Safety record in brief:1 NTSB incident (Dec 1989)6 ADs may apply22 service difficulty reports
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FAILURE OF THE PILOT IN COMMAND IN THE BEECH 300 TO COMPLY WITH AN ATC CLEARANCE IN A TIMELY MANNER, WHILE DIVERTING HIS ATTENTION, AND FAILURE OF THE ATC CONTROLLER TO ASSURE THAT IFR SEPARATION WAS MAINTAINED.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for MIA90IA039)
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 |
|---|---|---|---|
| 2022-03-23 | Rudder Control System | Feb 22, 2022 | Airframe (300)Only with: Equipped with a Garmin G1000 integrated avionics system installed per STC SA01535WI-D with GSA 9000 yaw servo software version 2.13 or earlier. |
| 2004-17-02 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series Airplanes | Oct 4, 2004 | Airframe (300)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; … |
| 2002-23-13 | Pratt & Whitney Canada PT6A Series Turboprop Engines | Dec 31, 2002 | Engine (PT6A-60A)Only with: Engines with turbine exhaust ducts P/N 3012290, 3031988, 3032117, 3035784, 3035786, 3105890-01, 3112167-01, or 3111780-01 installed. |
| 98-04-24 | Raytheon Aircraft Company Models E55, E55A, 58, 58A, 58P, 58PA, 58TC, 58TCA Airplanes… | Mar 13, 1998 | Airframe (300) |
| 97-25-03 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series Airplanes | Jan 21, 1998 | Airframe (300) |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 97-23-17 | Raytheon Aircraft Company 90, 100, 200, and 300 Series Airplanes (Formerly Known as… | Dec 29, 1997 | Airframe (300)Certain serial numbers: C90 LJ-683–LJ-1463; C90A LJ-683–LJ-1463; E90 LW-177–LW-347; F90 LA-1–LA-236; H90 LL-1–LL-61; A100 B-228–B-247; … |
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.
CABIN DOOR LIGHT ON @20300 MSL 6.5 PSI. WENT OFF AT 9200 MSL 0.3 PSI. EMERGENCY CHECKLIST ACCOMPLISHED. AIRCRAFT LANDED WITH NO INCIDENT.
From FAA Service Difficulty Reports; matched by N-number and serial number.CABIN DOOR WARNING LIGHT ILLUMINATED AT 17,500, STAYED ON UNTIL LANDING
From FAA Service Difficulty Reports; matched by N-number and serial number.NO AUTO FEATHER RT ENG DURING T/O ROLL.
From FAA Service Difficulty Reports; matched by N-number and serial number.ALT WARN ANNUNCIATOR PASSING 12K, CABIN PRESSURE WAS 12K. PAX. 02 MASK DROPPED. UNABLE TO CONTROL CABIN ALTITUDE BELOW FLIGHT ALTITUDE. THE PRESSURE CONTROLLER WAS THE CAUSE. PRESSURE CONTROLLER WAS REPLACED. NO FURTHER ACTION REQUIRED.
From FAA Service Difficulty Reports; matched by N-number and serial number.MS HEARD LOUD AIR-LEAK COMING FROM THE CABIN DOOR. NOISE INCREASED AS DIFFERENTIAL PRESSURE INCREASED. CABIN DOOR SEAL WAS REPLACED.
From FAA Service Difficulty Reports; matched by N-number and serial number.RIGHT PROP PITCH ANNUNCIATOR ILLUMINATED IN FLIGHT. THE PROBLEM WAS SOLVED BY ADJUSTING THE PROXIMITY SWITCH. NO FURTHER ACTION REQUIRED.
From FAA Service Difficulty Reports; matched by N-number and serial number.HOT SMELL/ FUMES IN COCKPIT AFTER BATTERY ON AND GEN TIES CLOSED. VERIFIED FUME/ELECTRICAL BURNT SMELL COMING FROM MFD. REMOVED AND REPLACED MFD.
From FAA Service Difficulty Reports; matched by N-number and serial number.RT PROP PITCH LIGHT ILLUMINATED IN FLIGHT CAUSED BY A FAULTY PROXIMITY SWITCH. PROXIMITY SWITCH WAS REPLACED. OPERATIONAL CHECK WAS GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.RIGHT PROPELLER PITCH LIGHT ILLUMINATED AFTER TAKEOFF. REPLACED A FAULTY PROPELLER SWITCH. NO FURTHER ACTION REQUIRED.
From FAA Service Difficulty Reports; matched by N-number and serial number.GEAR FAILED TO RETRACT. REPLACED A FAULTY LANDING GEAR CONTROL HANDLE. NO FURTHER ACTION REQUIRED
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 22 reports.