# N364DH: Airbus Industrie A300 B4-203, registration cancelled 2017-05-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 16, 2017
- Exported to: Georgia
- Status when cancelled: Valid registration
- 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: 141
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 3, 2000
- Certificate issued: June 29, 2016
- Last registry action: June 29, 2016
- Mode S code: A41B7B
- Owner when cancelled: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N364DH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=364DH
- Page: https://openairdocs.org/deregistered/N364DH-2017-05-16

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 (133, newest 50)

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

- [SDR DHLA200900036](https://openairdocs.org/sdr/DHLA200900036), Jun 16, 2009: OIL FILTER. CLOGGED. FILTER CLOG LIGHT ILLUMINATED ON MWP. FILTER NR 2 OIL CLOG LIGHT ILLUMINATED ON S/O PANEL AFTER TAKEOFF. REMOVED AND REPLACED MAIN ENGINE OIL FILTER P/N AC9380F
- [SDR DHLA200900032](https://openairdocs.org/sdr/DHLA200900032), May 26, 2009: SWITCH. FAILED. ENGINE NR 2 "OIL CLOG" LIGHT ILLUMINATED INFLIGHT ENGINE 2 WAS SHUTDOWN WITH INFLIGHT ENGINE SHUTDOWN ABNORMAL PROCEDURE ALL ENG IND NORMAL. REPLACED NR 2 ENG O
- [SDR DHLA200900025](https://openairdocs.org/sdr/DHLA200900025), Apr 14, 2009: COALESCER BAG. DIRTY. REPLACED NR 2 COALESCER P/N 20D10-3 IAW MM 21-51-16. THIS DOES NOT CLOSE DMI.
- [SDR DHLA200900023](https://openairdocs.org/sdr/DHLA200900023), Apr 8, 2009: COALESCER BAG. CONTAMINATED. NR 2 PACK STILL HAS AN OILY ODOR 25 MIN INTO FLT R FWD CABIN SMOKE LIGHT ILLUM COMPLIED WITH EMERGENCY CHECK LIST SMOKE LIGHT WENT OUT WHEN NR 2 PACK SELECTED O
- [SDR DHLA200900022](https://openairdocs.org/sdr/DHLA200900022), Apr 4, 2009: ENGINE. LEAKING. STRONG OIL ODOR FROM PACK NR 2 WHEN THROTTLE AT IDLE AND HP VALVE ON ENGINE NR 2 OPEN. ALL PRESS AND TEMPS NORMAL. PLACED NR 2 PACK ON DMI LIST PER MEL 21-51-01
- [SDR DHLA20090020](https://openairdocs.org/sdr/DHLA20090020), Apr 3, 2009: COALESCER BAG. CONTAMINATED. FLT 165 OIL ODOR WITH NR 2 PACK OPERATING. DEFFERED NR 2 PACK IAW MEL 21-51-01 CAT C ASSIGNED DMI 34713 PLACARDS INSTALLED. R/R NR 2 COALESCAR SOCK IAW MM 21-51
- [SDR DHLA200900021](https://openairdocs.org/sdr/DHLA200900021), Apr 1, 2009: UNKNOWN. ODOR. ACFT HAS AN UNUSUAL ODOR COMING THRU THE A/C PACKS FLT DECK DUCT TEMP WAS AT 150 COMPT TEMP 68. RAN NR 1 AND NR 2 PACK SYS OPS CKED NORMAL ON GROUND IAW AMM 21-
- [SDR DHLA200800004](https://openairdocs.org/sdr/DHLA200800004), Jan 10, 2008: UPLOCK SWITCH. MALFUNCTIONED. FLT 165, RIGHT MAIN GEAR DOOR DID NOT RETRACT AFTER GEAR EXTENDED. ABNORMAL PROCEDURE ACCOMPLISHED. CLEANED AND RESECURED RT MLG INBD DOOR UPLOCK SWITCHES, OPER
- [SDR DHLA200700079](https://openairdocs.org/sdr/DHLA200700079), Dec 8, 2007: SEQUENCE VALVE. MALFUNCTIONED. UPON GEAR RETRACTION, RT MAIN GEAR WOULD NOT RETRACT. UNSAFE LIGHT AND GEAR DOOR LIGHTS BOTH ILLUMINATED. PERFORMED LANDING GEAR UNSAFE INDICATION ABNORMAL PROC
- [SDR DHLA200700040](https://openairdocs.org/sdr/DHLA200700040), Aug 8, 2007: PITOT TUBE. MALFUNCTIONED. NO AIRSPEED INDICATION ON STANDBY AIRSPEED INDICATION AT 80 KTS ON CAPT AND FO'S INDICATORS. REJECTED T/O TO WEIGHT 231.2 OAT 26 DEGS C PA 103FT BRAKE TEMP 200 
- [SDR DHLA200700039](https://openairdocs.org/sdr/DHLA200700039), Aug 8, 2007: PITOT LINE. OBSTRUCTED. NO AIRSPEED INDICATION ON STANDBY A/S IND AT 80KTS ONCA AND FO IND REJECTED T/O WEIGHT 273.6 26C OAT P.A 73FT BRAKE TEMP230 1. FLUSHED PITOT STATIC SYSTEM AS PE
- [SDR DHL2007364001](https://openairdocs.org/sdr/DHL2007364001), Jul 1, 2007: FRAME. BENT. DURING A "A"-8 CHECK AT AVBOURNE HVY MX IN MIAMI, THE FOLLOWING DISCREPANCIES WERE NOTED. EXISTING FRAME DOUBLER AT STA 1499 FRAME 21 BETWEEN STR 6 AND 7R WAS B
- [SDR DHL2007364007](https://openairdocs.org/sdr/DHL2007364007), Feb 15, 2007: MECHANISM. CONTAMINATED. LEFT MAIN DOOR SLIDE WARNING LIGHT FLASHING IN FLIGHT WITH SLIDE ARMED AND NO DOORS LIGHT ILLUMINATED. REMOVED ICE DEBRIS FROM LT DOOR SLIDE ARMING MECHANISIM. 
- [SDR DHL2006364007](https://openairdocs.org/sdr/DHL2006364007), Jun 27, 2006: SMOKE DETECTOR. ACTIVATED. PRIOR TO T/O, DURING STATIC RUNUP, MWP SMOKE LIGHT ACCOMPANIED BY MAIN DECK SMOKE DETECTORS 7 & 8 ILLUMINATED ACCOMPANIED BY ACRID SMELL. REPLACED GRD AIR CART 
- [SDR DHL2006364006](https://openairdocs.org/sdr/DHL2006364006), Jun 27, 2006: SMOKE WARNING. MALFUNCTIONED. MWP SMOKE WARNING DURING T/O ACCOMPANIED BY ILLUMINATION OF CABIN DETECTORS NR 7 & NR 8 CAUSED REJECTED TAKEOFF, LIGHTS WENT OUT WHILE WAITING ON TAXIWAY. PERFO
- [SDR DHL2006364504](https://openairdocs.org/sdr/DHL2006364504), May 11, 2006: TEE FITTING. CRACKED. PERFORM EDDY CURRENT INSPECTION OF NR 1 PYLON RIB NR 4 I/B SIDE TEE BRACKET TO VERIFY PREVIOSLY ID CRACK AS PER SB A300-54-068. REMOVED AND REPLACED "T" BRACKET
- [SDR DHL2006364503](https://openairdocs.org/sdr/DHL2006364503), Apr 26, 2006: SEAT TRACK. CORRODED. CABIN FLOOR SEAT TRACK FLANGE AT FS 37 - FS 22 AT RBL 16 HAS CORROSION (MARKED 35/079) UNDER THE FLOOR PANEL. REMOVED CORROSION FROM FS 22 - FS 37 IAW A300 SRM 
- [SDR DHL2006364502](https://openairdocs.org/sdr/DHL2006364502), Apr 26, 2006: SEAT TRACK. CORRODED. CABIN SEAT TRACK FLANGE AT FS 42 - FS 47 RBL16 HAS CORROSION. REMOVED CORROSION AT CABIN FLOOR SEAT TRACK FLANGE BETWEEN FS 42- FS 47 AT RBL 16 IAW A300 SRM 51-
- [SDR DHL2006364501](https://openairdocs.org/sdr/DHL2006364501), Apr 26, 2006: SEAT TRACK. CORRODED. CABIN FLOOR SEAT TRACK FLANGE AT FS 37 - FS 22 AT RBL 58, SUPPORT FLANGES FOR FLOOR PANELS HAS CORROSION. REMOVED CORROSION AT CABIN SEAT TRACK FLANGES FS 22 - 
- [SDR DHL2006364505](https://openairdocs.org/sdr/DHL2006364505), Apr 26, 2006: SEAT TRACK. CORRODED. FOUND CABIN FLOOR SEAT TRACK FLANGE AT FS 25 - FS 22 AT LBL78 HAS CORROSION AT FLOOR SUPPORT FLANGE (MARKED 35/088). REMOVED CORROSION AT SEAT TRACK FROM FS 22 
- [SDR DHL2006364509](https://openairdocs.org/sdr/DHL2006364509), Apr 26, 2006: SEAT TRACK. CORRODED. CABIN FLOOR SEAT TRACK FLANGE AT FS 70 AT RBL 78 HAS CORROSION. CUTOUT CORRODED SECTION. FABRICATED, AND INSTALLED REPAIR AT SEAT TRACK FLANGE AT FS 70 RBL78 IA
- [SDR DHL2006364506](https://openairdocs.org/sdr/DHL2006364506), Apr 25, 2006: SEAT TRACK. CORRODED. FOUND CABIN SEAT TRACK FLANGE AT FS 45 - FS 46 AT LBL 38 HAS CORROSION. REMOVED CORROSION AT FLANGE SEAT TRACK FS 45-46 LBL38 PER A300 SRM 51-40-11 ORIG MAT .07
- [SDR DHL2006364507](https://openairdocs.org/sdr/DHL2006364507), Apr 25, 2006: SEAT TRACK. CORRODED. CABIN SEAT TRACK FLANGE FS 47 - FS 54 AT RBL 38 HAS CORROSION. REMOVED CORROSION AT SEAT TRACK FROM FS 47 - FS 54 RBL38 IAW A300 SRM 51-40-11. FOUND OUT OF LIMI
- [SDR DHL2006364508](https://openairdocs.org/sdr/DHL2006364508), Apr 25, 2006: SEAT TRACK. CORRODED. CABIN SEAT TRACK FLANGE BETWEEN FS 41 - FS 47 HAS CORROSION LBL16. REMOVED CORROSION FROM FS 41 - FS 47 IAW A300 SRM 51-40-11. FOUND OUT OF LIMITS FROM FS 44 - 
- [SDR DHL2006364500](https://openairdocs.org/sdr/DHL2006364500), Apr 25, 2006: SEAT TRACK. CORRODED. CABIN FLOOR PANEL SUPPORT AT FRAME 47 THRU FRAME 50 AT LBL 78 SEAT TRACK FLANGE BEAM HAS CORROSION. REMOVED CORROSION AT SEAT TRACK FROM FR 47 TO FR 50 LBL 78 I
- [SDR DHL2006364511](https://openairdocs.org/sdr/DHL2006364511), Apr 22, 2006: STRUCTURE. CORRODED. UPPER FUSELAGE LT STA 4641 (FS 75) STR 6L HAS CORROSION. REMOVED CORROSION AT UPPER FS LT STA 4641 (FS 75) STR 6L MAT. REMOVED .020 MAT, REMAINING.063 BEYOND LI
- [SDR DHL2006364510](https://openairdocs.org/sdr/DHL2006364510), Apr 22, 2006: STRINGER. CORRODED. UPPER FUSELAGE RT, STA 4641 (FR75) STR 6R HAS CORROSION. REMOVED CORROSION AT UPPER FUSELAGE STA 4641 (FR75) STR 6R. MAT REMOVED .017 MAT REMAINING .O66 BEYOND 
- [SDR DHL2006364005](https://openairdocs.org/sdr/DHL2006364005), Mar 30, 2006: DOWNLOCK SWITCH. DIRTY. RIGHT MLG RED UNSAFE LIGHT ILLUMINATED ON S/O PANEL ON GEAR EXTENSION. GEAR WARNING SOUNDED. PERFORMED ABNORMAL FORWARD PANEL INDICATED 3 GREEN. UNABLE TO DUPLI
- [SDR DHL2006364004](https://openairdocs.org/sdr/DHL2006364004), Mar 24, 2006: THROTTLE CABLE. STIFF. AT FL350-MINUS 48C NR 1 THROTTLE VERY DIFFICULT TO MOVE. THROTTLE DOES NOT MOVE AT ALL IN AUTO THROTTLE. PERFORMED IN FLT ENG SHUT DOWN DUE TO JAMMED NR 1 THROT
- [SDR DHL2006364003](https://openairdocs.org/sdr/DHL2006364003), Mar 16, 2006: BRAKE. OVERHEATED. RTO - BRAKES HOT LIGHT NR 1 BRAKE LIGHT ON S/O PANEL BRAKE TEMP MAX 420 WITH FANS ON BRAKE COOLED WHILE STOPPED AND ROSE TO 320 DURING TAXI IN. RTO=105 KIAS, 5 
- [SDR DHL2006364002](https://openairdocs.org/sdr/DHL2006364002), Jan 28, 2006: SLIDE. UNKNOWN. L1 DOOR WILL NOT MOVE TO THE OPEN AND LOCKED POSITION. TRANSF'D TO DMI 24185 PER MEL 52-61-01-2 CAT -C-. DEF: BY 8597. REF DMI 24185 L1 DOOR WILL NOT MOVE TO TH
- [SDR DHL2006364001](https://openairdocs.org/sdr/DHL2006364001), Jan 12, 2006: FITTING. LOOSE. WHEN LANDING GEAR RETRACTED AFTER TAKEOFF, THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED ON BOTH INDICATORS WITH GEAR HANDLE OFF VIBRATION WAS FELT WITH HANDLE 
- [SDR DHL2005364003](https://openairdocs.org/sdr/DHL2005364003), Oct 2, 2005: SELECTOR VALVE. INOPERATIVE. ON THE GROUND DURING TAXI WHEN MAKING LARGE TURN REQUIRING MORE THAN 10 DEG TILLER. TILLER IS VERY DIFFICULT TO TURN; REQUIRES TWO HANDS. ALSO DURING THIS TIME,
- [SDR DHAL200536400](https://openairdocs.org/sdr/DHAL200536400), Jul 28, 2005: ROLLER. LOOSE. ON DEPARTURE FROM CVG. NOSE GEAR DOORS LIGHT REMAINED ON. PERFORMED ABNORMAL PROCEDURE AND CONTINUED TO DESTINATION RII REQUIRED. FOUND RT NOSE GEAR DOOR UPLATC
- [SDR DHL2005364001](https://openairdocs.org/sdr/DHL2005364001), Apr 25, 2005: FRAME. DAMAGED. FRAME 47 REPAIR RSA FROM AIRBUS IS INTERIM FOR 6 MONTH REF RAS/AS/0114/2004 MSI 05574. REPAIR DESIGN APPROVAL SHEET REF RAS/AS/0114/2004 ISSUE B DATE 12/10/04 I
- [SDR DHL2004364018](https://openairdocs.org/sdr/DHL2004364018), Dec 18, 2004: STRINGER. CRACKED. DURING A-CHECK IN MIAMI, FLORIDA AT AVBORNE HEAVY MAINTENANCE DISCREPANCY AS FOLLOWS, N/R 4418 CRACK AT FR 21 STR 9R INTERNAL. REMOVED FASTENERS OUT OF DAMAGE A
- [SDR DHL2004364017](https://openairdocs.org/sdr/DHL2004364017), Nov 19, 2004: BRAKE ASSY. BINDING. EXCESSIVE BREAKAWAY THRUST REQUIRED TO MOVE AIRCRAFT NR 3 BRAKE ASSY, REMOVED. FOUND NR 3 BRAKE BOUND. REMOVED NR 3 BRAKE ASSY PER MM 32-00-00 AND 32-42-27 XFER
- [SDR DHL2004364015](https://openairdocs.org/sdr/DHL2004364015), Oct 29, 2004: PROXIMITY SENSOR. MALFUNCTIONED. FRONT PANEL LEFT MAIN LANDING GEAR RED UNSAFE MOMENTARILY ILLUMINATED ON APP TO CVG. 2ND OFFICER LEFT MAIN LANDING GEAR INDICATED GREEN AT ALL TIMES WITH LANDIN
- [SDR DHL2004364016](https://openairdocs.org/sdr/DHL2004364016), Aug 24, 2004: FRAME. CORRODED. IN CONJUCTION WITH DHL2004364015, REMOVE & REPLACE DOUBLER AT FRA, 26 & LONGERON 43 LEFT. REMOVED FLOOR PANEL, SIDE WALL PANEL TO GAIN ACCESS TO REPAIR AT STR 4
- [SDR DHL3642004015](https://openairdocs.org/sdr/DHL3642004015), Aug 21, 2004: SKIN. CORRODED. FUSELAGE LAP SEAM 44L HAS A BULGE AND A RIVET POPPED JUST AFT OF FR 26. OPEN ACCESS PANELS FOR SHEETMETAL REPAIR AREA FRAME 26 STRINGER 43. CUT OUT LONGERON 43 
- [SDR DHL2004364014](https://openairdocs.org/sdr/DHL2004364014), Aug 20, 2004: LANDING GEAR. SLOW. LT MAIN GEAR TOOK 15 SECONDS LONGER THAN OTHER GEAR TO EXTEND,TO LOCK.
- [SDR DHL2004364013](https://openairdocs.org/sdr/DHL2004364013), Aug 6, 2004: PROXIMITY SENSOR. MALFUNCTIONED. COULD NOT RAISE LANDING GEAR HANDLE ON SYSTEM 2. COMPLIED WITH ABNORMAL PROC. DID RAISE GEAR ON SYSTEM 1. PROBES ON MWP WAS CAPT PITOT LIGHT ON S/O PANEL. COMPL
- [SDR DHL2004364012](https://openairdocs.org/sdr/DHL2004364012), Jul 10, 2004: BULB. INOPERATIVE. NOSE GEAR INDICATOR ON PILOT'S LANDING GEAR PANEL DID NOT ILLUMINATE GREEN WHEN GEAR EXTENDED. ABNORMAL PROCEDURE ACCOMPLISHED THREE GREEN ON S/O PANEL. RELAMPE
- [SDR DHL2004364011](https://openairdocs.org/sdr/DHL2004364011), Jul 9, 2004: LEVER. MALFUNCTIONED. EXIT DOOR 1R ESCAPE SLIDE DISARM LEVER DOES NOT REACH FULL DISARM POSITION. DEFERRED IAW MEL 52-61-01-2 DMI NR 17140 CAT (C) PLACARD INSTALLED.
- [SDR DHL2004364010](https://openairdocs.org/sdr/DHL2004364010), Jun 29, 2004: LANDING GEAR. MALFUNCTIONED. UNABLE TO RAISE THE LANDING GEAR HANDLE AFTER TAKEOFF. SYSTEM 1 INOPERATIVE. COMPLIED WITH ABNORMAL PROCEDURES. DEFERRED NR 1 LEVER LOCK AND WARNING SYSTEM IAW 
- [SDR DHL2004364009](https://openairdocs.org/sdr/DHL2004364009), Jun 11, 2004: GIRT BAR. DIRTY. UNABLE TO DISARM R-1 DOOR. REMOVED DIRT FROM GIRT BAR. OPS CHECK GOOD IAW 52-10-00. NO PARTS REPLACED.
- [SDR DHL2004364008](https://openairdocs.org/sdr/DHL2004364008), Jun 4, 2004: PROXIMITY SENSOR. FAILED. LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. COMPLETED ABNORMAL PROCEDURE AND GEAR HANDLE OPERATED NORMALLY. SWITCHED TO SYSTEM 1. PERFORMED OPS CHECK
- [SDR DHL2004364007](https://openairdocs.org/sdr/DHL2004364007), Jun 3, 2004: PROXIMITY SENSOR. FAULTY. UPON GEAR RETRACTION GEAR WOULDN'T RAISE. LANDING GEAR HANDLE CANNOT BE RAISED. COMPLETED ABNORMAL, GEAR RAISED NORMALLY. LANDING GEAR LEVER LOCK WAS IN POSITIO
- [SDR DHL2004364006](https://openairdocs.org/sdr/DHL2004364006), Jun 2, 2004: FIRE LOOP. FAULTY. ON CLIMBOUT ENGINE NR 2 LOOP-A LIGHT ILLUMINATED WITH SINGLE STROKE CHIME (SSC) ON MASTER WARNING PANEL (MWP). RAN ABNORMAL PROCEDURE AND TEST WAS SUCCESSFUL. D
- [SDR DHL2004364005](https://openairdocs.org/sdr/DHL2004364005), May 30, 2004: FIRE LOOP. MALFUNCTIONED. LOOPS-A ON ENGINE NR 2 ILLUMINATED ON S/O'S PANEL WITH LOOPS LIGHT ON MASTER WARNING PANEL (MWP) ILLUMINATED WITH A CHIME. COMPLETED ABNORMAL PROCEDURES. LOOP-B

All 133: https://openairdocs.org/deregistered/N364DH-2017-05-16/reports.md

## Other aircraft with N364DH

- [Registered now](https://openairdocs.org/aircraft/N364DH): Sikorsky UH-60L, S/N 95-26602

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