N880RW

Part: FASTENER — DAMAGED (ZONE 100) · airframe 28,146 hrs · 21,115 cycles

EMERGENCY VENT SUPPORT BRACKET FOUND DAMAGED AT FR 31. REPLACED IAW EMBRAER 170 AMM 20-10-01.

Part: SHEAR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 28,146 hrs · 21,115 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CENTER FUSELAGE III, FLOOR STRUCTURE, RH SHEAR PANEL CORRODED AT FR87R TO FR88R, RBL 24. REPLACED CFII FLOOR STRUCTURE RH SHEAR PANEL AT FR87 TO FR88, RBL24, WITH NEW IAW SRM 51-42-01.

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 28,146 hrs · 21,115 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CENTER FUSELAGE III, FLOOR STRUCTURE, TOP UPPER SHEET CORRODED AT FR 85L TO FR 86L, LBL12. REPLACED CFIII FLOOR STRUCTURE TOP UPPER SHEET AT FR85 FO FR86, LBL 12 WITH NEW IAW SRM 51-43-03.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 28,146 hrs · 21,115 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CENTER FUSELAGE III, FLOOR STRUCTURE, GUSSET PLATE CORRODED AT FR90R, RBL12. REPLACED CFIII FLOOR STRUCTURE GUSSETT PALTE AT FR90, RBL12, WITH NEW IAW SRM 51-41-02

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 28,146 hrs · 21,115 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CFIII, FLOOR STRUCTURE, GUSSET PLATE CORRODED AT FR 90R, RBL26. CENTER FUSELAGE III FLOOR STRUCTURE GUSSET PLATE AT FR90, RBL26 WAS REPLACED WITH NEW IAW SRM 51-41-02.

Part: SUPPORT PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,146 hrs · 21,115 cycles

WHILE IN HEAVY CHECK FOUND ON CFIII SUPPORT PANEL CORRODED AT FR 88R TO FR 90R,RBL36. REPLACED CFIII PANEL SUPPORT AT FR 88R TO FR 90R, RBL 36, IAW SRM 51-42-01 & 51-43-03.

Part: SPLICE — CORRODED (ZONE 200) · corrosion level 2 · airframe 28,146 hrs · 21,115 cycles

DURING HEAVY CHECK MAINTENANCE FOUND CENTER FUSELAGE III, SPLICE CORRODED AT FR87R TO 88R, RBL40. REPLACED CFIII SPLICE AT FR87 TO FR88, RBL40, WITH NEW IAW SRM 51-42-02.

Part: RIB — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,146 hrs · 21,115 cycles

CENTER FUSELAGE II LOWER PORTION, WFF RIB FOUND CORRODED AT FR 47. INSTALLED NEW RIB I.A.W. SRM 51-41-01.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,685 hrs · 20,759 cycles

ROW 2 EMERGENCY OVERHEAD LIGHT INOP. R&R ELPU 2 IAW AMM 33-50-01

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

WHILE IN HEAVY MAINT CHECK - FOUND CORROSION AFT CARGO FLOOR SUPPORT BRACKET AT FR 80 STR 26R. REMOVED AND REPLACED FLOOR SUPPORT BRACKET AT FR 80 STR 26R, IAW SRM 51-41-01. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: CLOSEOUT PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

WHILE IN HEAVY MAINT CHECK - FOUND CORROSION ON FWD CARGO CLOSE OUT PANEL BY FR 25. REMOVED AND REPLACED CLOSE OUT PANEL IAW SRM 51-40-02. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: FINGER DOUBLER — CORRODED (FRAMES 79-80) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

FOUND CORROSION IN THE AFT CARGO DOOR CUTOUT STRUCTURE FINGER DOUBLER. REMOVED AND REPLACED THE FINGER DOUBLER IAW SRM 51-40-08.

Part: SHEAR TIE — CORRODED (FRAME 84) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

FOUND CORROSION ON FRAME 84, STRINGER 27R SHEAR TIE. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-08.

Part: FLOORBEAM — CORRODED (FRAME 90) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

FOUND CORROSION ON THE AFT CABIN RT SIDE FLOORBEAM FRAME 90. REPAIRED IAW ETD2016-170-031513.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

WHILE IN HEAVY MAINT CHECK * MAJOR* FOUND CORROSION AFT CARGO SHEAR CLIPS AT FR 85 STR 27R-29R. REMOVED AND REPLACED SHEAR CLIPS AS REQUIRED IAW SRM 51-40-02,51-23-04 AND 51-40-08. ACFT REMAINS IN HEAVY MAINT CHECK UNTIL COMPLETION.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

WHILE IN HEAVY MAINT CHECK 8 MAJOR * FOUND CORROSION AFT CARGO SHEAR CLIPS AT FR 81 STR 27R-29R. REMOVED AND REPLACED SHEAR CLIPS IAW SRM 51-40-02, 51-40-08 AND 51-23-04. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

WHILE IN HEAVY MAINT CHECK * MAJOR * FOUND CORROSION AFT CARGO SHEAR CLIPS AT FR 83 STR 27R-29R. REMOVED AND REPLACED SHEAR CLIPS. IAW SRM 51-40-08. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

WHILE IN HEAVY MAINT CHECK * MAJOR * FOUND CORROSION AFT CARGO SHEAR CLIPS AT FR 82 STR 27R-29R. REMOVED AND REPLACED SHEAR CLIPS. IAW SRM 51-40-08. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

WHILE IN HEAVY MAINT CHECK * MAJOR * FOUND CORROSION AFT CARGO INTERNAL DOUBLER FOR DRAIN MAST AT FR 86-87 STR 26R-28R. REMOVED AND REPLACED INTERNAL DOUBLER FOR AFT DRAIN MAST IAW SRM 51-40-08. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: SLIDE — CRACKED (PAX DOOR) · airframe 23,785 hrs · 17,865 cycles

WHILE ACFT IN HEAVY MAINT CHECK - AFT PAX DOOR EMERGENCY EVACUATION SLIDE BACK STRUCTURE CRACKED AROUND TOP FASTENER. EVACUATION SLIDE ASSY WAS REMOVED AND REPLACED IAW AMM 25-65-01. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

WHILE IN HEAVY MAINT CHECK * MAJOR* FOUND CORROSION ON AFT CARGO SHEAR CLIPS AT FR 88 STR 27R-29R. REMOVED AND REPLACED SHEAR CLIPS IAW SRM 51-23-04 AND 51-40-02. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

WHILE IN HEAVY MAINT CHECK *MAJOR* FOUND CORROSION IN AFT CARGO SHEAR CLIPS FR 86 STR 27R -28R. REMOVED AND REPLACED SHEAR CLIPS IAW SRM 51-40-08. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

WHILE IN HEAVY MAINT CHECK *MAJOR* FOUND CORROSION IN AFT CARGO SHEAR CLIPS FR 87 STR 27R -28R. REMOVED AND REPLACED SHEAR CLIPS IAW SRM 51-40-08. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: CLOSEOUT PANEL — CORRODED (FRAMES 77-80) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

CORROSION ON THE AFT CARGO CLOSEOUT PANEL. REMOVED AND REPLACED THE AFT CARGO CLOSEOUT PANEL IAW AMM 20-10-01.

Part: SUPPORT BRACKET — CORRODED (FRAMES 86-87) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

SUPPORT BRACKET ON THE DRAIN MAST SUPPORT FRAMES 86 - 87, STRINGERS 26R - 28R. REMOVED AND REPLACED THE SUPPORT BRACKET.

Part: SUPPORT — CORRODED (FRAMES 80-81) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

CORRODED PANEL SUPPORT BETWEEN FRAMES 80 AND 81, STRINGER 27R. REMOVED AND REPLACED THE PANEL SUPPORT IAW SRM 51-40-08.

Part: SUPPORT — CORRODED (FRAME 80) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

AFT CARGO PANEL SUPPORT AT FRAME 80, STRINGER 27R. REPLACE THE PANEL SUPPORT.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

LT FLOOR DOUBLER CORRODED AS MARKED FR 80. REMOVED AND REPLACED FR 80 STGR 26R - 28R REF SRM 51-40-08, SRM 51-40-02.

Part: STAND OFF — CORRODED (FRAME 88) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

WASTE WATER SERVICE BOX WIRE STAND OFF IS NOT ATTACHED AND CORRODED. REMOVED AND REPLACED THE STAND OFF IAW SRM 51-40-08.

Part: SPLICE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

LT SPLICE, FRAMES 87 - 88. REMOVED DAMAGED AREA ON THE LT SPLICE. FOUND WITHIN LIMITS. IAW SRM 51-70-12.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

LEFT SHEAR PANEL FRAMES 87 - 88. REMOVED AND REPLACED THE SHEAR PANEL IAW SRM 51-40-08, SRM 51-23-04, AND SRM 51-40-02.

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

RIGHT SHEAR PLATE, FRAMES 87 - 88. REMOVED AND REPLACED THE SHEAR PANEL IAW SRM 51-40-08 .

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

CENTER GUSSET PLATE FRAME 90. REMOVED AND REPLACED THE GUSSET IAW SRM 51-40-08.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

CENTER GUSSET PLATE FRAME 90 CORRODED. REMOVED AND REPLACED THE GUSSET IAW SRM 51-40-08.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

CENTER SHEAR PANEL FRAMES 87 - 88. REMOVED AND REPLACED THE SHEAR PANEL IAW SRM 41-40-08.

Part: FRAME SPLICE — CORRODED (FRM 90) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

CENTER FRAME SPLICE 90. REPLACED FRAME SPLICE IAW SRM 51-40-08.

Part: SUPPORT — CORRODED (FRAMES 88-90) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

LT AFT PANEL SUPPORT FRAMES 88 - 90. REMOVED AND REPLACED THE PANEL SUPPORT IAW SRM 51-40-02 , AND 51-40-08.

Part: FLOORBEAM — CORRODED (FRAME 16) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

FWD RIGHT FLOORBEAM CORRODED, FRAME 16. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-41-01.

Part: SEAT TRACK — CORRODED (FRAMES 18-20) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

FWD LT SEAT TRACK CORRODED FRAMES 18 - 20. REMOVED ANP REPLACED THE SEAT TRACK IAW SRM 51-40-08, AND SRM 51-40-02 .

Part: DOUBLER — CORRODED (FRAME 16) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

LEFT FLOOR DOUBLER CORRODED, FRAME 16. REPLACED THE DOUBLER IAW EAMS W/O H6152.

Part: SEAT TRACK — CORRODED (FRAMES 16-17) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

FWD RIGHT SEAT TRACK CORRODED, FRAMES 16 - 17. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-08.

Part: FLOOR SUPPORT — CORRODED (FRAMES 15-16) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

LEFT FLOOR SUPPORT CORRODED BETWEEN FRAMES 15 - 16. REPLACED THE FLOOR SUPPORT .

Part: DOUBLER — CORRODED (FRAME 19) · corrosion level 2 · airframe 23,785 hrs · 17,865 cycles

LEFT FLOOR DOUBLER CORRODED AT FRAME 19. REMOVED ANP REPLACED THE DOUBLER IAW SRM 51-40-08, AND SRM 51-40-02.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,127 hrs · 16,775 cycles

EMERGENCY LIGHT INOPERATIVE IN FIRST CLASS SECTION. R & R THE NR 2 ELPU IAW AMM 33-50-01. PERFORMED ELPU FULL CHARGE IAW AMM 33-50-01.