N811HC

Part: FAILSAFE — CRACKED (FRAME 30) · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 100044 HEAVY CHECK COE/MAJOR REPAIR: FRAME 30 FAIL SAFE CRACKED AROUND STRINGER 15L. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-817-A01.

Part: SKIN — CORRODED (FRAMES 31-32) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200196 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 31-32 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 8L-10L. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112410_01...15825 ISSUE A, DATED 2/12/2020.

Part: SKIN — CORRODED (FRAMES 24-25) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200242 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 24-25 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 13-14R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112402_01...15785 ISSUE A, DATED 2/10/2020.

Part: SKIN — CORRODED (FRAMES 40-41) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200161 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 40-41 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 8L-9L. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112410_01...15825 ISSUE A, DATED 2/12/2020.

Part: SKIN — CORRODED (FRAMES 24-25) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200245 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 24-25 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 5R-6R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112397_01...15822 ISSUE A, DATED 2/10/2020.

Part: SKIN — CORRODED (FRAMES 24-25) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200244 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 24-25 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 6R-7R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112397_01...15822 ISSUE A, DATED 2/10/2020.

Part: SKIN — CORRODED (FRAMES 29-30) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200207 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 29-30 HAS LEVEL 2 CORROSION STRINGERS 5R-6R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112414_01...15827 ISSUE A, DATED 2/10/2020.

Part: SKIN — CORRODED (FRAMES 34-35) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200183 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 34-35 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 5R-6R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112414_01...15827 ISSUE A, DATED 2/10/2020.

Part: SKIN — CORRODED (FRAMES 43-44) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

DURING HEAVY CHECK, TAIL FUSELAGE LT CROWN PANEL INTERIOR SURFACE WAS CORRODED, FRAMES 43-44, STRINGERS 1L-2L. REPAIRED IAW SRM 530000-300-862-A01.

Part: SKIN — CORRODED (FRAMES 30-31) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200198 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 30-31 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 8L-10L. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112410_01...15825 ISSUE A, DATED 2/12/2020.

Part: SKIN — CORRODED (FRAMES 33-34) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200184 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 33-34 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 4L-5L. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112410_01...15825 ISSUE A, DATED 2/12/2020.

Part: SKIN — CORRODED (FRAMES 34-35) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200180 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 34-35 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 5L-6L. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-803-A01.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 31-32 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 4L-5L. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-803-A01.

Part: SKIN — CORRODED (FRAMES 23-23A) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200316 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE L/H UPPER SKIN PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION FRAMES 23-23A BETWEEN STRINGERS 6AL-7L. CORRECTIVE ACTION: REPAIRED PER SRAS CETS-3143/16...10437 ISSUE B, DATED 2/12/2020.

Part: SKIN — CORRODED (FRAMES 30-31) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200200 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 30-31 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 5R-6R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112414_01...15827 ISSUE A, DATED 2/10/2020.

Part: SKIN — CORRODED (FRAME 23) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200310 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN AFT OF FRAME 23 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 6AR-7R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112397_01...15822 ISSUE A, DATED 2/10/2020.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200182 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE R/H LOWER SKIN PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION FRAMES 34-35 BETWEEN STRINGERS 11R-12R. CORRECTIVE ACTION: REPAIR PER SRM 530000-300-801-A01.

Part: SKIN — CORRODED (FRAMES 40-41) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200165 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 40-41 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 11R-12R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112417_01...15813 ISSUE A, DATED 2/5/2020.

Part: SKIN — CORRODED (FRAMES 42-43) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200145 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 42-43 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 2R-3R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112667_01...15812 ISSUE A, DATED 2/7/2020.

Part: SKIN — CORRODED (FRAMES 23B-23C) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200283 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 23B-23C CORRODED BETWEEN STRINGERS 5AR-6R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112397_01...15822 ISSUE A, DATED 2/10/2020.

Part: SKIN — CORRODED (FRAMES 29-30) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200205 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 29-30 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 12R-13R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112417_01...15813 ISSUE A, DATED 2/5/2020.

Part: SKIN — CORRODED (FRAMES 43-44) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

HEAVY CHECK: TAIL FUSELAGE LT PANEL INTERIOR SURFACE WAS CORRODED FRAMES 43-44 BETWEEN STRINGERS 9L-10L. REPAIRED PER SRM 530000-300-803-A01.

Part: SKIN — CORRODED (FRAMES 41-42) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200154 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 41-42 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 8R-9R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112414_01...15827 ISSUE A, DATED 2/10/2020.

Part: SKIN — CORRODED (FRAMES 23A-23B) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200304 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 23A-23B HAS LEVEL 2 CORROSION BETWEEN STRINGERS 12R-13R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112402_01...15785 ISSUE A, DATED 2/10/2020.

Part: SKIN — CORRODED (FRAMES 39-40) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200174 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 39-40 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 5R-6R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112414_01...15827 ISSUE A, DATED 2/10/2020.

Part: SKIN — CORRODED (FRAME 23) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200321 HEAVY CHECK COE/MAJOR REPAIR: FORWARD FUSELAGE R/H UPPER SKIN PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION FWD OF FRAME 23 BETWEEN STRINGERS 8R-10R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0111812_01...15731 ISSUE A, DATED 1/21/2020.

Part: SKIN — CORRODED (FRAMES 33-34) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200188 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 33-34 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 7R-8R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112414_01...15827, ISSUE A, DATED 2/10/2020.

Part: SKIN — CORRODED (FRAMES 30-31) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 200199 HEAVY CHECK COE/MAJOR REPAIR: FUSELAGE INNER SKIN BETWEEN FRAMES 30-31 HAS LEVEL 2 CORROSION BETWEEN STRINGERS 10L-11L. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0112410_01...15825 ISSUE A, DATED 2/12/2020.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 800012 HEAVY CHECK COE/MINOR REPAIR: PASSENGER DOOR INTERCOSTAL FWD OF PRESSURE RELIEF DOOR IS CRACKED. CORRECTIVE ACTION: REPLACED INTERCOSTAL WITH OEM PART.

Part: WEB — CORRODED (FRAMES 14-20) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 100030 HEAVY CHECK COE/MINOR REPAIR: CARGO DOOR SILL HORIZONTAL WEB HAS LEVEL 2 CORROSION BETWEEN FRAMES 14-20. CORRECTIVE ACTION: REPLACED WEB WITH OEM PART.

Part: FRAME — CORRODED (FRM 17) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

HEAVY CHECK. FRAME 17 FORWARD SIDE HAS CORROSION BETWEEN STRINGERS 17L-20L. REPLACED THE FRAME SEGMENT.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

HEAVY CHECK COE/MAJOR REPAIR: RT CREASE BEAM WEB BETWEEN FRAMES 22-23 UPPER SURFACE HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED WITH FABRICATION.

Part: FAILSAFE — CORRODED (FRAME 23A) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 100021 HEAVY CHECK COE/MAJOR REPAIR: FRAME 23A FAIL SAFE HAS LEVEL 2 CORROSION ABOVE STRINGER 21L. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-817-A01.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

HEAVY CHECK COE/MINOR REPAIR: CARGO DOOR THRESHOLD VERTICAL PLATE REPAIRED DOUBLER HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED DOUBLER.

Part: FLOORBEAM — CORRODED (FRAME 36) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 100019 HEAVY CHECK COE/MINOR REPAIR: FLOORBEAM 36 UPPER SURFACE HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED RH OB SECTION PER SRM 530000-300-857-A01.

Part: FLOORBEAM — CORRODED (FRAME 30) · corrosion level 2 · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 100016 HEAVY CHECK COE/MINOR REPAIR: FLOORBEAM 30 UPPER SURFACE HAS MULTIPLE AREAS OF LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED WITH OEM PART.

Part: SKIN — CRACKED (PAX DOOR) · airframe 28,037 hrs · 29,993 cycles

WO 209669 NR 800010 HEAVY CHECK COE/MAJOR REPAIR: PASSENGER DOOR INNER SKIN CRACKED JUST FORWARD OF PRESSURE RELIEF FOOR, COMMON TO THE STAIR NUT PLATE. CORRECTIVE ACTION: REPAIRED PER SRM 521100-300-812-A01.

Part: COWLING — LOOSE (RT ENGINE) · airframe 28,037 hrs · 29,993 cycles

HEAVY CHECK COE/MAJOR REPAIR: RT ENGINE CENTER HINGE COWL IS LOOSE AT FORWARD AND AFT ATTACH POINTS. CORRECTIVE ACTION: REPAIRED PER SRM 541162-300-801-A01.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 27,944 hrs · 29,876 cycles

WO 206741 NR 2 DISCREPANCY: LT FUSELAGE SIDE DENT ON SKIN PANEL, FWD OF MAIN CARGO DOOR AFT OF FRAME 12 & BELOW STRINGER 11. CORRECTIVE ACTION: REPAIR PER SRAS ES_0105046_01...15151 ISSUE B, DATED 9/10/2019.

Part: STRUCTURE — DAMAGED (LT WING) · airframe 27,842 hrs · 29,728 cycles

WO 201960/DISCREPANCY: FASTENER HOLE ELONGATED ON LT WING LOWER SIDE FOR ICE DETECTOR PROBE. CORRECTIVE ACTION: TEMPORARY REPAIR PER SRAS ES-0098805-01...14613, ISSUE A, DATED 5/17/2019.

Part: STRINGER — CORRODED (FRAMES 16-17) · airframe 27,476 hrs · 29,208 cycles

STRINGER 6R CORRODED. REPAIRED AND SPLICED BETWEEN FRAMES 16-17.

Part: TRUSS — CORRODED · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

THE LT R/S SHEAR TRUSS MEMBER HAD CORROSION. REPAIRED IAW SRM 535730-300-801-A01.

Part: FITTING — CORRODED (RT MLG TRUNNION) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

RIGHT MLG FORWARD TRUNNION STRUT LOWER FITTING ON FUSELAGE HAS CORROSION AROUND LINK ATTACH HOLE. REPAIRED SRM 53-57-30-300-801-A01.

Part: TRUSS — CORRODED (RT MLG) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

RIGHT MLG TRUSS SHEAR MEMBER CORRODED AROUND FORWARD FITTING ATTACH HOLE COMMON TO FORWARD SUPPORT TRUSS. REPAIRED IAW SRM 53-57-30-300-801-A01.

Part: TRUSS — CORRODED (LT MLG) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

LEFT MLG TRUSS SHEAR MEMBER CORRODED AROUND FORWARD FITTING ATTACH HOLE. REPAIRED IAW SRM 53-57-30-300-801-A01.

Part: TRUSS — CORRODED (LT MLG) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

LEFT MLG TRUSS SHEAR MEMBER FORWARD SUPPORT TRUSS HAD CORROSION AROUND AFT SIDE OF FITTING ATTACH HOLE. REPAIRED IAW SRM 535730-300-801-A01.

Part: FITTING — CORRODED (LT TRUNNION) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

LEFT WHEEL WELL, AFT TRUNNION SUPPORT HAS 2 CORROSION BY THE BORE. REPAIRED IAW SRM 53-57-30-300-801-A01.

Part: STRINGER CLIP — CORRODED (FRAME 18) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

STRINGER 7R CLIP CORRODED AT FRAME 18. REPLACED THE STRINGER CLIP.

Part: STRINGER CLIP — CORRODED (FRAME 18) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

STRINGER 7AR CLIP CORRODED AT FRAME 18. REPLACED THE STRINGER CLIP.

Part: STRINGER CLIP — CORRODED (FRAME 18) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

STRINGER 11R CLIP CORRODED AT FRAME 18. REPLACED THE STRINGER CLIP.

Part: STRINGER — CORRODED (FRAMES 16-17) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

STRINGER 6R CORRODED BETWEEN FRAMES 16 - 17. REPAIRED THE STRINGER IAW SRM 53-00-00-300-824-A01.

Part: STRINGER CLIP — CORRODED (FRAME 18) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

STRINGER 10AR CLIP CORRODED AT FRAME 18. REPLACED THE STRINGER CLIP.

Part: STRINGER CLIP — CORRODED (FRAME 18) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

STRINGER 6R CLIP CORRODED AT FRAME 18. REPLACED THE STRINGER CLIP.

Part: FITTING — CORRODED (RT TRUNNION) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

RIGHT WHEEL WELL AFT TRUNNION SUPPORT FUSELAGE FITTING CORRODED BY THE BORE. REPAIRED IAW SRM 53-57-30-300-801-A01.

Part: STRINGER CLIP — CORRODED (FRAME 17) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

STRINGER 12AR CLIP CORRODED AT FRAME 17. REPLACED THE STRINGER CLIP.

Part: STRINGER CLIP — CORRODED (FRAME 17) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

STRINGER 11R CLIP CORRODED AT FRAME 17. REPLACED THE STRINGER CLIP.

Part: SEAT TRACK — CORRODED (FRAME 36) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

LEFT INBOARD SEAT TRACK CORRODED FORWARD OF FRAME 36. REPAIRED IAW SRM 53-00-00-300-853-A01.

Part: STRINGER — DAMAGED (FRAMES 21-22) · airframe 27,476 hrs · 29,208 cycles

STRINGER 16L IS DAMAGED BETWEEN FRAMES 21 - 22. REPAIRED THE STRINGER IAW SRM 53-00-00-300-824-A01.

Part: PRESSURE DECK — CORRODED (FRAMES 26-27) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

RIGHT PRESSURE DECK BY THE OTBD SEAT TRACK CORRODED, FRAMES 26 - 27. REPAIRED IAW SRAS PCE-1310/18.12735.

Part: WEB — DAMAGED (FRAMES 24-25) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

RIGHT CREASE BEAM WEB HAS AREAS OF DAMAGE, FRAMES 24 - 25. REPLACED THE CREASE BEAM WEB.

Part: STIFFENER — CORRODED (FRAMES 26-27) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

UNDERFLOOR PRESSURE DECK STIFFENER HAD CORROSION, FRAMES 26 - 27. REPLACED THE STIFFENER.

Part: FLOORBEAM — CORRODED (FRAME 22) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

FLOORBEAM AT FRAME 22 UPPER SURFACE HAS CORROSION AROUND THE FLOOR PANEL SCREW HOLES BETWEEN THE LT SEAT TRACKS. REPAIRED IAW SRM 53-00-00-300-852-A01.

Part: FLOORBEAM — CORRODED (FRAME 21) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

FLOORBEAM AT FRAME 21 UPPER SURFACE CORRODED AROUND FLOOR PANEL SCREW HOLES BETWEEN LT SEAT TRACKS. REPAIRED IAW SRM 530000-3000-833-A01.

Part: WEB — CORRODED (FRAMES 24-25) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

LEFT CREASE BEAM WEB HAS AREAS OF DAMAGE FRAMES 24-25. REPAIRED.

Part: FAILSAFE — CORRODED (FRAME 29) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

CORROSION ON FRAME 29 FAIL SAFE BETWEEN STRINGERS 18L - 18R. REPLACED THE FAIL SAFE.

Part: SEAT TRACK — CORRODED (FRAME 36) · corrosion level 2 · airframe 27,476 hrs · 29,208 cycles

RIGHT INBOARD SEAT TRACK CORRODED FORWARD OF FRAME 36. REPAIRED THE SEAT TRACK IAW SRM 53-00-00-300-853-A01.

Part: BULKHEAD — CORRODED (FWD) · corrosion level 2 · airframe 27,413 hrs · 29,124 cycles

FWD PRESSURE BULKHEAD, UPPER BONDING POINTS FOR RADOME HAD CORROSION. REPAIRED.

Part: BULKHEAD — CORRODED (FWD) · corrosion level 2 · airframe 27,413 hrs · 29,122 cycles

FORWARD PRESSURE BULKHEAD LOWER CONTACT POINTS WITH RADOME CORRODED. REPAIRED IAW SRM 531110-300-808-A01.

Part: ANGLE — CORRODED (FRAMES 13-14) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

UPPER ATTACH ANGLE FOR VERTICAL WEB HAS CORROSION AT STRINGER 15L BETWEEN FRAMES 13-14. REPLACED ANGLE.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

BRIDGING CHECK COE/MINOR REPAIR. INTERCOSTAL AT BL0 BETWEEN FLOORBEAMS 10-11 HAS LEVEL 2 CORROSION. REPLACED WITH NEW PART.

Part: SUPPORT BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

BRIDGING CHECK COE/MINOR REPAIR. FLOORBOARD SUPPORT BEAM ON FLOORBEAM 10, LT SIDE HAS LEVEL 2 CORROSION. REPLACED SUPPORT BEAM WITH NEW PART.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

BRIDGING CHECK COE/MINOR REPAIR. CLIP BETWEEN FRAMES 9-10 LT SIDE ATTACHED TO O2 BOTTLE SUPPORT INTERCOSTAL HAS LEVEL 2 CORROSION. REPLACED WITH OEM CLIP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

BRIDGING CHECK/MINOR REPAIR: FLOORBEAM 13 HAS LEVEL 2 CORROSION AT NUT CLIP HOLES. REPLACED FLOORBEAM WITH OEM PART.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

CHECK/MINOR REPAIR: LEVEL 2 CORROSION ON FLOORBEAM 10 AT LBL 2. REPLACED FLOORBEAM 10 WITH OEM PART.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 27,412 hrs · 29,121 cycles

BRIDGING CHECK COE/MAJOR REPAIR. STRINGER 1R AT FRAME 22 IS EXFOLIATED. REPAIRED IAW SRM 530000-300-847-A01.

Part: SKIN — DENTED (FRAME 14) · airframe 27,412 hrs · 29,121 cycles

DURING LIGHTENING STRIKE INSPECTION, FOUND A PROTRUDING DENT AT FRAME 14, UNDER STRINGER 14R. REPAIRED THE SKIN IAW SRM 530000-300-808-A01 REV. 95.

Part: FRAME — DAMAGED (FRAME 23) · airframe 27,412 hrs · 29,121 cycles

FRAME 23 DAMAGED AT FLANGES. REPAIRED IAW SRAS ES-3379/16.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 27,412 hrs · 29,121 cycles

BRIDGING CHECK COE/MAJOR REPAIR. EXTERNAL FUSELAGE SKIN HAS A LIGHTNING STRIKE BETWEEN FRAMES 3/4, STRINGERS 14R & 15R. REPAIRED PER SRM 51-21-17.

Part: SKIN — DAMAGED (FRAMES 21-22) · airframe 27,412 hrs · 29,121 cycles

LIGHTNING STRIKE DAMAGE ON FWD FUSELAGE LOWER SKIN PANEL BETWEEN FRAMES 21 & 22 AT STRINGER 21L. REPAIRED IAW SRAS CETS-3588/16.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

RIGHT WING PANEL 623GT HAS CORROSION ON INNER SURFACE. REPLACED WITH OEM PART.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

CHECK/MAJOR REPAIR: LT WING RIB 5 FLANGES LEVEL 2 CORROSION BETWEEN STIFFENER 3-4, 6-7 AND 8-9. REPAIR PER SRAS S571R0404.10605 DATED 9/19/2016.

Part: SKIN PANEL — CORRODED (FRAMES 23C-23D) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

CENTER FUSELAGE LT UPPER SKIN PANEL INNER SURFACE HAS CORROSION, FRAMES 23C-23D, STRINGER 6A-7. REPAIRED IAW SRAS CETS-3143/16..

Part: SKIN — CORRODED (FRAMES 23B-23C) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

CENTER FUSELAGE LT UPPER SKIN PANEL INNER SURFACE HAS CORROSION, FRAMES 23B - 23C, STRINGER 7A - 8L. REPAIRED IAW CETS-3143/16.

Part: SKIN PANEL — CORRODED (FRAMES 23C-23D) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

CENTER FUSELAGE LT UPPER SKIN PANEL INNER SURFACE HAS CORROSION, FRAMES 23C-23D, STRINGER 5A-6. REPAIRED PER SRAS CETS-3143/16.

Part: SKIN — DAMAGED (FRAME 8) · airframe 27,412 hrs · 29,121 cycles

LIGHTENING STRIKE AT FRAME 8, AFT SKIN EDGE AT BUTT JOINT BETWEEN FWD AND AFT NOSE FUSELAGE CROWN SKIN PANELS. REPAIRED IAW CETS-3232/16.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 27,412 hrs · 29,121 cycles

BRIDGING CHECK COE/MAJOR REPAIR. PERMANENT REPAIR OF FRAME 27. REPAIRED PER SRAS S535R0324 8690 ISSUE B DATED 8/25/2016.

Part: RIB — CRACKED (RT WING) · airframe 27,412 hrs · 29,121 cycles

RIB 6R UPPER FLANGE CRACKED/TORN BETWEEN STIFFENER 5-6. REPAIRED PER SRAS S571R0403.

Part: STRINGER — DAMAGED (FRAME 23) · airframe 27,412 hrs · 29,121 cycles

STRINGERS 21 LT & RT ARE DAMAGED BETWEEN FRAMES 23-23A. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-825-A01.

Part: SKIN — DENTED (FRAME 18) · airframe 27,412 hrs · 29,121 cycles

SKIN DENT OUT OF LIMITS LOCATED 8.0 INCH AFT OF FRAME 18 AND 1.2 INCH BELOW STRINGER 18L. REPAIRED PER DT/S-4553/14.

Part: SKIN — DENTED (FRAME 8) · airframe 27,412 hrs · 29,121 cycles

NOSE FUSELAGE SECTION LT AFT LOWER LOBE SKIN PANEL HAS A DENT AT THE INTERSECTION OF FRAME 8 AND TWO INTERCOSTALS. REPAIRED IAW CETS-2897/16...10457 ISSUE B.

Part: SKIN — DENTED (FUSELAGE) · airframe 27,412 hrs · 29,121 cycles

HEAVY CHECK/MAJOR REPAIR, THREE DENTS AFT OF FRAME 40 BETWEEN STR 14R-15R AND ONE DENT FWD OF FRAME 40 BETWEEN STR 14R-15. DENTS ARE BELOW CREASE BEAM. REPAIRED PER SRAS 3054/16.10553.

Part: SKIN — DENTED (FUSELAGE) · airframe 27,412 hrs · 29,121 cycles

CHECK/MAJOR REPAIR: DENT AFT OF FRAME 13A AND STRINGER 2A LT. REPAIRED PER ASI EO ASI-SB-ATR72-5330-0472 REV 1.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

LEFT WING LOWER SKIN PANEL INTERAL SURFACE OUTBOARD OF RIB 4 OF STIFFENER 5 HAS CORROSION. REPAIRED IAW CETS-3192/16.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

CORROSION FOUND ON LT WING LOWER SKIN INTERNAL SURFACE, INBOARD OF RIB 5 AND FORWARD SIDE OF STIFFENER 9. REPAIRED IAW CETS-3192/16.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

CHECK/MINOR REPAIR: LT WING ACCESS PANEL 523GT HAS LEVEL 2 CORROSION. REPLACED 523GT DOOR.

Part: CREASE BEAM — CORRODED (FRAME 20) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

LEFT CREASE BEAM, INBD CHORD, HAS SURFACE CORROSION AT FRAME 20. FABRICATED AND REPLACED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 27,412 hrs · 29,121 cycles

BRIDGING CHECK COE/MAJOR REPAIR, EXTERIOR FUSELAGE SKIN AT FR 28D STR 21 HAS EVIDENCE OF A LIGHTNING STRIKE. REPAIRED PER SRAS ES-3038/16.10546.

Part: HINGE FITTING — CORRODED (LT AILERON TAB) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

LEFT AILERON TAB INBOARD HINGE FITTING HAS CORROSION. REPLACED.

Part: HINGE FITTING — CRACKED (RT AILERON TAB) · airframe 27,412 hrs · 29,121 cycles

RIGHT AILERON TAB, INBOARD HINGE FITTING CRACKED. REPLACED.

Part: SKIN — DAMAGED (FRAME 23) · airframe 27,412 hrs · 29,121 cycles

LIGHTNING STRIKE ON FWD CENTER FUSELAGE CROWN PANEL, AFT EDGE AT FRAME 23, STRINGER 2AR. REPAIRED IAW SRAS ES-3379/16.

Part: SKIN PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

BRIDGE CHECK COE & MAJOR REPAIR. LEVEL 2 CORROSION & SCRIBE DAMAGE ON CTR FUSELAGE AFT CROWN PANEL AT ADF ANTENNA LOCATION. DOUBLER REPAIR IAW SRM 535127-300-801-A01.

Part: PANEL — DAMAGED (LT WING) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

BRIDGING CHECK COE/MAJOR REPAIR. LEVEL 2 FRETTING DAMAGE ON LT WING UPPER REMOVABLE PANEL LANDING AT 521DT. REPAIRED PER SRAS CETS-3082/16...10429 ISSUE B DATED 11/22/2016.

Part: SKIN — CORRODED (FRAMES 17-18) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

LOWER FUSELAGE SKIN CORRODED. REPAIRED.

Part: SKIN — DAMAGED (FRAME 23) · airframe 27,412 hrs · 29,121 cycles

LOWER FUSELAGE SKIN WHERE ADF 2 ANTENNA MOUNTS, HAS NUMBEROUS AREAS OF DAMAGE AND SCRIBE LINES. REPAIRED IAW SRAS CE-15/16.

Part: SKIN — DAMAGED (FRAME 23) · airframe 27,412 hrs · 29,121 cycles

LIGHTNING STRIKE ON FWD FUSELAGE CROWN PANEL, AFT EDGE OF FRAME 23, STRINGER 2AR. REPAIRED IAW SRAS ES-3379/16.

Part: SEAT TRACK — GOUGED (ZONE 100) · airframe 27,412 hrs · 29,121 cycles

RIGHT INBOARD SEAT TRACK GOUGED AFT OF FLOORBEAM FRAME 17. REPAIRED IAW SRM 530000-300-853-A01.

Part: SEAT TRACK — DAMAGED (FRAME 28) · airframe 27,412 hrs · 29,121 cycles

RIGHT INBOARD SEAT TRACK HAS DAMAGE IN CLAW AREA AT FRAME 28. REPAIR IAW SRM 530000-300-853-A01 REV. 95.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

WO 156011 NR 100039 BRIDGE CHECK COE & MINOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING AFT FUSELAGE RT OTBD SEAT TRACK, FRAMES 41 - 44. REPLACED SEAT TRACK WITH OEM PART.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

BRIDGE CHECK COE & MINOR REPAIR. INTERIOR LEVEL 2 CORROSION AFFECTING REAR CTR FUSELAGE, LT INBD SEAT TRACK, FRAMES 36 - 38. REPLACED WITH SEAT TRACK OEM PART.

Part: SUPPORT BRACKET — CORRODED (LT AILERON) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

LEFT AILERON TRIM ACTUATOR BRACKET HAS CORROSION COMMON TO INBOARD SIDE BONDING ATTACH. REPLACED AILERON TRIM ACTUATOR SUPPORT.

Part: ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

AFT PAX DOOR, LOWER FWD CORNER, BEAM CLIP HAS CORROSION. REPLACED WITH NEW BEAM CLIP.

Part: SEAT TRACK — CORRODED (FRAMES 36-38) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

WO 156011 NR 100035 BRIDGING CHECK COE/MINOR REPAIR: R/H INBOARD SEAT TRACK HAS AREAS OF LEVEL 2 CORROSION ON UPPER SURFACE AT FRAMES 36 & 38. CORRECTIVE ACTION: REPLACED SEAT TRACK.

Part: HINGE — CORRODED (AILERON TAB) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

BRIDGING CHECK COE/MINOR REPAIR. RT AILERON TRIM TAB HINGES ARE EXFOLIATED. LEVEL 2 CORROSION. REPLACED HINGE WITH OEM PART.

Part: HINGE — CORRODED (AILERON TAB) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

BRIDGING CHECK COE/MINOR REPAIR. RT AILERON TRIM TAB HINGE SECOND FROM OB IS EXFOLIATED. LEVEL 2 CORROSION. REPLACED HINGE WITH OEM PART.

Part: SEAT TRACK — CORRODED (FRAMES 41-44) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

LEFT OUTBOARD SEAT TRACK HAS CORROSION ON UPPER SURFACE BETWEEN FRAMES 41 & 44. REPLACED THE SEAT TRACK.

Part: THRESHOLD — CORRODED (FRAMES 36-39) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

AFT RT SERVICE DOOR THRESHOLD HAS AREAS OF CORROSION ON UPPER SURFACE. REPLACED THE THRESHOLD.

Part: FASTENER — LEAKING (RT WING) · airframe 27,412 hrs · 29,121 cycles

RT WING OUTER BOX LOWER SKIN HAS LEAKING FASTENERS RIB 22. REPAIRED IAW SRAS ES-172/16.

Part: FAILSAFE — CRACKED (FRAME 28) · airframe 27,412 hrs · 29,121 cycles

FRAME 28A FAIL SAFE ANGLE IS BENT AND CRACKED BETWEEN STRINGERS 15R-16R. REPAIRED IAW SRM 53-00-00-300-817-A01.

Part: FASTENER — LEAKING (LT WING) · airframe 27,412 hrs · 29,121 cycles

LEFT WING OUTER BOX LOWER SKIN HAS LEAKING FASTENERS BETWEEN RIBS 22-23. REPAIRED IAW ES-171/16.

Part: FASTENER — LEAKING (LT WING) · airframe 27,412 hrs · 29,121 cycles

LEFT WING OUTER BOX LOWER SKIN HAS INACCESSIBLE LEAKING FASTENERS RIB 22. REPAIRED IAW ES-171/16.

Part: FASTENER — LEAKING (LT WING) · airframe 27,412 hrs · 29,121 cycles

LEFT WING OUTER BOX LOWER SKIN HAS LEAKING FASTENERS RIB 19. REPAIRED PER SRAS ES-171/16.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

MAIN CARGO DOOR THRESHOLD UPPER SURFACE HAS CORROSION JUST OB OF SEAT TRACK. REPLACED WITH OEM PART.

Part: FRAME — CORRODED (FRM 28) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

FRAME 28 HAS CORROSION ON AFT SURFACE BETWEEN STRINGERS 20L & 21L BELOW FAILSAFE ANGLE. REPLACED THE FRAME.

Part: SEAT TRACK — CORRODED (FRAME 26-28) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

RIGHT OUTBOARD SEAT TRACK HAS CORROSION BETWEEN FRAMES 26-28. REPAIRED IAW SRM 530000-300-853-A01.

Part: KEELBEAM — CORRODED (FRAME 26) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

KEEL BEAM WEB, LT SIDE AT FRAME 26 HAS AREAS OF CORROSION. REPAIRED.

Part: SPAR — SCRATCHED (LT WING) · airframe 27,412 hrs · 29,121 cycles

SCRATCH DAMAGE ON LT WING FRONT SPAR, UPPER CAP STRIP, RIB 30-31. REPAIRED IAW SRAS CE-222/16.

Part: SEAT TRACK — DAMAGED (FRAMES 23 A&B) · airframe 27,412 hrs · 29,121 cycles

LEFT OUTBOARD SEAT TRACK HAS DAMAGE IN CLAW AREA BETWEEN FRAMES 23A AND 23B. REPAIRED IAW SRM 530000-300-853-A01 REV. 95.

Part: SKIN — DAMAGED (FRAME 36) · airframe 27,412 hrs · 29,121 cycles

LOWER LEFT LATERAL FUSELAGE SKIN HAS DAMAGE FROM THE PASSENGER ENTRY DOOR BOTTOM SHOOT BOLT. REPAIRED IAW SRM 536125-300-802-A01.

Part: SKIN — DAMAGED (FRAME 39) · airframe 27,412 hrs · 29,121 cycles

LOWER LEFT LATERAL FUSELAGE SKIN HAS DAMAGE FROM THE PASSENGER ENTRY DOOR BOTTOM SHOOT BOLT. REPAIRED IAW SRM 536125-300-802-A01.

Part: SPAR — CHAFED (LT WING) · airframe 27,412 hrs · 29,121 cycles

SCRATCH DAMAGE ON LT WING FRONT SPAR, UPPER CAP STRIP, RIB 19. REPAIRED IAW SRAS CE-222/16.

Part: SUPPORT BRACKET — CORRODED (RUDDER TRIM) · corrosion level 2 · airframe 27,412 hrs · 29,121 cycles

RUDDER TRIM TAB BELLCRANK SUPPORT BRACKET HAS CORROSION ON NUT PLATES UPPER SURFACE. REPLACED THE BRACKET AND SUPPORT ASSEMBLY WITH OEM PART.

Part: SPAR CAP — DAMAGED (RT WING) · airframe 27,412 hrs · 29,121 cycles

SCRATCH DAMAGE ON RT WING, FRONT SPAR LOWER CAP, RIB 25-26. REPAIRED IAW ES-189/16.