Registered owner
Ari Ben Aviator Inc
Owner type
Corporation
Serial number
ME-34
Year built
1978
Type
Fixed wing multi engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
May 23, 1978
Certificate issued
August 23, 2004
Expires
January 31, 2028
Mode S code
A65DC3

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming O&VO-360 model are included below.

On this page

Airworthiness directives that may apply · 55

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

1963In forceSuperseded2026
ADs by the year they took effect: 61 ADs
19631
19641
19661
19671
19692
19772
19781
19794
19804
19811
19823
19881
19892
19911
19921
19951
19963
19972
19982
19991
20001
20021
20042
20053
20065
20071
20081
20102
20122
20171
20212
20222
20231
20241
20261
See all 62 ADs

Information bulletins that may apply · 12

Advisory, not mandatory.

See all 20 bulletins

NTSB investigations · 1

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

FAA incident reports · 3

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Service difficulty reports · 5

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

SDR YHLR20119403Display · false indicationATTITUDE DISPLAY SLOWLY ROLLS RT AND PITCHES DOWNWARD ON GROUND AND IN FLIGHT. REPLACED EFD-1000 PRO DISPLAY AS REQUIRED. PERFORMED SYS OPS CHECKS IAW EFD1000 INSTALLATION MANUAL 900-00003-001.Feb 23, 2011 · N5090M · Beech 76 · Directional Gyro and Indicating SystemSDR YHLR20119363Control Unit · failedACU BREAKER IS POPPED. ISOLATED TO ACU. POSSIBLE POWER SPIKE DAMAGED ACU. REPLACED ACU AS REQUIRED. PERFORMED SYSTEM OPERATIONAL CHECKS IN ACCORDANCE WITH ASPEN AVIONICS EFD1000 INSTALLATION MANUAL 900-00003-001.Jan 27, 2011 · N5090M · Beech 76 · Directional Gyro and Indicating SystemSDR YHLR20109297Connector · contaminatedNO VOR NR 2 DISPLAY ON PFD, ACU BREAKER POPS. ISOLATED TO ACU. FOUND EVIDENCE OF WATER ON CONNECTORS. REPLACED ACU AS REQUIRED. PERFORMED SYS OPS CHECKS IAW INSTALLATION MANUAL 900-00003-001.Nov 30, 2010 · N5090M · Beech 76 · Navigation System WiringSDR YHLR20109012Display · failedASPEN EFD-1000PRO DISPLAY SHOWS "PITOT FAIL". VERIFIED SQUAWK. DISPLAY ALSO "X’D" OUT. REPLACED DISPLAY AS REQUIRED. PERFORMED SYS OPS CHECKS IAW INSTALLATION MANUAL 900-00003-001.Jun 30, 2010 · N5090M · Beech 76 · Central DisplaySDR 2010FA0000421Module · failed(YHLR) AA EFD-1000 PRIMARY FLIGHT DISPLAY SHOWS "RSM LINK FAIL" MESSAGE ON INITIALIZATION. RSM WAS REPLACED, NEW SN 3884. PERFORMED SYS OPS CHECKS AND RSM CALIBRATION AS REQUIRED BY DOCUMENT 900-00003-001 REV F, SYS OPS CHECKS SATISFACTORY.Apr 7, 2010 · N5090M · Beech 76 · Directional Gyro and Indicating System

STCs that may be installed · 215

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

See all 215 STCs

Earlier aircraft with this N-number · 1

This aircraft carried N5090M before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.