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 IPXA2020032353383Floorbeam · crackedINSPECTION TYPE:2CFWD. CARGO FLOOR BEAM IS CRACKED AT STA. 6-70, Z=-98 AND BETWEEN X=-37 & X=-64.REPAIRED CRACKED FLOOR BEAM AT STA. 6-70, Z=-98 AND BETWEEN X=-37 TO X=-64 IAW VT-SAA EA 011-5310-01-A8053 REV. I/R AND UPS EO MD11-5310-75857-A. (MAJOR)Feb 16, 2020 · N282UP · Doug MD11F · Fuselage Main, Floor BeamSDR IPXA2020032053378Support Angle · crackedINSPECTION TYPE:2CCENTER CARGO COMPARTMENT L/H SLOPE PANEL SUPPORT ANGLE IS CRACKED AT STA. 1741.REMOVED AND REPLACED CRACKED CENTER CARGO COMPARTMENT L/H SLOPE PANEL SUPPORT ANGLE AT STA. 1741 IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR)Feb 16, 2020 · N282UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020030952943Spar Cap · corrodedINSPECTION TYPE:2CR/H WING REAR SPAR UPPER CAP AFT FLANGE HAS CORROSION BETWEEN STA. XORS.= 763.0-826.5.REPAIRED CORRODED R/H WING REAR SPAR UPPER CAP AFT FLANGE BETWEEN STA. XORS.= 763-826.5 IAW VT-SAA EA 011-5710-01-A8057 REV. I/R AND UPS EO MD11-5740-75653-Feb 16, 2020 · N282UP · Doug MD11F · Wing SparSDR IPXA2020031353136Doubler · wornINSPECTION TYPE:2CR/H WING FIXED L/E SKIN REPAIR DOUBLER HAS DEEP WEAR BETWEEN STA. XIS= 163.4 AND 164.972.REMOVED, INSPECTED AND REPLACED R/H WING FIXED L/E SKIN REPAIR DOUBLER BETWEEN STA. XIS= 163.4 TO 164.972 IAW VT-SAA EA 011-5740-01-A8035 REV. I/R AND UPFeb 15, 2020 · N282UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020030652850Rib · crackedINSPECTION TYPE:2CRT WING FIXED L/E RIB (FORMER) IS CRACKED AT XOS=584.8912.REPAIRED CRACKED RT WING FIXED L/E RIB (FORMER) AT XOS=584.8912 IAW MD-11 SRM 57-00-00 REPAIR GENERAL, FIGURE 204. (MAJOR)Feb 15, 2020 · N282UP · Doug MD11F · Wing, Rib/BulkheadSDR IPXA2020030252620Stiffener · crackedINSPECTION TYPE:2CRT WING L/E STIFFENER AT O/B SIDE OF PANEL 618FB IS CRACKED.REMOVED AND REPLACED CRACKED RT WING L/E STIFFENER AT O/B SIDE OF PANEL 618FB IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR)Feb 15, 2020 · N282UP · Doug MD11F · Wing Miscellaneous StructureSDR FDEA2020021850343Lamp · inoperativeL1 DOOR REMOTE BOTTLE PRESSURE TEST SWITCH WILL NOT TEST. RELAMPED AND OPS CHECKED GOOD I.A.W. M.M. 25-61-04-5-0.Feb 15, 2020 · N599FE · Doug MD11F · Emergency EquipmentSDR IPXA2020031353131Filler · corrodedINSPECTION TYPE:2CLT WING T/E PANEL HAS BULGE FWD OF I/B AILERON.REPAIRED CORRODED LT WING T/E SPACER FILLER BETWEEN XORS 414 TO XORS 420 IAW VT-SAA EA 011-5700-01-A8051 REV. IR AND UPS EO MD11-5710-75648-A. (MINOR)Feb 14, 2020 · N282UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020030452785Spar Cap · corrodedINSPECTION TYPE:2CL/H WIING REAR SPAR UPPER CAP HAS CORROSION FWD. OF #3 SPOILER I/B END.REAPIRED CORRODED L/H WING REAR SPAR UPPER CAP AFT FLANGE BETWEEN STA. XORS.= 551-650 IAW VT-SAA EA 011-5710-01-A8045 REV. I/R AND UPS EO MD11-5710-75647-A. (MINOR)Feb 14, 2020 · N282UP · Doug MD11F · Wing SparSDR IPXA2020030452784Spar Cap · corrodedINSPECTION TYPE:2CL/H WING REAR SPAR UPPER CAP AFT FLANGE HAS CORROSION FWD. OF #3 SPOILER O/B END.REPAIRED CORRODED L/H WING REAR SPAR UPPER CAP AFT FLANGE BETWEEN STA. STA. XORS.= 551-650 IAW VT-SAA EA 011-5710-01-A8045 REV. I/R AND UPS EO MD11-5710-75647-AFeb 14, 2020 · N282UP · Doug MD11F · Wing SparSDR IPXA2020030452783Spar Cap · corrodedINSPECTION TYPE:2CL/H WING REAR SPAR UPPER CAP AFT FLANGE HAS CORROSION FWD. # 2 SPOILER.REPAIRED CORRODED L/H WING REAR SPAR UPPER CAP AFT FLANGE BETWEEN STA. XORS.= 551-650 IAW VT-SAA EA 011-57140-01-A8045 REV. I/R AND UPS EO MD11-5710-75647-A. (MINOR)Feb 14, 2020 · N282UP · Doug MD11F · Wing SparSDR IPXA2020030352713Skin · corrodedINSPECTION TYPE:2CL/H WING UPPER FWD. SKIN HAS CORROSION BETWEEN STA. XORS,=222.65 TO 230.6.REPAIRED CORRODED L/H WING UPPER FWD. SKIN BETWEEN STA. XORS.= 222.65 TO 230.6 IAW VT-SAA EA 011-5730-01-A8038 REV. I/R AND UPS EO MD11-5730-75670-A. (MINOR)Feb 14, 2020 · N282UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020030252639Intercostal · crackedINSPECTION TYPE:2C#2 PYLON CARRY THRU REAR SPAR INTERCOSTAL IS CRACKED AT STA. YID= 375, XID= -7.1 AND ZID= 65.REPAIRED CRACKED #2 PYLON CARRY THRU REAR SPAR INTERCOSTAL AT STA. YID= 375, XID= -7.1 AND ZID= 65 IAW SRM 55-30-02 REPAIR 7 FIG. 204. (MAJOR)Feb 14, 2020 · N282UP · Doug MD11F · Nacelle/Pylon Miscellaneous StructureSDR IPXA2020030252619Doubler · crackedINSPECTION TYPE:2CLT WING FIXED L/E SKIN SPLICE DOUBLER AT XOS 789 IS CRACKED.REMOVED AND REPLACED CRACKED LT WING FIXED L/E SPLICE DOUBLER AT XOS 789 IAW MD-11 SRM 51-33-01. (MINOR)Feb 14, 2020 · N282UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020022875553Landing · crackedINSPECTION TYPE:2CL/H WING FIXED L/E LOWER STRINGER (PANEL LANDING) IS CRACKED AT STA. XOS.= 906.5607.REPAIRED CRACKED L/H WING FIXED L/E LOWER STRINGER AT STA. XOS.= 906.5607 IAW SRM 57-40-03 REPAIR 1 FIG. 201. (MAJOR)Feb 14, 2020 · N282UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020022652495Support Angle · crackedINSPECTION TYPE:2CLT WING O/B FLAP I/B FWD HINGE FAIRING FWD I/B SUPPORT CLIP IS CRACKED.REMOVED AND REPLACED CRACKED LT WING O/B FLAP I/B FWD HINGE FAIRING FWD I/B SUPPORT CLIP IAW MD-11 SRM 51-33-01. (MINOR)Feb 14, 2020 · N282UP · Doug MD11F · Wing Miscellaneous StructureSDR IPXA2020022435378Skin · crackedINSPECTION TYPE:2CL/H WING L/E LOWER SKIN IS CRACKED AT STA. XOS= 776.REPAIRED CRACKED L/H WING L/E LOWER SKIN AT STA. XOS.= 776 IAW SRM 57-40-02 REPAIR 7 FIG. 201. (MAJOR)Feb 14, 2020 · N282UP · Doug MD11F · Wing, Plate/SkinSDR FDEA202002140339Switch · unsecurePDIS 583 32-10 9710 14FEB20 IND OPEN AFTER DEPARTING KDTW AND SELECTING THE GEAR HANDLE UP, THE GEAR FAILED TO RETRACT WHICH WAS VERIFIED ON BOTH THE PRIMARY AND SECONDARY INDICATIONS. COMPLIED WITH QRH PROCEDURE WHICH RESULTED IN GEAR SAFFeb 14, 2020 · N583FE · Doug MD11F · Landing Gear Retraction/Extension SystemSDR IPXA2020031653180Door Frame · crackedINSPECTION TYPE:2CL-3 DOOR JAMB WEB (INNER SKIN) IS CRACKED AT STA. 1254 AND Z=-18.REPAIRED CRACKED L-3 DOOR JAMB WEB (INNER SKIN) AT STA. 1254 AND Z=-18 IAW SRM 53-40-15 REPAIR 3 FIG. 201. (MAJOR)Feb 13, 2020 · N282UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2020031353128Beam · crackedINSPECTION TYPE:2CMAIN CABIN L3 PLUG DOOR LOWER FWD STOP FITTING (BEAM) IS BROKEN OFF.REMOVED AND REPLACED BROKEN MAIN CABIN L3 PLUG DOOR LOWER STOP FITTING (BEAM) IAW MD-11 SRM 51-33-01. (MINOR)Feb 13, 2020 · N282UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2020031353135Door Frame · crackedINSPECTION TYPE:2CR-3 DOOR JAMB INNER SKIN (WEB) IS CRACKED AT STA. 1256.75 AND Z=60.REPAIRED CRACKED R-3 DOOR JAMB INNER SKIN (WEB) AT STA. 1256.75 AND Z=60 IAW VT-SAA EA 011-5310-01-A8034 REV. I/R AND UPS EO MD11-5310-75793-A. (MAJOR)Feb 13, 2020 · N282UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2020030952893Doubler · corrodedINSPECTION TYPE:2CCENTER CARGO INTERMEDIATE FUSELAGE STA. BETWEEN STA. 1721 TO 1741 AND L=51R TO L51L INTERNAL RING DOUBLER HAS HEAVY CORROSION.REMOVED, FABRICATED AND REPLACED RING DOUBLER BETWEEN STA. 1721 TO 1741 AND L51R TO L51L IAW DWG. AGA7808 AND NGA631Feb 13, 2020 · N282UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020030352744Angle · crackedINSPECTION TYPE:2CMAIN CABIN LONGERON 15 R/H "T" ANGLE IS CRACKED AT STA. 1341.REMOVED, FABRICATED AND REPLACED LONG. 15 R/H "T" ANGLE AT STA. 1341 IAW DWG. AEA7568 AND SRM 51-31-01. (MINOR)Feb 13, 2020 · N282UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020030252616Skin · damagedINSPECTION TYPE:2CPREVIOUS MAJOR REPAIR AT LOWER FWD CARGO DOOR CUTOUT AFT SIDE HAS EDGE DAMAGE.REPAIRED DAMAGED PREVIOUS MAJOR REPAIR AT LOWER FWD CARGO DOOR CUTOUT AFT SIDE IAW VT-SAA EA 011-5330-01-A8036 REV. IR AND UPS EO MD11-5330-75654-A. (MINOR)Feb 13, 2020 · N282UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020022875552Door Frame · crackedINSPECTION TYPE:2CMAIN CABIN L-3 DOOR JAMB WEB IS CRACKED AT STA. 1313 AND Z=-15.REPAIRED CRACKED L-3 DOOR JAMB WEB AT STA. 1313 AND Z=-15 IAW SRM 53-40-15 REPAIR3 FIG. 201. (MAJOR)Feb 13, 2020 · N282UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2020021452125Seal · damagedINSPECTION TYPE:N/A*** DIVERTED*** APPROACHING TOP OF DESCENT FOR EWR, WITH ANTI-ICE SELECTEDON RCVD LEVEL 2 A-ICE DISAG. CONSULTED WITH FLIGHT CONTROL FOR DIVERT TO RDU.REPLACED DAMAGED SEAL ON LEFT OUTBD HORIZ STAB LEADING EDGE ANTI-ICE DUCT EXPANSION SLEEVEFeb 13, 2020 · N272UP · Doug MD11F · Airfoil Anti/De-ice SystemSDR IPXA2020022652494Stiffener · crackedINSPECTION TYPE:2CRT MLG W/W O/B AFT AREA LOWER VERTICAL STIFFNER IS CRACKED.REMOVED AND REPLACED CRACKED RT MLG W/W O/B AFT AREA LOWER VERTICAL STIFFNER IAW MD-11 SRM 51-35-01. (MINOR)Feb 12, 2020 · N282UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020022652523Doubler · crackedINSPECTION TYPE:2CL/H WING L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS.= 633.4 TO 636.8.REPAIRED CRACKED L/H WING L/E BEADED DOUBLER BETWEEN STA. SOX.= 633.4 TO 636.8 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)Feb 12, 2020 · N282UP · Doug MD11F · Wing, Plate/SkinSDR FDEA2020021420322Fire Loop · damagedPDIS 572 26-10 5139 12FEB20 MEM OPEN U LOGPAGES:2749371 INTERMITTENT LEVEL 1 FIRE DET 2 FAIL AND ASSOCIATED LEVEL 3 FIRE WARNING DURING DESCENT 13FEB20 11:40 MEM REPLACED #2 Feb 12, 2020 · N572FE · Doug MD11F · Fire DetectionSDR IPXA2020030952897Support Angle · crackedINSPECTION TYPE:2CCAC AT STA. 6-90 , FLOOR AREA R/H SUPPORT ANGLE IS CRACKED.REMOVED, FABRICATED AND REPLACED SUPPORT ANGLE IAW DWG. AAN7185 AND SRM 51-33-01. (MINOR)Feb 11, 2020 · N282UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020030952896Support Web · crackedINSPECTION TYPE:2CCENTER ACCESSORY COMP. AT STA. 6-90 R/H CIELING SUPPORT WEB IS CRACKED.REMOVED, FABRICATED AND REPLACED WEB IAW DWG. ADA7652 AND SRM 51-33-01. (MINOR)Feb 11, 2020 · N282UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020022652492Mount Bracket · crackedINSPECTION TYPE:2CAFT FUSELAGE COMPARTMENT 316 HAS RT UPPER SURGE DUCT UPPER MOUNT BRACKET CLIP CRACKED.REMOVED AND REPLACED CRACKED AFT FUSELAGE COMPARTMENT 316 RT UPPER SURGE DUCT UPPERMOUNT BRACKET CLIP IAW MD-11 SRM 51-33-01. (MINOR)Feb 11, 2020 · N283UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020030952962Skin · crackedINSPECTION TYPE:2C#1 ENG. I/B T/R AFT FIXED INNER BARREL SKIN IS CRACKED.REPAIRED #1 ENG. I/B T/R AFT FIXED INNER BARREL UPPER SKIN IAW VT-SAA EA 011-7830-01-A8032 REV. I/R AND UPS EO MD11-7830-755551-A. (MINOR)Feb 10, 2020 · N282UP · Doug MD11F · Engine Thrust ReverserSDR IPXA2020030952961Skin · crackedINSPECTION TYPE:2C#3 ENG. L/H T/R AFT FIXED INNER BARRELL UPPER SKIN IS CRACKED AT STA. NAC=194 & 11:00 POS.REPAIRED #3 ENG. L/H T/R FIXED INNER BARRELL UPPER SKIN IAW VT-SAA EA 011-7830-01-A8301 REV. I/R AND UPS EO MD11-7830-75553-A. (MINOR)Feb 10, 2020 · N282UP · Doug MD11F · Engine Thrust ReverserSDR IPXA2020030252714Skin · crackedINSPECTION TYPE:2C#3 ENG. R/H T/R AFT INNER BARREL UPPER SKIN IS CRACKED AT STA. NAC=194 & 1:00 POS.REPAIRED CRACKED #3 ENG. R/H T/R IAW VTSAA EA 011-7830-01-A8030 REV. I/R AND UPS EO MD11-7830-75552-A. (MINOR)Feb 10, 2020 · N282UP · Doug MD11F · Engine Thrust ReverserSDR FDEA202002100300Fire Warning · false activationPDIS 572 26-10 5129 10FEB20 JFK FACT U ON FINAL HAD A ENGINE 3 FIRE WARNING START LEVER AND #3 FIRE HANDLE RED. SEVERAL SECONDS THAN EXTINGUISHED. NO ABNORMAL INDICATIONS. FACT 10FEB20 07:37 JFK U PERFORMED ENGINE RUN PER MD11 JRH. NO FAULFeb 10, 2020 · N572FE · Doug MD11F · Fire DetectionSDR IPXA2020022875551Doubler · crackedINSPECTION TYPE:2CR/H WING L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS.= 584.8 TO 589.8.REPAIRED CRACKED R/H WING L/E BEADED DOUBLER BETWEEN STA. XOS.= 584.8 TO 589.8 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)Feb 9, 2020 · N282UP · Doug MD11F · Wing, Attach FittingsSDR IPXA2020022875550Doubler · crackedINSPECTION TYPE:2CR/H WING L/E BEADED DOUBLER IS CRACKED BEYTWEEN STA. XOS.= 768.2 TO 772.8.REPAIRED CRACKED R/H WING L/E BEADED DOUBLER BETWEEN STA. XOS.= 768.2 TO 772.8 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)Feb 9, 2020 · N282UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020022875549Doubler · crackedINSPECTION TYPE:2CL/H WING L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS.= 653.0 TO 658.REPAIRED CRACKED L/H WING L/E BEADED DOUBLER BETWEEN STA. XOS.= 653.0 TO 658 IAW SRM 57-40-02 REPAIR 15 FIG.205. (MAJOR)Feb 9, 2020 · N282UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020022652525Doubler · crackedINSPECTION TYPE:2CL/H WING L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS.= 610.8 TO 621.6.REPAIRED CRACKED L/H WING L/E BEADED DOUBLER BETWEEN STA. XOS.= 610.8 TO 621.6 IAW SRM 57-40-05 REPAIR 15 FIG. 205. (MAJOR)Feb 9, 2020 · N282UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020022652524Doubler · crackedINSPECTION TYPE:2CR/H WING L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS.= 759.1 TO 763.6.REPAIRED CRACKED R/H WING L/E BEADED DOUBLER BETWEEN STA. XOS. = 759.1 TO 763.6 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)Feb 9, 2020 · N282UP · Doug MD11F · Wing, Plate/SkinSDR FDEA202002090295Hinge Bracket · corrodedRIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE (HOLE # 4) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57- 4Feb 9, 2020 · N575FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2020021090294Hinge Bracket · corrodedRIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE CORROSION. CORROSION AT RIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE (HOLE # 4) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57Feb 9, 2020 · N575FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2020021090293Hinge Bracket · corrodedLEFT HAND WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE CORROSION. CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR OUTBOARD HOLE BORE (HOLE # 4) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-4Feb 9, 2020 · N575FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2020021090292Hinge Bracket · corrodedLEFT HAND WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE CORROSION. CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR INBOARD HOLE BORE (HOLE # 4) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57- 44-Feb 9, 2020 · N575FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2020021080289Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (HOLE # 4) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-4Feb 8, 2020 · N576FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2020021080288Hinge Bracket · corrodedLEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (HOLE # 4) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM Feb 8, 2020 · N576FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2020021080287Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (HOLE # 4) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57Feb 8, 2020 · N576FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2020021080286Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (HOLE # 4) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM Feb 8, 2020 · N576FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2020021080285Hinge Bracket · corrodedRIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE INBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (HOLE # 3) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR BUSHING FABRIFeb 8, 2020 · N576FE · Doug MD11F · Wing, Control Surface Attach Fittings
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