Boeing MD-11F

Service difficulty reports · 31,320

Newest first. General aviation reporting is voluntary.

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 FDEA201701150170Hinge Bracket · corrodedRT WING OUTBD FLAP OUTBD FWD HINGE BRACKET SIDE ATTACH UPPER BORE FOUND CORROSION. CORROSION AT RT WING O/B FLAP O/B FWD HINGE BRACKET UPPER O/B MOUNT BORE. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZE BUSHING WAS FABRICATED AND INSTALLED IJan 15, 2017 · N604FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201701150169Hinge Bracket · corrodedRT WING OUTBD FLAP OUTBD FWD HINGE BRACKET SIDE ATTACH LOWER BORE FOUND CORROSION. CORROSION AT RT WING O/B FLAP O/B FWD HINGE BRACKET UPPER O/B MOUNT BORE. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA. 0.389", FINAL HOLE DIA. 0.409" Jan 15, 2017 · N604FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201701150168Hinge Bracket · corrodedRT WING OUTBD FLAP OUTBD FWD HINGE BRACKET ACTUATOR OUTBD LUG BORE FOUND CORROSION. CORROSION AT RT WING O/B FLAP O/B FWD HINGE BRACKET UPPER O/B MOUNT BORE. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA. 1.248", FINAL HOLE DIA 1.256" Jan 15, 2017 · N604FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201701150176Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD HINGE BRACKET FOR ACTUATOR OTBD LUG BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330808 PART 1 STEP 1B.Jan 15, 2017 · N604FE · Doug MD11F · Wing, Attach FittingsSDR FDEA201701150175Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD HINGE BRACKET ACTUATOR INBD LUG BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-T0330808 PART 1 STEP 1B.Jan 15, 2017 · N604FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201701150174Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE BRACKET UPPER OTBD MOUNT BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08. BUSHING FABRICATED AND INSTALLED EA 1-5750-T0330808 PART 1 STEP 1A.Jan 15, 2017 · N604FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201701150173Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD FWD HINGE BRACKET UPPER INBD MOUNT BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08. BUSHING FABRICATED AND INSTALLED EA 1-5750-T0330808 PART 1 STEP 1A.Jan 15, 2017 · N604FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201701150164Connector · dirtyAT 80-90 KNOTS, RECEIVED A NR 1 ENGINE FIRE ALERT, AFTER STOPPING AIRCRAFT COMPLIED WITH QRH PROCEDURE, INCLUDING DISCHARGING SINGLE FIRE BOTTLE. FOUND HIGH RESISTANCE TO GROUND 2 MEGA OHMS ON B LOOP CAUSED BY WATER AND CARBON. CLEANED ON ALL CONNECTORS CHJan 15, 2017 · N592FE · Doug MD11F · Fire DetectionSDR FDEA201701140162Light · inoperativeL1 PRESS TO TEST DOOR SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED REMOTE PRESSURE INDICATOR ASSEMBLY IAW AMM 25-61-04-4-0. OPS CHECKED OK. GOOD FOR SERVICE.Jan 14, 2017 · N620FE · Doug MD11F · Emergency EquipmentSDR IPXA2017011612822Smoke Goggles · brokenFOUND COURIER SMOKE GOGGLES BROKEN. R&R COURIER SMOKE GOGGLES PER AMM 35-13-00.Jan 14, 2017 · N275UP · Doug MD11F · Emergency EquipmentSDR IPXA2017020213634Fitting · corrodedINSPECTION TYPE: 3C, RIGID CARGO BARRIER FLOOR FITTING NR 3 HAS CORROSION. REPAIRED IAW EA 011-5310-01-A6594 REV. I/R AND EO MD11-5310-63078-A.Jan 13, 2017 · N270UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2017020213633Fitting · corrodedINSPECTION TYPE: 3C, RIGID CARGO BARRIER FLOOR FITTING NR 2 HAS CORROSION. REPAIRED IAW EA 011-5310-01-A6593 REV. I/R AND EO MD11-5310-63070-A.Jan 13, 2017 · N270UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2017020213632Fitting · corrodedINSPECTION TYPE: 3C, RIGID CARGO BARRIER FLOOR FITTING NR 10 HAS CORROSION. REPAIRED IAW EA 011-5340-01-A6599 REV. I/R AND EO MD11-5340-63091-A. (MINOR)Jan 13, 2017 · N270UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2017020213631Fitting · corrodedINSPECTION TYPE: 3C, RIGID CARGO BARRIER FLOOR FITTING NR 4 HAS CORROSION. REPAIRED IAW EA 011-5310-01-A6593 REV. I/R AND EO MD11-5310-63070-A.Jan 13, 2017 · N270UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2017013113556Beam · crackedINSPECTION TYPE: 3C, BS 6-79 ABOVE LONGERON 43L, HORIZONAL BEAM HAS A TWO INCH CRACK. REMOVED, FABRICATED, AND REPLACED THE BEAM IAW DWG. ADA7667 AND SRM 51-33-01.Jan 13, 2017 · N270UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2017012913388Beam · crackedINSPECTION TYPE: 3C, FWD CARGO BAY HORIZONTAL BEAM IS CRACKED AT BS 6-79 ABOVE LONGERON 43R. REMOVED, FABRICATED AND REPLACED THE BEAM IAW DWG ADA7667 AND SRM 51-33-01.Jan 13, 2017 · N270UP · Doug MD11F · Fuselage Main, StructureSDR FDEA201701130159Washer · missingWHILE IN A TURN TO FINAL APPROACH, HAD A LEVEL 2 TAILCONE UNLOCK ALERT. LASTED A FEW SECONDS AND THEN EXTINGUISHED FOR THE REMAINDER OF THE FLIGHT. INSPECTED RIGHT TAILCONE LATCH CAM FOLLOWER ASSY. FOUND THE INSTALLATION HAD MISSING WASHERS. THE CAM ARM Jan 13, 2017 · N618FE · Doug MD11F · Aerodynamic FairingsSDR FDEA201701130147Hinge Bracket · corrodedLEFT WING, INBD FLAP FWD HINGE BRACKET PIVOT SPOT FACE FOUND CORRODED. CORROSION REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. REPAIRED IAW EA 1-5750-T0330593 A, PART 1, STEP 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jan 13, 2017 · N604FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201701130146Hinge Bracket · corrodedLEFT WING, INBD FLAP AFT HINGE BRACKET PIVOT OUTBOARD LUG BORE FOUND CORRODED. CORROSION REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-74282 C, PART 5, STEP 2A & 2B. REPAIR CLASSIFIED AS MAJJan 13, 2017 · N604FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201701130145Hinge Bracket · corrodedLEFT WING, INBD FLAP AFT HINGE BRACKET PIVOT INBD LUG BORE FOUND CORRODED. CORROSION REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-74282 C, PART 5, STEP 2A & 2B. REPAIR CLASSIFIED AS MAJOR Jan 13, 2017 · N604FE · Doug MD11F · Wing, Attach FittingsSDR FDEA201701130144Bracket · corrodedRIGHT WING, INBD FLAP INBD AFT HINGE BRACKET PIVOT OUTBOARD LUG BORE FOUND CORRODED. CORROSION REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZE BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-74277 D, PART 5, STEP 2A & 2B. REPAIR CLASSIFJan 13, 2017 · N604FE · Doug MD11F · Wing, Attach FittingsSDR FDEA201701130143Bracket · corrodedRIGHT WING INBD FLAP INBD AFT HINGE BRACKET PIVOT INBD LUG BORE FOUND CORROSION. CORROSION REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZE BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-74277, D, PART 5, STEP 2A & 2B. REPAIR CLASSIFIED ASJan 13, 2017 · N604FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201701130142Skin · corrodedAFT ACCESSORY BAY , FOUND FUSELAGE SKIN WITH CORROSION BETWEEN BS 2140 AND 2164, AT LONGERON 33 TO LONGERON 35R. FUSELAGE SKIN RH STA 2140 TO STA 2164, LONGERON 33 TO LONGERON 35 CARRIED OUT REPAIR AS PER SRM 53-70-01-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIEJan 13, 2017 · N604FE · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2017011712880Fitting · corrodedINSPECTION TYPE:3C, RIGID CARGO BARRIER FLOOR FITTING NR 5 HAS HEAVY CORROSION. REMOVED AND REPLACED RCB FLOOR FITTING NR 5 IAW MD11-2520-58701-D. (MINOR)Jan 13, 2017 · N270UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017011712879Fitting · corrodedINSPECTION TYPE:3C, RIGID CARGO BARRIER FLOOR FITTING NR 1 HAS CORROSION. REMOVED AND REPLACED RCB FLOOR FITTING NR 1 IAW EO MD11-2520-58701-D. (MINOR)Jan 13, 2017 · N270UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017020113573Skin · corrodedINSPECTION TYPE: 3C,AFT UPPER EXTERIOR SKIN HAS CORROSION BETWEEN BS 2104 & 2163.685, LONGERONS 11 - 13L. REPAIRED THE SKIN IAW EA 011-5330-01-A6600 REV. I/R AND EO MD11-5330-63118-A.Jan 12, 2017 · N270UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2017012913390Frame · corrodedINSPECTION TYPE: 3C, BAY FRAME ANGLE HAS CORROSION AT BS 430 RBL 2 - 9. REMOVED, FABRICATED AND REPLACED THE FRAME ANGLE IAW DWG ABA8678 AND SRM 51-35-01Jan 12, 2017 · N270UP · Doug MD11F · Fuselage Main, FrameSDR IPXA2017012913389Intercostal · corrodedINSPECTION TYPE: 3C, E/E BAY BS 475, RBL 9-12 INTERCOSTAL HAS CORROSION. REMOVED, FABRICATED AND REPLACED THE INTERCOSTAL IAW DWG ABA7655 AND SRM 51-33-01.Jan 12, 2017 · N270UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017012513266Frame · crackedINSPECTION TYPE: 3C, FUSELAGE FRAME AT BS 469.173, LBL 60 IS CRACKED. REPAIRED THE FRAME IAW SRM 53-10-07, REPAIR 1, FIG. 201.Jan 12, 2017 · N270UP · Doug MD11F · Fuselage Main, FrameSDR IPXA2017012713320Support Angle · crackedINSPECTION TYPE: 3C, AVIONICS BAY BILGE FRAME SUPPORT ANGLE AT BS 430 LBL 2 IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE SUPPORT ANGLE IAW DWG ABA8678, AND SRM 51-35-01.Jan 12, 2017 · N270UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017012513261Skin · crackedINSPECTION TYPE: 3C, UPPER RT AFT TAILCONE PATIO DOOR SKIN CRACKED. REPAIRED SKIN IAW SRM 52-00-00, FIG 204.Jan 12, 2017 · N270UP · Doug MD11F · Tail Cone DoorsSDR IPXA2017012513226Pan · gougedINSPECTION TYPE:3C, MAIN CARGO DOOR FWD. PAN IS GOUGED 23 INCHES FROM BOTTOM. REMOVED, FABRICATED AND REPLACED MAIN CARGO DOOR FWD LOWER PAN IAW DWG ACA7301 AND SRM 51-35-01 & N51-33-01. (MINOR)Jan 12, 2017 · N270UP · Doug MD11F · Cargo/Baggage DoorsSDR IPXA2017012213049Angle · corrodedINSPECTION TYPE: 3CT, ANGLE CORRODED IN FWD E/E BAY BS 475 RBL 4.5. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT ANGLE IAW DWG NCA6042, AND SRM 51-33-01.Jan 12, 2017 · N270UP · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201701120137Door · crackedAIR CONDITIONING DOOR STRUCTURE ON THE PLANE AFT UPPER CORNER APPEARS TO BE CRACKED. REPAIRED THE AREA IAW SRM 53-20-15.Jan 12, 2017 · N612FE · Doug MD11F · Air Conditioning DoorsSDR IPXA2017011312673Start Valve · inoperativeDURING CLIMB AT FL200. THE NR 1 ENGINE START VALVE LIGHT ILLUMINATED. ACCOMPLISHED QRH PROCEDURE. NR 1 MANIFOLD DEPRESSURISED INSPECTED START VALVE WIRE FROM CONNECTOR P1-8157 TO COWLING AND FOUND NO CHAFED WIRE. REPLACED THE START VALVE.Jan 12, 2017 · N251UP · Doug MD11F · Engine Start Valves/ControlsSDR FDEA201701110828Cadc · failedAFTER TAKEOFF PASSING THRU 3000 FEET GOT ALT MISCOMPARE ON CAPT PFD. ABOUT 10,000 F/O GOT SAME. WE WERE VMC ABOVE CLOUD LAYER AT THAT TIME. RAN AIRSPEED UNRELIABLE CHECKLIST. ALSO GOT IAS MISCOMPARE. CAPT ALT INDICATED FL330 AND F/O IND 32850. FGP ALTITUDE INDJan 11, 2017 · N522FE · Doug MD11F · Air Data ComputerSDR IPXA2017020813816Fuel Tank · corrodedINSPECTION TYPE: 3C, CENTER WING TANK UPPER SKIN HAS CORROSION AT RBL 89 TO 101.5 AT STRINGER 15. REPAIRED IAW EA 011 5730-01-A6596 AND EO MD11-5730-63200-A. (MAJOR)Jan 11, 2017 · N270UP · Doug MD11F · Fuel StorageSDR IPXA2017020513684Floor Panel · puncturedINSPECTION TYPE: 3C, MAIN CABIN FLOOR PANEL 262GF HAS A PUNCTURE. REMOVED, FABRICATED AND REPLACED THE FLOOR PANEL IAW EO MD11-5320-27286-C.Jan 11, 2017 · N270UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2017020113595Skin · corrodedINSPECTION TYPE: 3C, SKIN HAS CORROSION ABOVE STRINGER 15. REPAIRED THE SKIN IAW EA 011-5730-01-A6609 REV. I/R AND EO MD11-5730-63128-A.Jan 11, 2017 · N270UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2017013113519Thrust Reverser · crackedINSPECTION TYPE: 3C, NR 2 ENGINE LT THRUST REVERSER CORE COWL UPPER CLOSE-OUT WEB IS CRACKED. REMOVED AND REPLACED THE CLOSE-OUT WEB IAW SRM 54-05-41.Jan 11, 2017 · N270UP · Doug MD11F · Engine Thrust ReverserSDR IPXA2017013113515Skin · corrodedINSPECTION TYPE: 3C, SKIN HAS CORROSION. REPAIRED THE SKIN IAW EA 011-5730-01-A6602 REV. I/R AND EO MD11-5730-63089-A.Jan 11, 2017 · N270UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2017013113523Skin · corrodedINSPECTION TYPE: 3C, SKIN HAS CORROSION. REPAIRED THE SKIN IAW EA 011-5730-01-A6601 REV. I/R AND EO MD11-5730-63090-A.Jan 11, 2017 · N270UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2017012913386Skin · corrodedINSPECTION TYPE: 3C, SKIN CORRODED ABOVE STRINGER 15. REPAIRED IAW EA 011-5730-01-A6591 REV. I/R AND EO MD11-5730-63084-A.Jan 11, 2017 · N270UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2017012913385Structure · corrodedINSPECTION TYPE: 3C, STRUCTURE IS CORRODED ABOVE STRINGER 15. REPAIRED IAW EA 011-5730-01-A6590 REV. I/R AND EO MD11-5730-63082-A.Jan 11, 2017 · N270UP · Doug MD11F · Fuselage Main, StructureSDR IPXA2017012913384Skin · corrodedINSPECTION TYPE:3C, UPPER SKIN HAS CORROSION ABOVE STRINGERS 2, 3, & 4 AT RBL 105. REPAIRED CORRODED THE SKIN IAW EA 011-5730-01-A6595 REV. I/R AND EO MD11-5730-63085-A.Jan 11, 2017 · N270UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2017012513263Longeron Splice · crackedINSPECTION TYPE: 3C, CENTER CARGO BAY LONGERON 38L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED THE LONGERON SPLICE IAW SRM 51-33-01.Jan 11, 2017 · N270UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2017012313143Support Angle · corrodedINSPECTION TYPE:3C, AFT CARGO COMP FLOOR SUPPORT ANGLE/FLOOR BEAM CAP STA 1841 LONG 42R IS CORRODED. REPAIRED CORRODED SUPPORT ANGLE AT STA 1841, LONG 42R IAW DWG AGA3857 AND SRM 51-35-01. (MINOR)Jan 11, 2017 · N270UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017011112615Solenoid · defectiveL1 DOOR MAKES LOUD KNOCKING NOISE WHEN OPENING DOOR. DEFERRED IAW MEL 52-10-1-2-0-1 DMP C/W PLACARD INSTALLED. R&R DOOR SOLENOID REF AMM 52-11-003. OPS CK GOOD.Jan 11, 2017 · N274UP · Doug MD11F · Passenger/Crew DoorsSDR FDEA201701110123Anti-Ice System · malfunctionedLEVEL 1 ALERT "A-ICE SENSOR FAIL" AT FL350. STAYED ON FOR REMAINDER OF FLIGHT. IDENTIFIED PARTS, (W/KIT) PNEUMATIC PRESSURE. UPGRADED PNEU SYSTEM. CFDS SENSOR READOUT, PSC 1 SHOWED PE1 XXXX AND PSC 2 SHOWED PE1B XXXX. READINGS RETURN TO NORMAL AFTER PSC 1 Jan 11, 2017 · N603FE · Doug MD11F · Air Intake Anti/De-Ice SystemSDR FDEA201701110121Support · crackedRIGHT WING LEADING EDGE AT XOS 912.02. ACCESS PANEL SUPPORT FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-31-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Jan 11, 2017 · N604FE · Doug MD11F · Wing Miscellaneous Structure
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