- Registered owner
- Del Mar College
- Location
- Corpus Christi, TX
- Owner type
- Government
- Serial number
- 130
- Year built
- 1973
- Type
- Fixed wing multi engine
- Engine
- Turbo-jet
- Airworthiness
- Standard, transport
- Airworthiness date
- August 14, 1973
- Certificate issued
- June 16, 2015
- Expires
- June 30, 2028
- Mode S code
- A27CB6
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every GE CJ610-SER model are included below.
On this page
Airworthiness directives that may apply · 31
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1975 | 2 |
|---|---|
| 1978 | 2 |
| 1979 | 1 |
| 1980 | 2 |
| 1981 | 3 |
| 1984 | 1 |
| 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 31 ADs
Information bulletins that may apply · 5
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N26ATMatched 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 25B 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 · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR G41A20130402001Tire · separatedAFTER LANDING IN MMPR, WHILE PERFORMING THE WALK AROUND INSPECTION, THE CAPTAIN NOTICED A SECTION OF THE TREAD MISSING ON THE NR 1 MAIN TIRE. NO OTHER DAMAGE WAS REPORTED BUT THE TREAD SEPARATION. THE CAUSE OF THE TREAD SEPARATION COULD NOT BE DETERMINED. MSDR G41A201207300005Bonding Jumper · frayedDEPARTING ELP ON AN EMPTY LEG TO IAH, 5 MIN AFTER TAKEOFF, THE CAPTAIN REPORTED THAT AFTER FLYING THROUGH A RAIN CLOUD TRANSMITTING ON THE NR 1 AND NR 2 COMM RADIOS BECAME GARBLED AND UNREADABLE. RECEIVING SEEMED NORMAL. CAPTAIN CHOSE TO RETURN TO ELP. LOCASDR 2011F00033Filter · contaminatedCABIN WAS PRESSURIZING BUT PILOT REPORTED ERRATIC CABIN RATE OF CLIMB AND ELECTED TO RETURN TO BASE. MX CHECKED TAILCONE FOR PRESSURE LEAKS NONE FOUND. MX CHECKED PRESSURE CONTROLLER AND FOUND CONTAMINATION IN THE FILTER WHICH APPEARED TO BE AN INSECT. REPLSDR G41A2007003Engine · flamed outLEARJET N26AT WAS ON THE WAY FROM ELP TO LAX AT FL 410, THE CREW WAS EXPERIENCING SEVERE WEATHER AND REQUESTED TO GO TO FL 450. DURING THE CLIMB THEY HIT TURBULENCE AND THE LT ENGINE FLAMED OUT. THEN REQUESTED TO GO DOWN TO FL 250, RELIT THE LT ENGINE, THEN
STCs that may be installed · 106
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 25B
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