- Registered owner
- Shores Kenneth E
- Location
- Robstown, TX
- Owner type
- Individual
- Serial number
- LW-27
- Year built
- 1972
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- October 26, 1972
- Certificate issued
- March 31, 2011
- Expires
- March 31, 2030
- Mode S code
- A45721
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 45
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1974 | 2 |
|---|---|
| 1976 | 2 |
| 1977 | 4 |
| 1978 | 4 |
| 1979 | 1 |
| 1980 | 1 |
| 1981 | 1 |
| 1982 | 1 |
| 1985 | 1 |
| 1987 | 1 |
| 1988 | 1 |
| 1989 | 2 |
| 1990 | 2 |
| 1992 | 2 |
| 1997 | 3 |
| 1998 | 4 |
| 1999 | 1 |
| 2001 | 1 |
| 2002 | 1 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 4 |
| 2006 | 1 |
| 2008 | 3 |
| 2009 | 1 |
| 2021 | 1 |
| 2023 | 1 |
See all 50 ADs
Information bulletins that may apply · 5
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N379VMMatched 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 Beech E-90 aircraft
FAA incident reports
No FAA accident or incident reports matched to N379VMMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Beech E-90 aircraft
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR VQMAF010510Circuit Board · burned outA CABIN ALTITUDE WARNING PRESSURE SWITCH TEST WAS PERFORMED BY METHOD 2, AS REFERENCED IN MM 21-30-00, PAGE 214, ITEMS A-F. DETERMINED THAT THE TEST FAILED ITEM C OF THE TEST, BECAUSE THERE WAS NO VISUAL AMBER "CABIN ALTITUDE HIGH" WARNING ANNUNCIATION AVAILABSDR 2008FA0000670Fuel Line · crackedWHILE PERFORMING ENGINE RUNS FOR RIGHT ENGINE FLOW PACK CHANGE FOUND FUEL LEAK FROM FUEL LINE FROM FCU TO TOP OF START CONTROL UNIT. FITTING CRACKED ABOVE SCU. REMOVED CRACKED FUEL LINE FROM FCU TO TOP OF START CONTROL UNIT. INSTALLED OVERHAULED LINE P/N 30SDR 2006FA0000252Boot · mismanufacturedON INSTALLATION OF NEW LT AND RT WING DE-ICE BOOTS, PMA P/N SMR2014-21-1, -2, WAS DISCOVERED AIR INLET TUBES ARE INSTALLED IN WRONG LOCATION, MAKING IT IMPOSSIBLE TO MATCH BOOT CENTERLINE WITH LE CENTERLINE. OEM DRAWINGS SHOW 1 INCH FROM BOOT CENTERLINE TO ISDR 2006FA0000251Boot · mislocatedUPON INSTALLATION OF NEW LT AND RT WING DE-ICE BOOTS WITH NEW PMA P/N SMR2014-21-1, AND -2, IT WAS DISCOVERED THE AIR INLET TUBES ARE INSTALLED IN THE WRONG LOCATION, MAKING IT IMPOSSIBLE TO MATCH THE BOOT CENTERLINE WITH THE LE CENTERLINE. MFG AND OEM DRAWINSDR 98ZZZX792Skin · crackedIT APPEARS THAT VIBRATION AND LEFT HAND PROPELLER HARMONICS CAUSED OIL CANNING BETWEEN TWO STRINGERS THAT INDUCED THE ORIGINAL SKIN CRACK WHICH ENLARGED ITSSELF. FOUND DURING THE BEECH COMPLETE INSPECTION. SUBMITTER STATED IF GONE UNDETECTED COULD CAUSE HORISDR 95ZZZX5255Wheel · crackedCRACKS WERE FOUND IN THE BOLT HOLES OF THE WHEEL HALF CAUSING THE TIRE TO DEFLATE MORE THAN THE ALOTTED AMOUNT.
STCs that may be installed · 305
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech E-90
STC SA02054SEInstallation of winglets and related system changes.STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.