N636RW

Part: SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,081 hrs · 28,829 cycles

CORROSION FOUND ON AFT WET AREA FLOOR SPLICE AT FR 88, LH SIDE. REPLACED IAW SRM 51-42-02

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,081 hrs · 28,829 cycles

CORROSION FOUND ON FWD FUSELAGE SHEAR TIE CLIP AT FR17, BETWEEN STGR 22R AND 23R. REPLACED IAW SRM 51-41-01 AND 51-41-02

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,081 hrs · 28,829 cycles

CORROSION FOUND ON FWD FUSELAGE SHEAR TIE CLIP AT FR17, BETWEEN STGR 26L AND 27L. REPLACED IAW SRM 51-41-01 AND 51-41-02

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,081 hrs · 28,829 cycles

CORROSION FOUND ON FWD FUSELAGE SHEAR TIE CLIP AT FR17, BETWEEN STGR 24R AND 25R. REPLACED IAW SRM 51-41-01 AND 51-41-02

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,081 hrs · 28,829 cycles

CORROSION FOUND ON FWD FUSELAGE FRAME SUPPORT ANGLE AT FR17 AND STGR 23R. REPLACED IAW SRM 51-41-02 AND 51-43-01

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,081 hrs · 28,829 cycles

CORROSION FOUND ON FWD FUSELAGE FRAME SHEAR TIE CLIP AT FR17, BETWEEN STGR 27L AND 28L. REPLACED IAW SRM 51-41-01 AND 51-41-02

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,081 hrs · 28,829 cycles

LEVEL 2 CORROSION FOUND FWD FUSELAGE LOWER SHEAR CLIPS AT FR16 BETWEEN STRG 24R AND STRG 25R. CLIP WAS REPLACED IAW SRM 51-41-01

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,081 hrs · 28,829 cycles

CORROSION FOUND ON FWD FUSELAGE FRAME SHEAR TIE CLIP AT FR17, BETWEEN STGR 27R AND 28R. REPLACED IAW SRM 51-41-01 AND 51-41-02

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,081 hrs · 28,829 cycles

LEVEL 2 CORROSION FOUND FWD FUSELAGE LOWER SHEAR CLIPS AT FR17 BETWEEN STRG 25L AND STRG 26L. CLIP WAS REPLACED IAW SRM 51-41-01

Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,081 hrs · 28,829 cycles

CORROSION AT DRAIN MAST SUPPORT BRKT AT FR 17, BETWEEN STGR 26R & STRG 27R. R&R DRAIN MAST SUPPORT BRKT IAW SRM 51-41-01 & 51-41-02.

Part: SKIN — DENTED (ZONE 200) · airframe 46,081 hrs · 28,829 cycles

MAJOR. FWD FUSELAGE LH, RH AND MID SKINS REQUIRES REPLACEMENT DUE TO HAIL DAMAGE. SKINS REPLACED IAW SRM. 51-41-02, 51-43-04 AND ETD 2018-170--088691 REV A

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,081 hrs · 28,829 cycles

LEVEL 2 CORROSION FOUND ON AFT WET AREA FLOOR STRUCTURE FLOOR GUSSET AT FR89 RBL 11. REPLACED AFT WET AREA GUSSET AT FR89 AND RBL 11 IAW SRM 51-41-02

Part: GUSSET — CORRODED · airframe 46,081 hrs · 28,829 cycles

LEVEL 2 CORROSION FOUND ON AFT WET AREA FLOOR STRUCTURE GUSSET AT FR90 RH OUTBD. GUSSET REPLACED IAW SRM 51-41-02.

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,081 hrs · 28,829 cycles

AFT WET AREA FLOOR STRUCTURE CORRODED AT L/H I/B FR 90. R&R L/H I/B GUSSET PLATE IAW SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,081 hrs · 28,829 cycles

AFT WET AREA FLOOR STRUCTURE CORRODED AT RH I/B FR 90. R&R R/H I/B GUSSET PLATE IAW SRM 51-41-02.

Part: PANEL SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,081 hrs · 28,829 cycles

LEVEL 2 CORROSION FOUND ON AFT WET AREA FLOOR PANEL SUPPORT ANGLE BETWEEN FR88 AND FR90 RH SIDE. SUPPORT WAS REPLACED TAW SRM 51-41-01

Part: SEAT TRACK — CORRODED (MAIN CABIN FLOOR) · corrosion level 2 · airframe 46,081 hrs · 28,829 cycles

CORROSION FOUND CENTER FUSELAGE III LH I/B SEAT TRACK, BETWEEN FRAMES 74-84. REPAIRED PER ETD 2021-170-039820 PSE 53-23-005

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,081 hrs · 28,829 cycles

CORROSION FOUND ON CENTER FUSELAGE 1 L/H INBOARD CABIN SEAT TRACK. REPLACED IAW SRM 51-41-02, 51-43-03 AND 51-43-04

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,081 hrs · 28,829 cycles

LEVEL 2 CORROSION FOUND CENTER FUSELAGE RH INBD SEAT TRACK. TRACK WAS REMOVED AND REPLACED SEAT TRACK BETWEEN FR23 AND FR34 IAW SRM 51-41-02

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,081 hrs · 28,829 cycles

LEVEL 2 CORROSION FOUND CENTER FUSELAGE LH INBD SEAT TRACK. TRACK WAS REMOVED AND REPLACED SEAT TRACK BETWEEN FR43 AND FR59 IAW SRM 51-41-02

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 46,081 hrs · 28,829 cycles

LEVEL 2 CORROSION FOUND CENTER FUSELAGE RH INBD SEAT TRACK. TRACK WAS REMOVED AND REPLACED SEAT TRACK BETWEEN FR43 AND FR59 IAW SRM 51-41-02

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,573 hrs · 27,121 cycles

DURING EMERGENCY LIGHT TEST, THE EXIT SIGN AT THE BOTTOM RIGHT CORNER OF THE L2 DOOR CUT-OUT DID NOT ILLUMINATE. R&R EXIT LIGHT AND EMERGENCY LIGHT POWER UNIT NR 3 IAW AMM 33-50-15.

Part: SKIN — DAMAGED (RT HORIZ STAB) · airframe 43,569 hrs · 27,117 cycles

DAMAGE TO R/H HORZ STAB LOWER O/B SKIN, RIB 14 AND HORZ STAB TIP FAIRING. REPLACED LOWER SKIN FROM RIB 12 TO RIB 14 WITH AN EXTERNAL SPLICE AT CUT LINE. REPLACED RIB 14 AND TIP FAIRING. REF ETD2020-170-012614 AND AERNOVA TI 170-20-074.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. CFIII LOWER STRUCTURE FR 74, STR 29R-29L, SUPPORT CORRODED. INSTALLED NEW SUPPORT PER 51-41-02 & 03 PSE 53.23.003 AND FCS 53-23-00-003 AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CF III LOWER FUSELAGE FR 88 STR 27R STRINGER TIP FOUND CORRODED. REPAIRED CORROSION IAW SRM ETD2020-170-007095 ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CF III FUSELAGE LOWER FR 88 89 STR 27 - 28R WASTE PAN DOUBLER CORRODED. REPLACED WASTE PAN DOUBLER IAW SRM 51-41-02 AND SRM 51-43-03 ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: FRAME — GOUGED (L1 DOOR) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

***AIRCRAFT IS IN HEAVY CHECK*** L1 DOOR FRAME GOUGED AT INBD CORNER MIDDLE AREA. REPAIRED L1 DOOR FWD FRAME IAW ETD2020-170-006483. (MAJOR REPAIR) ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CF III LOWER FUSELAGE FR89, STR 27-28R SHEAR CLIP FOUND CORRODED. REPLACED SHEAR CLIP IAW SRM 51-41-01 AND SRM 51-41-02 ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CF III LOWER FUSELAGE FR86-87 STR 27-28R FWD DRAIN AREA INTERCOSTAL CORRODED. REPLACED INTERCOSTAL IAW SRM 51-41-02 AND SRM 51-43-01 ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CF III LOWER FUSELAGE FR 88, STR 27R, STRINGER AFT TIP FOUND CORRODED. REPAIRED STRINGER IAW ETD2020-170-007095.(MAJOR REPAIR) ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. CFIII LOWER STRUCTURE FR 74, STR28L&29L SHEAR CLIP CORRODED. INSTALLED PER SRM 51-41-01/02 PSE 53-23-003 FCS 53-23-00-002 AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. FWD FUSELAGE LWR STRUCTURE FR 16, STR 26-27L SHEAR CLIP CORRODED. REPLACED PER SRM 51-41-01, PSE 53-21-003 FCS 53-10-00-005 AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. CFIII LOWER STRUCTURE FR 75, STR 29-29 LH SHEAR CLIP CORRODED. INSTALLED PER SRM 51-41-01/02 PSE 53-23-003 FCS 53-23-00-002 AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

***AIRCRAFT IS IN HEAVY CHECK*** FWD FUSELAGE LOWER STRUCTURE FR16 STR 27-28-28L SHEAR CLIP CORRODED. REPLACED SHEAR CLIP IAW SRM 51-41-01 AND SRM 51-41-02 ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. CFIII LOWER STRUCTURE, FR 76 AT STR 28-29R SHEAR CLIP CORRODED, REPLACED PER SRM 51-41-01 & 02 PSE 53-23-003 FCS 53-23-00-002. AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. CFIII LOWER STRUCTURE, FWD FVR BTW STR 29 SUPPORT PLATE CORRODED. REPLACED PER SRM 51-41-02. PSE 53-23-003 FCS 53-23-00-001 AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. CFIII LOWER STRUCTURE FR 75, STR 28L-29L SHEAR CLIP CORRODED. INSTALLED PER SRM 51-41-01/02 PSE 53-23-003 FCS 53-23-00-002 AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. CFIII LOWER STRUCTURE FR 75, STR 28-29R ,SHEAR CLIP CORRODED. INSTALLED PER SRM 51-41-01/02 PSE 53-23-003 FCS 53-23-00-002 AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK** PASSENGER CABIN FWD WET AREA FLOOR STRUCTURE FR16 LBL46", SILL WEB CORRODED. REPLACED SILL IAW SRM 51-41-02 & 51-43-02. AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CF III LOWER STRUCTURE, FR 82, STR 28-29, SHEAR CLIP FOUND CORRODED. REPLACED SHEAR CLIP IAW SRM 51-41-01 AND 51-41-02 ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: SKIN — CRACKED (LT WING) · airframe 43,426 hrs · 27,027 cycles

** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK** LH WING SLAT TRACK #5 CUTOUT CRACKED. REPAIRED AREA IAW ETD2020-170-005412. AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK** PASSENGER CABIN FWD WET AREA FLOOR STRUCTURE FR16 LBL42", BRACKET FOUND CORRODED. REPLACED BRACKET IAW SRM 51-43-03.AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK** PASSENGER CABIN FWD WET AREA FLOOR STRUCTURE FR16-18 LBL11", SEAT TRACK UPPER FLANGE FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-41-01, 51-41-02, 51-43-04 & 51-43-03. AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK** PASSENGER CABIN FWD WET AREA FLOOR STRUCTURE FR16 LBL42", BRACKET FOUND CORRODED. REPLACED BRACKET IAW SRM 51-43-03. AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK** FWD WET AREA FLOOR STRUCTURE FR 13-14 RBL 38, SILL UPPER WEB CORRODED. R&R'D SILL WEB PER SRM 51-41-02 AND SRM 51-43-02 AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK** CABIN FWD WET AREA FLOOR STRUCTURE FR 16 LBL13FLOOR DOUBLER UPPER SURFACE CORRODED. R&R'D DOUBLER PER SRM 51-41-02 AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK** CABIN FWD WET AREA FLOOR STRUCTURE FR 14-17, RBL 11 SEAT TRACK UPPER FLANGE CORRODED. R&R'D SEAT CRACKED PER SRM 51-41-01, 51-43-03 & 04 AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK** PASSENGER CABIN FWD WET AREA FLOOR STRUCTURE FR19 LBL42", BRACKET UPPER SURFACE FOUND CORRODED. REPLACED BRACKET IAW SRM 51-43-03. AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK** PAX CABIN FWD WET AREA FLOOR STRUCTURE FR 14 RBL 16", CROSSBEAM UPPER FLANGE FOUND CORRODED. REPAIRED IAW SRM 53-00-10 REPAIR 03. AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

***WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK*** CFIII LOWER FUSELAGE FR85, STR 28-29R SHEAR CLIP FOUND CORRODED. REPLACED SHEAR CLIP PER SRM 51-41-01 AND SRM 51-41-02. AIRCRAFT REMAINS OUT OF SERVICE FOR THE REMAINDER OF HEAVY CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

***WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK*** CF III FUSELAGE FR87, STR 27-28R SHEAR CLIP CORRODED. REPLACED SHEAR CLIP IAW SRM 51-41-01 AND SRM 51-41-02. AIRCRAFT REMAINS OUT OF SERVICE FOR THE REMAINDER OF HEAVY CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK** CFIII LOWER FUSELAGE FR 86 STR 28R- 29R. SHEAR CLIP CORRODED. R&R'D SHEAR CLIP PER 51-41-01 AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

***AIRCRAFT IS IN HEAVY CHECK*** CFIII LOWER FUSELAGE FR85, STR 28-29R SHEAR CLIP FOUND CORRODED. REPLACED SHEAR CLIP PER SRM 51-41-01 AND SRM 51-41-02 ***AIRCRAFT REMAINS IN HEAVY CHECK***

Part: BRACKET — CRACKED (FUSELAGE) · airframe 43,426 hrs · 27,027 cycles

** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK** 2 BRACKETS CRACKED AT CROSSBEAM FR 12. R&R'D BOTH BRACKETS SRM 51-41-01 AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 43,426 hrs · 27,027 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. CFIII AFT WET AREA FLOOR STRUCTURE FR 85, LBL 28 SUPPORT ANGLE CRACKED. CRACK IS .6 INCHES LONG. R&R'D ANGLE PER SRM 51-41-01. PSE 53-23-005 FCS NON EFFECTIVE AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. CFIII AFT WET AREA FLOOR STRUCTURE FR 84, LBL11, SEAT TRACK UPPER FLANGE CORRODED. REPAIRED UPPER FLANGE USING DOUBLER REPAIR PER SRM 53-23-10 REPAIR 4 PSE53-23-005 FCS NOT EFFECTIVE AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. CFIII AFT WET AREA FLOOR STRUCTURE FR 84 RBL 11 SEAT TRACK CROWN CORRODED. REPLACED PER 51-43-03 AND -04 FCS NON EFFECTIVE, PSE 53-23-005 AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. CFIII AFT WET AREA FLOOR SUPPORT AT FR 87-88 L/H SHEAR PANEL CORRODED. R&R'D SHEAR PANEL SRM 51-41-01 & 02. PSE 52-23-005 AND FCS 53-23-00-010 AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. CFIII AFT WET AREA FLOOR STRUCTURE FR 87-88 R/H SHEAR PANEL SUPPORT CORRODED. R&R'S SUPPORT PER SRM 51-41-02 AND 51-42-02 PSE 53-23-005 AND FCS 53_23-00-010 AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. CFIII AFT WET AREA FLOOR STRUCTURE FR 90 LBL 33, SUPPORT CORRODED. R&R'D SUPPORT PER SRM 51-41-01 &02. PSE 53-23-005, FCS NON EFFECTIVE AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK** CFIII AFT WET AREA FLOOR STRUCTURE FR 90, RBL 23 GUSSET PLATE CORRODED. R&R'S GUSSET PLATE PER SRM 51-41-02., PSE 53-23-005 AND FCS 53_23-00-010 AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. CFIII WET AREA FLOOR STRUCTURE FR 84, RBL 45, PANEL SUPPORT WEB FOUND CORRODED. R&R'D SUPPORT WEB PER SRM 51-41-01/02. PSE 58.23.005, FCS 53-23-00-010 AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. CFIII AFT WET AREA FLOOR SUPPORT AT FR 87-88 LBL 42 SPLICE PLATE CORRODED. R&R'D SPLICE PLATE SRM 51-41-01 & 02. PSE 52-23-005 AND FCS 53-23-00-010 AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. CFIII AFT WET AREA FLOOR STRUCTURE FR 84 LBL 45, PANEL SUPPORT WEB CORRODED. R&R'D SUPPORT WEB PER SRM 51-41-01 & 02. PSE 53-23-005. FCS NON EFFECTIVE AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. CFIII AFT WET AREA FLOOR STRUCTURE FR 87-88, RBL 42, SPLICE PLATE CORRODED. R&R'D SPLICE PLATE PER SRM 51-41-02. PSE 53-23-005. FCS 53-23-00-010 AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. CFIII AFT WET AREA FLOOR STRUCTURE, FR 87-88 MID SHEAR PANEL SUPPORT CORRODED. R&R'S SUPPORT PER SRM 51-41-02 AND 51-42-02 PSE 53-23-005 AND FCS 53_23-00-010 AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,426 hrs · 27,027 cycles

** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK** CFIII AFT WET AREA FLOOR STRUCTURE PANEL SUPPORT CORRODED. R&R'D PANEL SUPPORT PER SRM 51-42-01 AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 43,426 hrs · 27,027 cycles

WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK. CFLL TO CFIII FUSELAGE JUNCTION FR 59, STR 9R-10R BOTH STRINGER SPLICES CRACKED. CRACKS ARE .5 INCHES. INSTALLED NEW SPLICES PER SRM 51-43-04 PSE 53-22-002 FCS 53-22-00-003 AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: SKIN — CRACKED (LT WING) · airframe 43,426 hrs · 27,027 cycles

** WHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK** LH WING SLAT TRACK #4 CUTOUT CRACKED. REPAIRED AREA IAW SRM 57-49-01 REPAIR 6 PARAGRAPH 4. AIRCRAFT REMAINS OUT OF SERVICE FOR COMPLETION OF HEAVY CHECK.

Part: GLOWSTRIP — DEBONDED (CABIN) · airframe 39,243 hrs · 24,485 cycles

PHOTOLUMINESCENT STRIP DISBONDED NEXT TO SEAT 1C. R&R PHOTOLUMINESCENT STRIP IAW AMM 33-50-00-01.

Part: LEVER — LACK OF LUBE (R1 DOOR) · airframe 38,099 hrs · 23,769 cycles

R1 DOOR ARMING LEVER DIFFICULT TO OPERATE. APPLIED LPS GREASLESS LUBRICANT TO THE R1 DOOR.

Part: RIB — NOT REPORTED (AILERONS) · airframe 37,941 hrs · 23,674 cycles

AILERONS REQUIRED UNUSUAL FORCE TO TURN PAST CENTER. CONTROLS LOCK IN PLACE UNLESS UNUSUAL FORCE IS APPLIED. DECLARED EMERGENCY, DIVERTED, AND LANDED WITHOUT INCIDENT. R & R THE LT RIB 52 IAW SRM 51-41-01. INSTALLED REINFORCEMENT DOUBLE ON FWD SIDE IAW SB170-0066, REV 02. REPAIR IS NON FCS.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,938 hrs · 23,670 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE SHEAR TIE AT FRAME 17, BETWEEN STR 25R AND 26R. MAINTENANCE REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-08, 51-40-02, AND 51-23-06. AIRCRAFT IS CURRENTLY STILL OUT OF SERVICE FOR HEAVY CHECK COMPLETION.

Part: SHEAR TIE — CORRODED (FRAME 17) · corrosion level 2 · airframe 37,938 hrs · 23,670 cycles

MAINTENANCE REPORTED CORROSION ON THE SHEAR TIE AT FRAME 17, BETWEEN STRINGERS 26 AND 27R. MAINTENANCE REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-08, 51-40-02, AND 51-23-06.

Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 37,938 hrs · 23,670 cycles

MAINTENANCE REPORTED CORROSION ON THE SHEAR TIE, FRAME 16, BETWEEN STRINGERS 27 AND 28R. MAINTENANCE REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-08, 51-40-02, 51-40-08, & 51-23-06.

Part: SHEAR TIE — CORRODED (FRAME 16) · corrosion level 2 · airframe 37,938 hrs · 23,670 cycles

MAINTENANCE REPORTED CORROSION ON THE SHEAR TIE, FRAME 16, BETWEEN STR 26 AND 27R. MAINTENANCE REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-08, 51-40-02, & 51-23-06.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,938 hrs · 23,670 cycles

WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE SHEAR CLIP AT FR-17, BETWEEN STR-27R & STR-28R. LOCATED AT THE FORWARD END OF THE FORWARD CARGO COMPARTMENT. MAINTENANCE REMOVED AND REPLACED THE SHEAR CLIP AT FR-17, BETWEEN STR-27R & STR-28R. LOCATED AT THE FORWARD END OF THE FORWARD CARGO COMPARTMENT IAW SRM 51-40-08, 51-40-02, 53-10-04 & 51-21-01.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 37,930 hrs · 23,664 cycles

L2 DOOR EXIT SIGN FOUND BROKEN. R & R THE SIGN IAW AMM 33-50-15.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 35,212 hrs · 21,948 cycles

EXIT IDENTIFIER SIGN BY L1 DOOR BROKEN. R&R EXIT IDENTIFIER SIGN BY L1 DOOR, OPS CHECK GOOD REF AMM 33-50-15.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 34,576 hrs · 21,510 cycles

A STRONG JET EXHAUST ODOR COMING FROM ECS IN COCKPIT, F/A REPORT NO ODOR IN CABIN .TURNED NR 1 PACK OFF AND ODOR DISSIPATED FOR APPROX 45 MINUTES THEN RETURNED WITH NR 1 PACK SELECTED OFF. NR 1 ENGINE ITT 100 ABOVE E2 ITT ECS DUCT PRESSURE PULSATING PACK 1 :5-60 PSI, NR 2 PACK 16 -47 PSI, NR 1 PACK SELECTED OFF AND ELT CONDUCTED AT FL310.

Part: LIGHT — DAMAGED (CABIN) · airframe 33,730 hrs · 20,896 cycles

RIGHT PAX CABIN EMERGENCY LIGHT STRIPS NR 2 AND 3 ARE WORN AND DAMAGED. FAILED LIGHT CHECK. R & R THE EMERGENCY LIGHTS IAW AMM 33-50-21.

Part: GUST LOCK — LACK OF LUBE (L1 DOOR) · airframe 33,630 hrs · 20,829 cycles

L1 DOOR GUST LOCK WILL NOT ENGAGE. CLEANED AND LUBRICATED LATCH ON GUST LOCK MECHANISM REF AMM 52-11-23. OPS CHECKED GOOD.

Part: GUST LOCK — INOPERATIVE (PAX DOOR) · airframe 32,866 hrs · 20,329 cycles

MAIN CABIN DOOR GUST LOCK NOT LATCHING. LUBRICATED L1 DOOR GUST LOCK MECHANISM, OPS TEST GOOD AT THIS TIME IAW 52-11-00.

Part: FRAME SPLICE — CORRODED (FRM 90) · corrosion level 2 · airframe 32,794 hrs · 20,278 cycles

SPLICE ON RT SIDE OF FRAME 90 HAS CORROSION AROUND GALLEY MOUNT HOLE. R & R SPLICE MOUNT IAW SRM 51-31-00.

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 32,794 hrs · 20,278 cycles

PANEL SHEAR ON RT SIDE BETWEEN FRAME 87 AND FRAME 88 HAS CORROSION AROUND GALLEY MOUNT HOLES. R & R SHEAR PANEL IAW SRM 51-41-01 AND 51-42-01.

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 32,794 hrs · 20,278 cycles

SHEAR PANEL IN MIDDLE BETWEEN FRAME 87 AND FRAME 88 HAS CORROSION AROUND GALLEY MOUNT HOLES. R & R SHEAR PANEL IAW SRM 51-41-01 AND 51-42-01.

Part: SENSOR — OUT OF LIMITS (LT WOW) · airframe 32,787 hrs · 20,273 cycles

AFTER TAKEOFF, GEAR WOULD NOT RETRACT. HANDLE WOULD NOT MOVE WITHOUT FORCE OR USING RELEASE. TROUBLESHOT IN REF WITH AMM 32-62-03 AND FIM 27-03-00. FOUND OTBD LEFT WOW OUT OF RANGE. ADJUSTED AND PERFORMED OPS CHECK, EXTENSION AND RETRACTION, LANDING GEAR CHECKS OK.

Part: LIGHT — MISSING (CABIN) · airframe 32,732 hrs · 20,234 cycles

EMERGENCY LIGHT MISSING FROM ACFT, LT SIDE OF AISLE AT ROW 17, 18. REPOSITIONED THE EMERGENCY LIGHT AT SEAT 17/18 IAW AMM 25-60-07.

Part: FITTING — OUT OF ADJUST (L2 GIRT BAR) · airframe 32,074 hrs · 19,811 cycles

AFT L2 DOOR LT GIRT BAR INDICATION SHOWS CLEAR WHEN DOOR IS ARMED, MFD SHOWS DOOR CLOSED AND LOCKED. ADJUSTED L2 DOOR FWD GIRT BAR FLOOR FITTING IAW AMM 52-12-00. OPS CHECK GOOD.

Part: INDICATOR — OUT OF ADJUST (L2 DOOR GIRT BAR) · airframe 31,974 hrs · 19,741 cycles

L2 DOOR GIRT BAR INDICATION INOPERATIVE. ADJUSTED L2 DOOR LOWER SLIDE INDICATOR IAW AMM 52-12-00. OPS CHECK AND VISUAL CHECKS GOOD.

Part: GLOWSTRIP — DISLODGED (CABIN) · airframe 31,534 hrs · 19,436 cycles

FLOOR GLOW IN DARK STRIP SEAT 18B HAS SLID. REPOSITIONED EGRESS FLOOR STRIP IAW AMM 33-52-21 TO CORRECT POSITION. NO OVERLAY VISIBLE.

Part: LIGHT — MISSING (ROWS 20-22) · airframe 30,909 hrs · 19,040 cycles

TWO LIGHT STRIPS MISSING FROM AISLE AT ROW 20-22 ON AB SIDE. R & R THE STRIP IAW AMM 33-50-21.

Part: SNAP RING — DAMAGED (L1 DOOR) · airframe 30,866 hrs · 19,014 cycles

L1 DOOR MAKES LOUD NOISE WHEN ARMED, ARMING HANDLE FEELS ROUGH. REPLACED SNAP RING ON AFT BELL CRANK OF L1 DOOR IAW AMM 52-11-40. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (ZONE 100) · airframe 30,530 hrs · 18,784 cycles

FWD RT EMERGENCY LIGHT INOPERATIVE. R & R FWD RT EMERGENCY FLOOR LIGHTING STRIP AMM 33-50-21.

Part: GLOWSTRIP — FAILED (CABIN) · airframe 29,741 hrs · 27,304 cycles

FWD RT PHOTOLUMINESCENT STRIP NOT GLOWING. R & R FWD RT PHOTOLUMINESCENT STRIP IAW AMM 33-50-21.

Part: LIGHT — UNSECURE (CABIN) · airframe 29,689 hrs · 18,279 cycles

AISLE PATH LIGHTING HAS 3 GAPS ON LT SIDE. SECURED THE EMERGENCY LIGHT IAW AMM 33-50-21.

Part: LIGHT — UNSECURE (CABIN) · airframe 29,616 hrs · 18,241 cycles

EMERGENCY LIGHTS IN ROW 12 - 14 ARE MOVING, CAUSING BLANK SPOTS. ADJUSTED THE EMERGENCY LIGHT STRIPS IAW AMM 33-50-21.

Part: WARNING LIGHT — FALSE ACTIVATION (EMERGENCY LIGHTS) · airframe 29,378 hrs · 18,094 cycles

EMERGENCY LIGHT BATTERY FAULT ADVISORY. PERFORMED POWER RESET. AFTER ACFT POWERED BACK UP, MESSAGE REMAINED OFF. OPS CHECKED GOOD IAW AMM 33-50-01.

Part: LIGHT — INOPERATIVE (ZONE 100) · airframe 28,737 hrs · 17,693 cycles

EMERGENCY LIGHTS, INOPERATIVE. R & R IAW AMM 33-50-21. OPS CHECKED GOOD.

Part: FLAP — LACK OF LUBE (PAX DOOR) · airframe 28,661 hrs · 17,652 cycles

VENT FLAP ON MAIN CABIN DOOR IS HARD TO CLOSE. LUBRICATED VENT FLAP IAW CMM 52-11-22. OPS CHECKED GOOD.

Part: SIGN — DETACHED (GALLEY) · airframe 28,389 hrs · 17,484 cycles

FRONT GALLEY EMERGENCY EXIT SIGN IS OFF. R & R FRONT GALLEY EMERGENCY EXIT SIGN REF AMM 33-50-19. OPS CHECK GOOD.

Part: LIGHT — OBSTRUCTED (CABIN) · airframe 27,912 hrs · 17,210 cycles

PORTION OF EMERGENCY LIGHT STRIP AT SEAT 2A NOT VISIBLE. ADJUSTED EMERGENCY LIGHT STRIP, IAW AMM 33-50-21.

Part: GLOWSTRIP — OUT OF ALIGNMENT (CABIN) · airframe 27,760 hrs · 17,117 cycles

LT ROW 1 AND 2 GLOW STRIPS OVERLAPPED. ALIGNED GLOW STRIPS IAW AMM 33-50-21.

Part: GLOWSTRIP — BROKEN (ZONE 100) · airframe 27,760 hrs · 17,117 cycles

GLOW STRIP LT ROW 9, 10, 11 BROKEN. GLOW STRIPS LT ROW 9, 10, AND 11 OVERLAP, NOT BROKEN. REALIGNED GLOW STRIPS IAW AMM 33-50-21.

Part: LIGHT — UNSECURE (CABIN) · airframe 27,643 hrs · 17,050 cycles

EMERGENCY LIGHT STRIP MISSING BY 15 ACFT. SECURED EMERGENCY LIGHT STRIP IAW AMM 33-50-21.

Part: LIGHT — OUT OF POSITION (ROW 21) · airframe 27,522 hrs · 16,989 cycles

EMERGENCY LIGHT STRIP AT ROW 21 NOT VISIBLE. ADJUSTED LIGHT STRIP AT ROW 21 IAW 33-50-21.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 27,522 hrs · 16,989 cycles

EMERGENCY LIGHT STRIP AT ROWS 1, 9, AND 11 A SIDE NOT VISIBLE. ADJUSTED LIGHT STRIP IAW 33-50-21.

Part: DOOR — OBSTRUCTED (AFT LEFT) · airframe 27,385 hrs · 16,912 cycles

AFT LEFT DOOR, , WILL NOT CLOSE AND HAS SOMETHING OBSTRUCTING IT. INSPECTED DOOR AND FOUND SCREW WEDGED INTO DOOR HINGE. REMOVED HARDWARE AND DOOR CHECKS GOOD IAW AMM 52-12-00.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 27,324 hrs · 16,875 cycles

CORROSION ON AFT RT GUSSET PLATE. R & R AFT RT GUSSET PLATE AT FR90, PN .

Part: BEAM — CORRODED (FUSELAGE) · airframe 27,324 hrs · 16,875 cycles

CORROSION FOUND ON RT CF III BEAM. REMOVED OLD RT CFIII EXTENDED BEAM AND MATCH DRILLED NEW BEAM AND INSTALLED.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,324 hrs · 16,875 cycles

CORROSION FOUND ON AFT LT FLOOR SUPPORT GUSSET PLATE. R & R AFT LT FLOOR SUPPORT.

Part: SHEAR WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,324 hrs · 16,875 cycles

CORROSION FOUND ON LT SHEAR WEB BETWEEN FRAMES 87-88 AROUND FASTENER HOLES. R & R LT SHEAR WEB.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,324 hrs · 16,875 cycles

CORROSION FOUND ON FWD CARGO DOOR LOWER SILL BEAM. R & R FWD CARGO DOOR LOWER SILL BEAM

Part: FITTING — DEFORMED (GIRT BAR) · airframe 27,324 hrs · 16,875 cycles

PERMANENT DEFORMATION, R1 DOOR EVAC SLIDE AFT FLOOR FITTING IS GOUGED. REWORK R1 DOOR EVAC SLIDE AFT FLOOR FITTING IAW ETD 2014-170-024655.

Part: STRUCTURE — GOUGED (VERTICAL STAB) · airframe 27,324 hrs · 16,875 cycles

PERMANENT DEFORMATION, GOUGE IN TIP RIB OF VERTICAL STAB. BLENDED GOUGES ON TIP RIB OF VERTICAL STAB IAW ETD2014-170-024401.

Part: STRUCTURE — DAMAGED (HORIZONTAL STAB) · airframe 27,324 hrs · 16,875 cycles

DAMAGE ON LT HORIZONTAL STAB TIP AND T/E. REPAIRED HORIZONTAL STABILIZER IAW ETD 2014-170-024373 AND TI170-14-038.

Part: SEAL DEPRESSOR — CORRODED (ZONE 100) · airframe 27,324 hrs · 16,875 cycles

CORROSION FOUND ON FWD CARGO DOOR CUTOUT, LOWER BEAM SEAL REST. R & R SEAL REST.

Part: SKIN — DAMAGED (FRAME 33) · airframe 27,324 hrs · 16,875 cycles

PERMANENT DEFORMATION, TOOL DAMAGE ON FUSELAGE SKIN BENEATH 191 PANEL SKIRT ON LT AND RT SIDES. BLENDED DAMAGE AFT OF FRAME 33 AND BELOW STR 17R IAW ETD2014-170-024937.

Part: SUPPORT — CRACKED (VAPOR BARRIER) · airframe 27,324 hrs · 16,875 cycles

VAPOR BARRIER LOWER SUPPORT CRACKED AT BOLTHEADS ON UPPER WING BOX BETWEEN RT FLOORBEAM AND RT SILL BETWEEN FR 54-55. REMOVED CRACKED VAPOR BARRIER LOWER SUPPORT FABRICATED AND INSTALLED NEW VAPOR BARRIER SUPPORT IAW SRM 170/175 51-31-00 AND 51-40-03, 51-41-01.

Part: SUPPORT — CRACKED (VAPOR BARRIER) · airframe 27,324 hrs · 16,875 cycles

VAPOR BARRIER LOWER SUPPORT CRACKED AT BOLTHEADS ON UPPER WING BOX SKIN BETWEEN FR54-55 BETWEEN RT AND RT CENTER FLOORBEAMS. REMOVED CRACKED VAPOR BARRIER SUPPORT FABRICATED SUPPORT AND INSTALLED IAW SRM 170/175 51-31-00 AND 51-40-03 AND 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FRAMES 85-86) · airframe 27,324 hrs · 16,875 cycles

LT UPPER SHEET BETWEEN FRAMES 85-86 FOUND CORRODED. R & R UPPER SHEET.

Part: STRUCTURE — GOUGED (SERVICE DOOR) · airframe 27,324 hrs · 16,875 cycles

PERMANENT DEFORMATION, AFT SERVICE DOOR HAS A GOUGE LOWER AFT CORNER. BLENDED DAMAGE AREA IAW ETD2014-170-04428.

Part: SUPPORT — CRACKED (VAPOR BARRIER) · airframe 27,324 hrs · 16,875 cycles

VAPOR BARRIER LWR SUPPORT WEB DENTED BETWEEN RT AND RT CENTER FLOORBEAMS BETWEEN FR54-55. REMOVED CRACKED VAPOR BARRIER SUPPORT FABRICATED AND INSTALLED NEW VAPOR BARRIER SUPPORT IAW SRM 170/175 51-31-00 AND 51-40-03, 51-41-01.

Part: SUPPORT — CRACKED (VAPOR BARRIER) · airframe 27,324 hrs · 16,875 cycles

VAPOR BARRIER LOWER SUPPORT CRACKED AT BOLTHEADS ON UPPER WING BOX BETWEEN LT FLOORBEAM AND LT SILL BETWEEN FR54-55. REMOVED CRACKED VAPOR BARRIER LWR SUPPORT FABRICATED AND INSTALLED NEW VAPOR BARRIER SUPPORT IAW SRM 170/175 51-31-00 AND 51-41-01.

Part: SHEAR TIE — CORRODED (FRAME 84) · corrosion level 2 · airframe 27,324 hrs · 16,875 cycles

SHEAR TIE CORRODED ON FRAME 84 BETWEEN STRINGERS 27 AND 28R. R & R SHEAR TIE.

Part: FLOORBEAM — CORRODED (FRAME 77) · airframe 27,324 hrs · 16,875 cycles

FRAME 77 LT AND RT CARGO FLOORBEAM BETWEEN S29L AND 29R CORRODED. R & R FLOOR SUPPORT. MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (FRAME 84) · corrosion level 2 · airframe 27,324 hrs · 16,875 cycles

SHEAR TIE CORRODED AT FRAME 84 BETWEEN S28-29R. R & R SHEAR TIE. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (FRAME 81) · corrosion level 2 · airframe 27,324 hrs · 16,875 cycles

FRAME 81, FLOORBEAM BETWEEN S29L AND 29R CORRODED. R & R FLOORBEAM. MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (FRAME 85) · corrosion level 2 · airframe 27,324 hrs · 16,875 cycles

SHEAR TIE CORRODED AT FRAME 85 BETWEEN S27-28R. R & R SHEAR TIE. MAJOR REPAIR.

Part: SEAL DEPRESSOR — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,324 hrs · 16,875 cycles

CORROSION FOUND ON AFT CARGO DOOR CUTOUT LOWER CENTER SEAL REST. R & R SEAL REST.

Part: SHEAR TIE — CORRODED (FRAME 53) · airframe 27,324 hrs · 16,875 cycles

SHEAR TIE CORRODED AT FRAME 83 BETWEEN S27-28R. R & R SHEAR TIE. MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (FRAME 87) · corrosion level 2 · airframe 27,324 hrs · 16,875 cycles

SHEAR TIE CORRODED AT FRAME 87 BETWEEN S27-28R. R & R SHEAR TIE. MAJOR REPAIR.

Part: CHANNEL — CORRODED (FRAME 87) · corrosion level 2 · airframe 27,324 hrs · 16,875 cycles

CHANNEL FWD OF FRAME 87 BETWEEN S27-28R. R & R U CHANNEL. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (FRAME 78) · airframe 27,324 hrs · 16,875 cycles

FRAME 78 LT CARGO FLOORBEAM BETWEEN S29L AND 29R CORRODED. R & R FLOORBEAM. MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (FRAME 86) · corrosion level 2 · airframe 27,324 hrs · 16,875 cycles

SHEAR TIE CORRODED AT FRAME 86 BETWEEN S27-28R. R & R SHEAR TIE. MAJOR REPAIR.

Part: SHEAR TIE — CORRODED (FRAME 83) · airframe 27,324 hrs · 16,875 cycles

SHEAR TIE CORRODED AT FRAME 83 BETWEEN S28-29R. R & R SHEAR TIE. MAJOR REPAIR.

Part: CHANNEL — CORRODED (FRAME 87) · corrosion level 2 · airframe 27,324 hrs · 16,875 cycles

U CHANNEL FWD OF FRAME 87 BETWEEN S27-28R. R & R U CHANNEL. MAJOR REPAIR.

Part: FITTING — GOUGED (GIRT BAR) · airframe 27,324 hrs · 16,875 cycles

R1 DOOR EVACUATION SLIDE FWD FLOOR FITTING IS GOUGED. REWORK R1 DOOR EVAC SLIDE FWD FLOOR FITTING IAW ETD 2014-170-024655.

Part: RIB — CRACKED · airframe 27,324 hrs · 16,875 cycles

CRACK ON RIB 4 RT, REWORKED AND REPAIRED CRACKED FLANGE IAW ETD2014-170-024140.

Part: LIGHT — FADED (SEAT 1C) · airframe 26,971 hrs · 16,667 cycles

SEAT 1C EMERGENCY LIGHT FADED. R & R LIGHT IAW AMM 33-50-21.

Part: ROLL PIN — MISSING (L1 DOOR) · airframe 26,105 hrs · 16,143 cycles

L1 DOOR ACTUATOR ROLL PIN AFT SIDE OF DOOR MISSING ROLLER. INSPECTED AND FOUND L1 DOOR AFT HANDLE LOCK ROLLER MISSING, FWD STILL PRESENT. VERIFIED L1 DOOR LATCHED, LOCKED, AND CLOSED, FERRIED. REPLACED L1 DOOR AFT LOCK ROLLER IAW AMM 52-11-20, PERFORMED ADJUSTMENT/TEST IAW AMM 52-11-00.

Part: ENGINE — ODOR (NR 1) · airframe 23,991 hrs · 14,853 cycles

STRONG ODOR SEEMS TO BE ASSOCIATED WITH NR 1 BLEED, NOTICED AFTER TAKEOFF UNTIL NR 1 BLEED WAS DESELECTED. REMOVED AND REPLACED ENGINE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,960 hrs · 13,647 cycles

LEVEL 2 CORROSION - CF II RHIB FLOORBEAM. REMOVED AND REPLACED RHIB SEAT TRACK IAW EMB 170 SRM 51-12-01, 51-43-01, 51-40-02, 51-42-04, 51-43-02, 51-23-06, AND 51-23-00.

Part: SERVICE PANEL — CORRODED (WASTE SERVICE) · airframe 21,960 hrs · 13,647 cycles

LEVEL 2 CORROSION - WASTE SERVICE PANEL/BOX AND DOUBLERS ON INTERNAL SIDE. REMOVED AND REPLACED WASTE SERVICE PANEL/BOX ASSY IAW EMB ETD 2012-170-007321.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,960 hrs · 13,647 cycles

LEVEL 2 CORROSION - FLOOR CLOSE OUT PLATE AT DAD PANEL JUST AFT OF L1 DOOR AT FRM 19. REMOVED AND REPLACED CORRODED CLOSE OUT PLATE IAW EMB 170 SRM 51-41-02 AND 51-43-02.

Part: PCU — LEAKING (LT WING) · airframe 21,367 hrs · 13,261 cycles

CREW REPORTED HYD 1 LOW QTY IN FLIGHT. DECLARED EMERGENCY, LANDING WAS UNEVENTFUL. FOUND LT MID MFS PCU LEAKING. REMOVED AND REPLACED LT MID MFS PCU, OPS AND LEAK CHECK GOOD.

Part: DOOR — UNKNOWN (L1) · airframe 21,252 hrs · 13,193 cycles

L1 MAIN CABIN DOOR HARD TO OPEN AND CLOSE. PERFORMED OPS CHECK ON L1 DOOR IAW MM 52-11-21. OPS CHECKED GOOD.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,306 hrs · 10,773 cycles

LEVEL 2 CORROSION FWD CARGO DOOR CUTOUT, LOWER AFT SEAL REST. REPLACED SEAL REST IAW EMB 170 MM 20-10-01-02.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,306 hrs · 10,773 cycles

LEVEL 2 CORROSION AFT AVIONICS RACK GUSSET AT FR90. REMOVED AND REPLACED AFT AVIONICS RACK GUSSET IAW EMB 170 SRM 51-31-00, 51-40-04, AND 51-41-02.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,306 hrs · 10,773 cycles

LEVEL 2 CORROSION LT SHEAR PLATE AT FR87 BETWEEN LT SILL PLATE AND LT SEAT TRACK BEAM. REMOVED AND REPLACED SHEAR PLATE AS NEEDED IAW EMB 170 SRM 51-42-01.

Part: SERVICE PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,306 hrs · 10,773 cycles

LEVEL 2 CORROSION WASTE TANK SERVICE PANEL MOUNT STRIP ON I/B FWD CORNER. INSTALLED SERVICEABLE WASTE WATER BOX ASSY IAW EMB 170 SRM 51-43-04.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,306 hrs · 10,773 cycles

LEVEL 2 CORROSION POTABLE WATER SERVICE PANEL CUTOUT ON I/B FWD INTERNAL SIDE. REPAIRED WATER SERVICE PANEL DOUBLER IAW EMB 170 SRM 51-43-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,306 hrs · 10,773 cycles

LEVEL 2 CORROSION LT SEAT TRACK BEAM BETWEEN FR86 AND FR89. REPLACED SEAT TRACK IAW 53-00-10.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,306 hrs · 10,773 cycles

LEVEL 2 CORROSION LT SILL PLATE BETWEEN FR87-88 ON TOP OF LT SHEAR PLATE. REMOVED AND REPLACED LT SILL PLATE IAW EMB 170 SRM 51-40-02 AND 51-42-02.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,306 hrs · 10,773 cycles

LEVEL 2 CORROSION RT SHEAR PLATE BETWEEN FR87-88 AND RT SEAT TRACK BEAM AND RT SILL PLATE. REMOVED, FABRICATED, AND INSTALLED SHEAR PLATE IAW EMB 170 SRM 51-42-07.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,306 hrs · 10,773 cycles

LEVEL 2 CORROSION RT SILL PLATE AT FR89. REMOVED RT SILL PLATE, MATCH DRILLED, AND INSTALLED IAW EMB 170 SRM 51-40-02, 51-41-00, 51-42-03, AND 51-43-01.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,306 hrs · 10,773 cycles

LEVEL 2 CORROSION POTABLE WATER SERVICE PANEL MOUNT STRIP ON I/B FWD CORNER. REPAIRED POTABLE WATER SERVICE PANEL DOUBLER IAW EMB 170 SRM 51-43-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,306 hrs · 10,773 cycles

LEVEL 2 CORROSION RT SEAT TRACK BEAM GUSSET AT FR90. REMOVED, MATCH DRILLED NEW PART, AND INSTALLED IAW EMB 170 SRM 51-40-02 AND 51-41-02.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,306 hrs · 10,773 cycles

LEVEL 2 CORROSION WASTE TANK HOLD DOWN GUSSET AT FR90. REMOVED AND REPLACED IAW EMB 170 SRM 51-31-00 AND 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,306 hrs · 10,773 cycles

LEVEL 2 CORROSION RT SEAT TRACK BEAM BETWEEN FR86-89. REMOVED AND INSTALLED BEAM IAW EMB 170 SRM 51-40-02, 51-40-00, AND 51-43-01.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,306 hrs · 10,773 cycles

LEVEL 2 CORROSION MID SHEAR PLATE BETWEEN FR87-88 AND LT/RT SEAT TRACK BEAMS. REMOVED AND REPLACED SHEAR PLATE AS NEEDED IAW EMB 170 SRM 51-42-01.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,306 hrs · 10,773 cycles

LEVEL 2 CORROSION LT SEAT TRACK BEAM GUSSET AT FR90. REMOVED AND REPLACED IAW EMB 170 SRM 51-31-00, 51-40-04, AND 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,306 hrs · 10,773 cycles

LEVEL 2 CORROSION RH SEAT TRACK BEAM BETWEEN FR85-86. REMOVED AND INSTALLED UPPER SUPPORT IAW EMB 170 SRM 51-31-00, 51-41-01 AND 51-43-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,306 hrs · 10,773 cycles

LEVEL 2 CORROSION RT SEAT TRACK BEAM BETWEEN FR12 AND FR18. REMOVED AND REPLACED CORRODED SEAT TRACK IAW EMB 170 SRM 51-41-01, 51-41-02, AND 51-43-01.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,306 hrs · 10,773 cycles

LEVEL 2 CORROSION RT SHEAR PLATE BETWEEN FR12 AND FR14. REMOVED AND REPLACED RT SHEAR PLATE BETWEEN FR12 AND FR 14 IAW EMB 170 SRM 51-43-02 AND 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,306 hrs · 10,773 cycles

LEVEL 2 CORROSION FR 17 BETWEEN LT SEAT TRACK AND RT SILL PLATE. INSTALLED DOUBLER STRAP AT CORRODED AREA PER EMB ETD 2010-170/10633.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,306 hrs · 10,773 cycles

LEVEL 2 CORROSION LT SHEAR PLATE AT FR19. REMOVED AND INSTALLED NEW SHEAR PLATE AT FR 19 IAW EMB 170 SRM 51-41-02, 51-43-02 AND 51-40-02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,306 hrs · 10,773 cycles

LEVEL 2 CORROSION RT SILL PLATE AT FR17. REMOVED AND REPLACED RT STILL IAW EMB 170 SRM 51-40-02 AND 51-41-02.

Part: DOOR — CORRODED (LAVATORY SERVICE) · airframe 17,306 hrs · 10,773 cycles

LEVEL 2 CORROSION ON FWD INBOARD CORNER AROUND LATCHES OF WASTE DOOR. REMOVED AND REPLACED WASTE SERVICE DOOR IAW EMB 170 MM 53-03-60.

Part: ACTUATOR — MALFUNCTIONED (TE FLAP) · airframe 15,558 hrs · 9,727 cycles

FLAP FAIL MESSAGE ON FINAL APPROACH INTO YHZ WHEN FLAPS WERE SELECTED 3. CANCELLED APPROACH AND RAN QRH. MESSAGE DISAPPEARED WHEN FLAPS RETRACTED. ON NEXT APPROACH MESSAGE RETURNED WHEN FLAPS BROUGHT FROM 1 TO 2. RAN QRH AND WHEN LEVER BROUGHT BACK TO 1 MESSAGE REMAINED ILLUMINATED. SLATS WERE AT 3 AND FLAPS AT 2, WHICH DID NOT AGREE WITH FLAPS 1 SELECTED. FINISHED QRH AND DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. ON CALL MAINTENANCE INSPECTED IAW FIM 27-51-00, NO FAULTS FOUND. OPS CHECK GOOD. A/C WAS ROUTED INTO IND WHERE R1, R2, R3, R4, AND L1 FLAP ACTUATORS WERE REPLACED AND SI 275057 TO CLEAN AND LUBE FLAP TRACKS WAS COMPLIED WITH.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,353 hrs · 7,253 cycles

LEVEL 2 CORROSION ON CENTER SHEAR PANEL BETWEEN FR 87 AND FR 88. REPLACED CENTER SHEAR PANEL IAW EMB SRM 51-41-01.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,398 hrs · 7,253 cycles

LT BEAM BETWEEN FR 86 AND FR 89 LEVEL 2 CORROSION. REMOVED AND REPLACED LT BEAM BETWEEN FR 86 AND FR 89 IAW SRM 51-41-00 AND 51-43-01.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,353 hrs · 7,253 cycles

LEFT I/B UPPER GUSSET PLATE AT FR90 LEVEL 2 CORROSION. REMOVED AND REPLACED LEFT I/B UPPER GUSSET PLATE AT FR90 IAW SRM 51-41-02.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,353 hrs · 7,253 cycles

LEFT BEAM UPPER SHEET BETWEEN CROSS BEAM FR 85 TO FR 86 LEVEL 2 CORROSION. REPLACED IAW SRM 51-43-03 AND 51-21-01.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,353 hrs · 7,253 cycles

LEVEL 2 CORROSION ON RT SHEAR PANEL BETWEEN FR87 AND FR88. REPLACED RT SHEAR PANEL IAW SRM 51-41-01 AND 51-42-02.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,353 hrs · 7,253 cycles

WASTE SERVICE BAY INNER DOUBLER LEVEL 2 CORROSION. REPLACED DOUBLER IAW SRM 51-43-04.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,398 hrs · 7,253 cycles

LEVEL 2 CORROSION ON RT BEAM BETWEEN FR86 AND FR89. REMOVED AND REPLACED RT BEAM BETWEEN FR 86 AND FR 89 IAW SRM 51-41-00 AND 51-43-01.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,353 hrs · 7,253 cycles

LEVEL 2 CORROSION ON LT SHEAR PANEL BETWEEN FR 87 AND FR 88. REPLACED LT SHEAR PANEL IAW EMB 170 SRM 51-41-01 AND 51-42-02.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,398 hrs · 7,253 cycles

RIGHT UPPER GUSSET PLATE AT FR90 LEVEL 2 CORROSION. REMOVED AND REPLACED GUSSET PLATE AT FR90 IAW SRM 51-41-02.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,398 hrs · 7,253 cycles

RIGHT O/B UPPER GUSSET PLATE AT FR90 LEVEL 2 CORROSION. REMOVED AND REPLACED RIGHT O/B UPPER GUSSET PLATE AT FR90 IAW SRM 51-41-02.

Part: FLAP SYSTEM — MALFUNCTIONED (LE FLAPS) · airframe 9,638 hrs · 6,149 cycles

FLIGHT 7533, ON DESCENT, CREW SELECTED FLAPS (1) AND GOT SLAT FAIL MESSAGE FOLLOWED BY SPOILER FAULT AND SHAKER ANTICIPATED. RECYCLED TO ZERO AND MESSAGES WENT AWAY. ON SECOND RECYCLE SLAT FAIL MESSAGE REMAINED. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ON-CALL MAINTENANCE CLEARED SF-ACE INHIBITS AND RELEASED MOTOR BRAKE. HAS NOT REPEATED THIS DATE 05/07/2008.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 4,936 hrs · 3,241 cycles

FLIGHT 7637 IND TO ORD. CREW NOTIFIED BY THE B FLIGHT ATTENDANT THAT THERE WAS A SMOKE SMELL, LITE SMOKE, AND THE AFT LAVATORY SMOKE DETECTOR WAS GOING OFF. APU OVERSERVICED WITH OIL.