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 FDEA202104100871Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD FORWARD MOUNT LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD FORWARD FORWARD MOUNT LUG HOLE BORE (#6 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PSDR FDEA202104100870Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- SDR FDEA202104100869Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-SDR FDEA202104100868Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT OUTBOARD HOLE BORE (#2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-SDR FDEA202104100867Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT INBOARD HOLE BORE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE UPPER MOUNT INBOARD HOLE BORE (#2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-SDR FDEA202104100866Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRISDR IPXA2021041268116Battery Pack · inoperativeINSPECTION TYPE:NAEMER LIGHT INOP.R&R EMER LIGHT BATTERY PACK PER MD11 AMM 33-51-01-401, SYSTEM CHECKS OKAY. IPC 33-51-01-05-015.SDR FDEA202104090857Skin · dentedFUSELAGE SKIN DENT / SCRATCH FOUND AT STATION 1833 LONGERON 35 RIGHT - LONGERON 36 RIGHT DUE TO LOADER CONTACT . FUSELAGE SKIN DENT AND SCRATCH AT STATION 1833 , LONGERON - 35 RIGHT - LONGERON - 36 RIGHT CARRIED OUT REPAIR AS PER SRM 53-00-01-2R FIGURE 2SDR FDEA202104090862Wire Harness · failedPDIS 584 26-10 1474 09APR21 MEM OPEN U LOGPAGES:385225 DURING CLIMBOUT FROM PANC 12 MINUTES INTO FLIGHT RECEIVED LEVEL 3 AUDIBLE ENGINE 3 FIRE WARNING. THREE WARNINGS TWO CONSECUTIVE TIMES. NO VISUAL INDICATIONS. ALL ENGINE 3 INDICATIONS NORMSDR IPXA2021051369343Intercostal · crackedINSPECTION TYPE:3CRT MLG W/W INTERCOSTAL BELOW AFT UPPER BRAKE ACCUMULATOR IS CRACKED.REPAIRED CRACKED RT MLG W/W INTERCOSTAL BELOW AFT UPPER BRAKE ACCUMULATOR IAW SRM 53-40-12, REPAIR 3, FIGURE 201. (MINOR)SDR IPXA2021051169290Intercostal · crackedINSPECTION TYPE:3CLT MLG W/W KEEL BEAM INTERCOSTAL BELOW UPPER FWD BRAKE ACCUMULATOR IS CRACKED.REPAIRED CRACKED LT MLG W/W KEEL BEAM INTERCOSTAL BELOW UPPER FWD BRAKE ACCUMULATOR IAW SRM 53-40-12, REPAIR 3, FIGURE 201. (MINOR)SDR IPXA2021051069148Intercostal · crackedINSPECTION TYPE:3CLT MLG W/W KEEL BEAM INTERCOSTAL ABOVE FLAP FOLLOW-UP MECHANISM IS CRACKED.REMOVED AND REPLACED CRACKED LT MLG W/W INTERCOSTAL ABOVE FLAP FOLLOW-UP MECHANISM IAW SRM 51-33-01 & 51-35-01. (MINOR)SDR IPXA2021043068812Stiffener · crackedINSPECTION TYPE:3CR/H MLG W/W O/B WALL 4TH VERTICAL STIFFNER FROM DOOR OPENING IS CRACKEDREMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. ANB7203 AND SRM 51-31-01. (MINOR)SDR FDEA202104080848Seat Track · corrodedCABIN - RIGHT STATION 5-10, X = -27.5 SEAT TRACK FOUND CORROSION. CABIN RIGHT STATION 5-10 X = -27.5 SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEATSDR FDEA202104080847Seat Track · corrodedCABIN - LEFT STATION 1541 X = 27.5 SEAT TRACK FOUND CORROSION. CABIN - LEFT STATION 1541 X =27.5 SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101. ALLOWABLE DAMAGE 1. CORRODED SEAT SEAT TRACK REPAIRED BY SECTIONAL SDR FDEA202104080844Seat Track · corrodedCABIN - RIGHT STATION 5-93 X = -8.5 SEAT TRACK FOUND CORROSION. CABIN - RIGHT STATION 5-93 X =-8.5 SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 . ALLOWABLE DAMAGE 1. CORRODED SEAT SEAT TRACK REPAIRED BY SECTIONASDR FDEA202104080843Seat Track · corrodedCABIN - LEFT STATION 5-23 X = 8.5 SEAT TRACK FOUND CORROSION . CABIN - LEFT STATION 5-23 X =8.5 SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 . ALLOWABLE DAMAGE 1 . CORRODED SEAT SEAT TRACK REPAIRED BY SECTIONAL SESDR FDEA202104080842Seat Track · corrodedCABIN - RIGHT STATION 1521 , X = -8.5 SEAT TRACK FOUND CORROSION . CABIN RIGHT STATION 1521 . X = -8.5 SEAT TRACK CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIR BY SECTIONAL SEATSDR FDEA202104080849Fire Loop · failedON CLIMBOUT FROM MEM LEVEL 1 FIRE DET 3 FAULT FOLLOWED BY MOMENTARY LVL 3 ENGINE FIRE CYCLING IMMEDIATLY BACK TO LVL 1 FIRE DET 3 FAULT. LVL 1 FIRE DET 3 FAULT CYCLED ON & OFF FOR 10 MIN THEN EXTINGUSHED TROUBLESHOT PER MD-11 FIM 26-11-00-1-1. NO FAULTSSDR FDEA202104070837Fire Loop · shortedON TAKEOFF PASSING 3000 FT, MOMENTARY LEVEL 3 MANF 3 FAIL ALERT FOR ABOUT 3 SECONDS ALERT WENT AWAY AND #2 BLEED VALVE CLOSED. REF WDM 36-23-02 PG 1 SH 1, REMOVED MFC REF AMM 36-23-01-4. CONTINUITY CHECKED GOOD AT R5-1054A BETWEEN PINS 5C AND 6C. FROM ANSDR FDEA202104060828Doubler · crackedRIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 655 FOUND CRACK. RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT STATION XOS 655 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MSDR FDEA202104060827Fitting · crackedLOWER FORWARD CARGO COMPARTMENT BILGE STATION 6-0 LONGERON 44 LEFT SPLICE FITTING FOUND WITH CRACK.. LOWER FORWARD CARGO COMPARTMENT STATION 6-0 TO STATION 6-10 LONGERON 44 LEFT SPLICE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01-0G . FABRICATED SPLICESDR FDEA202104050820Floor Panel · delaminatedCABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL #231HF AT STATION 595 TO STATION 675 FOUND DELAMINATED. DELAMINATED FLOOR PANEL #231HF AT CABIN STATION 595 TO STATION 675 REMOVED AS PER AMM 53-21-04-4. FLOOR PANEL #231HF FABRICATED AS PER FEDEX DRAWING SRZSDR FDEA202104050819Floor Panel · delaminatedCABIN - MAIN DECK CARGO COMPARTMENT FLOOR PANEL #231LF AT STATION 675 TO STATION 735 FOUND DELAMINATED. DELAMINATED FLOOR PANEL #231LF AT CABIN STATION 675 TO STATION 735 REMOVED AS PER AMM 53-21-04-4. FLOOR PANEL #231LF FABRICATED AS PER FEDEX DRAWING SRZSDR FDEA202104050823Skin · crackedRIGHT HAND WING DROOPED LEADING EDGE UPPER SKIN TRAILING EDGE FOUND CRACK AT XDLE 319. RIGHT HAND WING DROOPED LEADING EDGE UPPER SKIN TRAILING EDGE AREA AT XDLE 319 REPAIR CARRIED OUT AS PER SRM 57-40-01-2R REPAIR 5 FIGURE 201. REPAIR CLASSIFIED AS MAJOSDR FDEA202104050822Doubler · crackedRIGHT HAND WING FIXED LEADING EDGE COMPARTMENT AT STATION XOS 545 BEADED DOUBLER FOUND CRACKS. RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT STATION XOS 545 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS SDR FDEA202104050821Doubler · crackedRIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER FOUND CRACKS AT STATION XOS 650. RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT STATION XOS 650 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS SDR FDEA202104050824Skin · crackedCRACK FOUND APPROXIMATELY 1.1 INCH IN LENGTH DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND WING FIXED LEADING EDGE CUTOUT NUMBER 5 AT XOS XOS 490 SLAT DOOR. RIGHT HAND WING FIXED LEADING EDGE CUTOUT NUMBER 5 AT XOS 490 SLAT DOOR REPAIR CASDR FDEA202104030817Frame · dentedCABIN - LEFT HAND MAINFRAME AT STATION 5-32 LONGERON 12 LEFT FRAME FOUND DENT. CABIN - AT LEFT HAND MAINFRAME STATION 5-32 LONGERON 12 LEFT , DENTED FRAME REPAIRED AS PER SRM 53-00-07-2R REPAIR 2 FIGURE 201. REPETITIVE INSPECTION REQUIRED - - INITIAL AT 14,SDR FDEA202104030816Frame · dentedCABIN - LEFT HAND MAIN FRAME AT STATION 1761 LONGERON 12 LEFT EXISTING REPAIR ANGLE ANGLE FOUND DENT. CABIN - AT LEFT HAND MAINFRAME STATION 1761 LONGERON 12 LEFT , DENTED EXISTING REPAIR ANGLE REMOVED AS PER SRM 51-31-01-0G AND REPAIRED AS PER SRM 53-00-0SDR IPXA2021040567775Sensor · failedINSPECTION TYPE:NA**ATB - SDR FILED OPEN - NO EMERG DECLARED - NO EQUIP USED.** LVL 1 ANTI -ICE SENSOR FAIL AT FL240 ON CLIMBOUT. MEL 36 10 2 1 DEFER PNEU SUPPLY 1 DMP C/W.SDR IPXA2021041268067Angle · crackedINSPECTION TYPE:C2RH O/B WING T/E REAR SPAR SUPPORT ANGLE CRACK.REMOVED,FABRICATED AND REPLACED CRACKED SUPPORT ANGLE IAW SRM 51-35-01 AND 51-31-01 (MINOR).SDR IPXA2021040367682Support Angle · crackedINSPECTION TYPE:CCTR CARGO L/H SIDE WALL AT STA. 1741 HAS A SUPPORT ANGLE CRACKEDREMOVED, FABBED, AND INSTALLED IAW SRM 51-31-01 AND DRAWING ADA0130SDR IPXA2021040367681Support Angle · crackedINSPECTION TYPE:CCTR CARGO L/H SIDE WALL ST STA. 1701 HAS A PANEL SUPPORT ANGLE CRACKEDREMOVED,FABBED,AND INSTALLED IAW SRM 51-31-01 AND DRAWING ADA0130SDR IPXA2021042168472Hinge Bracket · corrodedINSPECTION TYPE:2CR/H WING O/B FLAP I/B HINGE BRACKET LUG HOLE AT STA. XW 486.403 HAS CORROSION.REPAIRED R/H WING O/B FLAP I/B HINGE BRACKET LUG IAW VT-SAA EA 011-5700-01-A9029 REV. I/R AND UPS EO MD11-5700-80086-A. (MINOR)SDR IPXA2021041268124Skin · puncturedINSPECTION TYPE:C2RH WING O/B AILERON WEDGE HAS A HOLE AT UPPER SURFACE.REMOVED AND REPLACED RH O/B AILERON WEDGE IAW SRM 51-37-01 AND DWG #NRC6741 (MINOR).SDR IPXA2021033067562Door · inoperativeINSPECTION TYPE: NA**SDR FILED OPEN** R1 ENTRY DOOR WILL NOT OPEN. DEFERRED R1 ENTRY DOOR IAW MEL 52 10 3 1 2 1 CONTROL #M740124 PLACARD INSTALLED.SDR IPXA2021033067550Wire · sparksEMERGENCY DECLARED, O2 MASK DROPPED BUT NOT DONNED - LANDED UNEVENTFULLY - AC OOS** ON DESCENT SPARK FROM BEHIND GALLEY AREA RPRTD BY ACM SMOKE & FUMES NOTED. AFT CB'S FROM GALLEY PULLED SMOKE & FUMES SUBSIDED. GROUND SERVICE BUS C/B POPPED AFTER LANDING. MASDR IPXA2021032967416Skin · crackedINSPECTION TYPE:N/AFUSELAGE CRACKED NEAR #3 PACK DOOR AT UPPER AFT CORNERREPAIRED IAW UPS EO MD11-5330-79787-ASDR IPXA2021040967986Hinge Fitting · gougedINSPECTION TYPE:C2LH O/B ELEVATOR ACTUATOR HINGE FITTING GOUGE AT XE=211.000 AND YH=347.REPAIRED GOUGE HINGE FITTING IAW VT-SAA EA 011-5500-01-A9012 REV I/R AND UPS EO MD11-5550-79937-A (MINOR).SDR IPXA2021040867956Hinge Fitting · gougedINSPECTION TYPE:C2LH I/B ELEVATOR #2 MOUNT HINGE FITTING BOTH LUGS ARE GOUGED .REPAIRED #2 HINGE FITTING LUGS IAW VT-SAA EA 011-5520-01-A9007 REV I/R AND UPS EO MD11-5510-79928-A (MINOR).SDR FDEA202103270785Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMMSDR FDEA202103270784Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 5SDR FDEA202103270783Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG BORE HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD- MD-SDR FDEA202103270782Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR ACTUATOR LUG BORE HOLE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 SDR IPXA2021032867371Indicator · inoperativeINSPECTION TYPE:N/AL1 DOOR SLIDE REMOTE PRESSURE IND INOP.R & R L1 DOOR REMOTE PRESSURE INDICATOR PER AMM 25-61-04 . OPS CHECKS GOOD .SDR IPXA2021042168492Longeron Splice · crackedINSPECTION TYPE:2CCENTER CARGO LONGERON 29 R/H SPLICE FITTING IS CRACKED BETWEEN STA. 5-113 TO 1541.REMOVED, FABRICATED AND REPLACED SPLICE FITTING IAW DWG. A5A7112 AND SRM 51-33-01. (MINOR)SDR IPXA2021041468221Support Angle · crackedINSPECTION TYPE:C2CENTER CARGO COMPARTMENT LH SIDEWALL SUPPORT ANGLE IS CRACK AT STA.1681.REMOVED,FABRICATED AND REPLACED CRACKED SUPPORT ANGLE IAW VT-SAA EA 011-5350-01-A9011 REV I/R AND UPS EO MD11-5350-79950-A (MINOR).SDR IPXA2021041268070Stiffener · crackedINSPECTION TYPE:2CAFT CARGO COMP. VERTICAL STIFFNER IS CRACKED AT STA. 1841 AND LONG. 48 L/H.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRM 51-33-01. (MINOR)SDR IPXA2021041268069Stiffener · crackedINSPECTION TYPE:2CAFT CARGO COMP. VERT. STIFFNER IS CRACKED AT STA. 1841 AND LONG. 49 R/H.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. ADA7170 AND SRM 51-33-01. (MINOR)
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