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 FDEA201606101919Hinge · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT INBD HOLE BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE, DIA: 0.579" FINAL HOLE DIA: 0.598" MAXIMUM ALLOWABLE DIA: 0.584". REPAIR BUSHING FABRICATED AND INJun 10, 2016 · N620FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201606091906Frame · damagedAGING AIRCRAFT, EXISTING REPAIR ON FRAME AT MAIN DECK CARGO COMPARTMENT, STA 1661, LONGERON L12R. EXISTING REPAIR ON FRAME AT MAIN CARGO COMPARTMENT STA 1661, LONGERON L12R EVALUATED AND FOUND DAMAGED. REPAIR CARRIED OUT AT FRAME AT MAIN CARGO COMPARTMENT, SJun 9, 2016 · N620FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201606091904Doubler · crackedLEFT WING FIXED L/E COMPARTMENT AT STA 631, BEADED DOUBLER FOUND CRACKED. DOUBLER REPAIRED IAW SRM 57-40-02-2R, FIG 203 REPAIR 15. THE REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 9, 2016 · N578FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201606091903Doubler · crackedLEFT WING FIXED L/E COMPARTMENT AT STA 735 BEADED DOUBLER FOUND CRACKED. DOUBLER REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Jun 9, 2016 · N578FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201606091902Doubler · crackedLEFT WING FIXED L/E COMPARTMENT AT STA 702, BEADED DOUBLER FOUND CRACKED. DOUBLER REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 9, 2016 · N578FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201606091901Doubler · crackedLEFT WING FIXED L/E COMPARTMENT AT STA 670 BEADED DOUBLER FOUND CRACKED. DOUBLER REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 9, 2016 · N578FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201606091900Doubler · crackedLEFT WING FIXED L/E COMPARTMENT AT STA 626 BEADED DOUBLER FOUND CRACKED. DOUBLER REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 9, 2016 · N578FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201606091899Doubler · crackedRT WING FIXED L/E COMPARTMENT AT STA 627 BEADED DOUBLER CRACKED. CRACKED BEADED DOUBLER REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. THE REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Jun 9, 2016 · N578FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201606091898Doubler · crackedLEFT WING FIXED L/E COMPARTMENT AT STA 667 RIB DOUBLER FOUND CRACKED. DOUBLER R & R IAW SRM 51-31-01-0G. THE NEW RIB DOUBLER FABRICATED IAW DWG: ARB3954, REV K. THE REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Jun 9, 2016 · N578FE · Doug MD11F · Wing, Rib/BulkheadSDR FDEA201606091897Seat Track · damagedMAIN DECK CARGO COMPARTMENT LT BS 6-3, X= 47.5 SEAT TRACK FOUND CROWN DAMAGED. SEAT TRACK REPAIRED IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 9, 2016 · N578FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201606081879Skin · crackedAGING AIRCRAFT, EXISTING SKIN REPAIR DOUBLER FOUND AT FWD CARGO DOOR CUTOUT FWD JAMB AT STA 895, LONGERON L39R-L41R EXISTING REPAIR AT FWD CARGO DOOR CUTOUT FWD JAMB AT STA 895, L39R-L41R EVALUATED AND FOUND CRACK. REPAIR CARRIED OUT AT FWD CARGO DOOR CUTOUT Jun 8, 2016 · N620FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201606081888Door Frame · crackedCABIN, MAIN DECK CARGO COMPARTMENT L3 DOOR AFT LOWER FUSELAGE JAMB WEB CRACKED AT LT BS 1310 BETWEEN LONGERON 26L-27L. WEB REPAIRED IAW 53-40-15-2R, FIG 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 8, 2016 · N620FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201606081887Door Frame · crackedCABIN, MAIN DECK CARGO COMPARTMENT L3 DOOR FWD LOWER FUSELAGE JAMB WEB CRACKED AT LT BS 1256 BETWEEN LONGERON 26L-27L. CRACKED WEB REPAIRED IAW 53-40-15-2R, FIG 201, REPAIR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 8, 2016 · N620FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201606081881Frame · chafedCABIN, MAIN DECK CARGO COMPARTMENT FRAME CHAFED AT RT BS 535, LONGERON 19R. DAMAGED FRAME REPAIRED IAW SRM 53-20-07-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 8, 2016 · N620FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201606081880Frame · chafedCABIN, MAIN DECK CARGO COMPARTMENT FRAME CHAFED AT RT BS 535, LONGERON 24R. FRAME REPAIRED IAW SRM 53-20-07-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 8, 2016 · N620FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201606081872Stick Shaker · false activationSTICK SHAKER: AFTER TAKEOFF AND BEFORE FLAP RETRACTION, THE STICK SHAKER ACTIVATED FOR ABOUT 2 SECONDS. THE PDF SHOWED BOXED, SLATS, IN AMBER. ALTITUDE WAS ABOUT 300 FEET. NO CURRENT OR PREVIOUS LEG FAULTS IN FCC'S. PERFORMED OPERATION TEST OF SLAT POSITJun 8, 2016 · N588FE · Doug MD11F · Stall Warning SystemSDR IPXA2016060704342Bottle · low pressureRIGHT ENTRY DOOR PRESSURE INDICATES BELOW MIN PRESSURE, OUT OF GREEN BAND. SERVICED DOOR PNEUMATIC STORAGE SYSTEM IAW AMM 12-25-04-600-800.Jun 7, 2016 · N252UP · Doug MD11F · Service DoorsSDR IPXA2016060704353Battery Pack · dischargedEMERGENCY LIGHT BATTERY 1 LOW. R & R EMERGENCY LIGHT BATTERY IAW MM 133-51-01 TESTS GOOD EFF SOURCE 33511001.Jun 7, 2016 · N290UP · Doug MD11F · Emergency LightingSDR FDEA201606071865Skin · damagedLEFT WING FIXED LE ANTI-ICE TELESCOPIC DUCT INNER SKIN BEADED AT STATION XOS 464, SURFACE FOUND DAMAGED. REPAIR CARRIED OUT PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jun 7, 2016 · N620FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201606071864Trunnion · crackedDURING HFEC INSPECTION ON NLG RT TRUNNION FITTING LOWER SECTION, EXISTING REPAIR AREA FOUND ONE EACH CRACK PROPAGATION, APPROX 0.50 INCH IN LENGTH AT STATION Y=595. CRACKED AREA REPAIRED IAW SRM 53-10-14-2R, REPAIR 2 FIG 202. INITIAL INSPECTION TO BE CARRIEDJun 7, 2016 · N578FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR IPXA2016060704320Warning Message · false activationDURING PREFLIGHT OBSERVED LEVEL 1, EMERGENCY LIGHT, BATTERY 1 LOW ALERT, PERFORMED OPS TEST OF THE EMERGENCY LIGHTING BATTERY POWER SUPPLY. TEST PASSED IAW AMM 33-51-01.Jun 6, 2016 · N260UP · Doug MD11F · Central WarningSDR IPXA2016060604292Door · unsecureDURING LANDING ROLL, LEVEL 1 MESSAGE CABIN DOOR AFT LT. FOUND OUTER DOOR HANDLE NOT FULLY STOWED. RE-SEQUENCED DOOR. OPS CK SEVERAL TIMES. LIGHT AND DOOR, OPS CK GOOD IAW AMM 52-12-13.Jun 5, 2016 · N278UP · Doug MD11F · Door Warning SystemSDR IPXA2016060704347Handle · inoperativeGEAR HANDLE WOULD NOT RAISE TO THE UP POSITION. REPLACED LANDING GEAR CONTROL MECHANISM REF 32-31-02-401, OPS OK.Jun 4, 2016 · N255UP · Doug MD11F · Landing Gear SelectorSDR FDEA201606041827Block · wornINTERMITTENT SLAT DISAGREE ON APPROACH, WENT AROUND. FOLLOWED QRH, NO SLAT & FLAPS 28 DEGREE LANDING. 194 WAS APPROACH SPEED. R & R FWD ATTACH NR 12 BOLT & ATTACHING HARDWARE IAW AMM. R & R L4B SLAT POSITION SENSOR IAW AMM 27-84-03-4. SENSOR STILL REQUIREJun 4, 2016 · N602FE · Doug MD11F · Leading Edge DevicesSDR FDEA201606021791Tire · leakingAFTER TAKEOFF LEVEL 1 TIRE PRESSURE LOW ALERT. NR 7 & 8 TIRE PRESSURE BOXED AMBER. NR 7 PRESSURE 232 PSI, NR 8 PRESS 60 PSI AT APPROX 47 PSI REC LEVEL 2 TIRE FAIL. R & R NR 7 & 8 MAIN TIRE ASSEMBLIES IAW AMM 32-41-01-4 DUE TO NR 8 TIRE LOW PRESSURE 32 PSI.Jun 2, 2016 · N523FE · Doug MD11F · TireSDR FDEA201606011784Longeron · corrodedLOWER FUSELAGE AFT OF LOWER BEACON, RIVET HEAD POPPED & SKIN BULGING. REPLACE FACTORY SPLICE & LONGERON.Jun 1, 2016 · N529FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2016060104117Power Supply · inoperativeFOUND EMERGENCY LIGHT TEST FUNCTION INOPERATIVE. REPLACED EMERGENCY LIGHTS POWER PACK 33-51-01, REV 85.02 AND ACC FIM 33-51-02-00 REV 83.00. OPS TEST SATISFACTORY.Jun 1, 2016 · N293UP · Doug MD11F · Emergency LightingSDR IPXA2016053104044Battery Pack · dischargedEMERGENCY LIGHT BATTERY LOW, 1 DISPLAYED DURING EMERGENCY LIGHT TEST. R & R EMERGENCY LIGHTING POWER SUPPLY IAW AMM 33-51-01-700-802. OPS CK GOOD IAW AMM 33-51-01-700-802.May 31, 2016 · N285UP · Doug MD11F · Emergency LightingSDR IPXA2016053104112Sign · brokenNR 1 DOOR RT EXIT SIGN BROKEN. R AND R RETAINER IAW AMM 33-27-05.May 30, 2016 · N291UP · Doug MD11F · Emergency LightingSDR IPXA2016053104039Battery Pack · no testEMERGENCY LIGHT TEST FAILED. R & R EMERGENCY POWER SUPPLY BATTERY IAW AMM 33-51-01. IPC 33-51-10-01.May 30, 2016 · N260UP · Doug MD11F · Emergency LightingSDR FDEA201605291778Relay · malfunctionedINFLIGHT AT FL 320 DEU'S 4 - 6 & MCDU 2 WENT BLANK & IMMEDIATELY GOT LEVEL 1 BUSS RT EMERGENCY AC OFF ALERT. ALSO OFF LIGHT RT EMERGENCY AC ON OVERHEAD & ELECTRICAL DISPLAY, MANY ASSOCIATED ALERTS, SELECT FADEC ALTERNATE, SINGLE LAND, ATC TRANSPONDER 2 FAIL, May 29, 2016 · N574FE · Doug MD11F · AC InverterSDR FDEA201605281748Battery · dischargedUPON CLOSING & ARMING R1 DOOR, NO LIGHT ON SLIDE PRESS TO TEST BUTTON, MEL 25-61-02. R1 EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE IAW MEL 25-61-02, VERIFY & RECORD IN THE AML. EVAC SLIDE SYS PRESS ADEQUATE ONCE EACH FLIGHT DAY. CHECKED R1 SLIDE PRESS. May 28, 2016 · N575FE · Doug MD11F · Emergency EquipmentSDR IPXA2016061104500Longeron · crackedINSPECTION TYPE: 3C, LONGERON 45R CRACKED AND CORRODED BETWEEN BS 5-93 AND 5-113. REPAIRED L45R IAW EA 011-5310-01-A6299, REV IR AND EO MD11-5310-61026-A.May 26, 2016 · N257UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201605261740Arming Lever · brokenLOCKING LATCH FOR L1 DOOR, DISARM LEVER BROKEN OFF. R & R THE L1 DOOR ARMING LEVER. OPERATIONS CHECKED NORMAL IAW AMM 52-11-02-4. ACFT OK TO CONTINUE.May 26, 2016 · N574FE · Doug MD11F · Passenger/Crew DoorsSDR KO0R201605260057Wire · cutCOURIER AREA ATTIC AT 53-901 TERMINAL STRIP FOUND TWO CUT WIRES.May 26, 2016 · N411SN · Doug MD11F · Light System WiringSDR KO0R201605260056Switch · intermittentELECTRICAL CONTROL PANEL HAS INTERMITTENT EMER POWER SWITCH.May 26, 2016 · N411SN · Doug MD11F · Emergency LightingSDR KO0R201605260055Light · inoperativeEMERGENCY LIGHTING INOPERATIVE.May 26, 2016 · N411SN · Doug MD11F · Emergency LightingSDR IPXA2016061004442Structure · wornINSPECTION TYPE: 1C, LOWER CASCADE SUPPORT RING BEARING LUG BORE WORN BEYOND REPAIRABLE LIMITS. R & R NR 1 THRUST REVERSER IAW AMM 78-13-01-000-868 AND -400-868.May 24, 2016 · N281UP · Doug MD11F · Engine Thrust ReverserSDR FDEA201605241727Hinge · corrodedRIGHT WING, OTBD FLAP, INBD FWD HINGE, WING SIDE, BARREL NUTS HOLE SURFACE CORROSION. CORROSION AT RT WING, OTBD FLAP, INBD FWD HINGE, WING SIDE, BARREL NUT HOLE SURFACE REWORKED IAW CMM 57-44-08. EXISTING THICKNESS: UPPER 0.368", LOWER 0.365". MATERIAL REMOVMay 24, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605241726Hinge · corrodedLEFT WING, OTBD FLAP, INBD FWD HINGE, WING SIDE, BARREL NUTS, HOLE SURFACE CORROSION. CORROSION AT LT WING, OTBD FLAP 11B, FWD HINGE, WING SIDE, BARREL NUT, HOLE SURFACE REWORKED IAW CMM 57-44-08. EXISTING THICKNESS: UPPER 0.371", LOWER: 0.3955", MATERIALMay 24, 2016 · N595FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR IPXA2016052303771Battery Pack · inoperativeON PREFLIGHT CREW REPORTS EMERGENCY LIGHTS WILL NOT TEST. RELAMPED EMERGENCY LIGHTS BATTERY MODULE REF AMM 33-51-01-00-8010 EFF SOURCE 33-51-01-05-015J.May 23, 2016 · N252UP · Doug MD11F · Emergency LightingSDR FDEA201605231720Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE BRACKET, WING SIDE, SIDE ATTACH SURFACE FOUND CORROSION. REWORKED IAW CMM 57-44-08. EXISTING THICKNESS: UPPER 0.402", LOWER 0.378", MATERIAL REMOVED: UPPER 0.010", LOWER 0.010" AND REMAINING THICKNESS: UPPER 0.392", LOWER 0May 23, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201605231719Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE BRACKET, WING SIDE, SIDE ATTACH SURFACE FOUND CORROSION. REWORKED IAW CMM 57-44-08. EXISTING THICKNESS: UPPER 0.392", LOWER 0.353", MATERIAL REMOVED: UPPER 0.010", LOWER 0.010" AND REMAINING THICKNESS: UPPER 0.382", LOWER May 23, 2016 · N615FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR IPXA2016052303772Limit Switch · inoperativeINSPECTION TYPE:R1, ENTRY DOOR INOPERATIVE. REPLACED S1 592 OPEN DOOR LIMIT SWITCH IAW AMM 52-11-02-830-805.May 22, 2016 · N275UP · Doug MD11F · Door Warning SystemSDR IPXA2016052403781Power Supply · inoperativeEMERGENCY LIGHTS, TEST FAIL. BATTERY LOW, EVEN THOUGH ACFT WAS POWERED FOR SEVERAL HOURS. R & R BATTERY POWER SUPPLY OF EMERGENCY LIGHTS IAW MM 33-51-01-4.May 22, 2016 · N296UP · Doug MD11F · Emergency LightingSDR FDEA201605221724Landing · crackedFOUND PANEL LAND CRACKED AT STATION XOS 906 LT WING. INSTALLED REPAIR.May 22, 2016 · N522FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201605221713Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT OTBD LUG BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.313", FINAL HOLE DIA: 1.326" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BMay 22, 2016 · N615FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201605221712Hinge Bracket · corrodedRIGHT WING INBD FLAP OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.250", FINAL HOLE DIA: 1.285" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BMay 22, 2016 · N615FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201605221711Hinge Bracket · corrodedLEFT WING INBD FLAP OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT OTBD LUG BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.2834", FINAL HOLE DIA: 1.315" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABMay 22, 2016 · N615FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201605221710Hinge Bracket · corrodedLEFT WING INBD FLAP OTBD AFT HINGE BRACKET, FLAP SIDE, PIVOT INBD LUG BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.250", FINAL HOLE DIA: 1.315" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRMay 22, 2016 · N615FE · Doug MD11F · Trailing Edge Flaps
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