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 FDEA202311191863Pseu · failedSLAT DISAG ON EXTENSION DURING APPROACH PHASE. COMPLIED WITH QRH RESULTING IN FLAP 28/SLATS RETRACT LANDING. EMERGENCY DECLARED. REPLACED PSEU PER ABOVE REFERENCE, OPS CHECKS OK. PANELS OPENED FOR ACCESS FOR SLAT LUBE. LUBRICATED INBOARD AND OTBOARD SLSDR IPXA2023112058316Unknown · unknownEMER PWR TST FAIL FOLLOWED FIM 24-30-03-00 AND PERFORMED THE OPS TEST OF THE BATTERIES IAW AMM 24-34-02. TEST OK.SDR FDEA202311181862Tire · damagedUPON TOUCHDOWN PDX RWY10R, RECEIVED LVL2 ANTI-SKID R FAIL, IMMEDIATELY FOLLOWED BY LVL2 TIRE FAIL. #7 TIRE FAIL INDICATION. SAME TIRE AS ANTI SKID SYSTEM MEL FOR THIS AIRCRAFT 32-45-01-01. REMOVED AND REPLACED #7 MAIN WHEEL/TIRE ASSEMBLY. IAW MD-11 AMM 3SDR IPXA2023112077301Unknown · unknownL 1 ENTRY DOOR CABIN DOOR SWITCH FAULTY **OII 2** REMOVED & REPLACED L1 FWD PASSENGER DOOR LOCK PIN RELEASE SOLENOID REF AMM 52-10-06 OPS CHECK GOOD PLACARD REMOVEDSDR IPXA2023112016092Unknown · unknownON CLIMB STRONG OIL BURN SMELL FILLED COCKPIT. DECLARED EMER AND RETURNED TO DFW. RAN SMOKE REMOVAL CHECKLIST PERFORMED CLEANING OF THE AIR CONDITIONING PACK AND DISTRIBUTION DUCTS FOR ODOR REF AMM 21-53-00-160-802. ODOR BEGAN TO DISSIPATE AFTER AN HOUR, FOR TSDR IPXA2023111616092Unknown · unknownATB, EMERGENCY DECLARED, ON CLIMB STRONG OIL BURN SMELL FILLED COCKPIT. DECLARED EMER AND RETURNED TO DFW. RAN SMOKE REMOVAL CHECKLIST REPLACED PACKS 1,2,3 COALESER BAGS... AWAITING RUN QUALIFIED AMT FOR BURNOUT PROCEDURESDR IPXA2023111614965Unknown · unknownLEFT ELECTRIC EXTERNAL DOOR CONTROL SWITCH INTERMITTENTLY STICKS IN UP POSITION OPERATED DOOR SWITCH MULTIPLE TIMES COULD NOT DUPLICATE FAULT SWITCH OPERATES NORMALLY AT THIS TIME REF AMM 52-11-00SDR IPXA00300Unknown · unknownR1 DOOR WOULD NOT ARM - HANDLE WOULD NOT STOW UP (ARMED) POSITION ARMING LEVER INSIDE WOULD NOT STOW ALL THE WAY, ARMING LEVER OUTSIDE WAS ALSO STICKING OUT BUT INDICATIONS SHOWED DOOR ARMED. FOUND €˜ARMED€™ FLAG WINDOW PLATE LOWER SIDE ON DOOR GETTING CAUGHSDR IPXA2023111599751Unknown · unknownCREW ENTRY DOOR (L-1) WILL NOT OPEN W/ INTERIOR OR EXTERIOR SWITCH PERFORMED OPS CK OF DOOR REF AMM 52-10-01, CKS NORMAL FROM INTERIOR AND EXTERIOR SWITCHES , THIS CLEARS DMISDR FDEA202311151854Strap · damagedDURING WALK-AROUND, MX NOTED DENTS ON THE LH HORZ STAB L/E AT APPROXIMATELY STATIONS XFS260, XFS264, XFS279. REMOVED LH HORIZONTAL STAB CENTER LEADING EDGE REF AMM 55-11-02-4. ROUTED LEADING EDGE TO SHEET METAL. FINISHED DRILLING UP STRAP AND COUNTERSUNSDR FDEA202311151853Anti-Skid Sys · failedUPON TOUCHDOWN PDX RWY10R, RECEIVED LVL2 ANTI-SKID R FAIL, IMMEDIATELY FOLLOWED BY LVL2 TIRE FAIL. #7 TIRE FAIL INDICATION. SAME TIRE AS ANTI SKID SYSTEM MEL FOR THIS AIRCRAFT 32-45-01-01. REINSTALLED AUX STRUCTURE AFT SPAR CLOSE OUT PANEL RT MLG OUTBD PERSDR IPXA2023110774176Unknown · unknownDOOR R1 SLIDE/RAFT INDICATOR LIGHT DID NOT ILLUMINATE DURING PRE-FLIGHT TEST. REMOVED AND INSTALLED R1 SLIDE/RAFT INDICATOR LIGHT ASSY. OPS CHECK GOOD. NO DEFECTS NOTED. PER AMM 25-61-04/401SDR FDEA202311071842Collar · shearedDURING PUSHBACK, FOUND RH STEERING CYLINDER'S STEERING COLLAR PIN SHEARED OFF. INSTALLED NLG RT STEERING CYLINDER COLLAR PIN, REFERED AMM 32-52-30-4. NOSE GEAR STEERING CYLINDER OPS CHECK. A/C OK FOR SERVICESDR FDEA202311061835Floor Panel · damagedMAIN CARGO - OVER WING - FLOOR BOARD - HAS DAMAGED & MISSING INSERTS - PANEL #262GF STA 1159, RBL 48. FABRICATED NEW MAIN CARGO DECK FLOOR PANEL 262GF AT STA 1159 PER FEDEX DRAWING SRZ-25-005 AND MD11 SRM 53-00-50-2R PARAGRAPH 4. STEPS E-G.SDR FDEA202311021824Floor Panel · wornMAIN CARGO- OVER WING- FLOOR BOARD- HAS DAMAGED AND MISSING INSERTS- PANEL # 271JF STA 1481 TO 5-32 LBL 75-107. FACRICATED NEW MAIN CARGO DECK FLOOR PANEL 271JF PER FEDEX DRAWING SRZ-25-005 AND MD11 SRM 53-00-50-2R PARAGRAPH 4. STEPS E-G.SDR IPXA2023110271134Unknown · unknownLEVEL ONE EMER LT BAT 1 LO R&R EMERGENCY LIGHTING BATTERY POWER SUPPLY IAW AMM 33-51-01, OPS CHECKS GOOD AT THIS TIME. DMP REVERSED PLACARD REMOVED.SDR IPXA2023110167359Unknown · unknownR1 DOOR PNEUMATIC DOOR ASSIST BOTTLE PRESSURE BELOW GREEN GAUGE. SERVICED R1 DOOR ASSIST BOTTLE AS REQ, LEAK CKS OK. REF AMM 12-25-04 THIS CLEARS DMI 2802094 DMP REVERSED.SDR IPXA2023102721121Unknown · unknown**EMERGENCY DECLARED**ANTI SKID FAIL AS PER FIM 32-40-11-00 STEP #2 RESET CB ANTI SKID CONTROL SYST 1 AND 2. ALERT DOES NOT SHOW, SYST OKSDR FDEA202310231792Floorboard · delaminatedMAIN CARGO FLOORBOARD 262NF HAS DAMAGED AND MISSING INSERTS. AFTER FURTHER INSPECTION FOUND FLOORBOARD 262DF DELAMINATED, FABRICATED FLOORBOARD REF FEDEX DWG SRZ-25-005 MAJOR REPAIR .SDR FDEA202310221787Pressure Switch · failedR1 DOOR EVAC SLIDE PRESSURE PRESS-TO-TEST INDICATING SYSTEM INOP. REMOVED AND REPLACED REMOTE PRESSURE INDICATOR ASSY. OPS GOOD OK FOR SERVICESDR FDEA202310191778Skin · crackedSKIN CRACKED AT UPPER AFT CORNER OF #3 AIR CONDITIONING COMPARTMENT DOOR CUTOUT. REPAIRED IN REF. TO ENGINEERING AUTHORIZATION: #1-5330-T0376720; PART 1. TITLE: FUSELAGE - NO. 3 RH AIR CONDITIONING DOOR JAMB SKIN FOUND WITH CRACK IN UPPER AFT CORNER-OMISSIOSDR FDEA202310191773Skin · damagedRIGHT WING - INBOARD FLAP OUTBOARD EDGE FLANGE FASTENER HOLE FOUND ELONGATED AT APPROXIMATELY STATION YIFH = 34.500. RIGHT WING - INBOARD FLAP OUTBOARD EDGE FLANGE ELONGATED FASTENER HOLE AT APPROXIMATELY STATION YIFH = 34.500 REPAIRED AS PER EA # 1-5750-TSDR IPXA2023101942411Unknown · unknownL1 DOOR SLIDE DISARMED INDICATOR LIGHT BROKEN. C/W R&R'D L1 DOOR SLIDE DISARMED INDICATOR LIGHT IAW IPC 52-11-70-01-170 & SWPM 20-20-03. PERFORMED OPERATIONAL CHECK IAW AMM TASK 52-10-01-700-801.SDR IPXA2023101838691Power Supply · faultedEMER LTS BAT 1 LO MESSAGE DURING TEST REVERSED DMP. R&R'D EMER LIGHT BATTERY POWER SUPPLY PER AMM 33-51-01. OPS CHECK GOOD. DEFERRAL CLEARED.SDR IPXA2023101700187Unknown · unknownEMERGENCY LIGHT TEST LEVEL 1 ALERT DISPLAYED €ŒEMERGENCY LT BAT 1 LO€? REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY PER AMM 33-51-01-400-802. OPS CHECK GOODSDR FDEA202310141763Float · unknownAPPROXIMATELY 3 HOURS INTO FLIGHT, FL 340, RECEIVED A LEVEL 2 FUEL QTY/USED CHK. COMPLIED WITH QRH. WHEN SYSTEM WAS SWITCHED TO MANUAL AND THE TAIL TANK WAS ISOLATED, THE TAIL TANK CONTINUED TO DECREASE 400LBS IN 4 MINUTES. SUSPECT THE FUEL LEAK WAS INSDR FDEA202310141762Doubler · corrodedRIGHT WING OUTBOARD OF MAIN LANDING GEAR ABOVE PANEL 641BB HAS CORROSION. AREA IS AROUND INBOARD SIDE OF FASTENER RETAINING RING ABOVE GROSS WEIGHT DOUBLER. PERFORMED STRAP AND FILLER REPAIR OF AREA THAT WAS BLENED REF. EA# 1-5730-T0376395 "MAJOR REPAIR"SDR IPXA2023101365995Unknown · unknownSLIDE PRESSURE GAUGE IS DIFFICULT TO READ. ADJUSTED LOWER ENTRY DOOR COVER TO GIVE BEST VIEW POSSIBLE OF BOTTLE PRESSURE GAUGE PER MD11 AMM 25-23-07-400-802. PRIMARY MEANS OF CHECKING SLIDE BOTTLE PRESSURE ON A/C 256 IS USING THE REMOTE LOW PRESSURE SWITCH. SESDR IPXA2023110758601Spar Cap · corroded*MAJOR REPAIR* RH UPPER WING REAR SPAR HAS CORROSION 13" FWD OF O/B AILERON O/B SIDE. 49-044 (STR). ACCOMPLISHED EO-88539-REQ1, AND EA#011-5710-01-B0114, REV. IR, AUDIT COMPLETESDR IPXA2023110429669Unknown · unknownRH LE COVE HAS A CRACKED BEADED DOUBLER AT FASTENER AT APPROX XOS 670. 49-033 ACCOMPLISH REPAIR TO THE RH WING FIXED LE BEADED DOUBLER BETWEEN XOS=667.6 TO XOS=673.7 PER MD11 SRM 57-40-02, REPAIR 15, REV 70. INSTALLED REPLACEMENT BEADED DOUBLER AT R/H WING LSDR IPXA2023110429401Doubler · cracked*SDR FILED OPEN* RH LE COVE HAS A CRACKED BEADED DOUBLER AT FASTENER AT APPROX XOS 613. 49-032 C/W STEP 15SDR IPXA2023110431678Doubler · crackedRH LE COVE HAS A CRACKED BEADED DOUBLER AT FASTENER AT APPROX XOS 690. 49-034 ACCOMPLISH REPAIR OF THE RH WING FIXED LE BEADED DOUBLER BETWEEN XOS=692.038 TO XOS=698.127 PER MD11 SRM 57-40-02, REPAIR 15, REV 70 AND BOEING SR ID 3-4484182131. REVIEWEDSDR FDEA202310111799Channel · corrodedCAC LOOKING FWD, FOUND CENTER LINE LONGERON 52 BELLFRAME "J" ANGLE WITH HEAVY CORROSION. (MKD) APPROX. FIVE INCHES IN LENGHT STA 1129 (6-70) LOCATION TRIMMED OUT CORRODED SECTION OF J-CHANNEL (P/N ADA0112-11) AND APPLIED FILLER AND DOUBLER REPAIR PER SRM SDR FDEA202310111747Floorboard · delaminatedMAIN CARGO FLOORBOARD 263QF HAS DAMAGED AND MISSING INSERTS. AFTER FURTHER INSPECTION FOUND FLOORBOARD 263QF DELAMINATED. FABRICATED FLOORBOARD REF FEDEX DWG SRZ-25-005 MAJOR REPAIR.SDR FDEA202310111741Vane · failedR/H WING O/B FLAP I/B HINGE, AREA ABOVE FLAP, FLAP VANE BOTTOM SIDE HAS A DEEP GOUGE WITH SCREW IMBEDDED INSIDE SKIN. REPAIRED R/H WING O/B FLAP I/B HINGE, AREA ABOVE FLAP, FLAP VANE BOTTOM SIDE GOUGE PER SRM 57-50-80-2R, PG.25-26, REPAIR INSTRUTION 4, FIGSDR FDEA202310091736Floorboard · damagedMAIN CARGO FLOORBOARD 262KF HAS DAMAGED MISSING INSERTS. AFTER CLEANING FLOORBOARD FOUND LARGE HOLE. FABRICATED FLOORBOARD 262KF REF FEDEX DWG SRZ-25-005 MAJOR REPAIR.SDR FDEA202310091732Longeron · crackedDURING ACCOPLISHMENT OF SNRM NO: N00708, HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AND FOUND ADDITIONAL 02EA CRACK APPROXIMATELY 0.25 INCH AND 0.5 INCH AS MARKED PROPAGATE FROM THE LOWER FASTENER HOLE OF LOWER INTERNAL LONGERON REVEAL BY THE TRSDR FDEA202310071716Fitting · crackedDURING INSPECTION ON THE RIGHT HAND NOSE LANDING GEAR TRUNNION FITTING AFT OF NOSE LANDING GEAR DOOR AFT HINGE FITTING SLOT OUT AREA FOUND SUSPECT CRACK AT STATION 583. RIGHT HAND NOSE LANDING GEAR TRUNNION FITTING AFT OF NOSE LANDING GEAR DOOR AFT HINGESDR FDEA202310061830Bracket · crackedRH WING, SUPPORT BRACKET P/N ARB0068-2 REQUIRES FABRICATION 0005108155 : SHERWIN, SAMUEL M - 18-OCT-2023 03:57 FABRICATED SUPPORT BRACKET P/N ARB0068-2 REF DAC DWG ARB0068, EA# 1-5710-T0376494 BUY BACK FABRICATED SUPPORT BRACKET P/N ARB0068-2 REF DAC DWG SDR IPXA2023100939811Unknown · unknownWHILE OPENING ENG #2 FAN COWL TO FOM FOUND R/H FAN COWL DELAMINATED (SEE ATTACHMENT) R+R #2 ENGINE R/H FAN COWL PER AMM 71-12-01. REFERENCE HYUNG CHOE LABOR ROW, FAN COWL WAS REPLACED. ADDED FAN COWL TO FAULT.SDR IPXA2023100656723Light · damagedL1 DOOR FEW EMERGENCY LIGHT LENS DAMAGED REMOVED AND REPLACED L1 FWD EMERGENCY LIGHT ASSY. DOCUMENT REFERENCE: AM 33 52 01SDR IPXA2023100639811Unknown · unknown*** SDR FILED OPEN *** WHILE OPENING ENG #2 FAN COWL TO FOM FOUND R/H FAN COWL DELAMINATED (SEE ATTACHMENT)SDR FDEA202310061714Stringer · crackedUPPER AUXILIARY TANK - STRINGER 47 AT STATION XCW -46 FOUND CRACK DURING PERFORMING W/C 57.20.01.3. UPPER AUXILIARY TANK - STRINGER 47 AT STATION XCW -46 REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR AS PERSDR FDEA202310061712Support · corrodedLOWER CENTER CARGO COMPARTMENT BILGE STATION 1841 X=-2 WEB LOWER SUPPORT FOUND WITH CORROSION. CORRODED LOWER SUPPORT AT WEB LOWER CENTER CARGO COMPARTMENT BILGE STATION 1841 X=-2 REMOVED FROM STATION 1841, X=-50 TO X=50 AND REPLACED WITH FABRICATED LOWESDR FDEA202310051711Longeron · corrodedLOWER CENTER CARGO COMPARTMENT BILGE STATION 5-110, LONGERON 45 LEFT HAND FLOOR BEAM FOUND WITH SURFACE CORROSION. CORROSION AT LOWER CENTER CARGO COMPARTMENT BILGE STATION 5-110, LONGERON 45 LEFT HAND REMOVED AS PER MD-11 SRM 51-21-01-0G AND FOUND OUT LISDR FDEA202310051710Longeron · corrodedLOWER CENTER CARGO COMPARTMENT BILGE STATION 5-53 LONGERON 43 RIGHT HAND FOUND WITH CORROSION. CORROSION AT LOWER CENTER CARGO COMPARTMENT BILGE STATION 5-53 LONGERON 43 RIGHT HAND FOUND OUT LIMIT AS PER MD-11 SRM 53-00-00-2R REPAIR GENERAL FIGURE 205. SDR FDEA202310041698Fitting · crackedDURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013 PER DRAWING NUMBER SN10550000 REV D ON RIGHT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION 2164, EXISEING CRACK INDICATION FOUND FROM 2SDR FDEA202310031694Bracket · corrodedRIGHT WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORRODED REWORKED AND FOUND WITHIN LIMIT IAW CMM 57-44-07.OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED IAW CMM 57-44-07 AND EA 1-5750-T0331808 A PART 2 STEP SDR FDEA202310031693Bracket · corrodedRIGHT WING WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. RIGHT WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT IAW CMM 57-44-07.OVERSIZED REPAIR BUSHING FASDR FDEA202310031692Bracket · corrodedLEFT WING WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. LEFT WING WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT IAW CMM 57-44-07. OVERSIZED REPAIR BU
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