- Registered owner
- Alpine Aviation Inc
- Location
- Provo, UT
- Owner type
- Corporation
- Serial number
- U59
- Year built
- 1969
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- January 26, 1990
- Certificate issued
- August 5, 2011
- Expires
- August 31, 2027
- Mode S code
- A0A17E
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 47
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1971 | 5 |
|---|---|
| 1972 | 3 |
| 1974 | 1 |
| 1975 | 1 |
| 1976 | 1 |
| 1978 | 3 |
| 1979 | 1 |
| 1980 | 1 |
| 1982 | 3 |
| 1983 | 1 |
| 1985 | 1 |
| 1987 | 1 |
| 1988 | 1 |
| 1990 | 2 |
| 1992 | 2 |
| 1995 | 1 |
| 1996 | 3 |
| 1997 | 3 |
| 1998 | 1 |
| 2001 | 1 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 4 |
| 2006 | 2 |
| 2021 | 1 |
| 2023 | 1 |
See all 47 ADs
Information bulletins that may apply · 6
Advisory, not mandatory.
NTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports · 5
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20020426010979INormal Cruise · Billings, MT(-23) On April 26, 2002, tima, flt 5131, en route from gtf to bil, had the rear fairing from the cargo pod depart the aircraft. The flight crew stated they heard a bang approximately 30 miles out descending through 9000 ft. mls into bil. The flight crew…Accident 19940820022259ARoll-Out (Fixed Wing) · Helena, MTLeft main gear collapsed turning off runway on high speed taxiway. Down lock hook missed lockplate. Rigging suspectIncident 19861213083169ILevel Off Touchdown · Bangor, MEDiverted when gear could not be extended for landing. Suspect improper maintenance.Incident 19860210025669IClimb · Manchester, NHLeft engine failed during climb. Diverted. Found internal failure of power section.Incident 19820222005419ITo Aborted (Fixed Wing) · Cedar Rapids, IAAborted takeoff due to power loss on right engine. Right engine power section p t disc blade damaged.
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR TIMA2019090904Switch · intermittentLANDING GEAR DID NOT RETRACT WHEN SELECTED. INSPECTION DETERMINED THAT ONE OF THE ELECTRICAL SWITCHES ON THE SERVICE VALVE WAS INTERMITTANT.SDR TIMA20170413004Relay · failedWHEN LANDING GEAR WAS SELECTED DOWN, THE GEAR FAILED TO EXTEND NORMALLY. LANDING GEAR CIRCUIT BREAKER HAD TRIPPED. MANUAL GEAR EXTENSION PROCEDURE WAS USED. PILOT MADE AN UNEVENTFUL LANDING. INSPECTION REVEALED THAT THE LANDING GEAR MOTOR RELAY HAD HIGH RESDR TIMA20140403009Rib · crackedINSPECTION REVEALED 3 CRACKS IN THE LT ELEVATOR LE RIB. THE RIB WAS REPLACED WITH A NEW RIB.SDR YDA2005F00001Cover · burnedTHE RT ENGINE WAS REPORTED TO BE THROWING SPARKS OUT THE LOWER PORTION OF THE COWL. UPON INVESTIGATION, THE STARTER GEN WAS FOUND TO HAE BURN SPOTS ON THE BRUSH BAND COVER. THE STARTER GEN WAS REMOVED AND A SERVICEABLE STARTER GEN WAS INSTALLED. UPON FURTHESDR TIM2005F00005Fire Detector · contaminatedFIRE DETECTOR GAVE A FALSE FIRE WARNING IN FLIGHT. MOISTURE WAS PROBABLE CAUSE. AFTER TAXI, THE FIRE WARNING LIGHT EXTINGUISHES. NO OTHER PROBLEMS WITH THE SYSTEM. (K)SDR TIM2002F00002Actuator · leakingTHE AIRCRAFT HAD NEEDED INFREQUENT SERVICING OF THE HYD. FLUID RESERVOIR AND YET NO LEAKS HAD BEEN DISCOVERED. SINCE THE AMOUNT OF FLUID ADDED HAD NEVER BEEN AN ALARMING AMOUNT, THE AIRCRAFT HAD ALWAYS BEEN RETURNED TO SERVICE. THE LEAK OF HYD. FLUID WAS DISSDR TIM2002F00003Inlet · burnedDURING A POST INSPECTION CHECK OF AIRCRAFT SYSTEMS, IT WAS DETERMINED THE LEFT ENGINE INLET DEICER WAS INOPERATIVE. A CLOSE INSPECTION OF THE SURFACE OF THE DEICER REVEALED IRREGULAR BULGING AND INDICATORS OF HIGH HEAT. THE DEICER WAS REPLACED AND THE REST OFSDR 2000ZZZX618Latch · wornNOSE BAGGAGE DOOR LATCH CLOSES DOOR, BUT LATCH PIVOT IS WORN ELONGATED. REPLACED LATCH WITH SERVICEABLE LATCH. THE LATCH APPEARS TO HAVE BEEN ON THE AIRCRAFT QUITE A WHILE SO THIS WEAR MAY HAVE BEEN NORMAL. INSPECTION OF OTHER LATCHES REVEALED NOTHING ABNORMSDR 99ZZZX4555Taper Pins · looseINSPECTION OF ELEVATOR TORQUE TUBE REVEALED LOOSE TAPER PINS ATTACHING THE TUBE TO THE COLLAR. ENTIRE TORQUE TUBE ASSEMBLY WAS REPLACED WITH A SERVICEABLE UNIT. THE MM PROVIDES LIMITED CRITERIA FOR RESTORING ORIGINAL SECURITY BETWEEN TUBE AND COLLAR. PERHAPSDR 99ZZZX4703Skin · crackedINSPECTION REVEALED TOP SIDE SKIN OF RIGHT AILERON CRACKED. REPLACED AILERON WITH SERVICEABLE AILERON WHILE ORIGINAL IS REPAIRED. SUBMITTER STATED IT APPEARED THE CRACK MAY HAVE BEEN THE RESULT OF AN IMPROPERLY INSTALLED OR SECURED EXISTING SURFACE DOUBLER. SDR 99ZZZX3914Tire · failedTHE TIRE TREAD CAP SEPARATED FROM TIRE ON NEWLY RECAPPED TIRE, 24 TOTAL CYCLES ON TIRE.SDR 99ZZZX2231Fuel Controller · failedFUEL CONTROLLER FAILED IN-FLIGHT AND DROPPED FUEL PRESSURE TO MIN-FLOW.
STCs that may be installed · 172
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech 99
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller