Boeing MD-11F
Service difficulty reports · 31,320
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 FDEA201311282889Support Fitting · damagedCABIN UPPER CARGO DOOR LOWER JAMB SUPPORT FITTING NR 5, HOLE B & C DIAMETER OVERSIZED TO 0.520 INCH. REPAIR BUSHINGS 02 EACH FABRICATED AND INSTALLED AS PER SRM 53-00-15 FIGURE 201 REPAIR 5 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.SDR CLCA20131128001Engine · shutdownDURING DECENT, ENG NR 2 FADEC BACK UP POWER APPEARED, THEN ENG NR 2 SHUT DOWN.SDR FDEA201311272882Support · crackedCENTER CARGO COMPARTMENT DOOR CUTOUT UPPER JAMB FRAME SUPPORT FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 53-50-15 FIGURE 201 REPAIR 2 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.SDR FDEA201311272886Coalescer Bag · dirtyVERY RANCID ODORS EMANATING FROM A/C PACKS. INSPECTED SYS & FOUND ALL 3 COALESCER BAGS TO BE DIRTY. R & R THE COALESCER BAGS & OPERATIONS CHECKED OK. ACFT IS OK FOR CONTINUED SERVICE.SDR FDEA201311262885Slide Raft · inoperativeR1 DOOR SLIDE INFLATION CYLINDER LOW PRESS LIGHT ILLUMINATED. R & R RT EVACUATION SLIDE RAFT CONTAINER IAW MM 25-61-01-4 & ADJUST TEST IAW MM 25-61-01-5.SDR FDEA201311252865Skin · chafedCENTER CARGO DOOR FWD CUTOUT STATION 1708 FUSELAGE SKIN BETWEEN LONGERON 40RT & LONGERON 41RT FOUND EXISTING BLEND OUT. FUSELAGE SKIN CARRIED OUT REPAIR AS PER FEDEX EA 1-5330-T0304376 PART 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118. REPETISDR FDEA201311242862Frame · dentedCABIN RT HAND STATION 1641 LONGERON 12 RT FRAME FOUND WITH DENT. FRAME REPAIRED PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53. REPEAT INSPECTION REQUIRED, INITIAL AT 14,500 FLIGHT CYCLES AND REPETITIVE INSPECTION AT 9,500 FLIGHT CYCLES AS PER SRM 53- 00- SDR FDEA201311242861Frame · dentedCABIN RT HAND STATION 1621 LONGERON 12RT FRAME FOUND WITH DENT. FRAME REPAIRED AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53. REPEAT INSPECTION REQUIRED, INITIAL AT 14,500 FLIGHT CYCLES AND REPETITIVE INSPECTION AT 9,500 FLIGHT CYCLES AS PER SRM 53- 0SDR FDEA201311242860Skin · crackedRIGHT WING LE LOWER ACCESS PANEL 619CB, CUTOUT INBD CORNER, FOUND CRACK AT STATION XOS 612 DURING OTBD SLAT DRIVE CABLE INSPECTION. CRACK AT STATION XOS 612 TRIMMED OUT AND REPAIR CARRIED OUT AS PER SRM 57-40-02 FIGURE 202 REPAIR 7 REVISION 53. REPAIR CLASSISDR FDEA201311222852Vane · delaminatedRIGHT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATION AT XIFH 160 TO XIFH 187. FLAP VANE ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-22-4 REVISION 77.0 ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REVISION 77.0 FOUND SATISFACTORY. REPAIR CLASDR FDEA201311202831Panel · missingFOUND A PANEL MISSING ON NR 3 ENG INBD, PANEL MPN AUB7726-501. SS OIL 20NOV13 09:05 SYD U NO RESTRICTION IAW1-5480-T0304174 NR 3 ENG PYLON PANEL 488EL MISSING FROM INBD SIDE. OK TO CONTINUE IAW EA 1-5480-T0304174. COMPLIED WITH PT1 OF EA 1-5480-T0304174 C0SDR FDEA201311192828Sensor · failedUPON CONFIGURATION AT 15 DEG FLAPS, LEVEL 2 SLAT DISAGREE ILLUMINATED, GO AROUND. RAN CHECKLIST ON EXTENDED DOWNWIND. DURING GO AROUND THERE WAS SOME FEEL THAT CONFIGURATION WAS OFF. LANDED SLAT STOW FLAPS 28 DEGREES AT 185KTS & MAX BRAKES. RAN SLATS VERSDR WRLA20131118603Spinner · failedSPINNER CAME APART AND DAMAGED 15 C-1 FAN BLADES AND ENGINE INLET COWL. FOUND FOD TO NR 3 ENG. BLADES, SPINNER & ENG. INLET COWL. REPLACED ENG. INLET COWL, SPINNER AND ALL 38 FAN BLADES, REF AMM 22-31-02. HIGH POWER ENGINE RUN C/W REF. AMM 71-00-00. ALL OPSSDR IPXA2013112000878Skin · damagedRT WING I/B FLAP COVE PANEL HAS .1250" HOLE 120" FROM INBD EDGE. REPAIR IAW EO B747-5750-52755-A.SDR IPXA2013112000877Skin · damagedRT WING INBD FLAP COVE PANEL HAS .1250 INCH HOLE, 58 INCHES FROM INBD EDGE. REPAIRED IAW EO B747-5750-52758-A.SDR IPXA2013112000876Skin · damagedRT WING INBD MID FLAP COVE PANEL HAS .1250 INCH HOLE 58 INCHES FROM INBD EDGE. REPAIRED IAW EO B747-5750-52756-A.SDR FDEA201311162795Bottle · leakingAFTER SERVICING OF R4 AFT PASSENGER DOOR STORAGE RESERVOIR, FOUND AN AIR LEAK COMING FROM THE INDICATOR. R & R R4 AFT PASSENGER DOOR STORAGE RESERVOIR IAW MM:52-11-04-4 AND MM:52-11-07-2. SERVICED THE STORAGE RESERVOIR IAW MM:12-25-04-3. LEAK TEST OK. ACFSDR IPXA2013112000900Bottle · low pressurePNEUMATIC PRECHARGE FOR L1 ENTRY DOOR EMERGENCY EXIT PRESSURE BELOW GREEN BAND. SERVICED L1 DOOR BOTTLE IAW AMM 12-25-04-600-801.SDR FDEA201311142822Light · pulledEMERGENCY LIGHT PANEL PULLED OUT OF THE NEXT INBD PANEL. HAD MOUNT HOLES RIPPED OUT. REPLACED R1 DOOR PASSENGER SLIDING CEILING PANEL PER AMM 25-23-23-2. EMERGENCY LIGHTS OPS CHECKED GOOD.SDR FDEA201311142781Sign · damagedWHEN CLOSING THE R1 DOOR FOR PUSHBACK, THE PANEL WHICH HOUSES THE EMERGENCY EXIT SIGN LIGHT ASSY MOVED OUT OUT OF SEQUENCE AND CAUGHT ON THE DOOR. ENTRY PANEL CAUGHT AND WAS RIPPED OUT OF POSITION. NO RESTRICTION IAW AMM 25-23-23-2. R1 DOOR SLIDING CEILINSDR FDEA201311142777Seat Track · corrodedFOUND SEAT TRACK CORRODED. REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118.SDR FDEA201311142776Floor Support · corrodedFOUND FLOOR SUPPORT TIE-DOWN INBD AREA WITH CORRODED. REMOVED AND REPLACED IAW SRM 51-31-01, REVISION 53. NEW FLOOR SUPPORT FABRICATED IAW DWG WSP 0668, REVISION B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118.SDR FDEA201311142775Cargo Track · corrodedMAIN DECK CARGO TRACK AT BS 1411-1491, X=-75.25, FLANGE AREA FOUND CORRODED. CARGO TRACK REPAIRED BY SECTIONAL REPLACEMENT BS 1391 - 1531 IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118.SDR FDEA201311142773Longeron Splice · crackedCENTER CARGO LONGERON SPLICE 44R CRACKED AT BS 1651. LONGERON SPLICE FABRICATED IAW DWG AFA7105 REVISION H. REMOVED AND REPLACED WITH NEW IAW SRM 51-33-01, REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118.SDR FDEA201311132756Access Panel · crackedRIGHT WING L/E SLAT DRIVE MECHANISM ACCESS PANEL 618FB LT FORWARD CUTOUT AREA CRACKED APPROXIMATELY 0.75" AT WS XOS 490. REPAIRED IAW SRM 57-40-02, FIGURE 202, REPAIR 7, REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118.SDR FDEA201311132755Longeron · corrodedCENTER CARGO LONGERON 44R, FOUND CORRODED AT BS 1641-1651. REPAIRED IAW SRM 53-00-05 FIGURE 201/202, REPAIR 1, REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118.SDR FDEA201311132759Fairing · damagedFOUND NR 3 ENGINE PYLON AFT BOAT TAIL DAMAGED. FWD LOWER SECTION DEPARTED ACFT. DAMAGE TO AFT CENTER BODY AND TAIL CONE. DAMAGE TO EXHAUST NOZZEL AROUND TAIL CONE AT 12 O`CLOCK POSTION.SDR FDEA201311132753Warning Light · false indicationON FIRST LANDING ATTEMPT, LANDING GEAR SHOWED ALL UNSAFE, CONFIGUATION DISPLAYED ALSO, CYCLED GEAR AND ALL SHOWED SAFE. TOWER STATED GEAR WAS DOWN ON FIRST ATTEMPT. PERFORMED TEST OF PROXIMITY SWITCH ELECTRONICS UNIT, IAW MM 31-71-01-2. ALL UNITS FUNCTIOSDR FDEA201311122738Support Beam · crackedCENTER CARGO DOOR ACTUATOR SUPPORT BEAM CRACKED AT BS 1746. REPAIRED IAW SRM 53-50-15 FIGURE 201, REPAIR 2, REVISION 53 AND EA1-5310-T0206160 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118SDR FDEA201311122737Longeron Splice · crackedCENTER CARGO, LONGERON SPLICE CRACKED AT BS 5-123, LONGERON 39L. LONGERON SPLICE FABRICATED IAW DRAWING A5A7114, REVISION J. REMOVED AND REPLACED WITH NEW SPLICE IAW SRM 51-33-01, REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201311122735Cargo Track · corrodedMAIN DECK CARGO DOOR FLOOR CARGO TRACK AT BS 1942, LBL 107.25, FOUND CORRODED. REPAIRED BY SECTIONAL REPLACEMENT FROM BS 1831 TO 2007 IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118SDR FDEA201311122745Slat System · malfunctionedDURING SLAT EXTENSION, THE SLATS REMAINED RETRACTED. RAN QRH AND MADE A SLATS RET 28 FLAP LANDING. PERFORMED OPS CHECK OF SLATS REF AMM 27-80-01-5. OPS CHECKED GOOD.SDR IPXA2013111300839Structure · corrodedEVIDENCE OF APU TAIL PIPE FIRE. PAINT BLISTERED SHOWING ALUMINUM ALSO ADDITIONAL ITEM, DURING HFEC INSPECTION OF FUSELAGE, FOUND HEAVY CORROSION UNDER FAIRING. REMOVED CORROSION IAW SRM 51-21-01. MAPPING INFO SENT TO ENG TRANSFERRED TO NR 551043 AS A MAJOR RSDR FDEA201311082717Bulb · unsecureRT LT DOOR SLIDE PRESSURE WILL NOT TEST. SECURED LIGHT IN SOCKET ASSY, TESTED NORMAL IAW MM 25-61-04-5. ACFT OK TO CONTINUE.SDR FDEA201311072711Support Fitting · crackedCARRIED OUT HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AND FOUND LOWER DOOR FRAME NR 7 SUPPORT FITTING CRACKED AT HOLE "B" AND "C". REMOVED AND REPLACED IAW SRM 51-33-01, REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.SDR FDEA201311072710Support Fitting · crackedCARRIED OUT HIGH FREQUENCY EDDY CURRENT INSPECTION AND FOUND LOWER DOOR FRAME NR 3 SUPPORT FITTING WITH CRACK INDICATION AT HOLE NO "A" AND "C". REMOVED AND REPLACED IAW SRM 51-33-01, REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.SDR FDEA201311072709Skin · crackedTHREE FASTENER HOLES FOUND CRACKED, DURING OPEN-HOLE HFEC INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 683.4 AND XORS 713.6. REPAIRED IAW SRM 57-20-02, REPAIR 5, FIGURE 201, REVISION 53 AND EA 1-5710-122470, REVISION B, PART 3. REPAIR CLASDR FDEA201311072708Skin · crackedLEFT WING L/E LOWER ACCESS PANEL 518FB CUTOUT INBD CORNER FOUND CRACKED AT WS 492. REPAIRED IAW SRM 57-40-02, FIGURE 202, REPAIR 7, REVISION 53. CLASSIFIED MAJOR REPAIR IAW GMM 6-2-100 REVISION 118.SDR FDEA201311072707Skin · crackedLEFT WING L/E LOWER ACCESS PANEL 519CB CUTOUT INBD CORNER FOUND CRACKED AT WS XOS 612. REPAIRED IAW SRM 57-40-02, FIGURE 202, REPAIR 7, REVISION 53. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 118.SDR IPXA2013110880784Skin · corrodedDURING HFEC INSPECTION OF FASTENERS ON HEAT DAMAGED AREA ABOVE APU EXHAUST, FOUND HEAVY CORROSION BETWEEN AND UNDER EMPENNAGE FAIRING. REMOVED CORROSION IAW SRM 51-21-01. ACCOMPLISHED INTERNAL DVI IAW EO MD11-5330-52665A. NO STRUCTURAL DEFECTS OR FASTENER SDR FDEA201311062698Frame · dentedBS 1681, LONGERON 12R, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.SDR FDEA201311062704Skin · crackedLEFT WING FIXED L/E FOUND CRACKED AT WS XOS 670. REPAIRED IAW SRM 57-40-02 FIGURE 203, REPAIR 15, REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118.SDR FDEA201311062703Doubler · crackedLEFT WING FIXED L/E BEADED DOUBLER FOUND CRACKED AT WS XOS 761. REPAIRED IAW SRM 57-40-02 FIGURE 203, REPAIR 15, REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118.SDR FDEA201311062702Skin · crackedRT WING L/E LOWER SURFACE AT NR 14, SLAT TRACK CUTOUT FOUND CRACKED WS XOS 892.5. REPAIRED IAW SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 53. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 118.SDR FDEA201311062701Frame · dentedBS 1721, LONGERON 12R, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.SDR FDEA201311062700Frame · dentedBS 1701, LONGERON 12R, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.SDR FDEA201311062699Frame · dentedBS 1641, LONGERON 12R, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 118.SDR FDEA201311062697Frame · dentedBS 1741, LONGERON 12L FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.SDR FDEA201311062696Frame · dentedBS 1681, LONGERON 12L FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.SDR FDEA201311062695Skin · crackedRIGHT WING L/E DROOP UPPER SURFACE SKIN FOUND CRACKED AT XDLE 324. REPAIRED IAW SRM 57-40-01 FIGURE 201 REPAIR 5 REVISION 53. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 118.
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