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"

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 FDEA201703070806Monitor · failedAFTER DEPLOYING THE ADG, DID NOT PICK UP LT EMERGENCY AC BUSS. DETERMINED BY DISCHARGE GOING FROM -47 TO (-2) TO (0). ADG GROUND TEST CARRIED OUT IAW AMM 24-25-00-700-802, FOUND POWER MONITOR U1-540 FAILED. REMOVED AND REPLACED POWER MONITOR IAW AMM 24Mar 7, 2017 · N621FE · Doug MD11F · AC InverterSDR FDEA201703060782Hinge Bracket · corrodedLT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE SURFACE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING THICKNESS 0.405", MATERIAL REMOVED 0.005", REMAINING THICKNESS 0.400". MINIMUM ALLOWABLEMar 6, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR IPXA2017030614753Sealant · separatedSEPARATION OF SHEET METAL ON FUSELAGE AFT OF L1 DOOR. PRESSURE CHECK FUSELAGE REF AMM 21-00-00 AND SMALL SEALANT LEAK. REAPPLIED SEALANT RE SREO M-5100-19877-H. LEAK CHECK OK. BS 515, 6" BELOW FLOOR LINE.Mar 5, 2017 · N290UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2017030514721Wire · pulledEMERGENCY LIGHT BATTERY 1 LOW. FOUND WIRES PULLED FROM CONNECTOR P1-1756B, PINS 5, AND 6. PINNED THE CONNECTOR IAW AMM 20-30-05. EMERGENCY LIGHTS TEST CHECKED GOOD IAW AM 33-51-01.Mar 5, 2017 · N260UP · Doug MD11F · Emergency LightingSDR IPXA2017030714832Solenoid · inoperativeL1 DOOR ELECTRIC OPERATION INTERMITTENT FROM BOTH SWITCHES. TROUBLESHOT IAW FIM TASK 52-11-00-101. FOUND LOCK RELEASE SOLENOID FAILED. REMOVED AND REPLACED IAW AMM 52-11-00-101 ALL OPS CHECKED GOOD IAW 52-11-05-05-525 & 52-34-01-05-855Mar 5, 2017 · N295UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2017030614746Strap · missingL1 DOOR RED SAFETY STRAP MISSING. INSTALLED NEW RED SAFETY STRAP IAW AMM 52-12-12.Mar 4, 2017 · N283UP · Doug MD11F · Passenger/Crew DoorsSDR FDEA201703030767Tire · failed35 MINUTES INTO FLIGHT, RECEIVED A TIRE FAILURE ALERT. THE NR 6 TIRE INDICATIONS WENT BLANK. REMOVED AND REPLACED THE NR 6 TIRE AND WHEEL ASSMBLY. TIRE PRESSURE CHECKED OK ON CONFIGURATION PAGE.Mar 3, 2017 · N578FE · Doug MD11F · Tire TubeSDR FDEA201703030755Seat Track · crackedMAIN DECK CARGO COMPT FLOOR SEAT TRACK AT STA 6-96, X=-8.5 FOUND CRACKED. MAIN DECK CRACKED FLOOR SEAT AT STA 6-96, X=-8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 6-60 TO STA 6-100, X=-8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSMar 3, 2017 · N583FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201703030756Seat Track · corrodedMAIN DECK CARGO COMPT FLOOR SEAT TRACK AT STA 1139, X=- 8.5 FOUND CORROSION AS MARKED. MAIN DECK CORRODED FLOOR SEAT TRACK AT STA 1139, X=- 8.5 REPAIRED BY SECTIONAL REPLACEMENT FROM STA 6-100 TO STA 1149, X= - 8.5 AS PER SRM 53-00-02-2R FIG 201 REPAIR 1. REPMar 3, 2017 · N583FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2017030814874Attach Fitting · chafedINSPECTION TYPE: 2C, RIGHT WING NR 4 SLAT LOWER ATTACH FITTING CHAFED. REPAIRED THE ATTACH FITTING IAW EA 011-5740-01-A6670 REV I/R, AND EO MD11-5750-63394-A.Mar 3, 2017 · N255UP · Doug MD11F · Leading Edge DevicesSDR IPXA2017030314665Switch · inoperativeL-1 ENTRY DOOR INTERM IN ELECT. R & R L1 DOOR CONTROL POWER INTERLOCK SWITCH. OPS CHECKED GOOD IAW AMM 52-11-02.Mar 2, 2017 · N295UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2017030314642Latch · inoperativeFIRE EXTINGUISHER LATCH IN COURIER SECTION WILL NOT CLOSE. ADJUSTED THE QUICK-RELEASE STRAP AND INSTALLED THE FIRE EXTINGUISHER IAW AMM 26-24-01, PB 401, REV 88.Mar 2, 2017 · N274UP · Doug MD11F · Extinguishing SystemSDR FDEA201703020724Warning Light · false activationL1 DOOR ALERT, DURING TAXI. SPRAY LUBED GIRT BAR & SWITCH AREA, CLEANED SWITCH, L1 DOOR CONNECTOR BACK SHELL, MOVED ROLLERS IAW SMP. OPERATED DOOR FIVE TIMES, DOOR SLIDE ARMED & DISARMED, L1 DOOR CLOSED LIGHT ON ECAM OUT IAW MM 52-11-02-2. OPS CHECKED NORMar 2, 2017 · N528FE · Doug MD11F · Door Warning SystemSDR FDEA201703010718Indicator · damagedR1 DOOR SLIDE BOTTLE PRESS LIGHT STAYS ILLUMINATED. LIGHT DOES NOT SPRING BACK DURING TROUBLESHOOTING FOUND ON THE REMOTE PRESSURE INDICATOR THAT THE UPPER DOOR LINER JACK GROUNDED TO SELF PER WDM 25-61-01. REMOVED AND REPLACED REMOTE PRESSURE INDICATOR ASSEMMar 1, 2017 · N605FE · Doug MD11F · Emergency EquipmentSDR IPXA2017030114607Power Supply · inoperativeDURING PREFLIGHT INSPECTION, EMERGENCY LIGHT SYSTEM TEST DID NOT FUNCTION PROPERLY. R & R THE EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-01. OPS CHECKED GOOD.Mar 1, 2017 · N251UP · Doug MD11F · Emergency LightingSDR IPXA2017031615207Floor Panel · corrodedINSPECTION TYPE: 3C, MAIN CABIN FLOOR PANEL AT BS 475 - 500, RBL 63 HAS CORROSION. REMOVED AND REPLACED THE FLOOR PANEL IAW DWG WSP0789 AND SRM 50-33-01.Feb 28, 2017 · N287UP · Doug MD11F · Fuselage Floor PanelSDR IPXA2017031615225Seat Track · corrodedINSPECTION TYPE: 3C, MAIN CABIN SEAT TRACK AT BS 495 - 505, RBL 27 HAS CORROSION. REPAIRED THE SEAT TRACK IAW EA 011-5310-01-A6697, REV I/R, AND EO MD11-5310-63603-A.Feb 28, 2017 · N287UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2017031615220Seat Track · corrodedINSPECTION TYPE: 3C, MAIN CABIN SEAT TRACK HAS CORROSION AT BS 495 - 510, RBL 66. REPAIRED THE SEAT TRACK IAW EA 011-5310-01-A6698, REV I/R, AND EO MD11-5310-63604-A.Feb 28, 2017 · N287UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201702280686Panel · corrodedUPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= -27.5 TO X= -36 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= -27.5 TO X= -36 REMOVED PER AMMFeb 28, 2017 · N583FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201702280683Panel · corrodedUPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0785-502 AT STA 488, X= 27.5 TO X= 36 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0785-502 AT STA 488, X= 27.5 TO X= 36. REMOVED AS PER AMMFeb 28, 2017 · N583FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201702280682Panel · corrodedUPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= 19 TO X= 27.5 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= 19 TO X= 27.5. REMOVED AS PER AMMFeb 28, 2017 · N583FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201702280681Panel · corrodedUPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0786-501 AT STA 488, X=8.5 TO X= 19 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0786-501 AT STA 488, X= 8.5 TO X= 19. REMOVED AS PER AMM 53Feb 28, 2017 · N583FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201702280680Panel · corrodedUPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= 0.0 TO X= 8.5 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= 0.0 TO X= 8.5 REMOVED AS PER AMM Feb 28, 2017 · N583FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201702280679Panel · corrodedUPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0785-502 AT STA 488, X= 0.0 TO X= -8.5 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0785-502 AT STA 488, X= 0.0 TO X= -8.5 REMOVED AS PER AMFeb 28, 2017 · N583FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201702280678Panel · corrodedUPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= -8.5 TO X= -17 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= -8.5 TO X= -17 REMOVED PER AMM 5Feb 28, 2017 · N583FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201702280677Panel · corrodedUPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0786-501 AT STA 488, X= -17 TO X= -27.5 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL PN: WSP0786-501 AT STA 488, X= -17 TO X= -27.5 REMOVED PER AMM Feb 28, 2017 · N583FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201702280676Panel · corrodedUPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0790-502 AT STA 488, X= -75.25 TO X= -86.25 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0790-502 AT STA 488, X= -75.25 TO X= -86.25 REMOVEFeb 28, 2017 · N583FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201702280685Floor Panel · corrodedMAIN DECK RIGID CARGO BARRIER FLOOR SUPPORT PANEL AT STA 485, X=-36 TO X=-47.5 CORRODED AS MARKED. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT PANEL AS PER AMM 53-21-10-2. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100. CORROSION ON FLOOR SUPPORT PANEL EXCEEDED LIMITFeb 28, 2017 · N583FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201702280684Floor Panel · corrodedMAIN DECK RIGID CARGO BARRIER FLOOR SUPPORT PANEL AT STA 485, X=86.25 TO X= 107.25 CORROSION AS MARKED. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT PANEL AS PER AMM 53-21-10-2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. CORROSION ON FLOOR SUPPORT PANEL EXCEEDFeb 28, 2017 · N583FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201702280673Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK FLANGE FOUND WITH CORROSION AT BS 1603, RBL 8.5. CORROSION REMOVED IAW SRM 51-21-01-0G AND FOUND OUT OF LIMITS IAW SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. REPLACED THE SEAT TRACK IAW SRM 53-00-52-2R FIGURE 201 REPAIR 1. Feb 28, 2017 · N621FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2017032515480Skin · corrodedINSPECTION TYPE: 3C, AFT FUSELAGE RIGHT SIDE EXTERIOR SKIN HAS CORROSION BETWEEN BS 2129 - 2163.685, LONGERON 32 - 35R. REPAIRED THE SKIN IAW EA 011-5330-01-A6699-IR, AND EO MD11-5330-63701-AFeb 27, 2017 · N287UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2017032315441Skin · corrodedINSPECTION TYPE: 3C, EXTERIOR AFT FUSELAGE SKIN AT BS 2140 TO 2163.685, LONG. 12 - 13R. REPAIRED THE SKIN IAW EA 011-5330-01-A6705, REV I/R, AND EO MD11-5330-63687-A. (MAJOR)Feb 27, 2017 · N287UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2017032115389Door · wornINSPECTION TYPE: 3C, NR 3 ENGINE. INBD THRUST REVERSER DOOR LAND HAS WEAR DAMAGE ON THE UPPER END. REPAIRED IAW EA 011-7830-01-A6702, REV I/R, AND EO MD11-7830-63601-A.Feb 27, 2017 · N287UP · Doug MD11F · Engine Thrust ReverserSDR IPXA2017031915293Hinge Fitting · wornINSPECTION TYPE: 3C, NR 3 ENGINE INBD FAN COWL, AFT HINGE FITTING IS WORN. REPAIRED THE HINGE FITTING IAW EA 011-7110-01-A7610, REV. I/R, AND EO MD11-7110-63629-A.Feb 27, 2017 · N287UP · Doug MD11F · Nacelle/Pylon, Main FrameSDR IPXA2017031915292Frame · crackedINSPECTION TYPE: 3C, TRANSVERSE FRAME IS CRACKED AT BS 469.173, LBL 60. REPAIRED THE TRANSVERSE FRAME IAW SRM 53-10-07, REPAIR 1, FIG 201. MAJOR REPAIR.Feb 27, 2017 · N287UP · Doug MD11F · Fuselage Main, FrameSDR IPXA2017031915296Skin · corrodedINSPECTION TYPE: 3C, LEFT HORIZONTAL LOWER FAIRING ATTACH SKIN HAS CORROSION AT BS 2160 AND LONGERON 35L. REPAIRED THE SKIN IAW SRM 57-70-01, REPAIR 3, FIG 201. MAJOR REPAIR.Feb 27, 2017 · N287UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2017031615210Skin · chafedINSPECTION TYPE: 3C, LT WING LOWER JOINT SPLICE PLATE HAS CHAFE DAMAGE AT XCW 118.200. REPAIRED IAW EA 011-5730-01-A6711, REV I/R, AND EO MD11-5730-63623-A.Feb 27, 2017 · N287UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2017031615218Support Fitting · wornINSPECTION TYPE: 3C, MAIN CABIN RIGID CARGO BARRIER SUPPORT FITTING NR 4 HAS WEAR DAMAGE. REPAIRED THE SUPPORT FITTING IAW EA 011-5340-01-A6694, REV I/R, AND EO MD11-5340-63583-A.Feb 27, 2017 · N287UP · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201702270668Skin · crackedDURING ACCOMPLISHMENT OF NDT INSPECTION AT LT WING LOWER SKIN PANELS OUTER WING ACCESS DOOR CUTOUT AT STA XORS=696, 01 EA FASTENER HOLE 32 FOUND CRACK AS MARKED. LT WING LOWER SKIN PANEL ACCESS DOOR CUT OUT AT STA XORS 696, 01 EACH CRACKED FASTENER HOLE CARRIFeb 27, 2017 · N583FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201702270667Skin · crackedDURING ACCOMPLISHMENT OF NDT INSPECTION AT RT WING LOWER SKIN PANELS OUTER WING ACCESS DOOR CUTOUT AT STA XORS=696, 01 EA FASTENER HOLE 18 FOUND CRACK AS MARKED. RT WING LOWER SKIN PANEL ACCESS DOOR CUTOUT AT STA XORS, 01 EACH CRACKED FASTENER HOLE CARRIED OUTFeb 27, 2017 · N583FE · Doug MD11F · Wing, Plate/SkinSDR IPXA2017031215017Splice Plate · chafedINSPECTION TYPE: 3C, RIGHT WING LOWER JOINT SPLICE PLATE IS CHAFED AT XCW 118.200. REPAIRED SPLICE PLATE EA 011-5730-01-A6700, REV I/R, AND EO MD11-5730-63561-A.Feb 27, 2017 · N287UP · Doug MD11F · Wing, Plate/SkinSDR IPXA2017022714493Relay · failedEMERGENCY LIGHT BATTERY 1 LOW MESSAGE DURING EMERGENCY LIGHT TEST. R & R RELAY R 25100 IAW WDM 33-51-14. OPS CHECKED OK IAW AMM 33-50-00.Feb 27, 2017 · N260UP · Doug MD11F · Emergency LightingSDR FDEA201702270671Trunnion · wornNOSE LANDING GEAR LT FUSELAGE TRIUNION FITTING OUTBOARD BUSHING HAS WEAR AT THE UPPER SIDE AND INBOARD BUSHING LOOSE IN FITTING AND CAN BE REMOVED BY HAND. ACCOMPLISHED A REPAIR ON THE NOSE LANDING GEAR, LEFT TRUNNION FITTING OTBD BUSHING IAW SRM 53-10-14-2RFeb 27, 2017 · N614FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA201702270670Trunnion · corrodedCENTER LANDING GEAR RIGHT TRUNNION SUPPORT FITTING LOWER FACE HAS AREAS OF CORROSION. REPAIRED THE CENTER LANDING GEAR RT TRUNNION FITTING IAW SRM 53-40-14, REP 1.Feb 27, 2017 · N614FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR IPXA2017032515493Longeron · corrodedINSPECTION TYPE: 3C, CENTER CARGO BAY, LONGERON 48R HAS CORROSION BETWEEN SPLICE FITTING AND LONGERON FWD OF BS 1531. REPAIRED THE LONGERON IAW EA 011-5310-01-A6695, REV I/R, AND EO MD11-53-10-63709-A. MAJORFeb 26, 2017 · N287UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2017032115384Inlet · gougedINSPECTION TYPE: 3C, NR 2 ENGINE INTAKE LIP HAS SEVERAL GOUGES. REPAIRED INTAKE LIP ASSY IAW EA 011-5430-01-A6713, REV I/R, AND EO MD11-5430-63643-A.Feb 26, 2017 · N287UP · Doug MD11F · Nacelle/Pylon, Main FrameSDR IPXA2017031915298Support Fitting · crackedINSPECTION TYPE: 3C, CENTER CARGO AFT OVERHEAT DETECTOR SUPPORT ASSY IS CRACKED. REPAIRED THE SUPPORT IAW EA 011-2610-01-A6701 REV I/R, AND EO MD11-2610-63562-A.Feb 26, 2017 · N287UP · Doug MD11F · Fuselage Main, Attach FittingsSDR IPXA2017031615209Longeron Splice · crackedINSPECTION TYPE: 3C, CENTER CARGO BAY LONGERON 48L SPLICE FITTING IS CRACKED AT BS 5-73. REMOVED, FABRICATED AND REPLACED THE LONGERON SPLICE IAW DWG AEA7653, AND SRM 51-31-01.Feb 26, 2017 · N287UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA2017031415116Skin · chafedINSPECTION TYPE: 3C, EXTERIOR FUSELAGE SKIN UNDER WING TO BODY FAIRINGS AT BS 1159, LONGERON 44R HAS DEEP WEAR FROM PANEL CONTACT. REPAIRED THE SKIN IAW SRM 53-40-01, REPAIR 3, FIG 201. MAJORFeb 26, 2017 · N287UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA2017031215020Intercostal · crackedINSPECTION TYPE: 3C, FWD. CARGO BAY AT BS 6-50, LONGERON 41L,INTERCOSTAL FOUND CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-35-01, AND SRM 51-33-01.Feb 26, 2017 · N287UP · Doug MD11F · Fuselage Miscellaneous Structure
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