N917HA
Registered owner: DEPT OF HOMELAND SECURITY, DC (owner ≠ operator)
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.
18 reports on file, 1995-11-20 – 2002-12-09.
Part: PACKING — LEAKING (#2 NACELLE) · airframe 41,603 hrs · 47,905 cycles
9 DEC. 2002FUEL DRIPPING OUT OF GEAR WELL ABOVE CONTACTOR BOX #2 NACELLE. WIGGINS FITTING FWD OF NACELLE FIRE SEAL WAS FOUND LEAKING. REPLACED O-RINGS PN AS3209-218 LEAK CHECK GOOD.10 DEC. 2002FUEL COMING OUT OF DRAIN ON INBD SIDE OF #2 NACELLE. FOUND LEAK AT REFUEL/DEFUEL T FITTING IN #2 NACELLE LEAKING AT BOTTOM. REPLACED O-RINGS PN AS3209-220, LEAK CHECK GOOD.
Part: BATTERY — DISCHARGED (CABIN) · airframe 41,123 hrs · 47,412 cycles
CENTER ISLE EXIT SIGN WHITE DOWN LIGHT AND RIGHT HAND AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY AND POWER SUPPLY.
Part: BATTERY — DISCHARGED (CABIN) · airframe 40,756 hrs · 46,991 cycles
TWO OF THE FOUR RED EMERGENCY FLOOR LIGHT FORWARD END ARE INOP. REMOVED AND REPLACED EMERGENCY BATTERY 3352 PS1.
Part: HYDRAULIC SYSTEM — MALFUNCTIONED (NR 1) · airframe 40,179 hrs · 46,360 cycles
DURING SINGLE ENGINE TAXI, CREW REPORTED LOST NR 1 STANDBY HYDRAULIC SYSTEM PRESSURE AND THE USE OF THE NORMAL BRAKE SYSTEM. CREW USED THE PARKING BRAKE TO STOP THE A/C. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY.
Earlier reports · 1995–2001 · 14 reports
2001
Part: PUMP — MALFUNCTIONED (NR 1 ENGINE) · airframe 38,892 hrs · 44,859 cycles
DURING SINGLE ENGINE TAXI, NR 2 AC GENERATOR ON LINE, NR 1 STANDBY HYDRAULIC PUMP FAILED CAUSING LOSS OF NR 1 HYDRAULIC PRESSURE. RECYCLED NR 2 AC GENERATOR, NR 1 STANDBY HYDRAULIC PUMP RETURNED TO NORMAL. INSPECTED BRAKES AND HYDRAULIC SYSTEM, NO LEAKS NOTED. STARTED AND TAXIED AIRCRAFT AROUND AIRPORT, COULD NOT DUPLICATE.
Part: COMPUTER — FAILED (COCKPIT) · airframe 37,391 hrs · 43,356 cycles
IN FLIGHT, NR 2 AHRS FLAGGED AND GOR ELECTRICAL SMELL IN COCKPIT AND CABIN. REPLACED 2 AHRS UNIT.
1999
Part: LIGHT — INOP (CABIN)
FLOOR EMERGENCY LIGHT 5TH LIGHT AFT IS INOP. REMOVED AND REPLACEDD LIGHT ASSY.
1998
Part: POWER SUPPLY — INOPERATIVE (EQUIP PANEL)
SBY - FLT 3200 - PASSENGER EXIT SIGN AT BOARDING DOOR INOP. REMOVED AND REPLACED POWER SUPPLY 3351 PS1. OPS CHECK GOOD. (M)
Part: VALVE — LEAKING (NR 1 NACELLE)
CRW/CLT - FLT 3342 - DURING DESCENT, NR 1 HYDRAULIC ISOLATE AND ROLL SPOILER INBD HYDRAULIC CAUTION LIGHTS ILLUMINATED WITH REDUCED NR 1 HYDRAULIC SYSTEM QUANTITY. PERFORMED ZERO FLAP LANDING WITH NO NORMAL WHEEL BRAKES. REMOVED AND REPLACED NR 1 ANTI-SKID CONTROL VALVE. LEAK AND OPS CHECK GOOD. (X)
Part: DOOR — OUT OF ADJUST (NLG)
CLT/EWN - FLT 3284 - AFTER GEAR UP SELECTION, NOSE GEAR DOORS OPENED. CYCLED GEAR, NOSE GEAR DOORS OPENED AGAIN. AIR TURNBACK TO CLT. ADJUSTED NOSE GEAR DOORS, ACTUATOR END ONE TURN OUT. CYCLED GEAR, OPS CHECK GOOD. (X)
Part: VALVE — FAILED (NLG WW)
CLT/HHH - FLT 3172 - AFTER GEAR RETRACTION, NOSE GEAR DOOR AMBER LIGHT CAME ON. CREW CYCLED GEAR AND LIGHT ON AGAIN. AIR TURNBACK TO CLT. REMOVED AND REPLACED SOLENOID SEQUENCE VALVE, OPS CHECKED GOOD. (X)
1997
Part: CLUTCH SPRING — FAILED (AILERON CONTROLS)
FLT EN69 - BWI-ORF - EXPERIENCED A ROLL CONTROL DISCONNECT ON LANDING, AFTER TOUCHDOWN AT ORF. REMOVED AND REPLACED THE ROLL CONTROL DISCONNECT CLUTCH BUSHINGS PER FCD8-27-291. ALSO, REMOVED AND REPLACED THE CLUTCH SPRING. (M)
Part: BUSHINGS — FAILED (AILERON CONTROLS)
FLT EN69 - BWI-ORF - EXPERIENCED A ROLL CONTROL DISCONNECT ON LANDING, AFTER TOUCHDOWN AT ORF. REMOVED AND REPLACED THE ROLL CONTROL DISCONNECT CLUTCH BUSHINGS PER FCD8-27-291. ALSO, REMOVED AND REPLACED THE CLUTCH SPRING. (M)
Part: BUSHING — MISSING (LT MLG DOOR)
FLT 3393 - YYZ-BWI - THE LEFT GEAR DOOR WAS OPEN IN FLIGHT WITH NO ADVISORY LIGHT ON, DID NOT CLOSE UPON GEAR UP SELECTION. THE AIRCRAFT CONTINUED TO BWI AND LANDED WITHOUT INCIDENT. INSTALLED HARDWARE ON FORWARD DOOR AFT CONNECTING ROD ASSEMBLY. (M)
Part: BOLT — MISSING (LT MLG DOOR)
FLT 3393 - YYZ-BWI - THE LEFT GEAR DOOR WAS OPEN IN FLIGHT WITH NO ADVISORY LIGHT ON, DID NOT CLOSE UPON GEAR UP SELECTION. THE AIRCRAFT CONTINUED TO BWI AND LANDED WITHOUT INCIDENT. INSTALLED HARDWARE ON FORWARD DOOR AFT CONNECTING ROD ASSEMBLY. REF HNAA9791702.
Part: BUSHING — MISSING (LT MLG DOOR)
FLT 3393 - YYZ-BWI - THE LEFT GEAR DOOR WAS OPEN IN FLIGHT WITH NO ADVISORY LIGHT ON, DID NOT CLOSE UPON GEAR UP SELECTION. THE AIRCRAFT CONTINUED TO BWI AND LANDED WITHOUT INCIDENT. INSTALLED HARDWARE ON FORWARD DOOR AFT CONNECTING ROD ASSEMBLY. REF HNAA9791702.
1996
Part: ENGINE — FAILED (NR 1)
FLT NR 3461 - MIA-MCO - ON CLIMB-OUT, THE NR 1 ENGINE LOW OIL PRESSURE WARNING LIGHT CAME ON, PRESSURE DECREASED, AND THE CREW SHUT THE ENGINE DOWN. THE AIRCRAFT TURNED BACK TO MIA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 1 ENGINE. (M)
1995
Part: SPRING — BROKEN (STAY STRUT ACT)
FLT NR 3162 - DCA-ISP - AFTER GEAR DOWN SELECTION, DURING APPROACH, THE LEFT GEAR UNSAFE LIGHT ILLUMINATED AND STAYED ON. AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED IN ISP WITHOUT INCIDENT. REMOVED AND REPLACED THE STAY STRUT OUTBOARD SPRING. (M)