Boeing MD-11F
Service difficulty reports · 31,317
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 = 'MD11F' 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 = 'MD11F' 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 IPXA2020051855416Doubler · crackedINSPECTION TYPE:2CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 551.5 555.5.REPAIRED CFRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 555.1 TO 555.5 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)SDR IPXA2020051855415Doubler · crackedINSPECTION TYPE:2CL/H WING FIXED L/E BEADED DOBLER IS CRACKED BETWEEN STA. XOS. 789.6 TO 795.7.REPAIRED CRACKED L/G WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 789.6 TO 795.7 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)SDR IPXA2020051155173Angle · crackedINSPECTION TYPE:3CL/H UPPER WING TO BODY FAIRING ATTACH FRAME HAS BOTTOM L-ANGLE CRACKED AT STA 1401.REMOVED FABRICATED AND INSTALLED L-ANGLE AT L/H WING TO BODY FRAME AT STA 1401 IAW SRM 51-35-01 AND SRM 51-33-01. (MINOR)SDR IPXA2020062256768Bulkhead · damagedINSPECTION TYPE:3C NR 1 PYLON INTERNAL BULKHEAD INSIDE ACCESS PANELS 438CR/DR HAS ELONGATED HOLE. REPAIRED ELONGATED HOLE ON NR 1 PYLON BULKHEAD WEB AT YWN 315.500 INSIDE ACCESS PANEL 438CR/DR IAW EA 011-5410-01-A8220 AND EO MD11-5410-76813-A. (MAJOR)SDR IPXA2020061056338Beltframe · dentedINSPECTION TYPE:3C MAIN CABIN BELT FRAME DENTED AT STA 715 LONGERON 13R. CUTOUT DAMAGE AND ACCOMPLISHED PERMANENT REPAIR ON BELT FRAME IN MAIN CABIN AT STA 715 LONGERON 13R IAW EA 011-5310-01-A8168 REV I/R AND EO MD11-5310-76728-A. (MAJOR)SDR IPXA2020060856248Beltframe · dentedINSPECTION TYPE:3C MAIN CABIN BELT FRAME DENTED AT STA 695 LONGERON 12R. CUT OUT DAMAGE AND ACCOMPLISHED PERMANENT REPAIR OF MAIN CABIN BELT FRAME AT STA 695 LONGERON 12R IAW EA 011-5310-01-A8171 REV I/R AND EO MD11-5310-76700-A. (MAJOR)SDR IPXA2020060856217Door Frame · crackedINSPECTION TYPE:3C MAIN CABIN L3 DOOR LWR FWD DOOR JAMB WEB CRACKED BETWEEN STA 1256.75 AND 1250.75 BETWEEN DOOR STOP 7 AND Z-19. CUTOUT DAMAGE, FABRICATED REPAIR DOUBLER AND ACCOMPLISHED PERMANENT REPAIR AT MAIN CABIN L3 DOOR JAMB BETWEEN STA 1256.75 AND 1250SDR IPXA2020052645695Shear Tie · crackedINSPECTION TYPE:3CCENTER WING TANK RH ACCESS ENTRANCE STRUTURE UPPER LH SHEAR TIE CRACKED.REMOVED, FABRICATED CRACKED SHEAR TIE AND INSTALLED IN CENTER WING TANK RH ACCESS ENTRANCE IAW DRAWING APB7351-2 AND MD-11 SRM 51-30-01. (MINOR)SDR IPXA2020051155170Tee Fitting · crackedINSPECTION TYPE:3CR3 DOOR AFT DOOR JAMB AT STA 1341 LONGERON 15R T-FITTING IS CRACKED,REMOVED, FABRICATED AND INSTALLED R3 DOOR AFT DOOR JAMB T-FITTING AT STA 1341 LONGERON 15R IAW DRAWING AEA7568. (MINOR)SDR IPXA2020051155169Tee Fitting · crackedINSPECTION TYPE:3CMAIN CABIN T-FITTING CRACKED AT AFT END AT STA 1341 LONGERON 15L AFT OF L3 DOOR.REMOVED, FABRICATED AND INSTALLED MAIN CABIN T-FITTING AT STA 1341 LONGERON 15L IAW DRAWING AEA7568. (MINOR)SDR IPXA2020052055483Frame · wornINSPECTION TYPE:3CTAILCONE FRAME AT LH MIDDLE GUIDE PIN WORN THRU.REPAIRED LH TAILCONE FRAME IAW SRM 53-80-07 REPAIR 1 FIG 201. (MINOR)SDR IPXA2020052055479Frame · crackedINSPECTION TYPE:3CTAILCONE RH FRAME CRACKED AT MIDDLE GUIDE PIN.REPAIRED RH TAILCONE FRAME IAW SRM 53-80-01 REPAIR 1 FIG 201. (MINOR).SDR IPXA2020051555336Frame · wornINSPECTION TYPE:C3TAILCONE FRAME AT LH UPPER GUIDE PIN WORN THRU.REPAIRED LH TAILCONE FRAME IAW SRM 53-80-07 REPAIR 1 FIG 201. (MINOR)SDR IPXA2020051555335Frame · wornINSPECTION TYPE:3CTAIL CONE FRAME AT RH UPPER GUIDE PIN WORN THRU.REPAIRED RH TAILCONE FRAME IAW SRM 53-80-07 REPAIR 1 FIG 201. (MINOR)SDR FDEA2020042080758Structure · wornRH WING, DROOP L/E INBD SIDE HAS DEEP WEAR MARKS INSTALLED REPAIR DOUBLER PER SRM 57-40-01 REPAIR 15SDR IPXA2020060856214Stringer · crackedINSPECTION TYPE:3C LT WING STRINGER 40 IS CRACKED BETWEEN XORS 737.6 AND XORS 772.5.CUT OUT DAMAGE. FABRICATED REPAIR PARTS AND ACCOMPLISHED PERMANENT REPAIR ON LT WING STRINGER 4O BETWEEN STA XORS 737.6 AND XORS 772.5 IAW SRM 57-00-03 REPAIR 4, FIG 201 REV 66SDR IPXA2020051855417Doubler · crackedINSPECTION TYPE:2CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 728.6 TO 740.84.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 728.6 TO 740.84. IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)SDR IPXA2020042954737Pump · crackedINSPECTION TYPE:3CRUDDER MOTOR PUMP IN TAIL COMP. IS CRACKED.REMOVED AND REPLACED RUDDER MOTOR PUMP AND LEAKED AND OP'S CHECKED GOOD IAW AMM 27-26-20-000-802. (MINOR)SDR IPXA2020060856218Skin · crackedINSPECTION TYPE:3C LT WING UPPER SURFACE T/E WEDGE SKIN IS CRACKED JUST O/B OF I/B AILERON. CUTOUT DAMAGE AREA AND ACCOMPLISHED PERMANENT REPAIR ON LT WING UPPER SURFACE T/E WEDGE SKIN JUST O/B OF I/B AILERON IAW SRM 57-50-01, REPAIR 6 FIG 202 REV-66 (MAJOR).SDR IPXA2020051855405Crossbeam · crackedINSPECTION TYPE:3CR3 DOOR PLUG UPPER AFT CROSS BEAM IS CRACKED.REPLACED R3 DOOR PLUG UPPER AFT CROSS BEAM IAW SRM 51-35-01 DRAWING ADA3462. (MINOR)SDR IPXA2020041754330Tensioner · failedFORWARD CABLE TO OPEN CREW ENTRY DOOR, LEFT SIDE IS OFF TRACK. REPLACED THE TENSIONER IAW MM 52-11-03. ADJUSTED AND TESTED IAW 52-11-02.SDR FDEA2020041760751Support Fitting · damagedFUSELAGE Ï¿½ CENTER STRUCTURE INSTALLATION Ï¿½ WHILE ACCOMPLISHING INSPECT/REPLACE HI-LOKS ON LEFT HAND INBOARD FLAP SUPPORT FITTING AT YIFH 61 FOUND THE EXISTING INSTALLED HI-LOKS EXCEEDS LIMITS AS PER WORKCARD E1-5310-7-5004 PART 5 STEP 13. COMPLIED WITHSDR FDEA2020041760750Support Fitting · damagedFUSELAGE Ï¿½ CENTER STRUCTURE INSTALLATION Ï¿½ WHILE ACCOMPLISHING INSPECT/REPLACE HI-LOKS ON RIGHT HAND INBOARD FLAP SUPPORT FITTING AT YIFH 61 FOUND THE EXISTING INSTALLED HI-LOKS EXCEEDS LIMITS AS PER WORKCARD E1-5310-7-5004 PART 6 STEP 13. COMPLIED WITSDR IPXA2020041754307Windshield · crackedINSPECTION TYPE:N/A*** ATB *** AT FL230 ANTI ICE ON WHEN DESELECTING ANTI ICE L SW L WINDSHEILD POPPED AND SHATTERED CRACKS ACROSS ENTIRE WINDSHEILD.R/R WINDOW ASSY PER MM 56-11-01 ALL OPS CHECK GOOD TORQUED TERMINAL BLOCKS PER SWPM 20-20-03. ESR: IPC 56-11-05SDR 9WGA2020041601Pump · unknownENGINE 2 (RPM LOW) AUTO SHUTDOWN NO VIB NOTED, AFTER ENG #2 SHUTDOWN IN FLIGHT NOTED ALL PUMPS OFF ON #2 TANK.SDR IPXA2020060856215Doubler · crackedINSPECTION TYPE:3C LT O/B WING L/E BEADED DOUBLER IS CRACKED JUST I/B OF NR 12 SLAT TRACK BETWEEN XOS 772 AND XOS 776. CUTOUT DAMAGE, FABRICATED PART AND ACCOMPLISHED PERMANENT REPAIR OF LT WING L/E BEADED DOUBLER O/B OF NR 12 SLAT TRACK BETWEEN XOS 772 AND XOSDR IPXA2020052645698Door · gougedINSPECTION TYPE:3CL/H A/C BAY ACCESS DOOR 113DL HAS A GOUGE ON INTERIOR AFT SIDE FLAT EDGE.ACCOMPLISHED PERMANENT REPAIR OF L/H AIRCONDITION DOOR INTERIOR AFT SIDE IAW EA 011-5200-01-A8164 AND EO MD11-5240-76587-A. {MINOR)SDR IPXA2020052635669Doubler · crackedINSPECTION TYPE:3CRT WING FIXED L/E SKIN SPLICE DOUBLER IS CRACKED AT XOS 789.REMOVED AND INSTALLED NEW SPLICE DOUBLER AT RT WING FIXED L/E SKIN AT XOS 789. IAW DRAWING ARB3954 AND MD11 SRM51-33-01. (MINOR)SDR IPXA2020052635667Skin · crackedINSPECTION TYPE:3C, LT OTBD WING L/E SKIN IS CRACKED JUST OTBD OF NR 7 SLAT TRACK.ACCOMPLISHED PERMANENT REPAIR IAW SRM 57-40-01 REPAIR 17 FIGURE 201 REV 66. (MAJOR)SDR IPXA2020052255600Doubler · crackedINSPECTION TYPE:3CRT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN XOS 661 - 667.REMOVED DAMAGE AND ACCOMPLISHED PERMANENT REPAIR ON RT WING FIXED L/E BEADED DOUBLER BETWEEN XOS 661 - 667 IAW SRM 57-40-02 REPAIR 15 FIG 205. (MAJOR)SDR IPXA2020052255599Doubler · crackedINSPECTION TYPE:3CRT WING FIXED L/E SKIN BEADED DOUBLER IS CRACKED AT XOS-499.CUTOUT DAMAGE AND ACCOMPLISHED PERMANENT REPAIR ON RH WING LE SKIN BEADED DOUBLER IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)SDR IPXA2020051855408Doubler · crackedINSPECTION TYPE:3CL/H WING L/E SPLICE DOUBLER IS CRACKED JUST O/B OF #12 SLAT TRACK.REPLACED LH WING L/E SPLICE DOUBLER IAW SRM 51-33-01 AND DRAWING ARB3954. (MINOR)SDR IPXA2020051555323Skin · crackedINSPECTION TYPE:3CR/H WING FIXED L/E LOWER SKIN IS CRACKED AT STA. XOS. 774.8529.REPAIRED CRACKED R/H WING FIXED L/E LOWER SKIN AT STA. XOS. 774.8529 IAW SRM 57-40-02 REPAIR 7 FIG. 201. (MAJOR)SDR IPXA2020051555322Doubler · crackedINSPECTION TYPE:2CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 667.67-673.76.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 667.67 TO 673.76 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)SDR IPXA2020051355219Doubler · crackedINSPECTION TYPE:3CR/H WING FIXED L/E PANEL LANDING INTERNAL DOUBLER IS CRACKED AT STA. XOS. 906.REPAIRED CRACKED R/H WING FIXED L/E PANEL LANDING INTERNAL DOUBLER AT STA. XOS.906 IAW SRM 57-40-03 REPAIR 1 FIG. 201 (MAJOR)SDR IPXA2020051355217Skin · crackedINSPECTION TYPE:3CR/H WING #1 SLAT EXTERIOR SKIN IS CRACKED BETWEEN STA. 185-191.REPAIRED CRACKED R/H WING #1 SLAT EXTERIOR SKIN BETWEEN STA. 185-191 IAW SRM 57-40-01 REPAIR 8 FIG. 201. (MAJOR)SDR IPXA2020051155159Skin · crackedINSPECTION TYPE:3CRT WING FIXED L/E PANEL LANDING CRACKED AT XOS 615.REMOVED, FABRICATED AND INSTALLED RT WING FIXED L/E LANDING / DOUBLER BETWEEN STA XOS 602 - XOS 629 IAW DWG ARB1180 AND SRM 51-31-01. { MINOR }SDR IPXA2020041765279Ground Wire · unsecureR1 DOOR WILL NOT OPEN. FOUND A LOOSE WIRE FOR S2-731. SECURED THE GROUND WIRE & PERFORMED OPERATIONAL CHECK OF THE R1 DOOR SEVERAL TIMES IAW MM 52-10-01-700-801.SDR FDEA2020041750749Computer · failedAT CRUISE FL 370 ABOUT 60 MIN INTO FLIGHT, HAD A MOMENTARY "TIRE FAIL" AND ALL TIRES WERE MISSING FROM DISPLAY, THEN THE INDICATIONS RETURNED TO NORMAL. AT FL 250 DESCENDING TO 10,000, WE GOT THE LEVEL 2 "TIRE FAIL" INDICATION WITH THE CAWS ALERT "TIRE FAILURESDR FDEA2020041740745Hinge Bracket · corrodedRIGHT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (NR4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57SDR FDEA2020041740744Hinge Bracket · corrodedRIGHT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (NR4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-4SDR FDEA2020041740743Hinge Bracket · corrodedRIGHT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (NR3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATESDR FDEA2020041740742Hinge Bracket · corrodedLEFT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (NR4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-4SDR FDEA2020041740741Hinge Bracket · corrodedLEFT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (NR4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44SDR FDEA2020041740740Hinge Bracket · corrodedLEFT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT HAND WING, WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (NR3 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-44-07. REPAIR BUSHING FABRICATED SDR IPXA2020041554256Lamp · inoperativeL1 DOOR PRESSURE WAS GOOD, BUT THE LIGHT DOES NOT ILLUMINATE. REPLACED THE LAMP, OPS CHECKED OK.SDR IPXA2020051555288Bulkhead · corrodedINSPECTION TYPE:2C#3 ENG. PYLON AFT BULKHEAD ASSY. HAS CORROSION COMMON TO THE INNER BORE LUG OF BULKHEAD P/N AUB7502-507 & AUB 7502-509.REPAIRED #3 ENG. PYLON AFT BULKHEAD ASSY. IAW VT-SAA EA 011-5410-01-A8166 REV. I/R AND UPS EO MD11-5410-76449-A. (MINOR).SDR FDEA202004130739Unknown · malfunctionedUP ELEVATOR JAMMED DURING FLARE. ABLE TO FORCE CONTROLL COLUMN AFTER LANDING. VERIFIED ELEVATOR BUS SUPPORT IN GOOD CONDITION REF AMM 27-31-01-4-0. LOAD FEEL CHECK PASSED REF AMM 22-00-03-700-801. INSPECTED ALL ACCESABLE SECTORS, PULEYS, CONT. ROD AND CABLSDR IPXA2020041554232Connector · out of positionINSPECTION TYPE:N/AUPON LANDING RIGHT WHEEL BRAKES DID NOT WORKFOUND BRAKE SYSTEM #1 INOP ON RT TRUCK. REPLACED ANTI-SKID CONTROL MAN. IAW MM-32-45-20-000-801. NO HELP. REPLACED RT GEAR SYS #1 GLAND SWIVEL UNIT IAW MM 32-44-06-401. NO HELP. FOUND CONNECTORS P1SDR FDEA202006120736Control Unit · malfunctionedGEN 3 ON MEL. AT GEAR DOWN GOT "GEN 1 OFF" A/C WENT ON EMERGENCY POWER LOST ALL ASSOCIATED SYSTEMS. GEN 1 CAME BACK ONLINE EXITING THE RUNWAY. PERFORMED T/S AND REPL EPCU IAW AMM 24-08-01-4 REF WRI: 24-00 4955.
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