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 IPXA13M78670Trunnion · crackedINSPECTION TYPE:2C, APPROX .5 INCH LONG CRACK AT TYPICAL CRACK LOCATION ON LT NLG TRUNNION FITTING. REPAIRED LT NLG TRUNNION FITTING REF SRM 53-10-14, REPAIR 2, FIG 202.May 17, 2013 · N251UP · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR IPXA13M78430Gauge · out of positionNR 1 DOOR SLIDE PRESSURE INDICATOR NOT READABLE. APPEARS SLIDE PACK HAS SHIFTED DOWN AND PRESSURE GAUGE IS NOT READABLE. REPOSITIONED AS MUSH AS POSSIBLE TO ALIGN PRESS GAUGE WITH INSPECTION. GAUGE IS NOW VIEWABLE THROUGH WINDOW REF AMM 25-23-07-401, 25-61-May 17, 2013 · N281UP · Doug MD11F · Escape SlideSDR IPXA13M78480Floorboard · puncturedINSPECTION TYPE:4C MAIN CABIN FLOORBOARD 263EF HAS ONE PUNCTURE. FABRICATED MAIN CABIN FLOORBOARD IAW EO MD11-5320-27386-C.May 16, 2013 · N271UP · Doug MD11F · Fuselage Floor PanelSDR FDEA201305151004Coalescer Bag · dirtyIN HIGH HUMIDITY CONDITIONS, APPROACHING GATE, COCKPIT FILLED WITH VISIBLE MOISTURE AND GOT MOMENTARY CABIN AIR SMOKE LIGHT AND WARNINGS. (NR 2 ENG WAS SHUTDOWN). R & R THE NR 1 WATER SEPARATOR COALESCER ASSY IAW AMM 21-54-05-01. OPS TEST NORMAL IAW AMM 21May 15, 2013 · N522FE · Doug MD11F · Humidity Control SystemSDR IPXA3M78333Brake · damagedNR 10 MAIN BRAKE FIRE AT BLOCK IN REMOVED NR 10 BRAKE IAW MM 32-43-20-000-802. INSPECTED AXLE AND SURROUNDING AREA NO DEFECTS NOTED INSTALLED NEW BRAKE IAW MM 32-43-20-400-802.May 15, 2013 · N286UP · Doug MD11F · Landing Gear Brake SystemSDR FDEA201305140986Hydraulic System · unknownAFTER LEVEL OFF, RECEIVED A HYD 3 LEVEL OFF, CHECKED NR 3 HYD FLUID, IT WAS DECREASING RAPIDLY. SHUTOFF NR 3 PUMPS AND RMPS. FLUID KEPT DECREASING TO 0. REPAIRED WIRING INSULATION AS NEEDED IAW SWPM 20-10-01. FINSHED INSTALL OF AC 601 APU IAW WC 49T1901. May 14, 2013 · N597FE · Doug MD11F · Hydraulic System, MainSDR IPXA3M78312Unknown · odorCREW COMMENTED SMELLING AN ACIDIC ELECTRICAL ODOR IN THE CONTROL PANEL DURING GEAR EXTENSION. QUICKLY DISSIPATED AFTER LANDING. VISUALLY INSPECTED INLET OF PACKS. RAN PACKS FOR AT LEAST .5 HR. CIRCUIT BREAKERS AND CFDS CHECKED, NO FAULT OR DISCREPANCY NOMay 14, 2013 · N292UP · Doug MD11F · Air Distribution SystemSDR IPXA3M78318Warning Light · false indicationDURING EMERGENCY LIGHT TEST, LEVEL 1 EMERGENCY LIGHT BATTERY 1 LOW DISPLAYED. ACCOMPLISHED SYS OPS TEST IAW AMM 33-51-700-802. ALL SYSTEMS OPS NORMAL.May 13, 2013 · N279UP · Doug MD11F · Emergency LightingSDR IPXA3M78510Wedge · dentedINSPECTION TYPE:2C, LT INBD FLAP SKIN DENTED (AT XIFH216). REPAIRED LT INBD FLAP, INBD WEDGE SKIN AT STA XIFH216 IAW STASA EA 011-5700 -01-A4636, REV IR AND EO MD11-5750-50859-A. (MAJOR)May 12, 2013 · N283UP · Doug MD11F · Trailing Edge FlapsSDR IPXA13M78456Door Frame · corrodedINSPECTION TYPE:2C, AFT/BULK CARGO DOOR FRAME CORRODED, BS 1954, L33L - L44L. R & R AFT CARGO DOOR FRAME IAW SRM 51-31- 01, 51-33-01, 51-35-01. (MINOR)May 10, 2013 · N283UP · Doug MD11F · Fuselage Main, StructureSDR FDEA201305100964Skin · crackedLEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 683.4 AND STA XORS=713.6, SIX FASTENER HOLES FOUND CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION. REPAIRED IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 52. REPAIR CLASSIFMay 10, 2013 · N644FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201305100963Skin · crackedRIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 683.4 AND STA XORS=713.6. THREE FASTENER HOLES FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION. REPAIRED IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 52. REPAIR CLMay 10, 2013 · N644FE · Doug MD11F · Wing, Plate/SkinSDR IPXA3M78545Longeron · corrodedINSPECTION TYPE:2C, LONGERON 48L CORRODED AT BS 1541. REMOVED FABRICATED AND INSTALLED REPLACEMENT SECTION OF LONGERON IAW DWG AFA7775, SRM 53-00-00, 53-00-05, 51-33-01.May 9, 2013 · N283UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA3M78511Skin · dentedINSPECTION TYPE:2C, 12 DENTS ON FUSELAGE EXTERIOR SKIN AFT OF BULK CARGO DOOR, BS 1958- 2007, L36L -L42L. REPAIRED FUSELAGE SKIN AT NOTED LOCATION IAW STASA EA 011-5330-01- A4630, REV IR AND EO MD11-5330-50829-A. FAA 8100-9 DATED 20 MAY 2013 (MINOR)May 9, 2013 · N283UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA13M78376Doubler · crackedINSPECTION TYPE:2C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 629. REPAIRED RT WING L/E INNER BEADED DOUBLER BETWEEN XOS 625-629 IAW SRM 57-40-02, REPAIR 15, FIG 203 (MAJOR).May 9, 2013 · N283UP · Doug MD11F · Wing, Plate/SkinSDR IPXA3M78349Doubler · crackedINSPECTION TYPE:2C, RT WING L/E INNER BEADED DOUBLER CRACKED INBD OF NR 11 SLAT TRACK REPAIRED RT WING L/E INNER BEADED DOUBLER BETWEEN STA XOS 698-703 IAW EO MD11-5730-48222-A.May 9, 2013 · N283UP · Doug MD11F · Wing, Plate/SkinSDR FDEA201305080941Frame · dentedMAIN DECK BS 1701, LONGERON 12R, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.May 8, 2013 · N644FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201305080940Frame · dentedMAIN DECK BS 1661, LONGERON 12R, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.May 8, 2013 · N644FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201305080939Frame · dentedMAIN DECK BS 1741, LONGERON 12L, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.May 8, 2013 · N644FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201305080938Frame · dentedMAIN DECK BS 1701, LONGERON 12L, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.May 8, 2013 · N644FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201305080937Frame · dentedMAIN DECK BS 1661, LONGERON 12L, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REVISION 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.May 8, 2013 · N644FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201305070928Skin · misrepairedFUSELAGE SKIN, BS 979, LONGERON 47-48R MISREPAIRED. REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 1 REV 52. EO 1-5100-7- 5001B3, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.May 7, 2013 · N580FE · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA3M78542Frame · crackedINSPECTION TYPE:4C FRAME AT BS 427.668 APPX 11 O'CLOCK POS IS CRACKED. REPAIRED FUSELAGE DROP CEILING FRAME AT BS 427.668 AT 11:00 POS REF EA 011-5310-01-A4625. REV I/R, EO MD11-5310-50864-A.May 6, 2013 · N271UP · Doug MD11F · Fuselage Main, FrameSDR FDEA201305060915Skin · crackedNR 3 AIRCONDITIONING COMPARTMENT AFT UPPER CORNER CUT-OUT SKIN FOUND CRACKED. NR 3 AIRCONDITIONING COMPARTMENT AFT UPPER CORNER CUT-OUT SKIN CARRIED OUT REPAIR IAW SRM 53-20-15, REPAIR 3, FIG 201, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.May 6, 2013 · N580FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201305060919Skin · corrodedRIGHT WING UPPER SURFACE FOUND CORROSION AT XORS 255 DURING SPOILER, UPPER SURFACE INSPECTION. CORROSION REMOVED AND FOUND EXCEED LIMITS IAW SRM 57-20-01, FIG 101, REV 52. DOUBLER REPAIR CARRIED OUT IAW EA 1-5730-167610. REPAIR CLASSIFIED AS MAJOR IAW GMM May 6, 2013 · N580FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201305060918Vane · delaminatedRT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. R & R RT WING INBD FLAP VANE IAW AMM 27-50-22-4, REV 76.1 CARRIED OUT FLAP VANE ADJUSTMENT TEST IAW AMM 27-50-22-5, REV 76.1. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 116.May 6, 2013 · N644FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201305060917Seat Track · corrodedCABIN - RT BS 1019 X= -8.5 SEAT TRACK FOUND CORROSION. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT BS 1009 TO 1049 IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REV 52 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.May 6, 2013 · N644FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201305060916Rib · wornRT WING NR 4 L/E SLAT INBD SLAT TRACK RIB FWD HOLE FOUND WORN AFTER REMOVAL OF NR 3 SLAT. NR 4 SLAT REWORKED IAW SRM 57-40-02 REPAIR 10, FIGURE 201, REVISION 52. FINAL HOLE DIAMETER 1.125" AND THE CHAFING MARK STILL EXIST, REPAIR ACCOMPLISHED IAW EA 1-5750-May 6, 2013 · N580FE · Doug MD11F · Leading Edge DevicesSDR FDEA201305050913Lamp · inoperativeRT DOOR ESCAPE SLIDE DID NOT TEST. REPLACED LAMPS FOR SLIDE TEST SWITCH, OPS CHECKED NORMAL.May 5, 2013 · N613FE · Doug MD11F · Escape SlideSDR FDEA201305040910Cap · misrepairedLT WING T/E LOWER ACCESS PANEL 541JB CUT-OUT FWD EDGE LOWER CAP MISREPAIRED. REPAIRED IAW EA 1-5710-167609. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.May 4, 2013 · N580FE · Doug MD11F · Wing Main, Frame StructureSDR IPXA13M78470Finger Doubler · corrodedINSPECTION TYPE:4C, FINGER DOUBLER HAS CORROSION ON UPPER SURFACE OF CENTER FUEL TANK AFT END 24" RT OF CENTER LINE. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER (PRODUCTION DOUBLER) ON UPPER SURFACE OF CENTER FUEL TANK AFT END 24 " RT OF CENTERLINE REF DWMay 3, 2013 · N271UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA13M78455Door Frame · crackedINSPECTION TYPE:4C, CRACK IN LIGHTNING HOLE FWD LOWER SIDE OF R3 DOOR FRAME AT BS 1254. REPAIRED LIGHTNING HOLE AT FWD LOWER SIDE OF R3 DOOR IAW SRM 53-40-15, REPAIR 3, FIG 201.May 3, 2013 · N271UP · Doug MD11F · Fuselage Main, StructureSDR FDEA201305030905Indicator · inoperativeLEFT SLIDE SYS PRESS-TO-TEST INDICATING SYS INOPERATIVE. R & R L1 SLIDE REMOTE PRESSURE INDICATOR IAW MM 25-61-04-4. OPS CHECK NORMAL IAW MM 25-61-04-5.May 3, 2013 · N608FE · Doug MD11F · Escape SlideSDR FDEA201305030903Rib · crackedRIGHT WING NR 5 SLAT FOUND INBD INNER RIB CRACKED. NR 5 SLAT FABRICATED AND INSTALLED IAW EA 1-5750-166127, STEP 2 AND 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.May 3, 2013 · N580FE · Doug MD11F · Leading Edge DevicesSDR FDEA201305030902Support Fitting · damagedMAIN CARGO DOOR LOWER FRAME SUPPORT FITTING NR 6 HOLE DIAMETER (D ) ABOVE THE LIMIT (0.580). R & R IAW SRM 51-31-01, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.May 3, 2013 · N580FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201305030901Support Fitting · damagedMAIN CARGO DOOR LOWER FRAME SUPPORT FITTING NR 1 HOLE DIAMETER ABOVE THE LIMIT (0.580). R & R IAW SRM 51-31-01, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.May 3, 2013 · N580FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201305030900Support Fitting · damagedMAIN CARGO DOOR LOWER FRAME SUPPORT FITTING NR 7 HOLE DIAMETER (A & C ) ABOVE THE LIMIT (0.580). R & R IAW SRM 51-31-01, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.May 3, 2013 · N580FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201305030899Skin · crackedNR 3 AIR CONDITIONING COMPARTMENT AFT UPPER CORNER CUT-OUT SKIN FOUND CRACKED. REPAIRED IAW SRM 53-20-15, REPAIR 3, FIG 201 REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 116.May 3, 2013 · N580FE · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA3M78501Skin · dentedINSPECTION TYPE:4C, CENTER CARGO DOOR DENTED ON LOWER EDGE BELOW FWD LOCK PIN WINDOW. REPAIRED DENT AT CENTER CARGO DOOR FWD LOWER CORNER AT APPROX STA 1717 REF STA SA EA 011-5231-01-A4621, REV IR, EO MD11-5230-50845-A.May 2, 2013 · N271UP · Doug MD11F · Cargo/Baggage DoorsSDR FDEA201305020898Fmu · faulted"FADEC ALT" MANUAL THROTTLES AT T/O NR 2 WOULD NOT ACHIEVE "MAX POWER" AT FADEC BAR, BOTH EPR & N1 NOTED BELOW NR 1 & 3 ENG. FADEC MODE IN NORMAL AND ALT. ALL ENGINE PARAMETERS WITHIN SPECIFIED LIMITS OUTLINED IN JRH. PERFORMED MAX POWER ASSURANCE RUN. NOTMay 2, 2013 · N643FE · Doug MD11F · Fuel Controlling SystemSDR FDEA201305020896Light · inoperativeL1 DOOR SLIDE REMOTE PRESSURE PRESS TO TEST INOPERATIVE. REPLACED LIGHT ASSY IAW MM 25-61-04 AND TESTED IAW MM 25-61-04-5.May 2, 2013 · N642FE · Doug MD11F · Escape SlideSDR IPXA3M78529Longeron Splice · crackedINSPECTION TYPE:4C, CENTER CARGO LONGERON SPLICE CRACKED AT L-40L AND STA 5-123. FABRICATED AND REPLACED CENTER CARGO COMPT LONGERON SPLICE AT L-40L AND STA 5-123 SRM 51-33-01, PARA 8.May 1, 2013 · N271UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA3M78509Longeron Splice · crackedINSPECTION TYPE:4C, LONGERON 33LT SPLICE FITTING CRACKED AT STA 5-123. REMOVED, FABRICATED AND INSTALLED REPLACEMENT L33L SPLICE FITTING AT STA 5-123 IAW DWG A5A7112 AND SRM 51-33-01. (MINOR)May 1, 2013 · N271UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA3M78500Skin · dentedINSPECTION TYPE:4C, RT FUSELAGE EXTERNAL SKIN DENTED AROUND RIVET HEAD, LOCATED 54' AFT OF AFT CARGO DOOR HINGE. REPAIRED RT FUSELAGE SKIN DENT BETWEEN STA 1821 TO 1841 AND L-27R TO L28R REF SRM 53-00-01, REPAIR 1, FIG 201 EA 01-5330-01-A4615 IR EO MD11-53May 1, 2013 · N271UP · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201305010893Beam · corrodedCENTER WHEEL WELL BS 1461 TO 1490 RT DIAGONAL I-BEAM FOUND CORRODED. R & R WITH NEW FABRICATED I-BEAM IAW SRM 51-31-01, REV 52 AND EA 1-53-167608. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.May 1, 2013 · N580FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201305010892Bulkhead · canningOIL CANNING AT CENTER LANDING GEAR RT VERTICAL WEB BETWEEN BS 1401 TO 1441, Z= -119 TO Z= -83. REPAIRED IAW EO 1-5100-7- 5001B3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.May 1, 2013 · N580FE · Doug MD11F · Fuselage Main, BulkheadSDR FDEA201305010891Bulkhead · canningOIL CANNING AT CENTER LANDING GEAR LT VERTICAL WEB BETWEEN BS 1401 TO 1441, Z= -119 TO Z= -80. CARRIED OUT INSPECTION IAW EA 1-5310-167604, REPAIRED IAW EO 1-5100-7-5001B3 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.May 1, 2013 · N580FE · Doug MD11F · Fuselage Main, BulkheadSDR IPXA3M78335Stringer · crackedINSPECTION TYPE: 4C, RT WING UPPER STRINGER CRACKED AT XORS 623 AT FUEL ACCESS PANEL 635BT. REPAIRED RT WING UPPER STRINGER 12 IAW SRM 57-00-03, REPAIR 5, FIG 202.Apr 30, 2013 · N271UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA3M78334Stringer · crackedINSPECTION TYPE: 4C, RT WING UPPER STRINGER 14 CRACKED AT ACCESS PANEL 634CT AT XORS 506. REPAIRED RT WING UPPER STRINGER IAW SRM 57-00-03, REPAIR 5, FIG 202.Apr 30, 2013 · N271UP · Doug MD11F · Wing, Longeron/StringerSDR CLCA20130430002Unknown · malfunctionedAFTER DEPARTING MIA, AND DURING CRUISE FLIGHT, LEVEL 1 ALERT 1, 2, 3 LHEDF OFF. ENGINE HYD PUMP CONTROL CIRCUIT BREAKER OUT. RETURNED TO MIA WITHOUT INCIDENT.Apr 30, 2013 · N984AR · Doug MD11F · Hydraulic System, Main
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