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 FDEA201011134338Seat Track · corrodedSEAT TRACK CORRODED STA 690 TO 740, LBL 45. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION FROM BAC 1520-792-7178- T6 DIM. 172" LONG, 2EA ANGLES FROM BAC 1503-100122-7178-T6511 DIM. 16" LONG, AND STRAP FROM 7075T6 0.250" DIM. 8" X 2" IAW SRM 53-SDR FDEA201011134342Floorbeam · corrodedFLOORBEAM CORRODED STA 440, LBL 25 TO BL 0. CUT OUT DAMAGED AREA DIMS 2.5" X 2". FABRICATED UPPER CHORD USING BAC1505-100617-7075T3 DIMS 15.10", SUPPORT ANGLE USING BAC1490-2785-7075T6 DIMS 15.10", SUPPORT ANGLE USING BAC1490-2831-7075T6 DIMS 11.65", REINFORCSDR FDEA201011134345Floorbeam · corrodedFLOORBEAM CORRODED STA 380, RBL 25 TO RBL 45. CUT OUT DAMAGED AREA DIMS 2.3" X .90". FABRICATED 2 REPAIR ANGLES USING BAC1490- 2888-7075T6 DIMS 13.4" X 2.7" AND 10.2" X 2.6" AND INSTALLED IAW SRM 53-10-8 AND SRM 53-10- 2.SDR FDEA201011134336Seat Track · corrodedSEAT TRACK CORRODED STA 480 TO 680 LBL 25. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION AT BS 480TO 690 LBL 25 FROM BAC 1520-792-7178T6 DIM. 209.5" LONG, SPLICE REPAIR 2EA. FROM 1503-100122 7178T6 DIM 14.375" , AND STRAP FROM 7075T6 0.250" DISDR FDEA201011134341Floorbeam · corrodedFLOORBEAM CORRODED STA 560, LBL 25 TO LBL 45. CUT-OUT DAMAGED AREA TOP TEE CAP FLOORBEAM BS 560 LBL 36.40 TO 39 APPROX DIM. 2.6" X .90", FABRICATED REPAIR PARTS 2EA ANGLES FROM BAC 1490-2888-7075T6 DIM.19.5" X 0.90" AND 9.6" X .080". REPAIR FILLER FROM 2024SDR DALA1102199855Skin · debondedRT WING OTBD SPOILER PANEL LOWER SURFACE AT INBD END EXISTING REPAIR DOUBLER DISBONDED. REMOVED SPOILER PANEL IAW AMM 27-61-01. REMOVED RT OTBD SPOILER, REPAIRED ON TRAVELER NR 2312N00542. INSTALLED RT OTBD SPOILER OPS AND RIGGING CHECK ON WORK CARD 2760-9800SDR DALA1035459855Seat Track · gougedDURING M-CHECK FOUND MAN CABIN FS 891 RBL 24 SEAT TRACK LUG IS GOUGED OUT OF LIMITS. REMOVED SEAT TRACK FACTORY SPLICE STA 842 RBL 24 AND CUT AT BS 936.5, RBL 24 RECEIVED NEW TRACK AND SPLICE ,TRIMMED LOCATED, DRILLED, DEBURRED, TREATED AND PRIMED IAW SRM 53-SDR DALA1035469855Seat Track · brokenDURING M-CHECK FOUND MAIN CABIN FS 597 LBL 45 SEAT TRACK LUGS ARE BROKEN. R & R LBL 45, SEAT TRACK STA 570-654 LOCATED DRILLED AND INSTALLED SPLICE ACA7413-505 & SPLICE PLATE ACA7414-3 IAW SRM 51-30-2 ,51-30-5 53-23-0 FIG 4, 51-10-4, 53-05, FIG 4F 51-10-3, 51-SDR DALA1035969864Frame · gougedDURING M-CHECK FOUND FWD CARGO, TOP OF FWD SIDE OF FR 598, BOTTOM OF LT SIDEWALL LOWER ATTACH SUPPORT IS GOUGING THROUGH FRAME DOUBLER. BLENDED GOUGE IAW SRM 53-01, FIG 1 OUT OF LIMITS. FORMED AND FABRICATED DOUBLER IAW SRM 53-01, 51-10-4, 51-10-3. INSTALLEDSDR FDEA201011094616Skin · gougedGOUGE EXTERIOR FUSELAGE BOTTOM FWD CORNER OF C2 CUT OUT STA 950E, STR 26R. CUT OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER USING 2024T3 .090 DIMS 50" X 31", FABRICATED 2 EACH STRUCTURAL FILLERS USING 2024T3 .071 DIMS 55" X 14" AND 51" X 13", FABRICATED 1 SDR FDEA201010184107Skin · gougedMCD INNER SURROUND SKIN GOUGED STA 480, STR 8L. REMOVED GOUGED INNER SKIN DIM. 22" X 11" AT BS 480 STR 8L IAW SRM 51-30-2. FABRICATED NEW INNER SKIN FROM 2024 T-3 0.125" DIM. 22" X 11" IAW SRM 53-10-2 FIG 3A. INSTALLED NEW INNER SKIN IAW SRM 51-30-2 REV 103.SDR DALA1025739856Panel · delaminatedDURING LINE CHECK FOUND DELAMINATION ON LT WING OTBD SPOILER PANEL. REPLACED SPOILER PANEL IAW AMM 21-61-01-401 AND CARD 2760-9901M-LO.SDR C8GA2010000056Switch · inoperativeDURING TAKEOFF ROLL AT 80 KNOTS. THE AMBER AFT AIR-STAIR LIGHT ILLUMINATED. ACFT ABORTED TAKEOFF WHERE IT PRECEDED WITH OUT INCIDENT. POST FLIGHT INSP WAS PERFORMED, THE UPPER CONTROL HANDLE SWITCH DETERMINED TO BE AT FAULT. ITEM WAS DEFERRED AND ACFT WAS RESDR ABXR201009250040Mount · corrodedDURING FERRY FLIGHT FLIGHT, PREP FOUND NR1 PYLON AFT MOUNT RECEIVER RUSTED AND PITTED. R & R NR1 PYLON AFT MOUNT IAW MM.SDR ABXR201009250041Isolator · corrodedDURING FERRY FLIGHT PREP FOUND NR 1 PYLON YOKE LOWER ISOLATION ABSORBER RUSTED AND PITTED. R & R LOWER ISOLATION ABSORBER IAW MM.SDR ABXR201009250042Isolator · corrodedDURING FERRY FLIGHT PREP FOUND NR1 PYLON UPPER VIBRATION ISOLATOR RUSTED AND PITTED. R & R NR1 PYLON UPPER VIBRATION ISOLATOR IAW MM.SDR ABXR201009250043Mount · corrodedDURING FERRY FLIGHT PREP FOUND NR2 PYLON AFT ENGINE MOUNT CORRODED. R AND R AFT MOUNT ASSY IAW MM.SDR ABXR201009250044Fitting · corrodedDURING FERRY FLIGHT PREP FOUND NR 2 PYLON FWD LOWER SPLICE FITTING CORRODED. R & R SPLICE FITTING IAW SRM.SDR ABXR201009250045Fitting · corrodedDURING FERRY FLIGHT PREP FOUND NR 2 PYLON FWD. UPPER SPLICE FITTING CORRODED. R & R NR2 PYLON FWD UPPER SPLICE FITTING IAW AMM.SDR ABXR201009250046Yoke · corrodedDURING FERRY FLIGHT PREP FOUND NR 2 ENGING FWD. YOKE CORRODED. R & R NR 2 ENG FWD YOKE IAW AMM.SDR ABXR201009250047Push-Pull Cable · damagedDURING FERRY FLIGHT PREP FOUND NR 2 ENGINE THROTTLE DOES NOT MOVE FROM THROTTLE LEVER. R & R NR 2 ENGINE THROTTLE PUSH PULL CABLE IAW MM.SDR ABXR201009250048Control Cable · brokenDURING FERRY FLIGHT PREP FOUND NR 1 T/R SECTOR ON AFT 'P' DOME DOESN'T MOVE WITH T/R HANDLE MOVEMENT. REPLACED CABLE 47C IAW AMM.SDR ABXR201009250049Control Cable · brokenDURING FERRY FLIGHT PREP FOUND THRUST REVERSER CONTROL CABLE 48C BROKEN. R & R CABLE 48C IAW AMM.SDR ABXR201009250050Control Cable · brokenDURING FERRY FLIGHT PREP FOUND CABLE RUN 52C FOR RT THRUST REVERSER CORRODED AND BROKEN STRANDS. R & R CABLE 52C IAW AMM.SDR ABXR201009250051Control Cable · brokenDURING FERRY FLIGHT PREP FOUND NR 1 ENGINE FWD TELESCOPING BRAIDED CABLE RUSTED, WORN, AND BROKEN STRANDS. R & R NR1 ENGINE FWD TELESCOPING GRAIDED CABLE IAW AMM.SDR ABXR2010092400039Link · corrodedDURING FERRY FLIGHT, PREP FOUND NR1 PYLON AFT MOUNT UPPER INBD "H" DOG BONE AND OTBD BOLT RUSTY. R & R BOLT AND MOUNT LINK IAW MM.SDR DALA1023519860Wedge · damagedDURING GROUND INSP, FOUND DAMAGE TO LT FLAP T/E WEDGE OTBD OF AFT INBD SPOILER. REPAIRED IAW SRM 57-03-10.SDR DALA1023539860Access Panel · damagedDURING GROUND INSP FOUND DAMAGE TO LT INBD FLAP ACCESS PANEL. REPLACED IAW SRM 53-00-00.SDR DALA1022529868Frame · damagedDURING M-CHECK, FOUND 2 EA MISDRILLED HOLES IN AFT ACCY CANTED FRAME AT BS 1275 L3R. REPAIRED IAW SRM 53-02 FIG 18 & SRM 51-30-5.SDR FDEA201008313205Light · damagedCOCKPIT EMERGENCY EXIT LIGHT DOES NOT TEST ON PRE-FLIGHT. R & R COCKPIT EMERGENCY LIGHT ASSY IAW AMM 33-50-101-2-0, OPS CHECKS GOOD. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION. R & R COCKPIT EMERGENCY LIGHT ASSY IAW AMM 33-50-101-2-0, OPS CHECKS GOOD. SDR FDEA201008313206Light · looseEMERGENCY EXIT LIGHT IN COCKPIT POPS OUT OF ITS HOUSING ON ROTATION AND LANDING. FOUND LIGHT NOT PROPERLY SET, RE-SET SAME, OPS CHECK NORMAL AND NOW IS SECURE. ACCOMPLISHED IAW MM 33-50-101-2-0.SDR FDEA201008313247Sill · misinstalledNO EDGE DISTANCE BETWEEN PILOT HOLES AND FASTENER HOLES ON CTR SILL. REMOVED MCD CENTER UPPER SILL IAW SRM, REV 103, 51-30-2. LOCATED AND DRILLED NEW SILL IAW SRM 51-30-5. INSTALLED NEW SILL IAW SRM 51-30-2.SDR DALA1020669885Engine · failedDURING CLIMB AT 4400 FEET ENGINE NR1 EXPERIENCED A COMPRESSOR STALL. THE ENGINE RECOVERED ON IT'S OWN, BUT SMOKE WAS EVIDENT IN THE CABIN AND THE COCKPIT AFTER THE EVENT. FLIGHT CREW COMPLETED THEIR SMOKE CLEARING PROCEDURES AND RETURNED ACFT TO DEPARTURE AIPOSDR FDEA201008283168Skin · damagedDOUBLE DRILLED HOLES MCD CUT-OUT SKIN BS 610 - BS 602, STR 3L. CUTOUT DAMAGED SKIN AREAS, FABRICATED REPAIR DOUBLERS & FILLERS & INSTALLED REPAIR PARTS AT MCD CUTOUT INNER SKIN IAW EA 7-5330-135586.SDR FDEA201008273162Skin · gougedMAIN CARGO DOOR AFT FRAME INNER SKIN IS GOUGED IN NUMEROUS PLACES, BS 620. REMOVED MAIN CARGO DOOR AFT INNER SKIN, FABRICATED NEW SKIN & INSTALLED NEW SKIN IAW SRM 51-10-2, SRM 51-30-2 & HAYES INTERNATIONAL DWG NO. 53FX1551.SDR FDEA201008263158Frame · corrodedAFT PIT, FRAME 990, AFT SIDE SURFACE HAS CORROSION BETWEEN 26R AND 27R. CUT OUT DAMAGE ON BS 990 FRAME BETWEEN STRINGER 26R AND 27R IAW SRM, REV 103, 51-40-4 FIG 2. FABRICATED FILLER, & DOUBLERS IAW SRM 51-40-4 FIG 2. INSTALLED DOUBLERS AND FILLER IAW SRM 51SDR FDEA201008132999Seat Track · corrodedCABIN BS 760 -825 LBL 24 SEAT TRACK, IB FLANGE, HAS CORROSION. REMOVED DAMAGED SECTION OF SEAT TRACK AND BEAM SECTION. FABRICATED NEW BEAM SECTION USING BAC1506-1108 7075T-6 DIMS 96" AND SEAT TRACK SECTION USING BAC1520-841 DIMS 95 1/8" AND INSTALLED IAW DWG SDR FDEA201008133000Seat Track · corrodedCORROSION SEAT TRACK FLANGE MAIN CABIN BS 760.95 - 850 LBL 45. REMOVED DAMAGED SEAT TRACK FROM BS 740 TO BS 850 AND FABRICATED NEW SEAT TRACK SECTION FROM MATERIAL BAC 1520-14667178T6 DIM: 15 7/8" AND INSTALLED NEW PART IAW SRM 51-10-2, SRM 51-30-2 & DWG. NR SDR FDEA201008122957Floorbeam · corrodedCORROSION FLOORBEAM, TOP MAIN CABIN FRONT OF 9G BARRIER. CUTOUT DAMAGED AREA, FABRICATED REPAIR ANGLES & FILLER & INSTALLED FLOORBEAM. REPAIR AT BS 344 IAW SRM 53-10-8, FIG 9, SRM 51-10-2, SRM 51-30-2.SDR FDEA201008122959Shear Tie · corrodedCORROSION ON SHEAR TIE AT BS 700 BETWEEN STRINGERS 28L AND 27L. REMOVED DAMAGED SHEAR TIE IAW SRM, REV 103, 53-10-4 FIG 13. FABRICATED SHEAR TIE USING 7075-T6, .050" X 6" X 7/8" AND DOUBLER USING 7075-T6, .050" X 7 5/8" X 3 5/8" IAW SRM 53-10-4 FIG 13. INSTALSDR FDEA201008122962Hinge · looseAFT HINGE SECTION HAS EXCESSIVE MOVEMENT AT HINGE AND PIN AREA. REMOVED MCD LOWER HINGE ASSY, LOCATED & DRILLED NEW HINGE ASSY & INSTALLED NEW LOWER HINGE ASSY IAW SRM 51-30-2, SRM 51-10-2, & DWG B27-53-070 B & DWG NR 52-487 & 52FX1433.SDR FDEA201008102898Bulkhead · crackedCRACK COMING FROM RIVET HEAD BS 1183, BULKHEAD LBL 58 BETWEEN STR 18R TO 19R LEVEL. CUTOUT CRACKED AREA, FABRICATED REPAIR DOUBLER & FILLER & INSTALLED REPAIR PARTS AT BS 1183 LBL 58 IAW SRM 51-30-2, SRM 51-10-2 & EA 7-5310-135579.SDR FDEA201008102899Seat Track · corrodedCORROSION ON SEAT TRACK AT STA 950, 10", PRODUCTION SPLICE, RBL 45. REMOVED CORRODED SEAT TRACK IAW SRM 51-30-2 AND FABRICATED NEW SEAT TRACK FROM PN BAC1520-7927178T6511, DIM: 91" IAW SRM 53-10-5 FIG 1 REV 103. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2. REMOSDR FDEA201008092889Skin · puncturedPUNCTURE IN SKIN LOWER RUDDER LT SIDE, APPROX VERTICAL STABILIZER FIN STA 110. CUT DAMAGED SECTION OF RUDDER SKIN DIM 1" X 1 1/2" IAW SRM 51-10-1 AND 55-20-3 FIG 1. FABRICATED REPAIR DOUBLER FROM 2024T3 .032" DIM 4 3/4 X 4 3/4" IAW SRM 55-20-3 FIG 1 INSTASDR FDEA201008032786Window · crackedL-2 COCKPIT WINDOW ARCING IN FLIGHT SUBSEQUENTLY SHATTERED. R & R L-2 (PILOTS SLIDING WINDOW ) IAW AMM 56-12-011-4. ADJUSTMENT AND TEST ACCOMPLISHED IAW AMM 56-12-011-5.SDR FDEA201008012764Seat Track · damagedSEAT TRACK DAMAGED STA 600, BL 0. REMOVED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178 T6511 DIMS 120" AND INSTALLED IAW SRM 53-10-2 AND SRM 51-30-2.SDR FDEA201007312770Skin · misrepairedNON-COMPLIANT REPAIR LOCATED AT STA 259, STR 18L. REMOVED PREVIOUS REPAIR, CUT OUT DAMAGE AREA DIM 17.5" X 22", FABRICATED REPAIR DOUBLERS (-1) FROM 2024T3 .090" DIM 25.X22.125" (-2) FROM 2024T3 .063 DIM 27.375"X13.625", REPAIR PARTS AND INSTALLED 2EA REPSDR C8GA201000013Switch · faultedDURING TAKEOFF ROLL WITH THE ACFT BELOW 60 KNOTS THE TAKEOFF WARNING HORN SOUNDED. TAKEOFF WAS ABORTED WITHOUT INCIDENT AND RETURNED TO THE BLOCKS. POST FLIGHT INSP WAS PERFORMED, STABILIZER TAKEOFF WARNING SWITCH S533 WAS AT FAULT. R & R THE STABILIZER TAKEOSDR FDEA201007302742Floorbeam · corrodedCORROSION ON LOWER FLANGE OF MAIN CABIN FLOORBEAM AT BS 720, BL0 TO LBL 35. CUT OUT 2 EACH DAMAGED AREAS DIMS 1.75" X .9" EACH, FABRICATED TWO ANGLES USING 7075-O .071 DIMS 34.25" X 2.75" AND 29 5/8" X 2.5", HEAT TREATED ANGLES FROM 7075-O TO T6 CONDITIONSDR FDEA201007302741Stringer · corrodedCORROSION ON STR 27L, AT BS 550 UNDER CLAMP STAND-OFF BRACKET. REMOVED CORROSION IAW SRM 51-10-6 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. CUT OUT DAMAGED AREA IAW SRM 53-10-3 FIG 1. FABRICATED NEW SECTION OF STRINGER 20" X 2 1/2" IAW SRM 53-10-3 FIG 1
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