Pratt & Whitney JT8D-17
Service difficulty reports · 1,680
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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 = '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 DALA1033579853Bulkhead · crackedDURING M-CHECK AND IAW AD-FAR AFT ACCY COMPARTMENT-AFT PRESSURE BULKHEAD RT LOWER CORNER HAS CRACK IN 5910130-85 GUSSET AND 5910130-87 DOUBLER, JUST ABOVE -37 SEAL CHANNEL. NDT VERIFIED CRACK STOPS ABOVE -37 SILL CHANNEL USING A2469 ZETEC IAW NDT SPM 06-10-01.SDR DALA1033589853Frame · gougedDURING M-CHECK, FOUND AFT ACCESSORY COMPARTMENT RT SIDE CANTED STA 1243, BETWEEN STRINGER 13-14, FRAME GOUGED ON BOTH SIDES COMPLETELY THROUGH. RT CANTED FRAME STA 1243 BETWEEN STR 13-14 CUTOUT DAMAGE 2" X 1" NDT HFEC VERIFIED DAMAGED REMOVED IAW NDT SPM 06-10SDR C8GA2010000076Connector · damagedON APPROACH, THE NLG DID NOT INDICATE GREEN. LIGHT REMAINED RED, ALL 3 LANDING GEAR WERE MANUALLY EXTENDED. ACFT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED. R & R THE NLG POSITION SWITCH, R & R NLG LOCK SWITCH CONNECTOR PLUG, REPLACED 2 EACH WIRSDR FDEA201011234481Frame · damaged2 EACH OPEN HOLES IN FRAME AND REPAIR DOUBLER - STA 950C AT STR 24L. REMOVED REPAIR DOUBLER IAW SRM 51-30-2 REV 103 FORMED NEW REPAIR DOUBLER FROM 7075 O .080" DIM 8" X 4 1/2" IAW SRM 53-10-2 FIG 5 AND 51-20-1 FIG 7 INSTALLED REPAIR DOUBLER IAW SRM 51SDR DALA1033099853Frame · crackedDURING M-CHECK FOUND CRACK IN FRAME STA 1230 L2, LT CUT OUT DAMAGED AREA 3.5" X 8750" IAW SRM 53-02, FIG 32. PERFORMED NDT SPM 06-10-01. CRACK WAS REMOVED. FABRICATED -3 REPAIR ANGLE FROM S09530095-03 FABRICATED -29 FILLER FROM .050 7075-T6 FABRICATED L ANGLESDR DALA1033129853Seat Track · corrodedDURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 285-313, LBL 22 SEAT TRACK HAS CORROSION. REMOVED CORROSION FROM BS 200-313, LBL 22 IAW SRM 51-10-3. ORIG MAT .100, REMOVED .051, AREA BLENDED 3" X 1.5" OUT OF LIMITS IAW SRM 53-05, FIG 4B. REMOVED SEAT TRACK ISDR DALA1035699855Bulkhead · crackedDURING M-CHECK FOUND STA 69 BULKHEAD RT WEB HAS CRACK APPROX 2 INCHES LONG. GAIN ACCESS, CUT OUT DAMAGE AREA 2" X .5", HFEC INSPECTED VERIFIED DAMAGE. REMOVED FABRICATED DOUBLER AND FILLER LOCATED, DRILLED DEBURRED TREATED PRIMED AND INSTALLED DOUBLER AND FILLSDR DALA1036299855Intercostal · damagedDURING M-CHECK, FOUND BS 218- 237, BL0 WEB HAS MANY ELONGATED HOLES. REMOVED INTERCOSTAL IAW SRM 51-30-2 & 51-30-5. LOCATED, DRILLED & INSTALLED NEW INTERCOSTAL IAW SRM 51-10-4 & 52-30-5.SDR DALA1036709855Floorbeam · crackedDURING M-CHECK, FOUND FWD CARGO BS 655, LT STRUT CRACKED AT LOWER END. REMOVED SEVERAL FASTNER'S FOR ACCESS IAW SRM 51-30-2, STOPPED DRILLED CRACK IAW SRM 53-01, FIG 2. FABRICATED REPAIR DOUBLER IAW SRM 53-01, FIG 2 TREATED & PRIMED IAW SRM 51-10-3. INSTALLESDR DALA1035819855Frame · damagedDURING M-CHECK, FOUND AFT CARGO COMPARTMENT BS 1088 BETWEEN L30 & L29R FRAME HAS A HOLE ON TOP SIDE. FORMED REPAIR ANGLE DRILLED AND LOCATED, TRIMMED, TREATED, PRIMED & INSTALLED IAW SRM A53-10-05, 53-13-3, FIG 3, 51-30-2, 53-10-2, 51-30-5, 53-03, PG 4.SDR DALA1036469855Longeron Splice · crackedDURING M-CHECK, FOUND AFT CARGO COMPARTMENT BETWEEN STA 1068 & 1088, L29L SPLICE CRACKED. R & R CRACKED SPLICE AT AFT CARGO COMPARTMENT IAW SRM 51-30-5.SDR DALA1100789855Frame · damagedAFT CARGO COMPT BS 1108, L26L FRAME HAS A HOLE ON TOP SIDE. FABRICATED AND INSTALLED REPAIR STRAP IAW DC9-A-53-10-05-801-663A-A. REQUIRED INSP COMPLETED.SDR DALA1100899864Skin · chafedAFT ACCESSORY BETWEEN CANTED FRAME 1314 AND 1326 SKIN IS CHAFED BELOW RT SIDE OF VENTRAL STAIRWAY CROSSFRAME SUPPORT. BLENDED AREA OUT OF LIMITS. FABRICATED DOUBLER CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW SRM 53-01, FIG 4, 53-33-0 FIG 5, 51-10-SDR DALA1031879853Intercostal · crackedDURING M-CHECK FOUND FWD CARGO BETWEEN STA.218 AND 237 JUST OTBD OF LT LONG 28. INTERCOSTAL HAS CORROSION AND CRACKED APPROX 1 IN. DRILLED STOP HOLE IN INTERCOSTAL IN FWD CARGO STA 218-237 JUST OTBD OF LONG 28. FABRICATED REPAIR DOUBLERS FROM .025" 7075T6. SDR DALA1032969884Rib · damagedDURING LINE CHECK FOUND FLAP DAMAGE TO LT WING FLAP T/E 4 FT OTBD FROM INBD MOST EDGE. REMOVED T/E PANEL 788 IAW CMM 27-50-1. REMOVED DAMAGED RIB SRM 57-03 INSTALLED NEW CHANNEL AND DRILLED UP NEW TIP IAW SRM 57-50-09. INSTALLED INBD LT FLAP T/E TIP, IAW SRSDR DALA1032809853Support Angle · crackedDURING M-CHECK FOUND LT WING FLAP, NR4 FLAP HINGE INBD INSIDE ACCESS HOLE SUPPORT ANGLE IS CRACKED. REMOVED DAMAGED SUPPORT ANGLE ON LT WING NR4 FLAP HINGE INBD SIDE AND FORMER IAW SRM 51-30-02. INSTALLED SUPPORT ANGLE PN 09-2700-3-2300. PO 0297W013 AND INSTSDR DALA1032819853Support Angle · crackedDURING M-CHECK, FOUND LT WING FLAP, NR4 FLAP HINGE OTBD INSIDE ACCESS HOLE SUPPORT ANGLE IS CRACKED. REMOVED FLAP HINGE SUPPORT ANGLE (NR 4) IAW SRM 51-30-02. INSTALLED NEW SUPPORT ANGLE PN 09-2700-3-2828, PO0304W007 AND NEW BRACKET PN 09-2100-3-0515 IAW SRSDR DALA1032829853Seat Track · corrodedDURING M-CHECK FOUND MAIN PASSENGER CABIN STA 200-285, RBL44, SEAT TRACK HAS CORROSION IN SEVERAL AREAS. REMOVED CORROSION AT RBL 44, BS 200-285, ORIGINAL MATERIAL .115 MAT, REMAINING .080 OUT OF LIMITS IAW SRM 53-01, FIG 1, REMOVED SEAT TRACK IAW SRM 51-30-2SDR DALA1032839853Skin · damagedDURING M-CHECK, FOUND FUSELAGE EXTERIOR, LT WINDOW BELT, WINDOW NR6 AFT EDGE OF CUTOUT CRACKED AS MARKED. REF SID INSP PROCEDURE SEQUENCE 1, METHOD 01, FOR PSE 53.09.021 SID MANUAL VOL II, SECTION 253-30-09. ATTACH SSI REPORT FORM 5100-3201. ENTER INTO DEF TOSDR DALA1032849853Seat Track · corrodedDURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 200-285, RBL 22 SEAT TRACK HAS CORROSION SEVERAL AREAS. REMOVED CORROSION IAW SRM 53-05. FOUND TO BE OUT OF LIMITS. ORIGINAL MAT .080, REMOVED .017, .063 REMAINING. REMOVED FLOOR SUPPORT AND SEAT TRACK IAW SRM SDR DALA1032859853Longeron · crackedDURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 160 LONG 4L IS CRACKED REMOVED L4L END CLIP, REPAIR SPLICE & 19" SECTION OF LONGERON IAW SRM 51-10-4,51-10-2,51-30-2 & 51-30-5. RECIEVED NEW SECTION OF LONGERON PN2777922-3 PO1021994. LOCATED & DRILLED FASTENER SDR DALA1032869853Former · crackedDURING M-CHECK FOUND MAIN PASSENGER CABIN APB NR4 FORMER FROM FLOOR LEVEL RT SIDE OTBD END IS CRACKED. REMOVED EXISTING END CLIP, TRIMMED OUT CRACKED 1" X 2" NDT TO VERIFY, CRACK CONTAINED, RECEIVED 2EA CLIPS PN 09-5300-3-0914, PO1031968, PN9915558-234N, PO10SDR DALA1032879853Longeron · crackedDURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 160, LONG 3 IS CRACKED. RECEIVED L3L END CLIP, REPAIR SPLICE & 18.8125" SECTION OF LONGERON IAW SRM 51-10-4, 51-10-2, 51-30-2 & 51-30-5. RECEIVED NEW SECTION OF LONGERON 18.8125" PN S2777922-1 PO 1021968 & END CLISDR DALA1032749853Skin · crackedDURING M-CHECK, FOUND FUSELAGE EXTERIOR STA 1258 BETWEEN L5R AND L6R SKIN CRACKED AT FASTENER FABRICATED FILLER AND DOUBLER MATERIAL 7075-T6 .040 LOT NR 1022364 IAW SRM 53-01, FIG 4 MAT ID IAW SRM 53-33-0 LOCATED DRILLED AND DEBURRED HOLES IAW SRM 51-10-01. ISDR FDEA201011174410Battery Pack · inoperativeL1 DOOR EMERGENCY SLIDE LIGHT INOP. R & R SHIELD ASSY AND RELAMPED DUE TO CORROSION. NO HELP MM 33-50-041-2. R & R BATTERY PACK ASSY IAW MM 33-50-051-2. OPS CHECK NORMAL. PREMATURE REMOVAL/INSTALLATION.SDR DALA1101019855Attach Fitting · crackedPYLON REAR SPAR AFT MOUNT UPPER ATTACH FITTING CLIP CRACKED AT BOLT. REMOVED CRACKED CLIP IAW SRM 51-30-5. FABRICATED CLIP IAW DWG 9915500. INSTALLED NEW CLIP IAW SRM 51-30-5.SDR DALA1032649853Web · crackedDURING M-CHECK, FOUND NOSE W/W LT TUNNEL STA 105, LBL 25 PRESSURE DECK WEB CRACKED MATERIAL ID FOR DOUBLER REPAIR .025 DMS1592, T1-6AL-4VPO NR1022171, FILLER .040 2024-T3, PO1022422 IAW 10-02-801-663A. REMOVED WEB SUPPORT BRACKET, FITTING BRACKET AND WIRE BUNDSDR TSAA1027019Indicator · failedDURING CLIMB, THE CREW SELECTED FLAPS UP AND NOTED A SPLIT-FLAP INDICATION, WITH NO ROLL ENCOUNTERED. CREW ATTEMPTED TO SELECT FLAPS 1 WITH NO EFFECT. CREW DECLARED AN EMERGENCY, ACCOMPLISHED T/E FLAPS DISAGREE CHECK LIST WITH FLAPS 15. ACFT LANDED WITHOUT SDR DALA1035319864Skin · damagedDURING M-CHECK, FOUND FWD CARGO COMPARTMENT, DURING INSPECTION, MATERIAL THINNING INDICATION BETWEEN OUTER SKIN AND INNER DOUBLER AT DME ANTENNA STA 340 MIN. REMAINING MATERIAL .041 DEFER TO ENGINEERING. R & R DOUBLER AND FINGER DOUBLER PN 09-5300-3-0014 AND PSDR DALA1036699855Structure · crackedDURING M-CHECK, FOUND MAIN CABIN STA 1151, LBL 41 HAS CORROSION AROUND SCREW HOLE. TRIMMED OUT CRACK IAW SRM 53-01, FIG 4, SH 4. NDT SPM 06-10-01.001. FABRICATED DOUBLER & FILLER IAW SRM 53-01, FIG 4, SH 4. INSTALLED IAW SRM 51-30-5.SDR DALA1031909853Floor Panel · crackedDURING M-CHECK FOUND CABIN FLOOR PANEL NR78 IS CRACKED AT AFT END SCREW HOLE APR 1.5 IN CUT OUT CRACK (ZAE) FLOOR PANEL NR78 1.5"X 4.7" IAW SRM 53-05. MATERIAL IS 7075-T6 .025 PO122211 FILLER, DOUBLER 7075-T6.032, PO1022537. FABRICATED DOUBLER & FILLER IAW SSDR DALA1032029853Window Frame · crackedDURING M-CHECK FOUND CABIN/WINDOW FRAME CRACKED BETWEEN STA 889 AND 908 RT SIDE WINDOW 36R AT TOP AFT FASTENER. REMOVED DAMAGE IAW SRM 53-05, FIG 122 FORMED, ALODINED AND PRIMED REPAIR ANGLE IAW 51-10-3 NDT GOOD INSTALLED REPAIR PARTS AND FASTNERS USING MATERSDR DALA1032899855Floor Support · corrodedDURING M-CHECK, FOUND MAIN CABIN STA 160 TO 218 BL 0 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION, ORIG MAT .060. REMOVED .035, REMAINING .025, FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED AND INSTALLED NEW FLOOR SUPPORT FROM S2652479 7075T6 PO1021997 IASDR DALA1034819855Seat Track · corrodedDURING M-CHECK FOUN MAIN CABIN STA 303 TO 313 LBL 22 SEAT TRACK HAS CORROSION. REMOVED CORROSION ORIGINAL MAT.090. REMOVED .070 REMAINING .020 OUT OF LIMITS. R & R SEAT TRACK IAW SRM 51-10-3 53-05, FIG4B 51-30-5 51-30-1, 51-10-3 51-30-2, 53-05, FIG 4F P125 02SDR DALA1034879855Seat Track · corrodedDURING M-CHECK FOUND MAIN CABIN STA 200 TO 285, RBL 22 SEAT TRACK HAS CORROSION. ORIGINAL MATERIAL .090, REMOVED .031, REMAINING .059, R & R SEAT TRACK STA 200-285 IAW SRM 51-10-3, 53-01 FIG 1, 51-10-1, 51-30-5, 51-10-2, 51-10-4, 53-05 FIG 4F,51-10-3B, P125.SDR DALA1035099853Cusp Web · damagedDURING M-CHECK, FOUND LT CUSP WEB HAS 4 EA REPAIRS WITHIN 6 INCHES OF EACH OTHER BETWEEN STA 693 AND 712, OUT OF LIMITS IAW DELTA TOPPS MAN 30-10-70 PAR 6B. REMOVED CUSP WEB IAW SRM 51-30-1, 51-30-2, 51-30-5. FAB AND INSTALLED NEW IAW SRM 51-10-4, DWG 991051 &SDR DALA1031729853Attach Fitting · crackedDURING M-CHECK FOUND MAIN PASSENGER CABIN APB NR5 FORMER FROM FLOOR LEVEL RT SIDE UPPER OTBD ATTACH CLIP IS CRACKED. REMOVED OTBD UPPER CLIP FROM RT NR5 FORMER MAIN CABIN APB IAW SRM 51-30-2. RECEIVED NEW UPPER RT CLIP OTBD IAW SRP DC-9-A-53-10-25-801-663A-ASDR DALA1031839853Floor Panel · crackedDURING M-CHECK, FOUND MAIN CABIN FLOOR PANEL NR51 CRACKED AT FWD END FASTENER HOLE. TRIMMED OUT CRACK FROM FLOOR PANEL NR51 WEB (1.7"X 2.2") IAW SRM 53-01 FIG 4 SHT.4 PERFORMED HFEC INSP OF CUTOUT AREA IAW NDT SPM 06-10-01.001 NO CRACKS NOTED. FABBED REPAIR SDR DALA1031859853Floor Panel · corrodedDURING M-CHECK, FOUND MAIN PASSENGER CABIN FLOOR PANEL NR70 HAS CORROSION ON TOP OF PANEL AROUND FASTENER HOLES. BLENDED CORROSION AROUND FASTNER HOLES ON CABIN FLOOR PANEL NR70 ORIG MAT .025. REMOVED .008, REMAINING .017 DETERMINED TO BE OUT OF LIMITS IAW SSDR DALA1031869853Floor Panel · crackedDURING M-CHECK, FOUND MAIN CABIN FLOOR PANEL NR67 CRACKED AT END. REMOVED FASTENERS AND SECTION OF SKIN AT DAMAGED AREA FABRICATED FILLER FROM 7075T6 .025 AND DOUBLER FROM 7075T6 .032 USED NDT TO VERIFY NO CRACK EXISTS IAW NDT SPM 06-10-01.001 PRIMED PARTS IASDR DALA1032019853Doubler · crackedDURING M-CHECK, FOUND FUSELAGE EXTERIOR STA 133 LT SIDE, L1 DOOR HOLD OPEN LATCH DOUBLER HAS APPROX 1 INCH CRACK. R & R FUSELAGE EXTERIOR L1 DOOR HOLD OPEN LATCH DOUBLER PN J060283-3, PO/LOT 0298W028 AT LT FS133 IAW SRM 53-04, FIG 24, SHTS 1-5. TOP COAT PROTECSDR DALA1031769853Longeron · crackedDURING M-CHECK FOUND MAIN CABIN STA 389, LONGERON 17 RT IS CRACKED AT FRAME IAW 5310-01313-01, STEP 4 PRIOR TO FURTHER FLIGHT. REMOVED SPLICE AT BS 399, RT L-17 IAW SRM 51-30-2 & 51-30-05. CUT OUT SECTION RT LONGERON 17 RS 379-399 IAW SRM 53-02, FIG 18. FSDR DALA1031779853Bulkhead · gougedDURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 1136 UPPER LT BULKHEAD WEB FWD SIDE IS GOUGED. GOUGE FOUND OUT OF LIMITS IAW SRM 53-01, FIG 1. REMOVED DAMAGE AND NDT VERIFIED IAW NDT SPM 06-10-01. FABRICATED REPAIR ANGLE FROM .090 7075-0 AND HEAT TREATED TO SDR DALA1031939853Floor Support · crackedDURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 160-200, LBL 56, FLOOR SUPPORT CRACKED 4EA PLACES. REMOVED DAMAGED FLOOR SUPPORT FROM FS 160 TO FS 200, LBL 56. RECEIVED Z ANGLE FLOOR SUPPORT PN S4616493-12500. CUSTOMER FURNISHED. LOCATED AND DRILLED HOLES INSDR DALA1032009853Doubler · corrodedRT MLG W/W-DOOR HINGE ATTACH DOUBLER CORRODED FROM BS 787-837. REMOVED CORROSION. FOUND OUT OF LIMITS MAT LOSS AT 100 PERCENT. MAT ID 0507075-T6 IAW DWG 9923459, REV AE FABRICATED, LOCATED, DRILLED, DEBURRED, TREATED & PRIMED NEW DOUBLER IAW DWG9923459 REV ASDR DALA1032049853Attach Angle · crackedDURING M-CHECK FOUND NR 2 ENGINE PYLON LOWER ATTACH ANGLE APPROX STA 1136 CRACKED. STOP DRILLED CRACK .25 AT EACH END IAW SRM 54-04, FIG 10, SHEET 2, HFEC INSPECTED STOP DRILL AREA IAW SPM 06-10-01.001 CRACK FOUND TO BE CONTAINED A2700 MAT ID FOR REPAIR ANGLE SDR CA101118008Dome · stripped(CAN) DURING TAKEOFF ROLL AT APPROX 80 KNOTS, ENGINE NR 2 NOSE DOME FELL OFF IN THE ENGINE INLET. THIS CAUSED THE ENGINE TO STALL (LOUD BANGS). THE TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE 4 STUDS THASDR DALA1034389855Hinge Bracket · crackedDURING M-CHECK FOUND RT WING; NR4 FLAP HINGE INBD ATTACH BRACKET CRACKED. R & R DAMAGED BRACKET IAW SRM 51-30-2, SRM 51-10-4, SRM 51-10-3, SRM 51-30-2M.SDR CA101122001Hinge · sheared(CAN) ON ARRIVAL OF THE MAINTENANCE PERSONNEL THEY FOUND THE INBOARD HINGE BROKEN AND THE CRACK ON THE KRUGER FLAP INBD SKIN WHICH COULD HAVE BEEN CAUSED WHEN THE KRUGER FLAP WAS EXTENDED CATCHING THE WING (WHICH WAS NOT DAMAGED) BENDING THE UPPER INBD SKIN OFSDR DALA1034379853Floor Panel · corrodedDURING M-CHECK FOUND FLOOR PANEL NR26 HAS CORROSION ALONG FWD END, TOP AND BOTTOM SIDES. REMOVED 3 STIFFENERS AND TOILET DRAIN FROM PANEL IAW SRM 51-30-2. FAB NEW PANEL HAT IAW DWG NR9957918. ALODINED NEW PANEL HAT IAW SRM 51-10-3. PRIMED IAW SRM 51-10-3. PA
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