N503AW
Registered owner: CSI AVIATION INC, NM (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
8 reports on file, 2023-02-03 – 2026-07-01.
Part: ANGLE — CRACKED (ZONE 400) · airframe 20,957 hrs · 30,625 cycles
RIGHT 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-INSTALLED MLG ACTUATOR, MLG DRAG BRACE AND RECONNECTED PLUMBING, ELECTRICAL WIRING. RIGGING, LEAK AND RETRACT/EXTENSION PERFORMED. SATISFACTORY IAW AMM 32-30-03, 32-11-01, AND 32-31-37.
Part: ANGLE — CRACKED (ZONE 400) · airframe 20,957 hrs · 30,625 cycles
LEFT 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 REPLACED WITH NEW IAW KINGAIR SIRM 20-50-03. RE-INSTALLED MLG ACTUATOR, MLG DRAG BRACE AND ECONNECTED PLUMBING/ELECTRICAL WIRING. RIGGING, LEAK AND RETRACT/EXTENSION PERFORMED SATISFACTORY. REF BEECH B200 AMM CH. 32-30-03, 32-11-01 AND 32-31-37.
Part: STIFFENER — CRACKED (ZONE 200) · airframe 20,510 hrs · 30,103 cycles
WHILE 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 LINE FOR STIFFENER #5. THE #9 STRINGER IS INLINE WITH THE #5 ZEE STIFFENER. REPLACED AFT PRESSURE BULKHEAD LOWER WEB IAW KING AIR SIRM 20-50. INSTALLED Z STIFFENERS PN 101-440119-53/-57 IAW TEXTRON FIELD REPAIR FR-BB-1514-15422 REV -.
Part: SKIN — CRACKED (FRM 181 S16) · airframe 19,316 hrs · 28,577 cycles
BELLY SKIN CRACKED 3/8"AT APPROX FS 181.0 AT STRINGER 16. REPAIRED IAW KING AIR SIRM 20-10-16.
Part: SKIN — CRACKED (BS 168 S15-16L) · airframe 19,316 hrs · 28,577 cycles
BELLY 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 .050, 2024-T3 DOUBLER AND .040, 2024-T3 SHIM, COATED DOUBLER AND SHIM WITH BONDERITE M-CR 1201 AERO ALODINE, AND INTEGRAL PRODUCTS SEALANT AC 350 B-1/2 CONFORMING TO AMS-S-8802F, TYII, CL B-1/2. DOUBLER AND SHIM INSTALLED WITH MS20470AD RIVETS IRW SIRM 20-50-02.
Part: FRAME — CRACKED (ZONE 100) · airframe 18,525 hrs · 27,477 cycles
FRAME 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.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 18,525 hrs · 27,477 cycles
FRAME 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.
Part: UNKNOWN — UNKNOWN · airframe 18,310 hrs · 27,145 cycles
RH 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-ATA53-36613