N711MPShort Bros SD3-60
This N-number isn't registered right now. Below is its last known registration, canceled Oct 23, 2018.
Safety record in brief:No NTSB accidents or incidents since 19821 AD may apply5 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Great Lakes Turbines INC
- Owner type
- Corporation
- City, state
- Franksville, WI
- Certificate issued
- May 14, 2012
- Canceled
- Oct 23, 2018
- Airworthiness
- Standard · Transport
- Airworthiness date
- Sep 17, 1986
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Short Bros
- Model
- SD3-60
- Serial number
- SH3698
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 39
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A980E5
Engine
- Make and model
- P&W Canada Pt6a-60a
- Type
- Turbo-prop
- Power
- 1050 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2012 – 2018Great Lakes Turbines INCFranksville, WI
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (1)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2002-23-13 | Pratt & Whitney Canada PT6A Series Turboprop Engines | Dec 31, 2002 | Engine (PT6A-60A)Only with: Engines with turbine exhaust ducts P/N 3012290, 3031988, 3032117, 3035784, 3035786, 3105890-01, 3112167-01, or 3111780-01 installed. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (5)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Engine fuel and control · wire · brokenOct 5, 2003
ABORTED TAKEOFF DUE TO LT ENGINE NO FUEL FLOW INDICATION. AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED, FOUND BROKEN WIRE AT FUEL FLOW TRANSMITTER. WIRE WAS REPAIRED AND AIRCRAFT RETURNED TO SERVICE. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · selector valve · lack of lubeSep 28, 2001
MAIN LANDING GEAR INDICATORS STAYED GREEN ON GEAR UP SELECTION, ACCOMPLISHED NORMAL AND ABNORMAL CHECKLIST. THE PROBLEM PERSISTED. FLIGHT RETURNED TO HOME BASE. NO OTHER DIFFICULTIES OCCURRED THROUGHOUT THE FLIGHT. FURTHER INSPECTION FOUND 3 WAY SELECTOR VALVE ASSY NOT SEATED PROPERLY. LUBED…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · selector valve · lack of lubeSep 28, 2001
MAIN LANDING GEAR INDICATORS STAYED GREEN ON GEAR UP SELECTION. ACCOMPLISHED NORMAL AND ABNORMAL CHECKLIST. THE PROBLEM PERSISTED. FLIGHT RETURNED TO HOME BASE. NO OTHER DIFFICULTIES OCCURRED THROUGHOUT THE FLIGHT. FURTHER INSPECTION FOUND 3 WAY SELECTOR VALVE ASSY NOT SEATED PROPERLY. LUBED…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 5 reportsShow fewer reports
- Hydraulic power · hydraulic system · contaminatedApr 13, 2001
FLT 3825 - DECLARED EMERGENCY AND LANDED SAFE. AFTER BOTH HYD WARNING LIGHT ON CWP ILLUMINATED. CHECKED HYD SYSTEM FOUND OUT LOTS OF AIR IN THE SYSTEM. COMPLIED WITH BLEEDING AND COMPLETED HYD SYSTEM REPLENISHMENT OBSERVED HYD SYSTEM. NO FAULT NOTED. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Hydraulic power · pipe · rupturedJun 16, 1998
HYDRAULIC PRESSURE FAILED IN-FLIGHT. HYDRAULIC FLUID LOSS DUE TO .50 INCH RUPTURE OF PIPE. P/N SD3-73-1019XA REQUIRING SHUT DOWN OF HYDRAULIC PUMPS AND RETURN TO FIELD. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026