N397LG
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.
32 reports on file, 2000-09-14 – 2018-11-10.
Part: FLOAT SWITCH — FAILED (FUEL TANK) · airframe 8,901 hrs · 36,964 cycles
UPON LANDING, THE "FUEL" CAUTION ILLUMINATED WITH 51 GALLONS INDICATED. THE MECHANIC ARRIVED AND DETERMINED THAT THE LOW FUEL FLOAT SWITCH WAS THE SOURCE OF THE FAILURE. THIS AIRCRAFT REMAINS OOS AT THIS TIME TO REPLACE THIS SWITCH AS WELL AS PERFORM OTHER SCHEDULED MAINTENANCE TASKS.
Part: BRAKE ASSY — DAMAGED (MAIN ROTOR) · airframe 8,866 hrs · 36,842 cycles
UPON DISASSEMBLY OF ROTOR BRAKE. BRAKE ASSEMBLY DRIVE FLANGE AND HYDRAULIC DRIVE COUPLING HAD EXTREME HEAT DAMAGE AND METAL TRANSFER. THE DAMAGE CONTAINED TO THESE ITEMS PARTS WERE ORDERED AND REPLACED GROUND RUN MOC CHECKS COMPLETED AND AIRCRAFT RETURNED TO SERVICE. RE: AIRCRAFT SYSTEM MALFUNCTION / COMPONENT FAILURE.
Earlier reports · 2000–2012 · 30 reports
2012
Part: BATTERY BOX — CRACKED (TAIL BOOM) · airframe 5,977 hrs
DURING 200 HOUR ICA INSPECTION OF THE TAILBOOM MOUNTED BATTERY, FOUND A CRACK APPROX 1.5 INCHES IN LENGTH IN BATTERY TRAY SUPPORT.
Part: STRUCTURE — CHAFED (TAIL BOOM) · airframe 5,978 hrs · 1 cycles
THE NEGATIVE BATTERY CABLE WAS FOUND TO HAVE RUBBED THE (INSIDE) TAIL BOOM BEYOND LIMITS.
2011
Part: SEARCH LIGHT — MALFUNCTIONED · airframe 5,628 hrs
THE LEFT SEARCHLIGHT WILL NOT SHUT OFF. THIS HAS BEEN A RECURRING EVENT FOR THIS PARTICULAR HELICOPTER OVER THE PAST 3 MONTHS. THERE HAS BEEN 3 SEARCHLIGHTS REPLACED. THE TEAR DOWN REPORTS STATE THAT A SOLID STATE RELAY HAS BEEN REPLACED TO RETURN THE LIGHT TO SERVICEABILITY EACH TIME. THIS IS NOT THE ONLY ACFT EXPERIENCING THESE PROBLEMS. 2 OTHER ACFT WITHIN THE SAME REGION HAVE EXPERIENCED THIS SAME DISCREPANCY RECENTLY.
2008
Part: CANISTER — FULL (FUEL PURGE) · airframe 4,202 hrs
AFTER DEPARTURE FROM BASE HOSPITAL AND ENROUTE TO SENDING HOSPITAL, PILOT NOTICED A PERSISTENT FUEL ODOR IN THE CABIN. THE PILOT THEN ABORTED THE MISSION AND RETURNED TO BASE MAINTENANCE HELIPAD. TROUBLESHOT THE PROBLEM. FOUND THE FUEL PURGE CANISTER FULL OF FUEL, THE MECHANIC DRAINED THE CANISTER. CONDUCTED OPERATIONAL CHECK FLIGHT AND RETURNED AIRCRAFT TO SERVICE.
2002
Part: BLEED VALVE — FAILED (ENGINE)
BLEED VALVE INOPERATIVE. WILL NOT CLOSE. REPLACED WITH USED UNIT CORRECTED PROBLEM.
2001
Part: EXCITER — INOPERATIVE (IGNITION SYS)
IGNITION EXCITER HE 931, UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: IGNITER — INOPERATIVE (IGNITION SYS)
IGNITER, UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: PRESSURE SWITCH — FAILED (FUEL SYS)
LOW FUEL PRESSURE SWITCH, UNIT INOPERATIVE. FAILED TEST. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: LINER — WORN (BALL JOINT)
TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT CORRECTED PROBLEM.
Part: POWER SUPPLY — INOPERATIVE (EXTERIOR LIGHTS)
POWER SUPPLY BOX, UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: SWITCH — FAILED (STARTER)
SWITCH IS INOPERATIVE. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M)
Part: CLOCK — INOPERATIVE (INSTRUMENT PANEL)
CLOCK IS INOPERATIVE. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M)
Part: DISPLAY — INOPERATIVE (COCKPIT)
VEMD (ASTAR AFTER 3018) INTERMITTENT SCREEN 2 INOPERATIVE. REPLACED WITH NEW UNITS, CORRECTED PROBLEM.
Part: VALVE — INOPERATIVE (ENGINE)
COMPLETE VALVE ASSEMBLY, UNIT INOPERATIVE. HAS DELAYED SHUT-DOWN. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: INDICATOR — INOPERATIVE (COCKPIT)
UNIT INOPERATIVE. GYRO WILL NOT CAGE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: TURBINE WHEEL — RATCHETING (ENGINE)
EXCESSIVE RUBBING CAUSING MR TO RACHET. REPLACED WITH RENTAL UNIT, CORRECTED PROBLEM.
Part: FMU — LEAKING (FUEL CONTROL)
LEAKING FUEL FROM DRIVE DRAIN. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: TUBE — CRACKED (AIR OIL VENT) · airframe 193 hrs
CRACKED BEYOND SERVICABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: CLOCK — INOPERATIVE (COCKPIT) · airframe 193 hrs
UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: ALTIMETER — INOPERATIVE (COCKPIT) · airframe 175 hrs
UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: DISPLAY — INOPERATIVE (COCKPIT) · airframe 163 hrs
UNIT INOPERATIVE. WILL NOT TRANSFER INFORMATION BETWEEN SCREENS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
2000
Part: TURBINE — STUCK (ENGINE)
PT WHEEL STICKS. REPLACED WITH NEW UNIT.CORRECTED PROBLEM.
Part: ENGINE — FAILED (NR 1) · airframe 148 hrs
N1 LOCKUP. REPLACED WITH RENTAL ENGINE. CORRECTED PROBLEM.
Part: VENT LINE — CRACKED (OIL SYSTEM) · airframe 102 hrs
TUBE, AIR VENT - OIL, CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: STARTER GEN — INOPERATIVE (ENGINE) · airframe 102 hrs
STARTER/GENERATOR UNIT INOPERATIVE. BRUSH SPRING BROKE RESULTING IN FAN DAMAGE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: LINE — WORN (P2) · airframe 102 hrs
P2 HOSE WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: COUPLING — WORN (P2 LINE) · airframe 102 hrs
P2 UNION WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: SUPPORT BRACKET — WORN (ROTOR BRAKE) · airframe 102 hrs
BRAKE LINING SUPPORT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: LIGHT — SHORTED (SEARCH LIGHT)
SEARCH LIGHT ASSEMBLY (SX-5) HAD INTERNAL SHORT. WILL NOT LIGHT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: DISPLAY — INOPERATIVE (COCKPIT)
UNIT INOPERATIVE. BRIGHTNESS FAILURE CODE ON NEARLY ALL LIGHTS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)