N8495D

No registry detail on file · not in current registry

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.

9 reports on file, 2011-11-06 – 2011-11-12.

OTHER · 2011-11-12 Matched by certificate designator
ATA 5730

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 24,118 hrs · 21,024 cycles

LT LOWER PLANK FUEL ACCESS HOLE AT WS 54.897 HOLE NR 1 HAS PITTING CORROSION ON I/B EDGE OF CUTOUT MEASURING APPROXIMATELY .002 DEEP IN CRITICAL AND NON-CRITICAL REGION. REF DI 54304. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.

Source: SDR REXA201100715
OTHER · 2011-11-12 Matched by certificate designator
ATA 5730

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 24,118 hrs · 21,024 cycles

RT LOWER PLANK FUEL ACCESS HOLE AT WS 54.897 HOLE NR 1 HAS PITTING CORROSION ON I/B EDGE OF CUTOUT MEASURING APPROXIMATELY .002 DEEP IN A NON-CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.

Source: SDR REXA201100714
OTHER · 2011-11-07 Matched by certificate designator
ATA 5312

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 24,118 hrs · 21,024 cycles

THE 621.00 PRESSURE BULKHEAD FWD FACE HAS 5" EACH CHAFES 30" ABOVE FLOOR AT LBL 27, 18, RBL 18, 27, 36 ON PREVIOUSLY BLENDED AREAS APPROX .001" DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Source: SDR REXA201100758
OTHER · 2011-11-07 Matched by certificate designator
ATA 5320

Part: BEAM — CRACKED (FUSELAGE) · airframe 24,118 hrs · 21,024 cycles

FS 280 TRANSVERSE BEAM AFT J-ANGLE IS CRACKED JUST O/B OF LBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 AND BOMBARDIER SERVICE CORP STANDARD REPAIR 601R-53-0110.

Source: SDR REXA201100811
OTHER · 2011-11-07 Matched by certificate designator
ATA 5320

Part: BEAM — CRACKED (FUSELAGE) · airframe 24,118 hrs · 21,024 cycles

FS 280 TRANSVERSE BEAM IS CRACKED JUST O/B OF LBL 9 & RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-926, 601R-53-11--2227 AND BOMBARDIER SERVICE CORP STANDARD REPAIRS 601R-53-0107, 601R-53-0110.

Source: SDR REXA201100810
OTHER · 2011-11-07 Matched by certificate designator
ATA 5320

Part: POST — DAMAGED (FUSELAGE) · airframe 24,118 hrs · 21,024 cycles

UPON REMOVAL OF FS 409+128 VERTICAL POST FOUND SEVERAL PREVIOUSLY ELONGATED HOLES MEASURING .248 AND .250 COMMON TO FS 409+128 BULKHEAD CAP ANGLE. REPAIRED IAW BOMBARDIER REO 601R-53-41-1512.

Source: SDR REXA201100760
OTHER · 2011-11-07 Matched by certificate designator
ATA 5520

Part: HINGE FITTING — CHAFED (RT ELEVATOR) · airframe 24,118 hrs · 21,024 cycles

RIGHT ELEVATOR HINGE FITTING NR 2 AND STAB HINGE FITTING NR 2 HAVE MULTIPLE CHAFES. REPAIRED IAW BOMBARDIER REO 601R-55-11-393 AND 601R-55-21-340.

Source: SDR REXA201100757
OTHER · 2011-11-07 Matched by certificate designator
ATA 5520

Part: HINGE FITTING — CHAFED (LT ELEVATOR) · airframe 24,118 hrs · 21,024 cycles

LEFT ELEVATOR HINGE FITTING NR 2 AND STAB HINGE FITTING NR 2 HAVE MULTIPLE CHAFES. REPAIRED IAW BOMBARDIER REO 601R-55-11-393 AND 601R-55-21-341.

Source: SDR REXA201100756
OTHER · 2011-11-06 Matched by certificate designator
ATA 5312

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 24,118 hrs · 21,024 cycles

FS 621.00 PRESSURE BULKHEAD FWD FACE HAS 5 EACH CHAFES WITH DENTS 2 INCHES ABOVE FLOOR AT LBL 31-23-13 AND RBL 23-42. MAXIMUM DENT DAMAGE IS .045". REPAIRED IAW BOMBARDIER REO 601R-53-61-4252.

Source: SDR REXA201100755