Boeing MD-11F

Service difficulty reports · 31,320

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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 IPXA2018080652449Skin · crackedTHE LEFT WING FIXED L/E LOWER SKIN WAS CRACKED AT XOS 776. REPAIRED THE SKIN IAW SRM 57-40-02, REPAIR 7, FIG 201. MAJOR.Jul 26, 2018 · N290UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2018072732078Bottle · low pressureRT CABIN DOOR SLIDE BOTTLE PRESSURE READS ZERO. PLACARDED R2 DOOR INOP PER MEL 52-10-3-1-2-1. SERVICED EMERGENCY BOTTLE REF MM 12-25-04, OK FOR SERVICE.Jul 26, 2018 · N286UP · Doug MD11F · Escape SlideSDR IPXA2018081032632Stiffener · crackedLOWER STIFFENER IN THE RT MLG WW, BEHIND THE NR 3 HYDRAULIC RESERVOIR WAS CRACKED. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-31-01, AND SRM 51-33-01.Jul 25, 2018 · N290UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2018081032592Door Frame · crackedCENTER LANDING GEAR DOOR LOWER FWD CORNER WAS CRACKED. REMOVED AND REPLACED CENTER GEAR DOOR FWD LOWER FRAME IAW SRM 51-35-02.Jul 25, 2018 · N290UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2018080832581Web · crackedRT OVERWING UPPER FUEL TANK AFT WEB WAS CRACKED, BS 1372, RBL 80. REPAIRED THE WEB IAW EO MD11-5710-69412-A. MAJOR.Jul 25, 2018 · N290UP · Doug MD11F · Fuselage Miscellaneous StructureSDR SRXR201807250009Housing · chafedNR 2 LT TR FWD FRAME ACTUATOR HOUSING SUPPORT BRACKET IS CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER ON NR 2 LT TR FWD FRAME LOWER BALLSCREW ACTUATOR HOUSING PER CMM 78-32-02 REPAIR 16.Jul 25, 2018 · N412SN · Doug MD11F · Engine Thrust ReverserSDR SRXR201807250007Doubler · chafedFWD TAIL CONE IS CHAFED ON DOUBLER AT AFT TAI CONE. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER AT FWD TAIL CONE PER SRM 53-00-00 FIG 204.Jul 25, 2018 · N412SN · Doug MD11F · Aerodynamic FairingsSDR SRXR201807250006Doubler · gougedAFT TAILCONE FWD LH SIDE OF FRAME DOUBLER IS GOUGED. REMOVED, FABRICATED AND INSTALLED NEW ANGLE REPAIR PER SRM 53-00-00 FIG 210.Jul 25, 2018 · N412SN · Doug MD11F · Aerodynamic FairingsSDR SRXR201807250005Housing · crackedNR 2 ENG RT TR FWD FRAME LOWER BALLSCREW ACTUATOR HOUSING SUPPORT BRACKET IS CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER ON NR 2 RT TR FWD LOWER FRAME HOUSING PER CMM 78-32-02 REPAIR 16.Jul 25, 2018 · N412SN · Doug MD11F · Engine Thrust ReverserSDR SRXR201807250004Web · crackedAFT TAILCONE LT FWD FLOOR FRAME WEB IS CRACKED. REMOVED DAMAGED, FABRICATED AND INSTALLED REPAIR DOUBLER ON AFT TAILCONE LT FWD FLOOR FRAME WEB PER SRM 53-80-02 AND DWG AKC7602.Jul 25, 2018 · N412SN · Doug MD11F · Aerodynamic FairingsSDR IPXA2018081332767Cover · damagedRIGHT INBD ELEVATOR INBD UPPER L/E COVER PANEL DAMAGED. REPAIRED THE ELEVATOR COVER PANEL IAW EA 011-5520-01-A7405, REV IR, AND EO MD11-5520-69534-A.Jul 24, 2018 · N290UP · Doug MD11F · Elevator, Plate/SkinSDR FDEA201807221661Support · corrodedLT WING MLG SUPPORT ASSY P/N ARB7118 LOWER PAD HAS PITTING CORROSION. REMOVED CORROSION PER SRM 57-20-14-2R REPAIR 4(B).Jul 22, 2018 · N594FE · Doug MD11F · Wing, Landing Gear Attach FittingsSDR FDEA201807221660Support · corrodedLT WING MLG SUPPORT ASSY P/N ARB7118 UPPER PAD HAS PITTING CORROSION. REMOVED CORROSION PER SRM 57-20-14-2R REPAIR 4(B).Jul 22, 2018 · N594FE · Doug MD11F · Wing, Landing Gear Attach FittingsSDR FDEA201807221659Support · corrodedLT MLG RETRACT ACT. ATTACH SUPPORT (A) FRAME A/C ATTACH HOLES ARE CORODED REAMED TWO LOWER MOUNTING HOLES AND ONE UPPER FWD HOLE TO 1.064 DIA. REAMED ONE UPPER AFT MOUNTING HOLE TO 1.068 DIA. PER SRM 57-20-14-2R REPAIR 2.Jul 22, 2018 · N594FE · Doug MD11F · Wing, Landing Gear Attach FittingsSDR FDEA201807221805Light · inoperativeSLIDE BOTTLE TEST LIGHT INOP ON L1 DOOR. R&R BULBS ON SLIDE BOTTLE TEST LIGHT ON L1 DOOR & OPS CHECKED GOOD REF AMM 25-61-04-4.Jul 22, 2018 · N603FE · Doug MD11F · Escape SlideSDR FDEA201807221804Support · corrodedLT WING MLG SUPPORT ASSY P/N ARB7118 LOWER PAD HAS PITTING CORROSION. REMOVED CORROSION PER SRM 57-20-14-2R REPAIR 4(B).Jul 22, 2018 · N594FE · Doug MD11F · Wing, Landing Gear Attach FittingsSDR FDEA201807221803Support · corrodedLT WING MLG SUPPORT ASSY P/N ARB7118 UPPER PAD HAS PITTING CORROSION. REMOVED CORROSION PER SRM 57-20-14-2R REPAIR 4(B).Jul 22, 2018 · N594FE · Doug MD11F · Wing, Landing Gear Attach FittingsSDR FDEA201807221802Support · corrodedLT MLG RETRACT ACT ATTACH SUPPORT (A) FRAME A/C ATTACH HOLES ARE CORRODED. REAMED TWO LOWER MOUNTING HOLES AND ONE UPPER FWD HOLE TO 1.064 DIA. REAMED 1 UPPER AFT MOUNTING HOLE TO 1.068 DIA PER SRM 57-20-14-2R REPAIR 2.Jul 22, 2018 · N594FE · Doug MD11F · Wing, Landing Gear Attach FittingsSDR IPXA2018072331979Battery Pack · dischargedEMERGENCY POWER LIGHTS DO NOT WORK OR TEST DURING SHUTDOWN. T/S PER AWD 33-51-01, REMOVED AND REPLACED U1 1756 BATERY PACK AND RELAY R2-5700 PER AMM 33-51-01/ 487. SYSTEM CKS OK FOR SVC REF: 33-51-10-01 ITEM 005J.Jul 22, 2018 · N295UP · Doug MD11F · Emergency LightingSDR FDEA201807211799Support · corrodedLT NR 1 SPOILER ACTUATOR LOWER HINGE I/B BUSHING HOLE SPOT FACE FOUND WITH CORROSION. CORROSION AT LT NR 1 SPOILER ACTUATOR LOWER HINGE I/B BUSHING HOLE SPOT FACE REWORKED AS PER SRM 51-21-01-0G. EXISTING THICKNESS: 0.406", MATERIAL REMOVED I/B FACE: 0.041" , Jul 21, 2018 · N605FE · Doug MD11F · SpoilersSDR FDEA201807211798Support · excess playLT WING NR 1 SPOILER ACTUATOR FOUND LOWER HINGE FREE PLAY. LT NR 1 SPOILER ACTUATOR LOWER HINGE I/B AND O/B HOLES REWORKED AS PER SRM 51-21-01-0G. I/B HOLE EXISTING HOLE DIA 0.954"-0.970", FINAL HOLE DIA 1.069", O/B HOLE EXISTING HOLE DIA 1.500"-1.505", FINALJul 21, 2018 · N605FE · Doug MD11F · SpoilersSDR FDEA201807211797Support · corrodedRT NR 1 SPOILER ACTUATOR LOWER HINGE I/B BUSHING HOLE SPOT FACE FOUND WITH CORROSION. CORROSION AT RT NR 1 SPOILER ACTUATOR LOWER HINGE I/B BUSHING HOLE SPOT FACE REWORKED AS PER SRM 51-21-01-0G. EXISTING THICKNESS: 0.406", MATERIAL REMOVED I/B FACE: 0.035", OJul 21, 2018 · N605FE · Doug MD11F · SpoilersSDR FDEA201807211796Support · excess playRT NR 1 SPOILER LOWER HINGE FOUND FREE PLAY. RT NR 1 SPOILER LOWER HINGE HOLE REWORKED AS PER SRM 51-21-01-0G. EXISTING HOLE DIA 0.954"-0.964", FINAL HOLE DIA 1.069", REPAIR BUSHING 01 EA FABRICATED AND INSTALLED AS PER EA 1-5750-T0341116 PT 1 STEP 4 AND STEP Jul 21, 2018 · N605FE · Doug MD11F · SpoilersSDR SRXR201807210003Doubler · crackedLT WING L/E BEADED DOUBLER IS CRACKED IN 2 PLACES AT XOS 695. ACCOMPLISHED REPAIR AT LT WING L/E BEADED DOUBLER AT STA XOS 695 PER SRM 57040-02 REPAIR 15 REF NRC A042990.Jul 21, 2018 · N412SN · Doug MD11F · Wing, Plate/SkinSDR FDEA201807201809Frame · corrodedLEFT MLG 'A' FRAME HAS RUST BY TOP AFT MOUNT BOLT REMOVED AND REPLACED PER DWG.Jul 20, 2018 · N594FE · Doug MD11F · Main Landing GearSDR FDEA201807201791Doubler · corrodedLT WING FOUND UNDERWING LOWER FRONT SPAR DOUBLER AT STA XOS 1198.587 JUST AFT OF NR 8 SLAT CAVITY, WITH CORROSION AS MARKED. LT WING LOWER FRONT SPAR DOUBLER AT STA XOS 1198.587 AFT OF NR 8 SLAT CAVITY CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAIJul 20, 2018 · N582FE · Doug MD11F · Wing SparSDR FDEA201807241788Hinge Bracket · corrodedRT O/B FLAP FWD HINGE (WING SIDE) ACTUATOR O/B HOLE BORE FOUND WITH CORROSION. HINGE ACTUATOR O/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.250", FINAL HOLE DIA 1.253", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHIJul 20, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR IPXA2018072031899Light · inoperativeRT ENTRY DOOR LIGHTING IS INOP IN BOTH DIM AND BRIGHT MODES. RELAMPED RT ENTRY DOOR CEILING LIGHT IAW AMM 33-11-12-05. CHECKS NORMAL.Jul 19, 2018 · N294UP · Doug MD11F · Flight Compartment LightingSDR IPXA2018071931865Switch · defectiveIN THE BLOCKS AT LOAD COMPLETE ATTEMPTED TO SHUT L DOOR, L1 DOOR WOULD NOT SHUT CLOSED AND STAY LOCKED. R&R L1 OUTSIDE CONT SWITCH S1-1013 REF WDM 52-11-01. OPS CK NORMAL. EFF SOURCE REF: 52-11-05-05.Jul 19, 2018 · N288UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2018071831853Light · inoperativeEMERGENCY LIGHTS INOP. FOUND THAT EMERGENCY LIGHTS WILL COME ON IN ARM POSITION AND WILL NOT TEST. ORDERED CONTROL RELAY R2-5700 AND CONTROL SWITCH $1-346. PERF T/S IAW FIM 33-51-02-00 AND OPERATIONAL TEST OF EMER LIGHT SYS IAW AMM 33-50-00-700-802. EMER LIGHTJul 18, 2018 · N296UP · Doug MD11F · Emergency LightingSDR IPXA2018081032633Bracket · crackedNR 1 UPPER PYLON OTBD WEB BRACKET, FWD OF PRECOOLER WAS CRACKED. REMOVED AND REPLACED THE BRACKET IAW SRM 51-31-01, AND 54-05-41.Jul 17, 2018 · N290UP · Doug MD11F · Nacelle/Pylon Miscellaneous StructureSDR IPXA2018071831768Light · inoperativeON PREFLIGHT LVL EMER LT BAT 1 LOW. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-51-01 MESSAGE REMAINS. DEFERRAL IAW MEL 33-50-4 DMP C/W DI LOG UPDOWN. PLACARD INSTALLED ESR 33-51-20-01Jul 17, 2018 · N296UP · Doug MD11F · Emergency LightingSDR FDEA201807171769Pipe · leakingAT APPROXIMATELY 1000' ON DEPARTURE HYD 2L & R PUMP FAULT LIGHTS ILLUMINATED FOLLOWED IMMEDIATELY BY HYD 2 FAIL LEVEL 2 ALERT AND LOSS OF ALL HYD 2 FLUID. INSPECTED NR 2 ENG CASE DRAIN FILTERS FOR LEFT AND RIGHT EDP'S FOR METAL AND OR JELLYING OF HYD FLUID. NOJul 17, 2018 · N625FE · Doug MD11F · Hydraulic System, MainSDR FDEA201807171768Warning System · activatedAFTER TAKEOFF AND DURING SLAT RETRACTION, HAD A SLAT DISAGREE WITH A ROLL TO THE RIGHT. COMPLETED FUNCTIONAL TEST OF THE RIGHT OUTBOARD SLAT RANGE OF MOVEMENT CHECKED IAW AMM 27-80-00-710-802, ALL CHECKED GOOD, OK FOR SERVICE.Jul 17, 2018 · N575FE · Doug MD11F · Leading Edge Slat Position Indicating SystemSDR FDEA201807171767Warning System · false activationTSI ISSUED FOR MX TO COMPLY WITH FOR FLAP DISAGREE. PERFORMED FLAP POSITION INDICATION SYSTEM ADJUSTMENT TEST REF AMM 27-54-00-5. NO FAULTS FOUND. ALL READINGS WITHIN TOLERANCE. VISUALLY INSPECTED LINKAGE, HARDWARE, WIRE HARNESSES AND CONNECTORS OF EACH INBOAJul 17, 2018 · N593FE · Doug MD11F · Trailing Flap Position Indicating SystemSDR FDEA201807171765Warning System · false activationAT FL 350 IN LEVEL CRUISE .82M RECEIVED FLAP DISAGREE W/FLAPS AT 0 DEGREE/RET9 INDICATING 0 DEGREE/RET ON CONFIG PAGE. UPPER AND LOWER AIRSPEED FEET CAME TOGETHER ON CA SIDE. AP1 WAS ENGAGED. FO SIDE SHOWED NORMAL. THIS OCCURRED SEVERAL TIMES INTERMITTENTLY AJul 17, 2018 · N593FE · Doug MD11F · Trailing Flap Position Indicating SystemSDR FDEA201807171764Bracket · corrodedLT O/B FLAP O/B FWD (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. IDLER BRACKET ATTACH HOLE BORE REWORKED AS PER SRM 51-21-01-0G. EXISTING HOLE DIA 1.0", FINAL HOLE DIA 1.384", LOCAL BLEND POSITION 9 O'CLOCK POSITION, L=0.25" X W= 0.25", DEPTH=0.065". I/B Jul 17, 2018 · N605FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201807171763Hinge · corrodedRT O/B FLAP O/B AFT HINGE (FLAP SIDE) PIVOT I/B HOLE BORE FOUND WITH CORROSION. AFT HINGE (FLAP SIDE) PIVOT I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. EXISTING HOLE DIA 1.148", FINAL HOLE DIA 1.182", MAXIMUM ALLOWABLE HOLE DIA 1.150". OJul 17, 2018 · N605FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201807171762Hinge · corrodedRT O/B FLAP I/B AFT HINGE PIVOT I/B HOLE BORE FOUND WITH CORROSION. AFT HINGE PIVOT I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. EXISTING HOLE DIA 1.149", FINAL HOLE DIA 1.182", MAXIMUM ALLOWABLE HOLE DIA 1.150". REPAIR BUSHING FABRICATEDJul 17, 2018 · N605FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201807171761Hinge · corrodedLT O/B FLAP I/B AFT HINGE (FLAP SIDE) I/B PIVOT HOLE BORE FOUND WITH CORROSION. CORRODED PIVOT HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. EXISTING HOLE DIA 1.124". FINAL HOLE DIA 1.182", MAXIMUM ALLOWABLE HOLE DIA 1.150". OVERSIZED BUSHING Jul 17, 2018 · N605FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201807171760Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) ACTUATOR I/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) ACTUATOR I/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.221", FINAL HOLE DIA 1.248", MAXIMUM ALLOWABLE HOLE DIA 1.2Jul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201807171759Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE FOUND WITH CORROSION. FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-09. EXISTING THICKNESS UPPER: 0.409", LOWER: 0.399", MATERIAL REMOVED UPPER: 0.013", LOWER: 0.013", REMAJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201807171758Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) LOWER BARREL NUT HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER BARREL NUT HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.389", FINAL HOLE DIA 0.406", MAXIMUM ALLOWABLE HOLEJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201807171757Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) UPPER BARREL NUT HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) UPPER BARREL NUT BORE (7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.389", FINAL HOLE DIA 0.406", MAXIMUM ALLOWABLE Jul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201807171756Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE SURFACE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING THICKNESS 0.430", MATERIAL REMOVED: 0.007", (FWD) AND 0.01Jul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201807171755Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE SURFACE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING THICKNESS: 0.435". MATERIAL REMOVED: 0.007" (FWD), 0.024" Jul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201807171754Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT O/B HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.597", FINAL HOLE DIA 0.613", MAXIMUM ALLOWABLE HOLE DJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201807171753Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) LOWER MOUNT I/B HOLE BORE (3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.596", FINAL HOLE DIA 0.613", MAXIMUM ALLOWJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201807171752Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) ACTUATOR O/B HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) UPPER MOUNT O/B HOLE BORE (2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 0.955", MAXIMUM ALLOWABLE HOLE DIA 0.944". OVERSIJul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201807171751Hinge Bracket · corrodedRT O/B FLAP O/B FWD HINGE (WING SIDE) PIVOT HOLE BORE FOUND WITH CORROSION. FWD HINGE (WING SIDE) PIVOT HOLE BORE (4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 2.312", FINAL HOLE DIA 2.316", MAXIMUM ALLOWABLE HOLE DIA 2.3135Jul 17, 2018 · N605FE · Doug MD11F · Wing, Control Surface Attach Fittings
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