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 IPXA2020011751004Handle · inoperativeINSPECTION TYPE:N/AATB - LEFT MAIN GEAR PRI/SEC GEAR IND. RED WGEAR HANDLE UFOUND THE LEFT DOWN LOCK LINK REQUIRED LUBRCIATION. ACCOMPLISHED PER AMM 12-21-00 CYCLED GEAR SEVERAL TIMES. NORMAL RETRACTION REF AMM 32-00-00-501SDR IPXA2020021252065Floorbeam · corrodedINSPECTION TYPE:2CAFT CARGO FLOOR BEAM SUPPORT ANGLE IS CORRODED BETWEEN STA. X= -7 TO -9.5 AT Y= 1841.REPAIRED CORRODED AFT CARGO FLOOR BEAM SUPPORT ANGLE BETWEEN STA. X= -7 TO -9.5 AT Y= 1841 IAW VT-SAA EA 011-5316-01-A8007 REV. I/R AND UPS EO MD11-5310-754SDR FDEA2020011650136Longeron · crackedNOSE LANDING GEAR Ï¿½ WHILE CARRING OUT RIGHT HAND TRUNNION FITTING REPAIR FOUND LONGERON 49 RIGHT HAND CRACK AT STATION Y=595. NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING AREA CRACK LONGERON 49 RIGHT HAND STATION Y=595. REMOVED AND REPLACED AS PER MD-11SDR FDEA2020011650135Longeron · crackedNOSE LANDING GEAR Ï¿½ WHILE CARRING OUT LEFT HAND TRUNNION FITTING REPAIR FOUND LONGERON 49 LEFT HAND CRACK AT STATION Y=595. NOSE LANDING GEAR LEFT HAND TRUNNION FITTING AREA CRACK LONGERON 49 LEFT HAND STATION Y=595 REMOVED AND REPLACED AS PER MD-11 SRM SDR IPXA2020020351743Door Frame · crackedINSPECTION TYPE:2CL-3 DOOR JAMB LOWER AFT WEB IS CRACKED AGT STA. 1313 & Z=-15.REPAIRED CRACKED L-3 DOOR JAMB LOWER AFT WEB AT STA. 1313 & Z=-15 IAW SRM 53-40-15 REPAIR 3 FIG. 201. (MAJOR)SDR IPXA2020013151605Cargo Track · corrodedINSPECTION TYPE:2CAFT CARGO SEAT TRACK IS CORRODED AT STA. 1931 AND X=20.REPAIRED CORRODED SEAT TRACK BETWEEN STA. 1911.5 TO 1967 IAW SRM 53-00-52 REPAIR 1 FIG. 201. (MAJOR)SDR IPXA2020013105591Tee Fitting · crackedINSPECTION TYPE:2CMAIN CABIN LONGERON 15 R/H T ANGLE IS CRACKED AT STA. 1341.REMOVED, FABRICATED AND REPLACED T ANGLE IAW DWG. AEA7568 AND SRM 51-31-01. (MINOR)SDR IPXA2020013105590Tee Fitting · crackedINSPECTION TYPE:2CMAIN CABIN LONGERON 15 R/H T ANGLE IS CRACKED AT STA. 1219.REMOVED, FABRICATED AND REPLACED T ANGLE IAW DWG. AEA7568 AND SRM 51-31-01. (MINOR)SDR IPXA2020013105589Tee Fitting · crackedINSPECTION TYPE:2CMAIN CABIN LONGERON 15 L/H T ANGLE IS CRACKED AT STA. 1341.REMOVED, FABRICATED AND REPLACED T ANGLE AT STA. 1341 IAW DWG. AEA7568 AND SRM 51-3101. (MINOR)SDR IPXA2020013105588Longeron · crackedINSPECTION TYPE:2CMAIN CABIN LONGERON 15 L/H T ANGLE IS CRACKED ATS TA. 1219.REMOVED, FABRICATED AND FREPLACED T ANGLE IAW DWG. AEA7588 AND SRM 51-31-01. (MINOIR)SDR FDEA2020011640127Angle · corrodedMAIN CARGO DECK, STA1341 RBL104 CORROSION ON ANGLE AT BASE OF OVERWING FUEL TANK, 2020-01-14] AREA REPAIRED PER EA 1-5710-T0351898.SDR IPXA2020021435285Hinge Bracket · crackedINSPECTION TYPE:2CL/H O/B FLAP I/B HINGE ASSY. HAS A CRACKED BRACKET.REMOVED AND REPLACED BRACKET IAW SRM 51-31-01. (MINOR)SDR IPXA2020021091961Cam · gougedINSPECTION TYPE:2CELEVATOR LOAD FEEL ASSEMBLY CAM HAS GOUGE DAMAGE.REPAIRED DAMAGED ELEVATOR LOAD FEEL ASSEMBLY CAM IAW VT-SAA EA 011-2730-01-A8010 REV. I/R AND UPS EO MD11-2730-75438-A. (MINOR)SDR IPXA2020020751898Doubler · wornINSPECTION TYPE:2CTAIL CONE L/H INTERNAL PRODUCTION DOUBLER HAS WEAR AT STA. 2165, X=36 AND Z=35-60.REPAIRED DAMAGED TAIL CONE INTERNAL PRODUCTION DOUBLER IAW UPS EO MD11-5350-66790-A. (MINOR)SDR IPXA2020020751895Doubler · wornINSPECTION TYPE:2CTAIL CONE R/H INTERNAL PRODUCTION DOUBLER HAS WEAR AT STA. 2165, X=-36.5 AND Z=35-60.REPAIRED DAMAGED TAIL CONE INTERNAL PRODUCTION DOUBLER IAW UPS EO MD11-5353-66790-A. (MINOR)SDR IPXA2020020351741Spar Cap · corrodedINSPECTION TYPE:2CL/H WING REAR SPAR UPPER CAP IS CORRODED BETWEEN STA. XORS.=784.5 TO 826.5.REPAIRED CORRODED L/H WING REAR SPAR UPPER CAP BETWEEN STA. XORS.=784.5 TO 826.5 IAW VT-SAA EA 011-5710-01-A8006 REV. I/R AND UPS EO MD11-5710-75380-A. (MINOR)SDR IPXA2020020351740Spar Cap · corrodedINSPECTION TYPE:2CL/H WING REAR SPAR UPPER CAP IS CORRODED BETWEEB STA. XORS.=784.5 TO 826.5 AND SKIN BETWEEN XORS.=762.5 TO 779.5.REPAIRED CORRODED AREAS OF SKIN AND CAP AT NOTED LOCATIONS IAW VT-SAA EA 011-5710-01-A8006 REV. I/R AND UPS EO MD11-5710-75380-A.SDR IPXA2020013151604Longeron · crackedINSPECTION TYPE:2CMAIN CABIN LONGERON 15 L/H IS CRACKED AT STA. 1341.REMOVED, FABRICATED AND REPLACED T ANGLE IAW DWG. AEA7568-21 AND SRM 51-35-01. (MINOR)SDR IPXA2020013151620Tee Fitting · crackedINSPECTION TYPE:3CMAIN CARGO LONGERON 15R TEE ANGLE IS CRACKED AT STA 1341.REMOVED AND REPLACED CRACKED MAIN CARGO LONGERON 15R TEE ANGLE AT STA 1341 IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR)SDR IPXA2020011550944Battery Pack · dischargedDURING AN EMERGENCY LIGHT TEST, LEVEL 1 EMERGENCY BATTERY 1 LEVEL LOW ILLUMINATED. R & R EMERGENCY LIGHT BATTERY IAW AMM 33-51-01-401. OK FOR SERVICE.SDR IPXA2020020755855Spar Cap · corrodedINSPECTION TYPE:2CR/H WING REAR SPAR UPPER CAP HAS CORROSION BETWEEN STA. XORS. =718-783.REPAIRED CORRODED R/H WING REAR SPAR UPPER CAP BETWEEN STA. XORS. =718-783 IAW VT-SAA EA 011-5710-01-A8008 REV. I/R AND UPS EO MD11-5750-75362-A. (MINOR)SDR IPXA2020012951538Doubler · crackedINSPECTION TYPE:2CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS.=728.66 TO 734.75.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS.=728.66 TO 734.75 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)SDR IPXA2020012451334Doubler · crackedINSPECTION TYPE:2CR/H WING FIXED L/E BEADED DOBLER IS CRACKED BETWEEN STA. XOS=703.54-708.96.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS= 703.54 TO 708.96 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)SDR IPXA2020011540910Solenoid · inoperativeON ARRIVAL, THE L1 DOOR WOULD NOT OPERATE. R & R THE DOOR SOLENOID. OPS CHECKED GOOD IAW AMM 52-11-02, AND WDM 52-11-01.SDR FDEA2020011320119Skin · corrodedREFER TO WRI #53108830 W/O #00076033 TO COMPLY WITH EA # T 1-5310-T0349168 A P2 TITLE : FUSELAGE Ï¿½ MAINFRAME Ï¿½ SKIN CORROSION ADJACENT THE VHF ANTENNA STATION 1721 Ï¿½ 1741 LONGERON 50L Ï¿½ 50R, BLENDOUT REPAIR FUSELAGE - STATION 1721 - 1741 LONGERON 5SDR FDEA2020011320118Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR EVALUATED AND FOUNDSDR FDEA2020011320117Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (HOLE # 3) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRICASDR IPXA2020012951523Trunnion · crackedINSPECTION TYPE:2CNOSE GEAR L/H TRUNNION FITTING IS CRACKED AT STA. 582.5, Z=-114 & X=24.0.REPAIRED CRACKED NOSE GEAR L/H TRUNNION FITTING AT STA. 582.5, Z=-114 & X=24.0 IAW SRM 53-140-14 REPAIR 2 FIG.202. (MAJOR)SDR FDEA202001100103Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57SDR FDEA202001100102Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52- 03. SDR FDEA202001100101Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT HOLE BORE (HOLE A AND B) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52- 03. SDR FDEA202001100100Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03. OVSDR FDEA2020020650266Fairing · delaminatedRH WING TRAILING EDGE OUTBD ISLAND P/N ARC7203-13 DELAMINATED REPAIRED IAW SRM 57-50-80-2R PAR 2 (2) WET LAY UP.SDR FDEA202001100099Hinge Fitting · corrodedLEFT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04. OVERSIZED SDR FDEA202001100098Hinge Fitting · corrodedLEFT WING - FLAP SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04. OVERSIZSDR FDEA202001100097Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSIZED BUSHING FSDR IPXA2020013105574Attach Fitting · gougedINSPECTION TYPE:3CLT WING I/B AILERON ATTACH LUGS FOR ACTUATOR ARE GOUGED.REPAIRED GOUGED LT WING I/B AILERON ATTACH LUGS FOR ACTUATOR IAW VT-SAA EA 011-2710-01-7997 IR AND UPS EO MD11-5750-75251-A. (MINOR)SDR IPXA2020013195544Doubler · crackedINSPECTION TYPE:2CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS.= 494.0 TO 500.0.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS.= 494.0 TO 500.0 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)SDR IPXA2020013195543Doubler · crackedINSPECTION TYPE:2CL/H WING FIXED L/E BEADED DOUBLER IS CRACLED BETWEEN STA. XOS.=692-703.2.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS.= 692 TO 703.2 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOTR)SDR IPXA2020013105585Doubler · crackedINSPECTION TYPE:2CL/H WING FIED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS.= 610.8 TO 621.6.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS.= 610.8 TO 621.6 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)SDR FDEA202001100105Beam · crackedCABIN - R3 DOOR UPPER #1 STOP BEAM FOUND CRACKED . CABIN - R3 DOOR , CRACKED UPPER #1 STOP BEAM REMOVED AND REPLACED AS PER SRM 51- 31-01-0G . REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 .SDR FDEA202001100104Beam · crackedCABIN - L3 DOOR LOWER #7 STOP BEAM CRACKED . CABIN - L3 DOOR , CRACKED LOWER #7 STOP BEAM REMOVED AND REPLACED AS PER SRM 51- 31-01-0G . REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 .SDR IPXA2020012975467Doubler · crackedINSPECTION TYPE:2CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS=728.6 TO 734.7.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS=728.6 TO 734.7 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)SDR IPXA2020012975465Doubler · crackedINSPECTION TYPE:2CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS=661.7 TO 667.6.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS= 661.7 TO 667.6 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)SDR IPXA2020012951521Doubler · crackedINSPECTION TYPE:2CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS.= 633 TO 636.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS.= 633 TO 636 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)SDR IPXA2020012745336Doubler · crackedINSPECTION TYPE:2CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS= 692.0 TO 698.1.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA, XOS= 692.0 TO 698.1 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)SDR IPXA2020012451335Doubler · crackedINSPECTION TYPE:2CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS= 759.1 TO 768.2.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS= 759.1 TO 768.2 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)SDR FDEA202001100090Skin · damagedRIGHT HAND WING DROOPLED LEADING EDGE OUTBOARD SKIN EXISTING REPAIR DOUBLER FOUND WITH DAMAGED AT STATION XDLE 329.775 DAMAGED EXISTING REPAIR DOUBLER AT RIGHT HAND WING DROOPED LEADING EDGE OUTBOARD SKIN AT STATION XDLE 329.775 REMOVED AS PER SRM 51-33-01SDR FDEA202001100106Seat Track · damagedCABIN - SEAT TRACK AT STATION 1291 X = - 47.5 FOUND DAMAGE . CABIN - AT SEAT TRACK STATION 1291 X = - 47.5 DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIOSDR FDEA202001100091Doubler · crackedDURING NDT FPI AND HFEC SURFACE INSPECTION AFTER THE INITIAL BLENDOUT ON THE RIGHT HAND WING UPPER WING SURFACE MAIN LANDING GEAR SUPPORT DOUBLER AT YW 467 , FOUND 1.5 INCH CRACK. RIGHT HAND WING UPPER WING SURFACE MAIN LANDING GEAR SUPPORT CRACKED DOUBLER
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