Pratt & Whitney JT8D-217A
Service difficulty reports · 235
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 = 'JT8D217A' 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 = 'JT8D217A' 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 AALA20170321006Bolt · wornFLIGHT DIVERTED DUE TO AN AIRFRAME VIBRATIONS BETWEEN THE AFT LAVATORIES. UNEVENTFUL LANDING. LEFT ENGINE ANTI-ICE VALVE MOUNTING BOLT WORN AND LOOSE. REMOVED AND REPLACED WITH NEW HARDWARE IAW AMM 75-10-01. OPERATIONAL CHECK GOOD. AIRCRAFT WAS GROUNDED.SDR AALA20150612001Compressor Blade · damagedAIR INTERRUPT, RETURNED & EMER DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB, CREW REPORTS A COMPRESSOR STALL ON RT ENG FOLLOWED BY A REDUCTION IN EPR & INCREASE IN EGT. ACCOMPLISHED CARD 72-96-12 71-91-12 & BORESCOPE WITH A DETAILED VISUSDR AALA20110331TUL07Exciter · failedMCO INFLIGHT TPA-ORD. CREW REPORTED LIGHTNING STRIKE TO RIGHT SIDE OF AIRCRAFT WITH RIGHT ENGINE SHUTDOWN (SINGLE ENGINE TIME 1 MINUTE). EMERGENCY DECLARED DIVERTED MCO LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE EXCITER,SDR AALA20100418SFO01Tube · leakingSFO - CREW REPORTED RIGHT ENGINE OIL PRESSURE LIGHT DROPPED TO 20 PSI AND STABILIZED. RIGHT HAND THROTTLE REDUCED TO IDLE. FLIGHT RETURNED SFO LANDED WITHOUT INCIDENT. FOUND OIL LEAK AT 11 O`CLOCK POSITION. REMOVED AND REPLACED OIL TUBE AT OIL FILTER DIFFESDR ASMF200711003Blade · damagedDURING TRANSIT CHECK, FIVE BLADES WERE DETECTED DAMAGED DUE TO A FOD IN LT ENGINE. (4) BLADES WERE DETECTED WITH NICKS ON BLADES LEADING EDGE AND WERE REWORKED IAW MM 72-33-21 BEING WITHIN LIMITS. ONE BLADE WAS DETECTED WITH DENT WITH DEPTH OF 0.135 INCHES ANDSDR ASMF200708007Control Valve · leakingDURING TRANSIT CHECK WAS DETECTED A HYDRAULIC LEAK IN THE LT ENGINE REVERSE CONTROL VALVE. THE VALVE WAS REPLACED IAW MM 78-31-04, TESTED CORRECT AND 6/4 OF HYDRAULIC FLUID WERE REPLENISHED IAW MM 12-13-82.SDR GTIA200700015Floorbeam · corrodedCABIN FLOORBEAM CORRODED. REPLACED FLOOR SUPPORT BEAM.SDR GTIA200700013Intercostal · crackedAFT CARGO CABIN FLOOR INTERCOSTAL CRACKED. REPLACED INTERCOSTAL.SDR GTIA200700014Floorbeam · corrodedCORROSION ON FLOORBEAM ANGLE. REPLACED FLOORBEAM.SDR GTIA200700012Floorbeam · corrodedCORROSION AFT CARGO CABIN FLOORBEAM. INSTALLED NEW FLOORBEAM.SDR GTIA200700009Floor Support · corrodedCORROSION ON FLOOR SUPPORT. REPAIRED FLOOR SUPPORT.SDR GTIA200700010Floorbeam · corrodedCORROSION AT FWD CABIN FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT.SDR GTIA200700011Floorbeam · corrodedCORROSION ON FLOORBEAM. INSTALLED NEW FLOORBEAM.SDR GTIA200700008Longeron · corrodedAFT CARGO COMPT LONGERON 29R HAS CORROSION. MADE LONGERON REPAIR.SDR GTIA200700007Door · obstructedUNABLE TO OPEN RT AFT OVERWING EXIT. FOUND TRIM PANEL OVERLAPPING UPPER AFT CORNER PREVENTING IT FROM OPENING.SDR ASMF200612002Regulator Valve · failedAIRCRAFT RETURNED DUE TO AIR CONDITIONING SYSTEMS FAILED, RT SYSTEM WAS SHUTDOWN, LT SYSTEM DID NOT OPERATE AND SMOKE ODOR WAS DETECTED. DURING MAINTENANCE CHECK, THE CHIP DETECTORS WERE CHECKED, WATER SEPARATORS WERE REPLACED IAW MM 21-20-2, BITE TO BOTH CONTSDR ASMF200604013Fan Blade · damagedDURING TRANSIT CHECK, IT WAS DETECTED ONE LEFT ENGINE C1 FAN BLADE DAMAGED BY AN SCREW SANK INTO THE ACOUSTIC PANEL (FOD). THE DAMAGE WAS EVALUATED IAW M/M 72-00-00 BEING WITHIN LIMITS. DURING OVERNIGHT CHECK, THE FAN BLADE WAS REWORKED IAW M/M 72-00-00 REMASDR ASMF200603005Filter · dirtyCAPTAIN REPORTED THAT DURING TAXING LT ENGINE DID NOT ACCELERATE EVEN WITH THRUST LEVER FULLY FORWARDED, RETURNING TO PLATFORM. DURING CHECK, MAINTENANCE PERSONNEL DETECTED THAT THE LT ENGINE ACCELERATED VERY SLOWLY, SO THRUST BUMP PROCEDURE WAS PERFORMED WITHSDR AALA20060143Engine · shutdownDEN - RIGHT ENGINE FAILED AFTER TAKEOFF AT ABOUT 300 FEET ABOVE GROUND LEVEL. RIGHT HAND ENGINE EXHAUST GAS TEMPERATURE AT ROTATION WAS ABOUT 570 DEGREES. ENGINE FIRE/DAMAGE/SEPARATION CHECKLIST FOLLOWED, HAD N1 AND N2 BUT NO RESTART. LANDED DEN WITHOUT INCISDR 06FDEA0547Fuel Control · malfunctionedNO THROTTLE RESPONSE ON NR 1 ENGINE ON TAKEOFF. REMOVED AND REPLACED NR 1 ENGINE FUEL CONTROL IAW FX B 727-200 MM 73-20-001-2. PERFORMED ENGINE RUN AND TRIM MED IAW FX B727-200 MM 71-00-030 AND 71-00-097 AND OPS AND LEAK CHECK GOOD. ALSO REMOVED AND REPLACESDR ASMF200602001Fan Blade · damagedDURING TRANSIT CHECK, DETECTED 09 LEFT ENGINE FAN BLADES WITH DAMAGES. ONE OF THEM WAS OUT OF LIMITS. 04 FAN BLADES WERE REPLACED IAW M/M 72-33-21 AND 06 WERE REWORKED IAW M/M 72-33-22. ENGINE WAS OPERATIONAL CHECKED IAW MPCM 71-00-01 AND M/M 71-00-00, TESTSDR ASMF200512019Annunciator · failedAIRCRAFT RETURNED TO PLATFORM DURING TAXING THE SLAT DISAGREE LIGHT NOT TURNED ON. DURING MAINTENANCE REVISION, THE SLAT DISAGREE LIGHT WAS FAILING INTERMITTENTLY. THE PSEU BITE WAS PERFORMED, THE SLATS SENSORS A, B, C, D WERE CLEANED, THE COCKPIT DISAGREE LIGSDR ASMF200501201Engine · vibrationCAPTAIN REPORTED THAT DURING FLIGHT WITH EPR BETWEEN 1.0 AND 1.2 IN THE LT ENGINE; VIBRATION AMPLITUDE OCCASIONALLY WITH PEAKS FROM 4 TO 0 AND WHEN THE LT ENGINE WAS SHUTDOWN, VIBRATION WAS FELT IN ALL THE AIRCRAFT. THE LT ENGINE CHIP DETECTORS, ACCESSORIES, PSDR ASMF200512007Pin · brokenDURING PUSH BACK THE NOSE LANDING GEAR TOWING FUSE PIN WAS BROKEN. IT WAS REPLACED IAW MM 32-21-14 AND THE NOSE LANDING GEAR AND GENERAL INSPECTIONS FOR EXCESSIVE LOAD WERE PERFORMED IAW MM 05-51-03 AND MM 32-20-00 RESPECTIVELY, NO DAMAGES WERE FOUND.SDR GTIA050264Frame · crackedFRAME CANT 1463 AT APPROX LONGERON 19 AND 20 ON AC RT HAS CRACKED WEBBING. INSTALLED PERMANENT REPAIR ON CANTED FRAME FS 1463 BETWEEN R18L AND R25L, IAW EA REV ORIGINAL HAS BEEN ACCOMPLISHED. (K)SDR ASMF200505030Skin · crackedCAPTAIN REPORTED THAT HE PERFORMED THE FINAL APPROACH AND LANDING WITH 3450 POUNDS OUT OF BALANCE BETWEEN TANKS. OUT OF BALANCE INSPECTION WAS PERFORMED IAW MM, DETECTING A CRACK IN THE RT WING IB FLIGHT SPOILER OF 9 INCHES LONG. SPOILER WAS REPLACED IAW MM 27SDR T48R20050011Engine · damagedENGINE WAS REMOVED FROM N803NK FOR INFLIGHT SHUTDOWN. DISASSEMBLY AND INSPECTION REVEALED THE HPC, HPT AND LPT MODULES HAVE HEAVY IMPACT DAMAGE.SDR GTIA050099Web · puncturedAT STA 200, NR 1 SEAT TRACK LT FLOOR WEB HAS A PUNCTURE. CUT OUT PUNCTURE FROM FLOOR WEB STA 200, NR 1 SEAT TRACK. FABRICATE DOUBLERS AND FILLERS. TREATED AND PRIMED, INSTALLED DOUBLER AND FILLER IAW SRM. (K)SDR GTIA050076Wire · brokenUPON PREFLIGHT (COCKPIT SETUP) COULD NOT GET RUDDER CONTROL MANUAL LIGHT DURING TEST, AIRCRAFT TAIL SWAP TO 817NK. TROUBLESHOT DOWN TO BROKEN WIRE AT CANT. STA 1485, REPAIRED BROKEN WIRE IAW SRM. OPS CHECK, OK. (K)SDR GTIA050097Support Angle · crackedAFT CARGO DOOR FWD UPLOCK SUPPORT ANGLE CRACKED. REMOVED AND FABRICATED NEW ANGLE IAW SRM. TREATED AND PRIMED, INSTALLED SUPPORT ANGLE IAW SRM. (K)SDR GTIA050084Web · corrodedCABIN STA 180-200, RBL 54, RBL59, SUB FLOOR CORRODED. REMOVED CORROSION AT WEB. MATERIAL LOSS OUT OF LIMITS. REMOVED FWD AIRSTAIR. REMOVED FLOOR SUPPORT RT STA 160 TO 200. CUT OUT DAMAGED AREA AND FABED DOUBLER. PRIMED AND TREATED, INSTALLED FLOOR SUPPORSDR GTIA050093Strap · corrodedALUMINUM STRAP ON LOWER SIDE OF L2 DOOR THRESHOLD HAS CORROSION. STRAP CORROSION IS OUT OF LIMITS. FABRICATED NEW STRAP IAW SRM. TREATED AND PRIMED, INSTALLED STRAP ON L2 DOOR THRESHOLD IAW SRM. (K)SDR GTIA050079Doubler · corrodedG-2 GALLEY, CART ENCLOSURE, AFT LOWER LIP AND (2 EA) DOUBLERS ARE CORRODED. REMOVED LOWER LIP AND DOUBLERS, FOUND LIP AND DOUBLERS OUT OF LIMITS. FABRICATED LIP CHANNEL AND DOUBLERS OUT OF LIMITS. FABRICATED LIP CHANNEL AND DOUBLERS. TREAT AND PRIMED. INSSDR GTIA050078Support Angle · corrodedG-2 GALLEY, UPPER SECTION, LOWER EDGE AND SUPPORT ANGLE ARE CORRODED. REMOVED CORROSION ON LOWER EDGE AND SUPPORT ANGLE. FOUND SUPPORT ANGLE OUT OF LIMITS FABRICATED SUPPORT ANGLE IAW SRM. PRIMED AND INSTALLED SUPPORT ANGLE. (K)SDR GTIA050098Doubler · crackedHORIZONTAL STABILIZER, RT SIDE IB UPPER BRACKET SUPPORT HAS CRACK ON DOUBLER. REMOVED CRACKED DOUBLER. FABRICATED NEW DOUBLER. TREATED AND PRIMED, INSTALLED DOUBLER IAW SRM. (K)SDR GTIA050096Skin · dentedDENT ON AFT CARGO DOOR SKIN 21 INCHES FROM AFT EDGE AND 11 INCHES FROM BOTTOM EDGE OF DOOR (X=0.035 INCH, D=1.75 INCH, D/X=50). STRIPPED AREA OF DENT ON AFT CARGO DOOR FS 1185 IS UNDER CONDITION IAW SRM. DYE PENETRANT INSP, NO CRACK FOUND. REMOVED LATCH HANSDR GTIA050095Skin · dentedDENT ON FUSELAGE SKIN FS421 BETWEEN LONGERONS 19R AND 20R (D=0.5 INCH, X=0.008 INCH, D/X - 62.5 INCHES). REMOVED CARGO DOOR TO FOM IAW SRM. FOUND DENT HAS GOUGED IN CENTER, REMOVED DAMAGED AREA OF SKIN (1.5 INCH X 0.8 INCH) IAW SRM. FABRICATED DOUBLER AND FSDR GTIA050082Cusp Web · corrodedMID PIT STA 522-636, A LONG 18, RBL 52, FLOOR PANEL UNDER FEDDER CABLES CORRODED. REMOVED CORROSION FROM 522-636, FOUND OUT OF LIMITS. REMOVED WEB STA 503-598, FABED NEW WEB, PRIMED AND TREATED. INSTALLED WEB AT STA 503-598, RBL 52, IAW SRM. (K)SDR GTIA050081Seat Track · crackedRT OB SEAT TRACK HAS AREA OF CORROSION AT FS 229. REMOVED CORROSION, FOUND OUT OF LIMITS. FABRICATED NEW SEAT TRACK. FOUND WEB OB OF SEAT TRACK FS 218 CRACKED, FABED DOUBLER AND FILLER IAW SRM. PRIMED AND TREATED. INSTALLED DOUBLER, FILLER AND SEAT TRACK SDR GTIA050094Frame · crackedFROM C/O 0155770 RT WING L/E 2 EA FORMERS ST APPROX STA 351 CRACKED. FABRICATED DOUBLER IAW SRM. HEAT TREATED 2 EA DOUBLER IAW SRM. TREATED AND PRIMED INSTALLED REPAIR DOUBLER IAW SRM. LP NR 01476783. (K)SDR GTIA050083Floor Support · corrodedAFT CARGO COMPARTMENT, STA 1174, LBL 12, MAIN CABIN FLOORBEAM UPPER FLOOR SUPPORT ANGLE IS CORRODED (EXFOLIATION). REMOVED DAMAGED FLOORBEAM AND FOUND OUT OF LIMITS. FABRICATED NEW SUPPORT ANGLE, PRIMED AND TREATED. INSTALLED FLOOR SUPPORT ANGLE IAW SRM. (SDR ASMF200503002Fuel Control · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF RIGHT ENGINE WITHOUT ACCELERATION AND PARAMETERS WERE BELOW NORMAL IN IDLE. THE ACCELERATION CHAMBER WAS SERVICED AND FCU WAS LUBRICATED IAW MM 73-00-00, TESTED CORRECT. AIRCRAFT RETURNED TO PLATFORM AGAIN DUSDR GTIA050071Skin · dentedSKIN DENT AT STA 1174, BETWEEN LONGERON 17L AND 18L. REMOVED SAF-T-GLO, GALLEY 4 AND SIDE WALL PANEL TO FOM AT LT FS 1184. FOUND DENT TO BE (D=1.5 INCH, X=0.050, D/X=30) COND 2. REFORMED DENT AREA TO ORIGINAL CONTOUR. INSTALLED DOUBLER IAW SRM 53-04, FIG SDR GTIA050055Skin · dentedLT WING FLAP VANE NR 4 HAS DENT TOP SIDE. REMOVED DAMAGED SKIN AND CORE. FABRICATED NEW CORE AND DOUBLER, TREATED DOUBLER AND BONDED CORE IAW 57-50. (K)SDR GTIA050061Floor Support · brokenFLOOR SUPPORT STA 1136 BROKEN AFT PIT 28R-28L. REMOVED FLOOR SUPPORT AND LOCATED NEW FLOOR SUPPORT AT STA 1136, 28R-28L. INSTALLED FLOOR SUPPORT FS 1136, 28R-28L, AFT PIT IAW SRM. (K)SDR GTIA050037Motor · inoperativePRIMARY LONG TRIM INOPERATIVE, TAIL SWAP WITH AIRCRAFT 829. REMOVED AND REPLACED LONG TRIM MOTOR AND REPAIRED MOTOR GROUNDS, SYSTEM OPS CHECK GOOD. (K)SDR GTIA050056Support Angle · corrodedTHRESHOLD SUPPORT ANGLE, STA 1212, ON DOOR JAMB BEAM IS CORRODED. REMOVED CORROSION AT SUPPORT ANGLE. MATERIAL LOSS OUT OF LIMITS. REMOVED SUPPORT ANGLE AT STA 1212. FABRICATED NEW SUPPORT ANGLE, HEAT TREATED REPAIR PART. INSTALLED SUPPORT ANGLE AT STA 12SDR GTIA050064Skin · dentedFUSELAGE SKIN DENTED AT FS 304 BETWEEN LONGERON 28L-29L. (D=0.5 INCH, X=0.015 INCH D/X= 33.3). DENT WAS FOUND TO BE LESS THAN 1.0 INCH FROM FRAME REQ A CUT OUT REPAIR. CUT OUT DAMAGED SKIN AT FS 304 BETWEEN LONGERON 28L-29L. FABED NEW SKIN SECTION, REPAIR SDR GTIA050053Skin · dentedDENT AT FS 245, LONGERON 18L (D=1.250 INCH, X=0.054 D/X=23.14). REMOVED AIRCRAFT SKIN AT STA FS 245, LONGERON 18L (20 INCHES X 14 INCHES). FABRICATED REPAIR PARTS IAW SRM. INSTALLED, REPAIR AT FS STA 245 LONGERON 18L. (K)SDR GTIA050052Stiffener · corrodedAFT CARGO COMPARTMENT, STA 1338, 27L-27R AFT SIDE OF FALSE BULKHEAD, LOWER STIFFENERS ARE CORRODED. REMOVED CORROSION AT STIFFENER STA 1338L, 29L. MATERIAL LOSS OUT OF LIMITS. REMOVED STIFFENER AT STA 1338L, 29L, LOCATED AND DRILLED NEW STIFFENER. INSTALLE
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