- Registered owner
- Alpine Aviation Inc
- Location
- Provo, UT
- Owner type
- Corporation
- Serial number
- U-104
- Year built
- 1969
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- June 30, 1970
- Certificate issued
- February 14, 2011
- Expires
- February 28, 2030
- Mode S code
- AC66F6
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 44
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 | 2 |
| 1979 | 1 |
| 1980 | 1 |
| 1982 | 3 |
| 1983 | 1 |
| 1985 | 1 |
| 1987 | 1 |
| 1988 | 1 |
| 1989 | 1 |
| 1990 | 2 |
| 1992 | 3 |
| 1995 | 1 |
| 1996 | 3 |
| 1997 | 2 |
| 1998 | 1 |
| 2001 | 1 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 2 |
| 2021 | 1 |
| 2023 | 1 |
See all 46 ADs
Information bulletins that may apply · 3
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N899CAMatched 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 99A aircraft
FAA incident reports · 3
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20051104027169INormal Cruise · Great Falls, MT(-23) On 11/04/05, alpine aviation inc., d/b/a alpine air, enroute from fca to bil with the pilot onboard, at 13,000 ft. started developing right engine problems. The pilot first noticed that the right engine torque indicator was fluctuating and then the oil…Incident 19910411013689IForced/Precautionary Landing · Syracuse, NYNR2 engine oil presssure light on. Shut engine down and returned. Wire broken off at cannon plug at oil transmitterIncident 19900509024779IOther Ground Ops · Syracuse, NYAircraft tipped down on tail when unloading passengers.
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR TIMA20221003012None · noneWE WERE SCHEDULED FOR AN AIRCRAFT SWAP IN KBTM. I TOOK OFF OUT OF KRXE AT 10AM ON OUR IFR FLIGHT PLAN. ON THE WAY INTO KBTM WE ENCOUNTED SOME WEATHER, WE DID THE ILS 15 INTO KBTM. INBOUND ON THE ILS WE PUT THE GEAR DOWN AND NOTICED WE DIDN'T HAVE THE RIGHT GEASDR TIMA201808220001Handle · shortedWITH LANDING GEAR HANDLE SELECTED DOWN, NO GREEN DOWN AND LOCKED INDICATION ALONG WITH RED HANDLE WARNING. PILOT NOTED LANDING GEAR CIRCUIT BREAKER TRIPPED. RESET THE CIRCUIT BREAKER WHICH RESULTED IN NORMAL OPERATION. INVESTIGATION FOUND LANDING GEAR SELECSDR TIMA20161128016Circuit Breaker · defectiveAFTER TAKEOFF THE LANDING GEAR FAILED TO RETRACT. LANDING GEAR CB WAS POPPED. PILOT ELECTED TO RETURN TO THE AIRFIELD AND LANDED UNEVENTFULLY. SUBSEQUENT INVESTIGATION FOUND THE LANDING GEAR REMOTE CIRCUIT BREAKER HAD VERY HIGH RESISTANCE IN THE CLOSED POSISDR TIMA20151111007Flasher · faultyGEAR IN TRANSIT WARNING STAYED ON AFTER GEAR SELECTED UP, FOLLOWING TAKEOFF. PILOT RETURNED TO TAKEOFF AIRFIELD FOR UNEVENTFUL LANDING. SUBSEQUENT INSPECTION DETERMINED ALL GEAR FUNCTIONS WERE NORMAL. ERRONEOUS IN TRANSIT WARNING DETERMINED TO BE CAUSED BY SDR TIMA20120608009Skin · crackedA CRACK WAS DISCOVERED IN THE UPPER WING SKIN OUTBOARD OF THE NACELLE AND AFT OF THE MAIN WING SPAR ON THE RIGHT WING. REMOVED THE DAMAGED SECTION OF SKIN. FABRICATED A NEW SECTION OF SKIN USING THE SAME TYPE MATERIAL AND THICKNESS AND INSTALLED USING A SPLISDR TIMA20110006Cam · damagedWHEN THE PILOT SELECTED GEAR UP AFTER DEPARTURE FROM BIL, THE GREEN LIGHTS EXTINGUISHED BUT THE RED IN-TRANSIT LIGHT DID NOT EXTINGUISHED. EXTENDED THE GEAR AND GOT 3 GREEN, RETRACTED THEM AGAIN AND STILL HAD THE IN TRANSIT LIGHT STAY ON. AT THIS POINT RETURSDR TIMR20070008Switch · inoperativeGEAR-IN-TRANSIT LIGHT DID NOT EXTINGUISH AFTER TAKE-OFF AND GEAR UP. PILOT CYCLED GEAR AGAIN WITH SAME RESULT. PILOT RETURNED TO DEPARTURE AND LANDED. MECHANIC FOUND THAT THE LT POWER LEVER SWITCH HAD FAILED. REPLACING THE SWITCH RESOLVED THE PROBLEM.SDR TIM2005F00013Engine · failedAIRCRAFT IN FLIGHT AT 13000 FT OIL PRESSURE AND TORQUE STARTS TO FLUCTUATED SLIGHTLY, MOMENTS LATER THE ENGINE FAILED. NO CAUSE FOR FAILURE HAS BEEN FOUND AT THIS TIME. THE ENGINE HAS BEEN TAGGED. THE ENGINE HAS 87.5 HOURS SINCE REPAIRS TO THE ENGINE AT AN SDR TIM2002F00006Collar · crackedDURING AN INSPECTION OF THE ELEVATOR, IT WAS FOUND THAT THE OUTBOARD ELEVATOR COLLAR WAS CRACKED AT THE TAPER PIN. THE DEFECTIVE TORQUE TUBE WAS REPLACED AND THE NEW TUBE (SERVICEABLE) WAS RIGGED IAW MM. INSPECTION OF THE CRACKED COLLAR WAS INCONCLUSIVE AS TSDR 20010320CW009Mount · chafedIT WAS DISCOVERED DURING AN ENGINE CHANGE, THAT THE TUBE MOUNT HAD CHAFE MARKS BEYOND LIMITS. THE TUBE MOUNT WAS REPLACED WITH A SERVICABLE TUBE MOUNT. THE CAUSE OF THE CHAFING WAS DUE TO INDEQUATE CLEARANCE BETWEEN MOUNT AND BAFFLING AND FUEL LINES.SDR 20001019SH029Case · crackedDURING PROPELLER CHANGE ON LEFT ENGINE, A SERIES OF CRACKS WERE FOUND ON THE INBOARD EXHAUST FLANGE. THE FLANGE IS A PART OF THE POWER SECTION, SO FIELD REPAIR WAS NOT POSSIBLE. THE AFFECTED POWER SECTION WAS REPLACED WITH A SERVICEABLE POWER SECTION. A POSSDR 99ZZZX2516Rod · corrodedSHIMMY DAMPENER ROD WAS FOUND TO HAVE CORROSION INSIDE AND OUT CAUSING FLUID TO LEAK BY THE O-RINGS. CORROSION SEEMS TO BE FROM NORMAL OPERATION. ROD WAS REPLACED.
STCs that may be installed · 147
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech 99A
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