- Registered owner
- Calspan Corporation
- Location
- Buffalo, NY
- Owner type
- Corporation
- Serial number
- 218
- Year built
- 1969
- Type
- Fixed wing multi engine
- Engine
- Turbo-jet
- Airworthiness
- Experimental, research and development, crew training, market survey
- Airworthiness date
- January 3, 2018
- Certificate issued
- December 2, 1980
- Expires
- January 31, 2029
- Mode S code
- A00A57
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 29
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 |
|---|---|
| 1978 | 2 |
| 1979 | 1 |
| 1980 | 2 |
| 1981 | 3 |
| 1984 | 2 |
| 1985 | 2 |
| 1986 | 2 |
| 1988 | 1 |
| 1989 | 1 |
| 1992 | 1 |
| 1995 | 1 |
| 1998 | 2 |
| 1999 | 1 |
| 2001 | 2 |
| 2005 | 3 |
| 2007 | 1 |
| 2010 | 1 |
See all 29 ADs
Information bulletins that may apply · 3
Advisory, not mandatory.
Airframe · Gates Lear Jet 24D
SAIB 2026-07MAIN LANDING GEAR ATTACH SECTION, Trunnion PinsSAIB NM-13-38Flight Controls Control Column SectionEngine · GE CJ-610-8A
SAIB NE-08-49R1Turbine Engine Combustion SectionHistorical bulletins · 1
NTSB investigations
No NTSB investigations matched to N101VSMatched 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 Gates Lear Jet 24D aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2005FA0000188Pump · flakingTHE INTERNAL COATING IN THE GEAR SECTION OF THE FUEL PUMP STARTED FLAKING OFF AND GOT INTO THE HIGH PRESSURE FUEL LINE THAT GOES TO THE JET PUMPS IN THE RT WING. THE MATERIAL CLOGGED UP THE ORIFICES IN THE JET PUMPS, NOT ALLOWING FUEL TO BE TRANSFERRED FROM SDR 96ZZZX5476Check Valve · flap brokenTHERE ARE 2 EACH PN 6600255-2 HOT AIR CHECK VALVES INSTALLED AS PARTS OF KIT PN 2881701-1 FOR AMR 79-8 FOR LEAR 28229 AIRCRAFT. BOTH CHECK VALVES HAD FAILURES OF THE RETENTION SPRING AND MOUNT PIN OF THE HINGED PORTION OF THE FLAPPER IN THE CHECK VALVE. THIS
STCs that may be installed · 80
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Gates Lear Jet 24D
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 SA2622NMInstallation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101)STC ST03885ATInstallation of an Avionica, Inc. avCM Cellular Module