N453
Registered owner: WILLE CHAD C, IA (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
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.
17 reports on file, 1996-05-01 – 2012-10-03.
Part: HEAT SHIELD — DAMAGED (APU) · airframe 21,768 hrs · 21,526 cycles
APU AFT HEATSHIELD HAS 6 PULLED THRU SCREWS. REPAIRED 6 SCREW HOLES ON APU AFT HEATSHIELD IAW BOMBARDIER REO 601R-49-81-160.
Part: STRUCTURE — DAMAGED (HORIZ STAB) · airframe 21,768 hrs · 21,526 cycles
REFERENCE ROUTINE DMI 53252-3000-0046- TEMPORARY REPAIR TO THE HORZ STAB RIGHT O/B BUSHING BORE. PERFORM PERMANENT REPAIR AS REQUIRED. REMOVED AND REPLACED STAB RIGHT BORE BUSHINGS AND VERT BUSHING HORZ LUGS REMOVED & FIRST OVERSIZED.
Part: BUSHING — DAMAGED (HORIZ STAB) · airframe 21,768 hrs · 21,526 cycles
HORIZONTAL STABILIZER PIVOT FITTING HAS SPINNING BUSHING ON LEFT O/B LUG. REPAIRED HORIZONTAL STABILIZER PIVOT FITTING BUSHINGS IAW SB 601R-55-007 REV C.
Part: TRUNNION — DAMAGED (MLG) · airframe 21,768 hrs · 21,526 cycles
DURING COLD WORK OF THE MLG TRUNNION LOWER FLANGES FOUND 2 EA OVERSIZED HOLES AND ONE MISSING HOLE FROM FACTORY. REPAIRED EACH OVERSIZED HOLES AND TREATED MISSING HOLE IAW REO 601R-57-21-1759 REV A, 601R-57-21-1758.
Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 21,768 hrs · 21,526 cycles
CARGO BAY TIE DOWN TRACKS LBL 9 AND RBL 9 AND FS 559+112 ARE CORRODED. REMOVED CORRODED CARGO TRACKS AND INSTALLED NEW SERVICEABLE CARGO TRACKS IAW AMM 53-01-11.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 21,768 hrs · 21,526 cycles
LAST SECTION OF CARGO BAY TIE DOWN TRACK ON LBL 9 IS CORRODED. REMOVED UNSERVICEABLE TIE DOWN TRACK AND REPLACED WITH SERVICEABLE TIE DOWN TRACK IAW CRJ 200 AMM 53-01-11.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 21,768 hrs · 21,526 cycles
CARGO BAY TIE DOWN TRACK AT FS 589 +96 AND LBL 27, RBL 29 AND RBL 27 CORRODED. REMOVED UNSERVICEABLE TIE DOWN TRACKS AND REPLACED WITH SERVICEABLE TIE DOWN TRACKS IAW AMM 53-01-11.
Part: SKIN — DAMAGED (LT AILERON) · airframe 21,768 hrs · 21,526 cycles
REF ROUTINE DMI 53252-5000-0051 TEMPORARY REPAIR TO THE LEFT AILERON L/E PERFORM PERMANENT REPAIR AS REQUIRED. REMOVED DAMAGED SKIN AND INSTALLED NEW SERVICEABLE L/E SKIN IAW CRJ 200 SRM 51-42-21, 51-42-06.
Part: STRUCTURE — CHAFED (LT WING) · airframe 21,768 hrs · 21,526 cycles
LEFT O/B FLAP ROLLER GUIDE MOUNT STRUCTURE IS CHAFING THE AFT WING. BLENDED DAMAGE TO SMOOTH CONTOUR IAW BOMBARDIER REO 601R-57-53-950.
Part: HINGE — CORRODED (LAV SERVICE DOOR) · corrosion level 2 · airframe 21,768 hrs · 21,526 cycles
LAV SERVICE DOOR HINGES ARE CORRODED. REMOVED CORRODED HINGES, LOCATED, DRILLED & INSTALLED NEW SERVICEABLE HINGES IAW CRJ 200 SRMS 51-40-11, 51-41-02, 51-42-06, 52-00-00.
Part: BRACKET — CRACKED (HYDRAULIC BAY) · airframe 21,768 hrs · 21,526 cycles
FORWARD O/B ACCUMULATOR BRACKET IS CRACKED IN THE NOSE HYD COMPARTMENT. REMOVED & REPLACED BRACKET P/N 601R-75250-557 IAW CRJ 200 SRM 51-42-06, 51-42-21.
Part: VANE — CHAFED (TE FLAP) · airframe 21,768 hrs · 21,526 cycles
RIGHT I/B FLAP VANE LEADING EDGE CHAFED 3 SPOTS. INBOARD LEADING EDGE FOUND TO BE OUT OF LIMITS. BLENDED DAMAGE ON RIGHT I/B FLAP VANE LEADING EDGE FOUND CENTER AND AFT LEADING EDGE TO BE WITHIN LIMITS IAW REO 601R-57-52-004 REV C. REPLACED I/B LEADING EDGE WITH NEW SERVICEABLE LEADING EDGE IAW CRJ 200 SRM 51-40-11 & 51-42-13.
Part: FITTING — CRACKED (FUSELAGE) · airframe 21,768 hrs · 21,526 cycles
CLIP AT RBL 27 IS CRACKED. REMOVED AND REPLACED CLIP REO 601R-53-41-059.
Part: STRIKER — GOUGED (FUSELAGE) · airframe 21,768 hrs · 21,526 cycles
PAX DOOR SEAL STRIKER AT FS 310.00 AND STR L8 GOUGED. REPAIRED DAMAGE SECTION IAW REO 601R-53-22-033 REV C.
Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 21,768 hrs · 21,526 cycles
TWO GOUGES ON THE AFT RIGHT SIDE OF 280 BULKHEAD FROM CONTACT WITH CONTACT WITH GALLEY STORAGE COMPARTMENT DOOR. CUT OUT DAMAGE ON THE RIGHT SIDE AT FS 280 AND INSTALLED REPAIR DOUBLER AND FILLER IAW REO 601R-53-11-1727 REV E.
Earlier reports · 1996–2000 · 2 reports
2000
Part: BLANKET — SHORTED (LT HORIZ STAB)
LEFT HORIZONTAL STABLILIZER HEAT BLANKET SHEARED, BURNING A .6250 INCH HOLE IN THE LEADING EDGE OF THE HORIZONTAL STABILIZER 5 INCHES OUTBOARD FROM THE INBOARD EDGE. (X)
1996
Part: P3 LINE — LOOSE (LT ENGINE)
ON CLIMB-OUT AT 44,000 FEET, THE LT ENGINE FLAMED OUT. RESTARTED ENGINE AND UPON LANDING, MAINTENANCE INSPECTED THE LEFT ENGINE INLET, COMPRESSOR BLADES, TURBINE BLADES, INLET GUIDE VANES, INLET GUIDE VANE RIGGING, T-2 HOSE, AND P-3 LINE. FOUND P-3 LINE LOOSE. TIGHTENED P-3 LINE.