- Registered owner
- Ati Jet Inc
- Location
- El Paso, TX
- Owner type
- Corporation
- Serial number
- 106
- Year built
- 1984
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- July 20, 1984
- Certificate issued
- May 11, 2026
- Expires
- May 31, 2033
- Mode S code
- AB40D1
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Garrett TFE731 model are included below.
On this page
Airworthiness directives that may apply · 54
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1974 | 5 |
|---|---|
| 1975 | 1 |
| 1978 | 1 |
| 1980 | 1 |
| 1982 | 1 |
| 1983 | 1 |
| 1984 | 1 |
| 1986 | 3 |
| 1987 | 2 |
| 1989 | 2 |
| 1990 | 2 |
| 1991 | 1 |
| 1992 | 1 |
| 1993 | 1 |
| 1994 | 4 |
| 1995 | 3 |
| 1996 | 3 |
| 1997 | 1 |
| 1998 | 1 |
| 1999 | 2 |
| 2000 | 2 |
| 2001 | 3 |
| 2005 | 2 |
| 2007 | 2 |
| 2008 | 3 |
| 2009 | 1 |
| 2010 | 1 |
| 2012 | 1 |
| 2014 | 1 |
| 2016 | 1 |
| 2018 | 1 |
| 2022 | 1 |
Airframe · Gates Learjet 55
AD 2022-05-01SpoilersAD 2018-19-04TE Flap Control SystemAD 2009-03-01Lavatory light assemblyInformation bulletins that may apply · 4
Advisory, not mandatory.
Airframe · Gates Learjet 55
SAIB 2026-07MAIN LANDING GEAR ATTACH SECTION, Trunnion PinsSAIB NM-16-24Fuselage: Main Plate/SkinSAIB CE-02-19Engine · Garrett TFE731 series
SAIB NE-06-70NTSB investigations
No NTSB investigations matched to N824MGMatched 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 Learjet 55 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 · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR G41A2026FA0000235Fms · defectiveAIRCRAFT DEPARTED KELP HEADING TO KAUS. ABOUT 10 MINUTES AFTER TAKEOFF, THE CAPTAIN NOTICED THE FMS SCREEN HAD GONE BLANK. ATTEMPT TOP RE POWER WAS MADE WITH NO EFFECT. THE CAPTAIN DECIDED TO RETURN TO ELP. ATI MAINTENANCE AND AVIONICS MET THE AIRCRAFT AND VESDR G41A2024092400735Hydraulic Line · rupturedON THE MORNING OF 9/21/2024, N824MG WAS DEPARTING EMPTY FROM KLBB HEADING BACK TO KELP WHEN THE CAPTAIN NOTICED THE HYDRAULIC PRESSURE INDICATOR FLUCTUATING. NO OTHER ISSUE OR DISCREPANCY NOTICED. THE CAPTAIN ELECTED TO RETURN TO KLBB FOR PRECAUTIONARY PURPOSESDR 2020FA0000489Control Valve · failedDEPARTED KFCM, REFUELED AT KLNK. DURING FLIGHT, PILOTS BANKED HARD LEFT, EMERGENCY DESCENT TO LAND IN SALINA, KS. CHIEF PILOT STATED "FUEL CONTROL VALVE FAILED AND WERE 'DANGEROUSLY LOW ON FUEL'". HE FURTHER STATED, "OUR 55'S ARE OLD AND SOMETHING'S ALWAYS SDR 2020FA0000445Control Box · defectiveON 10/8/2020, N824MG DEPARTED KLNK WITH PASSENGERS FLYING TO KELP. AFTER TAKEOFF THE CREW ATTEMPTED TO START THE FUEL TRANSFER AND NOTICED THE TRANSFER/CROSS FLOW VALVES TRANSITION LIGHTS WERE NOT ILLUMINATING WITH ANY OF THE TRANSFER OPTIONS. THE CAPTAIN NOSDR G41A2019FA0000148Tire · blownON 5-8-2019, DEPART BHM TO MAF. AT APPROXIMATELY 120 KNOTS ABOUT TO TAKE OFF, THE NR 1 & 2 MAIN TIRES BLEW OUT AT THE SAME TIME. THE CAPTAIN STOPPED THE AIRCRAFT SAFELY ON A TAXI WAY. THE CREW COULD NOT DETERMINE IF THEY HAD RUN OVER DEBRIS OR NOT, THE CREW STSDR G41A20160628002Wire · pulledON THE AFTERNOON OF 6-24-2016, ACFT DEPARTED, AT FL290, THE CAPTAIN NOTICED THE NR 2 ENGINE HAD STARTED A SLIGHT ROLLBACK ON THE N1 AND N2 INDICATORS. THEY ATTEMPTED TO CONTINUE TO THEIR CRUISING ALTITUDE, THE ROLLBACK CONTINUED AND GRADUALLY GOT WORSE. THE SDR 2015FA0000388Valve · leakingON DESCENT, THE CAPTAIN NOTICED THE OIL PRESSURE ON THE RT ENGINE, FLUCTUATING FROM NORMAL OPERATING PRESSURE OF 42PSI DOWN TO 25PSI. IT GRADUALLY DROPPED DOWN TO 20PSI AND HE THEN ELECTED TO SHUT THE ENGINE DOWN AND DECLARE AND EMERGENCY. THE ACFT WAS LANDESDR 2011F00143Warning Light · false activationDEPARTING, THE CAPTAIN REPORTED THAT AT ABOUT 60 KTS THE AMBER CABIN PRESSURE WARNING LIGHT ILLUMINATED, THE CAPTAIN DECIDED TO ABORT THE TAKEOFF. AFTER ROLLING CLEAR OF THE RUNWAY ONTO A TAXIWAY, HE SWITCHED THE CABIN AIR FROM ON TO OFF THEN BACK ON. THE CAB
STCs that may be installed · 95
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Gates Learjet 55
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