# N584SW: 1999 Embraer EMB-120ER

- Status: Valid registration
- Airframe: [Embraer EMB-120ER](https://openairdocs.org/model/embraer-emb-120er) (registry code 3260203, 32 seats)
- 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) (Embraer S.A.), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (Pratt & Whitney Canada Corp.) (OpenAirDocs)
- Serial number: 120352
- Year built: 1999
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: July 29, 1999
- Certificate issued: March 5, 2019
- Expires: March 31, 2029
- Mode S code: A78669
- Registered owner: [Berry Aviation Inc](https://openairdocs.org/faa-owner/BERRY%20AVIATION%20INC)
- Location: [San Marcos, TX](https://openairdocs.org/faa-place/TX/San%20Marcos)
- Owner type: Corporation
- Owner's area on the map: 29.8817° N, 97.9848° W: Placed by OpenAirDocs at the center of ZIP code 78666, within about 8 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=584SW
- Page: https://openairdocs.org/aircraft/N584SW

From the FAA registry file of October 21, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 61 in force

### Matched by airframe (Embraer EMB-120ER)

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2025-02-09](https://openairdocs.org/ad/2025-02-09): Fuselage · Embraer EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Mar 18, 2025
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2017-10-04](https://openairdocs.org/ad/2017-10-04): Landing Gear · Embraer EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Jun 29, 2017
- [AD 2011-08-09](https://openairdocs.org/ad/2011-08-09): Fuel · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Aug 1, 2011
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2010-19-04](https://openairdocs.org/ad/2010-19-04): Airborne Auxiliary Power · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Oct 27, 2010
- [AD 2008-04-18 R1](https://openairdocs.org/ad/2008-04-18-R1): Fuel · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Nov 16, 2009
- [AD 2009-15-18](https://openairdocs.org/ad/2009-15-18): Fuel · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Sep 2, 2009
- [AD 2008-15-01](https://openairdocs.org/ad/2008-15-01): Elevator trim system · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Aug 21, 2008
- [AD 2007-26-21](https://openairdocs.org/ad/2007-26-21): EMB-120 wing section · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Feb 20, 2008
- [AD 2006-12-14](https://openairdocs.org/ad/2006-12-14): Shut-off and crossbleed valves of the bleed air system · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Jul 18, 2006
- [AD 2006-11-10](https://openairdocs.org/ad/2006-11-10): De-icing system ejector flow control valves · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Jun 30, 2006
- [AD 2006-10-09](https://openairdocs.org/ad/2006-10-09): Wiring harnesses · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Jun 20, 2006
- [AD 2006-07-18](https://openairdocs.org/ad/2006-07-18): Elevator control surface · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective May 12, 2006
- [AD 2006-02-02](https://openairdocs.org/ad/2006-02-02): Auxiliary power unit (APU) · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Feb 24, 2006
- [AD 2005-25-01](https://openairdocs.org/ad/2005-25-01): Electrical harnesses · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Jan 9, 2006
- [AD 2004-14-25](https://openairdocs.org/ad/2004-14-25): Lower rotating beacon to the airframe · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Aug 23, 2004
- [AD 2004-14-24](https://openairdocs.org/ad/2004-14-24): Rotary variable inductive transducers (RVITs) · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Aug 23, 2004
- [AD 2004-13-12](https://openairdocs.org/ad/2004-13-12): Airplane Flight Manual - propeller synchronizer switch · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Aug 6, 2004
- [AD 2004-13-13](https://openairdocs.org/ad/2004-13-13): Access door ramp of the fueling control panel · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Aug 3, 2004
- [AD 2004-12-18](https://openairdocs.org/ad/2004-12-18): Vertical Cargo Nets in Cargo-Configured Cabins · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Jul 27, 2004
- [AD 2004-12-12](https://openairdocs.org/ad/2004-12-12): Main landing gear (MLG) · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Jul 21, 2004
- [AD 2004-06-07](https://openairdocs.org/ad/2004-06-07): Pitot/static 1, 2 and auxiliary sensors · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Apr 29, 2004
- [AD 2004-01-04](https://openairdocs.org/ad/2004-01-04): Hydraulic tube assemblies · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Feb 13, 2004
- [AD 2003-15-05](https://openairdocs.org/ad/2003-15-05): Flight idle stop system circuit breaker · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 1 more. Effective Sep 4, 2003
- [AD 2003-12-12](https://openairdocs.org/ad/2003-12-12): Airplane Flight Manual - flight attendant's seat · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 1 more. Effective Jul 28, 2003
- [AD 2001-22-14](https://openairdocs.org/ad/2001-22-14): Fire Extinguishing System Bottle Cartridges · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 105 more. Effective Dec 10, 2001
- [AD 2001-20-17](https://openairdocs.org/ad/2001-20-17): Airplane Flight Manual-Ice Accretion · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 1 more. Effective Oct 22, 2001
- [AD 2001-15-17](https://openairdocs.org/ad/2001-15-17): Transponder Control Panels · Bombardier ATR42-200, ATR42-300, ATR42-320 and 30 more. Effective Aug 20, 2001
- [AD 2001-06-18](https://openairdocs.org/ad/2001-06-18): AFM Revisions - Limitations Section - Ice Protection System · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 1 more. Effective Apr 16, 2001
- [AD 2000-23-30](https://openairdocs.org/ad/2000-23-30): Elevator Control Cable · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 1 more. Effective Jan 2, 2001
- [AD 2000-23-09](https://openairdocs.org/ad/2000-23-09): Hydraulics · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 1 more. Effective Dec 20, 2000
- [AD 2000-22-12](https://openairdocs.org/ad/2000-22-12): Circuit Breakers · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 1 more. Effective Dec 12, 2000
- [AD 2000-22-08](https://openairdocs.org/ad/2000-22-08): Mass-Balance Weights of the Aileron · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 1 more. Effective Dec 11, 2000
- [AD 2000-19-07](https://openairdocs.org/ad/2000-19-07): Direct Current (DC) Relay Box · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Oct 31, 2000
- [AD 2000-19-10](https://openairdocs.org/ad/2000-19-10): Prevent Sudden Change In Pitch Attitude · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 1 more. Effective Oct 13, 2000
- [AD 99-19-28](https://openairdocs.org/ad/99-19-28): Brake Assemblies Of Main Landing Gear · Embraer - Empresa Brasileira de Aeronautica EMB-120ER and EMB-120RT. Effective Oct 20, 1999
- [AD 99-17-04](https://openairdocs.org/ad/99-17-04): Aileron Control Cables And Nylon Grommets · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Sep 22, 1999
- [AD 99-02-18 R1](https://openairdocs.org/ad/99-02-18-R1): Titanium Thermal Insulating Blankets · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Mar 3, 1999
- [AD 98-15-22](https://openairdocs.org/ad/98-15-22): Wing De-Ice Boot · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Aug 27, 1998
- [AD 98-13-29](https://openairdocs.org/ad/98-13-29): AFM - Limitation Section - Power Levers · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Jul 29, 1998
- [AD 98-03-19](https://openairdocs.org/ad/98-03-19): Prevent Generator Overload Conditions · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Mar 18, 1998
- [AD 97-05-02](https://openairdocs.org/ad/97-05-02): Channel Fairings And Shims · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Apr 2, 1997
- [AD 97-02-21](https://openairdocs.org/ad/97-02-21): Inspect Wing Skin For Fuel Leakage · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Mar 3, 1997
- [AD 96-25-12](https://openairdocs.org/ad/96-25-12): Auxiliary Power Units · BAE Systems HS 748 Series 2A, HS 748 Series 2B, 707-100 Long Body and 74 more. Effective Jan 13, 1997
- [AD 95-26-15 R1](https://openairdocs.org/ad/95-26-15-R1): Traffic Alert and Collision Avoidance Systems · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 159 more. Effective Dec 26, 1996
- [AD 96-09-24](https://openairdocs.org/ad/96-09-24): AFM- Icing · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Jun 11, 1996
- [AD 95-25-11](https://openairdocs.org/ad/95-25-11): AFM - Limitations Sections Propeller · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Dec 27, 1995
- [AD 95-22-01](https://openairdocs.org/ad/95-22-01): Fluorescent Lighting System · Aerospace Lighting Fluorescent lighting systems, A310-203, A310-204 and 74 more. Effective Dec 4, 1995

### Matched by engine (Pratt & Whitney Canada PW118)

- [AD 2012-26-08](https://openairdocs.org/ad/2012-26-08): Propeller shafts · Pratt & Whitney Canada PW118, PW118A, PW118B and 20 more. Effective Feb 15, 2013
- [AD 2006-19-06](https://openairdocs.org/ad/2006-19-06): Propeller shaft · Pratt & Whitney Canada PW118, PW118A, PW118B and 14 more. Effective Sep 29, 2006
- [AD 2003-21-03](https://openairdocs.org/ad/2003-21-03): Low pressure rotor speed (NL) sensor · Pratt & Whitney Canada PW118, PW120, PW120A and 1 more. Effective Nov 20, 2003
- [AD 2003-16-04](https://openairdocs.org/ad/2003-16-04): Fuel heaters · Pratt & Whitney Canada PW118, PW118A, PW118B and 19 more. Effective Sep 10, 2003
- [AD 98-14-02](https://openairdocs.org/ad/98-14-02): Fuel Manifold Transfer Tubes · Pratt & Whitney Canada PW118, PW118A, PW118B and 17 more. Effective Aug 31, 1998
- [AD 97-17-05](https://openairdocs.org/ad/97-17-05): Gas Generator Case Drain Ports · Pratt & Whitney Canada PW118, PW118A, PW118B and 17 more. Effective Sep 9, 1997
- [AD 94-03-02](https://openairdocs.org/ad/94-03-02): High Pressure Turbine Disks · Pratt & Whitney Canada PW118, PW118A, PW120 and 5 more. Effective Feb 16, 1994
- [AD 92-01-08](https://openairdocs.org/ad/92-01-08): High Pressure Rotor · Pratt & Whitney Canada PW118, PW118A, PW120 and 5 more. Effective Jul 27, 1992
- [AD 91-06-02](https://openairdocs.org/ad/91-06-02): Turbomachinery Magnetic Chip Detector · Pratt & Whitney Canada PW118, PW118A, PW120 and 6 more. Effective Mar 29, 1991
- [AD 91-01-03](https://openairdocs.org/ad/91-01-03): Hydromechanical Fuel Control Units · Pratt & Whitney Canada JT15D-5, PW118, PW118A and 3 more. Effective Jan 7, 1991
- [AD 88-26-51](https://openairdocs.org/ad/88-26-51): High Pressure Turbine Components · Pratt & Whitney Canada PW118, PW118A, PW120 and 2 more. Effective Sep 22, 1989

### Historical (superseded or no longer in force)

- [AD 2008-04-18](https://openairdocs.org/ad/2008-04-18) (historical): Critical Design Configuration Control Limitations (CDCCL) · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER, EMB-120FC and 2 more. Effective Apr 3, 2008
- [AD 2001-17-01](https://openairdocs.org/ad/2001-17-01) (historical): Aileron and Elevator · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Aug 27, 2001
- [AD 2001-13-14](https://openairdocs.org/ad/2001-13-14) (historical): Airplane Flight Manual--Placard on the Main Instrument Panel, and the "LIGHT-HEAVY" Inflation Switch of the 
Leading Edge Deicing Boots · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Jul 12, 2001
- [AD 2001-02-06](https://openairdocs.org/ad/2001-02-06) (historical): Icing Conditions · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Mar 5, 2001
- [AD 2000-20-05](https://openairdocs.org/ad/2000-20-05) (historical): Landing Gear Doors · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Nov 13, 2000
- [AD 99-02-18](https://openairdocs.org/ad/99-02-18) (historical): Titanium Thermal Insulating Blankets · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Mar 3, 1999
- [AD 97-26-06](https://openairdocs.org/ad/97-26-06) (historical): AFM - Limitation Section - Ice · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Jan 23, 1998
- [AD 97-26-22](https://openairdocs.org/ad/97-26-22) (historical): Movable Backstop Of Elevator Pitch Trim · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Jan 13, 1998
- [AD 92-16-51](https://openairdocs.org/ad/92-16-51) (historical): Backup Flight Idle Stop System · Embraer - Empresa Brasileira de Aeronautica EMB-120, EMB-120ER and EMB-120RT. Effective Sep 23, 1992
- [AD 2012-11-14](https://openairdocs.org/ad/2012-11-14) (historical): Propeller shafts · Pratt & Whitney Canada PW118, PW118A, PW118B and 20 more. Effective Jul 20, 2012

## Information bulletins (advisory) (1 in force)

- [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008

## NTSB investigations

None matched to N584SW.

## FAA accident and incident reports

None matched to N584SW.

## Service difficulty reports (104, newest 50)

As reported by operators and repair stations.

- [SDR HKGA20210208001](https://openairdocs.org/sdr/HKGA20210208001), Feb 7, 2021: STRINGER. CRACKED. DURING SCHEDULED MAINTENANCE A FUEL LEAK WAS NOTED AT ACCESS PANEL 622EB. MAINTENANCE PERSONNEL EVALUATED THE LEAK AND DETERMINED ITS SOURCE TO BE FROM A RIVET 
- [SDR HKGA202002207001](https://openairdocs.org/sdr/HKGA202002207001), Feb 17, 2020: CONNECTOR. INTERMITTENT. A MAINTENANCE TEST FLIGHT FOR NACELLE FLAP DISAGREEMENT WAS IN PROGRESS. DURING THE TEST FLIGHT THE CREW WAS IN CRUISE CONFIGURATION AND INCREMENTALLY SET THE F
- [SDR SWIA2015021340722](https://openairdocs.org/sdr/SWIA2015021340722), Feb 12, 2015: WIRE. BROKEN. FWD TWO RED EMERGENCY LIGHTS INOPERATIVE. REPAIRED THE WIRE FOR THE EMERGENCY LIGHTS AND RELAMPED. OPS CHECKED GOOD.
- [SDR SWIA201439905](https://openairdocs.org/sdr/SWIA201439905), Nov 9, 2014: CONTROL VALVE. FAILED. WHILE TAXIING AT NORMAL TAXI SPEED WITH ANTI-SKIDS ON, BRAKES FELT SPONGY. FELT LIKE ACFT WOULD NOT COME TO A STOP UNTIL TAXI SPEED IS VERY LOW AND THEN THE BRA
- [SDR SWIA201439282](https://openairdocs.org/sdr/SWIA201439282), Sep 14, 2014: RELAY. FAILED. FLIGHT IS RETURNING TO DEPARTURE AFTER ANTI-SKID FAILED. REMOVED AND REPLACED ANTI-SKID RELAYS K0255 AND K0021 IAW AMM. OPS CHECKED GOOD.
- [SDR SWIA201439068](https://openairdocs.org/sdr/SWIA201439068), Jul 31, 2014: POTENTIOMETER. INOPERATIVE. PEDAL STEERING INOPERATIVE ILLUMINATED AFTER TAKEOFF. REMAINED ILLUMINATED AFTER GEAR RETRACTION. REMOVED AND REPLACED RUDDER FEEDBACK POTENTIOMETER AND OPS CHE
- [SDR SWIA201438699](https://openairdocs.org/sdr/SWIA201438699), Jul 12, 2014: BATTERY PACK. INOPERATIVE. F/A REPORTS FLASHLIGHT INOPERATIVE. R & R F/A FLASHLIGHT BATTERIES. OPS CHECKED GOOD.
- [SDR SWIA201438546](https://openairdocs.org/sdr/SWIA201438546), Jul 2, 2014: LIGHT. INOPERATIVE. LEFT FWD OVERWING EMERGENCY LIGHT IS INOPERATIVE. C-CHECK, R & R LT FWD OVERWING EMERGENCY LIGHT ASSY.
- [SDR SWIA201438548](https://openairdocs.org/sdr/SWIA201438548), Jun 12, 2014: RIB. CRACKED. LT NACELLE FLAP OTBD SIDE RIB STIFFENER CRACKED. C-CHECK, REPLACED OTBD SIDE RIB STIFFENER AT LT NACELLE FLAP IAW SRM.
- [SDR SWIA201438547](https://openairdocs.org/sdr/SWIA201438547), Jun 12, 2014: SEAT TRACK. CORRODED. PASSENGER SEAT TRACK IS CORRODED. C-CHECK, R & R SEAT TRACK IAW ETS.
- [SDR SWIA201438549](https://openairdocs.org/sdr/SWIA201438549), Jun 9, 2014: STRINGER. CRACKED. RIGHT WING STRINGER NR 10 CRACKED AT RIB NR 16, 1ST PANEL OTBD OF NACELLE. C-CHECK, PERFORMED RT WING NR 10 STRINGER REPAIR AT RIB 16 IAW ETD.
- [SDR SWIA201437783](https://openairdocs.org/sdr/SWIA201437783), May 24, 2014: WIRE. OVERHEATED. WIRE SHOWS SIGNS OVERHEATING IN RIGHT DC RELAY BOX, W208-0240-2, FOR WINDSHIELD HEAT. REPLACED WIRE W208-0240-2 IN RT DC RELAY BOX IAW WM.
- [SDR SWIA201437779](https://openairdocs.org/sdr/SWIA201437779), May 24, 2014: SKIN. CRACKED. LT ENGINE NACELLE OTBD SIDE FWD OF FWD COWL DOOR SKIN CRACKED. REPAIRED DAMAGED SKIN ON LT ENGINE NACELLE OTBD SIDE FWD OF FWD COWL DOOR SKIN BY MEANS OF A DOUB
- [SDR SWIA201437778](https://openairdocs.org/sdr/SWIA201437778), May 24, 2014: LENS. BROKEN. IN CABIN EMERGENCY LIGHT AFT LENS IS BROKEN. R & R WITH NEW EMERGENCY TRACK LIGHT AFT LENS IAW AMM.
- [SDR SWIA201437800](https://openairdocs.org/sdr/SWIA201437800), May 14, 2014: SIGN. BROKEN. EMERGENCY EXIT SIGN AT 6A IS BROKEN. REPLACED EXIT SIGN.
- [SDR SWIA201437601](https://openairdocs.org/sdr/SWIA201437601), May 13, 2014: LAMP. INOPERATIVE. FLOOR EMERGENCY LIGHT AT ROW 5 IS INOPERATIVE, REPLACED THE LAMPS.
- [SDR SWIA201436579](https://openairdocs.org/sdr/SWIA201436579), Feb 28, 2014: SIGN. LOOSE. SMALL VERTICAL EMERGENCY EXIT SIGN AT 6C IS LOOSE. FLT 6221 TIGHTENED SIGN.
- [SDR SWIA201335504](https://openairdocs.org/sdr/SWIA201335504), Dec 3, 2013: LIGHT. INOPERATIVE. FWD OVERHEAD EMERGENCY LIGHT AT ROW 2 DOES NOT ILLUMINATE. FLT 5442 RELAMPED.
- [SDR SWIA201335329](https://openairdocs.org/sdr/SWIA201335329), Nov 17, 2013: ACCESS PANEL. CRACKED. LT WING NR 1 FUEL ACCESS PANEL FWD STRINGER 10 CRACKED. REPAIRED LT WING NR 1 FUEL PANEL FWD STRINGER 10 IAW SRM.
- [SDR SWIA201333287](https://openairdocs.org/sdr/SWIA201333287), Apr 19, 2013: LIGHT. INOPERATIVE. ONE WHITE FLOOR EMERGENCY LIGHT AT ROW 3 IS BURNED OUT. (FLT 5541) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201332888](https://openairdocs.org/sdr/SWIA201332888), Feb 24, 2013: LIGHT. INOPERATIVE. EMERGENCY OVERHEAD LIGHT AT EXIT ROW 9 BURNED OUT. (FLT 5312) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201332889](https://openairdocs.org/sdr/SWIA201332889), Feb 19, 2013: LIGHT. INOPERATIVE. EXIT ROW SEATS 9 B&C EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 5339) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201332828](https://openairdocs.org/sdr/SWIA201332828), Feb 14, 2013: COMPUTER. FAILED. AIRCRAFT BEGAN YAWING AFTER YAW ENGAGED. (FLT 5336) REPLACED THE CAPTS AHRS COMPUTER AND BOTH AUTO-PILOT COMPUTERS. PN-622-6190-204 S/N ON-2667 S/N OFF-3072, P/
- [SDR SWIA201232292](https://openairdocs.org/sdr/SWIA201232292), Nov 29, 2012: PRESSURE SWITCH. FAILED. LEFT ENGINE AIR INLET DEICE FAILED IN FLIGHT IN ICING CONDITIONS. (FLT 5317) REPLACED LEFT ENGINE AIR INLET DEICE BOOT PRESSURE SWITCH.
- [SDR SWIA201231569](https://openairdocs.org/sdr/SWIA201231569), Aug 18, 2012: CLAMP. LOOSE. LEFT PACK OVERHEATING SMELL ON DESCENT. (FLT 5437) TIGHTENED A LOOSE CLAMP FOR LEFT PACK TEMPERATURE INLET CONTROL VALVE.
- [SDR SWIA201231105](https://openairdocs.org/sdr/SWIA201231105), Jun 23, 2012: APU. FAULTY. SMOKE IN THE CABIN. (FLT 5447) REPLACED APU ASSEMBLY.
- [SDR SWIA201230891](https://openairdocs.org/sdr/SWIA201230891), Jun 2, 2012: SWITCH. OUT OF POSITION. SMOKE MAP LIGHT AND AURAL WARNING SOON AFTER LEFT PACK FAIL. (FLT 5322) REPOSITIONED RAM AIR INLET VALVE SWITCH TO CLOSED POSITION.
- [SDR SWIA201230878](https://openairdocs.org/sdr/SWIA201230878), Jun 2, 2012: CONTROLLER. FAILED. RECEIVED A CABIN ALT MESSAGE. (FLT 5616) REPLACED THE ELECTRONIC CONTROLLER AND TRIPLE INDICATOR IN REFERENCE TO EMB 120 AMM. P/N 22201T011400 S/N OFF 241 P/N 7
- [SDR SWIA201230308](https://openairdocs.org/sdr/SWIA201230308), Apr 8, 2012: LAMP. BURNED OUT. FLT 5614, NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201127381](https://openairdocs.org/sdr/SWIA201127381), Aug 25, 2011: LIGHT. INOPERATIVE. OVERHEAD EMERGENCY LIGHT AT ROW 9 IS OUT. (FLT 6426) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201125962](https://openairdocs.org/sdr/SWIA201125962), Mar 9, 2011: STRINGER. CORRODED. FORWARD FUSELAGE STRINGER 18 IS CORRODED. (C-CHECK) REPAIRED FORWARD FUSELAGE STRINGER 18 PER SRM.
- [SDR SWIA201125956](https://openairdocs.org/sdr/SWIA201125956), Mar 9, 2011: WINDOW. CRACKED. CAPTAINS DIRECT VISION WINDOW IS CRACKED. (C-CHECK) REPLACED LEFT SIDE DIRECT VISION WINDOW.
- [SDR SWIA201125964](https://openairdocs.org/sdr/SWIA201125964), Mar 8, 2011: STRINGER. CRACKED. CRACKED STRINGER IN LEFT WING THROUGH NR 2 FUEL PANEL. (C-CHECK) PERFORMED STRINGER SPLICE REPAIR AT LEFT WING NR 10 STRINGER BETWEEN RIBS 9 & 7 PER SRM.
- [SDR SWIA201125963](https://openairdocs.org/sdr/SWIA201125963), Mar 8, 2011: SPAR CAP. CRACKED. LEFT WING FORWARD SPAR CAP INBOARD OF NACELLE CRACKED AT HI-LOK. (C-CHECK) REPAIRED LEFT WING AUX SPAR PER EMBRAER TECHNICAL DISPOSITION.
- [SDR SWIA201125715](https://openairdocs.org/sdr/SWIA201125715), Feb 24, 2011: LIGHT. INOPERATIVE. MAIN CABIN EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201125517](https://openairdocs.org/sdr/SWIA201125517), Jan 26, 2011: WIRE. BROKEN. AFT FLOOR LEVEL EMERGENCY LIGHT IS OUT. (FLT 6473) REPAIRED BROKEN WIRE.
- [SDR SWIA201025270](https://openairdocs.org/sdr/SWIA201025270), Dec 1, 2010: LIGHT. INOPERATIVE. WHITE EMERGENCY LIGHT AT SEAT 11 A FLOOR LEVEL INOPERATIVE. (FLT 6917) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201025239](https://openairdocs.org/sdr/SWIA201025239), Nov 23, 2010: LIGHT. INOPERATIVE. LAST FLOOR LEVEL EMERGENCY LIGHT ON LEFT SIDE BURNT OUT. (FLT 6385) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201024916](https://openairdocs.org/sdr/SWIA201024916), Sep 19, 2010: WIRE. OUT OF POSITION. FLIGHT DECK STARTED TO SMELL STRONGLY OF ELECTRONICS, NO SMOKE IN EVIDENCE. (FLT 6854) REPAIRED AND REPOSITIONED WIRE BEHIND OVERHEAD ELECTRICAL PANEL.
- [SDR SWIA201023629](https://openairdocs.org/sdr/SWIA201023629), Feb 3, 2010: WIRE. LOOSE. EMERGENCY LIGHT OVER THE PASSENGER DOOR IS INTERMITTENT. (FLT 6282) RESEATED CONNECTOR WIRE.
- [SDR SWIA200922698](https://openairdocs.org/sdr/SWIA200922698), Sep 21, 2009: AHRS. MALFUNCTIONED. CAPTAINS EADI SCREEN WENT BLANK FOR 10 SEC, THEN SCREEN CAME BACK ON WITH RED FLAGS AND BANK AT 30°, EVEN IN LEVEL FLIGHT. (FLT 6490) REPLACED THE PILOTS AHC85
- [SDR SWIA200922167](https://openairdocs.org/sdr/SWIA200922167), Jul 19, 2009: WIRE. BROKEN. FOUR FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOP. (FLT 6455) REPAIRED BROKEN WIRE.
- [SDR SWIA200922652](https://openairdocs.org/sdr/SWIA200922652), Jul 8, 2009: STRINGER. CORRODED. STRINGER 19 CORRODED. (C-CHECK) REPAIRED PER SRM.
- [SDR SWIA200921312](https://openairdocs.org/sdr/SWIA200921312), Mar 29, 2009: TERMINAL. UNSECURE. FLT 6339 - ELECTRICAL ODOR COMING FROM GALLEY AREA. RESECURED LOOSE TERMINAL CONNECTOR TO THE BULB.
- [SDR SWIA200920803](https://openairdocs.org/sdr/SWIA200920803), Jan 7, 2009: ROD END. BINDING. FLT 7808 - ELEVATOR TRIM BINDS IN FLIGHT. REPLACED ROD ENDS ON LEFT AND RIGHT ELEVATOR TRIM CONTROL RODS.
- [SDR SWIA200820609](https://openairdocs.org/sdr/SWIA200820609), Dec 4, 2008: ENGINE. OVERSPEED. FLT 5700 - RIGHT NP WENT TO 103 PERCENT DURING TAKE OFF. ACCOMPLISHED ENGINE RUNS, UNABLE TO DUPLICATE.
- [SDR SWIA200820470](https://openairdocs.org/sdr/SWIA200820470), Nov 7, 2008: ACTUATOR. FAULTY. FLT 5711 - RIGHT MAIN GEAR WOULD NOT RETRACT. REPLACED RIGHT MAIN GEAR ACTUATOR, P/N 1959-000-07, S/N ON 685, S/N OFF: B118.
- [SDR SWIA200819905](https://openairdocs.org/sdr/SWIA200819905), Jul 25, 2008: SMOKE DETECTOR. FALSE ACTIVATION. BAGGAGE SMOKE "WARN" ON GLARESHIELD. (FLIGHT NR 3610) REPLACED AFT CARGO SMOKE DETECTOR IAW AMM 26-15-01. OPS CHECK GOOD. 
- [SDR SWIA200819698](https://openairdocs.org/sdr/SWIA200819698), May 26, 2008: BATTERY PACK. DISCHARGED. FLIGHT ATTENDANT REPORTS THAT SEVERAL EMERGENCY EXIT SIGNS ARE INOP. FLIGHT 5408 - REPLACED THE MIDDLE ELBP. OPS CHECK GOOD. 
- [SDR SWIA200819480](https://openairdocs.org/sdr/SWIA200819480), Apr 12, 2008: TIRE. FAILED. FLT 5780 - NR 1 MAIN TIRE FOUND FLAT AFTER LANDING. REPLACED NR 1 AND NR 2 MAIN WHEEL ASSEMBLIES PN 3-1446-1, SN/OFF 0695, PN 3-1446-1, SN/OFF 1267. 

All 104: https://openairdocs.org/aircraft/N584SW/reports.md

## Related

- Other Embraer EMB-120ER aircraft: https://openairdocs.org/model/embraer-emb-120er/aircraft.md
- STCs for the Embraer EMB-120ER: https://openairdocs.org/model/embraer-emb-120er/stcs.md
- The Pratt & Whitney Canada PW118 engine: https://openairdocs.org/engine/pratt-whitney-canada-pw118.md

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