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N103BA

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1971 Beech 65-B80 · Lycoming IGSO-540-B1A

Open in FAA registry

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Registered owner
Bemidji Aviation Services Inc
Location
Bemidji, MN
Owner type
Corporation
Serial number
LD-435
Year built
1971
Type
Fixed wing multi engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
February 3, 1971
Certificate issued
October 7, 1981
Expires
July 31, 2028
Mode S code
A00FF3
Beech 65-B80Airframe model · 9 seats · 2 engines · 15 registeredTCDS 3A20Airframe · Beech 65-B80TCDS 1E7Engine · Lycoming IGSO-540-B1A

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 37

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

1962In forceSuperseded2026
See all 39 ADs

Information bulletins that may apply · 5

Advisory, not mandatory.

Historical bulletins · 2
SAIB CE-10-34R1Alternative Methods of Compliance (AMOC) to Airworthiness Directive (AD) 89-25-10 and 89-25-08Issued Aug 20, 2013SAIB CE-10-34Alternative Methods of Compliance (AMOC) to Airworthiness Directive (AD) 89-25-10 and AD 89-25-08Issued May 18, 2010

NTSB investigations

No NTSB investigations matched to N103BAMatched 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 65-B80 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.

Incident 19870129004949IRoll-Out (Fixed Wing) · Hibbing, MNDuring rollout aircraft struck a coyote. Landing gear torque knee failed but runway heading was maintained on snow.Jan 29, 1987 · Minor damage

Service difficulty reports · 3

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

SDR 2008FA0000240Bolt · failedNR 1 ENGINE SHUTDOWN IN FLIGHT. SUSPECTED NR 7 CONNECTING ROD BOLT FAILURE. CAUSING CYL SEPARATION FROM CASE AND CRANK CASE CRACK. AC LANDED SAFELY WITHOUT OTHER DAMAGE. (K)Mar 7, 2008 · N103BA · Beech 65B80 · Reciprocating Engine Power SectionSDR 2002FA0001123Points · meltedMELTING OF NYLON WHERE IT CONTACTS POINT ARM DURING OPENING AND CLOSING OF POINTS DURING OPERATION. INFERIOR NYLON USED, NOT RESISTANT TO WEAR OR HEAT.Sep 19, 2002 · N103BA · Beech 65B80 · Magneto/DistributorSDR 98ZZZX2598Stud · failedCYLINDER HOLD DOWN STUD BROKE UNDER NUT. SUSPECT DEFECTIVE STUD.Jun 11, 1998 · N103BA · Beech 65B80 · Reciprocating Engine Power Section

STCs that may be installed · 236

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

See all 236 STCs