N656Z

No registry detail on file · not in current registry

Operators of this aircraft

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

OperatorRolePeriodBasis
AIRCRAFT CHARTER SERVICES INC (A59A)Certificate holderMatched by certificate designator

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.

6 reports on file, 2014-06-16 – 2019-10-19.

OTHER · 2019-10-19 Matched by certificate designator
ATA 5730

Part: COVER — BROKEN (LT WING TIP) · airframe 5,480 hrs · 4,303 cycles

WING TIP HEAT LEADING EDGE VENT COVER PLATE MISSING VENT LOUVER. TWO MORE HAVE STARTED TO CRACK.

Source: SDR 17GR159101919
NO WARNING INDICATION · 2016-10-29 Matched by certificate designator
ATA 7330

Part: TRANSMITTER — INOPERATIVE (FUEL FLOW) · airframe 4,330 hrs · 3,351 cycles

FUEL FLOW STOPPED INDICATING. FOUND FUEL FLOW TRANSMITTER TO BE INOPERATIVE. REMOVED AND REPLACED WITH OVERHAULED UNIT.

Source: SDR 2016FA0000577
OTHER · 2015-09-01 Matched by certificate designator
ATA 3340

Part: BULB — BURNED OUT (TAXI LIGHT)

WING RECOGNITION, TAXI BULB BURNED OUT.

Source: SDR 17GR2015090100002
OTHER · 2015-09-01 Matched by certificate designator
ATA 3340

Part: BULB — BURNED OUT (LANDING LIGHT) · airframe 3,771 hrs · 2,908 cycles

LANDING LIGHT BULBS ARE BURNING OUT IN 100 HOURS OF OPERATION. WE HAVE 3 AIRPLANES THAT USE THIS BULB AND WE HAVE REPLACED 17 BULBS SINCE APRIL 2014.

Source: SDR 17GR090101
NO TEST · 2014-11-12 Matched by certificate designator
ATA 7420

Part: IGNITER — NO TEST (ENGINE) · airframe 3,296 hrs · 2,524 cycles

IGNITER LEAD FAILED TO TEST. PREVIOUS ANALYSIS ON LEADS HAVE SHOWN THAT THE LEADS ARE SHORTING INSIDE ADJACENT TO THE IGNITER PLUG ADAPTER.

Source: SDR 2014FA0000656
OTHER · 2014-06-16 Matched by certificate designator
ATA 7200

Part: STRIP — CHAFED (FAN CASE) · airframe 3,108 hrs · 2,364 cycles

FAN CASE ABRAIDABLE WEAR STRIP ON LT AND RT ENGINE WORN BEYOND LIMITS AT SEVERAL POINTS AROUND THE CIRCUMFERENCE. BOTH ENGINES SHOWED GREATEST WEAR AT 9 AND 2 POSITIONS. THE WEAR IS TAKING PLACE AT THE MID POINT OF THE N1 ON THE ABRAIDABLE MATERIAL.

Source: SDR 2014F00097