR 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 SERSDR 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.SDR 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 WASSDR 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 SSDR 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 CORROSIOSDR EIA2001015Engine · failedKFAR - RIGHT ENGINE FAILED IN FLIGHT. (M)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 BSDR 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 FOUNDSDR 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.SDR 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.SDR CA000209047Panel · missing(CAN) ON ARRIVAL FOUND RT ENG UPPER COWL OVERPRESSURE RELIEF PANEL MISSING. INSTALLED.SDR CA000209045Receptacle · failed(CAN) DURING TAXI BURNING SMELL NOTED AND TRACED TO GALLEY OVEN. A/C RETURNED. GALLEY OVEN RECEPTACLE AT FAULT REPLACED.SDR 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 DURRSDR CA991231034Seat · damaged(CAN) CAPTAINS CHAIR FAILED TO LOCK FORE AND AFT. CHAIR REPLACED.SDR CA991210062Outflow Valve · inoperative(CAN) CABIN AUTO PRESSURIZATION SYSTEM INOPERATIVE. REPLACED OUTFLOW VALVE.SDR 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.SDR CA991210063Duct · failed(CAN) CREW REPORTED LACK OF OXYGEN AND DIZZEYNESS. LT WATER SEPARATOR AFT DUCT REPLACED. SYSTEM SERVICEABLE.SDR CA991231032Windshield · arced(CAN) DURING RAMP CHECK OBSERVED ARCING AND SMOKE AT TOP OF CENTER OF FIRST OFFICERS WINDSCREEN. RT WINDOW AND HEAT CONTROLLER REPLACED.SDR CA990927085Panel · cracked(CAN) LEFT TRAPEZOIDAL PANEL FLANGE CRACKED ALONG FORWARD UPPER HORIZONTAL OUTER FLANGE. REPAIRED.SDR AU990778Skin · delaminated(AUS) LEFT ELEVATOR TRAILING EDGE INBOARD SKIN DELAMINATED FOR APPROXIMATELY 50.8 MM (2 INCHES).SDR 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 ANDSDR CA990715040Rudder Peddle · cracked(CAN) CAPTAIN'S RUDDER PEDAL ATTACH BRACKET CRACKED. FAA AD 89-14-02 REPLACED.SDR 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 SDR CA990719034Bracket · cracked(CAN) FIRST OFFICER'S RUDDER PEDAL ATTACH BRACKET CRACKED. REPLACED. REFER TO FAA AD 89-14-02.SDR AU990736Wire · damaged(AUS) SEVEN ELECTRICAL CABLES DAMAGED AT THE OUTER INSULATION JACKET. NO EVIDENCE OF EXPOSED CONDUCTORS.SDR 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.
Back to Pratt & Whitney JT8D-7A