Q400. Serial Number 4094
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1 Offers for Lease Q400 Serial Number 4094 TTSN 25,724 Flight Hours TCSN 29,806 Flight Cycles Availability: January 2018 Page 1 of 9
2 Date of Manufacture: July 2004 Model Designation: Q400 Standard Avionics: Avionics o Automatic Flight Control System o Autopilot with Dual Flight Director o Dual Attitude and Heading Reference System (APIRS) o Dual Air Data Computers o EFIS (Electronic Flight Instrument System) (Thales V810 incorporated) o Cat II capability o Engine and Systems Integrated Display (ESID) Navigation o Dual VHF (VOR, Glideslope and Marker) o Dual ADF, DME and ATC Mode S (EHS capable) o Dual Flight Guidance Module o Single Flight Management System with GPS (UNS-1E) Communication o Dual VHF System (8.33 khz frequency spacing) o Service Interphone and Passenger Address System Other Systems o Integrated Standby Flight Instrument System (Thales) o Dual Radio Altimeter (Honeywell KRA-405B) o Enhanced Ground Proximity Warning System (EGPWS) (Honeywell Mk V) o TCAS II/ACAS (Change 7.1) (Honeywell CAS 67A) o Audio Integrating System o Solid State Cockpit Voice Recorder (2 hr) (Honeywell 6022) o Emergency Locator Transmitter (3 frequency) (Kannad 406AF) o Centralized Maintenance and Diagnostic System o Passenger boarding and music system (Team) o Enhanced surveillance Page 2 of 9
3 Additional Installed Options: 51 ft 3 baggage compartment G3 Galley with stowage locations for four aisle trolleys and 2 SU and & 5 Hot Jugs Lavatory Wash water system Installation of second radio altimeter Full face oxygen and smoke masks for flight crew and observer Puritan Bennet Auxiliary Power Unit (APU) including DC generation and titanium tailcone Interior: 78 passenger seats G3 Galley G6 Galley 2 nd Flight attendant seat Page 3 of 9
4 Page 4 of 9
5 Interior Page 5 of 9
6 G3 Galley Page 6 of 9
7 G6 Galley Page 7 of 9
8 Flight Compartment Page 8 of 9
9 Aircraft Type A/C Serial No Report Date Operator DHC-8-Q Nov-17 Flybe A/C Reg'n Build Date Total Cycles C-FXIC 22-Jul-04 25,724 29,806 Inspection Status Check Description Last Done Interval Date Heavy Maintenance Checks Flight Hours Flight Cycles Next due Remaining Interval Unit A Check Aug-17 25,710 29,800 26, Flight Hours C Check 6,000 6-Aug-17 25,710 29,800 31,710 5,986 Flight Hours Calendar Inspections 12 Months Aug-17 N/A N/A 6-Aug Days 24 Months Aug-17 N/A N/A 6-Aug Days 3 Years 1,095 6-Aug-17 N/A N/A 6-Aug-20 1,002 Days 6 Years 2, Apr-17 N/A N/A 26-Apr-23 1,995 Days 9 Years 3,285 5-Jun-13 N/A N/A 5-Jun-22 1,670 Days Left Engine Type Serial Number Total Cycles PW150A Since New Since OH Since LSV Since New Since OH Since LSV PCE-FA0242 Turbo Machine 23,497 10,368 2,446 21,969 10,393 2,308 RGB RGM-FA ,857 2,446 2,446 23,913 2,308 2,308 LLP's Description Part Number Serial No Cycles Since New Cycles Remaining Cycle Life Limit Rotor, Compressor, 1st Stage A002WAE9 10,368 9,632 20,000 Rotor, Compressor, 2nd Stage A00321BL 10,368 9,632 20,000 Rotor, Compressor, 3rd Stage A0031CBT 10,368 9,632 20,000 Impeller, Centrifugal, HP A ,368 4,632 15,000 Disc, HP Turbine A00322RY 10,368 9,632 20,000 Cover, HP Turbine, Front A0031XND 10,368 9,632 20,000 Cover, HP Turbine, Rear A00320AF 10,368 9,632 20,000 Disc, LP Turbine A00320NL 10,368 9,632 20,000 Cover, LP Turbine, Front A ,368 9,632 20,000 Disc, Power Turbine, 1st Stage A001MX51 23,497 6,503 30,000 Disc, Power Turbine, 2nd Stage A001MLC0 23,497 6,503 30,000 Right Engine Type Serial Number Total Cycles PW150A Since New Since OH Since LSV Since New Since OH Since LSV PCE-FA0213 Turbo Machine 24,646 4,644 1,226 21,822 4,549 1,169 RGB RGM-FA ,854 24,854 1,226 21,838 21,862 1,169 LLP's Description Part Number Serial No Cycles Since New Cycles Remaining Cycle Life Limit Rotor, Compressor, 1st Stage A003KEPC 4,644 15,356 20,000 Rotor, Compressor, 2nd Stage A003D4EC 4,644 15,356 20,000 Rotor, Compressor, 3rd Stage A002W3KP 12,939 7,061 20,000 Impeller, Centrifugal, HP A003EEBA 4,644 10,356 15,000 Disc, HP Turbine A003CYEC 4,644 15,356 20,000 Cover, HP Turbine, Front A003ERMY 4,644 15,356 20,000 Cover, HP Turbine, Rear A003D0HW 4,644 15,356 20,000 Disc, LP Turbine A003CPNL 4,644 15,356 20,000 Cover, LP Turbine, Front A003D0X4 4,644 15,356 20,000 Disc, Power Turbine, 1st Stage A001FT6D 24,646 5,354 30,000 Disc, Power Turbine, 2nd Stage A001FCRR 24,646 5,354 30,000 Landing Gear Description Installed Cycles Date Nose Gear Part Number Serial No Since New Since Restoration Remaining Last Restored Next Due Overhaul Interval NLG Dressed Shock Strut Assy MA ,868 9,911 10,089 N/A 16-Mar-23 20,000 Main Gear, Left Dressed Shock Strut Assy MLG MA ,735 19,735 10,265 N/A 27-Sep-22 30,000 Main Gear, Right Dressed Shock Strut Assy MLG MA ,735 19,735 10,265 N/A 27-Sep-22 30,000 Propellers Left (Hub, Actuator and BP Assy) Model Part Number Manuf. Date Serial Number TSN O/H Date Date Due R408/6-123-F/ Feb-09 DAP , Aug Aug-24 Description Part Number Serial Number Restoration MI Limit Since MI Remaining Date Next Due Blade&Bearing # ,997 5,003 11, Aug Aug-24 Blade&Bearing # ,999 5,001 11, Aug Aug-24 Blade&Bearing # ,997 5,003 11, Aug Aug-24 Blade&Bearing # ,988 8,012 11, Feb Feb-26 Blade&Bearing # ,988 8,012 11, Feb Feb-26 Blade&Bearing # ,997 5,003 11, Aug Aug-24 Propeller Hub Assy MG ,997 4,003 10, Aug Aug-24 Right (Hub, Actuator and BP Assy) Model Part Number Manuf. Date Serial Number TSN O/H Date Date Due R408/6-123-F/ Aug-11 DAP , Mar Mar-26 Description Part Number Serial Number Restoration MI Limit Since MI Remaining Date Next Due Blade&Bearing # ,416 5,584 11, Jul Jul-24 Blade&Bearing # ,365 9,635 11, May May-26 Blade&Bearing # ,404 9,596 11, Dec Dec-26 Blade&Bearing # ,017 8,983 11, Jul Jul-26 Blade&Bearing # ,708 5,292 11, Oct Oct-24 Blade&Bearing # ,600 8,400 11, Mar Mar-26 Propeller Hub Assy MG152/11 2,600 7,400 10, Mar Mar-26 APU Hamilton Sundstrand Total Cycles Serial No Description Part Number Since New Since Repair Since New Since Repair APU Assy APS 1000 (T-62T-46C12) C SPE ,122 1,782 16,252 N/A Compressor Wheel (Impeller) SIF2663 1,782 N/A 5,235 N/A Turbine Wheel H452D 12,438 N/A 10,335 N/A specified "Data Date." While diligent efforts have been made by Bombardier to verify such specifications to the extent possible, Bombardier shall not be held responsible for any inaccurate data supplied by the previous operator. Prospective customers are strongly encouraged to Page 9 of 9
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