N844KH
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.
7 reports on file, 2011-09-20 – 2013-09-23.
Part: SKIN — CORRODED (FUSELAGE) · airframe 38,743 hrs · 41,854 cycles
DURING CHECK, CORROSION FOUND ON FUSELAGE SKIN, FORWARD AND BELOW RT SIDE WINDOW.
Part: SKIN — CORRODED (BS 434) · airframe 38,473 hrs · 41,372 cycles
DURING ROUTINE VISUAL INSPECTION, CORROSION DAMAGE FOUND ON FUSELAGE SKIN LOCATED AT BS 435, SL1504. DAMAGE LENGTH IS 1.375", WIDTH IS .5", AND DEPTH IS .02".
Part: ENGINE — SURGES · airframe 38,022 hrs · 40,588 cycles
ACFT HAD A LOW SPEED TAKEOFF ABORT (LESS THAN 80 KNOTS) DUE TO ENGINE SURGE.
Part: GENERATOR — FAILED (NR 1) · airframe 37,821 hrs · 40,304 cycles
LT AC GENERATOR LIGHT ILLUMINATED AT TAKEOFF. ACFT ABORTED AND RETURNED TO GATE.
Part: ACCUMULATOR — LEAKING (HYD SYSTEM) · airframe 37,594 hrs · 39,928 cycles
AFTER COMPLETION OF ENGINE TREND MONITORING, HYD CAUTION LIGHT ILLUMINATED ON CENTRAL WARNING PANEL. BOTH MAIN AND EMERGENCY ACCUMULATOR PRESSURE LOW. AUTO FUNCTION DID NOT WORK. EMERGENCY DECLARED. ACFT RETURNED TO AIRPORT WITH NO FURTHER INCIDENT. R & R EMERGENCY ACCUMULATOR IAW AMM 29-10-20-04 AND ENGINEERING CHANGE ORDER. OPS AND LEAK CHECK GOOD.
Part: LOCK RING — BROKEN (MLG ROLLER GUIDE) · airframe 37,532 hrs · 39,855 cycles
LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION AFTER TAKEOFF. FLIGHT RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. REPLACED BROKEN ROLLER GUIDE LOCK RING ON LT MLG INBD AND OTBD ROLLER GUIDE SWITCH. ADJUSTED/TESTED LANDING GEARS (EXTENSION AND RETRACTION) IAW AMM 32-30-00. OPS CHECK NORMAL. RII ACCOMPLISHED FOR LANDING GEAR EXTENSION AND RETRACTION.
Part: RIB — CRACKED (RT WING TE FLAP) · airframe 37,465 hrs · 39,784 cycles
DURING A ROUTINE INSPECTION IAW JOB CARD 0600-541-01I, A CRACK HAS BEEN FOUND IN THE LOWER BEND RADIUS OF THE RT FLAP RIB NR5 LOCATED APPROX AT STA WS202.