N807HC

Part: AOA — FAULTED (LEFT) · airframe 29,293 hrs · 30,620 cycles

FLIGHT 1700, AIR TURNBACK, ON TAKEOFF, THE MASTER CAUTION, FLIGHT CTR ON CAS AND STICK PUSHER SHAKER FAULT LIGHTS ILLUMINATED. AIRCRAFT WAS RETURNED TO DEPARTURE, NO EMERGENCY WAS DECLARED. LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED EXTENSIVE TROUBLESHOOTING, REPLACED THE L/H AOA PROBE. OPS CHECKS GOOD. SUCCESSFUL OCF PERFORMED.

Part: PROXIMITY SWITCH — FAULTY (STICK SHAKER) · airframe 29,208 hrs · 30,500 cycles

FLIGHT 1700, HNL-ITO AIR TURNBACK/APPROX. 14:15 DISCREPANCY: AFTER GEAR WAS RETRACTED, FLIGHT CONTROL LIGHT ON CAP AND STICK SHAKER LIGHTS ILLUMINATED. AIRCRAFT WAS RETURNED TO HNL. NO EMERGENCY DECLARED. LANDED WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION: MAINTENANCE REPLACED THE PROXIMITY SWITCH. AIRCRAFT RETURNED TO SERVICE.

Part: AOA — FAULTY · airframe 29,208 hrs · 30,499 cycles

FLIGHT 1700, HNL-ITO/AIR TURNBACK AT APPROX.1045Z DISCREPANCY: FLIGHT CONTROL LIGHT ON CAP AND STICK SHAKER FAULT LIGHTS ILLUMINATED AFTER TAKEOFF. AIRCRAFT RETURNED TO HNL. NO EMERGENCY DECLARED. LANDED WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION: MAINTENANCE REPLACED THE CAPT AOA PROBE. OPS CHECKS GOOD.

Part: AOA — FAULTY (FIRST OFFICER'S) · airframe 29,205 hrs · 30,494 cycles

FLIGHT 1700, HNL-ITO/ AIR TURNBACK DISCREPANCY: ON CLIMB OUT, THE STICK PUSHER/SHAKER FAULT LIGHT ILLUMINATED IN ADDITION TO THE MASTER CAUTION LIGHT. THE AIRCRAFT WAS RETURNED TO HNL. NO EMERGENCY DECLARED. LANDED WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION: MAINTENANCE REPLACED THE FO AOA PROBE. PERFORMED OPS TEST IN FLIGHT CONFIG. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,113 hrs · 30,384 cycles

WO 187945 NR 200099 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE LT UPPER SKIN PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 41-42, STRINGERS 3L-4L. CORRECTIVE ACTION: REPAIRED PER SRAS ES-0089130-01...13814 DATED 12/4/2018.

Part: PANEL — CORRODED (LT OVERWING) · corrosion level 2 · airframe 29,113 hrs · 30,384 cycles

WO 187945 NR 500032 HEAVY CHECK COE/MINOR REPAIR: LEVEL 2 CORROSION ON LH OVERWING FUEL PANEL 523GT. CORRECTIVE ACTION: REPLACED WITH OEM PART.

Part: PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 29,113 hrs · 30,384 cycles

HEAVY CHECK COE/MINOR REPAIR: LEVEL 2 CORROSION ON RT OVERWING FUEL PANEL 623GT. REPLACED WITH OEM PART.

Part: HINGE FITTING — CORRODED (LT AILERON) · corrosion level 2 · airframe 29,113 hrs · 30,384 cycles

HEAVY CHECK COE/MINOR REPAIR: LEVEL 2 CORROSION ON LT WING INBOARD AILERON HINGE FITTING. REPLACED FITTING WITH OEM PART.

Part: STRINGER — CORRODED (FRAME 29) · corrosion level 2 · airframe 29,113 hrs · 30,384 cycles

WO 187945 NR 100012 HEAVY CHECK COE/MINOR REPAIR: LEVEL 2 CORROSION ON FRAME 29 STRINGER SPLICE 17R. CORRECTIVE ACTION: REPLACED WITH OEM STRINGER.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 29,113 hrs · 30,384 cycles

LEFT HORIZONTAL STAB LEADING EDGE HAS CORROSION. REPLACED LEADING EDGE WITH NEW.

Part: FLOORBEAM — CORRODED (FRAME 17) · corrosion level 2 · airframe 29,113 hrs · 30,384 cycles

FLOORBEAM, FRAME 17 HAS CORROSION. REPAIRED IAW 0043023.

Part: FLOORBEAM — CORRODED (FRAME 15) · corrosion level 2 · airframe 29,113 hrs · 30,384 cycles

FLOORBEAM 15 HAS CORROSION BETWEEN CENTER SEAT TRACKS. REPAIRED IAW SRM 530000-300-852-A01.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 29,113 hrs · 30,384 cycles

FWD CARGO DOOR, FWD LOWER CORNER, INTERNAL SURFACE OF OUTER SKIN HAS MULTIPLE AREAS WITH CRACKS. REPAIRED IAW SRAS S523R0080.

Part: PAN — CORRODED (CARGO) · corrosion level 2 · airframe 29,113 hrs · 30,384 cycles

FWD CARGO DOOR HAS CORROSION AT INBOARD LOWER STRUCTURE. REPLACED LOWER PAN WITH OEM PART.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,105 hrs · 30,384 cycles

BRIDGING CHECK COE & MINOR REPAIR. RT SERVICE DOOR THRESHOLD DOUBLER HAS LEVEL 2 CORROSION. REPLACED DOUBLER WITH OEM PART.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,105 hrs · 30,384 cycles

BRIDGING CHECK COE & MINOR REPAIR. BRACKET AFT OF FRAME 37, HAS LEVEL 2 CORROSION AT THRESHOLD ATTACH LOCATION. REPLACED BRACKET WITH OEM PART.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,105 hrs · 30,384 cycles

BRIDGING CHECK COE & MINOR REPAIR. RT SERVICE DOOR THRESHOLD, DRAIN CHANNEL HAS LEVEL 2 CORROSION. REPLACED DRAIN CHANNEL WITH OEM.

Part: THRESHOLD — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,113 hrs · 30,384 cycles

LEFT PASSENGER DOOR THRESHOLD, DOUBLER AND DRAIN CHANNEL HAVE CORROSION. REPLACED THRESHOLD WITH OEM PART.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,105 hrs · 30,382 cycles

HEAVY CHECK COE & MAJOR REPAIR. FRAME 39 FWD DOUBLER AT LEVEL OF SERVICE DOOR, THRESHOLD HAS LEVEL 2 CORROSION. REPAIR IAW SRAS CE 4529 15 9581 DATED 10 1 15.

Part: CLOSEOUT PANEL — CORRODED (FRAMES 35-36) · corrosion level 2 · airframe 29,113 hrs · 30,384 cycles

RIGHT OUTBOARD SEAT TRACK CLOSE OUT PANEL FRAMES 35-36 HAS CORROSION. REPLACED THE CLOSEOUT PANEL.

Part: FAILSAFE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,105 hrs · 30,382 cycles

HEAVY CHECK COE & MINOR REPAIR. FRAME 14 FAIL SAFE HAS LEVEL 2 CORROSION. STRINGER 20L - 21L. REPAIR IAW SRAS CE-4472 15 9584 DATED 9 17 2015.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,105 hrs · 30,382 cycles

BRIDGING CHECK COE & MAJOR REPAIR. LT CREASE BEAM OUTER CHORD HAS LEVEL 2 CORROSION, AT FRAMES 39 - 40. REPAIR IAW SRAS CE 4530 15 9582 DATED 10 5 15.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,105 hrs · 30,382 cycles

HEAVY CHECK COE & MAJOR REPAIR. FRAME 13 HAS LEVEL 2 CORROSION ON THE AFT SIDE, BETWEEN STRINGER 19L - 20L. REPAIRED IAW SRAS ES-4388 15 9551 DATED 9 21 15.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,105 hrs · 30,382 cycles

BRIDGING CHECK COE & MINOR REPAIR. STRINGER CLIP AT FRAME 13, STRINGER 20 LT, HAS LEVEL 2 CORROSION. REPLACED STRINGER CLIP WITH OEM PART.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,105 hrs · 30,382 cycles

BRIDGING CHECK COE & MINOR REPAIR. STRINGER CLIP AT FRAME 13, STRINGER 20 RT, HAS LEVEL 2 CORROSION. REPLACED STRINGER CLIP WITH OEM PART.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · corrosion level 2 · airframe 29,105 hrs · 30,384 cycles

BRIDGING CHECK COE & MINOR REPAIR. AFT PAX DOOR, FWD SIDE OF VENT DOOR AREA HAS LEVEL 2 CORROSION ON INTERCOSTAL. REPLACED WITH OEM PART.

Part: SPLICE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 29,105 hrs · 30,382 cycles

WO 151753 NR 800007 BRIDGING CHECK COE & MINOR REPAIR. AFT PAX DOOR, UPPER PAN SPLICE ON AFT EDGE HAS LEVEL 2 SURFACE CORROSION. REPLACED SPLICE WITH OEM PART.

Part: FITTING — CORRODED (PAX DOOR) · corrosion level 2 · airframe 29,105 hrs · 30,382 cycles

BRIDGING CHECK COE & MINOR REPAIR. AFT PAX DOOR, FWD SIDE OF VENT DOOR AREA HAS LEVEL 2 CORROSION ON CLIP. REPLACED WITH OEM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · corrosion level 2 · airframe 29,105 hrs · 30,384 cycles

BRIDGING CHECK COE & MINOR REPAIR. AFT PAX DOOR, FWD SIDE OF VENT DOOR AREA HAS LEVEL 2 CORROSION ON INTERCOSTAL. REPLACED WITH OEM PART.

Part: SKIN — GOUGED (LT WING) · airframe 29,113 hrs · 30,384 cycles

LEFT WING UPPER COMPOSITE SKIN GOUGED BETWEEN RIB 25-26. REPAIRED IAW SRAS ES-4416/15.10341.

Part: SPAR — GOUGED (LT WING) · airframe 29,113 hrs · 30,384 cycles

LEFT WING FRONT SPAR UPPER LEADING EDGE FLANGE HAS NUMEROUS GOUGES, RIBS 25-31. REPAIRED IAW SRAS ES-4389/15.10431.

Part: HINGE FITTING — CORRODED (RT AILERON) · corrosion level 2 · airframe 29,105 hrs · 30,384 cycles

BRIDGING CHECK COE & MINOR REPAIR. RT AILERON OTBD HINGE FITTING IS EXFOLIATED AT THE GROUNDING CONNECTION POINT. REPLACED WITH OEM PART.