Boeing MD-11F

Service difficulty reports · 31,317

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'MD11F'
  ORDER BY difficulty_date DESC"

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SDR FDEA202406020763Slide Raft · failed inspREF WRI 25-60/4187 AND MEL 25-61-02,IF OHMMETER READS ZERO OR NEAR ZERO RESISTANCE, THE EVACUATION SLIDE IS INOPERATIVE; CHANGE TO MEL 52-10-03-03 MAIN ENTRY DOORS/SLIDES . REMOVED AND REPLACED THE R1 DOOR SLIDE/RAFT CONTAINER.Jun 2, 2024 · N609FE · Doug MD11F · Escape SlideSDR FDEA202406010756Lamp · failedESCAPE SLIDE BOTTLE PRESSURE LIGHT FOR 1R IS INOPERATIVE. RELEASED FOR SERVICE PER MEL : 25-61-02 CATEGORY : C. AMM: 25-61-15-5 RELAMPED WITH MS25237-368 BULBS AND REPLACED BATTS, FUNCTIONAL TEST GOOD MM 25-61-15-5 ITEM CLOSEDJun 1, 2024 · N609FE · Doug MD11F · Escape SlideSDR IPXA2024061440112Floor Support · corrodedCOURIER AREA RCB WALL FLOOR SUPPORT P/N WSP0785-501 AT STA X=7.00 FROM CL (114-26) ATA 51. REMOVED AND REPLACED FLOOR PANEL P/N WSP0785-501 PER DAC DWG WSP0785, DWG SP11530078, AND PER MD11 SRM CHAPTER 51 GUIDELINES. USE ORIGINAL PART AS SAMPLE IN ACCORDANCE WMay 31, 2024 · N292UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2024061440026Floor Support · corrodedCOURIER AREA AT THE RCB WALL FLOOR SUPPORT P/N WSP0785-501 HAS CORROSION. REMOVED AND REPLACED FLOOR PANEL P/N WSP0785-501 PER DAC DWG WSP0785, DWG SP11530078, AND IAW SRM 51 GUIDELINES. USE ORIGINAL PART AS SAMPLE IAW GMM 09-08 REV 6.May 31, 2024 · N292UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2024061442717Fitting · corrodedMAIN CARGO COMPARTMENT RCB WALL FLOOR FITTING # 5 FROM LH TO RH IS CORRODED, 51-05. REMOVED AND REPLACED FLOOR FITTING P/N WSP0750-507 PER DAC DWG WSP0750, DWG SP11250221, AND PER MD11 SRM CHAPTER 51 GUIDELINES. USE ORIGINAL PART AS SAMPLE IN ACCORDANCE WITH UMay 31, 2024 · N292UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2024062627236Attach Angle · crackedAGING FINDING - (AA023) RIGHT WING OUTBOARD FLAP INBOARD FLAP CARRIAGE HAS A CRACKED ATTACH ANGLE AT THE FORWARD SIDE. DRILLED AND INSTALLED CLIP ANGLE ON RIGHT WING OUTBOARD FLAP INBOARD FLAP CARRIAGE IAW MD-11 SRM 51-31-01-0G-0. REVIEWED.May 30, 2024 · N292UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2024062615248Attach Angle · cracked#1 PYLON UPPER RIB TO WING ATTACHEMENT HAS A CRACKED ANGLE AT STA YN 302. INSTALLED ANGLE BRACKET AT #1 PYLON UPPER RIB TO WING ATTACHEMENT STA YN 302 IN REF MD11 SRM 54-05-41-0G-0.May 30, 2024 · N292UP · Doug MD11F · Nacelle/Pylon, Attach FittingsSDR IPXA2024053012991Battery · no testEMER TEST FAIL ILLUMINATED DURING PREFLIGHT. REPLACED #1 AND #2 SHIPS BATTERIES PER MM 24-34-02/401. EMERGENCY POWER TEST SUCCESSFUL PER MM 24-24-00-700-802.May 30, 2024 · N293UP · Doug MD11F · Emergency LightingSDR IPXA2024062695457Door Frame · gougedMCD FWD DOOR FRAME HAS GOUGES UPPER & LOWER DUE TO NET WAS INSTALL INCOMING MARK MM002. INSTALLED FREME SECTION FWR SIDE LWER AREA AT MCD REF MD11 SRM 51-35-01/ 51-33-01 APPLY PAINT REF MD11 SRM 51-21-02.May 29, 2024 · N292UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2024061595522Pan · gougedMCD AFT DOOR FRAME HAS GOUGE ON UPPER SIDE DUE TO NET WAS INSTALL INCOMING MARK MM 001. ACCOMPLISHED REPAIR PER EO-90717-REQ1 REV 1 AND VT-SAA EA 011-5230-01-B0207, REV. IR.May 29, 2024 · N292UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2024061401811Stringer · crackedUPPER CENTER AUXILIARY TANK HAS CRACK ON EXISTING REPAIR LOCATED BETWEEN STA X17 AND X46/STR52. (015-81). ACCOMPLISHED REPAIR PER EO-90710-REQ1 AND VT-SAA EA 011-5710-01-B0212,REV. I/R ,PRIOR TO FURTHER FLIGHT.May 29, 2024 · N292UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2024061401648Stringer · crackedUPPER CENTER AUXILIARY TANK HAS CRACK ON EXISTING REPAIR LOCATED BETWEEN STA X17 AND X-17/STR48. (015-79). ACCOMPLISHED REPAIR PER MD11 SRM 57-10-03-2R-1, REPAIR 1 (REV 70).May 29, 2024 · N292UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2024061401870Stringer · crackedUPPER CENTER AUXILIARY TANK HAS CRACK ON EXISTING REPAIR LOCATED BETWEEN STA X17 AND X46/STR48. (015-83) ATA 57. ACCOMPLISHED REPAIR PER MD11 SRM 57-10-03-2R-1, REPAIR 1 (REV 70).May 29, 2024 · N292UP · Doug MD11F · Fuel StorageSDR IPXA2024061401854Stringer · crackedUPPER CENTER AUXILIARY TANK HAS CRACK ON EXISTING REPAIR LOCATED BETWEEN STA X17 AND X46/STR49. (015-82) ATA 57. ACCOMPLISH MD11 SRM 57-10-03-2R-1, REPAIR 1 (REV 70).May 29, 2024 · N292UP · Doug MD11F · Fuel StorageSDR FDEA202405290755Slide · no testESCAPE SLIDE BOTTLE PRESSURE LIGHT FOR 1R IS INOPERATIVE. AMM: 25-61-15-5 RELAMPED WITH MS25237-368 BULBS AND REPLACED BATTERIES, FUNCTIONAL TEST GOOD MM 25-61-15-5 ITEM CLOSEDMay 29, 2024 · N609FE · Doug MD11F · Escape SlideSDR IPXA2024053095522Door Frame · gougedMCD AFT DOOR FRAME HAS GOUGE ON UPPER SIDE DUE TO NET WAS INSTALL INCOMING MARK MM 001.May 29, 2024 · N292UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2024053095457Door Frame · gougedMCD FWD DOOR FRAME HAS GOUGES UPPER & LOWER DUE TO NET WAS INSTALL INCOMING MARK MM002.May 29, 2024 · N292UP · Doug MD11F · Cargo/Baggage DoorsSDR IPXA2024052995457Door Frame · gougedOPEN, MCD FWD DOOR FRAME HAS GOUGES UPPER & LOWER DUE TO NET WAS INSTALL INCOMING MARK MM002May 29, 2024 · N292UP · Doug MD11F · Fuselage Main, StructureSDR FDEA202405290741Floorbeam · damagedTO CARRY OUT CRACK REPAIR AS PER E.A.#: 1-5310-T0368267 P2 TITLE: FUSELAGE - MAIN FRAME - MAIN DECK CARGO OVERWING FLOOR BEAM AT STA 1256.750 CRACK REPAIR. REPAIR CARRIED OUT AS PER E.A.#: 1-5310-T0368267 A P2, TITLE: FUSELAGE - MAINFRAME - MAIN DECK CARGOMay 29, 2024 · N615FE · Doug MD11F · Fuselage Main, Floor BeamSDR FDEA202405290740Fitting · crackedRIGHT HAND MAIN LANDING GEAR DOOR LOWER UPLATCH FITTIING FOUND CRACK ( 1 EACH FORWARD SIDE) AT STATION 1433.562. RIGHT HAND MAIN LANDING GEAR DOOR LOWER UPLATCH CRACKED FITTING AT STATION 1433.562 REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-33-01-0G. FIMay 29, 2024 · N615FE · Doug MD11F · Landing Gear DoorsSDR IPXA2024062685023Support Beam · corrodedLEFT WING T/E PANEL SUPPORT BEAM HAS CORROSION JUST FWD OF I/B AILERON. INSTALLED FALSE SUPPORT TEE CAP, GUSSET, 3 ANGLES AND 1 FILLER AT LT WING T/E PANEL SUPPORT BEAM IAW SRM 57-50-02-2R-9 REPAIR 9. ACCOMPLISHED SRM 57-50-02-2R-9, REPAIR 9 (REVISION 70).May 28, 2024 · N292UP · Doug MD11F · Wing Miscellaneous StructureSDR IPXA2024062585094Support Beam · crackedLEFT WING O/B FLAP O/B HINGE PANEL SUPPORT FRAME IS CRACKED. INSTALLED REPLACEMENT SUPPORT FRAME AT L/H WING O/B FLAP O/B HINGE PANEL REF. MD-11 SRM 51-35-01-OG-0.May 28, 2024 · N292UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2024061485833Floor Support · corrodedFWD SIDE OF RCB WALL FLOOR PANEL # WSP0786-501 HAS CORROSION BETWEEN FITTING # 4 & 5. REMOVED AND REPLACED FLOOR FITTING P/N WSP0750-507 PER DAC DWG WSP0750, DWG SP11250221, AND PER MD11 SRM CHAPTER 51 GUIDELINES. USE ORIGINAL PART AS SAMPLE IN ACCORDANCE WITHMay 28, 2024 · N292UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2024061482250Sidewall Panel · corrodedNEED TO REMOVE RCB WALL TO ACCESS CORROSION ON LOWER SIDE OF WALL. INSTALLED RCB WALL, 18EA FITTINGS, 8EA HYDROSTATIC STRAP, 4EA SUPPORT RODS, 20EA FLOOR FITTING BOLTS, 3EA COVERS AND RCB WALL NETS 2EA IN REF TO MD11 AMM 25-59-13-400-801.May 28, 2024 · N292UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2024061860654Duct · crackedAVIONICS COMPARTMENT LH VENTILATION DUCT JOINT HAS CRACK DAMAGE. INSTALLED AVIONICS COMPARTMENT L/H VENTILATION DUCT IN REF TO MD-11 AMM 20-10-11-960-801.May 26, 2024 · N292UP · Doug MD11F · Air Distribution SystemSDR IPXA2024052860654Duct · cracked**SDR FILED OPEN** AVIONICS COMPARTMENT LH VENTILATION DUCT JOINT HAS CRACK DAMAGEMay 26, 2024 · N292UP · Doug MD11F · Air Distribution SystemSDR FDEA202405230721Doubler · chafedLOWER FORWARD CARGO COMPARTMENT DOOR CUT OUT FORWARD JAMB LOWER EDGE DOUBLER FOUND WITH CHAFE, LONGERON 38R - LONGERON 42R AT STATION 895. LOWER FORWARD CARGO COMPARTMENT DOOR CUTOUT FORWARD JAMB LOWER EDGE DOUBLER LONGERON 38R - LONGERON 42R AT STATION 89May 23, 2024 · N615FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA202405230720Skin · chafedLOWER FORWARD CARGO COMPARTMENT DOOR CUT OUT AFT JAMB LOWER EDGE DOUBLER FOUND WITH CHAFE, STATION 1002.3,LONGERON 39-42 RIGHT HAND SIDE. LOWER FORWARD CARGO COMPARTMENT DOOR CUTOUT AFT JAMB LOWER EDGE DOUBLER WORK ACCOMPLISHED AS PER EA # 1-5330-T0308423CMay 23, 2024 · N615FE · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2024062699862Seat Track · crackedMAIN CABIN SEAT TRACK IS CRACKED AT STA 1168 RBL 8.0 ATA 53. INSTALLED 1EA SEAT TRACK SECTION AND 1 EA SPLICE REPAIR AT MAIN CABIN STA 1168 RBL 8.0 PER REF MD-11 SRM 53-00-52-2R-1. APPLIED CIC ON SEAT TRACK SECTION AT MAIN CABIN STA 1168 RBL 8.08 PER REF EO# EMay 22, 2024 · N292UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2024062206514Spar Cap · unknownLEFT OUTER WING SKIN AND REAR LOWER CAP AT XORS=420.375 REQUIRES PERMANENT REPAIR. PER TASK CARD LINE # 684. ACCOMPLISHED EO-90563-REQ1 (VT-SAA EA 011-5720-01-B0205 REV. IR).May 22, 2024 · N292UP · Doug MD11F · Wing SparSDR IPXA2024052997178Door · out of positionDOOR L-1 DOES NOT COMPLETELY SEAL WHEN CLOSED. TOP FRAME HAS 1/2 - 3/4€? GAP IN PERIMETER OF THE SEAL/EDGE. W/REF TO AMM 52-11-02 L1 PLUG DOOR PUSHES AGAINST STOPS WHEN PRESSURIZED UNDER FAIR WITHIN LIMITS DURING PRESSURIZATION. NO RECENT SYSTEM HISTORY NOR AMay 22, 2024 · N293UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2024052310468Solenoid · faultedL1 DOOR WILL NOT CLOSE OR OPEN (INTERMITTENTLY) REMOVED AND REPLACED L1 DOOR LOCK PIN RELEASE SOLENOID S2-730 PER MD11 WDM 52-11-01, MD11 SWPM 20-20-03, AND MD11 AMM 20-50-02/201. OPS CHECK GOOD. THIS CLEARS DEFERRAL. PLACARD REMOVED.May 22, 2024 · N278UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2024052297178Door · out of alignment**SDR FILED OPEN**DOOR L-1 DOES NOT COMPLETELY SEAL WHEN CLOSED. TOP FRAME HAS 1/2 - 3/4€? GAP IN PERIMETER OF THE SEAL/EDGE.May 22, 2024 · N293UP · Doug MD11F · Passenger/Crew DoorsSDR FDEA202405210709Trunnion · damagedLANDING GEAR: WHILE ACCOMPLISHING RIGHT HAND NOSE LANDING GEAR TRUNNION FITTING REPAIR, TRIMMED OUT CRACKED AREA, FOUND STATION 595 LONGERON CRACKED. LANDING GEAR: RIGHT HAND NOSE LANDIING GEAR TRUNNION FITTING AREA CRACKED LONGERON REMOVED AND REPLACED INMay 21, 2024 · N615FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR IPXA2024051842150Battery · no testDURING PDC, FOUND "EMER LT BAT 1 LO" WHEN TESTING EMERGENCY LIGHTING SYSTEM. REVERSED DMP. R/R EMERGENCY POWER SUPPLY BATTERY REF MM 33-51-01. OPS CK OK. DEFERRAL CLEARED, PLACARD REMOVED.May 18, 2024 · N275UP · Doug MD11F · Emergency LightingSDR FDEA202405170680Hydraulic Line · failedBOS - HYDRAULIC SYS 3 FAILURE PASSING DURING CLIMB OUT. RESERVOIR LEVEL DEPLETED TO ZERO. FOUND SLAT SYSTEM HYDRAULIC LINE LEAKING FLUID. MADE A CUT APROX 3 FT INBOARD AND 3 FT OTBD FROM CENTER OF PYLON. INSTALLED 6 FT LONG FLEX LINE MADE OF THREE 2 FT LONMay 17, 2024 · N582FE · Doug MD11F · Hydraulic System, MainSDR FDEA202405140666Actuator · crackedAPPROX 2 MIN AFTER GEAR RETRACTION, LEVEL 2 HYD 3 FAIL CAUTION. TURNED BACK TOWARDS MEMPHIS AND PROCEEDED WITH QRH FOR HYD 3 FAIL. NOSE GEAR SHOWED UNSAFE, AFTER DISCUSSION WITH MOC, FLEET CAPTAIN, AND TECH PILOT A LOW APPROACH WAS CONDUCTED TO VERIFY NOSMay 14, 2024 · N596FE · Doug MD11F · Nose/Tail Landing GearSDR FDEA202405140665Frame · chafedMAIN DECK - CARGO BARRIER NET LEFT HAND SUPPORT YOKE AT STATION 535 LONGERON 24- LEFT EXISTING REPAIR OUTER ANGLE FOUND CHAFFED. MAIN DECK - AT LEFT HAND FRAME STATION 535 LONGERON 24 LEFT EXISTING REPAIR, CHAFFED OUTER REPAIR ANGLE REMOVED AND REPAIR CARRIMay 14, 2024 · N615FE · Doug MD11F · Fuselage Main, FrameSDR FDEA202405140664Frame · chafedMAIN DECK - CARGO BARRIER NET LEFT HAND SUPPORT YOKE AT STATION 535 LONGERON LONGERON 19 - LEFT EXISTING REPAIR OUTER ANGLE FOUND CHAFFED. MAIN DECK AT EXISTING REPAIR AT LEFT HAND FRAME STATION 535 LONGERON 19 LEFT CHAFED OUTER REPAIR ANGLE REMOVED AND REMay 14, 2024 · N615FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA202405140663Hose · leakingAT APPROX 5 HRS INTO FLIGHT, MOCC INFORMED US OF A HYD LEAK INDICATION ON #3. RAN QRH, SELECTED MANUAL ON HSC AND TURNED HYD#3 OFF. #3 HYD QUANTITY STABILIZED AT 6.1. ABOUT 3 HRS LATER MOCC REPORTED #3HYD QUANTITY OF 8.25, WITH OUR DISPLAY STILL SHOWINMay 14, 2024 · N599FE · Doug MD11F · Hydraulic System, MainSDR FDEA202405130655Seat Track · damagedCABIN - LEFT HAND SEAT TRACK AT STATION 755, X = 8.5 FOUND CROWN DAMAGED. CABIN - AT LEFT HAND SEAT TRACK STATION 755, X = 8.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TMay 13, 2024 · N615FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202405130654Doubler · crackedLEFT WING - LEADING EDGE LOWER ACCESS PANEL CUTOUT FORWARD EDGE DOUBLER AT STATION XOS 547 FOUND CRACK ABOUT 1". LEFT WING LEADING EDGE LOWER ACCESS PANEL CUTOUT FORWARD EDGE AT STATION XOS 547 CRACKED DOUBLER REMOVED AND REPLACED AS PER MD -11 SRM 51-31-0May 13, 2024 · N615FE · Doug MD11F · Wing, Plate/SkinSDR IPXA2024051311197Slat System · malfunctioned**EMERGENCY DECLARED** **ATB** DURING CLIMB, AFTER SLATS RETRACT COMMAND, THE AIRCRAFT BEGAN AN UNCOMMANDED ROLL TO THE LEFT. WAS UNABLE TO LEVEL THE WING WITH THE YOKE INPUTS. MAINTAINED AN APPROXIMATE 20* BANK UNTIL SLATS WERE RE PERFORMED FIM SLAT DISAGREE May 10, 2024 · N284UP · Doug MD11F · Leading Edge Slat Control SystemSDR FDEA202405100634Cable · brokenL1 DOOR WILL NOT CLOSE. L1 DOOR CABLE ON AFT SIDE OF DOOR IS BROKEN. INSTALLED FWD AND AFT LOWER PASSENGER DOOR DRIVE CABLES IN REF TO AMM 52-11-03-4. OPS CHECK GOOD AT THIS TIME. SEE WRI 52-10/3556 FOR SLIDING CEILING PANEL INSTALLATION. SEE WRI 12-10/3562May 10, 2024 · N624FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA202405090630Warning Message · illuminatedON PREFLIGHT LEVEL 1 EMER LT BAT 1 LO. REPLACED EMERGENCY LIGHTING POWER SUPPLY BATTERY. OPS CHK SATISFACTORY.A/C OK FOR SERVICEMay 9, 2024 · N522FE · Doug MD11F · Emergency LightingSDR FDEA202405090629Floor Support · crackedCABIN - STATION 1887, X = 57.5 FLOOR SUPPORT APPROXIMATELY OF 1.50 INCH FOUND CRACK. CABIN - CRACKED FLOOR SUPPORT AT STATION 1887, X = 57.5 REMOVED AND REPLACED FROM STATION 1887 TO STATION 2007, X = 57.5 AS PER MD-11 SRM 51-31-01-0G. FLOOR SUPPORT FABRICMay 9, 2024 · N615FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA202405090628Floor Support · crackedCABIN - STATION 1887, X = 24 FLOOR SUPPORT APPROXIMATELY OF 1.50 INCH FOUND CRACK. CABIN AT STATION 1887, X = 24 CRACKED FLOOR SUPPORT REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G AT STATION 1887 TO STATION 2007, X = 24. FLOOR SUPPORT FABRICATED BY MAMay 9, 2024 · N615FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA202405090627Floor Support · crackedCABIN - STATION 1887, X - 2 FLOOR SUPPORT APPROXIMATELY OF 1.25 INCH FOUND CRACK. CABIN AT STATION 1887, X = - 2 CRACKED FLOOR SUPPORT REMOVED AND REPLACED AT STATION 1887 TO STATION 2007, X = - 2 AS PER MD-11 SRM 51-31-01-0G. FLOOR SUPPORT FABRICATED BY MMay 9, 2024 · N615FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA202405090626Floor Support · crackedCABIN - STATION 1887, X = 2 FLOOR SUPPORT APPROXIMATELY OF 1.5 INCH FOUND CRACK. CABIN AT STATION 1887, X = 2 CRACKED FLOOR SUPPORT REMOVED AND REPLACED FROM STATION 1887 TO STATION 2007, X = 2 AS PER MD-11 SRM 51-31-01-0G. FLOOR SUPPORT FABRICATED BY MACHMay 9, 2024 · N615FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA202405090625Cargo Track · damagedCABIN - MAIN DECK CARGO COMPARTMENT, SEAT TRACK AT STATION 5-10, X = 47.5 FOUND CROWN DAMAGED. CABIN - MAIN DECK CARGO COMPARTMENT, AT SEAT TRACK STATION 5-10, X = 47.5 DAMAGED CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 10May 9, 2024 · N615FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
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