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 FDEA201306201351Skin · misrepairedRUDDER SKIN MISREPAIRED. REPAIRED PER SRM 55-40-01 REPAIR 4 FIGURE 201 REVISION 52 AND EA1-5540-T0300978. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116.Jun 20, 2013 · N525FE · Doug MD11F · Rudder, Plate/SkinSDR IPXA13M78955Battery · inoperativeDURING EMERGENCY LIGHT TEST THE EMERGENCY LT BATT 1 LOW MESSAGE ILLUMINATED, COMPLIED WITH FIM 33-51-02-00. REPLACED EMERGENCY LIGHT BATTERY IAW AM AMM 33-51-01-00/400-802. OPS CHECKED GOOD.Jun 20, 2013 · N259UP · Doug MD11F · Emergency LightingSDR IPXA13M79143Skin · chafedINSPECTION TYPE:1C, RT WING FIXED L/E UPPER SURFACE IS CHAFED JUST INBD OF XORS 1094. REPAIRED RT WING FIXED L/E UPPER SUFACE JUST INBD OF XORS 1094, REF STASA, EA 011-5730-01-A4740, REV I/R, EO MD11-5730-51306-A AND FAA FORM 81 00-9.Jun 19, 2013 · N287UP · Doug MD11F · Wing, Plate/SkinSDR IPXA13M79139Skin · corrodedINSPECTION TYPE:1C, MAIN CABIN SUBFLOOR CENTER WING BOX UPPER SKIN CORRODED ABOVE STR17 AT RBL106. REPAIRED CORRODED CENTER WING UPPER WING IAW STASA EA 011-5730-01- A4738 REV IR AND EO MD11-5730-51290-A (MINOR).Jun 19, 2013 · N287UP · Doug MD11F · Wing, Plate/SkinSDR FDEA201306191346Uplock · inoperativeAFTER TAKEOFF, LEFT MAIN GEAR DID NOT RETRACT. RED LIGHT ON GEAR HANDLE SPOT AND RED LIGHT ON CONFIG PANEL. SPEED MAX 220. PERFORMED CHECKLIST. CHECKLIST WORKED. NORMAL FLT AND LANDING. REPLACED GEAR UNLOCK CYLINDER. OPS CHECKS NORMAL THROUGH LEAK CHECK Jun 19, 2013 · N596FE · Doug MD11F · Landing Gear Retraction/Extension SystemSDR FDEA201306191343Frame · dentedFRAME BS 1761, LONGERON 12L FOUND DENTED. REPAIRED IAW SRM 53- 00-07 FIGURE 201 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR AS IAW GMM 6-2-100 REVISION 116.Jun 19, 2013 · N645FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201306181332Frame · dentedFRAME, BS 1701, LONGERON 12R FOUND DENTED. REPAIR CARRIED OUT IAW SRM 53-00 07 FIGURE 201 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.Jun 18, 2013 · N645FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201306181330Stringer · misrepairedLEFT WING INBD FLAP FAIRING AFT LOWER AREA MISREPAIRED. SRM 51-31-01 REV.52 & EO1-5100-7-5001 B3 PART 1. .REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116Jun 18, 2013 · N525FE · Doug MD11F · Wing, Control SurfacesSDR FDEA201306181328Frame · dentedFRAME BS 1721, LONGERON 12R, FOUND DENTED. REPAIR CARRIED OUT IAW SRM 53-00 07 FIGURE 201 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.Jun 18, 2013 · N645FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201306181326Frame · dentedRIGHT FRAME BS 1641, LONGERON 12R FOUND DENTED. REPAIR CARRIED OUT IAW SRM 53-00 07 FIGURE 201 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.Jun 18, 2013 · N645FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201306181322Frame · chafedCABIN - LEFT SUPPORT YOKE, BS 535, LONGERON 19L, FRAME FOUND CHAFED. REPAIRED IAW SRM 53-20-07 FIGURE 202 REPAIR 1 REVISION 52. CLASSIFIED A MAJOR REPAIR IAW GMM 6-2-100 REVISION 116.Jun 18, 2013 · N645FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201306181331Frame · dentedFRAME BS 1681, LONGERON 12L FOUND DENTED. REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.Jun 18, 2013 · N645FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201306181329Frame · dentedFRAME BS 1701, LONGERON 12L FOUND DENTED. REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.Jun 18, 2013 · N645FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201306181324Frame · chafedLEFT SUPPORT YOKE BS 535, LONGERON 21L FRAME FOUND CHAFED. REPAIRED IAW SRM 53-20-07 FIGURE 201 REPAIR 1 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.Jun 18, 2013 · N645FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201306181319Skin · chafedLEFT INBD AILERON LOWER SKIN CHAFED AT TWO LOCATIONS. DAMAGED SKIN REMOVED AND FABRICATED NEW SKIN AS PER EA 1-5750-T0300853 AND REPLACED. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 116.Jun 18, 2013 · N645FE · Doug MD11F · AileronsSDR FDEA201306181333O-Ring · crackedTWENTY MINUTES AFTER TAKE OFF, LEVEL 1 "HYD 3 ELEV OFF" CHECKED QRH. ALSO NOTED A STEADY REDUCTION IN HYD 3 QTY, RETURNED TO DEPARTURE. ENROUTE, LEVEL 1"HYD 3 FAIL", COMPLIED WITH QRH AND LANDED. FOUND NR 3 HYD SYS PRESSURE TRANSDUCER (APTE-150-5000G) LOOSEJun 18, 2013 · N624FE · Doug MD11F · Hydraulic System, MainSDR FDEA201306181325Hinge Fitting · corrodedRIGHT WING OTBD FLAP AFT HINGE FWD MOUNT INBD (2A) FOUND WITH CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-04, REV 76. REPAIR ACCOMPLISHED IAW EA 1-5750-T0300851, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jun 18, 2013 · N525FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201306181318Fitting · corrodedRT WING OTBD FLAP VANE FITTING (F) MOUNTING HOLE FOUND WITH CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW SRM 57-50-02, FIG 201, REVISION 52. REPAIR BUSHING FABRICATED IAW SRM 57-50-02, FIG 201, REV 52 AND INSTALLED IAW AMM 27-50-02-04, REV 76.1. RT OTBJun 18, 2013 · N525FE · Doug MD11F · Trailing Edge FlapsSDR IPXA3M79089Doubler · crackedINSPECTION TYPE:1C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 664. REPAIRED LT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS 661-667 IAW SRM 57-40-02, REPAIR 15, FIG 203. (MAJOR)Jun 17, 2013 · N287UP · Doug MD11F · Wing, Plate/SkinSDR IPXA3M79043Vane · puncturedINSPECTION TYPE:1C, RT INBD FLAP VANE LOWER SURFACE PUNCTURED AT XIFH 194 15.5" FROM T/E. REPAIRED RT INBD FLAP VANE LOWER SKIN IAW SRM 57-50-80, REPAIR 2 WET. (MAJOR)Jun 17, 2013 · N287UP · Doug MD11F · Trailing Edge FlapsSDR IPXA3M78975Doubler · crackedINSPECTION TYPE:1C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED AT XOS 791.8529. REPAIRED LT WING FIXED L/E BEADED DOUBLER AT XOS 791.8529 REF EO MD11-5730-48222-A.Jun 17, 2013 · N287UP · Doug MD11F · Wing, Plate/SkinSDR FDEA201306171314Compensator · malfunctionedENROUTE, ONE HOUR NOTED FUEL REMAINING 2.5K BELOW PLANNED BURN. RECEIVED LEVEL 2 FUEL QUANTITY/USE CHECK AFTER. FOLLOWED QRH. ALL FUEL USED & TANK LEVEL SAME, MISSING 3.5K FUEL NOW. TANK 2 DROPPED FROM 8.7K - 6.5K IN 10-15 MIN, LOSING FUEL FASTER THAN BUJun 17, 2013 · N610FE · Doug MD11F · Fuel Indicating SystemSDR FDEA201306161311Skin · misrepairedLT WING INBD FLAP SKIN MISREPAIRED. REPAIRED IAW EA 1-5750-166138. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jun 16, 2013 · N525FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201306161310Bracket · corrodedRT WING-OTBD FLAP ASSY INBD AFT HINGE INBD LUG PIVOT BORE CORROSION AFTER REMOVAL OF OTBD FLAP ASSY. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04, REV.76. EXISTING HOLE DIAMETER 1.1525 INCH, FINAL HOLE DIAMETER 1.1605 INCH, MAXIMUM HOLE DIAMETER 1.15 IJun 16, 2013 · N572FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201306161313Hydraulic Line · failedWHEN CONFIGURING FOR LANDING, SLATS EXTENDED LOST THE NR 3 HYD SYS. RAN QRH PROCEDURES AND MANUALLY EXTENDED THE GEAR. REMOVED BROKEN LINE ON RT HOR STAB TRIM MOTOR AND CAPPED. CLEANED OUT HOR STAB AREA. INSTALLED NEW HYD LINE ON RT HOR. STAB TRIM MOTOR ANJun 16, 2013 · N589FE · Doug MD11F · Hydraulic System, MainSDR FDEA201306161312Fire Loop · false activationLEVEL 1, FIRE DETECTION 1 FAIL APPROX 5 MINUTES AFTER TAKEOFF FOLLOWED BY INTERMITTENT ENGINE 1 FIRE WARNING (ENGINE OPERATING INDICATIONS WERE NORMAL). ALL INDICATIONS STOPPED UNTIL FINAL APPROACH, AT WHICH TIME HAD INTERMITTENT LEVEL 1, FIRE DETECT 1, FAIJun 16, 2013 · N606FE · Doug MD11F · Fire DetectionSDR FDEA201306161309Skin · crackedTEN FASTENER HOLES FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT(HFEC) INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 683.4 AND 713.6. REPAIRED IAW SRM 57-20-02, REPAIR 5, FIG 201, REV 52. REPAIR CLASSIFIED MAJOR IJun 16, 2013 · N525FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201306161308Skin · crackedNINE FASTENER HOLES FOUND CRACK INDICATION. DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 683.4 AND 713.6. REPAIRED IAW SRM 57-20-02, REPAIR 5, FIG 201, REV 52. REPAIR CLASSIFIED MAJOR IJun 16, 2013 · N525FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201306161307Wedge · delaminatedLEFT WING OTBD FLAP UPPER SURFACE INBD LOWER T/E CORNER DELAMINATED. REPAIRED IAW EA 1-5750-T0300875. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REV 116.Jun 16, 2013 · N525FE · Doug MD11F · Trailing Edge FlapsSDR IPXA13M79128Doubler · crackedINSPECTION TYPE:1C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 631. REPAIRED LT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS 629 - 633 IAW STASA, EA 011-5730-01-A4730 REV IR AND EO MD11-5730-51278-A.Jun 15, 2013 · N287UP · Doug MD11F · Wing, Plate/SkinSDR IPXA13M79127Doubler · crackedINSPECTION TYPE:1C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 640. REPAIRED LT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS636 -643 IAW STASA EA 011-5730-01-A4731, REV IR AND EO MD11-5730-51294-A.Jun 15, 2013 · N287UP · Doug MD11F · Wing, Plate/SkinSDR FDEA201306151302Structure · corrodedRIGHT WING OTBD FLAP, INBD FWD (WING SIDE) HINGE ACTUATOR HOLE INBD BORE CORROSION.Jun 15, 2013 · N525FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201306151301Structure · corrodedRIGHT WING OTBD FLAP, INBD FWD (WING SIDE) HINGE PIVOT HOLE BORE CORROSION.Jun 15, 2013 · N525FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201306151300Hinge · corrodedRIGHT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE PIVOT HOLE CORRODED. REWORKED IAW CMM 57-44-09, REV 76. FOUND OUT OF LIMITS. REPAIRED IAW EA 1-5750-T0300831, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jun 15, 2013 · N525FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201306151299Bulkhead · canningCENTER LANDING GEAR WHEEL WELL-OIL CANNING FOUND AT RT KEEL BEAM WEB , X=31.50, STA.Y=1435, 43" ABOVE FWD DOOR HINGE LINE. OIL CANNING MEASURED 0.228", MAXIMUM ALLOWABLE 0.19". REPAIRED IAW EA 1-5310-T0300744, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100Jun 15, 2013 · N525FE · Doug MD11F · Fuselage Main, BulkheadSDR FDEA201306151298Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE ACTUATOR HOLE OTBD BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-09, REV 76. REPAIR ACCOMPLISHED IAW EA 1-5750-T0300829, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jun 15, 2013 · N525FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201306151297Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD (WING SIDE) HINGE ACTUATOR HOLE INBD BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-09 REV 76. REPAIR ACCOMPLISHED IAW EA 1-5750-T0300829, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jun 15, 2013 · N525FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR IPXA3M79052Door Frame · crackedINSPECTION TYPE:4C, R-3 FWD LOWER DOOR JAMB CRACKED. REPAIRED R-3 FWD LOWER DOOR JAMB REF SRM 53-40-15, REPAIR 3, FIG 201.Jun 14, 2013 · N274UP · Doug MD11F · Fuselage Main, StructureSDR FDEA201306141290Frame · misrepairedMAIN DECK CARGO BS 535, L19LT FRAME MISREPAIRED. REPAIRED IAW SRM 53-20-07, FIG 202, REPAIR 1, REV 52 EO 1-5100-7-5001, B3 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jun 14, 2013 · N525FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201306141289Frame · misrepairedMAIN DECK CARGO BS 535, L24L FRAME MISREPAIRED. REPAIRED IAW SRM 53-20-07, FIG 201, REPAIR 1, REV 52, EO1-5100-7-5001, B3 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jun 14, 2013 · N525FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201306141285Doubler · crackedLEFT WING FIXED L/E COMPARTMENT STATION XOS 755, BEADED DOUBLER CRACKED. REPAIRED AS PER SRM 57-40-02, FIGURE 203, REPAIR 15, REV.52. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV.116.Jun 14, 2013 · N572FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201306141291Hinge · corrodedLEFT WING OTBD FLAP FWD (WING) HINGE PIVOT HOLE BORE CORROSION. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-09, REV 76. REPAIR ACCOMPLISHED IAW EA 1-5750-T0300829, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.Jun 14, 2013 · N525FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201306141288Support Fitting · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION, OPEN HOLE INSPECTION CARRIED OUT AND FOUND NR 7 LOWER CARGO DOOR FRAME SUPPORT FITTING HOLE "C" WITH CRACK INDICATION AT 12 O'CLOCK POSITION (PLAIN VIEW) AND APPROX 0.080" IN LENGTH. R & R IAW SRM 51-31-01, REV 5Jun 14, 2013 · N525FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201306141287Support Fitting · crackedDURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT AND FOUND NR 4 LOWER CARGO DOOR FRAME SUPPORT FITTING HOLE "D" WITH CRACK INDICATION AT 1 O'CLOCK POSITION AND APPROX 0.085" IN LENGTH. R & R IAW SRM 51-31-01, REV 52 REPAIR CLASSIFIED MAJOR Jun 14, 2013 · N525FE · Doug MD11F · Fuselage Main, StructureSDR IPXA13M79197Vane · delaminatedINSPECTION TYPE:4C, RT WING INBD FLAP VANE IS DELAMINATED AT STA. XIFH 191 LOWER SURFACE. REMOVED DAMAGE AND REPAIRED IAW SRM 57-50-80, EA 011-5753-01- A4734, REV IR AND EO MD11-5750-51342-A.Jun 13, 2013 · N274UP · Doug MD11F · Trailing Edge FlapsSDR IPXA13M79137Floor Panel · corrodedINSPECTION TYPE:2C, CORROSION ON RCB FLOOR PANEL WSP0789-501, BS 479, LBL48. R & R FLOOR PANEL IAW DWG SP11530078-7005.Jun 13, 2013 · N252UP · Doug MD11F · Fuselage Floor PanelSDR IPXA13M79111Vane · delaminatedINSPECTION TYPE:4C LT IB FLAP VANE LOWER SKIN DELAMINATED AT XIFH 186, 13" FROM T/E REPAIRED LT IB FLAP VANE SKIN PER MD11 SRM 57-50-80 REPAIR 2 FIG.201 (MAJOR)Jun 13, 2013 · N274UP · Doug MD11F · Trailing Edge FlapsSDR IPXA3M79079Floor Panel · corrodedINSPECTION TYPE:4C, CORRODED FLOOR PANEL AT BS 482 AND LBL 62. R & R FLOOR PANEL IAW EO MD1 1-5330-27218-D.Jun 13, 2013 · N252UP · Doug MD11F · Fuselage Floor PanelSDR FDEA201306131270Door Frame · crackedMAIN DECK DOOR NR 3 RT AFT DOOR JAMB LOWEST LIGHTENING HOLE FOUND CRACKED. REPAIRED AS PER SRM 53-40-15, FIGURE 201, REPAIR 3, REV.52. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV.116.Jun 13, 2013 · N572FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201306131269Door Frame · crackedMAIN DECK DOOR NR 3 RT FWD DOOR JAMB LOWEST LIGHTENING HOLE FOUND CRACKED. MAIN DECK DOOR 3R BS 1256.75, LONGERON 27 CRACK WEB REPAIRED AS PER SRM 53-40-15, FIGURE 201, REPAIR 3, REV.52. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV.116.Jun 13, 2013 · N572FE · Doug MD11F · Fuselage Main, Structure
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