- Registered owner
- Thunderun Aviation Corp
- Location
- Glenwood, NY
- Owner type
- Corporation
- Serial number
- 175
- Year built
- 1999
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- May 28, 1999
- Certificate issued
- December 30, 2022
- Expires
- December 31, 2029
- Mode S code
- A23018
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 21
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1975 | 1 |
|---|---|
| 1983 | 1 |
| 1992 | 1 |
| 1995 | 2 |
| 1996 | 2 |
| 1998 | 2 |
| 1999 | 4 |
| 2000 | 1 |
| 2001 | 2 |
| 2004 | 1 |
| 2005 | 2 |
| 2007 | 2 |
| 2018 | 1 |
See all 22 ADs
Information bulletins that may apply · 4
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N240BMatched 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 31A aircraft
FAA incident reports
No FAA accident or incident reports matched to N240BMatched 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 31A aircraft
Service difficulty reports · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
Reports on N240B not matched to an aircraft · 2
They name N240B, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 2006FA0000566Windshield · crackedPILOTS WINDSHIELD OUTER PANE CRACKED AT 39,000 FT. IT IS BELIEVED THAT A HEATING ELEMENT SHORTED CAUSING THE OUTER PANE TO CRACK. WINDSHIELD REMAINS STRUCTURALLY INTERGRAL WITH THE OUTER PANE CRACKED. MFG ENGINEERING IS EVALUATING THE FAILURE. (K)SDR 95ZZZX4440Switch · faultyINTERMITTENTLY, THE PILOTS 4-WAY TRIM SWITCH WOULD FAIL WITH AUTOPILOT ENGAGED AND WOULD CAUSE TRIM FOR AUTOPILOT TO TRIM PITCH UP, DISCONNECTING ANY OTHER PITCH MODES AND TRIM FULL NOSE UP ATTITUDE IF AUTOPILOT WAS NOT DISCONNECTED. THE CAUSE IS APPARENTLY T
STCs that may be installed · 103
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Learjet 31A
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)
Earlier aircraft with this N-number · 2
These aircraft carried N240B before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.