Mcdonnell Douglas MD-11
Service difficulty reports · 7,956
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 aircraft_model_key = 'MD11' 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 aircraft_model_key = 'MD11' 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 FDEA200906172133Wire · shortedDURING SERVICE CHK FOUND RAM AIR DOOR CTL FOR PACK NR 3 CB POPPED. ON INVESTIGATION FOUND OVHD CB PANEL WIRE BUNDLE TOUCHING A SCREW ON THE PANEL CAUSING A WIRE TO CHAFE AND SHORT TO GND. PERFORMED INSP ON ASSOCIATED WIRE BUNDLE, FOUND WIRE NR 8201-317-22 CHSDR FDEA200906162119Longeron Splice · crackedCABIN - LEFT STA 1521-1541 LONGERON -6 SPLICE FITTING FOUND CRACKED. SPLICE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL2 REV40. (MAJOR CAT A REPAIR)SDR WRLA2009152Seat Track · crackedDURING C-CHK IN TPE - INSPECTION FOUND: CRACK ON SEAT TRACK AT STA 635 AT X= 47.6 (REF EGAT NRC U05109). CUT OUT SEAT TRACK FROM Y= 605 TO 725 AT X= 47.5 AND REPAIRED SEAT TRACK IAW MD-11 SRM 53-70-00 VOL 1 REV 40 FIG 1. JOB COMPLETED AND CONDITION CHECK NSDR WRLA2009154Floor Support · corrodedDURING 4C-CHK IN TPE - EGAT FOUND: MID DECK CABIN FLOOR SUPPORT CORROSION ON STA 735 X= 8.5 & -8.5 (REF EGAT NRC U05053). REMOVED DAMAGED SUPPORT IAW MD-11 SRM VOL 2 51-35-01 REV 40. FABRICATED NEW SUPPORT IAW EI W2009A53B-601 REV O. INSTALLED NEW SUPPORTSDR WRLA2009153Floor Support · corrodedDURING 4C-CHK IN TPE - EGAT FOUND: MID DECK CABIN FLOOR SUPPORT CORROSION ON STA 1361 AT X= -52 (REF EGAT NRC U05055). REMOVED DAMAGED SUPPORT IAW MD-11 SRM VOL 2 51-35-01 REV 40. FABRICATED NEW SUPPORT IAW EI W2009A53-B-595 REV O. INSTALLED NEW SUPPORT ISDR WRLA2009148Hinge · crackedDURING 4C-CHK IN TPE - EGAT FOUND: FOUND LT O/B I/B AFT HINGE INTERNAL SUPPORT CRACKED (REF EGAT NRC U05094). REPLACED O/B FLAP I/B AFT HINGE SUPPORT IAW EI W2009A57B-637 REV O. CONDITION CHK NORMAL AND JOB COMPLETE.SDR WRLA2009149Floor Support · corrodedDURING 4C-CHK IN TPE - EGAT FOUND: FOUND MID DECK CABIN FLOOR SUPPORT CORROSION ON STA 1887 AT X= 30-35 (REF EGAT NRC U05052). REMOVED DAMAGED SUPPORT IAW MD-11 SRM VOL 2 51-35-01 REV 40. FABRICATED NEW SUPPORT IAW EI W2009A53-B-602 REV 0. INSTALLED NEW SUSDR CO1Y200900004Fitting · corrodedFOUND CORROSION ON 4 EA HOLES AND LUG FACES OF RT FRAME FITTING. REMOVED CORROSION AND INSTALLED REPAIR BUSHINGS IAW ARP-TPR-09-0017-02B. (K)SDR WRLA2009115Skin · gougedDURING A-8 CHECK AT DELTA AIRLINES (ATL) INSPECTION FOUND BULK CARGO DOOR AFT DOOR SKIN GOUGED. BLENDED OUT DAMAGE TO EXT SKIN. FABRICATED REPAIR PER SRM 52-10-00. CHEMICALLY TREAT PER PS 900-2-1 NR 2. FABRICATED PAN DOUBLER PER ERA 474608-14. INSTALLED PSDR WRLA2009117Panel · crackedDURING C-CHK IN TPE INSPECTION FOUND STEP PANEL CRACKED IN AVIONICS COMP FWD CORNER OF LADDER - SIDE PANEL AT STA 348 (REF EGAT NRC U05042). PER AMM 20-50-02-900-801 / 910-801 REV 63 REPLACED THE STEP COVER. CONDITION CHECK NORMAL & JOB COMPLETE.SDR WRLA2009116Channel · crackedDURING C-CHK IN TPE INSPECTION FOUND THE RIGHT WING FUEL ACCESS CHANNEL CRACKED AT F/ACCESS PNL 633AT, 634BT, 636AB, 636BB, 636CB, & 638DB (REF EGAT NRC U05081). REPLACED THE DAMAGED CHANNELS AND RUB STRIP AT F/ACCESS PNLS 633AT, 634BT, 636AB, 636BB, 636CB, SDR WRLA2009113Support · corrodedDURING C-CHK IN TPE INSPECTION FOUND CORROSION AT CAC BATTERY AND CHARGER SUPPORT ASSY STA 1149 (REF EGAT NRC U05083). BLENDED OUT THE CORROSION AREA AND REQUESTED NDT TO PFM REWORK AREA FOR UT CHK. MEASURED REWORK AREA DEPTH=0.0125 INCH IAW MD-11 SRM 51-00-SDR WRLA2009110Strap · crackedDURING C-CHK IN TPE INSPECTION FOUND FWD CEILING PNL SUPPORT STRAP HAS CRACK AND RIVETS MISSING AT WBL +35 STA 968 (REF EGAT NRC U05085). REPLACED THE DAMAGED PNL SUPPORT STRAP IAW MD-11F VOL 2 51-35-01 REV 40. CHECK NORMAL AND JOB COMPLETE.SDR WRLA2009109Channel · crackedDURING C-CHK IN TPE INSPECTION FOUND CRACK FROM VERT STAB ACCESS PNL 364FR. FOUND AFT FUSELAGE UPPER SKIN CHANNEL BOTH ENDS CRACKED AT STA 2065 BETWEEN X=13.65 AND X=-13.65 (REF EGAT NRC U05086). REPAIRED THE CHANNEL ON VERT STAB ACCESS PNL 364FR IAW MD-11F SDR WRLA2009108Web · crackedDURING C-CHK IN TPE INSPECTION FOUND SUPPORT BEAM WEB CRACK AT CENTER CARGO STA 1841 X=-15 TO X=16 (REF EGAT NRC U05094). REMOVED THE DAMAGED WEB & FASTENERS IAW MD-11F SRM VOL 2 51-33-01 AND 51-35-01 REV 40. INSTALLED NEW WEB IAW MD-11F SRM VOL 2 51-33-01 ASDR WRLA2009107Housing · crackedDURING C-CHECK IN TPE INSPECTION FOUND CRACK IN CENTER CARGO STATION 1761 AT X=20. PDU HOUSING HAD A CRACK (REF EGAT NRC U01224). IAW AMM 20-50-02-910-801 REV 63, REMOVED AND INSTALLED PDU HOUSING AT CENTER CARGO STA 1761 X=20.SDR WRLA2009103Support Angle · crackedDURING C-CHECK IN TPE INSPECTION FOUND PRESSURE BULKHEAD SUPPORT ANGLE CRACK AT STA 1521 BETWEEN X=15 & X=-15 (REF EGAT NRC U05078). REPLACED THE SUPPORT ANGLE ON PRESSURE BULKHEAD AT STA 1521 BETWEEN X=15 & X=-15 IAW MD-11 SRM 51-35-01 VOL 2 REV 40. CONDITISDR WRLA2009097Rib · crackedDURING C-CHK IN TPE INSPECTION FOUND RT O/B TRAILING EDGE FLAP STOP RIB CRACKED AT XW486. REPAIRED RT O/B FLAP LEADING EDGE RIB IAW EGAT EI W2009A57B-504 REV 00. CONDITION CHECK NORMAL & JOB COMPLETE.SDR WRLA2009096Rib · crackedDURING C-CHK IN TPE INSPECTION, FOUND LEFT O/B TRAILING EDGE FLAP STOP RIB CRACKED AT XW486. REPAIRED LT O/B FLAP LEADING EDGE RIB IAW EGAT EI W2009A57B-503 REV 00. CONDITION CHECK NORMAL & JOB COMPLETE.SDR 2009FA0000298Fitting · corrodedFOUND CORROSION ON 4 EA HOLES AND LUG FACES OF RT FRAME FITTING. REMOVED CORROSION AND INSTALLED REPAIR BUSHINGS IAW ARP-TPR-09-0014-04B. (K)SDR 2009FA0000297Fitting · corrodedFOUND CORROSION ON 4 EA HOLES AND LUG FACES OF LT FRAME FITTING. REMOVED CORROSION AND INSTALLED REPAIR BUSHING IAW APR-TPR-09-0014-04B. (K)SDR WRLA2009094Panel · damagedDURING C2-CHK IN TPE INSPECTION FOUND NR 2 ENG PYLON UPPER PANEL 457BR AND 457FR RIVET HOLES DAMAGED 20EA. REPAIRED NR 2 ENG PYLON UPPER IAW EGAT EI W2009A54B-498 REV 00. CONDITION CHECK NORMAL & JOB COMPLETE.SDR WRLA2009104Support Bracket · crackedDURING C-CHECK IN TPE INSPECTION FOUND LEFT WING O/B TRAILING EDGE FLAP I/B FAIRING STRUCTURE HAS TWO BRACKETS CRACKED AT STA YW490.55 (REF EGAT NRC U05071). REPLACED THE TWO BRACKETS ON LEFT WING O/B TRAILING EDGE FLAP I/B FAIRING STRUCTURE IAW MD-11F SRM VOSDR WRLA2009093Vane · debondedDURING C2-CHK IN TPE INSPECTION FOUND THE RT I/B FLAP VANE DISBONDED 13X20 INCHES AT STA XW188. PER AMM 27-50-22-000-801 REV 63 REMOVED RIGHT I/B FLAP VANE. PER ATTACHED SHEET 078656 TO REPAIR DISBONDED AREA. PER AMM 27-50-22-830-80V REV 63 ADJUSTMENT OF ISDR WRLA2009112Strap · crackedDURING C-CHK IN TPE INSPECTION FOUND THE UPPER RIB STRAP IN THE RIGHT WING FIXED L/E CAVITY, XOS789, HAD CRACK (REF EGAT NRC U05034). REMOVED THE DAMAGED STRAP AT RIGHT WING FIXED L/E CAVITY, XOS789, IAW MD-11F SRM VOL 2 51-51-35-01 REV 40. INSTALLED NEW STRSDR WRLA2009111Strap · crackedDURING C-CHK IN TPE INSPECTION FOUND THE UPPER RIB STRAP IN THE RIGHT WING FIXED L/E CAVITY, XOS667, HAD CRACK (REF EGAT NRC U05033). REMOVED THE DAMAGED STRAP AT RIGHT WING FIXED L/E CAVITY, XOS667, IAW MD-11F SRM VOL 2 51-51-35-01 REV 40. FABRICATED THE PASDR WRLA2009106Angle · crackedDURING C-CHECK IN TPE INSPECTION FOUND A CRACK IN THE ANGLE OF RIGHT O/B TRAILING EDGE FLAP I/B FAIRING HINGE STRUCTURE AT STA XW486.483 (REF EGAT NRC U05029). REPAIRED THE ANGLE OF RIGHT O/B TRAILING EDGE FLAP I/B HINGE FAIRING STRUCTURE IAW MD-11F SRM 57-0SDR WRLA2009105Angle · crackedDURING C-CHECK IN TPE INSPECTION FOUND A CRACK IN THE ANGLE OF RIGHT O/B TRAILING EDGE FLAP I/B FAIRING STRUCTURE AT STA XW486.483 (REF EGAT NRC U05030). REPAIRED THE ANGLE OF RIGHT O/B TRAILING EDGE FLAP I/B FAIRING STRUCTURE IAW MD-11F SRM 57-00-01 VOL 1 FISDR WRLA2009114Structure · crackedDURING C-CHK IN TPE INSPECTION FOUND CRACK ON LEFT WING T/E BEAL SEAL LAND Y=1474 & Z=100 (REF NRC U05016). REPLACED LEFT WING T/E BEAL SEAL LAND AT Y=1474 & Z=100 PER MD-11F SRM 51-33-01 VOL 2 REV 40. CONDITION CHECK NORMAL & JOB COMPLETE.SDR WRLA2009092Floor Support · corrodedDURING C3 CHECK IN TPE INSPECTION FOUND: CORROSION ON THE PANEL SUPPORT OF CABIN FLOOR AT STA Y=860 & X=61 (REF EGAT N/R U05037). REMOVED THE DAMAGED PANEL SUPPORTS PER MD-11 SRM 51-35-01 VOL 2 REV 40. FABRICATE NEW SUPPORT IAW EGAT EI W2009P53B-374 REV 0SDR WRLA2009091Floor Support · corrodedDURING C3 CHECK IN TPE INSPECTION FOUND: CORROSION ON THE PANEL SUPPORT OF CABIN FLOOR AT STA Y=775 & X=85 (REF EGAT N/R U05038). REMOVED THE DAMAGED PANEL SUPPORTS PER MD-11 SRM 51-35-01 VOL 2 REV 40. REPLACE NEW SUPPORT PER MD-11 SRM 51-35-01 VOL 2 REV 4SDR WRLA2009089Web · crackedDURING C3 CHECK IN TPE INSPECTION FOUND: CRACK ON NR 1 ENG PYLON INTERNAL WEB CRACK AT STA 300 (REF GET N/R U05024). REPAIRED THIS CRACKED AREA PER MD-11 SRM 57-00-01 VOL 1 FIG 10 REV 40 AND JOB CARD ATTACH SHEET 079586. JOB COMPLETED AND CONDITION CHECK NOSDR WRLA2009090Doubler · crackedDURING C3 CHECK IN TPE INSPECTION FOUND: CRACK ON THE DB DOUBLER FASTENER AREA OF THE LEFT WING OUTBOARD FIXED CAVITY AT STA XOS627 (REF EGAT N/R U05035). REPAIR THIS CRACKED AREA B PER MD-11 SRM 57-00-01 VOL 1 FIG 10 REV 40. PERFORM ET INSPECTION FOR CUTOUSDR WRLA2009088Angle · crackedDURING C3 CHECK IN TPE INSPECTION FOUND: CRACK ON NR 3 ENG PYLON INTERNAL ANGLE AT STA 180 (REF GET N/R U05032). REPLACED THE INTERNAL ANGLE PER MD-11 SRM 51-35-01 VOL 2 REV 40. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR WRLA2009087Stiffener · crackedDURING C3 CHECK IN TPE INSPECTION FOUND: CRACK ON ZEE STIFFENERS OF LT WING FIXED L/E UPPER PNL 516ET (REF EGAT N/R U05031). REMOVED THE DAMAGED STIFFENERS (ARB2440-503/503) 2EA PER MD-11 SRM 51-35-01 VOL 2 REV 40. STOP DRILLED WITH 0.25 INCH DIA HOLE AT ENSDR WRLA2009086Stiffener · crackedDURING C3 CHECK IN TPE INSPECTION FOUND: CRACK ON ZEE STIFFENERS OF RT WING FIXED L/E UPPER PNL 616ET (REF EGAT N/R U05027). REMOVED THE DAMAGED STIFFENERS (ARB2440-504/506) 2EA PER MD-11 SRM 51-35-01 VOL 2 REV 40. STOP DRILLED WITH 0.25 INCH DIA HOLE AT ENSDR WRLA2009085Rib · crackedDURING C3 CHECK IN TPE INSPECTION FOUND: CRACK ON RIGHT WING FIXED L/E CAVITY XOS1025 - LOWER RIB CRACKED FROM FASTENERS AREA (REF EGAT N/R U50534). REPAIR THIS CRACKED RIB PER MD-11 SRM 57-00-01 VOL 1 FIG 10 REV 40. JOB COMPLETED AND CONDITION CHECK NORMALSDR WRLA2009084Seat Track · corrodedDURING C3 CHECK IN TPE INSPECTION FOUND SEAT TRACK CORROSION AT STA 859. REPAIRED THIS CORRODED SEAT TRACK IAW SRM 53-70-00 VOL 1 FIG 1 REV 40, JOB COMPLETED AND CONDITION CHECK NORMAL.SDR WRLA2009083Door · crackedDURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON FLIPPER DOOR FWD EDGE OF RT MLG GR - ABOUT .5 INCH (REF EGAT N/R U05029). REMOVED THIS CRACKED FLIPPER DOOR PER AMM 32-14-08-000-801, REPAIRED THE FLIPPER DOOR IAW SRM VOL 1 52-10-00 FIG 18 REV 40, REINSTALLEDSDR WRLA2009082Door · crackedDURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON FLIPPER DOOR FWD UPPER EDGE OF LT MLG GR - ABOUT .5 INCH (REF EGAT N/R U05028). REMOVED THIS CRACKED FLIPPER DOOR PER AMM 32-14-08-000-801, REPAIRED THE FLIPPER DOOR IAW SRM VOL 1 52-10-00 FIG 18 REV 40, RE-INSDR WRLA2009081Step · crackedDURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON STEP PANEL OF AVIONICS COMPARTMENT LADDER AT STA 348 (REF EGAT N/R U05026). REMOVED AND FABRICATED NEW PANEL IAW EGAT EI W2009P57B-351 REV 00, INSTALLED PANEL IAW SRM 51-35-01 VOL 2 REV 40, AND JOB COMPLETE & CSDR WRLA2009080Support Bracket · deformedDURING C3 CHECK IN TPE INSPECTION FOUND DEFORM ON THE GND JACKS SUPPORT BRACKET INSIDE OF RT WING FUELING STATION (REF EGAT N/R U05025). REMOVED BRACKET IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED SUPPORT BRACKET IAW EGAT EI W2009P57B-350 REV 00, INSTALLED THISDR WRLA2009079Support Bracket · crackedDURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON LWR PANEL SUPPORT BRACKET OF RIGHT WING T/E AT STA XOSP465.027 (REF EGAT N/R U05023). REMOVED SUPPORT BRACKET IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED SUPPORT BRACKET IAW EGAT EI W2009P57B-350 REV 00, INSTALLESDR WRLA2009078Doubler · crackedDURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON DOUBLER OF RIGHT WING FIXED L/E CAVITY UPPER RIB AT STA XOS789 (REF EGAT N/R U05018). REMOVED THIS CRACKED CHORD DOUBLER IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED DOUBLER IAW EGAT EI W2009P57B-358 REV 00, INSTSDR WRLA2009077Doubler · crackedDURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON DOUBLER OF RIGHT WING FIXED L/E CAVITY UPPER RIB AT STA XOS667. REMOVED THIS CRACKED CHORD DOUBLER IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED DOUBLER IAW EGAT EI W2009P57B-358 REV 00, INSTALLED THIS DOUBLER IAW SDR WRLA2009076Doubler · crackedDURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON DOUBLER OF LT WING FIXED L/E CAVITY UPPER RIB AT STA XOS667. REMOVED THIS CRACKED CHORD DOUBLER IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED DOUBLER IAW EGAT EI W2009P57B-355 REV 00, INSTALLED THIS DOUBLER IAW SRMSDR WRLA2009075Doubler · crackedDURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON DOUBLER OF LT WING FIXED L/E CAVITY UPPER RIB AT STA XOS789. REMOVED THIS CRACKED CHORD DOUBLER IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED DOUBLER IAW EGAT EI W2009P57B-357 REV 00, INSTALLED THIS DOUBLER IAW SRMSDR WRLA2009074Step · crackedDURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON RT STEP SUPPORT OF CAC COMPARTMENT. REMOVED SUPPORT BRACKET IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED SUPPORT BRACKET IAW EGAT EI W2009P57B-339 REV 00, INSTALLED THIS SUPPORT BRACKET IAW SRM 51-35-01 VOL 2 REV SDR WRLA2009073Rib · crackedDURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON LWR CHORD OF LT WING FIXED L/E NOSE CAVITY NEARBY FASTENER AT STA XOS546. REMOVED THIS CRACKED CHORD DOUBLER IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED DOUBLER IAW EGAT EI W2009P57B-338 REV 00, INSTALLED THIS DOSDR WRLA2009072Fitting · crackedDURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON 1EA RT CLIP OD CAC COMPARTMENT. REMOVE THIS DAMAGED CLIP PER SRM 51-33-01 VOL 2 REV 40, FABRICATE THIS CLIP PER EGAT EI W2009P53B-354 REV 00, INSTALLED THIS CLIP PER SRM 51-33-01 VOL 2 REV 40, AND JOB COMPLETED
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