N1105G, cancelled Dec 24, 2022

Service difficulty reports · 38

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N1105G' AND deregistration_id = 'N1105G-2022-12-24'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FXGA201408221431Skin · crackedTO 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 EDT2014-120-061520. PERMANENT REPAIR INSPECTION REQUIRED. INTERNAL & EXTERNAL DETAILED INSPECTION REQUIRED AT EVAug 20, 2014 · N1105G · Emb EMB120FC · Fuselage Main, Plate/SkinSDR FXGA20120323002Stringer · corrodedDURING HEAVY MX, FOUND LT PROFILE STRINGER CORRODED. STRINGER WAS REPLACED.Mar 23, 2012 · N1105G · Emb EMB120FC · Fuselage Main, Longeron/StringerSDR FXGA20120323001Skin · corrodedDURING HEAVY MX, FOUND LOWER BELLY SKIN, CORRODED IN SEVERAL SPOTS. SKIN WAS REPLACED.Mar 23, 2012 · N1105G · Emb EMB120FC · Fuselage Main, Plate/SkinSDR FXGA1105GSkin · dentedDENT ON ENTRY DOOR SKIN NEAR OPERATING LEVER WAS REPAIRED IAW SRM 52-10-01.Jul 16, 2010 · N1105G · Emb EMB120FC · Passenger/Crew DoorsSDR SWIA200211221Actuator · failedINBOARD FLAPS CONTROL FAULT FROM 15 DEGREES TO 0 DEGREES WHEN RETRACTING THEM. REPAIRED ENVIRONMENTAL SPLICE AT LEFT I/B FLAP ACTUATOR CANNON PLUG. INSPECTED WIRING AT CANNON PLUGS AND FCU. FOUND LEFT INBOARD FLAP ACTUATOR BAD. REPLACED LEFT FLAP ACTUATOR Sep 11, 2002 · N1105G · Emb EMB120RT · Trailing Edge Flap ActuatorSDR SWIA200211202Wire Harness · faultyON 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. CYCLED GEAR - SAME RESULTS. RETURNED TO SFO. PERFORMED GEAR SWING. OPS CHECKED GOOD BUT NOTICED Sep 5, 2002 · N1105G · Emb EMB120RT · Landing Gear System WiringSDR SWIA200211005Indicator · burned outFIRST OFFICER'S EHSI SCREEN BURNED OUT. REPLACED FIRST OFFICER'S EHSI SCREEN. OPS CHECK GOOD.Jul 2, 2002 · N1105G · Emb EMB120RT · Integrated Flight SystemSDR SWIA200210834Sensor · malfunctionedTAKEOFF 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 AURAL WARNING SOUNDS OUTSIDE OF GREEN BAND GOOD.Apr 28, 2002 · N1105G · Emb EMB120RT · Elevator Tab Control SystemSDR SWIA200110339Actuator · failedNOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED NOSE GEAR RETRACTION ACTUATOR. SWUNG GEAR CHECK GOOD. LEAK CHECK GOOD.Nov 4, 2001 · N1105G · Emb EMB120RT · Landing Gear ActuatorSDR SWIA200110178Control Unit · malfunctionedTAXI 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 S/N OFF: 156Sep 19, 2001 · N1105G · Emb EMB120RT · Trailing Edge Flap Control SystemSDR SWIA200110099Circuit Breaker · trippedON 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 DEFECTS NOTED.Aug 16, 2001 · N1105G · Emb EMB120RT · DC Power Distribution SystemSDR SWIA200110098Buss · failedON 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 LIGHTS CAME ON. FOLLOWED QRH PROCEDURE TO AFM 3-8 PROCEDURE - EMERGENCY DC BUS FAILED.RESET EMERGENCY Aug 16, 2001 · N1105G · Emb EMB120RT · DC Power Distribution SystemSDR SWIA972660Harness · damagedFOUND 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 50040-000-01.Jun 1, 2001 · N1105G · Emb EMB120RT · Engine Fuel Indicating SystemSDR SWIA972522Connector · contaminatedPOWER 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 CONDITIONER CANNON PLUGS. REPAIRED AUXILIARY GENERATOR DRAIN LINE. OPS CHECKS GOOD. CONDUCTEApr 20, 2001 · N1105G · Emb EMB120RT · Fuel Control/Turbine EnginesSDR SWIA972252Connector · contaminatedFLAP ASSYMETRY INDICATION OUTBOARD SECTION ON APPROACH. AIRCRAFT REMAINED CONTROLLABLE, LANDED UNEVENTFULLY. FOUND ANTI-ICING FLUID IN RIGHT OUTBOARD FLAP ELECTRICAL CONNECTOR. CLEANED CONNECTOR. CYCLED FLAPS NUMEROUS TIMES. GROUND OPS CHECK GOOD.Jan 2, 2001 · N1105G · Emb EMB120RT · Trailing Flap Position Indicating SystemSDR SWIA972215Warning Horn · activatedON TAKE OFF ROLL WE RECIEVED AN AUTO FEATHER WARNING. ABORTED AND RETURNED TO GATE. MAINTENANCE COULD NOT DUPLICATE PROBLEM, SYSTEM CHECK GOOD.Dec 16, 2000 · N1105G · Emb EMB120RT · Propeller Feathering/ReversingSDR SWIA972114Fuse · failedPART OF FLOOR LEVEL EMERGENCY LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED BAD FUSE. OPS CHECK GOOD 33-00-00.Nov 17, 2000 · N1105G · Emb EMB120RT · Emergency LightingSDR SWIA972071Computer · failedOUTBOARD 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 PANEL IAW 27-50-04. OPS CHECK GOOD. P/N FLAP COMP: 307-500-101, S/N ON: 0156, P/N ANNUN PANEL: 3Oct 27, 2000 · N1105G · Emb EMB120RT · Trailing Edge Flap Control SystemSDR SWIA971982Aileron · fodON APPROACH AILERONS WERE BINDING WHEN DEFLECTED RIGHT OR LEFT. FOUND SCREW TRAPPED BETWEEN INNER AILERON AND WING SURFACE, INNER ROOT OF LEFT AILERON. REMOVED SCREW, INSPECTED AFFECTED AREA, NO DAMAGE FOUND. FUNCTIONAL CHECK OF AILERON TRAVEL OK ON GROUNDSep 13, 2000 · N1105G · Emb EMB120RT · Aileron Control SystemSDR SWIA971694Switch · failedI/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 STABILIZER PRESSURE SWITCH IAW MM 30, OPS CHECKS GOOD. (S/N N122) ON, (S/N L216) OFF.Feb 15, 2000 · N1105G · Emb EMB120RT · Airfoil Anti/De-ice SystemSDR SWIA971675Line · collapsedLEFT 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 CHECKS GOOD.Jan 30, 2000 · N1105G · Emb EMB120RT · Air Intake Anti/De-Ice SystemSDR SWIA971440Np Indication · oscillationAFTER 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 FLUCTUATIONS ARE STILL WITHIN ACCEPTABLE LIMITS AT THIS TIME PER EMBRAER OPERATIONAL BULLETIN Mar 4, 1999 · N1105G · Emb EMB120RT · Propeller Indication SystemSDR SWIA971338Tracks · lack of lubeLEFT OUTBOARD FLAP DISAGREEMENT WOULD NOT RETRACT. RETURNED TO SEA. RESET FLAP CONTROL PANEL AND CLEANED AND LUBED FLAP TRACKS, OPS CHECKS GOOD.Dec 10, 1998 · N1105G · Emb EMB120RT · Trailing Edge FlapsSDR SWIA971266Actuator · failedON FLAP RETRACTION AFTER DEPARTURE INBOARD FLAPS DID NOT RETRACT AND ASYMMETRY LIGHT ON FLAP PANEL ILLUMINATED. RETURNED TO PDX. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR IAW MM 27-50-7. OPS AND LEAKS CHECKS GOOD.Sep 2, 1998 · N1105G · Emb EMB120RT · Trailing Edge Flap ActuatorSDR COMA9710320Sign · brokenEMERGENCY LIGHT AT RT OVERWING EXIT IS BROKEN. REPLACED LIGHT ASSY.Jun 28, 1997 · N1105G · Emb EMB120RT · Emergency LightingSDR COMA9710191Actuator · malfunctionFLAP CONTROL FAULT WARNING DURING TAKEOFF. REPLACED THE LEFT HAND OUTBOARD FLAP ACTUATOR.Mar 30, 1997 · N1105G · Emb EMB120RT · Trailing Edge Flap ActuatorSDR COMA9710156Actuator · malfunctionFLAP CONTROL FAULT WARNING AFTER TAKE OFF. REPLACED THE LEFT NACELLE FLAP ACTUATOR.Feb 22, 1997 · N1105G · Emb EMB120RT · Trailing Edge Flap ActuatorSDR COMA9710034Deice Lead · failedLEFT PROPELLER DE-ICE FAILS AFTER 90 SECONDS ON BOTH TIMERS AND NORMAL OR COLD. REPLACED LEFT PROPELLER NR 1 BLADE DEICE LEADS.Jan 15, 1997 · N1105G · Emb EMB120RT · Propeller/Rotor Anti-Ice/De-Ice SystemSDR COMA9610323Auto Feather · failed testLEFT AUTOFEATHER FAILED TO TEST. TROUBLESHOT PROBLEM,COULD NOT DUPLICATE.Nov 5, 1996 · N1105G · Emb EMB120RT · Propeller Feathering/ReversingSDR COMA9610307Flap · chafingNACELLE FLAP DISAGREEMENT WARNING WHEN FLAPS LOWERED. FOUND RT NACELLE FLAP CHAFING AT THE OUTBD HINGE. REPLACED FLAP.Oct 15, 1996 · N1105G · Emb EMB120RT · Leading Edge DevicesSDR COMA9610251Oil Bypass Line · failedRT ENGINE LOST OIL PRESSURE DURING FLIGHT. ENGINE SECURED AND ACFT DIVERT TO DAY. REPLACED LEAKING OIL COOLER BYPASS LINE.Aug 23, 1996 · N1105G · Emb EMB120RT · Engine Oil Distribution (Airframe Furnished)SDR COMA9610165Spinner · loose rivetsLEFT PROPELLER SPINNER HAS LOOSE RIVETS. REPLACED SPINNER.Jun 3, 1996 · N1105G · Emb EMB120RT · Propeller Spinner SectionSDR COMA9511196Actuator · defectiveFLAP CONTROL FAULT WARNING. REPLACED THE LEFT INBOARD FLAP ACTUATOR.Nov 6, 1995 · N1105G · Emb EMB120RT · Trailing Edge Flap ActuatorSDR COMA9511973Compressor · fod damageDURING PREFLIGHT INSPECTION, FOUND COMPRESSOR BLADE DAMAGE ON RT ENGINE. REPLACED ENGINE.Sep 25, 1995 · N1105G · Emb EMB120RT · Turbine Engine Compressor SectionSDR COM11909End Rib · chafedROUTINE 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 INSTALLED PER AERODESIGN REPORT NR 1538-1, REV IR, DATED 5-23-95.May 23, 1995 · N1105G · Emb EMB120RT · Trailing Edge FlapsSDR COM11872Hose Assy · leakingGREEN SYSTEM HYDRAULIC FLUID QUANTITY FELL TO ZERO DURING FLIGHT. REPLACED LEAKING DOOR ACTUATOR LINE ON LT MLG.Apr 20, 1995 · N1105G · Emb EMB120RT · Landing Gear Door Retract SectionSDR COM11864Support · crackedTHE 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 AERODESIGN REPORT 1327-2. P/N 120-17056-013, 2 EA, 120-17056-007, 2 EA, 120-17062-013, 1 EA, 120-17060-0Apr 17, 1995 · N1105G · Emb EMB120RT · Wing Miscellaneous StructureSDR COM11729Pcu · defectiveRT ENGINE NP FLUCTUATED BETWEEN 97 AND 102 PERCENT. ALL OTHER ENGINE PARAMETERS WERE NORMAL. REPLACED THE RT PROPELLER PITCH CONTROL UNIT.Jan 14, 1995 · N1105G · Emb EMB120RT · Propeller Controlling System
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