N63BVBeechcraft E-90
This N-number isn't registered right now. Below is its last known registration, canceled Oct 19, 2012.
Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply8 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Individual owner
- Canceled
- Oct 19, 2012
- Airworthiness
- Standard · Normal
- Airworthiness date
- Nov 9, 1977
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Beechcraft
- Model
- E-90
- Serial number
- LW-256
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 10
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A83B90
Engine
- Make and model
- P&W Canada Pt6a-60a
- Type
- Turbo-prop
- Power
- 1050 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- until 2012Individual owner
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (6)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2004-17-02 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series Airplanes | Oct 4, 2004 | Airframe (E-90)Certain serial numbers: 65-A90, B90, C90, C90A LJ-76; 65-A90, B90, C90, C90A LJ-114–LJ-1691; E90 LW-1–LW-347; F90 LA-2–LA-236; 99, 99A, A99A, B99, C99 U-1–U-239; 100, A100 B-1–B-94; … |
| 2002-23-13 | Pratt & Whitney Canada PT6A Series Turboprop Engines | Dec 31, 2002 | Engine (PT6A-60A)Only with: Engines with turbine exhaust ducts P/N 3012290, 3031988, 3032117, 3035784, 3035786, 3105890-01, 3112167-01, or 3111780-01 installed. |
| 2002-01-10 | Raytheon Aircraft Company Beech Models 65-90, 65-A90, 65-A90-1, 65-A90-4, B90, C90… | Feb 22, 2002 | Airframe (E-90)Certain serial numbers: 65-90 LJ-1–LJ-1559; 65-A90 LJ-1–LJ-1559; B90 LJ-1–LJ-1559; C90 LJ-1–LJ-1559; C90A LJ-1–LJ-1559; 65-A90-1 LM-1–LM-141; … |
| 99-10-07 | Raytheon Aircraft Corporation Beech Models 65-90, 65-A90, 65-A90-1, 65-A90-2, 65-A90-3… | Jun 8, 1999 | Airframe (E-90) |
| 97-25-03 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series Airplanes | Jan 21, 1998 | Airframe (E-90) |
Show all 6 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 97-23-17 | Raytheon Aircraft Company 90, 100, 200, and 300 Series Airplanes (Formerly Known as… | Dec 29, 1997 | Airframe (E-90)Certain serial numbers: C90 LJ-683–LJ-1463; C90A LJ-683–LJ-1463; E90 LW-177–LW-347; F90 LA-1–LA-236; H90 LL-1–LL-61; A100 B-228–B-247; … |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (8)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Windows · windshield · crackedDec 16, 2008
DURING CRUISE AT FL240 APPROX 80 TO 90 MILES FROM KCPR, THE RT SIDE FRONT WINDSHIELD CRACKED. AT THE TIME, THE TEMPERATURE OUTSIDE WAS -38 DEGREES CELSIUS AND THE WINDSHIELD HEAT WAS OFF WITH CLEAR SKIES OBSERVED. THE PILOT CONTACTED ATC AND LET THEM KNOW THE WINDOW WAS BROKEN AND THE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Ignition · cowling · bentApr 6, 2007
DURING TAKEOFF ROLL OF THE AC, AT THE POINT OF LIFTOFF, THE PILOT NOTICED THE LT ENGINE UPPER AFT COWLING HAD COME OPEN. THE TAKEOFF WAS ABORTED AND THE AC CAME TO A SAFE STOP ON THE RUNWAY. THE PILOT SHUTDOWN THE LT ENGINE AND TAXIED BACK TO THE HANGAR ON THE RT ENGINE. MAINT INSPECTED THE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · trim tab · wrong partSep 10, 2004
DURING A DETAILED INSPECTION OF THE AIRCRAFT THE RUDDER TRIM TAB HORN BUSHING WAS FOUND TO BE WORN BEYOND ALLOWED LIMITS. REPLACEMENT OF THE HORN IN THE TRIM TAB IS NOT A GOOD OPTION, DUE TO THE AMOUNT OF DISASSEMBLY OF THE TAB IN ORDER TO ACCOMPLISH THE TASK. A REPLACEMENT TRIM TAB WAS PURCHASED.…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 8 reportsShow fewer reports
- Landing gear · stator · brokenApr 26, 2004
AFTER LANDING THE PILOT WROTE UP, RIGHT BRAKE HAS INTERMITTENT RAPID CYCLES OF, ON AND OFF BRAKE PRESSURE. ALSO INDICATED, APPEARS TO BE LEAKING HYDRAULIC FLUID. MAINTENANCE INSPECTED THE BRAKE AND FOUND THE INNER BRAKE CARRIER LINING BROKEN. THE PIECE OF THE INNER CARRIER LINING ASSEMBLY…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · torque knee · crackedMar 3, 2003
DURING COMPLIANCE OF SB 32-3134 AND AD 2002-01-10, RIGHT LANDING GEAR UPPER TORQUE KNEE WAS FOUND TO BE CRACKED AT PROTRUSION OF CENTER LUG. THIS UNIT HAD BEEN INSPECTED MULTI TIMES PRIOR TO THIS INSPECTION AND PASSED THOSE INSPECTIONS. UNITS EXACT TOTAL TIME AND TOTAL LANDINGS IS UNKNOWN, BUT IS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · torque link · crackedAug 21, 2001
DURING THE COMPLIANCE OF RAYTHEON RECURRING SERVICE BULLETIN 32-3134, INSPECTION OF THE MAIN LANDING GEAR TORQUE KNEE'S, CRACKS WERE FOUND IN THE RADIUS AREA OF THE UPPER TORQUE KNEE, ON EACH SIDE OF THE SINGLE LUG. THE CRACK IN THIS WAS IN THE AREA NOTED TO BE INSPECTED ON THE SERVICE BULLETIN.…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · support bracket · crackedAug 3, 2001
THE RIGHT INBOARD LANDING GEAR ACTUATOR SUPPORT BRACKET IS CRACKED AT THE BOTTOM AREA OF THE BRACKET WHERE IT ATTACHES TO THE WING SPAR STRUCTURE. THE WING SPAR STRUCTURE IS NOT EFFECTED BY THIS CRACK. THE CRACK IS APPROXIMATELY .5 INCH LONG AND IS THE RADIUS OF THE FLANGE OF THE BRACKET. THE PART…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · wheel · splitJun 12, 1995
DURING TAKEOFF ROLL, PILOT HEARD A LOUD BANG. WHEN AIRCRAFT CAME TO A STOP, THE OUTBOARD WHEEL HALF HAD SPLIT IN HALF STARTING AT INBOARD WHEEL HALF MATING FLANGE AND CRACK WORKING ITS WAY TOWARD WHEEL BEAD AREA.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026