# Embraer EMB-120 - Type: Aircraft model (FAA registry) - Registry code: 3260201 - Manufacturer (registry): EMBRAER - Model: EMB-120 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-prop - Seats: 32 - Weight class: 12,500 to 19,999 lb - Certification: Type certificated - Data sheet: [TCDS A31SO](https://openairdocs.org/tcds/A31SO) (OpenAirDocs) - Holder: Embraer S.A. - Registered aircraft: 3 - Page: https://openairdocs.org/model/embraer-emb-120 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [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 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 All 68: https://openairdocs.org/model/embraer-emb-120/ads.md ## Information bulletins (advisory) (3) - [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 ## Registered aircraft (3) - [N564SW](https://openairdocs.org/aircraft/N564SW): [Freight Runners Express Inc](https://openairdocs.org/faa-owner/FREIGHT%20RUNNERS%20EXPRESS%20INC), [Milwaukee, WI](https://openairdocs.org/faa-place/WI/Milwaukee), built 1998, S/N 120339 - [N653CT](https://openairdocs.org/aircraft/N653CT): [Ameriflight LLC](https://openairdocs.org/faa-owner/AMERIFLIGHT%20LLC), [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas), built 1991, S/N 120.243 - [N859BE](https://openairdocs.org/aircraft/N859BE): [Blue Eagle Airways Inc](https://openairdocs.org/faa-owner/BLUE%20EAGLE%20AIRWAYS%20INC), [San Juan, PR](https://openairdocs.org/faa-place/PR/San%20Juan), built 1983, S/N 120147 ## NTSB investigations (2) 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 LAX97FA189](https://openairdocs.org/ntsb/LAX97FA189), May 21, 1997: Embraer EMB-120 (N198SW), San Diego, CA, substantial damage. Probable cause: The failure of maintenance personnel to allow adequate time for the engine oil to drain back into the engine oil reservoir prior to adding additional oil, thereby overfilling the reservoir, which… - [NTSB DCA95MA054](https://openairdocs.org/ntsb/DCA95MA054), Aug 21, 1995: Embraer EMB-120RT (N256AS), Carrollton, GA, destroyed, 8 fatal. Probable cause: the in-flight fatigue fracture and separation of a propeller blade resulting in distortion of the left engine nacelle, causing excessive drag, loss of wing lift, and reduced directional control of… ## FAA accident and incident reports (19) 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 20120817017649I](https://openairdocs.org/incident/20120817017649I), Aug 17, 2012: Embraer EMB-120 (N653CT), Cedar City, UT, Minor damage. Aircraft made a left turn approximately at 80 knots on take-off roll. Flight crew responded by inputting full right rudder and positioning power levers in… - [Incident 20040921023059I](https://openairdocs.org/incident/20040921023059I), Sep 21, 2004: Emb EMB120 (N189SW), Salt Lake City, UT, Minor damage. (-23) Bird strike on departure from slc. Aircraft continued to cody, WY. On-call mx found dent in fuselage right side aft of radome. Aircraft ferried back to… - [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… - [Incident 20000725020549I](https://openairdocs.org/incident/20000725020549I), Jul 25, 2000: Emb EMB120 (N216SW), Reno, NV. (-23) (Potential flight control problem)on 07/25/2000, Reno, NV, 1919 skw 3651 declared an emergency while on a 10 mile final for runway 16R. The pilot… - [Incident 19981230043479I](https://openairdocs.org/incident/19981230043479I), Dec 30, 1998: Emb EMB120 (N563SW), Ontario, CA, Minor damage. (-5) The abovementioned aircraft diverted to Ontario International Airport, due to co-pilots windshield shattering at approximately 23,000 feet AGL. The… - [Incident 19980911036429I](https://openairdocs.org/incident/19980911036429I), Sep 11, 1998: Emb EMB120ER (N195SW), Billings, MT. (-5) During takeoff the right torque gauge fluctuated between 24 and 80 percent torque. Flight crew aborted takeoff and taxied aircraft back to the gate.… - [Accident 19970521013909A](https://openairdocs.org/incident/19970521013909A), May 21, 1997: Emb EMB120 (N198SW), San Diego, CA, Substantial damage. (.19) See .19 for complete narrative - [Accident 19950821024859A](https://openairdocs.org/incident/19950821024859A), Aug 21, 1995: Emb EMB120 (N256AS), Carrollton, GA, Destroyed, 8 fatal. Declared an emergency due to engine failure. Unable to make airport, crashed in a field. (.4)atlantic southeast airline flight 529 was climbing through… - [Incident 19940807034159I](https://openairdocs.org/incident/19940807034159I), Aug 7, 1994: Emb EMB120 (N195SW), San Diego, CA, Minor damage. Loaded aft of center of gravity. Tail settled to ramp. - [Incident 19931105048059I](https://openairdocs.org/incident/19931105048059I), Nov 5, 1993: Emb EMB120 (N198SW), Salt Lake City, UT, Minor damage. Section on NR2 engine cowling departed on climb. Returned.found cowling not properly secured by ground maintnance. - [Incident 19920925044899I](https://openairdocs.org/incident/19920925044899I), Sep 25, 1992: Emb EMB120 (N190SW), Billings, MT. Left main gear doors failed to close after departure. Returned. Landed safely. - [Incident 19911204060469I](https://openairdocs.org/incident/19911204060469I), Dec 4, 1991: Emb EMB120 (N195SW), Salt Lake City, UT. Lost all pressurization on climb. Emergency descent. Returned. Found incorrect cargo door stops installed. - [Incident 19910509020689I](https://openairdocs.org/incident/19910509020689I), May 9, 1991: Emb EMB120 (N188SW), Palm Springs, CA. Encountered severe turbulence during climb. Returned. One crew and two passengers slightly injured. - [Incident 19900417025129I](https://openairdocs.org/incident/19900417025129I), Apr 17, 1990: Emb EMB120 (N189SW), Billings, MT. Auto feather aural warning activated on takeoff. Aborted. Returned and deplaned. Problem could not be duplicated. - [Incident 19890207016589I](https://openairdocs.org/incident/19890207016589I), Feb 7, 1989: Emb EMB120 (N188SW), Billings, MT. Unable to raise gear on takeoff. Returned. Unable to duplicate problem. Beleive frost on downlocks prevented unlock - [Incident 19881114068589I](https://openairdocs.org/incident/19881114068589I), Nov 14, 1988: Emb EMB120 (N187SW), Great Falls, MT. Unsafe gear door light indication after takeoff. Returned. Frozen slush cleaned off door proximity switch. - [Incident 19881027058999I](https://openairdocs.org/incident/19881027058999I), Oct 27, 1988: Emb EMB120 (N189SW), Great Falls, MT. Gear door light remained on after takeoff. Returned. Happened two times. Cleaned proximity switches. - [Incident 19881015064079I](https://openairdocs.org/incident/19881015064079I), Oct 15, 1988: Emb EMB120 (N187SW), Billings, MT. Shut down one engine en route. Notified ATC and landed without incident. NR2 engine oil pump had failed. ## Service difficulty reports (605, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2025F00223](https://openairdocs.org/sdr/2025F00223), Jun 12, 2025: ENGINE. FIRE. ON JUNE 12TH, 2025, PHOENIX AIR GROUP, INC. (PAG) WAS TRANSPORTING PASSENGERS FROM POINT MUGU NAVAL AIR STATION (KNTD) TO SAN NICOLAS ISLAND NAVAL OUTLYING FIEL - [SDR EY2R2024071200001](https://openairdocs.org/sdr/EY2R2024071200001), Jul 12, 2024: HUB. CRACKED. A SMALL CRACK WAS FOUND AT ONE OF THE TWO DOWEL PIN LOCATIONS ON THE PROPELLER HUB MOUNTING FLANGE. THE CRACK APPEARS TO HAVE ORIGINATED AT A LARGE PIT ON THE M - [SDR JIKA2022060801](https://openairdocs.org/sdr/JIKA2022060801), Jun 8, 2022: WARNING LIGHT. ACTIVATED. AIRCRAFT DIVERTED INTO KPSC DUE TO SMOKE WARNING ANNUNCIATOR ILLUMINATION. THE AIRCRAFT LANDED WITHOUT INCIDENT. NO SMOKE WAS NOTED VISUALLY UPON LANDING. MX RA - [SDR JIKA2022050601](https://openairdocs.org/sdr/JIKA2022050601), May 6, 2022: SENSOR. DEFECTIVE. FOUND A DEFECTIVE PROX SENSOR. REMOVED AND REPLACED SENSOR. ISSUE REMAINED. REMOVED AND REPLACED WARNING COMPUTER WITH NO CHANGE NOTED. FOUND SIGNAL WIRE SHORTI - [SDR JIKA2021062901](https://openairdocs.org/sdr/JIKA2021062901), Jun 29, 2021: HMU. FAILED. WHILE CRUISING AT 10,000 FEET, WITHOUT WARNING THE NUMBER 2 ENGINE FAILED. FIRST OFFICER CALLED OUT "POWER LOSS" ON NUMBER 2, MEMORY ITEMS AND QRH WERE COMPLETE - [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 2016FA0000463](https://openairdocs.org/sdr/2016FA0000463), Sep 28, 2016: DUCT. TORN. APPROX 1245 LOCAL TIME, WHEN RT "DUCT LEAK" LIGHT ILLUMINATED. CREW SECURED THE RT ENGINE BLEED VALVE AND RT AC PACK, WAITED THREE MINUTES FOR COOL DOWN AND ANN - [SDR SWIA2015F00020](https://openairdocs.org/sdr/SWIA2015F00020), Jan 5, 2015: BLADE. CRACKED. DURING MAJOR INSPECTION, FOUND FPI CRACK INDICATION IN FILLET RADIUS OF BLADE SHANK. - [SDR SWIA201436333](https://openairdocs.org/sdr/SWIA201436333), Feb 12, 2014: ROD END. DIRTY. MAIN CABIN DOOR DIFFICULT TO OPEN. FLT 5348 CLEANED & LUBED MAIN CABIN DOOR LOWER ROD ENDS. - [SDR SWIA201436328](https://openairdocs.org/sdr/SWIA201436328), Feb 8, 2014: CONTROLLER. FAILED. AIRCRAFT WOULD NOT PRESSURIZE. FLT 1371 REPLACED THE ELECTRONIC CONTROLLER FOR TROUBLESHOOTING PURPOSES, PN: 22201T011400, SN ON: 359 & SN OFF: 438. - [SDR SWIA201436332](https://openairdocs.org/sdr/SWIA201436332), Feb 4, 2014: LIGHT. INOPERATIVE. SQUARE EMERGENCY LIGHT ABOVE ROW 3 IS BURNED OUT. FLT 5291RELAMPED. - [SDR SWIA201436329](https://openairdocs.org/sdr/SWIA201436329), Feb 3, 2014: CONTROLLER. FAILED. RECEIVED CABIN ALT LIGHT. FLT 6452 REPLACED ELECTRONIC CONTROLLER. PN 22201T011400, SN ON 107 & SN OFF 520. - [SDR SWIA201335781](https://openairdocs.org/sdr/SWIA201335781), Dec 30, 2013: WIRE. UNSECURE. STRONG ELECTRICAL SMOKE SMELL THAT GOT PROGRESSIVELY WORSE. FLT 5459 RESECURED RT SIDE NR 2 BUS TIE CONTACTOR WIRE LOOP AT ATTACHING STUDS. RESECURED BOTH ENDS - [SDR SWIA201335732](https://openairdocs.org/sdr/SWIA201335732), Dec 23, 2013: PROXIMITY SENSOR. FAILED. LG WOULD NOT COME UP UNTIL DOWN LOCK RELEASE SWITCH WAS PRESSED. THE GEAR EXTENDED NORMALLY FOR LANDING. FLT 5335 REPLACED THE NLG PROXIMITY SENSOR & PERFORMED - [SDR SWIA201335771](https://openairdocs.org/sdr/SWIA201335771), Dec 20, 2013: WARNING SYSTEM. FALSE INDICATION. RECEIVED IDLE 1 UNLOCK & IDLE 2 UNLOCK CAUTIONS. FLT 5353 CHECKED WIRING FROM LT & RT WEIGHT ON WHEELS SWITCHES & BOTH FLIGHT IDLE STOP SOLENOIDS & THE MICRO SW - [SDR SWIA201335716](https://openairdocs.org/sdr/SWIA201335716), Dec 19, 2013: FCU. FAILED. RECEIVED CONTROL FAULT WHEN SELECTING FLAPS 25. RAN QRH PROCEDURE, LANDED FLAPS 15. FLT 6359 REPLACED FCU IAW AMM PN 347200-1001, SN ON 0253 & SN OFF 0140. - [SDR SWIA201335733](https://openairdocs.org/sdr/SWIA201335733), Dec 16, 2013: LIGHT. INOPERATIVE. WHITE FLOOR EMERGENCY LIGHTS ARE BURNED OUT AT ROW 6. FLT5650 RELAMPED. - [SDR SWIA201335715](https://openairdocs.org/sdr/SWIA201335715), Dec 16, 2013: LIGHT. INOPERATIVE. EMERGENCY LIGHT ABOVE ROW 3 IS BURNED OUT. FLT 5291 RELAMPED. - [SDR SWIA201335723](https://openairdocs.org/sdr/SWIA201335723), Dec 15, 2013: SWITCH. STUCK. MAIN CABIN DOOR DID NOT OPEN NORMALLY, USE OF THE FWD DOOR EMERGENCY VLV WAS REQUIRED TO OPEN DOOR. FLT 5474 FOUND SWITCH FOR MAIN CABIN DOOR STUCK IN. FREED OU - [SDR SWIA201335782](https://openairdocs.org/sdr/SWIA201335782), Dec 13, 2013: SUPPORT FITTING. CORRODED. ONE FUSELAGE SKIN SUPPORT CLIP AT FRAME 18A & BETWEEN STRINGERS 20R & 21R IS WORN, CORRODED BEYOND LIMITS. C-CHECK REPLACED SKIN SUPPORT CLIP AT FRAME 18A & BET - [SDR SWIA201335765](https://openairdocs.org/sdr/SWIA201335765), Dec 12, 2013: LIGHT. INOPERATIVE. FLOOR EMERGENCY LIGHT AT 9A IS BURNED OUT. FLT 6359 RELAMPED. - [SDR SWIA201335641](https://openairdocs.org/sdr/SWIA201335641), Dec 12, 2013: LIGHT. INOPERATIVE. WHITE FLOOR EMERGENCY LIGHT AT ROW 8A IS BURNED OUT. FLT 5376 RELAMPED. - [SDR SWIA201335784](https://openairdocs.org/sdr/SWIA201335784), Dec 11, 2013: FLOOR SUPPORT. CORRODED. CORROSION SPOTS ON FLOOR T SUPPORT TO THE LT BUTT STRAP AT FRAME. C-CHECK REPLACED SHORT FLOOR T SUPPORT TO THE LT BUTT STRAP AT FRAME 15 & INSTALLED FASTENERS - [SDR SWIA201335783](https://openairdocs.org/sdr/SWIA201335783), Dec 11, 2013: SKIN. CRACKED. RT NACELLE LOWER AFT OTBD CORNER SKIN IS CRACKED. C-CHECK STOP DRILLED CRACK & INSTALLED REPAIR DOUBLER IAW SRM. - [SDR SWIA201335678](https://openairdocs.org/sdr/SWIA201335678), Dec 11, 2013: SIGN. BROKEN. LOWER EMERGENCY EXIT SIGN IN ROW 9 IS BROKEN. FLT 5356 REPLACED LOWER EMERGENCY EXIT SIGN IN ROW 9. - [SDR SWIA201335578](https://openairdocs.org/sdr/SWIA201335578), Dec 11, 2013: GROUND STUD. LOOSE. EMERGENCY EXIT SIGN ROW 6A DOES NOT ILLUMINATE. FLT 5427 SECURED THE GROUND STUD FOR THE EMERGENCY EXIT SIGN AT ROW 6A. - [SDR SWIA201335653](https://openairdocs.org/sdr/SWIA201335653), Dec 10, 2013: LAMP. BURNED OUT. OVERHEAD EMERGENCY LIGHT AT ROW 9 IS BURNED OUT. REPLACED LAMP. - [SDR SWIA201335785](https://openairdocs.org/sdr/SWIA201335785), Dec 9, 2013: SUPPORT BRACKET. CRACKED. CTR BRACKET BEHIND CAPT`S DV WINDOW CUTOUT IS CRACKED AT FRAME 12. C-CHECK REPLACED CTR SUPPORT BRACKET AT FRAME 12 BEHIND CAPT`S DV WINDOW CUTOUT IAW SRM. - [SDR SWIA201335786](https://openairdocs.org/sdr/SWIA201335786), Dec 8, 2013: FLOOR SUPPORT. CORRODED. CORROSION SPOTS ON SHORT FLOOR T SUPPORT TO THE LEFT BUTT STRAP AT FRAME 16. C-CHECK REPLACED CABIN FLOOR T SUPPORT LT BUTT STRAP AT FRAME 16. - [SDR SWIA201335792](https://openairdocs.org/sdr/SWIA201335792), Dec 5, 2013: BRACKET. CRACKED. PILOTS SIDE AFT INBD FLOOR PROP CRACKED UNDER JUMP SEAT FLOOR. C-CHECK REPLACED PILOTS SIDE AFT INBD FLOOR PROP L BRACKET UNDER JUMP SEAT FLOOR. - [SDR SWIA201335791](https://openairdocs.org/sdr/SWIA201335791), Dec 5, 2013: BRACKET. CRACKED. COPILOTS SIDE AFT INBD FLOOR PROP CRACKED UNDER JUMP SEAT FLOOR. C-CHECK REPLACED COPILOTS SIDE AFT INBD FLOOR PROP L BRACKET UNDER COCKPIT STEP. - [SDR SWIA201335790](https://openairdocs.org/sdr/SWIA201335790), Dec 5, 2013: STRUCTURE. CRACKED. COPILOT AFT INBD FLOOR PROP CRACKED. C-CHECK REPAIRED COPILOTS INBD AFT FLOOR PROP IAW ETD. - [SDR SWIA201335665](https://openairdocs.org/sdr/SWIA201335665), Dec 5, 2013: PROXIMITY SENSOR. OUT OF ADJUST. ON TAKEOFF THE LT MLG WOULD NOT RETRACT. FLT 5449 ADJUSTED LT MLG UPLOCK PROX SENSOR. SWUNG GEAR SEVERAL TIMES. NO FURTHER DEFECTS NOTED. - [SDR SWIA201335536](https://openairdocs.org/sdr/SWIA201335536), Dec 5, 2013: LIGHT. INOPERATIVE. EMERGENCY LIGHT NEXT TO COURTESY LIGHT DOES NOT ILLUMINATE. FLT 7391 REPLACED THE EMERGENCY LAMP AT THE MAIN CABIN DOOR. OPERATIONS CHECKED GOOD PN 209. - [SDR SWIA201335502](https://openairdocs.org/sdr/SWIA201335502), Dec 5, 2013: LIGHT. INOPERATIVE. LAST FLOOR EMERGENCY WHITE LIGHT IS BURNED OUT. FLT 6264 RELAMPED. - [SDR SWIA201335797](https://openairdocs.org/sdr/SWIA201335797), Dec 4, 2013: PROBE. CHAFED. LT OTBD WING 2ND PROBE OTBD OF NACELLE CHAFING ON LOWER STRINGER. C-CHECK BLENDED OUT CHAFE MARK IN LT OTBD WING 2ND PROBE OTBD OF NACELLE ON LOWER STRINGER IAW - [SDR SWIA201335796](https://openairdocs.org/sdr/SWIA201335796), Dec 4, 2013: ANGLE. CRACKED. RT INBD WING RIB NR 5 FWD LOWER ANGLE CLIP CRACKED. C-CHECK REPLACED RT INBD WING RIB NR 5 FWD LOWER ANGLE CLIP IAW SRM. - [SDR SWIA201335795](https://openairdocs.org/sdr/SWIA201335795), Dec 4, 2013: ANGLE. CRACKED. RT INBD WING RIB NR 8 FWD OF PANEL, LOWER ANGLE CLIP CRACKED. C-CHECK REPLACED LOWER ANGLE CLIP ON RT INBD WING RIB NR 8 FWD OF PANEL IAW SRM. - [SDR SWIA201335793](https://openairdocs.org/sdr/SWIA201335793), Dec 4, 2013: SKIN. CORRODED. BETWEEN ROWS 2 & 3 OF THE BELLY, HAS QUITE A LOT OF SURFACE CORROSION ON RIBS & SKIN. C-CHECK REMOVED, BLENDED OUT & APPLIED CONVERSION COATING TO TRACES OF COR - [SDR SWIA201335571](https://openairdocs.org/sdr/SWIA201335571), Nov 30, 2013: CONNECTOR. LOOSE. RT MAIN GEAR WOULD NOT RETRACT. FLT 7390 TIGHTENED RT MLG DOWN LOCK UPPER PROX SENSOR CANNON PLUG & ADJUSTED UPLOCK PROX SENSOR. SWUNG GEAR MULTIPLE TIMES WITH - [SDR SWIA201335576](https://openairdocs.org/sdr/SWIA201335576), Nov 29, 2013: BATTERY PACK. DISCHARGED. ROW 6A EMERGENCY LIGHTS DO NOT ILLUMINATE. FLT 5504 REPLACED ELBP. PN D366-04-001 SN ON 176 SN OFF 489 - [SDR SWIA201335291](https://openairdocs.org/sdr/SWIA201335291), Nov 11, 2013: LIGHT. BROKEN. EMERGENCY EXIT LIGHT BROKEN, ROW 6 RT SIDE. FLT 5638 RELAMPED. - [SDR SWIA201335562](https://openairdocs.org/sdr/SWIA201335562), Nov 8, 2013: FITTING. CRACKED. CRACKED AT LT NACELLE INBD FITTING WHERE POWER CONDITION CONTROL CABLES GO THROUGH. C-CHECK REPLACED LT NACELLE INBD FITTING PN 120-22916-002 IAW SRM & AMM. - [SDR SWIA201335513](https://openairdocs.org/sdr/SWIA201335513), Nov 4, 2013: SUPPORT FITTING. CRACKED. MAIN CABIN DOOR ROTATING ARM ATTACH SUPPORT FITTING CRACKED. C-CHECK REPLACED MAIN CABIN DOOR CUT OUT LOWER FITTING FRAME PN 120-18804-001 IAW SRM. - [SDR SWIA201335525](https://openairdocs.org/sdr/SWIA201335525), Oct 30, 2013: CLEAT. CRACKED. RT WING NR 3 FUEL PANEL AFT OTBD SKIN CLEAT CRACKED. C-CHECK REPLACED LOWER SKIN CLEAT PN 120-61344-606 ON RT WING OTBD AFT OF NR 3 FUEL ACCESS PANEL IAW AMM & - [SDR SWIA201335524](https://openairdocs.org/sdr/SWIA201335524), Oct 30, 2013: CLEAT. CRACKED. RT WING NR 5 FUEL PANEL INBD FWD UPPER TWO SKIN CLEATS CRACKED. C-CHECK REPLACED TWO UPPER SKIN CLEATS PN 120-17062-613 & 120-17063-609 ON RT WING FWD INBD OF N - [SDR SWIA201335523](https://openairdocs.org/sdr/SWIA201335523), Oct 30, 2013: CLEAT. CRACKED. RT WING NR 6 FUEL PANEL INBD FWD UPPER SKIN CLEAT CRACKED. C-CHECK REPLACED UPPER SKIN CLEAT PN 120-17063-611 ON RT WING FWD INBD OF NR 6 FUEL ACCESS PANEL IAW - [SDR SWIA201335526](https://openairdocs.org/sdr/SWIA201335526), Oct 29, 2013: WEB. CHAFED. LT MLG BAY OTBD WEBBING CHAFED BEYOND LIMITS. C-CHECK REPLACED LT NACELLE OTBD GEAR WELL WEBBING IAW SRM. - [SDR SWIA201335137](https://openairdocs.org/sdr/SWIA201335137), Oct 29, 2013: HYDRAULIC SYSTEM. LOW. GEAR DISAGREE ON TAKEOFF, RT MAIN GEAR DID NOT SHOW UP & LOCKED UNTIL SECOND ATTEMPT. GREEN SYSTEM QUANTITY LIGHT ILLUMINATED. FLT5291 SERVICED GREEN SYSTEM & P - [SDR SWIA201335527](https://openairdocs.org/sdr/SWIA201335527), Oct 28, 2013: CLEAT. CRACKED. RT WING HAS FOUR LEAKING RIVETS BY THE NR 4 FUEL PANEL & LOWER SKIN CLEAT CRACKED AT RIB 18. C-CHECK REPLACED LOWER SKIN CLEAT PN 120-61345-615 ON RT WING AT RI All 605: https://openairdocs.org/model/embraer-emb-120/reports.md ## STCs that may be installed (OpenAirDocs) (69, first 50) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [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 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 SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc - [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc - [STC SA5845NM](https://openairdocs.org/stc/SA5845NM): Installationof cabin interior fluorescent lighting system. Bruce Aerospace 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 ST00075WI-D](https://openairdocs.org/stc/ST00075WI-D): Installation of provisions for the Bendix/King CAS 66A TCAS I system. Honeywell International Inc - [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 ST01805WI](https://openairdocs.org/stc/ST01805WI): Modification of Rockwell Collins TCAS II System Installation with DC powered TCAS Transmitter Receiver Processor. Rockwell Collins 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 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 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 SA5472NM](https://openairdocs.org/stc/SA5472NM): Installation of a Teledyne Controls Flight Data Acquisition Unit P/N 2231266-4. Teledyne Controls - [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 SH1053NE](https://openairdocs.org/stc/SH1053NE): Remove existing starter-generator and install Aircraft Parts starter generator P/N 400SG135Q. Skurka Aerospace Inc - [STC ST02540AT-D](https://openairdocs.org/stc/ST02540AT-D): Installation of replacement fuel tank sealant system. FFC Manufacturing - [STC ST151CH](https://openairdocs.org/stc/ST151CH): Installation of strobe upper anticollision light, P/N 30-1033-53. Honeywell International Inc - [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 ST01468CH](https://openairdocs.org/stc/ST01468CH): Installation of various SMR Technologies electrical propeller deicer models. SMR Technologies - [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 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 ST02490AT](https://openairdocs.org/stc/ST02490AT): Installation of MPC Products Corp. GA2201 RVDT. Chippewa Aerospace - [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 ST02174AT](https://openairdocs.org/stc/ST02174AT): Reduction in maximum zero fuel weight to 23,218 lbs. to reduce payload to FAR 135 limit of 7,500 lbs. For model EMB-120FC. North South Airways - [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 ST01898AT](https://openairdocs.org/stc/ST01898AT): Installation of an AlliedSignal Wulfsberg GNS-XLS flight management system with AFIS. Aviation Technologies Group All 69: https://openairdocs.org/model/embraer-emb-120/stcs.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.