N255SL
Registered owner: HOP-A-JET WORLDWIDE JET CHARTER INC, FL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| ACE AVIATION SERVICES CORPORATION (V6NA) | 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.
12 reports on file, 2017-06-23 – 2021-04-06.
Part: DOOR — CRACKED (ZONE 100) · airframe 13,976 hrs · 9,685 cycles
GROUND DAMAGE; MAIN ENTRANCE DOOR, LOWER. AFT CORNER AT UPPER SEAM (STOWED) DENTED AND CRACKED. DAMAGE AREA 1.5 INCHES BY 2.0 INCHES. SKIN DENT WORKED SMOOTH; DAMAGED AREA REMOVED. EDDY CURRENT INSPECTION PERFORMED AROUND REMOVED AREA VERIFIED NO FURTHER DAMAGE. A FILLER AND DOUBLER SHEET METAL REPAIR WAS INSTALLED PER FAA DER APPROVED DATA.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,459 hrs · 8,634 cycles
AT SCHEDULED INSPECTION, DETERMINED STRINGER 21, BETWEEN FS 151.9 AND FS 176.59 TO BE CORRODED. DAMAGED STRINGER SECTION REMOVED, SKIN CLEANED AND INSPECTED AND STRINGER SPLICE REPAIR PERFORMED PER STRUCTURAL REPAIR MANUAL AND DER DRAWING.
Part: RIB — CRACKED (RUDDER) · airframe 12,459 hrs · 8,634 cycles
AT SCHEDULED INSPECTION, DISCOVERED RUDDER RIB AT WL 126.0 TO BE CRACKED. RIB REPAIRED WITH DOUBLER PER LEARJET 60 STRUCTURAL REPAIR MANUAL SECTION 55-40-01.
Part: AXLE — CORRODED (RT MLG) · airframe 12,459 hrs · 8,634 cycles
AT SCHEDULED INSPECTION, DETERMINED RIGHT MAIN LANDING GEAR AXLE CORRODED. REPLACED AXLE WITH NEW.
Part: SUPPORT BRACKET — CRACKED (THRUST REVERSER) · airframe 12,459 hrs · 8,634 cycles
AT SCHEDULED INSPECTION, DISCOVERED RIGHT THRUST REVERSER OUTBOARD FORWARD FAIRING SUPPORT BRACKET. REPLACED SUPPORT BRACKET WITH NEW.
Part: SKIN — CRACKED (RUDDER) · airframe 12,459 hrs · 8,634 cycles
AT SCHEDULED INSPECTION, DISCOVERED RUDDER LOWER LEADING EDGE SKIN CRACKED. REPLACED RUDDER LOWER LEADING EDGE SKIN.
Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 12,459 hrs · 8,634 cycles
AT SCHEDULED INSPECTION, DISCOVERED RIGHT THRUST REVERSER AFT STANG FAIRING BRACKET CRACKED. REPLACED RIGHT THRUST REVERESER STANG FAIRING AFT BRACKET.
Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 12,459 hrs · 8,634 cycles
AT SCHEDULED INSPECTION, DISCOVERED LEFT THRUST REVERSER INBOARD STANG FAIRING AFT BRACKET CRACKED.
Part: TORQUE TUBE — CORRODED (RUDDER) · airframe 12,459 hrs · 8,634 cycles
AT SCHEDULED INSPECTION, DISCOVERED RUDDER TORQUE TUBE CORRODED. REPLACED RUDDER TORQUE TUBE WITH NEW.
Part: SUPPORT ANGLE — CRACKED (LT AILERON) · airframe 12,459 hrs · 8,634 cycles
AT SCHEDULED INSPECTION, FOUND CRACK AT RIVET HOLE ON LEFT AILERON ANGLE SUPPORT AT AILERON STATION 32.0. PERFORMED DOUBLER REPAIR PER DER DRAWING.
Part: COMPUTER — OUT OF ADJUST (NLG STEERING) · airframe 11,461 hrs · 7,957 cycles
AFTER TAKEOFF, RECEIVED NOSE STEER UNSAFE LIGHT. RETURNED AND LANDED WITHOUT INCIDENT. AFTER LANDING NOSE STEERING WAS UNAVAILABLE. RECALIBRATED NOSE STEERING COMPUTER.
Part: SOLENOID VALVE — INOPERATIVE (ENGINE BLEED) · airframe 11,433 hrs · 7,932 cycles
WHILE ADDING POWER FOR TAKE OFF, A LOUD OSCILLATING SOUND FOLLOWED BY RIGHT RED OIL PRESSURE ANNUNCIATOR, OIL PRESSURE GAUGE WAS ALSO ZERO. ABORTED TAKEOFF & RETURNED TO RAMP. RIGHT ENGINE BLEED AIR SHUTOFF VALVE SOLENOID REPLACED.