- Registered owner
- Acc Integrated Services Inc
- Location
- Milwaukee, WI
- Owner type
- Corporation
- Serial number
- SH 3601
- Year built
- 1982
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, transport
- Airworthiness date
- December 28, 1982
- Certificate issued
- December 3, 1997
- Expires
- February 28, 2029
- Mode S code
- A40DDD
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 1
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
Engine · Pratt & Whitney Canada PT6A-65R
AD 97-04-12Compressor Bleed-off ValveInformation bulletins that may apply · 2
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N360SAMatched 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 Short Bros SHORTS SD3-60 aircraft
FAA incident reports · 6
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20081231854079IApproach · Peoria, IL(-23) Incident nr [privacy data omitted]. On approach to pia, crew selected gear down and got a visual in-transit indication on the left gear. Aircraft landed without incident at pia.Incident 19940728031769IRoll-Out (Fixed Wing) · Reading, PANarrative: while landing on runway 31 at rdg, the aircraft struck a deer causing minor damage to the stub wing. CFR was called out; however, it was not utilized. The aircraft taxied to the gate under its own power. Submission of this report closes this…Incident 19930520019099IOther Ground Ops · New York, NYFuel truck struck the parked aircraft. Was moving away without the use of a guide person.Incident 19930422016249IFcd/Prec Ldg From Cruise · Middletown, PASmoke in cockpit. Diverted to Middletown. Safe landing. Found "acm" blowing oil into hot bleed lines."acm" replacedIncident 19920701032229ITo Aborted (Fixed Wing) · Philadelphia, PARight engine would not reach top before temperature limits. Aborted. Found a defective pt vane ring.Incident 19910108061029ITo Aborted (Fixed Wing) · Reading, PAHydraulic warning lights on takeoff roll. Aborted.
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DATA2015101501Pitot Line · blockedUPON TAKEOFF ROLL & ACCELERATION, AT APPROX 89 KNOTS, THE FIRST OFFICER NOTICED HIS AIRSPEED INDICATOR WAS INDICATING 0. PIC RETARDED POWER LEVERS TO IDLE & ABORTED THE TAKEOFF. ACFT RETURNED TO BLOCK. UPON INSPECTION, TECHNICIAN CLEARED PITOT TUBE OF A NOTSDR DAT2005F00005Tire · failedDURING DEPARTURE ON TAKEOFF ROLL, ACCELERATION WAS NORMAL THROUGH 85 KNOTS, FLIGHT CREW HEARD A NOISE OUTSIDE OF THE AIRCRAFT. AC STARTED TO PULL TO LT AND THERE WAS CORRECTION MADE TO STRAIGHTEN THE AIRCRAFT. FLIGHT CREW NOTICED DURING THE CORRECTION THE ACSDR 2004F00313Hose · crackedUPON BRAKE APP PRIOR TO MLG RETRACTION, FO HEARD A THUD. RETRACTED MLG NOTICED RT HYD IND ON CWP PRIOR TO ACCELERATION ALT. OBSERVED FALLING IND & HYD QTY GAUGE & 0 PRESSURE ON MAIN SYS PRESS GAUGE. CONTINUED TO CLIMB TO 2000 MSL. NORMAL EXTENSION FAILED. CSDR 20000517SH002Smoke Detector · false indicationDURING FLIGHT, THE ''SMOKE FWD'' LIGHT CAME ON. THE CHECKLIST WAS FOLLOWED AND THE ENTIRE CONTENTS OF THE COCKPIT EXTINGUISHER WAS EMPTIED INTO FWD COMPARTMENT. THE LIGHT EVENTUALLY WENT OUT. INSPECTION AFTER LANDING REVEALED NO EVIDENCE OF FIRE/ SMOLDERING
STCs that may be installed · 6
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Engine · Pratt & Whitney Canada PT6A-65R
STC SE00014ENInstallation of the Pratt & Whitney Engine Services, Inc. CrossCheck Engine Monitor Kit P/N HUMS-K-071-1, Rev. A on the specified PT6A engine models and kit P/N HUMS-K-071-2 on the specified A250 engine models.STC SE00020ENInstallation of the Pratt & Whitney Engine Services, Inc. TrendCheck/ TrendCheck Plus Engine Monitor Kit P/N TREND-K-010-1STC SE8652SWInstallation of a flexible hose from the Propeller Primary Governor to the Fuel Control Unit.STC SE01805NYInstallation of Fuel Nozzle Adapters using studs and nuts.STC SE09257SCConvert P&W Engine Models PT6A-15AG, -27, and -28, into PT6A-34 configuration.STC SE659NEInstallation of oil tank filler neck check valve, P/N TSA-76A.