# N229SW: 1995 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: 120.305
- Year built: 1995
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: November 22, 1995
- Certificate issued: August 7, 2014
- Expires: August 31, 2027
- Mode S code: A20415
- 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=229SW
- Page: https://openairdocs.org/aircraft/N229SW

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

None matched to N229SW.

## NTSB investigations on N229SW not matched to an aircraft (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 NYC64I0104](https://openairdocs.org/ntsb/NYC64I0104), Feb 11, 1964: Canadair CL-44 (N229SW), Gander Newfoundld, Canada, incident, minor damage

## 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 19960425012409I](https://openairdocs.org/incident/19960425012409I), Apr 25, 1996: Emb EMB120ER (N229SW), Las Vegas, NV. Narrative: at rotation during takeoff a vibration was felt as well as rapid pressurization fluctuations. The landing gear was retracted and the vibration and…

## Service difficulty reports (119, 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 HKGA20230314001](https://openairdocs.org/sdr/HKGA20230314001), Mar 14, 2023: SPLICE. BROKEN. WHILE ACCOMPLISHING A REPAIR OF THE IB SIDE SKIN OF THE RH ENGINE NACELLE, AFTER REMOVAL OF THE EXISTING STRINGER [PN 120-41441-002] THE FWD. SPLICE-PROFILE 1 [
- [SDR HKGA20170427004](https://openairdocs.org/sdr/HKGA20170427004), Apr 27, 2017: FRAME. CORRODED. DURING A ROUTINE INSPECTION, CORROSION WAS NOTED AT FRAME 21, BETWEEN STRINGERS 20 AND 21R. CORROSION DAMAGE WAS REMOVED AND REPAIRED IAW SRM 53-00-01.
- [SDR SWIA201438500](https://openairdocs.org/sdr/SWIA201438500), May 27, 2014: WIRE. BROKEN. CABIN EMERGENCY LIGHT AFT FEMALE CONNECTOR IS BROKEN OFF WIRES FROM AIRFRAME. INSTALLED CONNECTOR AND REPLACED THE TERMINAL CONNECTOR IAW AMM.
- [SDR SWIA201438499](https://openairdocs.org/sdr/SWIA201438499), May 25, 2014: SHEAR TIE. CORRODED. BELLY SKIN SHEAR TIE CORRODED AT FRAME 38. REPLACED SHEAR TIE IAW SRM.
- [SDR SWIA201438498](https://openairdocs.org/sdr/SWIA201438498), May 8, 2014: SKIN. DAMAGED. LOWER SKIN ON RIGHT SIDE AND FWD OF BS 1531.8 IS DAMAGED. REPLACED LOWER SKIN IAW SRM.
- [SDR SWIA201438497](https://openairdocs.org/sdr/SWIA201438497), May 8, 2014: SKIN. DAMAGED. LOWER SKIN ON LEFT SIDE AND FWD OF BS 1531.8 IS DAMAGED. REPAIRED SKIN IAW ETD.
- [SDR SWIA201438496](https://openairdocs.org/sdr/SWIA201438496), May 8, 2014: STRINGER. DAMAGED. STRINGER 19L IS DAMAGED BETWEEN FRAMES 43 - 45. REPAIRED STRINGER IAW SRM.
- [SDR SWIA201438495](https://openairdocs.org/sdr/SWIA201438495), May 8, 2014: STRINGER. DAMAGED. STRINGER 20L IS DAMAGED BETWEEN FRAMES 43 - 45. REPAIRED STRINGER IAW SRM.
- [SDR SWIA201438494](https://openairdocs.org/sdr/SWIA201438494), May 8, 2014: STRINGER. DAMAGED. STRINGER 21L IS DAMAGED BETWEEN FRAMES 43 - 45. REPAIRED STRINGER IAW SRM.
- [SDR SWIA201438493](https://openairdocs.org/sdr/SWIA201438493), May 8, 2014: STRINGER. DAMAGED. STRINGER 21R IS DAMAGED BETWEEN FRAMES 43 - 45. REPAIRED STRINGER IAW SRM.
- [SDR SWIA201438492](https://openairdocs.org/sdr/SWIA201438492), May 8, 2014: STRINGER. DAMAGED. STRINGER 20R IS DAMAGED BETWEEN FRAMES 43 AND 45. REPAIRED STRINGER IAW SRM.
- [SDR SWIA201436596](https://openairdocs.org/sdr/SWIA201436596), Feb 28, 2014: LIGHT. INOPERATIVE. WHITE EMERGENCY LIGHT ON FLOOR BY SEAT 4A IS BURNED OUT. FLT 6233 RELAMPED.
- [SDR SWIA201436465](https://openairdocs.org/sdr/SWIA201436465), Feb 13, 2014: UNKNOWN. ODOR. BURNING SMELL COMING FROM LAVATORY. FLT 6246 AIR OUT AIRCRAFT, NO NEW ODOR, SUSPECT AIRCRAFT HEATING TO EMIT BURNING ODOR.
- [SDR SWIA201335430](https://openairdocs.org/sdr/SWIA201335430), Nov 22, 2013: WIRE. BROKEN. EMERGENCY OVERHEAD LIGHTING AT ROW 8 ABC DOES NOT ILLUMINATE. FLT 5371 REPAIRED BROKEN WIRE ON LIGHT ASSEMBLY AT ROW 8 ABC.
- [SDR SWIA201335350](https://openairdocs.org/sdr/SWIA201335350), Nov 15, 2013: LIGHT. INOPERATIVE. EMERGENCY OVERHEAD LIGHTS IN ROW 9 SEATS B-C ARE BURNED OUT. FLT 6346 RELAMPED.
- [SDR SWIA201335043](https://openairdocs.org/sdr/SWIA201335043), Oct 20, 2013: DRAIN. BROKEN. BLUE HYDRAULIC SYSTEM NACELLE DRAIN IS CRACKED & BROKEN. C-CHECK REPLACED NACELLE DRAIN MASS ON RT OTBD NACELLE FOR BLUE HYDRAULIC SYSTEM IAW SRM.
- [SDR SWIA201335044](https://openairdocs.org/sdr/SWIA201335044), Oct 12, 2013: STRINGER. CRACKED. RT WING HAS A CRACKED STRINGER FWD OF FUEL ACCESS PANEL CUTOUT NR 2. C-CHECK REPAIRED STRINGER NR 10 ON RT WING FWD OF NR 2 FUEL ACCESS PANEL IAW SRM.
- [SDR SWIA201335045](https://openairdocs.org/sdr/SWIA201335045), Oct 11, 2013: FIREWALL. CHAFED. RT ENGINE FIRE WALL IS CHAFED AT 12 O CLOCK POSITION. C-CHECK REPAIRED IAW ETD.
- [SDR SWIA201335046](https://openairdocs.org/sdr/SWIA201335046), Oct 10, 2013: STRINGER. CORRODED. STRINGER 18L CORRODED NEAR FRAME 13A. C-CHECK SPLICED IN NEW FRONT SECTION OF STRINGER 18L IAW SRM.
- [SDR SWIA201335047](https://openairdocs.org/sdr/SWIA201335047), Oct 5, 2013: FIREWALL. CRACKED. LT GEAR WELL THRU ACCESS 434 FZ, FIREWALL HAS CRACKS. C-CHECK REPLACED UPPER SUPPORT BULKHEAD AT LT NACELLE FRAME 14 PART 120 32357-001 IAW SRM.
- [SDR SWIA201335048](https://openairdocs.org/sdr/SWIA201335048), Oct 4, 2013: BRACKET. CRACKED. FOUND A CRACK UNDER THE CAPTAINS DV WINDOW LOWER CHANNEL ON A RIB BRACKET RIGHT NEXT TO THE TILLER HANDLE. C-CHECK NEW FRAME NR 9 SPLICED IN AT UPPER END AT LT 
- [SDR SWIA201335051](https://openairdocs.org/sdr/SWIA201335051), Oct 3, 2013: FITTING. CRACKED. LT NACELLE INBD FITTING CRACKED. C-CHECK REPLACED STRUCTURAL COMPONENT IAW SRM. REPLACED INBD FITTING PN 120-22916-002 AT LT NACELLE IAW SRM.
- [SDR SWIA201335050](https://openairdocs.org/sdr/SWIA201335050), Oct 3, 2013: SKIN. DAMAGED. RT NACELLE OTBD FWD & ABOVE MLG DOOR OVERSIZED RIVETS PULLING THROUGH SKIN. C-CHECK DOUBLER INSTALLED OVER AREA & INTERNAL TO BRING RIVETS BACK TO ORIGINAL SIZE
- [SDR SWIA201335049](https://openairdocs.org/sdr/SWIA201335049), Oct 3, 2013: COWLING. CRACKED. LT EXHAUST MIDDLE COWL IS CRACKED OUT IN THE AREA BY OTBD COWL PIN LATCH RECEPTACLE AREA. C-CHECK REPAIRED LT EXHAUST MIDDLE COWL OTBD DOOR AFT PIN FRAME IAW SR
- [SDR SWIA201335064](https://openairdocs.org/sdr/SWIA201335064), Oct 2, 2013: SKIN. CRACKED. RT WING SKIN CLEAT CRACKED, TOP & INBD PANEL 5. C-CHECK REPLACED 1 UPPER SKIN CLEAT PN120-17063-009 ON RT WING INBD OF NR 5 FUEL PANEL IAW SRM.
- [SDR SWIA201335063](https://openairdocs.org/sdr/SWIA201335063), Oct 2, 2013: SKIN. CRACKED. RT WING SKIN CLEAT TOP MID OTBD OF FUEL STICK NR 4 CRACKED. C-CHECK REPLACED 1 UPPER SKIN CLEAT SUPPORT BRACKET PN 120-17063-009 ON RT WING OTBD OF NR 4 FUEL ST
- [SDR SWIA201335062](https://openairdocs.org/sdr/SWIA201335062), Oct 2, 2013: SKIN. CRACKED. RT WING SKIN CLEAT TOP MID OTBD OF FUEL PANEL NR 4 CRACKED. C-CHECK REPLACED 1 UPPER SKIN CLEAT PN120-17063-009 ON RT WING OTBD OF NR 4 FUEL PANEL IAW SRM.
- [SDR SWIA201335061](https://openairdocs.org/sdr/SWIA201335061), Oct 2, 2013: SKIN. CRACKED. RT WING SKIN CLEAT BOTTOM AFT INBD OF FUEL PANEL NR 4 CRACKED. C-CHECK REPLACED SKIN CLEAT ON RT WING INBD OF NR 4 FUEL PANEL BOTTOM IAW SRM.
- [SDR SWIA201335060](https://openairdocs.org/sdr/SWIA201335060), Oct 2, 2013: SKIN. CRACKED. RT WING SKIN CLEAT TOP 2ND AFT AT PANEL 2 CRACKED. C-CHECK REPLACED 1 UPPER SKIN CLEAT ON RT WING AFT OF NR 2 FUEL ACCESS PANEL IAW SRM.
- [SDR SWIA201335059](https://openairdocs.org/sdr/SWIA201335059), Oct 2, 2013: FLAP. CHAFED. RT NACELLE FLAP EXTERIOR SIDE CHAFED NEAR INBD HINGE. C-CHECK REPLACED RT NACELLE FLAP IAW SRM.
- [SDR SWIA201335058](https://openairdocs.org/sdr/SWIA201335058), Oct 2, 2013: FRAME. CHAFED. RT AFT EXHAUST COWL FRAME CHAFFED. C-CHECK REPAIRED IAW SRM.
- [SDR SWIA201335057](https://openairdocs.org/sdr/SWIA201335057), Oct 2, 2013: SKIN. CRACKED. LT WING FUEL PANEL L4 FROM OTBD NACELLE HAS FOUR CRACKED SKIN CLEATS ON UPPER INBD SIDE OF BAY. C-CHECK REPLACED SKIN CLEATS ON LT WING FUEL PANEL NR 4 UPPER IN
- [SDR SWIA201335056](https://openairdocs.org/sdr/SWIA201335056), Oct 2, 2013: SKIN. CRACKED. LT WING L3 FUEL PANEL HAS 2 OTBD UPPER & ONE INBD SKIN CLEAT CRACKED. C-CHECK REPLACED SKIN CLEATS ON LT WING AT NR 3 FUEL PANEL UPPER OTBD IAW SRM.
- [SDR SWIA201335055](https://openairdocs.org/sdr/SWIA201335055), Oct 2, 2013: SKIN. CRACKED. LT WING L2 FUEL PANEL HAS 2 OTBD UPPER SKIN CLEATS CRACKED, C-CHECK REPLACED SKIN CLEATS ON LT WING NR 2 FUEL PANEL UPPER OTBD IAW SRM.
- [SDR SWIA201335054](https://openairdocs.org/sdr/SWIA201335054), Oct 2, 2013: SUPPORT FRAME. CRACKED. RT HYDRAULIC PACK LOWER SUPPORT FRAME CRACKED. C-CHECK REPLACED RT HYDRAULIC PACK LOWER SUPPORT FRAME & SECURED IAW SRM.
- [SDR SWIA201335053](https://openairdocs.org/sdr/SWIA201335053), Oct 2, 2013: CHANNEL. CRACKED. RT NACELLE, INBD SIDE, CHANNEL CRACKED NEAR FWD ENGINE MOUNT. C-CHECK REPLACED ANGLE PN 120-35340-001 AT RT NACELLE, INBD SIDE, CHANNEL NEAR FWD ENGINE MOUNT IA
- [SDR SWIA201335052](https://openairdocs.org/sdr/SWIA201335052), Oct 2, 2013: CHANNEL. CRACKED. PAX DOOR CRACKED & MINOR CORROSION AT BAY 18. C-CHECK INSTALLED NEW CHANNEL PN 120-21059-001 AT PAX DOOR BAY 18 IAW SRM. CLEANED & REMOVED MINOR CORROSION ALSO 
- [SDR SWIA201335067](https://openairdocs.org/sdr/SWIA201335067), Oct 1, 2013: FRAME. CHAFED. CHAFED FRAME ON RT HYD BAY FWD SIDE. C-CHECK REPLACED RT HYD BAY FWD CUT OUT FRAME PN 120-44444-002 IAW SRM.
- [SDR SWIA201335066](https://openairdocs.org/sdr/SWIA201335066), Oct 1, 2013: BUTTSTRAP. CORRODED. CORROSION ON CENTER FLOOR BUTT STRAP BETWEEN FRAME 31 TO FRAME 37. C-CHECK REPLACED BUTT STRAP PN 120-46163-001 AT FUSELAGE CENTER FLOOR BETWEEN FRAME 31 TO FRA
- [SDR SWIA201335065](https://openairdocs.org/sdr/SWIA201335065), Oct 1, 2013: STRINGER. CORRODED. STRINGER 19L AT FRAME 13A HAS CORROSION. C-CHECK SPLICED NEW FRONT SECTION OF STRINGER 19L IAW SRM.
- [SDR SWIA201335070](https://openairdocs.org/sdr/SWIA201335070), Sep 27, 2013: SUPPORT BRACKET. CRACKED. RT WING, RIB 21, 3 UPPER FWD MOST SKIN CLEAT SUPPORT BRACKETS CRACKED. C-CHECK REPLACED 3 SKIN CLEAT SUPPORT BRACKETS PN120-17062-613 & 120-17063-609 ON RT WING
- [SDR SWIA201335069](https://openairdocs.org/sdr/SWIA201335069), Sep 27, 2013: SUPPORT BRACKET. CRACKED. RT WING RIB 20, 2ND FWD MOST, UPPER SKIN CLEAT SUPPORT BRACKET CRACKED. C-CHECK REPLACED 1 UPPER SKIN CLEATS SUPPORT BRACKET PN120-17063-009 AT RT WING RIB 20 I
- [SDR SWIA201335068](https://openairdocs.org/sdr/SWIA201335068), Sep 27, 2013: SUPPORT BRACKET. CRACKED. RT WING RIB 22, 2ND & 3RD FWD MOST, UPPER SKIN CLEAT SUPPORT BRACKETS CRACKED. C-CHECK REPLACED 2 UPPER SKIN CLEATS SUPPORT BRACKET PN120-17063-009 AT RT WING R
- [SDR SWIA201334085](https://openairdocs.org/sdr/SWIA201334085), Jul 21, 2013: SIGN. BROKEN. FLOOR LEVEL EXIT ROW SIGN SEAT 6C IS BROKEN. FLT#5362 RELAMPED.
- [SDR SWIA201333499](https://openairdocs.org/sdr/SWIA201333499), May 19, 2013: WIRE. DAMAGED. LEFT ENGINE HIGH OIL PRESSURE INDICATION ON THE GAUGE, NO MAP WARNING INDICATION. SHUTDOWN LT ENGINE, DECLARED AN EMERGENCY AND CONTINUED ON. UNDER THE FLOORBOA
- [SDR SWIA201332962](https://openairdocs.org/sdr/SWIA201332962), Mar 9, 2013: TERMINAL. DAMAGED. EMERGENCY EXIT LIGHT IN FORWARD CABIN DOES NOT ILLUMINATE. (FLT 5387) REPAIRED TERMINAL END ON EMERGENCY EXIT SIGN IN CABIN FORWARD OF SEAT 1 C/B.
- [SDR SWIA201232387](https://openairdocs.org/sdr/SWIA201232387), Dec 16, 2012: LIGHT. INOPERATIVE. EMERGENCY OVERHEAD LIGHT OVER MAIN CABIN DOOR BURNED OUT. (FLT 5458) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201232258](https://openairdocs.org/sdr/SWIA201232258), Nov 27, 2012: WIRE. DAMAGED. SECOND RED FLOOR TRACK LIGHT INOPERATIVE. (SERVICE) REPAIRED WIRE ON FLOOR EMERGENCY TRACK LIGHT.
- [SDR SWIA201232233](https://openairdocs.org/sdr/SWIA201232233), Nov 22, 2012: LIGHT. INOPERATIVE. EMERGENCY LIGHT ON FLOOR AT 2A BURNED OUT. (FLT 5321) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201232127](https://openairdocs.org/sdr/SWIA201232127), Nov 8, 2012: WIRE. LOOSE. LOOSE WIRES COMING OUT OF THE EMERGENCY FLOOR LIGHTS IN ROW 1. EMERGENCY LIGHTS ASSOCIATED WITH THE LOOSE WIRES ARE INOPERATIVE. (FLT 3453) RECONNECTED WIRES FO

All 119: https://openairdocs.org/aircraft/N229SW/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/N229SW/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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