N924HA
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.
25 reports on file, 1995-02-10 – 2002-02-26.
Part: PCU — MALFUNCTIONED (NR 1 PROPELLER) · airframe 36,862 hrs · 41,832 cycles
DURING TAKEOFF AFTER V1 NR 1 PROP RPM DROPPED TO 1188 FOR 5 SECONDS. REPLACED PROP CONTROL UNIT.
Part: VALVE — MALFUNCTIONED · airframe 36,584 hrs · 41,540 cycles
Oil temp on number 1 engine clombed to 110 degrees on climb-out, temp stayed in yellow ark for less than 10 minutes. Removed and replaced oil temp regulator valve.
Earlier reports · 1995–2000 · 23 reports
2000
Part: HOSE — RUPTURED (NR 1 MLG) · airframe 33,357 hrs · 38,136 cycles
DURING TAXI OUT, NUMBER 2 ISO VALVE, ROLL SPOILER OUTBOARD AND NOSE WHEEL STEERING CAUTION LIGHTS ILLUMINATED. NUMBER 2 HYDRAULIC QUANTITY DROPPED TO 1.5 QUARTS.
Part: BRACKET — CRACKED (LT WING) · airframe 32,691 hrs · 37,415 cycles
FOUND TWO CRACKS IN THE LOWER LEG OF THE LT AILERON INPUT QUADRANT BRACKET AT STATION YW417.9. REPAIRED BRACKET IAW EO8-57-00-687.
1999
Part: CABLE — LOOSE (PAX DOOR)
PAX DOOR WILL NOT OPEN. FOUND LOWER CABLE OFF PULLEY. REPOSITIONED CABLE ON PULLEY, OPS CHECK GOOD.
Part: PCU — MALFUNCTIONED (NR 2 ENGINE)
NR 2 ENG EXCEEDED 135 PERCENT TQ FOR LESS THEN 10 SEC. REMOVED AND REPLACED PROP, PCU, HMU, TSCU AND TQ PROB. INSPECTED OIL FILTERS AND BORESCOPED ENGINE.
Part: HOSE — LEAKING (NR 2 HYD SYST)
LOSS OF NR 2 HYDRAULIC QUANTITY AND PRESSURE AFTER TAKEOFF (LEAK FROM NOSE GEAR AREA). REPLACED NOSE GEAR DRAG STRUT ACTUATOR HOSE ASSEMBLY. INSPECTED ENGINE DRIVEN PUMP PER MM PROCEDURE 05-50-33. NO CONTAMINATION FOUND IN CASE DRAIN FILTER. GROUND RAN AIRCRAFT IAW PROCEDURE. RUNUP AND LEAK CHECK GOOD.
1998
Part: WINDSHIELD — ARCED (COCKPIT)
PHL - FLT 3038 - CAPTAINS WINDSHIELD ARCS AT WINDSHIELD HEAT CONNECTIONS. OPERATED PER MEL 30-10. (M)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
CHO - FLT 3251 - FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED 3352-PS1 AND 3352-PS2 BATTERY POWER SUPPLIES AND BASE ASSEMBLIES. POWER SUPPLIES P/N OFF 61-0479-1X S/N SBY106 AND ORF61. POWER SUPPLY BASE P/N OFF NSN7 AND PS207. (M)
1997
Part: BATTERY — DISCHARGED (CABIN)
CHO/PHL - FLT 3201 - DURING PRE-FLIGHT CHECKS, FOUND THE AFT CEILING OVERHEAD EMERGENCY LIGHT AND LEFT HAND AFT EXTERIOR EGRESS LIGHTS INOPERABLE. REMOVED AND REPLACED 3351-PS3 EMERGENCY BATTERY. (X)
Part: BATTERY — DISCHARGED (CABIN)
TRI/CLT - FLT 3417 - DURING PRE-FLIGHT CHECKS, SEVERAL EMERGENCY LIGHTS WERE FOUND INOPERABLE IN THE CABIN. REMOVED AND REPLACED THE EMERGENCY BATTERY AND POWER SUPPLY. REF: OPERATOR CONTROL NR 98ZZZX2202. X)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
TRI/CLT - FLT 3417 - DURING PRE-FLIGHT CHECKS, SEVERAL EMERGENCY LIGHTS WERE FOUND INOPERABLE IN THE CABIN. REMOVED AND REPLACED THE EMERGENCY BATTERY AND POWER SUPPLY. REF: OPERATOR CONTROL NR HNAA9792400.
Part: ANGLE — CRACKED (NLG WW)
FOUND DURING PHASE CHECK, THE RIGHT OUTER NOSE LANDING GEAR WELL ANGLE WAS CRACKED AT THE SIDEWALL. REMOVED AND REPLACED THE ANGLE IAW ESR8-53-93-11. (M)
Part: STATOR — FAILED (TURBINE SECTION)
ENGINE S/N 120314 FAILED ON TAKEOFF. PT1 STATOR BROKE LOOSE AND FELL BACK INTO THE PT1 DISC, CUTTING THE PT BLADE UNTIL COMPLETE FAILURE OF BLADES. REFERENCE HNAA 9792427.
Part: ENGINE — FAILED (NR 1)
FLT 3319 - CLT-PHF - AFTER TAKEOFF, A LOUD BANG CAME FROM THE NR 1 ENGINE. ALL INDICATIONS WERE NORMAL DURING SHUTDOWN. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 1 ENGINE. (M)
1996
Part: SELECTOR VALVE — FAILED (LANDING GEAR)
FLT 3444 - TLH - TPA - ON APPROACH INTO TPA, THE LANDING GEAR WAS SELECTED DOWN, NO RESPONSE. THREE RED LIGHTS AND HANDLE LIGHT ILLUMINATED. THE CREW CYCLED THE GEAR HANDLE AND THE GEAR CAME DOWN. AIRCRAFT LANDED IN TPA WITHOUT INCIDENT. REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE. (M)
Part: WIRE — LOOSE (CABIN)
FLT NR 3184 - SBY-PHL - DURING PREFLGIHT CHECKS, FOUND THE RIGHT FORWARD EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED POWER SUPPLY 3351-PS2, NO FIX. MAINTENANCE FOUND WIRES NOT SEATED IN MATRIX BLOCK. RESEATED WIRES, OPS CHECK GOOD. (M)
Part: SELECTOR VLV — FAILED (LANDING GEAR)
FLT NR 3260 - HPN-BWI - ON APPROACH INTO BWI, THE LANDING GEAR WOULD NOT EXTEND WHEN SELECTED DOWN. LOWERED GEAR USING ALTERNATE SYSTEM AND LANDED IN BWI WITHOUT INCIDENT. REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE. (M)
Part: BATTERY — DISCHARGED (CABIN)
FLT NR 3040 - FLL-TPA - DURING PREFLIGHT WALKAROUND, FOUND DS3 AND DS4 FLOOR PROX EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BASE AND BATTERY. REFERENCE HNAA9692417
Part: BASE — FAILED (CABIN)
FLT NR 3040 - FLL-TPA - DURING PREFLIGHT WALKAROUND, FOUND DS3 AND DS4 FLOOR PROX EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BASE AND BATTERY. (M)
Part: ACTUATOR — FAILED (RT MLG DOOR)
FLT NR 3046 - FLL-TPA - AFTER TAKEOFF AND GEAR RETRACTION, THE RIGHT GEAR DOOR CAUTION LIGHT STAYED ILLUMINATED. THE DOOR CLOSED, BUT THE LIGHT REMAINED ON THE AIRCRAFT CONTINUED ON TO TPA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE RIGHT FORWARD GEAR DOOR ACTUATOR. (M)
1995
Part: CONTROL UNIT — FAILED (NR 1 ENGINE)
BWI/RDU - FLT 3393 - THE AUTOFEATHER WOULD NOT ARM ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 1 TORQUE SENSOR CONTROL UNIT. (X)
Part: SENSOR — FAILED (NLG)
CLT/CHA - FLT 3204 - THE NOSE GEAR CYCLED SEVERAL TIMES IN GEAR WELL IN CRUISE. THE INTRANSIT AND HANDLE LIGHTS CYCLED ON AND OFF. THE AIRCRAFT CONTINUED ON TO CHA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NOSE LANDING GEAR DRAG STRUT SENSOR.
Part: EEL — FAILED (CABIN)
FLT 3111 - LYH-DCA - DURING PREFLIGHT WALKAROUND, FOUND FIRST TWO EMERGENCY LIGHTS AT ROW 1 BURNED OUT. CLEANED CONNECTOR 3352-PS3, OPERATIONAL CHECK GOOD. (W)
Part: BRAKE SYST — REQD SERVICE (MLG)
PHF-PHL - FLT 3091 - AFTER LANDING ROLLOUT, CREW REPORTED MOMENTARY LOSS OF BRAKES WHEN TURNING. FOUND AIR IN BRAKE SYSTEM, BLED AS REQUIRED.