N922HA
Registered owner: HILLER AVIATION GROUP INC, AZ (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| HENSON AIRLINES | Operator | on 1991-07-16 | Operator named in NTSB report |
Accident & incident history
Operated by HENSON AIRLINES (per NTSB report)
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.
11 reports on file, 1995-02-12 – 2001-03-22.
Part: ENGINE — LACK OF LUBE (NR 2 ENGINE) · airframe 35,268 hrs · 40,548 cycles
DURING TAKEOFF ROLL, NR 2 ENGINE OIL PRESSURE FLUXED INTO THE YELLOW ARC. THERE WERE NO ASSCOIATED WARNING LIGHTS. CREW ABORTED TAKEOFF. SERVICED NR 2 ENGINE WITH THREE QUARTS OF OIL.
Part: STRINGER — DENTED (BS 151-157)
REINSPECT AND EVALUATE APPROX 10 DENTS ON STR 30S, BETWEEN STATIONS X151.6 AND X157.0 FOR PERMANENT REPAIR. ALSO, GENERATE DMT FOR PERM REPAIR. DEFERED PER DISPOSITION ON 8\14\99 SEQ 29. REPAIRED IAW EO8-53-99-316.
Part: FRAME — CORRODED (BS 240)
FRAME CORRODED AT FRAME LEG JOINT STA X240 STR 31R. REPAIRED IAW EO8-53-99-318.
Part: UNKNOWN — ODOR (COCKPIT)
DURING TRAINING FLIGH, EXPERIENCED SMOKE-LIKE SMELL IN COCKPIT. UNABLE TO DUPLICATE. NO DISCREPANCY FOUND.
Part: SENSOR — MALFUNCTIONED (LT MLG)
FLT 3270 - CLT-CRW - LEFT MAIN GEAR DOOR REMAINED OPEN AFTER GEAR RETRACTION. INSPECTED PROX SENSORS AND WIRING PERFORMED NEAR/FAR TARGET TEST. PERFORMED SEVERAL GEAR RETRACTIONS. COULD NOT DUPLICATE. (M)
Part: ENGINE — FAILED (NR 1)
FLT 3402 - LYH-PIT - AFTER TAKEOFF, THE NR 1 ENGINE AUTOFEATHERED AND THE TORQUE INDICATION DROPPED TO ZERO. THE AIRCRAFT TURNED BACK TO LYH AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE AND THE TORQUE SENSOR CONTROL UNIT. (M)
Part: HYD SYSTEM — REQD SERVICE (NR 2)
SBY/PHL - FLT 3184 - WHEN SELECTING LANDING GEAR DOWN ON APPROACH INTO PHL, THE DOORS DID NOT OPEN AND GEAR DID NOT COME DOWN. PERFORMED ALTERNATE GEAR EXTENSION AND LANDED IN PHL WITHOUT INCIDENT. BLED NR 2 HYDRAULIC SYSTEM, GEAR SWING CHECKED GOOD. (X)
Part: ENGINE HARNESS — FAILED (NR 2 ENGINE)
FLT NR 3068 - PHL-LYH - ON TAKEOFF, THE RIGHT PROP DECREASED FROM 1200 RPM TO 600 RPM. THE CREW ABORTED THE TAKEOFF WITHOUT INCIDENT. REMOVED AND REPLACED THE ENGINE HARNESS BETWEEN P3 AND P42 AND REMOVED AND REPLACED THE REVERSION RELAY 7611-K2.
Part: REVERSION RELAY — FAILED (NR 2 ENGINE)
FLT NR 3068 - PHL-LYH - ON TAKEOFF, THE RIGHT PROP DECREASED FROM 1200 RPM TO 600 RPM. THE CREW ABORTED THE TAKEOFF WITHOUT INCIDENT. REMOVED AND REPLACED THE ENGINE HARNESS BETWEEN P3 AND P42 AND REMOVED AND REPLACED THE REVERSION RELAY 7611-K2.
Part: ECU — FAILED (NR 2 ENGINE)
FLT 3217 - LYH-PHL - AFTER LANDING, THE NR 2 PROP STABILIZED AT 650 RPM. THE CREW CYCLED THE CONDITION LEVER TO START FEATHER, THEN BACK TO MINIMUM AND THE PROP WOULD NOT COME OUT OF FEATHER. REMOVED AND REPLACED THE NR 2 ELECTRONIC CONTROL UNIT.
Part: SELECTOR VALVE — FAILED (LANDING GEAR)
HPN-PHL - FLT 3108 - ON APPROACH, LANDING GEAR DID NOT EXTEND ON NORMAL GEAR EXTENSION. PERFORMED ALTERNATE GEAR EXTENSION AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE.