# N566SW: 1998 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: 120341
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: August 3, 1998
- Certificate issued: June 13, 2013
- Expires: June 30, 2029
- Mode S code: A73ED9
- Registered owner: [Jahn566sw LLC](https://openairdocs.org/faa-owner/JAHN566SW%20LLC)
- Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)
- Owner type: LLC
- Owner's area on the map: 25.7304° N, 80.2336° W: Placed by OpenAirDocs at the center of ZIP code 33133, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=566SW
- Page: https://openairdocs.org/aircraft/N566SW

From the FAA registry file of October 22, 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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB LAX00IA106](https://openairdocs.org/ntsb/LAX00IA106), Feb 21, 2000: Embraer 120 (N566SW), Fresno, CA, incident, no damage. Probable cause: Moisture contamination of the elevator trim actuator units resulting in their failure to operate at below freezing temperatures

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20000221003129I](https://openairdocs.org/incident/20000221003129I), Feb 21, 2000: Emb EMB120ER (N566SW), Fresno, CA. On February 21, 2000, at approximatley 0958 hours PDT, a sky west airlines aircraft, flight number 5353, an Embraer 120, N566SW on a domestic revenue flight…

## Service difficulty reports (102, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR JIKA2023071800401](https://openairdocs.org/sdr/JIKA2023071800401), Jul 14, 2023: UNKNOWN. UNKNOWN. PILOT REPORTED AFTER DEPARTURE FROM BQN DURING CLIMB OUT AT APPROX 11,000FT THE LEFT ENGINE TORQUE DROPPED TO 0, ENGINE OIL PRESSURE DROPPED TO 0 SUBSEQUENTLY E
- [SDR SWIA2015F00020](https://openairdocs.org/sdr/SWIA2015F00020), Jan 5, 2015: BLADE. CRACKED. DURING MAJOR INSPECTION, FOUND FPI CRACK INDICATION IN FILLET RADIUS OF BLADE SHANK.
- [SDR SWIA201439693](https://openairdocs.org/sdr/SWIA201439693), Oct 27, 2014: SOCKET. INOPERATIVE. RED EMERGENCY LIGHTS ARE INOPERATIVE NEAR THE CABIN MAIN ENTRY DOOR. R & R THE LIGHT SOCKET ASSY AND REPAIRED WIRING, OPS CHECKED GOOD, IAW AMM AND WDM.
- [SDR SWIA201438606](https://openairdocs.org/sdr/SWIA201438606), Jun 25, 2014: LAMP. INOPERATIVE. NR 4 FLOOR WHITE EMERGENCY LIGHT STRIP INOPERATIVE. REPLACED THE LAMP IN NR 4 FLOOR WHITE EMERGENCY LIGHT STRIP IAW AMM.
- [SDR SWIA201437934](https://openairdocs.org/sdr/SWIA201437934), May 29, 2014: SKIN. GOUGED. GOUGE APPROXIMATELY 3.5 INCHES LONG, .2500 INCHES WIDE, .0625 INCHES DEEP ON AFT FUSELAGE AT CARGO DOOR, WITHIN .2500 INCHES OF RIVETS BETWEEN SKIN EDGE AND RIV
- [SDR SWIA201437727](https://openairdocs.org/sdr/SWIA201437727), May 25, 2014: PROPELLER. OVERSPEED. RIGHT PROPELLER SPEED WENT TO 103.7 PERCENT RPM. CHANGED PCU AND TRANSFER TUBE. OPS CHECK GOOD.
- [SDR SWIA201436684](https://openairdocs.org/sdr/SWIA201436684), Mar 4, 2014: OXYGEN MASK. UNWANTED DEPLOY. OXYGEN MASK DEPLOYED DURING FLIGHT. RESTOWED.
- [SDR SWIA201334655](https://openairdocs.org/sdr/SWIA201334655), Aug 28, 2013: SUPPORT. CRACKED. LT NACELLE FLAP INBD INTERIOR VERTICAL SUPPORT CRACKED. C-CHECK REPLACED LT NACELLE FLAP INTERIOR VERTICAL SUPPORT IAW SRM.
- [SDR SWIA201334657](https://openairdocs.org/sdr/SWIA201334657), Aug 22, 2013: FITTING. CRACKED. RT WING UPPER CLIP CRACKED 2ND FROM FWD AT RIB 20. C-CHECK REPLACED UPPER WING CLIP AT RT WING 2ND FROM FWD AT RIB 20, IAW SRM.
- [SDR SWIA201334656](https://openairdocs.org/sdr/SWIA201334656), Aug 22, 2013: FITTING. CRACKED. RT WING LOWER SMALL CLIP CRACKED AT RIB 15 2ND FROM FWD. C-CHECK REPLACED RT WING LOWER SMALL CLIP AT RIB 15, 2ND FROM FWD IAW SRM.
- [SDR SWIA201334658](https://openairdocs.org/sdr/SWIA201334658), Aug 20, 2013: SUPPORT FITTING. CRACKED. LT OTBD WING HAS ONE CRACKED UPPER SKIN SUPPORT CLIP AT STATION 20A. C-CHECK REPLACED LT OTBD WING ONE CRACKED UPPER SKIN SUPPORT CLIP AT WING STATION 20A IAW S
- [SDR SWIA201334210](https://openairdocs.org/sdr/SWIA201334210), Aug 13, 2013: LIGHT. INOPERATIVE. EMERGENCY LIGHT AT PASSENGER ENTRYWAY IS BURNED OUT. FLT#6338 RELAMPED.
- [SDR SWIA201334208](https://openairdocs.org/sdr/SWIA201334208), Aug 7, 2013: CAP. LOOSE. FLOOR EMERGENCY LIGHTS FAILED. FLT#6023 REINSTALLED LOOSE FUSE CAP.
- [SDR SWIA201333801](https://openairdocs.org/sdr/SWIA201333801), Jun 26, 2013: PCU. FAILED. ON TAXI OUT AIRCRAFT PERFORMED AN UNCOMMANDED RT TURN. DURING TAKEOFF ROLL WARNING LIGHT ON MAP FLASHED A COUPLE OF TIMES & THE AIRCRAFT JERKED TO THE RT TWO TI
- [SDR SWIA201333714](https://openairdocs.org/sdr/SWIA201333714), Jun 14, 2013: SOCKET. FAILED. EMERGENCY FLOOR LEVEL LIGHTING SYSTEM HAS FIVE LIGHTS NOT WORKING. REPLACED 1 MOLEX SOCKET AT MID STRIP PLUG & REPLACED SOCKET AT MID STRIP.
- [SDR SWIA201333069](https://openairdocs.org/sdr/SWIA201333069), Mar 26, 2013: SIGN. MISSING. LOWER LEFT SIDE OF THE EMERGENCY EXIT SIGN ON ROW 6 IS MISSING. (FLT 6327) REPLACED LOWER LEFT SIDE OF EMERGENCY EXIT SIGN AT ROW 6A.
- [SDR SWIA201332906](https://openairdocs.org/sdr/SWIA201332906), Feb 27, 2013: SIGN. DETACHED. EMERGENCY EXIT SIGN AT ROW 6 FELL. (FLT 5488) REPLACED 6C LOWER EMERGENCY EXIT SIGN LIGHT ASSEMBLY.
- [SDR SWIA201332617](https://openairdocs.org/sdr/SWIA201332617), Jan 18, 2013: LIGHT. INOPERATIVE. CABIN FLOOR EMERGENCY LIGHT BURNED OUT NEAR ROW 3. (FLT 6268) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201232456](https://openairdocs.org/sdr/SWIA201232456), Dec 26, 2012: LIGHT. INOPERATIVE. FLOOD LIGHT OVER SEAT 6A DOES NOT ILLUMINATE. (SERVICE) RELAMPED FLOOD LIGHT.
- [SDR SWIA201232444](https://openairdocs.org/sdr/SWIA201232444), Dec 22, 2012: LIGHT. INOPERATIVE. ONE WHITE EMERGENCY TRACK LIGHT DOES NOT ILLUMINATE. (FLT 5401) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201232239](https://openairdocs.org/sdr/SWIA201232239), Nov 25, 2012: LIGHT. INOPERATIVE. EMERGENCY FLOOR LEVEL LIGHT ROW 8A IS BURNED OUT. (FLT 5647) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201232181](https://openairdocs.org/sdr/SWIA201232181), Nov 10, 2012: WIRE. BROKEN. AFT FOUR FLOOR EMERGENCY LIGHTS INOPERATIVE. (FLT 5632) REPAIRED BROKEN WIRE ON AFT RED FLOOR LEVEL LIGHT AND REPLACED FUSE.
- [SDR SWIA201231940](https://openairdocs.org/sdr/SWIA201231940), Sep 29, 2012: LIGHT. DETACHED. ROW 5 FLOOR EMERGENCY WHITE LIGHT FOUND DETACHED AN UNCOVERED FROM SOCKETS. (FLT 5816) RE-ATTACHED FLOOR EMERGENCY WHITE LIGHT IAW AMM.
- [SDR SWIA201231873](https://openairdocs.org/sdr/SWIA201231873), Sep 28, 2012: HANDLE. LACK OF LUBE. MAIN CABIN DOOR HARD TO OPEN AND CLOSE. (FLT 5405) LUBRICATED HANDLE ASSEMBLY.
- [SDR SWIA201231869](https://openairdocs.org/sdr/SWIA201231869), Sep 25, 2012: LIGHT. INOPERATIVE. EMERGENCY FLOOR LIGHT AT ROW 5 IS OUT. (FLT 5339) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201231870](https://openairdocs.org/sdr/SWIA201231870), Sep 22, 2012: WIRE. DAMAGED. TWO RED FLOOR EMERGENCY LIGHTS AT ROW 9 FAIL TO ILLUMINATE. (FLT 5538) REPAIRED WIRE FOR FLOOR EMERGENCY EXIT IN REFERENCE TO EMB 120-WDM.
- [SDR SWIA201231560](https://openairdocs.org/sdr/SWIA201231560), Aug 15, 2012: LIGHT. INOPERATIVE. FLOOR EMERGENCY LIGHT AT 5A IS INOPERATIVE. (SERVICE) REPLACED LIGHT FIXTURE FOR EMERGENCY LIGHT AT ROW 5 IN REFERENCE TO EMB 120 MM.
- [SDR SWIA201231037](https://openairdocs.org/sdr/SWIA201231037), Jun 15, 2012: WIRE. BROKEN. FLOOR EMERGENCY STRIP AT ROW 5 HAS ONE WHITE LIGHT OUT. (SERVICE) SPLICED BROKEN WIRE AT ROW 5 FLOOR STRIP EMERGENCY LIGHTS.
- [SDR SWIA201231033](https://openairdocs.org/sdr/SWIA201231033), Jun 15, 2012: SOCKET. BROKEN. EMERGENCY LIGHT ON FLOOR AT 11A IS BROKEN. (FLT 6332) REPLACED AFT FLOOR STRIP EMERGENCY LIGHTING SOCKET ASSEMBLY IN REFERENCE TO M/M.
- [SDR SWIA201230953](https://openairdocs.org/sdr/SWIA201230953), Jun 7, 2012: SHOULDER BELT. FRAYED. F/A'S SHOULDER HARNESS IS FRAYED AND IS DIFFICULT TO TAKE ON AND OFF. (FLT 5614) REPLACED F/A'S SEAT BELT HARNESS IN REFERENCE TO AMM.
- [SDR SWIA201230952](https://openairdocs.org/sdr/SWIA201230952), Jun 7, 2012: LINKAGE. LACK OF LUBE. CABIN DOOR DIFFICULT TO PUSH OPEN. (FLT 5614) LUBRICATED LINKAGES THROUGHOUT CABIN DOOR OPENING AND LOCKING MECHANISMS.
- [SDR SWIA201230940](https://openairdocs.org/sdr/SWIA201230940), Jun 5, 2012: LIGHT. INOPERATIVE. FLOOR LEVEL EMERGENCY LIGHTS AT 8A ARE INOPERATIVE. (FLT 5473) RELAMPED EMERGENCY LIGHTS.
- [SDR SWIA201230645](https://openairdocs.org/sdr/SWIA201230645), May 4, 2012: WIRE. BROKEN. ONE FLOOR EMERGENCY LIGHT AT 3A IS OUT. (FLT 6282) REPAIRED BROKEN WIRE AT FLOOR ESCAPE EMERGENCY LIGHT AT 3A.
- [SDR SWIA201230408](https://openairdocs.org/sdr/SWIA201230408), Apr 15, 2012: LIGHT. INOPERATIVE. FLOOR EMERGENCY LIGHT AT 3A IS OUT. (FLT 5529) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201230231](https://openairdocs.org/sdr/SWIA201230231), Mar 26, 2012: LIGHT. INOPERATIVE. FLOOR EMERGENCY LIGHT AT ROW 10 IS OUT. (FLT 6232) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201229553](https://openairdocs.org/sdr/SWIA201229553), Feb 1, 2012: WIRE. DAMAGED. FLOOR EMERGENCY LIGHT AT 7A IS OUT. (FLT 5403) REPAIRED FLOOR EMERGENCY LIGHT WIRE AT 7A.
- [SDR SWIA201229313](https://openairdocs.org/sdr/SWIA201229313), Jan 17, 2012: LIGHT. INOPERATIVE. THE 7A FLOOR EMERGENCY LIGHT IS OUT. (FLT 6379) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201129116](https://openairdocs.org/sdr/SWIA201129116), Dec 31, 2011: WIRE. BROKEN. A WHITE FLOOR LEVEL EMERGENCY LIGHT AT 3A IS OUT. (FLT 5610) REPAIRED FLOOR LEVEL EMERGENCY LIGHT WIRING.
- [SDR SWIA201129095](https://openairdocs.org/sdr/SWIA201129095), Dec 21, 2011: CONTROL VALVE. MALFUNCTIONED. LEFT BRAKE LOCKED UP DURING TAXI. (FLT 6352) REPLACE INBOARD BRAKE CONTROL VALVE. P/N: 39-651-2 S/N OFF: 506
- [SDR SWIA201128259](https://openairdocs.org/sdr/SWIA201128259), Oct 15, 2011: PIVOT. LACK OF LUBE. PAX DOOR DIFFICULT TO OPEN. (FLT 5326) LUBRICATED MCD HANDLE PIVOT POINT AND DOOR ROLLERS.
- [SDR SWIA201128116](https://openairdocs.org/sdr/SWIA201128116), Oct 6, 2011: ROLLER. LACK OF LUBE. MAIN CABIN DOOR IS HARD TO OPEN. (FLT 6327) LUBED PAX DOOR LOCK ROLLERS ON FUSELAGE AT LOCK MECHANISM IN DOOR.
- [SDR SWIA201127890](https://openairdocs.org/sdr/SWIA201127890), Sep 24, 2011: FUSE. BLOWN. NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5343) REPLACED NR 1 EMERGENCY LIGHT FUSE.
- [SDR SWIA201126918](https://openairdocs.org/sdr/SWIA201126918), Jul 24, 2011: COMPUTER. FAILED. AUTO PILOT DISCONNECTED WITH RED MSG ON AP CONTROL PANEL. DISPLAY MSG ON MAP AND PITCH AND ROLL FLAGS ON EFIS DISPLAY ON BOTH SIDES. CAPT AND FO EFIS SCREENS NO
- [SDR SWIA201126447](https://openairdocs.org/sdr/SWIA201126447), Jun 10, 2011: SHIM. OUT OF ADJUST. MAIN CABIN DOOR HARD TO OPEN. (FLT 6310) ADJUSTED FORWARD UPPER SHIM STACK ON MAIN CABIN DOOR.
- [SDR SWIA201126236](https://openairdocs.org/sdr/SWIA201126236), May 14, 2011: WIRE. BROKEN. FLOOR LEVEL EMERGENCY LIGHT AT ROW 4 IS OUT. (FLT 6263) REPAIRED BROKEN WIRE AT FLOOR LEVEL EMERGENCY LIGHT NEAR ROW 4.
- [SDR SWIA201126235](https://openairdocs.org/sdr/SWIA201126235), May 12, 2011: LIGHT. UNSECURE. FLOOR LEVEL EMERGENCY LIGHT AT ROW 6 IS OUT. (FLT 6263) RE-SECURED EMERGENCY LIGHT.
- [SDR SWIA201126068](https://openairdocs.org/sdr/SWIA201126068), Apr 16, 2011: ROLLER. LACK OF LUBE. MAIN CABIN DOOR IS HARD TO OPEN. (FLT 6358) LUBED MAIN CABIN DOOR ROLLERS.
- [SDR SWIA201125982](https://openairdocs.org/sdr/SWIA201125982), Apr 1, 2011: WIRE. BROKEN. FLOOR EMERGENCY LIGHT NEAR ROW 4 IS OUT. (FLT 6307) REPAIRED BROKEN WIRE AT FLOOR EMERGENCY LIGHT NEAR ROW 4.
- [SDR SWIA201125668](https://openairdocs.org/sdr/SWIA201125668), Feb 23, 2011: LIGHT. INOPERATIVE. RED EMERGENCY FLOOR LIGHT AT ROW 6 IS OUT. (FLT 6711) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201025193](https://openairdocs.org/sdr/SWIA201025193), Nov 10, 2010: CONTROLLER. FAILED. F/A COULD NOT OPEN CABIN DOOR. HAD TO RELIEVE PRESSURE TO GET DOOR OPEN. (FLT 6677) REPLACED ELECTRONIC ALTITUDE CONTROLLER.

All 102: https://openairdocs.org/aircraft/N566SW/reports.md

## STCs that may be installed (OpenAirDocs) (72, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Embraer EMB-120ER)

- [STC ST01305WI-D](https://openairdocs.org/stc/ST01305WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc
- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST104CH](https://openairdocs.org/stc/ST104CH): Installation of a TCAS I and optional Data Recorder Unit. Acron Aviation Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST01110DE](https://openairdocs.org/stc/ST01110DE): Installation of a Luma Technologies Multiple Alarm Panel (MAP). Peregrine
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC ST03022AT](https://openairdocs.org/stc/ST03022AT): Installation of a Sandel Model ST3400 Terrain Awareness and Warning System (TAWS). Woven Electronics, LLC
- [STC ST03375AT](https://openairdocs.org/stc/ST03375AT): Installation of Garmin GPS 165 TSO Global Positioning System (GPS). Woven Electronics
- [STC ST00598WI](https://openairdocs.org/stc/ST00598WI): Conversion of airplane from a passenger configuration to an all cargo configuration. Worldwide Aviation LLC
- [STC SA8840SW](https://openairdocs.org/stc/SA8840SW): Replace core assembly of AiResearch Primary/Secondary Air-to-Air Heat Exchanger, part number 194546-3. Honeywell International Inc
- [STC SA8466SW](https://openairdocs.org/stc/SA8466SW): Recore of AiResearch Engine Oil Coolers Part Numbers 160282-3 and 160282-4 with LORI Core Assembly Part Number L8602548-1. Honeywell International Inc
- [STC ST00895DE](https://openairdocs.org/stc/ST00895DE): Installation of the Garmin G700 TXi Avionics Suite. Peregrine
- [STC ST02635LA](https://openairdocs.org/stc/ST02635LA): Modification to replace the existing Mode S Transponder system with the ACSS NXT-600 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST00007IB](https://openairdocs.org/stc/ST00007IB): Installation of a Honeywell Mode S Transponder model MST 67 and TCAS II model CAS 81. Embraer Engineering & Technology Center - USA Inc
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST03089NY](https://openairdocs.org/stc/ST03089NY): Replacement of certain Goodrich pneumatic deicer boots. SMR Technologies Inc
- [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC ST02499AK](https://openairdocs.org/stc/ST02499AK): Approval of the Thomas Global Systems TFD8601Active Matrix Liquid Crystal Display installed. ADS-B Technologies, LLC
- [STC ST04136CH](https://openairdocs.org/stc/ST04136CH): Installation of a TFD-8601 EFIS (Electronic Flight Instrument System) Display. StandardAero Business Aviation Services, LLC
- [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS
- [STC ST01157SE](https://openairdocs.org/stc/ST01157SE): Installation of increased security cockpit door. Cascade Aviation Services Inc
- [STC ST02600LA](https://openairdocs.org/stc/ST02600LA): Replacement of original SAFT 4076-9 Nickel-Cadmium battery with a Concorde RG-380E/40B or RG-380E/44 or RG-380E/46 Valve Regulated Lead Acid Battery. Concorde Battery Corporation
- [STC ST02660NY-D](https://openairdocs.org/stc/ST02660NY-D): Installation of a Rockwell Collins TCAS-94. B/E Aerospace Inc
- [STC ST02661NY-D](https://openairdocs.org/stc/ST02661NY-D): Installation of a Honeywell CAS-67A TCAS 11. B/E Aerospace Inc
- [STC ST02014LA](https://openairdocs.org/stc/ST02014LA): Installation of Hawker 9750W0370-7 Steel Cased, 24 Volt, 43 Amp-hour, Sealed Lead Acid Battery. Securaplane Technologies
- [STC ST01713WI](https://openairdocs.org/stc/ST01713WI): Modification of a Rockwell Collins, Inc. AHC-85( ) (AHRS) installation. Rockwell Collins Inc
- [STC ST00673WI-D](https://openairdocs.org/stc/ST00673WI-D): Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System installation. Rockwell Collins Inc
- [STC ST00682WI-D](https://openairdocs.org/stc/ST00682WI-D): Modification of Collins VHF-20/VHF-20A/VHF-20B VHF COMM Receiver Transmitter with CTL-20 Control Pro Line I System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System Installation in accordance with Collins Installation Instructions as listed on AML No. ST00682WI-D, Revision -, or later FAA approved revisions. Rockwell Collins Inc
- [STC ST02540AT-D](https://openairdocs.org/stc/ST02540AT-D): Installation of replacement fuel tank sealant system. FFC Manufacturing
- [STC SA8815SW](https://openairdocs.org/stc/SA8815SW): Installation of a single Mode S Transponder with provisions for a Bendix TCAS II. Worldwide Aviation LLC
- [STC ST01142WI-D](https://openairdocs.org/stc/ST01142WI-D): Modification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92E control head. Rockwell Collins Inc
- [STC ST01307WI-D](https://openairdocs.org/stc/ST01307WI-D): Modification of a Collins TVI-920/TVI-920D Vertical Speed/TCAS Indicator installation. Rockwell Collins Inc
- [STC ST02990AT](https://openairdocs.org/stc/ST02990AT): Installation of Control Column Push-To-Talk (PTT) Switch with Gold Contacts. Chippewa Aerospace, Inc
- [STC ST02517AT](https://openairdocs.org/stc/ST02517AT): Installation of Avidyne FlightMax 850 display. Chippewa Aerospace, Inc
- [STC ST02777AT](https://openairdocs.org/stc/ST02777AT): Installation of a FA2100CVR Cockpit Voice Recorder (CVR). Chippewa Aerospace, Inc
- [STC ST02778AT](https://openairdocs.org/stc/ST02778AT): Installation of a FA2100FDR Flight Data Recorder (FDR). Chippewa Aerospace, Inc
- [STC ST02605AT](https://openairdocs.org/stc/ST02605AT): Installation of MPC Products Corp. Rotary Variable Transformer (RVT) P/N GA2200A (3-position sensors right side; Rudder pedal-yaw, and control column-pitch and roll,) and p/n GA2202A (2-position sensors left side, column-itch and roll) to replace existing Flight Data Recorder System (FDRS) Potentiometers position sensors. Chippewa Aerospace, Inc
- [STC ST02515AT](https://openairdocs.org/stc/ST02515AT): Installation of Honeywell MK VI EGPWS. Chippewa Aerospace
- [STC ST00062DE-D](https://openairdocs.org/stc/ST00062DE-D): Installation of MK VI GPWS system. Learjet Inc
- [STC ST00110DE-D](https://openairdocs.org/stc/ST00110DE-D): Installation of UNC UNS-1M navigation management system. Learjet Inc
- [STC ST00111DE-D](https://openairdocs.org/stc/ST00111DE-D): Installation of AlliedSignal CAS 66 TCAS I system. Learjet Inc
- [STC ST00136DE](https://openairdocs.org/stc/ST00136DE): Installation of Universal Navigation Corp UNS-1M navigation management system. Learjet Inc
- [STC ST58CH](https://openairdocs.org/stc/ST58CH): Installation of provisions of a BFG TCAS 1 and optional data recorder unit. Goodrich Avionics Systems Inc
- [STC ST09475SC](https://openairdocs.org/stc/ST09475SC): Installation of a Universal Avionics UNS-1K FMS with Internal TSO-129A GPS Sensor. Aircraft Modification and Engineering Services, In
- [STC ST00685NY](https://openairdocs.org/stc/ST00685NY): Baggage Restraint System Installation. Field Aviation Co, Inc

All 72: https://openairdocs.org/aircraft/N566SW/stcs.md

## Related

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

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