N426GF
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Jet Linx Aviation, LLC (9JLA) | 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.
6 reports on file, 2014-02-06 – 2021-10-27.
Part: ACTUATOR — DEFECTIVE (ROLL TRIM) · airframe 6,988 hrs · 6,663 cycles
THE MAINTENANCE TEAM FOUND THE RIGHT ROLL TRIM INOP DURING POST FLIGHT CHECKS. IT WAS DETERMINED THAT THE RIGHT ROLL TRIM ACTUATOR WAS DEFECTIVE. THE ACTUATOR WAS REMOVED AND REPLACED WITH AN OVERHAULED UNIT. OPS CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE
Part: RIB — CRACKED (HORIZ STAB) · airframe 4,935 hrs · 5,010 cycles
DURING A D CHECK INSPECTION, FOUND HORIZONTAL STABILIZER RIBS CRACKED AT HSS 350. PERFORMED A BORESCOPE INSPECTION OF THE HORIZONTAL STABILIZER RIBS IAW CHAPTER 55-10-00 IN THE MODEL 400 & 400A MM. FOUND A TOTAL OF 7 RIBS WITH CRACKS, 2 45A2112-0005, 2 45A2113-0005, 2 45A21101-0011 & 1 45A21116-0005. AD 2014-15-15 & THE 400 & 400A AIRWORTHINESS & LIMITATION MANUAL, TACK CODE 045505 REQUIRE INSPECTION OF THE HORIZONTAL STABILIZER RIBS PRIOR TO THE ACCUMULATION OF 7,400 HOUR INITIAL WITH RECURRENT INSPECTIONS EVERY 2,400 HOURS.
Part: RADAR — DEFECTIVE (WEATHER RADAR) · airframe 4,436 hrs · 4,636 cycles
THE CREW REPORTED THE WEATHER RADAR AS INOPERATIVE. TROUBLESHOOTING FOUND THE RADAR UNIT DEFECTIVE. PN 622-8440-003 SN 2091. TOTAL TIME & CYCLES IN SERVICE OF RADAR, 58.1 TT & 42 TC AFTER AN OVERHAUL DATED JULY 01 2014.
Part: WIRE HARNESS — DEFECTIVE (LT ENGINE) · airframe 4,295 hrs · 4,532 cycles
THE LT ENG ANTI-ICE ANNUNCIATOR WOULD NOT ILLUMINATE WHEN THE SYS WAS ACTIVATED. EXTENSIVE TROUBLESHOOTING FOUND THE LT ENG WIRING HARNESS PN 3052134-01 SN AA87179 DEFECTIVE. A NEW WIRING HARNESS OF THE SAME PART NUMBER WAS INSTALLED. FUNCTIONAL CHECKS WERE SATISFACTORY. THE ACFT WAS RETURNED TO SERVICE.
Part: WIRE HARNESS — INTERMITTENT (LT ENGINE) · airframe 4,198 hrs · 4,467 cycles
DURING THE CLIMB AFTER TAKEOFF THE CREW REPORTED THAT THE LT EFC FAILED. ONCE THE ACFT WAS IN CRUISE FLIGHT THE EFC WAS RESET & NO FAULTS WERE NOTED UNTIL THE DESCENT FOR LANDING WHERE THE EFC FAILED ONCE MORE. TROUBLESHOOTING FOUND THAT THE LT ENG PROBE HARNESS PN 3052134-01 TO BE INTERMITTENT. THE DEFECTIVE HARNESS WAS R & R WITH A NEW CONDITION HARNESS. OPERATIONAL CHECKS WERE SATISFACTORY & THE ACFT WAS RETURNED TO SERVICE.
Part: CIRCUIT CARD — DEFECTIVE (AUTOPILOT SYS) · airframe 4,111 hrs · 4,407 cycles
THE CREW REPORTED THAT ON 2014/01/26 THAT THE YAW DAMPENER DISENGAGED DURING FLIGHT WHILE IN TURBULENCE, THE NR 1 FCC CARD WAS REPLACED WITH A TESTED UNIT PN 822-1019-313 & SN 1C68V. FUNCTIONAL CHECKS WERE SATISFACTORY & THE ACFT WAS RETURNED TO SERVICE. THE CREW REPORTED AGAIN THAT THE YAW DAMPENER DISENGAGED DURING FLIGHT. TROUBLESHOOTING IDENTIFIED THE NR 1 FCC CARD SN 1C68V AS DEFECTIVE & WAS REPLACED WITH A OVERHAULED UNIT. FUNCTIONAL CHECKS WERE SATISFACTORY & THE ACFT WAS RETURNED TO SERVICE.