N68054, cancelled Feb 3, 2024
Service difficulty reports · 186
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N68054' AND deregistration_id = 'N68054-2024-02-03' 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 n_number = 'N68054' AND deregistration_id = 'N68054-2024-02-03' 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 FDEA201406081356Skin · crackedFOUND RT WING CRACKED JUST ABOVE ANTI-ICE TELESCOPING DUCT CUT OUT. ACCOMPLISH HFEC IAW NTM PT6 20-30-00. REPAIRED IAW EA 8-5710-T0308735 P1 AND SRM 57-40-01 REPAIR 10.SDR FDEA201406081357Skin · crackedRIGHT WING FUEL PNL DOOR CUT OUT HAS A 1"X1/8" STRIP OF PAINT MISSING & LOOKS LIKE A POSSIBLE CRACK. REQUESTED NDT VERIFY. CONFIRMED & MARKED END CRACK LOCATED RT WING FUEL PNL DOOR CUT OUT IAW NDTSPM PT 6. FABRICATED DOUBLER & FILLER, TREATED & PRIMED RESDR FDEA201212134289Light · inoperativeR1 DOOR SLIDE TEST LIGHT INOPERATIVE. REMOVED AND REPLACED PRESSURE INDICATION LIGHT ASSY IAW AMM 25-61-03-2, OPS CHECKED GOOD. OK FOR SERVICE.SDR FDEA201206072130Coalescer Bag · odorPACK ODOR LIKE DIRTY SOCK. R & R NR 2 AND NR 3 COALESCER BAGS IAW MM 21-54-03-2, RAN PACKS FOR 20 MIN AT FULL HOT, FOUND NO FOUL ODOR IN ACFT AT THIS TIME, OK TO CONTINUE.SDR FDEA201206072129Unknown · odorPACK ONE HAS STRONG ODOR. NR 1 COALESCER ALREADY REPLACED, RAN PACKS, NO ODOR AT THIS TIME IAW M/M 21-54-03-2.SDR FDEA201110254643Spar Cap · crackedRT WING REAR SPAR LOWER CAP EO 8-5710-7-5007, PT 2 INSP FOUND CRACK AT FWD, OTBD HOLE COMPLIED WITH EA 8-5710-156726 FOR RT WING REAR SPAR LOWER CAP REPAIR OF FWD OTBD HOLE.SDR FDEA201110254641Door Frame · corrodedAFT CARGO COMPARTMENT DOOR SILL HAS CORROSION AT NUTPLATE HOLES AS MARKED. REMOVED CORROSION AT 12 EA HOLES IAW SRM 51-21-01, 12 EA AREAS ARE WITHIN LIMITS IAW SRM 53-00-01. 1 NUTPLATE HOLE IS OUT OF LIMITS. CUT OUT DAMAGE AND REPAIRED IAW SRM 53-00-01, SDR FDEA201110214618Skin · crackedAFT FUSELAGE OUTER SKIN IS CRACKED APPROX. 3" AT BS 2132 BETWEEN L4R AND L5R. REMOVED DAMAGE IAW SRM 53-00-01, NDT HFEC CHECKED GOOD IAW NTSPM 06-10-01, FABRICATED REPAIR USING 7075-T6 .071 BATCH 0002069744 IAW SRM 53-00-01, FIG 4, SH 2 TREATED AND PRIMED ASSDR FDEA201110214614Skin · crackedRT WING OTBD FLAP UPPER SURFACE 21" FROM THE OTBD EDGE HAS 3EA CRACKS AROUND FASTENER HOLES. REPAIRED RT WING OTBD FLAP UPPER SURFACE CRACKS AT 21" FROM OTBD EDGE IAW SRM 57-10-00, FIG 6 , SH 1-3. MAJOR REPAIR.SDR FDEA201110214613Skin · crackedRT WING OTBD FLAP UPPER SURFACE STA XORS 587 HAS 2 EA CRACKS AROUND FASTENER HOLES. REPAIRED RT WING OTBD FLAP UPPER SURFACE AT STA XORS 587 IAW SRM 57-10-00 VOL 1,FIG 85 SHEET 3. MAJOR REPAIR.SDR FDEA201110174551Doubler · wornAFT FUSELAGE ACCESS DOOR 311AB CUTOUT DOUBLER WORN AND RT SIDE IS ALMOST KNIFE EDGE. REPAIRED IAW EA8-5310-150998SDR FDEA201110164540Cargo Track · corrodedAFT CARGO COMPARTMENT SEAT TRACK, RBL 25 BETWEEN FS 1940 TO FS 1964, GOUGED AND CORRODED. R & R AFT CARGO COMPARTMENT SEAT TRACK AT IAW SRM 51-31-01, MAJOR REPAIR.SDR FDEA201110164539Cargo Track · corrodedAFT CARGO COMPARTMENT SEAT TRACK AT RBL 25 BETWEEN FS 1800 TO 1920, HAS GOUGED AND CORRODED. R & R AFT CARGO COMPARTMENT SEAT TRACK IAW SRM 51-31-01, MAJOR REPAIR.SDR FDEA201110154528Cargo Track · gougedAFT CARGO BAY CARGO TRACK, LBL 25 BETWEEN BS 1920-1964 GOUGED AND CORRODED. REMOVED, AND FABRICATED, REPAIR SPLICES AND PLATES AND REPLACED CARGO TRACK IAW SRM 53-70-00 FIG.1 AND SRM 51-31-01. MAJOR REPAIR.SDR FDEA201110154530Floorbeam · corrodedAFT CARGO COMPARTMENT FLOORBEAM BS 1902 IS CORRODED FROM RBL15 TO LBL15. REMOVED DAMAGE IAWSRM 53-00-01 FIG.8 AND SRM 51-31-01. FABRICATED REPAIR ANGLE AND FILLER IAW SRM 53-00-01. INSTALLED REPAIR ANGLE AND FILLER IAW SRM 53-00-01 FIG 8 AND SRM 51-31-01. MSDR FDEA201110144503Skin · puncturedLEFT WING, INBD FLAP, LOWER OTBD SKIN PUNCTURED. TRIMMED OUT DAMAGE IAW 57-00-01, HFEC IAW NTSPM 06-10-01. NO CRACKS NOTED. FABRICATED SKIN DOUBLER, TEE DOUBLERS, TEE FILLER AND SKIN FILLER IAW SRM 57-00-01 FIG.3 INSTALLED ALL REPAIR PARTS IAW SRM 57-00-0SDR FDEA201110124454Pulley · wornL1 DOOR FWD DRIVE TRACK, UPPER FORWARD PULLEY WORN. FURTHER INSPECTION FOUND PULLEY TO BE SPLIT. MINOR REPAIR R & R L1 DOOR UPPER FWD DRIVE PULLEY IAW SRM 51-31--01 AND MM 52-11-00. NO RIG DISTURBED AND OPS CHECKED GOOD IAW MM 52-11-00-5.SDR FDEA201110114424Shear Tie · crackedMCD CABIN RT SIDEWALL AT STA 1800 AT L-18 SHEAR TIE CRACKED. REMOVED AND REPLACED DAMAGED SECTION OF SHEAR TIE IAW SRM 53-30-00 FIG 10, SRM 51-31-01 AND SRM 51-21-02. MAJOR REPAIR.SDR FDEA201110104409Seat Track · damagedSEAT TRACK AT RBL 45.5 BETWEEN FS 1821 AND FS 1841 UPPER LOBE HAS ELONGATED HOLE. REPLACEMENT ACCOMPLISHED ON NON-ROUTINE N00471 AND IS CLASSIFIED AS MAJOR REPAIR.SDR FDEA201110104408Seat Track · damagedSEAT TRACK AT RBL 45.5 BETWEEN FS 1801 AND FS 1821 UPPER LOBE HAS ELONGATED HOLES. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 53-70-00 FIG 1. FABRICATED SEAT TRACK SECTION, REPAIR SPLICES AND PLATES. INSTALLED REPAIR PARTS IAW SRM 53-70-00 AND SRM 51-31-01SDR FDEA201110044289Seat Track · damagedSEAT TRACK AT LBL45.5 BETWEEN FS 1621 AND 1641 UPPER LOBE HAS ELONGATED HOLE. REMOVED DAMAGED SEAT TRACK SECTION , FABRICATED TRACK, REPAIR SPLICES AND PLATES IAW SRM 53-70 00 FIG.1 VOL. 1. INSTALLED SEAT TRACK, SPLICES AND PLATES IAW SRM 53-70-00 FIG.1. SDR FDEA201110044288Seat Track · gougedSEAT TRACK AT LBL 45.5 BETWEEN FS 1721 AND FS1741 LOBE IS GOUGED. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED TRACK , REPAIR SPLICES AND PLATES IAW SRM 53-70-00 FIG.1 VOL.1. INSTALLED SEAT TRACK, SPLICES AND PLATES IAW SRM 53-70-00 FIG.1. MAJOR REPAIRSDR FDEA201110044290Seat Track · gougedSEAT TRACK AT LBL 45.5 BETWEEN FS 1621 AND FS 1641 UPPER SURFACE IS GOUGED. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 53-70-00 FIG.1 FABRICATED REPAIR SLICES AND PLATES IAW SRM 53-70-00 FIG 1. INSTALLED TRACK SECTION, SPLICES AND PLATES IAW SRM 53-70-00 FSDR FDEA201110044291Seat Track · damagedSEAT TRACK AT LBL 45.5, FS 1721-1741 UPPER LOBE HAS ELONGATED HOLES. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED REPAIR SLICES AND PLATES AND INSTALLED IAW SRM 53-70-00 FIG 1.SDR FDEA201102260785Oxygen Mask · leakingAFTER O2 MASK WERE USED IN FLIGHT ALL 3 O2 BOTTLES DROPPED TO 0 PSI. SERVICED ALL 3, CREW O2 BOTTLES PER AMM 12-14-35. CHECKED ALL BOTTLES AND MASK SYSTEMS FOR LEAKS PER AMM 35-11-00-06-0. FOUND ONE RT COURIER MASK SLIGHTLY LEAKING AT INTIAL BOTTLE RESERVISDR FDEA201010284183Bungee Cylinder · damagedAFTER T/O, LT MAIN REMAINED UNSAFE FOLLOWED QRH CYCLED NO CHANGE. GEAR APPEARED TO BE DOWN ENTIRE TIME. UNEVENTFUL LANDING. REMOVED & REPLACED L/H MLG BUNGEE CYCLINDER ASSY ACFT OK FOR SERVICE.SDR 07FDEA05029Seat Track · damagedMAIN CABIN, BS 1240, LBL 48, SEAT TRACK SCALLOP CHIPPED AND WORN RE-EVALUATED TRACK. TRACK HAS CHIPPED/BROKEN AREAS. OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21 AND 22. REMOVED DAMAGED SECTION AND INSTALLED FABED/NEW SECTION IAW DC/MD10-10 SRM 51-SDR 07FDEA05016Door Frame · corrodedMAIN CARGO DOOR JAMB TOP SURFACE UNDER NR 5 SPOOL FITTING HAS EXFOLIATION, STA 712. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IN REF TO MD/DC10-10 SRM 53-00-01 FIG 1 VOL I. ORIGIONAL .100, REMOVED .047, REMAINING .053. LOCATION OF DAMAGE AT STA 712SDR 07FDEA05015Door Frame · corrodedMAIN CARGO DOOR LOWER JAMB TOP SURFACE MOST AFT PART OF JAMB AT STA 766 HAS SURFACE CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IN REF TO MD/DC10-10 SRM 53-00-01 VOL I. ORIGIONAL .100, REMOVED.027, REMAINING .073. LOCATION OF DAMAGE STA 766, SDR 07FDEA04989Seat Track · damagedMAIN CABIN APPROX AT STA 1256 AND STA 1264 SEAT TRACK SCALLOPS (3EA) ELONGATED (N7513) AT LBL 48 EVALUATED SEAT TRACK FOUND TO BE OUT OF LIMITS IAW DC/MD10 SRM 53-70-00 VOL I PG 21 AND 22. MAT ID S4929150 PO NR 595343.1 IAW DC/MD10 SRM 53-42-01 FIG 5 VOL III.SDR 07FDEA04988Seat Track · damagedCABIN FLOOR TRACK SCALLOP BROKEN OUT AT STA 1139 LBL 48 EVALUATED SEAT TRACK, FOUND BROKEN SCALLOP, OUT OF LIMITS IAW DC/MD10 SRM 53-70-00 VOL I PG 21 AND 22. REMOVED AND REPLACED OUT OF LIMIT SECTION IAW DC/MD10 SRM 51-31-01 VOL II PG 1 AND DC/MD10 SRM 51-SDR 07FDEA04987Seat Track · corrodedMAIN CABIN APPROX AT STA 1531 LBL 27 SEAT TRACK HAS CORROSION. REMOVED AND REPLACED SEAT TRACK AT STA 1490 TO 1531 LBL 27 IAW DC-10/MD-10 SRM 53-70-00, VOL I, FIG 1.SDR 07FDEA04931Seat Track · damagedMAIN CABIN FLOOR TRACK SCALLOP BROKEN OUT AT STA 792 LBL 49. CHECK LIMITS AND IS OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21. REMOVED SEAT TRACK IAW DC/MD10-10 SRM 51-31-01 VOL II PG 1. FABRICATED SPLICE PLATE AND SPLICE HAT IAW DC/MD10-10 SSDR 07FDEA04930Seat Track · damagedCABIN FLOOR TRACK SCALLOP BROKEN OUT AT STA 1059 LBL 48. FOUND TO BE OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 PGS 21 & 22 VOL I REMOVED TRACK IAW DC/MD10-10 SRM 51-31-01 VOL II PGS 1-10. IAW DC/MD10-10 SRM 53-42-01 VOL III PGS 13 & 14. FABRICATED SEAT TSDR 07FDEA04929Seat Track · gougedCABIN FLOOR TRACK GOUGED AT STA 1119 RBL 48 2 EACH SCALLOPS.SDR 07FDEA04928Seat Track · gougedCABIN FLOOR TRACK GOUGED AT STA 1119 RBL 48 2 EACH SCALLOPS. BLENDED AREA .500 MAX LIMIT GAP .510 REMAIN. OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21 & 22. MAT ID TRACK, SPLICE HAT & PLATE. REMOVED DAMAGED TRACK INSTALLED NEW SECTION IAW DC/MD10-1SDR 07FDEA04927Seat Track · wornFOUND MAIN CABIN AT STA 1441 RBL 48 SEAT TRACK WORN. BLENDED SEAT TRACK, WIDTH OF SCALOP HAS .200 REMAINING MIN IS .260 OUT OF LIMITS IAW DC 10 SRM 53-70-00 VOL I PG 21". REMOVED AND REPLACED DAMAGED SECTION OF TRACK IAW DC/MD10 51-31-01. ALODINED & PRIMESDR 07FDEA04926Seat Track · damagedFOUND MAIN CABIN, BS 1085, RBL 28, SEAT TRACK SCALLOP CHIPPED. BLENDED AREA; CHECKED LIMITS. GAP BETWEEN SCALLOPS IS.520 MAX ALLOWED IS .500 OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21. REMOVED DAMAGED TRACK SECTION AND INSTALLED NEW SECTION IAWSDR 07FDEA04925Angle · chafedNR 1 PYLON THRUST LINK RUBBING AGAINST WING O/B THRUST ANGLE, STA YN348 CENTERED THRUST LINK, CLEANED AREA AROUND ATTACHMENT PIN & BUSHING, INSPECTED AREA OF BEARING & BUSHING IAW FEDEX WORK CARD 54X1201ALI-P1 LUBED THRUST LINK BEARING IAW FEDEX MM 12-21-02SDR 07FDEA04924Seat Track · damagedMAIN CABIN FLOOR TRACK SCALLOP BROKEN OUT AT STA 814 LBL 29. CHECKED LIMITS ON SEAT TRACK SCALLOPS. SCALLOPS TO SCALLOPS IS .510 OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21. DIAL CALIPERS USED T8278D. REMOVED SEAT TRACK IAW DC/MD10-10 SRM 51-SDR 07FDEA04909Door Frame · corrodedMAIN CARGO DOOR LOWER JAMB AT NR 7 SPOOL LOCATION, ALL FOUR HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,D TO .517 AND HOLE D TO .484 TO REMOVE CORROSION IN REF TO MD/DC10-10 SRM 53-50-01 FIG 17 VOL I. ACCOMPLISHED BHEC IN REF TO NTSPM 06-SDR 07FDEA04908Door Frame · corrodedMAIN CARGO DOOR LOWER JAMB AT NR 6 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,C TO 0517 AND HOLE D TO .484 TO REMOVE CORROSION IN REF TO MD/DC10-10 SRM 53-50-00 FIG 17 VOL I. ACCOMPLISHED BHEC IN REF TO NTSPM 06-10-SDR 07FDEA04907Door Frame · corrodedMAIN CARGO DOOR LOWER JAMB AT NR 5 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,D TO .517 AND HOLE D TO .484 TO REMOVE CORROSION IN REF TO MD/DC10-10 SRM 53-50-01 FIG 17 VOL I. ACCOMPLISHED BHEC IN REF TO NTSPM 06-10-SDR 07FDEA04906Door Frame · corrodedMAIN CARGO DOOR LOWER JAMB AT NR 4 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,C TO .460 TO REMOVE CORROSION. WITHIN LIMITS OF MD/DC10-10 SRM 53- 50-00 FIG 17 VOL I. HOLE D REAMED TO REMOVE CORROSION AND INSTALLED BSDR 07FDEA04905Door Frame · corrodedMAIN CARGO DOOR LOWER JAMB AT NR 2 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,C,D TO REMOVE CORROSION AND INSTALLED REPAIR BUSHINGS. FOUND REPAIR BUSHINGS WOULD NOT MEET THE LIMITS STATED IN MD/DC10-10 SRM 53-50-00 SDR 07FDEA04904Door Frame · corrodedMAIN CARGO DOOR LOWER JAMB AT NR 1 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,C,D TO REMOVE COROSION AND INSTALLED REPAIR BUSHINGS. FOUND REPAIR BUSHINGS WOULD NOT MEET THE LIMITS STATED IN MD/DC10-10 SRM 53-50-00 FSDR 07FDEA04903Beam · corrodedMAIN CARGO DOOR JAMB TOP SURFACE UNDER CENTERING GUIDE HAS SURFACE CORROSION, STA 660. REMOVED AND REPLACED BEAMS ACA7225-1 AND ACA7226-1 IN REF TO DAC DRAWING ACA7224 REV G AND DC/MD10-10 SRM 51-31-01 VOL II PG 1, MD/DC10-10 SRM 51-33-01 VOL II PG 1 AND DC/SDR 07FDEA04799Skin · crackedRT HORIZONTAL STAB UPPER REAR SKIN PANEL HAS APPROXIMATELY A I/2 INCH LONG CRACK INDICATION. REPAIRED RIGHT HAND HORIZONTAL STAB SKIN PANEL IN REFERENCE TO EA 8-5510-109228.SDR 07FDEA02092Door Frame · corrodedEXFOLIATION CORROSION LOCATED AT LOWER AFT CARGO DOOR CUTOUT, FWD LOWER CORNER. CORROSION EXCEEDED SRM LIMITS AFTER REMOVAL, REQUIRED EA TO FLY UNTIL NEXT C CHECK.SDR 06FDEA03090Loop · faultyCLIMBOUT FROM MEMPHIS GOT A LEVEL 3 AIR MAN NR 2 FAILED WARNING WENT AWAY AFTER THROTTLE WAS AT IDLE FOR A COUPLE OF MINUTES, DUMPED 6000 LBS FUEL FOR LANDING. ACN RELEASED FOR SERVICE PER MEL/CDL: 36-23-01-02 CATEGORY: C EXPIRATION: 05SEP06 "MEL 36-23-01-02
Back to N68054, cancelled Feb 3, 2024