1988 DEHAVILLAND DHC-8-102
Starts from the median asking price of 163 comparable Turboprop listings ($1,025,000), then adjusts for:
- Year +7 vs comparable listings +10.5%
- Airframe time +45,202 hr vs comps -20.0%
- No Modern GPS navigator (60% of comps have one) -2.7%
- No Autopilot (61% of comps have one) -1.1%
- No ADS-B (57% of comps have one) -1.5%
Shown as a range. An estimate from asking-price comparables and FAA supply data — not an appraisal.
Overview
| Make / Model | DeHavilland DHC-8-102 |
|---|---|
| Type | Turboprop |
| Airframe time | 53,531 hrs |
| Engine time | 52,868 SNEW |
| Prop blades | 4 |
| Avionics / Traffic (TCAS / TAS) | TCAS II |
| Annual | April 2025 |
| Airworthy | Yes |
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 | 1988 |
|---|---|
| Manufacturer | DEHAVILLAND |
| Model | DHC-8-102 |
| Condition | Used |
Airframe
| Total Time | 53,531 |
|---|---|
| Total Landings | 57,001 |
| Max Takeoff Weight | 34,500 lb |
Engine 1
| Engine 1 Make/Model | PRATT & WHITNEY PW120A |
|---|---|
| Engine 1 Time | 52,868 SNEW |
| Engine 1 TBO | 8000 |
| Hot Section Time 1 | 2,216 |
Engine 2
| Engine 2 Make/Model | PRATT & WHITNEY PW120A |
|---|---|
| Engine 2 Time | 45,512 SNEW |
| Engine 2 TBO | 8000 |
| Hot Section Time 2 | 1,072 |
Props
| Prop 1 Manufacturer | HAMILTON STANDARD |
|---|---|
| Prop 1 Model | 14SF-7 |
| Prop 2 Manufacturer | HAMILTON STANDARD |
| Prop 2 Model | 14SF-7 |
| Number of Blades | 4 |
Avionics
| Avionics/Radios | HF TCAS II |
|---|
Interior
| Number of Seats | 37 |
|---|---|
| Configuration | Passenger |
| Galley Configuration | Forward |
| Lavatory Configuration | Forward |
Inspection Status
| Inspection Status | Last C-check April 2025. |
|---|---|
| Airworthy | Yes |
Auxiliary Power Unit
| APU | Yes |
|---|
Range from base
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