# N472AS: 1980 Airbus Industrie A300 B4-203, registration cancelled 2008-12-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 9, 2008
- Exported to: United Arab Emirates
- Status when cancelled: Triennial form not returned
- Airframe: [Airbus Industrie A300 B4-203](https://openairdocs.org/model/airbus-industrie-a300-b4-203) (registry code 3930306)
- Engine: [GE CF6-50C2](https://openairdocs.org/engine/ge-cf6-50c2) (registry code 30085)
- Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs)
- Serial number: A0125
- Year built: 1980
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 20, 2000
- Certificate issued: September 12, 2000
- Last registry action: January 16, 2007
- Mode S code: A5C899
- Owner when cancelled: [Dmcmag I LLC](https://openairdocs.org/faa-owner/DMCMAG%20I%20LLC)
- Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)
- Owner type: Corporation
- Owner's area on the map: 25.7795° N, 80.2996° W: Placed by OpenAirDocs at the center of ZIP code 33126, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N472AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=472AS
- Page: https://openairdocs.org/deregistered/N472AS-2008-12-09

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 (28)

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

- [SDR XN0A1361](https://openairdocs.org/sdr/XN0A1361), Feb 8, 2007: CONNECTOR. DIRTY. APU QUIT AT 22,000 FEET, RUNNING ON ONE GENERATOR TRIED TO RESTART, APU WOULD NOT START. DROPPED TO 20,000 FEET, RESTARTED APU AND IT QUIT AGAIN AT 20,000 FEET.
- [SDR XN0A1360](https://openairdocs.org/sdr/XN0A1360), Feb 3, 2007: CONTROL UNIT. MALFUNCTIONED. RUDDER WILL ONLY GO .5 TO .6666 OR 20 UNITS TO THE LT DURING GROUND CONTROL CHECK. FOUND ARTIFICIAL FEEL AND TRIM UNIT CATCHING ON TRIM STOP. REMOVED AND REPLAC
- [SDR XN0A1359](https://openairdocs.org/sdr/XN0A1359), Feb 1, 2007: GCU. FAULTED. NR 1 PITCH TRIM TRIPPED BEFORE TAXI. ALL COCKPIT LIGHTS STARTED FLASHING WITH POWER-UP FOR TAXI. LOST VSI INDICATORS TEMPORARILY. LOST TAWS INDICATIONS. FOUND N
- [SDR XN0A1353](https://openairdocs.org/sdr/XN0A1353), Sep 18, 2006: HYDRAULIC SYSTEM. LEAKING. ON ENGINE START, BLUE HYDRAULIC SYSTEM LEVEL LOW LIGHT CAME ON. INSPECTED SYSTEM FOR LEAK, SERVICED BLUE SYSTEM WITH 2 GALLONS IAW A300 AMM CHAPTER 12-12-29.
- [SDR XN0A1352](https://openairdocs.org/sdr/XN0A1352), Aug 31, 2006: INDICATOR. STICKING. FCPI INDICATOR STICKING, ELEV POSITION. FOUND C/P LOOSE ON FCPI IND. RESECURED C/P, OPS CHECK GOOD IAW A300 AMM 27-35-00.
- [SDR XN0A1351](https://openairdocs.org/sdr/XN0A1351), Aug 22, 2006: UPLOCK. DAMAGED. AFTER GEAR RETRACTION, LT LIGHTS, DOOR AND GEAR UNSAFE STAYED ON. REMOVED AND REPLACED LT MLG UPLOCK ASSY IAW AMM CHAPTER 32-31-44, LEAK AND OPS CHECKS GOOD. PE
- [SDR XN0A1348](https://openairdocs.org/sdr/XN0A1348), Aug 4, 2006: WARNING LIGHT. ILLUMINATED. ON TAXI NR 2 MANIFOLD FAULT AND APU MANIFOLD FAULT LIGHT ILLUM, WILL NOT RESET. FOUND LT FLOW CONTROL VALVE LEAKING, R&R FLOW CONTROL VALVE IAW A300 AMM CHAPTER
- [SDR XN0A1330](https://openairdocs.org/sdr/XN0A1330), May 11, 2006: CONTROL LEVER. MALFUNCTIONED. ON TAKEOFF L/G WOULD NOT RETRACT- SYSTEM 1 OR SYSTEM 2, NO HELP. NORMAL LANDING ACCOMPLISHED. DURING TROUBLESHOOTONG FOUND LANDING GEAR LEVER CONTROL MODULE RES
- [SDR XN0A1323](https://openairdocs.org/sdr/XN0A1323), Apr 27, 2006: WIRE. BROKEN. ON TAXI OUT F/O HSI HEADING FLAG APPEARS DURING ALL TURNS. FOUND BROKEN WIRE AT BACK OF COMPASS COUPLER RACK. REPAIRED AND OPS CHECK GOOD IAW A300 AMM CHAPTER 3
- [SDR XN0A1319](https://openairdocs.org/sdr/XN0A1319), Apr 19, 2006: SHAFT. SHEARED. AFTER BLOCK OUT, DURING CROSS START- NR 2 ENGINE WOULD NOT START. NO N1 OR N2 INDICATIONS. START VALVE OPEN LIGHT CAME ON BUT NO START. FOUND STARTER SHAFT SHEA
- [SDR XN0A1315](https://openairdocs.org/sdr/XN0A1315), Apr 1, 2006: FLAP. MALFUNCTIONED. FLASHING KRUEGER LIGHT AFTER SLATS RETRACTED WITH CONFIG LIGHT ILLUMINATED AND RT LOW-SPEED AILERON CROSSHATCHED. SLAT/FLAP HANDLE IN SLATS EXTEND, KRUEGER INDI
- [SDR XN0A1313](https://openairdocs.org/sdr/XN0A1313), Mar 29, 2006: CONTROLLER. MALFUNCTIONED. REJECTED T/O DUE TO MOMENTARY CONFIG LIGHT ON MAIN WARNING PANEL AND AUDIO CHIMES. R&R MASTER WARNING CONTROLLER IAW A300 AMM CHAPTER 33-15-11, OPS CK GOOD. WIT
- [SDR XN0A1309](https://openairdocs.org/sdr/XN0A1309), Mar 9, 2006: WARNING LIGHT. FALSE INDICATION. CONFIG LIGHT ILLUMINATED ON TAKEOFF ROLL WITH MASTER WARNING. PERFORMED OPERATIONAL CHECK OF MASTER WARNING AND TAKEOFF CONFIG, CHECKED PROX BOX FOR DEFECTS AND
- [SDR XN0A1285](https://openairdocs.org/sdr/XN0A1285), Dec 16, 2005: GYRO. INOPERATIVE. NR 3 DG INOPERATIVE. PLACED NR3 DG ON DEFERRAL IAW MEL 34-11-07 CAT C DMI NR 51005 PLACARDS INSTALLED. (ORIG/OPEN)
- [SDR XN0A1238](https://openairdocs.org/sdr/XN0A1238), May 24, 2005: INDICATOR. FAILED. BTB DUE FAIL FLAG ON NR 1 ALT FLAG IN VIEW. REMOVED AND REPLACED NR 1 ALT INDICATOR. OPS CK NORMAL IAW MM 34-12-21 (STATUS:ORIG/CLOSED)
- [SDR XN0A1224](https://openairdocs.org/sdr/XN0A1224), Jan 19, 2005: CONTROL BOX. MALFUNCTIONED. ON TAXI, GREEN BRAKES VERY SPONGY, ALT BRAKES NO BRAKING. REMOVED AND REPLACED ANTI-SKID CONTROL BOX IAW A300 MM 32-42-72. SERVICED EMERGENCY BRAKE RESERVOIR IA
- [SDR XN0A1216](https://openairdocs.org/sdr/XN0A1216), Dec 14, 2004: WIRE. CHAFED. NR 3 WITH SLAT RETRACTION LOW SPEED AILERONS (RED LIGHT) & CONFIG LIGHT ON FWD PANEL ILLUMINATED. TRANFERED TO DMI LIST IAW ENA A300 MEL 27-11-01, CAT "B" DMI 4
- [SDR XNOA1191](https://openairdocs.org/sdr/XNOA1191), Jun 29, 2004: A/C PACK. SHUTDOWN. ON TAXI, NR 1 PACK SHUT-OFF. RE-SEATED CIRCUIT BREAKER AND OPS CHECK GOOD IAW A300 AMM CHAPTER 21-51-00.
- [SDR XNOA01092](https://openairdocs.org/sdr/XNOA01092), Dec 3, 2002: REGULATOR. FAILED. DURING FLIGHT CONTROL CHECK AILERONS CONTROL VERY HEAVY. WILL NOT RETURN TO NEUTRAL. REMOVED & REPLACED LT CONTROL CABLE TENSION REGULATOR ASSY IAW A300 MM 27-1
- [SDR XNOA01042](https://openairdocs.org/sdr/XNOA01042), Mar 29, 2002: ENGINE. OUT OF RIG. NR 1 ENGINE IS SLOW TO SPOOL. LAGS BEHIND NR 2 ENGINE BY 35 PERCENT N1. PERFORMED STATIC RIG CHECK VSV. NO FAULT FOUND. BOROSCOPED 1,5,6,13,14 COMPRESSOR, HPT-1
- [SDR XNOA01040](https://openairdocs.org/sdr/XNOA01040), Mar 26, 2002: ENGINE. OUT OF TRIM. NR 1 ENGINE IS SLOW TO SPOOL & WILL NOT OBTAIN MAX POWER. TRIMMED NR 1 ENGINE MEC IAW A300 MM 71-00-00. OPS & LEAK CHECK GOOD.
- [SDR XN0A01033](https://openairdocs.org/sdr/XN0A01033), Dec 4, 2001: PUMP. FAILED. RETURNED TO THE GATE DUE NR 1 ENGINE GREEN HYD PUMP INOP. REMOVED AND REPLACED NR 1 ENGINE GREEN HYD PUMP IAW MM 29-11-00. OPS CHECK/LEAK CHECK GOOD.
- [SDR XN0A01025](https://openairdocs.org/sdr/XN0A01025), Sep 21, 2001: UPLOCK. OUT OF ADJ. NOSE DOOR AMBER LIGHT REMAINED ON AFTER GEAR RETRACTION AND NOSE DOOR OPENED UP AT GEAR NEUTRAL. ADJUSTED NLG RT FWD DOOR UPLOCK ASSEMBLY IAW A300 MM 32-22-11 L
- [SDR XN0A01024](https://openairdocs.org/sdr/XN0A01024), Sep 20, 2001: UPLOCK. OUT OF ADJ. NOSE GEAR DOOR LIGHT ILLUMINATED AFTER TAKEOFF WHEN GEAR RETRACT. INSPECTED NOSE GEAR DOORS, FOUND NO DAMAGE. INSPECTED NOSE GEAR DOOR UPLOCK ASSY AND MECHANISM
- [SDR XN0A01022](https://openairdocs.org/sdr/XN0A01022), Sep 19, 2001: UHF COMM. INOPERATIVE. NUMBER 2 RADIO DOES NOT TRANSMIT. TRANSFERRED NR 2 UHF COMM TRANSMIT TO DMI LOG IAW ENA MEL 23-10-01.
- [SDR XNA01014](https://openairdocs.org/sdr/XNA01014), Jul 25, 2001: WARNING LIGHT. ILLUMINATED. ON TAXI, KRUEGER LIGHT FLASHING AND CONFIG LIGHT ON MWP. TRANSFERRED TO DMI 1421 IAW 27-84-01. DEACTIVATED LEFT NOTCH AND KRUEGER IAW SP 27-84-02. PLACARDS INST
- [SDR XNA01012B](https://openairdocs.org/sdr/XNA01012B), Jun 21, 2001: WARNING LIGHT. ILLUMINATED. KRUEGER LIGHT FLASHING AND CONFIGURATION HORN/FLAPS O-SLATS 16. TRANSFERRED TO DMI LIST PER ENA A300 MEL 27-84-02. DMI 1352 PLACARDS INSTALLED. SP 27-84-02 COMP
- [SDR XNA01009](https://openairdocs.org/sdr/XNA01009), May 15, 2001: ENGINE. MALFUNCTIONED. LOUD BANG RIGHT ENGINE AT 16000 FT. EGT WENT TO RED LINE. SHUT ENGINE DOWN AT 06:12 Z.

## Other aircraft with N472AS

- [Registered now](https://openairdocs.org/aircraft/N472AS): Boeing 737-990ER, S/N 60580, built 2015

---
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.
