Boeing MD-11F

Service difficulty reports · 31,317

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Query with SQL
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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IPXA2020072768238Lug · wornINSPECTION TYPE:S/V, RIGHT WING OTBD FLAP INBD AFT HINGE OTBD ACTUATOR LUG BUSHING LOOSE. REPAIRED THE LOOSE BUSHING IAW SOPM 20-20-07 & CMM 57-52-04. (MINOR)Jul 26, 2020 · N273UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2020072768236Lug · wornINSPECTION TYPE:S/V, RIGHT WING OTBD FLAP OTBD AFT HINGE FITTING OTBD ACTUATOR LUG BUSHING LOOSE. REPAIRED THE LOOSE BUSHING IAW CMM 57-52-04 & SOPM 20-20-7. (MINOR)Jul 26, 2020 · N273UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2020072768243Hinge · corrodedINSPECTION TYPE:S/V, RT OTBD FLAP OTBD FWD HINGE O/B LWR STUD MOUNT HOLE HAD CORROSION. REPAIRED THE FLAP O/B HINGE IAW EA 011-5740-01-A8439, REV I/R, AND EO MD11-5740-77319-A. MINORJul 26, 2020 · N273UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2020072768242Hinge · corrodedINSPECTION TYPE:S/V, RT OTBD FLAP FWD HINGE INBD LWR STUD MOUNT HOLE HAD SURFACE CORROSION. REPAIRED THE FLAP HINGE STUD MOUNT IAW CMM 57-44-09 REPAIR 1-1.Jul 26, 2020 · N273UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2020072758281Warning Message · false activationDURING DESCENT PASSING 14000 FT, AVIONICS FAN OVRD LVL 1 MESSAGE. TROUBLESHOT IAW FIM 21-26-04. INSPECTED PASSENGER, & CARGO DOOR SEALS FOR MED FUSELAGE PRESSURE DECAY TEST IAW AMM 21-00-00. TEST PASSED SATISFACTORILY.Jul 26, 2020 · N257UP · Doug MD11F · Central WarningSDR FDEA2020072761660Hinge Fitting · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION.Jul 26, 2020 · N585FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2020072761659Hinge Fitting · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION.Jul 26, 2020 · N585FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2020072761658Hinge Fitting · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE BORE FOUND CORROSION.Jul 26, 2020 · N585FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2020072761657Hinge Fitting · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION.Jul 26, 2020 · N585FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2020072761656Hinge Fitting · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION.Jul 26, 2020 · N585FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2020072761655Hinge Fitting · corrodedRIGHT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION.Jul 26, 2020 · N585FE · Doug MD11F · Trailing Edge FlapsSDR IPXA2020081459051Intercostal · corrodedINSPECTION TYPE:3CLOWER VERTICAL STABILIZER INTERCOSTAL IA CORRODED BETWEEN STA. YID= 245 AND YID= 251.REPAIRED CORRODED LOWER VERTICAL STAB INTERCOSTAL BETWQEEN STA. YI=245 TO YID= 251 IAW VT-SAA EA 011-5532-01-A8458 REV. I/R AND UPS EO MD11-5530-77511-A. (MAJul 25, 2020 · N279UP · Doug MD11F · Vertical StabilizerSDR IPXA2020081258988Angle · corrodedINSPECTION TYPE:C3LH FWD #2 ENG PICKLE BARREL SUPPORT STRUTURE INSIDE ACCESS PANEL #361EL HAS CORROSION ON AFT ANGLE SUPPORT.REPLACED CORRODED ANGLE SUPPORT AT #2 ENG PICKLE BARREL INSIDE PANEL 361EL IAW SRM 51-33-01. (MINOR)Jul 25, 2020 · N279UP · Doug MD11F · Nacelle/Pylon, Main FrameSDR IPXA2020081459033Floorbeam · crackedINSPECTION TYPE:1C3CMAIN CARGO FLOOR BEAM HAS CRACK AND DENT AT STA Y=979 AND X=-107.REPAIRED FLOOR BEAM AT STA Y=979 AND X=-107 IAW VT-SAA EA # 011-5310-01-A8440-IR AND UPS EO # MD11-5310-77493-A. MAJORJul 24, 2020 · N279UP · Doug MD11F · Fuselage Main, Floor BeamSDR FDEA202007241641Hinge Fitting · corrodedLT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (NR 8 HOLE). REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-Jul 24, 2020 · N585FE · Doug MD11F · Trailing Edge FlapsSDR FDEA202007241640Hinge Fitting · corrodedLT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LT WING, WING SIDE OUTBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (NR 8 HOLE). REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09Jul 24, 2020 · N585FE · Doug MD11F · Trailing Edge FlapsSDR FDEA202007241639Hinge Fitting · corrodedLT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE (NR 4 HOLE). REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. OVERSIZED BUSHING FABRICATEJul 24, 2020 · N585FE · Doug MD11F · Wing, Attach FittingsSDR FDEA202007231630Hinge Fitting · corrodedLT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT LT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08. SJul 23, 2020 · N585FE · Doug MD11F · Trailing Edge FlapsSDR FDEA202007231631Hinge Fitting · corrodedLT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE, INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. CORROSION AT LT WING, WING SIDE OUTBOARD FLAP INBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (NR 8 HOLE). REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- Jul 23, 2020 · N585FE · Doug MD11F · Trailing Edge FlapsSDR FDEA202007231629Bulkhead · crackedCENTER LANDING GEAR COMPARTMENT DOUBLER, ADJACENT TO SPOILER FEED THRU ROD BS 1382 FORWARD BULKHEAD RIGHT CORNER FOUND CRACKED. CENTER LANDING GEAR COMPARTMENT / DOUBLER ADJACENT TO SPOILER FEED THROUGH ROD STATION 1382 . X = -31.50 FORWARD BULKHEAD RIGHT Jul 23, 2020 · N585FE · Doug MD11F · Fuselage Main, BulkheadSDR FDEA202007231628Doubler · crackedCENTER LANDING GEAR COMPARTMENT, DOUBLER ADJACENT TO SPOILER FEED THRU ROD BS 1382, FORWARD BULKHEAD LEFT CORNER FOUND CRACKED. ENTER LANDING GEAR COMPARTMENT / DOUBLER ADJACENT TO SPOILER FEED THROUGH ROD STATION 1382 . X = -31.50 FORWARD BULKHEAD LEFT CORJul 23, 2020 · N585FE · Doug MD11F · Fuselage Main, BulkheadSDR FDEA202007231627Seat Track · damagedCABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK TOP SURFACE CORROSION AT BS 1114 - 6.0 , LBL 8.5. REPAIR CARRIED OUT PER SRM 53-00-52-2R . REPAIR 1 . FIGURE 201 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jul 23, 2020 · N585FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202007231626Seat Track · damagedCABIN - MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT BS 6-03 , RBL 47.5. REPAIRED IAW SRM 53-00-52-2R, REPAIR 1, FIGURE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 23, 2020 · N585FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202007221617Skin · crackedCRACK FOUND DURING HFEC INSPECTION ON RIGHT FIXED LEADING EDGE SKIN ADJACENT TO CORNER SLAT ACTUATOR ACCESS DOOR FORWARD INBOARD APPROX 1.5 INCHES AS MARK. AT XOS 490.850 . RIGHT WING FIXED LEADING EDGE SKIN ADJACENT TO CORNER SLAT ACTUATOR ACCESS DOOR Jul 22, 2020 · N585FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2020073021617Skin · crackedCRACK FOUND DURING HFEC INSPECTION ON RIGHT FIXED LEADING EDGE SKIN ADJACENT TO CORNER 5 SLAT ACTUATOR ACCESS DOOR FORWARD INBOARD APPROX 1.5 INCHES AS MARK.Jul 22, 2020 · N585FE · Doug MD11F · Wing, Plate/SkinSDR IPXA2020072748186Skin · crackedINSPECTION TYPE:2CCLG FWD L/H DOOR INNER SKIN IS CRACKED.REPAIRED CRACKED CLG FWD L/H DOOR INNER SKIN IAW MD-11 SRM 52-00-00 FIG 204. (MINOR)Jul 22, 2020 · N292UP · Doug MD11F · Cargo/Baggage DoorsSDR IPXA2020072258091Pan · crackedINSPECTION TYPE:4C, CLG R/H AFT DOOR LOWER AFT PAN CRACK.REMOVED AND REPLACED CRACKED CLG R/H DOOR AFT PAN IAW SRM 51-31-01,51-33-01,51-35-01. (MINOR)Jul 22, 2020 · N292UP · Doug MD11F · Landing Gear DoorsSDR FDEA2020072321617Skin · crackedCRACK FOUND DURING HFEC INSPECTION ON RIGHT FIXED LEADING EDGE SKIN ADJACENT TO CORNER 5 SLAT ACTUATOR ACCESS DOOR FORWARD INBOARD APPROX 1.5 INCHES AS MARK.Jul 22, 2020 · N585FE · Doug MD11F · Wing, Plate/SkinSDR 9WGA2020072321201Compressor · vibrationNR 2 ENGINE COMPRESSOR VIBRATION HIGH 5.0 NOT CORRECTABLE, STRONG RUDDER PEDAL VIBRATION AND HAD TO REDUCE POWER.Jul 22, 2020 · N512JN · Doug MD11F · Turbine Engine Compressor SectionSDR IPXA2020072258090Angle · crackedINSPECTION TYPE:4C, LT OTBD FLAP, INBD HINGE FAIRING TEE ANGLE CRACKED AT THE INBD SIDE. REMOVED AND REPLACED THE TEE ANGLE IAW SRM 51-35-01, AND 51-33-01. MINOR.Jul 22, 2020 · N292UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2020072258089Support Angle · crackedINSPECTION TYPE: 4C, LEFT OTBD FLAP INBD HINGE AFT FAIRING SUPPORT ANGLE WAS CRACKED. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-31-01. MINORJul 22, 2020 · N292UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2020072258088Stiffener · crackedINSPECTION TYPE: 4C, LEFT WING FIXED L/E LOWER SPAR CAP RIB STIFFENER CRACKED AT AFT END OF THE NR 8 SLAT TRACK. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-31-01, AND SRM 51-35-01. MINOR.Jul 22, 2020 · N292UP · Doug MD11F · Wing Miscellaneous StructureSDR IPXA2020072258087Intercostal · crackedINSPECTION TYPE: 4C, FWD CARGO INTERCOSTAL, RT SIDE RAIL WAS CRACKED BETWEEN BS 6-30 TO 6-50. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-31-01.Jul 22, 2020 · N292UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020072258083Rib · damagedINSPECTION TYPE: 4C, ON REMOVAL OF WEAR STRIPS AND NUTPLATES, FOUND NUMEROUS ELONGATED HOLES ON BOTH SIDES OF THE NR 1 PYLON V-RIB. REMOVED AND INSTALLED THE V-RIB IAW SRM 54-05-41. MINOR.Jul 22, 2020 · N292UP · Doug MD11F · Nacelle/Pylon Miscellaneous StructureSDR IPXA2020072258082Skin Splice · crackedINSPECTION TYPE:4C, LEFT WING L/E SKIN SPLICE DOUBLER CRACKED AT XOS 774. REMOVED, FABRICATED, AND INSTALLED THE SKIN SPLICE DOUBLER IAW SRM 51-31-01. MINOR.Jul 22, 2020 · N292UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2020072258101Web · crackedINSPECTION TYPE: 4C, CENTER ACCESSORY BAY, CABIN FLOOR SUPPORT, RT SIDE WEB CRACKED AT FASTENER. REPAIRED THE WEB IAW SRM 51-35-00, AND 51-31-01. MINOR.Jul 22, 2020 · N292UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020072258098Stiffener · crackedINSPECTION TYPE: 4C, LEFT MLG WW, OTBD AFT VERTICAL STIFFENER FOURTH FROM AFT, WAS CRACKED. REMOVED AND REPLACED THE VERTICAL STIFFENER IAW SRM 51-35-01, PG 35, AND 51-33-01. MINORJul 22, 2020 · N292UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020072258095Stiffener · crackedINSPECTION TYPE: 4C, LT MLG WW OTBD AFT SIDE VERTICAL STIFFENER FIFTH FROM AFT, FOUND CRACKED. REMOVED AND RELACED THE VERTICAL STIFFENER IAW SRM 51-35-01, PG 35, AND 51-33-01. MINOR.Jul 22, 2020 · N292UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020072258094Stiffener · crackedINSPECTION TYPE:4C, RT MLG WW AFT OTBD VERTICAL STIFFENER THIRD FROM FWD, FOUND CRACKED. REMOVED AND REPLACED VERTICAL STIFFENER IAW SRM 51-35-01, PG 35, AND 51-33-01, PG 45. MINOR.Jul 22, 2020 · N292UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2020072258093Inlet · crackedINSPECTION TYPE:4C, NR 2 ENGINE INLET LIP SKIN CRACKED AROUND ONE FASTENER AT 6 O'CLOCK POSITION. REPAIRED THE NR 2 ENGINE INLET LIP SKIN IAW SRM 54-10-01, REPAIR 4.Jul 22, 2020 · N292UP · Doug MD11F · Engine Air Intake SystemSDR IPXA2020082159277Skin · corrodedL/H FUSELAGE SKIN HAS CORROSION AROUND HORZ, BODY FAIRING BETWEEN STA. 2140-2163 @ L33L. REPAIRED CORRODED SKIN ON L/H FUSELAGE SKIN BETWEEN STA. 2140-2163 @ L33L IAW SRM 53-70-01 REPAIR 3 FIG. 201. (MAJOR)Jul 21, 2020 · N279UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020081459041Tee Fitting · corrodedINSPECTION TYPE:3CLOWER FWD RUDDER R/H T/E BLADE SEAL LANDING TEE HAS CORROSION.REPAIRED LOWER FWD RUDDER R/H BLADE SEAL LANDING TEE CORROSION IAW VT-SAA EA 011-5540-01-A8453 REV. IR AND UPS EO MD11-5540-77501-A. (MAJOR)Jul 21, 2020 · N279UP · Doug MD11F · Rudder StructureSDR IPXA2020081459039Skin · corrodedINSPECTION TYPE:3CRT AFT FUSELAGE SKIN BETWEEN STA 1997.750 - 2163.681 AND BETWEEN LONGERONS 31R - 35R HAS CORROSION.REPAIRED RT AFT FUSLAGE SKIN CORROSION BETWEEN STA 1997.750 - 2163.681 AND BETWEEN LONGERON 31R - 35R IAW VT-SAA EA 011-5330-01-A8459 REV. IR AJul 21, 2020 · N279UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020081459047Tee Fitting · corrodedINSPECTION TYPE:3CLOWER FWD RUDDER L/H T/E BLADE SEAL TEE HAS CORROSION.REPAIRED LOWER FWD RUDDER L/H T/E BLADE SEAL TEE CORROSION IAW VT-SAA EA 011-5540-01-A8452 REV. IR AND UPS EO MD11-5540-77496-A. (MAJOR)Jul 21, 2020 · N279UP · Doug MD11F · Rudder StructureSDR IPXA2020081098821Skin · corrodedINSPECTION TYPE:C3, LT FUSELAGE SKIN HAS CORROSION AROUND HORIZONTAL BODY FAIRING BETWEEN STA 2140 - 2163 LONG 33L.REPAIRED CORRODED SKIN ON LH FUSELAGE SKIN BETWEEN STA 2140 - 2163 LONG 33 IAW SRM 53-70-01 REPAIR 3 FIG 201. (MAJOR)Jul 21, 2020 · N278UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2020072258071Warning Message · false activationAPU DOOR DIASG LVL 1 CAME ON AFTER TAKEOFF. MESSAGE WENT AWAY AFTER 10 MINS INFLIGHT. OPS TESTED APU INLET & EXHAUST DOORS IAW AMM 49-17-01. OPS TESTED GOOD.Jul 21, 2020 · N283UP · Doug MD11F · Central WarningSDR IPXA2020072258092Computer · inoperativeFLIGHT CONTROL ANOMOLY IN PITCH USING AUTOPILOT 2 AT ABOUT 1500' ON FINAL. GO AROUND AND EMERGENCY DECLARED SECOND APPROACH SAME PROBLEM AND A/C WAS LANDED MANUALLY. AUTOPILOT 2 INOP PER MEL 22-10-1-0-1 DMP 22-10-1-0-1 ACCOMPLISHED. M714168 ASSIGNED. FCC CHANJul 21, 2020 · N296UP · Doug MD11F · Autopilot SystemSDR 9WGA2020072158101Cabin Pressure · malfunctionedDIVERSION DUE TO UNABLE TO MAINTAIN CABIN ALTITUDE. CABIN INFLOW LOW ALERT DISPLAYED SHORTLY AFTER TO. AIRCRAFT UNABLE TO MAINTAIN CABIN ALTITUDE UNDER 10,000FT.Jul 21, 2020 · N581JN · Doug MD11F · Cabin Pressure Control SystemSDR IPXA2020080318476Shear Tie · crackedINSPECTION TYPE:C3, BLADDER TANK LEFT HAND SIDE SHEAR TIE CRACKED AT LOWER FRAME AT APPROX STA 1289.REMOVED CRACKED SHEARTIE, FABRICATED AND INSTALLED IN LH BLADDER TANK STA 1289 IAW SRM 51-33-01 AND SRM 51-35-01. (MINOR)Jul 20, 2020 · N279UP · Doug MD11F · Fuselage Internal Mounting StructureSDR IPXA2020080358475Shear Tie · crackedINSPECTION TYPE:C3, CENTER WING BLADDER TANK AT RH SIDE HAS SHEAR TIE AT LOWER FRAME WITH A CRACK AT APPROX STA 1289.REMOVED CRACKED SHEARTIE, FABRICATED AND INSTALLED ON RH WING BLADDER TANK AT STA 1289 IAW SRM 51-35-01 AND SRM 51-33-01. (MINOR)Jul 20, 2020 · N279UP · Doug MD11F · Fuselage Internal Mounting Structure
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