N135MF
Registered owner: ZMOG MANAGEMENT COMPANY LLC, CA (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.
21 reports on file, 2004-01-13 – 2012-03-23.
Part: COMBUSTION LINER — CRACKED (NR 2 ENGINE) · airframe 4,981 hrs · 13,463 cycles
DURING INSPECTION OF ENGINE, FOUND THE COMBUSTION LINER CRACKED. REPLACING THE COMBUSTION LINER.
Part: BLADE — CRACKED (MAIN ROTOR) · airframe 4,981 hrs · 13,463 cycles
DURING INSPECTION OF THE MAIN ROTOR BLADES, FOUND 3 OF THEM WITH 45 DEGREE CRACKS 1.9 METERS OTBD OF THE BLADE BOLT.
Earlier reports · 2004–2011 · 19 reports
2011
Part: BLADE — CRACKED (MAIN ROTOR) · airframe 4,959 hrs · 13,402 cycles
THE MECHANIC FOUND A CRACK IN A MAIN ROTOR BLADE WHILE PERFORMING AN AIRWORTHINESS INSP OF THE ACFT. THE BLADE IS CRACKED 73" FROM THE BLADE CUFF TO THE T/E. THE CRACK EXTENDS FORWARD AT A 45 DEGREE ANGLE APPROX 6" IN LENGTH. MFG HAS ISSUED ASB EC135-62A-014 WHICH PERTAINS TO THIS MRB CRACK. THE ACFT IS CURRENTLY OOS AWAITING A REPLACEMENT BLADE.
2007
Part: FUEL CONTROL — INOPERATIVE (NR 1 ENGINE) · airframe 2,470 hrs · 6,370 cycles
DURING AN 800 HOUR INSPECTION, FOUND NR 1 ENGINE FUEL DEGRADE LIGHT WOULD NOT ILLUMINATE WHEN ENGINE PUT IN MANUAL MODE AND TWIST GRIP WAS ENGAGED. REMOVED AND REPLACED FCU 3 TIMES BEFORE TEST WOULD PASS. FUEL CONTROL P/N 0319858090 S/N ANR855, P/N 0319858240 S/N 578B BOTH FAILED THE FUNCTIONAL TEST. INSTALLED P/N 031985820 S/N 658B AND PROBLEM WAS CURED.
2004
Part: CABLE — DISCONNECTED (BALL BEARING CON) · airframe 400 hrs
WARRANTY. CABLE UNWEDGED FROM AFT CABLE. REPLACED WITH SERVICABLE UNIT. 04/07/2004
Part: IGNITER — UNSERVICEABLE (ENGINE) · airframe 400 hrs
WARRANTY. ELECTRODE GONE IN UNIT. REPLACED WITH SERVICEABLE ASSET UNIT. 04/26/2004
Part: INJECTOR — CLOGGED (ENGINE) · airframe 400 hrs
INJECTOR REMOVED DUE TO SUSPECTED CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004
Part: HOUSING — BROKEN (T/R CONTROL)
THE TAIL ROTOR/ ANTI-TORQUE BALL BEARING CONTROL SYSTEM CONTROL CABLE HOUSING BROKE AND SEPARATED FROM THE ACTUATOR HOUSING NEAR THE AFT SUPPORT ON THE TAIL BOOM. THIS DISCREPANCY WAS FOUND DURING A SCHEDULED INSPECTION.
Part: MANIFOLD — CLOGGED (RT INJECTOR) · airframe 400 hrs
UNIT REMOVED DUE TO SUSPECT CLOGGING, RETURNED TO TEC BY TONY N, WITHOUT NOTIFICATION. HARCARD WAS ENCLOSED. REPLACED WITH SERVICABLE UNIT. 04/01/2004
Part: MANIFOLD — CLOGGED (RT INJECTION) · airframe 400 hrs
UNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004
Part: INJECTOR — CLOGGED (PREFERENCE INJEC) · airframe 400 hrs
UNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004
Part: MANIFOLD — CLOGGED (LT FUEL INJECTOR) · airframe 400 hrs
UNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004
Part: MANIFOLD — CLOGGED (LT INJECTION) · airframe 400 hrs
UNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004
Part: MASTER SWITCH — FAILED (MAIN) · airframe 367 hrs
FAILED SEVERAL TIMES ON AIRCRAFT. HARDCARD ENCLOSED. REPLACED WITH SERVICABLE UNIT. 03/09/2004
Part: MOUNT — LEAKING (M/R GEARBOX) · airframe 359 hrs
UNIT LEAKING AND FAILED. REPLACEMENT UNIT SENT. REPLACED WITH SERVICABLE UNIT. 03/08/2004
Part: RADIO — INOPERATIVE (FM SYSTEM) · airframe 351 hrs
FM RADIO CHANNELS ARE FROZEN, WILL NOT CHANGE OR TRANSMIT. TFM-550 CAME FACTORY INSTALLED ON NEW EC135 ROTORWING AIRCRAFT PURCHASE FROM EUROCOPTER. REPLACED WITH SERVICABLE UNIT.
Part: WINDOW — CRACKED (COCKPIT) · airframe 285 hrs
WINDOW CRACKED NEAR BOTTEM LT CORNER. REPLACED WITH SERVICABLE UNIT. 02/11/2004
Part: MOUNT — LEAKING (M/R GEARBOX) · airframe 268 hrs
MAIN ROTOR GEARBOX MOUNT LEAKING. REPLACED WITH SERVICEABLE UNIT. 01/16/2004
Part: MOUNT — LEAKING (M/R GEARBOX) · airframe 267 hrs
MAIN ROTOR GEARBOX MOUNT LEAKING. REPLACED WITH SERVICEABLE UNIT. 01/16/2004
Part: MOUNT — LEAKING (M/R GEARBOX) · airframe 267 hrs
Z-ARIS MOUNT LEAKING AFTER 267.8 HOURS REPLACED WITH SERVICEABLE UNIT.
Part: MOUNT — LEAKING (M/R GEARBOX) · airframe 268 hrs
Z-ARIS MOUNT IS LEAKING AFTER 267.8 HOURS. REPLACED WITH SERVICEABLE UNIT.