- Registered owner
- Acc Integrated Services Inc
- Location
- Milwaukee, WI
- Owner type
- Corporation
- Serial number
- SH3653
- Year built
- 1984
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, transport
- Airworthiness date
- June 8, 1995
- Certificate issued
- July 17, 1995
- Expires
- November 30, 2027
- Mode S code
- A0CE19
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney PT6A model are included below.
On this page
Airworthiness directives that may apply · 26
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1968 | 1 |
|---|---|
| 1969 | 1 |
| 1970 | 1 |
| 1975 | 1 |
| 1977 | 1 |
| 1978 | 2 |
| 1980 | 2 |
| 1986 | 1 |
| 1990 | 1 |
| 1992 | 1 |
| 1994 | 1 |
| 1995 | 1 |
| 1997 | 1 |
| 2001 | 1 |
| 2002 | 1 |
| 2005 | 1 |
| 2011 | 2 |
| 2012 | 1 |
| 2014 | 2 |
| 2015 | 1 |
| 2016 | 1 |
| 2022 | 1 |
| 2024 | 1 |
See all 28 ADs
Information bulletins that may apply · 5
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N151CAMatched 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 · 8
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 19940518022579IFcd/Prec Ldg From Cruise · Montoursville, PALeft engine oil presure dropped. Shut down. Power turbine failed. Evidence compressor rub.Incident 19930917046649INormal Cruise · Charlottesville, VAOdor in cockpit. Pilots went on oxygen. Landed safely at destination. Found stain bag in forward compartment.Incident 19920614028839IFcd/Prec Ldg From Cruise · Wilkes Barre Sc, PAPropeller went to underspeed then overspeed condition. Secured engine. Removed governor and proximity control box.Incident 19920613026949IFcd/Prec Ldg From Cruise · Middletown, PAUnable to maintain propeller synch on NR2 engine. Feathered engine. Replaced fuel control and HP pump.Incident 19901214063209IForced/Precautionary Landing · Middletown, PAAircraft out of trim on takeoff. Returned. Landed safely. Replaced bearings in rudder bellcrank. Rerigged trim tab.Incident 19900802042709IFcd/Prec Ldg From Cruise · Middletown, PAFire detector light in forward baggage compartment. Fire bottle discharged. No fire. Replaced faulty detector.Incident 19880605041859IForced/Precautionary Landing · Philadelphia, PAUnable to retract flaps on climb out. Returned to airport. Found left flap signaling cable broken.Incident 19880105012829IGround Taxi, Other Airplane · State College, PAGear problem. Returned. Lost brakes and steering. Veered off taxiway. Found faulty system accumulator.
Reports on N151CA not matched to an aircraft · 3
They name N151CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Incident 19810611045229IBeech 99 · Middletown, PADuring climb had fire warning for left engine due to sensor malfunction.Incident 19810211007709IBeech 99A · Coraopolis, PAEngine fire during taxi. Maintenance found a ruptured fuel line on dukes epa fuel recovery modification.Incident 19800129020239IBeech 99 · Harrisburg, PADuring training flight one engine shut down. Unable to restart due to failure of glow plugs.
Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DATA2020031601Switch · out of adjustIN CLIMB AT 3500 FEET WHEN PILOTS REDUCED THROTTLE THE RIGHT PROPELLER WENT INTO FEATHER. QRH PROCEDURES FOLLOWED, EMERGENCY DECLARED AND AIRCRAFT RETURNED TO BASE (SJU). SUBSEQUENT MAINTENANCE INVESTIGATION FOUND AUTOFEATHER MICRO-SWITCHES OUT OF ADJUSTMENT. SDR DATA2015072101Pump · leakingON DESCENT HYD RT CWP LIGHT ILLUMINATED. HYD PANEL SHOWED RESERVOIR CONTENTS, UPPER RED. LT & RT FLUID TEMP 70 DEG, MAIN SYS 3000 PSI. SHORTLY THEREAFTER BOTH HYD LT & HYD RT CWP WARNING LIGHTS ILLUMINATE. HYD PANEL SHOWED RESERVOIR CONTENTS LOWER RED. FLSDR DATA20140923002Flex Hose · leakingAFTER TAKEOFF CREW EXPERIENCED LT ENG SURGE. RETURNED SAFELY TO POINT OF ORIGIN. FOUND TO BE CAUSED BY ENG P2.5 BLEED AIR LEAK. REPLACED P2.5 FLEXIBLE HOSE.SDR DATA20130425002Probe · out of toleranceIN CRUISE, CREW OBSERVED A RT LOW FUEL PRESSURE ANNUNCIATION FOLLOWED BY RT ENGINE FLAMEOUT. DECLARED AN EMERGENCY AND COMPLETED AN UNEVENTFUL SINGLE ENGINE APPROACH AND LANDING. DISCOVERED AFT FUEL TANK QTY SYS WAS INDICATING 400 LBS WHEN EMPTY AND ENGINE FSDR DATA20130307001Bleed Valve · stickingON APPROACH, THE CREW INITIATED A GO-AROUND. UPON INCREASING THRUST, THE CREW EXPERIENCED SURGING AND TORQUE FLUCTUATION ON THE RIGHT ENGINE. FOLLOWING QRH PROCEDURES THE CREW DECLARED AN EMERGENCY, SHUTDOWN THE AFFECTED ENGINE, AND COMPLETED AN UNEVENTFUL SSDR DATA200700007Engine · failedN151CA DEPARTED MKE AT 00:00 ON A REPOSITION FLIGHT TO DNV. UPON REACHING CRUISE (5000FT) ALTITUDE, CRUISE POWER WAS SET BY THE FIRST OFFICER AS THE CAPTAIN WAS THE PILOT FLYING. SHORTLY AFTER CRUISE POWER WAS SET THE RIGHT ENGINE FAILED. BOTH TORQUE AND ITSDR DATA200700006Engine · surgesTHE CREW WAS DEPARTING CHARLESTON, SC, THE PILOT SMOOTHLY ADVANCED THE THROTTLES TO ALLOW THE PROPS TO SPIN UP TO MAX RPM, BEFORE SETTING TAKEOFF POWER. THE LEFT ENGINE STARTED SURGING AND BACKFIRING WHILE THE PILOT ADVANCED THE THROTTLES. THE COPILOT CALLESDR 2001F00263Bleed Valve · malfunctionedA/C DEPARTED CHEYENNE, WY, AFTER FUEL TOP OFF AND CLIMBING OUT THE LT ENGINE TORQUE DROPPED TO 2500 NR AND NG DROPPED 3 PERCENT. THE PILOT INCREASED THE POWER LEVERS, THE TORQUE ROSE AND THEN SETTLED BACK TO 2500 NR. THE CREW MADE A PRECAUTIONARY ENGINE SHUT DSDR 20001129SH008Wheel · failedUPON LANDING IN MLI, THE LEFT MAIN WHEEL BLEW OUT. THE MLI MECHANIC REMOVED AND REPLACED THE LT MAIN WHEEL ASSY. THERE WAS NO DAMAGE TO THE BRAKE AND STRUT. OPS CHECKED GOOD. (X)SDR 96ZZZM1063Microswitch · out of adjustAT CVG, CAPTAIN REPORTED THAT THE LEFT GENERATOR WOULD NOT COME ON LINE. AT THE REQUEST OF MAINTENANCE, ANOTHER ATTEMPT WAS MADE, AT THIS TIME THE GENERATOR CAME ON LINE AND REMAINED ON LINE. PILOT ALSO REPORTED THAT THIS HAD BEEN A PRIOR PROBLEM. AIRCRAFT
STCs that may be installed · 57
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 PT6A series
STC SE12225ACThis STC will incorporate P&W 1700 rpm propeller reduction gearbox on P&WC engines to allow 1700 rpm propeller installationSTC SE00010ENInstructions for Continued Airworthiness for the PT6A-25, and, -25A engine models that define specific maintenance tasks and their associated maintenance schedules, and that are used as a supplement to the applicable Pratt & Whitney Canada manuals.STC SE000010ENInstructions for Continued Airworthiness for the PT6A-25 and PT6A-25A engine models that define specific maintenance tasks and their associated maintenance schedules, and that are used as a supplement to the applicable Pratt & Whitney Canada manuals.