- Registered owner
- Southwest Aviation Specialties LLC
- Location
- Tulsa, OK
- Owner type
- LLC
- Serial number
- 1054
- Year built
- 2002
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- April 30, 2002
- Certificate issued
- July 14, 2015
- Expires
- July 31, 2028
- Mode S code
- A0D6EF
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada PT6A-6 model are included below.
On this page
Airworthiness directives that may apply · 70
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 |
| 1980 | 2 |
| 1991 | 1 |
| 1992 | 1 |
| 1995 | 1 |
| 1996 | 3 |
| 1997 | 4 |
| 1998 | 5 |
| 1999 | 2 |
| 2000 | 2 |
| 2001 | 2 |
| 2002 | 4 |
| 2003 | 3 |
| 2005 | 2 |
| 2007 | 2 |
| 2008 | 2 |
| 2009 | 2 |
| 2010 | 7 |
| 2011 | 4 |
| 2012 | 5 |
| 2013 | 2 |
| 2014 | 3 |
| 2015 | 1 |
| 2016 | 1 |
| 2017 | 1 |
| 2020 | 1 |
| 2022 | 3 |
| 2023 | 1 |
| 2024 | 2 |
| 2025 | 1 |
| 2026 | 3 |
See all 79 ADs
Information bulletins that may apply · 11
Advisory, not mandatory.
Airframe · Piaggio P180
SAIB CE-12-05Navigation: Water freezing in Pitot-Static SystemSAIB CE-03-42SAIB CE-01-40SAIB CE-01-35SAIB ACE-98-29SAIB ACE-96-07SAIB ACE-95-04Engine · Pratt & Whitney Canada PT6A-6 series
SAIB NE-15-21Fuel Injector NozzleSAIB NE-12-04Turbine/ Turboprop Engine: Reduction GearboxSAIB NE-06-34SAIB CE-03-24NTSB investigations
No NTSB investigations matched to N153SLMatched 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 Piaggio P180 aircraft
FAA incident reports
No FAA accident or incident reports matched to N153SLMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Piaggio P180 aircraft
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR V2JA0781054100212Switch · dirtyDESCRIPTION OF EVENT: CREW REPORTS UNCOMMANDED AUTOFEATHER ON SHORT FINAL. CLEANED & ADJUSTED AUTOFEATHER CAM SWITCHES IAW AMM 76-11-00. OP`S CHECK IAW AMM 71-00-00.SDR V2JA078L105492112Fcu · unserviceableIN FLIGHT AND ON SHORT FINAL, THE AUTOFEATHER SYSTEM WAS ATTEMPTING AN UNCOMMANDED FEATHER. PERFORMED ENGINE GROUND RUNS AND NOTED RT ENGINE LAGS IN THE AUTOFEATHER RANGE. R & R RT ENGINE FCU IAW EMM CH: 73-20-00. PERFORMED STATIC RIGGING, OPS, LEAKS AND FISDR V2JA2012091000001Engine · failedENGINE OIL LEAK. FIXED LEAK, RAN ENGINE, NO OIL LEAK WAS FOUND. DURING DEPARTURE, HEARD A NOISE IN AFT SECTION OF PLANE AND NOTICED A VIBRATION. SHORTLY AFTER, A SLOW DECREASE IN OIL PRESSURE ON ENGINE NR 1. BETWEEN 60 AND 70PSI, RAN ENGINE SECURING PROCSDR V2JA078L105482812Propeller · malfunctionedRIGHT PROPELLER UNCOMMANDED AUTOFEATHER PRIOR TO LANDING. ADJUSTED BETA VALVE AND INSPECTED BETA RING IAW AMM, CH: 76-10-00. OPS CHECKED GOOD, NO DEFECTS NOTED.SDR V2JA2012082200001Autofeather Sys · malfunctionedTHE CREW REPORTS THEY RECEIVED AN UNCOMMANDED AUTOFEATHER ON THE LT ENGINE ON THE DESCENT. LANDED SAFELY.SDR 2012FA0000137Elevator · misinstalledACFT WAS IN FACILITY FOR PAINT. FLIGHT CONTROLS REMOVED: PAINTED, BALANCED AND REINSTALLED. DUE TO THE ELEVATORS BEING MISLABELED, THE ELEVATORS WERE INSTALLED ON THE OPPOSITE SIDE (LT ELEV ON THE RT SIDE AND THE RT ELEV ON THE LT SIDE). THERE IS NO WARNING INSDR 2012F00013Autofeather Sys · malfunctionedAUTOFEATHER CYCLES DURING LANDINGSDR 2012F00012Autofeather Sys · malfunctionedAUTOFEATHER CYCLES DURING LANDING WITH LOW POWER SETTING.SDR 2010F00185Warning Light · illuminatedBAGGAGE DOOR LIGHT ILLUMINATED DURING CLIMB, PILOT REFFERED TO QRH AND SECURED NR1 ENGINE, PLANE RETURNED TO FIELD WITHOUT INCIDENT, NO EMERGENCY WAS DECLARED.SDR PAI5200642401Line · chafedDURING 3000 HOUR D-CHECK FOUND OIL SCAVENGE LINE PN 3040124 AT SCAVENGE PUMP CHAFED APPROX 50 PERCENT THROUGH BY CONTACT WITH CRIMP TYPE CLAMP THAT SECURES HEAT SLEEVE ON OIL COOLER FLEX LINE. SAME CONDITION FOUND ON BOTH LT AND RT ENGINES. INSTALLED NEW SCASDR PAI5200641881Stop · brokenDURING D CHECK (3000 HOUR INSPECTION) FOUND RUDDER STOP LOCATED AT BOTTOM OF RUDDER BROKEN IN TWO. BREAK OCCURRED AT SCREW HOLES USED TO ATTACH WEAR STRIP TO RUDDER STOP. SMALL AREA OF METAL EXISTS AROUND THE SCREW HOLES, SUGGEST REDESIGN OF THIS PART.SDR PAI52006S4188Tube · chafedDURING D-CHECK (3000 HOUR INSPECTION) FOUND WING LEADING EDGE ANTI-ICE PLUMBING CHAFFED 50 PERCENT OF WALL THICKNESS BY LEADING EDGE TEMP SENSOR BRACKET.
STCs that may be installed · 118
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Piaggio P180
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA02279ATInstallation of a Boom Beam bulb, starter, and ballastSTC SA04837NYInstallation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights