N169HQ
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.
23 reports on file, 2009-12-24 – 2013-12-22.
Part: FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 14,227 hrs · 9,272 cycles
DURING HEAVY CHECK, AT FRAME 84 CORRODED . MX FABRICATED DOUBLER, INSTALLED REPAIR DOUBLERS AND FILLER, IAW SRM II 53-00-10.
Part: GUST LOCK — LACK OF LUBE (L1 DOOR) · airframe 13,147 hrs · 8,630 cycles
CREW REPORTED THAT THE L1 DOOR WAS HARD TO CLOSE. MAINTENANCE LUBED GUST LOCK PER EMB AMM AND OPS CHECKED GOOD.
Part: PANEL — CRACKED (NR 2 EXHAUST) · airframe 11,432 hrs · 7,390 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE WORKED DMI 337987103 NUMBER TWO ENGINE AFT PYLON FAIRING INBOARD EXHAUST GRILL IS CRACKED. MAINTENANCE REMOVED AND REPLACED NUMBER TWO ENGINE AFT PYLON FAIRING INBOARD EXHAUST GRILL IAW EMB ETD 2012-190-011599B , REV B. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
Part: PANEL — CRACKED (NR 1 EXHAUST) · airframe 11,432 hrs · 7,390 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE WORKED DMI 337987/02 NUMBER ONE ENGINE INBOARD AFT EXHAUST PANEL GRILL IS CRACKED. MAINTENACE REPLACED GRILL HEAT SHIELD NUMBER ONE ENGINE AFT PYLON FAIRING INBOARD POSITION IAW EMB ETD 2012-190-011599-B REV B. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
Earlier reports · 2009–2012 · 19 reports
2012
Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,470 hrs · 6,727 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND FLOOR SPLICE ON RT SHEER PLATE HAS CORROSION AT FR 87-88. MX REMOVED AND REPLACED FLOOR SPLICE ON RIGHT O/B SHEER PLATE AT FR 87-88 IAW EMB 190 SRM 51-40-00, 51-42-02. PN 170-65644-001. A/C REMAINS IN CMH FOR COMPLETION.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 10,470 hrs · 6,727 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND ECS BRACKET CRACKED, EMERGENCY RAM AIR VALVE. MX REMOVED AND REPLACED THE ECS BRACKET IAW EMB 190 SRM 51-40-02, 51-41-01. P/N 190-27133-003. A/C REMAINS IN CMH FOR COMPLETION.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 10,470 hrs · 6,727 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND ECS BRACKET CRACKED, EMERGENCY RAM AIR VALVE. MX REMOVED AND REPLACED ECS BRACKETS THAT HOLD THE EMERGENCY RAM AIR VALVE IAW EMB 190 SRM 51-40-02, 51-41-01 P/N 190-27131-001. A/C REMAINS IN CMH FOR COMPLETION.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 10,470 hrs · 6,727 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND ECS BRACKET CRACKED, EMERGENCY RAM AIR VALVE. MX REMOVED AND REPLACED ECS BRACKET IAW EMB 190 SRM 51-40-02, 51-41-01. PN 190-27151-003. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,470 hrs · 6,727 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND RIGHT I/B CF3 SEAT TRACK BEAM CORRODED. MX REMOVED AND REPLACED RIGHT CF3 LOWER TRACK PN 170-86082-005 IAW EMB 190 SRM 51-41-01, 51-41-02, 51-43-01, 51-43-02. A/C REMAINS IN CMH FOR COMPLETION.
Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,470 hrs · 6,727 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND RT SHEAR PLATE BETWEEN FR 87-88 HAS CORROSION. MX REMOVED AND REPLACED RT SHEAR PLATE BETWEEN FR 87-88 IAW EMB 190SRM 51-42-01. PN 170-91919-001. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,470 hrs · 6,728 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND GUSSET ON RT I-BEAM HAS CORROSION. MX REMOVED AND REPLACED GUSSET ON RT I-BEAM AT SPAR 90 AND GUSSET ON THE LT SIDE ALSO. BOTH P/N 170-60257-001. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,470 hrs · 6,727 cycles
WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE RT I BEAM BETWEEN FRAMES 87 & 88. MAINTENANCE REMOVED & REPLACED THE RT I BEAM BETWEEN FRAMES 87 & 88 IAW EMB 190 SRM 51-41-01, 51-43-03, 51-40-02 AND 51-43-02. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,470 hrs · 6,727 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND LT I-BEAM HAS CORROSION ON FASTENER AT FR 88. MX REMOVED AND REPLACED LT I-BEAM SEAT TRACK IAW EMB 190 SRM 51-40-02, 51-43-01, 51-41-01. PN 170-65669-003. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,470 hrs · 6,728 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND GUSSET ON OUTBD RT I-BEAM HAS CORROSION AT FR 90. MX REMOVED AND REPLACED GUSSET P/N 170-60259-001 ON RT I-BEAM AT FR 90 IAW EMB 190 SRM 51-41-02. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
Part: SERVICE PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,470 hrs · 6,727 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND WASTE BOX IS DELAMINATING AND CORRODED. MX REMOVED AND REPLACED WASTE BOX ASSEMBLY IAW EMB 190 SRM 51-23-02, 51-40-02,51-43-03, 51-41-02. PN 170-65078-403. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,470 hrs · 6,727 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND GUSSET ON LT SHEAR PLATE HAS CORROSION AT FR 87-88. MX REMOVED AND REPLACED GUSSET ON LT SHEAR PLATE AT FR 87-88. PN 170-65644-001. A/C REMAINS IN CMH FOR COMPLETION.
2011
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 7,910 hrs · 5,230 cycles
CREW REPORTED EMERGENCY LIGHTS WOULDN'T TURN OFF AFTER TEST. MAINTENANCE PERFORMED RESET OF EMERGENCY LIGHTS PER EMB AMM, AND OPS CHECK GOOD.
Part: WARNING SYSTEM — FALSE ACTIVATION (OVERWING EXIT) · airframe 7,800 hrs · 5,173 cycles
CREW REPORTED OWE SHOWED OPEN DURING CLIMB, CREW RETURNED TO FIELD AT DCA AND LANDED WITHOUT INCIDENT. AN EMERGENCY WAS NOT DECLARED. MAINTENANCE INSPECTED RT OVERWING EXIT PER EMB AMM AND REPORTED NO DEFECTS FOUND. A/C WAS RETURNED TO SERVICE.
2010
Part: UNKNOWN — SMOKE (CABIN) · airframe 5,588 hrs · 3,994 cycles
CREW REPORTED SMOKE IN THE CABIN DURING TAKEOFF, DECLARED EMERGENCY AND RETURNED TO FIELD AT CMH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE PACKS, TAT PROBES, EBAYS, AND ENGS, PER EMB AMM AND RAN ENGINES ON GROUND FOR 19 MIN. MTX WAS UNABLE TO DUPLICATE ANY FAULTS & SMELLS, A/C WAS RELEASED BACK INTO SERVICE.
Part: PIN — OUT OF POSITION (L1 DOOR) · airframe 4,257 hrs · 3,296 cycles
CREW REPORTED L-1 DOOR BUSTLE COVER PIN IS HANGING FROM THE DOOR. MAINTENANCE RE-INSTALLED THE PIN PER EMB AMM.
Part: PIN — OUT OF POSITION (L1 DOOR) · airframe 4,072 hrs · 3,210 cycles
THE CREW REPORTED, DISCOVERED THE BUSTLE IN OUT ON THE L-1 DOOR. MAINTENANCE RE-INSTALLED THE BUSTLE PIN ON THE MAIN CABIN DOOR PER EMB AMM, NO FURTHER DEFECTS WERE NOTED. THE A/C WAS THEN RELEASED BACK INTO SERVICE.
Part: SKIN — CRACKED (FUSELAGE) · airframe 3,676 hrs · 3,035 cycles
DENT DISCOVERED FWD OF PASSENGER DOOR BY PILOT. THIS WAS CLASSIFIED AS A MAJOR REPAIR. THE DAMAGE IS A DENT WITH A CRACK LOCATED BETWEEN FRAMES 11 AND 12 (2.5 INCHES AFT OF FRAME 11), STRINGERS 17L AND 18L (0.75 INCH BELOW STRINGER 17L AND 2.75 INCH ABOVE STRINGER 18L). THE DENT MEASURES 2.75 X 3.5 INCHES WITH A 1.0 INCH CRACK IN THE BOTTOM. MAINTENANCE EVALUATED AND SENT INFO TO EMBRAER, RECEIVED A ETD2010-190/00048 FOR REPAIR. AC REPAIRED AND RETURNED TO SERVICE.
2009
Part: SENSOR — FAULTY (LE SLAT) · airframe 3,629 hrs · 3,022 cycles
CREW DECLARED EMERGENCY FOR SLAT FAIL INTO DEN, LANDED WITHOUT INCIDENT. MTX DISPATCHED TO A/C TO TROUBLESHOOT, AND FOUND FAULT CODE 27811014ACE. MTX REMOVED AND REPLACED THE RT OUTBOARD SKEW SENSOR PER EMB AMM, A/C WAS THEN RELEASED BACK INTO SERVICE.