N453

WILLE CHAD C BLERIOT XI · 2011 · Fixed-wing single-engine · 1 engine · 1 seat · Valid Registration

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

PIPER PA-28 No injuries Part 91 — operator not named in the NTSB record
Source: NTSB case MKC77DCD46

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.

OTHER · 2012-10-03 Matched by certificate designator
ATA 4910

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.

Source: SDR A6WA20121008545
OTHER · 2012-10-03 Matched by certificate designator
ATA 5514

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.

Source: SDR A6WA20121008544
OTHER · 2012-10-03 Matched by certificate designator
ATA 5514

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.

Source: SDR A6WA20121008546
OTHER · 2012-10-03 Matched by certificate designator
ATA 5743

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.

Source: SDR A6WA20121008549
OTHER · 2012-09-28 Matched by certificate designator
ATA 5347

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.

Source: SDR A6WA20121008542
OTHER · 2012-09-28 Matched by certificate designator
ATA 5347

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.

Source: SDR A6WA20121008543
OTHER · 2012-09-28 Matched by certificate designator
ATA 5347

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.

Source: SDR A6WA20121008541
OTHER · 2012-09-28 Matched by certificate designator
ATA 5751

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.

Source: SDR A6WA20121008547
OTHER · 2012-09-28 Matched by certificate designator
ATA 5720

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.

Source: SDR A6WA20121008548
OTHER · 2012-09-27 Matched by certificate designator
ATA 5246

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.

Source: SDR A6WA2012108436
OTHER · 2012-09-26 Matched by certificate designator
ATA 5320

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.

Source: SDR A6WA20121008437
OTHER · 2012-09-26 Matched by certificate designator
ATA 5753

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.

Source: SDR A6WA20121008550
OTHER · 2012-09-26 Matched by certificate designator
ATA 5320

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.

Source: SDR A6WA20121008539
OTHER · 2012-09-25 Matched by certificate designator
ATA 5320

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.

Source: SDR A6WA20121008540
OTHER · 2012-09-25 Matched by certificate designator
ATA 5312

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.

Source: SDR A6WA20121008538
Earlier reports · 1996–2000 · 2 reports

2000

OTHER · 2000-10-31 Matched by certificate designator
ATA 3010

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)

Source: SDR 20001129SH015

1996

ENGINE FLAMEOUT · 1996-05-01 Unresolved
ATA 7320

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.

Source: SDR 96ZZZX2894