Boeing MD-11F

Service difficulty reports · 31,320

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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 FDEA201210023529Access Panel · corrodedRT WING T/E LOWER ACCESS PANEL NR 641JB CUT-OUT FORWARD TEE FITTING, FOUND CORROSION. TEE FITTING REPAIRED IAW EA 1-5710-163502. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 115.Oct 2, 2012 · N618FE · Doug MD11F · Wing, Plate/SkinSDR IPXA2M76145Skin · dentedINSPECTION TYPE:4C, LT FUSELAGE SKIN DENT REPAIR BETWEEN BS 1811-1841 AND BETWEEN L28L AND L29L. REPAIRED SKIN IAW EA 011-5330-01-A4331 REV I/R, UPS EO -5330-49039-A.Oct 1, 2012 · N294UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2M76144Fitting · crackedINSPECTION TYPE: 4C, VERTICAL STABILIZER AFT SPAR NR4 RT BANJO FITTING AFT SIDE FLANGE CRACKED. REPAIRED NR 4 RT BANJO FITTING AFT SIDE FLANGE REF STASA EA 011-5530- 01-A4354 REV I/R, EO MD11-5530-49025-A, SRM 55-30-02, REPAIR 5, FIG 202, 8100-9, SR 1- 23Oct 1, 2012 · N294UP · Doug MD11F · Vertical StabilizerSDR FDEA201210013527Power Supply · inoperativePRE-DISPATCH CHECK FOUND EMERGENCY LIGHT TEST FAILED. R & R THE EMERGENCY LIGHTING BATTERY POWER SUPPLY, OPS TEST PASSED .Oct 1, 2012 · N605FE · Doug MD11F · Emergency LightingSDR FDEA201209303517Longeron · crackedBS 595, LONGERON 49 RT FASTENER HOLE COMMON TO RT NLG TRUNNION FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01 REVISION 50 AND SRM 51-33-01 REVISION 50. NEW LONGERON FABRICATED AND REWORKED AS PER DRAWING ACA3796 REVISION A. REPAIR CLASSIFIED AS MAJSep 30, 2012 · N618FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA12M76021Trunnion · crackedINSPECTION TYPE: 4C, APPROX 1.4" LONG TYPICAL CRACK AT NLG LT TRUNNION FITTING. REPAIRED NLG LT TRUNNION FITTING REF EA 011-5310-01-A4307 I/R, EO MD11-5310-48930-A.Sep 29, 2012 · N294UP · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA201209283487Structure · corrodedOVERWING TANK PANEL BS 1234, "X" = 0, FOUND CORRODED. EXFOLIATION CORROSION REMOVED IAW SRM 51-21-01 REVISION 50. FOUND ACCEPTABLE AS PER EA 1-5730-163505, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Sep 28, 2012 · N618FE · Doug MD11F · Fuselage Main, StructureSDR IPXA12M75612Battery · inoperativeEMERGENCY LIGHTING SYS TEST FUNCTION INOPERATIVE. R & R POWER SUPPLY RECHARGEABLE BATTERY EMERGENCY CTS MM 33-51-01-00-802 AND 01-400-802.Sep 28, 2012 · N256UP · Doug MD11F · Emergency LightingSDR IPXA12M75572Controller · false activationSMOKE INDICATION FROM MAIN CABIN. EMERGENCY DECLARED. R & R MISCELLANEOUS SYS CONTROLLER REF MM 31-42-01. PERFORMED RTS TEST OF MISCELLANEOUS SYS CONTROLLER SYS CHECK OK.Sep 28, 2012 · N279UP · Doug MD11F · Smoke DetectionSDR IPXA2M75572Warning Message · illuminatedAIR TURN BACK DUE TO SMOKE INDICATION FROM MAIN CABIN. EMERGENCY DECLARED. OPEN.Sep 28, 2012 · N279UP · Doug MD11F · Smoke DetectionSDR FDEA201209273470Access Panel · crackedRT WING L/E LOWER SURFACE ACCESS PANEL 619AB CUTOUT, FORWARD EDGE FOUND CRACKED AT STA XOS 608. REPAIRED AS PER SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Sep 27, 2012 · N618FE · Doug MD11F · Wing, Plate/SkinSDR IPXA12M75659Skin · dentedINSPECTION TYPE:3C, R1 DOOR EXTERIOR SKIN DENTED AT UPPER AFT CORNER. REPAIRED R1 DOOR SKIN AT UPPER AFT CORNER BETWEEN STA YNPD 17.3-5.5 IAW SRM 52-01-01, REPAIR 3, FIG 201.Sep 27, 2012 · N285UP · Doug MD11F · Passenger/Crew DoorsSDR FDEA201209273478Static Wick · missingDURING CLIMBOUT, WE WERE INSTRUCTED TO RETURN TO DEPARTURE DUE TO POSSIBLE DAMAGE DURING PUSHBACK. LEFT UPPER WINGLET MISSING STATIC WICKS. REPAIRED L/H UPPER WINGLET CAP PER PART 2 OF EA 1-5720-162680. INSTALLED UPPER WINGLET CAP IAW MM 57-31-01-4 A/C OSep 27, 2012 · N574FE · Doug MD11F · Pitot/Static SystemSDR FDEA201209273471Skin · crackedRT WING FIXED L/E LOWER SURFACE AT STATION XOS 775 (NR 12 SLAT TRACK LOWER CUTOUT) FOUND CRACKED. REPAIRED AS PER SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Sep 27, 2012 · N618FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201209273469Access Panel · crackedLT WING - L/E LOWER SURFACE ACCESS PANEL 519CB CUTOUT INBD CORNER FOUND CRACKED. REPAIR CARRIED OUT AT LEFT HAND WING LEADING EDGE LOWER SURFACE ACCESS PANEL 519CB CUTOUT INBOARD CORNER AS PER SRM 57-40-02 FIGURE 202 REPAIR 7 REVISION 50. REPAIR CLASSIFIEDSep 27, 2012 · N618FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201209263444Doubler · crackedRT WING REFUELING ACCESS DOOR COMPARTMENT UPPER BEADED DOUBLER CRACKED BETWEEN XOS 640 AND XOS 648. REPAIRED AS PER SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Sep 26, 2012 · N618FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201209263443Doubler · crackedRT WING LOWER FIXED L/E AT XOS 612 INBD REFUELING PANEL CUTOUT FWD CORNER, FOUND CRACKED.SRM 51-31-01 REVISION 50. NEW DOUBLER FABRICATED AS PER DRAWING ARB2933 REVISION AJ AND INSTALLED AS PER SRM 51-31-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-Sep 26, 2012 · N618FE · Doug MD11F · Wing, Plate/SkinSDR IPXA12M75578Aileron Sys · malfunctionedDURING CLIMB AT FLAP RETRATION LEVEL 1 AILERON DEFLECT INOP FOLLOWED BY LVL 2 AILERON DEFLECT DISAGREE. ACFT HAD UNCOMMANDED ROLL TO LEFT. RAN QRH CHECKLIST. NO RESOLUTION. DECLARED EMERGENCY, DIVERTED. ACCOMPLISHED FIM TROUBLESHOOTING 27-10-05, BLOCK 16Sep 26, 2012 · N276UP · Doug MD11F · Aileron Control SystemSDR IPXA2M75578Warning Message · activatedDURING CLIMB AT FLAP RETRACTION LEVEL 1 AILERON DEFLECT INOPERATIVE FOLLOWED BY LEVEL 2 AILERON DEFLECT DISAGREE. ACFT HAD UNCOMMANDED ROLL TO LEFT. RAN QRH CHECKLIST. NO RESOLUTION. DECLARED EMERGENCY, DIVERTED. OPEN.Sep 26, 2012 · N276UP · Doug MD11F · Aileron Control SystemSDR IPXA2M75542Computer · inoperativeDIVERSION-ON CLIMB OUT "RUDDER STANDBY LOWER OFF" AND "RUDDER STANDBY UPPER OFF" ILLUMINATED. CFDS SHOW UPR RUDDER STANDBY OFF AND LOWER RUDDER STANDBY OFF MESSAGE, TROUBLESHOT IAW FIM29-20-04-00, REPLACED HSC IAW AMM29-08-01, TEST OK.Sep 26, 2012 · N278UP · Doug MD11F · Rudder Control SystemSDR FDEA201209253428Longeron · crackedDURING X-RAY INSPECTION, AT CABIN STATION 5-0, LONGERON 1R, FORWARD SECTION INBD ROW FROM EDGE TO NR 2 HOLE HAS A CRACK INDICATION APPROX 2.25" IN LENGTH. REPAIRED AS PER SRM 53-00-05 FIGURE 202 REPAIR 1 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-Sep 25, 2012 · N585FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201209253427Longeron · crackedDURING X-RAY INSPECTION AT CABIN STATION 5-0, LONGERON 2L, FORWARD SECTION INBD ROW FROM EDGE CRACK INDICATION FOUND APPROX .3750" IN LENGTH. REPAIRED IAW SRM 53-00-05 FIGURE 202 REPAIR 1 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 11Sep 25, 2012 · N585FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201209253426Longeron · crackedDURING X-RAY INSP AT CABIN STATION 5-0, LONGERON 2R STRINGER FORWARD SECTION OTBD ROW FROM EDGE CRACK INDICATION FOUND APPROX .3750" IN LENGTH. REPAIRED IAW SRM 53-00-05 FIGURE 202 REPAIR 1 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION Sep 25, 2012 · N585FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201209253435Trunnion · crackedNLG WHEEL WELL, RT TRUNNION FITTING LOWER AREA FOUND CRACKED. REPAIRED AS PER SRM 53-10-14 FIGURE 202 REPAIR 2 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Sep 25, 2012 · N618FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA201209253434Trunnion · crackedNLG WHEEL WELL LT TRUNNION FITTING LOWER AREA FOUND CRACKED. REPAIRED AS PER SRM 53-10-14 FIGURE 202 REPAIR 2 REVISION 50 AND REPAIR PARTS INSTALLED AS PER SRM 53-10-14 FIGURE 202 REPAIR 2 AND SRM 51-33-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6Sep 25, 2012 · N618FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA201209253433Skin · chafedFORWARD CARGO DOOR FORWARD LOWER CUTOUT FOUND EDGE CHAFED. TRIMMED OUT AND REPAIR CARRY-OUT AS PER SRM 53-00-15 FIGURE 202 REPAIR 8 REVISION 50 AND SRM 51-33-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.Sep 25, 2012 · N618FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201209253432Tee Fitting · corrodedLT WING T/E LOWER ACCESS PANEL 541JB CUTOUT FORWARD TEE FOUND CORRODED AT XW317. CUTOUT FORWARD AREA REMOVED AS PER SRM 51-31-01 REVISION 50 AND REPLACED WITH NEW TEE AS PER SRM 51-35-01 REVISION 50 AND SRM 51-33-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR Sep 25, 2012 · N618FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA201209243418Hinge · damagedDURING FPI ON RT INBD FLAP, OTBD HINGE (FLAP SIDE) PIVOT INBD HOLE FOUND DAMAGED. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 REVISION 74. REPAIRED IAW EA 1-5750-162593 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.Sep 24, 2012 · N585FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR IPXA2M75770Trunnion · crackedINSPECTION TYPE: 3C, NLG RT TRUNION FITTING CRACKED. REPAIRED NLG RT TRUNION IAW EA 011-5310-01-A4305 REV.IR AND UPS EO 5310-48760-A. MAJOR.Sep 24, 2012 · N285UP · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR IPXA2M75493Skin · damagedFUSELAGE SKIN DAMAGE AT BS 13.25. REPAIRED IAW EO MD11-5330-48624-A.Sep 24, 2012 · N284UP · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201209233408Bushing · wornLEFT INBD FLAP, OTBD AFT (FLAP SIDE) HINGE PIVOT INBD BUSHING WORN. WORN BUSHING REMOVED AS PER CMM 20-20-07 REVISION 74. FOUND EXCEED LIMITS AS PER CMM 57-52-03 REVISION 74. NEW BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-162592 PART 1. REPAIR CLSep 23, 2012 · N585FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201209233407Hinge · corrodedLEFT OTBD FLAP, OTBD FORWARD (WING) HINGE ACTUATOR OTBD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-162588. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.Sep 23, 2012 · N585FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201209233405Hinge · corrodedLEFT OTBD FLAP, OTBD FORWARD (WING) HINGE ACTUATOR INBD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-162588. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.Sep 23, 2012 · N585FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201209233402Hinge · corrodedRT OTBD FLAP, INBD FORWARD (WING) HINGE ACTUATOR OTBD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-162587 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115Sep 23, 2012 · N585FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA201209233400Hinge · corrodedRT OTBD FLAP, INBD FORWARD (WING) HINGE ACTUATOR, INBD HOLE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 REVISION 74. EXISTING HOLE DIAMETER 1.249", FINAL HOLE DIAMETER 1.254", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED AS PESep 23, 2012 · N585FE · Doug MD11F · Wing Main, Frame StructureSDR IPXA2M75561Warning Message · false activationEMERGENCY BATTERY 1 LOW ALERT MESSAGE WHEN CARRYING OUT PRE-FLT. ACCOMPLISHED FIM 33-51-02-00, FIG 104 BLOCKS 1-3. PERFORMED EMERGENCY LIGHTING TEST IN REF TO AMM 33-51-01. OPS CHECKED GOOD.Sep 23, 2012 · N256UP · Doug MD11F · Emergency LightingSDR FDEA201209233411Bushing · wornRIGHT INBD FLAP, OTBD AFT (FLAP SIDE) PIVOT OTBD BUSHING WORN. WORN BUSHING REMOVED IAW CMM 20-20-07, REV 74. HOLE MEASURED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 74. EXISTING HOLE DIAMETER 1.258", MAXIMUM HOLE DIAMETER 1.220". NEW BUSHING FABRICATEDSep 23, 2012 · N585FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201209233410Bushing · wornRT INBD FLAP OTBD AFT (FLAP SIDE) HINGE PIVOT INBD BUSHING WORN. WORN BUSHING REMOVED IAW CMM 20-20-07 REV 74. HOLE MEASURED AND FOUND EXCEED LIMIT IAW CMM 57-52-03 REV 74. EXISTING HOLE DIAMETER 1.255", MAXIMUM HOLE DIAMETER 1.220". NEW BUSHING FABRICATEDSep 23, 2012 · N585FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201209233409Bushing · wornLEFT INBD FLAP, OTBD AFT (FLAP SIDE) HINGE PIVOT OTBD BUSHING WORN. REMOVED IAW CMM 20-20-07, REV 74. HOLE MEASURED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 74. EXISTING HOLE DIAMETER 1.254", MAXIMUM HOLE DIAMETER 1.220". NEW BUSHING FABRICATED AND INSSep 23, 2012 · N585FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201209233404Hinge Fitting · corrodedLEFT OTBD FLAP, INBD FORWARD (WING SIDE) HINGE ACTUATOR INBD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 74. EXISTING DIAMETER 1.228", FINAL DIAMETER 1.232", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED IAW EA 1-575Sep 23, 2012 · N585FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR IPXA2M75771Doubler · crackedINSPECTION TYPE: 3C LT WING FIXED L/E BEADED DOUBLER CRACKED NEAR XOS 693. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLERS BETWEEN XOS679-708 IAW STASA EA-011-5730-01-A4303 REV IR AND EO 5730-48823-A, FAA 8100-9. MAJOR.Sep 22, 2012 · N285UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2M75714Skin · crackedINSPECTION TYPE:3C, LT WING FIXED L/E INTERNAL SKIN SPLICE DOUBLER CRACKED NEAR XOS584. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FORMER IAW DWG ARB2931 AND ARM 51-33-01 (MINOR).Sep 22, 2012 · N285UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2M75709Doubler · crackedINSPECTION TYPE: 3C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED NEAR XOS613. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS 610-616 IAW SRM 57-40-02. REPAIR 15, FIG 203 (MAJOR).Sep 22, 2012 · N285UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2M75684Doubler · crackedINSPECTION TYPE: 3C, PREVIOUSLY INSTALLED REPAIR DOUBLER CRACKED IN LT WING FIXED L/E ON STRINGER, NEAR XOS906. REPLACED REPAIR DOUBLER IN LT WING FIXED L/E NEAR XOS906 IAW SRM 57-40-03, REPAIR 1, FIG 201. (MAJOR)Sep 22, 2012 · N285UP · Doug MD11F · Wing Miscellaneous StructureSDR IPXA2M75683Doubler · crackedINSPECTION TYPE:3C LT WING FIXED L/E BEADED DOUBLER CRACKED NEARS XOS628. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIG 203. (MAJOR)Sep 22, 2012 · N285UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2M75671Doubler · crackedINSPECTION TYPE: 3C, LEFT WING FIXED L/E BEADED DOUBLER CRACKED NEAR STA XOS 541. REPAIRED IAW SRM 57-40-02, REPAIR 15 FIG 203. (MAJOR)Sep 22, 2012 · N285UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2M75512Battery Pack · inoperativeDURING PDC, FOUND EMERGENCY LIGHT INOPERATIVE. R & R BATTERY POWER SUPPLY IAW MM 33-51-01-401. TEST SATISFACTORY.Sep 22, 2012 · N259UP · Doug MD11F · Emergency LightingSDR WRNA201200011Hydraulic Line · brokenHYD NR 3 FAIL DURING CRUISE, FL380 20 MIN FROM SVMI. AIRCRAFT RETURNED TO AIRFIELD, LANDING NORMAL. MX FOUND PIPE ASSY BROKEN, TO HORIZONTAL STAB TRIM MOTOR NR 1. REMOVED AND REPLACED HYD LINE IAW 27-43-04. PERFORMED SYSTEM TEST AND FUNCTIONAL TEST OF HORISep 22, 2012 · N950AR · Doug MD11F · Hydraulic System, MainSDR FDEA201209213382Beam · crackedCENTER CARGO DOOR ACTUATOR MOUNTING BEAM FOUND CRACKED AT BS 1746 TO 1750. REPAIRED AS PER EA 1-5310-162594. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.Sep 21, 2012 · N585FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201209213380Longeron · corrodedCENTER CARGO COMPARTMENT LONGERON 49 LEFT CORRODED AT BS 1531 TO 1541. REPAIRED IAW EA 1-5310-162591. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.Sep 21, 2012 · N585FE · Doug MD11F · Fuselage Main, Longeron/Stringer
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