N901UP
Registered owner: RYAN AIR LLC, NY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Gama Aviation LLC (O2GA) | 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.
2 reports on file, 2019-06-05 – 2025-01-06.
Part: DRIVE UNIT — INTERMITTENT (FLAP SYS) · airframe 18,942 hrs · 11,551 cycles
FLAPS FAIL MESSAGE OCCURED AFTER TAKEOFF/ENROUTE, POSTION INDICATED FALPS 0 AND SLATS NOT EXTENED. EMERGENCY DECLARED. T/S FLAPS SYSTEM. POWERED AIRCRAFT AND REVIEWED BIT CHECK ON FLAP CONTROLLER, FLAP CONTROLLER SHOWED BIT FAULT 2 (MOTOR FAULT) ANO BIT FAULT 6 (NO COMMAND). CLEAR FAULTS AND RAN FLAPS THROUGH SEVERAL CYCLES AND MONITORED THE DC CURRENT TO PDU. FOUND NO FAULTS LOGGED IN FLAP CONTROLLER. FLAP FROM FULL UP TO FULL. DOWN SHOWED 36 AMPS ANO FROM FULL DOWN TO FULL UP WAS 32 AMPS. WITH FLAPS DOWN, INSPECTED L/H AND R/H FLAP TRACKS, ROLLERS AND ACTUATORS FOR ANY SIGNS OF DAMAGE. NO DAMAGE NOTED. T/S SYSTEM FURTHER. PER WUP FSR, REMOVED THE FLAP HANDLE AND CLEANED THE INTERNALS OF DUST AND DEBRIS. SMALL AMOUNT OF DEBRIS FOUND. REINSTALLED FLAP HANDLE AS REQUIRED. REMOVED FLAP PDU P/N MP50G-4 S/N 430A AND INSTALLED A "OVERHAULED" FLAP PDU P/N MP50G-4 S/N 166B AS NEEDED. PERFORMED FLAP OPERATIONAL CHECKS. ALL CHECKS FOUND GOOD. NO FAULTS POSTED ON ELCAS OR FLAP CONTROLLER. ALL WORK DONE IAW CE75O AMM 27-52-00.
Part: HOSE — RUPTURED (HYD SYSTEM) · airframe 15,007 hrs · 9,265 cycles
AFTER TAKEOFF GEAR SELECTED TO UP POSITION, CAS MESSAGE 'HYD VLUME LOW A'. THE HYDRAULIC QUANTITY DROPPED TO ZERO, FOLLOWED BY 'HYD PTU FAIL' CAS MESSAGE. EMERGENCY WAS DECLARED. DIVERTED TO KMSY. LANDING AND BRAKING WERE UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED A RUPTURED RIGHT MLG ACTUATOR RETRACT HOSE. GEAR SWINGS WERE PERFORMED AND SYSTEM BLED. AIRCRAFT WAS RETURNED TO SERVICE.