Registered owner
Med Air LLC
Owner type
LLC
Serial number
216
Year built
2002
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
September 23, 2005
Certificate issued
August 20, 2025
Expires
August 31, 2032
Mode S code
AA8471

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Alliedsign TFE731 model are included below.

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Airworthiness directives that may apply · 67

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1974In forceSuperseded2026
ADs by the year they took effect: 73 ADs
19745
19751
19781
19801
19821
19831
19861
19891
19902
19921
19931
19942
19951
19963
19971
19982
19992
20003
20012
20021
20034
20054
20063
20072
20083
20091
20105
20112
20124
20132
20143
20151
20161
20171
20191
20222
20231
See all 75 ADs

Information bulletins that may apply · 2

Advisory, not mandatory.

Engine · Alliedsign TFE731 series

SAIB NE-06-70Issued Sep 25, 2006
Historical bulletins · 1

NTSB investigations

No NTSB investigations matched to N777QLMatched 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 45 aircraft

FAA incident reports

No FAA accident or incident reports matched to N777QLMatched 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 45 aircraft

Service difficulty reports · 6

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR V6NA20191230604Skin · corrodedAT INSPECTION DETERMINED SKIN CORROSION AT UPPER FORWARD TCAS ANTENNA. REMOVED CORROSION AND DETERMINED REMAINING THICKNESS PER ULTRASONIC INSPECTION. REMAINING THICKNESS ACCEPTABLE.Nov 6, 2019 · N777QL · Lear 45LEAR · Fuselage Main, Plate/SkinSDR V6NA201912300603Structure · corrodedAT SCHEDULED INSPECTION DISCOVERED CORROSION ON BAGGAGE DOOR AROUND LATCHES AND KEYHOLE. REMOVED CORROSION AND DETERMINED REMAINING THICKNESS PER ULTRASONIC INSPECTION. REMAINING THICKNESS ACCEPTABLE.Nov 6, 2019 · N777QL · Lear 45LEAR · Service DoorsSDR V6NA20191230602Skin · corrodedAT SCHEDULED INSPECTION DISCOVERED CORROSION ON SKIN AFT OF LEFT MAIN LANDING GEAR WELL. REMOVED CORROSION AND DETERMINED REMAINING THICKNESS PER ULTRASONIC INSPECTION. REMAINING THICKNESS ACCEPTABLE PER FAA DER.Nov 6, 2019 · N777QL · Lear 45LEAR · Fuselage Main, Plate/SkinSDR V6NA2019123010601Skin Panel · corrodedAT SCHEDULED INSPECTION DISCOVERED CORROSION FORWARD OF PANEL 510AL. REMOVED CORROSION. DETERMINED REMAINING THICKNESS BY ULTRASONIC INSPECTION. REMAINING THICKNESS DETERMINED TO BE ACCEPTABLE.Nov 6, 2019 · N777QL · Lear 45LEAR · Fuselage Main, Plate/SkinSDR V6NA2019050701Bushing · missingWHILE INVESTIGATING PILOT REPORT OF LEFT / RIGHT AND FORWARD PLAY, DETERMINED CONTROL WHEEL DRUM BEARING (P/N MS27646-43) TO BE WORN. UPON FURTHER INVESTIGATION, DETERMINED BEARING WEAR RESULTING OF MISSING CONTROL WHEEL DRUM BUSHINGS (P/N'S 4527102086-003 ANDMay 5, 2019 · N777QL · Lear 45LEAR · Control Column SectionSDR WCEA2014FA0000454Controller · malfunctionedPRIOR TO FLIGHT, THE PRESSURIZATION CONTROLLER HAD BEEN CHANGED DUE TO FAILURE AND A REPAIRED UNIT INSTALLED IAW MM, 21-30-03. ALL OPS CHECKS PERFORMED WITH NO DISCREPANCIES NOTED. PREPARED FOR DEPARTURE WITH NO DISCREPANCIES. 30 MINUTES INTO FLIGHT, NOTICEJul 29, 2014 · N777QL · Lear 45LEAR · Cabin Pressure Controller

STCs that may be installed · 159

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 159 STCs