Safety record in brief:1 NTSB accident (substantial damage, Apr 2018)22 ADs may apply31 service difficulty reports
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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.
Failure of the right main landing gear drag brace bolt for reasons that could not be determined based on the available information.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN18LA164)
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 |
|---|---|---|---|
| 2014-02-03 | Flight Controls | Mar 7, 2014 | Airframe (1900C)Certain serial numbers: 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-439 |
| 2013-24-03 | Stabilizers | Jan 13, 2014 | Airframe (1900C)Certain serial numbers: 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-439 |
| 2009-23-03 | Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft… | Dec 14, 2009 | Airframe (1900C)Certain serial numbers: 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-439 |
| 2009-23-01 | Hawker Beechcraft Corporation Model 1900, 1900C, and 1900D Airplanes | Dec 8, 2009 | Airframe (1900C)Certain serial numbers: 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-439. Only with: Equipped with Hawker Beechcraft MLG actuator P/N 114-380041-11, -13, -15, or -15OVH (or FAA-approved equivalent, including Frisby P/N 1FA10043-3). |
| 2006-18-51 | Raytheon Aircraft Company Models 1900, 1900C, and 1900D Airplanes | Sep 8, 2006 | Airframe (1900C)Certain serial numbers: 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-439 |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2005-18-21 | Raytheon Aircraft Company Models 1900, 1900C, 1900C (C-12J), and 1900D Airplanes | Sep 13, 2005 | Airframe (1900C)Certain serial numbers: 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-439 |
| 2004-17-02 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series Airplanes | Oct 4, 2004 | Airframe (1900C)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; … |
| 2004-09-30 | Raytheon Aircraft Company Model 1900C Airplanes | Jun 18, 2004 | Airframe (1900C)Certain serial numbers: 1900C UB-1–UB-35 |
| 2004-09-07 | Raytheon Aircraft Company Model 1900, 1900C, 1900C (C-12J), and 1900D Airplanes | Jun 14, 2004 | Airframe (1900C)Certain serial numbers: 1900 UA-1–UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-113. Only with: Applies to airplanes that do not have canted bulkhead Kit No. 129-4005-1 incorporated. |
| 2004-01-13 | Raytheon Aircraft Company Model 1900, 1900C, and 1900D Airplanes | Feb 19, 2004 | Airframe (1900C)Certain serial numbers: 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900 UD-1–UD-6; 1900D UE-1–UE-427. Only with: Equipped with vent blower assembly P/N 114-380028-1, 114-380028-3, 114-380028-5, or 114-380028-7. |
| 2003-20-10 | Raytheon Aircraft Company Beech Models 1900, 1900C, and 1900D Airplanes | Oct 15, 2003 | Airframe (1900C) |
| 2003-03-18 | Raytheon Aircraft Company Beech Models 1900, 1900C, and 1900D Airplanes | Feb 5, 2003 | Airframe (1900C) |
| 2001-22-16 | Raytheon Aircraft Company Beech Models 1900, 1900C (C-12J), and 1900D Airplanes | Dec 17, 2001 | Airframe (1900C)Certain serial numbers: 1900 UA-2; 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-302 |
| 2001-18-07 | Raytheon Aircraft Company Beech Models 1900, 1900C, and 1900D Airplanes | Oct 12, 2001 | Airframe (1900C)Certain serial numbers: 1900 UA-2; 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-345; … |
| 2000-20-07 | Raytheon Aircraft Company Beech Models 1900, 1900C, and 1900D Airplanes | Nov 22, 2000 | Airframe (1900C)Certain serial numbers: 1900D UE-1–UE-376. Only with: Airplanes required to have a cockpit voice recorder (CVR) installed; for 1900 and 1900C, all serials with RAC Kit No. 114-3020 (-1, -3, -7, or -9), 114-3032-1, or 114-3008-1 incorporated, or where RAC installed the CVR. |
| 97-15-13 R2 | Raytheon Aircraft Company Beech Models 1900, 1900C, and 1900D Airplanes | May 28, 1999 | Airframe (1900C)Certain serial numbers: 1900 UA-1–UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-157 |
| 99-04-08 | Raytheon Aircraft Company Models 1900, 1900C, and 1900D Airplanes | Mar 26, 1999 | Airframe (1900C)Certain serial numbers: 1900 UA-2; 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-299 |
| 99-01-03 | Raytheon Aircraft Company Models 1900, 1900C, and 1900D Airplanes | Feb 8, 1999 | Airframe (1900C)Certain serial numbers: 1900 UA-1; 1900 UA-2; 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; … |
| 98-26-16 | Raytheon Aircraft Company Models 1900, 1900C, and 1900D Airplanes | Feb 5, 1999 | Airframe (1900C)Certain serial numbers: 1900 UA-2; 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-271 |
| 98-21-20 | Raytheon Aircraft Company Models 1900, 1900C, and 1900D Airplanes | Nov 20, 1998 | Airframe (1900C)Certain serial numbers: 1900 UA-2; 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-268 |
| 97-26-15 | Raytheon Aircraft Company Models 1900, 1900C, and 1900D Airplanes | Jan 25, 1998 | Airframe (1900C)Certain serial numbers: 1900 UA-2; 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-249; …. Only with: Equipped with at least one P/N 114-380041-11 (or FAA-approved equivalent) main landing gear actuator. |
| 97-25-03 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series Airplanes | Jan 21, 1998 | Airframe (1900C) |
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.
FOUND FUEL TANK INTERCONNECT TUBES IN LEFT AND RIGHT MAIN LANDING GEAR WELLS TO BE CHAFED WHERE THE TUBES PASS THROUGH THE OUT BOARD KEEL BEAM. THE RIGHT HAND SIDE WORN TO OVER 90% OF THE WALL THICKNESS. THE LEFT HAND SIDE WAS WORN TO APPROX 75% OF THE WALL THICKNESS.
From FAA Service Difficulty Reports; matched by N-number and serial number.RIGHT MAIN LANDING DRAG BRACE DISCONNECTED FROM WING ATTACH POINT. LANDING GEAR STRUT RETRACED THE AFT CONTACTING WING STRUCTURE. INVESTIGATION FOUND DRAG BRACE ATTACH BOLT BROKEN AT GREASE GALLEY.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING TAKEOFF ROLL BAGGAGE DOOR ANNUNCIATION ILLUMINATED. PILOT ABORTED TAKEOFF. INSPECTION REVEALED THE NOSE BAGGAGE DOOR SWITCH HAD FAILED.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING MX INSPECTION, THE LT SIDE SEAT RAIL WAS FOUND TO BE CORRODED.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING MX, THE RT SIDE SEAT RAIL WAS FOUND TO BE CORRODED.
From FAA Service Difficulty Reports; matched by N-number and serial number.INSPECTION REVEALED CORROSION DEVELOPING ON THE LT UPPER MAIN SPAR CAP UNDER THE VORTEX GENERATORS.
From FAA Service Difficulty Reports; matched by N-number and serial number.RIGHT WING DEBOND. UPPER SKIN OF BONDED PANEL IN AREA AROUND FUEL BAY ACCESS OVAL PANEL DEBONDED FROM FUEL ACCESS DISH & HONEYCOMB CORE.
From FAA Service Difficulty Reports; matched by N-number and serial number.LEFT WING DEBOND. UPPER SKIN OF BONDED PANEL IN AREA AROUND FUEL BAY ACCESS OVAL PANEL DEBONDED FROM FUEL ACCESS DISH & HONEYCOMB CORE.
From FAA Service Difficulty Reports; matched by N-number and serial number.SEVERAL CRACKS DEVELOPED IN THE SKIN OTBD OF THE LT NACELLE & AFT OF THE MAIN SPAR ORIGINATING FROM VARIOUS RIVETS.
From FAA Service Difficulty Reports; matched by N-number and serial number.TWO CRACKS WERE DISCOVERED IN THE VERTICAL STABILIZER RIB AT CSS 69. REPAIRED IAW SRM 51-10-21.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 31 reports.