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 IPXA2015090493132Skin · corrodedINSPECTION TYPE: 4C, CORROSION ON CENTER WING UPPER SKIN AT STR 15 XCW -70 TO XCW -94 ACCOMPLISHED PERMANENT BLEND REPAIR ON CENTER WING UPPER SKIN AT STR 15 XCW -70 TO XCW -94 IAW EA 011-5730-01-A5933, REV I /R AND EO MD11-5730-58608-A.Aug 12, 2015 · N284UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2015090493131Skin · corrodedINSPECTION TYPE:4C, CORROSION ON CENTER WING UPPER SKIN AT STR 15 XCW -18 ACCOMPLISHED PERMANENT BLEND REPAIR ON CENTER WING UPPER SKIN AT STRINGER 15 XCW -18 IAW 011-5730-01-A5933, REV I/R AND EO MD11-5730-58608-A.Aug 12, 2015 · N284UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2015090493130Skin · corrodedINSPECTION TYPE:4C, CORROSION ON CENTER WING UPPER SKIN AT STR 15 XCW 17 ACCOMPLISHED PERMANENT BLEND REPAIR ON CENTER WING UPPER SKIN AT STRINGER 15 XCW 17 IAW EA 011-5730-01-A5933, REV I/R AND EO MD11-5730-58608-A.Aug 12, 2015 · N284UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2015090393077Spar Cap · corrodedINSPECTION TYPE:4C, RT WING REAR SPAR UPPER CAP AFT HORIZONTAL FLANGE HAS CORROSION AT BS XORS 480.25. ACCOMPLISHED PERMANENT BLEND REPAIR ON RT WING REAR SPAR UPPER CAP HORIZONTAL FLANGE AT BS XORS 480.25 IAW EA 011-5710-01-A5943, REV I/R AND EO MD11-5710-58Aug 12, 2015 · N284UP · Doug MD11F · Wing SparSDR IPXA2015090193000Floor Panel · damagedINSPECTION TYPE:4C, UPPER CARGO FLOOR PANEL 261BF HAS EDGE DAMAGE. FABRICATED NEW UPPER CARGO FLOOR PANEL 261BF IAW SREO MD11-5320-27386-C.Aug 12, 2015 · N284UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2015090192999Floor Panel · damagedINSPECTION TYPE: 4C, UPPER CARGO FLOOR PANEL 272DF HAS DAMAGE ON BOTTOM SURFACE. FABRICATED NEW UPPER CARGO FLOOR PANEL 272DF IAW SREO MD11-5320-27386-C.Aug 12, 2015 · N284UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2015090192997Floor Panel · damagedINSPECTION TYPE:4C, UPPER CARGO FLOOR PANEL 261CF HAS EDGE DAMAGE. FABRICATED NEW UPPER CARGO FLOOR PANEL 261CF IAW SREO MD11-5320-27386-C.Aug 12, 2015 · N284UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2015081492351Light · inoperativeR1 DOOR SLIDE TEST LIGHT INOPERATIVE. R & R 2 EA 1.5 VOLT C CELLS BATTERIES AND REPLACED THE LAMP FOR THE PRESS TO TEST INDICATOR IAW WDM 25-61-01. OPS CHECKED GOOD.Aug 12, 2015 · N277UP · Doug MD11F · Escape SlideSDR FDEA201508122541Stiffener · crackedLEFT WING INBD LE SUPPORT STIFFENER CRACKED ON PANEL 515HB. REMOVED DAMAGED SUPPORT STIFFENER, FABRICATED NEW STIFFENER, INSTALLED NEW STIFFENER IAW DWG ARB4372 & SRM 51-31-01.Aug 12, 2015 · N522FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA201508122539Skin · corrodedLEFT WING UPPER SKIN SURFACE, STRINGER 15, BETWEEN XORS 141 & 145, LIGHT SURFACE CORROSION. REPAIRED IAW EA 1-5730-T0319403.Aug 12, 2015 · N522FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201508122538Smoke Warning · false activationON LANDING ROLL RECEIVED LEVEL 3 CABIN SMOKE ALERT UPPER DECK. CREW VERBAL REPORTED, IT LOOKED LIKE WAS WORKING THE PORTION OF MDC AFT OF COMPARTMENT TEMP IND ON AIR PAGE. CABIN SMOKE ALERT EXTINGUISHED BY ITSELF AFTER FEW SECONDS. CHECKED INSIDE OF MDC & Aug 12, 2015 · N612FE · Doug MD11F · Smoke DetectionSDR FDEA201508122536Doubler · crackedLEFT WING LE AT APPROX STATION XOS 602, FOUND PANEL SUPPORT FRAME DOUBLER WITH SIGNS OF CRACK. REMOVED IAW SRM 51-31-01-0G, NEW FRAME DOUBLER FABRICATED IAW DWG ARB2933 REVISION T SHEET 2. NEW DOUBLER INSTALLED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED MAJOR IAug 12, 2015 · N529FE · Doug MD11F · Wing Miscellaneous StructureSDR IPXA2015090493104Barrier · corrodedINSPECTION TYPE:4C, MAIN CARGO, RIGID CARGO BARRIER HAS CORROSION ON LOWER FORWARD SURFACE X=47.5. ACCOMPLISHED TIME LIMITED BLEND REPAIR ON MAIN CARGO RIGID CARGO BARRIER LOWER FORWARD SURFACE AT X=47.5 IAW EA 011-5310-01-A5926, REV I/R AND EO MD11-5310-5844Aug 11, 2015 · N284UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2015082992856Skin · delaminatedINSPECTION TYPE: 1C, AREA OF DELAMINATION ON LOWER SURFACE OF RT OTBD AIRLERON, OTBD END REPAIRED DELAMINATED IAW SRM 57-60-80. REPAIR 1 AND 51-62-01, PARA. 7.Aug 11, 2015 · N284UP · Doug MD11F · AileronsSDR FDEA201508112535Skin · damagedRIGHT WING NR 6 SLAT LE HAS 1 EACH CREASE IN SKIN. MARKED IN RED GREASE PENCIL. INSTALLED REPAIR DOUBLER IAW SRM 57-40-02 REPAIR 2.Aug 11, 2015 · N522FE · Doug MD11F · Leading Edge DevicesSDR FDEA201508112533Frame · crackedRIGHT WING NR 9 SLAT LE FRAME PN ARB2920-14 HAS ONE EACH CRACK ON LOWER AFT END. REMOVED PN ARB 2920-14 FORMER. FABRICATED ARB 2920-14 FORMER & INSTALLED IAW ARB 2920.Aug 11, 2015 · N522FE · Doug MD11F · Leading Edge DevicesSDR IPXA2015090593163Vane · chafedINSPECTION TYPE: 4C, LT OB FLAP VANE NR 5 TRACK CHAFE DAMAGE OB SIDE, FWD. REPAIRED IAW EA 011-5753-01-A5950 REV. IR AND EO MD11-5740-58633-A. MINOR REPAIR.Aug 10, 2015 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2015090593162Track · chafedINSPECTION TYPE:4CLH OB FLAP VANE NR 5 TRACK CHAFE DAMAGE OB SIDE, FWDREPAIRED CHAFE DAMAGE TO NOTED FLAP VANE TRACK PER VTSAA EA 011-5753-01-A5950 REV. IR AND UPS EO MD11-5740-58633-A. MINOR REPAIR.Aug 10, 2015 · N284UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2015090393063Stringer · crackedINSPECTION TYPE:4C, LT WING STRINGER 10 CRACKED AT BETWEEN BS XORS 737 AND XORS 772. ACCOMPLISHED PERMANENT REPAIR ON LT WING STR 10 FROM BS XORS 737 TO XORS 772.5 IAW SRM 57-00-03, REPAIR 5, FIGURE 202.Aug 10, 2015 · N284UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA2015090493098Angle · crackedINSPECTION TYPE:4C, RT WING INTERNAL BULKHEAD CLIP CRACKED BS XOR S562 BETWEEN STRINGERS 12-13. REMOVED FABRICATED AND INSTALLED REPLACEMENT CLIP IAW EA 011-5710-01-A5924, REV IR AND EO MD11-5710-58452-A.Aug 10, 2015 · N284UP · Doug MD11F · Wing Main, Frame StructureSDR FDEA201508172576Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT INBD HOLE, SURFACE CORROSION. REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING THICKNESS 0.711", MATERIAL REMOVED 0.006", REMAINING THICKNESS 0.705", MINIMUM ALLOWABLE THICKNESS 0.720". REAug 9, 2015 · N529FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201508092523Indicator · inoperativePRE FLY CHECK, RT ENTRY DOOR EVAC SLIDE PTT INDICATOR INOPERATIVE. RELEASED FOR SERVICE IAW MEL 25-61-02 CATEGORY C EXPIRATION 19 AUG 15. VERIFY & RECORD IN THE AML, EVAC SLIDE SYS PRESS ADEQAUTE ONCE EACH FLIGHT DAY. REPLACED BATTERIES & LAMPS, NO HELP.Aug 9, 2015 · N643FE · Doug MD11F · Emergency EquipmentSDR FDEA201508092519Hinge · corrodedRIGHT WING, FLAP SIDE, OTBD FLAP INBD HINGE, PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-52-04. EXISTING DIAMETER =1.150", FINAL DIAMETER =1.158", MAXIMUM ALLOWABLE DIAMETER =1.150". REPAIR ACCOMPLISHED IAW EA 1- 5Aug 9, 2015 · N529FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201508092518Hinge · corrodedLEFT WING, FLAP SIDE, OTBD FLAP, INBD HINGE, PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-52-04. EXISTING DIAMETER =1.149", FINAL DIAMETER =1.190", MAXIMUM ALLOWABLE DIAMETER =1.150". REPAIR ACCOMPLISHED IAW EA 1- Aug 9, 2015 · N529FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201508082516Hinge · corrodedRIGHT WING, FLAP SIDE, INBD FLAP OTBD HINGE, OTBD PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING DIAMETER = 1.256", FINAL DIAMETER =1.260", MAXIMUM ALLOWABLE DIAMETER =1.220". REPAIR ACCOMPLISHED IAW EAug 8, 2015 · N529FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201508082515Hinge · corrodedRIGHT WING, FLAP SIDE, INBD FLAP OTBD HINGE, INBD PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING DIAMETER = 1.256", FINAL DIAMETER =1.260", MAXIMUM ALLOWABLE DIAMETER =1.220". REPAIR ACCOMPLISHED IAW Aug 8, 2015 · N529FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201508082514Hinge · corrodedLEFT WING, FLAP SIDE, INBD FLAP OTBD HINGE, OTBD PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-52-03. EXISTING DIAMETER = 1.328", FINAL DIAMETER =1.338", MAXIMUM ALLOWABLE DIAMETER =1.220". REPAIR ACCOMPLISHED IAW EA Aug 8, 2015 · N529FE · Doug MD11F · Trailing Edge FlapsSDR IPXA2015090293046Doubler · crackedINSPECTION TYPE:4C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR BS XOS 880. REPAIRED LT WING BEADED DOUBLER XOS 879-884 IAW SRM 57-40-02, REPAIR 15, FIG 206.Aug 7, 2015 · N284UP · Doug MD11F · Wing Main, Frame StructureSDR IPXA2015090493110Skin · chafedINSPECTION TYPE: 4C, LT WING FIXED L/E SKIN HAS CHAFE DAMAGE BEWEEN XORS 1007 - 1038, REPAIRED IAW SRM 57-40-02, REPAIR 5, FIGURE 201.Aug 7, 2015 · N284UP · Doug MD11F · Wing, Plate/SkinSDR FDEA201508072511Stator · disintegratedNR 3 MAIN BRAKE CTR STATOR DISINTEGRATED, ALL OTHERS COMING APART. WILL R & R BRAKE. R&R NR 3 BRAKE ASSY IAW MM 32-43-20-4. OK FOR SERV.Aug 7, 2015 · N592FE · Doug MD11F · BrakeSDR FDEA201508072509Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, OTBD ACTUATOR HOLE BORE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 7, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508072508Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, LOWER MOUNT OTBD HOLE BORE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 7, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508072507Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, LOWER MOUNT OTBD HOLE BORE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 7, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508072506Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, LOWER MOUNT INBD HOLE BORE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 7, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508072505Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, SIDE LOAD FITTING BARREL NUT HOLE SPOT FACE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 7, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508072504Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP INBD HINGE, PIVOT HOLE BORE FOUND CORROSIONS. ASSEMBLY R & R IAW AMM 57-53-01-4. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 7, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508072503Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT BS 750 X= 8 FOUND CROWN DAMAGED. REPAIRED IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Aug 7, 2015 · N529FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201508072502Hinge Bracket · corrodedRIGHT WING, WING SIDE, OTBD FLAP OTBD HINGE, BARREL NUT HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED, FOUND WITHIN LIMITS. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.Aug 7, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508072501Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP OTBD HINGE, LOWER MOUNT OTBD HOLE BORE FOUND CORROSIONS. CORROSION AT HOLE 3, REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER = 0.580", FINAL HOLE DIAMETER =0.595", MAXIMUM ALLOWABLE HOLE DIAMETER =0.5Aug 7, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508072500Hinge · corrodedRIGHT WING, WING SIDE, OTBD FLAP OTBD HINGE, LOWER MOUNT INBD HOLE BORE FOUND CORROSIONS. CORROSION AT HOLE NR 3, REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER = 0.580", FINAL HOLE DIAMETER =0.595", MAXIMUM ALLOWABLE HOLE DIAMETER =Aug 7, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508072499Hinge · corrodedLEFT WING, WING SIDE, OTBD FLAP OTBD HINGE, PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIAMETER =2.3105", FINAL HOLE DIAMETER =2.334", MAXIMUM ALLOWABLE HOLE DIAMETER =2.3135". REPAIR BUSHING Aug 7, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508072498Skin · corrodedLEFT WING LE DROOP PANEL, UPPER SURFACE SKIN FOUND CRACKED FROM STATION XDLE 329.774 - XDLE 325.114. REPAIRED IAW SRM 57-40-01-2R FIGURE 201 REPAIR 5. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Aug 7, 2015 · N529FE · Doug MD11F · Leading Edge DevicesSDR FDEA201508072497Hinge Bracket · corrodedLEFT WING, WING SIDE, OTBD FLAP INBD HINGE, SIDE LOAD FITTING BARREL NUT HOLE SPOT FACE, FOUND CORRODED. REPAIRED IAW CMM 57-44-08. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.Aug 7, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508072496Hinge · corrodedLEFT WING, WING SIDE, OTBD FLAP INBD HINGE, OTBD ACTUATOR HOLE BORE, FOUND CORROSIONS. CORROSION AT HOLE 8, REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER = 1.219", FINAL HOLE DIAMETER =1.252", MAXIMUM ALLOWABLE HOLE DIAMETER =1.220".Aug 7, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508072495Hinge · corrodedLEFT WING, WING SIDE OTBD FLAP, INBD HINGE INBD ACTUATOR HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER = 1.215", FINAL HOLE DIAMETER =1.254", MAXIMUM ALLOWABLE HOLE DIAMETER =1.220". REPAIRED BAug 7, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508072494Hinge · corrodedLEFT WING, WING SIDE OTBD FLAP, INBD HINGE PIVOT HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER =2.309", FINAL HOLE DIAMETER =2.336", MAXIMUM ALLOWABLE HOLE DIAMETER =2.3135". REPAIRED BUSHING, Aug 7, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508072493Hinge · corrodedLEFT WING, WING SIDE OTBD FLAP, INBD HINGE LOWER MOUNT OTBD HOLE BORE FOUND CORROSIONS. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER = 0.643", FINAL HOLE DIAMETER =0.721", MAXIMUM ALLOWABLE HOLE DIAMETER =0.709". REPAIREAug 7, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201508072492Hinge · corrodedLEFT WING, WING SIDE OTBD FLAP, INBD HINGE LOWER MOUNT INBD HOLE BORE FOUND CORROSION. CORROSION REWORKED & FOUND EXCEEDS LIMIT IAW CMM 57-44-08. EXISTING HOLE DIAMETER = 0.703", FINAL HOLE DIAMETER =0.723", MAXIMUM ALLOWABLE HOLE DIAMETER =0.709". REPAIREDAug 7, 2015 · N529FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR KO0R201508070138Longeron · corrodedCORROSION ON FWD END OF LONGERON 34L AT STATION 5 - 7.Aug 7, 2015 · N512JN · Doug MD11F · Fuselage Main, Longeron/StringerSDR KO0R201508070137Longeron · corrodedCORROSION ON LONGERON 37R AT FRAME STATION 5 - 32.Aug 7, 2015 · N512JN · Doug MD11F · Fuselage Main, Longeron/Stringer
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