Owner type Government
Year built 1996
Type Fixed wing multi engine
Engine Turbo-prop
Airworthiness Standard, normal
Airworthiness date August 19, 1996
Certificate issued January 13, 1997
Expires April 30, 2029 From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada PT6A-6 model are included below.
On this page Registration Potential ADs 47 Information bulletins 6 NTSB investigations 0 FAA incident reports 1 Difficulty reports 11 Potential STCs 439 Related links Airworthiness directives that may apply · 47 Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
1968 In force Superseded2026 ADs by the year they took effect: 53 ADs 1968 1 1969 1 1970 1 1975 1 1977 1 1980 2 1992 3 1994 3 1995 1 1996 1 1997 2 1998 6 1999 4 2002 2 2003 2 2004 1 2005 4 2006 2 2007 1 2008 2 2010 2 2011 1 2012 1 2016 1 2019 1 2021 1 2022 1 2023 1 2024 1 2025 1 2026 1
See all 53 ADs Information bulletins that may apply · 6 Advisory, not mandatory.
All 6 Airframe 2 Engine 4
NTSB investigations No NTSB investigations matched to N991LL Matched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Raytheon B300 aircraft FAA incident reports · 1 FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Reports on N991LL not matched to an aircraft · 1 They name N991LL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Service difficulty reports · 11 Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2005FA0001000 Skin · delaminated DURING A POST FLIGHT CHECK, A MECHANIC NOTICED A BULGE ON THE UNDERSIDE OF THE IB LEADING EDGE OF THE LT WING. UPON FURTHER INVESTIGATION, A DELAMINATION AREA OF APPROXIMATELY 22 INCHES X 10 INCHES WAS FOUND. AFTER REMOVAL OF THE LEADING EDGE AND CLOSER EXA Jun 6, 2005 · N991LL · Beech B300 · Leading Edge Devices SDR LX52003F00002 Power Supply · odor THE POWER SUPPLY EMITTED A FOUL ODOR THAT WAS NOTICED THROUGH OUT AIRCRAFT AND THEN UNIT FAILED. Oct 1, 2003 · N991LL · Beech B300 · Electrical Power System SDR CGO2002F00002 Plate · failed DURING FREON AIR CONDITIONING SYSTEM TROUBLESHOOTING, FOUND COMPRESSOR FAILED. UPON REMOVAL OF OLD UNIT FOR REPLACEMENT, FOUND PIVOT PLATE CRACKED COMPLETELY THROUGH. Sep 11, 2002 · N991LL · Beech B300 · Cabin Cooling System SDR 20010215CW001 Valve · inoperative LT BRAKE DE-ICE LIGHT NOT ILLUMINATING. LIGHT SYSTEM / SWITCH IS INOPERATIVE. Jan 11, 2001 · N991LL · Beech B300 · Ice/Rain Protection System SDR 20000517SH014 Shutoff Valve · stuck VALVE STICKING PARTIALLY OPEN WHEN SELECTED OFF. (X) May 5, 2000 · N991LL · Beech B300 · Engine Bleed Air System SDR 20000613SH016 Pressure Switch · inoperative PRESSURE SWITCH INOPERATIVE ON AIR CONDITIONING COMPRESSOR. Apr 17, 2000 · N991LL · Beech B300 · Cabin Compressor System SDR 99ZZZX4174 Switch · malfunctioned THE RED LIGHT IN THE LANDING GEAR HANDLE, 'GEAR UNSAFE LIGHT', WOULD NOT EXTINGUISH WITH LANDING GEAR IN FULLY RETRACTED POSITION. JACKED AIRCRAFT, CHECKED ALL UP AND LOCK SWITCHES, AND ASSOCIATED WIRING. CYCLED LANDING GEAR THROUGH TEN COMPLETE EXTENSION/RE Oct 25, 1999 · N991LL · Beech B300 · Landing Gear Position and Warning SDR 99ZZZX4173 Switch · malfunctioned THE RED LIGHT IN THE LANDING GEAR HANDLE, 'GEAR UNSAFE LIGHT', WOULD NOT EXTINGUISH WITH LANDING GEAR IN FULLY RETRACTED POSITION. JACKED AIRCRAFT, CHECKED ALL UP AND LOCK SWITCHES, AND ASSOCIATED WIRING. CYCLED LANDING GEAR THROUGH TEN COMPLETE EXTENSION/RE Oct 25, 1999 · N991LL · Beech B300 · Landing Gear Position and Warning SDR 98ZZZX1902 Bearing · failed THIS STARTER/GENERATOR WAS REMOVED FROM AIRCRAFT FOR BRUSH CHANGE. THE BEARINGS WERE FOUND VERY ROUGH, EXTREMELY CLOSE TO TOTAL FAILURE. THEY WOULD NOT HAVE MADE 1,000 HOUR TBO! THIS UNIT HAS THE LATEST SPRING LOADED BEARINGS, AND THE FINNED COMMUTATOR END F Apr 17, 1998 · N991LL · Beech B300 · Starter-Generator SDR 96ZZZX5076 Flame Detector · malfunctioned LEFT ENGINE FIRE LIGHT CAME ON, SIGNAL VOLTAGE TOO HIGH. BEECH HAS NEW STYLE FLAME DETECTOR FOR BETTER RELIABILITY. Sep 11, 1996 · N991LL · Beech B200 · Fire Detection SDR 96ZZZX3835 Detector · malfunction CREW REPORTED INTERMITTENT FIRE WARNING ON LEFT ENGINE. FOUND LOWER FIREWALL FIRE DETECTOR BAD. THIS DETECTOR HAS BEEN SUPERCEDED BY A NEW STYLE. Jul 11, 1996 · N991LL · Beech B200 · Fire Detection STCs that may be installed · 439 Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 439 STCs