Safety record in brief:1 NTSB accident (substantial damage, May 2007)2 ADs may apply15 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
The total failure of the nose landing gear actuator and the subsequent nose gear collapse during landing.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for SEA07LA133)
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 (B-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 (B-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.
DURING CLIMB PILOT NOTICED BLUE SMOKE THAT SMELLED ELECTRICAL. HE CALLED IN FOR EMERGENCY LANDING, OPEDED HIS WINDOWS AND VENTS AND RETURNED BACK TO BIL FOR TROUBLE SHOOTING ON THE AIRCRAFT. MX FOUND WIRE FOR NOSE BAG DOOR WARNING SHORTED AND DEACTIVATED CABIN HEATER CIRCUIT LIMITING RESISTER.…
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT SELECTED WINDSHIELD HEAT AND SMOKE EMITTED FROM BEHIND RIGHT PANEL. PILOT SELECTED WINSHIELD HEAT TO OFF FOR REMAINDER OF FLIGHT. MAINTENANCE INSPECTED WINDSHIELD HEAT SYSTEM AND FOUND LOOSE CONNECTION AT CO-PILOT GROUND TERMINAL FOR WINDSHIELD HEAT. TERMINAL WAS REPAIRED AND SYSTEM CHECKED…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING AD 92-15-13 INSPECTION 1 INCH CRACK WAS LOCATED IN THE LT ANGLE AT FS 207.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING CRUISE FLIGHT, THE RIGHT ENGINE DEVELOPED TORQUE FLUCTUATIONS. PILOT NOTED FLUCTUATING OIL PRESSURE READINGS AND AS OIL PRESSURE DROPPED TO ZERO. SHUTDOWN THE RIGHT ENGINE. PILOT MADE AN UNSCHEDULED LANDING. SUBSEQUENT INSPECTION REVEALED SIGNIFICANT OIL LOSS WITH OIL EXITING THE ENGINE AIR…
From FAA Service Difficulty Reports; matched by N-number and serial number.SHORTLY AFTER TAKEOFF, THE BAGGAGE DOOR ANNUNCIATOR ILLUMINATED NECESSITATING A RETURN FOR LANDING TO VERIFY DOORS WERE SECURE. IT WAS DETERMINED THAT THE RT NOSE BAGGAGE DOOR ANNUNCIATOR SWITCH WAS OUT OF ADJUSTMENT.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING APPROACH FOR LANDING, THE RT ENG OIL PRESS BEGAN FLUCTUATING. OIL PRESS DROPPED TO 40 PSI WITH THROTTLE AT IDLE & THE OIL PRESS ANNUNCIATOR ILLUMINATED. RT ENG WAS SHUTDOWN AT 1.5 MILES ON FINAL. ACFT LANDED UNEVENTFULLY. SUBSEQUENT INSPECTION REVEALED A 90 DEGREE FITTING ON THE OIL COOLER…
From FAA Service Difficulty Reports; matched by N-number and serial number.CRACKED FUEL LINE FROM FCU TO STARTER CONTROL UNIT.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING CRUISE, PILOT HEARD A CLUNK AND THE -GEAR IN TRANSIT- LIGHT CAME ON. RETURNED TO AIRPORT, PERFORMED FLY-BY WHICH CONFIRMED NOSE GEAR HANGING OUT BUT NOT FULLY EXTENDED. NOSE GEAR COLLAPSED ON LANDING. INVESTIGATION REVEALED THAT THE ACTUATOR SHAFT HAD SHEARED JUST ABOVE THE CLEVIS BOLT…
From FAA Service Difficulty Reports; matched by N-number and serial number.WHILE INSPECTING THE HORIZONTAL STABILIZER, THE LT SHEAR PLATE WAS FOUND TO HAVE A CRACK RUNNING ACROSS IT. THE ELEVATOR CONTROL HORN IS ATTACHED TO THE SHEAR PLATE WHICH IS ATTACHED TO THE HORIZONTAL STABILATOR. THE CRACK MUST HAVE DEVELOPED UNDER NORMAL CIRCUMSTANCES. DO NOT HAVE AN IDEA FOR THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.FITTING FOUND TO BE CRACKED DURING STRUCTURAL INSPECTION. (CNTRL NR 82)
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 15 reports.