N454

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, 2008-05-15 – 2012-10-09.

OTHER · 2012-10-09 Matched by certificate designator
ATA 5320

Part: PLUG — UNSERVICEABLE · airframe 21,720 hrs · 20,938 cycles

UNSERVICEABLE FREEZE PLUG ON ACCESS HOLE 131AL. REMOVED AND REPLACED FREEZE PLUG.

Source: SDR A6WA20121016552
OTHER · 2012-10-08 Matched by certificate designator
ATA 5730

Part: SKIN — CHAFED (BUTE DOOR) · airframe 21,720 hrs · 20,938 cycles

BUTE DOOR 594PB INNER SKIN CHAFED. CHAFED DOOR IS OUT OF LIMITS .008 RECEIVED DRILLED & LOCATED NEW SKIN IAW CRJ 200 SRM 51-40-11. INSTALLED DOOR IAW CRJ 200 SRM 51-42-06.

Source: SDR A6WA20121016558
OTHER · 2012-10-06 Matched by certificate designator
ATA 5743

Part: TRUNNION — DAMAGED (MLG) · airframe 21,720 hrs · 20,938 cycles

FOUND OVERSIZE HOLES ON LOWER MLG TRUNNION FLANGE 1 LT & 1 RT DURING COLD WORKING PROCESS. REPAIRED 2 EA OVER SIZE HOLES ON MLG TRUNNION FLANGES 1 LT & 1 RT IAW BOMBARDIER REO 601R-57-21-1767 REV -.

Source: SDR A6WA20121016557
OTHER · 2012-10-05 Matched by certificate designator
ATA 7110

Part: FIRESHIELD — CHAFED (RT COWLING) · airframe 21,720 hrs · 20,938 cycles

RIGHT ENGINE LOWER CORE COWL HAS A HOLE CHAFED THROUGH THE FIRE SHIELD. REPAIRED IAW REO 601R-71-12-4135 NR 10/14/12 SEE SHEET METAL TRACKER FORM 412 FOR WORKING PROGRESS.

Source: SDR A6WA20121016555
OTHER · 2012-10-05 Matched by certificate designator
ATA 5312

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 21,720 hrs · 20,938 cycles

BULKHEAD DAMAGED AT LEFT ENTRY SIDE OF FLIGHT COMPARTMENT AT EDGE CLOSE OUT. REMOVED & REPLACED DAMAGED 280 BULKHEAD PANEL.

Source: SDR A6WA20121016554
OTHER · 2012-10-05 Matched by certificate designator
ATA 7110

Part: SKIN — CHAFED (RT COWLING) · airframe 21,720 hrs · 20,938 cycles

RIGHT ENGINE LOWER CORE COWL INNER SKIN FORWARD AT 6 O`CLOCK HAS A CHAFING POINT. BLENDED IAW REO 601R-71-12-4135.

Source: SDR A6WA20121016556
OTHER · 2012-09-30 Matched by certificate designator
ATA 5312

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 21,720 hrs · 20,938 cycles

RIGHT AFT FS 280 BULKHEAD CORNER IS GOUGED & SKIN DENTED. FABRICATED & INSTALLED DOUBLER & FILLER TO 280 RIGHT BULKHEAD SKIN CORNER IS .010, WITHIN LIMITS IAW REO 601R-53-11-1727 REV F.

Source: SDR A6WA20121016553
OTHER · 2012-09-28 Matched by certificate designator
ATA 5312

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,720 hrs · 20,938 cycles

FS 202.75 BULKHEAD IS CRACKED AROUND THE PARKING BRAKE CABLE. REPAIRED FS 202.75 BULKHEAD AT LBL 23.71, WL 69.684 IAW REO 601R-53-11-563 REV B REPAIR TO TYPE V.

Source: SDR A6WA20124M551
WARNING INDICATION · 2008-05-15 Unresolved
ATA 2751

Part: POSITION SENSOR — DEFECTIVE (TE FLAPS) · airframe 19,673 hrs · 16,880 cycles

FLIGHT 5569 IAH TO LBB - WHILE ON A VISUAL APPROACH INTO LBB THE CREW RECEIVED A FLAPS FAIL CAUTION MSG ON THE EICAS. THE CREW RAN THEIR QRH, RAN APPROPRIATE CHECK LISTS, DECLARED AN EMERGENCY WITH LBB TOWER AND LANDED WITH OUT INCIDENT. REMOVED AND REPLACED THE LT BPSU IAW 27-51-10-400-801.

Source: SDR CHQA200800095