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 FDEA201708312418Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER FOUND CRACKED AT XOS 627 - 628. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFED AS MAJOR IAW GMM 6-2-100.Aug 31, 2017 · N586FE · Doug MD11F · Wing, Plate/SkinSDR IPXA2017091321675Hinge Fitting · chafedINSPECTION TYPE: 3C, NR 3 NACELLE INBD FAN COWL FWD HINGE FITTING CHAFED. REPAIRED THE HINGE FITTING IAW EA 011-7110-01-A6987, REV IR, AND EO MD11-7110-65660-A.Aug 31, 2017 · N274UP · Doug MD11F · Nacelle/Pylon, Plate/SkinSDR FDEA201708312429Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STA 972, X=-47.5 FOUND CROWN DAMAGED AS MARKED. REPAIRED SEAT TRACK AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 31, 2017 · N586FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708312428Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STA 5-23, X=75.25 FOUND CROWN DAMAGED. REPAIRED SEAT TRACK AT EXISTING SPLICE STA 5-0, X=75.25 TO STA 5-63, X=75.25 AS PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 31, 2017 · N586FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708312419Former · crackedRT WING FIXED LEADING EDGE FORMER FOUND CRACK AT STA XOS 584 AS MARKED. REMOVED AND REPLACED WITH NEW FABRICATED FORMER PER SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. NEW FORMER PN: FX ARB2931-14 FABRICATED AS PER DRAWING ARB 2931 REV H.Aug 31, 2017 · N586FE · Doug MD11F · Wing Main, Frame StructureSDR IPXA2017090121239Fmc · malfunctionedDURING DECENT, FMC WOULD NOT ALLOW A SPEED GREATER THAN 310 KIAS. DID NOT FOLLOW PROFILE. PERFORMED RTS TEST BOTH FMCS PASSED, FMC SPEED ERROR INDUCED BY THE NR 3 MAIN FUEL TANK QTY INOPERATIVE TIP MESSAGE.Aug 31, 2017 · N273UP · Doug MD11F · Flight Management Computing Hardware SystemSDR FDEA201708302412Control Valve · failedAFTER TAKE OFF, RECEIVED A LEVEL 2 FLAP DISAGREE. MATCHED FLAPS BACK TO 10'. RAN QRH INBOARD FLAPS WOULD NOT MOVED PAST 10'. MADE A FLAPS 10'. LANDED AT THE NEAREST SUITABLE AIRPORT. INSTALLED A NEW INBOARD WING FLAP CONTROL VALVE IAW AMM 27-52-03-4. PERAug 30, 2017 · N529FE · Doug MD11F · Trailing Edge Flap Control SystemSDR IPXA2017082921129Warning System · false indicationR1 EVACUATION SLIDE REMOTE PRESS TO TEST INDICATING INOPERATIVE. PERFORMED A OOS CHECK OF THE L1 DOOR IAW AMM 52-10-01, NO DEFECTS NOTED.Aug 29, 2017 · N293UP · Doug MD11F · Emergency EquipmentSDR IPXA2017082921148Fmu · malfunctionedNUMBEROUS FAULTS DISPLAYED DURING FLIGHT ON NR 3 ENGINE. SELECT FADEC ALT RPM LO COMPLETED BOTH CHECKLISTS. ENGINE RELIGHT, NR 3 ENGINE FADEC MAINT REMAIN FOUND NR 3 ENG FADEC FAULT CODE 351-19 , FMU FF VALVE POS, TROUBLESHOT IAW FRM/FIM 73-21-00-101 STEPAug 29, 2017 · N289UP · Doug MD11F · Fuel Controlling SystemSDR IPXA2017082921089Skin · dentedDENT 4 INCHES INBD OF THE RT PITOT TUBE DOUBLER. REPAIR IAW EO MD11-5330-65425-AAug 29, 2017 · N260UP · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201708292410Bolt · missingNOSE LANDING GEAR FWD TOW HITCH RT ATTACH BOLT FOUND MISSING UPON ARRIVAL AT STATION. INSPECTED AND FOUND THE RT TOW LUG PIN MISSING AND LT PIN NUT LOOSE. ACCOMPLISHED HFEC OF RT AND LT TOW FITTING ATTACH LUGS NDTSPM PART 06. NO DEFECTS NOTED. INSTALAug 29, 2017 · N572FE · Doug MD11F · Nose/Tail Landing GearSDR FDEA201708292397Longeron · crackedLOWER FORWARD CARGO COMPARTMENT LT TUNNEL LONGERON 35L BETWEEN STA 899-919 FOUND WITH CORROSION. LONGERON CORRODED AREA CRACKED AND FOUND OUT-LIMIT PER SRM 53-00-00-2R FIG 205. REPAIR CARRIED OUT PER SRM 53-00-05-2R REPAIR 1 FIG 202. REPAIR CLASSIFIED AS MAJOAug 29, 2017 · N624FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2017082921080Drum · brokenR1 DOOR WILL NOT OPEN LOUD GRINDING NOISE. ACCOMPLISHED EO MD11-5210-65441-A THRU PARA 6 A (5) FINISHED REMAINING STEPS OF EO MD11-5210-65441-A. R&R BROKEN DOOR AFT CABLE DRUM AND SUPPORT ASSY ROLLER CHAIN GUARD BRACKET.Aug 28, 2017 · N283UP · Doug MD11F · Passenger/Crew DoorsSDR FDEA201708282392Longeron · crackedEXISTING LONGERON REPAIR AT FWD CARGO STA 1039 LONG 52. EXISTING LONGERON REPAIR AT FWD CARGO STA 1039 L52 EVALUATED AND FOUND CRACKED. FWD CARGO STA 1039 LONGERON 52 CARRIED OUT REPAIR AS PER SRM 53-00-05-2R FIG 202 REPAIR 1 EO 1-5100-7-5001 B6 PT1. REPAIR CAug 28, 2017 · N624FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201708282391Skin · dentedRT WING INBOARD AILERON ASSEMBLY LOWER SURFACE FOUND DENT AS MARKED. REPAIR CARRIED OUT AS PER EA 1-5750-T0335265-PT1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 28, 2017 · N624FE · Doug MD11F · AileronsSDR FDEA201708282386Seat Track · chafedCABIN STA 1401-1431, X=-8.5 SEAT TRACK FOUND CHAFFING AS MARKED. SEAT TRACK CHAFING FOUND EXCEED LIMIT AS PER SRM 53-00- 52-1A FIG 101 ALLOWABLE DAMAGED 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1391 TO STA 1431, X=-8.5 PER SRM 53-00-52-Aug 28, 2017 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708282390Doubler · crackedLT WING FIXED L/E LOWER SURFACE PANEL CUTOUT AT XOS 993 CRACKED AS MARKED. REPAIR CARRIED OUT ON LT WING FIXED LEADING EDGE LOWER SURFACE PANEL CUT OUT AT XOS 993 AS PER SRM 57-40-03-2R REPAIR 1 FIG 201. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.Aug 28, 2017 · N624FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708282389Seat Track · corrodedCABIN SEAT TRACK STA 5-113 TO 5-123, X=-8.5 FOUND CORROSION AS MARKED. REPAIR CARRIED OUT BY SECTIONAL REPLACEMENT FROM STA 5-83 TO STA 5-123, X=-8.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.Aug 28, 2017 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708282388Seat Track · chafedCABIN STA 1401-1431, X=-47.5 SEAT TRACK FOUND CHAFING AS MARKED. CHAFING FOUND EXCEED LIMIT PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1391 TO STA 1431, X=-47.5 PER SRM 53-00-52-2R FIG 201 REPAIR 1. REAug 28, 2017 · N624FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2017082821071Seal · brokenNR 4 EMERGENCY DESCENT DEVICE HAS A SEAL BROKEN. REMOVED & REPLACED THE DEVICE IAW MM 25-61-01, AND 25-61-01-01-030 K.Aug 28, 2017 · N284UP · Doug MD11F · Emergency EquipmentSDR IPXA2017082821052Lever · bindingL1 DOOR SLIDE ARMING HANDLE HAS RESISTANCE DURING ARM POSITION. EXERCISED SLIDE ARM LEVER, CHECKS OK IAW AMM 52-10-01,OK FOR SERVICE.Aug 26, 2017 · N292UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2017082720987Lamp · inoperativeL1 SLIDE PRESSURE LIGHT IS INTERMITTENT. REPLACED THE LAMP IN THE REMOTE PRESSURE INDICATOR IAW AMM 25 61 04 401, OPS NORMAL.Aug 26, 2017 · N270UP · Doug MD11F · Escape SlideSDR IPXA2017091421707Web · crackedINSPECTION TYPE: 3C, RIGHT OVERWING UPPER FUEL TANK AFT WEB IS CRACKED AT BS 1372 AND RBL 80. REPAIRED WEB IAW EO MD11-5710-65393-A. MAJOR.Aug 25, 2017 · N274UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017082520947Door · unknownL1 DOOR ELECTRIC DRIVE INOPERATIVE. PERFORMED AN OPS CHECK OF L1 PASSENGER DOOR IAW AMM 52-11-02 PB 201. FOUND GOOD.Aug 25, 2017 · N288UP · Doug MD11F · Passenger/Crew DoorsSDR FDEA201708252370Power Supply · failedEMERGENCY LIGHT TEST FAILED WITH EMERGENCY LIGHT BATTERY 1 LOW. REPLACED THE POWER SUPPLY IAW AMM 33-51-01-4, TESTED OK IAW AMM 33-50-00-5. ACFT OK FOR SERVICE.Aug 25, 2017 · N618FE · Doug MD11F · Emergency LightingSDR FDEA201708252356Lamp · inoperativeL1 MAIN CREW ENTRANCE SLIDE LIGHT WILL NOT TEST. RELACED THE LAMPS. CHECKED OK IAW MM 25-61-04-5. ACFT OK TO CONTINUE.Aug 25, 2017 · N614FE · Doug MD11F · Escape SlideSDR IPXA2017091521746Skin · chafedINSPECTION TYPE: C3, NR 2 PYLON BOX ASSY LT SKIN CHAFED BETWEEN YID 500 - 515 AND ZID 36 - 56. REPAIRED IAW EA 01-5430-01-A6964, REV IR, AND EO MD 11-5430-65689-A. MAJOR.Aug 24, 2017 · N274UP · Doug MD11F · Nacelle/Pylon, Plate/SkinSDR IPXA2017091521739Web · chafedINSPECTION TYPE: 3C, NR 2 PYLON WEB IS CHAFED BETWEEN YID=500 - YID=515 AND ZID=36 AND ZID=66. REPAIRED IAW EA 011-5430-01-A6971, REV I/R, AND EO MD11-5430-65657-A. MAJOR.Aug 24, 2017 · N274UP · Doug MD11F · Nacelle/Pylon Miscellaneous StructureSDR IPXA2017091321676Skin · corrodedINSPECTION TYPE: 3C, CENTER WING TANK UPPER FORWARD SKIN PANEL CORRODED JUST OUTBOARD OF XCW=100 ALONG STRINGER 16. REPAIRED IAW EA 011-5730-01-A6986 REV. IR AND EO MD11-5730-65658-A.Aug 24, 2017 · N274UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2017091221624Doubler · corrodedINSPECTION TYPE: 3C CENTER WING TANK PRODUCTION DOULBER HAS CORROSION AT BS 1371 AND LBL 55-76. REMOVED, FABRICATED AND REPLACED THE DOUBLER IAW DWG APB7241 AND SRM 51-31-01.Aug 24, 2017 · N274UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017090821472Floor Support · crackedINSPECTION TYPE: 3C, LOWER FWD CARGO BAY FLOOR SUPPORT CRACKED AT STATION 6-73, ADJACENT TO LONGERON 43L. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT FLOOR SUPPORT IAW DWG ADA7667, AND SRM 51-33-01.Aug 24, 2017 · N274UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017082520950Motor · inoperativeMOTOR DOES NOT RUN WHEN TEST BUTTONS ARE DEPRESSED. PRESSING RESET BUTTON, NO HELP. INSTALLED FO'S EVAS SYS IAW AMM 25-69-00.Aug 24, 2017 · N273UP · Doug MD11F · Emergency EquipmentSDR IPXA2017091521740Tee Fitting · corrodedINSPECTION TYPE: C3, FORWARD UPPER RUDDER AT ZFR=450.173 FRONT SPAR TEE ANGLE CORRODED. REMOVED, FABRICATED, AND REPLACED TEE ANGLE IAW DWG AMC7292 AND SRM 51-33-01.Aug 23, 2017 · N274UP · Doug MD11F · Rudder StructureSDR IPXA2017091421714Fitting · wornINSPECTION TYPE: 3C, RIGID CARGO BARRIER SIDE FITTING NR 8 WORN. REPAIRED THE CARGO BARRIER SIDE FITTING IAW EA 011-5340-01-A6979, REV I/R, AND EO MD11-5340-65640-A.Aug 23, 2017 · N274UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2017091521750Floorbeam · corrodedINSPECTION TYPE: 3C, AFT CARGO FLOORBEAM ANGLE AT BS 1842 AND LBL 7 IS CORRODED. REPAIRED THE FLOORBEAM ANGLE IAW EA 011-5310-01-A6977, REV I/R, AND EO MD11-5310-65694-A. MAJOR.Aug 23, 2017 · N274UP · Doug MD11F · Fuselage Main, Floor BeamSDR IPXA2017091321673Fitting · chafedINSPECTION TYPE: 3C, RCB NR 12 SIDE FITTING CHAFED. REPAIRED IAW EA 011-5340-01-A6978, REV IR, AND EO MD11-5340-65638-A.Aug 23, 2017 · N274UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2017091221628Support Angle · crackedINSPECTION TYPE: 3C, EXTERIOR FUSELAGE RT SIDE BS 1964, FAIRING SUPPORT ANGLE IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE FAIRING SUPPORT ANGLE IAW DWG AJC7405, AND SRN 51-33-01.Aug 23, 2017 · N274UP · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201708232316Skin · crackedDURING ACCOMPLISHMENT OF HFEC INSPECTION ON RT WING FIXED LEADING EDGE SKIN CUTOUT, FOUND 1 EA CRACK AT CORNER NR 2 SLAT ANTI-ICE TELESCOPING DUCT CUTOUT UPPER OUTBOARD CORNER, APPROX 0.6" IN LENGTH, AS MARKED. REPAIR CARRY OUT AS PER SRM 57-40-01-2R FIG 201 RAug 23, 2017 · N624FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708232315Skin · crackedDURING ACCOMPLISHMENT OF HFEC INSPECTION ON RT WING FIXED LEADING EDGE SKIN CUTOUT, FOUND 1 EA CRACK AT CORNER NR 1 SLAT ANTI-ICE TELESCOPING DUCT CUTOUT UPPER INBOARD CORNER, APPROX 0.6" IN LENGTH, AS MARKED. REPAIR CARRY OUT AS PER SRM 57-40-01-2R FIG 201 RAug 23, 2017 · N624FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708232314Doubler · crackedEXISTING REPAIR AT RT WING FIXED LEADING EDGE BEADED DOUBLER STA XOS 667 WITH 1 CRACK. REMOVED AND REPLACED WITH NEW BEADED DOUBLER AS PER SRM 57-40-02-2R REPAIR 15 FIG 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 23, 2017 · N624FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708232313Fitting · crackedNOSE LANDING GEAR LT FORWARD TRUNNION FITTING FOUND SUSPECTED CRACKED AS MARKED. CARRIED OUT REPAIR AS PER SRM 53-10-14-2R FIG 202 REPAIR 2. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 23, 2017 · N624FE · Doug MD11F · Main Landing Gear Attach SectionSDR FDEA201708232312Doubler · crackedLT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 626 CRACKED AS MARKED. BEADED DOUBLER AT XOS 626 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 23, 2017 · N624FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708232311Doubler · crackedLT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 640 CRACKED AS MARKED. BEADED DOUBLER AT XOS 640 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 23, 2017 · N624FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708232310Doubler · crackedRT WING FIXED LEADING EDGE COMPARTMENT AT STA XOS 627 BEADED DOUBLER FOUND CRACKED. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 23, 2017 · N624FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708232308Doubler · crackedRT WING FIXED LEADING EDGE COMPARTMENT AT STA XOS 645 BEADED DOUBLER FOUND CRACKED. BEADED DOUBLER REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 23, 2017 · N624FE · Doug MD11F · Wing, Plate/SkinSDR IPXA2017082320877Dump Valve · warning lightNR 2 DUMP VALVE LIGHT DISAGREE ILLUMINATED. CHECKLIST COMPLIED WITH.Aug 23, 2017 · N281UP · Doug MD11F · Aircraft Fuel Distribution SystemSDR IPXA2017090621422Longeron Splice · crackedINSPECTION TYPE: 3C, LONGERON SPLICE 6L FOUND CRACKED AT STATION 5-123. REMOVED, FABRICATED, AND REPLACED THE LONGERON SPLICE IAW DWG A5A7112, & SRM 51-31-01.Aug 23, 2017 · N274UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201708232320Former · crackedRT WING-FIXED LEADING EDGE COMPARTMENT AT STA XOS 1025 FORMER FOUND CRACKED. FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-0G. FORMER FABRICATED AS PER DWG ARB 2920 REV BB. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.Aug 23, 2017 · N624FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA201708232309Stiffener · crackedRT WING FIXED LEADING EDGE STA XOS 542 STIFFENER CRACKED. STIFFENER REMOVED AND REPLACED AS PER SRM 51-31-01-0G. STIFFENER FABRICATED AS PER DWG ARB2918 REV G. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100.Aug 23, 2017 · N624FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA201708232305Wedge · delaminatedLEFT WING TRAILING EDGE OTBD FLAP, INBD TRAILING EDGE WEDGE FOUND DELAMINATED AT XOF 460 - 468, TOP SURFACE. REPAIRED AND SMOOTHED IAW SRM 57-50-80-2R, REPAIR 1, PARA 4A (1)(A). PERMANENT REPAIR AND EA 1-5750-T0335176, P1. REPAIR CLASSIFIED AS MAJOR IAW Aug 23, 2017 · N584FE · Doug MD11F · Trailing Edge Flaps
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