Registered owner
Pacific Mission Aviation
Owner type
Corporation
Serial number
LD-412
Type
Fixed wing multi engine
Engine
Reciprocating
Airworthiness
Special flight permit
Airworthiness date
February 19, 1991
Certificate issued
November 24, 1987
Expires
November 30, 2028
Mode S code
A54958

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 24

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1966In forceSuperseded2026
ADs by the year they took effect: 26 ADs
19661
19711
19742
19761
19771
19783
19792
19801
19821
19851
19881
19891
19901
19961
19971
19981
19991
20002
20041
20051
20231
See all 26 ADs

Information bulletins that may apply · 3

Advisory, not mandatory.

Historical bulletins · 2

NTSB investigations · 1

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

Investigations on N44MA not matched to an aircraft · 1

They name N44MA, but no registry record covers the date, the aircraft registered then was built later, or the investigation describes another 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 N44MA not matched to an aircraft · 1

They name N44MA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

Service difficulty reports · 12

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR CVU2010F00000Actuator · malfunctionedTHE RT MLG FREEFELL TO THE DOWN AND LOCKED POSITION WHILE THE GEAR WAS BEING EXTENDED. INSP REVEALED FAILURE OF THE NUT INSIDE ASSY NR 50-8103672. REPLACED BOTH RT AND LT MAIN GEAR ACTUATORS.Jan 4, 2010 · N44MA · Beech 65B80 · Landing Gear ActuatorSDR CVU2009F00001Fork · crackedDURING A RECURRENT INSP REQUIRED BY AD 2004-23-02C, A CRACK WAS FOUND AT THE LOCATION ILLUSTRATED. WERE THE WELD MEETS THE SURFACE, AFTER USING DYE PENETRANT THE CRACK BECAME VISIBLE.Nov 6, 2009 · N44MA · Beech 65B80 · Nose/Tail Landing GearSDR CVU2009F00000Starter · noisyON STARTUP, ONCE THE BENDIX GEAR ENGAGED, A LOUD NOISE WAS HEARD, WHICH SOUNDED LIKE GEARS GRINDING. UPON CLOSER INSP, NO TEETH REMAINED ATTACHED TO THE BENDIX. THE HAD ALL SHEARED OFF THE CASING AND THE CASING WAS LOOSE. THE SNAP RING WHICH NORMALLY HELD IFeb 3, 2009 · N44MA · Beech 65B80 · Engine StarterSDR CVU2008F00000Starter · intermittentPART REMOVED FOR OVERHAUL AFTER INTERMITTENT OPERATION. (K)Jul 7, 2008 · N44MA · Beech 65B80 · Engine StarterSDR 2008FA0000468Hinge · cracked(2) OF THE HINGE LINKS HAD CRACKED OFF ON ONE END. UPON DISASSEMBLY IT WAS DETERMINED THAT A CRACK HAD FORMED LENGTHWISE BETWEEN THE FASTENERS AND THE HINGE LINKS. POSSIBLE CAUSE MAY HAVE BEEN FATIGUE. (K)Jul 1, 2008 · N44MA · Beech 65B80 · Fuselage, Door HingeSDR 2006FA0001212Bellcrank · crackedA CRACK WAS FOUND ON THE RT BELLCRANK SUPPORT ASSY. DURING A MANDITORY 5 YEAR INSPECTION IAW MSB 2231 REV 1. (K)Nov 22, 2006 · N44MA · Beech 65B80 · Elevator StructureSDR CVU2006F00000Camshaft · wornSMALL PARTICLES OF METAL FOUND IN OIL. IDENTIFIED NR 5 AND NR 6 CAM AND ASSOCIATED LIFTERS WORN. REMOVED FOR REPAIR. RECOMMEND THE USE OF 16702 ENGINE OIL ADDITIVE ON A REGULAR BASIS. (K)Feb 2, 2006 · N44MA · Beech 65B80 · Reciprocating Engine Power SectionSDR CVU2005F00002Lifter · wornSMALL METAL FLAKES KEPT RE-APPEARING IN THE OIL SCREENS. FOUND WORN CAM NR 5 AND NR 6 CYLINDER INTAKE VALVES. ENGINES REMOVED FOR REPAIR. USE MFG ENGINE OIL ADDITIVE FROM TIME OF OVERHAUL. RUN ENGINE FREQUENTLY. (K)Jul 15, 2005 · N44MA · Beech 65B80 · Reciprocating Engine Power SectionSDR CVU2005F00001Camshaft · wornSMALL METAL FLAKES KEPT RE-APPEARING IN THE OIL SCREENS. FOUND WORN CAM NR 5 AND NR 6 CYLINDER INTAKE VALVES. ENGINES REMOVED FOR REPAIR. USE MFG ENGINE OIL ADDITIVE FROM TIME OF OVERHAUL. RUN ENGINES FREQUENTLY. (K)Jul 15, 2005 · N44MA · Beech 65B80 · Reciprocating Engine Power SectionSDR CVU2004F00000Pump · failedVACUUM PUMP FAILED UNDER NORMAL OPERATING CONDITIONS. (VFR DAY)Sep 23, 2004 · N44MA · Beech 65B80 · Vacuum Distribution SystemSDR CVU2003F00000Pump · failedPUMP FAILED UNDER NORMAL OPERATING CONDITIONS (VFR DAY).Sep 20, 2003 · N44MA · Beech 65B80 · Vacuum Distribution SystemSDR CVU2002F00000Magneto · damagedPRIMARY COIN HOLD DOWN RETAINERS LOOSE WITHIN MAGNETO CASE. THE LOOSE RETAINERS, IN TURN, GOT CAUGHT IN THE TIMING WHEEL/GEAR AND CHEWED UP SEVERAL TEETH. PROBABLE CAUSE- THE RETAINERS WERE NOT INSTALLED PROPERLY. FORTUNATELY THE DAMAGE WAS AT THE R20 TIMIDec 15, 2001 · N44MA · Beech 65B80 · Magneto/Distributor

STCs that may be installed · 217

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 217 STCs

Earlier aircraft with this N-number · 1

This aircraft carried N44MA before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.