N881TW
Registered owner: HINTERLAND HOLDINGS LLC, AK (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.
8 reports on file, 1999-03-16 – 2009-12-22.
Part: FLAP — MALFUNCTIONED (WING) · airframe 5,847 hrs · 2,423 cycles
ON FLIGHT FROM CMH TO SUA CREW OBSERVED A "FLAP FAIL" MESSAGE AT APPROX FLAP 20 DEGREE. CREW ELECTED TO DIVERT TO PBI FOR LONGER RUNWAY. MAINTENANCE WAS ABLE TO CLEAR SQUAWK BY RESETTING SYSTEM. FLAP SYSTEM OPERATING NORMAL.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 5,847 hrs · 2,423 cycles
ON FLIGHT FROM CMH TO SUA CREW OBSERVED A "FLAP FAIL" MESSAGE AT APPROX FLAP 20 DEGREE. CREW ELECTED TO DIVERT TO PBI FOR LONGER RUNWAY. MAINTENANCE WAS ABLE TO CLEAR SQUAWK BY RESETTING SYSTEM. FLAP SYSTEM OPERATING NORMAL.
Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 5,824 hrs · 3,414 cycles
IN CRUISE PILOTS WINDSHIELD CRACKED JUST RT OF CTR LINE FROM BOTTOM TO THE TOP OF THE PANE. DIVERTED FOR INSPECTION. MX INSPECTED AND APPLIED TAPE IAW CH56-10-01. MEL'D THE WINDSHIELD HEAT. CONTINUED ON.
Part: UNKNOWN — ODOR (CABIN) · airframe 4,504 hrs · 3,705 cycles
SMELLED STRONG ODOR AFTER TAKEOFF. RETURN TO BLOCK. SMELL WENT AWAY BY THE TIME AIRCRAFT LANDED. COULD NOT DUPLICATE WITH GROUND RUN.
Part: TUBE — CHAFED (HYD SYSTEM)
PRESSURE LINE FROM NR 1 ENGINE DRIVEN PUMP CHAFED AT AFTMOST CLAMP LOCATION (NEAR NR 1 SYSTEM RESERVOIR) UNTIL THE LINE FAILED UNDER PRESSURE CAUSING A COMPLETE LOSS OF NR 1 HYDRAULIC SYSTEM IN FLIGHT. CLAMP CUSHION FAILED CAUSING METAL TO METAL CONTACT. SUSPECT THAT DEFECT WAS NOT READILY VISIBLE BEFORE FAILURE. (K)
Part: VALVE — INOPERATIVE (NLG)
PILOT NOTED UNUSUAL NOISE AFTER GEAR RETRACTION FOLLOWED BY A NOSE GEAR DOOR VISUAL AND AURAL WARNING. CYCLED GEAR DOWN AND HAD 3 GREEN DOWN AND LOCKED INDICATION. NOSE GEAR DOOR REMAINED OPEN. PILOT ELECTED TO LAND FOR MAINTENANCE. MAINTENANCE WAS ABLE TO DUPLICATE PROBLEM WITH AIRCRAFT ON JACKS.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 3,781 hrs · 2,225 cycles
COPILOT WINDSHIELD CRACKED OUTER PLY.
Part: VALVE — FAILED (AUX FUEL CELL)
RIGHT AUXILIARY FUEL SHUT-OFF VALVE FAILED IN OPEN POSITION CAUSING FUEL IMBALANCE.