N138LN

EUROCOPTER DEUTSCHLAND GMBH EC 135 P2+ · 2004 · Rotorcraft · 2 engines · 7 seats · Valid Registration

Registered owner: AIR METHODS LLC, CO (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
Air Methods Corp. (QMLA)Certificate holderMatched by certificate designator

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.

3 reports on file, 2011-06-14 – 2023-09-25.

OTHER; FLT CONT AFFECTED · 2023-09-25 Matched by certificate designator
ATA 3100

Part: TACHOMETER — FAULTED (INSTRUMENT PANEL) · airframe 7,450 hrs · 24,100 cycles

TRIPLE TACH FAILURE IN FLIGHT. ROTOR NEEDLE SWUNG FULL DEFLECTION AND BACK TO ZERO MULTIPLE TIMES. NO CHANGE IN ROTOR STABILIZATION. NO ASSOCIATED WARNINGS OR AUDIBLE TONES.

Source: SDR QMLA2023092520076
WARNING INDICATION · 2023-09-19 Matched by certificate designator
ATA 3100

Part: TACHOMETER — UNKNOWN (UNKNOWN) · airframe 7,432 hrs · 24,059 cycles

IN CRUISE FLIGHT AROUND 18 MINUTE AWAY FROM SYRACUSE, I RECEIVED A ROTOR RPM LOW AURAL ALERT AND CONFIRMED THAT BOTH MY NR AND #2 ENGINE N2 WERE BLEEDING QUICKLY TO ZERO. NO CHANGE IN AIRCRAFT PERFORMANCE, SOUND, OR HANDLING CHARACTERISTICS. I LOWERED THE COLLECTIVE, CHOSE A SAFE PLACE TO LAND AND CHOSE TO KEEP THE AIRCRAFT AT AN ATTITUDE THAT WOULD ALLOW MY NR TO BE HIGH JUST IN CASE MY ASSESMENT OF THE SITUATION WAS INCORRECT. UPON MECHANIC RESPONDING TO SCENE AND SOME MENIAL MAINTENANCE WE PERFORMED TESTING ON TRIPLE TACH PER THE REQUIRED MANUAL AND IT TESTED FINE. PERFORMED NORMAL GROUND RUN AND TESTED AIRCRAFT AGAIN. NO ISSUES. RETURNED TO SERVICE AND FLEW BACK TO BASE.

Source: SDR QMLA2023092120074
OTHER · 2011-06-14 Matched by certificate designator
ATA 6210

Part: BLADE — CRACKED (MAIN ROTOR) · airframe 3,063 hrs

(4) CRACKS IN MAIN ROTOR BLADE UPPER SKIN AT BLADE STATION 75" APPROX 3" LONG, T/E AT BLADE STATION 78" APPROX .5" AND (2) IN INBD TRIM TAB AT BLADE STATION 152" APPROX .5" EA.

Source: SDR QMLDMR0281