Safety record in brief:1 NTSB incident (minor damage, Mar 2012)31 ADs may apply45 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.
A failure of the nose landing gear end cap due to fatigue. Contributing to the failure were the ineffective inspection and the unknown effect of grain direction on fatigue life.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ENG12IA024)
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 (1900D)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 (1900D)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 (1900D)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 (1900D)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 (1900D)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 (1900D)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 (1900D)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; … |
| 2004-09-07 | Raytheon Aircraft Company Model 1900, 1900C, 1900C (C-12J), and 1900D Airplanes | Jun 14, 2004 | Airframe (1900D)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 (1900D)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 (1900D) |
| 2003-09-12 | Raytheon Aircraft Company Model 1900D Airplanes | Jun 27, 2003 | Airframe (1900D)Certain serial numbers: 1900D UE-1–UE-50; 1900D UE-52–UE-350; 1900D UE-352–UE-358; 1900D UE-360; 1900D UE-361; 1900D UE-363–UE-369; … |
| 2003-04-26 | Raytheon Aircraft Company Model 1900D Airplanes | Apr 21, 2003 | Airframe (1900D)Certain serial numbers: 1900D UE-1–UE-265; 1900D UE-266–UE-388; 1900D UE-389–UE-410 |
| 2003-03-18 | Raytheon Aircraft Company Beech Models 1900, 1900C, and 1900D Airplanes | Feb 5, 2003 | Airframe (1900D) |
| 2001-22-16 | Raytheon Aircraft Company Beech Models 1900, 1900C (C-12J), and 1900D Airplanes | Dec 17, 2001 | Airframe (1900D)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 (1900D)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; … |
| 2001-04-05 | Raytheon Aircraft Company Beech Model 1900D Airplanes | Apr 9, 2001 | Airframe (1900D)Certain serial numbers: 1900D UE-156–UE-299. Only with: Equipped with a KLN-90B GPS incorporated in accordance with AlliedSignal STC SA00245WI-D. |
| 2000-20-07 | Raytheon Aircraft Company Beech Models 1900, 1900C, and 1900D Airplanes | Nov 22, 2000 | Airframe (1900D)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. |
| 99-16-12 | Raytheon Aircraft Company Model Beech 1900D Airplanes | Sep 27, 1999 | Airframe (1900D)Certain serial numbers: 1900D UE-1–UE-246. Only with: Airplanes that incorporate the electric elevator trim option. |
| 99-12-07 | Raytheon Aircraft Company Model 1900D Airplanes | Jul 23, 1999 | Airframe (1900D)Certain serial numbers: 1900D UE-1–UE-338 |
| 97-15-13 R2 | Raytheon Aircraft Company Beech Models 1900, 1900C, and 1900D Airplanes | May 28, 1999 | Airframe (1900D)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 (1900D)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 (1900D)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 (1900D)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 (1900D)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 |
| 98-13-11 | Raytheon Aircraft Company Model 1900D Airplanes | Aug 3, 1998 | Airframe (1900D)Certain serial numbers: 1900D UE-1–UE-271 |
| 98-09-12 | Raytheon Aircraft Company Model 1900D Airplanes | Jun 12, 1998 | Airframe (1900D)Certain serial numbers: 1900D UE-1–UE-160 |
| 97-26-15 | Raytheon Aircraft Company Models 1900, 1900C, and 1900D Airplanes | Jan 25, 1998 | Airframe (1900D)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 (1900D) |
| 97-17-08 | Raytheon Aircraft Company Model 1900D Airplanes (Formerly Known as Beech Aircraft… | Sep 24, 1997 | Airframe (1900D)Certain serial numbers: 1900D UE-176–UE-280; 1900D UE-282; 1900D UE-284. Only with: Airplanes that have not had the propeller removed and re-installed since factory installation, or have not had the attaching bolts re-torqued. |
| 97-10-14 | Raytheon Aircraft Company Model 1900D Airplanes (formerly Beech Aircraft Corporation) | Jul 7, 1997 | Airframe (1900D)Certain serial numbers: 1900D UE-1–UE-215 |
| 95-02-17 | Beech Aircraft Corporation Model 1900D Airplanes | Apr 17, 1995 | Airframe (1900D)Certain serial numbers: 1900D UE-1–UE-131 |
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.
PILOT REPORTED THAT THERE WAS A STRONG ELECTRICAL ODOR IN THE COCKPIT. MX INSPECTED ACFT DUCT SYS, RAN ACFT AND OPS CHECKED SYS WITH FLIGHT CREW, NO DEFECTS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT REPORTED GLARE SHIELD EMERGENCY LIGHTS FAIL TO ILLUMINATE ON CAPTAIN`S SIDE. MAINTENANCE REPLACED THE SWITCH, OPS CHECKED GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A SCHEDULED ROUTINE INSPECTION, FOUND A DENT IN THE RT FUSELAGE LOCATED BETWEEN STRINGERS 10R AND 11R AT FS 228.25 AND 243.25 IN A AREA OF 6" BY 4.6", WITH A DEPTH OF .15". REPAIRED IAW EO 12-1900-53-063. MAJOR REPAIR
From FAA Service Difficulty Reports; matched by N-number and serial number.- DURING A SCHEDULED ROUTINE INSP FOUND THAT THE HORIZONTAL STAB FWD SPAR WEB MISREPAIRED. REPAIRED IAW EO 12-1900-55-053. MAJOR REPAIR
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB LT FWD SPAR CAP ANGLE AT UPPER 2ND FASTENER HOLE, CRACK RADIATES UPWARD AND DOWNWARD AT THE OB EDGE OF FASTENER HOLE, .2 ICHES IN LENGTH. REPAIRED IAW EO 12-1900-55-052. MAJOR REPAIR
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB RT FWD SPAR CAP ANGLE AT THE UPPER FASTENER HOLE AT VSS 84.10, 20 PERCENT, CRACK RADIATES DOWNWARD & OTBD FROM FASTENER HOLE, .15 INCHES IN LENGTH. REPAIRED IAW EO 12-1900-55-054. MAJOR REPAIR
From FAA Service Difficulty Reports; matched by N-number and serial number.MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP FOUND CRACK AT A PREVIOUS REPAIR AT FS 163.97 AND STRINGER 9AR FRAME PROTRUDING OUT OF A STOP DRILL, .25" IN LENGTH. REPAIRED IAW EO 12-1900-53-060.
From FAA Service Difficulty Reports; matched by N-number and serial number.MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT FS 451 AND STRINGER 10R IN THE BEND RADIUS PROTRUDING UPWARD, .5" IN LENGTH. REPAIRED IAW EO 12-190 0-53-059.
From FAA Service Difficulty Reports; matched by N-number and serial number.CREW TRIED TO EXTENDED THE GEAR NORMALLY BUT THE GEAR FAILED TO EXTEND. CREW RAN CHECKLIST AND EXTENDED THE GEAR MANUALLY. AFTER MANUAL EXTENSION THERE WERE NO ABNORMAL INDICATIONS NOTED. MX R & R RT MAIN LANDING GEAR ACTUATOR IAW TC 1900-3230.10, REV 1. OPS, LEAK AND RIG CHECKED GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A SMALL CRACK ON THE HORIZONTAL STAB AFT SPAR CENTER WEB AT 2-OCLOCK POSITION AS VIEWED FROM REAR, .125" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW FR EO 02401. MATERIALS UTILIZED ARE INCLUDED IN…
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 45 reports.