# Service difficulty reports: N1105G, cancelled Dec 24, 2022

A list on [N1105G, cancelled Dec 24, 2022](https://openairdocs.org/deregistered/N1105G-2022-12-24.md).

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

- [SDR FXGA201408221431](https://openairdocs.org/sdr/FXGA201408221431.md): Skin · cracked · Aug 20, 2014 · N1105G · Emb EMB120FC · Fuselage Main, Plate/Skin
  > 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 EDT2014-120-061520. PERMANENT REPAIR INSPECTION REQUIRED. INTERNAL & EXTERNAL DETAILED INSPECTION REQUIRED AT EV
- [SDR FXGA20120323002](https://openairdocs.org/sdr/FXGA20120323002.md): Stringer · corroded · Mar 23, 2012 · N1105G · Emb EMB120FC · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MX, FOUND LT PROFILE STRINGER CORRODED. STRINGER WAS REPLACED.
- [SDR FXGA20120323001](https://openairdocs.org/sdr/FXGA20120323001.md): Skin · corroded · Mar 23, 2012 · N1105G · Emb EMB120FC · Fuselage Main, Plate/Skin
  > DURING HEAVY MX, FOUND LOWER BELLY SKIN, CORRODED IN SEVERAL SPOTS. SKIN WAS REPLACED.
- [SDR FXGA1105G](https://openairdocs.org/sdr/FXGA1105G.md): Skin · dented · Jul 16, 2010 · N1105G · Emb EMB120FC · Passenger/Crew Doors
  > DENT ON ENTRY DOOR SKIN NEAR OPERATING LEVER WAS REPAIRED IAW SRM 52-10-01.
- [SDR SWIA200211221](https://openairdocs.org/sdr/SWIA200211221.md): Actuator · failed · Sep 11, 2002 · N1105G · Emb EMB120RT · Trailing Edge Flap Actuator
  > 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 WIRING AT CANNON PLUGS AND FCU. FOUND LEFT INBOARD FLAP ACTUATOR BAD. REPLACED LEFT FLAP ACTUATOR
- [SDR SWIA200211202](https://openairdocs.org/sdr/SWIA200211202.md): Wire Harness · faulty · Sep 5, 2002 · N1105G · Emb EMB120RT · Landing Gear System Wiring
  > 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. CYCLED GEAR - SAME RESULTS. RETURNED TO SFO. PERFORMED GEAR SWING. OPS CHECKED GOOD BUT NOTICED
- [SDR SWIA200211005](https://openairdocs.org/sdr/SWIA200211005.md): Indicator · burned out · Jul 2, 2002 · N1105G · Emb EMB120RT · Integrated Flight System
  > FIRST OFFICER'S EHSI SCREEN BURNED OUT. REPLACED FIRST OFFICER'S EHSI SCREEN. OPS CHECK GOOD.
- [SDR SWIA200210834](https://openairdocs.org/sdr/SWIA200210834.md): Sensor · malfunctioned · Apr 28, 2002 · N1105G · Emb EMB120RT · Elevator Tab Control System
  > 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 AURAL WARNING SOUNDS OUTSIDE OF GREEN BAND GOOD.
- [SDR SWIA200110339](https://openairdocs.org/sdr/SWIA200110339.md): Actuator · failed · Nov 4, 2001 · N1105G · Emb EMB120RT · Landing Gear Actuator
  > 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.md): Control Unit · malfunctioned · Sep 19, 2001 · N1105G · Emb EMB120RT · Trailing Edge Flap Control System
  > 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 S/N OFF: 156
- [SDR SWIA200110099](https://openairdocs.org/sdr/SWIA200110099.md): Circuit Breaker · tripped · Aug 16, 2001 · N1105G · Emb EMB120RT · DC Power Distribution System
  > 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 DEFECTS NOTED.
- [SDR SWIA200110098](https://openairdocs.org/sdr/SWIA200110098.md): Buss · failed · Aug 16, 2001 · N1105G · Emb EMB120RT · DC Power Distribution System
  > 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 LIGHTS CAME ON. FOLLOWED QRH PROCEDURE TO AFM 3-8 PROCEDURE - EMERGENCY DC BUS FAILED.RESET EMERGENCY
- [SDR SWIA972660](https://openairdocs.org/sdr/SWIA972660.md): Harness · damaged · Jun 1, 2001 · N1105G · Emb EMB120RT · Engine Fuel Indicating System
  > 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 50040-000-01.
- [SDR SWIA972522](https://openairdocs.org/sdr/SWIA972522.md): Connector · contaminated · Apr 20, 2001 · N1105G · Emb EMB120RT · Fuel Control/Turbine Engines
  > 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 CONDITIONER CANNON PLUGS. REPAIRED AUXILIARY GENERATOR DRAIN LINE. OPS CHECKS GOOD. CONDUCTE
- [SDR SWIA972252](https://openairdocs.org/sdr/SWIA972252.md): Connector · contaminated · Jan 2, 2001 · N1105G · Emb EMB120RT · Trailing Flap Position Indicating System
  > FLAP 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.
- [SDR SWIA972215](https://openairdocs.org/sdr/SWIA972215.md): Warning Horn · activated · Dec 16, 2000 · N1105G · Emb EMB120RT · Propeller Feathering/Reversing
  > 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.md): Fuse · failed · Nov 17, 2000 · N1105G · Emb EMB120RT · Emergency Lighting
  > 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.md): Computer · failed · Oct 27, 2000 · N1105G · Emb EMB120RT · Trailing Edge Flap Control System
  > 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 PANEL IAW 27-50-04. OPS CHECK GOOD. P/N FLAP COMP: 307-500-101, S/N ON: 0156, P/N ANNUN PANEL: 3
- [SDR SWIA971982](https://openairdocs.org/sdr/SWIA971982.md): Aileron · fod · Sep 13, 2000 · N1105G · Emb EMB120RT · Aileron Control System
  > 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 SCREW, INSPECTED AFFECTED AREA, NO DAMAGE FOUND. FUNCTIONAL CHECK OF AILERON TRAVEL OK ON GROUND
- [SDR SWIA971694](https://openairdocs.org/sdr/SWIA971694.md): Switch · failed · Feb 15, 2000 · N1105G · Emb EMB120RT · Airfoil Anti/De-ice System
  > 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 STABILIZER PRESSURE SWITCH IAW MM 30, OPS CHECKS GOOD. (S/N N122) ON, (S/N L216) OFF.
- [SDR SWIA971675](https://openairdocs.org/sdr/SWIA971675.md): Line · collapsed · Jan 30, 2000 · N1105G · Emb EMB120RT · Air Intake Anti/De-Ice System
  > 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 CHECKS GOOD.
- [SDR SWIA971440](https://openairdocs.org/sdr/SWIA971440.md): Np Indication · oscillation · Mar 4, 1999 · N1105G · Emb EMB120RT · Propeller Indication System
  > 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 FLUCTUATIONS ARE STILL WITHIN ACCEPTABLE LIMITS AT THIS TIME PER EMBRAER OPERATIONAL BULLETIN
- [SDR SWIA971338](https://openairdocs.org/sdr/SWIA971338.md): Tracks · lack of lube · Dec 10, 1998 · N1105G · Emb EMB120RT · Trailing Edge Flaps
  > 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.md): Actuator · failed · Sep 2, 1998 · N1105G · Emb EMB120RT · Trailing Edge Flap Actuator
  > ON 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.
- [SDR COMA9710320](https://openairdocs.org/sdr/COMA9710320.md): Sign · broken · Jun 28, 1997 · N1105G · Emb EMB120RT · Emergency Lighting
  > EMERGENCY LIGHT AT RT OVERWING EXIT IS BROKEN. REPLACED LIGHT ASSY.
- [SDR COMA9710191](https://openairdocs.org/sdr/COMA9710191.md): Actuator · malfunction · Mar 30, 1997 · N1105G · Emb EMB120RT · Trailing Edge Flap Actuator
  > FLAP CONTROL FAULT WARNING DURING TAKEOFF. REPLACED THE LEFT HAND OUTBOARD FLAP ACTUATOR.
- [SDR COMA9710156](https://openairdocs.org/sdr/COMA9710156.md): Actuator · malfunction · Feb 22, 1997 · N1105G · Emb EMB120RT · Trailing Edge Flap Actuator
  > FLAP CONTROL FAULT WARNING AFTER TAKE OFF. REPLACED THE LEFT NACELLE FLAP ACTUATOR.
- [SDR COMA9710034](https://openairdocs.org/sdr/COMA9710034.md): Deice Lead · failed · Jan 15, 1997 · N1105G · Emb EMB120RT · Propeller/Rotor Anti-Ice/De-Ice System
  > 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.md): Auto Feather · failed test · Nov 5, 1996 · N1105G · Emb EMB120RT · Propeller Feathering/Reversing
  > LEFT AUTOFEATHER FAILED TO TEST. TROUBLESHOT PROBLEM,COULD NOT DUPLICATE.
- [SDR COMA9610307](https://openairdocs.org/sdr/COMA9610307.md): Flap · chafing · Oct 15, 1996 · N1105G · Emb EMB120RT · Leading Edge Devices
  > 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.md): Oil Bypass Line · failed · Aug 23, 1996 · N1105G · Emb EMB120RT · Engine Oil Distribution (Airframe Furnished)
  > 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.md): Spinner · loose rivets · Jun 3, 1996 · N1105G · Emb EMB120RT · Propeller Spinner Section
  > LEFT PROPELLER SPINNER HAS LOOSE RIVETS. REPLACED SPINNER.
- [SDR COMA9511196](https://openairdocs.org/sdr/COMA9511196.md): Actuator · defective · Nov 6, 1995 · N1105G · Emb EMB120RT · Trailing Edge Flap Actuator
  > FLAP CONTROL FAULT WARNING. REPLACED THE LEFT INBOARD FLAP ACTUATOR.
- [SDR COMA9511973](https://openairdocs.org/sdr/COMA9511973.md): Compressor · fod damage · Sep 25, 1995 · N1105G · Emb EMB120RT · Turbine Engine Compressor Section
  > DURING PREFLIGHT INSPECTION, FOUND COMPRESSOR BLADE DAMAGE ON RT ENGINE. REPLACED ENGINE.
- [SDR COM11909](https://openairdocs.org/sdr/COM11909.md): End Rib · chafed · May 23, 1995 · N1105G · Emb EMB120RT · Trailing Edge Flaps
  > 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 INSTALLED PER AERODESIGN REPORT NR 1538-1, REV IR, DATED 5-23-95.
- [SDR COM11872](https://openairdocs.org/sdr/COM11872.md): Hose Assy · leaking · Apr 20, 1995 · N1105G · Emb EMB120RT · Landing Gear Door Retract Section
  > 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.md): Support · cracked · Apr 17, 1995 · N1105G · Emb EMB120RT · Wing Miscellaneous Structure
  > 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 AERODESIGN REPORT 1327-2. P/N 120-17056-013, 2 EA, 120-17056-007, 2 EA, 120-17062-013, 1 EA, 120-17060-0
- [SDR COM11729](https://openairdocs.org/sdr/COM11729.md): Pcu · defective · Jan 14, 1995 · N1105G · Emb EMB120RT · Propeller Controlling System
  > RT ENGINE NP FLUCTUATED BETWEEN 97 AND 102 PERCENT. ALL OTHER ENGINE PARAMETERS WERE NORMAL. REPLACED THE RT PROPELLER PITCH CONTROL UNIT.

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N1105G-2022-12-24/reports

---
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