# N463AP: British Aerospace BAE 146 SERIES 100A, registration cancelled 2004-09-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 2, 2004
- Exported to: Canada
- Status when cancelled: Valid registration
- Airframe: [British Aerospace BAE 146 SERIES 100A](https://openairdocs.org/model/british-aerospace-bae-146-series-100a) (registry code 1500260)
- Engine: [Lycoming AL503 series](https://openairdocs.org/engine/lycoming-al503-series) (registry code 41583)
- Data sheets: [TCDS A49EU](https://openairdocs.org/tcds/A49EU) (OpenAirDocs)
- Serial number: E1063
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: February 13, 1987
- Certificate issued: December 2, 1998
- Last registry action: November 6, 2002
- Mode S code: A5A4CE
- Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%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/N463AP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=463AP
- Page: https://openairdocs.org/deregistered/N463AP-2004-09-02

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 British Aerospace BAE 146 SERIES 100A: https://openairdocs.org/model/british-aerospace-bae-146-series-100a.md

## Service difficulty reports (84, newest 50)

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

- [SDR A6WA200100059](https://openairdocs.org/sdr/A6WA200100059), Nov 11, 2001: FCU. MALFUNCTIONED. UNABLE TO CONTROL POWER ON NR 2 ENGINE. POWER INCREASED REGARDLESS OF THRUST LEVER POSITION SHUTDOWN ENGINE WITH T-HANDLE. MAINTENANCE REMOVED AND REPLACED FUEL
- [SDR A6WA200100037](https://openairdocs.org/sdr/A6WA200100037), Jun 6, 2001: SCREW. MISSING. UPPER HINGE COVER PANEL ON LEFT HAND ELEVATOR HELD ON BY ONLY ONE SCREW; FOUR SCREWS MISSING. MAINTENANCE REMOVED AND REPLACED MISSING SCREWS.
- [SDR A6WA9900049](https://openairdocs.org/sdr/A6WA9900049), May 29, 1999: ANGLE. CRACKED. FORWARD PASSENGER DOOR, INTERNAL ANGLE CRACKED. REPLACED ANGLE. (X)
- [SDR A6WA9900048](https://openairdocs.org/sdr/A6WA9900048), May 29, 1999: SKIN. DAMAGED. REPAIR TO RIGHT SIDE OF FUSELAGE AT FRAMES 11-13 AT LAP 'E' AREA. C/W REPAIR IAW BAE 146 SRM AND FAX CW/RJ/0754-99, CW/RJ/0761-99 AND DRAWING HC537H9411. (X)
- [SDR A6WA9900054](https://openairdocs.org/sdr/A6WA9900054), May 7, 1999: STIFFENER. CRACKED. LEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER NR 176 BEWEEN RIBS 7 AND 8 CRACKED, FORWARD END. REPLACED LEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENE
- [SDR A6WA9900053](https://openairdocs.org/sdr/A6WA9900053), May 7, 1999: STIFFENER. CRACKED. RIGHT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER, NR 176 BETWEEN RIBS 7 AND 8, CRACKED FORWARD END. REPAIRED RT WING TRAILING EDGE UPPER SHROUD SKIN STIFFEN
- [SDR A6WA9900052](https://openairdocs.org/sdr/A6WA9900052), May 7, 1999: STIFFENER. CRACKED. RIGHT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER, NR 172 BETWEEN RIBS 3 AND 4, CRACKED FORWARD END. REPLACED RT WING TRAILING EDGE UPPER SHROUD SKIN STIFFEN
- [SDR A6WA9900051](https://openairdocs.org/sdr/A6WA9900051), May 7, 1999: STIFFENER. CRACKED. LEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER, NR 178 BETWEN RIBS 8 AND 9, CRACKED FORWARD END. REPLACED LT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER
- [SDR 17WA9900050](https://openairdocs.org/sdr/17WA9900050), May 7, 1999: STIFFENER. CRACKED. LEFT WING TRAILING EDGE UPPER SHROUD SKIN STIFFENER NR 177 BETWEEN RIBS 8 AND 9 CRACKED FORWARD END. REPAIRED LEFT WING SKIN TRAILING EDGE, UPPER WING SKIN TRAI
- [SDR A6WA9900055](https://openairdocs.org/sdr/A6WA9900055), Apr 21, 1999: STIFFENER. CRACKED. UPPER WING SKIN TRAILING EDGE STIFFENER IS CRACKED AT FORWARD END LOCATED BETWEEN RIBS 9 AND 10, LEFT WING. REPAIRED LT WING SKIN TRAILING EDGE UPPER WING SKIN 
- [SDR 99ZZZX2700](https://openairdocs.org/sdr/99ZZZX2700), Jan 1, 1999: SLIDE. DEPLOYED. ORD - FLT 545 - WHILE INSPECTING GIVE BAR MECHANISM ON FORWARD PASSENGER DOOR, SLIDE PARTIALLY DEPLOYED. REMOVED AND REPLACED FORWARD PASSENGER DOOR SLIDE IAW M
- [SDR 99ZZZM548](https://openairdocs.org/sdr/99ZZZM548), Jan 1, 1999: SLIDE. OUT OF POSITION. WHILE INSPECTIONG GIVE BAR MECHANISM ON FORWARD PASSENGER DOOR SLIDE PARTIALLY DEPLOYED. REMOVED AND REPLACED FORWARD PASSENGER DOOR SLIDE IAW MM. (M)
- [SDR 99ZZZM471](https://openairdocs.org/sdr/99ZZZM471), May 23, 1998: HANDLE. OUT OF ADJUST. FORWARD PAX DOOR, SLIDE ARMING HANDLE HITS THE HANDLE RECESS NOT ALLOWING THE GIRT BAR TO FULLY ENGAGE INTO LUGS. REMOVED UPPER DOOR COVER AND ARMING HANDLE REC
- [SDR 99ZZZM461](https://openairdocs.org/sdr/99ZZZM461), May 22, 1998: BRACKET. CRACKED. LEFT WING, FORWARD HYD LINE CLAMP BRACKET, RIB 5, CRACKED. REPLACED BRACKET. (M)
- [SDR 99ZZZM457](https://openairdocs.org/sdr/99ZZZM457), May 22, 1998: STIFFENER. CRACKED. RIGHT WING TE LOWER SHROUD SKIN STIFFENER CRACKED BETWEEN RIB 7/8. REPLACED STIFFENER IN RIGHT WING TE LOWER SHROUD SKIN BETWEEN RIBS 7/8. (M)
- [SDR 99ZZZM449](https://openairdocs.org/sdr/99ZZZM449), May 22, 1998: DOOR. DAMAGED. NR 3 ENGINE AFT INBOARD FAN DOOR LOWER DOOR SPLITTER AREA HAS CHAFED STIFFENER, 2ND FROM FORWARD. REPLACED ABOVE STIFFENER PER SRM. (M)
- [SDR 99ZZZM448](https://openairdocs.org/sdr/99ZZZM448), May 22, 1998: SKIN. CHAFED. NR 3 ENGINE AFT INBOARD FAN DOOR INNER TITANIUM SKIN CHAFED THROUGH. REPLACED PAN AND PATCHED SMALL AREA 2.25 BY 3.5 USING TAZ PER PSI. (M)
- [SDR 99ZZZM446](https://openairdocs.org/sdr/99ZZZM446), May 22, 1998: DOOR. CRACKED. NR 1 ENGINE AFT LEFT COWL DOOR SECOND STIFFENER ON LOWER SPLITTER ASSY CRACKED. REPLACED SECOND STIFFENER ON NR 1 ENGINE LEFT COWL DOOR. (M)
- [SDR 99ZZZM445](https://openairdocs.org/sdr/99ZZZM445), May 22, 1998: BULKHEAD. CRACKED. NR 1 ENGINE LEFT AFT COWL DOOR BULKHEAD AT VENT TUBE AREA CRACKED. REPAIRED CRACK IN FLANGE OF BULKHEAD BY PATCHING IAW BAE/AIR WISC SRM STANDARD PRACTICES. (M)
- [SDR 99ZZZM472](https://openairdocs.org/sdr/99ZZZM472), May 21, 1998: BULKHD LONGERON. CRACKED. FRAME 29 MAIN LANDING GEAR BAY ROOF PRESSURE BULKHEAD, LONGERONS NR 3, NR 9, NR 15 CRACKED. REPAIRED PRESS BULKHEAD LONGERONS NR 3, NR 9, AND NR 15 PER REPAIR D
- [SDR 99ZZZM470](https://openairdocs.org/sdr/99ZZZM470), May 21, 1998: MASK. TORN. CAIN OXYGEN MASKS FOR PASSENGERS FILTERS TORN SEAT 3A, 10B, 12A, 12B, 14C, 15C, 13E, 10F. REMOVED AND REPLACED FILTER TO PER COMPONENT MM TO 3A, 10B, 12A, 12B, 
- [SDR 99ZZZM464](https://openairdocs.org/sdr/99ZZZM464), May 21, 1998: STIFFENER. CRACKED. RIGHT WING TE SHROUD TOP SKIN STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 7/8. REPAIRED RIGHT WING TE TOP SHROUD SKIN STIFFENER BETWEEN RIBS 7/8. (M)
- [SDR 99ZZZM459](https://openairdocs.org/sdr/99ZZZM459), May 21, 1998: STIFFENER. CRACKED. LEFT WING TE SHROUD TO PSKIN STIFFENERS ARE CRACKED AT FORWARD END IN AREA BETWEEN RIBS 8/9. REPAIRED LEFT WING TE SHROUD TO SKIN STIFFENER BETWEEN RIBS 8/9. (M
- [SDR 99ZZZM458](https://openairdocs.org/sdr/99ZZZM458), May 21, 1998: STIFFENER. CRACKED. LEFT WING TE TOP SKIN STIFFENER IS CRACKED AT FORWARD END IN AREA BETWEEN RIBS 7/8. REPAIRED LEFT WING TE TOP SKIN STIFFENER BETWEEN RIBS 7/8 IAW BAE FAX NR JM/
- [SDR 99ZZZM455](https://openairdocs.org/sdr/99ZZZM455), May 21, 1998: BRACKET. CRACKED. ANGLE BRACKET, P/N HC361JO137-006 CRACKED. LOCATED AT RIGHT ECS DUCT FRAME 45 SUPPORT OVERTEMP SWITCH BRACKET. MANUFACTURED BRACKET IAW AIR WISC/BAE SRM STANDAR
- [SDR 99ZZZM454](https://openairdocs.org/sdr/99ZZZM454), May 21, 1998: STIFFENER. CRACKED. LEFT WING TRAILING EDGE SHROUD TOP SKIN STIFFENER IN AREA BETWEEN RIBS 9/10 IS CRACKED AT FORWARD END. REPAIRED LEFT WITH TE SHROUD TOP SKIN STIFFENER BETWEEN R
- [SDR 99ZZZM451](https://openairdocs.org/sdr/99ZZZM451), May 21, 1998: DOOR. DAMAGED. NR 4 ENGINE AFT OUTBOARD FAN DOOR LOWER DOOR SPLITTER AREA 2ND STIFFENER FROM FORWARD CHAFED. REPLACED NR 4 ENGINE AFT OUTBOARD FAN DOOR LOWER DOOR SPLITTER ARE
- [SDR 99ZZZM450](https://openairdocs.org/sdr/99ZZZM450), May 21, 1998: DOOR. DAMAGED. NR 4 ENGINE AFT OUTBOARD FAN DOOR LOWER DOOR SPLITTER AREA, STIFFENER AT FORWARD CORNER CHAFED BADLY. REPLACED NR 4 ENGINE AFT OUTBOARD FAN DOOR LOWER DOOR SPLI
- [SDR 99ZZZM436](https://openairdocs.org/sdr/99ZZZM436), May 21, 1998: STIFFENER. CRACKED. RIGHT WING TE TOP SHROUD SKIN STIFFENER CRACKED AT FORWARD END INBOARD OF RIB 9. REPAIRED RIGHT WING TE TOP SHROUD SKIN STIFFENER BETWEEN RIBS 8/9 IAW BAE FAX N
- [SDR 99ZZZM463](https://openairdocs.org/sdr/99ZZZM463), May 20, 1998: FALSE SPAR. CRACKED. RIGHT WING TE HAS TEMP REPAIR (STOP DRILL) TO CRACK IN FALSE SPAR CAP BETWEEN RIBS 7/8, NEEDS PERM REPAIR. REPAIRED RIGHT WING TE BETWEEN RIBS 7/8. (M)
- [SDR 99ZZZM462](https://openairdocs.org/sdr/99ZZZM462), May 20, 1998: STIFFENER. CRACKED. TOP RIGHT WING T/E SKIN STIFFENER TWIX WING RIBS 3/4 CRACKED AT AFT END. REPAIRED RIGHT WING TE TOP SHROUD SKIN STIFFENER BETWEEN RIBS 3/4. (M)
- [SDR 99ZZZM460](https://openairdocs.org/sdr/99ZZZM460), May 20, 1998: STIFFENER. CRACKED. LEFT WING TE SHROUD BOTTOM SKIN STIFFENER CLEATS ARE CRACKED IN AREA BETWEEN RIBS 8/9. REPLACED BOTH CLEATS AS PER POSITIONS ABOVE USING BAE STANDARD PRACTICES 
- [SDR 99ZZZM440](https://openairdocs.org/sdr/99ZZZM440), May 20, 1998: GUSSET. CORRODED. NR 2 GUSSET PLATES CORRODED LEFT SIDE FRAME 15 FLOORBEAM. REPLACED TWO GUSSET PLATES LEFT SIDE FRAME 15 FLOORBEAM. (M)
- [SDR 99ZZZM469](https://openairdocs.org/sdr/99ZZZM469), May 19, 1998: FLOORBEAM. CORRODED. FORWARD VESTIBULE FLOORBEAM AT FRAME 15 HAS A SMALL SPOT OF CORROSION APPROX 5 INCHES OUTBOARD OF 3RD INTERCOSTAL FROM LEFT SIDE, INLINE WITH CLOSET WALL AT C/P
- [SDR 99ZZZM468](https://openairdocs.org/sdr/99ZZZM468), May 19, 1998: GUSSETT. CORRODED. FORWARD VESTIBULE, CENTER GUSSET PLATE ON THE 2ND INTERCOSTAL FROM RIGHT SIDE IS CORRODED. REPLACED FORWARD VESTIBULE GUSSET PLATE CENTER ON NR 2 INTERCOSTAL FR
- [SDR 99ZZZM467](https://openairdocs.org/sdr/99ZZZM467), May 19, 1998: GUSSET. CORRODED. FORWARD VESTIBULE, GUSSET PLATE ON FLOORBEAM AT FRAME 15 AND 2ND INTERCOSTAL FROM RIGHT SIDE HAS SOME SURFACE CORROSION AND APPEARS TO BE MADE OF TOO THIN OF MA
- [SDR 99ZZZM466](https://openairdocs.org/sdr/99ZZZM466), May 19, 1998: FRAME. CORRODED. FORWARD VESTIBULE, FLOOR PANEL (UNDER GALLEY UNIT) HAS SOME SURFACE CORROSION IN A COUPLE SPOTS ALONG AFT EDGE. REMOVED SURFACE CORROSION FORWARD VESTIBULE AT A
- [SDR 99ZZZM456](https://openairdocs.org/sdr/99ZZZM456), May 19, 1998: STIFFENER. CRACKED. RIGHT WING TE SHROUD LOWER SKIN STIFFENER CLEATS CRACKED BETWEEN RIBS 8/9, AFT END OF STIFFENER. REPLACED BOTH CLEATS OF RT WING TE SHROUD LOWER SKIN STIFFENER,
- [SDR 99ZZZM442](https://openairdocs.org/sdr/99ZZZM442), May 19, 1998: SILL. CORRODED. FORWARD VESTIBULE, SERVICE DOOR SILL PLATE HAS SEVERAL SMALL SPOTS OF SURFACE CORROSION. REMOVED AND REPLACED SILL PLATE WITH NEW. (M)
- [SDR 99ZZZM439](https://openairdocs.org/sdr/99ZZZM439), May 19, 1998: FLOOR STRIP. CORRODED. FLOOR STRIPS FOR FORWARD CABIN BULKHEADS NEED CLEANED, CORROSION REMOVED, PAINTED, ETC. CLEANED, REMOVED CORROSION ALODINED, PRIMED, PAINTED, AND REATTACHED PHO
- [SDR 99ZZZM465](https://openairdocs.org/sdr/99ZZZM465), May 18, 1998: FRAME. CORRODED. FORWARD VESTIBULE, FORWARD END OF SEAT RAIL, INBOARD RIGHT FLOORBEAM AT FRAME 18 IS CORRODED. REMOVED SURFACE CORROSION FORWARD VESTIBULE FRAME 18 INBOARD SEAT 
- [SDR 99ZZZM452](https://openairdocs.org/sdr/99ZZZM452), May 18, 1998: PLATE. WORN. WHILE CMP/WITH SSI 52-82-101-WEAR WAS DICV'D ON BOTTOM AFT CORNERS OF NOSE GEAR DOORS WHERE THEY ABUT TAB ON SPADE DOOR. TAB IS ALSO WORN. MANUFACTURED 2 BUTMEN
- [SDR 99ZZZM443](https://openairdocs.org/sdr/99ZZZM443), May 17, 1998: BRACKET. CORRODED. FORWARD VESTIBULE, STEW SEAT MOUNT BRACKETS ON 2ND AND 3RD INTERCOSTALS FROM LEFT SIDE ARE LIGHTLY CORRODED. REMOVED CORROSION TREATED PRIMED AND PAINTED FORWAR
- [SDR 99ZZZM453](https://openairdocs.org/sdr/99ZZZM453), May 15, 1998: BRACKET. CRACKED. MLG DOOR UPLOCK COVER BRACKET ON THE RIGHT SIDE OF WEB AT FRAME 32 IN MLG BAY IS CRACKED. REPLACED SAID BRACKET P/N HC536H0826-000U. (M)
- [SDR 99ZZZM438](https://openairdocs.org/sdr/99ZZZM438), May 15, 1998: INTERCOSTAL. CRACKED. AFT VEST, UNDER FLOOR INTERCOSTAL BETWEEN FRAMES 41 AND 42 IS CRACKED, CENTER INTERCOSTAL, CRACK IS APPROX 2.5 TO 3 INCHES LONG. COMPLIED WITH PATCH REPAIR IAW 
- [SDR 99ZZZM473](https://openairdocs.org/sdr/99ZZZM473), May 14, 1998: SPRING. FAILED. FORWARD VESTIBULE TRASH BIN DOOR ASSY, NEEDS CLEANED. ANGLE REPAIR, DOOR SPRINGS, ETC. REMOVED AND REPLACED SPRINGS. REPAIRED ANGLE AND CLEANED AND INSPECTED. (
- [SDR 99ZZZM447](https://openairdocs.org/sdr/99ZZZM447), May 12, 1998: BRACKET. CRACKED. NR 3 ENGINE NOSE COWL INBOARD FIREBOTTLE HAS ONE ATTACH BRACKET MOUNTED TO FIREWALL THAT IS CRACKED BADLY. REMOVED NR 3 NOSE AND TRANSFERRED DISCREPANCY TO W/C.
- [SDR 99ZZZM444](https://openairdocs.org/sdr/99ZZZM444), May 12, 1998: RIB. CRACKED. NR 2 PYLON BOX STRUCTURE HAS A CRACK IN THE LOWER OUTBOARD FLANGE OF RIB NR 5 THAT IS APPROX .5 INCH LONG. NR 2 PYLON CRACK OF APPROX .5 INCH LONG IS ACCEPTABLE
- [SDR 99ZZZM441](https://openairdocs.org/sdr/99ZZZM441), May 11, 1998: SILL. CORRODED. PASSENGER DOOR SILL PLATE CORRODED FRAME 15. REMOVED AND REPLACED FORWARD PAX DOOR SILL PLATE. (M)
- [SDR 99ZZZM437](https://openairdocs.org/sdr/99ZZZM437), May 7, 1998: BRACKET. CRACKED. STRUCTURAL INSPECTION MLG BAY, POS N/A WEB AT FRAME 32, DETAILED VISUAL INSPECTION. PERFORMED DV ON WEB AT FRAME 32 IN LEFT AND RIGHT MLG BAY. FOUND CRACKED BRA

All 84: https://openairdocs.org/deregistered/N463AP-2004-09-02/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 19910224012209I](https://openairdocs.org/incident/19910224012209I), Feb 24, 1991: Bac 146100A (N463AP), Aspen, CO, Minor damage. Captain discovered wrinkles in fuselage exterior metal skin on walk-around. Aircraft taken out of service.

## Other aircraft with N463AP

- [Registered now](https://openairdocs.org/aircraft/N463AP): Amazon.Com Services MK30, S/N 1786501224

---
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.