N121KL

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 holder—Matched 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.

5 reports on file, 2016-02-05 – 2020-03-02.

OTHER · 2020-03-02 Matched by certificate designator
ATA 7310

Part: SHUTOFF VALVE — BLOCKED (RT ENGINE) · airframe 4,075 hrs · 5,805 cycles

RH ENGINE WOULD NOT START (HUNG START) IN AUTO. ENGINE WOULD START IN MANUAL MODE. TROUBLESHOT FOUND MOTIVE FLOW PRESSURE LOW. EMERGENCY FUEL SHUTOFF UNIT WAS RESTRICTING MOTIVE FLOW WHICH REDUCED IDLE FLOW PRESSURE TO THE FCU.

Source: SDR A59A202003020301
OTHER · 2020-01-24 Matched by certificate designator
ATA 2560

Part: NONE — NONE · airframe 3,898 hrs

WHILE USING LIFE VEST CERTIFIED 1/16/2018 FOR TRAINING FOUND THAT THE C02 INFLATOR CARTRIDGE WAS TO RIGID TO BE PUNCTURED TO INFLATE THE VEST.

Source: SDR 17GRA59A01
NO TEST · 2018-06-04 Matched by certificate designator
ATA 7600

Part: ANTI-ICE VALVE — FAILED (ENGINE) · airframe 3,548 hrs · 5,410 cycles

DURING START, THE ANTI-ICE LIGHT WARNING ILLUMINATED. FOUND THE STATOR ICE VALVE FAILED.

Source: SDR 17GR060518
OTHER · 2018-01-05 Matched by certificate designator
ATA 7321

Part: EEC — MALFUNCTIONED (ZONE 400) · airframe 3,392 hrs · 5,293 cycles

PILOTS ATTEMPTED START AND START HUNG AT 16%. SAW ITT RISE HOWEVER ENGINE WOULD NOT ACCELERATE. REMOVED EEC AND INSTALLED ON LT ENGINE PROBLEM FOLLOWED.

Source: SDR A59A201801090105
FALSE WARNING · 2016-02-05 Matched by certificate designator
ATA 2841

Part: PROBE — DEPARTED (FUEL QTY) · airframe 2,545 hrs · 4,682 cycles

PILOTS REPORTED THAT AS FUEL WAS BURNED THE LEFT QUANTITY WOULD STOP SHOWING BURN AT AROUND 2300 AND THE RIGHT SIDE WOULD CONTINUE TO SHOW FUEL BURNED. AS THE RH SIDE SHOWED ABOUT 1100 THE LEFT WOULD DRIFT DOWN TO 1100. SYSTEM FUNCTIONED NORMAL ABOVE AND BELOW THESE PARAMETERS. REMOVED ACCESS PANELS FROM WING. FOUND NR 4 PROBE LAYING IN WING OFF OF MOUNT. FOUND MOUNT TO BE SERVICEABLE AND NOT DEFECTIVE. APPEARS PROBE WAS REMOVED FOM AND NOT REINSTALLED IN MOUNTING. REINSTALLED PROBE AND TESTED SYSTEM. SYSTEM TESTED WITHIN SPECIFICATIONS.

Source: SDR 17GR201602080001