N908WN

Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 57,715 hrs · 34,816 cycles

CRACKED CARGO TRACK, RBL 13.84, BTW BS 727D - 787. PERFORMED A PERMANENT REPAIR ON THE CARGO TRACK IAW SRM 53-00-53-2R-3, REPAIR 3, PARAGRAPH 2 A, FIGURE 203, ALTERNATIVE 1 & 2.

Part: ACCESS PANEL — DAMAGED (ZONE 500) · airframe 57,715 hrs · 34,816 cycles

ELONGATED HOLES ON ACCESS PANEL 561AB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 561AB IAW B737-700 SRM 51-70-04-<BR>2R-10 REPAIR 10.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 57,715 hrs · 34,816 cycles

MAIN CABIN - FLOOR STRUCTURE SUPPORT HAS A CRACK AT BS 540; BL 0 TO LBL 24.75. REPLACED BREAK PANEL SUPPORT AND FASTENERS ON FLOOR STRUCTURE STA 540 BL 0 TO LBL 24.75 AT MAIN CABIN I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG 143A0060 SHEET 46 REV-.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 57,715 hrs · 34,816 cycles

AAI INSPECTION: MAIN CABIN - FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75. REPLACED BREAK PANEL SUPPORT AND FASTENERS ON FLOOR STRUCTURE STA 540 BL0 TO RBL 24.75 AT MAIN CABIN B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG 143A0060 SHEET 46 REV-.

Part: WEB — CORRODED (ZONE 200) · airframe 57,715 hrs · 34,816 cycles

MAIN CABIN - AFT BULKHEAD FRAME 1016; UPPER WEB STRUCTURE FITTING HAS CORROSION AT BS 1016; BL 0. REPLACED FITTING LOC. AFT BULKHEAD FRAME BS 1016; UPPER WEB STRUCTURE AND BL 0 I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 DWG 148A2237 SHEET 1 REV-.

Part: ACCESS PANEL — DAMAGED (ZONE 500) · airframe 57,715 hrs · 34,816 cycles

ELONGATED HOLE ON ACCESS PANEL 561BB TRAILING EDGE HOLES AT LT WING . REPAIRED ACCESS PANEL 561BB TRAILING EDGE HOLES AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.

Part: ACCESS PANEL — DAMAGED (ZONE 500) · airframe 57,715 hrs · 34,816 cycles

ELONGATED HOLE ON ACCESS PANEL 561CB TRAILING EDGE HOLES AT LT WING. REPAIRED ACCESS PANEL 561CB IAW B737-700 SRM 51-70-04-<BR>2R-10 REPAIR 10.

Part: HANDLE — DETERIORATED (ZONE 800) · airframe 57,715 hrs · 34,816 cycles

DETERIORATED ENTRY DOORWAY LINING HANDLE NUTS AT FWD GALLEY AREA (4EA). REPLACED ENTRY DOORWAY LINING HANDLE NUTS AT FWD GALLEY AREA (4EA) IAW B737-700 AMM 52-11-31-400-802 STEP 3.G ITEM 2.

Part: LIGHT — DETERIORATED (ZONE 200) · airframe 57,715 hrs · 34,816 cycles

DETERIORATED PHOTOLUMINESCENT STRIP (5EA) LH AND (5EA) RH SIDE AT PASSENGER CABIN. REPLACED THE PHOTOLUMINESCENT STRIP (5EA) LT AND (5EA) RT SIDE IN PAX CABIN IAW AMM 33-51-15-400-802.

Part: BRACKET — CRACKED (ZONE 100) · airframe 57,715 hrs · 34,816 cycles

CRACK BRACKET LOCATED BS 540 LBL 6 AT AIR CONDITIONING BAY. REPLACED BRACKET LOCATED BS 540 LBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND SRM 51-40-02-0G-0.

Part: ANGLE — CRACKED (ZONE 500) · airframe 57,715 hrs · 34,816 cycles

CRACK ACCESS PANEL 551FB TRAILING EDGE ANGLE AT LT WING. REPLACED ANGLE ON ACCESS PANEL 551FB TRAILING EDGE ANGLE AT LT WING AT LT WING IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 115A2710 SHEET 9 REV A<BR>MEASURE OF CRACK IS L=0.611.

Part: NUT PLATE — CORRODED (ZONE 500) · airframe 57,715 hrs · 34,816 cycles

CORROSION ON RAIL NUTPLATES LOCATED LEADING EDGE OFSS331 AT LT WING. REPLACED RAIL NUTPLATES LOCATED LEADING EDGE OFSS331 AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.

Part: HINGE — CORRODED (ZONE 200) · airframe 57,715 hrs · 34,816 cycles

CORROSION HINGE TOILET SERVICE DOOR 145AL AT LOWER FUSELAGE (2 EA). REPLACED HINGE TOILET SERVICE DOOR 145AL (2EA) I.A.W B737-700 SOPM 20-50-01 REV 39 AND DWG 146A7410-6 SHEET 6 REV -.

Part: NUT PLATE — CORRODED (ZONE 500) · airframe 57,715 hrs · 34,816 cycles

CORROSION ON RAIL NUT PLATES LEADING EDGE LOCATED OFSS449 AT LT WING. REPLACED RAIL NUT PLATES LEADING EDGE LOCATED OFSS449 AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.

Part: SHIELD — CORRODED (ZONE 100) · airframe 57,715 hrs · 34,816 cycles

CORROSION WEB SHIELD, BTW BS 767 - 794, RBL 23, WL156. REPLACED THE WEB SHIELD IAW SRM 51-10-02-0G-0, ITEM 9, AND DWG 146A0081, SHEET 37, REV-.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 57,715 hrs · 34,816 cycles

CRACK WEB - INTERCOSTAL BTW BS 727A - 727B, LBL 24. REPLACED WEB - INTERCOSTAL AND FASTENERS IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, PARAGRAPH 9, DRAWING 146A7502, SHEET 27, REV -, AND DRAWING 146A7500, SHEET 116, REV -.

Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 57,715 hrs · 34,816 cycles

CRACKED CARGO TRACK LBL 17.24, BS 767. PERFORMED A PERMANENT REPAIR ON THE CARGO TRACK IAW SRM 53-00-53-2R-3, REPAIR 3, PARAGRAPH 2 A, FIGURE 203, ALTERNATIVE 1 & 2.

Part: ANGLE — CRACKED (ZONE 100) · airframe 57,715 hrs · 34,816 cycles

CRACKED ANGLE LOCATED BTW BS907 TO BS927 AND BTW STR25R TO STR27R AT AFT CARGO COMPARTMENT. REPLACED ANGLE AND FASTENERS LOCATED BTW BS907 TO BS927 AND BTW STR25R TO STR27R AT AFT CARGO COMPARTMENT IAW DWG 147A7221, SHEET 24, REV-, SRM 51-40-02-0G-0 & SRM 51-10-02-0G-0.

Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 57,715 hrs · 34,816 cycles

CORROSION WEB - INTERCOSTAL BTW BS 727A - 727B, RBL 14, WL 148. REPLACED WEB - INTERCOSTAL IAW SRM 51-10-02-0G-0, PARAGRAPH 9, DWG 146A7500, SHEET 114, REV-, DWG 146A1201, SHEET 50, REV-.

Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 57,715 hrs · 34,816 cycles

CRACK TRACK RBL 13.84, BS 727C - 727E, BS 747- 767. PERFORMED A PERMANENT REPAIR ON THE CARGO TRACK IAW SRM 53-00-53-2R-3, REPAIR 3, PARAGRAPH 2 A, FIGURE 203, ALTERNATIVE 1.

Part: WEB — CORRODED (ZONE 100) · airframe 57,715 hrs · 34,816 cycles

CORROSION WEB - INTERCOSTAL LOCATED BTW BS767 TO BS787 RBL23 WL156 AT AFT CARGO COMPARTMENT. REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BTW BS767 TO BS787 RBL23 WL156 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG 146A0081 SHEET 37 REV -.

Part: FITTING — CRACKED (ZONE 100) · airframe 57,715 hrs · 34,816 cycles

CRACK FITING LOCATED BS947.5 AT LEVEL STR26L AT AFT CARGO COMPARTMENT. REPLACED FITING LOCATED BS947.5 AT LEVEL STR26L AT AFT CARGO COMPARTMENT I.A.W SRM 51-40-02 AND DWG 149A8103 SHEET 7 REV. A

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 57,715 hrs · 34,816 cycles

CRACKED SUPPORT ANGLE, BS 867, LBL12 IN AFT CARGO COMPARTMENT. REPLACED ANGLE - SUPPORT LOCATED BS867 LBL12 AT AFT CARGO COMPARTMENT IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 149A8102 SHEET: 17 REV: -. MEASUREMENT OF CRACK L: 0.690.

Part: ANGLE — CRACKED (ZONE 600) · airframe 57,715 hrs · 34,816 cycles

CRACK ON ANGLE LOCATED AUXILIARY TRACK SLAT 7 RH WING. REPLACED ANGLE LOCATED AUXILIARY TRACK SLAT 7 RH WING IAW B737-700 SRM 51-40-02 AND DWG# 114A5020 SHEET: 40 REV: A .

Part: ANGLE — CRACKED (ZONE 500) · airframe 57,715 hrs · 34,816 cycles

CRACK ON ANGLE LOCATED AUXILIARY TRACK SLAT 1 LH WING . REPLACED ANGLE LOCATED AUXILIARY TRACK SLAT 1 LH WING IAW B737-700 SRM 51-40-02 AND DWG# 114A5010 SHEET: 14 REV: C.

Part: PRESSURE DECK — CRACKED (ZONE 100) · airframe 57,715 hrs · 34,816 cycles

CRACK INDICATION ON THE HORIZONTAL PRESSURE DECK WEB, RBL 40, BS 663. CRACK LENGTH 0.312 INCH APPROX. REPAIRED THE PRESSURE DECK IAW SRM 53-40-51?2R-2, REPAIR 2.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 57,715 hrs · 34,816 cycles

CORRODED FLOORBEAM, BS 986.5, RBL 43, WL 208.1. REPAIRED THE FLOORBEAM IAW EA 25-153-02825-WIP1, EA 25-153-02825-WIP2, AND EA 25-153-02825.

Part: TIE CLIP — CRACKED (ZONE 200) · airframe 57,715 hrs · 34,816 cycles

CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA. REPLACED TIE CLIP AND FASTENERS LOCATED STA277 AND STR10R PASSENGER CABIN IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A1110, SHEET 18 REV- .

Part: PLATE — CORRODED (ZONE 200) · airframe 57,715 hrs · 34,816 cycles

CORROSION ON PLATE LOCATED 1016 PLUS 14 INCHES RBL 4 WL 208.1 AT PASSENGER CABIN. REPLACED PLATE LOCATED BTW BS1006 TO BS1030 RBL 4 WL 208.1 AT PASSENGER CABIN IAW SRM 51-10-02-0G-0 ;SRM 51-40-02-0G-0 AND DWG 147A5600 SHEET 32 REV B.

Part: SHIELD — CORRODED (ZONE 100) · airframe 57,715 hrs · 34,816 cycles

CORROSION WEB SHIELD, BETWEEN BS 492.4 - 500A, RBL 24, WL 156. REPLACED WEB SHIELD AND FASTENERS IAW SRM 51-40-02, DWG 143A0080, SHEET 23, REV-, AND SRM 51-10-02-0G-0, PARAGRAPH 9.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,715 hrs · 34,816 cycles

CORROSION ON SUPPORT ZEE BTW BS 500C - 500D, RBL 24, WL 156. REPLACED THE SUPPORT ZEE IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND DWG 143A7501, SHEET 1, REV B.

Part: ATTACH ANGLE — DETERIORATED (ZONE 200) · airframe 57,715 hrs · 34,816 cycles

DETERIORATED TARGET ATTACH ANGLE ON FWD ENTRY DOOR FRAME. REPLACED TARGET ATTACH ANGLE ON FWD ENTRY DOOR FRAME I.A.W B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 141A6101 SHEET 11 REV. -

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 57,715 hrs · 34,816 cycles

CRACKED WEB - INTERCOSTAL BETWEEN BS 500C - 500D, RBL 24. REPLACED THE WEB INTERCOSTAL IAW SRM 51-10-02-0G, ITEM 9, SRM 51-40-02-0G, AND DWG 143A7505, SHEET 82, REV-.

Part: PLATE — CORRODED (ZONE 200) · airframe 57,715 hrs · 34,816 cycles

CORROSION ON PLATE LOCATED 1016 PLUS 14 INCHES LBL 3 WL 208.1 AT PASSENGER CABIN. REPLACED PLATE AND FASTENERS LOCATED BTW BS1006 TO BS1030 LBL 3 WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9; AND DRAWING 147A5600 SHEET: 32 REV:B.

Part: ACCESS PANEL — DAMAGED (ZONE 600) · airframe 57,715 hrs · 34,816 cycles

ELONGATED HOLES ON ACCESS PANEL 661BB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.

Part: ACCESS PANEL — DAMAGED (ZONE 600) · airframe 57,715 hrs · 34,816 cycles

ELONGATED HOLES ON ACCESS PANEL 661AB TRAILING EDGE AT RT WING . REPAIRED ACCESS PANEL 661AB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.

Part: ACCESS PANEL — ELONGATED (ZONE 600) · airframe 57,715 hrs · 34,816 cycles

ELONGATED HOLES ON ACCESS PANEL 661CB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661CB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 57,715 hrs · 34,816 cycles

CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 40 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 40 WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 143A5400 SHEET 105 REV-.

Part: WEB — CRACKED (ZONE 200) · airframe 57,715 hrs · 34,816 cycles

CRACK ON WEB LOCATED BTW BS 277 TO BS 294.5 BL 0 WL 208.1 AT FWD GALLEY AREA. REPLACED WEB LOCATED BTW BS 277 TO BS 294.5 BL 0 WL 208.1 AT FWD GALLEY AREA IAW B73-700 SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51-40-02-0G-0 AND DWG DWG 141A5400 SHEET 20 REV-.

Part: FITTING — WORN (ZONE 800) · airframe 57,715 hrs · 34,816 cycles

WORN HARDWARE AND PLATE ON GIRT BAR FITTING ON AFT PAX DOOR. REPLACED THE HARDWARE AND PLATE ON GIRT BAR FITTING IAW AMM 25-66-02-400-801, STEP 3.D.(1)(G)(H)(J)(K).

Part: PLATE — WORN (ZONE 800) · airframe 57,715 hrs · 34,816 cycles

WORN HARDWARE AND PLATE, ON GIRT BAR FITTING. REPLACED THE HARDWARE AND PLATE ON THE GIRT BAR FITTING IAW AMM 25-66-02-400-801, STEP 3.D.(1)(G)(H)(J)(K).

Part: LENS — BROKEN (ZONE 200) · airframe 57,715 hrs · 34,816 cycles

BROKEN EMERGENCY LIGHT LENS ON OVERHEAD STOWAGE BIN LH SIDE AT PASSENGER CABIN (8 EA). REPLACED EMERGENCY LIGHT LENS ON OVERHEAD STOWAGE BIN LH SIDE AT PASSENGER CABIN (8 EA) IAW B737-700 AMM 33-51-03-960-801 STEP 2.D.(3)(A)(C).

Part: WEB — CRACKED (ZONE 200) · airframe 57,715 hrs · 34,816 cycles

CRACK ON WEB LOCATED BTW BS 312 TO BS 328 LBL 47 WL 208.1 AT FWD GALLEY AREA . REPLACED WEB LOCATED BTW BS 312 TO BS 328 LBL 47 WL 208.1 AT FWD GALLEY AREA IAW SRM 51-40-02-0G-0 ;SRM 51-10-02-0G-0 AND DWG 141A5410 SHEET 26 REV-.

Part: BULB — BURNED OUT (ZONE 200) · airframe 57,715 hrs · 34,816 cycles

BURNED EMERGENCY EXIT LIGHT BULB ON SIDEWALL 231YJW AT PASSENGER CABIN. REPLACED EMERGENCY EXIT LIGHT BULB ON SIDEWALL 231YJW AT PASSENGER CABIN IAW AMM 33-51-01-960-801.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 57,715 hrs · 34,816 cycles

CRACKED INTERCOSTAL, BTW BS 294.5 - 303.9, STRINGER 16L. REPAIRED THE INTERCOSTAL IAW EA 25-153-02830-WIP1, AND EA 25-153-02830.

Part: WEB — CRACKED (ZONE 200) · airframe 57,715 hrs · 34,816 cycles

CRACK ON WEB LOCATED BTW BS 328 TO BS 344 LBL 47 WL 208.1 AT FWD GALLEY AREA. REPLACED WEB LOCATED BTW BS 328 TO BS 344 LBL 47 WL 208.1 AT FWD GALLEY IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 141A5400 SHEET 44 REV-.

Part: ACCESS PANEL — CRACKED (ZONE 500) · airframe 57,715 hrs · 34,816 cycles

CRACK ACCESS PANEL 561CB TRAILING EDGE HOLES AT LT WING. REPAIRED ACCESS PANEL 561CB IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.

Part: ACCESS PANEL — CRACKED (ZONE 500) · airframe 57,715 hrs · 34,816 cycles

CRACK ACCESS PANEL 561BB TRAILING EDGE HOLES AT LT WING. REPAIRED ACCESS PANEL 561BB TRAILING EDGE HOLES AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.

Part: BRACKET — WORN (ZN 800 DOOR) · airframe 57,715 hrs · 34,816 cycles

WORN HARDWARE AND PLATE ON GIRT BAR FITTING. REPLACED THE HARDWARE AND PLATE IAW AMM 25-66-02-400-801 STEP 3.D.(1)(G)(H)(J)(K).

Part: BRACKET — WORN (ZONE 800) · airframe 57,715 hrs · 34,816 cycles

WORN HARDWARE AND PLATE ON GIRT BAR FITTING. REPLACED THE HARDWARE AND PLATE IAW AMM 25-66-02-400-801 STEP 3.D.(1)(G)(H)(J)(K).

Part: LENS — BROKEN (ZONE 200) · airframe 57,715 hrs · 34,816 cycles

BROKEN EMERGENCY LIGHT LENS ON OVERHEAD STOWAGE BIN RH SIDE AT PASSENGER CABIN (8 EA). REPLACED EMERGENCY LIGHT LENS ON OVERHEAD STOWAGE BIN RH SIDE AT PASSENGER CABIN (8 EA) IAW AMM 33-51-03-960-801 STEP 2.D(3)(A) AND STEP 2.D(3)(C).

Part: WEB — CRACKED (OZNE 200) · airframe 57,715 hrs · 34,816 cycles

CRACK ON INTERCOSTAL WEB LOCATED BTW BS 344 TO BS 360 LBL 26.75 WL 208.1 AT FWD GALLEY AREA. REPLACED INTERCOSTAL WEB LOCATED BTW BS 344 TO BS 360 LBL 26.75 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND DWG 141A5400 SHEET 31 REV-.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 57,715 hrs · 34,816 cycles

CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0; 51-10-02-0G-0 PARAGRAPH AND DWG 143A5400 SHEET 105 REV-.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 57,715 hrs · 34,816 cycles

CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 LBL 13 WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG: 143A5400; SHEET: 105; REV: -.

Part: ACCESS PANEL — CRACKED (ZONE 500) · airframe 57,715 hrs · 34,816 cycles

CRACK ACCESS PANEL 561AB TRAILING EDGE HOLES AT LT WING. REPAIRED ACCESS PANEL 561AB IAW B737-700 SRM 51-70-04-<BR>2R-10 REPAIR 10.

Part: NUT PLATE — CRACKED (ZONE 500) · airframe 57,715 hrs · 34,816 cycles

CRACK RAIL NUT PLATE LOCATED ORSS 297 TRAILING EDGE AT LT WING. REPLACED RAIL NUT PLATE LOCATED ORSS 297 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 ITEM 9 AND DWG:115A3712 SHEET: 5 REV: - AND PERFORMED ADJUSTMENT CHECK OF MISMATCH AT LOWER FIXED PANEL IAW AMM 27-51-21-820-801 STEP 2.G(8).<BR>DIMENSIONS WITHIN THE LIMITS.

Part: PLATE — DETERIORATED (ZONE 800) · airframe 57,715 hrs · 34,816 cycles

DETERIORATED GIRT BAR HARDWARE AND PLATE SERVICE DOOR AT FWD GALLEY. REPLACED GIRT BAR HARDWARE AND PLATE IAW AMM 25-66-02-400-801. TESTED OK.

Part: GIRT BAR — DETERIORATED (ZONE 800) · airframe 57,715 hrs · 34,816 cycles

DETERIORATED GIRT BAR HARDWARE AND PLATE ENTRY DOOR AT FWD GALLEY AREA. REPLACED THE GIRT BAR HARDWARE AND PLATE IAW AMM 25-66-02-400-801. TESTED OK.

Part: STIFFENER — CRACKED (ZONE 100) · airframe 57,715 hrs · 34,816 cycles

CRACK ON VERTICAL STIFFENER BS 540 AND RBL 24.97 BULKHEAD AREA FWD CARGO COMPARTMENT. REPLACED VERTICAL STIFFENER BS 540 AND RBL 24.97 BULKHEAD AREA FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DRAWING 111A2001 SHEET 76;77;78 REV- AND DRAWING 111A2000 SHEET 37 REV -.

Part: PLATE — DETERIORATED (ZONE 800) · airframe 57,715 hrs · 34,816 cycles

DETERIORATED GIRT BAR HARDWARE AND PLATE ENTRY DOOR AT FWD GALLEY AREA. REPLACED GIRT BAR HARDWARE AND PLATE ON THE ENTRY DOOR IAW AMM 25-66-02-400-801, TESTED OK.

Part: GIRT BAR — DETERIORATED (ZN 800 DOOR) · airframe 57,715 hrs · 34,816 cycles

DETERIORATED GIRT BAR HARDWARE AND PLATE ON SERVICE DOOR FWD. REPLACED THE GIRT BAR HARDWARE AND PLATE IAW AMM 25-66-02-400-801. TESTED OK.

Part: STIFFENER — CRACKED (ZONE 100) · airframe 57,715 hrs · 34,816 cycles

CRACK ON VERTICAL STIFFENER BS 540 AND LBL 24.97 BULKHEAD AREA FWD CARGO COMPARTMENT. REPLACED VERTICAL STIFFENER BS 540 AND LBL 24.97 BULKHEAD AREA FWD CARGO COMPARTMENT IAW SRM 51-10-02, SRM 51-40-02, AND DRAWING 111A2001, SHEET 76, 77, 78 REV- AND DRAWING 111A2000, SHEET 37, REV -.

Part: STIFFENER — CRACKED (ZONE 100) · airframe 57,712 hrs · 34,815 cycles

CUSTOMER REQUEST: PERFORM DETAIL VISUAL INSPECTION ON BS 540 BULKHEAD VERTICAL STIFFENERS BTW RBL 54.60 TO LBL 54.60 AT FWD CARGO COMPARTMENT. PERFORMED DETAILED VISUAL INSPECTION ON BS 540 BULKHEAD VERTICAL STIFFENERS BTW RBL 54.60 TO LBL 54.60 AT FWD CARGO COMPARTMENT AND FOUND CRACK ON VERTICAL STIFFENER LOCATED RBL 24.97 BS 540 SEE TTG8Q015JRAB AND VERTICAL STIFFENER LOCATED LBL 24.97 BS 540 SEE TTG8Q015JBVJ I.AW B737-700 SRM 51-10-04-0G-0.

Part: PLATE — MISSING (GIRT BAR) · airframe 57,564 hrs · 34,721 cycles

R2 DOOR AFT GIRT BAR PLATE ASSY MISSING. FOUND MISSING PLATE ASSEMBLY AND REINSTALLED IAW AMM 25-66-02.

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 56,814 hrs · 34,259 cycles

AFT CARGO HAS A 12 INCH CRACK ON A CENTER FLOOR PANEL PANEL 140 BF <[01]. PART ADDED; [02] OK TO CONTINUE PER MEL 25-16-01SP1B 262364; [03] REMOVED PANEL 140BF FROM AFT CARGO PANEL. REF: AMM 25-52-10;[04] FABRICATED AFT. CARGO PNL. I/A/W AMM. 25-52-10 INSTALLATION REQUIRED.; [05] INSTALLED FLOOR PANEL 140BF AFT CARGO CENTER FLOOR REF AMM 25-52-10-400-801-NG-01; [06] SEE MXI FOR INDIVIDUAL STEPS.

Part: LENS — DETACHED (ZONE 200) · airframe 56,091 hrs · 33,831 cycles

CREW REPORTS FWD SERVICE (R1) DOOR EMERGENCY EXIT LENSE FELL OFF.<[01] R&R EXIT SIGN LIGHT ASSEMBLY PER AMM 33-51-01. OPS CHECK GOOD

Part: SEAT BACK — OUT OF ADJUST (ZONE 200) · airframe 54,369 hrs · 32,805 cycles

ROW 12DEF WILL NOT STAY UPRIGHT<[01] OK TO CONTINUE PER MEL 25-6-01.;[02] REF AUTHORIZATION #215455.;[03] ADJUSTED ROW 12DEF SEATS BACK LIMIT BREAKOVER FORCE IAW AMM 25-22-00.<BR>REF L/P#2748650

Part: CONTROL UNIT — FAILED (WINDOW HEAT) · airframe 54,094 hrs · 32,632 cycles

CAPTS L1 WINDOW CRACKED IN FLIGHT<[01] CW;[02] R/R L FRONT WINDOW IAW AMM 56-11-11. <BR>R/R L FRONT WINDOW HEAT CONTROL UNIT IAW AMM 30-41-11. OPS CHECK NORMAL.

Part: WINDOW — CRACKED (ZONE 200) · airframe 54,094 hrs · 32,632 cycles

CAPTS L1 WINDOW CRACKED IN FLIGHT<[01] CW;[02] R/R L FRONT WINDOW IAW AMM 56-11-11. <BR>R/R L FRONT WINDOW HEAT CONTROL UNIT IAW AMM 30-41-11. OPS CHECK NORMAL.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,295 hrs · 31,498 cycles

LOUD POP/BANG ON TAKEOFF ROLL REJECTED TAKEOFF AT 120 KNTS. BRAKE COOL RETURNED 27.0M FT POUNDS. NO ABNORMAL ENGINE INDICATION OR WARNINGS. NO BIRDS WITNESSED ON TAKEOFF ROLL. NO ENGINE OR AIRFRAME VIBRATIONS NOTED<[01] PERFORMED BIRD STRIKE INSPECTION PER AMM 05-51-18; NO BIRD STRIKE NOTED. INSPECTED ALL TIRES PER AMM 32-45-00; PRESSURES GOOD NO DISCREPANCIES NOTED. PERFORMED EEC BITE ON #1 AND #2 ENGINES; NO FAULTS NOTED PER FIM 73-00 TASK 801. RAN PACKS WITH APU BLEED; PRESSURE AND PACKS OPS NORMAL PER AMM 21-00-00. NO HIGH ENERGY STOP NOTED AND BRAKE COOLING COMPLIED WITH PER AMM 05-51-07. AIRCRAFT OK FOR SERVICE

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 51,548 hrs · 31,049 cycles

EMERGENCY INDICATOR LIGHT ON RAW 20ABC INOP.<[01] RECONNECTED AND RELAMPED EMERGENCY INDICATOR LIGHT ON R0W 20ABC PER AMM 33-51-03-960-801.;[02] VERIFIED.<BR>VERIFIED MEASUREMENTS.

Part: LIGHT — MISSING (ZN 200 FUS TOP) · airframe 51,548 hrs · 31,049 cycles

L1190 EMERGENCY EXIT LIGHT INDICATOR LH AFT GALLEY NOT FOUND.<[01] REPLACED AND PERFORMED GOOD INSTALLATION CHECK FOR L1190 EMERGENCY EXIT LIGHT INDICATOR LH AFT GALLEY PER AMM 33-51-01-960-802.;[02] VERIFIED.<BR>VERIFIED MEASUREMENTS.

Part: BAFFLE — CRACKED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

FWD CARGO BAY BAFFLE AT BS 400 TO 420 LBL 24 IS CRACKED AT UPPER FWD FASTENER HOLE<[01] REMOVED AND REPLACED AT FWD CARGO BAY BAFFLE BETWEEN BS 400 TO 420 LBL 24 WL 155 IAW SRM 51-10-02; SRM 51-40-02. DWG#143A7505.;[02] VERIFIED CORRECTIVE ACTION AND MEASUREMENTS TABLE. CARD COMPLETE.

Part: FITTING — CORRODED (ZN 800 DOOR) · airframe 51,548 hrs · 31,049 cycles

CORROSION ON FWD ENTRY DOOR UPPER HINGE BOX FITTING<[01] REMOVED AND REPLACED FWD ENTRY DOOR UPPER HINGE BOX FITTING IAW SRM 51-40-02 AND DWG #141A8180;[02] VERIFIED CORRECTIVE ACTION 1;[03] VERIFIED MEASUREMENT TABLE

Part: SHIELD — CORRODED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

CORROSION; FLOOR TO SIDEWALL SUPPORT (SIDE SHIELD); BS 767; +3 +7; +11; RBL22; WL156<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT (SHIELD) BS767-793 RBL 22 WL 156 I.A.W SRM 51-10-02-0G PAR 9C; SRM 51-40-02-0G-0 AND DWG 146A0081.;[02] VERIFIED CORRECTIVE ACTION #1

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

CORROSION; FLOOR TO SIDEWALL SUPPORT; BS 767; +5 +10; =14; +18; LBL22; WL156<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BS 727 TO BS 847 LBL 22 IAW SRM 51-40-02 AND DWG 146A7500;[02] THIS CARD WILL BE ACCOMPLISHED ON CUSTOMER CARD NBR: TTG8Q00NY14E;[03] VERIFIED CORRECTIVE ACTION #2.

Part: SUPPORT ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

CORROSION; FLOOR TO SIDEWALL SUPPORT; BS 767; RBL22; WL156<[01] REMOVED CORROSION FROM AFT CARGO BEY FLOOR TO SIDE WALL SUPPORT ANGLE IN AREA OF (2'X2'X0.025'DEEP) AT BS 767; RBL 22; WL 156; OUT OF 0.040' ORIGINAL MATERIAL THICKNESS FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2 DET.4A; FIG 103-D<BR><BR>THIS FAULT WILL BE ACCOMPLISHED ON CARD # TTG8Q00NY164.;[02] VERIFIED CORRECTIVE ACTION AND MEASUREMENTS TABLE. REPAIR WILL BE ACCOMPLISHED ON CARD # TTG8Q00NY164. <BR>CARD COMPLETE.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

CORROSION; FLOOR TO SIDEWALL SUPPORT; BS767; LBL22; WL156<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BS 727 TO BS 847 LBL 22 IAW SRM 51-40-02 AND DWG 146A7500;[02] ALL MAINTENANCE ACTION COMPLETED.;[03] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BS 727 TO BS 847 LBL 22 IAW SRM 51-40-02 AND DWG 146A7500;[04] VERIFIED CORRECTIVE ACTION 1-3

Part: SUPPORT ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

CORROSION; FLOOR TO SIDEWALL SUPPORT; BS 747; +4 +6; +8; RBL22; WL156<[01] REMOVED CORROSION FROM AFT CARGO BEY FLOOR TO SIDE WALL SUPPORT ANGLE IN AREA OF (1'X2'X0.020'DEEP) AT BS 747+4; (1.5'X2'X0.015'DEEP) AT BS 747+6; (2.5'X1.2'X0.010'DEEP) AT BS 7247+8; RBL 22; WL 156; OUT OF 0.040' ORIGINAL MATERIAL THICKNESS FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2 DET.4A; FIG 103-D<BR><BR>THIS FAULT WILL BE ACCOMPLISHED ON CARD # TTG8Q00NY164.;[02] VERIFIED CORRECTIVE ACTION AND MEASUREMENTS TABLE. REPAIR WILL BE ACCOMPLISHED ON CARD # TTG8Q00NY164. <BR>CARD COMPLETE.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

CORROSION; FLOOR TO SIDEWALL SUPPORT; BS 747; +14 +18; LBL22; WL156<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BS 727 TO BS 847 LBL 22 IAW SRM 51-40-02 AND DWG 146A7500;[02] THIS CARD WILL BE ACCOMPLISHED ON CUSTOMER CARD NBR: TTG8Q00NY14E;[03] VERIFIED CORRECTIVE ACTION #2.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

CORROSION; FLOOR TO SIDEWALL SUPPORT; BS 727E; +2 +6; 10; +14; +18; RBL22; WL156<[01] REMOVED; FABRICATED AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT BS 727 TO BS 767 RBL 22; PER SRM 51-40-02 AND DWG 146A7500.;[02] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 1 AND MEASUREMENT TABLE.

Part: BEAM — CRACKED (ZN 800 DOOR) · airframe 51,548 hrs · 31,049 cycles

CRACK FOUND DURING HFEC INSPECTION OF #5 BEAM 1' FROM I/B EDGE. MEASURED AT L:0.8' MARKED<[01] ALL WORK PERFORMED TO ADDRESS CRACK FOUND DURING HFEC INSPECTION OF #5 BEAM 1' FROM I/B EDGE MEASURED AT L:0.8' WAS ACCOMPLISHED ON WO# P7769598-1;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.

Part: BEAM — CRACKED (ZN 800 DOOR) · airframe 51,548 hrs · 31,049 cycles

CRACK FOUND DURING HFEC INSPECTION OF #4 BEAM 1' FROM I/B EDGE. MEASURED AT L:0.9' MARKED<[01] ALL WORK PERFORMED TO ADDRESS CRACK FOUND DURING HFEC INSPECTION OF #4 BEAM 1' FROM I/B EDGE MEASURED AT L:0.9' WAS ACCOMPLISHED ON WO# P7769598-1;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.

Part: FRAME — CRACKED (ZN 800 DOOR) · airframe 51,548 hrs · 31,049 cycles

BS312 FRAME IS CRACKED IN RADIUS OF FRAME AT FWD ENTRY DOOR HEADER FRAME<[01] REPAIRED IN CUSTOMER FAULT TTG8Q00NY1TZ;[02] REPAIRED PER EA M-22-153-01244

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS500 - BS500D LBL23 WL156.<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BETWEEN BS 400 - BS 500D LBL 23 WL 156 IAW SRM 51-40-02 AND DWG#143A7500.;[02] CORRECTED : REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BETWEEN BS 396 - BS 500D LBL 23 WL 156 IAW SRM 51-40-02 AND DWG#143A7500.;[03] VERIFIED CORRECTIVE ACTION 2 AND MEASUREMENTS TABLE. CARD COMPLETE.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS400 LBL24 WL155.<[01] REMOVED AND REPLACED CLIP (ATTACH ANGLE) AT FWD CARGO BAY BS 400 LBL 24 IAW SRM 51-10-02 SRM 51-40-02 AND DWG# 143A7505.;[02] VERIFIED CORRECTIVE ACTION AND MEASUREMENTS TABLE. CARD COMPLETE.

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. MARKED<[01] REMOVED AND REPLACED GUSSET BS500D S-19R WL193<BR>IAW SRM 51-40-02 & DWG 143A7902

Part: FLOORBEAM — CORRODED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

CORROSION FLOOR BEAM UPPER CHORD BS 987 RBL 48 WL 208<[01] ACCOMPLISHED REPAIR ON FAULT#TTG8Q00NU8D9 PER SRM 53-70-51-2R-4 REPAIR 4 AND PER EA#23-153-03055-WIP1;[02] VERIFIED CORRECTIVE ACTION #1

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

FWD FLOOR PANEL 221GF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] VERIFIED COMPLETION OF REPAIR OF UPPER SKIN ON PANEL 221GF IAW SRM 53-00-50-2R-1;[02] VERIFIED CORRECTIVE ACTION ITEM 1 COMPLETED.;[03] VERIFIED MEASUREMENT TABLE COMPLETED.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

FWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH ASERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.1.A DUE TO AMOUNT OF ALL DAMAGE.;[02] REPLACED PANEL. JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

AFT FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241XF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[02] VERIFIED CORRECTIVE ACTION #1

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

AFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS<[01] AFT FLOOR PANEL 241AAF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: SILL DRAIN — CORRODED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

R/H AFT MOPSIL HAS CORROSION BS 955 RBL 55; BS 959 RBL 55; AND BS 967-987 RBL 50<[01] REMOVED AND REPLACED ASD MOP SILL I.A.W SRM 51-10-02-0G-0 PAR 9C; SRM 53-10-15-1A-1 ALLOWABLE DAMAGE 1; SRM 51-40-02-0G AND DWG 147A8501.;[02] VERIFIED CORRECTIVE ACTION 1

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

AFT FLOOR PANEL 242VCF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 242VF<[01] AFT FLOOR PANEL 242VCF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[02] VERIFIED MEASUREMENTS TABLE.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

FWD FLOOR PANEL 221EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] VERIFIED COMPLETION OF REPAIR OF UPPER SKIN ON PANEL 221EF IAW SRM 53-00-50-2R-1;[02] VERIFIED CORRECTIVE ACTION ITEM 1 COMPLETED.<BR>VERIFIED MEASUREMENT TABLE COMPLETED.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

FWD FLOOR PANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221CF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS/TAPES TO THIS FAULT RECORD.;[02] FINAL INSPECTION. JOB COMPLETE.<BR><BR>VERIFIED MEASUREMENTS TABLE.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

FWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEET TO THIS FAULT RECORD.;[02] FINAL INSPECTION. JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

AFT FLOOR PANEL 241ACF UPPER SKIN PREVIOUS REPAIR HAS AREAS OF PULLED STRANDS.<[01] REPAIRED AFT FLOOR PANEL 241ACF UPPER SKIN PULLED STRANDS IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.

Part: FLOOR SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

INTERCOSTAL CRACKED BS 380-400 BL 0 WL 208<[01] REMOVED AND REPLACED ANGLE TO INTERCOSTAL BS 380-400 BL 0 WL 208 I.A.W SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PAR 9C AND DWG 143A5400.;[02] VERIFIED.<BR>VERIFIED MEASUREMENTS.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

FWD FLOOR PANEL 222BF UPPER SKIN PREVIOUS REPAIR HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222BF UPPER SKIN PREVIOUS REPAIR WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] REPLACED PANEL. JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

AFT FLOOR PANEL 241ADF UPPER SKIN PREVIOUS REPAIR HAS AREAS OF PULLED STRANDS.<[01] REMOVED FAILED PREVIOUS REPAIR THEN REPAIRED UPPER SURFACE OF AFT FLOOR PANEL 241ADF IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

FWD FLOOR PANEL 221FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221FF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT FO ALL DAMAGE.;[02] REPLACED PANEL. JOB COMPLETE.

Part: STRINGER — CORRODED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

STRINGER 25R; BS 539 HAS CORROSION AROUND FASTENERS COMMON TO SKIN<[01] STRINGER 25R; BS 539 CORROSION AROUND FASTENERS COMMON TO SKIN WAS 'REPAIRED PER EA 23-153-03025. THIS IS A CATEGORY A REPAIR AS DEFINED IN 737-700 SRM 51-00-06.';[02] VERIFIED STEPS COMPLETE; CORRECTIVE ACTION COMPLETE WITH MEASUREMENTS

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

FWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222CF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

FWD FLOOR PANEL 221DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] REPLACED PANEL. JOB COMPLETE.

Part: FLOOR SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

INTERCOSTAL CRACKED BS 312-328 RBL 30 WL 208<[01] REMOVED AND REPLACED INTERCOSTAL BS 312-328 RBL30 WL 208 I.A.W SRM 51-40-05-0G-0; SRM 51-40-02-G-0 AND DWG 141A5400.;[02] VERIFIED CORRECTIVE ACTION 1.<BR>VERIFIED MEASUREMENTS TABLE.<BR>JOB COMPLETE.

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

GUSSET AT STRINGER 19L BS 500D IS CRACKED<[01] REMOVED AND REPLACED GUSSET AT STRINGER 19L BS 500D IAW SRM 51-10-02 SRM 51-40-02 DWG# 143A7902.;[02] VERIFIED MEASUREMENTS TABLE.

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

GUSSET AT STRINGER 21L BS 500D IS CRACKED<[01] REMOVED AND REPLACED GUSSET AT STRINGER 21L BS 500D IAW SRM 51-10-02 SRM 51-40-02 DWG# 143A7902.;[02] VERIFIED MEASUREMENTS TABLE.;[03] CORRECTION FOR STEP 5; IS RII.

Part: FLOORBEAM — CORRODED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

CORROSION ON BS 986 FLOORBEAM; RBL 46; WL 208<[01] REPAIRED PASSENGER FLOORBEAM BS 986 IAW SRM 53-70-51-2R-4 REPAIR 4 AND PER EA#23-153-03055-WIP-1;[02] CORROSION ON BS 986 FLOORBEAM; RBL 46; WL 208 WAS REPAIRED IAW EA 23-153-03055;[03] VERIFIED STEPS COMPLETE; CORRECTIVE ACTION COMPLETE WITH MEASUREMENTS

Part: FLOORBEAM — CORRODED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

CORROSION ON BS 986 FLOOR BEAM; LBL46; WL208<[01] ACCOMPLISHED REPAIR PER SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4 FIGURE 205;[02] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASUREMENT TABLE.

Part: SEAL — CRACKED (ZN 300 STABILIZE) · airframe 51,548 hrs · 31,049 cycles

RT. HORIZONTAL STAB UPPER FORWARD SLIDE SEAL CRACKED.<[01] VERIFIED STEP 5 IN PARTIAL ITEM 1; OK TO INSTALL GIVEN.;[02] REMOVED AND REPLACED RT HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-400-802.;[03] VERIFIED.<BR>VERIFIED MEASUREMENTS.

Part: PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 51,548 hrs · 31,049 cycles

PANEL 195CL AFT CORNER RADIUS IS CRACKED.<[01] CRACKED AFT CORNER RADIUS ON PANEL 195CL WERE REPAIRED IAW SRM 51-70-05-2R-6.;[02] VERIFIED CRACKED AFT CORNER RADIUS ON PANEL 195CL WERE REPAIRED IAW SRM 51-70-05-2R-6.

Part: PANEL — CRACKED (ZN 500 LEFT WING) · airframe 51,548 hrs · 31,049 cycles

LT WING L/E PANEL 521TB FWD O/B CORNER IS CRACKED (MARKED)<[01] LT WING L/E PANEL 521TB FWD O/B CORNER WITH CRACK WAS REPAIRED IAW SRM 51-70-05-2R-6.;[02] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTS

Part: STIFFENER — CRACKED (ZN 300 STABILIZE) · airframe 51,548 hrs · 31,049 cycles

RH HORIZONTAL STABILIZER RIB 5 (STAB STA. 129.50); 3RD STIFFENER FROM FRONT SPAR; BOTTOM AREA WITH A CRACK.<[01] NDI REQUEST TO VERIFY CRACK AT DISCREPANCY AREA.;[02] HFEC INSPECTED SUSPECTED CRACK AREA IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23.<BR>CRACK NOTED AT DISCREPANCY AREA.<BR>EQUIP USED:<BR>-NORTEC 500D ID: IS000680 CAL DUE: 05/2024;[03] REMOVED THE DAMAGED PART AT RH HORIZONTAL STABILIZER STA 129.50 RIB 3RD VERTICAL STIFFENER AND INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-4;[04] VERIFIED CORRECTIVE ACTION ITEM 3.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 50,106 hrs · 30,093 cycles

R/H AFT EXTERIOR EMERGENCY EXIT LT INOP.<[01] RELAMPED AFT R/H EE EXTERIOR LT IAW AMM 33-51-04.

Part: COWLING — PULLED (ZN 400 NACELLE/P) · airframe 50,091 hrs · 30,084 cycles

#1 ENGINE OUTBID SIDE COWL HAS MULTIPLE WORKING RIVETSON NO COWL PULLING THRU<[01] REMOVED AND REPLACED #1 ENGINE INLET COWL PER AMM 71-11-01

Part: SIGN — MISSING (ZN 800 DOOR) · airframe 49,889 hrs · 29,952 cycles

EMERGENCY EXIT LIGHT LENS COVER AFT OF L2 DOOR MISSING BOTTOM ATTACHMENT SCREW (MARKED)<[01] REPLACED L2 DOOR EXIT SIGN ASSEMBLY IAW AMM 33-51-01. OPS CHECK GOOD.;[02] CW INSPECTION PER AMM 33-51-01

Part: PANEL — DAMAGED (ZN 100 FUS LOWER) · airframe 49,780 hrs · 29,884 cycles

3 RIPS FOUND IN FWD CARGO BIN FLOOR.<[01] OK TO CONTINUE PER MEL#25-16-01; SP-1B.<BR>AUTH#122455;[02] R&R FWD CARGO FLOOR PANEL IAW AMM 25-52-10

Part: LIGHT — INOPERATIVE (PAX CABIN) · airframe 48,161 hrs · 28,832 cycles

LEFT SIDE OVER WING EMERGENCY EXIT FLOOD LIGHT INOP<[01] OK TO CONTINUE PER MEL 33-2-03. SP 1B;[02] RELAMPED L/H OVERWING EMER.EXIT FLOOD LIGHT I.A.W AMM 33-51-01<BR>OPS CHCK GOOD.

Part: EPSU — INOPERATIVE · airframe 47,580 hrs · 28,455 cycles

EMERGENCY AREA AISLE LIGHTS INOP AT ROWS 1 AND 4 L/H SIDE. / [01] REPLACED THE FWD GALLEY (M1675) EMERGENCY POWER SUPPLY AND BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 46,061 hrs · 27,534 cycles

SUPPLEMENTAL INFORMATION: EMERGENCY EXIT LIGHT BATTERY PACK (M1673 AFT GALLEY; CEILING; L/H) WILL NOT CHARGE ; EMERGENCY EXIT LIGHT BATTERY PACK (M1673 AFT GALLEY; CEILING; LH) WILL NOT CHARGE / [01] REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1673; OPS CHECK GOOD IAW AMM 33-51-06-960-805.; [02] VERIFIED STEP 1<BR>AUDIT CW

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 46,061 hrs · 27,534 cycles

SUPPLEMENTAL INFORMATION: EMERGENCY EXIT LIGHT BATTERY PACK (M1672 AFT GALLEY; CEILING; R/H) WILL NOT CHARGE ; EMERGENCY EXIT LIGHT BATTERY PACK (M1672 AFT GALLEY; CEILING; RH) WILL NOT CHARGE / [01] REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1672; OPS CHECK GOOD IAW AMM 33-51-06-960-805.; [02] VERIFIED STEP 1<BR>AUDIT CW

Part: DOOR FRAME — OUT OF ADJUST (L1 DOOR) · airframe 46,061 hrs · 27,534 cycles

FWD ENTRY DOOR AFT FRAME TARGET HAS EVIDENCE OF RUBBING PER TASK CARD STEP 6 DOOR REQUIRES ADJUSTMENT PER TASK 52-11-00-820-801 / REMOVED AND REPLACED DAMAGED TARGET ANGLE ON FWD ENTRY DOOR AFT SIDE IAW SRM 51-40-02-0G-0 SECTION 6 AND BOEING DWG # 141A6124 ID:0001 REV:- ACCOMPLISHED FWD ENTRY DOOR GUIDE ARM ADJUSTMENT TO ACHIEVE PROPER CLEARANCE IAW AMM 52-11-00-820-801. ADJUSTMENT CHECK GOOD. VERIFIED STEP 1 AUDIT CW

Part: NONE — CORRODED (FUSELAGE) · airframe 46,061 hrs · 27,534 cycles

SUPPLEMENTAL INFORMATION: A113-09 AFT CARGO COMPARTMENT STA 727E TO 747; L/H Z ANGLE HAS SEVERAL AREAS OF CORROSION. ; / [01] REMOVED CORROSION ON Z ANGLE IAW SRM 51-10-02-0G-0 ITEM 15; [02] EVALUATED ALLOWABLE LIMITS ORIG. 'T' .040 REMAINING .032 LOSS ;008 FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103 TOOL USED AAR# 36649 DUE 12/08/22; [03] VERIFIED ITEMS 1 2 AND MEASURMENT TABLE; [04] VERIFIED ITEMS 1; 2 AND 3; [05] REMOVED & REPLACED L/H Z-ANGLE IAW B737-700 SRM 53-00-53-2R-5 REPAIR 5 ON W/O 43008/1600/0027; [06] FAULT TTG8Q009H434; [07] VERIFIED STEP 5; [08] VERIFIED STEP 6<BR>AUDIT C/W

Part: ANGLE — CORRODED (FUSLEAGE) · airframe 46,061 hrs · 27,534 cycles

SUPPLEMENTAL INFORMATION: A113-13 AFT CARGO COMPARTMENT STA 727D TO 727E; L/H Z ANGLE HAS SEVERAL AREAS OF CORROSION. ; / [01] REMOVED CORROSION ON Z ANGLE IAW SRM 51-10-02-0G-0-ITEM 15; [02] EVALUATED ALLOWABLE LIMITS .ORIG 'T' .040 REMAINING .033 LOSS .007 FOUND OUT LIMITS IAW SRM 53-00-53-1A-2 FIG 103 TOOL USED AAR#36649 DUE 12/08/22; [03] VERIFIED ITEMS 1 AND 2 AND MEASUREMENT TABLES; [04] VERIFIED ITEMS 1; 2 AND 3; [05] REMOVED & REPLACED L/H Z-ANGLE IAW B737-700 SRM 53-00-53-2R-5 REPAIR 5 ON W/O 43008/1600/0027; [06] FAULT TTG8Q009H434; [07] VERIFIED STEPS 5;6; [08] AUDIT C/W

Part: ANGLE — CORRODED (FUSELAGE) · airframe 46,061 hrs · 27,534 cycles

SUPPLEMENTAL INFORMATION: A113-08 AFT CARGO COMPARTMENT STA 747 TO 767; L/H Z ANGLE IS CORRODED. ; / [01] REMOVED CORROSION ON Z-ANGLE IAW SRM 51-10-02-0G-0 ITEM 15; [02] EVALUATED ALLOWABLE LIMITS. ORIG 'T' .040 REMAINING .028 LOSS .012 FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103 TOOL USED AAR# 36649 DUE 13/08/22; [03] VERIFIED ITEMS 1 AND 2 AND MEASURMENT TABLE; [04] VERIFIED ITEMS 1; 2 AND 3; [05] REMOVED & REPLACED L/H Z-ANGLE IAW B737-700 SRM 53-00-53-2R-5 REPAIR 5 ON W/O 43008/1600/0027; [06] FAULT TTG8Q009H434; [07] VERIFIED STEPS 5;6; [08] AUDIT C/W

Part: ANGLE — CORRODED (FUSELAGE) · airframe 46,061 hrs · 27,534 cycles

SUPPLEMENTAL INFORMATION: A113-01 AFT CARGO COMPARTMENT STA 947 FLOORBOARD SUPPORT ANGLE RBL 20 TO LBL 10; HORIZONTAL FLANGE HAS SEVERAL AREAS OF CORROSION. ; / [01] REMOVED CORROSION ON SAT 947 FLOORBOARD SUPPORT ANGLE AND CHECK WITH 10X MAGNIFYING GLASS IAW SRM 51-10-02-0G-0 ITEM 15; [02] VERIFIED STEP 1 COMPLETE; [03] VERIFIED STEP 1; [04] EVALUATED ALLOWABLE LIMITS: ORIG 'T' .080 REMAINING .077 LOSS.003 FOUND NOT PUBLISHED TOOL USED AAR #36649 DUE 12/08/22; [05] VERIFIED ITEM 4; [06] VERIFIED ITEMS 4 AND 5; [07] SUMMARY EA 21-153-03653 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q009GYL3.; [08] REMOVED DAMAGE FROM AFT CARGO COMPARTMENT BS 947.5 BULKHEAD SUPPORT RAIL LBL 10 TO RBL 20 AND REPAIRED IAW EA 21-153-03653; [09] ALL WORK C/W<BR>AUDIT C/W

Part: ANGLE — CORRODED (FUSELAGE) · airframe 46,061 hrs · 27,534 cycles

A113-06 AFT CARGO COMPARTMENT STA 767 TO 787; L/H Z ANGLE HAS SEVERAL AREAS OF CORROSION. ; / [01] REMOVED CORROSION Z-ANGLE IAW SRM 51-10-02-0G-0 ITEM 15; [02] EVALUATED ALLOWABLE LIMITS .ORIG 'T' .040 REMAINING .027 LOSS .013 FOUND OUT LIMITS IAW SRM 53-00-53-1A-2FIG 103 TOOL USED AAR#36649 DUE 12/08/22; [03] VERIFIED ITEMS 1 AND 2; [04] VERIFIED ITEMS 1; 2 AND 3; [05] VERIFIED MATERIAL FOR Z ANGLE REPAIR PARTS P/N BAC1496-377-7075-T6 TAG # A93220 IAW SRM 53-00-53-2R-5 REPAIR 5; [06] VERIFIED ITEM 5; [07] VERIFIED ITEM 5; [08] FABRICATED REPAIR Z ANGLE FROM BETWEEN STA 747 AND 727E TO 849 L/H IAW SRM 53-00-53-2R-5 REPAIR 5; [09] VERIFIED STEP 8 IS COMPLETE; [10] VERIFIED ITEM 8. OK TO TREAT AND PRIME; [11] AP

Part: ANGLE — CORRODED (FUSELAGE) · airframe 46,061 hrs · 27,534 cycles

AFT CARGO, BS 727E - 747, RT ZEE ANGLE HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION ON Z ANGLE IAW SRM 51-10-02-0G-0 ITEM 15. FOUND OUT LIMITS IAW SRM 53-00-53-1A-2, FIG 103. REMOVED THE ZEE ANGLE FROM BS 727-747 IAW SRM 51-40-02-O-OG. FABRICATED A NEW ZEE ANGLE IAW SRM 53-00-53-2R-5, REPAIR 5. TREATED AND PRIMED NEW ANGLE IAW AMM 51-21-41-370-803, AND 51-21-72-370-801. REMOVED & REPLACED THE ZEE ANGLE IAW SRM 53-00-53-2R-5 REPAIR 5.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 46,061 hrs · 27,534 cycles

SUPPLEMENTAL INFORMATION: A113-16 AFT CARGO CO APARTMENT STA 727B TO 727C; L/H Z ANGLE HAS SEVERAL AREAS OF CORROSION. ; / [01] REMOVED CORROSION ON Z ANGLE IAW SRM 51-10-02-0G-0 ITEM 15; [02] EVALUATED ALLOWABLE LIMITS : ORIG. 'T' .040 REMAINING .038 LOSS .002 FOUND WITHIN LIMITS IAW SRM 53-00-53-1A-2 FIG 103 TOOL USED AAR # 36649 DUE 12/08/22; [03] VERIFIED ITEM 1 AND 2 AND MEASURMENT TABLE; [04] VERIFIED ITEMS 1 THROUGH 3; [05] REMOVED & REPLACED L/H Z-ANGLE IAW B737-700 SRM 53-00-53-2R-5 REPAIR 5 ON W/O 43008/1600/0027; [06] FAULT TTG8Q009H434; [07] VERIFIED STEPS 5;6; [08] AUDIT C/W

Part: ANGLE — CORRODED (FUSELAGE) · airframe 46,061 hrs · 27,534 cycles

SUPPLEMENTAL INFORMATION: A113-14 AFT CARGO COMPARTMENT STA 727C TO 727D; L/H Z ANGLE HAS SEVERAL AREAS OF CORROSION. ; / [01] REMOVED CORROSION ON Z ANGLE IAW SRM 51-10-02-0G-0 ITEM 15; [02] EVALUATED ALLOWABLE LIMITS : ORIG 'T'.040 REMAINING .027 LOSS .013 FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103 TOOL USED AAR#36649 DUE 12/08/22; [03] VERIFIED ITEM 1 AND 2 AND MEASURMENT TABLE; [04] VERIFIED ITEMS 1; 2 AND 3; [05] VERIFIED MATERIAL FOR Z ANGLE REPAIR PARTS P/N BAC1496-377-7075-T6 FAG# A93226 IAW SRM 53-00-53-2R-5 REPAIR 5; [06] VERIFIED ITEM 5; [07] VERIFIED ITEM 5; [08] FABRICATED REPAIR Z ANGLE FROM BETWEEN STA 727 AND 747 TO 727 L/H IAW SRM 53-00-53-2R-5 REPAIR 5; [09] VERIFIED STEP 8 IS COMPLETE; [10] VERIFIED ITEM 8. OK TO TREAT AND PRIME; [11] APPLIED ALODINE AND PRIME ON REPAIR PARTS IAW SRM 51-20-01-0G-0 AND AMM 51 21-72-370-804; [12] VERIFIED ITEM 11; [13] VERIFIED ITEM 11; [14] OK TO INSTALL; [15] STARTED INSTALLNG L/H Z ANGLE IAW SRM 51-40-02-OG-0; [16] VERIFIED ITEM 15; [17] FINISHED INSTALLING L/H Z-ANGLE IAW SRM 51-40-02-OG-O; [18] REMOVED & REPLACED L/H Z-ANGLE IAW B737-700 SRM 53-00-53-2R-5 REPAIR 5; [19] VERIFIED STEPS 17;18; [20] AUDIT C/W

Part: SHIELD — CORRODED (FUSELAGE) · airframe 46,061 hrs · 27,534 cycles

AFT CARGO BS 767 - 787, CARGO DOOR SURROUND FWD SHIELD HAD SEVERAL AREAS OF CORROSION. REMOVED CORROSION ON FWD SHIELD IAW SRM 51-10-02-0G-0 ITEM 15. FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103. REMOVED DAMAGED SHIELD IAW SRM 51-40-02-OG-0. LOCATED AND DRILLED NEW SHIELD IAW DWG 146A0081 REV A. INSTALLATION ACCOMPLISHED ON FAULT TTG8Q004G200.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 46,061 hrs · 27,534 cycles

SUPPLEMENTAL INFORMATION: A113-03 AFT CARGO COMPARTMENT STA 867+3'; LBL 9; FLOORBOARD SUPPORT ANGLE HORIZONTAL FLANGE BOLT HOLE IS CORRODED. ; / [01] REMOVED CORROSION FLOOR BOARD SUPPORT ANGLE IAW SRM 51-10-02-0G-0 ITEM 15;13] OK TO INSTALL REPAIR PARTS; [14] COMPLETED STEPS 11 AND 12 OF EA 21-153-03623; [15] C/W STEPS 11 AND 12 OF EA 21-153-03623<BR><BR>OK TO INSTALL SUPPORT ANGLE; [16] REPAIR ANGLE INSTALLATION COMPLETE; 3 EA 1/4 TURN RECEPTACLES NEED TO BE INSTALLED. EA NUMBER IS MARKED AND EDGE SEALED IAW EA STEPS 11 AND 13.; [17] VERIFIED STEP 16 C/W; [18] INSTALLED 3 EA TURN RECEPTACLES IAW SRM 51-40-02-0G-0 AND DWG 149A8113 REV A; [19] VERIFIED STEP 18; [20] VERIFIED ITEM 18 AND 19; [21] SUMMARY EA 21-153-03623 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q009GZSK.; [22] VERIFIED ALL STEPS OF EA 21-153-03623 HAVE BEEN ACCOMPLISHED.; [23] VERIFIED ABOVE ITEM 22.<BR>AUDITED.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 46,061 hrs · 27,534 cycles

SUPPLEMENTAL INFORMATION: A113-04 AFT CARGO COMPARTMENT STA 787 +10'; L/H Z ANGLE FASTENER HOLE IS CORRODED. ; / [01] REMOVED CORROSION AFT CARGO Z-ANGLE STA 787 +10 L/H IAW SRM 51-10-02-0G-0 ITEM 15; [02] VERIFIED STEP 1 IS COMPLETE; [03] VERIFIED STEP 1; [04] EVALUATED ALLOWABLE LIMITS. BRIG 'T' .040 REMAINING .033 LOSS ;007 FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103 TOOL USED AAR #36649 DUE 12/08/22; [05] VERIFIED ITEM 4; [06] VERIFIED ITEMS 4 AND 5; [07] REMOVED & REPLACED L/H Z-ANGLE IAW B737-700 SRM 53-00-53-2R-5 REPAIR 5 ON W/O 43008/1600/0027; [08] FAULT TTG8Q009H434; [09] VERIFIED STEP 7; [10] VERIFIED STEP 8<BR>AUDIT C/W

Part: ANGLE — CORRODED (FUSELAGE) · airframe 46,061 hrs · 27,534 cycles

SUPPLEMENTAL INFORMATION: A113-12 AFT CARGO COMPARTMENT STA 727D TO 727E; R/H Z ANGLE HAS SEVERAL AREAS OF CORROSION. ; / [01] REMOVED CORROSION ON Z ANGLE IAW SRM 51-10-02-0G-0 ITEM 15; [02] EVALUATED ALLOWABLE LIMITS. ORIG 'T' 040 REMAINING .033 LOSS .007 FOUND OUT LIMITS IAW SRM 53-00-53-1A-2 FIG 103 TOOL USED AAR#36649 DUE 12/08/22; [03] VERIFIED ITEMS 1 2 AND MEAURMENT TABLE; [04] VERIFIED ITEMS 1; 2 AND 3; [05] REMOVED & REPLACED R/H Z-ANGLE FROM STA 727-747 IAW B737-700 SRM 53-00-53-2R-5 REPAIR 5 ON W/O 43008/1600/0024; [06] FAULT TTG8Q009H3XC; [07] REMOVED & REPLACED R/H Z-ANGLE FROM STA 727-747 IAW B737-700 SRM 53-00-53-2R-5 REPAIR 5 ON FAULT TTG8Q009H3XC; [08] VERIFIED STEP 5; [09] VERIFIED STEPS 6;7<BR>AUDIT C/W

Part: ANGLE — CORRODED (FUSELAGE) · airframe 46,061 hrs · 27,534 cycles

SUPPLEMENTAL INFORMATION: A113-15 AFT CARGO COMPARTMENT STA 727C TO 727D; R/H Z ANGLE HAS SEVERAL AREAS OF CORROSION. ; / [01] REMOVED CORROSION ON Z ANGLE IAW SRM 51-10-02-0G-0 ITEM 15; [02] EVALUATED ALLOWABLE LIMITS: ORIG 'T' .040 REMAINING .029 LOSS.011 FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103 TOOL USED AAR#36649 DUE12/08/22; [03] VERIFIED ITEM 1 AND 2 AND MEASURMENT TABLE; [04] VERIFIED ITEMS 1; 2 AND 3; [05] REMOVED & REPLACED R/H Z-ANGLE FROM STA 727-747 IAW B737-700 SRM 53-00-53-2R-5 REPAIR 5 ON W/O 43008/1600/0024; [06] FAULT TTG8Q009H3XC; [07] VERIFIED STEP 5; [08] REMOVED & REPLACED R/H Z-ANGLE FROM STA 727-747 IAW B737-700 SRM 53-00-53-2R-5 REPAIR 5 ONFAULT TTG8Q009H3XC; [09] VERIFIED STEP 6;8<BR>AUDIT C/W

Part: DOOR — LOOSE (R1 DOOR) · airframe 46,061 hrs · 27,534 cycles

R1 SERVICE DOOR IS SAGGING. ; / [01] REMOVED FWD GALLEY SERVICE DOOR GUIDE ARM IAW AMM 52-41-21-000-801.; [02] REMOVED LOWER GUIDE PLATE IAW SRM 51-40-02-0G-0.; [03] REMOVED FWD GALLEY SERVICE DOOR FUSELAGE TORQUE TUBE ACCESS PANEL IAW SRM 51-40-02-0G-0.; [04] REPLACED BEARING ON LOWER GUIDE PLATE OF UPPER HINGE IAW SOPM 20-50-03 STEPS 4.B AND 6.B.3)(C); [05] VERIFIED ITEM 4; [06] OK TO INSTALL LOWER GUIDE PLATE; [07] DISPLACED FWD GALLEY SERVICE DOOR FUSELAGE TORQUE TUBE IAW AMM 52-41-41-000-801 STEP 2.F.(2); [08] RE-INSTALLED LOWER GUIDE PLATE OF UPPER HINGE IAW SRM 51-40-02-0G-0 STEP 9 AND AMM 51-31-00-390-810; [09] RE-SECURED FWD GALLEY SERVICE DOOR FUSELAGE TORQUE TUBE IAW AMM 51-41-41-400-801 STEP 3.F.(3)

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 45,341 hrs · 27,090 cycles

RIGHT HORIZONTAL STABILIZER UPPER SLIDER CRACKED. ; / [01] REMOVED AND REPLACED SLIDER SEAL IAW 20-50-11 AND SRM 51-40-02; [02] REMOVED AND REPLACED SLIDER SEAL IAW AMM 53-31-31

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 45,341 hrs · 27,090 cycles

LEFT HORIZONTAL STABILIZER UPPER SLIDER CRACKED. ; / [01] REMOVED AND REPLACED SLIDER SEAL IAW AMM 20-50-11 AND SRM 51-40-02; [02] REMOVED AND REPLACED SLIDING SEAL IAW AMM 53-31-31

Part: GIRT BAR — OUT OF POSITION (L2 DOOR) · airframe 44,534 hrs · 26,618 cycles

AFT ENTRY DOOR SLIDE CATCHING ON THRESHOLD WHEN CLOSING ; / PERFORMED GVI OF AFT ENTRY DOOR SLIDE-NO DEFECTS. REPOSITIONED GIRT IAW/REF AMM 25-66-11. OK FOR SERVICE.

Part: SIGN — LOOSE (EMERGENCY EXIT) · airframe 44,370 hrs · 26,531 cycles

EMERGENCY EXIT LIGHT NEEDS SECURING ; SIGN LOOSE AT THE EMERGENCY EXIT ROWS / RESECURED LIGHT ASSYRIAN. OPS CK OKAY REF AM 33-51-01

Part: SEAL — DAMAGED (HORIZONTAL STAB) · airframe 42,210 hrs · 25,245 cycles

L/H HORIZONTAL STAB UPPER FWD SLIDING SEAL DAMAGED / R&R L/H HORIZONTAL STAB UPPER FWD SLIDING SEAL REF AMM 53-31-31.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 41,465 hrs · 24,768 cycles

R1 DOOR ESCAPE SLIDE SKIRT DISPLACED. REPOSITIONED SLIDE PER MT.

Part: REGULATOR — FAILED (NR 2 ENGINE) · airframe 41,149 hrs · 24,555 cycles

DECLARED EMERGENCY-----------------------------------------DEPARTING FL390 CABIN ALTIMETER HORN AND LIGHT CAME ON FOLLOWED QRH & QRC CABIN ALTITUDE WAS CONTROLLABLE NO DISCOMFIT NOTED BY CREW AND PASSENGER. / R&R #2 ENGINE HIGH STAGE PRESSURE REGULATOR PER AMM.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 40,995 hrs · 24,452 cycles

AFT CARGO DOOR CUTOUT AFT CORNER THRESHOLD CRACKED / AFT CARGO AFT CORNER SCUFF PLATE REAPIRED ON EA 1-A53-2076 REV 11

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 40,995 hrs · 24,452 cycles

AFT CARGO COMPARTMENT CUTOUT FWD CORNER THRESHOLD CRACKED IN RADIUS / AFT CARGO FWD CARGO SCUFF PLATE REPAIRED ON EA 1-A53-2076 REV 11

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 40,995 hrs · 24,452 cycles

FWD CARGO DOOR SURROUND FWD CORNER SCUFF PLATE CRACKED / FWD CARGO DOOR SURROUND FWD CORNER SCUFF PLATE REPLACED IAW AIPC D638A001-SWA-0102 REF 80; SRM 51-40-05-0G-0; AND AMM 53-11-02-420-801 ATAG: TN0345

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 40,995 hrs · 24,452 cycles

FWD CARGO DOOR SURROUND AFT CORNER SCUFF PLATE CRACKED / FWD CARGO DOOR SURROUND AFT CORNER SCUFF PLATE REPLACED IAW AIPC D638A001 REF 85 AND SRM 51-40-05-0G-0 AND AMM 53-11-02-420-801 ATAG:WN0037

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 40,995 hrs · 24,452 cycles

L/H HORIZONTAL STABILIZER LEADING EDGE CRACKED RIB AT LEADING EDGE STA. 113.5. / R&R RIB IAW DWG AND SRM.

Part: SCUFF PLATE — CRACKED (L1 DOOR) · airframe 40,995 hrs · 24,452 cycles

FORWARD ENTRY FORWARD CORNER SCUFF PLATE CRACKED. / REPLACED FORWARD ENTRY, L-1 DOOR FORWARD ENTRY SCUFF PLATE IAW B737-700 DWG# 141A8230, INSTALL ACCOMPLISHED ON TASK CARD # J725-025-00-01Y.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 40,995 hrs · 24,452 cycles

FLOOR PANEL 241ADF HAD LOOSE FIBERS ON UPPER SURFACE BETWEEN BS. 887 TO BS. 1016. / REPAIRED FLOOR PANEL 241ADF IAW SRM.

Part: STRINGER — CRACKED (LT WING) · airframe 40,995 hrs · 24,452 cycles

L/H WING INTERNAL STRINGER U-8 CRACKED AT LAST FASTENER 12" OUTBOARD OF RIB 19. / REPAIRED STRINGER IAW EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 40,995 hrs · 24,452 cycles

L/H HORIZONTAL STABILIZER LEADING EDGE PANEL 331B CRACKED RIB AT LEADING EDGE STA. 105.26. / R&R RIB IAW SRM AND DWG.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 40,995 hrs · 24,452 cycles

PASSENGER CABIN FLOOR PANEL 221BF, AFT OUTBOARD TAB OF FLOOR PANEL BROKEN OFF AND MISSING, BETWEEN BS. 270 TO BS. 420. / REPAIRED FLOOR PANEL 221BF IAW SRM.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 40,995 hrs · 24,452 cycles

RUDDER HINGE ARM FWD BALANCE WEIGHT IS CORRODED / PAINTED NEW RUDDER HINGE ARM; FWD BALANCE WEIGHT IAW AMM 51-21-73-370-803. REMOVED AND INSTALLED NEW RUDDER HINGE ARM; FWD BALANCE WEIGHT IAW CMM 55-40-09 STEP 2.C. (3).(A)-2.C.(3).B).(B) 7) TORQUED BOLTS FOR RUDDER HINGE ARM; FWD BALANCE WEIGHT IAW AMM 20-50-11-910-801. TABLE 203. TORQUE WRENCH AAR 41858 CAL DUE 03/05/20 WN0642

Part: PLATE — CRACKED (LT WING) · airframe 40,995 hrs · 24,452 cycles

L/H WING INBOARD WIGGLE PLATE FOR WING TRAILING EDGE PANEL 551EB CRACKED. / R&R WIGGLE PLATE IAW SRM.

Part: INTERCOSTAL — CRACKED (CABIN FLOOR) · airframe 40,995 hrs · 24,452 cycles

FORWARD WET AREA FLOOR INTERCOSTAL STA 312-328 RBL 31 IS CRACKED ON UPPER FLANGE AT FORWARD FLOOR BOARD HOLE / REMOVED AND REPLACED INTER COSTAL @ STA 312-328 RBL 31 IAW BOEING DWG #141A5400 AND 737 SRM 51-40-02

Part: WEB — CORRODED (AFT CARGO THRESH) · airframe 40,995 hrs · 24,452 cycles

AFT CARGO COMPARTMENT DOOR THRESHOLD WEB HAS MULTIPLE AREAS OF CORROSION FROM STA 747-827 RBL 25 W/L 157 / AFT CARGO COMPARTMENT DOOR THRESHOLD WEB REPLACED FROM STA 747 - 827 RBL 25 W/L157 IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A8120 ID: 39 REV: -; AND BOEING DWG 146A8340 ID:0028 REV:- REMOVED CORROSION FROM ORIGINAL WEB; ORIGINAL THICKNESS: .045'; REMOVED: .037'; REMAINING: .008'; WEB OUT OF LIMITS IAW SRM 53-60-15-01-1 AND SRM 53-60-15-1A-1 P/N: 146A8123-24 ATAG: TN0324

Part: BRACKET — CORRODED (AFT CARGO COMPT) · airframe 40,995 hrs · 24,452 cycles

AFT CARGO COMPARTMENT FLOOR PANEL TO FLOOR PANEL BRACKET UPPER AND LOWER SIDES HAVE CORROSION AT STA 767+4 RBL 15-LBL 15 W/L 157 / REMOVED CORRSION FROM AFT CARGO COMPARTMENT FLOOR PANEL TO PANEL BRACKET AND CHECKED LIMIT FOUND TO BE OUT OF LIMITS ORIG 'T' .070' REMAIN .047' LOSS .023' REPLACED WITH NEW PART 146A9401-4 IAW SRM 51-10-02; SRM 53-00-53-1A-2 AND DWG 146A7560 REV -. P/N 146A9401-4 A TAG WN1199.

Part: INTERCOSTAL — CRACKED (CABIN FLOOR) · airframe 40,995 hrs · 24,452 cycles

FORWARD WET AREA FLOOR MACHINE INTERCOSTAL STA 344-360 BL0 UPPER FLANGE IS CRACKED AT AFT FLOOR BOARD HOLE / REMOVED AND REPLACED INTERCOSTAL PN 141A5410-23 IN FWD WET AREA STA 344-360 BL O' IAW SRM 51-40-02-0G-0 AND BOEING DWG #141A5400.

Part: BRACKET — CORRODED (AFT CARGO COMPT) · airframe 40,995 hrs · 24,452 cycles

AFT CARGO COMPARTMENT FLOOR PANEL TO FLOOR PANEL BRACKET HAS AREAS OF CORROSION AT STA 887 LBL10-RBL 10 W/L 157 / REMOVED CORROSION FROM AFT CARGO COMPARTMENT FLOOR PANEL TO FLOOR PANEL BRACKET TO BE OUT OF LIMITS WITH 100% LOSS IAW SRM 53-00-53-1A-2 REPLACED WITH NEW P/N 146A9401U39 IAW BOEING DWG 146A7500 REV - P/N 146A9401-3 AAG TN0339

Part: INTERCOSTAL — CRACKED (CABIN FLOOR) · airframe 40,995 hrs · 24,452 cycles

FORWARD WET AREA FLOOR MACHINE INTERCOSTAL STA 344-360 LBL11 UPPER FLANGE IS CRACKED AT FORWARD FLOOR BOARD HOLE / REMOVED AND REPLACED FORWARD WET AREA MACHINE INTERCOSTAL STA 344-360 LBL 11 IAW BOEING DWG# 141A5400 AND 737 SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 40,995 hrs · 24,452 cycles

AFT CARGO COMPARTMENT R/H "Z" ANGLE CORRODED BETWEEN BS. 727 TO BS. 767, RBL 21. / R&R Z ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 40,995 hrs · 24,452 cycles

AFT CARGO COMPARTMENT 'Z' ANGLE FLOOR PANEL TO SIDEWALL PANEL HAS AREAS OF CORROSION STA 847-867 RBL 20 W/L 157 / AFT CARGO Z-ANGLE SHIELD STA 847 TO STA 867 R/H SIDE HAS CORROSION. BLENDED AND REMOVED CORROSION I/A/W SRM 51-10-02-0G-0. MAT THICKNESS IS .050; MAT LOSS IS .008; MAT REMAINING IS .042 'OUT OF LIMITS' I/A/W SRM 53-00-53-1A-2. REMOVED SHIELD I/A/W SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW SHIELD AND INSTALLED I/A/W SRM 51-40-05-0G-0; BOEING DWG 146A0081 REV: A; AND SRM 51-40-02-0G-0 P/N 146A8127-10

Part: STRAP — CORRODED (FUSELAGE) · airframe 40,995 hrs · 24,452 cycles

AFT CARGO COMPARTMENT R/H STRAP AREAS CORRODED BETWEEN BS. 767 TO BS. 827, RBL 21, ON THE UPPER AND LOWER SIDES INBOARD OF THE THRESHOLD WEB. / REPAIRED STRAP IAW SRM & DWG.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 40,995 hrs · 24,452 cycles

AFT CARGO COMPARTMENT R/H 'Z' ANGLE CONNECTING THE FLOOR PANEL TO THE SIDEWALL PANEL HAS AREAS CORRODED FROM STA 767-787 RBL 23 W/L 157 / REMOVED AND REPLACED AFT CARGO COMPARTMENT R/H 'Z' ANGLE (SHEILD) CONNECTING THE FLOOR PANEL TO THE SIDEWALL PANEL FROM STA 767-787 RBL 23 W/L 157; IAW B737-700 SRM 51-40-02-0G-0 AND BOEING DWG# 146A0081 REV A P/N 146A8127-12 REMOVED CORROSION ORIG T .050' REMAINING .028' LOSS .012' 'OUT OF LIMITS' IAW SRM 53-00-53-1A-2

Part: ATTACH ANGLE — CORRODED (BS 312) · airframe 40,995 hrs · 24,452 cycles

FORWARD PASSENGER CABIN L/H CREASE BEAM ATTACH "L" ANGLE THRESHOLD SUPPORT CORRODED AT BS. 312+8, LBL 62 UPPER AND LOWER SURFACES. / R&R "L" ANGLE PER SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 40,995 hrs · 24,452 cycles

AFT CARGO COMPARTMENT L/H "Z" ANGLE CORRODED BETWEEN BS. 717+4 TO BS. 847, LBL 21. / R&R L/H Z-ANGLE PER SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 40,995 hrs · 24,452 cycles

AFT CARGO COMPARTMENT R/H "Z" ANGLE HAD MULTIPLE CRACKS AT THE FRAMES BETWEEN BS. 727 TO BS. 767, RBL 21. / R&R Z-ANGLE IAW SRM AND DWG.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 40,995 hrs · 24,452 cycles

PASSENGER CABIN SIDEWALL PANEL 231YJW EXIT SIGN BROKEN. / R&R LENS IAW AMM.

Part: CREASE BEAM — CORRODED (BS 947-986) · airframe 40,995 hrs · 24,452 cycles

PASSENGER CABIN AFT WET AREA R2 CREASE BEAM INNER CHORD CORRODED BETWEEN BS. 947 TO BS. 986+6, RBL 50, ON UPPER SURFACE. / R&R INNER CHORD IAW SRM AND DWG.

Part: FLOOR PANEL — CRUSHED (PAX CABIN) · airframe 40,995 hrs · 24,452 cycles

PASSENGER CABIN FLOOR PANEL 231WF HAD CRUSHED EDGE BETWEEN BS. 520 TO BS. 537.45. / REPAIRED FLOOR PANEL 231WF IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 40,995 hrs · 24,452 cycles

CABIN FLOOR PANEL 221BF HAS PEELING FIBERS FROM TOP OF PANEL / REPAIRED DAMAGE ON FLOOR BOARD 221BF. BONDED REPAIR PLY AND CURED. TAP TEST GOOD. IAW B737-700 SRM 53-00-50-2R-1 REV 68; SRM 53-00-50-2R-0 REV 68.

Part: NONE — CRACKED (CABIN) · airframe 40,995 hrs · 24,452 cycles

CABIN FLOOR; PANEL BREAK-ASSY; AT STA 540 RBL 2 WL 208 BROKE OFF AT FASTENERS / REMOVED DAMAGED PANEL BREAK ASSEMBLY AT STA. 540 BRL 2 WL 208 AND INSTALLED NEW PANEL P/N 143A5240-36 A TAG # WN3289 IAW BOEING DWG 143A0060 REV - A.

Part: FLOOR PANEL — CRUSHED (CABIN) · airframe 40,995 hrs · 24,452 cycles

SUPPLEMENTAL INFORMATION: PASSENGER CABIN FLOOR PANEL 241SF UPPER I/B EDGE CRUSHED. / REPAIRED PASSENGER CABIN FLOOR PANEL 241SF IAW B737 SRM 53-00-50-2R-2 REPAIR 2 PARA 3

Part: FLOOR PANEL — CRUSHED (CABIN) · airframe 40,995 hrs · 24,452 cycles

PASSENGER CABIN FLOOR PANEL 241MF UPPER SURFACE EDGE CRUSHED AT INSERT. / EVALUATED; PREPPED; CLEANED AND REPAIRED EDGE DAMAGE AT UPPER SURFACE ON FLOORBOARD 241MF IAW B737 SRM 53-00-50-2R-4; PAR 3(A-K1; L1-M1; & N)- REV.68

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 40,995 hrs · 24,452 cycles

CABIN FLOOR PANEL 222CF HAS PEELING FIBERS FROM TOP SIE OF PANEL / REPAIRED CABIN FLOOR PANEL 222CF IAW B737 SRM 53-00-50-2R-1 REV 68; 53-00-50-2R-0 REV 68 (A36551) (A09256)

Part: FLOOR PANEL — PEELING (CABIN) · airframe 40,995 hrs · 24,452 cycles

PASSENGER CABIN FLOOR PANEL 241AF UPPER SURFACE PEELED BETWEEN BS. 537.45 TO BS. 727B. / R&R FLOOR PANEL 241AF IAW DWG AND SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 40,995 hrs · 24,452 cycles

CABIN FLOOR PANEL 221CF HAS PEELING FIBERS FROM TOP OF PANEL / REPAIRED PANEL 221CF PEELING FIBERS FROM TOP OFF AND IAW B737-700 SRM 53-00-50-2R-0 REV 68; SRM 53-00-50-2R-1 REV 68 A38440; A72331

Part: NONE — CRACKED (CABIN) · airframe 40,995 hrs · 24,452 cycles

CABIN FLOOR; PANEL BREAK-ASSY; AT STA 540 LBL 2 WL 208 CRACKED IN RADIUS / REMOVED AND REPLACED CRACKED CABIN FLOOR PANEL BREAK ASSY AT STA 540 LBL 2 WL 208.OBTAINED NEW PART - PART NO 143A5240-35; DRILLED; AND INSTALLED IAW SRM 51-40-05-0G-0; 5140-2-0G-0 AND BOEING DRAWING 143A0060 REV A.

Part: FLOOR PANEL — PEELING (CABIN) · airframe 40,995 hrs · 24,452 cycles

CABIN FLOOR PANEL 222BF HAD PEELING FIBERS FROM TOP SIDE OF PANEL BETWEEN BS. 270 TO BS. 420. / REPAIRED FLOOR PANEL 222BF IAW SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 40,995 hrs · 24,452 cycles

CABIN FLOOR PANEL 221DF HAS PEELING FIBERS FROM TOP SIE OF PANEL / REPAIRED CABIN FLOOR PANEL 221DF PEELING FIBERS ON UPPER SURFACE IAW B737-700 SRM'S 53-00-50-2R-1 REV 68 AND 53-00-50-2R-0 REV 68 (A72331) (A09236)

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 40,995 hrs · 24,452 cycles

CABIN FLOOR PANEL 221EF DELAMINATED ON TOP SIDE OF PANEL, BETWEEN BS. 270 TO BS. 420. / REPAIRED FLOOR PANEL 221EF IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,995 hrs · 24,452 cycles

FORWARD CARGO UPPER FREE FLANGE ON LONGITUDINAL INTERCOSTAL CRACKED AT BS. 480+14.5, STR. 23L. / R&R INTERCOSTAL IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 40,995 hrs · 24,452 cycles

FORWARD CARGO STRINGER CLIP GUSSET COMMON TO FRAME CRACKED IN RADIUS AT BS. 500D, STR. 22L. / R&R GUSSET IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,995 hrs · 24,452 cycles

FORWARD CARGO UPPER FREE FLANGE ON LONGITUDINAL INTERCOSTAL CRACKED AT BS. 480+14.5, STR. 20L. / R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,995 hrs · 24,452 cycles

FORWARD CARGO UPPER FREE FLANGE ON LONGITUDINAL INTERCOSTAL CRACKED AT BS. 480+14.5, STR. 22L. / R&R INTERCOSTAL IAW SRM AND DWG.

Part: BAFFLE — CRACKED (BS 500-500A) · airframe 40,995 hrs · 24,452 cycles

FORWARD CARGO Z-ANGLE BAFFLE CRACKED BETWEEN BS. 500 TO BS. 500A, LBL 24, FASTENER HOLE. / R&R Z-ANGLE BAFFLE IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (BS 500D) · airframe 40,995 hrs · 24,452 cycles

FORWARD CARGO STRINGER CLIP GUSSET COMMON TO FRAME CRACKED AT BS. 500D, STR. 21L, IN UPPER RADIUS. / R&R GUSSET IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 40,995 hrs · 24,452 cycles

FORWARD CARGO STRINGER CLIP GUSSET COMMON TO FRAME CRACKED IN UPPER RADIUS AT BS. 500D, STR. 19L. / R&R GUSSET IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (BS 500D) · airframe 40,995 hrs · 24,452 cycles

FORWARD CARGO STRINGER CLIP GUSSET COMMON TO FRAME CRACKED AT BS. 500D, STR. 19R, IN UPPER RADIUS. / R&R GUSSET IAW SRM & DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,221 hrs · 23,940 cycles

RT CABIN OVERWING EMERGENCY LIGHT INOP. R&R SIGN LIGHT ASSEMBLY IAW AMM.

Part: COVER — UNSECURE (CABIN) · airframe 39,361 hrs · 23,394 cycles

R1 DOOR EXIT LIGHT COVER FELL OFF. SECURED COVER PER SIP.

Part: CONTROL VALVE — FAILED (LT A/C PACK) · airframe 39,143 hrs · 23,253 cycles

AT FL410 CABIN ALT. LIGHT AND WARNING HORN ACTIVATED. PRESSURIZATION WENT TO AUTO FAIL. MANUALLY CONTROLLED CABIN VIA MANUAL OUTFLOW VALVE OPERATION. GEEN ALT. LIGHT ON PRESS CONTROLLER NEVER ILLUMINATED. R&R L/H PACK FLOW CONTROL VALVE PER AMM.

Part: SHUTOFF VALVE — FAILED (NR 1 ENGINE) · airframe 39,143 hrs · 23,253 cycles

AT FL410 CABIN ALT. LIGHT AND WARNING HORN ACTIVATED. PRESSURIZATION WENT TO AUTO FAIL. MANUALLY CONTROLLED CABIN VIA MANUAL OUTFLOW VALVE OPERATION. GEEN ALT. LIGHT ON PRESS CONTROLLER NEVER ILLUMINATED. R&R #1 PRESSURE REGULATORY SHUTOFF VALVE PER AMM.

Part: SHUTOFF VALVE — FAILED (CABIN PRESSURE) · airframe 39,143 hrs · 23,253 cycles

AT FL410 CABIN ALT. LIGHT AND WARNING HORN ACTIVATED. PRESSURIZATION WENT TO AUTO FAIL. MANUALLY CONTROLLED CABIN VIA MANUAL OUTFLOW VALVE OPERATION. GEEN ALT. LIGHT ON PRESS CONTROLLER NEVER ILLUMINATED. R&R PRESSURE REGULATORY AND SHUTOFF VALVE PER AMM.

Part: CONTROL VALVE — FAILED (RT A/C PACK) · airframe 39,143 hrs · 23,253 cycles

AT FL410 CABIN ALT. LIGHT AND WARNING HORN ACTIVATED. PRESSURIZATION WENT TO AUTO FAIL. MANUALLY CONTROLLED CABIN VIA MANUAL OUTFLOW VALVE OPERATION. GEEN ALT. LIGHT ON PRESS CONTROLLER NEVER ILLUMINATED. R&R R/H PACK FLOW CONTROL VALVE PER AMM.

Part: VALVE — FAILED (NR 1 HIGH STAGE) · airframe 39,143 hrs · 23,253 cycles

AT FL410 CABIN ALT. LIGHT AND WARNING HORN ACTIVATED. PRESSURIZATION WENT TO AUTO FAIL. MANUALLY CONTROLLED CABIN VIA MANUAL OUTFLOW VALVE OPERATION. GEEN ALT. LIGHT ON PRESS CONTROLLER NEVER ILLUMINATED. R&R HIGH STAGE VALVE PER AMM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 38,904 hrs · 23,101 cycles

RT FORWARD SEVERAL EMERGENCY LIGHTS INOP. R&R CHARGER PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,904 hrs · 23,101 cycles

RT FORWARD SEVERAL EMERGENCY LIGHTS INOP. R&R BATTERY PACK PER AMM.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 38,021 hrs · 22,552 cycles

R1 DOOR LOWER EXIT SIGN COVER FELL OUT. REINSTALLED LENS IAW AMM.

Part: COVER — BROKEN (EXIT SIGN) · airframe 38,021 hrs · 22,552 cycles

L2 DOOR EMERGENCY EXIT SIGN BROKEN. R&R COVER PER AMM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 38,002 hrs · 22,538 cycles

R1 DOOR SLIDE PRESSURE GAUGE LOW. R&R SLIDE PER MT & AMM.

Part: FLOOR PANEL — CRACKED (AFT CARGO COMPT) · airframe 37,082 hrs · 21,930 cycles

AFT CARGO PIT FLOOR PANEL LINING CRACKED JUST FORWARD OF DOOR. O.K. TO CONTINUE PER MEL 25-16-01; SP1D TRACKING #5295 / R & R CARGO FLOOR PANEL AS PER M/M 25-52-10 CL# 5420

Part: LENS — LOOSE (R2 DOOR) · airframe 36,862 hrs · 21,790 cycles

R2 DOOR LOWER RT EMERGENCY EXIT LIGHT LENS COVER LOOSE LOWER CLIP. SECURED COVER PER EA & AMM.

Part: NONE — NONE (RT WING) · airframe 36,035 hrs · 21,263 cycles

SUPPLEMENTAL INFORMATION: RIGHT WING #8 SLAT I/B AUX TRACK COVER ANGLE BRACKET ON THE SLAT IS CRACKED / REMOVED AND REPLACED RIGHT WING #8 SLAT I/B AUX TRACK COVER ANGLE BRACKET PER AMM. 20-50-11

Part: FAIRING — CRACKED (TAILCONE) · airframe 36,023 hrs · 21,255 cycles

UPPER SURFACE TAIL CONE FAIRING CRACKED AT 11:00 POSITION. REPAIRED SKIN PER EA.

Part: RETAINING CLIP — OUT OF ADJUST (R1 DOOR) · airframe 35,764 hrs · 21,088 cycles

R1 DOOR GIRT BAR RETAINER CLIPS OUT OF ADJUST. ADJUSTED CLIPS PER MM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 34,993 hrs · 20,612 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 34,993 hrs · 20,612 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.

Part: PANEL — CRACKED (RIGHT WING) · airframe 34,550 hrs · 20,310 cycles

LOWER R/H L/E PANEL 621YB FWD OUTBRD FASTENER HOLE IS CRACKED THROUGH TO PANEL EDGE. / REPAIRED LOWER R/H L/E PANEL 621YB FWD OUTBRD FASTENER HOLE CRACKED THROUGH TO PANEL EDGE PER SRM 51-70-05-2R-6 REPAIR 6 ;51-70-14-2R-3REPAIR 3AND M.M. 51-21-99 SEE WIP'S AND SUB TASKS FOR INDIVIDUAL SIGN OFFS

Part: PANEL — DELAMINATED (RIGHT WING) · airframe 34,550 hrs · 20,310 cycles

LOWER R/H L/E PANEL 621YB FWD OUTBRD FASTENER HOLE IS CRACKED THROUGH TO PANEL EDGE. / ON FURTHER EVALUATION OF PANEL 621YB EDGE OF PANEL IS DELAMINATED NOT CRACKED REPAIRED DELAMINATION PER SRM 51-70-40-2R-13

Part: WEB — DAMAGED (WHEEL WELL RH) · airframe 34,550 hrs · 20,310 cycles

TOOLING DAMAGE ON 663 VERTICAL WEBB AT RBL 42 DAMAGE CAN BEEN SEEN FROM WHEEL WELL SIDE / FACT AS A RESULT OF POST REPAIR INSPECTION

Part: ANGLE — CORRODED (FWD CARGO RH) · airframe 34,550 hrs · 20,310 cycles

FWD CARGO BAY; R/H TRANSITION ANGLE HAS CORROSION AROUND NUTPLATES FROM BS 490-500A . (MARKED) / REMOVED AND REPLACED TRANS. ANGLE PER SRM 51-40-02

Part: FLOORBEAM — CORRODED (BS 270) · airframe 34,549 hrs · 20,310 cycles

FLOORBEAM CORRODED AT BS 270, BETWEEN RBL 10 TO LBL 10. R & R THE FLOORBEAM IAW EA.

Part: FAIRING — CRACKED (LWR FUSELAGE) · airframe 34,244 hrs · 20,104 cycles

PANEL 192AR HAS A CRACK 8 INCHES AFT OF THE LEADING EDGE / R & RPANEL 192AR IAW 53-51-21

Part: WEB — CRACKED (LT MLG WW) · airframe 34,244 hrs · 20,104 cycles

WING CENTER SECTION REAR SPAR VERTICAL PRESSURE DECK WEB CRACKED AT BS 663, LBL 35. REPAIRED WEB PER SRM.

Part: SLIDER — CRACKED (HORIZONTAL STAB) · airframe 34,179 hrs · 20,058 cycles

RT HORIZONTAL STAB. UPPER FWD SLIDER IS CRACKED / REMOVED AND REPLACED R/H UPPER FWD HORZ STAB SLIDER PER AMM 53-31-31.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,598 hrs · 19,697 cycles

RT EXTERIOR OVERWING EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW AMM.

Part: COVER — LOOSE (R2 DOOR) · airframe 32,836 hrs · 19,242 cycles

R2 DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED COVER PER MT.

Part: LIGHT — MISSING (CABIN) · airframe 30,216 hrs · 17,674 cycles

RIGHT WING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED A NEW LIGHT ASSEMBLY IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 28,538 hrs · 16,715 cycles

R2 DOOR EMER EXIT LIGHT LENS COVER BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,958 hrs · 16,383 cycles

R1 DOOR Z ANGLE CORRODED. R & R Z ANGLE IAW SRM.

Part: ANGLE — CORRODED (L1 DOOR) · airframe 27,958 hrs · 16,383 cycles

L1 DOOR Z ANGLE CORRODED. R & R Z ANGLE IAW.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 27,958 hrs · 16,383 cycles

AFT FLOORBEAM CORRODED AT BS 986, RBL 43. REPAIRED FLOOR BEAM IAW SRM.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 27,958 hrs · 16,383 cycles

L1 DOOR FWD LOWER FRAME, CORRODED AT BS 303.9, STRINGER 17L. REPAIRED FRAME IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 27,958 hrs · 16,383 cycles

RIGHT HORIZONTAL STABILIZER, STATION 92.7, RIB STIFFENER LOCATED 19" AFT OF THE FRONT SPAR CRACKED. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 27,958 hrs · 16,383 cycles

RIGHT HORIZONTAL STABILIZER, STATION 92.7, RIB STIFFENER LOCATED 28" AFT OF THE FRONT SPAR CRACKED. REPAIRED RIB IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 27,958 hrs · 16,383 cycles

LONGITUDINAL FLOORBEAM FLANGE, HOLE NR 9 CRACKED AT BS 727B, RBL 45.5. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 27,958 hrs · 16,383 cycles

LONGITUDINAL FLOORBEAM FLANGE, HOLE NR 8 CRACKED AT BS 727B, LBL 45.5. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 27,958 hrs · 16,383 cycles

LONGITUDINAL FLOORBEAM FLANGE, HOLE NR 8 CRACKED AT BS 727B, RBL 45.5. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 27,958 hrs · 16,383 cycles

LONGITUDINAL FLOORBEAM FLANGE, HOLE NR 10 CRACKED AT BS 727B, RBL 45.5. REPAIRED BEAM IAW EA.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 27,716 hrs · 16,244 cycles

LEFT WING LOWER SKIN HYD LINE SUPPORT BRACKET CRACKED. REPAIRED BRACKET IAW EA.

Part: BATTERY — FAILED (CABIN) · airframe 27,716 hrs · 16,244 cycles

EMERGENCY LIGHTS BATTERIES FAILED CAPACITY TEST AT LOCATION M1668. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 27,716 hrs · 16,244 cycles

EMERGENCY LIGHTS BATTERIES FAILED CAPACITY TEST AT LOCATION M1673. R & R BATTERY IAW AMM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 27,716 hrs · 16,244 cycles

FLOORBOARD SUPPORT CRACKED AT BS 540, UPPER LT OF CTR AT THE INBD END. R & R SUPPORT IAW SRM.

Part: BATTERY — FAILED (CABIN) · airframe 27,716 hrs · 16,244 cycles

EMERGENCY LIGHTS BATTERIES FAILED CAPACITY TEST AT LOCATION M1672. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 27,716 hrs · 16,244 cycles

EMERGENCY LIGHTS BATTERIES FAILED CAPACITY TEST AT LOCATION M1670. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 27,716 hrs · 16,244 cycles

EMERGENCY LIGHTS BATTERIES FAILED CAPACITY TEST AT LOCATION M1669. R & R BATTERY IAW AMM.

Part: SLIDE — UNSECURE (R2 DOOR) · airframe 26,393 hrs · 15,449 cycles

R2 DOOR SLIDE FELL OUT OF CONTAINER INADVERTENTLY. REINSTALLED SLIDE IAW MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 24,342 hrs · 14,296 cycles

R2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: HOOK — LOOSE (R1 DOOR) · airframe 23,829 hrs · 13,985 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR J HOOK LOOSE. R & R J HOOK IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 21,412 hrs · 12,609 cycles

NR 3 FLIGHT DECK WINDOW FRAME CRACKED AT FASTENER HOLE E - F POST IN NR 8 HOLE FROM TOP. REPAIRED FRAME IAW ACO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 21,412 hrs · 12,609 cycles

FLOOR SUPPORT CRACKED AT BS 540 BETWEEN RBL 1 TO RBL 24. R & R SUPPORT IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 21,412 hrs · 12,609 cycles

FLOOR SUPPORT CRACKED AT BS 540 BETWEEN RBL 25 TO RBL 45. R & R SUPPORT IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,412 hrs · 12,609 cycles

RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT REAR SPAR AT STATION 98. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,087 hrs · 12,416 cycles

RT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED IN FOUR PLACES OTBD OF RIB AT STAB STATION 101.90, 0.25 LONG 12.50" AFT OF FWD SPAR, 0.75 LONG 19.0" AFT OF FWD SPAR, 0.90 LONG 28.5" AFT OF FWD SPAR & 1.10 LONG 37.0" AFT OF FWD SPAR. REPAIRED SKIN IAW SRM.

Part: BATTERY — FAILED (CABIN) · airframe 21,087 hrs · 12,416 cycles

RT EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 21,087 hrs · 12,416 cycles

LT EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST. R & R BATTERY IAW AMM.

Part: WEB — CRACKED (RT MLG DOOR) · airframe 21,087 hrs · 12,416 cycles

RT MLG INNER DOOR WEB CRACKED AT THE RADIUS LOCATED FWD EDGE OF HINGE. R & R DOOR IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 20,877 hrs · 12,295 cycles

CENTER AISLE OVERWING EMERGENCY LIGHT FIXTURE LOOSE. R & R SIGN ASSEMBLY IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 18,421 hrs · 10,886 cycles

R2 DOOR EMERGENCY EXIT INDICATOR LIGHT LENS MISSING. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 16,455 hrs · 9,712 cycles

AFT CABIN EMERGENCY EXIT LIGHTS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 16,124 hrs · 9,508 cycles

STRINGER CLIP CRACKED AT BS 500B, STR 16R. REMOVED AND REPLACED CLIP IAW DWG AND SRM.

Part: LENS — BROKEN (CABIN) · airframe 15,322 hrs · 9,067 cycles

LT EEPLS LENSES BROKEN BETWEEN ROW 4 TO ROW 20. REMOVED AND REPLACED LENSES PER MM.

Part: HOLDER — LOOSE (GIRT BAR) · airframe 15,280 hrs · 9,044 cycles

LI DOOR SLIDE GIRT BAR HOLDER LOOSE. REPLACED RIVET PER SRM.

Part: BATTERY — FAILED (CABIN) · airframe 14,215 hrs · 8,447 cycles

DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT LIGHT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 14,215 hrs · 8,447 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 10 TO ROW 11. REMOVED AND REPLACED COVER PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 14,215 hrs · 8,447 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EMERGENCY EXIT BATTERY CHARGER INOP AT ROW 10. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 14,215 hrs · 8,447 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EMERGENCY EXIT BATTERY CHARGER INOP AT ROW 16. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 14,215 hrs · 8,447 cycles

DURING SCHEDULED HC2 CHECK, RT EMERGENCY EXIT LIGHT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,148 hrs · 8,411 cycles

DURING SCHEDULED MV1 CHECK, FOUND FLOOR PATH EMERGENCY LIGHT INOP, ROW 2ABC. REPLACED LAMPS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,148 hrs · 8,411 cycles

DURING SCHEDULED MV1 CHECK, FOUND FLOOR PATH EMERGENCY LIGHT INOP, ROW 2ABC. REPLACED LAMPS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,745 hrs · 8,177 cycles

DURING SCHEDULED MV1 CHECK FOUND, LT EEPLS INOP AT ROW 1. RELAMPED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,570 hrs · 7,490 cycles

EEPLS INOP AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — MISSING (CABIN) · airframe 11,414 hrs · 6,858 cycles

EEPLS COVER MISSING AT ROW 11. INSTALLED COVER PER MM.

Part: LENS — LOOSE (CABIN) · airframe 10,861 hrs · 6,554 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS LOOSE AT ROW 1. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 10,814 hrs · 6,522 cycles

FWD EEPLS NEAR FWD ENTRY DOOR MISSING. INSTALLED EEPLS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 10,794 hrs · 6,509 cycles

LT EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 10,771 hrs · 6,497 cycles

FWD EEPLS LENS LOOSE. REMOVED AND REPLACED EEPLS ASSY PER MM.

Part: COVER — LOOSE (CABIN) · airframe 10,685 hrs · 6,450 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 10,586 hrs · 6,400 cycles

EEPLS LENS MISSING AT ROW 3. REMOVED AND REPLACED LENS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 10,267 hrs · 6,211 cycles

AFT EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,211 hrs · 6,178 cycles

DURING SCHEDULED MV3 CHECK, FOUND AFT EEPLS INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,211 hrs · 6,178 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT OVERHEAD SIDEWALL EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 8,569 hrs · 5,227 cycles

R1 DOOR EMERGENCY EXIT LIGHT OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: COVER — LOOSE (CABIN) · airframe 841 hrs · 5,134 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 7,562 hrs · 4,640 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS BROKEN BETWEEN ROW 2 TO ROW 4. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — MISSING (CABIN) · airframe 6,893 hrs · 4,212 cycles

LT EEPLS COVER MISSING AT ROW 1. INSTALLED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 6,861 hrs · 4,191 cycles

FWD EEPLS COVER MISSING. INSTALLED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,963 hrs · 3,002 cycles

DURING SCHEDULED HC2 CHECK, FOUND CABIN RT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: COVER — CRACKED (CABIN) · airframe 4,963 hrs · 3,002 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: TRACK — BROKEN (CABIN) · airframe 4,456 hrs · 2,690 cycles

EEPLS FLOOR TRACK BROKEN AT ROW 1. REMOVED AND REPLACED EEPLS ASSY PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 3,446 hrs · 2,086 cycles

DURING SCHEDULED MV3 CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EEPLS INOP. RELAMPED EEPLS.

Part: CAP — MISSING (CABIN) · airframe 1,748 hrs · 1,054 cycles

EEPLS END CAP AT ROW 1 ABC MISSING. INSTALLED END CAP PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 1,063 hrs · 622 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.