# N564SW: 1998 Embraer EMB-120

- Status: Valid registration
- Airframe: [Embraer EMB-120](https://openairdocs.org/model/embraer-emb-120) (registry code 3260201, 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: 120339
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: June 9, 1998
- Certificate issued: June 7, 2021
- Expires: June 30, 2028
- Mode S code: A7376B
- Registered owner: [Freight Runners Express Inc](https://openairdocs.org/faa-owner/FREIGHT%20RUNNERS%20EXPRESS%20INC)
- Location: [Milwaukee, WI](https://openairdocs.org/faa-place/WI/Milwaukee)
- Owner type: Corporation
- Owner's area on the map: 42.9751° N, 87.8989° W: Placed by OpenAirDocs at the center of ZIP code 53207, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=564SW
- Page: https://openairdocs.org/aircraft/N564SW

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): 70 in force

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

- [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 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 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 99-17-04](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 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
- [AD 90-17-12](https://openairdocs.org/ad/90-17-12): Flight Idle Lockout Device · Embraer - Empresa Brasileira de Aeronautica EMB-120 and EMB-120RT. Effective Sep 17, 1990

### 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

All 80: https://openairdocs.org/aircraft/N564SW/ads.md

## Information bulletins (advisory) (3 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
- [SAIB NM-08-10](https://openairdocs.org/saib/NM-08-10): Instruments - Potentiometers. Issued Dec 7, 2007
- [SAIB NM-06-39](https://openairdocs.org/saib/NM-06-39): . Issued Apr 14, 2006

## NTSB investigations

None matched to N564SW.

## FAA accident and incident reports (2)

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 20040508007159I](https://openairdocs.org/incident/20040508007159I), May 8, 2004: Emb EMB120 (N564SW), San Francisco, CA. (-23) Crew declared an emergency due to receiving a triple chime warning for engine control for the right engine. When the first officer proceeded with the…
- [Incident 20030610010689I](https://openairdocs.org/incident/20030610010689I), Jun 10, 2003: Emb EMB120ER (N564SW), San Jose, CA, Minor damage. (-23) N564SW, an Emb 120 er aircraft had just landed and was on the AOA ramp under taxi to park at the united air lines gate 2C. While making a left turn into…

## Service difficulty reports (78, newest 50)

As reported by operators and repair stations.

- [SDR SWIA201439209](https://openairdocs.org/sdr/SWIA201439209), Aug 22, 2014: CONNECTOR. UNSECURE. EMERGENCY LIGHTS ON FLOOR INOPERATIVE. SECURED CONNECTOR.
- [SDR SWIA201439167](https://openairdocs.org/sdr/SWIA201439167), Aug 14, 2014: BATTERY PACK. INOPERATIVE. F/A EMERGENCY FLASHLIGHT WEAK. R & R FLASHLIGHT BATTERIES IAW AMM. OPS CHECKED GOOD.
- [SDR SWIA201437454](https://openairdocs.org/sdr/SWIA201437454), May 9, 2014: CONTROL UNIT. FAILED. ADG DEPLOYED AFTER TAKEOFF. REPLACED AUTO DEPLOY CONTROL UNIT.
- [SDR SWIA201437453](https://openairdocs.org/sdr/SWIA201437453), May 9, 2014: LENS. BROKEN. EXIT SIGNS MISSING AT ROW 6 SEATS A & C. REPLACED BOTH EMERGENCY EXIT SIGN.
- [SDR SWIA201437532](https://openairdocs.org/sdr/SWIA201437532), May 3, 2014: CONNECTOR. OUT OF ADJUST. ONE LIGHT ON FLOOR LEVEL EMERGENCY LIGHT DOES NOT ILLUMINATE. ADJUSTED CONNECTION TO FLOOR LIGHTING.
- [SDR SWIA201436792](https://openairdocs.org/sdr/SWIA201436792), Jan 7, 2014: ATTACH FITTING. GOUGED. RT WING AT RIB 20 AILERON ATTACH FITTING HAS MINOR GOUGE AND SURFACE SCRATCHES. C-CHECK, REPLACED RT OTBD FLAP TRACK SUPPORT AND RIB 20 ASSY IAW SRM AND AMM.
- [SDR SWIA201335658](https://openairdocs.org/sdr/SWIA201335658), Dec 11, 2013: COVER. MISSING. RT SIDE OVERWING EXIT EMERGENCY LIGHT COVER MISSING. FLT 5646 REPLACED EMERGENCY EXIT LIGHT COVER FOR RT SIDE LOWER SIGN.
- [SDR SWIA201335472](https://openairdocs.org/sdr/SWIA201335472), Dec 2, 2013: CONNECTOR. DISCONNECTED. LANDING GEAR SYS DISAGREE WHEN SELECTING GEAR DOWN. LT MAIN RED B LIGHT, L MAIN GRN A LIGHT, ALL OTHER INDICATIONS NORMAL. VISUAL GEAR DOWN THROUGH CABIN WINDOW
- [SDR SWIA201333983](https://openairdocs.org/sdr/SWIA201333983), Jul 15, 2013: LIGHT. INOPERATIVE. MAIN CABIN DOOR EMERGENCY LIGHT WILL NOT ILLUMINATE. FLT#7425 REPLACED ENTRY LIGHT FIXTURE ASSEMBLY IAW AMM.
- [SDR SWIA201333982](https://openairdocs.org/sdr/SWIA201333982), Jul 15, 2013: BATTERY PACK. INOPERATIVE. FWD EMERGENCY LIGHT BATTERY PACK IS INOPERATIVE. FLT#7425 REPLACED FWD EMERGENCY POWER BATTERY LIGHT PACK IAW AMM. PN: D366-04-001, SNON: 234 & SNOFF: 213
- [SDR SWIA201333292](https://openairdocs.org/sdr/SWIA201333292), Apr 23, 2013: LIGHT. INOPERATIVE. EMERGENCY LIGHT ABOVE F/A SEAT IS BURNED OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201332614](https://openairdocs.org/sdr/SWIA201332614), Jan 21, 2013: LIGHT. INOPERATIVE. EMERGENCY OVERHEAD LIGHT AT MAIN CABIN DOOR DOES NOT ILLUMINATE. (FLT 6309) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201230455](https://openairdocs.org/sdr/SWIA201230455), Apr 18, 2012: WINDOW. LACK OF LUBE. UNABLE TO OPEN FIRST OFFICER'S DIRECT VISION WINDOW. (FLT 5487) LUBRICATED FIRST OFFICER'S DIRECT VISION WINDOW.
- [SDR SWIA201129097](https://openairdocs.org/sdr/SWIA201129097), Dec 22, 2011: CONTROLLER. FAILED. AUTO PRESSURE FAILED AND DEPRESSURIZED AT 5,000'. (FLT 6198) REPLACED ELECTRONIC PRESSURE CONTROLLER & PRESSURIZED AIRCRAFT. P/N: 22201T011400 S/N OFF: 512.
- [SDR SWIA201127597](https://openairdocs.org/sdr/SWIA201127597), Sep 7, 2011: CAM. OUT OF ADJUST. MAIN CABIN DOOR IS HARD TO OPEN. (FLT 7811) ADJUSTED MAIN CABIN DOOR FORWARD LOCK CAM.
- [SDR SWIA201127211](https://openairdocs.org/sdr/SWIA201127211), Aug 16, 2011: MECHANISM. LACK OF LUBE. MCD IS HARD TO OPEN. (FLT 6309) LUBRICATED PAX DOOR LATCHING MECHANISM.
- [SDR SWIA201126680](https://openairdocs.org/sdr/SWIA201126680), Jul 5, 2011: LIGHT. INOPERATIVE. FLOOR LEVEL EMERGENCY LIGHT NEAR MCD IS OUT. (FLT 6506) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201024476](https://openairdocs.org/sdr/SWIA201024476), Jul 1, 2010: TRANSMITTER. FAULTY. NR 2 ENGINE OIL PRESSURE SPIKED TO 80 PSI. ENGINE SHUT DOWN. (FLT 7772) REPLACED PRESSURE TRANSMITTER P/N APT-79-1000-80D, S/N OFF 4703-3-258.
- [SDR SWIA201024033](https://openairdocs.org/sdr/SWIA201024033), Mar 29, 2010: SPLICE. OVERHEATED. SPLICE SPBK38 DISCOLORED. (C CHECK) REPLACED SPLICE SPBK38.
- [SDR SWIA201024031](https://openairdocs.org/sdr/SWIA201024031), Mar 19, 2010: MOUNT FITTING. CRACKED. LEFT MOUNT CLIP AFT OF DV WINDOW FRAME 13 CRACKED. (C CHECK) REPAIRED PER SRM.
- [SDR SWIA201024032](https://openairdocs.org/sdr/SWIA201024032), Mar 17, 2010: SKIN. CRACKED. RIGHT NACELLE FLAP LOWER SKIN CRACKED. (C CHECK) REPLACED FLAP PER AMM.
- [SDR SWIA201023667](https://openairdocs.org/sdr/SWIA201023667), Feb 7, 2010: MECHANISM. LACK OF LUBE. MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6642) LUBED DOOR MECHANISM.
- [SDR SWIA200922281](https://openairdocs.org/sdr/SWIA200922281), Aug 6, 2009: HYDRAULIC LINE. LEAKING. HYDRAULIC FUMES IN COCKPIT. (FLT 7774) REPAIRED RUDDER HYDRAULIC LINE AT AFT BULKHEAD PER AMM.
- [SDR SWIA200921726](https://openairdocs.org/sdr/SWIA200921726), May 29, 2009: SIGN. BROKEN. AFT LOWER EMERGENCY EXIT SIGN BROKEN. (FLT 6457) REPLACED LIGHT ASSEMBLY.
- [SDR SWIA200921397](https://openairdocs.org/sdr/SWIA200921397), Apr 7, 2009: CABIN PRESSURE. FAILED. FLT 6388 - CABIN LOST PRESSURE. SYSTEM CHECKS ACCOMPLISHED AND CHECK NORMAL.
- [SDR SWIA200921344](https://openairdocs.org/sdr/SWIA200921344), Mar 22, 2009: LIGHT. BROKEN. FLT 5761 - EXIT ROW 6A EMERGENCY LIGHT BROKEN. REPLACED EXIT LIGHT ASSEMBLY.
- [SDR SWIA200921232](https://openairdocs.org/sdr/SWIA200921232), Mar 19, 2009: SIGN. BROKEN. FLT 5574 - EXIT SIGN ON MAIN CABIN DOOR BROKEN. REPLACED SIGN.
- [SDR SWIA200921057](https://openairdocs.org/sdr/SWIA200921057), Feb 13, 2009: STRINGER. CORRODED. C-CHECK, STRINGER 18L BETWEEN FRAME 13 AND 14 CORRODED, MAJOR REPAIR. REPAIRED PER EMB SRM 53-10-03.
- [SDR SWIA200921013](https://openairdocs.org/sdr/SWIA200921013), Feb 8, 2009: CONNECTOR. BURNED. FLT 7760 - ROTATING BEACON CONNECTOR BURNED. REPLACED BEACON ASSEMBLY AND CONNECTOR.
- [SDR SWIA200921012](https://openairdocs.org/sdr/SWIA200921012), Feb 8, 2009: COVER. MISSING. FLT 7759 - "EXIT" LIGHT COVER AT SEAT 6 C IS MISSING. REPLACED LIGHT ASSEMBLY.
- [SDR SWIA200820383](https://openairdocs.org/sdr/SWIA200820383), Nov 7, 2008: UNKNOWN. SMOKE. FLT 5734 - AFTER POWER REDUCTION IN DESCENT, AIRCRAFT FILLED WITH SMOKE. SMOKE LIGHT ON MAP ASSOCIATED WITH LAV DETECTOR. INSPECTED RT AND LT ENGINES, RT AND LT
- [SDR SWIA200820077](https://openairdocs.org/sdr/SWIA200820077), Sep 23, 2008: LIGHT. INOPERATIVE. FORWARD EMERGENCY LIGHT INOP. (FLT 5464) ALL FORWARD EMERGENCY LIGHTS CHECK NORMAL. 
- [SDR SWIA200820023](https://openairdocs.org/sdr/SWIA200820023), Jul 25, 2008: CONTACTOR. BURNED. FOUND CONTACTOR IN APU AUX RELAY BOX BURNED. C-CHECK, REPLACED APU CONTACTOR IN APU AUX RELAY SHELF. 
- [SDR SWIA200820022](https://openairdocs.org/sdr/SWIA200820022), Jul 25, 2008: BUSS BAR. BURNED. FOUND BUSS BARS IN APU RELAY BOX BURNED. C-CHECK, INSTALLED NEW SERVICABLE BUSS BARS. 
- [SDR SWIA200820026](https://openairdocs.org/sdr/SWIA200820026), Jul 24, 2008: SUPPORT ANGLE. CRACKED. AFT SUPPORT ANGLE IS CRACKED IN FRONT OF PAX DOOR. C-CHECK, REPLACED AFT SUPPORT ANGLE. 
- [SDR SWIA200820025](https://openairdocs.org/sdr/SWIA200820025), Jul 24, 2008: FLOOR SUPPORT. CRACKED. JUMP SEAT FLOORBOARD, LT AND RT FLOOR PROP ANGLES ARE CRACKED. C-CHECK, REPLACED RT FLOOR PROP ANGLES.
- [SDR SWIA200820028](https://openairdocs.org/sdr/SWIA200820028), Jul 22, 2008: FLOOR SUPPORT. CRACKED. RT FLOOR PROP CRACKED AT FRAME 13. C-CHECK, INSTALLED FILLER AND DOUBLER.
- [SDR SWIA200820027](https://openairdocs.org/sdr/SWIA200820027), Jul 22, 2008: FRAME. CRACKED. RT NACELLE O/B WHEEL WELL FRAME IS CRACKED. C-CHECK, INSTALLED REPAIR DOUBLER TO NR 2 NACELLE WHEEL WELL INNER WEB SUPPORT INTERCOSTAL O/B SIDE.
- [SDR SWIA200819242](https://openairdocs.org/sdr/SWIA200819242), Feb 15, 2008: SIGN. BROKEN. FLOOR EMERGENCY EXIT SIGN IS BROKEN. REPLACED EMERGENCY EXIT SIGN. OPS CHECK GOOD. 
- [SDR SWIA200718608](https://openairdocs.org/sdr/SWIA200718608), Aug 12, 2007: ROLLER. BINDING. MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN, FLIGHT NR 5752. LUBED ROLLERS AS REQUIRED. OPS CHECK GOOD AT THIS TIME.
- [SDR SWIA200718555](https://openairdocs.org/sdr/SWIA200718555), Jul 30, 2007: BATTERY PACK. DISCHARGED. SEVERAL EMERGENCY LIGHTS ARE INOP, FLIGHT NR 3684. REPLACED CENTER EMERGENCY LIGHT BATTERY IAW MM 33-50-02. OPS CHECK GOOD.
- [SDR SWIA200617646](https://openairdocs.org/sdr/SWIA200617646), Dec 21, 2006: WIRE. LOOSE. RIGHT PACK PRODUCES OVERHEATED ODOR. SECURED WIRE TO RIGHT PACK SWITCH "LOW". OPS CHECKED GOOD.
- [SDR SWIA200617501](https://openairdocs.org/sdr/SWIA200617501), Dec 21, 2006: WIRE. LOOSE. RIGHT PACK PRODUCES OVERHEATED SMELL. RESECURED WIRE TO RIGHT PACK SWITCH, OPERATIONAL CHECKS GOOD.
- [SDR SWIA200617639](https://openairdocs.org/sdr/SWIA200617639), Oct 18, 2006: FRAME. CRACKED. CENTER RIB FRAME 13 BEHIND PILOTS AFT DV POST IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CENTER SUPPORT BRACKET (RIB) AT FRAME 13 BEHIND PILOTS 
- [SDR SWIA200617638](https://openairdocs.org/sdr/SWIA200617638), Oct 18, 2006: FLOORBEAM. CORRODED. RIGHT SIDE FLOORBEAM AT FRAME 39 REQUIRES REPLACEMENT DUE TO CORROSION, DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT SIDE FLOORBEAM AT FRAME 39 PER 51-4
- [SDR SWIA200617637](https://openairdocs.org/sdr/SWIA200617637), Oct 18, 2006: FLOORBEAM. CORRODED. RIGHT SIDE FLOORBEAM AT FRAME 40 FLOOR REQUIRES REPLACEMENT DUE TO CORROSION, DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT SIDE FLOORBEAM AT FRAME 40 PE
- [SDR SWIA200616924](https://openairdocs.org/sdr/SWIA200616924), Jul 30, 2006: UNKNOWN. FUMES. WHEN THE BLEEDS ARE SWITCHED FROM ENGINE TO APU IN FLIGHT, OIL FUMES ARE SMELLED IN THE COCKPIT AND CABIN. COULD NOT DUPLICATE.
- [SDR SWIA200616776](https://openairdocs.org/sdr/SWIA200616776), Jun 6, 2006: GCU. MALFUNCTIONED. AFTER APU SHUTDOWN SMOKE FILLED THE COCKPIT. REPLACED APU GCU. REPLACED APU STARTER/GEN AND REPLACED FEEDER PROTECTION RELAY. OPERATIONAL CHECKS GOOD, PN23080-0
- [SDR SWIA200616570](https://openairdocs.org/sdr/SWIA200616570), Apr 7, 2006: SERVO. MALFUNCTIONED. ON PREFLIGHT OF FLIGHT CONTROLS. NOTICED RESISTANCE IN AILERON CIRCUIT. REPLACED AILERON SERVO IAW MM 22-10-05, OPERATIONAL CHECK GOOD.
- [SDR SWIA200515640](https://openairdocs.org/sdr/SWIA200515640), Sep 30, 2005: SERVO. MALFUNCTIONED. BINDING AND FRICTION FELT IN ELEVATOR MOVEMENT. REPLACED ELEVATOR SERVO IAW EMB 120 MM 22-10-05. OPERATIONAL CHECK GOOD.

All 78: https://openairdocs.org/aircraft/N564SW/reports.md

## Related

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

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