N928HA
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| HENSON AVIATION, INC. | Operator | on 1993-03-23 | Operator named in NTSB report |
Accident & incident history
Operated by HENSON AVIATION, INC. (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.
14 reports on file, 1995-04-12 – 2002-04-21.
Part: ENGINE — SHUTDOWN · airframe 36,545 hrs · 41,277 cycles
IN CRUISE FLIGHT THE #2 ENGINE OIL PRESSURE DROPPED BELOW 40 PSI. CREW SHUT DOWN ENGINE. ON THE GROUND IT WAS FOUND THAT THE ENGINE, NACELLE AND GEAR WERE COVERED WITH OIL AND THAT THE PROP WOULD NOT TURN. REPLACED #2 ENGINE.
Earlier reports · 1995–2001 · 13 reports
2001
Part: TRANSCEIVER — FAILED (WX RADAR) · airframe 34,683 hrs · 39,323 cycles
AIRCRAFT RETURNED TO TPA DUE TO WEATHER RADAR INOP. REPLACED RADAR R/T.
2000
Part: DRAG STRUT — FAILED (NLG) · airframe 31,447 hrs · 35,839 cycles
NOSE GEAR DID NOT EXTEND ON DOWN SELECTION. CYCLED GEAR, NOSE LANDING GEAR WAS SLOW TO EXTEND. REPLACED NLG DRAG STRUT UPPER LOCK LINK AND ALTERNATE RELEASE LINK BUSHINGS.
Part: BUSHING — WORN (NLG) · airframe 31,447 hrs · 35,839 cycles
NOSE GEAR DID NOT EXTEND ON DOWN SELECTION. CYCLED GEAR, NOSE LANDING GEAR WAS SLOW TO EXTEND. REPLACED NLG DRAG STRUT UPPER LOCK LINK AND ALTERNATE RELEASE LINK BUSHINGS.
1999
Part: WIRE — CHAFED (CABIN)
FORWARD CABIN EMERGENCY EXIT SIGNS INOPERATIVE. FOUND AFTER CHANGING EMERGENCY BATTERIES FOR SCHEDULED MAINTENANCE. REPAIRED CHAFED WIRES AND REPLACED DIODE AT RIGHT HAND CABIN SIDE WALL, OPERATIONAL CHECK GOOD.
Part: CONNECTOR — BROKEN (EMER EXIT DOOR)
FORWARD DOOR EMERGENCY EXIT SIGN, FORWARD AISLE DOWN LIGHT AND ROW 4 RED FLOOR EMERGENCY LIGHT INOPERATIVE. REPAIRED 3351-PS2 CONNECTOR, OPERATIONAL CHECK GOOD.
1998
Part: FRAME — CRACKED (APU BAY)
DURING AN APU CHANGE AT RON IN SBY, A CRACK WAS FOUND ON A FRAME AT THE 10 O'CLOCK POSITION. THE CRACK WAS REPAIRED IAW RD8-55-199. (M)
Part: BATTERY — DISCHARGED (CABIN)
ORF/PHF - FLT 3121 - ROW 8 OVERHEAD AISLE EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED BATTERY 3351-PS3. (X)
1997
Part: AIR CYCLE MACH — FAILED (APU BAY)
FLT - 3374 - AVL-CLT - WHILE PERFORMING PREFLIGHT CHECKS, SMOKE FILLED THE CABIN WHEN BLEED WAS TURNED ON. REMOVED AND REPLACED THE AIR CYCLE MACHINE. (M)
Part: DOOR STRUTS — BROKEN (AIRSTAIR DOOR)
FLT 3474 - HPN-PHL - THE CABIN DOOR WOULD NOT OPEN FROM INSIDE OR OUTSIDE. WHEN DOOR DID OPEN, IT FELL FREELY TO THE OPEN POSITION. REMOVED AND REPLACED THE AIRSTAIR DOOR STRUTS. (M)
1996
Part: POWER SUPPLIES — INOPERATIVE (CABIN)
FLT 3108 - GSO-BWI - DURING PREFLIGHT CHECKS, FOUND THE FORWARD CEILING EMERGENCY DOWN LIGHT INOP. SWAPPED PS1 AND PS2 POWER SUPPLIES. OPS CHECK GOOD. (M)
1995
Part: EEL BATTERY — DISCHARGED (CABIN)
TPA/JAX - FLT 3451 - DURING PRE-FLIGHT WALK-AROUND, FOUND 2 RED FLOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY AT SEATS 1DF.
Part: PSEU — FAILED (CABIN CLOSET)
FLT 3343 - RIC-DCA - AFTER GO AROUND TO DCA, THE GEAR WAS SELECTED UP AND THE RIGHT MAIN DOOR LIGHT REMAINED ON. AFTER SELECTING GEAR DOWN, RIGHT MAIN GEAR UNSAFE LIGHT CAME ON. SELECTED GEAR UP AND LL LIGHTS WENT OUT. UPON SELECTING GEAR DOWN AGAIN, LEFT AND RIGHT MAIN GEAR GREEN LIGHT CAME ON. THE NOSE GEAR UNSAFE LIGHT STAYED ON FOR APPROXIMATELY 5 SECONDS, THE WENT GREEN. INSPECTED THE RIGHT FORWARD DOOR, AFT DOOR AND SENSORS FOR OPERATION AND SECURITY. ADJUSTED THE RIGHT FORWARD DOOR ACTUATOR ROD END AND SENSOR TARGET. REMOVED AND REPALCED PROXIMITY SWITCH ELECTRONIC UNIT. (W)
Part: SEQUENCE VLV — FAILED (NLG)
FLT 3214 - SBY TO BWI - AFTER TAKEOFF, UPON GEAR RETRACTION, THE NOSE GEAR DOOR AMBER LIGHT REMAINED ON. THE GEAR WAS CYCLED DOWN AND THE RED NOSE UNSAFE LIGHT REMAINED ON AFTER MAIN GEAR GREEN LIGHTS CAME ON. CYCLED GEAR AGAIN AND LIGHTS REMAINED ON. AIRCRAFT TURNED BACK TO SBY AND LANDED WITHOUT INCIDENT. INSPECTED NOSE GEAR COMPONENTS FOR CONDITION AND SECURITY. PERFORMED SEVERAL GEAR SWINGS AND REMOVED AND REPLACED THE SOLENOID SEQUENCE VALVE AS A PRECAUTION. (W)