Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Jan 2017)2 ADs may apply12 service difficulty reports
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Individual owners are shown by city and state only.
The pilot's inability to maintain directional control during takeoff in crosswind conditions on a contaminated runway, which resulted in a runway excursion.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN17LA123)
THE PILOT'S IMPROPER INFLIGHT PLANNING/PREPARATION, AND HIS FAILURE TO ATTAIN THE PROPER TOUCHDOWN POINT. CONTRIBUTING TO THE ACCIDENT WAS THE DOWNDRAFT.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC92LA123)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2004-17-02 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series Airplanes | Oct 4, 2004 | Airframe (C-99)Certain serial numbers: 65-A90, B90, C90, C90A LJ-76; 65-A90, B90, C90, C90A LJ-114–LJ-1691; E90 LW-1–LW-347; F90 LA-2–LA-236; 99, 99A, A99A, B99, C99 U-1–U-239; 100, A100 B-1–B-94; … |
| 97-25-03 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series Airplanes | Jan 21, 1998 | Airframe (C-99) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
DEPARTED 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 PREFLIGHTED AND VISUALLY INSPECTED BOTH TIRES…
From FAA Service Difficulty Reports; matched by N-number and serial number.STARTED 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 MINS TO SEE IF IT WOULD GO UP OR DOWN.…
From FAA Service Difficulty Reports; matched by N-number and serial number.AFTER 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 RETRUNED TO KSLC IMMEDIATELY.
From FAA Service Difficulty Reports; matched by N-number and serial number.LEFT 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 ATTEMPTS TO CALL SLC AND PVU TOWER BUT I…
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT 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.
From FAA Service Difficulty Reports; matched by N-number and serial number.INSPECTION REVEALED 3 CRACKS IN THE LT ELEVATOR OTBD LE RIB. THE CRACKED RIB WAS R & R WITH A NEW RIB.
From FAA Service Difficulty Reports; matched by N-number and serial number.A 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.
From FAA Service Difficulty Reports; matched by N-number and serial number.LEFT TORQUE TUBE ASSY SUPPORT CRACKED.
From FAA Service Difficulty Reports; matched by N-number and serial number.LANDING 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 LONGER CONNECTED THE MOTOR TO THE PUMP.
From FAA Service Difficulty Reports; matched by N-number and serial number.PN 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 MELT DOWN OF THE BOARD IS UNKNOWN.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 12 reports.