N805HC

Part: CIRCUIT BREAKER — TRIPPED (BLUE HYD SYSTEM) · airframe 25,144 hrs · 33,341 cycles

FLIGHT 672, AIR TURNBACK, DURING CLIMB OUT, NO BLUE SYSTEM HYDRAULIC PRESSURE. CREW ELECTED TO RETURN TO DEPARTURE. EMERGENCY DECLARED. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED PRESSURIZATION OF HYDRAULIC SYSTEMS. NO DISCREPANCIES. FOUND CIRCUIT BREAKER OPEN. CLOSED CIRCUIT BREAKER. OPS CHECKS GOOD.

Part: TERMINAL — DAMAGED (STARTER/GEN) · airframe 24,320 hrs · 31,150 cycles

FLIGHT 612, ENROUTE HNL-LNY/AIR TURNBACK. MULTIPLE ELECTRICAL FAILURES IN FLIGHT. EADI, EHSI, AIR DATA INSTRUMENTS, MC AND MW INDICATIONS, DEPRESSURIZATION/DECOOLING. AIRCRAFT WAS RETURNED TO HNL, NO EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. AFTER EXTENSIVE TROUBLESHOOTING, MAINTENANCE REPLACED WIRE TERMINALS, LT STARTER/GENERATOR, REPAIRED MULTIPLE WIRE TERMINALS FOR STARTER/GEN AND CHECKED CIRCUITS FOR SHORTAGES. NO DEFECTS NOTED. OCF PASSED. AIRCRAFT RETURNED TO SERVICE.

Part: FIREWALL — CRACKED (RT NACELLE) · airframe 24,272 hrs · 31,074 cycles

RT ENGINE UPPER FIREWALL AFT OUTBOARD AREA WAS CRACKED. REPAIRED IAW ES-3628/18.13303.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 24,272 hrs · 31,074 cycles

COPILOT SIDE WINDOW LOWER FRAME CRACKED AT UPPER FWD LOCK FASTENER. REPAIRED IAW S531R5004.13332. MAJOR REPAIR

Part: RIB — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 24,272 hrs · 31,074 cycles

LEFT HORIZONTAL STAB TIP RIB HAD CORROSION. REPAIRED IAW SRAS ES-4176/18.13322.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 24,272 hrs · 31,074 cycles

CORROSION FOUND ON THE RT HORIZONTAL STAB LEADING EDGE. REPAIRED IAW ES-1735/16.10237 ISSUE B. MAJOR REPAIR.

Part: ANGLE — CRACKED (RUDDER) · airframe 24,272 hrs · 31,074 cycles

STABILIZER RUDDER UPPER FITTING, UPPER HORIZONTAL ANGLE CRACKED. REPLACED.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 24,272 hrs · 31,074 cycles

CORROSION WAS FOUND ON THE LT WING LOWER SKIN AROUND JACK ADAPTOR PLUG. REPAIR THE SKIN IAW ES-3676/18.13306.

Part: SEAT TRACK — CORRODED (FRAMES 36-38) · corrosion level 2 · airframe 24,272 hrs · 31,074 cycles

CABIN ENTRANCE SEAT TRACK BETWEEN FRAMES 36-38 HAD CORROSION. THE SEAT TRACK WAS REPLACED WITH NEW.

Part: CRANK ASSY — CORRODED (PAX DOOR) · corrosion level 2 · airframe 24,272 hrs · 31,074 cycles

PASSENGER DOOR EXTERNAL HANDLE CRANK HAD CORROSION. REPLACED THE DOOR CRANK.

Part: SKIN — DAMAGED (ZONE 100) · airframe 24,272 hrs · 31,074 cycles

RIGHT LOWER LOBE, AFT PANEL WAS DAMAGED AT THE DC GROUND CONNECTION. REPAIRED THE SKIN ES-4648/15.13319.

Part: FITTING — CORRODED (FRAME 8) · corrosion level 2 · airframe 24,272 hrs · 31,074 cycles

CORROSION AND ELONGATED HOLE IN THE FITTING OF THE RT COCKPIT FRAME 8 AT THE SIDE WINDOW UPPER SILL. REPAIRED IAW ES-4174/18.13325.

Part: FITTING — DAMAGED (LT ENG MOUNT) · airframe 24,272 hrs · 31,074 cycles

LT ENGINE INBOARD AFT MOUNT FITTING AT JUNCTION OF TUBES 1 & 2 WAS DAMAGED. REPAIED IAW ES-3657/18.13301.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 24,272 hrs · 31,074 cycles

CORROSION FOUND ON THE RT WING LOWER SKIN AROUND JACK ADAPTOR PLUG. REPAIRED IAW ES-3668/18.13300.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 24,272 hrs · 31,074 cycles

RIGHT WING LOWER SKIN HAD CORROSION BETWEEN RIBS 4 - 5, AROUND WATER DRAIN. REPAIRED IAW ES-3693/18.13304.

Part: FITTING — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 24,272 hrs · 31,074 cycles

LEFT OUTBOARD FLAP, INBOARD BEAM SUPPORT FITTING HAD CORROSION. FLAP BEAM SUPPORT FITTING WAS REPLACED.

Part: BELLCRANK — CORRODED (LT WING) · corrosion level 2 · airframe 24,272 hrs · 31,074 cycles

LT WING REAR SPAR BELLCRANK HAD CORROSION AT RIB 21. BELLCRANK REPLACED.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 24,272 hrs · 31,074 cycles

CORROSION WAS FOUND ON THE RT WING ACCESS PANEL 622FT BETWEEN RIBS 22-23. REPAIRED IAW CE-1744/16.0211 ISSUE B.

Part: CONNECTOR — DIRTY (FUEL TANK) · airframe 23,740 hrs · 29,691 cycles

ABORTED TAKEOFF DUE TO A FUEL CCAS LIGHT ILLUMINATED BETWEEN 80-90 KTS. MAINTENANCE TROUBLESHOT AND SUMPED THE FUEL TANKS, CHECKED AND CLEANED ALL FUEL PROBE CONNECTORS IN FLAP WELL. CHECKED GOOD.

Part: SEAT — MALFUNCTIONED (COCKPIT) · airframe 23,091 hrs · 27,979 cycles

FLIGHT 651, JHM-HNL: UNCOMMANDED MOVEMENT OF CAPTAIN SEAT TO THE FULL AFT POSITION DURING TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND POWER LEVERS REDUCED TO GROUND IDLE. THE FIRST OFFICER TOOK CONTROL OF THE AIRCRAFT, WHICH WAS TAXIED OFF THE RUNWAY AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE CAPTAIN SEAT. CHECKS GOOD FOR SECURITY AND OPERATION.

Part: CONTROL SWITCH — FAULTED (TE FLAPS SYS) · airframe 22,899 hrs · 27,458 cycles

AIR TURNBACK DUE TO A FLAP OVERSPEED WARNING FOLLOWED BY A FAILED ATTEMPT TO CYCLE THE FLAP HANDLE FROM THE 15 DEGREE POSITION. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT, NO EMERGENCY DECLARED. MAINTENANCE REPLACED THE FLAP CONTROL SWITCH. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (HYD SYSTEM) · airframe 22,730 hrs · 26,992 cycles

FLIGHT 612, ENROUTE, AIR TURNBACK, HYDRAULIC BLUE SYSTEM LOW LEVEL AND LOW PRESSURE WARNINGS IN FLIGHT. AFTER CONSULTING THE QRH, THE CREW RETURNED TO DEPARTURE. AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. OPS CHECKED GOOD. VERIFIED HYDRAULIC FLUID LEVEL WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: MODULE — FAILED (PROPELLER) · airframe 22,730 hrs · 26,993 cycles

DURING CLIMB, THE CREW RECEIVED A NR 2 SINGLE CHANNEL CAUTION. CREW ELECTED TO RETURN TO DEPARTURE. NO EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENACE REPLACED THE PROPELLER VALVE MODULE. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: GENERATOR — FAILED · airframe 22,706 hrs · 26,929 cycles

CREW RECEIVED A NR 1 ACW FAULT DURING CLIMB OUT. ELECTED TO RETURN TO DEPARTURE, NO EMERGENCY DECLARED. REPLACED THE NR 1 ACW GENERATOR.

Part: AHRS — MALFUNCTIONED · airframe 22,008 hrs · 25,206 cycles

FLT 610, ENROUTE, EFIS COMP ATTITUDE ON CAPTAIN`S SIDE DURING CLIMB AFTER TAKEOFF. CREW ELECTED TO RETURN TO DEPARTURE. NO EMERGENCY DECLARED. LANDED AIRCRAFT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE AHRS. OPS TESTED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CORRODED (LT HORIZ STAB) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MAJOR REPAIR. LT HORIZONTAL STABILIZER LE 331 HAS LEVEL 2 CORROSION ON UPPER & LOWER INNER MATING SURFACES. REPAIR IAW SRAS ES 1754/16... 10238 DATED 5 11 2016.

Part: SKIN — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MAJOR REPAIR. RT HORIZONTAL STABILIZER LE HAS LEVEL 2 CORROSION ON UPPER & LOWER INNER MATING SURFACES. REPAIR PER SRAS ES 1735 16 10237 DATED 5 11 2016.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MAJOR REPAIR. FWD CTR FUSELAGE CROWN, SKIN PANEL ADF 1 ANTENNA LOCATION, MOUNTING HOLES ARE DEFORMED. REPAIR PER CE 1914 16 10212 DATED 5 10 2016.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE MAJOR REPAIR. FWD CTR FUSELAGE CROWN, SKIN PANEL ADF2 ANTENNA LOCATION, MOUNTING HOLES ARE DEFORMED. REPAIR IAW CE 914 16 10212 DATED 5 10 16.

Part: SPLICE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. AFT PAX DOOR, AIRSTAIR SPLICE ANGLE HAS LEVEL 2 CORROSION. REPLACED SPLICE ANGLE WITH OEM PART.

Part: BRACKET — CORRODED (PAX DOOR) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. LT PAX DOOR HINGE COVER BRACKET HAS LEVEL 2 CORROSION. REPLACED BRACKET WITH OEM PART.

Part: LANDING — DAMAGED (RT WING) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MAJOR REPAIR. RT UPPER WING INBD REMOVABLE PANEL LANDING FOR ACCESS PANEL 622CT HAS FRETTING LEVEL 2. REPAIR IAW SRAS CE 1721 16 10167 DATED 5 10 16.

Part: ATTACH ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. LT PAX DOOR, LOWER AIRSTAIR ATTACH ANGLE HAS LEVEL 2 CORROSION. REPLACED ANGLE WITH OEM PART.

Part: BRACKET — CORRODED (PAX DOOR) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. LT PAX DOOR HINGE COVER BRACKET HAS LEVEL 2 CORROSION. REPLACED BRACKET WITH OEM PART.

Part: COVER PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. LT AOA PROBE COVER PANEL HAS LEVEL 2 CORROSION. REPLACED COVER PLATE WITH OEM PART.

Part: COVER PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. RT AOA PROBE COVER PANEL HAS LEVEL 2 CORROSION. REPLACED COVER PLATE WITH OEM PART.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MAJOR REPAIR. TAIL SECTION LOWER SKIN DOOR. REINFORCEMENT HAS LEVEL 2 CORROSION AT FRAME 45, FWD EDGE OF AVIONICS ACCESS DOOR CUT OUT. REPAIR IAW CE 1616 16 10190 DATED 5 10 2016.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MAJOR REPAIR. OVERHEAD HATCH CUT OUT PANEL INTERNAL SURFACE HAS LEVEL 2 CORROSION. REPAIR IAW CE 1606 16 10213 DATED 5 10 2016.

Part: GUIDE — CORRODED (TE FLAP) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. RT OTBD FLAP 2ND CAM GUIDE FROM INBD END HAS AREAS OF LEVEL 2 CORROSION. REPLACED GUIDE WITH OEM PART.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. LT FLOOR SUPPORT ANGLE BETWEEN FRAMES 39 - 40 HAS LEVEL 2 CORROSION. REPLACED ANGLE WITH OEM PART.

Part: GUIDE — CORRODED (TE FLAP) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. RT INBD FLAP 4TH CAM GUIDE FROM INBD END HAS AREAS OF LEVEL 2 CORROSION. REPLACED GUIDE WITH OEM PART.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MAJOR REPAIR. FWD PRESS BULKHEAD FWD SURFACE HAS AREAS OF LEVEL 2 CORROSION. REPAIR IAW CE 1586 16 0184 DATED 5 3 2016.

Part: GUIDE — CORRODED (TE FLAP) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. RT INBD FLAP 3RD CAM GUIDE FROM INBD END HAS LEVEL 2 CORROSION. REPLACED GUIDE WITH OEM PART.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MAJOR REPAIR. LT OTBD SEAT TRACK BETWEEN FRAMES 35-36 HAS AREAS OF LEVEL 2 CORROSION. REPAIRED IAW SRM 53-00-00-300-853-A01.

Part: SKIN — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE MAJOR REPAIR. RT HORIZONTAL STABILIZER LE HAS LEVEL 2 CORROSION ON UPPER & LOWER SURFACES AFT OF DE-ICING BOOT. REPAIR IAW ES-1735 16 10237 DATED 5 11 2016.

Part: SKIN — CORRODED (LT HORIZ STAB) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MAJOR REPAIR. LT HORIZONTAL STABILIZER LE HAS LEVEL 2 CORROSION ON UPPER & LOWER SURFACES AFT OF DE-ICING BOOT. REPAIR IAW SRAS ES-1754 16 10238 DATED 5 11 2016.

Part: ADAPTER — CORRODED (ZONE 300) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. LT VOR & LOCALIZER ANTENNA CONTOUR ADAPTER HAS LEVEL 2 CORROSION. REPLACED ADAPTER WITH OEM PART.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. RT WING LOWER TE DROP DOWN PANEL 632BB OTBD HINGE HAS LEVEL 2 CORROSION. REPLACED HINGE WITH OEM PART.

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. LT LOWER TE DROP DOWN PANEL 532BB HAS LEVEL 2 CORROSION ON HINGE. REPLACED HINGE WITH OEM PART.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MAJOR REPAIR. LT WING LOWER SKIN HAS LEVEL 2 CORROSION AROUND AFT WATER DRAIN CUT OUT, RIB 4 - 5, STRINGER 8 - 9. REPAIR IAW CE 1790 16 9506 DATED 5 11 16.

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. LT LOWER TE DROP DOWN PANEL 531BB HAS LEVEL 2 CORROSION ON HINGE. REPLACED HINGE WITH OEM PART.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. RT UPPER FUEL TANK ACCESS PANEL 622CT HAS LEVEL 2 CORROSION ON TOP SURFACE. REPLACED WITH OEM PART.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. LT UPPER FUEL TANK ACCESS PANEL 522CT HAS LEVEL 2 CORROSION ON TOP SURFACE. REPLACED PANEL WITH OEM PART.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. RT WING LOWER TE DROP DOWN PANEL 632BB INBD HINGE HAS LEVEL 2 CORROSION. REPLACED HINGE WITH OEM PART.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. RT LOWER TE DROP DOWN PANEL 631AB HAS LEVEL 2 CORROSION ON HINGE. REPLACED HINGE WITH OEM PART.

Part: PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MAJOR REPAIR. LT UPPER WING INBD REMOVABLE PANEL 521CT HAS LEVEL 2 CORROSION, BETWEEN RIBS 3 - 5. REPAIR IAW CE 1744 16 10236 DATED 5 11 2016.

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE MINOR REPAIR. LT LOWER TE EDGE DROP DOWN PANEL 531AB HAS LEVEL 2 CORROSION ON HINGE. REPLACED HINGE WITH OEM PART.

Part: HINGE — CORRODED (LT WING) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. LT LOWER TE DROP DOWN PANEL 532AB HAS LEVEL 2 CORROSION ON HINGE. REPLACED HINGE WITH OEM PART.

Part: PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MAJOR REPAIR. RT UPPER WING OTBD REMOVABLE PANEL 622FT HAS LEVEL 2 CORROSION, AROUND FASTENERS RIB 22 - 23. REPAIR IAW SRAS CE-744 16 10211 DATED 5 6 2016.

Part: PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE MAJOR REPAIR. RT UPPER WING INBD REMOVABLE PANEL 621CT HAS LEVEL 2 CORROSION, AROUND FASTENERS RIB 8 - 9. REPAIR IAW CE 1664 16 9114 DATED 4 29 2016.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. RT WING LOWER TE DROP DOWN PANEL 632AB HAS LEVEL 2 CORROSION ON OTBD HINGE. REPLACED HINGE WITH OEM PART.

Part: PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MAJOR REPAIR. LT UPPER WING OTBD REMOVABLE PANEL 522FT HAS LEVEL 2 CORROSION, AROUND FASTENERS RIB 22 - 23. REPAIR IAW CE 1744 16 10211 DATED 5 6 2016.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. RT WING LOWER TE DROP DOWN PANEL 632CB INBD HINGE HAS LEVEL 2 CORROSION. REPLACED HINGE WITH OEM PART.

Part: HINGE — CORRODED (RT WING) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. RT LOWER TE DROP DOWN PANEL 631AB HAS LEVEL 2 CORROSION ON HINGE. REPLACED HINGE WITH OEM PART.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MAJOR REPAIR. FWD CTR FUSELAGE RT LOWER SKIN PANEL HAS LEVEL 2 CORROSION, FRAMES 14 - 15 AT SKIN LAP, STRINGER 17R. REPAIRED IAW CE 1560 16 10201 DATED 5 6 2016.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MAJOR REPAIR. REAR CTR FUSELAGE RT LATERAL LOWER SKIN PANEL EXTERIOR SURFACE HAS LEVEL 2 CORROSION AT THE FWD & AFT EDGES OF THE SERVICE DOOR CUT OUT. REPAIRED IAW CE 1542 16 10208 5 9 2016.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MAJOR REPAIR. REAR CTR FUSELAGE RT LATERAL UPPER SKIN PANEL EXTERIOR SURFACE HAS LEVEL 2 CORROSION AT THE AFT EDGE OF THE SERVICE DOOR CUT OUT. REPAIRED IAW CE 1542 16 10208 DATED 5 9 2016.

Part: HINGE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,472 hrs · 23,939 cycles

HEAVY CHECK COE & MINOR REPAIR. LEVEL 2 CORROSION ON POTABLE WATER SERVICE DOOR HINGE. REPLACED HINGE WITH OEM PART.

Part: SKIN PANEL — CRACKED (CARGO DOOR) · airframe 20,690 hrs · 21,919 cycles

CARGO DOOR STRUT JAMMED INTO DOOR WHILE CLOSING. SUBSTANTIAL CRACKS LOCATED AT & AROUND THE FWD CARGO DOOR STRUT ATTACH POINT ON THE DOOR. OBSERVED DAMAGE APPEARS TO BE LOCALIZED & LIMITED TO DOOR ONLY. INNER SKIN OF THE FWD CARGO DOOR TORN. REPAIRED IAW SRAS CE-4872 15 9641 ISSUE B DATED 9 28 15.

Part: A/C PACK — FAULTY (AC BAY) · airframe 19,554 hrs · 19,020 cycles

STRONG BURNING ODOR, AIR TURN BACK. DURING CLIMB OUT A STRONG BURNING ODOR WAS SMELLED THROUGHOUT THE ACFT. IT WAS ALSO NOTED THAT THE AIR CONDITIONING WAS ONLY DELIVERING HOT AIR TO THE COCKPIT & CABIN. THE DECISION WAS MADE TO RETURN, NO EMER WAS DECLARED. THE ACFT LANDED WITHOUT FURTHER INCIDENT. TROUBLESHOOTING DISCOVERED THE NR 1 PACK FAULTY. PART ORDERED. ITEM WAS DEFERRED.

Part: SPLICE PLATE — CORRODED (LT WING) · corrosion level 2 · airframe 19,436 hrs · 18,738 cycles

CENTER WING, CTR SPLICE PLATE 521AT HAS LEVEL 2 CORROSION DAMAGE ON LOWER SURFACE & IN COUNTERSINKS. R & R WITH OEM PART.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,436 hrs · 18,738 cycles

SERVICE DOOR THRESHOLD HAS AREAS OF LEVEL 2 CORROSION FRAMES 36 - 37 & FWD OF FRAME 39. REPLACED THRESHOLD WEB WITH NEW OEM PART.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,436 hrs · 18,738 cycles

EXTERIOR FUSELAGE MOUNT PLATE FOR THE AFT RADIO ALTIMETER ANTENNA HAS MULTIPLE AREAS OF LEVEL 2 INTERGRANULAR CORROSION AROUND SCREW HOLES. REPLACED PLATE ASSEMBLY WITH NEW OEM PART.

Part: MOUNT FITTING — CHAFED (LT AILERON) · airframe 19,436 hrs · 18,738 cycles

LEFT AILERON MOUNT FITTING AT RIB 27 HAS CHAFING DAMAGE ON THE INBD EDGE OF THE OTBD EAR. REPAIR IAW SRAS DT S-7077 13 8150 DATED 12/30/2013.