N365DH, cancelled Feb 29, 2012

Service difficulty reports · 130

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N365DH' AND deregistration_id = 'N365DH-2012-02-29'
  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 DHLA200800013Mec · failedNR 1 ENGINE FAILED TO ACCELERATE WHEN TAKEOFF POWER WAS APPLIED. REJECTED PRIOR TO 70 KTS AT 5 DEGREE AMBIENT TEMP PRESS ALT 1360'. REMOVED AND REPLACED NR 1 MEC IAW MM 73-21-01. OPS CHECKS SERVICEABLE, NO LEAKS NOTED. MPA C/W IAW JRH.Feb 18, 2009 · N365DH · Airbus A300B42C · Fuel Controlling SystemSDR DHLA200800011AEngine · power lossDURING T/O ENG. 1 & 2 SPOOLED TO 60% N1, GO LEVERS SELECTED NR 1 ENG SPOOLED TO 80% N1 MAX, THROTTLE FULL FORWARD NO RESPONSE. OAT +5º C TAS LESS THAN 60KTS. REMOVED. CLEANED & INSTALLED PS-4 LINE. PERFORMED ACCELERATION CK ON NR 1 ENG. ENG. RUN OPS GOOD PEFeb 12, 2009 · N365DH · Airbus A300B4203 · Engine Fuel and ControlSDR DHLA200800138Nose Cowl · damagedRAMP DAMAGE TO INB D TOP SIDE OF NR 1 ENGINE NOSE COWL. ACFT STRUCK BY PORTABLE AIRSTAIRS WHILE PARKED ON RAMP. NR1 ENG COWL P/N NSL6051-533 REQUIRING REPLACEMENT.Dec 28, 2008 · N365DH · Airbus A300B42C · Engine Air Intake SystemSDR DHLA200800019Bottle · reads lowR1 DOOR ESCAPE SLIDE PRESSURE IN RED. REMOVED AND REPLACED SLIDE ASSY. AIRCRAFT WAS GROUNDED.Mar 1, 2008 · N365DH · Airbus A300B4203 · Escape SlideSDR DHLA200800003Skin · damagedLOWER FORWARD CARGO DOOR FUSELAGE LOWER FORWARD FRAME IS SCUFFED. DEFERRED IAW GMM 3.5 CAT I & LETTER REF. 942-057506/014/2008 ACCEPTABLE FOR 10 F.C. PLACARD INSTALLED.Jan 6, 2008 · N365DH · Airbus A300B4203 · Fuselage Main, Plate/SkinSDR DHLA200700043Inertia Reel · looseINERTIAL REEL CAME LOOSE DURING TAKEOFF ROLL. INSPECTED INERTIAL REEL. FOUND OK. REINSTALLED IN POSITION AS PER MM 25-61-13.Sep 12, 2007 · N365DH · Airbus A300B4203 · Emergency EquipmentSDR DHL2006365003Brake · overheatedCREW REPORTED NR 3 BRAKE REACHED 700 DEG ON T/O. PERFORMED ABORTED T/O AT 140 KTS, ALL LIGHTS ILLUMINATED. BRAKE HOT ILLUMINATED ON MWP. REMOVED & REPLACED BOGIE BEAM ASSY PER A300 M/M 32-11-14 OPS CHECKS GOOD.Aug 1, 2006 · N365DH · Airbus A300B4203 · BrakeSDR DHL2006365504Skin · dentedDENT ON LT WING I/B AILERON LOWER SKIN. INSTALLED DOUBLER REPAIR AT LT WING I/B AILERON LOWER SKIN AS PER A300 SRM 57-56-12.Jun 26, 2006 · N365DH · Airbus A300B4203 · AileronsSDR DHL2006365503Door Frame · corrodedLEFT AFT EMERGENCY EXIT DOOR CUT OUT FWD UPPER CORNER HAS CORROSION. FOUND CORROSION OUT OF LIMITS AT SKIN AN FRAME AREA IAW A300 SRM 53-16-00 FIG 602 & 53-10-00 PAGE 602. INSTALLED SKIN REPAIR IAW A300 SRM 53-16-00 FIG 715. INSTALLED FRAME REPAIR IAW A300 Mar 28, 2006 · N365DH · Airbus A300B4203 · Fuselage Main, StructureSDR DHL2006365501Stringer · corrodedFOUND AFT CARGO STRINGER 44R CORROSION BETWEEN FS 53& 54A. INSTALLED DOUBLER REPAIR AT AFT CARGO STR-44R BETWEEN FR 53 AND 54A AS PER A300 SRM 53-10-20. REINSTALLED SPLICE STRINGER SEGMENT AS PER A300 SRM 51-30-30, SEALED DOUBLER AREA AS PER A300 SRM 51-40-2Mar 9, 2006 · N365DH · Airbus A300B4203 · Fuselage Main, Longeron/StringerSDR DHL2006365500Seat Track · corrodedFLOOR TRACK SUPPORT BEAM AT STATION 1305 FR 16A AND LBL-78 AREA HAS SPOT OF CORROSION MARKED. REMOVED CORROSION AT FLOOR TACK SUPPORT BEAM AT STA 1305 FR 18A AND LBL 78 AS PER A300 SRM 51-40-11 FOUND OUT OF LIMITS AS OF PER A300 SRM 53-10-00. REMOVED AND REPMar 9, 2006 · N365DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2006365502Seat Track · corrodedMAIN CABIN FLOOR BBL 54 LT BETWEEN FR 18 AND FR 20 SEAT TRACK HAS CORROSION 3 SPOTS. REMOVED CORROSION AT MAIN CABIN FLOOR BBL 54 LT BETWEEN FR 18 AN 20 SEAT TRACK AS PER A300 SRM 51-40-11 FOUND OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK PER A300 SRM 51-Mar 7, 2006 · N365DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2006365002Warning System · activatedNOSE GEAR UNSAFE IND ON PILOTS INSTRUMENT PANEL. DEFERRED ITEM IAW MEL 32-31-01-1 ASSIGHNED DMI 24383 PLACARDS INSTALLED 35884. REFRENCE DMI#24383 NOSE GEAR UNSAFE INDON PILOTS INSTRUMENT PANEL. REPLACED NOSE GEAR TELESCOPIC DRUG STRUT ROCKER ARM PER MM 32-3Feb 15, 2006 · N365DH · Airbus A300B4203 · Landing Gear Position and WarningSDR DHL2006365001Switch · failedNOSE GEAR UNSAFE INDICATION ON S/O PANEL . FWD PANEL INDICATES DOWN AND LOCKED. TROUBLESHOOT SYS FOUND 79GB NOSE GEAR IND SWITCH BAD. SWAPPED WITH 40 GB NOSE GEAR IND SWITCH S/O GEAR IND OPS CK`D SERVICABLE ON GRD IAW MM 32-61-00.Feb 15, 2006 · N365DH · Airbus A300B4203 · Landing Gear Position and WarningSDR DHL2005365500Rib · crackedDURING ACCOMPLISHMENT OF EA57530001-001-A WHILE AT AVBORNE HEAVY MAINTENANCE INC LEFT INBOARD FLAP RIB NR 7 (FITTING} OUTBOARD SIDE FOUND CRACKED. REMOVED AND REPLACED NR 7 RIB IAW S/B A300-57-0242 REF ASTAR NON ROUTINE 034345.Oct 15, 2005 · N365DH · Airbus A300B4203 · Trailing Edge FlapsSDR DHL2005365007Latch · lack of lubeCOCKPIT DOOR LATCH IS FAULTY AND DIFFICULT TO LOCK. LUBED CREW ENTRY DOOR TO COCKPIT SYS OPS CHECKED GOOD ON GROUND IAW A300 M/M 52-00-00.Oct 4, 2005 · N365DH · Airbus A300B4203 · Fixed Inner DoorsSDR DHL2005365006Sensor · malfunctionedSTALL WARNING AT TAKEOFF WITH CONTINUOUS STICK SHAKER FROM TAKEOFF TO LANDING. REMOVED AND REPLACED AOA PROBE. OPS CHECKS OK IAW MM 27-36-15.Sep 22, 2005 · N365DH · Airbus A300B4203 · Stall Warning SystemSDR DHL2005367003Battery Pack · inoperativeL1 EMRG LT INOP. REMOVED AND REPLACED, L1 EMERG LT BATT PACK IAW 33-51-13.Aug 10, 2005 · N365DH · Airbus A300B4203 · Emergency LightingSDR DHL2005365005Call Horn · malfunctionedRTO RWR 27 MECHANIC CALL HORN ACTIVATED. MECHANIC CALL CURRENTLY DEFERRED. REF DMI 21755. NO PROVISIONS TO DEACTIOVATE CALL. BREIFED CREW. AC OK FOR SERVICEJul 23, 2005 · N365DH · Airbus A300B4203 · Flight Compartment EquipmentSDR DHL2005365004Warning Light · illuminatedON CLIMB OUT AT JFK ANGLE OF ATTACK PROBE HEAT LIGHT CAME ON. THIS WAS ON THE CAPTAINS SIDE ONLY. THE LIGHT WENT OUT AFTER 5 SEC. COULD NOT DUPLICATE. SYSTEM OPS CKS GOOD IAW MM 22-23-00.Jul 20, 2005 · N365DH · Airbus A300B4203 · Pitot/Static Anti-Ice SystemSDR DHL2005365003Fuel Line · rupturedAPU FIRE ON APU START DURING APPROACH. PERFORMED VISUAL INSP AND FOUND A RUPTURED FUEL LINE. FOUND NO STRUCTURAL DAMAGE. VERIFIED FUEL SHUT OFF VALVE IN CLOSED POS AND DEACTIVATED. EVACUATED REMAINING FUEL IN APU. PERFORMED HEAT DAMAGE EVALUATION IAWMay 18, 2005 · N365DH · Airbus A300B4203 · APU Engine Fuel and ControlSDR DHL2005365002Garlock Seal · leakingCREW REPORTED THAT ACFT LOSING OIL QUANTITY FROM 18 QUARTS BEFORE TAKEOFF THEN 10 QUARTS SHORTLY AFTER TAKEOFF,THEN DOWN TO 3 QUARTS AT 0545Z AND AT 0612Z 1 QT OIL QUANTITY REPORTED. NR 1 CSD LEAKING AT GARLOCK GEARBOX DRAIN CAVITY. R/R GARLOCK SEAL & O-RING IJan 25, 2005 · N365DH · Airbus A300B4203 · Turbine Engine Oil SystemSDR DHL2005365001Cable · out of adjustENG NR 2 WOULD NOT SHUTDOWN WHEN FUEL LEVER MOVED TO OFF. ENGINE SHUTDOWN WITH FIRE HANDLE. MAINTENANCE INDICATED SMOKE FROM NR 2 ENGINE AND NR 1 FIRE BOTTLE WAS DISCHARGED. ADJUSTED HP SHUTOFF VALVE FLEXIBLE CABLE IAW MM 76-12-31. OPS CK GOOD IAW 76-12-31Jan 15, 2005 · N365DH · Airbus A300B4203 · Fuel Controlling SystemSDR DHL2004365007Control Unit · malfunctionedON LANDING AUTOBRAKE DISARMED AND RE-ARMED BY ITSELF. NR 6 BRAKE LIGHT TEMP REACHED 400 DEG CELSIUS. ALL OTHER BRAKES TEMP REMAINED COLD. DEFERRED AUTO BRAKE SYSTEM TO DMI 18867 IAW MEL 32-42-07, CAT-C. MX NOTIFIED, PLACARD. INSPECTED NR 6 BRAKE IAW MM 32Dec 17, 2004 · N365DH · Airbus A300B4203 · Landing Gear Brake SystemSDR DHL2004365005Control Unit · inoperativeWHILE NORMAL BRAKES ARE BEING APPLIED, IF ANY AUTOBRAKE MODE IS SELECTED, EXPERIENCE A 3 SEC LOSS OF NORMAL BRAKES. IT IS AS IF THE ANTI SKID SYSTEM IS RELEASING THE BRAKES BUT THE ANTI SKID PANEL SHOWS NORMAL. REPLACED AUTOBRAKE CONTROL UNIT IAW MM 32-42-54Nov 3, 2004 · N365DH · Airbus A300B4203 · Landing Gear Brake SystemSDR DHL2004365004Servo Valve · dirtyAFTER T/O BRAKE HOT LIGHT ON MWP ILLUMINATED. WHEEL NR 7 BRAKE LIGHT ILLULMINATED. BRAKE HOT ABNORMAL PROCEDURES COMPLETED. SERVO UCV FOUND DIRTY. CLEANED, A/C TAXI PERFORMED OK AND STATIS IAW MM 32-42-48.Sep 26, 2004 · N365DH · Airbus A300B4203 · Landing Gear Brake SystemSDR DHL2004365003Connector · contaminatedAFTER DEPARTURE, THE LEFT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED ON THE CENTER PANEL AFTER GEAR RETRACTION. THE ASSOCIATED LIGHT WAS EXTINGUISHED ON THE SECOND OFFICERS PANEL. COMPLETED THE LANDING GEAR UNSAFE. FOUND OIL ON LT PROXIMITY SWITCH CONNECTOSep 8, 2004 · N365DH · Airbus A300B4203 · Landing Gear Position and WarningSDR DHL2004365002Windshield · crackedFO'S WINDSHIELD FRACTURED WHILE ENROUTE.Jul 22, 2004 · N365DH · Airbus A300B4203 · Flight Compartment WindowsSDR DHL2004365001Servo Valve · inoperativeLEFT MAIN ANTI SKID ON FWD LEFT WHEEL INOP. TRANSFERRED TO N/R 3831 W/O 24251. REMOVED AND REPLACED SERVO VALVE 1766 LEAK AND OPS CHECK NORMAL AS PER A300 MM 32-42-48. ANTI SKID TEST OF NR 1 WHEEL AND ANTI SKID SYSTEM, TEST IS NORMAL IAW A300 MM 32-42-00, TJun 26, 2004 · N365DH · Airbus A300B4203 · Brake Anti-Skid SectionSDR DHL2004365508Skin · dentedFUSELAGE SKIN DENTED AT FR26 BETWEEN STR29R & STR30R. REWORKED DENTED AREA AS REQUIRED IAW A300 SRM 51-41-10 AFTER REWORK FOUND DENT WITHIN LIMITS IAW A300 SRM 51-00-00 FIG 609. NOTE:08 DEPTH 1.5 LENGHT THICKNESS .063. HFEC INSPECTED AREA AT FR26 BETWEEN STJan 22, 2004 · N365DH · Airbus A300B4203 · Fuselage Main, Plate/SkinSDR DHL2004365514Frame · crackedREPAIR AT FR54, STR2L TO 5L DOES NOT CONFORM TO SRM. REMOVED REMAINING FASTENERS AND DOUBLER REPAIR FOR EVALUATION. PERFORMED NDT INSP OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR54, BETWEEN S-2L TO S-5L AND NO CRACKS NOTED. ACCOMPLISHED UT INSP, PROCJan 19, 2004 · N365DH · Airbus A300B4203 · Fuselage Main, FrameSDR DHL2004365507Skin · damagedREPAIR AT RIGHT FUSE FR19 STR 23R GOUGED. REMOVED EXISTING DOUBLER AT RIGHT FUSE FR19 STR23R IAW A300 SRM 51-30-30. SMOOTHED OUT FUSELAGE SKIN SECTION NEXT TO DOUBLER AREA AS PER A300 SRM 51-40-11. MAXIMUN MATERIAL LOSS-.011 ORIGINAL THICKNESS 0.63 FOUND TOJan 13, 2004 · N365DH · Airbus A300B4203 · Fuselage Main, Plate/SkinSDR DHL2004365515Seat Track · corrodedMAIN DECK SEAT TRACK BETWEEN FRAME 20 TO 26 APPROX. RBL77 HAS SEVERAL SPOTS OF CORROSION. REMOVED ALL CORROSION POINTS AT SEAT TRACKGOES BETWEEN FRAME 20 AND 26 RBL77 FOUND AREA OUT OF LIMITS IAW A300 SRM 51-40-11 AND 53-10-00. REMOVED AND REPLACED DAMAGED SEJan 7, 2004 · N365DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004365513Floorbeam · corrodedEXFOLATING CORROSION AT BOTTOM OF FLOOR BEAM FRAME 27 BELOW AFT END OF CARGO LOADING ROLLER AT 40 FT RT OF CENTER LINE. REMOVED CORROSION. FOUND OUT OF LIMITS .050 MAT LOSS. ACCOMPLISHED UT THICKNESS CHECK AFTER CORROSION REMOVED MAX THICKNESS FOUND .090. Jan 7, 2004 · N365DH · Airbus A300B4203 · Fuselage Main, Floor BeamSDR DHL2004365512Seat Track · corrodedMAIN DECK SEAT TRACK BETWEEN FRAME 20 TO 26 APPROX LBL 77 HAS SPOTS OF CORROSION. REMOVED SEAT TRACK FROM FRAME 19 TO 26.5 ACCCOMPLISH WITH N/R5169. AT MAIN DECK LBL 77 APPROX AS PER A300 SRM 53-10-00. WORK ACCOMPLISHED WITH N/R 5169. REMOVED AND REPLACED Jan 7, 2004 · N365DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004365511Seat Track · corrodedMAIN DECK SEAT TRACK BETWEEN FR19 TO 26 APPROX LBL 57 HAS SPOTS OF CORROSION. REMOVED CORROSION ON SEAT TRACK BETWEEN FRAMES 19 AND 26 APPROX LBL 57 AS PER A300 SRM 51-40-11. MATERIAL LOSS .038 INCH AT FRAME 21 AND .041 INCH AT FRAME 24, OUT OF LIMITS AS PERJan 7, 2004 · N365DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004365506Seat Track · corrodedMAIN DECK SEAT TRACK BETWEEN FRAME 20 TO 26 BL 0 HAS SPOTS OF CORROSION. REMOVED CORROSION IAW A300 SRM 51-40-11 PG 710. MATERIAL LOSS FROM FR22-FR26 APPROX 0.005 WITHIN LIMITS IAW A300 SRM 53-10-00 PG 619. MATL LOSS FROM FR21-FR22 IS 0.40 OUT OF LIMITS IAWJan 7, 2004 · N365DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004365504Seat Track · corrodedMAIN CABIN SEAT TRACK BETWEEN FR22 AND FR20 HAS CORROSION AREA RBL 36. REMOVED CORROSION AT MAIN CARGO SEAT TRACK FR20 APPROX 36 INCHES OF RBL, MATL LOST .030 INCH. FOUND OUT OF LIMITS AS PER A300 SRM 53-10-00 FIG 612 & 51-40-11. REMOVED CABIN SEAT TRACK FRJan 5, 2004 · N365DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004365510Seat Track · corrodedSEAT TRACK BETWEEN FR20 & FR21 APPROX LBL 78 PIECE OF TRACK MISSING & EVIDENCE OF CORROSION. CHECK OF SEAT TRACK BETWEEN FR20 & FR21 APPR LBL 78 FOUND OUT OF LIMITS IAW A300 SRM 53-10-00. REMOVED AND REPLACED SEAT TRACK FROM FRAME 19.5 TO FRAME 26.5 LBL 77 MJan 3, 2004 · N365DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004365509Seat Track · corrodedSEAT TRACK BETWEEN FR20 & FR21 APPROX RBL 58 EVIDENCE OF CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS AT SEAT TRACK FLANGES FR20 & FR21 APPROX RBL 58 AS PER A300 SRM 53-10-00 MATL LOSS .030 INCH CORROSION REMOVAL REF A300 SRM 51-40-11. REMOVED SEAT TRACKJan 3, 2004 · N365DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004365505Seat Track · damagedSEAT TRACK BETWEEN FR22 & FR23 APPROX RBL 18 EVIDENCE OF TOOL MARKINGS. REMOVED CORROSION I/B & O/B FLANGES FOUND OUT OF LIMITS, AT SEAT TRACK FR22 TO FR23 APPROX RBL 18 AS PER A300 SRM 51-10-00, 53-10-00, MATL LOST .030. REMOVED CABIN SEAT TRACK FROM FR18.5Jan 3, 2004 · N365DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004365503Seat Track · corrodedMAIN CABIN AFT OF FR20 APPROX BS 1360 APPROX LBL33 SEAT TRACK EVIDENCE OF CORROSION. REMOVED CORROSION AND FOUND AREA CRACK/ MAIN CABIN FR19 LBL 36 REF A300 SRM 51-10-00 & A300 SRM 53-10-00. REMOVED SEAT TRACK AT MAIN CARGO FROM FR18.5 TO FR26.5 LBL 36 AS PEJan 3, 2004 · N365DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004365502Seat Track · corrodedSEAT TRACK BETWEEN FR25 & FR27 APPROX LBL 18. SEVERAL PLACES EVIDENCE OF SURFACE CORROSION. REMOVED CORROSION AT SEAT TRACK BETWEEN FR25 AN FR27 APPROX LBL 18. CHECKED LIMITS FOUND OUT OF LIMITS IAW A300 SRM 51-10-00 & 53-10-00. REMOVED SEAT TRACK AT MAIN Jan 3, 2004 · N365DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004365501Seat Track · gougedSEAT TRACK AT FR38 CENTER TRACK GOUGED IN TWO PLACES. REWORK AREA GOUGED AT SEAT TRACK AT FR38 CENTER TRACK, FOUND OUT OF LIMITS IAW A300 SRM 53-10-00. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK BETWEEN FR37 AND 38 TO FR40 IAW A300 SRM 51-40-12, 51-3Jan 3, 2004 · N365DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2004365500Seat Track · damagedSEAT TRACK BETWEEN FR37 & 38 APPROX RBL 18 TOOL MARKING IN TWO PLACES. REWORKED DAMAGE AREAS AT SEAT TRACK BETWEEN FR 37 & 38 APPROX RBL 18. FOUND OUT OF LIMITS AS PER A300 SRM 53-10-00. CUT OUT DAMAGED SECTION OF SEAT TRACK ON FR37 TO 38 APPROX RBL 18 IAW Jan 3, 2004 · N365DH · Airbus A300B4203 · Fuselage, Seat/Cargo Attach FittingsSDR DHL2003365014Servo Valve · inoperativeRT REAR MAIN TIRE NR 8 BLOWN ON TAXI OUT ROLLED EMERGENCY EQUIPMENT AND MAINTENANCE TO VERIFY OKAY TO TAXI BACK TO BLOCKS. TROUBLESHOT FOUND NR 8 TIRE MAINTAINING PROPER PRESSURE. ALSO FOUND A PORTION OF THE TIRE RECAP PEELED OFF. REPLACED TIRE IAW MM 12-37-3Sep 8, 2003 · N365DH · Airbus A300B4203 · Landing Gear Brake SystemSDR DHL2003365013Downlock Switch · malfunctionedNO GREEN NOSE LIGHT ON S/O PANEL FOR LANDING GEAR. GPWS TOO LOW GEAR FORWARD GEAR INDICATIONS NORMAL. REMOVED AND REPLACED SYSTEM 2 NLG DOWNLOCK MICROSWITCH 79GB PER M/M 32-00-00 AND OPS CHECKED GOOD PER M/M 32-61-00.Aug 5, 2003 · N365DH · Airbus A300B4203 · Landing Gear Position and WarningSDR DHL2003365012Proximity Sensor · contaminatedNOSE GEAR DOWN AND LOCK LIGHT ON S/O PANEL DID NOT ILLUMINATE WHEN GEAR EXTENDED. ABNORMAL PROCEDURE COMPLETED. WHEN BELOW 500 FT AGL GPWS "TOO LOW", GEAR WARNING SOUNDED. CLEAN PROXIMITY SENSORS AT NOSE GEAR AND FOUND GREASE ON SENSORS. PERFORMED BITE TESAug 5, 2003 · N365DH · Airbus A300B4203 · Landing Gear Position and WarningSDR DHL2003365011Power Supply · dischargedL1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED CHARGE SUPPLY UNIT, OPS CHECKED OK IAW 33-51-00.Aug 5, 2003 · N365DH · Airbus A300B4203 · Emergency LightingSDR DHL2003365010Skin · dentedSMALL DENT FOUND AFT OF LOWER REAR CARGO DOOR AT STA NR 4096 (1617 INCHES). DEFERRED PER GMM 3.5 CAT I IAW A300 SRM 51-41-10 PG 701. CONTROL NR 13411. PLACARD INSTALLED. REF: DMI 13411 SMALL DENT FOUND AFT OF LOWER REAR CARGO DOOR AT STA NR 4096 (1617 INCJul 1, 2003 · N365DH · Airbus A300B4203 · Cargo/Baggage Doors
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