N101LN

No registry detail on file · not in current registry

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.

FALSE WARNING · 2011-09-14 Matched by certificate designator
ATA 2697

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.

Source: SDR QMLA2011091411095
SMOKE/FUMES/ODORS/SPARKS · 2011-07-16 Matched by certificate designator
ATA 2110

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.

Source: SDR QMLA2011071611079
ELECT. POWER LOSS-50 PC · 2011-04-13 Matched by certificate designator
ATA 2400

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.

Source: SDR QMLA2011041311046
Earlier reports · 1998–2010 · 13 reports

2010

FLT CONT AFFECTED · 2010-03-01 Matched by certificate designator
ATA 6710

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.

Source: SDR QMLA2010030110005

2000

OTHER · 2000-09-01 Unresolved
ATA 6240

Part: INDICATOR — INOPERATIVE (TACHOMETER) · airframe 851 hrs

TACHOMETER UNIT INOPERATIVE. NTL NEEDLE VIBRATED EXCESSIVELY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)

Source: SDR 20001214SH035
NO TEST · 2000-08-20 Unresolved
ATA 3340

Part: POWER UNIT — INOPERATIVE (STROBE)

UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Source: SDR R7MR32625
OTHER · 2000-05-01 Unresolved
ATA 6720

Part: ROD — WORN (BEARING)

ROD, PITCH CONTROL WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)

Source: SDR 20000801SH019
OTHER · 2000-04-05 Unresolved
ATA 6520

Part: BEARING — WORN (T/R ROD END)

ROD END WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)

Source: SDR 20000605SH009
OTHER · 2000-03-30 Unresolved
ATA 6220

Part: BALL JOINT — WORN (STARFLEX)

STARFLEX BALL JOINT - TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)

Source: SDR 20000605SH010

1999

OTHER · 1999-12-17 Unresolved
ATA 6220

Part: BEARING — WORN (STARFLEX)

TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)

Source: SDR 20000424SH016
OTHER · 1999-12-17 Unresolved
ATA 6410

Part: BEARING — WORN (TAIL ROTOR)

ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)

Source: SDR 20000424SH015
ELECT. POWER LOSS-50 PC; WARNING INDICATION · 1999-10-22 Unresolved
ATA 2435

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.

Source: SDR 99ZZZX4514
OTHER · 1999-09-08 Unresolved
ATA 7532

Part: BLEED VALVE — INOPERATIVE (ENGINE)

BLEED VALVE INOPERATIVE. CLOSES AT 98 PERCENT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Source: SDR 99ZZZX4167
OTHER · 1999-08-15 Unresolved
ATA 2840

Part: SWITCH — INTERMITTENT (FUEL PRESSURE)

FUEL PRESSURE SWITCH OPERATES INTERMITTENTLY. FLICKERS IN-FLIGHT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Source: SDR 99ZZZX4166
OTHER · 1999-06-30 Unresolved
ATA 6410

Part: HINGE — WORN (TAIL ROTOR)

ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WIT NEW UNIT, CORRECTED PROBLEM.

Source: SDR 99ZZZX3794

1998

OTHER · 1998-10-01 Unresolved
ATA 6240

Part: INDICATOR — STICKING (COCKPIT)

INDICATOR NEEDLE STICKS. TAPPING INDICATOR WILL FREE NEEDLE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.

Source: SDR 98ZZZX4100