Pratt & Whitney JT8D-1

Service difficulty reports · 195

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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 = 'JT8D1'
  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 YYFA201000007Pa System · inoperativePA SYSTEM INOPERATIVE.Apr 14, 2010 · N836NK · Doug MD83 · Interphone/Passenger Announcement (PA) SystemSDR FDEA201004141180Fire Loop · false activationAFTER T/O NR 1 ENG FIRE LIGHT ON NR 1 FIRE DETECT LOOP. POWER REDUCED ON NR 1 ENG IAW QRH. NR 1 FIRE LIGHT WENT OUT. FIRE DETECT LIGHT REMAINED ON. FIRE DETECT LIGHT OUT WHEN FIRE HANDLE PULLED. NO OTHER ABNORMAL INDICATIONS NOTED. TRACKING NR 10-1182.Apr 14, 2010 · N278FE · Boeing 727233 · Fire DetectionSDR DALA107779865Battery Pack · inoperativePRIOR TO FLIGHT, THE FLIGHT CREW FOUND THAT THE EMERGENCY LIGHTS IN THE FLIGHT DECK AND GALLEY WOULD NOT ILLUMINATE WHEN THE EMERGENCY LIGHTS SWITCH WAS PLACED IN THE ON POSITION. MX REPLACED THE BATTERIES IN BATTERY PACK B5-23 AND THE SYS OPERATED NORMALLY THApr 13, 2010 · N774NC · Doug DC951 · Emergency LightingSDR YYFA2010000021Interphone · intermittentCOCKPIT TO CABIN INTERPHONE INTERMITTENT.Apr 10, 2010 · N836NK · Doug MD83 · Interphone/Passenger Announcement (PA) SystemSDR YYFA201000006Pa System · inoperativeF/A PA SYS IS NOT WORKING IN FLIGHT.Apr 8, 2010 · N836NK · Doug MD83 · Interphone/Passenger Announcement (PA) SystemSDR DALA106839974Fuse · failedDURING A POWER SURGE, THE F/A REPORTED THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN DID NOT ILLUMINATE AS DID THE COACH CLASS SECTION OF THE CABIN. MX CONFIRMED THAT THE 1ST CLASS EMERGENCY LIGHT WAS INOPERATIVE AND DISCOVERED AMar 30, 2010 · N9338 · Doug DC931 · Emergency LightingSDR YYFA201000003Pa System · inoperativePA NOT WORKING PROPERLY IN FLIGHT BUT WORKING ON THE GROUND. UNABLE TO MAKE ANNOUNCEMENTS, VOLUME TOO LOW IN ALL HANDSETS.Mar 22, 2010 · N836NK · Doug DC983 · Interphone/Passenger Announcement (PA) SystemSDR MWE2008F00024Csd · overservicedRT CSD OUTLET TEMPERATURE WAS IN YELLOW ARC AND RISING. FOUND RT CSD WAS OVERSERVICED, DRAINED CSD TO PROPER LEVEL. (K)Jul 24, 2008 · N814ME · Doug DC981 · Alternator-Generator DriveSDR ASMF200803003Switch · burnedAIRCRAFT RETURNED TO PLATFORM DUE TO SMOKE IN THE CABIN. MAINTENANCE DETECTED A SHORT CIRCUIT IN THE LT ENGINE SYS (A) IGNITION SWITCH, SO BREAKERS K-26 AND L26 WERE PULLED OUT AND AC WAS SENT TO THE HANGAR. AT HANGAR, SWITCH S1-35 WAS DETECTED BURNED SO IT WAMar 30, 2008 · N583MD · Doug DC983 · Ignition SystemSDR 06FDEA00031Skin · crackedLFEC SHOWS CRACK INDICATIONS AT MCD DOUBLER LOWER FASTNER ROW BS 523, 524, 525 BETWEEN STR 27L AND 28L. COMPLIED WITH FED EX EA 7-5330-95979.Jan 5, 2006 · N490FE · Boeing 727200 · Cargo/Baggage DoorsSDR 05FDEA03554Skin · damagedFOUND FORWARD CARGO DOOR HAS MULTIPLE SCRATCHES ON EXTERIOR SKIN IN THE UNPAINTED AREA. REPAIRED PER E.A. 7-5230-91411.Oct 27, 2005 · N188FE · Boeing 72722 · Cargo/Baggage DoorsSDR 05FDEA03555Skin · damagedFOUND MATERIAL LOSS EXCEEDS 10 PERCENT AT BS 1081 STR 10L. REPAIRED PER E.O. 7-5330-7-2313F PT 5Oct 27, 2005 · N188FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 05FDEA03556Skin · damagedFOUND MATERIAL LOSS EXCEEDS 10 PERCENT AT BS 361 STR 19. REPAIRED PER E.O. 7-5330-7-2319 PT 5Oct 27, 2005 · N188FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 05FDEA03557Skin · damagedFOUND MATERIAL LOSS EXCEEDS 10 PERCENT AT BS 261 STR 14R. REPAIRED PER E.O. 7-5330-7-2319 PT 5Oct 27, 2005 · N188FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 05FDEA03558Skin · damagedFOUND MATERIAL LOSS EXCEEDS 10 PERCENT AT BS 361 STR 10R. REPAIRED PER E.O. 7-5330-7-2319 PT 5Oct 27, 2005 · N188FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 05FDEA03559Skin · damagedFOUND MATERIAL LOSS EXCEEDS 10 PERCENT AT BS 361 STR 10L. REPAIRED PER E.O. 7-5330-7-2319 PT 5Oct 27, 2005 · N188FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 05FDEA03560Floorbeam · corrodedFOUND CORROSION (C53-224-01) ON MAIN CARGO DECK FLOORBEAM UPPER AND LOWER FLANGE AT BS 1130 BETWEEN RBL 25 AND RBL 45, WL 208. REPAIRED MAIN DECK FLOORBEAM UPPER FLANGE AT BS 1130, RBL 45, WL 208 REF SRM 53-10- 8 FIG 10.Oct 27, 2005 · N188FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 05FDEA03487Frame · damagedN00737 FRAME BS 990 BTWN STR 22 LT- 24 LT DAMAGED. [OPEN]Oct 25, 2005 · N188FE · Boeing 727100 · Fuselage Main, FrameSDR ABXA050261Bulkhead · crackedAFT PRESSURE BULKHEAD DOOR UPPER LT CORNER 13 DOUBLER HAD RADIAL CRACK EXTENDING FROM STOP DRILL. CRACK EXCEEDED APPLICABILITY AND CRACK REPAIR LIMITS FOR PREVIOUS J060088-1 ANGLE REPAIR. STOP DRILLED CRACKS AND REPAIRED IAW SRM.Oct 11, 2005 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA050260Skin · corrodedFUSELAGE SKIN BULGED AT STA 579, LONERON 30, EVIDENCE OF CORROSION INTERNAL. REMOVED INTERNAL CORRODED DOUBLER / INSTALLED NEW DOUBLER IAW SRM.Oct 10, 2005 · N962AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ASMF200510001Outflow Valve · failedCAPTAIN REPORTED THE PRESSURIZATION VERY UNSTABLE, NOT POSSIBLE TO PRESSURIZE AIR CONDITIONING PACKAGES. THE CABIN PRESSURE CONTROL WAS RESEATED IAW MM 21-32-04. LATER, AIRCRAFT RETURNED TO PLATFORM, PNEUMATIC LEAK ON RT AIR CONDITIONING. THE RUBBER HOSE BETWOct 1, 2005 · N861LF · Doug MD83 · Pressure Regulator/Outflow ValveSDR ASMF200509014Valve · failedCAPTAIN REPORTED, DURING FLIGHT, THE F/O RMI CHANGED HEADING, BEING NECESSARY TO ADJUST CONTINUOUSLY. DURING REVISION, DETECTED A DIFFERENCE OF 20 GRADES BETWEEN COURSES. THE LT FLUX VALVE NR 1 WAS REPLACED IAW MM, SYNCHRONY TEST WAS PERFORMED IAW MM, BEING SASep 24, 2005 · N831LF · Doug MD83 · Attitude Gyro and Indicating SystemSDR GTIA050073Smoke · detectedDURING TAXI, AFT FLIGHT ATTENDANT REPORTED SMOKE IN THE AFT CABIN, ENTIRE AIRCRAFT SMELLED LIKE AN OVERHEATED PACK, GATE RETURN. OPS CHECKED RT AUTO-TEMP. NO DEFECTS NOTED, OPS CHECKED GOOD. (K)Mar 21, 2005 · N836NK · Doug DC983 · Air Distribution SystemSDR 2006FA0000814Frame · damagedDURING SCHEDULE INSP REQUIRED BY AD, FOUND 8.5 WEB SEPARATION AT FUSELAGE BS 950, RT BETWEEN STRINGER S-9 AND S-10. PARTIAL FRAME REPLACEMENT BETWEEN S-9 AND S-12 WAS ACCOMPLISHED. INSTALLED KIT NR 65C35283-2. ALL WORK DONE IAW DWG, SRM, SB, AND AD. (K)Jan 11, 2005 · N727PX · Boeing 72721 · Fuselage Main, FrameSDR C7WA200400073Sensing Element · erraticIN FLIGHT, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED, RT DUCT PRESSURE INDICATED 80 PSI. MADE PRECAUTIONARY LANDING. TIGHTENED ALL CLAMPS IN AIRSTAIR AREA. REPLACED LT AND RT PURGE LINE COUPLING SEALS. REMOVED AND REPLACED LOWER AFT BODY OVERHEAT LOOP DETEJan 7, 2005 · N7638U · Boeing 727222 · Overheat DetectionSDR C7WA200400072Warning Light · illuminatedLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED THEN EXTINGUISHED ON ITS OWN INFLIGHT. INSPECTED DUCTING IN AFT AIRSTAIR AREA AND RAN ENGINES AT TAKEOFF POWER. UNABLE TO DUPLICATE PROBLEM, NO LEAKS NOTED. SYSTEM OPERATIONAL, CHECK GOOD IAW MM. (K)Jan 7, 2005 · N7638U · Boeing 727222 · Overheat DetectionSDR GTIA040848Lanyard · misroutedR1 SLIDE GIRT BAR SLIDE PACK LANYARD NOT ROUTED PROPERLY. RE-ROUTED R1 SLIDE GIRT BAR LANYARD.Nov 16, 2004 · N836NK · Doug DC983 · Escape SlideSDR GTIA040846Selector · dirtyLP NR 3022501; DEPARTING DCA AFTER GEAR RETRACTION, ALL 3 RED UNSAFE LIGHTS REMAINED ILLUMINATED, GEAR DOOR LIGHT EXTINGUISHED. ACCOMPLISHED QRH PROCEDURE WITH NO CHANGE IN INDICATIONS. ACP BITE CHECK OF PSEU, CLEANED LANDING GEAR HANDLE SWITCH S1-89 AND THRNov 12, 2004 · N830NK · Doug DC982 · Landing Gear SelectorSDR GTIA040815A/C Pack · malfunctionedCABIN FILLED WITH SMOKE WHEN APU AIR WAS TURNED ON. FOUND RT PACK, DID AN AUTO SHUTDOWN. WHEN RT PACK COOLED DOWN, RAN LT AND RT PACK FOR 90 MINUTES. NO SMOKE AT THIS TIME. CHANGED LT AND RT COALESCER SOCKS FOR COMPANY CONV. WORK DOWN IAW MM 21-20-02. OPOct 19, 2004 · N836NK · Doug DC983 · Cabin Cooling SystemSDR GTIA040814Landing Gear · unknownAFTER TAKEOFF, LT MAIN RED GEAR REMAINED ON WITH GEAR HANDLE UP. FOLLOW QRH PROCEDURE. ADVISED DISPATCH FOR FUEL BURN AND CONSULTED WITH MECHANIC CONTROL. CONTINUED TO ACY AT REDUCED SPEED AND ALT. CHECKED GEAR UP AND DOWN PROX SENSORS WIRING RESISTANCE IAOct 19, 2004 · N829NK · Doug DC982 · Main Landing GearSDR ASMF200407009Servo Valve · leakingDURING TRANSIT CHECK, HYDRAULIC LIQUID LEAK WAS DETECTED ON RT MAIN LANDING GEAR WELL, BOTH SYSTEMS WERE PRESSURIZED, BRAKES AND CONTROL SURFACES WERE ACTUATED AND LEAK WAS DETECTED ON ANTI-SKID RT DOUBLE SERVO VALVE. SERVO VALVE WAS REPLACED IAW MM 32-43-02, Jul 5, 2004 · N205AM · Doug DC987 · Hydraulic System, MainSDR ASMF200407007Extinguisher · activatedDURING TRANSIT CHECK, CAPTAIN REPORTED (EXTINGUISHER AGENT NR 1) LIGHT TURNED ON. FIRE EXTINGUISHER WAS DETECTED ACTIVATED BY HIGH TEMPERATURE IN TAIL CONE AND COMPRESSOR CLAMP WAS LOOSEN. FIRE EXTINGUISHER AND CLAMP WERE REPLACED IAW MM 26-20-00, LEAKS TEST CJul 3, 2004 · N205AM · Doug DC987 · Fire Bottle, FixedSDR ASMF200406032Cadc · failedCAPTAIN REPORTED THAT DURING CRUISE AT 35,000 FEET, VERTICAL VELOCIMETER BAR FD TRI WAS OUT OF SERVICE AND CADC ABNORMAL PROCEDURE WAS PERFORMED. DURING TRANSIT CHECK AT TIJ, PITOTS AND STATIC PORTS WERE CHECKED BY OVERHEAT AND NO DAMAGE WAS DETECTED. PITOTS AJun 27, 2004 · N583MD · Doug DC983 · Pitot/Static SystemSDR ASMF200406030Selector Switch · failedAIRCRAFT RETURNED TO PLATFORM, APU OUT OF SERVICE AND ENGINE GENERATORS WITHOUT INDICATION OF VOLTAGE AND FREQUENCY. CIRCUIT BREAKERS B1-204, B1-205 AND B1-206 WERE CHECKED AND SWITCH SELECTOR S1-99 WAS REPLACED IAW MM 24-21-01, TEST CORRECT.Jun 26, 2004 · N583MD · Doug DC983 · AC Generator-AlternatorSDR AALA20040591Battery Pack · dischargedDFW CEILING EMERGENCY LIGHTS AT ROWS 3 THROUGH 6 INOPERATIVE. REPLACED BATTERY PACK AT B5100 FOR CEILING EMERGENCY LIGHTS AT ROWS 3 THROUGH 6. SYSTEM GROUND CHECKED NORMAL OPERATION.May 26, 2004 · N70504 · Doug DC982 · Emergency LightingSDR 04FDEA01447Connector · disconnectedDURING DESCENT AT FL 280 NR 2 ENGINE OIL TEMP INCREASED TO 135, FOLLOWED QRH PROCEDURES FOR HIGH OIL TEMP, OIL TEMP REMAINED IN YELLOW BAND. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN AFTER 15 MINUTES WITH OIL TEMP STILL IN YELLOW BAND. NR 2 ENGINE WAS SHUTDOWNMay 25, 2004 · N281FE · Boeing 727200 · Fuel HeaterSDR ABXA040184Drag Link · malfunctionedNOSE GEAR WOULD NOT EXTEND WHEN GEAR LEVER WAS PLACED DOWN. FOLLOWED ABNORMAL AND PULLED EMERGENCY GEAR EXTENSTION LEVER. NOSE GEAR EXTENDED AND LOCKED. RESET HANDLE. REPLACED RT NOSE LANDING GEAR DOOR HINGES IAW SRM 51-30-1 AND ADJUSTED NOSE LANDING GEAR DOOMay 21, 2004 · N958AX · Doug DC941 · Landing Gear Retraction/Extension SystemSDR 278229Accessory Unit · inoperativeDURING CLIMB, EXPERIENCED MULTIPLE WARNINGS FOR UNSAFE RT MAIN GEAR. ALTITUDE WARNING HORN SOUNDED AT 2000 FT, INADDITION TO WINDSHEAR LIGHT AND STICK SHAKER (NO SHEAR NOTED). AIRCRAFT RETURNED TO MSY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LANDINMay 18, 2004 · N7638U · Boeing 727222 · Landing Gear Retraction/Extension SystemSDR DL73S040432Floorbeam · crackedCRACKS WERE NOTED IN THE BS520 FLOORBEAM UPPER RADII WHERE THE SEAT TRACKS CROSS OVER THE BEAM. DAMAGE WAS REMOVED AND THE FLOORBEAM REPAIRED IAW ERA 089860-14.May 13, 2004 · N245WA · Boeing 737247 · Fuselage Main, Floor BeamSDR DL73S040433Fitting · corrodedDURING ACCOMPLISHMENT OF EO 3-085220-03, CORROSION DAMAGE WAS NOTED WHICH EXCEEDED THE ALLOWABLE LIMITS OF THE SUBJECT EO ON THE NR 6 AND NR 12 LUGS LOCATED AT BS 1088. CORROSION REMOVED AND DAMAGE REWORKED IAW ERA 089944-14.May 13, 2004 · N245WA · Boeing 737247 · Fuselage Miscellaneous StructureSDR DL73S040435Keelbeam · corrodedFUSELAGE KEEL LT LOWER CHORD FS 727A SPLICE. THE LT LOWER KEEL CHORD WAS FOUND WITH CORROSION AT THE FACTORY SPLICE LOCATION AT FS 727A. THE CORROSION WAS REMOVED WITH CUTOUTS IN THE CHORD FLANGES AND LOCAL BLENDS. THE REMOVED MATERIAL WAS REPAIRED WITH ALUMMay 13, 2004 · N245WA · Boeing 737247 · Fuselage Main, KeelSDR ABXA040183Link · damagedAIRCRAFT VIBRATES AT 320 KTS AT LOW ALTITUDE CLIMB AND CRUISE REGARDLESS OF POWER SETTINGS. REPLACED RT WING TO STRUCTURE TRAILING LINKS AND HARDWARE DUE TO EXCESSIVE MOVEMENT IAW MM 20-10, 20-15 & 20-16.May 11, 2004 · N962AX · Doug DC941 · Aerodynamic FairingsSDR GTIA040421Light · broken5 EA EMERGENCY LIGHTS BROKEN IN AFT STAIRWELL. REMOVED BROKEN LIGHTS. INSTALL 5 EA NEW LIGHTS.Apr 20, 2004 · N817NK · Doug DC982 · Emergency LightingSDR GTIA040422Light · brokenEMERGENCY LIGHT AT L1 DOOR HOLDER IS BROKEN. REMOVED EMERGENCY LIGHT. INSTALLED SERVICEABLE EMERGENCY LIGHT.Apr 20, 2004 · N817NK · Doug DC982 · Emergency LightingSDR GTIA040419Longeron · corrodedAFT PIT LONGERON 30 STA 1236 HAS CORROSION UNDER LIP IN RADIUS. REMOVED DAMAGED LONGERON FROM STA 1236-1309. FABRICATED NEW LONGERON. INSTALLED LONGERON.Apr 11, 2004 · N817NK · Doug DC982 · Fuselage Main, Longeron/StringerSDR GTIA040420Longeron · corrodedAFT PIT STA 1256 LONGERON 28R CORROSION UNDER LIP OF LONGERON. REMOVED DAMAGED LONGERON FROM STA 1255-1338. FABRICATED NEW LONGERON. INSTALLED LONGERON.Apr 11, 2004 · N817NK · Doug DC982 · Fuselage Main, Longeron/StringerSDR GTIA040462Longeron · corrodedAFT PIT LONGERON 29L AT STA 1193 HAS CORROSION UNDER LIP AT HI LOC ATTACH POINT. REMOVED SECTION OF LONG 29L FROM FS 1127-1202. FABRICATED NEW LONGERON. FABRICATED NEW LONGERON SPLICE. INSTALLED STRINGER SPLICE. INSTALLED LONGERON SECTION.Apr 11, 2004 · N817NK · Doug DC982 · Fuselage Main, Longeron/StringerSDR GTIA040459Skin · corrodedAFT CARGO FS 1022-1034, SKIN HAS CORRODED AT SKIN JOINT. REMOVED SPLICE DOUBLER FROM EXTERNAL SKIN. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN SPLICE AND DOUBLER. FABED FINGER DOUBLERS. INSTALLED NEW SKIN SPLICE AND DOUBLER AND FINGER DOUBLERS.Mar 26, 2004 · N817NK · Doug DC982 · Fuselage Main, Plate/SkinSDR GTIA040457Skin · corrodedRT SIDE FUSELAGE JUST AFT OF AFT CARGO DOOR WATER WASTE DRAIN AND SURROUNDING SKIN CORRODED. CUT OUT DAMAGED AREA. FABED DOUBLER. FABRICATED INTERNAL DOUBLER. FABRICATED FILLER. INSTALLED DOUBLERS AND FILLER.Mar 22, 2004 · N817NK · Doug DC982 · Fuselage Main, Plate/SkinSDR GTIA040456Skin · delaminatedLT WING IB FLAP OB VANE DELAMINATED. REMOVED LT IB OB FLAP VANE. INSTALLED VANE.Mar 21, 2004 · N817NK · Doug DC982 · Trailing Edge Flaps
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