Boeing MD-11F

Service difficulty reports · 31,317

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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 FDEA202502250291Frame · dentedCABIN - LEFT HAND FRAME AT STATION 1641 LONGERON S 12L FOUND DENT. CABIN - DENT AT LEFT HAND FRAME STATION 1641 LONGERON 12 LEFT, REPAIRED AS PER MD-11 SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPETITIVE INSPECTION REQUIRED - INITIAL AT 14,500 CYCLES AND REPFeb 25, 2025 · N572FE · Doug MD11F · Fuselage Main, FrameSDR FDEA202502250290Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1239 X = 8.5 FOUND CROWN WORN. MAIN DECK - AT SEAT TRACK STATION 1239, X = 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRAFeb 25, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202502250289Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1425 X = 8.5 FOUND CROWN WORN. MAIN DECK - AT SEAT TRACK STATION 1425, X = 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRAFeb 25, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202502250288Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1425 X = 47.5 FOUND CROWN WORN. MAIN DECK - AT SEAT TRACK STATION 1425, X = 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TFeb 25, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202502250287Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1425 X = - 8.5 FOUND CROWN WORN. MAIN DECK - AT SEAT TRACK STATION 1425, X = - 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEATFeb 25, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202502250286Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 879 X = 8.5 FOUND CROWN WORN. MAIN DECK - AT SEAT TRACK STATION 879, X = 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOABLE DAMAGE 1. CROWN WORN SEAT TRACK REFeb 25, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202502250285Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1541 X = 47.5 FOUND CROWN WORN. MAIN DECK Ï¿½ AT STATION 1541, X = 47.5 WORN SEAT TRACK CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEATFeb 25, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202502250284Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1256 X = - 8.5 FOUND CROWN WORN. MAIN DECK - AT SEAT TRACK STATION 1256, X = - 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEATFeb 25, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202502250283Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1256 X = -27.5 FOUND CROWN WORN. MAIN DECK - AT SEAT TRACK STATION 1256, X = - 27.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAFeb 25, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202502250282Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1545 X = -47.5 FOUND CROWN WORN. MAIN DECK - AT SEAT TRACK STATION 1545, X = - 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SFeb 25, 2025 · N572FE · Doug MD11F · Fuselage Floor PanelSDR FDEA202502250281Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1009 X = 27.5 FOUND CROWN WORN. MAIN DECK - AT SEAT TRACK STATION 1009, X = 27.5, WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD 11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TFeb 25, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202502250280Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 6-10 X = -75.5 FOUND CROWN WORN. MAIN DECK Ï¿½ AT SEAT TRACK STATION 6-10, X = -47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEFeb 25, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202502250279Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1239 X = -75.25 FOUND CROWN WORN. MAIN DECK - AT SEAT TRACK STATION 1239, X = - 75.25 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SFeb 25, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202502250277Skin · crackedRIGHT WING LEADING EDGE, SLAT ASSEMBLY NUMBER 5 UNDERSIDE COVE PANEL INBOARD EDGE FOUND WITH CRACKLINE FROM RIVETED HOLE, AT STATION XOS 660.537. RIGHT WING LEADING EDGE, SLAT ASSEMBLY NUMBER 5 UNDERSIDE COVE PANEL INBOARD EDGE AT STATION XOS 660.537 REPAIFeb 25, 2025 · N572FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA202502250276Skin · chafedFORWARD CARGO DOOR FUSELAGE CUTOUT FORWARD LOWER AREA FOUND EXISTING REPAIR CHAFE AT STATION 889. EXISTING CHAFFED REPAIR DOUBLERS AT FORWARD CARGO DOOR FUSELAGE CUTOUT FORWARD LOWER AREA AT STATION 889 REMOVED AS PER MD-11 SRM 51-33-01-0G. REPAIR CARRIEFeb 25, 2025 · N572FE · Doug MD11F · Standard Practices/StructuresSDR IPXA2025022176078Cable · brokenL1 DOOR LOWER FWD CABLE BROKEN OFF REPLACED FWD LWD CABLE PER AMM 52-11-09-401 AND ADJUSTED PER 52-11-02. OPS CHECK GOOD THIS CLEARS MEL 52-10-2-2-1 DMP.Feb 21, 2025 · N293UP · Doug MD11F · Passenger/Crew DoorsSDR FDEA202502210266Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-10 X = 27.5 FOUND CROWN WORN. MAIN DECK Ï¿½ AT SEAT TRACK STATION 5-10 X = 27.5 CROWN WORN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT Feb 21, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202502210265Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 5-10 X = 47.5 FOUND CROWN WORN. MAIN DECK Ï¿½ AT SEAT TRACK STATION 5-10 X = 47.5 CROWN WORN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT Feb 21, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202502210264Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1169 X = 47.5 FOUND CROWN WORN. MAIN DECK Ï¿½ AT SEAT TRACK STATION 1169, X = 47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. WORN CROWN SEATFeb 21, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202502210262Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 1169 X = -8.5 FOUND CROWN WORN. MAIN DECK Ï¿½ AT SEAT TRACK STATION 1169, X = -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEATFeb 21, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202502210261Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 829 X = 8.5 FOUND CROWN WORN. MAIN DECK Ï¿½ AT SEAT TRACK STATION 829, X = 8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACKFeb 21, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202502210260Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT STATION 849 X = -8.5 FOUND CROWN WORN. MAIN DECK Ï¿½ AT SEAT TRACK STATION 849, X = -8.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER MD-11 SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRAFeb 21, 2025 · N572FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025022061243Cable · brokenL1 DOOR AFT RAISE AND LOWERING CABLE BROKEN. INSTALLED SERVICABLE L1 DOOR AFT UPPER AND LOWER CABLES PER AMM 52-11-03.Feb 20, 2025 · N289UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2025022062146Pin · brokenL1 DOOR EMERGENCY EXIT DOOR LENS HAS A BROKEN GUIDE PIN. REMOVED AND INSTALLED NEW EXIT LIGHT ASSEMBLY IAW/ AMM 33-27-05Feb 20, 2025 · N289UP · Doug MD11F · Emergency LightingSDR IPXA2025021804449Battery · inoperativeEMER LT BAT 1 LO. R/R'D EMERGENCY LIGHT BATTERY POWER SUPPLY W/ REF TO MM 33-51-01, OPS TEST OK.Feb 18, 2025 · N278UP · Doug MD11F · Emergency LightingSDR IPXA2025021782873Pump · leaking**EMERGENCY DECLARED** LEVEL TWO HYD 3 FAIL DURING CRUISE. HYD 3 QUANTITY 0.0 QRH PROCEDURE ACCOMPLISHED W/ MANUAL GEAR EXTENSION. SERVICED HYD SYS 3 PER AMM 12-13-02, PER FORMED OPS AND LEAK CHECK OF #3 AFT EDP IN REFERENCE TO AMM 29-11-20. OPS CHECK GOOD ATFeb 17, 2025 · N292UP · Doug MD11F · Hydraulic Pump (Electric/Engine), MainSDR FDEA202502170237Trunnion · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND NOSE LANDING GEAR TRUNNION FITTING EXISTING TRIMMED OUT AREA AT STATION 583 FOUND CRACK APPROXIMATELY 0.15". LEFT HAND NOSE LANDING GEAR TRUNNION FITTING AT STATION 583 CRACKED AREA CARRIED OUT REPAIR INFeb 17, 2025 · N527FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA202502140232Battery · no testDURING POST FLIGHT CHECK FOUND EMGENCEY LIGHT TEST FAILED WITH ALERT EMER LT BAT 1 LO. REMOVED AND INSTALLED EMERGENCEY LIGHTING BATTERY POWER SUPPLY REF MM 33-51-01-4 . OPS CHECKS NORMAL REF MM 33-51-01-5. ACFT OK FOR SERVICE.Feb 14, 2025 · N610FE · Doug MD11F · Emergency LightingSDR IPXA2025021284329Flap System · faultedAIR TURNBACK AT 0849Z DUE MECHANICAL. AFTER FLAP RETRACTION RECEIVED LEVEL 2 AIL DEFLECT DISAG. PERFORMED QRH PROCEDURE. AIL DEFLECT DISAG REMAINED WITH NOTICEABLE ROLL. VERIFIED TORQUES AND SECURITY OF MOUNTING HARDWARE, VERIFIED TURNBUCKLES, ADJUSTMENT RODS,Feb 11, 2025 · N253UP · Doug MD11F · Trailing Edge Flap Control SystemSDR IPXA2025021177655Bottle · emptyR1 DOOR ASSIST BOTTLE DEPLETED. REMOVED AND REPLACED R1 DOOR ASSIST BOTTLE CHARGE VALVE IAW AMM 52-11-04-400-801 (H)(J)(K). C/W SERVICING IAW 12-25-04-600-801Feb 11, 2025 · N259UP · Doug MD11F · Passenger/Crew DoorsSDR 9WGA2025022480403Intercostal · crackedNR# 101 - PAC #3 DOOR HAS A CRACKED INTERCOSTAL. REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL P/N: ACA3820-14 AT #3 PAC DOOR IAW MD-11 SRM 51-35-01 AND DWG# ACA3820. O. AVIL D0011Feb 9, 2025 · N804SN · Doug MD11F · Passenger/Crew DoorsSDR FDEA202502070209Engine · vibrationEXPERIENCED AN ENGINE FAILURE AFTER TAKEOFF WITH HIGH EGT AND VIBRATION AT APPROXIMATELY 600 FEET. AFTER NOTIFYING TOWER FOR AIRBORNE RETURN TO TORONTO, EYE WITNESSES SAID THEY SAW A FIREBALL ON ENGINE 3 AFTER TAKEOFF. COMPLIED WITH QRH AND SECURED ENGINEFeb 7, 2025 · N642FE · Doug MD11F · Engine (Turbine/Turboprop)SDR IPXA2025022512801Seat Track · corrodedAFT CARGO COMPARTMENT. WASTE TANK CEILING AREA HAS CORRODED SEAT TRACK LOCATED AT STA 2007 AND LBL69. (015-40) ATA53.ACCOMPLISH REPAIR PER EO-92897-REQ1 AND VT-SAA EA 011-5342-01-B0389 I/R.Feb 6, 2025 · N251UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025022211516Skin · crackedRH WING XORS 372-402 L.E. EXTERNAL SURFACE LWR SIDE HAS CRACKED AS MARKED. 74-002 ATA CODE 57. ACCOMPLISHED REPAIR PER MD-11F- SRM 57-40-01-2R-17 REPAIR 17 FIGURE 201 REV 71.Feb 6, 2025 · N251UP · Doug MD11F · Wing, Plate/SkinSDR 9WGA20250214001Rib · crackedPAC #3 DOOR RIB CRACKED ON INTERIOR. REMOVED, FABRICATED AND INSTALLED NEW RIB (INTERCOSTAL) P/N ACA 3820-8 AT #3 PAC DOORIAW MD-11 SRM 51-35-01 AND DWG # ACA 3820. AIRCRAFT APPROVED FOR RETURN TO SERVICE.Feb 6, 2025 · N804SN · Doug MD11F · Passenger/Crew DoorsSDR IPXA2025022288776Trunnion · crackedWHILE PERFORMING REPEAT INSP. AT NLG LH TRUNNION REPAIR, 1 EA CRACK DETECTED APPROX. .5" IN LENGTH AS MARKED ON PART. ATA 32.ACCOMPLISHED REPAIR PER MD-11F SRM 53-10-14 REPAIR 2, FIGURE 203, REV 71.Feb 5, 2025 · N251UP · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA202502050175Warning Message · illuminatedAFTER TAKEOFF, MLG SELECTED UP, BOTH PRIMARY DISPLAY & SECONDARY SYNOPTIC DISPLAYED RED FOR LT MLG. RAN QRH & COORDINATED WITH GOC & MOCC FOR AIR TURN BACK. HANDLE DOWN, ALL PRIM DISPLAY & SEC SYNOPTIC DISPLAYED GREEN. SHORTLY SECONDARY SYNOPTIC DISPLAYED RED.Feb 5, 2025 · N596FE · Doug MD11F · Landing Gear Position and WarningSDR FDEA202502050174Gland Nut · leakingUNABLE TO RAISE LANDING GEAR HANDLE ON TAKEOFF. COMPLIED WITH QRH. STILL COULD NOT RAISE GEAR. FOUND MLG TRIM INTERLOCK CYLINDER NOT MOVING WITH HYDS ON, STOPPING MOVEMENT OF GEAR SELECTOR QUADRANT & VALVE. R & R TRIM CYLINDER INTERLOCK FUSE IAW AMM 32-37-06Feb 5, 2025 · N620FE · Doug MD11F · Landing Gear Retraction/Extension SystemSDR IPXA2025030765715Hinge · corrodedSTR-UPON REMOVAL OF HINGE 7 L/H O/B FLAP O/B AFT HINGE FOUND CORROSION ON MOUNTING HOLES. ACCOMPLISHED REPAIR PER EO-92991-REQ1 AND VT-SAA EA 011-5757-01-B0386 I/R. REVIEWEDFeb 4, 2025 · N255UP · Doug MD11F · Trailing Edge FlapsSDR IPXA2025030365863Mount · corrodedUPON REMOVAL OF HINGE 8 L/H O/B FLAP I/B AFT HINGE FOUND CORROSION ON MOUNTING HILES. FABRICATED REPLACEMENT BUSHING PER SR11570051 & MD-11-57-077 WITH FOLLOWING PROVISIONS: FABRICATED REPLACEMENT BUSHING FINAL DIAMETER BOLT HOLES WITH STANDARD INTERFERENCE FIFeb 4, 2025 · N255UP · Doug MD11F · Wing, Control Surface Attach FittingsSDR IPXA2025022264222None · noneTIME LIMITED REPAIR N251UP TAIL AFT BODY SECTION CORROSION BETWEEN STA 2119.685 AND 2163.681 AND BETWEEN L32R -L35R. ACCOMPLISHED REPAIR PER EO-92893-REQ1 AND VT-SAA EA 011-5330-01-B0375, REV. IR. REVIEWEDFeb 4, 2025 · N251UP · Doug MD11F · Standard Practices/StructuresSDR IPXA2025022863373Sidewall Panel · no discrepancyREMOVE L3 DOOR FOR STR. MAINT. REMOVED UPPER CARGO STA 1281 L/H SIDEWALL PNL PER MD11 AMM 25-23-02-000-801. REMOVED L3 DOOR PER MD11 AMM 52-12-12-000-801.REINSTALLED L3 DOOR PER MD11 AMM 52-12-12-400-801.Feb 4, 2025 · N251UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2025022863391Sidewall Panel · not reportedREMOVE R3 DOOR FOR STR. MAINT. REMOVED UPPER CARGO R/H STA 1281 SIDEWALL PNL PER MD11 AMM 25-23-02-000-801. REMOVED R3 DOOR PER MD11 AMM 52-12-12-000-801.REINSTALLED R3 DOOR PER MD11 AMM 52-12-12-400-801.Feb 4, 2025 · N251UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA2025021272371Slide · misinstalledL1 DOOR EMERGENCY EVACUATION SLIDE FOUND IMPROPERLY INSTALLED ON TO EVACUATION CONTAINER ATA 52-11. INSTALLED L-1 DOOR EMERGENCY EVACUATION SLIDE WITH CONTAINER ON L-1 DOOR ,CONNECTED FIRING LANYARD AND REMOVED LOCK PIN FROM REGULATOR VALVE ASSEMBLY IN REF TOFeb 4, 2025 · N251UP · Doug MD11F · Escape SlideSDR IPXA2025021272681Slide · misinstalledR1 DOOR EMERGENCY EVACUATION SLIDE FOUND IMPROPERLY INSTALLED ON TO EVACUATION CONTAINER ATA 52-11. INSTALLED R-1 DOOR EMERGENCY EVACUATION SLIDE WITH CONTAINER ON R-1 DOOR, CONNECTED FIRING LANYARD AND REMOVED LOCK PIN FROM REGULATOR VALVE ASSEMBLY IN REF TOFeb 4, 2025 · N251UP · Doug MD11F · Escape SlideSDR IPXA2025020764378Chain · brokenAPG DURING OPS CHECK OF L-1 PASSENGER DOOR EMERGENCY SYSTEM FOUND PNUEMATIC DRIVE CHAIN BROKEN ATA 52-11.Feb 4, 2025 · N251UP · Doug MD11F · Passenger/Crew DoorsSDR IPXA2025020563373Unknown · unknownREMOVE L3 DOOR FOR STR. MAINT. ATA 52-10 OK TO WORKFeb 4, 2025 · N251UP · Doug MD11F · Standard Practices/StructuresSDR IPXA2025020563391Unknown · unknownREMOVE R3 DOOR FOR STR. MAINT. OK TO WORKFeb 4, 2025 · N251UP · Doug MD11F · Standard Practices/StructuresSDR FDEA202502040172Bracket · damagedDURING APPROACH TO LANDING, GEAR WAS EXT AND INITIALLY INDICATED 4 GREEN/SAFE. AFTER APPX. 1 MIN GEAR INDICATION ON LEFT GEAR TURNED RED AND ON SYNOPTIC FLASHED BETWEEN GREEN AND RED. AFTER APPX. 10 MIN LEFT GEAR INDICATED SOLID GREEN ON SYNOPTIC. CREW FOFeb 4, 2025 · N596FE · Doug MD11F · Landing Gear Position and WarningSDR FDEA202502010164Coupler · failedHF2 WILL NOT ALLOW FREQUENCY CHANGES NOR TUNE ANYWHERE. FAIL DISPLAYED IN FREQUENCY WINDOW. CFDS HF2 FAULT, CODE 231114 HF2/COAX. EMERGENCY DECLARED. TUNED HF 2 TO 15MHZ UTC CLOCK FREQ, RECEIVED AUDIO BUT VERY WEAK, AFTER SEVERAL ATTEMPTS, NO LONGER RECEIVFeb 1, 2025 · N572FE · Doug MD11F · Communications System Wiring
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