Boeing MD-11F
Service difficulty reports · 31,316
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 FDEA202607210966Skin · crackedLEFT WING- LEADING EDGE SLAT TRACK NUMBER 16 LOWER CUTOUT FOUND CRACK ABOUT 0.75 INCH. LEFT HAND WING LEADING EDGE SLAT TRACK NUMBER 16 CRACKED SKIN AT XOS 1005.1241 LOWER CUTOUT FASTENERS REMOVED PER MD-11 SRM 51-31-01-0G AND TRIMMED OUT CRACKED SKIN PER MSDR FDEA202607210965Stiffener · crackedRIGHT WING- LEADING EDGE COMPARTMENT STIFFENER AT XOS 541 FOUND CRACK ABOUT 0.5 INCHES. RIGHT WING LEADING EDGE COMPARTMENT CRACKED STIFFENER AT XOS 541 REMOVED AS PER MD-11 SRM 51-33-01-0G AND MD-11 SRM 51-35-01-0G. FABRICATED STIFFENER AS PER DOUGLAS DRSDR FDEA202607210964Former · crackedRIGHT WING- LEADING EDGE COMPARTMENT FORMER AT XOS 559.442 FOUND CRACK ABOUT 0.5 INCHES. RIGHT WING LEADING EDGE COMPARTMENT CRACKED FORMER REMOVED AT XOS 559.442 PER MD-11 SRM 51-33-01-0G AND MD-11 SRM 51-35-01-0G. FABRICATED FORMER PER DOUGLAS DRAWINGSDR FDEA202607210963Angle · crackedRIGHT WING- LEADING EDGE COMPARTMENT ANGLE AT XOS 1083 FOUND CRACK ABOUT 0.5 INCHES. RIGHT WING LEADING EDGE COMPARTMENT CRACKED ANGLE AT XOS 1083 REMOVED AS PER MD-11 SRM 51-35-01-0G. FABRICATED ANGLE AS PER DOUGLAS DRAWING ARB2920 REVISION BB. FABRICATESDR FDEA202607210962Angle · crackedLEFT WING- LEADING EDGE COMPARTMENT ANGLE AT XOS 1083 FOUND CRACK ABOUT 0.6 INCHES. LEFT HAND WING LEADING EDGE COMPARTMENT CRACKED ANGLE AT XOS 1083 REMOVED AS PER MD-11 SRM 51-33-01-0G AND MD-11 SRM 51-35-01-0G. FABRICATED ANGLE PER DOUGLAS DRAWING ARB2SDR FDEA202607210961Angle · crackedLEFT HAND WING- LEADING EDGE COMPARTMENT ANGLE AT XOS1089 FOUND CRACK ABOUT 0.5 INCHES. LEFT HAND WING LEADING EDGE COMPARTMENT CRACKED ANGLE AT XOS 1089 REMOVED AS PER MD-11 SRM 51-33-01-0G AND MD-11 SRM 51-35-01-0G. FABRICATED ANGLE AS PER DOUGLAS DRAWISDR FDEA202607210960Former · crackedLEFT WING-LEADING EDGE COMPARTMENT FORMER AT XOS 559.422 FOUND CRACK ABOUT 0.5 INCHES. LEFT HAND WING LEADING EDGE COMPARTMENT CRACKED FORMER AT XOS 559.422 REMOVED AS PER MD-11 SRM 51-33-01-0G AND MD-11 SRM 51-35-01-0G. FABRICATED FORMER AS PER DOUGLAS DSDR FDEA202607200949Doubler · crackedRIGHT WING- LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 734 FOUND CRACK ABOUT 0.25 INCH. BEADED DOUBLER AT XOS 734 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA202607200948Doubler · crackedRIGHT WING- LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 494 FOUND CRACK ABOUT 1 INCH. RIGHT WING LEADING EDGE COMPARTMENT CRACKED BEADED DOUBLER AT XOS 494 REPAIR CARRIED OUT IAW SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM SDR FDEA202607200947Doubler · crackedRIGHT WING- LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 541 FOUND CRACK ABOUT 0.7 INCH. BEADED DOUBLER AT XOS 641 REPAIR CARRIED OUT IAW SRM 57-40-02-2R, REPAIR 15, FIGURE 203. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA202607200946Doubler · crackedLEFT WING, LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 745 FOUND CRACK ABOUT 0.4 INCH. LEFT WING LEADING EDGE COMPARTMENT CRACKED BEADED DOUBLER AT XOS 745 TRIMMED OUT AND REPAIR CARRIED OUT PER MD-11 SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSISDR FDEA202607190945Switch · inoperativePUSH TO TEST LIGHT ON DOOR 1L NOT ILLUMINATING DURING PREFLIGHT TEST. LEFT EVAC SLIDE REMOTE PRESS INDICATOR - INOPERATIVE. IAW MEL 25-61-02, R & R REMOTE PRESSURE SWITCH LIGHT ASSY IAW AMM 25-61-04-4. OPS CHECK NORMAL. ACFT OK FOR SERVICE.SDR FDEA202607170940Switch · faultedR1 DOOR SLIDE PRESSURE SWITCH LIGHT ON, PLUG READING STUCK CLOSED (0.0 OHM), BOTTLE PRESSURE INDICATES NORMAL ON SLIDE ASSY. REMOVED AND REPLACED R1 EVACUATION SLIDE. PUSHBUTTON PRESSURE INDICATOR SWITCH TESTS GOOD.SDR 9WGA2026071678101Engine · power lossAIRCRAFT TAKEOFF FROM JIB AIRPORT, DURING CLIMB OUT ENG 1 VIB 5.1 FOLLOWED BY RAPID DECELERATION OF N1 W/HIGH BUFFETING, SHUTDOWN ENG 1, AIRCRAFT RETURNED SAFELY TO JIB AIRPORT.SDR FDEA202607131056Skin · crackedRH WING SKIN ARB2363-2 CRACKED BELOW PYLON FOOTSTOOL AREA. THIS IS A MAJOR REPAIR. COMPLIED WITH EA 1-5730-T0387997.SDR FDEA202607130918Bulkhead · misalignedRIGHT ENGINE #3 PYLON AFT BULKHEAD FOUND LUG BORE HOLE MISALIGN.YWN 418. RIGHT ENGINE #3 PYLON AFT BULKHEAD LUG BORE HOLE MISALIGN HOLE REWORKED AS PER EA #1-5440-T0387700 PART1.TITLE: NACELLES/PYLON - ATTACH /MOUNT/HINGE - NO 3 PYLON AFT BULKHEAD - MD11-BSDR FDEA202607100887Test Switch · inoperativeR1 DOOR SLIDE PRESS TO TEST LIGHT IS INOPERATIVE AMM 25-61-04-4. R & R BATTERIES & BOTH LAMPS. NO HELP. R & R REMOTE PRESSURE INDICATOR ASSY IAW AMM 25-61-04-4. INDICATOR KIT BAD FROM STOCK. INDICATOR STILL INOP. SLIDE BOTTLE PRESSURE NORMAL. RELEASED FOSDR FDEA202607080862Fitting · chafedLEFT ENGINE PYLON - AFT PYLON BULKHEAD LUG FITTING FOUND WITH CHAFE AT EXTERIOR UPPER AREA.YWN-418. CARRIED OUT REPAIR IN ACCORDANCE WITH EA #1-5440-T0387673 PART 1 AND 2 TITLE: NACELLES/PYLON - ATTACH/MOUNT/HINGE- NR 1 PYLON AFT BULKHEAD LUG INSPECTION ANDSDR FDEA202607010824Skin · damagedLH WING LOWER SURFACE (NEAR FOOTSTOOL FITTING) HAS SEVERAL WEAR MARKS. C/W EA 1-5730-T0387611SDR FDEA202606190781Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1279, X= -47.5" FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 1279, X = - 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRSDR FDEA202606160754Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 755, X= -27.5" FOUND CROWN WORN. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 755, X = - 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROSDR FDEA202606160753Longeron Splice · crackedLOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON SPLICE FITTING FOUND CRACK BETWEEN STATION 1801-1821 LONGERON 46 RIGHT. CRACKED LONGERON SPLICE FITTING AT LOWER CENTER CARGO COMPARTMENT BILGE AREA BETWEEN STATION 1801-1821, LONGERON - 46 RIGHT REMOVED ASDR FDEA202606160752Seat Track · wornCABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 979, X= -27.5 FOUND CROWN WORN. CABIN - MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 979, X = - 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWASDR FDEA202606150745Seat Track · wornMAIN DECK CARGO SEAT TRACK AT STATION 1541, X= -47.5" FOUND CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT BS 1571 TO EXISTING SPLISDR FDEA202606150744Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1541, X= 27.5" FOUND CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, SDR FDEA202606150743Seat Track · wornCABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= 8.5" FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 6-10, X = 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGSDR FDEA202606150742Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= 27.5" FOUND CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-SDR FDEA202606150741Seat Track · wornCABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= 47.5" FOUND CROWN WORN. THE SEAT TRACK BS 6-10, X = 47.5 WAS EVALUATED & FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPSDR FDEA202606150740Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1279, X= -27.5" FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK BS 1279, X = - 27.5 WORN CROWN EVALUATED & FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRASDR FDEA202606150739Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 5-10, X= -8.5" FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 5-10, X = - 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRSDR FDEA202606150738Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 5-10, X= -27.5" FOUND CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT BS 5-63 TO EXISSDR FDEA202606150737Seat Track · wornCABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10, X= -8.5" FOUND CROWN WORN. THE SEAT TRACK BS 6-10, X = - 8.5 WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONALSDR FDEA202606120729Seat Track · wornCABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1009, X= 27.5 FOUND CROWN WORN. THE SEAT TRACK STATION 1009, X = 27.5 WAS EVALUATED & FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLSDR FDEA202606120728Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 6-10, X= -47.5 FOUND CROWN WORN. THE SEAT TRACK WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2SDR FDEA202606120727Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1079, X= -47.5 FOUND CROWN WORN. THE SEAT TRACK BS 1079, X = - 47.5 WAS EVALUATED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENSDR FDEA202606120726Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BS 1009, X= -47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT, AT SEAT TRACK STATION 1009, X = - 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROSDR FDEA202606120725Seat Track · wornMAIN DECK CARGO SEAT TRACK AT STATION 879, X= 27.5 FOUND CROWN WORN. THE SEAT TRACK BS 879, X = 27.5 WAS EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT BS 869 TO 909SDR FDEA202606110705Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 879, X= -27.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT AT SEAT TRACK STATION 879, X = - 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORNSDR FDEA202606110704Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 839, X= -8.5 FOUND CROWN WORN. THE SEAT TRACK STATION 839, X = - 8.5 EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT SDR FDEA202606110703Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 806, X= -8.5 FOUND CROWN WORN. SEAT TRACK STATION 810, X = - 8.5 CROWN EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACESDR FDEA202606110702Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 806, X= 8.5 FOUND CROWN WORN. EVALUATED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52-1A, FIGURE 101 ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLICES BS 745 TO 806, SDR FDEA202606100694Bearing · damagedNR 3 ENGINE PYLON AFT BULKHEAD LUG BORE HOLE FOUND WITH CORROSION AFTER SPHERICAL BEARING REMOVED. CORROSION AT 3 ENGINE PYLON AFT BULKHEAD LUG BORE HOLE CARRIED OUT REPAIR AS PER EA 1-5440-T0387710 PART 1. REPAIR CLASSIFED AS MAJOR IAW GMM 6-2-100.SDR FDEA202606100693Bearing · damagedNR 1 ENGINE PYLON AFT BULKHEAD LUG BORE HOLE FOUND WITH EXISTING DAMAGE AND CORROSION AFTER SPHERICAL BEARING REMOVED. REPAIR CARRIED OUT AS PER EA# 1-5440-T0387712 PART1 AND PART 2 AND PART 3. NR 1 PYLON, REMOVAL AND REPLACEMENT OF AFT BULKHEAD THIS EA DESDR FDEA202606030669Lug · corrodedRIGHT ENGINE PYLON AFT BULKHEAD LUG BORE HOLE FOUND WITH CORROSION AT 12 O'CLOCK, 3 O'CLOCK, 9 O'CLOCK AND 6 O'CLOCK POSITION AFTER SPHERICAL BEARING REMOVAL. CORROSION AT RIGHT ENGINE PYLON AFT BULKHEAD LUG BORE HOLE AT 12 O'CLOCK,3 O'CLOCK,9 O'CLOCK AND 6 O'SDR FDEA202606030668Lug · corrodedLEFT ENGINE PYLON AFT BULKHEAD LUG BORE HOLE FOUND WITH CORROSION AFTER SPHERICAL BEARING REMOVAL YWN 418. CORROSION AT LEFT ENGINE PYLON AFT BULKHEAD LUG BORE HOLE CARRIED OUT REPAIR IAW EA 1-5440-T0387673, PART 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-10SDR FDEA202606030666Bulkhead · worn#3 AFT PYLON BULKHEAD WORN REMOVED AND REPLACED AFT BULKHEAD.SDR FDEA202605180619Access Panel · crackedNR 3 PYLON COMPARTMENT THROUGH ACCESS PANEL 617BT OUTBOARD LOWER AFT WEB FOUND CRACK APPROXIMATELY 0.75" AT XFS 427 #3 PYLON COMPARTMENT ACCESS PANEL 617BT OUTBOARD LOWER AFT CRACKED WEB AT XFS 427 REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-31-01-0G. WSDR FDEA202605180618Access Panel · crackedNR 1 PYLON COMPARTMENT THROUGH ACCESS PANEL 517BT OUTBOARD LOWER AFT WEB FOUND CRACK APPROXIMATELY 0.5" AT XFS 427. #1 PYLON COMPARTMENT ACCESS PANEL 517BT OUTBOARD LOWER AFT CRACKED WEB AT XFS 427 REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-31-01-0G. WSDR FDEA202605090577Bearing · wornAFT SPHERICAL BEARING WORN. COMPLIED WITH EA 1-5450-T0386066 P2SDR FDEA202605050546Nacelle · not reportedNACELLES/PYLON - WING PYLON/STRUT - NO. 1 PYLON, INSPECTION AND REPAIR OF DAMAGE COMPLY WITH EA 1-5450-T0386263 REV NR POS. P2 COMPLY WITH E..A. 1-5450-T0386263 REV NR PS P2 EA: 1-5450-T0386263 PT 2 COMPLLIED WITH EA 1-5450-T0386263 PT 2 REMOVING AND
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