N748YX

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 47,892 hrs · 29,831 cycles

FWD FUSELAGE FLOOR STRUCTURE FOUND CORROSION ON RH INBD SEAT RACK BTWN FR20-23. MX REPLACED SEAT TRACK IAW SRM 51-43-03, 51-43-04, 51-41-01.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 47,892 hrs · 29,831 cycles

FWD FUSELAGE RH FLOOR SILL BTWN FR 17-20 RBL 48 FOUND CORRODED. MX REPLACED FLOOR SILL IAW SRM 51-41-02, 51-43-04.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 47,892 hrs · 29,831 cycles

FUSELAGE RH IM SEAT TRACK BTWN FR12-20 FOUND CORRODED. MX REPLACED SEAT TRACK IAW SRM 51-43-03, 51-43-04, 51-41-01, 51-41-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 47,892 hrs · 29,831 cycles

CF3 FLOOR STRUCTURE CORROSION FOUND ON RH PROFILE FLOOR SUPPORT BTWN FR88-90. MX REPLACED SUPPORT IAW SRM 51-42-01, 51-43-03.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 47,892 hrs · 29,831 cycles

AFT CARGO COMPARTMENT FR 84 BTWN STGR 27R -26R SHEAR CLIP CORRODED. MX REPLACED IAW SRM 51-41-01, 51-41-02.

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 47,892 hrs · 29,831 cycles

CF3 FLOOR STRUCTURE CORROSION FOUND ON RH GUSSET PLATE AT FR 90. MX REPLACED GUSSET IAW SRM 51-41-02

Part: SHEAR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 47,892 hrs · 29,831 cycles

CF3 FLOOR STRUCTURE CORROSION FOUND ON MID SHEAR PANEL BTWN FR87-88. MX REPLACED SHEAR PANEL IAW SRM 51-42-01.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 47,892 hrs · 29,831 cycles

CF3 FLOOR STRUCTURE CORROSION FOUND ON RH PROFILE SUPPORT AT FR 84. MX REPLACED IAW SRM 51-41-01, 51-41-02, 51-43-04.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 47,892 hrs · 29,831 cycles

AFT CARGO FR75 BTWN STR 29L-29R TWO SUPPORTS CORRODED. MX REPLACED SUPPORTS IAW SRM 51-41-01, 51-41-02.

Part: BEAM — CRACKED (ZONE 100) · airframe 47,892 hrs · 29,831 cycles

FWD FUSE NLG BAY UPPER BULKHEAD I-BEAM FOUND CRACKED ON LOWER FLANGE. MX REPLACED BEAM IAW ETD2025-170-000371

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 47,892 hrs · 29,831 cycles

AFT CARGO FR 74 BTWN STGR 29-28R SHEAR CLIP CORROSION. MX REPLACED SHEAR CLIP IAW SRM 51-41-01, 51-41-02, 51-43-02.

Part: DOUBLER — CRACKED (ZONE 200) · airframe 47,892 hrs · 29,831 cycles

****MAJOR****DMI R1250573/1 DENTS FOUND AT FR11-12 STR5-6L REPAIRED CRACK IAW SRM 53-10-01 REPAIR 12.

Part: SEAL REST — CORRODED (ZONE 100) · corrosion level 2 · airframe 47,892 hrs · 29,831 cycles

FWD CARGO DOOR CUTOUT FOUND CORROSION ON MID SEAL REST BTWN FR 25-26. MX REPLACED IAW SRM 51-41-01.

Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 47,892 hrs · 29,831 cycles

WASTE SERVICE DOOR FOUND CORROSION ON STOP NIPPLE BRACKET. MX REPLACED IAW SRM 51-41-02

Part: NONE — NONE · airframe 13,036 hrs · 8,871 cycles

BIRD STRIKE ON FWD FUSELAGE BELOW CAPTS WINDSHEIELD. REPAIRED DENT IAW ETD2023-170-005136. ALSO REF VP-008736-2023 N/R 2,3 FOR WORK PERFORMED.

Part: PANEL SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,589 hrs · 7,660 cycles

WHILE AC WAS IN FOR HVY CK FOUND FUSELAGE 3 FLOOR STRUCTURE GALLEY SUPPORT FITTING CORRODED BTWN FR 87-88, RBL 22.AAR MX REPLACED PANEL SUPPORT PN 170-86131-001 IAW SRM 51-43-01. AC REMAINS IN YQG FOR COMPLETION.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 11,589 hrs · 7,660 cycles

CORROSION FOUND AT FLOOR STRUCTURE R/H GUSET PLATE AT FR 90. R&R IAW SRM 51-41-02.

Part: UPPER SHEET — CORRODED (ZONE 200) · corrosion level 2 · airframe 11,589 hrs · 7,660 cycles

CORROSION FOUND AT FLOOR STRUCTURE R/H UPPER SHEET BTW FR 85-86. R&R IAW SRM 51-41-01 AND 51-43-01.

Part: PANEL SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,589 hrs · 7,660 cycles

WHILE AC WAS IN FOR HVY CK FOUND FUSELAGE 3 FLOOR STRUCTURE CORROSION FOUND ON RH PANEL SUPPORT BTWN FR 88-90. AAR MX REPLACED PANEL SUPPORT PN 170-86181-005 IAW SRM 51-42-01,51-43-01 AC REMAINS IN YQG FOR COMPLETION.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,589 hrs · 7,660 cycles

WHILE AC WAS IN FOR HVY CK FOUND PAX FLOOR STRUCTURE CORROSION FOUND ON LH IB SEAT TRACK CROWN TEETH BTWN FR19-20. AAR MX REPLACED SEAT TRACK PN 170-03264-001 IAW SRM 51-41-02, 51-43-03. AC REMAINS IN YQG FOR COMPLETION.

Part: SHEAR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,589 hrs · 7,660 cycles

WHILE AC WAS IN FOR HVY CK FOUND FUSELAGE 3 FLOOR STRUCTURE CORROSION FOUND ON RH SHEAR PANEL PN 170-91919-001 BTWN FR 87-88 AC REMAINS IN YQG FOR COMPLETION.

Part: HINGE — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,589 hrs · 7,660 cycles

WHILE AC WAS IN FOR HVY CK FOUND WASTE ACCESS DOOR HINGE FOUND WITH CORROSION. AAR MX REPLACED HINGE PN 170-85059-401 IAW SRM 51-41-02, 51-43-04,

Part: FRAME — CRACKED · airframe 11,589 hrs · 7,660 cycles

WHILE AC WAS IN FOR HVY CK FOUND LH FRAME 52 CRACKED (CRACK LENGTH 0.65" (SEQ 660) REPLACED FR 52 PN 171-19905-401 IAW SRM 51-41-01, 51-42-01, 51-43-03 THIS CLOSED DMI# R845164/1 AC RETURNED TO SERVICE.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 9,650 hrs · 6,357 cycles

EMERGENCY LIGHT BATTERY FAULT AND LIGHTS OVER ROWS 3 AND 8 ARE INOP. R&R FWD LH EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-50-01.

Part: SPAR — CRACKED (RT WINGLET) · airframe 7,155 hrs · 4,726 cycles

***WHILE A/C WAS OUT OF SERVICE FOR A HEAVY CHECK***RH WINGLET CRACKED AT FWD SPAR. REMOVED AND REPLACED RH WINGTIP IAW 170EO-57-30-0001_1. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SPAR — CRACKED (LT WINGLET) · airframe 7,155 hrs · 4,726 cycles

***WHILE A/C WAS OUT OF SERVICE FOR A HEAVY CHECK***LH WINGLET CRACKED AT FWD SPAR. REMOVED AND REPLACED LH WINGTIP IAW 170EO-57-30-0000_1. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SLIDE — PARTIAL DEPLOY (L1 DOOR) · airframe 6,579 hrs · 4,365 cycles

L1 DOOR SLIDE STARTED TO DEPLOY. SLIDE IS ENGAGED IN GIRT BAR. FERRIED TO IND. R&R L1 DOOR SLIDE, OPS CHECK GOOD REF AMM 25-65-01.

Part: LIGHT — DAMAGED (CABIN) · airframe 3,560 hrs · 2,468 cycles

PHOTOLUMINESCENT STRIP IN FRONT OF WARDROBE DAMAGED. R&R PHOTOLUMINESCENT STRIP PER AMM 33-50-21.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 1,085 hrs · 789 cycles

L1 DOOR EMERGENCY EXIT LIGHTED SIGN INOPERATIVE. R & R THE POWER SUPPLY IAW AMM 33-50-01.