# N365DH: 1981 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: 149
- Year built: 1981
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 5, 1999
- Certificate issued: May 8, 2009
- Last registry action: June 5, 2009
- Mode S code: A41F32
- 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/N365DH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=365DH
- Page: https://openairdocs.org/deregistered/N365DH-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 (130, newest 50)

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

- [SDR DHLA200800013](https://openairdocs.org/sdr/DHLA200800013), Feb 18, 2009: MEC. FAILED. NR 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 ME
- [SDR DHLA200800011A](https://openairdocs.org/sdr/DHLA200800011A), Feb 12, 2009: ENGINE. POWER LOSS. DURING 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. RE
- [SDR DHLA200800138](https://openairdocs.org/sdr/DHLA200800138), Dec 28, 2008: NOSE COWL. DAMAGED. RAMP 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 REPLACEME
- [SDR DHLA200800019](https://openairdocs.org/sdr/DHLA200800019), Mar 1, 2008: BOTTLE. READS LOW. R1 DOOR ESCAPE SLIDE PRESSURE IN RED. REMOVED AND REPLACED SLIDE ASSY. AIRCRAFT WAS GROUNDED.
- [SDR DHLA200800003](https://openairdocs.org/sdr/DHLA200800003), Jan 6, 2008: SKIN. DAMAGED. LOWER 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 IN
- [SDR DHLA200700043](https://openairdocs.org/sdr/DHLA200700043), Sep 12, 2007: INERTIA REEL. LOOSE. INERTIAL REEL CAME LOOSE DURING TAKEOFF ROLL. INSPECTED INERTIAL REEL. FOUND OK. REINSTALLED IN POSITION AS PER MM 25-61-13.
- [SDR DHL2006365003](https://openairdocs.org/sdr/DHL2006365003), Aug 1, 2006: BRAKE. OVERHEATED. CREW 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 BOGI
- [SDR DHL2006365504](https://openairdocs.org/sdr/DHL2006365504), Jun 26, 2006: SKIN. DENTED. DENT 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.
- [SDR DHL2006365503](https://openairdocs.org/sdr/DHL2006365503), Mar 28, 2006: DOOR FRAME. CORRODED. LEFT 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 & 53-10-0
- [SDR DHL2006365501](https://openairdocs.org/sdr/DHL2006365501), Mar 9, 2006: STRINGER. CORRODED. FOUND 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. REINSTA
- [SDR DHL2006365500](https://openairdocs.org/sdr/DHL2006365500), Mar 9, 2006: SEAT TRACK. CORRODED. FLOOR 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 AN
- [SDR DHL2006365502](https://openairdocs.org/sdr/DHL2006365502), Mar 7, 2006: SEAT TRACK. CORRODED. MAIN 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 TR
- [SDR DHL2006365002](https://openairdocs.org/sdr/DHL2006365002), Feb 15, 2006: WARNING SYSTEM. ACTIVATED. NOSE 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 UNS
- [SDR DHL2006365001](https://openairdocs.org/sdr/DHL2006365001), Feb 15, 2006: SWITCH. FAILED. NOSE 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 GE
- [SDR DHL2005365500](https://openairdocs.org/sdr/DHL2005365500), Oct 15, 2005: RIB. CRACKED. DURING ACCOMPLISHMENT OF EA57530001-001-A WHILE AT AVBORNE HEAVY MAINTENANCE INC LEFT INBOARD FLAP RIB NR 7 (FITTING} OUTBOARD SIDE FOUND CRACKED. REMOVED AND R
- [SDR DHL2005365007](https://openairdocs.org/sdr/DHL2005365007), Oct 4, 2005: LATCH. LACK OF LUBE. COCKPIT 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.
- [SDR DHL2005365006](https://openairdocs.org/sdr/DHL2005365006), Sep 22, 2005: SENSOR. MALFUNCTIONED. STALL WARNING AT TAKEOFF WITH CONTINUOUS STICK SHAKER FROM TAKEOFF TO LANDING. REMOVED AND REPLACED AOA PROBE. OPS CHECKS OK IAW MM 27-36-15.
- [SDR DHL2005367003](https://openairdocs.org/sdr/DHL2005367003), Aug 10, 2005: BATTERY PACK. INOPERATIVE. L1 EMRG LT INOP. REMOVED AND REPLACED, L1 EMERG LT BATT PACK IAW 33-51-13.
- [SDR DHL2005365005](https://openairdocs.org/sdr/DHL2005365005), Jul 23, 2005: CALL HORN. MALFUNCTIONED. RTO RWR 27 MECHANIC CALL HORN ACTIVATED. MECHANIC CALL CURRENTLY DEFERRED. REF DMI 21755. NO PROVISIONS TO DEACTIOVATE CALL. BREIFED CREW. AC OK FOR SERVICE
- [SDR DHL2005365004](https://openairdocs.org/sdr/DHL2005365004), Jul 20, 2005: WARNING LIGHT. ILLUMINATED. ON 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 OP
- [SDR DHL2005365003](https://openairdocs.org/sdr/DHL2005365003), May 18, 2005: FUEL LINE. RUPTURED. APU 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 
- [SDR DHL2005365002](https://openairdocs.org/sdr/DHL2005365002), Jan 25, 2005: GARLOCK SEAL. LEAKING. CREW 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 
- [SDR DHL2005365001](https://openairdocs.org/sdr/DHL2005365001), Jan 15, 2005: CABLE. OUT OF ADJUST. ENG 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 WA
- [SDR DHL2004365007](https://openairdocs.org/sdr/DHL2004365007), Dec 17, 2004: CONTROL UNIT. MALFUNCTIONED. ON 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 SY
- [SDR DHL2004365005](https://openairdocs.org/sdr/DHL2004365005), Nov 3, 2004: CONTROL UNIT. INOPERATIVE. WHILE 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 RELEASIN
- [SDR DHL2004365004](https://openairdocs.org/sdr/DHL2004365004), Sep 26, 2004: SERVO VALVE. DIRTY. AFTER 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 
- [SDR DHL2004365003](https://openairdocs.org/sdr/DHL2004365003), Sep 8, 2004: CONNECTOR. CONTAMINATED. AFTER DEPARTURE, THE LEFT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED ON THE CENTER PANEL AFTER GEAR RETRACTION. THE ASSOCIATED LIGHT WAS EXTINGUISHED ON THE SE
- [SDR DHL2004365002](https://openairdocs.org/sdr/DHL2004365002), Jul 22, 2004: WINDSHIELD. CRACKED. FO'S WINDSHIELD FRACTURED WHILE ENROUTE.
- [SDR DHL2004365001](https://openairdocs.org/sdr/DHL2004365001), Jun 26, 2004: SERVO VALVE. INOPERATIVE. LEFT 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
- [SDR DHL2004365508](https://openairdocs.org/sdr/DHL2004365508), Jan 22, 2004: SKIN. DENTED. FUSELAGE 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 
- [SDR DHL2004365514](https://openairdocs.org/sdr/DHL2004365514), Jan 19, 2004: FRAME. CRACKED. REPAIR 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 CIRCUM
- [SDR DHL2004365507](https://openairdocs.org/sdr/DHL2004365507), Jan 13, 2004: SKIN. DAMAGED. REPAIR 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 D
- [SDR DHL2004365515](https://openairdocs.org/sdr/DHL2004365515), Jan 7, 2004: SEAT TRACK. CORRODED. MAIN 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
- [SDR DHL2004365513](https://openairdocs.org/sdr/DHL2004365513), Jan 7, 2004: FLOORBEAM. CORRODED. EXFOLATING 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 .
- [SDR DHL2004365512](https://openairdocs.org/sdr/DHL2004365512), Jan 7, 2004: SEAT TRACK. CORRODED. MAIN 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 DEC
- [SDR DHL2004365511](https://openairdocs.org/sdr/DHL2004365511), Jan 7, 2004: SEAT TRACK. CORRODED. MAIN 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
- [SDR DHL2004365506](https://openairdocs.org/sdr/DHL2004365506), Jan 7, 2004: SEAT TRACK. CORRODED. MAIN 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 0.0
- [SDR DHL2004365504](https://openairdocs.org/sdr/DHL2004365504), Jan 5, 2004: SEAT TRACK. CORRODED. MAIN 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 I
- [SDR DHL2004365510](https://openairdocs.org/sdr/DHL2004365510), Jan 3, 2004: SEAT TRACK. CORRODED. SEAT 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 LI
- [SDR DHL2004365509](https://openairdocs.org/sdr/DHL2004365509), Jan 3, 2004: SEAT TRACK. CORRODED. SEAT 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
- [SDR DHL2004365505](https://openairdocs.org/sdr/DHL2004365505), Jan 3, 2004: SEAT TRACK. DAMAGED. SEAT 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 APPR
- [SDR DHL2004365503](https://openairdocs.org/sdr/DHL2004365503), Jan 3, 2004: SEAT TRACK. CORRODED. MAIN 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
- [SDR DHL2004365502](https://openairdocs.org/sdr/DHL2004365502), Jan 3, 2004: SEAT TRACK. CORRODED. SEAT 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. 
- [SDR DHL2004365501](https://openairdocs.org/sdr/DHL2004365501), Jan 3, 2004: SEAT TRACK. GOUGED. SEAT 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 
- [SDR DHL2004365500](https://openairdocs.org/sdr/DHL2004365500), Jan 3, 2004: SEAT TRACK. DAMAGED. SEAT 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
- [SDR DHL2003365014](https://openairdocs.org/sdr/DHL2003365014), Sep 8, 2003: SERVO VALVE. INOPERATIVE. RT 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 MAINTAINI
- [SDR DHL2003365013](https://openairdocs.org/sdr/DHL2003365013), Aug 5, 2003: DOWNLOCK SWITCH. MALFUNCTIONED. NO 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 79G
- [SDR DHL2003365012](https://openairdocs.org/sdr/DHL2003365012), Aug 5, 2003: PROXIMITY SENSOR. CONTAMINATED. NOSE 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 WARNI
- [SDR DHL2003365011](https://openairdocs.org/sdr/DHL2003365011), Aug 5, 2003: POWER SUPPLY. DISCHARGED. L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED CHARGE SUPPLY UNIT, OPS CHECKED OK IAW 33-51-00.
- [SDR DHL2003365010](https://openairdocs.org/sdr/DHL2003365010), Jul 1, 2003: SKIN. DENTED. SMALL 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 I

All 130: https://openairdocs.org/deregistered/N365DH-2012-02-29/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20060801020419I](https://openairdocs.org/incident/20060801020419I), Aug 1, 2006: Airbus A300B4203 (N365DH), Wilmington, OH, Minor damage. (-23) Crew received a hot brake annunciation during take-off roll at 140KIAS. V1 speed was 152KIAS. Crew elected to reject take-off. Aircraft remained on…

## Other aircraft with N365DH

- [Registered now](https://openairdocs.org/aircraft/N365DH): Kodiak KODIAK 100, S/N 100-0365, built 2026

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.