N242JT
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
AFTER DEPARTURE THE FLIGHT CREW REPORTED A RIGHT BLEED AIR OVERHEAT ANNUNCIATOR. THE CREW ELECTED TO DIVERT BACK TO THE AIRPORT FOR A SAFE LANDING. NO EMERGENCY WAS DECLARED. THE MAINTENANCE PROVIDER DETERMINED THE RIGHT BLEED AIR PRECOOLER WAS DEFECTIVE AND REQUIRED REPLACEMENT. THE COOLER WAS REMOVED, AND AN OVERHAULED UNIT WAS INSTALLED. OPS AND LEAK CHECKS WERE SATISFACTORY, AND THE AIRCRAFT WAS REPORTED TO SERVICE.
THE FLIGHT CREW REPORTED THAT DURING FLIGHT OF RECEIVING A RIGHT BLEED AIR OVERTEMP INDICATION. THE MAINTENANCE PROVIDER FOUND THE RIGHT BLEED AIR PRECOOLER HAD DAMAGE. THE PRECOOLER WAS REMOVED. AN OVERHAULED UNIT WAS INSTALLED. OPS AND LEAK CHECKS WERE PERFORMED SATISFACTORILY.
FLIGHT CREW REPORTED A AOA HEATER FAIL ANNUNCIATOR. THE MAINTENANCE PROVIDER REMOVED THE AOA SENSOR DUE TO FAILURE AND INSTALLED A NEW SENSOR. OPS CHECKS WERE SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.
THE FLIGHT CREW REPORTED A PRESSURIZATION MALFUNCTION AND A CABIN ALTITUDE ANNUNCIATOR WHILE IN FLIGHT. THE FAULT WITH THE PRESSURIZATION SYSTEM WAS DEFERRED BY MEL 21-30-02-008 UNTIL MAINTENANCE COULD BE HAD. THE MAINTENANCE VENDOR DETERMINED THAT THE CABIN AIR CONTROLLER WAS AT FAULT AND REPLACED IT WITH AN OVERHAULED UNIT. OPS CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.
THE BASE MAINTENANCE TEAM FOUND THE HF RADIO SYSTEM INOP DURING MAINTENANCE CHECKS. THE MAINTENANCE FOR THE HF RADIO WAS DEFERRED DUE TO PARTS AVAILABILITY. THE AIRCRAFT WAS RETURNED TO SERVICE. DURING THE MAINTENANCE EVENT THE DEFECTIVE ANTENNA COUPLER WAS REMOVED AND AN OVERHAULED ANTENNA COUPLER WAS INSTALLED. OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.
FLIGHT CREW REPORTED THAT THE TAWS SYSTEM HAD FAILED. THE MAINTENANCE VENDOR TROUBLESHOT AND FOUND THE EGPWS COMPUTER FAILED TESTING. THE COMPUTER WAS REPLACED WITH A REPAIRED UNIT. OPS CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE
A FLIGHT WAS CANCELLED WHEN THE FLIGHT CREW DISCOVERED AN OXYGEN LEAK. THE MAINTENANCE TEAM DETERMINED THAT A OXYGEN LINE TEE FITTING LEAKING. THE DEFECTIVE TEE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED PN AS4857-01. THE OXYGEN SYSTEM WAS SERVICE AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE.
DURING REPAIRS TO FIX A CABIN DOOR SEAL ANNUNCIATOR INDICATION, A CRACK WAS FOUND IN THE MAIN CABIN DOOR STRUCTURAL PLATE UNDER STEPS. THE CRACK WAS LOCATED ON THE PLATE AT THE ACCESS FOR THE DOOR CLOSE ASSIST SPRING. THE MAINTENANCE VENDOR COMPLETED REPAIRS, PER THE CESSNA 560XL NDL MANUAL AND THE 560XL SRM 52-10-10. A REPAIR DOUBLER WAS FABRICATED FROM ALUMINUM AND INSTALLED.