N101LN
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.
16 reports on file, 1998-10-01 – 2011-09-14.
Part: CONNECTOR — LOOSE (FIRE DETECTOR) · airframe 4,295 hrs · 15,782 cycles
IN CRUISE, DURING FERRY FLIGHT FIRE LIGHT ILLUMINATED. STARTED AUTHORITATIVE TYPE DECENT DOING NOTHING WITH FUEL CONTROL. ONCE IN DECENT LOOKED OVER THE REST OF THE INSTRUMENTS AND EVERYTHING LOOKED NORMAL. DID SLIGHT S TURN TO SEE IF I WAS TRAILING ANY SMOKE WHICH WAS NOT THE CASE. DECIDED TO KEEP POWER ON FOR LANDING. LANDING UNEVENTFUL. SHUTDOWN ACFT AND EXITED DOING A WALK AROUND TO FIND NO VISIBLE DAMAGE OR ANY INDICATION OF FIRE. TROUBLESHOOTING OF THE FIRE DETECTION SYS REVEALED A LOOSE CRIMP-TYPE CONNECTER ON THE FORWARD LOWER LT FIRE DETECTOR ELECTRICAL CONNECTION. CONNECTOR APPEARED TO BE FAIRLY NEW, BUT HAD NOT BEEN SUFFICIENTLY CRIMPED TO PROVIDE A SECURE CONNECTION. RE-CRIMPED THE CONNECTOR SECURELY, DOCUMENTED MX ON LOF LEAF 705490, THEN APPROVED THE ACFT FOR RETURN TO SERVICE/COMPLETION OF FERRY FLIGHT.
Part: BELT — SPLIT (AIR COMPRESSOR) · airframe 4,235 hrs
ON CLIMBOUT AFTER TAKEOFF, AIR CONDITIONER WAS TURNED ON. AIR CONDITIONER DID NOT BLOW COLD AIR AND ODOR OF BURNING RUBBER WAS DETECTED IN CABIN. AIR CONDITIONER WAS SWITCHED OFF, TAKEOFF WAS ABORTED AND ACFT LANDED BACK AT DEPARTURE POINT. VISUAL INSP AFTER LANDING, REVEALED THAT THERE WAS NO FIRE AND THAT THE AIR CONDITIONER BELT WAS SHREDDED.
Part: UNKNOWN — MULTIPLE FAIL · airframe 4,181 hrs
DURING FLIGHT, PILOT REPORTED THE ACFT ENCOUNTERED AN INTERMITTENT ELECTRICAL MALFUNCTION. NO CAUTION OR WARNING LIGHT ILLUMINATED. AT APPROX 10MIN INTO THE FLIGHT ALL RADIOS AND MOST SYS AND NAVIGATION INSTRUMENTS FAILED. ROTOR AND N2 REMAINED IN THE NORMAL OPERATING RANGE. ACFT MADE A PRECAUTIONARY LANDING. MECHANIC ARRIVED TO TROUBLESHOOT SYS TO FIGURE OUT THE CAUSE. AT THAT TIME, CHECKED THE MAIN ACFT BATTERY FOR PROPER CONNECTION. CHECKED OK. CHECKED WIRES ON THE STARTER GENERATOR, CHECKED OK. CHECKED THE MAIN WIRE GOING INTO THE AVIONICS BUSS BAR, IT TOO, CHECKED OK. CHECK ALL SWITCHES ON THE CENTER CONSOLE FOR PROPER OPERATION GEN., MASTER DISCONNECT AVIONICS SWITCH. BATTERY SWITCH, INSPECTED THE PP6 CARD UNDER THE SWITCH PANEL. ALL CHECKED OK. AT THIS TIME ELECTED TO START THE ACFT WITH AUX CART, ACFT STARTED NORMAL. AT THIS TIME THE GENERATOR WAS SWITCHED TO THE ON POSITION AND ALL ACFT SYS OPERATED NORMALLY. RAN THE ACFT FOR 15 MIN TO CHARGE UP ACFT BATTERY, THEN SHUTDOWN AND RESTARTED THE ACFT IN NORMAL CONFIGURATION. ACFT STARTED FINE, RAN IT AGAIN FOR10 MIN THEN SHUTDOWN AND SIGNED OFF AS ALL SYS ARE NORMAL COULD NOT DUPLICATE PROBLEM.
Earlier reports · 1998–2010 · 13 reports
2010
Part: ROD — BENT (CYCLIC STICK) · airframe 3,884 hrs · 14,410 cycles
THE PILOTS FELT STIFFNESS IN THE FWD QUADRANT OF THE CYCLIC DURING TAKEOFF. TAKEOFF WAS ABORTED LEFT ACFT RUNNING, CHECK FOR BINDING OF THE SERVOS, NONE FOUND. ACFT SHUTDOWN, BELLY PANEL REMOVED FLIGHT CONTROLS WERE INSP AND FOUND BENT PUSH PULL TUBE. NO OTHER PUSH PULL TUBE HAS SIGNS OF VISIBLE DAMAGE, NO OTHER PUSH PULL TUBE OR CONTROL SO SIGNS OF BEING JAMMED. CAN NOT FIND ANY DIRECT OR INDIRECT CAUSE OF THE DAMAGE.
2000
Part: INDICATOR — INOPERATIVE (TACHOMETER) · airframe 851 hrs
TACHOMETER UNIT INOPERATIVE. NTL NEEDLE VIBRATED EXCESSIVELY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: POWER UNIT — INOPERATIVE (STROBE)
UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: ROD — WORN (BEARING)
ROD, PITCH CONTROL WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: BEARING — WORN (T/R ROD END)
ROD END WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: BALL JOINT — WORN (STARFLEX)
STARFLEX BALL JOINT - TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
1999
Part: BEARING — WORN (STARFLEX)
TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: BEARING — WORN (TAIL ROTOR)
ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: BRUSHES — WORN (STARTER/GEN)
IN CRUISE, FUEL BOOST PUMP LIGHT ILLUMINATED WITH CORRESPONDING DROP IN FUEL PRESSURE. LIGHTS AND RADIOS THEN BEGAN FAILING. AS THE LIGHTS WERE DIMMING, FIRE WARNING LIGHT ILLUMINATED. THE AIRCRAFT LANDED AT AIRPORT WITHOUT FURTHER INCIDENT. GENERATOR FAIL LIGHT DID NOT ILLUMINATE. THE STARTER/GENERATOR BRUSHES WERE REPLACED AND A FUNCTIONAL TEST OF THE STARTER/GENERATOR SYSTEM WAS SATISFACTORILY PERFORMED.
Part: BLEED VALVE — INOPERATIVE (ENGINE)
BLEED VALVE INOPERATIVE. CLOSES AT 98 PERCENT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: SWITCH — INTERMITTENT (FUEL PRESSURE)
FUEL PRESSURE SWITCH OPERATES INTERMITTENTLY. FLICKERS IN-FLIGHT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: HINGE — WORN (TAIL ROTOR)
ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WIT NEW UNIT, CORRECTED PROBLEM.
1998
Part: INDICATOR — STICKING (COCKPIT)
INDICATOR NEEDLE STICKS. TAPPING INDICATOR WILL FREE NEEDLE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.