# N567SW: 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: 120342
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: August 4, 1998
- Certificate issued: June 13, 2013
- Expires: June 30, 2029
- Mode S code: A74290
- Registered owner: [Jahn 567sw LLC](https://openairdocs.org/faa-owner/JAHN%20567SW%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=567SW
- Page: https://openairdocs.org/aircraft/N567SW

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 N567SW.

## 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; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20120420012581I](https://openairdocs.org/incident/20120420012581I), Apr 20, 2012: Embraer EMB-120ER (N567SW), Los Angeles, CA, Minor damage. On 04/20/2012, at approximately 20:15 PDT, skywest airlines flight #6310, an EMB-120 (N567SW), Los Angeles (lax) to palm springs (psp), clipped the wing of…

## Service difficulty reports (103, newest 50)

As reported by operators and repair stations.

- [SDR JIKA2022110301](https://openairdocs.org/sdr/JIKA2022110301), Nov 3, 2022: ENGINE. OIL CONSUMPTION. PILOT PERFORMED EMERGENCY LANDING IN SAT DUE TO RT ENGINE ERRATIC OIL PRESSURE. INITIALLY WHEN LEAVING MMIO OIL LEVEL WAS GOOD. AFTER LANDING & CHECKING OIL IN 
- [SDR JIKA2022102601](https://openairdocs.org/sdr/JIKA2022102601), Oct 26, 2022: OIL SYSTEM. LOW. DURING CRUISE FLIGHT, GOT A MASTER WARNING AND THE OIL PRESSURE FOR RT ENGINE BEGAN TO FLICKER AND EVENTUALLY DROPPED BELOW 40 PSI. FOLLOWED QRH PROCEDURE & PRE
- [SDR JIKA2020011701](https://openairdocs.org/sdr/JIKA2020011701), Jan 17, 2020: HMU. FAILED. DURING INITIAL CLIMB, AT ABOUT 1,000 FEET AGL, LH PROPELLER INADVERTENTLY FEATHERED. WE PERFORMED MEMORY ITEMS, FOLLOWED BY QRH. ENGINE PARAMETERS RETURNED BACK
- [SDR JIKA2019091001](https://openairdocs.org/sdr/JIKA2019091001), Sep 3, 2019: HMU. ERRATIC. THE FLIGHT CREW REPORTED THAT AT APPROXIMATELY 800-1000' AGL, THE LT PROPELLER INADVERTENTLY FEATHERED. THE FLIGHT CREW RAN THE "INADVERTENT PROPELLER FEATHER" 
- [SDR JIKA2019083001](https://openairdocs.org/sdr/JIKA2019083001), Aug 27, 2019: TORQUE SENSOR. INTERMITTENT. THE FLIGHT CREW REPORTED THAT DURING INITIAL CLIMB OUT AT APPROXIMATELY 500 FEET, THERE WAS A PARTIAL LOSS OF POWER ON THE LEFT HAND ENGINE. THIS LOSS COULD BE 
- [SDR SWIA201439066](https://openairdocs.org/sdr/SWIA201439066), Jul 31, 2014: BATTERY PACK. INOPERATIVE. FLOOR LEVEL EMERGENCY LIGHTS BY 2A & 3A ARE INOPERATIVE. R & R THE BATTERY PACK IAW AMM. SYSTEM OPS CHECKED GOOD.
- [SDR SWIA201438506](https://openairdocs.org/sdr/SWIA201438506), Jun 30, 2014: BULB. INOPERATIVE. LEFT OVERWING EMERGENCY LIGHT WILL NOT ILLUMINATE. R & R BULB IAW AMM.
- [SDR SWIA201438386](https://openairdocs.org/sdr/SWIA201438386), Jun 20, 2014: RELAY. FAILED. ELECTRICAL ODORIN THE COCKPIT. R & R APU FEEDER PROTECTION RELAY, APU FEEDER PROTECTION RELAY STAND AND APU START CONTACTOR. OPS CHECK GOOD AT THIS TIME.
- [SDR SWIA201436590](https://openairdocs.org/sdr/SWIA201436590), Mar 1, 2014: HYDRAULIC LINE. LEAKING. LOST ALL FLUID IN THE GREEN HYD RESERVOIR. FOUND RT MLG FWD OTBD GEAR DOOR ACTUATOR HOSE LEAKING. FLT 5325 REPLACED HYD HOSE FOR THE RT MLG FWD OTBD GEAR DOOR A
- [SDR SWIA201436203](https://openairdocs.org/sdr/SWIA201436203), Jan 28, 2014: CHANNEL. CRACKED. PAX DOOR LOWER INNER CHANNEL CRACKED. C-CHECK R & R PAX DOOR LOWER INNER CHANNEL IAW SRM, PN 120-26563-001.
- [SDR SWIA201436204](https://openairdocs.org/sdr/SWIA201436204), Jan 23, 2014: RIB. CRACKED. RT WING INBD LE INBD FALSE RIB CRACKED. C-CHECK STOP DRILLED CRACK & INSTALLED REINFORCED DOUBLER 2024-T3 0.032" ON RT WING INBD LE INBD FALSE RIB IAW SRM.
- [SDR SWIA201436211](https://openairdocs.org/sdr/SWIA201436211), Jan 20, 2014: BRACKET. CRACKED. CRACK ON LOWER RT ANGLED FRAME UNDER OBSERVERS SEAT. C-CHECK INSTALLED INSERTION DOUBLER TO L BRACKET AT RT COCKPIT ENTRY STEP IAW SRM.
- [SDR SWIA201436210](https://openairdocs.org/sdr/SWIA201436210), Jan 20, 2014: BRACKET. CRACKED. CRACK ON LOWER LT ANGLED FRAME UNDER OBSERVERS SEAT. C-CHECK INSTALLED INSERTION DOUBLER TO LT BRACKET AT LT COCKPIT ENTRY STEP IAW SRM.
- [SDR SWIA201436209](https://openairdocs.org/sdr/SWIA201436209), Jan 20, 2014: ANGLE. CORRODED. CABIN PAX ENTRANCE LOWER THRESHOLD ANGLE IS CORRODED. C-CHECK REPLACED PAX DOOR ENTRYWAY LOWER & AFT LOWER THRESHOLD ANGLES IAW SRM.
- [SDR SWIA201436208](https://openairdocs.org/sdr/SWIA201436208), Jan 20, 2014: SUPPORT. CRACKED. CARGO COMPARTMENT AFT TRACK UPPER SUPPORT BOX IS CRACKED. C-CHECK REPLACED CARGO COMPARTMENT AFT TRACK UPPER SUPPORT IAW SRM, PN 120-48716-001.
- [SDR SWIA201436207](https://openairdocs.org/sdr/SWIA201436207), Jan 20, 2014: DRAIN MAST. CRACKED. RT NACELLE DRAIN MAST SHEET METAL PORTION CRACKED ON NACELLE. C-CHECK REPLACED RT NACELLE DRAIN MAST IAW SRM.
- [SDR SWIA201436206](https://openairdocs.org/sdr/SWIA201436206), Jan 20, 2014: FRAME. CRACKED. CRACK ON LT OTBD NACELLE OTBD OF FWD UPPER LATERAL FWD ATTACH POINT. C-CHECK REPLACED LT OTBD NACELLE FWD UPPER LATERAL FWD ATTACH POINT FRAME IAW SRM.
- [SDR SWIA201436205](https://openairdocs.org/sdr/SWIA201436205), Jan 20, 2014: RECEPTACLE. CRACKED. CRACK ON LT INBD NACELLE AT LOWER SHOOT BOLT RECEPTACLE. C-CHECK REPLACED LT INBD NACELLE LOWER SHOOT BOLT RECEPTACLE IAW SRM.
- [SDR SWIA201436215](https://openairdocs.org/sdr/SWIA201436215), Jan 19, 2014: DOOR FRAME. CRACKED. PAX DOOR FRAME 15 UNDERSIDE CRACKED. C-CHECK REPLACED PAX DOOR CHANNEL FRAME ASSEMBLY IAW SRM, PN 120-21058-003.
- [SDR SWIA201436214](https://openairdocs.org/sdr/SWIA201436214), Jan 19, 2014: FRAME. CRACKED. PAX DOOR AFT STEP FRAME CRACKED AT LOWER RADIUS. C-CHECK REPLACED PAX DOOR AFT STEP FRAME IAW SRM, PN 120-19619-001.
- [SDR SWIA201436213](https://openairdocs.org/sdr/SWIA201436213), Jan 19, 2014: BUTTSTRAP. CORRODED. CORROSION ON LT BUTT STRAP JUST FWD OF CARGO DOOR. C-CHECK NEW BUTT STRAP INSTALLED ON LT JUST FWD OF CARGO DOOR IAW SRM, PN 120-46163-001.
- [SDR SWIA201436212](https://openairdocs.org/sdr/SWIA201436212), Jan 19, 2014: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR TO WALL STRINGER UNDER LAVATORY. C-CHECK REPLACED CARGO SILL ASSEMBLY FLOOR SUPPORT IAW SRM, PN 120-06159-501.
- [SDR SWIA201435999](https://openairdocs.org/sdr/SWIA201435999), Jan 10, 2014: MODULE. FAILED. AFTER TAKEOFF, HAD TO USE THE DOWN LOCK RELEASE TO RAISE THE GEAR HANDLE, COMPLIED WITH THE QRH. DURING THE CLIMB, RECEIVED THE "FLAPS, TRIM, AUTOFEATHER" CONFI
- [SDR SWIA201436000](https://openairdocs.org/sdr/SWIA201436000), Jan 8, 2014: UNKNOWN. ODOR. UPON STARTING THE APU & OPENING THE BLEEDS, THE AIRCRAFT WAS FILLED WITH A VERY STRONG SMELL OF FUEL. FLT 5532 INSPECTED APU FOR FUEL LEAKS, NO LEAKS FOUND. SHU
- [SDR SWIA201335186](https://openairdocs.org/sdr/SWIA201335186), Oct 27, 2013: LIGHT. OBSTRUCTED. EMERGENCY FLOOR LIGHTING AT ROW 9 OBSTRUCTED. FLT 5438 REPOSITIONED FLOOR STRIP TO EXPOSE 2ND RED LIGHT.
- [SDR SWIA201335031](https://openairdocs.org/sdr/SWIA201335031), Oct 20, 2013: COVER. MISSING. EMERGENCY EXIT LIGHT COVER IS MISSING. FLT 5404 REPLACED EMERGENCY EXIT LIGHT ASSEMBLY BY FLIGHT ATTENDANT'S JUMP SEAT.
- [SDR SWIA201333691](https://openairdocs.org/sdr/SWIA201333691), Jun 9, 2013: LIGHT. INOPERATIVE. REAR RED FLOOR EMERGENCY LIGHT DOES NOT ILLUMINATE. RELAMPED.
- [SDR SWIA201333337](https://openairdocs.org/sdr/SWIA201333337), Apr 26, 2013: CONNECTOR. DISCONNECTED. FIVE FLOOR LEVEL EMERGENCY LIGHTS DO NOT ILLUMINATE. (FLT 5307) RECONNECTED LOOSE CONNECTOR ON FIRST ROW FLOOR EMERGENCY LIGHT.
- [SDR SWIA201232388](https://openairdocs.org/sdr/SWIA201232388), Dec 17, 2012: LIGHT. INOPERATIVE. EMERGENCY FLOOR LIGHT ADJACENT TO SEAT 11A BURNED OUT. (FLT 5442) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201232170](https://openairdocs.org/sdr/SWIA201232170), Nov 12, 2012: UNKNOWN. MALFUNCTIONED. RETURN TO FIELD DUE TO EXCESSIVE AND UNUSUAL CONTROL FORCES AND INPUTS TO MAINTAIN LEVEL FLIGHT. RUDDER & AILERON INPUT MUCH GREATER THAN NORMAL. (FLT 1352) COM
- [SDR SWIA201232023](https://openairdocs.org/sdr/SWIA201232023), Oct 10, 2012: COMPUTER. FAILED. UNCOMMANDED PITCH DOWN, CAPTAIN'S COMMAND BARS DISAPPEARED AND RECEIVED "FD" FLAG ON EADI, AND "EGPWS INOP" AND "TERRAIN INOP" ON MAP. (FLT 6246) REPLACED NR 1 
- [SDR SWIA201231780](https://openairdocs.org/sdr/SWIA201231780), Sep 10, 2012: DUCT. BLOWN. ON ROTATION DUCT LEAKAGE LIGHT ON LEFT SIDE CAME ON. (FLT 5367) FOUND BLOWN LEFT WRAP AROUND BLEED DUCT. REPLACED LEFT ENGINE WRAP AROUND BLEED DUCT IN REFERENC
- [SDR SWIA201230498](https://openairdocs.org/sdr/SWIA201230498), Apr 21, 2012: RIB. DAMAGED. DAMAGED RIB 27 WING TIP EDGE. (SERVICE) REPAIRED LEFT WING RIB 27 TRAILING EDGE.
- [SDR SWIA201230495](https://openairdocs.org/sdr/SWIA201230495), Apr 18, 2012: SIGN. BROKEN. EXIT ROW SIGN AT 6A BROKEN. (FLT 5506) REPLACED EXIT ROW'S SEAT 6A EMERGENCY LIGHT ASSEMBLY PER AMM.
- [SDR SWIA201230177](https://openairdocs.org/sdr/SWIA201230177), Mar 14, 2012: WIRE. BROKEN. THE CABIN FLOOR EMERGENCY LIGHTS BETWEEN ROW 3 AND 6 DO NOT ILLUMINATE. (FLT 5478) REPAIRED BROKEN WIRE BELOW FLOOR AT ROW 5.
- [SDR SWIA201230107](https://openairdocs.org/sdr/SWIA201230107), Mar 9, 2012: LIGHT. INOPERATIVE. OVERHEAD EMERGENCY LIGHT AT ROW 9 IS OUT. (C-CHECK) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201128409](https://openairdocs.org/sdr/SWIA201128409), Oct 24, 2011: LIGHT. INOPERATIVE. FLOOR EMERGENCY EXIT LIGHT NEAR MCD IS OUT. (FLT 5347) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201128036](https://openairdocs.org/sdr/SWIA201128036), Oct 1, 2011: WIRE. BROKEN. EMERGENCY LIGHTS ON FLOOR BY ROWS 1 AND 2 ARE INOPERATIVE. (FLT 5322) REPAIRED BROKEN WIRE ON TRACK LIGHTING AT FORWARD CONNECTOR TO RED LIGHTS.
- [SDR SWIA201127138](https://openairdocs.org/sdr/SWIA201127138), Aug 6, 2011: SEQUENCE VALVE. FAILED. LEFT MAIN GEAR DID NOT RETRACT FOR 2 MINS AFTER RAISING GEAR LEVER. (FLT 6323) REPLACED LEFT INBOARD SEQUENCE VALVE ASSEMBLY AND LEFT GEAR DOWN UNLOCKING ACTUAT
- [SDR SWIA201125702](https://openairdocs.org/sdr/SWIA201125702), Feb 20, 2011: SOCKET. FAULTY. OVERHEAD EMERGENCY LIGHT ABOVE ROW 6 FLICKERS. (FLT 6423)REPLACED LIGHT SOCKET FOR EMERGENCY LIGHT ABOVE ROW 6.
- [SDR SWIA201025021](https://openairdocs.org/sdr/SWIA201025021), Oct 6, 2010: SENSOR. FAULTY. RECEIVED INTERMITTENT "ELEC" LIGHT ON MAP. NUMEROUS RELAYS SWITCHING AND ELECTRICAL BURNING SMELL. (FLT 6571) REPLACED LT WOW SENSOR AND LANDING GEAR RELAY BOX.
- [SDR SWIA201024793](https://openairdocs.org/sdr/SWIA201024793), Aug 27, 2010: SERVO. MALFUNCTIONED. AFTER ENGAGING F/O'S AUTOPILOT, RUDDER KICKED HARD TAIL RIGHT. (FLT 6810) TROUBLESHOOTING AUTOPILOT SYSTEMS. REPLACED RUDDER PRIMARY SERVO AND SERVO SUPPORT PER
- [SDR SWIA201024810](https://openairdocs.org/sdr/SWIA201024810), Jul 31, 2010: STRINGER. CRACKED. LEFT INBOARD WING FUEL TANK LOWER STRINGER 10 IS CRACKED BETWEEN STATION 8-9. (C-CHECK) REPAIRED PER SRM.
- [SDR SWIA201024809](https://openairdocs.org/sdr/SWIA201024809), Jul 31, 2010: STRINGER. CRACKED. RIGHT INBOARD WING STRINGER 10 CRACKED BETWEEN RIBS 8 AND 9 AT ACCESS PANEL AREA. (C-CHECK) REPAIRED PER SRM.
- [SDR SWIA201023605](https://openairdocs.org/sdr/SWIA201023605), Jan 31, 2010: ROLLER. OUT OF ADJUST. MAIN CABIN DOOR DIFFICULT TO CLOSE. (FLT 6263) LUBED DOOR AND ADJUSTED MAIN CABIN DOOR FORWARD LOCK CAM ACTUATING ROD AND UPPER ROLLER.
- [SDR SWIA201023561](https://openairdocs.org/sdr/SWIA201023561), Jan 21, 2010: CUSHION. OUT OF POSITION. MAIN CABIN DOOR HARD TO CLOSE. (FLT 5815) REPOSITIONED FLIGHT ATTENDANT SEAT CUSHION.
- [SDR SWIA201023509](https://openairdocs.org/sdr/SWIA201023509), Jan 14, 2010: ROLLER. LACK OF LUBE. MAIN CABIN DOOR WILL NOT SHUT. (FLT 6175) LUBED ROLLERS AND ATTACH POINTS.
- [SDR SWIA201023457](https://openairdocs.org/sdr/SWIA201023457), Jan 6, 2010: SMOKE DETECTOR. MALFUNCTIONED. FLT 5763 - BAGGAGE SMOKE/FIRE WARNING LIGHT REMAINS ON. REPLACED AFT SMOKE DETECTOR.
- [SDR SWIA200923016](https://openairdocs.org/sdr/SWIA200923016), Nov 3, 2009: BONDING STRAP. OUT OF POSITION. AT CRUISE CABIN LOST PRESSURIZATION. (FLT 6843) REMOVED BONDING STRAP FROM OUTFLOW VALVE. ALL CABIN O2 MASKS DEPLOYED DUE TO LOSS OF PRESSURIZATION. INSPECTED, 
- [SDR SWIA200921352](https://openairdocs.org/sdr/SWIA200921352), Mar 28, 2009: LIGHT. BROKEN. FLT 7756 - EMERGENCY LIGHT ON OUTSIDE OF FUSELAGE RIGHT AFT SIDE INOP. REPLACED LIGHT HOUSING.

All 103: https://openairdocs.org/aircraft/N567SW/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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