Pratt & Whitney JT8D-9
Service difficulty reports · 686
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 = 'JT8D9' 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 = 'JT8D9' 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 03FDEA01668Frame · crackedRT 930 FRAME CRACKED AT LWR SHEAR TIE FASTENER HOLE ABOVE STR 14. REPAIRED CRACKED FRAME AT BS 930 STR 14 RT, PER SRM 53-10-4, EA 7-5310-55032.SDR MWEA030391Skin · gougedLEFT SIDE OF VERTICAL STABILIZER SKIN UNDER VERTICAL TO HORIZONTAL STABILIZER, FAIRING HAS A GOUGE FROM TOP SKIN RADIUS EXTENDING DOWN AT 1.5 INCHES. FABRICATED AND INSTALLED REPAIR DOUBLER.SDR MWEA030392Skin · dentedFUSELAGE SKIN HAS A DENT AT STATION 388 AT LONGERON 5 RIGHT. FABRICATED AND INSTALLED FILLER AND DOUBLER.SDR MWEA030393Longeron · crackedWHILE REPLACING DOME NUTS FOR FUSELAGE FILET PANEL, FOUND SUSPECT CRACK ON AFT END OF LONGERON 26 RT FRAME STATION 604. FABRICATED AND INSTALLED FITTING.SDR MWEA030395Skin · dentedFUSELAGE SKIN HAS A DENT AT STATION 967, 2 INCHES ABOVE LONGERON 27 LEFT. FABRICATED AND INSTALLED DOUBLER AND FILLERS.SDR 0301839852Controller · malfunctionedAT FL330, THE RED CABIN PRESSURE ANNUNCIATOR LIGHT ILLUMINATED. CREW INITIATED AN EMERGENCY DESCENT TO 10,000 FT & REGAINED CONTROL OF CABIN PRESSURIZATION IN MANUAL MODE. FLT CONTINUED & LANDED WITHOUT INCIDENT AT MSY WHERE MAINTENANCE MEL'D THE AUTOMATIC PRESDR SWAA032153Spacer · wornNR 1 ENGINE THROTTLE BINDING AT ABOUT HALF-WAY. REMOVED AND REPLACED SPACER BETWEEN TWO CONTROL CABLES PER MM.SDR 03FDEA01619Floorbeam · corrodedCORROSION ON FLOORBEAM, UPR & LWR SURFACE AROUND FASTENER HOLES AND TOP, BS 344, LBL 45 TO RBL 13, WL 208.SDR GAIA03086Frame · dentedDURING B-2 CHECK, FOUND MAIN CABIN FRAME BS 380 HAS A DENT IN THE RADIUS BELOW STRINGER 6LT. REF FASI N/R 53129, CUT OUT DAMAGE 4.75 BY 1.25, DOUBLER REPAIR PER B727 SRM 51-40-3 AND 53-10-4 FIG 1. (M)SDR SWAA032017Engine · leakingNR 2 ENGINE FUEL LEAKING FROM ENGINE CASE DIRECTLY UNDER P/D VALVE. REMOVED AND REPLACED NR 2 ENGINE PER MM.SDR RYN2004F00012Hinge · crackedAT (B) CHECK FOUND. MAIN CARGO DOOR AFT HINGE WITH 2 CRACKED LOBES ON THE AFT PART OF THE AIRFRAME HINGE. DRILLED, TREATED, PRIMED AND INSTALLED NEW HINGE SECTION ON MAIN CARGO DOOR.SDR 0301319862Control Cable · bindingCREW EXPERIENCED SIGNIFICANT BINDING OF THE AILERONS IMMEDIATELY AFTER TAKEOFF. AS AIRSPEED INCREASED, THE CONTROLLABILITY IMPROVED AND LESS FORCE WAS NEEDED TO MOVE THE CONTROL YOKE. FLIGHT RETURNED TO AN UNEVENTFUL LANDING BACK AT DTW. MAINTENANCE CONFSDR 2003FA0001044Skin · corrodedDURING A C-CHECK INSPECTION, CORROSION WAS FOUND ON LOWER SURFACE OF CENTER WING, CENTER SECTION, WHICH FORMS THE UPPER WALL OF THE RAM AIR DUCT USED FOR COOLING OF THE AIR CONDITION SYSTEM ABOVE LEFT PLENUM CHAMBER ASS AT LBL 20 AND STIFFENER 5. DURING CORROSDR 03FDEA01093Skin · lightning strikeN00177 LIGHTNING STRIKE BS 350 BETWEEN STR 2L AND STR 3L. FOUND LIGHTNING STRIKE DAMAGE TO BE OUT OF LIMITS. REPAIRED DAMAGE IAW SRM 53-30-3 AT BS 350 BETWEEN STR 2L AND 3L.SDR 03FDEA01094Floorbeam · corrodedCORROSION ON FLOOR SUPPORT BS 344, LBL 45, WL 208. CORROSION ON FLOORBEAM BS 344, LBL 45, WL 208. REPAIRED FLOORBEAM IAW SRM 53-10- 1, 51-10-1, 51-30-2 & 53-10-8.SDR A4J2003F00001Power Supply · inoperativeDURING B CHECK PIE MAINTENANCE FOUND BOTH FORWARD OVER WING ENERGENCY LIGHTS COME ON AN WILL NOT EXTINGUISH WHEN BATTERY IS TURNED OFF. REMOVED AND REPLACED POWER SUPPLY FOR FORWARD OVER WING EMERGENCY C4 LIGHTS IAW DC9 MM 33-53-0, OPERATES NORMAL IAW DC9 MM SDR 2003F00486Engine · leakingDURING DESCENT AT FORT LAUDERDALE (KFLL), THE CREW SHUTDOWN NR 3 ENGINE DUE TO EXCESSIVELY HIGH OIL TEMPERATURE, FLICKERING FILTER BYPASS LIGHT, LOW OIL PRESSURE ON THE GATE AND LOW OIL PRESSURE LIGHT ON STEADY AS WELL AS DECREASING OIL PRESSURE. LANDED AT KFSDR RYN2004F00020Warning Light · illuminatedAPU FIRE WARNING LIGHT AND BELL CAME ON AFTER TAKE-OFF FROM LAS. DISCHARGED APU FIRE BOTTLE. PERFORMED EMERGENCY ACTION ITEMS IAW QUICK REFERENCE HANDBOOK. AIRCRAFT LANDED WITHOUT INCIDENT IN LAS APU AND APU FIRE EXTINGUISHER, DEFERRED. AIRCRAFT REMOVED FSDR MP011603BSpar · corrodedDURING AD COMPLIANCE, A CLOSE VISUAL AND NDT HFEC INSP OF WING REAR SPAR, A CRACK AND CORROSION WAS FOUND IN THE HEEL OF THE INBOARD PORTION OF THE DETERMINED TO BE OUT OF LIMITS IAW MFG SRM. ENGINEERING WAS CONTACTED AND REPAIRS WERE DRAWN. A SECTION OF THESDR EIA2003052Skin · crackedLONGERON, 4 LEFT STA. 484 CRACK IN SKIN GOING RIVET TO RIVET 1.5 INCHES. REPAIRED CRACK AT LONGERON 4L SA 484 IN FUSELAGE SKIN IAW SRM 53-04, PG 218M, 218Z, 218AA, AB. ORIGINAL SKIN 2014 T6 .050 SUBSTITUTED 2024-T3 .050 IAW SRM 51-60-0 PG 5.SDR EIA2003051Frame · corrodedFORWARD CARGO PIT FRAME AT STA 351, SIDE AT BEND RADIUS. CORRODED BETWEEN LONGERON 30-29 R. INSTALLED REPAIR ON STA 351 FRAME SRM 51-30-02,1 AND 53-03 FIG 2A. HEAT TEATED AND FABRICATED DOUBLERS IAW SRM 53-03 PG 4E AND 4J.SDR EIA2003050Skin · damagedSKIN DENT AND LONGERONS BENT STA NR 275 TO 294 LONGERONS 20 AND 21 RIGHT. CUTOUT DAMAGED SKIN AREA AT BS 275 BETWEEN LONGERONS 20-22 REPAIRED IAW SRM 53-04 PG 42-44, 60BV, 60BU, 60RT, AND 60CK. CUTOUT DAMAGE LONGERON AREA 20R AT BS267-285 AND LONGERON 21 ATSDR 03FDEA00201Frame · dentedDENTED FRAME BS 950E, LBL 31, WL 150. DENT IN FRAME AT B.S. 950E, LBL 31, WL 150 FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND INSTALLED FABRICATED U CHANNEL IAW EA 7-5310-69418 AND ER 03-1450 .SDR GAIA03012OPControl Handle · stickingDURING TAKE OFF, ALL THREE GEAR UNSAFE LIGHTS (RED) AND TAIL SKID LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE DOORS LIGHTS OF FE PANEL WERE NOT ILLUMINATED. AIRCRAFT PERFORMED AN AIR TURN BACK AND LANDED WITHOUT FURTHER INCIDENT AT JAX. FOUND CONTSDR 03FDEA00193Floorbeam · corrodedCORROSION ON 950D FLOORBEAM UPPER FLANGE UPPER AND LOWER SURFACES RBL 25, LBL 25, WL 208. REMOVED CORROSION FROM FLOORBEAM BS 950D, RBL 10.5, FOUND OUT OF LIMITS IAW SRM 53-10-1. CUT OUT DAMAGED SECTION OF UPPER CHORD BS 950D LBL 37-RBL 37. FABRICATED REPAISDR 03FDEA00195Shear Tie · corrodedCORROSION ON SHEAR TIE, BS 720 NEXT TO STR 26R. REMOVED CORROSION ON SHEAR TIE, BS 720 BETWEEN STR 26-27 RIGHT, FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED, ALODINED AND PRIMED REPAIR PARTS. INSTALLED REPAIR, ALL WORK ACCOMPLISHED IAW SRM 51-10-3,SDR 03FDEA00196Stringer Clip · corrodedCORROSION ON STRINGER CLIP, BS 720C STR 26R. REMOVED STRINGER CLIP BS 720C STR 26R, REMOVED CORROSION ON CLIP IN A 1 INCH X 1 INCH AREA. BLENDED 0.020 INCH FROM 0.040 INCH OUT OF LIMITS IAW SRM 53-10-1 FIG 1. FABRICATED REPLACEMENT STR CLIP FROM 7075 T6 X 0SDR 03FDEA00198Floor Support · corrodedCORROSION ON FLOOR SUPPORT UNDER NUT PLATE BS 1165 - 1166, RBL 16, WL 155. REMOVED FLOOR SUPPORT BS 1166-1120, RBL 16, WL 155. FABRICATED REPAIR PARTS IAW SRM 53-10-5 AND SR 27-53-039. ALODINED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED IAW SRM 51-30-2.SDR 03FDEA00192Floorbeam · corrodedCORROSION (C53-224-011) ON TOP OF UPPER LOBE FLOORBEAM AT BS 620, RBL 3, TO RBL 23. CORROSION AT BS 620, WL 208, RBL 3 TO RBL 23 DETERMINED TO BE OUT OF LIMITS IAW B727, SRM 53-10-1 FIG 4. REMOVED UPPER CHORD OF BEAM FROM LBL 32 TO RBL 36.5. FABRICATED REPASDR 03FDEA00189Skin · dentedLT AFT FUSELAGE SEC 48, SKIN HAS A CREASED DENT AT BS. 1349, WL 196 APPROX 8 O'CLOCK POS. LEFT AFT FUSE, SEC 48, SKIN CREASE DENT AT B.S 1349, WL 196, REMOVED DAMAGE, FOUND TO GO THROUGH BONDED SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER IAW E.A 7-5450SDR 03FDEA00188Frame · corrodedCORROSION ON REINFORCEMENT FRAME, BS 1176.9, RBL 45 TO RBL 59, WL 208. REMOVED CORROSION ON REINFORCEMENT FRAME, BS 1176.9 RBL 45-59 WL 208. DETERMINED TO BE OUT OF LIMITS IAW 53-10-1. REMOVED AND REPLACED CHORD IAW SRM 51-30-2.SDR 03FDEA00181Floorbeam · corrodedCORROSION ON FLOORBEAM LOWER FRAME AROUND NUT PLATE HOLES, B.S.720, LBL 16 TO LBL 21, W.L. 200 AT PREVIOUS REPAIR.SDR 03FDEA00182Pressure Panel · gougedGOUGED AREA AT NLW UPPER WEB AT LT PRESSURE PANEL CUT OUT INBOARD SIDE, B.S 242. REMOVED DAMAGE AND REPAIRED IAW SRM 51-40-2. GOUGE WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1.SDR 03FDEA00183Floorbeam · corrodedCORROSION ON FLOORBEAM REPAIR STRAP BS 1130, RBL 30-RBL 36, WL 200. REMOVED CORROSION ON FLOORBEAM REPAIR STRAP BS 1130, FOUND TO BE OUT OF LIMITS, REMOVED DAMAGED STRAP, FABRICATED AND INSTALLED NEW STRAP IAW SRM 51-10-2, 51-10-3, 51-30-2, AND 51-30-5.SDR 03FDEA00175Frame · corrodedCORROSION FORWARD CARGO BAY ON LOWER FRAME AT STA 660, STR 28L TO 28R.SDR 03FDEA00174Web · gougedRT WHEEL WELL HAS GOUGE IN WEB. DAMAGE ON RT WHEEL WELL WEB COMMON TO K-BEAM AREA, BS 872, RBL 5.5, WL 150, FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER FROM 7075-T6 .040 INCH, LOT NR 472905. ALODINED, PRIMED, PAINTED, AND ISDR 03FDEA00177Web · corrodedCORROSION ON WEB, STA 1174, RBL 18, WL 208. REMOVED CORROSION AT STA 1174. WEB FOUND OUT OF LIMITS. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-1Q0-1, 51-40-2.SDR 03FDEA00176Shear Tie · crackedWHILE WORKING N00939, FOUND CRACKED SHEAR TIE AT BS 328, STR 26-27 LEFT. REPAIRED SHEAR TIE BS 328, STR. 26-27 LEFT, IAW SRM 53-10-4 FIG. 15.SDR 03FDEA00166Skin · dentedSKIN DENT, BS 720B+3, JUST BELOW STR 17R, REWORKED SKIN DENT, BS 720B+3 BELOW STR 17R. A=1.8 Y=.062 A/Y=12.9 AND OIL CANNED. OUT OF LIMITS IAW 53-30-01. REMOVED DAMAGED AREA 2.3 X 2.9. FABRICATED, ALODINED, PRIMED AND PAINTED AND INSTALLED REPAIR DOUBLERSDR 03FDEA00167Floorbeam · corrodedCORROSION ON FLOORBEAM, UPPER FLANGE AT BS 680 RBL 11, DAMAGED ON REPAIR DOUBLER, NO DAMAGE LIMITS ON REPAIR DOUBLER, REPAIRED FLOORBEAM AT BS 680, WL 208, RBL 11, IAW SRM 53-10-8 FIG 3.SDR 03FDEA00168Floorbeam · corrodedCORROSION ON TOP OF UPPER LOBE FLOORBEAM AT BS 344, LBL 3, TO LBL 60. REMOVED CORROSION ON UPPER LOBE OF FLOORBEAM AT 344, FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED, TREATED AND INSTALLED REPAIR UPPER LOBE IAW SRM 53-10-8, SR 27-53-007, SDR 03FDEA00169Floorbeam · corrodedCORROSION ON FLOORBEAM REPAIR FILLER B.S. 1070, RBL 42 TO LBL 36. REMOVED CORROSION ON FLOORBEAM REPAIR FILLER BS 1070. FOUND TO BE OUT OF LIMITS. REMOVED FILLER, FABRICATED REPLACEMENT AND INSTALLED IAW SRM 53-10-1, 53-10-8.SDR 03FDEA00158Floorbeam · corrodedCORROSION ON 950F FLOORBEAM UPPER FLANGE UPPER AND LOWER SURFACE FROM LBL 55 TO RBL 55, WL 208.SDR 03FDEA00157Floorbeam · corrodedCORROSION ON FLOORBEAM UPR FLANGE BS 1110, RBL 57 TO LBL 57, WL 208.SDR 03FDEA00153Skin · dentedDENT IN SKIN BS 460-480 BETWEEN 14.15RSDR 03FDEA00155Stringer · corrodedCORROSION ON STR 28R, BS 480-484, WL 150, INBOARD SIDE. REMOVED CORROSION FROM STR 28R AT B.S 480+4 INCH, FOUND TO BE OUT OF LIMITS. FABRICATED, ALODINED AND PRIMED REPAIR PARTS, AND INSTALLED IAW SRM 51-10-4, 53-10-1, 53-10-3, 51- 30-2 AND MM 51-20-15SDR 03FDEA00156Frame · corrodedWHILE WORKING CARD FOUND LOWER NOSE FRAME LT SIDE TO BE CORRODED AT BS 296 LBL 20. FOUND LOWER NOSE FRAME LT SIDE TO BE OUT OF LIMITS AT BS 296, LBL 70. REMOVED AND REPLACED LT FRAME IAW SRM 51-20-1, 51-30-7, 51-30-5.SDR SWAA030421Turbine · failedAIR TURNBACK, DECLARED EMERGENCY, DURING CLIMB EXPERIENCED NR 1 ENG HIGH EGT IND, REDUCED PWR TO NR 1 ENG. REMOVED AND REPLACED NR 1 ENG PER MM.SDR 03FDEA00143Skin · corrodedCORROSION ON SKIN AT BS 702, RBL 20, WL 150, BETWEEN STR 26R AND 27R.SDR 03FDEA00142Stringer · corrodedCORROSION IN SEVERAL AREAS IN STRINGER 26R FROM BS 620 TO 720A. REMOVED AND REPLACED STRINGER SECTION AT BS 675 - 720+10 IAW SRM 53-10-3.
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