- Registered owner
- Alpine Aviation Inc
- Location
- Provo, UT
- Owner type
- Corporation
- Serial number
- U-216
- Year built
- 1983
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- November 15, 1991
- Certificate issued
- April 8, 2004
- Expires
- February 28, 2030
- Mode S code
- A1D00F
From the FAA registry file of October 21, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney PT6A model are included below.
On this page
Airworthiness directives that may apply · 52
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1968 | 1 |
|---|---|
| 1969 | 1 |
| 1970 | 1 |
| 1971 | 5 |
| 1972 | 2 |
| 1975 | 1 |
| 1977 | 1 |
| 1978 | 2 |
| 1980 | 2 |
| 1983 | 1 |
| 1985 | 1 |
| 1986 | 1 |
| 1987 | 1 |
| 1989 | 1 |
| 1990 | 2 |
| 1992 | 4 |
| 1994 | 1 |
| 1995 | 1 |
| 1996 | 1 |
| 1997 | 2 |
| 1998 | 1 |
| 2001 | 2 |
| 2002 | 1 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 4 |
| 2006 | 1 |
| 2011 | 2 |
| 2012 | 1 |
| 2014 | 2 |
| 2015 | 1 |
| 2016 | 1 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 1 |
See all 56 ADs
Information bulletins that may apply · 8
Advisory, not mandatory.
NTSB investigations · 3
Matched to this aircraft by N-number and event date.
NTSB CEN17LA123Accident · No injuriesLimited investigationFinal reportDurango, COThe pilot's inability to maintain directional control during takeoff in crosswind conditions on a contaminated runway, which resulted in a runway excursion.NTSB ANC96LA076Accident · Minor injuriesLimited investigationFinal reportBarrow, AKan in-flight collision with a bird.NTSB ANC92LA123Accident · No injuriesLimited investigationFinal reportNuiqsut, AKThe pilot's improper inflight planning/preparation, and his failure to attain the proper touchdown point. Contributing to the accident was the downdraft.
FAA incident reports · 3
FAA accident and incident reports matched to this aircraft by N-number and event date.
Incident 20170123001549ITakeoff: Departure Roll · Durango, COOn January 23, 2017 N216CS departed the left side of the runway during takeoff from runway 21 in Durango, CO. This was a result of the PIC failing to maintain control of the aircraft during the takeoff roll on the contaminated runway. Prior to the incident…Accident 19960521031429ANormal Cruise · Barrow, AKStruck a duck cruising 800 AGL broke right side winshield and hit first officer. Treated for facial abrasions.Accident 19920808029679AFinal Approach · Nuiqsut, AKStruck raised lip of runway landing short collapsing all three main gears. Blamed severe downdraft on short final.
Service difficulty reports · 12
SDR TIMA20240108003Unknown · unknownDEPARTED THIS MORNING AS 5042 FOR KOLF. NO RUNWAY NOTAM, SO I CONTACTED CLINT AND HE SAID 1 INCH DRY SNOW. UPON ARRIVING TO OLF FOUND 2 INCH DRY SNOW OVER ICE, POOR BRAKING ACTION. LANDED AND SHUTDOWN UNEVENTFULLY. IN THE EVENING OPERATED AS 5041. I PREFLIGHTESDR TIMA20230224002None · noneSTARTED TRAINING FLIGHT, DID TRIM RUNAWAY, STEEP TURNS, CRUISE STALL, APPROACH TO LAND STALL. ON APPROACH TO LAND STALL RECOVERY, NOSE GEAR INDICATOR STAYED GREEN, BOTH MAIN INDICATORS WENT OUT BUT IN TRANSIT RED HANDLE LIGHT STAYED ON. RECYCLED GEAR AFTER 2 MSDR TIMA20230125001Wire · brokenAFTER DEPARTING SLC WHILE PILOT SMELLED BURNING ELECTRICAL FUMES DURING THE CLIMB TO 10,000 MSL. HE TURNED OFF THE NON-ESSENTIAL ELECTRONIC AND RAN THE EMERGENCY CHECKLIST FOR ELECTRICAL FIRES. THIS DID NOT PRODUCE ANY CHANGE SO HE CANCELLED THE FLIGHT AND RETSDR TIMA20220108009Generator · inoperativeLEFT BOTH STARTERS ON AFTER START UP ( FLEW A B MODEL FOR 2 WEEKS AND GOT USED TO THE NON
LOCKING TOGGLE SWITCH), COUPLE MINUTES AFTER TAKE OFF I NOTICED THE GENERATOR FAIL.
TOLD SLC I WAS RETURNING AND LOST POWER. MADE THE DECISION TO FLY INTO KPVU. MADE ATSDR TIMA20140723012Escape Hatch · unsecurePILOT FAILED TO ENSURE THAT THE PILOT HATCH WAS FULLY LATCHED PRIOR TO TAKEOFF. DURING CRUISE THE PILOT HATCH CAME OPEN IMPACTING THE UPPER FUSELAGE & THEN DEPARTED THE ACFT. ACFT CONTROL WAS NEVER COMPROMISED. ACFT LANDED WITHOUT FURTHER INCIDENT.SDR TIMA20140205003Rib · crackedINSPECTION REVEALED 3 CRACKS IN THE LT ELEVATOR OTBD LE RIB. THE CRACKED RIB WAS R & R WITH A NEW RIB.SDR TIMA20120111001Structure · crackedA CRACK WAS DISCOVERED IN THE HORIZONTAL STABILIZER UPPER CENTER TEE EXTRUSION AT THE AFT EDGE. EXTRUSION WAS REPAIRED BY INSTALLING A FILLER AND A DOUBLER IN ACCORADANCE WITH BEECHCRAFT FIELD REPAIR FR-CO-01905.SDR TIMA2010000013Support · crackedLEFT TORQUE TUBE ASSY SUPPORT CRACKED.SDR TIMA20080005Fitting · missingLANDING GEAR FAILED TO EXTEND WHEN SELECTED. GEAR WAS PUMPED DOWN AND AIRCRAFT LANDED WITHOUT INCIDENT. INVESTIGATION REVEALED THAT THE C-CLIP ON THE HYDRAULIC POWERPACK COUPLING WAS MISSING AND ALLOWED THE COUPLING TO MIGRATE ON THE SHAFT UNTIL IT NO LONGERSDR TIM2002F00011Circuit Board · burnedPN 993641581, A PRINTED CIRCUIT BOARD ASSEMBLY INSTALLED IN A TIME DELAY ASSEMBLY. THE ASSEMBLY IS PART OF THE HYDRAULIC SYSTEM AND IS IN THE LOW LIQUID LEVEL SENSOR CIRCUIT. A CHECK OF THE ELECTRICAL SYSTEM FOUND NO DEFECTS IN THE SYSTEM. THE CAUSE OF THE SDR TIMAP53Powerpack · inoperativeLANDING GEAR POWER PACK FAILED. INSPECTION OF THE POWER PACK REVELED MOTOR SHORTED, CAUSED BY INTERNAL LEAK IN THE POWER PACK. CREW LOWERED GEAR MANUALLY.SDR 20000331SH014Actuator · crackedHYDRAULIC FLUID FOUND IN WHEELWELL DURING POST-FLIGHT INSPECTION. LANDING GEAR RETRACTION PERFORMED, FOUND 2 INCH CRACK AROUND TOP OF ACTUATOR. ACTUATOR OVERHAULED. (X)