Pratt & Whitney JT8D-17
Service difficulty reports · 1,680
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 = 'JT8D17' 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 = 'JT8D17' 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 SROM200400042Skin · dentedDURING D CHECK INSPECTION C/W LOG 4755645 REPLACE SKIN PANEL BS 178-259 STR 24R - BLO. REMOVED AND REPLACED SKIN PANEL IAW B737 SRM 51-30-2. PANEL REPLACED TO ELIMINATE PREVIOUS REPAIRS DUE TO DENTS.SDR CA040402006Wire Harness · inoperative(CAN) DURING START UP, IT WAS OBSERVED THAT AC PACK WATER SEPARATOR CB POPPED FOLLOWED BY A PACK TRIP. A BURNING ODRO WAS SENSED. ENGINES WERE SHUTDOWN. MAINTENANCE BEGAN INSPECTION AND COCKPIT LIGHTING BEGAN TO FLICKER. COCKPIT WAS FILLING WITH SMOKE. NRSDR SROM200400043Support Beam · corrodedDURING D CHECK INSPECTION LT MLG SUPPORT BEAM HAS CORROSION IN OB ATTACH HOLE IN BETWEEN BUSHINGS. REMOVED BUSHINGS AND CORROSION. INSPECTED AND INSTALLED REPLACEMENT BUSHINGS IAW MFG EA 5750-01939 AND EA 10537. MINOR REPAIR.SDR SROM200400044Bear Strap · brokenDURING D CHECK INSPECTION BEAR STRAP HAS A HOLE BROKE FROM EDGE (NO E/D) STA 767, STR 18R. TRIMMED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER IAW MFG EA. 5330-01764 AND MFG EA 10311.SDR SROM200400034Doubler · dentedDURING D CHECK INSPECTION FOUND DENT AT STA 338 TO 344 JUST BELOW FWD AIRSTAIR DOOR CUTOUT BEYOND LIMITS IAW SRM 53-30-1 FIG 1 DETAIL 3. REF. SAD LOG 0176053 BEYOND LIMITS DUE TO CHANGES TO SRM INCLUDING PROXIMITY TO CUTOUTS AND SEAMS. REMOVED DAMAGED DOUBLESDR SROM200400033Skin · dentedDURING D CHECK INSPECTION C/W 069 LOG 4755642 REPLACE SKIN PANEL BS 908 - 1016 STR 20L TO 25L. REMOVED SKIN PANEL, RECEIVED AND INSTALLED NEW SKIN PANEL IAW MFG SRM 51-30-2.SDR SROM200400050Bear Strap · damagedDURING D CHECK INSPECTION, BEAR STRAP HAS A HOLE BROKEN FROM EDGE (NO E/D) AT STA 767 AND STR 18R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER IAW ASA EA 5330-01764 AND AAR EA 10311.SDR DHL2004783004Power Drain Vlv · faultyDURING ENGINE START NR 3 ENGINE AUTO ROLL BACK AT 40 PERCENT N2. ATTEMPTED 2ND START PER MAINTENANCE CONTROL, HAD NO FUEL FLOW INDICATION. REMOVED AND REPLACED NR 3 ENGINE FUEL PRESSURE AND DUMP VALVE IAW ASTAR B-727 M/M 73-12-1. ENGINE START IAW ASTAR JRH SDR DHL2004783003Switch · faultyDURING START OF ENGINE NR 3 ENGINE ROLLED BACK AT APPROXIMATELY 40 PERCENT N2. ALL INDICATIONS WERE NORMAL DURING THE FIRST START. ATTEMPTED RESTART, AFTER CONFERRING WITH MAINTENANCE CONTROL (MXC), AND ADVISED TO RESTART. START WAS SUCCESSFUL WITH NO ANOMASDR SROM200400010Stringer Clip · crackedDURING D CHECK INSPECTION FOUND STRINGER TO FRAME CLIP CRACKED AT STA 495-500, STR 24R. REMOVED DAMAGED STRINGER CLIP, FABRICATED AND INSTALLED REPLACEMENT STRINGER CLIP IAW B737 SRM 51-20-1, 51-30-2.SDR SROM200400011Skin · corrodedDURING D CHECK INSPECTION FOUND AFT PIT STA 807 LOWER FORWARD CARGO CUTOUT HAS NON-CPCP CORROSION. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR DOUBLER IAW 53-10-1, 51-40-3 AND 51-30-2.SDR SROM200400015Stringer · elongatedDURING D CHECK INSPECTION FOUND AFT CARGO PIT STRINGER 21R HAC ELONGATED HOLE STA 927. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER CHANNEL SRM 53-10-3.SDR DHL2004781002Wire · brokenENGINE NR 3 OIL TEMPERATURE WENT ABOVE 165 DEGREES CELSIUS, NEEDLE STUCK OFF SCALE HIGH. ACCOMPLISHED ABNORMAL PROCEDURE. OIL TEMPERATURE ABOVE 165 DEGREES CELSIUS FOR 5 MINUTES BEFORE SHUTDOWN OF ENGINE. ACCOMPLISHED IN-FLIGHT FAILURE SHUTDOWN CHECK LIST. SDR SROM200400008Shear Tie · crackedDURING D CHECK INSPECTION FOUND AT STA 747 SHEAR TIE CRACKED AT FASTNER HOLE BETWEEN STR 20L AND 21L. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR SHEAR TIE IAW SRM 53-10-4.SDR SROM200400009Stringer · elongatedDURING D CHECK INSPECTION FOUND AFT CARGO PIT STRINGER 20L HAS SEVERAL ELONGATED FASTNER HOLES AND MULTIPLE CRACK INDICATIONS AROUND HOLES STA 747 TO 887. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR STRINGER AND SPLICES IAW SRM 53-10-3.SDR SROM200400004Stringer Clip · crackedDURING D CHECK INSPECTION FOUND CRACKED STRINGER CLIP AT STA 639, STR 4L. REMOVED DAMAGED CLIP, ORDERED AND INSTALLED NEW CLIP IAW B737 SRM 51-30-2SDR CA040224005Torque Link · cracked(CAN) DURING THE SCHEDULED NOSE LANDING GEAR SEAL CHANGE AT THE C CHECK, A CRACK WAS DISCOVERED AT THE LOWER TORQUE LINK ATTACHMENT LUG. THE FINDING RESULTED IN THE TORQUE LINK BEING REPLACED. NOTE A FLEET CAMPAIGN HAS BEEN ISSUED TO VISUALLY INSPECT ALL TORSDR SROM200400003Shear Tie · damagedDURING D CHECK INSPECTION FOUND SHEAR TIE AT STA 380 BETWEEN STR 20R AND 21R HAS HOLES THAT ARE LARGER THEN SRM LIMITS. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE IAW B737 SRM 51-40-3.SDR SROM200400005Stringer Clip · crackedDURING D CHECK INSPECTION FOUND CRACKED STRINGER CLIP AT STA 639, STR 4R. REMOVED DAMAGED CLIP, ORDERED AND INSTALLED NEW STRINGER CLIP IAW B737 SRM 51-30-2.SDR SROM200400006Stringer Clip · crackedDURING D CHECK INSPECTION FOUND CRACKED STRINGER CLIP AT STA 616, STA 4L. REMOVED DAMAGED CLIP, ORDERED AND INSTALLED NEW STRINGER CLIP IAW B737 SRM 51-30-2SDR SROM200400002Shear Tie · damagedDURING D CHECK INSPECTION FOUND ELONGATED HOLE IN SHEAR TIE AT STA 500 BETWEEN STR 16R AND 17R, FORWARD UPPER HOLE. REMOVED DAMAGED SHEAR TIE. FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE IAW B737 SRM 53-10-4.SDR DHL2004783002Indicator · malfunctionedDURING NR 3 ENGINE START, ENGINE ROLLED BACK AND SHUT ITSELF DOWN. N2 WAS AT 51 PERCENT AT THE TIME, 2ND START WAS NORMAL. INSPECTED INTAKE AND EXHAUST; NO OBVIOUS DEFECTS. SERV FUEL CONTROL BURNER PRESS BELLOWS PER P&W JT8D M/M 73-21-01. DURING ENGINE STASDR SROM200400001Wire · damagedAFT LEFT EMERGENCY EXIT LIGHT UNDER FA JUMP SEAT INOPERATIVE. REPAIRED WIRE TO LIGHT ASSEMBLY. LIGHT OPS NORMAL WITH EMERGENCY LIGHTS TURNED ON.SDR CA040209002Window · cracked(CAN) DURING CLIMB, THE F/O OBSERVED THE R2 SLIDING WINDOW WAS CRACKED. THE DECISION WAS MADE TO RETURN TO BASE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE R2 WINDOW ASSY WAS REPLACED IAW MM 56-12-11 AND CHECKED SERVICEABLE. THE R2 WINDOW HEAT CONTROLLER AND TSDR AUS20040048Door Frame · cracked(AUS) AFT CARGO DOOR CUTOUT FRAME LOCATED AT BS 1090 RIB BL28 CRACKED. CRACK LENGTH 8.255MM (0.325IN).SDR CA040112003Brake Pads · damaged(CAN) DURING TAXI, CREW REPORTED THAT THERE WAS SOME DRAGGING FELT WHEN THE BRAKES WERE APPLIED. THE AIRCRAFT RETURNED TO THE BLOCKS. A DETAILED INSPECTION WAS CARRIED OUT AND NR 4 BRAKE WAS FOUND UNSERVICEABLE. THE BRAKE PADS WERE DAMAGED AND BROKEN. A SERVISDR 04FDEA00020Engine · failedAPPROACHING MAX POWER SETTING (215) FOR TAKEOFF ROLL NR 3 ENGINE FAIL LIGHT ILLUMINATED WITH A LOUD BANG. SUSPECT FAILURE OF NR 3 ENGINE. ENGINE EXPERIENCED TURBINE FAILURE AND IS SITTING IN THE POWERPLANT SHOP AWAITING SHIPMENT TO OVERHAUL FACILITYSDR 0400029860Engine · failedDURING TAKEOFF, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL AND LOSS OF POWER AT 105 KNOTS. FLIGHT CREW ABORTED TAKEOFF. MAINTENANCE FOUND METAL IN THE TAILPIPE. REPLACED THE NR 1 ENGINE.SDR CA040102002Adc · intermittent(CAN) PRIOR TO DEPARTURE THE FLIGHT CREW A MACH AIRSPEED WARNING CLACKER INOPERATIVE ASSOCIATED WITH A FLAG ON THE MACH AIRSPEED INDICATOR. RECTIFICATION THE MACH AIRSPEED INDICATOR WAS REPLACED. HOWEVER THE SNAG RETURNED ON DECEMBER 29. THE SYSTEM WAS PLACEDSDR CA031218008Fitting · broken(CAN) ON WALK AROUND, MAINTENANCE FOUND THE RT OB FOREFLAP OB LINK BROKEN. MAINTENANCE REPLACED THE FOREFLAP AND AIRCRAFT RETURNED TO SERVICE. CAUSE UNKNOWN. WILL UPDATE IF ADDITIONAL INFORMATION AVAILABLE.SDR C1HA200381034Compressor · stalledCOMPRESSOR STALL NR 2 ENGINE ON THROTTLE ADVANCE AT 1.4 EPR TEMPS NORMAL. ALL PARAMETERS NORMAL WIND WAS A CROSSWIND, RUNWAY 25R = WIND WAS 180 AT 14 GUSTING TO 19 INSPECTED INLET AND EXHAUST NR 2 ENG. NO DISCREPANCIES NOTED. RAN ENG TO 1.4 EPR - INTO WIND,SDR C1HA200396020Engine · leakingOIL QUANTITY DECREASED TO .1 GALLONS IN FLIGHT. OIL TEMP 112 AT POWER PRESSURE 49. AIRCRAFT DIVERTED INTO DFW. MAINTENANCE FOUND OIL COMING OUT OF THE COMBUSTION DRAIN, ENGINE CHANGE IN PROGRESS.SDR CA031208004Control Valve · malfunctioned(CAN) ON CLIMB OUT THROUGH 25,000 FT. FLIGHT CREW REPORTED, DUCT OVERHEAT ON RT PACK. COULD NOT CONTROL TEMPERATURE WITH RT PACK ON. AIRCRAFT LOST ALL PRESSURIZATION AT ABOUT 25,000 FT. AND COULD NOT CONTROL CABIN PRESSURE IN MANUAL. CREW CONTACTED ATC AND COSDR C1HA200381033Bleed Valve · malfunctionedENGINE NR 3 BLEED AIR TRIP LIGHT ILLUMINATED PERFORMED COM PROCEDURE 2.36.2. REMOVED AND REPLACED NR 3 ENGINE BLEED VALVE OPS CHECKS NORMAL IAW MM 36-10-01 OK TO CONTINUE SERVICE.SDR CA031202003Transponder · faulty(CA) WAS NOTIFIED THAT SEARCH AND RESCUE WAS RECEIVING AN ELT RESPONSE FROM A COMPANY AIRCRAFT. INSPECTED AND IT WAS DETERMINED THIS AIRCRAFT WAS AT FAULT. THE UNIT WAS DISCONNECTED AND A FURTHER INSPECTION FOUND WATER LOCATED AROUND THE RECEPTACLE AND CONNSDR SROM200300053Fan · failedDURING CRUISE FLIGHT AT 330 A BURNING ODOR WAS NOTED IN THE COCKPIT ONLY. ALL SYSTEMS CONTINUED TO FUNCTION NORMAL. PRECAUTIONARY LANDING AT FAI WAS MADE. UPON LANDING MAINTENANCE WAS UNABLE TO FIND THE SOURCE OF THE SMELL AND ALL OPERATIONS NORMAL. IT WASSDR DHL2003765001Engine · stalledON TAKE OFF, PRIOR TO REACHING TAKE OFF EPR HAD A SUSPECTED ENGINE COMPRESSOR STALL AND AN AUTO PACK TRIP EVENT. INSPECTED INLETS AND EXHAUSTS IAW M/M 05-21-10. NO DEFECTS NOTED. RUNWAY 33 BEING USED. WIND WAS AT 29 AT 26 KNOTS GUSTING TO 36. SUSPECT CROSS-WISDR AUS20031137Switch · faulty(AUS) NR 5 LEADING EDGE KRUEGER FLAP POSITION SWITCH FAULTY.SDR 03FDEA01867Smoke Detector · activatedAT 2000 FEET AGL ON TAKEOFF AT BIL ZONE 5 MAIN CARGO SMOKE LIGHT CAME ON WITH BELL. S/O PANEL RESET PUSHED, LIGHT AND BELL CAME ON AGAIN. RESET AGAIN, LIGHT AND BELL CAME ON A THIRD TIME AND THEN WERE RESET AND STAYED OUT.SDR CA031103002Isolation Valve · failed(CAN) DURING CLIMB, IT WAS OBSERVED THAT CABIN PRESSURE WAS NOT CONSISTENT WITH FLIGHT LEVEL. AIRCRAFT RETURNED TO BASE WITHOUT INCIDENT. AIRCRAFT WAS DISPATCHED UND ER MEL 21-01-01 WITH RT PACK INOP FLYING AT AN ALTITUDE OF FL 25,000 FT. THE ISOLATION VALVE WSDR C1HA200393018Compressor · stalledFLIGHT ATTENDANTS REPORTED A POSSIBLE COMPRESSOR STALL UPON LANDING ROLLOUT. RAN ALL 3 ENG AT RUN PAD CHECKED COMPRESSOR BLEED SYSTEM OPERATION IAW B727 MM 75-31-00. NO STALLS NOTED. OK FOR SERVICE.SDR CA031027005Module · failed(CAN) ON DECENT NR1 A SYS LOW PRESSURE LIGHT ILLUMINATED. SHORTLY, NR 2 A SYS LOW PRESSURE LIGHT ILLUM. CREW ACCOMPLISHED QRH FOR LOSS OF SYS A. EMERGENCY DECLARED & LANDED. MAINT CHECKED SERVICEABLE HYD SYS RES STANDPIPE & PRESSURE. ENG RAN AND HYD PRESSURE SSDR C1HA200392005Duct · damagedINFLIGHT NR 2 ENG FIRE LT, BELL ON HIGH EGT AND OIL TEMP CHECKLIST SHUTDOWN NR 2 ENG RETURN. DUMP FUEL, NR 2 ENG THROTTLE FELT STIFF, POSSIBLY BINDING. FUEL CUTOFF LEVER DIFFICULT TO MOVE. PERFORMED VISUAL INOP OF INLET, EXHAUST FOUND 13TH STAGE BLEED SADDLSDR AUS20031072Circuit Breaker · failed(AUS) PACK COOLING FAN CIRCUIT BREAKER (C) PHASE TERMINAL OVERHEATED.SDR CALA0300609Charger · inoperativeEMERGENCY PATH LIGHTS INOPERATIVE FROM 6DEF THROUGH 14DEF. REMOVED AND REPLACED FORWARD BATTERY PACK CHARGER IAW MM 33-53-00.SDR DHL2003782012Battery · malfunctionedON PRE-FLIGHT FOUND EMERGENCY EXIT LIGHTS INOPERATIVE. SWITCH IN OFF POSITION DURING PRE-FLIGHT. TROUBLESHOT SYSTEM FOUND PORTABLE EMERGENCY EXIT LIGHTS WITH LOW VOLTAGE .7 VDC / CHARGED BATTERIES / TESTED BATTERIES AFTER CHARGE / FOUND FULLY CHARGED TO 2.6 VSDR DHL2003784006Odor · detectedSTRANGE SMOKE ODOR IN COCKPIT. APPEARS TO BECOME MUCH STRONGER WITH GASPER FAN ON. DEFERRED IAW DHL MEL 21-24, CONTROL NR 14407. PLACARD INSTALLED.SDR DHL2003784005Roller · out of adjustAFTER TAKEOFF MAIN ENTRY DOOR HAD LARGE PRESSURE LEAK TILL DIFF REACHED 3.1 CABIN RATE OF CLIMB WAS 1+ TILL DOOR RESEATED. REPLACED MAIN ENTRY DOOR AFT UPPER AND LOWER ROLLER CAM CRANKS P/N 69-37418-502 AND ROLLERS FOR THE SAME PN KRP139805VT IAW BMM 52-11-0SDR CA031015003Link · broken(CAN) A LOUD BANG WAS HEARD UPON GEAR RETRACTION. ONCE GEAR WAS RETRACTED A STRONG VIBRATION WAS FELT. WHEN GEAR EXTENTED, VIBRATION WENT AWAY. RETURNED TO YYC FOR A NORMAL LANDING. RT NOSE LANDING GEAR DOOR DOG LINK FOUND BROKEN. LINK REPLACED, SWING CARRIEDSDR AUS20031033Sealant · deteriorated(AUS) NR 2 FUEL TANK LEAKING. INVESTIGATION FOUND TANK WING TO CENTERBOX LOWER ATTACHMENT FITTING INBOARD FASTENER SEALANT LIFTING. REMOVED SEALANT FOUND TO HAVE INCLUSIONS AND VOIDS RESULTING FROM IMPROPER CLEANING AT PREVIOUS SEALANT APPLICATION.
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