Location
Hyannis, MA
Owner type
Corporation
Serial number
2209
Year built
1989
Type
Fixed wing multi engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
September 30, 2013
Certificate issued
September 30, 2013
Expires
September 30, 2029
Mode S code
A6B093

From the FAA registry file of October 24, 2026.

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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.

1966In forceSuperseded2026
ADs by the year they took effect: 69 ADs
19661
19691
19751
19772
19781
19791
19821
19833
19871
19921
19952
19963
19974
19985
19991
20026
20033
20042
20053
20064
20071
20082
20091
20112
20123
20131
20141
20151
20162
20172
20211
20221
20242
20251
20262
See all 70 ADs

Information bulletins that may apply · 8

Advisory, not mandatory.

Historical bulletins · 1

NTSB investigations

No NTSB investigations matched to N530BNMatched 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 Pilatus Britten-Norman BN2B-20 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.

Service difficulty reports · 5

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

SDR HYIA20230623001Switch · failedPILOT REPORTED SPARKS COMING FROM LEFT LANDING LIGHT SWITCH WHEN TURNED ON. MAINTENANCE INSPECTED AND FOUND LEFT LANDING LIGHT SWITCH TO BE DEFECTIVE. REMOVED AND REPLACED THE SWITCH WITH NO FURTHER DEFECTS.Jun 19, 2023 · N530BN · Bnorm BN2 · Lighting SystemSDR HYIA20160711001Cylinder · failedDURING INSPECTION OF RIGHT ENGINE AFTER FAILED ENGINE CHANGE FUNCTIONAL CHECK FLIGHT; MAINTENANCE NOTED LARGE AMOUNTS OF METAL IN OIL SAMPLES. FURTHER INVESTIGATION REVEALED DAMAGED SPARK PLUGS, PISTON, AND CYLINDER WALL AT THE NR 2 CYLINDER. DURING REMOVAL OFJul 5, 2016 · N530BN · Bnorm BN2B20 · Engine (Reciprocating)SDR HYIA20151223004Caliper · faultyPILOT REPORTED NO PRESS LT BRAKE. PERFORMED DETAILED INSPECTION ON LT BRAKE SYS & FOUND BOTH BRAKE CALIPERS MAKING A SQUEAKING SOUND & VERY SPONGY. R & R BOTH LT BRAKE CALIPERS & BLED SYS IAW MM SEC 2 9, OPERATIONALLY CHECKED GOOD.Dec 17, 2015 · N530BN · Bnorm BN2B20 · BrakeSDR HYIA20150403001Caliper · failedPILOT REPORTED RT BRAKE FAILURE. R & R THE CALIPER & LINING ON THE RT BRAKE & SERVICED SYS. OPERATIONALLY CHECKED IT WITH NO FURTHER DEFECT NOTED.Apr 1, 2015 · N530BN · Bnorm BN2B20 · BrakeSDR HYIA20140415107Pump · weakDURING CLIMB THE PILOT REPORTED THE RT FUEL PRESS WOULD NOT REMAIN IN THE GREEN ARC. THE ENG DRIVEN FUEL PUMP WAS REPLACED & OPERATIONAL & LEAK CHECK WERE ACCOMPLISHED NO DEFECTS NOTED. THE ACFT WAS RELEASED FOR A FLIGHT CHECK & NO DISCREPANCY WAS REPORTED.Apr 12, 2014 · N530BN · Bnorm BN2B20 · Engine Fuel Pump

STCs that may be installed · 146

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

See all 146 STCs