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 FDEA202205121184Stringer · noneEXISTING REPAIR FOUND AT RIGHT HAND WING STRINGER END 9 (UPPER) XORS 819. EXISTING REPAIR AT RIGHT HAND WING STRINGER END 9 (UPPER) XORS 819 EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 57-00-03-2R REPAIR 3 FIGURE 201 . WING STRINGER END 9 CARMay 12, 2022 · N605FE · Doug MD11F · Wing Main, Frame StructureSDR IPXA2022052882601Stiffener · corrodedINSPECTION TYPE:3CAFT BODY BULK HEAD HAS A HORISONTAL STIFFENER THAT HAS CORROSION AT STA Y=2163.685.REMOVED, FAB AND REPLACED THE CORRODED STIFFENER IAW DWG AJC7001 AND SRM 51-33-01 (MINOR)May 11, 2022 · N257UP · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA202205111178Rib · crackedRIGHT WING - NUMBER 6 LEADING EDGE SLAT INNER RIB FOUND CRACK AT STATION XOS 858.175. RIGHT HAND WING - NUMBER 6 LEADING EDGE SLAT INNER RIB AT STATION XOS 858.175 REPAIR CARRIED OUT AS PER E.A. # 1-5750-T0368508 P1 TITLE: WINGS Ï¿½ FLIGHT SURFACES Ï¿½ RMay 11, 2022 · N605FE · Doug MD11F · Wing, Control SurfacesSDR IPXA2022051182000Battery Pack · dischargedEMER LT BAT LO1. REPLACED EMER PWR SUPPLY BATTERY. SYS OPS NORMAL REF AMM 33-51-01.May 11, 2022 · N262UP · Doug MD11F · Emergency LightingSDR FDEA202205111177Longeron · corrodedLOWER CENTER CARGO COMPARTMENT BILGE AREA BETWEEN STATION 5 - 113 TO STATION 1541 LEFT HAND LONGERON LEFT 49 FOUND CORROSION.May 11, 2022 · N605FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2022053182679Angle · crackedINSPECTION TYPE:3CCENTER WING BOX STRINGER 47 SPLICE REPAIR Z ANGLE CRACK BETWEEN STA. XCW=17.00 & XCW=-17.00REMOVED,FABRICATED AND REPLACED CRACKED Z ANGLE BETWEEN STA. XCW=17.00 & XCW=-17.00 IAW SRM 57-10-03 REPAIR 1 FIG 201,REV 68.01 (MAJOR).May 9, 2022 · N257UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2022052882602Stringer · crackedINSPECTION TYPE:3CUPPER CTR AUXILIARY TANK STRINGER 46 IS CRACKED AT STA XCW=17.00REMOVED,FAB,REPAIRED THE CRACKED STRINGER 46 AT STA XCW=17.00 IAW VTSAA EA 011-5730-01-A9562 REV I/R AND UPS EO MD11-5710-83696-A. FAA FORM 8100-9 SIGNED BY S.KANG (AR-605677) (May 9, 2022 · N257UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2022052782568Stringer · crackedINSPECTION TYPE:3CUPPER CTR AUXILIARY TANK STRINGER 45 AT STA X=-17 , X=-46 AND BETWEEN XCW=-6.00 AND XCW=-29.00 HAS A CRACKED.REMOVED, FAB, REPAIRED THE CRACKED STRINGER 45 AT STA X=-17,X=-46 AND BETWEEN XCW=-6.00 AND XCW=-29.00 IAW SRM 57-10-03 REPAIR 1 FIG May 9, 2022 · N257UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2022052582505Spar Web · corrodedINSPECTION TYPE:3C UPPER FWD RUDDER FRONT SPAR WEB HAS CORROSION.REMOVED, REPLACED UPPER FWD RUDDER IAW AMM 27-20-30-000-802 AND 27-20-30-400-801 (MINOR)May 9, 2022 · N257UP · Doug MD11F · Rudder StructureSDR IPXA2022051081919Door Actuator · inoperativeL1 ENTRY DOOR WILL NOT OPEN/CLOSE CONSISTENTLY.L1 ENTRY DOOR WILL NOT OPEN/CLOSE CONSISTENTLY.REMOVED AND REPLACED L1 DOOR ELECT. ACTUATOR IAW MM 52-11-01. OPS CHECK GOOD.May 9, 2022 · N273UP · Doug MD11F · Passenger/Crew DoorsSDR FDEA202205091158Spar Cap · noneEXISTING REPAIR FOUND AT RIGHT HAND WING FIXED LEADING EDGE LOWER SURFACE DOUBLER XOS 906. EXISTING REPAIR AT RIGHT HAND WING FIXED LEADING EDGE LOWER SURFACE DOUBLER XOS 906 EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH SRM 57-40-03-2R REPAIR 1 FIGUREMay 9, 2022 · N605FE · Doug MD11F · Wing SparSDR FDEA202205091157Beam · crackedCABIN - L3 DOOR #5 BEAM FROM UPPER FOUND WITH CRACK. REAMED AND REMOVED AND REPLACED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.May 9, 2022 · N605FE · Doug MD11F · Cargo/Baggage DoorsSDR FDEA202205091155Beam · crackedCABIN - R3 DOOR #1 BEAM FROM UPPER FOUND WITH CRACK. REMOVED AND REPLACED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.May 9, 2022 · N605FE · Doug MD11F · Cargo/Baggage DoorsSDR IPXA2022052882603Longeron Splice · crackedINSPECTION TYPE:3CCAC COMPARTMENT HAS A LONGERON 38R SPLICE THAT IS CRACKED AT STA 6-90.REMOVED,FAB, REPAIRED THE CRACKED LONGERON 38R SPLICE AT STA 6-90 IAW VTSAA EO 011-5330-01-A9568 REV I/R AND UPS EO MD11-5310-83794-A . FAA FORM 8100-9 SIGNED BY P.LAU (AR-May 8, 2022 · N257UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2022052582487Stiffener · crackedINSPECTION TYPE:3CR/H WING TO BODY CANTED PANEL CAP VERTICAL STIFFENER IS CRACKED AT STA. 1256.REMOVED, FABRICATED AND REPPLACED STIFFENER IAW DWG. AYB7104 AND SRM 51-33-01. (MINOR)May 8, 2022 · N257UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2022052582504Support Angle · crackedINSPECTION TYPE:3CL/H WING TO BODY SUPPORT ANGLE IS CRACKED AT STA. 5-113.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. A5A7064 AND SRM 51-33-01. (MINOR)May 8, 2022 · N257UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2022052582503Support Angle · crackedINSPECTION TYPE:3CR/H WING TO BODY SUPPORT ANGLE IS CRACKED AT STA. 1661.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. AFA7769 AND SRM 51-33-01. (MINOR)May 8, 2022 · N257UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2022052582502Support Angle · crackedINSPECTION TYPE:3CR/H WING TO BODY SUPPORT ANGLE IS CRACKED AT STA. 5-113.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. A5A7064 AND SRM 51-33-01. (MINOR)May 8, 2022 · N257UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2022052582498Support Angle · crackedINSPECTION TYPE:3CR/H WING TO BODY AREA HAS A SUPPORT ANGLE THAT IS CRACKED AT STA 1581.REMOVED,REPLACED ANGLE AT STA 1581 IAW SRM 51-31-01 (MINOR)May 8, 2022 · N257UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2022052382388Doubler · chafedINSPECTION TYPE:3CTAIL CONE HORZ. BEAM REPAIR DOUBLER HAS CHAFE DAMAGE.REMOVED, FABRICATED AND REPLACED DOUBLER IAW SRM 53-80-02 REPAIR 5. (MINOR)May 8, 2022 · N257UP · Doug MD11F · Fuselage Main, StructureSDR FDEA202205081153Windshield · crackedPDIS 614 56-10 2933 06MAY22 YYZ OPEN U RIGHT WINDSHIELD CRACKED DUE TO ARCING. TURNED OFF WINDSHIELD HEAT. STOPPED CRACKING. FACT 08MAY22 22:56 YYZ REPLACED R/H WINDSHIELD PANEL ASSY I.A.W WITH MD11 AMM 56-11-01-4-1.May 8, 2022 · N614FE · Doug MD11F · Flight Compartment WindowsSDR FDEA202205081151Seat Track · corrodedSEAT TRACK ON MAIN DECK STATION 1715 RBL 102 CORRODED BEYOND ALLOWABLE LIMITS REPAIR PER MD 11 SRM 53-00-52-2R FIG 201May 8, 2022 · N649FE · Doug MD11F · Fuselage Structure (General)SDR FDEA202205081149Check Valve · malfunctionedENROUTE HNL OVER PHX LVL 2 FUEL QTY/USED CHECK, POSSIBLE FUEL ALERT. DID A FUEL USED SUMMARY AND DETERMINED 3,000 LBS SHORT OF FUEL AND STILL DECREASING . COMPLIED WITH QRH AND ISOLATED ALL TANKS. FUEL STABILIZED 8000# LOW. WE DUMPED 6000# TO LOWER LANMay 8, 2022 · N602FE · Doug MD11F · Fuel Indicating SystemSDR FDEA202205081148Bracket · corrodedLEFT HAND FORWARD (WING) INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR HOLE BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.A. May 8, 2022 · N615FE · Doug MD11F · Wing, Control SurfacesSDR FDEA202205081147Hinge · corrodedLEFT HAND FORWARD (WING) INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR HOLE BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.AMay 8, 2022 · N615FE · Doug MD11F · Wing, Control SurfacesSDR FDEA202205081146Hinge · corrodedLEFT HAND FORWARD (WING) INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR HOLE BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM 57-44-07 AND E.AMay 8, 2022 · N615FE · Doug MD11F · Wing, Control SurfacesSDR FDEA202205081145Hinge Bracket · corrodedLEFT HAND WING - LEFT HAND FORWARD (WING) INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR HOLE BORE FOUND CORROSION. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED AS PER MD-11 CMM May 8, 2022 · N615FE · Doug MD11F · Wing, Control SurfacesSDR FDEA202205081144Doubler · crackedRIGHT HAND FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER FOUND CRACKS AT XOS 703. REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.May 8, 2022 · N605FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202205081143Doubler · crackedRIGHT HAND FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER FOUND CRACKS AT XOS 683. REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.May 8, 2022 · N605FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202205081142Doubler · crackedLEFT HAND WING FIXED LEADING EDGE COMPARTMENT XOS = 789 RIB DOUBLER FOUND CRACKS. DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. DOUBLER FABRICATED AS PER DRAWING ARB 3954 RIVISION K. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.May 8, 2022 · N605FE · Doug MD11F · Wing, Plate/SkinSDR IPXA2022052782569Spar Cap · corrodedINSPECTION TYPE:1CRT WING REAR SPAR UPPER CAP CORRODED AT XORS=960.0 AND XORS=1044.8REPAIRED CORRODED REAR SPAR UPPER CAP IAW VT-SAA EA 011-5710-01-A9573 REV I/R AND UPS EO MD11-5710-83775-A (MINOR).May 7, 2022 · N257UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2022052682544Tie Clip · brokenINSPECTION TYPE:3C#2 ENG PYLON AFT FAIRING HAS A BROKEN TEE ANGLE.REMOVED, REPLACED TEE ANGLE IAW EA-011-5450-01-A9572 I/R AND UPS EO MD11-5450-83748-A AND SRM 51-30-50. (MINOR)May 6, 2022 · N257UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2022052082305Box Beam · crackedINSPECTION TYPE:3CAFT CARGO WELD BOX ASSY. IS CRACKED AT STA. 1841 AND X=28.REMOVED, FABRICATED AND REPLACED BOX ASSY. IAW DWG. AGA7196 AND SRM 51-31-01. (MINOR)May 6, 2022 · N257UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2022052082304Stiffener · crackedINSPECTION TYPE:3CAFT CARGO VERTICAL STIFFENER IS CRACKED AT STA. 1841 AND LBL=30.REMOVED, FABRICATED AND REPLACED STIFFNER IAW DWG. AGA7170 AND SRM 51-31-01. (MINOR)May 6, 2022 · N257UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2022052082303Stiffener · crackedINSPECTION TYPE:3CAFT CARGO VERTICAL STIFFNER ANGLE IS CRACKED AT STA. 1841 LBL=31.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. AGA7170 AND SRM 51-31-01. (MINOR)May 6, 2022 · N257UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2022052382373Angle · crackedINSPECTION TYPE:3CCENTER CARGO SIDEWALL SUPPORT ANGLE IS CRACKED AT STA. 1741 L/H SIDE.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. ADA0130 AND SRM 51-35-01. (MINOR)May 6, 2022 · N257UP · Doug MD11F · Fuselage Main, StructureSDR FDEA202205061137Stringer · crackedRIGHT HAND FIXED LEADING EDGE COMPARTMENT XOS = 667 UPPER STRINGER FOUND CRACKED. RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT XOS = 667 UPPER STRINGER CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-03-2R REPAIR 2 FIGURE 202. REPAIR CLASSIFIED AS MAMay 6, 2022 · N605FE · Doug MD11F · Wing, Longeron/StringerSDR FDEA202205061135Stringer · crackedUPPER CENTER AUXILIARY TANK - STRINGER 47 LEFT HAND XCW = 46.5 FOUND CRACKS. UPPER CENTER AUXILIARY TANK - STRINGER 47 LEFT HAND XCW = 46.5 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSSIFIED AS MAJOR PER GMM 6-2-May 6, 2022 · N605FE · Doug MD11F · Fuselage Main, StructureSDR FDEA202205061134Stringer · crackedUPPER CENTER AUXILIARY TANK - STRINGER 47 RIGHT HAND XCW = - 17 FOUND CRACKS. UPPER CENTER AUXILIARY TANK - STRINGER 47 RIGHT HAND XCW = - 17 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSSIFIED AS MAJOR PER GMM 6-May 6, 2022 · N605FE · Doug MD11F · Fuselage Main, StructureSDR FDEA202205061133Stringer · crackedUPPER CENTER AUXILIARY TANK - STRINGER 52 RIGHT HAND XCW = - 46.5 FOUND CRACKS. UPPER CENTER AUXILIARY TANK - STRINGER 52 RIGHT HAND XCW = - 46.5 CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSSIFIED AS MAJOR PER GMMay 6, 2022 · N605FE · Doug MD11F · Fuselage Main, StructureSDR FDEA202205061132Stringer Clip · crackedLEFT HAND WING FIXED LEADING EDGE COMPARTMENT XOS=667 UPPER STRINGER FOUND CRACKED. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT XOS = 667 UPPER STRINGER CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-40-03-2R REPAIR 2 FIGURE 202. REPAIR CLASSIFIED AS MMay 6, 2022 · N605FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202205061131Doubler · noneEXISTING REPAIR FOUND ON RIGHT HAND WING UPPER SURFACE MAIN LANDING GEAR SUPPORT DOUBLER BETWEEN AUXILIARY SPAR AND YW 467. EXISTING REPAIR ON RIGHT HAND WING UPPER SURFACE MAIN LANDING GEAR SUPPORT DOUBLER BETWEEN AUXILIARY SPAR AND YW 467 EVALUATED AND FMay 6, 2022 · N605FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202205061130Doubler · corrodedLEFT HAND - UPPER WING MAIN LANDING GEAR SUPPORT DOUBLER SURFACE FOUND CORROSION.May 6, 2022 · N605FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202205061129Stiffener · crackedRIGHT WING FIXED LEADING EDGE XOS = 542 STIFFENER FOUND CRACKS. STIFFENER REMOVED AND REPLACED AS PER SRM 51-31-01-0G. STIFFENER FABRICATED AS PER DOUGLAS DRAWING ARB 2918 REVISION G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.May 6, 2022 · N605FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA202205061126Floorbeam · crackedCRACK FOUND APPROXIMATE 0.75" IN LENGTH AS MARKED DURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND SIDE OVERWING FLOORBEAM WEB AT UPPER FLANGES STATION 1256 , X=-107. CRACK FOUND APPROXIMATELY 0.75" IN LENGTH REPAIRED AS PER EA # 1-5310- T0368May 6, 2022 · N615FE · Doug MD11F · Fuselage Main, StructureSDR IPXA2022052782580Skin · chafedINSPECTION TYPE:3CL/H WING FIXED L/E LWR SKIN IS CHAFED BETWEEN STA XIS=328.74 AND XIS=341.555REPAIRED THE CHAFED SKIN AT STA XIS=328.74 AND XIS=341.555 IAW EA 011-5730-01-A9577 I/R AND UPS EO MD11-5730-83777-A (MINOR)May 5, 2022 · N257UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2022052582507Floor Panel · corrodedINSPECTION TYPE:3CRCB FLOOR PANEL P/N WSP0786Y501 HAS CORROSION BETWEEN STA X=-17 TO X=-27.5.REMOVED, REPLACED FLOOR PANEL P/N WSP0786Y501 IAW AMM 53-21-10-400-801 (MINOR)May 5, 2022 · N257UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2022052582506Former · crackedINSPECTION TYPE:3CL/H WING O/B L/E HAS ANGEL FORMER THAT IS CRACKED AT STA XOS STA .1183.REMOVED, REPLACED ANGLE AT STA XOS.1183 IAW SRM 51-31-01 (MINOR)May 5, 2022 · N257UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2022052082307Former · crackedINSPECTION TYPE:3CL/H WING FIXED L/E COMP. FORMER IS CRACKED AT STA. 585.REMOVED, FABRICATED AND REPLACED FORMER IAW DWG. ARB2931 AND SRM 51-31-01 & 51-33-01. (MINOR)May 5, 2022 · N257UP · Doug MD11F · Leading Edge DevicesSDR IPXA2022052082306Angle · crackedINSPECTION TYPE:3CFWD. CARGO SIDEWALL SUPPORT ANGLE IS CRACKED AT STA. 919 L/H SIDE.REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG. ADA0130 AND SRM 51-35-01.(MINOR)May 5, 2022 · N257UP · Doug MD11F · Fuselage Main, Plate/Skin
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