N213JQ

Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 37,787 hrs · 27,800 cycles

CAPTAIN WINDOW CRACKING IN FLIGHT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND TO BE MOISTURE INGRESS GIVING CRACKING APPEARANCE.

Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 37,549 hrs · 27,625 cycles

WINDSHIELD SHOWED SIGN OF CRACKS NEAR LOWER RIGHT CORNER ON CA SIDE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. CA WINDSHIELD WAS NOT CRACKED, IDENTIFIED AS DELAMINATION ALREADY ON DMI. DELAMINATION IS WITHIN LIMITS.

Part: SKIN — CRACKED (ZONE 600) · airframe 35,827 hrs · 26,239 cycles

DURING OVERNIGHT INSPECTION FOUND RH WING LOWER SKIN CRACKED JUST INBD OF RIB 17 AND JUST AFT OF FWD SPAR APROX 1.2 INCHES LONG. REPAIRED IAW ETD2025-170-901928 ALSO REF VP-002193-2025 N/R #3 FOR WORK ACCOMPLISHED.

Part: FLOOR SUPPORT — CORRODED (FRMS 86-89) · corrosion level 2 · airframe 33,583 hrs · 24,445 cycles

CF3 AFT IB FLOOR SUPPORT FR 86 FR89 FOUND CORRODED. MX REPLACED BEAM IAW SRM 51-40-08

Part: ANGLE — CORRODED (FRM 12) · corrosion level 2 · airframe 33,583 hrs · 24,445 cycles

CORRODED FLOOR BEAM PANEL SUPPORT ANGLE FOUND CORRODED AT FR 12 LBL21. MX REPLACED ANGEL IAW SRM 51-41-01

Part: SEAL REST — CORRODED (FWD CARGO DOOR) · corrosion level 2 · airframe 33,583 hrs · 24,445 cycles

FWD CARGO AFT LOWER SEAL RETAINER FOUND CORRODED. MX REPLACED SEAL REST IAW AMM 21-10-01 TABLE 201 AND 206

Part: SUPPORT FITTING — CORRODED (FRM 16 LBL 46) · corrosion level 2 · airframe 33,583 hrs · 24,445 cycles

CORRODED FLOOR SUPPORT TUB FITTING FOUND FR 16 LBL 46. MX REPLACED SUPPORT IAW SRM 51-43-03

Part: SEAL REST — CORRODED (FWD CARGO DOOR) · corrosion level 2 · airframe 33,583 hrs · 24,445 cycles

FWD CARGO FWD LOWER SEAL RETAINER FOUND CORRODED. MX REPLACED SEAL REST IAW AMM 21-10-01 TABLE 201 AND 206

Part: DOOR — CORRODED (WASTE) · corrosion level 2 · airframe 33,583 hrs · 24,445 cycles

CF3 FR86-89 STR26R-28R FOUND TO HAVE CORRODED WASTE DOOR. MX REPLACED DOOR IAW SRM 51-41-02

Part: RIB — CRACKED (VERTICAL STAB) · airframe 27,660 hrs · 19,887 cycles

WHILE AC WAS IN FOR HVY CK FOUND VERTICAL STAB REAR SPAR AFT FACE CRACK FOUND AT RIB 9/10. REPLACED V-STAB AFT RIB 9/10 PN 170-63629-005. IAW SRM 51-41-02, 51-41-01. SEE AAR NRC # 4500889-3000-0034 FOR WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.

Part: SEAT TRACK — CORRODED (FRM 19) · corrosion level 2 · airframe 27,660 hrs · 19,887 cycles

CORROSION ON FWD L/H I/B SEAT TRACK AT FR-19. REPLACED IAW SRM 51-41-01, 51-41-02, 51-43-03, 51-43-04 & 51-21-01

Part: GUSSET — CORRODED (FRM 90) · corrosion level 2 · airframe 27,660 hrs · 19,887 cycles

WHILE AC WAS IN FOR HVY CK FOUND CF3 FLOOR STRUCTURE CORROSION FOUND ON GUSSET PLATE RH SIDE AT FR 90. REPLACED GUSSET PLATE PN 170-60259-001 IAW SRM 51-41-02. SEE AAR NRC# 4500889-1000-0116 FOR WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.

Part: SEAT TRACK — CORRODED (FRMS 86-84) · corrosion level 2 · airframe 27,660 hrs · 19,887 cycles

WHILE AC WAS IN FOR HVY CK FOUND CENTER FUSELAGE III FRAME 90 STRINGER 28L EXTERNAL SKIN SHEAR CLIP HAS CORROSION SEAT TRACK PN 170-86081-005 REPLACED IAW SRM 51-53-03, 51-43-04. SEE AAR NRC 4500889-1000-0084 FOR WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 27,660 hrs · 19,887 cycles

RH H-STAB RIB 11A CRACKED. REPLACED IAW REPUBLIC AIRLINES EO. 170EO-55-10-0004_1 "MAJOR"

Part: POWER UNIT — INOPERATIVE (CABIN) · airframe 26,215 hrs · 18,613 cycles

AISLE EMERGENCY LIGHT ABOVE ROW 6 INOP. R&R ELPU 2.

Part: GIRT BAR — CORRODED (AFT SERVICE DOOR) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND -MAJOR -AFT SERVICE DOOR LOWER BEAM HAS SURFACE CORROSION AROUND GIRT BAR FITTINGS, REMOVED AND REPLACED R2 DOOR LOWER THRESHOLD BEAM REF EMB SRM 51-40-08,RESTORED SURFACE PROTECTION REF. E175 SRM 51-10-04, 51-10-05, AND 51-10-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION

Part: FINGER DOUBLER — CORRODED (FRAMES 24-26) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND - MAJOR - FWD CARGO BAY LOWER HORIZONTAL BEAM FWD FINGER DOUBLER CHAFED AND CORRODED,REMOVED AND REPLACED FWD CARGO FWD FINGER DOUBLER REF SRM 51-40-08,RESTORED SURFACE PROTECTION REF. E175 SRM 51-10-04, 51-10-05, AND 51-10-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: DOUBLER — CORRODED (WASTE SERVICE) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND - MAJOR- WASTE SERVICE BOX DOUBLER TO HAVE EVIDENCE OF CORROSION,REMOVED AND REPLACE WASTE SERVICE BOX SKIN DOUBLER AT FR87-FR88,REF E175 SRM 51-40-08, RESTORED SURFACE PROTECTION REF. E175 SRM 51-23-04, 51-23-05, 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND CORROSION ON RT INBD PAX SEAT TRACK FRAME 74-84. REMOVED RT INBD PAX SEAT TRACK FRAME 74-84. INSTALLED NEW RT INBD SEAT TRACK FR74-84. APPLIED TOPCOAT AND CIC TO RT INBD SEAT TRACK FR74-84. REF SRM 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND CORROSION ON LT CENTER(FIRST CLASS) PAX SEAT TRACK FRAME 23-29. REMOVED DAMAGED SECTION AND INSTALLED FABRICATED PARTS FOR LT INBOARD FIRST CLASS SEAT TRACK SPLICE, REF ETD2018-170-128047 AND SRM 53-00-10 R/01, RESTORED SURFACE PROTECTION REF SRM 51-10-04, 51-10-05, AND 51-10-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND RT SEAT TRACK FR12-FR21 HAS CORROSION BETWEEN FR14-FR16 AS MARKED. REMOVED RT SEAT TRACK FR12-FR21. REF SRM 51-40-08, INSTALLED RT SEAT TRACK FR12-21 REF SRM 51-40-08 APPLIED SURFACED PROTECTION TO RT SEAT TRACK AT FR 14-16 REF SRM 51-23-06 CPM 51-25-00. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND RT SHEAR PLATE, FOUND CORROSION ON UNDERLYING STRUCTURE. REMOVED AND REPLACED U-CHANNEL REF SRM 51-40-08 RESTORED SURFACE PROTECTION REF SRM 51-10-04, 51-10-05, AND 51-10-06.ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: SEAL REST — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND CORROSION ON THE AFT SERVICE DOOR SEAL REST SUPPORT. REMOVED AND REPLACED AFTER SERVICE DOOR CENTER SEAL REST REF SRM 51-40-08, SRM 5121-02, AND SRM 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND CORROSION ON LT OUTBD PAX SEAT TRACK FRAME 74-84. REMOVED AND REPLACED LT OUTBD SEAT TRACK AT FRAME 74-84 REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: SEAL REST — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND AFT CARGO CUTOUT STRUCTURE HAS CORROSION AROUND 2EA FASTENER HOLES WHERE METAL PROTECTIVE PLATE ATTACHES. REMOVED DAMAGE FROM AFT CARGO CUTOUT STRUCTURE ON FWD AND AFT CORNER SEAL REST AROUND 2EA FASTENER HOLES WHERE METAL PROTECTIVE PLATE ATTACHES REF SRM 51-10-03. REMOVED DAMAGED AFT CARGO DOOR AFT SEAL REST FITTING. LOCATED, AND DRILLED NEW AFT CARGO DOOR AFT SEAL REST FITTING REF SRM 51-40-08, 51-40-02. REMOVED DAMAGED AFT CARGO DOOR FWD SEAL REST FITTING, LOCATED, AND DRILLED NEW AFT CARGO DOOR FWD SEAL REST FITTING REF SRM 51-40-08, 51-40-02. INSTALLED AFT CARGO DOOR LOWER FWD AND AFT CORNER SEAL REST FITTINGS REF SRM 51-40-08. APPLIED TOP COAT TO SEAL RESTS AT AFT CARGO DOOR REF SRM 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: SEAL REST — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND AFT CARGO DOOR CUTOUT LOWER CENTER SEAL REST CORRODED. REMOVED AND REPLACED SEAL REST REF SRM 51-40-08, RESTORED SURFACE PROTECTION REF SRM 51-10-04, 51-10-05, AND 51-10-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND CORROSION/ CHAFING ON RT OUTBD PAX SEAT TRACK FRAME 23-34/43. REMOVED AND INSTALLED NEW SEAT TRACK AT FR 23/34 TO 43 REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06. APPLIED CIC REF CPM 51-25-00. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND CORROSION ON RT OUTBD PAX SEAT TRACK FRAME 74-84. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK AT FR 74-84 REF SRM 51-40-08 AND ETD2018-170-129236. RESTORED SURFACE PROTECTION REF SRM 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND FORWARD RT SILL FR12-FR14 HAS CORROSION, REMOVED AND REPLACED SILL REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-10-04, 51-10-05, AND 51-10-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: FLOOR SUPPORT — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND CORROSION ON RH UPPERSHEET FRAME 85-86 AFT WET AREA, REMOVED RH UPPERSHEET FRAME 85-86 AFT WET AREA. REF SRM 51-40-08.INSTALLED NEW RH UPPERSHEET FRAME 85-86 AFT WET AREA. REF SRM 51-40-08,RESTORED SURFACE PROTECTANT TO BOTTOM SIDE OF RH UPPERSHEET FASTENERS. REF SRM51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: FLOOR SUPPORT — CORRODED (FRAMES 86-89) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA LH BEAM Y=-10.748" FRAME 86-89,REMOVED CENTER FUSELAGE III WET AREA LH BEAM Y=-10.748" FRAME 86-89 PER EMB SRM 51-40-08. INSTALLED CENTER FUSELAGE III WET AREA LH BEAM Y=-10.748" FRAME 86-89 PER EMB SRM 51-40-08 . RESTORED SURFACE PROTECTION REF SRM 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: BEAM — CORRODED (FRAMES 86-89) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE THE ACFT IN HEAVY CHECK MAINT FOUND CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 RH BEAM. REMOVED AND REPLACED CENTER FUSELAGE III WET AREA 53-23 R/H BEAM Y=+10.748". REF: SRM 51-40-08. RESTORED SURFACE PROTECTION REF. E175 SRM 51-10-04, 51-10-05, AND 51-10-06. ACFT REMAIN IN HEAVY CHECK UNTIL COMPLETION.

Part: SPLICE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA LH SPLICE FRAME 87-88, REMOVED, LOCATED, DRILLED, AND COUNTERSUNK CENTER FUSELAGE III WET AREA LH SPLICE FRAME 87-88. REF SRM 51-40-08, 51-40-02, 51-40-04. INSTALLED CENTER FUSELAGE III WET AREA 53-23 LH SPLICE FRAME 87-88. REF SRM 51-40-08 APPLIED SURFACE PROTECTION TO CENTER FUSELAGE III WET AREA LH SPLICE FRAME 87-88. REF SRM 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA LH SHEAR PLATE FRAME 87-88,REMOVED LH SHEAR PANEL FRAME 87-88INSTALLED LH SHEAR PANEL FRAME 87-88 PER EMB SRM 51-40-08. APPLIED SURFACE PROTECTION TO LH SHEAR PANEL FRAME 87-88 PER EMB SRM 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION. .

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA LH CENTER GUSSET PLATE FRAME 90,REMOVED CENTER FUSELAGE III WET AREA 53-23 LH CENTER GUSSET PLATE FRAME 90 REF: EMB SRM 51-40-08. INSTALLED NEW CENTER FUSELAGE III WET AREA 53-23 LH CENTER GUSSET PLATE FRAME 90. REF: EMB SRM 51-21-01, SRM 51-40-08, APPLIED SURFACE PROTECTION TO CENTER FUSELAGE III WET AREA 53-23 LH CENTER GUSSET PLATE FRAME 90. REF: EMB SRM 51-23-05, SRM 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 LH GUSSET PLATE FRAME 90, REMOVED CENTER FUSELAGE III WET AREA 53-23 LH GUSSET PLATE FRAME 90. REF: EMB SRM 51-40-08. INSTALLED NEW CENTER FUSELAGE III WET AREA 53-23 LH GUSSET PLATE FRAME 90. REF: EMB SRM 51-21-01, SRM 51-40-08,APPLIED SURFACE PROTECTION TO CENTER FUSELAGE III WET AREA 53-23 LH GUSSET PLATE FRAME 90. REF: EMB SRM 51-23-05, SRM 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA RH CENTER GUSSET PLATE FRAME 90.REMOVED CENTER FUSELAGE III WET AREA RH CENTER GUSSET PLATE FRAME 90 REF: EMB SRM 51-40-08. INSTALLED NEW CENTER FUSELAGE III WET AREA RH CENTER GUSSET PLATE FRAME 90 REF: EMB SRM 51-21-01, SRM 51-40-08.APPLIED SURFACE PROTECTION TO CENTER FUSELAGE III WET AREA RH CENTER GUSSET PLATE FRAME 90. REF: EMB SRM 51-23-05, SRM 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 RH SHEAR PLATE FRAME 87-88. REMOVED AND REPLACED RH SHEAR PANEL @ FR87-FR88 REF EMB SRM 51-40-08. RESTORED SURFACE PROTECTION REF. E175 SRM 51-10-04, 51-10-05, AND 51-10-06. ACFT REMAIN IN HEAVY CHECK UNTIL COMPLETION

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 RH GUSSET PLATE FRAME 90. REMOVED AND REPLACED GUSSET REF: SRM 51-40-08,RESTORED SURFACE PROTECTION REF. E175 SRM 51-10-04, 51-10-05, AND 51-10-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: SPLICE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 RH SPLICE FRAME 87-88. REMOVED RH SPLICE @ FR87-88 REF EMB SRM 51-40-08 DRILLED AND TREATED NEW RH SPLICE PLATE,INSTALLED NEW RH SPLICE @ FR87-FR88 REF EMB SRM 51-40-08 APPLIED SURFACE PROTECTION REF SRM 51-23-05. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA CENTER SHEAR PANEL FRAME 87-88,EMOVED, LOCATED AND DRILLED CENTER FUSELAGE III WET AREA CENTER SHEAR PANEL FRAME 87-88 PER SRM 51-40-08, 51-40-02. INSTALLED CENTER FUSELAGE III WET AREA 53-23 CENTER SHEAR PANEL FRAME 87-88 PER SRM 51-40-08,APPLIED SURFACE PROTECTION TO CENTER FUSELAGE III WET AREA CENTER SHEAR PANEL FRAME 87-88 PER SRM 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE IN HEAVY CHECK MAINT FOUND CORROSION ON LT OUTBD PAX SEAT TRACK APPROX FRAME 21. REMOVED AND REPLACE LT OUTBD SEAT TRACK AT FRAME 17-21 REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-04, 51-23-05, 51-23-06. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.,

Part: INTERCOSTAL — CORRODED (FRAME 90-91) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA RH INTERCOSTAL JUST AFT OF RH GUSSET PLATE FRAME 90,REMOVED CENTER FUSELAGE III WET AREA RH INTERCOSTAL JUST AFT OF RH GUSSET PLATE FRAME 90, DRILLED UP NEW INTERCOSTAL AND PREPPED FOR INSTALLATION REF: EMB SRM 51-23-04,51-40-02,51-40-08. COMPLETED INSTALLATION OF NEW CENTER FUSELAGE III,APPLIED SURFACE PROTECTION TO CENTER FUSELAGE III WET. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: REINFORCEMENT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE IN HEAVY CHECK MAINT FOUND CORROSION STRUCTURAL CENTER FUSELAGE III DRY AREA RT FRAME 84 REINFORT STRUCTURE. REMOVED AND REPLACED CENTER FUSELAGE III DRY AREA RT FRAME 84 REINFORT STRUCTURE SRM 51-40-08. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION.

Part: FLOOR SUPPORT — CORRODED (FRAMES 87-90) · corrosion level 2 · airframe 22,971 hrs · 16,169 cycles

WHILE ACFT IN HEAVY CHECK MAINT FOUND CORROSION STRUCTURAL CENTER FUSELAGE III WET AREA 53-23 RH AFT PANEL SUPPORT FRAME 87-90. REMOVED CENTER FUSELAGE III WET AREA 53-23 RH AFT PANEL SUPPORT FRAME 87-90. REF: EMB SRM 51-40-08. APPLIED SURFACE PROTECTION TO CENTER FUSELAGE III WET AREA 53-23 RH AFT PANEL SUPPORT FRAME 87-90. REF: EMB SRM 51-23-05, SRM 51-23-06, ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETION

Part: TRIM PANEL — OUT OF POSITION (L1 DOOR) · airframe 17,672 hrs · 12,855 cycles

L1 DOOR WILL NOT LOCK FULLY INTO OPEN POSITION. ADJUSTED DOOR HINGE TRIM, CHECKS GOOD IAW MM 52-11-00.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,626 hrs · 12,828 cycles

LEVEL 2 CORROSION - CORROSION ON THE COCKPIT FLOOR STRUCTURE AFT OF THE COPILOT'S INBOARD SEAT TRACK. REPAIRED CORROSION ON COCKPIT FLOOR STRUCTURE REF ETD2016-170-084056 REV A.

Part: SUPPORT — CORRODED (LT MLG WW) · corrosion level 2 · airframe 17,626 hrs · 12,828 cycles

LEVEL 2 CORROSION - LT MLG UPLOCK SUPPORT CORRODED AT UPPER AFT OUTBOARD UPLOCK. R&R LT MLG AFT SUPPORT FOR UPLOCK ASSEMBLY.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 17,626 hrs · 12,828 cycles

LEVEL 2 CORROSION, MAJOR REPAIR - CORROSION, CENTER CROSSBEAM AT FR 17 BEHIND THE LT AND RT SEAT TRACK. BLENDED AFFECTED AREA, PERFORMED HFEC, INSTALLED REPAIR ANGLE REF ETD2016-170-015447.

Part: GUSSET — GOUGED (SERVICE DOOR) · airframe 17,626 hrs · 12,828 cycles

MAJOR REPAIR - GOUGE ON FWD SERVICE DOOR INTERIOR SKIN STRUCTURE CENTER GUSSET, AREA COVERED BY SLIDE. R&R CENTER GUSSET RT FWD SERVICE DOOR REF SRM 51-41-01 AND 51-43-05.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,626 hrs · 12,828 cycles

LEVEL 2 CORROSION - CORROSION ON LT IB SEAT TRACK BEAM FR 17/19. R&R SEAT TRACK P/N: 170-03264-001 REF SRM 51-41-02, 51-23-06.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,626 hrs · 12,828 cycles

LEVEL 2 CORROSION - FWD LT FLOOR SILL CORRODED AS MARKED AT FR 16. R&R FLOOR SILL 170-03275-005.

Part: SLIDE — PARTIAL DEPLOY (L1 DOOR) · airframe 17,135 hrs · 12,495 cycles

L1 SLIDE DEPLOYED SLIGHTLY AT THE GATE WITH AGENT OPENING. R & R L1 DOOR SLIDE IAW AMM 25-65-01.

Part: LIGHT — NO TEST (CABIN) · airframe 15,786 hrs · 11,622 cycles

TWO FWD MOST RT EMERGENCY LIGHT STRIPS FAILED A LIGHT OPERATIONAL TEST. R & R THE EMERGENCY LIGHT STRIPS IAW AMM 33-50-21.

Part: DOOR — OUT OF ADJUST (L1) · airframe 15,380 hrs · 11,371 cycles

L1 DOOR HARD TO OPEN/CLOSE. ADJUSTED L1 DOOR HOIST STOPS, OPS CHECK GOOD REF AMM 52-11-00.

Part: DOOR — OUT OF ADJUST (MAIN CABIN) · airframe 15,283 hrs · 11,303 cycles

MAIN CABIN DOOR STICKING WHEN OPENED. PERFORMED ADJUSTMENT & TEST OF DOOR IAW AMM 52-11-00.

Part: DOOR — LACK OF LUBE (MAI PAX) · airframe 15,277 hrs · 11,297 cycles

GATE AGENT CAN'T OPEN MAIN CABIN DOOR. PERFORMED GVI OF L1 DOOR, CLEANED AND LUBED SLIDES AND ROLLERS. DOOR OPS CHECKS GOOD IAW AMM 52-10-00.

Part: GLOWSTRIP — INOPERATIVE (SEAT 1A) · airframe 14,898 hrs · 11,054 cycles

GLOWSTRIP NEXT TO SEAT 1A DOES NOT GLOW. R & R THE GLOWSTRIP IAW MM 25-24-01.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 13,103 hrs · 9,961 cycles

FWD MOST RT EMERGENCY LIGHT NOT WORKING PROPERLY. R & R THE EMERGENCY LIGHT IAW AMM 33-50-21. OPS CHECKED GOOD.

Part: GIRT BAR — OUT OF ALIGNMENT (R1 DOOR SLIDE) · airframe 12,540 hrs · 9,590 cycles

R1 DOOR WOULD NOT ARM. FOUND GIRT BAR OUT OF ALIGNMENT. ADJUSTED, OPS CHECK GOOD.

Part: STEERING SYS — WARNING LIGHT (NLG) · airframe 12,422 hrs · 9,516 cycles

STEERING FAILED DURING APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT, TOWED TO GATE. PERFORMED ADJUSTMENT AND TEST IAW AMM 32-50-00. CHECKED GOOD.

Part: CABLE — FAILED (R2 DOOR SLIDE) · airframe 12,352 hrs · 9,472 cycles

R2 DOOR WILL NOT ARM. R & R AFT SERVICE DOOR EMERGENCY SLIDE FLEXBALL CABLE IAW AMM 52-42-40 AND 52-42-41. ADJUSTED AND OPS CHECKED GOOD IAW AMM 52-42-40.

Part: PLATE — OUT OF ADJUST (R2 DOOR AREA) · airframe 11,777 hrs · 9,064 cycles

R2 DOOR IS DIFFICULT AND VERY STIFF WHEN DISARMING. INSPECTED AND FOUND R2 AFT FLOOR PLATE OUT OF ADJUSTMENT. ADJUSTED R2 AFT FLOOR PLATE IAW AMM 52-42-00. OPERATIONALLY CHECKS GOOD AT THIS TIME.

Part: DOOR — LACK OF LUBE (R2) · airframe 11,772 hrs · 9,060 cycles

UNABLE TO DISARM R2 DOOR. CLEANED, LUBED, AND SECURED R2 DOOR IAW AMM 52-12-20. OPS CHECKED GOOD.

Part: SPAR — CRACKED (LT WING) · airframe 11,772 hrs · 9,060 cycles

LT WING LOWER SPAR AT RIB 10 A2 HOLE HAS CRACK INDICATIONS. COMPLIED WITH LT WING A2 SPAR II CRACK REPAIR TEMP REF ETD2014-170-015615, REV C. MAJOR REPAIR.

Part: SEAL SEAT — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,768 hrs · 9,057 cycles

CORROSION, CENTER SEAL REST FWD CARGO BAY. R & R SEAL REST, PN 170-66804-401.

Part: SEAL SEAT — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON CENTER SEAL REST IN FWD CARGO. R & R SEAL REST. MAJOR REPAIR.

Part: FINGER DOUBLER — GOUGED (ZONE 100) · airframe 11,768 hrs · 9,057 cycles

GOUGED FOUND ON FWD FINGER DOUBLER IN FWD CARGO. R & R FINGER DOUBLER. MAJOR REPAIR

Part: SEAL SEAT — CORRODED (ZONE 100) · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON AFT SEAL REST IN FWD CARGO. R & R SEAL REST. MAJOR REPAIR.

Part: SEAL SEAT — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON AFT SEAL REST FWD CARGO. R & R SEAL REST.

Part: CLOSEOUT PANEL — CORRODED (FWD CARGO BAY) · corrosion level 2 · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON FWD CARGO CLOSE OUT PANEL. R & R PANEL 170-67451-001.

Part: FINGER DOUBLER — GOUGED (ZONE 100) · airframe 11,768 hrs · 9,057 cycles

AFT FINGER DOUBLER GOUGED IN FWD CARGO. R & R FINGER DOUBLER. MAJOR REPAIR

Part: SUPPORT — CORRODED (WNG TO FUSE FAIR) · corrosion level 2 · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON FWD WING TO FUSELAGE FARING AFT NUTPLATE SUPPORT FLANGE HAS CORROSION AROUND NUTPLATES. REMOVED CORROSION. REWORKED AREA PERMITTED TO EXIST AS PERMANENT REPAIR REF ETD2014-170-016736, RESTORED SURFACE PROTECTION.

Part: SKIN — DENTED (SERVICE DOOR) · airframe 11,768 hrs · 9,057 cycles

TWO DENTS IN FWD SERVICE DOOR. DENT ONE ADDRESSED WITH ETD 2011-170-102905 PREVIOUSLY. DENT TWO HAS BEEN CONTOURED TO WITHIN LIMITS IAW ETD 201-170-016384.

Part: UPPER SHEET — CORRODED (ZONE 100) · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON LT UPPER SHEET FRAME 85-86. R & R UPPER SHEET.

Part: SUPPORT — CORRODED (FRAME 86) · corrosion level 2 · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON PANEL SUPPORT RT FRAME 86. R & R SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FRAMES 86-90) · corrosion level 2 · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON RT FLOOR SUPPORT FRAMES 86-90. R & R SUPPORT SUPPORT.

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON FLOOR DOUBLER AT FRAMES 13-16. R & R DOUBLER.

Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON LEFT SHEAR PLATE FRAMES 87-88. R & R SHEAR PLATE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-14) · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON RT FWD FLOOR SUPPORT FRAMES 12-14. R & R FLOOR SUPPORT.

Part: SEAT TRACK — CORRODED (FRAMES 12-20) · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON RT SEAT TRACK FRAMES 12-20. R & R SEAT TRACK.

Part: BEAM — CORRODED (FRAMES 86-89) · corrosion level 2 · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON LT BEAM AT FRAMES 86-89. R & R BEAM.

Part: FLOOR SUPPORT — CORRODED (FRAME 85) · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON RT FLOOR SUPPORT AT FRAME 85. R & R FLOOR SUPPORT.

Part: DOUBLER — CORRODED (ZONE 100) · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON FLOOR PANEL DOUBLER FRAMES 19-20. R & R DOUBLER.

Part: SEAT TRACK — CORRODED (FRAMES 12-20) · corrosion level 2 · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON LT SEAT TRACK FRAMES 12-20. R & R SEAT TRACK.

Part: MOUNT — CORRODED (LAVATORY) · corrosion level 2 · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON LAVATORY TIE DOWN SUPPORT FRAME 16 LT. R & R SUPPORT.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON RT GUSSET PLATE FRAME 90. R & R GUSSET PLATE.

Part: SPLICE — CORRODED (FRAME 90) · corrosion level 2 · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON FLOOR SPLICE LT CENTER FRAME 90. R & R LT CENTER FLOOR SPLICE.

Part: FLOORBEAM — CORRODED (FRAME 84) · corrosion level 2 · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON FLOORBEAM FRAME 84. REMOVED CORROSION AND REPAIRED FLOORBEAM IAW ETD2014-170-015495. MAJOR REPAIR

Part: SPLICE — CORRODED (FRAME 90) · corrosion level 2 · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON SPLICE FRAME 90. R & R SPLICE.

Part: UPPER SHEET — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON RT UPPER SHEET FRAMES 85-86. R & R UPPER SHEET.

Part: FLOORBEAM — CORRODED (FRAME 14) · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON FLOORBEAM FRAME 14 BETWEEN Y=+10.748 AND FUSALAGE RT. REMOVED CORROSION & INSTALLED ANGLE SUPPORT DOUBLER. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-16) · corrosion level 2 · airframe 11,772 hrs · 9,060 cycles

CORROSION FOUND ON LT FWD FLOOR SUPPORT BETWEEN FRAMES 12-16. R & R FLOOR SUPPORT.

Part: SPLICE — CORRODED (FRAME 89) · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON RT CENTER SPLICE FRAME 89. R & R SPLICE.

Part: SEAT TRACK — CORRODED (FRAME 84) · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON SEAT TRACK AT FRAME 84. REPAIRED SEAT TRACK IAW ETD2014-170-06110. MAJOR REPAIR

Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON RT SHEAR PLATE FRAMES 87-88. R & R SHEAR PLATE.

Part: GUSSET — CORRODED (ZONE 100) · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON FLOOR GUSSET LT FRAME 90. R & R GUSSET.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-20) · corrosion level 2 · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON RT AFT FLOOR SUPPORT FRAMES 17-20. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FRAME 85) · corrosion level 2 · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON LT FLOOR SUPPORT AT FRAME 85. R & R LT FLOOR SUPPORT.

Part: SHEAR PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON CENTER SHEAR PLATE FRAMES 87-88. R & R CENTER SHEAR PLATE.

Part: BEAM — CORRODED (FRAMES 86-89) · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON RT BEAM FRAMES 86-89. R & R BEAM.

Part: FLOOR SUPPORT — CORRODED (FRAMES 11-22) · corrosion level 2 · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON RIVET HEADS AT FLOOR SUPPORT BETWEEN FRAMES 11-22. R & R FLOOR SUPPORT.

Part: CROSSBEAM — CORRODED (FRAME 17) · airframe 11,768 hrs · 9,057 cycles

CORROSION FOUND ON CROSSBEAM FRAME 17 BETWEEN LT AND RT SEAT TRACK. REMOVED CORROSION BY BLENDING INSTALLED L-ANGLE SUPPORT DOUBLER ON CROSSFRAME, PN 170-21769-403. MAJOR REPAIR

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 11,647 hrs · 8,971 cycles

L2 EMERGENCY EXIT/SALIDA LIGHTED PLACARD INOPERATIVE. R & R AFT LT EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-50-01. OPS CHECK GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 10,167 hrs · 7,860 cycles

EMERGENCY LIGHT IN CABIN OVER COCKPIT INOPERATIVE. TROUBLESHOT IAW FIM 33-50-00, FOUND BAD FWD GALLEY BACKUP BATTERY. R & R FWD GALLEY BACKUP BATTERY IAW AMM 33-50-03. OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 7,687 hrs · 6,063 cycles

EMER LT BATT FAULT ON EICAS. PERFORMED TROUBLESHOOTING PER EMB 170 FIM 33-50-00-810-801, RESET MAU POWER AND PERFORMED OPS CHECK IAW AMM 33-50-00. NO DEFECTS NOTED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 6,548 hrs · 5,186 cycles

R2 EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY NR 4 IAW EMB 175 MM 33-50-01. OPS CHECK GOOD.

Part: SLIDE — DEFECTIVE (CABIN DOOR) · airframe 6,516 hrs · 5,160 cycles

F/A DISARMED MAIN CABIN DOOR AND WHEN GATE AGENT TRIED TO OPEN THE DOOR, THE DOOR APPEARED TO BE JAMMED AND THE GIRT BAR WAS STILL ATTACHED. REMOVED AND REPLACED L1 DOOR EVAC SLIDE IAW MM 25-65-01, NO DEFECTS NOTED. FWD PASSENGER DOOR ACT/LINKAGE CHECKS GOOD IAW EMB MM 52-11-20.

Part: GIRT BAR — UNSECURE (MAIN DOOR) · airframe 6,033 hrs · 4,817 cycles

MAIN DOOR GIRT BAR INDICATION SHOWS CLEAR WHEN ARMED. RE-SECURED GIRT BAR AS REQUIRED IAW EMB 170 MM 52-11-41. OPS CHECK GOOD.

Part: STRUCTURE — GOUGED (FUSELAGE) · airframe 5,956 hrs · 4,761 cycles

MAJOR REPAIR - GOUGE ON LT SIDE OF FUSELAGE AFT OF L1 DOOR BELOW PASS WINDOW, BETWEEN FR22-FR23 AND STR 14-STR 15. REPAIRED GOUGE IAW ETD2011-170-102930. PERFORMED HFEC AND FOUND CRACK IAW NDT MANUAL 51-00-00. CUT OUT CRACK AND GOUGE IAW EMB ETD 2010-170/00078 REV C. PERFOMED HFEC OF CUTOUT AREA IAW EMB NDT MANUAL 51-00-00, NO CRACKS NOTED. INSTALLED DOUBLER/REPAIR IAW EMB ETD 2011-170-102930. ALODINED, PRIMED, PAINTED, AND EDGE SEALED REPAIR IAW ETD 2011-170-102930.

Part: BATTERY — DISCHARGED (CABIN) · airframe 1,476 hrs · 1,225 cycles

EMERGENCY LIGHTS OVER ROWS 1 AND 6 WILL NOT ILLUMINATE WHEN EMERGENCY LIGHT SWITCH TURNED TO ON. MAINTENANCE REMOVED AND REPLACED THE FORWARD ELPU NR 2 IAW EMB 175 MM 33-50-01. OPS CHECK GOOD.