# Service difficulty reports: N706RG, cancelled Sep 10, 2019 A list on [N706RG, cancelled Sep 10, 2019](https://openairdocs.org/deregistered/N706RG-2019-09-10.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR SIMA200800701](https://openairdocs.org/sdr/SIMA200800701.md): Line · disconnected · Jan 3, 2008 · N706RG · Emb EMB135LR · Landing Gear Brake System > ON FLIGHT 4611, DURING TAXI BRAKES SEIZED AND COULD NOT BE RELEASED. AIRCRAFT TOWED BACK TO GATE. AIRCRAFT REMOVED FROM SERVICE. FOUND NR 4 NORMAL BRAKE LINE DISCONNECTED AND DAMAGED. REMOVED AND REPLACE NUMBER 4 NORMAL BRAKE LINE IAW EMB 32-10-01. OPERAT - [SDR SIMA200722203](https://openairdocs.org/sdr/SIMA200722203.md): Computer · failed · Aug 8, 2007 · N706RG · Emb EMB135LR · Attitude and Direction Data System > ON TAKEOFF ROLL ENGINE POWER WITH TO TAKEOFF RESERVE FOLLOWED BY YAW DAMPER AND AHRS FAIL MESSAGES. REMOVED AND REPLACED NUMBER ONE AHRS COMPUTER IAW EMB AMM 31-21-01, OPERATIONAL CHECKED GOOD. PERFORMED HIGH POWER RUNS IAW EMB AMM 76--12-01 WITH NO DEFECTS - [SDR SIMA200717702](https://openairdocs.org/sdr/SIMA200717702.md): Electronic Unit · failed · Jun 22, 2007 · N706RG · Emb EMB135LR · Landing Gear Retraction/Extension System > GEAR HANDLE FOUND TO BE UNMOVABLE FOLLOWED BY A LANDING GEAR AIR/GROUND FAIL MESSAGE, RETURNED TO YYZ. MESSAGE EXTINGUISHED ON APPROACH. REMOVED AND REPLACED LANDING GEAR ELECTRONIC CONTROL UNIT, LANDING GEAR CONTROL LEVER AND AIR/GROUND POSITION RELAY IAW E - [SDR SIMA200634605](https://openairdocs.org/sdr/SIMA200634605.md): Handle · cracked · Dec 6, 2006 · N706RG · Emb EMB135LR · Passenger/Crew Doors > MAIN ENTRANCE DOOR HANDLE FOUND CRACKED. STOPPED DRILLED CRACK, FABRICATED DOUBLER, CLEANED AND TREATED AREA. INSTALLED DOUBLER IAW EMB IC2006-145-9643 PARAGRAPH 1. - [SDR SIMA200634001](https://openairdocs.org/sdr/SIMA200634001.md): Sill · corroded · Dec 5, 2006 · N706RG · Emb EMB135LR · Fuselage Miscellaneous Structure > SERVICE DOOR FRAME CENTER SILL FOUND CORRODED. REMOVED CORROSION, PERFORMED NDT, TREATED BLENDED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER IAW EMB SRM 53-21-02. RETURN AIRCRAFT TO SERVICE. - [SDR SIMA200617001](https://openairdocs.org/sdr/SIMA200617001.md): Odor · detected · Jun 13, 2006 · N706RG · Emb EMB135LR · Air Distribution System > ORF - FLT 4526 - FLIGHT CREW REPORTED SMOKE ODOR INSIDE THE FLIGHT DECK CABIN. ALSO GEN NR 1 READING 120 AMP AND GEN NR 3 READING 20-25 AMP. FLIGHT CREW REPORTED RELAY CLICKING NOISE BEHIND FLIGHT DECK DOOR. RAI NR 3 GENERATOR, IAW AEA WORK CARD 24-800-00, - [SDR SIMA200613202](https://openairdocs.org/sdr/SIMA200613202.md): Odor · detected · May 7, 2006 · N706RG · Emb EMB135LR · Air Distribution System > LGA - FLT 4730 - ODOR IN CABIN WITH ANTI-ICE ON. APU MEL`D. MAINTENANCE PERFORMED OPS CHECKS OF THE APU WITH AIR ON AND OFF, WITH HOT AND COLD SETTINGS AND FOUND NO PRESENCE OF ANY ODOR. MEL RESTORED IAW EMB-135, AMM 30-00-00. OPS CHECK GOOD. AIRCRAFT RET - [SDR SIMA200503101](https://openairdocs.org/sdr/SIMA200503101.md): Skin · gouged · Jan 29, 2005 · N706RG · Emb EMB135LR · Fuselage Main, Plate/Skin > DURING AN MBV INSPECTION THE BAGGAGE DOOR CUT OUT WAS FOUND TO BE GOUGED AT THE AFT LOWER CORNER OUTER SKIN. REMOVED THE DAMAGED OUTER SKIN BY MAKING A CUTOUT. FABRICATED A FILLER, DOUBLER FOR REPAIR. REPAIR DONE IAW SRM. (SW21200503066) (K) - [SDR SIMA200503803](https://openairdocs.org/sdr/SIMA200503803.md): Skin · gouged · Jan 29, 2005 · N706RG · Emb EMB135LR · Fuselage Main, Plate/Skin > DURING AN INSPECTION OF AIRCRAFT, THE BAGGAGE DOOR CUT OUT WAS FOUND TO BE GOUGED AT THE AFT LOWER CORNER OUTER SKIN. REMOVED THE DAMAGED OUTER SKIN MY MAKING A CUTOUT. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K) - [SDR SIMA200502801](https://openairdocs.org/sdr/SIMA200502801.md): Sill · corroded · Jan 24, 2005 · N706RG · Emb EMB135LR · Fuselage Miscellaneous Structure > FOUND SERVICE DOOR CENTER SILL PREVIOUS REPAIR WAS FOUND CORRODED. REMOVED EXISTING SERVICE DOOR SILL AND INSTALLED NEW SILL SRM. (SW21200503066) (K) - [SDR SIMA20047205](https://openairdocs.org/sdr/SIMA20047205.md): Fcu · inoperative · Sep 26, 2004 · N706RG · Emb EMB135LR · Trailing Edge Flap Control System > ON TAKEOFF ROLL AT 25KIAS, RECEIVED SPOILERS DEPLOYED MESSAGE. TAKEOFF WAS ABORTED. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR SIMA200307008](https://openairdocs.org/sdr/SIMA200307008.md): Floorbeam · corroded · Mar 7, 2003 · N706RG · Emb EMB135LR · Fuselage Main, Floor Beam > ABI - DURING A IMBV INSPECTION THE LEFT OMEGA BEAM AT FRAME 33 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. BLENDED THE CORRODED AREA AND PEFORMED AN NDT INSPECTION. FABRICATED A DOUBLER, REPAIR DONE IAW EMB SRM (SRM EMB 145/1141 REV 20) CHAPTERS 53-21-10 FIG 2 - [SDR SIMA200307006](https://openairdocs.org/sdr/SIMA200307006.md): Sill · corroded · Mar 7, 2003 · N706RG · Emb EMB135LR · Fuselage Miscellaneous Structure > ABI - DURING A IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. BLENDED THE CORRODED AREA OF THE CENTER SILL AND PERFORMED AN NDT INSPECTION. FABRICATED A DOUBLER, REPAIR DONE IAW EMB SRM (SRM 145/1142 REV 20) CHAPTER - [SDR SIMA200307007](https://openairdocs.org/sdr/SIMA200307007.md): Floorbeam · corroded · Mar 6, 2003 · N706RG · Emb EMB135LR · Fuselage Main, Floor Beam > ABI - DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM BETWEEN FRAMES 23 AND 26 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT 6.25 INCH SECTION OF THE DAMGAED BEAM. FABRICATED AN EXTERNAL ANGLE, SHIMS AND FILLER. REPAIR DONE IAW EMB SRM (SRM 145/1142 R - [SDR SIMA200307901](https://openairdocs.org/sdr/SIMA200307901.md): Gusset · corroded · Feb 22, 2003 · N706RG · Emb EMB135LR · Fuselage Miscellaneous Structure > THIS IS A LEVEL TWO FINDING FOUND DURING A IMBV INSPECTION, RIGHT BEAM GUSSET AT FRAME 20 IS CORRODED. REMOVED AND INSTALLED NEW RIGHT BEAM GUSSET AT FRAME 20 IAW EMB 135 SRM 51-20-03, 51-40-02. (M) - [SDR SIMA200307902](https://openairdocs.org/sdr/SIMA200307902.md): Angle · corroded · Feb 22, 2003 · N706RG · Emb EMB135LR · Fuselage Miscellaneous Structure > ABI - THIS IS A LEVEL TWO FINDING, FOUND DURING A IMBV INSPECTION LT BEAM RAMP ANGLE IS CORRODED AT FRAME 19-20. REMOVED AND INSTALLED NEW BEAM RAMP ANGLE IAW EMB 135 SRM 51-20-01, 51-20-03, 51-40-02 AND 51-40-04. (M) - [SDR SIMA200307905](https://openairdocs.org/sdr/SIMA200307905.md): Sill · corroded · Feb 22, 2003 · N706RG · Emb EMB135LR · Fuselage Miscellaneous Structure > THIS IS A LEVEL TWO FINDING, FOUND DURING AN IMBV INSPECTION SERVICE DOOR FORWARD SILL IS CORRODED. REMOVED AND INSTALLED SERVICE DOOR SILL IAW EMB 135 SRM 51-40-02, 51-20-03 AND 51-40-06. (M) - [SDR SIMA200307906](https://openairdocs.org/sdr/SIMA200307906.md): Structure · corroded · Feb 22, 2003 · N706RG · Emb EMB135LR · Fuselage Miscellaneous Structure > ABI - THIS IS A LEVEL TWO FINDING, FOUND DURING AN IMBV INSPECTION, CROSS MEMBER AT FRAME 22 IS CORRODED. REMOVED AND INSTALLED NEW CROSSMEMBER IAW EMB 135 SRM 51-40-02, 51-40-03. (M) - [SDR SIMA200308903](https://openairdocs.org/sdr/SIMA200308903.md): Beam · corroded · Feb 22, 2003 · N706RG · Emb EMB135LR · Fuselage Main, Structure > THIS IS A LEVEL TWO FINDING, FOUND DURING AN IMBV INSPECTION CENTER BEAM RAMP IS CORRODED. REMOVED AND INSTALLED SERVICEABLE CENTER BEAM IAW EMB 135 SRM 51-40-02, 51-40-06 AND 51-20-03. (M) - [SDR SIMA200307904](https://openairdocs.org/sdr/SIMA200307904.md): Gusset · corroded · Feb 22, 2003 · N706RG · Emb EMB135LR · Fuselage Miscellaneous Structure > ABI - THIS IS A LEVEL TWO FINDING, FOUND DURING A IMBV INSPECTION CENTER BEAM GUSSETT IS CORRODED. REMOVED AND INSTALLED SERVICEABLE GUSSET IAW EMB 135 SRM 51-40-02, 51-20-03 AND 51-40-06. (M) - [SDR SIMA200307907](https://openairdocs.org/sdr/SIMA200307907.md): Doubler · corroded · Feb 21, 2003 · N706RG · Emb EMB135LR · Fuselage Floor Panel > THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION, LEFT CARGO FLOOR DOUBLER FROM STATION 65 TO 68 CORRODED. REMOVED AND INSTALLED CARGO FLOOR DOUBLER FROM STATION 65 TO 68 IAW EMB SRM 51-40-02. (M) - [SDR SIMA200232305](https://openairdocs.org/sdr/SIMA200232305.md): Windshield · cracked · Nov 14, 2002 · N706RG · Emb EMB135LR · Flight Compartment Windows > LGA - FLT 4463 - DURING CRUISE, AT 27,000 FEET, THE FIRST OFFICERS WINDOW SHATTERED. AN EMERGENCY WAS DECLARED AND AIRCRAFT CONTINUED TO LGA AND LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD IAW EMB MM. OPERATIONAL CHECK WAS - [SDR SIMA200122403](https://openairdocs.org/sdr/SIMA200122403.md): Floorbeam · corroded · Jul 31, 2001 · N706RG · Emb EMB135LR · Fuselage Main, Floor Beam > ABI - DURING AN MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE OMEGA BEAM AT FRAME 20. CORROSION WAS REMOVED AND DAMAGE WAS REPAIRED IAW EMB SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) - [SDR SIMA200122402](https://openairdocs.org/sdr/SIMA200122402.md): Beam · corroded · Jul 31, 2001 · N706RG · Emb EMB135LR · Fuselage Miscellaneous Structure > ABI - DURING AN MBV INSPECTION, FOUND CORROSION ON THE GALLEY CENTER BEAM. CORROSION WAS REMOVED AND DAMAGE WAS REPAIRED IAW EMB REPAIR STATEMENT GST 2592/01. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) - [SDR SIMA200121901](https://openairdocs.org/sdr/SIMA200121901.md): Beam · corroded · Jul 31, 2001 · N706RG · Emb EMB135LR · Buffet/Galleys > ABI - DURING MBB INSPECTION, FOUND CORROSION ON THE GALLEY CENTER BEAM. CORROSION WAS REMOVED AND REPAIR WAS CARRIED OUT IAW EMB REPAIR STATEMENT. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) - [SDR SIMA200121902](https://openairdocs.org/sdr/SIMA200121902.md): Floorbeam · corroded · Jul 31, 2001 · N706RG · Emb EMB135LR · Fuselage Main, Floor Beam > ABI - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE OMEGA BEAM AT FRAME 20. CORROSION WAS REMOVED AND REPAIR WAS CARRIED OUT IAW EMB SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) - [SDR SIMA200121903](https://openairdocs.org/sdr/SIMA200121903.md): Floorbeam · corroded · Jul 31, 2001 · N706RG · Emb EMB135LR · Fuselage Main, Floor Beam > ABI - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE LEFT CENTER OMEGA BEAM AT FRAME 20. CORROSION WAS REMOVED AND REPAIR WAS CARRIED OUT IAW EMB SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) - [SDR SIMA20011151](https://openairdocs.org/sdr/SIMA20011151.md): Controller · inoperative · Apr 25, 2001 · N706RG · Emb EMB145LR · Cabin Pressure Controller > XNA - FLT 3546 - CREW REPORTED PRESSURIZATION WAS INOPERATIVE IN AUTO/MANUAL. AIRCRAFT WAS RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED THE DIGITAL PRESSURE CONTROLLER. OPS CHECK WAS GOOD IAW EMB MM. AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR SIMA0432](https://openairdocs.org/sdr/SIMA0432.md): Skin · gouged · Feb 12, 2001 · N706RG · Emb EMB145LR · Fuselage Main, Plate/Skin > SAW - DURING PS-2 INSPECTION MAINTENANCE REPAIRED TDMI 706530052. GOUGE IN LEFT CENTER FUSELAGE BETWEEN FRAMES 16 AND 20 STRINGERS 15 AND 16. MAINTENANCE REPAIRED THE GOUGE IAW EO EB-53MR-012. AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR SIMA200003901](https://openairdocs.org/sdr/SIMA200003901.md): Smoke Detector · malfunctioned · Feb 8, 2001 · N706RG · Emb EMB145LR · Smoke Detection > ORD - FLT 4401 - DURING CLIMB, CREW REPORTED THE LAV SMOKE CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO ORD, LIGHT EXTINGUISHED DURING APPROACH. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPS CHECK WAS GOOD AND AIRCRAFT WAS RELEASED FOR FLIGHT. NEXT F - [SDR SIMA0173](https://openairdocs.org/sdr/SIMA0173.md): Control Unit · failed · Jan 17, 2001 · N706RG · Emb EMB145LR · Drag Control System > BOS - FLT 4975 - SPOILER FAIL MESSAGE IN FLIGHT AND ON GROUND. FAIL MESSAGE IN AIR WHEN LEVER IS OPEN. AFTER LEVER IS CLOSED, ALERT MESSAGE GOES AWAY. ALSO DAU WARNING ''MISCOMP'' MSG COMES ON WITH SPOILER FAIL MESSAGE IN AIR OR ON GROUND. AIRCRAFT FERRIED - [SDR 20001208SH005](https://openairdocs.org/sdr/20001208SH005.md): Dau · inoperative · Oct 11, 2000 · N706RG · Emb EMB135LR · Fire Detection > RIC - FLT 4942 - CREW REPORTED BOTH E1 AND E1 EXTINGUISHING SYSTEMS INOPERATIVE WITH GLARESHIELD. MASTER CAUTION LIGHT ILLUMINATED. MAINTENANCE FOUND NO EVIDENCE OF FIRE OR SMOKE. LEFT ENGINE FIRE BOTTLE AND NR 1 DATA ACQUISTION UNIT WERE REMOVED AND REPLAC - [SDR SIMA2856](https://openairdocs.org/sdr/SIMA2856.md): Fire Bottle · discharged · Oct 11, 2000 · N706RG · Emb EMB145LR · Extinguishing System > RIC - FLT 4942 - CREW REPORTED BOTH E1 AND E1 EXTINGUISHING SYSTEMS INOPERATIVE WITH GLARESHIELD. MASTER CAUTION LIGHT ILLUMINATED. MAINTENANCE FOUND NO EVIDENCE OF FIRE OR SMOKE. LEFT ENGINE FIRE BOTTLE AND NR 1 DATA ACQUISTION UNIT WERE REMOVED AND REPLAC - [SDR 20001229AP004](https://openairdocs.org/sdr/20001229AP004.md): Smoke Detector · malfunctioned · Jan 10, 2000 · N706RG · Emb EMB145LR · Smoke Detection > ORD - FLT 4065 - FLIGHT CREW GOT A AFT CARGO SMOKE INDICATION. DISCHARGED BOTH BOTTLES. NO SIGNS OF FIRE OR SMOKE. REMOVED AND REPLACED BOTH FIRE BOTTLES AND SMOKE DETECTOR. OPS CHECK GOOD. (M) - [SDR 20001229AP003](https://openairdocs.org/sdr/20001229AP003.md): Smoke Detector · malfunctioned · Jan 10, 2000 · N706RG · Emb EMB145LR · Smoke Detection > ORD - FLT 4065 - FLIGHT CREW GOT A AFT CARGO SMOKE INDICATION. DISCHARGED BOTH BOTTLES. NO SIGNS OF FIRE OR SMOKE. REMOVED AND REPLACED BOTH FIRE BOTTLES AND SMOKE DETECTOR. OPS CHECK GOOD. (M) - [SDR SIMA0105](https://openairdocs.org/sdr/SIMA0105.md): Smoke Detector · inoperative · Jan 10, 2000 · N706RG · Emb EMB145LR · Smoke Detection > ORD - FLT 4065 - FLIGHT CREW GOT A AFT CARGO SMOKE INDICATION. DISCHARGED BOTH BOTTLES. NO SIGNS OF FIRE OR SMOKE. REMOVED AND REPLACED BOTH FIRE BOTTLES AND SMOKE DETECTOR. OPS CHECK GOOD. (M) ## 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 = 'N706RG' AND deregistration_id = 'N706RG-2019-09-10' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N706RG-2019-09-10/reports --- 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.