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N416AW

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2002 Bombardier CL-600-2B19 · GE CF34 series

Open in FAA registry

© OpenStreetMap
Registered owner
Csi Aviation LLC
Location
Killeen, TX
Owner type
Corporation
Serial number
7603
Year built
2002
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
January 17, 2002
Certificate issued
May 7, 2026
Expires
May 31, 2033
Mode S code
A4EA7F
Bombardier CL-600-2B19Airframe model · 55 seats · 2 engines · 395 registeredTCDS A21EA-1Airframe · Bombardier CL-600-2B19Engine modelGE CF34 series

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every GE CF34 model are included below.

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Airworthiness directives that may apply · 201

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

1981In forceSuperseded2026
See all 279 ADs

Information bulletins that may apply · 10

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N416AWMatched 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 Bombardier CL-600-2B19 aircraft

FAA incident reports

No FAA accident or incident reports matched to N416AWMatched 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 Bombardier CL-600-2B19 aircraft

Service difficulty reports · 183

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

SDR A6WA202512038873Actuator · malfunctionedRECEIVED FLAPS FAIL WHEN SELECTING FLAPS FROM 8 TO 20. IT FAILED AT 8. C/W QRH. AIRSPEED 180 KNOTS WHEN FAILED. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPP 98-018I BOX 12. FLAPS RESET. REF 357078-1 FOR MEL REF 357077-4 PERFORMED FLAP FAIL RESET PROCEDURE. PJan 22, 2026 · N416AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA202409058806Control Unit · faultedFLAPS FAIL CAUT MESSAGE FLAPS FAILED AT 16K FT 250 KNOTS FAILED IN THE ZERO DEGREE POSITION. AIRCRAFT REMOVED FROM SERVICE R&R THE FECU IAW AMM 27-51-05. OPS CHECK GOOD. REMOVED PLACARD AND REMOVED FROM MEL. Sep 5, 2024 · N416AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA202409058804Control Unit · failedFLAPS FAIL CAUT MESSAGE FLAPS FAILED AT 16K FT 250 KNOTS FAILED IN THE ZERO DEGREE POSITION. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL ***** AIRCRAFT REMOVED FROM SERVICE ***** R&R THE FECU IAW Sep 5, 2024 · N416AW · Cndair CL6002B19 · Trailing Edge Flap Control System
See all 183 reports
Reports on N416AW not matched to an aircraft · 2

They name N416AW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

SDR PCAA9600269Engine · failedNR 1 ENGINE OIL PRESSURE WENT TO ZERO IN FLIGHT. SHUT DOWN NR 1 ENGINE IN FLIGHT. REMOVED AND REPLACED NR 1 ENGINE. OPERATIONAL CHECK NORMAL. INVESTIGATION CONTINUES. AIRCRAFT RETURNED TO SERVICE. (M)Feb 22, 1996 · N416AW · Dhav DHC8102 · Engine (Turbine/Turboprop)SDR PCAA9600260Oil Cooler · leaksLOW OIL PRESSURE ON NR 1 ENGINE REQUIRED PRECAUTIONARY SHUT-DOWN. (OIL LIGHT ILLUMINATED AND PRESSURE DROPPED SLOWLY TO 40 PSI AND SHUT-DOWN WAS INITIATED.) MASTER WARNING FLASHED WITHOUT CAPTION. REMOVED AND REPLACED OIL COOLER IAW MM. GROUND RAN AIRCRAFTJan 6, 1996 · N416AW · Dhav DHC8102 · Engine Oil Cooler

STCs that may be installed · 323

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

See all 323 STCs