N163HQ

Part: PIN — DETACHED (R1 GIRT BAR) · airframe 11,798 hrs · 7,257 cycles

CREW REPORTED THAT THE R1 DOOR SLIDE WOULD NOT ARM AND THE LEVER IS NOT MOVING. MAINTENANCE INSPECTED AND FOUND PIN HAD MIGRATED OUT OF GIRT BAR. MAINTENANCE REINSTALLED PIN IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.

Part: ROLL PIN — DAMAGED (SERVICE DOOR) · airframe 11,582 hrs · 7,069 cycles

CREW RECEIVED A FWD SERVICE DOOR OPEN MESSAGE. AN EMERGENCY WAS NOT DECLARED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED INDICATION TAB ROLL PIN IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.

Part: FIREWALL — CRACKED (APU BAY) · airframe 11,573 hrs · 7,067 cycles

DURING HEAVY CHECK, RT APU FIRE WALL CRACKED AT THE BEND. MX R & R FIREWALL IAW AMM 53-31-21, NO DEFECTS NOTED.

Part: DOUBLER — CORRODED (FLOOR PANEL) · corrosion level 2 · airframe 11,573 hrs · 7,067 cycles

DURING HEAVY CHECK, LT SIDE FLOOR DOUBLER AT FRAMES 19-20 CORRODED. MX R & R DOUBLER IAW SRM 51-40-02, 57-41-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 11,573 hrs · 7,067 cycles

DURING HEAVY CHECK, LT SEAT TRACK IS CORRODED. MX R & R SEAT TRACK IAW SRM 51-41-02, 51-43-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 11,573 hrs · 7,067 cycles

DURING HEAVY CHECK, SEAT TRACK CORRODED. R & R SEAT TRACK IAW SRM 51-41-01, 51-43-01, 51-43-02, 51-40-02.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 11,573 hrs · 7,067 cycles

DURING HEAVY CHECK, RT SEAT TRACK CORRODED. R & R SEAT TRACK IAW SRM 51-41-01, 51-43-01, 51-43-02, 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 11,573 hrs · 7,067 cycles

DURING HEAVY CHECK, RT SIDE FLOOR SUPPORT CORRODED. MX R & R FLOOR SUPPORT IAW SRM 51-41-01.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 11,573 hrs · 7,067 cycles

DURING HEAVY CHECK, GUSSET OF LT FLOORBEAM AT FRAME 90 IS CORRODED. MAINTENANCE R & R GUSSET IAW SRM 51-41-02.

Part: DOUBLER — CORRODED (FLOOR PANEL) · corrosion level 2 · airframe 11,573 hrs · 7,067 cycles

DURING HEAVY CHECK, LT SIDE FLOOR DOUBLER AT FRAMES 13-16 CORRODED. MX R & R DOUBLER IAW SRM 51-41-02, 51-40-02.

Part: SEAT BACK — CRACKED (COCKPIT) · airframe 11,573 hrs · 7,067 cycles

DURING HEAVY CHECK, METAL BACK SUPPORT CRACKED ON CO PILOTS SEAT. MAINTENANCE R & R METAL BACK SUPPORT ON CO PILOTS SEAT IAW SRM 51-40-02. PN F0424639 SEAT SHEET METAL.

Part: SEAT BACK — CRACKED (COCKPIT) · airframe 11,573 hrs · 7,067 cycles

DURING HEAVY CHECK, METAL BACK SUPPORT ON PILOTS SEAT CRACKED. MX R & R BACK SUPPORT IAW SRM 51-40-02.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 11,573 hrs · 7,067 cycles

DURING HEAVY CHECK WAS REPORTED GUSSET ON LT FLOORBEAM AT FRAME 90 CORRODED. MX R & R GUSSET IAW SRM 51-41-02.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 11,573 hrs · 7,067 cycles

DURING HEAVY CHECK, GUSSET AT RT FLOORBEAM FRAME 90 IS CORRODED. MX R & R GUSSET IAW SRM 51-41-02.

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 11,573 hrs · 7,067 cycles

DURING HEAVY CHECK, RT SHEAR PLATE BETWEEN FRAMES 87-88 IS CORRODED. MX R & R SHEAR PLATE IAW SRM 51-43-01, 51-42-01.

Part: GUSSET — CORRODED (FRAME 85) · corrosion level 2 · airframe 11,573 hrs · 7,067 cycles

DURING HEAVY CHECK, GUSSET ATTACHED TO LT FLOORBEAM AT FRAME 85 CORRODED. R & R GUSSET IAW SRM 51-42-00.

Part: FLOORBEAM — CORRODED (FRAME 87) · corrosion level 2 · airframe 11,573 hrs · 7,067 cycles

DURING HEAVY CHECK, FLOORBEAM FRAME 87 CORRODED. MX R & R FLOORBEAM IAW SRM 51-41-01, 51-23-06.

Part: GUSSET — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 11,573 hrs · 7,067 cycles

DURING HEAVY CHECK, GUSSET RT FLOOR SUPPORT BETWEEN FRAMES 85-86 CORRODED. R & R GUSSET IAW SRM 551-41-01, 51-43-01.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 11,573 hrs · 7,067 cycles

DURING HEAVY CHECK. GUSSET OF RT FLOORBEAM AT FRAME 90 IS CORRODED. R & R GUSSET IAW SRM 51-41-02.

Part: SHEAR PLATE — CORRODED (FRAME 87) · corrosion level 2 · airframe 11,573 hrs · 7,067 cycles

DURING HEAVY CHECK, LT SHEAR PLATE FRAME 87 IS CORRODED. MX R & R SHEAR PLATE IAW SRM 51-42-01.

Part: CONTROLLER — FAILED (HORIZONTAL STAB) · airframe 11,568 hrs · 7,063 cycles

FL 220, CREW RECEIVED STAB LOCK FAULT MESSAGE AND PITCH TRIM INDICATION WAS REPLACED BY AMBER DASHES. CREW RAN THE QRH PROCEDURES. DIVERTED, AND ATC DECLARED AN EMERGENCY. DURING DESCENT "STAB LOCK" FAULT MESSAGE WENT AWAY, AMBER DASHES REMAINED. LANDED AND TAXIED TO GATE WITHOUT INCIDENT. MAINTENANCE R & R THE HS-ACE IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.

Part: DOOR — UNSECURE (EMERGENCY EXIT) · airframe 11,481 hrs · 6,989 cycles

CREW RECEIVED A EMERGENCY DOOR OPEN MESSAGE. AN EMERGENCY WAS NOT DECLARED AND LANDED WITHOUT INCIDENT. MAINTENANCE SECURED THE LT OVERWING EMERGENCY EXIT DOOR IAW AMM WITH NO DEFECTS NOTED. ACFT IS GOOD FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 8,783 hrs · 4,878 cycles

DURING BI WEEKLY FOUND L1 DOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT (BATTERY) REF EMB 190 AMM 33-50-01. OPS CHECK GOOD.

Part: ACM — FAILED (AC BAY) · airframe 6,100 hrs · 3,192 cycles

CREW REPORTED SMOKE SMELL IN CABIN AND COCKPIT ON FINAL INTO OKC. AN EMERGENCY WAS NOT DECLARED, AND THE A/C LANDED WITHOUT INCIDENT INTO OKC. MAINTENANCE REMOVED AND REPLACED LT ACM AND LT HEAT EXCHANGER PER EMB AMM. A/C WAS THEN RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 6,100 hrs · 3,192 cycles

CREW REPORTED SULPHER SMELL ON FINAL IN COCKPIT ON APPROACH IN DEN. AN EMERGENCY WAS NOT DECLARED, AND THE AIRCRAFT LANDED WITHOUT INCIDENT AT DEN. MAINTENANCE PERFORMED OPS CHECK OF PACK 1 PER EMB AMM AND REPORTED NO SMELLS PRESENT AT THAT TIME. A/C WAS THEN RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 6,084 hrs · 3,179 cycles

CREW REPORTED BURNING ODOR IN CABIN AND FLIGHT DECK ON DESCENT INTO MKE. AN EMERGENCY WAS NOT DECLARED, AND THE A/C LANDED WITHOUT INCIDENT AT MKE. MAINTENANCE TROUBLESHOT PER EMB AMM AND PLACED PACK 2 ON MEL 21-51-00-1. DEN MAINTENANCE PERFORMED OPERATIONAL CHECK OF PACK 2 PER EMB AMM, AND WAS UNABLE TO DUPLICATE ANY ODORS, AND CLEARED MEL 21-51-00-1.

Part: BATTERY — DEFECTIVE (CABIN) · airframe 6,002 hrs · 3,140 cycles

LEFT EXIT ROW EMERGENCY EXIT SIGN INOP. MAINTENANCE FOUND EMERGENCY BATTERY DEFECTIVE AND REPLACED IAW EMB AMM, OPS CHECK GOOD.

Part: IRU — FAILED (NR 1) · airframe 2,428 hrs · 1,162 cycles

CREW REPORTED IRU 1 FAIL IN FLIGHT, DIVERTED TO DEN AND LANDED WITHOUT INCIDENT, NO EMERGENCY DECLARED. MAINTENANCE REMOVED AND REPLACED IRU 1 PER EMB AMM, A/C WAS THEN RELEASED INTO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 2,340 hrs · 1,111 cycles

EMERGENCY OVERHEAD LIGHT INOP DURING TEST. MAINTENANCE REMOVED AND REPLACED ELPU NR 2 PER EMB AMM, A/C WAS THEN RETURNED TO SERVICE.

Part: POWER UNIT — INOPERATIVE (CABIN) · airframe 1,367 hrs · 628 cycles

MAINTENANCE REMOVED AND REPLACED THE LT NR 1 EMERGENCY LIGHT POWER UNIT PER EMB AMM, DUE TO EMERGENCY LIGHTS BEING INOP.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 1,081 hrs · 484 cycles

CREW RETURNED TO FIELD AFTER TAKEOFF FROM DEN DUE TO LT OVERWING EXIT OPEN INDICATIONS. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. MAINTENANCE OPENED AND CLOSED THE LT OVERWING EXIT DOOR, VERIFIED DOOR INDICATIONS WERE GREEN AND NORMAL, OPS CHECK GOOD PER EMB AMM. A/C WAS THEN RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (OVERWING EXIT) · airframe 1,081 hrs · 484 cycles

CREW RECEIVED LT OVERWING EXIT INDICATION RIGHT AFTER TAKEOFF. CREW RETURNED TO FIELD AT DEN AND LANDED WITHOUT INCIDENT. MX INSPECTED THE DOOR PER AMM AND NO DEFECTS WERE NOTED. A/C WAS THEN RELEASED BACK INTO SERVICE.

Part: MECHANISM — OUT OF ADJUST (ESCAPE HATCH) · airframe 43 hrs · 23 cycles

CREW RECEIVED AN OPEN OVERWING INDICATION ON EICAS, WHILE FOLLOWING THE QRH CREW DECLARED EMERGENCY AND RTF, LANDED AT LAX WITHOUT INCIDENT. REPUBLIC AIRLINES ISSUED AN ENGINEERING ORDER TO ADJUST THE ESCAPE HATCH DOOR LOCK MECHANISM, MAINTENANCE C/W THIS ENGINEERING INSTRUCTION AND A/C WAS RELEASED BACK INTO SERVICE.