N165HQ

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,165 hrs · 7,836 cycles

CREW RECEIVED AN EMERGENCY LIGHT BATTERY FAULT MESSAGE. MAINTENANCE R & R MID CABIN RT EMERGENCY POWER PACK IAW AMM AND OPS CHECKED GOOD.

Part: FLASHLIGHT — MISSING (COCKPIT) · airframe 11,474 hrs · 7,154 cycles

CREW REPORTED THAT THE CAPTAIN`S FLASHLIGHT WAS MISSING. INSTALLED FLASHLIGHT IAW AMM.

Part: CLAMP — CORRODED (FUEL) · corrosion level 2 · airframe 11,358 hrs · 7,063 cycles

DURING HEAVY CHECK, CORROSION FOUND ON TWO CLAMPS, LT WING IN FUEL PANEL 521EB. R & R CLAMPS IAW AMM 20-10-13.

Part: LINE — CORRODED (FUEL SYS) · corrosion level 2 · airframe 11,358 hrs · 7,063 cycles

DURING HEAVY CHECK, CORROSION FOUND ON FUEL LINES LOCATED IN FUEL PANEL 621BB AREA. R & R FUEL LINES IAW 20-10-03, 20-10-13.

Part: LINE — CORRODED (FUEL SYS) · corrosion level 2 · airframe 11,358 hrs · 7,063 cycles

DURING HEAVY CHECK, CORROSION FOUND ON FUEL LINE UNDER PANEL 621EB. R & R FUEL LINE IAW AMM 20-10-03, 20-10-13.

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 11,358 hrs · 7,063 cycles

DURING HEAVY CHECK, A CRACK WAS FOUND ON BULKHEAD JUST AFT OF MLG WHEEL WELL. REPAIRED BULKHEAD IAW SRM 53-04-02, REPAIR 51.

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,358 hrs · 7,063 cycles

DURING HEAVY CHECK, WASTE BOX DOUBLER CORRODED. COMPLIED WITH SB 190-53-0056.

Part: PAN — CRACKED (CABIN SEAT) · airframe 11,358 hrs · 7,063 cycles

DURING HEAVY CHECK, FOUND SEAT PANS CRACKED. MX R & R SEAT PANS.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 11,358 hrs · 7,063 cycles

DURING HEAVY CHECK, RT CENTER SEAT TRACK HAS SIGNS OF CORROSION IN THE AREA OF FRAME 13. MAINTENANCE R & R RT CENTER SEAT TRACK IAW SRM 51-41-01, 51-41-02, 51-43-01, 51-43-02, 51-23-06

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 11,358 hrs · 7,063 cycles

DURING HEAVY CHECK, FOUND RT FLOOR SUPPORT BETWEEN FRAMES 12-14 CORRODED. R & R FLOOR SUPPORT IAW SRM 51-40-02, 51-40-04, 51-41-02, 51-43-04.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 11,358 hrs · 7,063 cycles

DURING HEAVY CHECK, RT FLOOR SUPPORT BETWEEN FRAMES 18 - 21, HAS SIGNS OF CORROSION. MX R & R RT FLOOR SUPPORT IAW SRM 51-40-02, 51-40-04, 51-41-02, 51-43-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 11,358 hrs · 7,063 cycles

DURING HEAVY CHECK, RT FLOOR REINFORCEMENT ON FRAME 84 HAS SIGNS OF CORROSION. MX REMOVED AND MATCH DRILLED INSTALLED RT FLOOR REINFORCEMENT ON FRAME 84 IAW SRM 51-40-02, 51-41-01. INSTALLED AND REMOVED IAW SWPM 20-67-00. PN 190652887-001 FLOOR SUPPORT. ACFT REMAINS UNTIL HEAVY CHECK IS COMPLETED.

Part: SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 11,358 hrs · 7,063 cycles

DURING HEAVY CHECK, LEFT SILL BETWEEN FRAMES 12-16 HAS SIGNS OF CORROSION. MX R & R LT SILL BETWEEN FRAMES 12-16 IAW SRM 51-40-02, 51-43-04, 51-41-02. PN 170-03275-005, SILL. AIRCRAFT REMAINS UNTIL HEAVY CHECK IS COMPLETED.

Part: SEAT TRACK — CORRODED (FRAMES 86-87) · corrosion level 2 · airframe 11,358 hrs · 7,063 cycles

DURING HEAVY CHECK, LEFT SEAT TRACK EXTENSION BETWEEN FRAMES 86-87 HAS SIGNS OF CORROSION. MAINTENANCE R & R SEAT TRACK IAW SRM 51-41-01, & 51-43-01.

Part: SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,358 hrs · 7,063 cycles

DURING HEAVY CHECK, OTBD SPLICE PLATE RT SHEAR PANEL BETWEEN FRAMES 87-88 HAS SIGNS OF CORROSION. MX R & R OTBD SPLICE PLATE IAW SRM 51-40-02, 51-42-02.

Part: SEAT TRACK — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 11,358 hrs · 7,063 cycles

DURING HEAVY CHECK, SEAT TRACK HAS SIGNS OF CORROSION FRAMES 85-86. MX R & R SEAT TRACK IAW SRM 51-41-01, 51-43-03.

Part: DOUBLER — CORRODED (FRAME 89) · corrosion level 2 · airframe 11,358 hrs · 7,063 cycles

DURING HEAVY CHECK, RT CENTER FLOOR DOUBLER ON FRAME 89 HAS SIGNS OF CORROSION. MAINTENANCE REMOVED AND INSTALLED DOUBLER IAW SRM 51-40-02, 51-43-01.

Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,358 hrs · 7,063 cycles

DURING HEAVY CHECK, FOUND LT SHEAR PANEL BETWEEN FRAMES 87-88 CORRODED. MX R & R SHEAR PANEL IAW SRM 51-42-01, 51-42-02.

Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,358 hrs · 7,063 cycles

DURING HEAVY CHECK, FOUND CENTER FLOOR SHEAR PANEL BETWEEN FRAMES 87-88 CORRODED. MAINTENANCE R & R CENTER FLOOR SHEAR PANEL IAW SRM 51-42-01.

Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,358 hrs · 7,063 cycles

DURING HEAVY CHECK, RT SHEAR PLATE BETWEEN FRAMES 87-88 HAS SIGNS OF CORROSION. R & R RT SHEAR PLATE BETWEEN FRAMES 87-88 IAW SRM 51-40-02, 51-42-01, 51-43-03.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,358 hrs · 7,063 cycles

DURING HEAVY CHECK, RT FLOOR SUPPORT AFT OF R2 DOOR HAS SIGNS OF CORROSION. MAINTENANCE R & R FLOOR SUPPORT IAW SRM 51-40-02, 51-43-01.

Part: NUT — LOOSE (HYD LINE) · airframe 11,358 hrs · 7,063 cycles

DURING HEAVY CHECK, RT WING HYDRAULIC LINE JAM NUT LOOSE ON SPAR 3 WITH POSSIBLE DAMAGE TO SPAR. MAINTENANCE REWORKED CHAFED AREA .025 MATERIAL LOSS AN ADDITIONAL WASHER WAS ADDED TO FWD SIDE OF SPAR.

Part: SEAT TRACK — CORRODED (FRAMES 13-18) · corrosion level 2 · airframe 11,358 hrs · 7,063 cycles

DURING HEAVY CHECK WAS REPORTED LEFT CENTER SEAT TRACK HAS SIGNS OF CORROSION FRAMES 13, 18. MAINTENANCE R & R LEFT CENTER SEAT TRACK IAW SRM 51-40-02, 51-40-01, 51-41-02, 51-43-03, 51-23-06 AND 20-67-00.

Part: DOUBLER — CORRODED (FRAME 90) · corrosion level 2 · airframe 11,358 hrs · 7,063 cycles

DURING HEAVY CHECK, DOUBLER HAS SIGNS OF CORROSION ON FRAME 90. MAINTENANCE R & R DOUBLER IAW SRM 51-41-02.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 11,358 hrs · 7,063 cycles

ALL EMERGENCY LIGHTS ARE DIRTY AND CRACKED. REPLACED CRACKED COVERS IAW AMM. OPS CHECKED GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 10,931 hrs · 6,711 cycles

CREW REPORTED THAT THE EMERGENCY LIGHT STRIPS NEXT TO BOTH SEAT 1D AND IN FRONT OF THE FWD CLOSET APPEAR TO BE DAMAGED. MX INSTALLED SERVICEABLE EMERGENCY LIGHT STRIPS IAW AMM AND OPS CHECKED GOOD.

Part: DOOR FRAME — DIRTY (EMERGENCY EXIT) · airframe 10,577 hrs · 6,396 cycles

CREW REPORTED LOUD WHISTLING NOISE COMING FROM THE LT EMERGENCY OVERWING EXIT DURING FLIGHT. AN EMERGENCY WAS NOT DECLARED AND PLANE LANDED WITHOUT INCIDENT. MX REMOVED LT OVERWING EXIT HATCH, INSPECTED SEAL AND NO DEFECTS FOUND. MX FOUND DEBRIS IN THE DOOR FRAME AREA, REMOVED DEBRIS AND RESECURED HATCH IAW AMM. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 10,224 hrs · 6,090 cycles

CREW REPORTED THAT THE FIRST OFFICERS FLASHLIGHT WAS NOT CHARGING. MAINTENANCE REMOVED AND REPLACED FIRST OFFICERS FLASHLIGHT, WOULD NOT ACCEPT CHARGE. MAINTENANCE REPLACED BATTERY IN NEW FLASHLIGHT ASSEMBLY PER EMB AMM AND OPS CHECKED GOOD.

Part: SLIDE — PARTIAL DEPLOY (L1 DOOR) · airframe 9,389 hrs · 5,393 cycles

CREW REPORTED THAT THE F/A OPENED THE L1 DOOR WHILE IT WAS STILL ARMED AND PARTIALLY BLEW THE EMERGENCY SLIDE. MAINTENANCE REPLACED THE SLIDE ASSY PER EMB AMM.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 9,133 hrs · 5,214 cycles

CREW REPORTED F/O'S FLASHLIGHT DOES NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED FLASHLIGHT PER AMM 33-51-0.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 8,564 hrs · 4,786 cycles

L1 DOOR SLIDE PARTIALLY DEPLOYED WHEN OPS OPENED THE DOOR AT THE JETBRIDGE.

Part: FLAP — OUT OF ADJUST (R1 DOOR) · airframe 8,178 hrs · 4,509 cycles

CREW REPORTED R1 VENT FLAP INOP. MAINTENANCE ADJUSTED AND RIGGED FLAPPER DOOR PER EMB AMM.

Part: HYDRAULIC LINE — CRACKED (LT PYLON) · airframe 7,292 hrs · 3,938 cycles

CREW REPORTED THE NR 1 HYDRAULIC SYSTEM QUANTITY DROPPING FROM 18% TO 4% DURING FLIGHT. CREW DECLARED AN EMERGENCY AND DIVERTED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A HYDRAULIC LINE CRACKED IN THE LEFT PYLON. MAINTENANCE REPLACED HYDRAULIC LINE IAW EMB AMM, OPS AND LEAK CHECK GOOD.

Part: SLIDE — UNWANTED DEPLOY (R2 DOOR) · airframe 6,406 hrs · 3,394 cycles

GROUND CREW INADVERTENTLY DEPLOYED R2 DOOR ESCAPE SLIDE. SLIDE DEPLOYED NORMALLY. MAINTENANCE REMOVED AND REPLACED R2 DOOR ESCAPE SLIDE PER EMB AMM, OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 5,671 hrs · 2,937 cycles

CREW REPORTED LT DOOR EMERGENCY OPEN EICAS MESSAGE AFTER TAKEOFF. AN EMERGENCY WASN'T DECLARED, AND THE A/C LANDED WITHOUT INCIDENT AT MCI. MAINTENANCE PERFORMED OPS CHECK OF LT EMERG EXIT DOOR PER EMB AMM, OPS CHECK GOOD.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 5,373 hrs · 2,784 cycles

CREW REPORTED FWD OVEN WAS SMOKING WHEN USED IN FLIGHT, NO EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT AT DEN. MAINTENANCE PLACED ITEM ON NEF 25-92-008.

Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 4,042 hrs · 2,124 cycles

CREW REPORTED TWICE AFTER POWER UP EMERGENCY LIGHTS CAME ON AND EMERGENCY LIGHT BATTERY FAULT ON EICAS. MX PERFORMED OPS CHECK OF ALL LIGHTS ON FA PANELS PER EMB AMM OPS CHECK NORMAL AC OK FOR SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 4,031 hrs · 2,120 cycles

CREW REPORTED EMERGENCY LIGHTS CAME ON IN FLIGHT. MX PERFORMED OPS CHECK OF LIGHT SWITCHES PER EMB AMM NO DEFECTS NOTED AC OK FOR SERVICE.

Part: PIN — UNSECURE (L1 DOOR) · airframe 3,659 hrs · 1,934 cycles

CREW REPORTED L-1 DOOR WILL NOT OPEN. MX RE-SECURED PIN PER EMB AMM, OPS CHECK GOOD.

Part: DOOR — MALFUNCTIONED (EMERGENCY EXIT) · airframe 3,449 hrs · 1,798 cycles

CREW REPORTED DOOR EMERGENCY RT OPEN OVERWING EXIT EICAS DURING FLIGHT. A/C LANDED AT DEN WITHOUT INCIDENT. MAINTENANCE REMOVED AND RE-INSTALLED RIGHT OVERWING EXIT DOOR NO DEFECTS NOTED, REF EMB 190 AMM 52-21-00.

Part: SENSOR — MALFUNCTIONED (LE SLAT) · airframe 2,350 hrs · 1,124 cycles

CREW RETURNED TO FIELD AT DEN DUE TO SLAT FAIL DURING CLIMB, NO EMERGENCY DECLARED. MAINTENANCE REMOVED AND REPLACED RIGHT O/B 3/4 SKEW SENSOR PER EMB AMM, AND A/C WAS RETURNED TO SERVICE.

Part: A/C PACK — FAULTY (AC BAY) · airframe 1,922 hrs · 869 cycles

CREW REPORTED ELECTRICAL SMELL AT THE REAR OF THE CABIN, DECLARED AN EMERGENCY AND RETURNED TO OMA WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT PER EMB AMM AND DETERMINED PACK NR 2 WAS AT FAULT AND PLACED ON MEL. A/C WAS THEN RETURNED TO SERVICE.

Part: DOOR — OUT OF POSITION (EMERGENCY EXIT) · airframe 744 hrs · 317 cycles

CREW REPORTED AN OVERWING EXIT OPEN LIGHT ON EICAS, RETURNED TO FIELD AT DEN AND LANDED WITHOUT INCIDENT, EMERGENCY WASN'T DECLARED. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT TO TROUBLESHOOT. MAINTENANCE FOUND THAT ONE OF THE OVERWING EXIT DOOR WAS PARTIALLY OUT OF THE UPPER AFT ROLLER, MAINTENANCE RE-INSTALLED THE DOOR, VISUALLY VERIFIED DOOR WAS ENGAGED, AND PRESSURIZED THE A/C TO 8.0 NO LEAKS NOTED. A/C WAS THEN RETURNED BACK INTO SERVICE.