Registered owner
Blue Horizon Point LLC
Location
Lewes, DE
Owner type
LLC
Serial number
RK-189
Year built
1998
Type
Fixed wing multi engine
Engine
Turbo-jet
Airworthiness
Standard, transport
Airworthiness date
May 30, 1998
Certificate issued
August 31, 2026
Expires
August 31, 2033
Mode S code
A54BA4

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada JT15D 5 model are included below.

On this page

Airworthiness directives that may apply · 47

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

1991In forceSuperseded2026
ADs by the year they took effect: 51 ADs
19911
19922
19937
19946
19951
19964
19971
19982
19992
20002
20014
20022
20031
20043
20062
20071
20081
20092
20112
20131
20142
20231
20261
See all 51 ADs

Information bulletins that may apply · 4

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N440LNMatched 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 400A 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 9JLA2021120916906Indicator · defectiveTHE FLIGHT CREW REPORTED THE THE RUDDER TRIM POSITION INDICATOR INOP DURING FLIGHT. THE MAINTENANCE TEAM DETERMINED THE RUDDER TRIM INDICATOR WAS DEFECTIVE. THE INDICATOR WAS REMOVED AND A REPAIRED UNIT WAS INSTALLED. OPS CHECKS WERE SATISFACTORY AND THE AIRCRDec 6, 2021 · N440LN · Beech 400A · Rudder Tab Control SystemSDR 9JLA2021080527087Static Inverter · failedTHE FLIGHT CREW REPORTED THAT THE NO2 INVERTER WAS INTERMITTENTLY FAILING DURING FLIGHT. THE MAINTENANCE TEAM REMOVED AND REPLACED THE NO2 INVERTER WITH INSPECTED UNIT. OPERATION CHECKS WERE SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE.Jul 11, 2021 · N440LN · Beech 400A · AC InverterSDR 9JLA2021072827088Heater · defectiveTHE FLIGHT CREW REPORTED THAT THE LEFT WINDSHIELD WILL NOT HEAT UP PROPERLY. THE LEFT OVERHEAD TEMP CONTROL LIGHT WILL NOT ILLUMINATE IN ANY OPERATION. WHEN SYSTEM IS TURNED ON, THE CREW STATED THEY WERE NOT ABLE TO SEE THROUGH THE DISTORTED VIEW. ONLY A 3 INCJul 11, 2021 · N440LN · Beech 400A · Windshield/Door Rain/Ice RemovalSDR MGOR20210209001Cable · corrodedUPON DEPARTURE, FLIGHT CREW LEVELED OFF AT 5000 FEET MSL TO VERIFY PROPER FLAP OPERATION. IN LEVEL FLIGHT 160KTS OF AIRSPEED, RECEIVED "FLAP ASYMMETRY" INDICATION AFTER EXTENDING FLAPS 20 DEGREES TO 30 DEGREES. UPON TAXI IN, FLAP ASYM EXTINGUISHED AND FLAPS SEFeb 6, 2021 · N440LN · Beech 400A · Trailing Edge Flap Control SystemSDR 9JLA2020120927052Shutoff Valve · defectiveTHE FLIGHT CREW REPORTED THAT THEY WERE RECEIVING LESS THAN 5% OF AIRFLOW INTO THE CABIN FROM THE RT ENGINE PRESSURE SOURCE IN CRUISE FLIGHT. RT ITT IS 30 DEGREES COOLER THAN THE LT ENGINE ITT. BELOW 25000 FT RT ENGINE PRESSURE UNABLE TO PRESSURIZE CABIN ALONov 23, 2020 · N440LN · Beech 400A · Pneumatic Distribution System

STCs that may be installed · 134

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

See all 134 STCs

Earlier aircraft with this N-number · 1

This aircraft carried N440LN before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.