N167HQ
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.
54 reports on file, 2010-04-03 – 2014-04-21.
Part: GUSSET — CORRODED (R1 DOOR) · corrosion level 2 · airframe 15,254 hrs · 9,692 cycles
DURING HEAVY CHECK, R1 DOOR ATTACH GUSSET HAS A FASTENER WITH CORROSION. MX R & R R1 DOOR ATTACH GUSSET FASTENER LOWER FORWARD CORNER IAW SRM 51-43-03.
Part: TERMINAL — CORRODED (APU) · corrosion level 2 · airframe 15,254 hrs · 9,692 cycles
DURING HEAVY CHECK, TERMINAL END APU ESC HAS BROKEN INSULATOR AND IS CORRODED. MX R & R TERMINAL END APU ESC IAW W206-00002-00N, SWPM 20-21-10. PN MS25036-132, TERMINAL END. AIRCRAFT REMAINS UNTIL HEAVY CHECK IS COMPLETED.
Part: BOLT — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,254 hrs · 9,692 cycles
DURING HEAVY CHECK RT APU ISLOATOR MOUNT HARDWARE IS CORRODED. MX R & R RT APU ISOLATOR MOUNT HARDWARE IAW AMM 53-31-35, PN NAS6304-13, BOLT.
Part: RUB STRIP — CORRODED (ZONE 500) · corrosion level 2 · airframe 15,254 hrs · 9,692 cycles
DURING HEAVY CHECK, LT ENGINE INBD FAN COWL UPPER METALLIC STRIP WORN AND CORRODED. MAINTENANCE R & R LT ENGINE INBD FAN COWL UPPER METALLIC STRIP IAW SRM 51-41-02, PN 341-2311-505, RUB STRIP.
Part: STRIP — CORRODED (FAN INLET) · corrosion level 2 · airframe 15,254 hrs · 9,692 cycles
DURING HEAVY CHECK, LT ENGINE FAN COWL AFT METALLIC STRIP IS WORN AND CORRODED. MX R & R LT ENGINE FAN COWL AFT METALLIC STRIP IAW SRM 51-42-02.
Part: RUB STRIP — CORRODED (ZONE 500) · corrosion level 2 · airframe 15,254 hrs · 9,692 cycles
DURING HEAVY CHECK, LT ENGINE OTBD FAN COWL UPPER METALLIC STRIP WORN AND CORRODED. MX R & R LT ENGINE OTBD FAN COWL UPPER METALLIC STRIP IAW SRM 51-41-02, PN 341-2311-505, RUB STRIP.
Part: STRIP — CORRODED (FAN INLET) · corrosion level 2 · airframe 15,254 hrs · 9,692 cycles
DURING HEAVY CHECK, LT ENGINE OTBD FAN COWL FWD METALLIC STRIP WORN AND CORRODED. MX R & R LT ENGINE OTBD FAN COWL FWD METALLIC STRIP IAW SRM 51-41-02, PN 341-2309-503 STRIP.
Part: SEAL REST — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 15,254 hrs · 9,692 cycles
DURING HEAVY CHECK, FWD CARGO DOOR FWD SEAL REST CORRODED. MAINTENANCE R & R SEAL REST IAW AMM 20-10-01.
Part: HINGE — CORRODED (WASTE DOOR) · corrosion level 2 · airframe 15,254 hrs · 9,692 cycles
DURING HEAVY CHECK, WASTE DOOR HINGE IS CORRODED. MX R & R WASTE DOOR ASSY IAW AMM 20-10-01, 20-10-02.
Part: SEAT TRACK — CORRODED (FRAME 87) · corrosion level 2 · airframe 15,254 hrs · 9,692 cycles
DURING HEAVY CHECK, SEAT TRACK AFT EXTENSION AT FRAME 87 HAS ONE FASTENER WITH CORROSION. MAINTENANCE R & R RT SEAT TRACK AFT EXTENSION AT FRAME 87 IAW SRM 51-40-01, 51-43-01, 51-41-01AND SWPM 20-67-000, PN 170-65669-004, BEAM.
Part: FASTENER — CORRODED (SEAT TRACK) · corrosion level 2 · airframe 15,254 hrs · 9,692 cycles
DURING HEAVY CHECK, LT SEAT TRACK AFT EXTENSION HAS ONE FASTENER BETWEEN FRAMES 85-86 CORRODED. MX R & R SEAT TRACK FASTENER IAW SRM 51-41-01.
Part: SUPPORT CHANNEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,254 hrs · 9,692 cycles
DURING HEAVY CHECK, SUPPORT CHANNEL NEAR FRAME 86 LT SIDE IS CORRODED. MAINTENANCE R & R IAW 51-41-01,51-42-01,51-43-03.
Part: SEAL REST — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 15,254 hrs · 9,692 cycles
DURING HEAVY CHECK, FWD CARGO DOOR CENTER LOWER SEAL REST IS CORRODED. R & R FWD SEAL REST IAW SRM 51-40-02, 51-41-01. MAJOR REPAIR.
Part: SEAL REST — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 15,254 hrs · 9,692 cycles
FWD CARGO DOOR CUTOUT CENTER LOWER SEAL REST HAS SIGNS OF CORROSION. R & R FWD SEAL REST IAW SRM 51-40-02, 51-41-01 IAW SRM 51-21-02. MAJOR REPAIR.
Part: BUSHING — CORRODED (RUDDER) · corrosion level 2 · airframe 15,254 hrs · 9,692 cycles
DURING HEAVY CHECK, LOWER RUDDER PCU TOGGLE LINK BUSHING THAT ATTACHES TO RUDDER TO TOGGLE LINK IS CORRODED. MX R & R LOWER RUDDER PCU TOGGLE LINK BUSHING THAT ATTACHES TO RUDDER TO TOGGLE LINK IAW AMM 27-22-02. PN 415406-1, BUSHING.
Part: STRUCTURE — CORRODED (SEAL REST) · corrosion level 2 · airframe 15,254 hrs · 9,692 cycles
DURING HEAVY CHECK, FWD CARGO DOOR CUT OUT AFT SEAL REST IS CORRODED. MX REMOVED AND MATCH DRILLED AND REPLACED FWD CARGO DOOR CUT OUT AFT SEAL REST IAW SRM 51-40-02 SEAL REST TO BE INSTALLED ON TASK CARD R190-53-21-009-0414, NO FURTHER ACTION REQUIRED ON THIS CARD NON FCS. PN 170-66803-402, SEAL REST.
Part: SEAT TRACK — CORRODED (FRAMES 13-14) · corrosion level 2 · airframe 15,254 hrs · 9,692 cycles
DURING HEAVY CHECK, RT SEAT TRACK BETWEEN FRAMES 13-14 HAS CORROSION. MX R & R SEAT TRACK IAW SRM 51-40-02, 51-41-02, & 51-23-00.
Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 15,254 hrs · 9,692 cycles
DURING HEAVY CHECK, LT RAM AIR DUCT SUPPORT BRACKET IS CRACKED. MX R & R LT RAM AIR DUCT SUPPORT BRACKET IAW SRM 51-40-02, 51-41-01, PN 190-27133-003, SUPPORT.
Part: SHEAR WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 15,254 hrs · 9,692 cycles
DURING HEAVY CHECK, LT SHEAR WEB JUST FORWARD OF L1 DOOR IS CORRODED. MX R & R SHEAR WEB IAW SRM 51-41-02, 51-43-02.
Part: SEAT TRACK — CORRODED (FRAME 16) · corrosion level 2 · airframe 15,254 hrs · 9,692 cycles
DURING HEAVY CHECK, SEAT TRACK ABOVE FRAME 16 IS CORRODED. MX R & R SEAT TRACK IAW SRM 51-41-01, 51-41-02, 51-43-01, 51-43-02.
Part: BOLT — CORRODED (ZONE 600) · corrosion level 2 · airframe 15,254 hrs · 9,692 cycles
DURING HEAVY CHECK, THREE LATCH BOLTS ON BOTTOM CENTER OVERWING RT CUT OUT ARE CORRODED. MAINTENANCE R & R LATCH BOLTS IAW AMM 20-10-01, PN MS21134-03009, BOLT.
Part: MOUNT BRACKET — CRACKED (NLG STEERING) · airframe 15,254 hrs · 9,692 cycles
DURING HEAVY CHECK, NOSE WHEEL STEERING MANIFOLD MOUNT BRACKET FWD AND AFT FOUND CRACKED. R & R MOUNT BRACKET IAW SRM 51-43-03.
Earlier reports · 2010–2013 · 32 reports
2013
Part: SLAT SYSTEM — MALFUNCTIONED · airframe 14,007 hrs · 8,999 cycles
DURING APPROACH, CREW REPORTED THAT THE SLATS FAILED AT POSITION 3. FOLLOWED QRH AND FLAPS CAME BACK UP BUT SLATS DID NOT. DECLARED AN EMERGENCY. ACFT LANDED AND TAXIED TO GATE WITHOUT INCIDENT. MX RESET THE SYS IAW AMM AND SLATS RETRACTED. ACFT IS GOOD FOR SERVICE.
Part: SENSOR — DEFECTIVE (SLATS) · airframe 14,007 hrs · 9,000 cycles
AFTER TAKEOFF, CREW RECEIVED A SLAT FAIL MESSAGE WITH SLATS AT POSITION 3. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED AND TAXIED TO GATE WTIHOUT INCIDENT. MX FOUND SLAT SKEW SENSOR AND HARNESS HAD FAILED AND REPLACED IAW AMM. ACFT IS GOOD FOR SERVICE.
Part: PRECOOLER — DEFECTIVE (CABIN AIR) · airframe 13,895 hrs · 8,933 cycles
ENROUTE, CREW REPORTED THAT THE ACFT LOST PRESSURIZATION AT FL280. DECLARED AN EMERGENCY AND PERFORMED EMERGENCY DECENT PROCEDURE. LANDED AND TAXIED TO THE GATE WITHOUT INCIDENT. MX FOUND THE PRECOOLER HAD FAILED AND CHANGED THE PRECOOLER AND GASKETS IAW AMM. ACFT OPS CHECKED GOOD.
Part: MASK — BROKEN (CABIN) · airframe 13,639 hrs · 8,798 cycles
CREW REPORTED THAT THE AFT DEMO O2 MASK NEEDED TO BE REPLACED. MAINTENANCE REMOVED AND REPLACED AFT O2 DEMO MASK PER EMB AMM AND OPS CHECKED GOOD.
Part: GRILL — CRACKED (NR 1 PYLON) · airframe 12,095 hrs · 7,766 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE REPLACED HEAT SHIELD GRILL NUMBER ONE ENGINE INBOARD AFT PYLON FAIRING. MAINTENANCE REMOVED AND REPLACED THE HEAT SHIELD GRILL IAW EMB ETD 2012-190-011648-B REV B. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
2012
Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 12,519 hrs · 8,067 cycles
CREW REPORTED GIRT BAR WOULD NOT DISENGAGE WHEN ATTEMPTING TO OPEN MAIN DOOR UPON ARRIVAL AND SLIDE DEPLOYED. MAINTENANCE REMOVED AND REPLACED L1 DOOR SLIDE IAW EMB AMM 52-11-51 AND REF EMB 25-65-0.
Part: COVER — MISSING (EXIT SIGN) · airframe 11,915 hrs · 7,643 cycles
CREW REPORTED MID CABIN EMERGENCY EXIT SIGN MISSING COVER. MAINTENANCE RE-INSTALLED MISSING COVER PER EMB AMM.
Part: BATTERY — FAILED (CABIN) · airframe 11,872 hrs · 7,615 cycles
MAINTENANCE REPORTED THE EMERGENCY LIGHT BATTERY NR 2 FAILED THE FUNCTIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY IAW AMM 33-50-01. OPS CHECKED GOOD.
Part: LINER — OUT OF POSITION (L1 DOOR) · airframe 11,734 hrs · 7,519 cycles
L1 DOOR GUST/EGRESS LATCH NOT LATCHING PROPERLY. MAINTENANCE ADJUSTED DOOR LINER TO PROPER POSITION AND DOOR OPERATED AS REQUIRED.
Part: ROLLER — INOPERATIVE (L1 DOOR) · airframe 10,807 hrs · 6,903 cycles
CREW REPORTED L1 DOOR WOULDN'T CLOSE. MAINTENANCE TROUBLESHOT PER EMB AMM, AND FOUND L1 DOOR ROLLER INOP. MAINTENANCE REPLACED L1 DOOR ROLLER PER EMB AMM.
Part: BOLT — CORRODED (PAX DOOR) · corrosion level 2 · airframe 10,113 hrs · 6,445 cycles
WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE AFT PAX DOOR (L2) AFT SLIDE FUNCTION FITTING INBOARD BOLT. MAINTENANCE REMOVED AND REPLACED THE BOLT, NUT & COTTER PIN ON THE AFT PAX DOOR (L2) AFT SLIDE FUNCTION FITTING INBOARD SIDE IAW EMB 190/195 AMM 20-10-01 REF P/N'S NAS6604D11 BOLT, MS14144-4 NUT & MS24665-153 COTTER PIN. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,113 hrs · 6,445 cycles
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND 3 GUSSETS ON FLOORBEAM AT FRAME 90 CORRODED. MAINTENANCE REMOVED AND REPLACED 2 GUSSETS AT FRAME 90 IAW EMB190 SRM 51-40-02, 51-41-02 AND 51-21-00. ONE GUSSET AT FRAME 90 WAS FOUND TO BE FREE OF CORROSION. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,113 hrs · 6,445 cycles
WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE LT SPLICE PLATE OF THE LT SHEAR WEB AT FRAME 88. MAINTENANCE REMOVED AND REPLACED THE LT SPLICE PLATE ON THE LT SHEAR WEB AT FRAME 88 IAW EMB 190 SRM 51-42-01. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,113 hrs · 6,445 cycles
WHILE A/C WAS IN FOR HEAVY CHECK FOUND 3 GUSSETS ON FLOORBEAM AT FR90 HAS POSSIBLE CORROSION. MX REMOVED AND REPLACED 2 GUSSETS AT FR90 IAW EMB 190 SRM 51-40-02, 51-41-02, 51-21-00 AND 1 GUSSET AT FR 90 WAS FOUND TO BE FREE OF CORROSION BELOW TOP COAT. P/N 'S 170-60257-001, AND 170-60259-001. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,113 hrs · 6,445 cycles
WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE LT SHEAR WEB AT FRAME 88. MAINTENANCE REMOVED AND REPLACED THE LT SHEAR WEB AT FRAME 88 IAW EMB 190 SRM 51-42-01. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,113 hrs · 6,445 cycles
WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE RT SHEAR PANEL AT FRAME 87-88. MAINTENANCE REMOVED AND REPLACED THE RT SHEAR PANEL AT FRAME 87-88 IAW EMB 190 SRM 51-40-02, 51-42-02, 51-42-01 & 51-43-01. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
2011
Part: GASKET — DAMAGED (BLEED AIR SYS) · airframe 8,590 hrs · 5,553 cycles
CREW REPORTED DUAL BLEED LEAK DURING CLIMBOUT OF LGA. CREW DECLARED EMERGENCY AND DIVERTED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HP GROUND CONNECT GASKET PER EMB AMM, OPS CHECK GOOD.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 7,812 hrs · 5,137 cycles
CREW REPORTED 1/2 RAINBOW LIGHTS WOULDN'T RESET OR EXTINGUISH. MAINTENANCE PERFORMED RESET OF F/O FWD PA PSU PANEL PER EMB AMM, AND REPORTED NO FAULTS WERE FOUND.
Part: LIGHT — MALFUNCTIONED (COCKPIT) · airframe 7,591 hrs · 5,036 cycles
CREW REPORTED COCKPIT EMERGENCY LIGHT WOULDN'T ILLUMINATE. MAINTENANCE PERFORMED POWER RESET PER EMB AMM, AND ALL WAS OPS CHECK GOOD.
2010
Part: DOOR — LACK OF LUBE (L1) · airframe 6,749 hrs · 4,632 cycles
CREW REPORTED THE L-1 DOOR WAS HARD TO OPEN. MAINTENANCE LUBED AND INSPECTED L-1 DOOR PER EMB AMM, AND REPORTED OPS CHECK GOOD.
Part: SLIDE — UNSERVICEABLE (L2 DOOR) · airframe 6,110 hrs · 4,247 cycles
CREW REPORTED ISSUES WITH OPENING THE L-2 DOOR, AND REPORTED THE L-2 DOOR SLIDE BECAME PARTIALLY UNRAVELED. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR SLIDE ASSEMBLY PER EMB AMM. A/C WAS THEN RETURNED TO SERVICE.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 6,104 hrs · 4,243 cycles
CREW REPORTED RT OVERWING EXIT OPEN MSG IN FLIGHT. MTX OPENED AND CLOSE RT /OW ESCAPE HATCH PER EMB AMM, ALL INDICATIONS WERE THEN NORMAL. A/C WAS THEN RETURNED TO SERVICE.
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 5,824 hrs · 4,075 cycles
CREW REPORTED RT OWE SHOWED OPEN IN FLIGHT. MAINTENANCE PLACED ON MEL 52-70-00-1. A/C WAS THEN RETURNED TO SERVICE.
Part: WARNING SYSTEM — MALFUNCTIONED (OVERWING DOOR) · airframe 5,802 hrs · 4,062 cycles
CREW REPORTED RT OWD MSG IN FLIGHT. MAINTENANCE RESET THE INDICATION PER EMB AMM. ENGINEERING INSTRUCTION ISSUED TO VERIFY RIG OF RT OWD AND SWITCH.
Part: UNKNOWN — UNKNOWN (OVERWING DOOR) · airframe 5,794 hrs · 4,057 cycles
CREW REPORTED RT OWD MSG IN FLIGHT. MAINTENANCE RE-INSTALLED OWD PER EMB AMM, NO MSGS PRESENT.
Part: WARNING SYSTEM — ACTIVATED (EMERGENCY EXIT) · airframe 5,777 hrs · 4,047 cycles
CREW REPORTED ON DESCENT, RECEIVED RIGHT OVERWING EXIT OPEN INDICATION ON MFD ON DESCENT INTO SAN, AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED, INSPECTED, AND RE-INSTALLED RT OVERWING EXIT DOOR PER EMB AMM, NO DEFECTS NOTED.
Part: WARNING SYSTEM — ACTIVATED (EMERGENCY EXIT) · airframe 5,777 hrs · 4,047 cycles
CREW REPORTED ON DESCENT, RECEIVED RIGHT OVERWING EXIT OPEN INDICATION ON MFD ON DESCENT INTO OKC, AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED, INSPECTED, AND RE-INSTALLED RT OVERWING EXIT DOOR PER EMB AMM, NO DEFECTS NOTED.
Part: DOOR — MALFUNCTIONED (EMERGENCY EXIT) · airframe 5,691 hrs · 4,000 cycles
CREW REPORTED EMERGENCY DOOR RT OPEN MSG ON EICAS IN FLIGHT AT FL320, MSG WENT AWAY AT FL180. MAINTENANCE REMOVED, INSPECTED, AND RE-INSTALLED THE RIGHT OVERWING EXIT DOOR PER EMB AMM, OPS CHECK GOOD.
Part: MECHANISM — LACK OF LUBE (L1 DOOR) · airframe 5,598 hrs · 3,957 cycles
CREW REPORTED L-1 DOOR VENT FLAP INOP. MAINTENANCE INSPECTED RIG OF L-1 DOOR VENT FLAP AND LUBED ALL MECHANICAL PARTS PER EMB AMM, AND REPORTED THE DOOR WAS OPERATING NORMALLY. A/C WAS THEN RETURNED TO SERVICE.
Part: ACM — MALFUNCTIONED (NR 2) · airframe 5,566 hrs · 3,939 cycles
CREW REPORTED SMOKE IN CABIN DURING CLIMB OUT OF MKE AND RETURNED TO FIELD AND LANDED AT MKE WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND ACM NR 2 TO BE AT FAULT, PLACED ON MEL 21-51-00-1, AND THE A/C WAS THEN RETURNED TO SERVICE.
Part: SLIDE — DEPLOYED (L1 DOOR) · airframe 4,687 hrs · 3,462 cycles
MX REPORTED THE L1 EMERGENCY EVAC SLIDE DEPLOYED AT THE GATE. MAINTENANCE REMOVED AND REPLACED THE L-1 SLIDE PER EMB AMM. A/C WAS RETURNED TO SERVICE.
Part: INDICATION SYS — MALFUNCTIONED (L1 DOOR) · airframe 4,580 hrs · 3,414 cycles
CREW REPORTED L-1 DOOR OPEN INDICATION SHOWING OPEN WHILE IN FLIGHT. MAINTENANCE TROUBLESHOT AND PLACED THE L-1 DOOR POSITION INDICATION ON MEL 52-70-001. THE AIRCRAFT WAS THEN RETURNED TO SERVICE.