N706RG
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
36 reports on file, 2000-01-10 – 2008-01-03.
Part: LINE — DISCONNECTED (NR 4 BRAKE) · airframe 18,373 hrs · 16,324 cycles
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. OPERATIONAL CHECK GOOD AND TAXI CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
Earlier reports · 2000–2007 · 35 reports
2007
Part: COMPUTER — FAILED (AHRS) · airframe 17,368 hrs · 1,551 cycles
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 NOTED. PERFORMED OPERATIONAL CHECKS OF YAW DAMPER IAW EMB AMM 22-11-00 WITH NO DEFECTS. AIRCRAFT RETURNED TO SERVICE.
Part: ELECTRONIC UNIT — FAILED (ZONE 200) · airframe 17,038 hrs · 15,225 cycles
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 EMB AMMS 32-32-01, 32-32-02, AND 32-13-02. PERFORMED OPERATIONAL CHECKS IAW AMM 32-30-00 AND 32-52-00 WITH NO FURTHER DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE.
2006
Part: HANDLE — CRACKED (CRACKED) · airframe 15,755 hrs · 14,158 cycles
MAIN ENTRANCE DOOR HANDLE FOUND CRACKED. STOPPED DRILLED CRACK, FABRICATED DOUBLER, CLEANED AND TREATED AREA. INSTALLED DOUBLER IAW EMB IC2006-145-9643 PARAGRAPH 1.
Part: SILL — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 15,755 hrs · 14,158 cycles
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.
Part: ODOR — DETECTED (COCKPIT)
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, OPS CHECK GOOD IAW EMB135, AMM 24-31-00. RAI NR 1 AND 2 GCUS, IAW EMB135 AMM 24-31-02, OPS CHECK GOOD. PERFORMED FCF FOUND SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)
Part: ODOR — DETECTED (CABIN)
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 RETURNED TO SERVICE. (M)
2005
Part: SKIN — GOUGED (FUSELAGE)
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)
Part: SKIN — GOUGED (FUSELAGE) · airframe 11,566 hrs · 10,646 cycles
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)
Part: SILL — CORRODED (FUSELAGE)
FOUND SERVICE DOOR CENTER SILL PREVIOUS REPAIR WAS FOUND CORRODED. REMOVED EXISTING SERVICE DOOR SILL AND INSTALLED NEW SILL SRM. (SW21200503066) (K)
2004
Part: FCU — INOPERATIVE (TE FLAPS)
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)
2003
Part: FLOORBEAM — CORRODED (GALLEY)
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 208 AND EMB REPAIR STATEMENT IC2003-145/0771. (M)
Part: SILL — CORRODED (SERVICE DOOR)
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 51-21-02 AND EMB REPAIR STATEMENT 1C2003-145/0771. (M)
Part: FLOORBEAM — CORRODED (GALLEY)
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 REV 20) CHAPTERS 53-22-10 FIG 201. (M)
Part: ANGLE — CORRODED (GALLEY)
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)
Part: SILL — CORRODED (SERVICE DOOR)
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)
Part: STRUCTURE — CORRODED (GALLEY)
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)
Part: BEAM — CORRODED (GALLEY)
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)
Part: GUSSET — CORRODED (GALLEY)
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)
Part: GUSSET — CORRODED (GALLEY)
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)
Part: DOUBLER — CORRODED (CARGO FLOOR)
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)
2002
Part: WINDSHIELD — CRACKED (COCKPIT)
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 GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
2001
Part: FLOORBEAM — CORRODED (FUSELAGE)
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)
Part: BEAM — CORRODED (FUSELAGE)
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)
Part: BEAM — CORRODED (GALLEY)
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)
Part: FLOORBEAM — CORRODED (FUSELAGE)
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)
Part: FLOORBEAM — CORRODED (FUSELAGE)
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)
Part: CONTROLLER — INOPERATIVE (COCKPIT)
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)
Part: SKIN — GOUGED (FUSELAGE)
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)
Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)
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 FLIGHT SAME DISCREPANCY. MAINTENANCE THEN REPLACED LAV COMPARTMENT SMOKE DETECTOR. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: CONTROL UNIT — FAILED (COCKPIT)
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 TO CMH WITH SPOILER SYSTEM DEACTIVATED FOR REPAIR. REPLACED SPOILER CONTROL UNIT IAW AMM 27-63-02-000-801A AND PERFORMED SYSTEM CHECKS. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
2000
Part: DAU — INOPERATIVE (LEFT ENGINE) · airframe 1,975 hrs · 1,742 cycles
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 REPLACED. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA2856. (X)
Part: FIRE BOTTLE — DISCHARGED (LEFT ENGINE) · airframe 1,975 hrs · 1,742 cycles
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 REPLACED. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR 20001208SH005. (X)
Part: SMOKE DETECTOR — MALFUNCTIONED (AFT CARGO BAY)
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)
Part: SMOKE DETECTOR — MALFUNCTIONED (AFT CARGO BAY)
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)
Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY)
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)