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 IPXA2022042181359None · crackedINSPECTION TYPE:3CAFT CARGO VERTICAL STIFFNER IS CRACKED AT STA. 1841 AND LONG. 48R.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. 7170 AND SRM 51-33-01. (MINOR)SDR IPXA2022042181358None · crackedINSPECTION TYPE:3CAFT CARGO VERTICAL STIFFNER IS CRACKED AT STA. 1841 AND LONG. 49R.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRM 51-31-01. (MINOR)SDR IPXA2022041681211Doubler · crackedINSPECTION TYPE:3CL/H WING FIXED L/E HAS A BEADED DOUBLER P/N ARB2894-1 THAT IS CRACK AT STA XOS=768 - XOS=772.REMOVED,FAB,REPLACED THE CRACKED BEADED DOUBLER P/N ARB2894-1 ON THE L/H WING FIXED L/E AT STA XOS=768 - XOS=772. IAW DWG ARB2894 AND MD11 SRM 57-40-SDR IPXA2022042581436Longeron · corrodedINSPECTION TYPE:2CCENTER CARGO LONGERON 49R HAS CORROSION AT STA. 5-93/1541.REPAIRED CORRODED CENTER CARGO LONGERON 49R BETWEEN STA. 5-103 TO 5-123 IAW VT-SAA EA 011-5310-01-A9540 REV. I/R AND UPS EO MD11-5310-83411-A. (MAJOR) REF FAA FORM 8100-9 BY. S. KANG (SDR IPXA2022042181352Longeron · corrodedINSPECTION TYPE:4CEXTERIOR FUSELAGE LONGERON 28R P/N AEA7545-2 HAS CORROSION BETWEEN STA Y=1207 - Y=1305.5.REPAIRED CORRODED LONGERON 28R P/N AEA7545-2 IAW EA 011-5300-01-A9541 REV I/R AND UPS EO MD11-5310-83430-A (MINOR)SDR IPXA2022042081326Stiffener · crackedINSPECTION TYPE:4CLOWER FUSELAGE R/H WING TO BODY HAS A STIFFENER P/N AYB7104-526 WITH A CRACK AT STA 1298.REMOVED,FAB AND REPLACED THE CRACK STIFFENER P/N AYB7104-526 IAW DWG AYB7104 AND MD11 SRM 51-33-01. (MINOR)SDR IPXA2022041881255Stiffener · crackedINSPECTION TYPE:1CAFT CARGO COMPARTMENT STEP UP BULKHEAD STIFFENER CRACK AT STA.1841 LON 49R.REMOVED,FABRICATED AND REPLACED CRACKED STIFFENER IAW MD-11 SRM 51-33-01 AND 51-35-01 (MINOR).SDR IPXA2022041681208Stiffener · crackedINSPECTION TYPE:4CAFT CARGO STEP UP HAS A STIFFENER P/N AGA7170-11 HAS A CRACK AT STA 1841.REMOVED, FAB AND REPAIRED THE CRACKED STIFFENER P/N AGA7170-11 IAW MD11 51-31-01 AND 51-35-01 (MINOR)SDR IPXA2022041681207Stiffener · crackedINSPECTION TYPE:4CAFT CARGO STEP UP HAS A STIFFENER P/N AGA7170-9 THAT IS CRACKED AT STA 1841.REMOVED,FAB AND REPLACED THE CRACKED STIFFENER P/N AGA7170-9 IAW MD11 SRM 51-31-01 AND 51-35-01 (MINOR)SDR IPXA2022041681206Longeron · corrodedINSPECTION TYPE:4CEXTERIOR FUSELAGE , LONGERON 28L P/N AEA7545-1 HAS CORROSION BETWEEN STA 1304-1309.REPAIRED CORRODED LONGERON 28L P/N AEA7545-1 IAW EA 011-5300-01-A9539 I/R AND UPS EO MD11-5310-83429-A (MINOR)SDR IPXA2022041381125Beam · crackedINSPECTION TYPE:2CR-3 DOOR PLUG UPPER HORZ. BEAM IS CRACKED AT THE FWD. END.REMOVED AND REPLACED BEAM IAW SRM 51-31-01 & 51-35-01. (MINOR)SDR IPXA2022040780931Ceiling Panel · tornL1 ENTRY DOOR OVERHEAD TRIM PANEL IS BINDING WHEN L1 DOOR IS OPENED. REMOVED TORN SLIDING CEILING PANEL CABEL & REPLACED PER AMM 25-23-23-400801.SDR FDEA202204060878Longeron · corrodedAFTER REMOVAL OF CORRODED LONGERON 52 SPLICE FITTING AT STATION 1119 - 6-10 LONGERON 52 CORRODED AT 6-10. FOUND LONGERON 52 CORRODED AT 6-10. CORROSION AT LONGERON 52 STATION 6-10 EVALUATED , FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FSDR FDEA202204060876Access Door · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND WING SLAT OF ACTUATOR ACCESS DOOR FORWARD INBOARD CORNER FOUND 01EA CRACK APPROXIMATELY 0.2 INCH. RIGHT HAND WING SLAT ACTUATOR ACCESS DOOR FORWARD INBOARD CORNER CRACKED AREA AT STATION XOS SDR FDEA202204060871Longeron · crackedCENTER CARGO - STATION 1581 TO STATION 1601 LONGERON 38 RIGHT SUSPECT CRACK. CENTER CARGO - STATION 1581 TO STATION 1601 LONGERON 38 RIGHT REPAIR CARRIED OUT AS PER SRM 53-00-05-2R FIGURE 202 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100.SDR IPXA2022042781515Frame · gougedINSPECTION TYPE:1CCENTER LANDING RH FWD DOOR GOUGE AT FWD FRAME(PAN).REMOVED AND REPLACED GOUGED FRAME IAW SRM 51-31-01 AND 51-33-01 (MINOR).SDR IPXA2022042281385Web · crackedINSPECTION TYPE:4CMAIN CARGO R3 DOOR TORQUE BOX LWR AFT WEB IS CRACKED AT STA Y=1313 AND Z=-16.REMOVED, FAB AND REPAIRED CRACKED AFT WEB P/N AEA0112-2 AT STA Y=1313 AND Z=-16 IAW MD11 SRM 53-40-15 FIG 201 REPAIR 3 (MAJOR)SDR IPXA2022042281383Stringer · crackedINSPECTION TYPE:4CR/H WING FIXED L/E LOWER STRINGER EXISTING REPAIR DOUBLER IS CRACKED AT STA XOS=906.5607.REMOVED, FAB AND REPLACED CRACK REPAIR DOUBLER AT STA XOS=906.5607 IAW MD11 SRM 57-40-03 FIG 201 REPAIR 1 (MAJOR)SDR IPXA2022042281392Brace · crackedINSPECTION TYPE:4CL/H WING T/E REAR SPAR HAS A BRACE THAT IS CRACKED.REMOVED,FAB REPLACED THE CRACKED BRACE IAW MD11 DWG ARC0295 AND SRM 51-31-01. (MINOR)SDR IPXA2022041981297None · crackedINSPECTION TYPE:4CR/H I/B FLAP I/B TRACK THE 2ND FITTING FROM THE BOTTOM IS CRACKED.REMOVED, REPLACED R/H I/B FLAP ASSY P/N NRC6055-508 IAW MD11 AMM 27-50-20-400-801 (MINOR)SDR IPXA2022041681205Stiffener · crackedINSPECTION TYPE:3CL/H MLG WHEEL WELL HAS A STIFFENER THAT IS CRACK AT AFT O/B WEB.REMOVED, FAB, AND REPLACED THE CRACK STIFFENER IAW DWG ANB7203, MD11 SRM 51-31-01 AND 51-35-01. (MINOR)SDR IPXA2022041581180Doubler · crackedINSPECTION TYPE:C4R/H O/B WING FIXED LEADING EGDE BEADED DOUBLER IS CRACKED AT STA XOS=661.7 -XOS=667.62 .REMOVED, FAB AND REPAIRED THE CRACK BEADED DOUBLER AT STA XOS=661.7 - XOS=667.62 IAW DWG ARB2893-2 AND MD11 SRM 57-40-02 REPAIR 15, FIG 205 REV 68.01 (MAJSDR IPXA2022041581179Floor Panel · corrodedINSPECTION TYPE:C4FWD CABIN FLOOR PANEL P/N WSP0788-502 AT STA Y=475.0 - Y=503.175 AND X=-36.000 - X=-47.500 HAS HEAVY CORROSION.REMOVED, REPLACED FLOOR PANEL WSP0788-502 IAW DWG WSP0788 AND DWG SP11530078, SRM 51-31-01 (MINOR)SDR FDEA202204050918Rib · crackedRIGHT HAND INBOARD FLAP, INBOARD LEADING EDGE CAVITIE HAS A ONE INCH TEAR IN LOWER FORWARD LIGHTNING HOLE. BLENDED DAMAGE AND APPLIED DOUBLER REPAIR IAW SRM 57-00-00-2R FIG 201, SEE ALSO EA 1-5750-T0368054SDR FDEA202204050852Light · no testEMER LIGHT BAT 1 LO ALERT ON EMER LT TEST. RETERMINATED PIN 7 AT PLUG J2 OF FWD CABIN EMERGENCY LIGHT PWR SUPPLY U1-1756SDR FDEA202204050873Brake · damagedBRAKE OVERHEAT ON TAXI OUT. NUMBER 5 BRAKE GOT TO 710. AIRCRAFT STOPPED AND WHILE STOPPED THE FUSE PLUG BLEW AND PRESSURE WENT TO ZERO. INSPECTED #5 MLG AXLE IAW MD11 AMM 32-43-20-4 NO HEAT DAMAGE, INSTALLED NEW #5 BRAKE AND TIRE. ALL TEST PASSED AND TSDR FDEA202204050870Floorboard · delaminatedMAIN DECK FLOOR BOARD PANEL # 245GF HAS DELAMINATION . REPLACED WITH NEW FABRICATED FLOOR BOARD PANEL PER FEDEX DRWG SRZ-25-005 ADA7178.SDR FDEA202204050866Floorboard · damagedMAIN DECK FLOOR BOARD PANEL #282GF HAS DAMAGE AND INSERTS ARE CORRODED. FABRICATED NEW FLOOR BOARD PANEL PER FEDEX DRWG SRZ-25-005 ,AFA3200.SDR FDEA202204050864Floorboard · delaminatedMAIN DECK FLOOR BOARD PANEL #241CF FOUND DISBONED DURING REMOVEL FOR INSPECTION. FABRICATE NEW FLOOR BOARD PANEL PER FEDEX DRWG SRZ-25-005, ADA8349 .SDR FDEA202204050859Brake · overtempBRAKE OVERHEAT ON TAXI OUT. NUMBER 5 BRAKE GOT TO 710. AIRCRAFT STOPPED AND WHILE STOPPED THE FUSE PLUG BLEW AND PRESSURE WENT TO ZERO. INSPECTED #5 MLG AXLE IAW MD11 AMM 32-43-20-4 NO HEAT DAMAGE, INSTALLED NEW #5 BRAKE AND TIRE. REF WRIS 32-40-6966,32-4SDR FDEA202204050847Skin · crackedRIGHT HAND WING SLAT TRACK NUMBER 12 CUTOUT LOWER OUTBOARD CORNER SKIN AT APPROXIMATELY STATION XOS 776 FOUND WITH CRACK. RIGHT HAND WING SLAT TRACK NUMBER 12 CUTOUT LOWER OUTBOARD CORNER SKIN AT APPROXIMATELY STATION XOS 776 CRACKED AREA REPAIR CARRIED SDR FDEA202204050844Doubler · crackedLEFT HAND WING OUTBOARD LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 616 TO 621 FOUND CRACK. LEFT HAND WING OUTBOARD LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 616 TO 621 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR SDR FDEA202204050842Doubler · crackedRIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 697 TO 703 FOUND CRACK. RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 697 TO 703 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 2SDR FDEA202204050841Doubler · crackedRIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 691 TO 697 FOUND CRACK. RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 691 TO 697 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 2SDR FDEA202204050840Doubler · crackedRIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 643 TO 648 FOUND CRACK. RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 643 TO 648 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203SDR FDEA202204050838Doubler · crackedRIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 584 TO 588 FOUND CRACK. RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 584 TO 588 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 20SDR IPXA2022042281387Skin · damagedINSPECTION TYPE:4CCENTER FUSELAGE LOWER SKIN PANEL HAS EXISTING CHAFED DAMAGED AT STA 1153 AND LONGERON 44L .REMOVED, REPAIRED EXISTING CHAFED DAMAGED AT STA 1153 AND LONGERON 44L IAW VTSAA EA 011-5340-01-A9535 REV I/R AND UPS EO MD11-5330-83452-A FAA FORM 810SDR IPXA2022042081338Floor Panel · corrodedINSPECTION TYPE:3CMAIN CABIN FLOOR PANEL WSP0785-501 HAS CORROSION BETWEEN STA Y=475.000 - Y=503.175 AND X=-27.500 - X=-36.000.REMOVED, REPLACED THE CORRODED FLOOR PANEL P/N WSP0785-501 IAW DWG WSP0785 AND MD11 SRM 51-31-01. (MINOR)SDR FDEA202204040831Warning Message · false activationDURING THE EMERG PWR TO ARM DURING PREFLIGHT RECEIVED EMER PWR TST FAIL LEVEL 1 ALERT 04APR22 04:56 MEM R OLD DISCREPANCY : 591 / 24-22 / 0006810 PART 04APR22 05:13 MEM U IDENTIFIED PARTS MARATHON MAIN MPN: 31433-001 CPN: 2412387 QTSDR FDEA202204040827Skin · crackedEMPENNAGE - AFT FUSELAGE RIGHT HAND SIDE ON TOP OF APU EXHAUST DOOR AREA APPROXIMATE STATION 2140 LONGERON 36 RIGHT FOUND SKIN CRACK 2.2 INCH. EMPENNAGE -AFT FUSELAGE RIGHT HAND SIDE ON TOP OF APU EXHAUST DOOR AREA APPROXIMATE STATION 2140 LONGERON 36 RIGHSDR IPXA2022041581177Floor Panel · corrodedINSPECTION TYPE:C4FWD CABIN FLOOR PANEL P/N WSP0786-501 AT STA Y=475.0 -Y=503.175 AND X=-17.000 - X=-27.500 HAS HEAVY CORROSION.REMOVED, REPLACED FLOOR PANEL IAW DWG WSP0786 AND DWG SP11530078, SRM 51-31-01 (MINOR)SDR IPXA2022041181076Stiffener · crackedINSPECTION TYPE:2CR/H MLG W/W 3RD STIFFNER AT O/B WEB IS CRACKED.REMOVED AND REPLACED STIFFNER IAW SRM 51-35-01. (MINOR)SDR FDEA202204030816Lug · corrodedRIGHT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR LUG BORE CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-07 ANDSDR FDEA202204030815Lug · corrodedRIGHT HAND WING - INBOARD FLAP ASSEMBLY . OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG BORE CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM57-44-07. REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM57-44-07 ANSDR FDEA202204020823Battery · dischargedMDIS 590 33-50 0749 02APR22 YYZ OPEN U DURING PRE FLIGHT, EMERGENCY LIGHTING SYSTEM TEST FAILS AND SHOWING MSG BAT 1 LO. REMOVED AND REPLACED POWER SUPPLY, EMERGENCY LIGHTING BATTERY REF. AMM 33-51-01-4. PERFORMED SDR FDEA202204011141Stiffener · corrodedCENTER WHEEL WELL LOWER AUX TANK ACCESS LANDING 143DZ FOUND 6 DOMENUTS DAMAGED. REPLACED STIFFNER REF AYB7113.SDR FDEA202204010808Skin · misrepairedAGING AIRCRAFT - EXISTING REPAIR DOUBLER ON EXTERIOR FUSELAGE SKIN BETWEEN STATION 383 TO STATION 399 , LONGERON 25 LEFT HAND TO LONGERON 27 LEFT HAND. EXISTING REPAIR DOUBLER ON EXTERIOR FUSELAGE SKIN BETWEEN STATION 383 TO STATION 399 LONGERON 25 TO LONGSDR FDEA202204010812Bolt · looseR/H MLG ACTUATOR "A" FRAME LOWER FWD ATTACH BOLT LOOSE. REMOVE AND INSTALL FITTING ASSEMBLY WITH NEW HARDWARE PER AMM 57-20-14-4.SDR FDEA202203310787Floorboard · delaminatedMAIN DECK AFT FLOOR BOARD PANEL 283BS DELAM FOUND TWO LOCATION. FABRICATED NEW FLOOR BOARD PANEL 283BS PER FEDEX DRWG SRZ-25-005 AGA3212SDR FDEA202203300758Valve · failedPDIS 601 32-30 3967 30MAR22 OAK OPEN U AFTER ROTATION ON TAKEOFF AND CALLING FOR GEAR UP , GEAR HANDLE EXTREMELY DIFFICULT TO MOVE STARTING ABOUT A THIRD THROUGH THE RANGE OF TRAVEL. GOT THE GEAR HANDLE TO MOVE TO THE UP POSITION WITH 20-30
Back to Boeing MD-11F