N487AL

BELL 407 · 1997 · Valid Registration

Registered owner: REDDING AIR SERVICE INC, CA (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
REDDING AIR SERVICE, INC. (AUMA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

O · 2017-01-16 Matched by certificate designator
ATA 7931

DURING CRUISE MODE OF FLIGHT, PILOT NOTICED ENGINE OIL PRESSURE INDICATED "0". ALL OTHER INDICATIONS WERE NORMAL. PILOTED ELECTED TO RETURN TO BASE.

Source: SDR ALGA2017012541279 · FAA SDRS
J · 2015-07-15 Matched by certificate designator
ATA 7250

DURING CRUISE FLIGHT ENGINE CHIP LIGHT ILLUMINATED. LANDED ON AN OFFSHORE PLATFORM, EXAMINED CHIP PLUG FOUND METAL PARTICLES. UPON RECOVERY OF AIRCRAFT & SUBSEQUENT TEAR DOWN OF ENGINE, THE NATURE OF THE PROBLEM WAS DETERMINED TO BE THE NUMBER FIVE BEARING IN THE TURBINE SECTION.

Source: SDR ALGA0730201536129 · FAA SDRS
O · 2004-06-10 Matched by certificate designator
ATA 6320

SPALLING ON GEAR TEETH, THIS IS A RECURRING EVENT ON C-47 GEARBOXES. REPLACED GEAR W/NEW PART.

Source: SDR ALGA095231 · FAA SDRS
O · 2004-06-10 Matched by certificate designator
ATA 6320

SPALLING ON GEAR TEETH. THIS IS A NEW STYLE GEAR AND THIS GEARBOX WAS REMOVED FOR HIGH VIBES. THIS IS A RECURRING EVENT ON C-47 GEARBOXES. REPLACED GEAR W/NEW PART.

Source: SDR ALGA095232 · FAA SDRS
O · 2000-11-13 Matched by certificate designator
ATA 7240

TURBINE RECEIVED IN SHOP TO PERFORM 2000 HOUR OVERHAUL. UPON REMOVAL OF OUTER COMBUSTION CASE AND COMBUSTION LINER, FOUND A HOLE IN DOME OF 1ST STAGE SHIELD. ALSO, FOUND THE BROKEN PIECE LODGED ON 1ST STAGE NOZZLE VANE. POSSIBLE IMPROPER METAL USED TO MAKE DOME. PART WAS SCRAPPED, UNABLE TO REPAIR. (X)

Source: SDR 20001206SH005 · FAA SDRS
O · 2000-07-08 Matched by certificate designator
ATA 6322

UPON DAILY INSPECTION, CRACKS IN CORNERS CAUSED BY INHERENT VIBRATIONS. (X)

Source: SDR 20000804SH020 · FAA SDRS
O · 1999-09-15 Matched by certificate designator
ATA 6510

FOUND NR 4 DISC PACK SPREAD JUST BEYOND LIMITS DURING 25-HOUR INSPECTION. FOUND NR 4 DISC PACK SPREAD BEYOND LIMITS. REMOVED NR 3 TAIL ROTOR DRIVESHAFT TO BLOWER SPLINE ADAPTER TO ENSURE IT STILL CONTAINED PROPER AMOUNT OF LUBRICANT. IT DID, BUT FOUND THE SPLINE ADAPTER P/N 406-040-316-101 HAD A STEP WORN IN IT. REPLACED THE SPLINE ADAPTER.

Source: SDR 99ZZZX4079 · FAA SDRS
O · 1999-08-01 Matched by certificate designator
ATA 6510

DURING 25-HOUR, DISC PACK AD 97-24-17 PARA 'A', FOUND DISC PACK DAMAGED.

Source: SDR 99ZZZX3347 · FAA SDRS
O · 1999-03-06 Matched by certificate designator
ATA 6220

MAIN ROTOR HUB REMOVED FOR BEARING EXTRUDING. BEARING COMPLETELY DEBONDED AT 2ND CONE FROM FLANGE.

Source: SDR 99ZZZX1693 · FAA SDRS
O · 1998-12-06 Matched by certificate designator
ATA 6510

DURING 25-HOUR INSPECTION, FOUND GAP BETWEEN THE NR 1 DISC (MOST FORWARD) AND NR 2 DISC BEYOND .015 INCH. (THE NR 1 DISC IS THE ONE WITH THE PART NUMBERS SHOWING).

Source: SDR 99ZZZX48 · FAA SDRS
O · 1998-08-07 Matched by certificate designator
ATA 6510

DURING 25 HOUR INSPECTION, GAP BETWEEN DISCS NR 1 AND NR 2, NR 2 AND NR 3, OF THE 10-DISC PACK EXCEED LIMITS.

Source: SDR 98ZZZX3519 · FAA SDRS
O · 1998-08-07 Matched by certificate designator
ATA 6510

DURING 25 HOUR INSPECTION, FOUND GAP BETWEEN DISC NR 1 AND NR 2, NR 9 AND NR 10, EXCEED LIMITS. (TOTAL NUMBER OF DISCS IN THE DISC PACK IS 10).

Source: SDR 98ZZZX3518 · FAA SDRS
O · 1998-08-03 Matched by certificate designator
ATA 6510

DURING 25 HOURS INSPECTION, FOUND GAP BETWEEN DISCS 9 AND 10 OF THE 10-DISC PACK EXCEED LIMITS.

Source: SDR 98ZZZX3521 · FAA SDRS
O · 1998-06-23 Matched by certificate designator
ATA 6510

WHILE PERFORMING A 25 HOUR INSPECTION, DISC PACK NR 7 WAS NOTED TO BE CRACKED. THE CRACKED DISC OF THE 10 DISCS IS THE NR 10 DISC. (THE VERY AFT DISC OF THE NR 7 DISC PACK).

Source: SDR 98ZZZX3520 · FAA SDRS