- Registered owner
- Hop-A-Jet Worldwide Jet Charter Inc
- Location
- Fort Lauderdale, FL
- Owner type
- Corporation
- Serial number
- 188
- Year built
- 2000
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- May 16, 2000
- Certificate issued
- June 30, 2011
- Expires
- June 30, 2027
- Mode S code
- A26BAC
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada 305 model are included below.
On this page
Airworthiness directives that may apply · 19
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1993 | 1 |
|---|---|
| 1994 | 1 |
| 1995 | 2 |
| 1996 | 1 |
| 1998 | 1 |
| 1999 | 2 |
| 2000 | 1 |
| 2001 | 1 |
| 2002 | 1 |
| 2003 | 1 |
| 2005 | 1 |
| 2010 | 1 |
| 2012 | 1 |
| 2013 | 1 |
| 2014 | 1 |
| 2017 | 2 |
| 2018 | 1 |
| 2019 | 1 |
| 2020 | 1 |
| 2022 | 1 |
See all 23 ADs
Information bulletins that may apply · 2
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N255SLMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Learjet 60 aircraft
FAA incident reports
No FAA accident or incident reports matched to N255SLMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Learjet 60 aircraft
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR V6NA2021040601Door · crackedGROUND 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 DAMAGSDR V6NA2019012301Stringer · corrodedAT 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.SDR V6NA201902192019Rib · crackedAT 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.SDR V6NA2019012407Bracket · crackedAT SCHEDULED INSPECTION, DISCOVERED LEFT THRUST REVERSER INBOARD STANG FAIRING AFT BRACKET CRACKED.SDR V6NA2019012406Bracket · crackedAT SCHEDULED INSPECTION, DISCOVERED RIGHT THRUST REVERSER AFT STANG FAIRING BRACKET CRACKED. REPLACED RIGHT THRUST REVERESER STANG FAIRING AFT BRACKET.SDR V6NA2019012405Support Bracket · crackedAT SCHEDULED INSPECTION, DISCOVERED RIGHT THRUST REVERSER OUTBOARD FORWARD FAIRING SUPPORT BRACKET. REPLACED SUPPORT BRACKET WITH NEW.SDR V6NA2019012404Skin · crackedAT SCHEDULED INSPECTION, DISCOVERED RUDDER LOWER LEADING EDGE SKIN CRACKED. REPLACED RUDDER LOWER LEADING EDGE SKIN.SDR V6NA2019012403Torque Tube · corrodedAT SCHEDULED INSPECTION, DISCOVERED RUDDER TORQUE TUBE CORRODED. REPLACED RUDDER TORQUE TUBE WITH NEW.SDR V6NA2019012402Axle · corrodedAT SCHEDULED INSPECTION, DETERMINED RIGHT MAIN LANDING GEAR AXLE CORRODED. REPLACED AXLE WITH NEW.SDR V6NA2019012401Support Angle · crackedAT SCHEDULED INSPECTION, FOUND CRACK AT RIVET HOLE ON LEFT AILERON ANGLE SUPPORT AT AILERON STATION 32.0. PERFORMED DOUBLER REPAIR PER DER DRAWING.SDR V6NA20170707001Computer · out of adjustAFTER TAKEOFF, RECEIVED NOSE STEER UNSAFE LIGHT. RETURNED AND LANDED WITHOUT INCIDENT. AFTER LANDING NOSE STEERING WAS UNAVAILABLE. RECALIBRATED NOSE STEERING COMPUTER.SDR V6NA20170623001Solenoid Valve · inoperativeWHILE 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.
STCs that may be installed · 157
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Learjet 60
STC ST01305WI-DModification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision.STC ST12461IBInstallation of Cockpit Voice Recorder with optional RIPS UpgradeSTC SA2622NMInstallation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101)