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 FDEA202506100864Seat Track · wornCABIN - FLOOR PANEL SEAT TRACK STATION 5-43 X = - 8.5 CROWN AREA FOUND WORN. CABIN - AT SEAT TRACK STATION 5-43, X = - 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAISDR FDEA202506100862Seat Track · wornCABIN SEAT TRACK AT STATION 6-10 X = 47.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 6-10, X=47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT SDR FDEA202506100861Seat Track · wornCABIN SEAT TRACK AT STATION 6-10 X = -27.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 6-10, X=-27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SESDR FDEA202506100860Seat Track · wornCABIN SEAT TRACK AT STATION 6-10 X = -8.5 FOUND CROWN WORN. CABIN-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 DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT SDR FDEA202506100859Seat Track · wornCABIN SEAT TRACK AT STATION 6-10 X = 8.5 FOUND CROWN WORN. CABIN-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 DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRSDR FDEA202506100858Seat Track · wornCABIN SEAT TRACK AT STATION 1009 X = 27.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1009, X=27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT SDR FDEA202506100857Seat Track · wornCABIN SEAT TRACK AT STATION 1009 X = 8.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 1009, X= 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TSDR FDEA202506100856Seat Track · wornCABIN SEAT TRACK AT STATION 879 X = -8.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 879, X= -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TSDR FDEA202506100855Seat Track · wornCABIN SEAT TRACK AT STATION 879 X = 47.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 879, X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TSDR FDEA202506100854Seat Track · wornCABIN SEAT TRACK AT STATION 879 X = 47.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 879, X= 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TSDR FDEA202506100853Seat Track · wornCABIN SEAT TRACK AT STATION 879 X = -27.5 FOUND CROWN WORN. CABIN-AT SEAT TRACK STATION 879, X=-27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT SDR FDEA202506050840Battery · inoperativeL1 PRESS TO TEST REMOTE SLIDE LIGHT IS INOP. REPLACED BATTERIES & BULBS, PREFORMED SLIDE FUNCTIONAL TEST IAW MM 25-61-05-01, OPS CHECKED GOOD, A/C OK FOR FLIGHT.SDR IPXA2025060844671Rib · damagedLEFT WING LOWER CHORD ON O/B SIDE OF ANTI ICE DUCT DAMAGED AT FWD L/E AND 4" FWD OF AFT END. VERIFIED THE INSTALLATION OF SLAT CAP IAW MD11 SRM 51-35-01 AND SRM 51-33-01. C/W FIT AND FARE ADJUSTMENT PER AMM 30-11-01-400-802SDR FDEA202506010827Lamp · failedNOSE GEAR GREEN LIGHT ON FORWARD PANEL INOP RELAMPED NOSE LANDING GEAR DOWN INDICATING BULB PER AMM 33-11-17-2. OPS CHECK GOOD. A/C OK FOR SERVICE.SDR FDEA202505310829Anti-Ice System · faultedAFTER SELECTING ANTI-ICE ALL ON, AVIONICS FAN OVERRIDE, BLEED AIR 3 OFF, BLEED AIR 1 OFF, PACK 2 FAULT. CABIN PRESSURE STARTED TO CLIMB, ELECTED TO DESCEND TO FL280. AFTER SWITCHING AIR CONTROL CHANNEL, SAME FAULTS RESUMED. SELECTING ALL ANTI-ICE OFF, ALLSDR FDEA202505290818Reservoir · dischargedFOUND L1 DOOR EMERGENCY DOOR PNEUMATIC ASSIST BOTTLE DISCHARGED AND EXTERNAL HANDLE IN EMERGENCY POSITION ON PRE-FLIGHT. RESET L1 DOOR EMERGENCY HANDLE. SERVICED L1 DOOR EMERGENCY ASSIST BOTTLE. A/C OK FOR SERVICE.SDR 9WGA2025063054519Spar · corrodedDURING HEAVY CHECK SPARS LOWER VERTICAL STABILIZER INTERNAL STRUCTURE LH SIDE UPPER AREA NEAR STA 1986 THROUGH ACCESS 361BL WAS FOUND CORROSION SPOT. REMOVED CORROSION AT SPARS LOWER VERTICAL STABILIZER INTERNAL STRUCTURE LH SIDE UPPER AREA NEAR STA 1986 ACCESDR 9WGA2025063054518Spar · corrodedDURING HEAVY CHECK SPARS LOWER VERTICAL STABILIZER INTERNAL STRUCTURE LOWER SECTION BETWEEN STA 1927 AND STA 2486 ACCESS PANEL 361BL SUPPORT PLATE WAS FOUND WITH CORROSION SPOTS. REMOVED CORROSION AT SPARS LOWER VERTICAL STABILIZER INTERNAL STRUCTURE LOWER SESDR IPXA2025052788839Bottle · low pressureL1 DOOR ASSIST BOTTLE PRESSURE BELOW GREEN BAND. L1 DOOR ASSIST BOTTLE SERVICED PER AMM 12-25-04-600-801.SDR 9WGA2025063054517Skin · corrodedDURING HEAVY CHECK ON HORIZONTAL STAB AFT FUSELAGE LH UPPER SIDE FOUND LIGHT CORROSION FROM STA 2007 TO STA 2163. REMOVED LITE CORROSION AT HORIZONTAL STABILIZER AFT FUSELAGE LH UPPER SIDE FROM STA 2007 TO STA 2163, MATERIAL REMOVED 0.002, ALODINED AND PRIMEDSDR FDEA202505240797Strap · out of alignmentEMPENNAGE LEFT HAND HORIZONTAL STABILIZER ASSEMBLY REQUIRED TO REPLACE LEADING EDGE PANEL #331CT PART NIMBER NLC6731-3 AS PER WORK CARD T1-5510-0377031 A P2. AT XFS = 217 - 211. E.A. #T 1-5510-T0377031 B P3 TITLE: STABILIZERS HORIZON STABILIZER LH HOSDR FDEA202505210779Battery · inoperativeCHECK FOUND LH DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST SWITCH LT INOP. RELEASED FOR SERVICE PER MEL : 25-61-02 REPLACED BATTERIES AT L1 DOOR SLIDE REMOTE PRESS INDICATOR, IAW MD11 AMM 25-61-04-4. OPS CHECK GOOD,SDR IPXA2025052569566Battery · inoperativeEMER LT BAT 1 LO MSG ON TEST. REVERSED DMP. REMOVED AND REPLACED L EMERGENCY POWER SUPPLY BATTERY PER AMM 33-51-01/401. OPS CHECKS GOOD. PLACARD REMOVED AC OK TO CONTINUE SERVICE.SDR IPXA2025052069566Battery · no test**SDR FILED OPEN** EMER LT BAT 1 LO MSG ON TEST. C/W.SDR FDEA202505190768Fitting · corrodedLANDING GEAR: UPON REMOVAL OF RIGHT HAND NOSE TRUNNION FITTING BUSHING, TRUNNION FITTING HOLE FOUND CORRODED. RIGHT HAND NOSE TRUNNION FITTING BUSHING BORE HOLE CORROSION REPAIR CARRIED OUT AS PER EA #1-5310-T0382646 PART 1 .TITLE : FUSELAGE - MAINFRAME - SDR FDEA202505180766Test Switch · misinstalledDURING PREFLIGHT, THE R1 PRESS TO TEST LIGHT DID NOT ILLUMINATE ON THE DOOR WHEN PRESSED. RELEASED FOR SERVICE PER MEL : 25-61-02 CATEGORY C. FOUND PUSH TO TEST SWITCH JAMMED IN TEST POSTION. REMOVED LAMP HOUSING FROM INDICATOR LAMP ASSY AND FOUND TO HAVSDR IPXA2025060641156Skin · corrodedFOUND CORROSION AT M. CABIN R/H TUNNEL AFT OF STA 1361. ACCOMPLISH REPAIR PER EO-93960-REQ1 AND VT-SAA EA 011-5730-01-B0493, REV. I/R, PRIOR TO FURTHER FLIGHT.SDR IPXA2025060501984Longeron · corrodedEXFOLIATED CORROSION AT FWD CARGO SUMP AREA STA 979-989 BL"0"/LONGERON 52.040-43, ATA 53-10. INSTALLED 2 EA LONGERON SECTION, 3 EA LONGERON SPLICE AND 1 EA DRAIN AT FWD CARGO SUMP AREA STA 969.6 TO STA 1009.5 IAW E.A.# 011-5310-01-B0490 P3 STEP 12. ACCOMPLISHSDR IPXA2025052303083Support · damagedFWD CARGO/CEILING PANEL SUPPORT IS DAMAGED AT STA 987/RBL107.MARKED 040-39, ATA 51-00.INSTALLED REPAIR ANGLE, INSTALLED FASTENERS IN NET TO CLEARENCE FIT HOLES, FILL REAMED HOLE WITH PR1422 SEALANT, AND INSTALLED CLIP NUT AT FWD CARGO/CEILING PANEL SUPPORT STASDR 9WGA2025051754201Fuel Sys · leakingAIRCRAFT IS AOG IN OST DUE TO RUNNING FUEL LEAK ON LEFT WING AROUND REAR SPAR, 5-INCH CRACK WAS DETECTED WITHIN TANK APPROXIMATELY STA. XORS 740, AT THE BASE OF THE REAR SPAR AND 1.5 INCH EXFOLIATION AREA, BOEING HAS BEEN CONTACTED. PER BOEING WGA HAS PERFORMESDR IPXA2025051507172Skin · damaged*** SDR FILED OPEN *** DAMAGE TO TOP PORTION OF R1 DOOR. COMPLETED TRIM OUT OF DAMAGE AT R1 OUTER SKIN UPPER EDGE. TRIM OUT MEASURES 2.4 X .550. DAMAGE TO BE DEFERRED IAW EO-93750-REQ1. DEFER FOR 45 DAYS WITH 15 DAY REINSPECT.SDR IPXA2025060884755Rib · crackedRH FIXED LE HAS A CRACK AT #3 RIB O/B OF #12 SLAT TRACK. INSTALLED 1EA RIB AT O/B OF #12 SLAT TRACK IN RH WING FIXED L/E COMPARTMENT AT STA XOS=794 REF. MD-11 SRM 51-33-01-0G-0 AND SRM 51-35-01-0G-0.SDR IPXA2025060864761Frame · corrodedCORROSION ON FRAME INSIDE FWD AVI BAY BETWEEN STA Y440 TO Y449 IN BILGE AREA ATA53-10. NSTALLED ALL REPAIR PARTS -1 FRAME SECTION, 2EA -2 SPLICE ANGLES, 2EA -3 SPLICE ANGLES, 2EA INTERCOSTALS, 2EA STRAPS, 2EA INTERCOSTAL CLIPS AND 2EA INTERCOSTAL ANGLES REF. ESDR IPXA2025051315997Evas Unit · failedCAPTAINS EVAS OPS CHECK FAILED. BLOWER DOES NOT RUN. REMOVED AND REPLACED CAPTAINS EVAS PER AMM 25-69-00. OPS CHECK GOOD.SDR IPXA2025051215997Evas Unit · no testCAPTAINS EVAS OPS CHECK FAILED. BLOWER DOES NOT RUN. REMOVED AND REPLACED CAPTAINS EVAS PER AMM 25-69-00. OPS CHECK GOOD.SDR 9WGA2025081854625Angle · crackedDURING HEAVY MAINTENANCE ANGLE BELOW FWD RH PATIO FLOOR HAS A CRACK. FABRICATED AND INSTALLED ANGLE STIFFENER AT PATIO FLOOR BELOW RH FWD IAW MD-11 SRM 51-31-10 AND DRAWING AKC7546. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025091854653Bolt · corrodedDURING HEAVY MAINTENANCE CORROSION FOUND ON LH OB ELEVATOR ACTUATOR MOUNT BOLT SURFACE ON INNER REAR SPAR AT STA. XE 198.SDR 9WGA2025062054624Bolt · corrodedDURING HEAVY MAINTENANCE CORROSION FOUND ON L/H O/B ELEVATOR ACTUATOR MOUNT BOLT SURFACE ON INNER REAR SPAR AT STA. XE 198.SDR 9WGA2025072354522Pushrod · corrodedDURING HEAVT CHECK RH INBD/OUTBD ELEVATOR PUSH RODS HAVE CORROSION AS MARKED (REPLACE AS REQUIRED) (PUSH RODS OF ACTUATORS). MAINTENANCE REMOVED AND REPLACED RODS ON RH IB OB ELEVATOR PUSH RODS IAW MD-11 AMM 55-20-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SDR 9WGA2025072354521Hinge · corrodedDURING HEAVY CHECK RH OUTBD ELEV DETACHABLE HING HAS HARDWARE WITH CORROSION. MAINTENANCE REMOVED AND REPLACED NUTPLATE RH OUTBD ELEV IAW MD-11F SRM 51-31-01-06-0 (HINGE). THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025072354520Pushrod · corrodedDURING HEAVY CHECK RH INBD /OUTB ELEVATOR PUSH RODS HAVE CORROSION AS MARKED (REPLACE AS REQUIRED) (PUSH RODS OF ACTUATORS).SDR 9WGA2025062054516Hinge · wornDURING HEAVY CHECK R/H ELEVATOR HINGE PANELS 346HB, 346FB, 346DB, 346BB, 345FB BARE COMPOSITE MATERIAL. REPAIRED HINGE PANELS # 346HB, 346FB, 346BD, 346BB, 345FB AND 345DB AT R/H ELEVATOR HINGE IAW MD-11 SRM 51-62-01-06-0 PRIMED AND TOP COATED PANEL IAW MD-11SDR 9WGA2025061754513Hinge · roughDURING HEAVY CHECK RH OUTBD ELEV HINGE DAMONER HAS ROUGH MATERIAL (EVALUATE IF WITHIN LIMITS). REMOVED ROUGH MATERIAL AT RH OUTBOARD ELEVATOR HINGE DAMPER MATERIAL. REMOVED 0.001 IAW MD-11 SRM 51-21-01-06-0, ALODINED AND PRIMED AREA IAW MD-11 SRM 51-21-01-06SDR 9WGA2025061754512Rib · corrodedDURING HEAVY CHECK RH OUTB ELEVATOR FOUND CORROSION ON RIB INSTL BEHIND ACCESS PANEL 346BZ. CLEANED CORROSION AT RH OB ELEVATOR BEHIND ACCESS PANEL 346BZ, MATERIAL REMOVED 0.002, ALODINED AND PRIMED AREA IAW MD-11 SRM 51-21-01-06-0. THE AIRCRAFT WAS APPROVEDSDR 9WGA2025061754511Paint · wornDURING HEAVY CHECK RH LE INBOARD ELEVATOR PAINT/PRIMER LAYERS ARE WORN (BARE MATERIAL). RH LE IB ELEVATOR WAS PAINTED IAW MD11F SRM 51-21-02-06-0. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025061354510Rod · looseDURING HEAVY CHECK R/H INBOARD ELEVATOR ROD IS LOOSE. RESECURED HARDWARE R/H INBOARD ELEVATOR ROD IAW MD-11 AMM 20-50-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025070154520Support · crackedDURING HEAVY CHECK MAINTENANCE LT FLAP HINGE SUPPORT WAS FOUND TO BE CRACKED. LT OTBD FLAP HINGE BRACKET ASSY WAS REMOVED AND REPLACED IAW MD-11 AMM 57-53-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025070154519Support · crackedDURING HEAVY MAINTENANCE LH FLAP HINGE SUPPORT WAS FOUND CRACKED.SDR 9WGA2025062054515Thrust Reverser · delaminatedDURING HEAVY CHECK ENGINE #3 THRUST REVERSER INBOARD FIXED STRUCTURE (COWL-ASSY) DELAMINATED. REPAIRED AREA AT ENGINE #3 THRUST REVERSER I/B FIXED STRUCTURE IAW MD-11 SRM 51-62-01-06-0. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025062054514Cowling · corrodedDURING HEAVY MAINTENANCE ENGINE #3 THRUST REVERSER OUTBOARD FIXED STRUCTURE (COWL-ASSY) DELAMINATED. REPAIRED AREA AT ENGINE #3 THRUST REVERSER O/B FIXED STRUCTURE (COWL-ASSY) IAW MD-11 SRM 51-62-01-06-0. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
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