N44AS
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.
9 reports on file, 2006-08-09 – 2011-03-14.
Part: ACTUATOR — MALFUNCTIONED (ELEVATOR TRIM) · airframe 10,091 hrs · 8,043 cycles
ON CLIMB OUT, PILOT REPORTED ELEVATOR TRIM JAMMED AND WOULD NOT MOVE. PILOT RETURNED ACFT BACK TO DEPARTURE AND DIFFERENT ACFT DEPARTED. MX INSPECTED ACFT AND FOUND ELEVATOR TRIM ACTUATOR WORN AND CHAIN ON ACTUATOR VERY LOOSE AND BINDING WHENEVER TRIM UP WAS SELECTED. CHAIN WOULD RELEASE WHEN DOWN WAS SELECTED AND LOCK UP AGAIN WHEN UP WAS AGAIN SELECTED. MX REPLACED ELEVATOR TRIM ACTUATOR AND PERFOMED ALL OPS CHECKS-ALL CHECKED NORMAL AND ACFT WAS RETURNED TO SERVICE.
Part: FRAME — DAMAGED (ZONE 200) · airframe 9,993 hrs · 7,942 cycles
DURING SCHEDULED MX, INSP NOTED DAMAGE TO A FRAME AT FUSELAGE STA 179.5 AND WATER LINE 107. MX PERFORMED A MAJOR REPAIR BY FABRICATING AND INSTALLING A DOUBLER IAW REPORT NR S-550-0047/07PRD AND SRM, CHAPTER 51.
Part: FRAME — DAMAGED (ZONE 200) · airframe 9,993 hrs · 7,942 cycles
DURING SCHEDULED MX, INSP NOTED DAMAGE TO A FRAME AT FUSELAGE STA 168 AND WATER LINE 121. MX PERFORMED A MAJOR REPAIR BY FABRICATING AND INSTALLING A DOUBLER IAW REPORT NR S-550-0047/07PRD AND SRM CHAP 51.
Part: FRAME — DAMAGED (ZONE 200) · airframe 9,993 hrs · 7,942 cycles
DURING SCHEDULED MX, INSP NOTED DAMAGE TO A FRAME AT FUSELAGE STA 205.23 AND WATER LINE 112. MX PERFORMED A MAJOR REPAIR BY REMOVING DAMAGED AREA AND INSTALLING A NEW SPLICE IAW REPORT S-550-0047/07PRD.
Part: FRAME — DAMAGED (ZONE 200) · airframe 9,993 hrs · 7,942 cycles
DURING SCHEDULED MX, INSP NOTED DAMAGE TO A FRAME AT FUSELAGE STA 180.77 AND WATER LINE 112. MX PERFORMED A MAJOR REPAIR BY REMOVING DAMAGED AREA AND INSTALLING A NEW SPLICE IAW REPORT S-550-0047/07PRD.
Part: SKIN — DAMAGED (LT WING) · airframe 9,064 hrs · 7,105 cycles
PULLED FASTENERS AND CRACK IN LT WING LOWER SKIN.
Part: DOUBLER — GOUGED (RT STUBWING) · airframe 8,743 hrs · 6,871 cycles
A SINGLE GOUGE WAS NOTED IN THE DOUBLER P/N 6511032-18, COMMON TO THE RT STUBWING LOWER SKIN ASSEMBLY.
Part: SKIN — BENT (ZONE 800) · airframe 8,743 hrs · 6,871 cycles
CABIN DOOR SKIN LOWER EDGE IS BENT AND TORN IN SEVERAL AREAS ACROSS THE BOTTOM OF THE DOOR.
Part: WEB — CRACKED (NLG WW) · airframe 8,743 hrs · 6,871 cycles
NOSE LANDING GEAR WHEEL WELL, FOUND WHEEL WELL TOP SKIN CRACKED.