- Registered owner
- Alpine Aviation Inc
- Location
- Provo, UT
- Owner type
- Corporation
- Serial number
- UE-60
- Year built
- 1993
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, commuter
- Airworthiness date
- September 3, 1993
- Certificate issued
- September 15, 2008
- Expires
- May 31, 2028
- Mode S code
- A7C602
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 54
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1994 | 1 |
|---|---|
| 1995 | 4 |
| 1996 | 5 |
| 1997 | 10 |
| 1998 | 5 |
| 1999 | 8 |
| 2000 | 2 |
| 2001 | 5 |
| 2002 | 1 |
| 2003 | 5 |
| 2004 | 3 |
| 2005 | 2 |
| 2006 | 2 |
| 2008 | 1 |
| 2009 | 2 |
| 2011 | 1 |
| 2012 | 1 |
| 2014 | 2 |
| 2023 | 1 |
| 2024 | 1 |
See all 62 ADs
Information bulletins that may apply · 6
Advisory, not mandatory.
Airframe · Beech 1900D
SAIB 2026-02Elevator Tab Control SystemSAIB CE-12-36Flight Controls: AileronSAIB CE-05-83SAIB CE-00-24SAIB CE-00-15Engine · Pratt & Whitney Canada PT6A-67D
SAIB NE-15-21Fuel Injector NozzleNTSB investigations
No NTSB investigations matched to N60MJMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Beech 1900D aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR TIMA20200609002Control Rod · brokenDURING 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.SDR A8OA2014F00087Annunciator · no indicationLT ENGINE AFX, AUTOFEATHER, ANNUNCIATOR DID NOT ILLUMINATE AT TAKEOFF POWER.SDR A8OA201207100001Pcb · failedNR 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.SDR NSVA20070214Actuator · malfunctionedAIRCRAFT 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. PERFOSDR NSVA20070095Switch · malfunctionedFLAPS 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.SDR NSVA20070036Shutoff Valve · inoperativeFOUND 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.SDR NSVA200600237Switch · out of adjustFOUND 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.SDR 12062005ACowling · looseLT 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.SDR 11042005ACircuit Breaker · trippedGEAR WOULD NOT COME UP AFTER TAKEOFF. RESET LANDING GEAR CONTROL CIRCUIT BREAKER. CYCLED LANDING GEAR FOUR TIMES, OPS CHECK GOOD.SDR 09212005CSwitch · failedDUAL 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.SDR 09152005BSwitch · failedLT 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.SDR 09132005AGround Wire · looseFLAP 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.SDR 09082005DGovernor · failedRT 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.SDR 06272005Eadi · failedBURNING ODOR PRESENT AND NR 1 EADI FLASHING ON AND OFF.
Reports on N60MJ not matched to an aircraft · 1
They name N60MJ, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
STCs that may be installed · 186
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 186 STCs
Earlier aircraft with this N-number · 1
This aircraft carried N60MJ before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.