N444YX

Part: ANGLE — CRACKED (FRM 52) · airframe 16,248 hrs · 10,887 cycles

FR 52 L ANGLE CRACKED LH SIDE AS MARKED. R&R L ANGLE ON LH SIDE AT FR 52. REF SRM 51-40-08.

Part: LIGHT — DAMAGED (CABIN) · airframe 13,270 hrs · 8,947 cycles

EMERGENCY FLOOR LIGHTING MCD BLEACHED OUT. R&R PHOTOLUMINESCENT INDICATOR STRIP LIGHT BENEATH WARDROBE IAW AMM33-50-21.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,908 hrs · 8,711 cycles

FWD PASSENGER PATHWAY EMERGENCY LIGHTING NOT ILLUMINATED WHILE EMERGENCY LIGHT SET TO ON. R&R #2 EMERGENCY LIGHTING BACK UP BATTERY IAW AMM 33-50-01.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,262 hrs · 7,595 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED LEVEL 2 CORROSION AT THE SILL WEB BETWEEN FR 12 - FR14 AND RBL24 TO RBL36. MAINTENANCE REMOVED AND REPLACED THE SILL WEB BETWEEN FR 12 - FR14 AND RBL24 TO RBL36 IAW SRM 51-43-04. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,262 hrs · 7,595 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED LEVEL 2 CORROSION ON SEVERAL AREAS ON THE AFT BELLY FAIRING ATTACHMENT FLANGE STRAP BETWEEN FR74 AND FR76 AND STRG 22L TO 28L. MAINTENANCE REMOVED AND REPLACED THE AFT BELLY ATTACHMENT FLANGE STRAP BETWEEN FR74 AND FR76 AND STRG 22L TO 28L IAW SRM 51-41-02 AND 51-43-04. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,262 hrs · 7,595 cycles

*** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK *** LEVEL 2 CORROSION WAS FOUND @ CENTER FUSELAGE 3 PASSENGER CABIN FLOOR STRUCTURE PANEL SUPPORT. PANEL WAS REPLACED IAW SRM 51-41-02. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,262 hrs · 7,595 cycles

*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** MAINTENANCE REPORTED LEVEL 2 CORROSION ON SEVERAL AREAS ON AFT BELLY FAIRING ATTACHMENT FLANGE STRAP BETWEEN FR74 TO FR76 AND STRG 22R - 28R. MAINTENANCE REMOVED AND REPLACED THE AFT BELLY FAIRING ATTACHMENT FLANGE STRAP BETWEEN FR74 TO FR76 AND STRG 22R - 28R IAW EMB SRM 51-41-02 AND 51-43-04. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: PANEL SUPPORT — CRACKED (FUSELAGE) · airframe 11,262 hrs · 7,595 cycles

*** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK *** A CRACK WAS FOUND @ CENTER FUSELAGE 3 PASSENGER CABIN FLOOR STRUCTURE PANEL SUPPORT. PANEL WAS REPLACED IAW SRM 51-41-01. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,262 hrs · 7,595 cycles

***WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK*** MAINTENANCE FOUND LEVEL 2 CORROSION @ CENTER FUSELAGE III PASSENGER CABIN FLOOR STRUCTURE SHEAR PANEL FR 87-88 AND LBL 12 TO RBL 12. SHEAR PANEL WAS REMOVED AND REPLACED IAW SRM 51-10-02. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,262 hrs · 7,595 cycles

***WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK*** MAINTENANCE FOUND LEVEL 2 CORROSION @ CENTER FUSELAGE III UNDER FLOOR PANEL SHEAR CLIP FR 88 BETWEEN STR 27R AND 28R. SHEAR CLIP REPLACED IAW SRM 51-41-02 AND 51-43-03. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,262 hrs · 7,595 cycles

***WHILE AIRCRAFT WAS OUT FOR HEAVY CHECK*** MAINTENANCE FOUND LEVEL 2 CORROSION @ CENTER FUSELAGE III PASSENGER CABIN FLOOR STRUCTURE BETWEEN FRAME 78-88 AND BETWEEN LBL 12 AND LBL 36. SHEAR PANEL REPLACED IAW SRM 51-42-01. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,262 hrs · 7,595 cycles

***WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK*** MAINTENANCE FOUND LEVEL 2 CORROSION @ CENTER FUSELAGE III PASSENGER CABIN FLOOR STRUCTURE AT RT SHEAR PANEL AND GALLEY SUPPORT BETWEEN FR 87 AND 88, RBL 12 TO RBL 36. SHEAR PANEL AND TWO GALLEY SUPPORTS WERE REPLACED IAW SRM 51-42-02 AND 51-43-02. AIRCRAFT REMAINS OUT OF SERVICE FOR REMAINDER OF HEAVY CHECK.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,262 hrs · 7,595 cycles

***WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK*** MAINTENANCE FOUND LEVEL 2 CORROSION @ CENTER FUSELAGE III PASSENGER CABIN FLOOR STRUCTURE LONGITUDINAL BEAM FR 87 RBL 12. BEAM WAS REPLACED IAW SRM 51-41-01 AND 51-43-03. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,262 hrs · 7,595 cycles

*** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK *** LEVEL 2 CORROSION WAS FOUND AT CENTER FUSELAGE 3 WASTE BOX ASSY. WASTE BOX WAS REPLACED IAW SRM 51-43-04. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,262 hrs · 7,595 cycles

*** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK *** LEVEL 2 CORROSION WAS FOUND @ CENTER FUSELAGE 3 PASSENGER CABIN FLOOR STRUCTURE. SPLICE PLATE WAS REPLACED IAW SRM 51-43-03. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,262 hrs · 7,595 cycles

*** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK *** LEVEL 2 CORROSION WAS FOUND @ CENTER FUSELAGE 3 PASSENGER CABIN FLOOR STRUCTURE PANEL SUPPORT. PANEL WAS REPLACED IAW SRM 51-43-03. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: WINGLET — CRACKED (LT WING) · airframe 11,262 hrs · 7,595 cycles

***WHILE A/C WAS OUT OF SERVICE FOR HEAVY CHECK*** LT WINGTIP ASSY FOUND CRACKED AT FRONT SPAR AREA. LT WINGTIP ASSY REPALCED IAW AMM 57-30-00-400-801-A. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: WINGLET — CRACKED (RT WING) · airframe 11,262 hrs · 7,595 cycles

*** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK *** RT WING TIP ASSY FRONT SPAR WAS FOUND CRACKED. RT WING TIP ASSY REPLACED IAW AMM 57-30-00/400. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 11,129 hrs · 7,496 cycles

2 EMERGENCY OVERHEAD LIGHTS INOP #1 FWD FA AFT OF CEILING LIGHT, #2 OVER ROW 9. R&R #1 EMERGENCY LIGHT BATTERY IAW AMM 33-50-01.

Part: SUPPORT ARM — OUT OF RIG (PAX DOOR) · airframe 10,361 hrs · 6,997 cycles

MAIN CABIN DOOR HARD TO CLOSE. ROLLER BEARING NOT MEETING UP WITH TRACK. FERRIED TO PIT. PERFORMED RIGGING OF R1 DOOR SUPPORT ARM ASSY IAW 52-11-00, OPS CHECK GOOD.

Part: LIGHT — BURNED OUT (CABIN) · airframe 6,736 hrs · 4,708 cycles

EMERGENCY LIGHT STRIP AT ROW 2 RIGHT SIDE IS BURNED OUT. R & R THE EMERGENCY LIGHT IAW AMM 33-50-21. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 4,464 hrs · 3,209 cycles

CREW RECEIVED AN EMERGENCY BATTERY FAULT AND COCKPIT EMERGENCY LIGHT WOULD NOT COME ON. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY 1 AND 4 IAW AMM AND OPS CHECKED GOOD.

Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 4,044 hrs · 2,906 cycles

CREW REPORTED THAT THE PHOTOLUMINESCENT STRIP NEAR SEATS A1 & A2 WAS INOPERATIVE. MAINTENANCE R & R PHOTOLUMINESCENT STRIP NEAR SEATS A1 & 2 IAW AMM AND OPS CHECKED GOOD.

Part: SLIDE — PARTIAL DEPLOY (L1 DOOR) · airframe 2,699 hrs · 1,980 cycles

F/A OPENED L1 DOOR WITHOUT DISARMING THE SLIDE AND THE SLIDE ONLY PARTIALLY DEPLOYED. ACFT WAS FLOWN VIA MAINTENANCE FERRY, WHERE SLIDE WAS R & R IAW AMM AND OPS CHECKED GOOD. SPECIFIC TIMES WILL BE PROVIDED WHEN AVAILABLE.