# N1105G: 1988 Embraer EMB-120FC, registration cancelled 2022-12-24 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 24, 2022 - Status when cancelled: Valid registration - Airframe: [Embraer EMB-120FC](https://openairdocs.org/model/embraer-emb-120fc) (registry code 3260204) - 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), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs) - Serial number: 120.105 - Year built: 1988 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: July 13, 2004 - Certificate issued: February 24, 2022 - Last registry action: April 7, 2022 - Mode S code: A02F41 - Owner when cancelled: [Ameriflight LLC](https://openairdocs.org/faa-owner/AMERIFLIGHT%20LLC) - Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas) - Owner type: LLC - Owner's area on the map: 32.9032° N, 97.0531° W: Placed by OpenAirDocs at the center of ZIP code 75261, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N1105G - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=1105G - Page: https://openairdocs.org/deregistered/N1105G-2022-12-24 From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Embraer EMB-120FC: https://openairdocs.org/model/embraer-emb-120fc.md ## Service difficulty reports (38) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR FXGA201408221431](https://openairdocs.org/sdr/FXGA201408221431), Aug 20, 2014: SKIN. CRACKED. TO REPAIR A CRACK ON THE FUSELAGE SKIN AT FS 2389 AT CENTERLINE. CUT OUT DAMAGE & INSTALL REPAIR DOUBLER ISE RDT2014-120-06-15-20 & EMAIL TITLED EDT2014-120-061 - [SDR FXGA20120323002](https://openairdocs.org/sdr/FXGA20120323002), Mar 23, 2012: STRINGER. CORRODED. DURING HEAVY MX, FOUND LT PROFILE STRINGER CORRODED. STRINGER WAS REPLACED. - [SDR FXGA20120323001](https://openairdocs.org/sdr/FXGA20120323001), Mar 23, 2012: SKIN. CORRODED. DURING HEAVY MX, FOUND LOWER BELLY SKIN, CORRODED IN SEVERAL SPOTS. SKIN WAS REPLACED. - [SDR FXGA1105G](https://openairdocs.org/sdr/FXGA1105G), Jul 16, 2010: SKIN. DENTED. DENT ON ENTRY DOOR SKIN NEAR OPERATING LEVER WAS REPAIRED IAW SRM 52-10-01. - [SDR SWIA200211221](https://openairdocs.org/sdr/SWIA200211221), Sep 11, 2002: ACTUATOR. FAILED. INBOARD FLAPS CONTROL FAULT FROM 15 DEGREES TO 0 DEGREES WHEN RETRACTING THEM. REPAIRED ENVIRONMENTAL SPLICE AT LEFT I/B FLAP ACTUATOR CANNON PLUG. INSPECTED WI - [SDR SWIA200211202](https://openairdocs.org/sdr/SWIA200211202), Sep 5, 2002: WIRE HARNESS. FAULTY. ON DEPARTURE FROM SFO, LANDING GEAR WOULD NOT RETRACT. ALL GREEN REMAINED ILLUMINATED & ALL REDS EXCEPT RIGHT A WERE ILLUMINATED W/GEAR HANDLE IN UP POSITION. C - [SDR SWIA200211005](https://openairdocs.org/sdr/SWIA200211005), Jul 2, 2002: INDICATOR. BURNED OUT. FIRST OFFICER'S EHSI SCREEN BURNED OUT. REPLACED FIRST OFFICER'S EHSI SCREEN. OPS CHECK GOOD. - [SDR SWIA200210834](https://openairdocs.org/sdr/SWIA200210834), Apr 28, 2002: SENSOR. MALFUNCTIONED. TAKEOFF TRIM AURAL WARNING SOUNDED ON TAKEOFF ROLL. ABORTED TAKEOFF. TRIM WAS SET IN THE GREEN BAND. REPLACED RIGHT ELEVATOR TRIM SENSOR. OPS CHECK OF TRIM AURA - [SDR SWIA200110339](https://openairdocs.org/sdr/SWIA200110339), Nov 4, 2001: ACTUATOR. FAILED. NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED NOSE GEAR RETRACTION ACTUATOR. SWUNG GEAR CHECK GOOD. LEAK CHECK GOOD. - [SDR SWIA200110178](https://openairdocs.org/sdr/SWIA200110178), Sep 19, 2001: CONTROL UNIT. MALFUNCTIONED. TAXI OUT RECEIVED FLAP CONTROL FAULT ANNUNCIATION ON OUTBOARD PAIR, ONE ROW OF LIGHTS. RETURNED TO GATE.REPLACED FLAP CONTROL UNIT. OPS CHECK GOOD.S/N ON: 0016 - [SDR SWIA200110099](https://openairdocs.org/sdr/SWIA200110099), Aug 16, 2001: CIRCUIT BREAKER. TRIPPED. ON APPROACH TO PDX, EMERGENCY DC BUS 2 FAILED WHEN FLAPS WERE SELECTED 15 DEGREES.REMOVED AND REPLACED EMERGENCY DC BUS 2 CIRCUIT BREAKER IAW WM 20-00-07. NO DE - [SDR SWIA200110098](https://openairdocs.org/sdr/SWIA200110098), Aug 16, 2001: BUSS. FAILED. ON APPROACH TO SEA THE ''EMERGENCY BUS OFF" LIGHT ON OVERHEAD PANEL LIGHT CAME ON, AND ON THE MAP PANEL THE AMBER APU, ELECTRIC, POWER OFF, DEICE AND BRAKES LIG - [SDR SWIA972660](https://openairdocs.org/sdr/SWIA972660), Jun 1, 2001: HARNESS. DAMAGED. FOUND BADLY DAMAGED WIRES IN LEFT WING TANK NEAR LAST UNDERWING PANEL. REMOVED WIRE HARNESS AND INSTALLED SERVICEABLE ASSEMBLY IAW EMB 120 MM 20-20-00. PN ON 50 - [SDR SWIA972522](https://openairdocs.org/sdr/SWIA972522), Apr 20, 2001: CONNECTOR. CONTAMINATED. POWER LEVER SPLIT OF 2 INCHES ON T/O, ABORTED. TRIED STATIC EVERYTHING WORKED. TOOK OFF, LEFT EEC FAILED. DEFERRED PER MEL 73-21-1. CLEANED OIL FROM LEFT SIGNAL - [SDR SWIA972252](https://openairdocs.org/sdr/SWIA972252), Jan 2, 2001: CONNECTOR. CONTAMINATED. FLAP ASSYMETRY INDICATION OUTBOARD SECTION ON APPROACH. AIRCRAFT REMAINED CONTROLLABLE, LANDED UNEVENTFULLY. FOUND ANTI-ICING FLUID IN RIGHT OUTBOARD FLAP ELECT - [SDR SWIA972215](https://openairdocs.org/sdr/SWIA972215), Dec 16, 2000: WARNING HORN. ACTIVATED. ON TAKE OFF ROLL WE RECIEVED AN AUTO FEATHER WARNING. ABORTED AND RETURNED TO GATE. MAINTENANCE COULD NOT DUPLICATE PROBLEM, SYSTEM CHECK GOOD. - [SDR SWIA972114](https://openairdocs.org/sdr/SWIA972114), Nov 17, 2000: FUSE. FAILED. PART OF FLOOR LEVEL EMERGENCY LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED BAD FUSE. OPS CHECK GOOD 33-00-00. - [SDR SWIA972071](https://openairdocs.org/sdr/SWIA972071), Oct 27, 2000: COMPUTER. FAILED. OUTBOARD FLAPS STUCK IN FLAPS 25 POSITION WITH ALL OTHER FLAPS IN THE UP POSITION. REPLACED FLAP COMPUTER IAW EMB120 MM 27-50-06. ALSO, REPLACED ANNUNCIATOR PAN - [SDR SWIA971982](https://openairdocs.org/sdr/SWIA971982), Sep 13, 2000: AILERON. FOD. ON APPROACH AILERONS WERE BINDING WHEN DEFLECTED RIGHT OR LEFT. FOUND SCREW TRAPPED BETWEEN INNER AILERON AND WING SURFACE, INNER ROOT OF LEFT AILERON. REMOVED - [SDR SWIA971694](https://openairdocs.org/sdr/SWIA971694), Feb 15, 2000: SWITCH. FAILED. I/B LEFT STABILIZER DEICE LIGHT ILLUMINATED IN FLIGHT, LIGHT CAME ON TIMERS 1 AND 2 AND REMAINED ON WITH SWTICH OFF. RETURNED TO PDX. REPLACED I/B LEFT STABILIZ - [SDR SWIA971675](https://openairdocs.org/sdr/SWIA971675), Jan 30, 2000: LINE. COLLAPSED. LEFT ENGINE INLET FAILED IN FLIGHT. RETURNED TO PDX. FOUND LEFT ENGINE INLET FLEX LINE COLLAPSED. INSTALLED NEW SERVICEABLE FLEX LINE IAW MM 30-00-00, OPS CHECK - [SDR SWIA971440](https://openairdocs.org/sdr/SWIA971440), Mar 4, 1999: NP INDICATION. OSCILLATION. AFTER DEPARTURE AND ON CLIMBOUT NP OSCILLATES BETWEEN 99.2 PERCENT AND 1001 PERCENT. WHEN 85 PERCENT NP WAS SET, OSCILLATIONS WERE +.4 PERCENT. RIGHT ENGINE NP - [SDR SWIA971338](https://openairdocs.org/sdr/SWIA971338), Dec 10, 1998: TRACKS. LACK OF LUBE. LEFT OUTBOARD FLAP DISAGREEMENT WOULD NOT RETRACT. RETURNED TO SEA. RESET FLAP CONTROL PANEL AND CLEANED AND LUBED FLAP TRACKS, OPS CHECKS GOOD. - [SDR SWIA971266](https://openairdocs.org/sdr/SWIA971266), Sep 2, 1998: ACTUATOR. FAILED. ON FLAP RETRACTION AFTER DEPARTURE INBOARD FLAPS DID NOT RETRACT AND ASYMMETRY LIGHT ON FLAP PANEL ILLUMINATED. RETURNED TO PDX. REMOVED AND REPLACED RIGHT INBO - [SDR COMA9710320](https://openairdocs.org/sdr/COMA9710320), Jun 28, 1997: SIGN. BROKEN. EMERGENCY LIGHT AT RT OVERWING EXIT IS BROKEN. REPLACED LIGHT ASSY. - [SDR COMA9710191](https://openairdocs.org/sdr/COMA9710191), Mar 30, 1997: ACTUATOR. MALFUNCTION. FLAP CONTROL FAULT WARNING DURING TAKEOFF. REPLACED THE LEFT HAND OUTBOARD FLAP ACTUATOR. - [SDR COMA9710156](https://openairdocs.org/sdr/COMA9710156), Feb 22, 1997: ACTUATOR. MALFUNCTION. FLAP CONTROL FAULT WARNING AFTER TAKE OFF. REPLACED THE LEFT NACELLE FLAP ACTUATOR. - [SDR COMA9710034](https://openairdocs.org/sdr/COMA9710034), Jan 15, 1997: DEICE LEAD. FAILED. LEFT PROPELLER DE-ICE FAILS AFTER 90 SECONDS ON BOTH TIMERS AND NORMAL OR COLD. REPLACED LEFT PROPELLER NR 1 BLADE DEICE LEADS. - [SDR COMA9610323](https://openairdocs.org/sdr/COMA9610323), Nov 5, 1996: AUTO FEATHER. FAILED TEST. LEFT AUTOFEATHER FAILED TO TEST. TROUBLESHOT PROBLEM,COULD NOT DUPLICATE. - [SDR COMA9610307](https://openairdocs.org/sdr/COMA9610307), Oct 15, 1996: FLAP. CHAFING. NACELLE FLAP DISAGREEMENT WARNING WHEN FLAPS LOWERED. FOUND RT NACELLE FLAP CHAFING AT THE OUTBD HINGE. REPLACED FLAP. - [SDR COMA9610251](https://openairdocs.org/sdr/COMA9610251), Aug 23, 1996: OIL BYPASS LINE. FAILED. RT ENGINE LOST OIL PRESSURE DURING FLIGHT. ENGINE SECURED AND ACFT DIVERT TO DAY. REPLACED LEAKING OIL COOLER BYPASS LINE. - [SDR COMA9610165](https://openairdocs.org/sdr/COMA9610165), Jun 3, 1996: SPINNER. LOOSE RIVETS. LEFT PROPELLER SPINNER HAS LOOSE RIVETS. REPLACED SPINNER. - [SDR COMA9511196](https://openairdocs.org/sdr/COMA9511196), Nov 6, 1995: ACTUATOR. DEFECTIVE. FLAP CONTROL FAULT WARNING. REPLACED THE LEFT INBOARD FLAP ACTUATOR. - [SDR COMA9511973](https://openairdocs.org/sdr/COMA9511973), Sep 25, 1995: COMPRESSOR. FOD DAMAGE. DURING PREFLIGHT INSPECTION, FOUND COMPRESSOR BLADE DAMAGE ON RT ENGINE. REPLACED ENGINE. - [SDR COM11909](https://openairdocs.org/sdr/COM11909), May 23, 1995: END RIB. CHAFED. ROUTINE INSPECTION, FOUND A SMALL HOLE CHAFED THROUGH THE INBOARD END CLOSING RIB OF THE RIGHT NACELLE FLAP. A SHEET METAL DOUBLER REPAIR WAS FABRICATED AND INS - [SDR COM11872](https://openairdocs.org/sdr/COM11872), Apr 20, 1995: HOSE ASSY. LEAKING. GREEN SYSTEM HYDRAULIC FLUID QUANTITY FELL TO ZERO DURING FLIGHT. REPLACED LEAKING DOOR ACTUATOR LINE ON LT MLG. - [SDR COM11864](https://openairdocs.org/sdr/COM11864), Apr 17, 1995: SUPPORT. CRACKED. THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-551/651-01I AND 5720-552/652-01I. THE SKIN SUPPORTS WERE REPAIRED IAW AERODE - [SDR COM11729](https://openairdocs.org/sdr/COM11729), Jan 14, 1995: PCU. DEFECTIVE. RT ENGINE NP FLUCTUATED BETWEEN 97 AND 102 PERCENT. ALL OTHER ENGINE PARAMETERS WERE NORMAL. REPLACED THE RT PROPELLER PITCH CONTROL UNIT. ## FAA accident and incident reports (5) 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 19990227012599I](https://openairdocs.org/incident/19990227012599I), Feb 27, 1999: Emb EMB120 (N1105G), Seattle, WA, Minor damage. Skywest 6852, N1105G, EMB120, arrived at ksea, 3 crew/29 pax @ 1215L. Aircraft was stopped, parking brake set and shutdown being accomplished, seat belt sign… - [Incident 19930807033459I](https://openairdocs.org/incident/19930807033459I), Aug 7, 1993: Emb EMB120RT (N1105G), Orlando, FL, Minor damage. Left engine began to autofeather. Shut engine down. Fire in tail pipe. Returned. Turbine oil pressure line failed. - [Incident 19910626052209I](https://openairdocs.org/incident/19910626052209I), Jun 26, 1991: Emb EMB120RT (N1105G), Ft Lauderdale, FL. Instructor retracted throttle abruptly. Prop went to feather. Engine continued to run. Landed safely. - [Incident 19890724041489I](https://openairdocs.org/incident/19890724041489I), Jul 24, 1989: Emb EMB120RT (N1105G), Key West, FL, Minor damage. Flap position indicator showed inboard flaps stuck down. Found access door was missing. - [Incident 19890308013669I](https://openairdocs.org/incident/19890308013669I), Mar 8, 1989: Emb EMB120RT (N1105G), Orlando, FL, Minor damage. Brake light on takeoff. Right wheel half and tire departed aircraft. Returned found wheel bolts had sheared. ## Other aircraft with N1105G - [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N1105G-undated): Hughes 269C, S/N 211029 --- 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.