N916HA
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.
10 reports on file, 1995-04-06 – 2002-03-29.
Part: FRAME — CORRODED
DuringC-check found correded frame leg @X510 from STR30S to STR32S. The damage was repaired per EO8-53-02-0366. This EO replaces frame segment form existing factory splice at STR33 to STR29S.
Part: WIRE — BROKEN (CABIN) · airframe 38,375 hrs · 44,165 cycles
FIRST TWO FLOOR LEVEL EMERGENCY LIGHTS WERE INOP. FOUND BROKEN WIRE UNDER FLOOR AT ROW 1. REPAIRED WIRE.
Part: CONTROL BOX — MALFUNCTIONED (COCKPIT) · airframe 37,206 hrs · 42,945 cycles
ON TAXI OUT THE EMERGENCY LIGHTS FLICKERED ON. REPLACED THE EMERGENCY LIGHTS CONTROL BOX.
Part: SPRING — BROKEN (MLG DOOR) · airframe 35,059 hrs · 40,617 cycles
NR 1 MLG FWD DOOR ALTERNATE EXTENSION ASSIST SPRING WAS FOUND BROKEN DURING ROUTINE MAINTENANCE. REPLACED THE SPRING.
Part: SWITCH — INOPERATIVE (NR 2 NACELLE)
NR 2 HYD ISO VALVE CAUTION LIGHT FLICKERED IN FLIGHT. THE LIGHT ILLUMINATED STEADILY AFTER ATTEMPTED GEAR EXTENSION. GEAR WOULD NOT EXTEND. CREW PERFORMED ALTERNATE GEAR EXTENSION. FOUND NR 2 HYDRAULIC RESRVOIR LOW LEVEL SWITCH INOP. REPLACED SWITCH.
Part: SIGN — LOOSE (ROW 4DF)
EMERGENCY LIGHT SIGN AT 4D-F KNOCKED OFF. RESECURED SIGN.
Part: POWER SUPPLY — INOPERATIVE (CABIN)
LEFT HAND FUSELAGE EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY 3351-PS1.
Part: HYDRAULIC LINE — FAILED (NR 1 ENGINE)
FLT 3480 - HHH-CLT - WHILE DESCENDING FOR A CLT ARRIVAL, THE NR 1 HYDRAULIC SYSTEM LOST QTY AND PRESSURE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. INSTALLED A TEMP FLEX LINE FROM THE HYDRAULIC PRESSURE MANIFOLD IN TH NR 1 NACELLE TO THE ANTI-SKID CONTROL VALVE. SERVICED AND BLED SYSTEM. PLACED ON DMT TO REPLACED WITH RIGID LINE. RIGID LINE WAS REPLACED THE NEXT DAY. (M)
Part: HINGE — FAILED (RT MLG DOOR)
FLT 3395 - YYZ-BWI - THE RIGHT MAIN LANDING GEAR DOOR WAS HANGING DOWN IN FLIGHT. THE AIRCRAFT CONTINUED ON TO BWI AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED FORWARD GEAR DOOR AFT HINGE ARM ASSEMBLY AND HARDWARE. PERFORMED EXTENSION AND RETRACTION THROUGH SEVERAL CYCLES. NO DISCREPANCIES NOTED. (M)
Part: ENGINE MOUNT — CRACKED (NR 1 ENG)
DURING 'A' CHECK, A CRACK WAS FOUND IN THE NR 1 ENGINE AFT OUTBOARD ENGINE MOUNT VERTICAL STRUT. REMOVED AND REPLACED NR 1 ENGINE AFT OUTBOARD ENGINE MOUNT VERTICAL STRUT.