1 / 13 · 🔍 click to zoom
1998 BOMBARDIER DASH 8-400
Starts from the median asking price of 128 comparable Turboprop listings ($1,547,963), then adjusts for:
- Year -2 vs comparable listings -3.8%
- Airframe time +27,141 hr vs comps -20.0%
- Engine time +22,102 hr vs comps (twin turbine) -20.0%
- No Autopilot (54% of comps have one) -1.0%
- No ADS-B (60% of comps have one) -1.6%
Shown as a range. An estimate from asking-price comparables and FAA supply data — not an appraisal.
Overview
| Make / Model | Bombardier DASH 8-400 |
|---|---|
| Type | Turboprop |
| Airframe time | 31,855 hrs |
| Engine time | 23,707 SNEW |
| Avionics / Terrain / EGPWS | EGPWS |
| Avionics / Traffic (TCAS / TAS) | TCAS II |
| Avionics / Flight management (FMS) | UNS-1EW |
| Inspection | Progressive |
Description
Canadian-registered De Havilland DHC-8-Q400 featuring a 72-passenger cabin, Head-Up Display upgrade and progressive C-check maintenance program. Combining strong regional-airline pedigree with proven operational versatility, this well-equipped aircraft is suited for demanding routes and remote operations. A second Q400 from the same fleet will soon be available for sale, offering buyers the opportunity to pursue a broader fleet acquisition.
Modifications
EQUIPMENT - OHU-4100 Head-Up Display - Dual USB Charging Ports COMMUNICATIONS - Skynode S200 SATCOM - SATCOM Antenna Installation – STC SA11-85
Avionics
Thales V810 Avionics Suite AHRU: Dual SFIM AHRU HUD: OHU-4100 Head-Up Display HGS Computer: HGS Computer Weather Radar: Weather Radar P660 EGPWS: Honeywell Mark V EGPWS SATCOM: Skynode S200 SATCOM TCAS II: Honeywell CAS 67A/67B TCAS II Processor Radio Altimeter: Dual Collins ALT-4000 Radio Altimeter Transceivers IRU: IRU / ATA-300 VHF COM: Dual 8.33 kHz VHF Transceivers DME: Dual DME DCE Transceivers ADC / Air Data: Dual Air Data Units Standby Instruments: Integrated Standby Indicator Transponder: Dual L3Harris NXT-600 ATC Transponders FMS: Dual Universal Avionics UNS-1EW FMS CVR: Honeywell Solid State CVR FDR: Honeywell Solid State FDR ELT: Kannad 406AF ELT DTU: Solid State DTU FAST: FAST Box (PW150)
Recommended avionics upgrades
No IFR GPS navigator is listed — a GTN 650Xi is the standard entry point for WAAS/LPV capability.
See prices & suppliers ›No autopilot is listed — a GFC 600 or S-TEC 3100 digital autopilot is a major capability and value add, subject to STC approval for this model.
Shop options ›No ADS-B is listed — a GTX 345 delivers required ADS-B Out plus In (traffic & weather) in one transponder.
See prices & suppliers ›Suggestions are based on the panel described in this listing; verify STC approval for this make/model before any installation.
Service Difficulty Reports (SDRs)
Checking FAA service difficulty reports…
Airworthiness Directives (ADs)
Checking airworthiness directives…
General
| Year | 1998 |
|---|---|
| Manufacturer | BOMBARDIER |
| Model | DASH 8-400 |
| Serial Number | 4004 |
| Condition | Used |
| Registration # | C-GHQP |
Airframe
| Total Time | 31,855 |
|---|---|
| Total Landings | 39,480 |
Engine 1
| Engine 1 Make/Model | PRATT & WHITNEY PW150A |
|---|---|
| Engine 1 Serial Number | PCE-FA0429 |
| Engine 1 Time | 23,707 SNEW |
| Engine 1 TBO | 3500 |
| Engine 1 Cycles | 29,784 |
| Hot Section Time 1 | 2,046 |
Engine 2
| Engine 2 Make/Model | PRATT & WHITNEY PW150A |
|---|---|
| Engine 2 Serial Number | PCE-FA0270 |
| Engine 2 Time | 25,248 SNEW |
| Engine 2 TBO | 3500 |
| Engine 2 Cycles | 32,068 |
| Hot Section Time 2 | 2,480 |
Avionics
| Avionics/Radios | Thales V810 Avionics Suite AHRU: Dual SFIM AHRU HUD: OHU-4100 Head-Up Display HGS Computer: HGS Computer Weather Radar: Weather Radar P660 EGPWS: Honeywell Mark V EGPWS SATCOM: Skynode S200 SATCOM TCAS II: Honeywell CAS 67A/67B TCAS II Processor Radio Altimeter: Dual Collins ALT-4000 Radio Altimeter Transceivers IRU: IRU / ATA-300 VHF COM: Dual 8.33 kHz VHF Transceivers DME: Dual DME DCE Transceivers ADC / Air Data: Dual Air Data Units Standby Instruments: Integrated Standby Indicator Transponder: Dual L3Harris NXT-600 ATC Transponders FMS: Dual Universal Avionics UNS-1EW FMS CVR: Honeywell Solid State CVR FDR: Honeywell Solid State FDR ELT: Kannad 406AF ELT DTU: Solid State DTU FAST: FAST Box (PW150) |
|---|
Additional Equipment
| Additional Equipment | EQUIPMENT - OHU-4100 Head-Up Display - Dual USB Charging Ports COMMUNICATIONS - Skynode S200 SATCOM - SATCOM Antenna Installation – STC SA11-85 |
|---|
Inspection Status
| Inspection Status | MAJOR CHECKS Aircraft maintained under a progressive C-check maintenance program. INSPECTION 40,000-Cycle – C-Check: Dec-2026 1CE05 Check – RH Wing: 32,490 hrs / Mar-2027 1CE06 Check – Cabin: 32,990 hrs / Aug-2027 PROPULSION / PROPELLERS LH Propeller – DAP0263: 7,192 hrs remaining RH Propeller – DAP0026: 860 hrs remaining Engine Gas Path Borescope – ENG 1: 33,000 hrs Engine Gas Path Borescope – ENG 2: 32,475 hrs LANDING GEAR NLG Drag Strut Overhaul: Mar-2027 LH MLG Shock Strut Overhaul: Dec-2027 RH MLG Shock Strut Overhaul: May-2028 |
|---|
Auxiliary Power Unit
| APU | Yes |
|---|
Range from base
Still-air range ring — type an aircraft to change it. Compare aircraft on the Range tool ›
Last flight
Actual flight path from FlightAware for C-GHQP. More flight tracking ›
