# N363DH: 1979 Airbus Industrie A300 B4-203, registration cancelled 2012-02-29

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 29, 2012
- Status when cancelled: Third renewal notice
- Airframe: [Airbus Industrie A300 B4-203](https://openairdocs.org/model/airbus-industrie-a300-b4-203) (registry code 3930306)
- Engine: [GE CF6-50 series](https://openairdocs.org/engine/ge-cf6-50-series) (registry code 30018)
- Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs)
- Serial number: 85
- Year built: 1979
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 31, 2000
- Certificate issued: May 7, 2009
- Last registry action: May 7, 2009
- Mode S code: A417C4
- Owner when cancelled: [Dhl Express (USA) Inc](https://openairdocs.org/faa-owner/DHL%20EXPRESS%20(USA)%20INC)
- Location: [Plantation, FL](https://openairdocs.org/faa-place/FL/Plantation)
- Owner type: Non-citizen corporation
- Owner's area on the map: 26.1125° N, 80.2749° W: Placed by OpenAirDocs at the center of ZIP code 33324, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N363DH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=363DH
- Page: https://openairdocs.org/deregistered/N363DH-2012-02-29

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Airbus Industrie A300 B4-203: https://openairdocs.org/model/airbus-industrie-a300-b4-203.md

## Service difficulty reports (164, newest 50)

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

- [SDR DHLA200900030](https://openairdocs.org/sdr/DHLA200900030), May 17, 2009: FAN. FAILED. ON LAST TAKEOFF 3RD HOT BRAKES ILLUM AT 80KTS REJECTED TAKEOFF PERF APPROP CHECKLISTS TAXI IN. REPLACED NR 3 BRAKE IAW MM 32-42-27, OPS CK NORMAL.
- [SDR DHLA200700067](https://openairdocs.org/sdr/DHLA200700067), Nov 23, 2007: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT DISARM WARNING DOES NOT ILLUMINATE. REPLACED LIGHT BULBS ON DISARM CAPSULE PER MM 33-51-00. OPS TEST OK.
- [SDR DHL2007363500](https://openairdocs.org/sdr/DHL2007363500), Sep 8, 2007: GUSSET. CRACKED. NR 2 ENG PYLON AT COWL HINGE FITTING O/B SIDE HAS A CRACK APPROX 3/4" ABOVE T BRACKET AT RIB 4. REMOVED AN REPLACED GUSSET HINGE FITTING AN T BRACKET AT NR 2 EN
- [SDR DHL2007363001](https://openairdocs.org/sdr/DHL2007363001), Jun 24, 2007: TRIPLER. DAMAGED. DURING A WEEKEND CHECK AT AVBOURNE HEAVY MX, THE FOLLOWING DISCREPANCIES WERE NOTED; TRIPLER DAMAGED ON PREVIOUS REPAIR AT FWD SIDE OF FWD CARGO DOOR CUT-OUT, F
- [SDR DHL2006363552](https://openairdocs.org/sdr/DHL2006363552), Nov 14, 2006: SKIN. CORRODED. BOTTOM OF L/W SKIN HAS CORROSION AT DRAIN HOLE FWD OF NR 6 FLAP TRACK. CORROSION BLEND OUT TO A MAJOR REPAIR AT L/W BOTTOM SKIN SLAT TRACK NR 9 DRAIN HOLE FWD O
- [SDR DHL2006363513](https://openairdocs.org/sdr/DHL2006363513), Oct 26, 2006: SEAT TRACK. CORRODED. CABIN FLOOR STRUCTURE FRAME 60 AND 61 AT BL 0 SEAT TRACK FLANGE HAS SURFACE CORROSION. INSTALLED ANGLE REPAIR AT CABIN SEAT TRACK FLANGE REF A300SRM 53-10-70 FI
- [SDR DHL2006363533](https://openairdocs.org/sdr/DHL2006363533), Oct 26, 2006: SEAT TRACK. CORRODED. CABIN FLOOR STRUCTURE FRAME 60 AND 61 AT BL 0 SEAT TRACK FLANGE HAS SURFACE CORROSION. INSTALLED ANGLE REPAIR AT CABIN SEAT TRACK FLANGE REF A300SRM 53-10-70 FI
- [SDR DHL2006363520](https://openairdocs.org/sdr/DHL2006363520), Oct 26, 2006: SEAT TRACK. CORRODED. CABIN FLOOR STRUCTURE FRAME 60 AND 61 AT BL 0 SEAT TRACK FLANGE HAS SURFACE CORROSION. INSTALLED ANGLE REPAIR AT CABIN SEAT TRACK FLANGE REF A300SRM 53-10-70 FI
- [SDR DHL2006363512](https://openairdocs.org/sdr/DHL2006363512), Oct 26, 2006: SEAT TRACK. CORRODED. CABIN FLOOR STRUCTURE FRAME 60 AND 61 AT BL 0 SEAT TRACK FLANGE HAS SURFACE CORROSION. INSTALLED ANGLE REPAIR AT CABIN SEAT TRACK FLANGE REF A300SRM 53-10-70 FI
- [SDR DHL2006363511](https://openairdocs.org/sdr/DHL2006363511), Oct 26, 2006: SEAT TRACK. CORRODED. CABIN FLOOR STRUCTURE FRAME 60 AND 61 AT BL 0 SEAT TRACK FLANGE HAS SURFACE CORROSION. INSTALLED ANGLE REPAIR AT CABIN SEAT TRACK FLANGE REF A300SRM 53-10-70 FI
- [SDR DHL2006363510](https://openairdocs.org/sdr/DHL2006363510), Oct 26, 2006: SEAT TRACK. CORRODED. CABIN FLOOR STRUCTURE FRAME 60 AND 61 AT BL 0 SEAT TRACK FLANGE HAS SURFACE CORROSION. INSTALLED ANGLE REPAIR AT CABIN SEAT TRACK FLANGE REF A300SRM 53-10-70 FI
- [SDR DHL2006363544](https://openairdocs.org/sdr/DHL2006363544), Oct 26, 2006: SEAT TRACK. CORRODED. CABIN FLOOR STRUCTURE FRAME 60 AND 61 AT BL 0 SEAT TRACK FLANGE HAS SURFACE CORROSION. INSTALLED ANGLE REPAIR AT CABIN SEAT TRACK FLANGE REF A300SRM 53-10-70 FI
- [SDR DHL2006363509](https://openairdocs.org/sdr/DHL2006363509), Oct 26, 2006: SEAT TRACK. GOUGED. MAIN CARGO DECK SEAT TRACK IS GOUGED AT FS 48 AND LBL 58. INSTALLED NEW SECTION OF SEAT TRACK AT MAIN CARGO FROM FS 44.5 TO 48.5 IAW A300SRM 53-10-10 AND 51-30-
- [SDR DHL2006363500](https://openairdocs.org/sdr/DHL2006363500), Oct 26, 2006: SEAT TRACK. CORRODED. CABIN FLOOR STRUCTURE AT FRAME 62 THRU 69 AT BL18L SEAT TRACK FLANGE SURFACE CORROSION. REMOVED LIGHT SURFACE CORROSION AT FS 62 TP FS 69 AT BL18L SEAT TRACK FL
- [SDR DHL2006363549](https://openairdocs.org/sdr/DHL2006363549), Oct 25, 2006: SEAT TRACK. CORRODED. CABIN FLOOR SEAT TRACK FLANGE AT BL 18 HAS CORROSION BETWEEN FRAME 30 AND FRAME 33. REMOVED AND REPLACED SEAT TRACK AND SPLICED IAW A300 SRM 53-10-10 PAGE 817, 
- [SDR DHL2006363506](https://openairdocs.org/sdr/DHL2006363506), Oct 25, 2006: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK FLANGE FS 48 TO 51, LBL18. REMOVED AND REPLACED SECTION OF SEAT TRACK AT FRAME 48 TO 51 IAW A300 SRM 51-10-40. FASTENERS INSTALLED IAW A
- [SDR DHL2006363505](https://openairdocs.org/sdr/DHL2006363505), Oct 25, 2006: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK FLANGE BETWEEN FS 50-52 LBL37. REMOVED SECTION OF SEAT TRACK AND REPLACED FROM FR50-52 LT IAW A300SRM 53-10-10 USED TMS 60-22457 7075-T6
- [SDR DHL2006363553](https://openairdocs.org/sdr/DHL2006363553), Oct 24, 2006: STRINGER. CORRODED. E/E COMPT FLOOR AREA BETWEEN FS 17 AND FS 18 AND BETWEEN STR 52L AND STR 54L FLOOR SKIN AND FRAME ANGLE AND STRINGER HAS CORROSION. COMPLIED WITH FSI REPAIR DIS
- [SDR DHL2006363508](https://openairdocs.org/sdr/DHL2006363508), Oct 24, 2006: SEAT TRACK. CORRODED. MAIN CARGO COMPARTMENT FLOOR SUPPORT FS 20.5 LBL 80 SURFACE CORROSION. FABRICATED NEW SEAT TRACK AS REQUIRED FROM TMS 60-24257 7075T6,REF A300 SRM 51-10-40, TRE
- [SDR DHL2006363507](https://openairdocs.org/sdr/DHL2006363507), Oct 24, 2006: CARGO TRACK. CORRODED. MAIN CARGO COMPARTMENT FLOOR SUPPORT FS 20.5 LBL 80 SURFACE CORROSION. FABRICATED NEW SEAT TRACK AS REQUIRED FROM TMS 60-24257 7075T6, REF A300 SRM 51-10-40, TR
- [SDR DHL2006363501](https://openairdocs.org/sdr/DHL2006363501), Oct 24, 2006: SKIN. DENTED. DENT IN FUSELAGE SKIN AT FS 13 STRINGER 31R APPROX. AVBORNE MAINTENANCE CAUSED DAMAGE. REWORKED DENT IN FUSELAGE SKIN AT FS 13 STRINGER 31R FOUND TO BE WITHIN L
- [SDR DHL2006363551](https://openairdocs.org/sdr/DHL2006363551), Oct 23, 2006: ATTACH FITTING. WORN. L/W ALL SPEED AILERON FITTINGS FOR ALL ACTUATORS THE 3RD FROM I/B HAS THE SLIDING PLATE AND FITTING WITH A WORN OUT GROOVE AT O/B SIDE, MADE BY A ACTUATOR GUIDE
- [SDR DHL2006363545](https://openairdocs.org/sdr/DHL2006363545), Oct 23, 2006: SEAT TRACK. CORRODED. MAIN CABIN FLOOR STRUCTURE UPPER FLANGE HAS CORROSION BETWEEN FS 12A AND 13A LBL18". REMOVED CORROSION AT MAIN CABIN FLOOR STRUCTURE UPPER FLANGE BETWEEN FS 12A
- [SDR DHL2006363547](https://openairdocs.org/sdr/DHL2006363547), Oct 23, 2006: SEAT TRACK. CORRODED. MAIN CABIN FLOOR STRUCTURE UPPER FLANGE HAS CORROSION BETWEEN FS 12A & 13A LBL18". REMOVED CORROSION AT MAIN CABIN FLOOR STRUCTURE UPPER FLANGE BETWEEN FS 12A &
- [SDR DHL2006363503](https://openairdocs.org/sdr/DHL2006363503), Oct 21, 2006: SEAT TRACK. CORRODED. CABIN FLOOR BETWEEN FRAME 15C AND 14C SEAT TRACK SUPPORT FLANGE AND SEAT TRACK FLANGE HAS CORROSION AT BL28R. REMOVED AND REPLACED CABIN FLOOR SEAT TRACK FROM F
- [SDR DHL2006363504](https://openairdocs.org/sdr/DHL2006363504), Oct 21, 2006: SEAT TRACK. CORRODED. CABIN FLOOR BETWEEN FRAME 15C AND 14C SEAT TRACK SUPPORT FLANGE AND SEAT TRACK FLANGE HAS CORROSION AT BL28R. REMOVED AND REPLACED CABIN FLOOR SEAT TRACK FROM F
- [SDR DHL2006363548](https://openairdocs.org/sdr/DHL2006363548), Oct 1, 2006: CARGO TRACK. CORRODED. MAIN CARGO COMPARTMENT FLOOR SUPPORT FS 20-22 LBL 60 AND LBL 80 SURFACE CORROSION UNDER CLIP NUT. REPLACED SECTION OF TRACK AS REQUIRED FROM TMS 60-24257 7075T6
- [SDR DHL2006363006](https://openairdocs.org/sdr/DHL2006363006), May 16, 2006: COMPUTER. FAULTED. CAPT'S AIR SPEED INDICATOR SHOWED -0- DURING T/O ROLL, ABORTED T/O AT 85 KIAS, WEIGHT 310,000 LBS, OAT 23' PA-37 FT, MAX BRAKE TEMP 250 DEGREES CELSIUS. REMOVED
- [SDR DHL2006363005](https://openairdocs.org/sdr/DHL2006363005), May 16, 2006: INDICATOR. MALFUNCTIONED. CAPT'S AIR SPEED INDICATION SHOWED -0- DURING T/O ROLL ABORTED T/O AT 90KIAS WEIGHT:31300 LBS, AOT 24'C PA 0 FT MAX OBSERVED BRAKE TEMP 400 DEGREES CELSIUS. REM
- [SDR DHL2006363004](https://openairdocs.org/sdr/DHL2006363004), May 4, 2006: SWITCH. MALFUNCTIONED. NOSE GEAR DOOR (ORANGE) IN TRANSIT LIGHT DID NOT COME ON WHEN EXTENDING GEAR (PILOTS PANEL) S/O PANEL OK. REPLACED RT NOSE GEAR DOOR SWITCH 38GB, NOSE GEAR DOOR
- [SDR DHL2006363003](https://openairdocs.org/sdr/DHL2006363003), Apr 12, 2006: SKIN. TORN. FUSELAGE SKIN AT AFT EDGE OF AFT CARGO COMPARTMENT DOOR CUTOUT IS TORN AND GOUGED 1.5 INCHES. DAMAGE IS AT FRAME 63A NEAR STRINGER 38. REPAIRED FUSELAGE SKIN AT
- [SDR DHL2006363002](https://openairdocs.org/sdr/DHL2006363002), Apr 12, 2006: SKIN. DAMAGED. AIRCRAFT DAMAGE ON AFT FUSELAGE BETWEEN FRAMES 65 AND 66 JUST BELOW STRINGER 36. REPAIRED FUSELAGE BETWEEN FRAMES 65 AND 66 AT STRINGER 36 IAW SRM 53-10-10 FIG 
- [SDR DHL2006363001](https://openairdocs.org/sdr/DHL2006363001), Feb 20, 2006: POWER SUPPLY. INOPERATIVE. LT EMERGENCY EXIT LIGHT AT L1 INOP. REMOVED & REPLACED LT EMERGENCY LIGHT POWER SUPPLY CK. GOOD IAW MM 3351-1.
- [SDR DHL2005363005](https://openairdocs.org/sdr/DHL2005363005), Jun 30, 2005: GCU. FAILED. POWER INTERUPTION B4 GEN 1 RESULTING IN RTO. DEFERRED NR 1 GEN IAW MEL 24-11-01 CONTROL NR 21499 ID NR 8742. PERFORMED AC GEN ADJ/TEST IAW MM 24-11-00 SYS OPS O
- [SDR DHL2005363004](https://openairdocs.org/sdr/DHL2005363004), Jun 18, 2005: SWITCH. MALFUNCTIONED. ON SHORT FINAL AFTER LANDING, GEAR EXTENSION, NOSE GEAR UNSAFE LIGHT (RED) ILLUMINATED ON PILOTS FRONT PANEL. ELECTED TO GO AROUND AND ACCOMPLISHED ABNORMAL PRO
- [SDR DHL2005363003](https://openairdocs.org/sdr/DHL2005363003), Jun 17, 2005: SWITCH. STICKING. NOSE GEAR INDICATED UNSAFE ON FWD PANEL DURING CVG APPROACH. THREE GREEN AND SAFE ON S/O PANEL. COMPLETED ABNORMAL PROCEDURE. FOUND 40GB SWITCH PLUNGER STICKING
- [SDR DHL2005363002](https://openairdocs.org/sdr/DHL2005363002), Apr 27, 2005: ENGINE. FAILED. AT VR ENGINE NR 2 FAILED. COMPLETED APPROPRIATE ABNORMAL PROCEDURES. DUMP 18,800 LBS OF FUEL. EGT TEMP EXCEEDED 7 SECONDS AT 940. PERFORM BOROSCOPE INSPECTION O
- [SDR DHL2004363014](https://openairdocs.org/sdr/DHL2004363014), Dec 18, 2004: BRAKE ASSY. MALFUNCTIONED. BRAKES GRAB ON RT SIDE. PERFORMED OPERATIONAL CHECK OF NORMAL, ALT, AND ANTI-SKID SYSTEMS. NO DEFECTS NOTED IAW MM 32-42-00.
- [SDR DHL2004363013](https://openairdocs.org/sdr/DHL2004363013), Dec 5, 2004: WARNING SYSTEM. ACTIVATED. T/O REJECTED DUE TO CONTINUOUS CHIME. NOTED CAB PRESSURE LIGHT FLICKER. REPLACED SEQUENCE BOX . SYS TESTS OK PER 21-31-00.
- [SDR DHL2004363012](https://openairdocs.org/sdr/DHL2004363012), Dec 5, 2004: WARNING SYSTEM. MALFUNCTIONED. RTO DUE TO CONTINUES CHIME. NO ANNUNCIATORS ILLUMINATED. REPLACE MWC PER MM 33-15-11. AURAL WARNING CHECKS OK PER MM 31-24-00.
- [SDR DHL200436311](https://openairdocs.org/sdr/DHL200436311), Dec 5, 2004: BRAKE. MALFUNCTIONED. ON REJECT, AUTO BRAKES DIDN'T ENGAGE UNTIL BRAKES APPLIED WITH PEDALS. ALSO, DID NOT DISENGAGE WITH PEDAL PRESSURE. DEFERRED AUTO BRAKES AS PER MEL 32-42-07. CA
- [SDR DHL200436310](https://openairdocs.org/sdr/DHL200436310), Dec 5, 2004: INDICATOR. INOPERATIVE. APPROXIMATELY 15 MINUTES AFTER TAKEOFF AT FLIGHT LEVEL 290, THE BRAKE TEMP ON WHEEL NR 8 INDICATED 700 DEGREES AND BRAKES HOT ILLUMINATED ON MASTER WARNING PANE
- [SDR DHL2004363009](https://openairdocs.org/sdr/DHL2004363009), Nov 20, 2004: B-NUT. LOOSE. AFTER LANDING AND WHILE APPLYING BRAKES, AIRCRAFT PULLS NOTICABLY TO THE RIGHT. ALSO, RIGHT BRAKE PEDAL FEELS "SOFT". FOUND LOOSE B-NUT ON MASTER CYLINDER LOCAT
- [SDR DHL2004363008](https://openairdocs.org/sdr/DHL2004363008), Nov 11, 2004: PITOT LINE. SEPARATED. DURING TAKEOFF ROLL, THERE WAS NO AIRSPEED INDICATED ON THE CAPTAIN'S AIRSPEED INDICATOR WHILE THE FIRST OFFICER'S CORRECTLY INDICATED 90KTS. TAKEOFF WAS ABORTE
- [SDR DHL2004363534](https://openairdocs.org/sdr/DHL2004363534), Oct 12, 2004: SKIN. DENTED. DURING C-CHECK, DISCREPANCY AS FOLLOWS, N/R 3912, AFT. FUSELAGE SKIN HAS DENT AT FR 77 AND STR 22R. BLENDED OUT AREA, FOUND DENT BEYOND LIMITS IAW SRM 53-10-10.
- [SDR DHL2004363532](https://openairdocs.org/sdr/DHL2004363532), Oct 12, 2004: SKIN. DENTED. DURING "C" CHECK AT AVBORNE HEAVY MAINTENACE IN MIAMI, FL DISCREPANCY AS FOLLOWS, N/R 3911, AFT FUSELAGE SKIN HAS DENT AT FS 65 AND STR 31R. BLENDED OUT AREA FO
- [SDR DHL2004363511](https://openairdocs.org/sdr/DHL2004363511), Oct 5, 2004: SEAT TRACK. CORRODED. DURING C-CHECK, DISCREPANCY AS FOLLOWS, N/R 3899 LBL 36 BETWEEN FRAME 15 AND FRAME 19 SEAT TRACK CORRODED. REMOVED CORROSION FROM AREA FRAME 15 TO FRAME 19 LBL 
- [SDR DHL2004363509](https://openairdocs.org/sdr/DHL2004363509), Oct 5, 2004: SEAT TRACK. CORRODED. DURING C-CHECK, DISCREPANCY AS FOLLOWS, NR 3898, RBL 36 BETWEEN FRAME AND FRAME 19 SEAT TRACK CORRODED. REMOVED CORROSION FROM AREA/FRAME IS TO FRAME 19 RBL 36 
- [SDR DHL2004363512](https://openairdocs.org/sdr/DHL2004363512), Oct 4, 2004: SEAT TRACK. CORRODED. DURING "C" CHECK IN MIAMI, FL AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 3900 MAIN CABIN SEAT TRACK FLANGE OUT OF LIMITS BETWEEN FRAME 27 TO FRAME
- [SDR DHL2004363530](https://openairdocs.org/sdr/DHL2004363530), Sep 30, 2004: SEAT TRACK. CORRODED. DURING C-CHECK, DISCREPANCY AS FOLLOWS, N/R 3887, FR.18-FR. 26.5 RBL 98 SEAT TRACKS MAIN CABIN CORRODED BEYOND LIMITS IAW SRM 51-40-11. REMOVED SEAT TRACKS FROM

All 164: https://openairdocs.org/deregistered/N363DH-2012-02-29/reports.md

## Other aircraft with N363DH

- [Registered now](https://openairdocs.org/aircraft/N363DH): Xag P100 PRO, S/N 1863FPEG8219425X6C82

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