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 IPXA2016101009190Skin · corrodedINSPECTION TYPE: 3C, MAIN CABIN CENTER WING UPPER SKIN HAS CORROSION AT STRINGER 15 & XCW-4 TO XCW 39. REPAIRED THE SKIN IAW EA 011-5730-01-A6498 REV. I/R AND EO MD11-5730-62088-A.Sep 16, 2016 · N258UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2016101109236Rib · corrodedINSPECTION TYPE: 3C, RIB CORRODED INSIDE UPPER FWD RUDDER. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT RIB IAW DWG AMC7292 AND SRM 51-35-01.Sep 16, 2016 · N258UP · Doug MD11F · Rudder, Spar/RibSDR IPXA2016101109228Intercostal · crackedINSPECTION TYPE: 3C, INTERCOSTAL IS CRACKED IN FWD CARGO BAY BS 655 - 675 L42 - 43L. REMOVED, FABRICATED AND REPLACED THE INTERCOSTAL IAW DWG ACA7049 AND SRM 51-33-0.Sep 16, 2016 · N258UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016101209279Longeron · crackedINSPECTION TYPE: 3C, MAIN CABIN LONGERON 27L IS CRACKED BELOW THE L3 DOOR. REMOVED, FABRICATED AND REPLACED THE LONGERON IAW DWG AEA7127 AND SRM 51-33-01.Sep 16, 2016 · N258UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2016101109219Rib · crackedINSPECTION TYPE: 3C, MULTIPLE DAMAGES ON THE NR 3 PYLON FAIRING 189AL RIB. REMOVED AND REPLACED THE RIB IAW SRM 54-01-42.Sep 16, 2016 · N258UP · Doug MD11F · Nacelle/Pylon, Main FrameSDR IPXA2016100809084Barrier · crackedINSPECTION TYPE: 3C. RCB LOWER FWD CLOSE-OUT CRACKED AT X=18RCB. REPAIRED IAW SRM 53-20-53 REPAIR 1 FIG. 201. (MAJOR)Sep 16, 2016 · N258UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016100809082Skin · corrodedINSPECTION TYPE: 3C, CENTER WING TANK UPPER SKIN CORRODED AT XCW 118 ALONG STRINGERS 3, 4, 9. THE SKIN REPAIRED IAW EA 011-5730-01-A6489 REV. IR AND EO MD11-5730-62061-A.Sep 16, 2016 · N258UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2016100809099Longeron · crackedINSPECTION TYPE: 3C. LONGERON 27R CRACKED BELOW R3 DOOR. REMOVED FABRICATED AND INSTALLED A REPLACEMENT LONGERON IAW DWG AEA7127 AND SRM 51-33-01.Sep 16, 2016 · N258UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2016100609001Skin · corrodedINSPECTION TYPE :3C, CENTER WING UPPER EXTERIOR SKIN CORRODED ALONG STRINGER 15 AT XCW-49. REPAIRED IAW EA 011-5730-01-A6482 REV. IR AND EO MD11-5730-62040-A.Sep 16, 2016 · N258UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2016100609000Skin · corrodedINSPECTION TYPE: 3C, CENTER WING UPPER EXTERIOR SKIN CORRODED ALONG STRINGER 17 BETWEEN XCW-20 AND -23. REPAIRED IAW EA 011-5730-01-A6482 REV. IR AND EO MD11-5730-62040-A.Sep 16, 2016 · N258UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2016100608999Skin · corrodedINSPECTION TYPE: 3C, CENTER WING UPPER EXTERIOR SKIN CORRODED ALONG STRINGER 15 AT XCW-5, -21, -30. REPAIRED IAW EA 011-5730-01-A6482 REV. IR AND EO MD11-5730-62040-ASep 16, 2016 · N258UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2016100709061Channel · crackedINSPECTION TYPE: 3C, FWD CARGO BAY CEILING PANEL SUUPORT CHANNEL CRACKED BS 919 X-65. REPAIRED IAW EA 011-2552-01-A6481 REV. IR AND EO MD11-2550-62058-A.Sep 16, 2016 · N258UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2016100208842Intercostal · crackedINSPECTION TYPE:3C, INTERCOSTAL CRACKED STA 6-30 - 6-50 BETWEEN L42L AND L43L. REMOVED FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW DWG ACA7049 AND SRM 51-33-01 (MINOR).Sep 16, 2016 · N258UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2016100208841Structure · crackedINSPECTION TYPE:3C, MULTIPLE CRACKS AND AREAS OF CORROSION ON LOWER LT SIDE OF LOWER AFT RUDDER . REMOVED AND REPLACED IAW AMM 27-20-20-4019 (MINOR).Sep 16, 2016 · N258UP · Doug MD11F · Rudder StructureSDR IPXA2016100208840Intercostal · crackedINSPECTION TYPE:3C, INTERCOSTAL CRACKED STA. 6-10 - 6-30 BETWEEN L42L AND L43L. REMOVED FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-33-01 AND DWG ACA7049 (MINOR)Sep 16, 2016 · N258UP · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201609163269Angle · dentedCABIN - MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR ANGLE DENTED AT LT STA 1701, LONGERON 12L. FRAME REPAIR ANGLE REMOVED PER SRM 51-33-01-0G AND REPAIRED PER SRM 53-00-07-2R FIG 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 16, 2016 · N617FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201609163286Battery · dischargedPRE-FLIGHT EMERGENCY LIGHT TEST BATTERY 1 LO. R & R POWER SUPPLY EMERGENCY LIGHT BATTERY REF MM 33-51-01-4 , OP CHECK GOOD. PART MFG, P/N 60-4411-5, SN 2068. R & R POWER SUPPLY EMERGENCY LIGHT BATTERY REF MM 33-51-01-4 , OPS CHECK GOOD.Sep 16, 2016 · N609FE · Doug MD11F · Emergency LightingSDR FDEA201609163283Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER BARREL NUT HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328319 PART 1, STEP 1C.Sep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163282Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER BARREL NUT HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0328319 PART 1, STEP 1C.Sep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163281Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, FWD MOUNT OTBD HOLE BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR WAS BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0328319 PART 1, STEP 1B.Sep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163280Hinge · corrodedRIGHT WING OTBD FLAP, INBD FORWARD HINGE, WING SIDE LOWER MOUNT INBD HOLE BORE CORRODED. REWORKED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. FABRICATED A REPAIR BUSHING AND INSTALLED IAW EA 1-5750-T0328311 PART 1 STEP 1.Sep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163279Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE, WING SIDE LOWER MOUNT OTBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE: DIA 0.707", FINAL HOLE: DIA 0.729", MAXIMUM ALLOWABLE HOLE: DIA 0.709". REPAIR BUSHING FABRICATED ANDSep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163278Hinge · corrodedRIGHT WING OTBD FLAP, INBD FORWARD HINGE, WING SIDE ACTUATOR INBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE: DIA 1.246", FINAL HOLE: DIA 1.250", MAXIMUM ALLOWABLE HOLE: DIA 1.220". REPAIR BUSHING FABRICATED ASep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163277Hinge · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE ACTUATOR OTBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIA 1.220", FINAL HOLE: DIA 1.224", MAXIMUM ALLOWABLE HOLE: DIA 1.220". REPAIR BUSHING FABRICATED ANSep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163276Hinge · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE ACTUATOR INBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE: DIA 1.249", FINAL HOLE: DIA 1.252", MAXIMUM ALLOWABLE HOLE: DIA 1.220". REPAIR BUSHING FABRICATED AND ISep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163275Hinge · corrodedRT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE LOWER BARREL NUT HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE: DIA 0.406", FINAL HOLE: DIA 0.421", MAXIMUM ALLOWABLE HOLE: DIA 0.391". REPAIR BUSHING FABRICATED AND ISep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163274Hinge Bracket · corrodedRT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE UPPER BARREL NUT HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIA 0.406", FINAL HOLE: DIA 0.421", MAXIMUM ALLOWABLE HOLE: DIA 0.391". REPAIR BUSHING FABRICATED ANSep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163273Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE LOWER MOUNT, OTBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIA 0.582", FINAL HOLE: DIA 0.598", MAXIMUM ALLOWABLE HOLE: DIA 0.584". REPAIR BUSHING FABRICATESep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163272Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE LOWER MOUNT INBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE: DIA 0.582", FINAL HOLE: DIA 0.598", MAXIMUM ALLOWABLE HOLE: DIA 0.584". REPAIR BUSHING FABRICATEDSep 16, 2016 · N617FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201609163271Door Frame · crackedR3 DOOR AFT LOWER FUSELAGE FRAME WEB CRACKED AT BS 1310, BETWEEN LONGERONS 2R AND 27R. REPAIRED IAW SRM 53-40-15-2R, FIG 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 16, 2016 · N617FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201609163270Angle · dentedCABIN, MAIN DECK CARGO COMPARTMENT FRAME EXISTING REPAIR ANGLE DENTED AT RT STA 1681, LONGERON 12R. FRAME ANGLE REMOVED PER SRM 51-33-01-0G AND REPAIRED PER SRM 53-00-07-2R FIG 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 16, 2016 · N617FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201609163268Frame · dentedCABIN MAIN DECK CARGO COMPARTMENT FRAME DENTED AT LT STA 1059, LONGERON 12L. FRAME REPAIRED PER SRM 53-00-07-2R FIG 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 16, 2016 · N617FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201609163267Frame · dentedCABIN, MAIN DECK CARGO COMPARTMENT FRAME DENTED AT LT STA 5-11, LONGERON 12L. FRAME REPAIRED PER SRM 53-00-07-2R FIG 201 REPAIR 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 16, 2016 · N617FE · Doug MD11F · Fuselage Main, FrameSDR IPXA2016101409364Ring · chafedINSPECTION TYPE: 3C, NR 2 ENGINE BELLMOUTH RING CHAFED ON FREE FLANGE 6:00 POSITION. THE DAMAGE WAS REPAIRED IAW EA 011-5410-01-A6501 REV. IR AND EO MD11-5410-62078-A.Sep 15, 2016 · N258UP · Doug MD11F · Nacelle/Pylon, Main FrameSDR IPXA2016101409357Skin · corrodedINSPECTION TYPE: 3C, RT AFT EXTERIOR FUSELAGE SKIN CORRODED BS 2135 - 2163 LONGERON 33 - 35R. REPAIRED THE SKIN IAW EA 011-5330-01-A6484 REV. IR AND EO MD11-5330-62117-A. (MAJOR)Sep 15, 2016 · N258UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2016101109263Access Panel · chafedINSPECTION TYPE: 3C, NR 3 PYLON ACCESS PANEL AT YN2=295 & YN2=300 HAS CHAFE DAMAGE. REPAIRED THE ACCESS PANEL IAW EA 011-5430-01-A6494 REV. I/R AND EO MD11-5430-62031-A.Sep 15, 2016 · N258UP · Doug MD11F · Nacelle/Pylon, Plate/SkinSDR IPXA2016101209289Skin · corrodedINSPECTION TYPE: 3C, FUSELAGE SKIN AT BS 2046 - 2140 CORRODED BETWEEN LONGERON 10 - 12R. REPAIRED IAW EA 011-5330-01-A6497 REV. I/R AND EO MD11-5330-62102-A. (MAJOR)Sep 15, 2016 · N258UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2016101109250Rib · crackedINSPECTION TYPE: 3C, RT WING NR 1 SLAT PERFORMANCE FAIRING RIB IS CRACKED. REPAIRED THE RIB IAW EA 011-5750-01-A6459 REV. I/R AND EO MD11-5750-62089-A.Sep 15, 2016 · N258UP · Doug MD11F · Leading Edge DevicesSDR IPXA2016100809090Intercostal · crackedINSPECTION TYPE:3C. INTERCOSTAL CRACKED IN RT SIDE OF VERTICAL STAB . REPAIRED THE INTERCOSTAL IAW EA 011-5530-01-A6456 REV. IR AND EO MD11-5530-62062-A. (MAJOR)Sep 15, 2016 · N258UP · Doug MD11F · Vertical StabilizerSDR IPXA2016101009186Torque Ring · damagedINSPECTION TYPE: 3C. NR 2 ENGINE RT THRUST REVERSER OUTER RING OF TORQUE BOX (FWD CASCADE SUPPORT RING) PUNCTURED & GOUGED. REPAIRED THE TORQUE RING IAW EA 011-7830-01-A6474 REV. I/R AND EO MD11-7830-62066-A. (MINOR)Sep 15, 2016 · N258UP · Doug MD11F · Engine Thrust ReverserSDR IPXA2016101009185Skin · corrodedINSPECTION TYPE: 3C. LEFT WING UPPER SKIN BETWEEN XORS 230-264 AND STRINGER 1 TO REAR SPAR HAS CORROSION. REPAIRED THE SKIN IAW EA 011-5730-01-A6488 REV. I/R AND EO MD11-5730-62080-A.Sep 15, 2016 · N258UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2016101009170Skin · damagedINSPECTION TYPE: 3C. RT WING L/E SKIN REPAIR DOUBLER AT XIS 165-172 IS BENT AND CHAFED. REMOVED, FABRICATED AND REPLACED THE REPAIR DOUBLER IAW EA 011-5730-01-A6460 REV. I/R AND EO MD11-5730-62082-A.Sep 15, 2016 · N258UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2016100508964Skin · chafedINSPECTION TYPE:3CCHAFE DAMAGE AND LOOSE RIVETS ON RT DROOP LEADING EDGE EXTERIOR SKINS. REPAIRED IAW SRM 57-40-01 REPAIR 15 FIG. 202 (MAJOR)Sep 15, 2016 · N258UP · Doug MD11F · Leading Edge DevicesSDR IPXA2016093008783Skin · corrodedINSPECTION TYPE:3C, LT WING UPPER EXTERNAL SKIN CORRODED STA XORS 163 - 170 BETWEEN STR 2 AND 3. CORROSION REPAIRED PER EA 011-5730-01-A6467 REV IR AND EO 5730-61992-A. (MINOR)Sep 15, 2016 · N258UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2016092708721Door Frame · crackedINSPECTION TYPE: 3C, R3 DOOR INNER FRAME WEB CRACKED BS 1256 Z -16. REPAIRED THE DOOR FRAME WEB IAW SRM 53-40-15 REPAIR 3 FIG. 201 (MAJOR).Sep 15, 2016 · N258UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2016092408583Door Frame · crackedINSPECTION TYPE: 3C, R3 DOOR FRAME INNER WEB CRACKED AT FLOOR LEVEL LIGHTENING HOLE BS 1305. CRACKED WEB REPAIRED IAW SRM 53-40-15 REPAIR 3 FIG. 201 (MAJOR).Sep 15, 2016 · N258UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2016092408582Door Frame · crackedINSPECTION TYPE: 3C, L3 DOOR FRAME INNER WEB CRACKED AT FLOOR LEVEL LIGHTENING HOLE BS 1305. WEB REPAIRED IAW SRM 53-40-15 REPAIR 3 FIG. 201 (MAJOR).Sep 15, 2016 · N258UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2016091608306Battery · dischargedL1 DOOR SLIDE BATTERY DOES NOT TEST. REPLACED LAMPS AND BATTERIES IN L1 SLIDE REMOTE PRESSURE INDICATOR IAW AMM 25-61-04. OPS CK GOOD.Sep 15, 2016 · N296UP · Doug MD11F · Emergency EquipmentSDR FDEA201609153261Seat Track · corrodedSEAT TRACK FLANGE FOUND CORRODED AT BS 1964 - 2000, X -107. REPAIR AS PER EA 1-5310-T0328362 P1. SEAT TRACK AT X=-107.5 - SPLICE REPAIR FROM STA 1831 TO STA 2007. REFER TO WRI: 53104412 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Sep 15, 2016 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201609153260Seat Track · corrodedSEAT TRACK FLANGE FOUND CORRODED AT BS 1818 - 1872, LBL 47.5. REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 15, 2016 · N617FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
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