Registered owner
Csi Aviation Inc
Owner type
Corporation
Serial number
BB-1514
Year built
1995
Type
Fixed wing multi engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
November 1, 1995
Certificate issued
August 6, 2022
Expires
August 31, 2029
Mode S code
A6452A

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney PT6A model are included below.

On this page

Airworthiness directives that may apply · 69

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1968In forceSuperseded2026
ADs by the year they took effect: 78 ADs
19681
19691
19701
19751
19761
19771
19782
19802
19831
19851
19861
19871
19891
19903
19912
19924
19943
19952
19963
19973
19987
19993
20013
20022
20033
20042
20055
20062
20071
20082
20101
20112
20121
20142
20151
20161
20191
20211
20221
20231
20241
See all 79 ADs

Information bulletins that may apply · 7

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N503AWMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Beech B200 aircraft

FAA incident reports

No FAA accident or incident reports matched to N503AWMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Beech B200 aircraft

Service difficulty reports · 8

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

SDR GRTA20260715002Angle · crackedLEFT MLG ACTUATOR INBOARD SUPPORT BRACKET CRACKED. REMOVED LEFT MLG ACTUATOR, ASSOCIATED PLUMBING/ELECTRICLA WIRING, AND LEFT MLG DRAG BRACE. REMOVED LH INBOARD AND OUTBOARD SUPPORT BRACKET ANGLES PN 101-120122-15 (INBOARD) AND 101-120122-13 (OUTBOARD) AND REJul 1, 2026 · N503AW · Beech B200 · Nacelle/Pylon Miscellaneous StructureSDR GRTA20260715001Angle · crackedRIGHT INBD MLG ACTUATOR SUPPORT BRACKET CRACKED. REMOVED RT MLG ACTUATOR, ASSOCIATED PLUMBING, ELECTRICLA WIRING, AND RT MLG DRAG BRACE. REMOVED RT INBD AND OTBD SUPPORT BRACKET ANGLES (INBD) AND 101-120122-14 (OTBD), REPLACED WITH NEW IAW SRM 20-50-03. RE-IJul 1, 2026 · N503AW · Beech B200 · Nacelle/Pylon Miscellaneous StructureSDR GRTA20250910001Stiffener · crackedWHILE PERFORMING THE AFT PRESSURE BULKHEAD INSPECTION FOUND A CRACK AT THE # 5 ZEE STIFFENER FROM THE TOP OF THE BULHEAD ON THE FWD SIDE OF THE BULKHEAD THE CRACK STARTS 2.1 INCHES FROM THE OUTBD R/H SIDE AND RUNS HORIZONTALY 21 INCHES JUST UNDER THE RIVET LIJul 7, 2025 · N503AW · Beech B200 · Fuselage Main, BulkheadSDR GRTA20240315004Skin · crackedBELLY SKIN CRACKED 3/8"AT APPROX FS 181.0 AT STRINGER 16. REPAIRED IAW KING AIR SIRM 20-10-16.Mar 14, 2024 · N503AW · Beech B200 · Fuselage Main, Plate/SkinSDR GRTA20240315001Skin · crackedBELLY SKIN CRACKED APPROX 3 1/2" ON FRAME AT FS 167.625 BETWEEN STRINGERS 15L AND 16. C/W SKIN DAMAGE REPAIR (PRESSURIZED AREA) COVER PATCH METHOD AND SHIM INSTALLATION IRW BEECHCRAFT SIRM 98-39006, REV D5, 20-10-16, 2. A-D & 20-10-10, 1-4, A.C. FABRICATED Mar 6, 2024 · N503AW · Beech B200 · Fuselage Main, Plate/SkinSDR GRTA20230506002Frame · crackedFRAME CRACKED AT FS 256.250 AND STRINGER 13L, PN 50-420068-31. REPAIRED CRACKED FRAME AT FS 256.250 AND STRINGER 13L USING 2024-T3, 0.063" ALCLAD IAW SIRM 20-10-34.Apr 18, 2023 · N503AW · Beech B200 · Fuselage Main, FrameSDR GRTA20230506001Unknown · unknownFRAME CRACKED AT LIGHTNING HOLE AT FS 187.383 JUST ABOVE STRINGER 10R. REPAIRED CRACK FS 187.383 ABOVE STRINGER 10R USING 0.071", 2024-T3 ALCLAD IAW SIRM 20-10-31.Apr 18, 2023 · N503AW · Beech B200 · Fuselage Main, FrameSDR GRTA20230213001Unknown · unknownRH FRAME CROSSTIE CRACKED AT APPROX FS 188.0 AND WL 119.0 - RH EMERGENCY EXIT CUT OUT LOWER AFT CORNER. REPAIRED IAW TEXTRON STANDARD REPAIR SR-KA-ATA53-36613Feb 3, 2023 · N503AW · Beech B200 · Fuselage Main, Structure

STCs that may be installed · 480

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 480 STCs

Earlier aircraft with this N-number · 1

This aircraft carried N503AW before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.