N60MJ
Registered owner: ALPINE AVIATION INC, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Alpine Aviation, Inc. (TIMA) | Certificate holder | — | Matched 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.
16 reports on file, 2005-06-24 – 2020-06-09.
Part: CONTROL ROD — BROKEN (RUDDER) · airframe 29,315 hrs · 45,006 cycles
DURING FLIGHT, PILOT EXPERIENCED LOSS OF RUDDER INPUT. LANDED SAFELY IN MOT. MAINTENANCE FOUND THE RUDDER CROSSOVER SHAFT WHICH CONNECTS PILOT WITH CO-PILOT PEDAL CONTROLS BROKEN.
Earlier reports · 2005–2014 · 15 reports
2014
Part: ANNUNCIATOR — NO INDICATION (LT AUTOFEATHER) · airframe 28,122 hrs · 43,494 cycles
LT ENGINE AFX, AUTOFEATHER, ANNUNCIATOR DID NOT ILLUMINATE AT TAKEOFF POWER.
2012
Part: PCB — FAILED (AUTOFEATHER SYS) · airframe 30,541 hrs · 41,667 cycles
NR 1 PROPELLER ATTEMPTED TO FEATHER IN FLIGHT WITH AUTOFEATHER ARMED. TROUBLESHOT AND FOUND 2 BAD DIODES ON PCBA123. REPLACED DEFECTIVE PC BOARD WITH INSPECTED UNIT. OPS CHECKED GOOD. NO FURTHER OCCURRENCES.
2007
Part: ACTUATOR — MALFUNCTIONED (ELEVATOR TRIM) · airframe 23,228 hrs · 35,549 cycles
AIRCRAFT IS PITCHING UP AND DOWN UNCOMMANDED. REQUIRES EXCESSIVE FORCE ON CONTROL WHEEL TO MAINTAIN DESIRED PITCH, EVEN WITH ELECTRIC TRIM DISCONNECTED. REMOVED AND REPLACED ELECTRIC ELEVATOR TRIM TAB ACTUATOR IAW REPS AIRLINER 1900D M/M 27-30-07-201. PERFORMED ELEVATOR ELECTRIC TRIM TAB CABLE RIGGING IAW 27-30-07-201 PAGE 10. PERFORMED ELEVATOR ELECTRIC TRIM OPERATION CHECK PROCEDURE 27-30-09. ALL CHECKS GOOD.
Part: SWITCH — MALFUNCTIONED (FLAP ASYMMETRIC) · airframe 22,650 hrs · 34,688 cycles
FLAPS DID NOT EXTEND TO 35 ON APPROACH AND LANDED FLAPS 17 AND WILL NOT RETRACT. ADJUSTED FLAP SAFETY ASYMMETRIC SWITCH, OPS CHECK GOOD IAW BEECHCRAFT 1900D MM 27-50-06-201.
Part: SHUTOFF VALVE — INOPERATIVE (LT ENGINE) · airframe 22,406 hrs · 34,332 cycles
FOUND LT ENGINE FIREWALL SHUTOFF VALVE IS INOP. REMOVED AND REPLACED LT ENGINE FIREWALL SHUTOFF VALVE PN/OFF/ON 118-389005-1, SN/OFF 9307076 SN/ON9031512, OPS CHECK GOOD.
2006
Part: SWITCH — OUT OF ADJUST (PAX DOOR) · airframe 22,229 hrs · 34,095 cycles
FOUND CABIN DOOR ANNUNCIATOR CAME ON IN FLIGHT. PERFORMED ADJUSTMENT OF AS DOOR TOP DOOR SILL SWITCH IAW MM 57-70-00. PRESSURIZED AIRCRAFT IAW MM 21-30-00, AS DOOR ANNUNCIATOR SYSTEM. OPS CHECK GOOD AT THIS TIME.
Part: FIRE BOTTLE — INOPERATIVE (LEFT) · airframe 21,286 hrs · 32,764 cycles
LEFT T HANDLE ILLUMINATED WHILE TAXING TO THE GATE AFTER LANDING ACTIVATED LEFT FIRE BOTTLE BUT IT FAILED TO DISCHARGE WITH T HANDLE PULLED. REMOVED AND REPLACED LT FIRE BOTTLE IAW SAAB WORK CARD 26-20-05 P/N ON AND OFF 30100023 S/N ON 28764A1 S/N OFF 25307A1.
Part: FIRE LOOP — OUT OF POSITION (LT ENGINE) · airframe 21,282 hrs · 32,764 cycles
LEFT T-HANDLE ILLUMINATED WHILE TAXIING TO GATE. LEFT -T- HANDLE ILLUMINATED WHILE TAXIING TO THE GATE AFTER LANDING ACTIVATED LEFT FIRE BOTTLE BUT IT FAILED TO DISCHARGE WITH -T- HANDLE PULLED. -T- HANDLE ON LT SIDE ILLUMINATED BECAUSE FIRE LOOP WAS TOUCHING THE EXHAUST STACK. REPOSITIONED FIRE LOOP, PERFORMED LT FIRE EXTINGUISHER ACTIVATION CHECK IAW COLGAN W/C 26-20-01, OPS CHECK GOOD. REMOVED & REPLACED LT FIRE BOTTLE IAW SAAB WORK CARD 26-20-05 P/N ON & OFF 30100023, S/N ON 28764A1, S/N OFF 25307A1.
2005
Part: COWLING — LOOSE (LEFT) · airframe 20,358 hrs · 31,490 cycles
LT TOP FWD ENGINE COWL CAME LOOSE IN FLIGHT. REMOVED AND INSPECTED LT TOP FWD ENGINE COWL, NO DEFECTS NOTED. REINSTALLED COWL AND SECURED LATCHES, NO DEFECTS NOTED.
Part: CIRCUIT BREAKER — TRIPPED (MLG) · airframe 20,303 hrs · 31,395 cycles
GEAR WOULD NOT COME UP AFTER TAKEOFF. RESET LANDING GEAR CONTROL CIRCUIT BREAKER. CYCLED LANDING GEAR FOUR TIMES, OPS CHECK GOOD.
Part: SWITCH — FAILED (BLEED AIR) · airframe 20,116 hrs · 31,109 cycles
DUAL ENVIROMENTAL FAIL. T/O ABORTED AT 50 KNOTS. PERFORMED OPS CHECK OF RIGHT TEST VALVE OPS CHECKED GOOD. CLEANED LEFT PNEUMATIC BLEED TEST SWITCH E305WDM, OPS CHECK GOOD.
Part: SWITCH — FAILED (FIRE TEST) · airframe 20,101 hrs · 31,094 cycles
LT ENGINE FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED INTERMITTENTLY THEREAFTER. BOTTLE PRESSURE READS NORMAL. REMOVED AND REPLACED UPPER LT FIRE TEST SWITCH IAW 31-10-00, OPS CHECK GOOD.
Part: GROUND WIRE — LOOSE (FLAP SYSTEM) · airframe 20,084 hrs · 31,073 cycles
FLAP WILL NOT GO DOWN WHEN SELECTED 17 DEGREES. MEL'ED FLAP SYSTEM. C/W MEL ON 9/15/2005 FOUND LOOSE GROUND, RESECURED, OPS CHECK GOOD.
Part: GOVERNOR — FAILED (RT ENGINE) · airframe 20,067 hrs · 31,044 cycles
RT ENGINE FEATHERING DURING T/O. PROP AT 500 RPM AND TQ AT 1000 IN GROUND FINE. REMOVED AND REPLACED RT PROP GOVERNOR, OPS CHECK GOOD.
Part: EADI — FAILED (COCKPIT) · airframe 19,755 hrs · 30,577 cycles
BURNING ODOR PRESENT AND NR 1 EADI FLASHING ON AND OFF.