# N292SW: 1996 Embraer EMB-120ER, registration cancelled 2020-10-31 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 31, 2020 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Embraer EMB-120ER](https://openairdocs.org/model/embraer-emb-120er) (registry code 3260203) - Engine: [Pratt & Whitney Canada PW118](https://openairdocs.org/engine/pratt-whitney-canada-pw118) (registry code 52116) - Data sheets: [TCDS A31SO](https://openairdocs.org/tcds/A31SO), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs) - Serial number: 120.319 - Year built: 1996 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: August 23, 1996 - Certificate issued: July 14, 2017 - Last registry action: July 14, 2017 - Mode S code: A2FE8D - Owner when cancelled: [Aerovision Engine Services LLC](https://openairdocs.org/faa-owner/AEROVISION%20ENGINE%20SERVICES%20LLC) - Location: [Muskegon, MI](https://openairdocs.org/faa-place/MI/Muskegon) - Owner type: LLC - Owner's area on the map: 43.1800° N, 86.2868° W: Placed by OpenAirDocs at the center of ZIP code 49441, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N292SW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=292SW - Page: https://openairdocs.org/deregistered/N292SW-2020-10-31 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Embraer EMB-120ER: https://openairdocs.org/model/embraer-emb-120er.md ## Service difficulty reports (84, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWIA201438397](https://openairdocs.org/sdr/SWIA201438397), Jun 26, 2014: LENS. MISSING. LEFT EMERGENCY EXIT LOWER LIGHT IS MISSING THE LENS. INSTALLED LT EMERGENCY EXIT LOWER LIGHT LENS IAW AMM. - [SDR SWIA2014061338162](https://openairdocs.org/sdr/SWIA2014061338162), Jun 1, 2014: SIGN. DETACHED. EMERGENCY EXIT SIGN NEXT TO THE EMERGENCY EXIT AT 9C IS BROKEN OFF. REPAIRED AND REINSTALLED EMERGENCY EXIT SIGN AT 9C. (2014NM060066) - [SDR SWIA201436367](https://openairdocs.org/sdr/SWIA201436367), Feb 18, 2014: PROXIMITY SENSOR. OUT OF ADJUST. LT MLG DID NOT COME UP ON FIRST RETRACTION ATTEMPT, CYCLED THE HANDLE & THE GEAR CAME UP. FLT 5344 ADJUSTED THE LT MLG UPLOCK PROX SENSOR IAW AMM. CW GEAR SWING - [SDR SWIA201435919](https://openairdocs.org/sdr/SWIA201435919), Jan 6, 2014: LIGHT. DETACHED. FLOOR EMERGENCY LIGHT ROW 2 DOES NOT ILLUMINATE. FLT 6310 REINSTALLED BULB, OPERATIONS CHECKED GOOD AT THIS TIME. - [SDR SWIA201335200](https://openairdocs.org/sdr/SWIA201335200), Nov 2, 2013: LIGHT. INOPERATIVE. EMERGENCY LIGHT AT ROW 9 IS BURNED OUT. FLT 5344 RELAMPED. - [SDR SWIA201333038](https://openairdocs.org/sdr/SWIA201333038), Feb 28, 2013: SKIN. CRACKED. DAMAGE AT FS STA 15370.0 LEFT FUSELAGE EXTERNAL SKIN BELOW AND AFT OF CARGO DOOR CUT OUT AREA, CRACKED. (C-CHECK) REPAIRED FUSELAGE REINFORCEMENT AND SKIN BY ME - [SDR SWIA201232451](https://openairdocs.org/sdr/SWIA201232451), Dec 22, 2012: UNKNOWN. MALFUNCTIONED. DEPARTING PDX ALL 3 LANDING GEAR DID NOT RETRACT UNTIL 2400 FT. AT THAT TIME GEAR RETRACTED NORMALLY. (FLT 5379) PERFORMED SEVERAL GEAR SWINGS WITH NO DEFECTS N - [SDR SWIA201231922](https://openairdocs.org/sdr/SWIA201231922), Sep 29, 2012: UNKNOWN. ODOR. BURNT PACK SMELL ON ENGINE BLEED. (FLT 5405) INSPECTED LEFT PACK, NO DEFECTS NOTED. RAN LEFT PACK, NO SMELL NOTED. - [SDR SWIA201231180](https://openairdocs.org/sdr/SWIA201231180), Jun 27, 2012: LIGHT. INOPERATIVE. FLOOR LEVEL EMERGENCY LIGHT NEAR MAIN CABIN DOOR OUT. (FLT 5293) RELAMPED EMERGENCY LIGHT. - [SDR SWIA201231117](https://openairdocs.org/sdr/SWIA201231117), Jun 23, 2012: SEQUENCE VALVE. FAILED. THE RED IN TRANSIT LIGHTS REMAINED ON WHEN LANDING GEAR LEVER WAS PLACED IN THE UP POSITION AND THE RIGHT MAIN GEAR DOWN AND LOCKED. (FLT 5616) REPLACED RIGHT O - [SDR SWIA201126640](https://openairdocs.org/sdr/SWIA201126640), Jun 27, 2011: LIGHT. INOPERATIVE. FORWARD CABIN EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT. - [SDR SWIA201126350](https://openairdocs.org/sdr/SWIA201126350), May 25, 2011: SIGN. BROKEN. EMERGENCY EXIT SIGN AT RIGHT SIDE OF ROW 6 BROKEN. (FLT 6379) REPLACED EMERGENCY LIGHT ASSEMBLY. - [SDR SWIA201025302](https://openairdocs.org/sdr/SWIA201025302), Dec 3, 2010: WIRE. LOOSE. EMERGENCY FLOOR RED LIGHT NOT WORKING AT ROW 1. (FLT 6818) RE-SECURED WIRE AT FLOOR LEVEL EMERGENCY LIGHT. - [SDR SWIA201025159](https://openairdocs.org/sdr/SWIA201025159), Nov 1, 2010: HOT WATER POT. SMOKE. AFT HOT JUG PRODUCING SMOKE. (FLT 6181) REPLACED HOT LIQUID CONTAINER. - [SDR SWIA201024421](https://openairdocs.org/sdr/SWIA201024421), Jun 14, 2010: REGULATOR. FAILED. LEFT ENGINE SHUT DOWN DUE TO BLEED LEAK INDICATION. (FLT 6687) REPLACED DE-ICE SYSTEM PRESSURE REGULATOR. P/N 38E96-6A, S/N OFF RF-1888. - [SDR SWIA200923167](https://openairdocs.org/sdr/SWIA200923167), Nov 3, 2009: SPLICE. BURNED. COCKPIT LEFT SIDE CURRENT SENSOR SPLICE BURNT. (C-CHECK) REPAIRED SPLICE PER WMM. - [SDR SWIA200923166](https://openairdocs.org/sdr/SWIA200923166), Oct 31, 2009: RIB. CRACKED. RIB CRACKED AT RIGHT INBOARD AND OUTBOARD UPPER NACELLE. (C-CHECK) REPLACED RIBS PER SRM. - [SDR SWIA200923161](https://openairdocs.org/sdr/SWIA200923161), Oct 30, 2009: FITTING. CRACKED. RIGHT NACELLE WHEEL WELL INBOARD AREA VERTICAL FRAME FITTING CRACKED. (C-CHECK) REPLACED FITTING PER SRM. - [SDR SWIA200923165](https://openairdocs.org/sdr/SWIA200923165), Oct 27, 2009: SPAR CAP. CRACKED. LEFT WING FORWARD UPPER AUX SPAR CAP CRACKED. (C-CHECK) REPAIRED PER ETD. - [SDR SWIA200923169](https://openairdocs.org/sdr/SWIA200923169), Oct 26, 2009: WIRE. BURNED. WIRE FROM CONTACTOR K0027 TO RCCB BURNT. (C-CHECK) REPLACED WIRE PER WMM. - [SDR SWIA200923172](https://openairdocs.org/sdr/SWIA200923172), Oct 25, 2009: CHANNEL. CRACKED. RIGHT NACELLE CHANNEL CRACKED. (C-CHECK) REPLACED CHANNEL PER SRM. - [SDR SWIA200923170](https://openairdocs.org/sdr/SWIA200923170), Oct 25, 2009: FITTING. CRACKED. LEFT NACELLE WHEEL WELL INTERNAL VERTICAL FITTING CRACKED. (C-CHECK) REPLACED FITTING PER SRM. - [SDR SWIA200923168](https://openairdocs.org/sdr/SWIA200923168), Oct 25, 2009: ANGLE. CRACKED. ANGLE CRACKED AT LEFT SIDE OF COCKPIT, BELOW FLOOR. (C-CHECK) REPLACED ANGLE PER SRM. - [SDR SWIA200923163](https://openairdocs.org/sdr/SWIA200923163), Oct 25, 2009: DOOR FRAME. CRACKED. PASSENGER DOOR FRAME CRACKED. (C-CHECK) REPLACED FRAME PER SRM. - [SDR SWIA200923162](https://openairdocs.org/sdr/SWIA200923162), Oct 24, 2009: FRAME. CRACKED. LEFT NACELLE FRAME 1 INBOARD SIDE CRACKED. (C-CHECK) REPLACED LEFT NACELLE FRAME PER SRM. - [SDR SWIA200923171](https://openairdocs.org/sdr/SWIA200923171), Oct 22, 2009: BELLCRANK. CORRODED. RIGHT AILERON BELLCRANK CORRODED. (C-CHECK) REPLACED RIGHT AILERON BELLCRANK PER AMM. - [SDR SWIA200923164](https://openairdocs.org/sdr/SWIA200923164), Oct 21, 2009: STRINGER. CORRODED. FUSELAGE STRINGERS 18 AND 19 CORRODED. (C-CHECK) REPAIRED AND REPLACED PER SRM. - [SDR SWIA200922868](https://openairdocs.org/sdr/SWIA200922868), Oct 5, 2009: WIRE. BROKEN. OVERHEAD EMERGENCY LIGHT ABOVE 9C INOP. (FLT 6254) REPAIRED BROKEN WIRE. - [SDR SWIA200922513](https://openairdocs.org/sdr/SWIA200922513), Aug 31, 2009: SIGNAL COND UNIT. FAULTY. LEFT PROP AUTO-FEATHERED UNCOMMANDED. (FLT 6181) REPLACED LEFT ENGINE TORQUE SIGNAL CONDITIONER. - [SDR SWIA200922496](https://openairdocs.org/sdr/SWIA200922496), Aug 25, 2009: SIGNAL COND UNIT. FAULTY. LEFT PROP AUTO-FEATHERED UNCOMMANDED. (FLT 6192) REPLACED TORQUE SIGNAL CONDITIONER. - [SDR SWIA200922428](https://openairdocs.org/sdr/SWIA200922428), Aug 22, 2009: WIRE. BROKEN. EMERGENCY LIGHTS EXIT SIGN INOP. (FLT 6110) REPAIRED BROKEN WIRE. - [SDR SWIA200922367](https://openairdocs.org/sdr/SWIA200922367), Aug 16, 2009: HMU. OUT OF RIG. LEFT PROPELLER SPEED INCREASED UNCOMMANDED ON TAXI. (FLT 6630) RIGGED LEFT HMU. - [SDR SWIA200922123](https://openairdocs.org/sdr/SWIA200922123), Jul 10, 2009: DOOR. LACK OF LUBE. MAIN CABIN DOOR HARD TO OPEN. (FLT 6357) INSPECTED AND LUBED MAIN CABIN DOOR. - [SDR SWIA200921625](https://openairdocs.org/sdr/SWIA200921625), May 12, 2009: BULB. LOOSE. FLT 6232 - EMERGENCY LIGHT AT THE FORWARD DOOR INOP. REPOSITIONED BULB. - [SDR SWIA200921624](https://openairdocs.org/sdr/SWIA200921624), May 11, 2009: BATTERY PACK. DISCHARGED. FLT 6249 - MULTIPLE EMERGENCY EXIT SIGN LIGHTS OUT IN MAIN CABIN. REPLACED FORWARD EMERGENCY BATTERY PACK. - [SDR SWIA200921139](https://openairdocs.org/sdr/SWIA200921139), Mar 11, 2009: SOCKET. FAILED. FLT 5406 - FORWARD FLOOR RED EMERGENCY LIGHT STRIP INOP. REPLACED SOCKET. - [SDR SWIA200921072](https://openairdocs.org/sdr/SWIA200921072), Feb 25, 2009: ROD END. WORN. FLT 1005 - LEFT MAIN GEAR DID NOT RETRACT ON CLIMB UNTIL CYCLED A SECOND TIME. INSTALLED NEW ROD END AND LEVER ASSEMBLY ON LEFT MAIN GEAR ACTUATOR, P/N 19502-00 - [SDR SWIA200820195](https://openairdocs.org/sdr/SWIA200820195), Oct 19, 2008: BULB. BROKEN. FLT 5557 - EXIT SIGN AT MAIN CABIN DOOR, COVER MISSING AND BULBS BROKEN. REPLACED EXIT SIGN. - [SDR SWIA200819883](https://openairdocs.org/sdr/SWIA200819883), Apr 5, 2008: ROD END. CORRODED. LT AND RT ELEVATOR UPPER BELLCRANK ROD ENDS SHOW SIGNS OF CORROSION. (FOUND AT C-CHECK) REPLACED THE LT AND RT ELEVATOR ROD END ASSEMBLIES IAW AMM 27-00-00. - [SDR SWIA200819882](https://openairdocs.org/sdr/SWIA200819882), Apr 5, 2008: BUTTSTRAP. CORRODED. BUTT STRAP UNDER LAV IS CORRODED. (FOUND AT C-CHECK) REPLACED BUTT STRAP IAW EMB 120, SRM 51-10-02, PAGE 3 AND 51-40-02. - [SDR SWIA200819356](https://openairdocs.org/sdr/SWIA200819356), Mar 5, 2008: RCCB. MALFUNCTIONED. FLT 5742 - SMOKE IN COCKPIT WHILE AT THE GATE. REPLACED RCCB FOR LEFT GROUND COOLING FAN. OPS CHECK GOOD. - [SDR SWIA200718920](https://openairdocs.org/sdr/SWIA200718920), Nov 29, 2007: LIGHT. INOPERATIVE. EMERGENCY LIGHT OVER PAX DOOR IS INOP. REPLACED EMERGENCY LIGHT. OPS CHECKS GOOD. - [SDR SWIA200718760](https://openairdocs.org/sdr/SWIA200718760), Oct 6, 2007: BULB. ODOR. FLT 5592 - THE ODOR OF SMOKE FILLED THE COCKPIT AND C/B A30 POPPED. REPLACED COURTESY LIGHT BULB. OPS CHECK GOOD. - [SDR SWIA200717789](https://openairdocs.org/sdr/SWIA200717789), Feb 1, 2007: BATTERY. DISCHARGED. ALL EMERGENCY LIGHTS AFT OF ROW 8 INOP. REPLACED THE AFT EMERGENCY LIGHT BATTERY IAW AFM 33-50-02. OPERATIONAL CHECKS GOOD. - [SDR SWIA200616927](https://openairdocs.org/sdr/SWIA200616927), Jul 25, 2006: SIGN. DEFECTIVE. LIGHTED EXIT SIGN AT FLOOR LEVEL SEAT 6C CAME APART. REPLACED EMERGENCY EXIT SIGN FIXTURE AT ROW 6. OPERATIONAL CHECKS GOOD. - [SDR SWIA200616833](https://openairdocs.org/sdr/SWIA200616833), Jun 20, 2006: SEAT TRACK. CORRODED. FOUND CORROSION IN LEFT FLOOR SEAT TRACK. REMOVED AND REPLACED SECTIONS OF LEFT FLOOR SEAT TRACKS IAW 53-20-10 SRM AND 51-21-04 CPM. - [SDR SWIA200616832](https://openairdocs.org/sdr/SWIA200616832), Jun 20, 2006: STRINGER. CRACKED. RIGHT INBOARD WING, LOWER FRONT STRINGER FORWARD OF NR 2 FUEL PANEL CRACKED. REPAIRED STRINGER FORWARD OF NR 2 FUEL PANEL AT RIGHT INBOARD WING IAW SRM120 57-20 - [SDR SWIA200616831](https://openairdocs.org/sdr/SWIA200616831), Jun 20, 2006: RIB. CRACKED. CRACK FOUND AT LEFT NACELLE INBOARD UPPER RIB BELOW EXHAUST MOUNT. REPLACED LEFT NACELLE INBOARD UPPER RIB IAW SRM 120 51-10-02 PG 3 SEC 3A. - [SDR SWIA200616761](https://openairdocs.org/sdr/SWIA200616761), Jun 4, 2006: WINDSHIELD. UNKNOWN. LOST PRESSURIZATION IN FLIGHT, DIVERTED TO FRESNO. REMOVED AND REPLACED LEFT WINDSHIELD IAW EMB MM 56-10-01 AND RII 56-200-1000. FUNCTIONAL CHECKS GOOD. - [SDR SWIA200616095](https://openairdocs.org/sdr/SWIA200616095), Jan 3, 2006: LIGHT. BURNED. OVERHEAD AISLE LIGHT OVER SEAT 10A MELTING HEAD LINER AND CAUSES LARGE BURN MARKS AND SMOKE (VERY FAINT). REPLACED CABIN LIGHT FIXTURE ASSEMBLY FOR SEAT 10A. OP All 84: https://openairdocs.org/deregistered/N292SW-2020-10-31/reports.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.