N107AL
Registered owner: AERO TECH SERVICES INC, PA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Gama Aviation LLC (O2GA) | Certificate holder | — | Matched by certificate designator |
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.
9 reports on file, 1995-05-11 – 2002-06-10.
Part: BLADE — MISSING (TURBINE WHEEL) · airframe 8,908 hrs
UPON INSPECTION OF ALL PARTS NR 2 WHEEL HAD ONE BLADE MISSING.
Part: FIRE WARNING — WILL NOT TEST (NR 1 SYS)
DURING PRESTART CHECK. NR 1 FIRE WARNING SYSTEM WOULD NOT TEST. AFTER ENGINES WERE RUN AND ENGINE COMPARTMENTS WERE DRIED OUT, SYSTEM TESTED NORMALLY.
Part: TURBINE WHEEL — DAMAGED (ENGINE)
UPON DISASSEMBLY OF TURBINE FOR EVALUATION DUE TO ENGINE QUITTING DURING OPERATION. UPON INSPECTION OF ALL PARTS NR 2 WHEEL HAD ONE BLADE MISSING. PERFORM INSPECTION OF WHEELS UPON ASSEMBLY AT MANUFACTURER FOR POSSIBLE IMPERFECTIONS.
Part: WIRING HARNESS — FAILED (HYD PACK)
IN-FLIGHT, HYDRAULIC BLOCK ILLUMINATED; SYSTEM SWITCHED TO NR 2 HYDRAULIC SYSTEM. RETURNED TO BASE WITHOUT INSTALLED NEW HARNESS.
Part: DETECTOR — LEAD LOOSE (NR 2 ENGINE)
IN CRUISE FLIGHT, THE NR 2 ENGINE FIRE LIGHT FLASHED ON AND OFF CONTINUOUSLY. DESCENDED TO 300 FEET, CHECKED SHADOW FOR SMOKE, NONE SEEN, RETURNED TO BASE. ALL ENGINE INSTRUMENTS NORMAL. REMOVED NR 2 ENGINE COWL, INSPECTED LOWER DETECTOR, INSPECTED UPPER DETECTOR, FOUND LEAD LOOSE ON UPPER DETECTOR. INSTALLED NEW LOCK WASHER AND NUT. OPS CHECK OK.
Part: TIE BOLT — UNDERSIZE (COMP ROTOR)
DISCOVERED DEFECT DURING TOLERANCE INSPECTION. THE TIE BOLT SHOULDER UNDER SIZE BY .002 INCH, .440 INCH, BPS .4420 INCH TO .4425 INCH.
Part: BEARING — FROZEN (FLYWEIGHTS)
DURING TEAR DOWN INVESTIGATION OF UNIT, FOUND 2523240 BEARINGS FROZEN CAUSING FLYWEIGHTS TO STICK.
Part: BLADE — SEPARATION (CAMBER SIDE)
DAILY INSPECTION FOUND BLADE SEPARATED 9 INCHES FROM TIP AND 2 INCHES FROM LEADING EDGE ON CAMBER SIDE OF BLADE. SEPARATED AT FACE PLATE TRANSITION AREA. SEPARATION BEYOND LIMITS.
Part: PC LINK — CORRODED (T/R)
DURING PMI INSPECTION (50-HOUR INSPECTION) FOUND T/R PC LINK CORRODED. LINK SCRAPPED DUE TO CORROSION AT BEARING HOLE.