Boeing MD-11F

Service difficulty reports · 31,317

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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"

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SDR IPXA2021061770685Doubler · crackedINSPECTION TYPE:3CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 661.71 TO 673.76.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 661.71 TO 673.76 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)May 28, 2021 · N283UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2021061770684Doubler · crackedINSPECTION TYPE:3CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED AT STA. XOS. 667.673.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER AT STA. XOS. 667.673 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)May 28, 2021 · N283UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2021061770683Doubler · crackedINSPECTION TYPE:3CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 692.038 TO 698.127.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 692.038 TO 698.127 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)May 28, 2021 · N283UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2021061170412Skin · crackedINSPECTION TYPE:3CL/H WING L/E LOWER SKIN IS CRACKED AT STA. XOS.= 490.850.REPAIRED CRACKED L/H WING FIXED L/E LOWER SKIN AT STA. XOS.=490.850 IAW SRM 57-40-01 REPAIR 17 FIG. 201. (MAJOR)May 28, 2021 · N283UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2021061170414Doubler · crackedINSPECTION TYPE:C3RH WING FIXED L/E SPLICE DOUBLER CRACK AT XOS STA.585.REMOVED,FABRICATED AND REPLACED CRACKED SPLICE DOUBLER IAW SRM 51-31-01 (MINOR).May 28, 2021 · N283UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2021062570961Structure · crackedINSPECTION TYPE:3C#1 ENGINE L/H T/R LOWER BIFURCATION ASSY STRUCTURE IS CRACKED.REPAIRED CRACKED 31 ENGINE L/H T/R LOWER BIFURCATION ASSY STRUCTURE IAW VT-SAA EA 011-7830-01-A9169 REV. IR AND UPS EO MD11-7830-80639-A. (MINOR)May 27, 2021 · N283UP · Doug MD11F · Engine Thrust ReverserSDR IPXA2021060970323Door · crackedINSPECTION TYPE:C3LT MLG DOOR EXTENSION FWD CORNER IS CRACKED.REMOVED AND REPLACED CRACKED DOOR CORNER IAW SRM 51-31-01 AND 51-35-01 (MINOR).May 27, 2021 · N283UP · Doug MD11F · Landing Gear DoorsSDR FDEA202105261407Spar Cap · crackedMDIS 612 57-30 0764 26MAY21 IND OPEN U L/H WING LOWER SPAR CAP CRACKED BETWEEN STATION XORS1043-1045 CRACKED AREA AT L/H WING OUTER REAR SPAR LOWER SPAR CAP BETWEEN STATION XORS1043- 1045 HAS BEEN REPAIRED AS PER SRM 57-20-10-2R FIG 201 REPMay 26, 2021 · N612FE · Doug MD11F · Wing SparSDR IPXA2021062570954Skin · corrodedINSPECTION TYPE:3CLT WING UPPER SKIN BETWEEN STA XORS 97 - XORS 130.40 AND BETWEEN STRINGER 11 - STRINGER 15 IS CORRODED.REPAIRED CORRODED LT WING UPPER SKIN BETWEEN STA XORS 97 - XORS 130.40 AND BETWEEN STRINGER 11 - STRINGER 15 IAW VT-SAA EA 011-5730-01-A918May 26, 2021 · N283UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2021060870303Skin · crackedINSPECTION TYPE:2CR/H I/B FLAP LOWER SKIN HAS A CRACK XIFH= 134.REPAIRED CRACKED R/H I/B FLAP LOWER SKIN BETWEEN STA. XIFH=133.9 TO 147.3 AND BETWEEN STA. YIFH= 34 TO 78 IAW SRM 57-50-01 REPAIR 1 FIG. 201. (MAJOR)May 26, 2021 · N271UP · Doug MD11F · Trailing Edge FlapsSDR FDEA202105251391Spar Cap · crackedDURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013 PER DRAWING NO. SN10550000 REVISION C ON LEFT HAND SIDE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION 2164, EXISTING CRACK INDICATION FOUND FROM May 25, 2021 · N598FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR FDEA202105251389Frame · crackedMAIN DECK CARGO COMPARTMENT-CABIN, DURING REMOVAL OF INSULATION BLANKET FOR SUPPORT BRACKET RECTIFICATION, FOUND FRAME AT STATION 5-32, LONGERON 12 LEFT CRACKED. MAIN DECK CARGO COMPARTMENT-CABIN AT LEFT HAND FRAME STATION 5-32, LONGERON 12 LEFT CRACKEDMay 25, 2021 · N598FE · Doug MD11F · Fuselage Main, FrameSDR FDEA202105251386Frame · dentedMAIN DECK CARGO COMPARTMENT-CABIN, FOUND FRAME AT STATION 1741, LONGERON 12 LEFT WITH DENT. MAIN DECK CARGO COMPARTMENT-CABIN AT LEFT HAND FRAME STATION 1741, LONGERON 12 LEFT DENT AREA REPAIRED AS PER SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPETITIVE INSPMay 25, 2021 · N598FE · Doug MD11F · Fuselage Main, FrameSDR FDEA202105251385Frame · dentedMAIN DECK CARGO COMPARTMENT-CABIN FOUND FRAME AT STATION 1761, LONGERON 12 LEFT WITH DENT MAIN DECK CARGO COMPARTMENT-CABIN AT LEFT HAND FRAME STATION 1761, LONGERON 12 LEFT DENT AREA REPAIRED AS PER SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPETITIVE INSPECMay 25, 2021 · N598FE · Doug MD11F · Fuselage Main, FrameSDR IPXA2021052569805Switch · inoperativeL1 CABIN DOOR SWITCHES ( INSIDE AND OUTSIDE) DONT WORK. THEY WORK WHEN WE ENTERED THE AIRCRAFT THEN STOPPED WORKING. DEFERRED PER MEL 52-10-3-1-2-1 PLACARD INST LOG UPDATEDPERFORMED INSP, CHECK & OPS CHECK OF L1 DOOR. OPS CHKS GOOD BOTH OUTSIDE AND INSIDE SMay 25, 2021 · N285UP · Doug MD11F · Passenger/Crew DoorsSDR FDEA202105251382Floor Panel · delaminatedFLIGHT DECK, FOUND FLOOR PANEL #216BF DELAMINATED. DELAMINATED FLOOR PANEL #216BF AT CABIN STATION 366 Ï¿½ STATION 386 REMOVED AS PER AMM 53-21-04. FLOOR PANEL #216BF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #216BF INSTALLED AS PEMay 25, 2021 · N598FE · Doug MD11F · Fuselage Floor PanelSDR FDEA202105251381Floor Panel · delaminatedFLIGHT DECK, FOUND FLOOR PANEL #215DF DELAMINATED. DELAMINATED FLOOR PANEL #215DF AT CABIN STATION 334 Ï¿½ STATION 366 REMOVED AS PER AMM 53-21-04. FLOOR PANEL #215DF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #215DF INSTALLED AS PEMay 25, 2021 · N598FE · Doug MD11F · Fuselage Floor PanelSDR FDEA202105251379Floor Panel · delaminatedFLIGHT DECK, FOUND FLOOR PANEL #217AF DELAMINATED. DELAMINATED FLOOR PANEL #217AF AT CABIN STATION 330 Ï¿½ STATION 352.5 REMOVED AS PER AMM 53-21-04. FLOOR PANEL #217AF FABRICATED AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FLOOR PANEL #217AF INSTALLED AS May 25, 2021 · N598FE · Doug MD11F · Fuselage Floor PanelSDR FDEA202105251393Trunnion · damagedUPON REMOVAL OF NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING FOUND BORE HOLE ELONGATED NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING ELONGATED BORE HOLE REWORKED AS PER MD-11 SRM 53-10-14-2R REPAIR 1 FIGURE 201 AND E.A. # 1-5310-T0361720 PART 2. REPAIR May 25, 2021 · N525FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA202105251392Trunnion · damagedUPON REMOVAL OF NOSE LANDING GEAR LEFT HAND TRUNNION FITTING FOUND BORE HOLE ELONGATED NOSE LANDING GEAR LEFT HAND TRUNNION FITTING ELONGATED BORE HOLE REWORKED AS PER MD-11 SRM 53-10-14-2R REPAIR 1 FIGURE 201 AND E.A. # 1-5310-T0361720 PART 1. REPAIR BUMay 25, 2021 · N525FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR IPXA2021061170439Floor Panel · corrodedINSPECTION TYPE:2CFWD CABIN FLOOR PANEL BETWEEN STA 475 - 500.175 AND BETWEEN RBL 62.1 - RBL 73.3 IS CORRODED.REPAIRED FWD CABIN FLOOR PANEL BETWEEN STA 475 - 500.175 AND BETWEEN RBL 62.1 - RBL 73.3 IAW VT-SAA EA 011-5310-01-A9155 REV IR AND UPS EO MD11-5320-8May 24, 2021 · N271UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2021061170438Floor Panel · corrodedINSPECTION TYPE:2CFWD CABIN FLOOR PANEL BETWEEN STA 475 - 500.175 AND RBL 47.5 - RBL 62.1 IS CORRODED.REPAIRED CORRODED FWD CABIN FLOOR PANEL BETWEEN STA 475 - 500.175 AND RBL 47.5 - RBL 62.1 IAW VT-SAA EA 011-5310-01-A9162 REV. IR AND UPS EO MD11-5320-80651-AMay 24, 2021 · N271UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2021061070373Mount · corrodedINSPECTION TYPE:C2RH O/B HOR STAB #6 HINGE FITTING O/B LUG BUSHING HAS CORROSION.REPAIRED CORRODED HINGE FITTING O/B LUG IAW VT-SAA EA 011-5523-01-A9154 REV I/R AND UPS EO MD11-5520-80624-A (MINOR).May 24, 2021 · N271UP · Doug MD11F · Elevator StructureSDR IPXA2021061070372Mount · corrodedINSPECTION TYPE:C2RH I/B ELEVATOR #3 BEARING MOUNT FITTING O/B BUSHING HAS CORROSION.REPAIRED CORRODED MOUNT FITTING IAW VT-SAA EA 011-5523-01-A9153 REV I/R AND UPS EO MD11-5520-80625-A (MINOR).May 24, 2021 · N271UP · Doug MD11F · Elevator StructureSDR IPXA2021061070377Floor Panel · corrodedINSPECTION TYPE:2CRCB FLOOR PANEL BETWEEN STA. 475-500.175 & BETWEEN X= -73.3 AND X= -107.250 HAS CORROSION.REPAIRED CORRODED FLOOR PANEL IAW VT-SAA EA 011-5320-01-A9167 REV. I/R AND UPS EO MD11-5320-80613-A. (MINOR)May 24, 2021 · N271UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2021060970339Skin · gougedINSPECTION TYPE:C2LH WING L/E SKIN IS GOUGE O/B OF #1 PYLON.REMOVED,FABRICATED AND REPLACED LT L/E SKIN IAW SRM 51-35-01 (MINOR).May 24, 2021 · N271UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2021060470167Floorbeam · corrodedINSPECTION TYPE:2CFWD CABIN FLOOR SUPPORT AT STA 421.578 BETWEEN RBL 65 & RBL 81 IS CORRODED.REMOVED AND REPLACED CORRODED FWD CABIN FLOOR SUPPORT AT STA 421.578 BETWEEN RBL 65 & RBL 81 IAW SRM 51-31-01. (MINOR)May 24, 2021 · N271UP · Doug MD11F · Fuselage Main, Floor BeamSDR FDEA202105241374Seat Track · wornMAIN DECK CARGO COMPARTMENT-CABIN, FOUND SEAT TRACK AT STATION 6-10, X = 8.5 CROWN AREA WORN MAIN DECK CARGO COMPARTMENT - CABIN AT SEAT TRACK STATION 6-10, X = 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLMay 24, 2021 · N598FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202105241373Seat Track · wornMAIN DECK CARGO COMPARTMENT-CABIN, FOUND SEAT TRACK AT STATION 6-10, X = -8.5 CROWN AREA WORN. MAIN DECK CARGO COMPARTMENT - CABIN AT SEAT TRACK STATION 6-10, X = -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWAMay 24, 2021 · N598FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2021061470509Support · damagedINSPECTION TYPE:2CFWD. CARGO CEILING SUPPORT HAS DAMAGED FASTENER HOLES BETWEEN STA. 909 TO 1009 AT X= -14.REPAIRED DAMAGED CEILING SUPPORT BETWEEN STA 909 TO 1009 AT X= -14 IAW VT-SAA EA 011 5320-01-A9158 REV. I/R AND UPS EO MD11-5320-80668-A. (MAJOR) REF 810May 23, 2021 · N271UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2021060870291Seat Track · crackedINSPECTION TYPE:2CFWD. CARGO CEILING AREA SEAT TRACK IS CRACKED AT STA. 635 AND X= -27.5.REPAIRED CRACKED SEAT TRACK BETWEEN STA. 625.0 TO 645.0 AND X= -27.5 IAW SRM 53-00-52 REPAIR 1 FIG. 201. (MAJOR)May 23, 2021 · N271UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202105231362Skin · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION ON CORNER 13 OF LEFT HAND FIXED LEADING EDGE SKIN ADJACENT TO CUTOUT FOUND CRACK APPROXIMATELY 0.3 INCH AT STATION XOS 657.25 LEFT HAND FIXED LEADING EDGE SKIN ADJACENT TO CUTOUT CORNER 13 CRACK APPROXIMATELY 0.3 INMay 23, 2021 · N598FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202105231361Skin · crackedRIGHT HAND WING FIXED LEADING EDGE SKIN EXISTING REPAIR DOUBLER FOUND CRACK AT STATION XOS 906. RIGHT HAND WING FIXED LEADING EDGE SKIN CRACKED EXISTING REPAIR DOUBLER AT STATION XOS 906 REMOVED AS PER MD11 SRM 51-31-01-0G AND REPAIRED AS PER MD11 SRM 57May 23, 2021 · N598FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202105231358Doubler · crackedLEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER FOUND CRACK AT STATION XOS 765. LEFT HAND WING FIXED LEADING EDGE DOUBLER CRACK AT STATION X0S 765 REPAIRED AS PER MD11 SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.May 23, 2021 · N598FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202105231360Doubler · crackedLEFT HAND WING FIXED LEADING EDGE RIB DOUBLER FOUND CRACK AT STATION XOS 789. LEFT HAND WING FIXED LEADING EDGE RIB DOUBLER CRACK AT XOS 789 REMOVED AS PER MD11 SRM 51-33-01-0G. RIB DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB3954 REVISION : K AND INSTAMay 23, 2021 · N598FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202105231359Doubler · crackedLEFT HAND WING FIXED LEADING EDGE SKIN SUPPORT BEADED DOUBLER FOUND CRACK AT STATION XOS 545. LEFT HAND WING FIXED LEADING EDGE SKIN SUPPORT BEADED DOUBLER AT STATION XOS 545 REPAIRED AS PER MD11 SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED ASMay 23, 2021 · N598FE · Doug MD11F · Wing, Plate/SkinSDR IPXA2021052469758Gauge · inoperativeINSPECTION TYPE:N/A**SUPPLEMENTAL SDR** 1 L ENTRY DOOR SLIDE INFLATION GAUGE IS NOT VISIBLE. TRANSFERRED TO NR # 449900 FOR PERM REPAIR.RMVD UPPER & LWR L1 DOOR LINER IAW MD11 MM 25-23-06-000-802 &25-23-07-000-802. R & R L-1 DOOR SLIDE/CONTAINER. ADJ CONTAINEMay 23, 2021 · N260UP · Doug MD11F · Escape SlideSDR IPXA2021060470161Stringer · crackedINSPECTION TYPE:2CR/H WING FIXED L/E UPPER STRINGER IS CRACKED AT STA. XOS. 667.679.REPAIRED CRACKED R/H WING FIXED L/E UPPER STINGER AT STA. XOS. 667.679 IAW SRM 57-40-03 REPAIR 2 FIG. 202. (MAJOR)May 22, 2021 · N271UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA2021060470166Longeron Splice · crackedINSPECTION TYPE:2CCENTER CARGO LONGERON 38R SPLICE FITTING AT STA 5-123 IS CRACKED.REMOVED AND REPLACED CRACKED CENTER CARGO LONGERON 38R SPLICE FITTING AT STA 5-123 IAW SRM 51-33-01. (MINOR)May 22, 2021 · N271UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2021060370113Stringer Splice · crackedINSPECTION TYPE:2CCENTER CARGO LONGERON 44R SPLICE FITTING IS CRACKED AT STA. 5-123.REMOVED, FABRICATED AND REPLACED SPLICE FITTING IAW DWG. A5A7116 AND SRM 51-33-01. (MINOR)May 22, 2021 · N271UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA202105211351Indication Sys · no testMDIS 602 25-60 1083 21MAY21 LAX OPEN U R1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATION IS NOT TESTING MEL 21MAY21 12:59 LAX U RELEASED FOR SERVICE PER MEL : 25-61-02 CATEGORY : C EXPIRATION : 31MAY21 "MEL 25-61-02: R1 EVACMay 21, 2021 · N602FE · Doug MD11F · Emergency EquipmentSDR IPXA2021061170437Spar Cap · corrodedINSPECTION TYPE:2CLT WING UPPER REAR SPAR CAP AFT FLANGE BETWEEN XORS 561.5 - XORS 576.5 IS CORRODED.REPAIRED CORRODED LT WING UPPER REAR SPAR CAP AFT FLANGE BETWEEN XORS 561.5 - XORS 576.5 IAW VT-SAA EA 011-5710-01-A9159 REV. IR AND UPS EO MD11-5710-80646-A. May 21, 2021 · N271UP · Doug MD11F · Wing SparSDR IPXA2021061170434Skin · corrodedINSPECTION TYPE:2CLT WING UPPER SKIN BETWEEN XORS 181 - XORS 185 AT STRINGER 16 IS CORRODED.REPAIRED CORRODED LT WING UPPER SKIN BETWEEN XORS 181 - XORS 185 AT STRINGER 16 IAW VT-SAA EA 011-5730-01-A9147 REV. IR AND UPS EO MD11-5730-80654-A. REF. FAA FORM 8100May 21, 2021 · N271UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2021061470507Support Angle · corrodedINSPECTION TYPE:C2RH O/B WING LOWER SUPPORT ANGLE HAS CORROSION AT LWR T/E.REMOVED,FABRICATED AND REPLACED CORRODED SUPPORT ANGLE IAW SRM 51-35-01 AND 51-31-01 (MINOR).May 21, 2021 · N271UP · Doug MD11F · Wing Miscellaneous StructureSDR IPXA2021061470506Skin · gougedINSPECTION TYPE:C2RT WING ACCESS PANEL 616ET GOUGE AT UPPER FWD SURFACE.REMOVED,FABRICATED AND REPLACED GOUGED PANEL(SKIN) IAW SRM 51-35-01 AND 51-31-01 (MINOR).May 21, 2021 · N271UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2021061470512Spar Cap · corrodedINSPECTION TYPE:2CR/H WING REAR SPAR CAP UPPER FLANGE HAS CORROSION BETWEEN STA. XORS. 1042.35 TO 1054.REPAIRED CORRODED R/H WING REAR SPAR CAP UPPER FLANGE BETWEEN STA. XORS. 1042.35 TO 1054 IAW VT-SAA EA 011-5710-01-A9137 REV. I/R AND UPS EO MD11-5710-80666-May 21, 2021 · N271UP · Doug MD11F · Wing SparSDR IPXA2021061170411Cap · corrodedINSPECTION TYPE:2CR/H WING LOWER CAP HAS CORROSION AT STA. XW= 320.REPAIRED CORRODED R/H WING LOWER CAP BETWEEN STA. XW= 275.230 & XW= 326.730 IAW SRM 57-50-02 REPAIR 9 FIG. 201. (MAJOR)..May 21, 2021 · N271UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2021060870300Spar Cap · corrodedINSPECTION TYPE:2CRT WING REAR SPAR UPPER CAP BELOW #3 SPOILER HAS CORROSION.REPAIRED CORRODED RT WING REAR SPAR UPPER CAP AT STA XORS 653.100 IAW VT-SAA EA 011-5700-01-A9140 REV. IR AND UPS EO MD11-5710-80599-A. (MINOR)May 21, 2021 · N271UP · Doug MD11F · Wing SparSDR IPXA2021060470165Skin · corrodedINSPECTION TYPE:2CLT WING UPPER SKIN BETWEEN XORS 286.5 - XORS 297 & BETWEEN STRINGER 17 AND FWD SPAR HAS 5 EA AREAS OF CORROSION.REPAIRED CORRODED LT WING UPPER SKIN BETWEEN XORS 286.5 - XORS 297 7 BETWEEN STRINGER 17 AND FWD SPAR 5 EA AREAS IAW VT-SAA EA 011May 21, 2021 · N271UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2021060470159Skin · crackedINSPECTION TYPE:2CR/H WING I/B FLAP CENTER BOX UPPER SKIN IS CRACKED AT STA.XIFH=147.3.REPAIRED CRACKED R/H WING UPPER SKIN AT STA. XIFH= 147.3 AND BETWEEN YIF= 26 TO YIFH= 28 IAW SRM 57-00-01 REPAIR 1 FIG. 201. (MAJOR)May 21, 2021 · N271UP · Doug MD11F · Trailing Edge Flaps
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