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 IPXA2017071419277Fuel Line · dentedINSPECTION TYPE:3C, CENTER TANK FUEL DISTRIBUTION PIPE HAD MULTIPLE DENTS. REPAIRED THE FUEL PIPE IAW EA 011-2820-01-A6886, REV IR, AND EO MD11-2820-64869-A.Jun 22, 2017 · N296UP · Doug MD11F · Aircraft Fuel Distribution SystemSDR IPXA2017071419276Stringer · crackedINSPECTION TYPE: 3C, STRINGER 47 CRACKED. REPAIRED THE STRINGER IAW SRM 57-10-03, REPAIR 1, FIG. 201. MAJOR.Jun 22, 2017 · N296UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2017071319260Longeron Splice · crackedINSPECTION TYPE: 3C, LONGERON SPLICE 51R CRACKED BS 1711. REMOVED AND REPLACED THE LONGERON SPLICE IAW SRM 51-33-01.Jun 22, 2017 · N296UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2017071419291Attach Angle · crackedINSPECTION TYPE: 3C, WING-TO-BODY FAIRING ATTACH ANGLE CRACKED BELOW THE R3 DOOR, BS 1281. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT ANGLE IAW DWG ANB7138, SRM 51-35-01, AND 51-31-01.Jun 22, 2017 · N296UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2017071219215Vent Line · dentedINSPECTION TYPE: 3C, CENTER TANK FUEL PIPE DENTED BETWEEN XCW 17 & 46. REPAIRED THE VENT PIPE IAW EA 011-2820-01-A6887, REV IR, AND EO MD11-2820-64865-A.Jun 22, 2017 · N296UP · Doug MD11F · Aircraft Fuel Distribution SystemSDR IPXA2017071019137Attach Bracket · crackedINSPECTION TYPE: 3C, EXTERIOR FUSELAGE,M RT BODY FAIRING ATTACH BRACKET IS CRACKED AT BS 1661. REMOVED, FABRICATED, AND REPLACED THE ATTACH BRACKET IAW DWG AFA7768, AND SRM 51-33-01.Jun 22, 2017 · N296UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2017071019135Sidewall Support · crackedINSPECTION TYPE: 3C, CENTER CARGO SIDEWALL SUPPORT ANGLE IS CRACKED AT BS 1821 LT SIDE. REMOVED, FABRICATED, AND REPLACED THE SIDEWALL SUPPORT IAW DWG AFA7295, AND SRM 51-33-01.Jun 22, 2017 · N296UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017071019133Sidewall Support · crackedINSPECTION TYPE: 3C, CENTER CARGO SIDEWALL SUPPORT ANGLE IS CRACKED AT BS 1781. REMOVED, FABRICATED, AND REPLACED THE SIDEWALL SUPPORT IAW DWG AFA0162, AND SRM 51-35-01.Jun 22, 2017 · N296UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017071019131Shear Tie · corrodedINSPECTION TYPE: 3C, CENTER CARGO BAY SHEAR TIE IS CORRODED AT BS 5-73 BETWEEN LONGERONS 48 - 49R. REMOVED, FABRICATED, AND REPLACED THE SHEAR TIE IAW DWG A5A7058-19, AND SRM 51-33-01. (MINOR)Jun 22, 2017 · N296UP · Doug MD11F · Fuselage Internal Mounting StructureSDR IPXA2017070819065Fitting · corrodedINSPECTION TYPE: 3C, FLOOR FITTING CORRODED. REMOVED AND REPLACED THE FLOOR FITTING REF EO MD11-2520-58701-DJun 22, 2017 · N296UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2017070819063Frame · corrodedINSPECTION TYPE: 3C, FRAME LOWER SUPPORT CORRODED BS 1781, LONGERON 50L - 50R. REPAIRED THE FRAME IAW SRM 53-00-07, REPAIR 5, FIG 202. MAJORJun 22, 2017 · N296UP · Doug MD11F · Fuselage Main, FrameSDR FDEA201706221739Door · chafedLOWER CENTER CARGO DOOR FWD LOWER EDGE CHAFED. REPAIRED IAW EA 1-5230-T0334004 PT1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 22, 2017 · N525FE · Doug MD11F · Cargo/Baggage DoorsSDR IPXA2017070518952Attach Angle · crackedINSPECTION TYPE: 3C, WING TO BODY PANEL ATTACH ANGLE BROKEN AT BS 1361. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT ATTACH ANGLE IAW DWG ANB7143, SRM 51-35-01, AND 51-31-01.Jun 22, 2017 · N296UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2017063018786Stiffener · crackedINSPECTION TYPE: 3C, RT WING FUEL ACCESS PANEL 634CT INTERNAL STIFFNER ANGLE IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE STIFFNER ANGLE IAW DWG ARB0358, SRM 51-35-01, AND 51-33-01.Jun 22, 2017 · N273UP · Doug MD11F · Wing Miscellaneous StructureSDR FDEA201706221750Door · damagedON AIRCRAFT ARRIVAL AT GATE, MX INFORMED CREW THAN THE NR 2 ENGINE PLATFORM FOR ACCESS ON ENGINE WAS OPEN. NO COCKPIT INDICATIONS, NO UNUSUAL FLIGHT CHARACTERISTIC DURING ANY PHASE OF FLIGHT. INSPECTED ALL DAMAGE TO THE NR 2 ENGINE PATIO DOORS AND WORK PLJun 22, 2017 · N604FE · Doug MD11F · Nacelle/Pylon, Main FrameSDR IPXA2017062318517Lamp · inoperativeEMERGENCY LIGHT INOPERATIVE AT COCKPIT DOOR. REPLACED THE LAMPS IAW MM 33-32-04. TESTED OK.Jun 22, 2017 · N279UP · Doug MD11F · Emergency LightingSDR FDEA201706221745Doubler · crackedLEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 646 FOUND CRACKED.Jun 22, 2017 · N525FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201706221744Doubler · crackedLEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 670 FOUND CRACKED.Jun 22, 2017 · N525FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201706221743Seat Track · crackedMAIN DECK FLOOR SEAT TRACK AT BS 635, LBL 27.5 FOUND CRACKED. SEAT TRACK SEGMENT CUT OUT BETWEEN BS 625 TO 665, AND REMOVED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. HFEC INSPECTION CARRIED OUT ON AREA FOUND NO CRACK EVIDENT. A NEW SEAT TRACK SEGMENT AND REJun 22, 2017 · N525FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201706221741Seat Track · crackedMAIN DECK FLOOR SEAT TRACK AT STA 695, X= -27.5 FOUND CRACKED.Jun 22, 2017 · N525FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201706221740Doubler · damagedMAIN DECK LEFT HAND FUSELAGE FRAME AT STA 535, L-24L FOUND REPAIR DOUBLER DAMAGED.Jun 22, 2017 · N525FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201706221738Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STA 1471, X= 8.5 FOUND CROWN DAMAGED.Jun 22, 2017 · N525FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201706221737Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STA 1134, X= 8.5 FOUND CROWN DAMAGED.Jun 22, 2017 · N525FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201706211723Warning System · false activationPDIS 575 32-30 4634 21JUN17 IND OPEN U ON TAKE OFF OUT OF JFK, WE HAD 4 UNSAFE GEAR INDICATIONS ON THE PRIMARY AND SECONDARY INDICATORS AFTER RAISING THE GEAR HANDLE. AS PER THE QRH, WE LOWERED THE GEAR HANDLE AND HAD 4 DOWN AND LOCKED. RAISED THE GEJun 21, 2017 · N575FE · Doug MD11F · Landing Gear Position and WarningSDR IPXA2017071219214Doubler · chafedINSPECTION TYPE: 3C, EXTENDED TAILCONE LT SIDE PREVIOUS INTERNAL REPAIR FOUND CHAFED. REMOVED AND REPLACED THE DOUBLER AT BS 2165 IAW EO MD11-5350-64832-A.Jun 21, 2017 · N296UP · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201706211733Seat Track · corrodedCABIN - RT STA 1199 X= -8.5 SEAT TRACK FOUND CORROSION. CABIN - RT STA 1199 X= -8.5 SEAT TRACK CORROSION FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CABIN - RT STA 1199 X= -8.5 DAMAGED FLOOR SEAT TRACK REPAIRED BY SECTIONAL REPLJun 21, 2017 · N521FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201706211732Seat Track · corrodedCABIN - RT STA 1441 X= -8.5 SEAT TRACK FOUND CORROSION. CABIN - RT STA 1441 X= -8.5 SEAT TRACK CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 AND REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1431 TO STJun 21, 2017 · N521FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201706211731Seat Track · corrodedCABIN - RT STA 5-43 X= -8.5 SEAT TRACK FOUND CORROSION. CABIN - RT STA 5-43 X= -8.5 SEAT TRACK CORROSION FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CABIN - RT STA 5-43 X= -8.5 DAMAGED FLOOR SEAT TRACK REPAIRED BY SECTIONAL REPLJun 21, 2017 · N521FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201706211730Seat Track · corrodedCABIN - RT STA 1551 X= -8.5 SEAT TRACK FOUND CORROSION. CABIN - RT STA 1551 X= -8.5 SEAT TRACK CORROSION FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CABIN RT STA 1551 X= -8.5 DAMAGED FLOOR SEAT TRACK REPAIRED BY SECTIONAL REPLAJun 21, 2017 · N521FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201706211724Seat Track · corrodedCABIN - RT STA 1531 X= -27.5 SEAT TRACK FOUND CORROSION. CABIN - RT STA 1531 X= -27.5 SEAT TRACK CORROSION FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED FLOOR SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-0 (STA Jun 21, 2017 · N521FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201706211722Doubler · crackedREWORK REQUIRED - RT WING LEADING EDGE INTERIOR BEADED DOUBLER AT APPROX STA XOS 550 UNDER REFUEL PANEL FOUND CRACKED. REPAIR CARRIED OUT AT RT WING LEADING EDGE INTERIOR BEADED DOUBLER AT APPROX XOS 550 PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIJun 21, 2017 · N619FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201706211736Brake Assy · defectiveSET TAKEOFF POWER AND AIRCRAFT IMMEDIATELY VEERED TO THE RIGHT. REJECTED TAKEOFF. BRAKES WORKED OK TAXIING BACK TO RAMP. ACCESSED CFDS & FOUND CURRENT FAULT "A/S VALVE SYS 3 08" W/ NO EIS ALERT NOTED. C/W RTS OF ASCU & OPS NORMAL & FAULT DISAPPEARED & NOT SHJun 21, 2017 · N610FE · Doug MD11F · BrakeSDR FDEA201706211729Monitor · failedDURING ADG CHECK WITH EMERGENCY INVERTER POWER CIRCUIT BREAKER PULLED, POWER WAS LOST TO THE LEFT AC AND ALL CAPTAIN'S DISPLAYS LOST POWER. AIR DRIVEN GENERATOR POWER MONITOR REMOVED AND REPLACED IAW AMM 24-25-06-4. ADG GROUND TESTED IAW AMM 24-25-00-700-802Jun 21, 2017 · N573FE · Doug MD11F · AC Generator-AlternatorSDR FDEA201706211728Battery Cable · arcedFOUND BATTERY B2-1 CONNECTOR P1-1805 NEGATIVE CONTACT HAD ARCING BURN, BATTERY SIDE CONTACT IS NORMAL. R & R THE BATTERY CONNECTOR .AND OPS TESTED NORMAL. NO DEFECTS FOUND IAW MM 24-34-02-5. ACFT OK FOR SERVICE.Jun 21, 2017 · N607FE · Doug MD11F · Electrical Power System WiringSDR FDEA201706201710Light · malfunctionedEMERGENCY LIGHT TEST DID NOT PASS. CARRIED OUT ADJUSTMENT TEST ON EMERGENCY LIGHTS IAW AMM 33-50-00-5. CHECKED GOOD.Jun 20, 2017 · N582FE · Doug MD11F · Emergency LightingSDR IPXA2017071619337Fitting · crackedINSPECTION TYPE: 3C, LONGERON 19R END FITTING CRACKED BETWEEN BS 1139 AND 6-90. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT END FITTING IAW EA 011-5310-01-A6875, REV IR, AND EO MD11-5310-64923-A. MAJOR.Jun 20, 2017 · N296UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2017071619336Frame · dentedINSPECTION TYPE: 3C, BS 655 FRAME DENTED ADJACENT TO LONGERON 12R. REPAIRED IAW EA 011-5310-01-A6872, REV IR, AND EO MD11-5310-64915-A. MAJOR.Jun 20, 2017 · N296UP · Doug MD11F · Fuselage Main, FrameSDR IPXA2017071419278Stringer · crackedINSPECTION TYPE: 3C, RIGHT WING STRINGER 16 CRACKED BETWEEN XORS 372 & 402. REPAIRED THE STRINGER IAW EA 011-5710-01-A6869, REV IR, AND EO MD11-5710-64900-A. MAJOR.Jun 20, 2017 · N296UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA2017071319258Tee Fitting · crackedINSPECTION TYPE: 3C, RIGHT WING T/E SUPPORT TEE CRACKED NEAR OPENING FOR PANEL 641BB. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT TEE IAW DWG ARC0341, AND SRM 51-33-01.Jun 20, 2017 · N296UP · Doug MD11F · Wing Miscellaneous StructureSDR IPXA2017070619006Longeron · corrodedINSPECTION TYPE: 3C, LONGERON 18R CORRODED BS 1189. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT LONGERON BETWEEN BS 1179 - 1199 IAW DWG AEA0220 AND SRM 51-33-01.Jun 20, 2017 · N296UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2017070619005Longeron · corrodedINSPECTION TYPE: 3C, LONGERON 18R CORRODED BS 1159 - 1179. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT LONGERON IAW DWG AEA0220, AND SRM 51-33-01.Jun 20, 2017 · N296UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2017070618989Longeron · corrodedINSPECTION TYPE: 3C, LONGERON 16R CORRODED AT BS 1179. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT LONGERON BETWEEN BS 1179 - 1199 IAW DWG AEA7065, AND SRM 51-33-01.Jun 20, 2017 · N296UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2017070518965Door Frame · crackedINSPECTION TYPE: 3C, L3 DOOR FRAME LOWER WEB IS CRACKED AT BS 1254, AND Z=-18. REPAIRED THE DOOR FRAME IAW SRM 53-40-15, REPAIR 3, FIG 201. MAJOR.Jun 20, 2017 · N296UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2017070518964Door Frame · crackedINSPECTION TYPE: 3C, R3 DOOR FRAME LOWER WEB IS CRACKED AT BS 1254 AND Z=-18. REPAIRED THE DOOR FRAME IAW SRM 53-40-15, REPAIR 3, FIG 201. MAJOR.Jun 20, 2017 · N296UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2017070318868Trunnion · crackedINSPECTION TYPE: 3C, LEFT NOSE LANDING GEAR TRUNNION FITTING IS CRACKED AT BS 582.5, Z=-114 AND RBL 24. REPAIRED THE TRUNNION FITTING IAW SRM 53-10-14, REPAIR 2, FIG 202. MAJOR.Jun 20, 2017 · N296UP · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR IPXA2017062118469Warning Message · false activationFOUND EMERGENCY LIGHT BATTERY 1 LOW ALERT DISPLAYED DURING TEST. TESTED IAW AMM 33-51-01-000.Jun 20, 2017 · N281UP · Doug MD11F · Emergency LightingSDR 9WGA5122017062101Engine · flamed outNR 1 ENGINE FLAMED OUT AT FL330 DURING DESCENT. RESTARTED AT FL170.Jun 20, 2017 · N512JN · Doug MD11F · Engine (Turbine/Turboprop)SDR IPXA2017071319257Skin · chafedINSPECTION TYPE: 3C, RT WING FIXED L/E SKIN IS CHAFED BEWTEEN XIS 158 & 163. REPAIRED THE RT WING FIXED L/E SKIN IAW EA 011-5730-01-A6861, REV I/R, AND EO MD11-5730-64872-A. MAJOR.Jun 19, 2017 · N296UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2017071119186Fairing · crackedINSPECTION TYPE: 3C, LT WING NR 1 SLAT PERFORMANCE FAIRING RIB IS CRACKED AT XIS 150.74. REPAIRED THE SLAT FAIRING IAW EA 011-5750-01-A6856, REV I/R, AND EO MD11-5750-64746-A.Jun 19, 2017 · N296UP · Doug MD11F · Leading Edge DevicesSDR IPXA2017071119185Skin · chafedINSPECTION TYPE: 3C, LT WING NR 8 SLAT INNER SKIN CHAFED AT XOS 1006.8 AND 1021.8. REPAIRED THE SLAT SKIN IAW EA 011-5754-01-A6871, REV I/R, AND EO MD11-5730-64833-A.Jun 19, 2017 · N296UP · Doug MD11F · Leading Edge Devices
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