Owner type
LLC
Serial number
5653
Year built
2006
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
November 27, 2017
Certificate issued
November 30, 2017
Expires
November 30, 2027
Mode S code
A88D72

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 129

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
ADs by the year they took effect: 161 ADs
19811
19826
19841
19881
19901
19912
19922
19931
19945
19955
19961
19971
19981
19993
20005
20017
20022
20034
20042
20055
20066
20076
20082
20095
20109
20113
20124
20133
20147
20154
20165
20178
20184
20195
20202
20214
20227
20238
20246
20253
20264
See all 162 ADs

Information bulletins that may apply · 5

Advisory, not mandatory.

Historical bulletins · 1

NTSB investigations

No NTSB investigations matched to N650HJMatched 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-600-2B16 aircraft

FAA incident reports

No FAA accident or incident reports matched to N650HJMatched 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-600-2B16 aircraft

Service difficulty reports · 6

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

SDR V6NA2022081101Seat Track · corrodedAT SCHEDULE INSPECTION, DISCOVERED SEAT RAIL UNDER LAVATORY TOILET CORRODED. REPLACED FLOOR RAIL WITH NEW.Aug 11, 2022 · N650HJ · Cndair CL6002B16 · Fuselage, Seat/Cargo Attach FittingsSDR V6NA202109028011Seat Track · corrodedAT SCHEDULED INSPECTION, DISCOVERED CORROSION ON SEAT RAIL BEAM UPPER SURFACE, FS574.00 TO 605.00, WL73.5. CORROSION WAS REMOVED. DOUBLER REPAIR ANGLES OF 0.063 IN. 2024-T3 WERE INSTALLED WET USING MS20426AD RIVETS AND HL18PB5 HILOKS. REPAIR PERFORMED PER FAA Aug 18, 2021 · N650HJ · Cndair CL6002B16 · Fuselage, Seat/Cargo Attach FittingsSDR V6NA202109021801Seat Track · corrodedAT SCHEDULED INSPECTION, DISCOVERED CORROSION ON SEAT RAIL BEAM UPPER SURFACE, FS574.00 TO 605.00, WL73.5. CORROSION WAS REMOVED. DOUBLER REPAIR ANGLES OF 0.063 IN. 2024-T3 WERE INSTALLED WET USING MS20426AD RIVETS AND HL18PB5 HILOKS. REPAIR PERFORMED PER FAA Aug 18, 2021 · N650HJ · Cndair CL6002B16 · Fuselage, Seat/Cargo Attach FittingsSDR V6NA20201206001Skin · dentedAT SCHEDULED INSPECTION, DISCOVERED DENT IN FUSELAGE BELLY SKIN AT FS 646 FRAME 640, TEN INCHES FROM CENTER. DAMAGE DIMENSIONS APPROXIMATELY 3.0 X 8.3. FASTENERS WERE REMOVED IN AREA, SKIN AND STRAP MECHANICALLY FORMED BACK TO ORIGINAL CONTOUR. REFORMED AREDec 3, 2020 · N650HJ · Cndair CL6002B16 · Fuselage Main, Plate/SkinSDR V6NA20191209401Pin · missingAT SCHEDULED INSPECTION DETERMINED NOSE LANDING GEAR UPPER TORQUE LING ATTACHMENT TO LOWER TORQUE LING CASTELLATED NUT MIGRATING OUTWARD OFF OF TORQUE LINK APEX PIN DUE TO SECURING PIN MISSING. INSPECTED OPPOSITE PIN AND DETERMINED EXISTING PIN TO BE WORN. NO Dec 4, 2019 · N650HJ · Cndair CL6002B16 · Nose/Tail Landing GearSDR V6NA2018082002Mount · corrodedPASSENGER DOOR AFT FRAME AT BS 349, THE DOOR POWER ASSIST CABLE MOUNT WAS CORRODED. CABLE MOUNT WAS REPAIRED IAW DRAWING HAJ-GEBD604-5653-M01-1.Aug 20, 2018 · N650HJ · Cndair CL6002B16 · Fuselage Main, Structure

STCs that may be installed · 857

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

See all 857 STCs