N777QL
Registered owner: MED AIR LLC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
6 reports on file, 2014-07-29 – 2019-11-06.
Part: SKIN — CORRODED (BS 245-256) · airframe 6,497 hrs · 4,745 cycles
AT INSPECTION DETERMINED SKIN CORROSION AT UPPER FORWARD TCAS ANTENNA. REMOVED CORROSION AND DETERMINED REMAINING THICKNESS PER ULTRASONIC INSPECTION. REMAINING THICKNESS ACCEPTABLE.
Part: SKIN PANEL — CORRODED (BS 396) · airframe 6,498 hrs · 4,745 cycles
AT SCHEDULED INSPECTION DISCOVERED CORROSION FORWARD OF PANEL 510AL. REMOVED CORROSION. DETERMINED REMAINING THICKNESS BY ULTRASONIC INSPECTION. REMAINING THICKNESS DETERMINED TO BE ACCEPTABLE.
Part: STRUCTURE — CORRODED (CARGO DOOR) · airframe 6,498 hrs · 4,745 cycles
AT SCHEDULED INSPECTION DISCOVERED CORROSION ON BAGGAGE DOOR AROUND LATCHES AND KEYHOLE. REMOVED CORROSION AND DETERMINED REMAINING THICKNESS PER ULTRASONIC INSPECTION. REMAINING THICKNESS ACCEPTABLE.
Part: SKIN — CORRODED (BS 396) · airframe 6,498 hrs · 4,745 cycles
AT 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.
Part: BUSHING — MISSING (CONTROL WHEEL) · airframe 6,361 hrs · 4,632 cycles
WHILE 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 AND 4527302001V32-003) ALLOWING SUFFICIENT GAP FOR ANGULAR AXIAL LOADS TO BE APPLIED ON RADIAL BEARING. BUSHINGS INSTALLED AND BEARING REPLACED.
Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 4,430 hrs · 3,258 cycles
PRIOR 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, NOTICED CABIN ALTITUDE RISE AND STARTED AN IMMEDIATE DESCENT. AT APPROXIMATELY FL240 THE PRESSURIZATION CONTROLLER BEGAN TO WORK AND HOLD CABIN ALTITUDE. THE DECISION WAS MADE TO LAND.