N473WN

Part: SEAL — CRACKED (ZONE 300) · airframe 70,453 hrs · 42,054 cycles

RIGHT HORIZONTAL STABILIZER UPPER FORWARD SLIDER CRACKED. R & R RT HORIZONTAL STAB UPPER FWD SLIDING SEAL IAW AMM 53-31-31.

Part: SEAT — OUT OF ADJUST (ZONE 200) · airframe 69,629 hrs · 41,540 cycles

SEAT 11F RECLINES INTO EXIT ROW. ADJUSTED SEAT RECLINE LOCK IN REF TO AMM 25-22-00.

Part: HANDLE — LOOSE (ZONE 800) · airframe 69,215 hrs · 41,307 cycles

FWD GALLEY SERVICE DOOR UPPER ASSIST HANDLE IS LOOSE.<[01] RE SECURED FWD GALLEY SERVICE DOOR ASSIST HANDLE REF AMM 20-50-11.

Part: HANDLE — LOOSE (ZONE 800) · airframe 69,215 hrs · 41,307 cycles

FWD ENTRY DOOR UPPER ASSIST HANDLE IS LOOSE.<[01] RE SECURED FWD ENTRY DOOR UPPER ASSIST HANDLE REF AMM 20-50-11.

Part: DOOR — OUT OF ADJUST (ZONE 100) · airframe 68,191 hrs · 40,717 cycles

A/C GROUND AIR ACCESS DOOR WILL NOT OPEN OR CLOSE. <[01] 01 - REMOVED AND REPLACED PER [AMM 52-49-01-401-NG (FORWARD FAIRING ACCESS DOOR - REMOVAL/INSTALLATION - PERMANENT)].

Part: SLIDE — OUT OF POSITION (ZN 800 DOOR) · airframe 67,661 hrs · 40,401 cycles

AFT LH EMERGENCY SLIDE FELL OUT OF HOUSING<[01] CW REPACK OF L2 DOOR SLIDE PER MT 725-61-06

Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 66,972 hrs · 39,973 cycles

AFT MEGAPHONE INOP<[01] REMOVED AND REPLACED AFT GAL MEGAPHONE IAW AMM 25-64-00. NO FURTHER DEFECTS NOTED AT THIS TIME

Part: LIGHT — INOPERATIVE (MID CABIN) · airframe 65,755 hrs · 39,229 cycles

R2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE.<[01] RELAMPED R2 DOOR EXTERIOR EMERGENCY LIGHT AS PER B737 AMM 33-51-04-960-801. TEST PASSED.;[02] VERIFIED STEP 1.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 65,755 hrs · 39,229 cycles

L/W O/B AFT FLAP; I/B AFT CORNER DISBONDED<[01] FINAL STATEMENT: REMOVED DAMAGE DELAMINATED UPPER AND LOWER SKINS ON L/W O/B AFT FLAP WEDGE I/B CORNER AS PER B737 SWRM 51-70-10-2R-4. PARAG. (7-A-1). INSTALLED HOT BONDER PERMANENT REPAIR AT L\W O\B AFT FLAP ON I\B CORNER UPPER AND LOWER SURFACE PER B737 SRM 57-53-01-2R-14 AND B737 SRM 51-70-10-2R-0PARAGRAPH (20.B) MATERIAL USED FIM ADHES AF 163-2K-06 PO#2053056 AND TOOL USED TEMPERATURE CONTROL ID:170006 DUE DATE 6/1/24.;[02] VERIFIED STEP 1;[03] CORRECTION: UPDATE MEASUREMENT TABLE

Part: PANEL — CORRODED (ZONE 100) · airframe 65,755 hrs · 39,229 cycles

PANEL # 192F CORRODED WHERE DME#1 ATTACHES.<[01] REMOVED AND REPLACED PANEL #192F AS PER REFS B737 AMM 53-51-21-000-802 & AMM 53-51-21-400-802.

Part: SEAL — DETERIORATED (HORIZONTAL STAB) · airframe 65,755 hrs · 39,229 cycles

RIGHT HORIZONTAL STABILIZER I/B BALANCE LWR T/E ACCESS PANEL 343AB 2 AFT ANGLE METAL SEALS WITH BROW COVERS DETERIORATED..<[01] REMOVED AND REPLACED FWD AND AFT ANGLE METAL SEAL (PART#186A3004-4 AND 186A3004-18) FROM PANEL 343AB RIGHT HORIZONTAL STABILIZER I/B BALANCE LWR T/E PER B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED AND INSPECTED STEP#1.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 65,755 hrs · 39,229 cycles

LT IB FLAP UPPER SURFACE OF TRAILING EDGE WEDGE HAS DELAMINATION 33' FROM OB END AND ON LOWER SURFACE 4' FROM OB END. 8-58<[01] FINAL STATEMENT: REMOVED AND REPLACED WEDGE AT LT WING I/B FLAP T/E REF B737-700 SRM 51-40-02-0G-0 AND DWG# 113A2100.;[02] VERIFIED STEP 1

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 65,755 hrs · 39,229 cycles

CORROSION ON LWR SURFACE OF F/O SEAT TRACK FWD OB. 8-66<[01] FINAL STATEMENT: REMOVED AND REPLACED F/O'S FWD O/B SEAT TRACK REF AMM 25-11-11-400-801 AND SRM 51-40-02-0G-0;[02] VERIFIED STEP 1

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 65,755 hrs · 39,229 cycles

CORROSION ON LWR SURFACE OF CAPT FWD OB SEAT TRACK. 8-62<[01] REPLACED CAPT FWD OB SEAT TRACK. REF AMM 25-11-11-400-801. FIXTURE TRACK BC 170026.;[02] CORRECTION STEP 1: REMOVE AND REPLACE CAPT FWD OB SEAT TRACK REF SRM 51-40-02-0G-0 AND REF AMM 25-11-11-400-801.;[03] CORRECTION STEP 2: REMOVED AND REPLACED CAPT FWD OB SEAT TRACK REF SRM 51-40-02-0G-0 AND REF AMM 25-11-11-400-801.;[04] VERIFIED STEP 3

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 65,755 hrs · 39,229 cycles

CORROSION ON LWR SURFACE OF CAPT SEAT TRACK FWD IB. 8-64<[01] REPLACED FWD CAPT SEAT TRACK. REF AMM 25-11-11-400-801. FIXTURE TRACK BC 170026.;[02] CORRECTION STEP#1. REMOVED AND REPLACED FWD CAPT SEAT TRACK. REF AMM 25-11-11-400-801. REF SRM 51-40-02-0G-0.;[03] VERIFIED STEP 2

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 65,755 hrs · 39,229 cycles

CORROSION ON LWR SURFACE OF CAPT SEAT TRACK AFT OB. 8-67<[01] CAPT SEAT TRACK AFT OB WILL BE REPLACED IN TC TTG8Q00SYP7V;[02] VERIFIED STEP 1

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 65,755 hrs · 39,229 cycles

CORROSION ON LWR SURFACE OF CAPT SEAT TRACK AFT IB. 8-63<[01] REPLACED AFT IB CAPT SEAT TRACK REF SRM 51-40-02-0G-0 AND AMM 25-11-11-400-801.;[02] CORRECTION STEP #1. REMOVED AND REPLACED AFT IB CAPT SEAT TRACK REF SRM 51-40-02-0G-0 AND AMM 25-11-11-400-801.;[03] VERIFIED STEP 2; SEAT TRACK REPLACED.

Part: SEAT TRACK — CORRODED (COCKPIT) · airframe 65,755 hrs · 39,229 cycles

CORROSION ON LWR SURFACE OF CAPT SEAT TRACK FWD IB. 8-68<[01] CAPT SEAT TRACK FWD IB WILL BE REPLACED TC TTG8Q00SYP7C.;[02] VERIFIED STEP 1

Part: WEB — CRACKED (BS 727 S18A) · airframe 65,755 hrs · 39,229 cycles

CRACK FOUND AT I/B LOWER FASTENER HOLE OF S-18A WEB AT STA 727 RIGHT SIDE. CRACK FOUND AT I/B LOWER FASTENER HOLE OF S-18A WEB FITTING AT STA 727 RIGHT SIDE. ( NOTE: CRACK INDICATION FOUND AT WEB FITTING LOCATED AT LOWER SECTION OF THE WEB)<[01] REMOVED AND REPLACED CRACKED SPLICE FITTING AT S-18A AT STA 727 RIGHT SIDE AS PER SRM 51-40-02-0G-0 AND DWG#146A0062. TOOL USED: B/C 175290. CALIBRATION DUE DATE: 03-20-2025.;[02] RII---VERIFIED STEP#1.

Part: ACCESS PANEL — DAMAGED (ZONE 100) · airframe 65,755 hrs · 39,229 cycles

ACCESS PANEL 193B HAS AN ELONGATED HOLE R/H SIDE ALF DOT 068<[01] APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #193B AS PER B737 SRM 51-70-04-2R-9 PARAG 4-D-M; MATERIAL USED: PO#2061896; PO#1690463; TOOL USED: HOT BONDER ID170006; DUE DATE 06-07-24.APPLIED TOPCOAT ON ACCESS PANEL 193B REF B-737 AMM 51-21-73-370-803;[02] VERIFIED STEP 1

Part: ATTACH ANGLE — CRACKED (HORIZONTAL STAB) · airframe 65,755 hrs · 39,229 cycles

GAP COVER 333AT SLIDING PANEL HAS ATTACH ANGLE CRACKED. 8-51<[01] REMOVED AND REPLACED BLADE ASSY AT GAP COVER PANEL 333AT REF B737-700 SRM 51-40-02-0G-0;[02] VERIFIED AND INSPECTED STEP#1.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 65,755 hrs · 39,229 cycles

FWD CEILING PANEL HAS EXIT LIGHT LENS BASE CRACKED AND LENS ATTACH BUTTON BROKED. 8-47<[01] REMOVED AND REPLACED HOUSING ASSY - EXIT SIGN AT CEILING ASSY - FWD CLOSE OUT LOWERED PER B737 AMM 33-51-01-960-801;[02] CORRECTION : REMOVED AND REPLACED HOUSING ASSY - EXIT SIGN AT CEILING ASSY - FWD CLOSE OUT LOWERED PER B737 AMM 33-51-01-960-802;[03] VERIFIED 1. AND 2.

Part: CHANNEL — CORRODED (BS 747-767 RBL21) · airframe 65,755 hrs · 39,229 cycles

AFT CARGO COMP. R/H Z CHANNEL BETWEEN ST 747 TO ST 767; RBL 21 HAVE LIGHT CORROSION AROUND NUTPLATE HOLES (6';10' AND 14'). (228-008)<[01] REMOVED AND REPLACED NEW Z CHANNEL AT AFT CARGO COMPARTMENT BETWEEN STA 727 TO STA 767 RBL 21. PER B737-700 SRM 51-40-02-0G-0 AND DWG#: 146A7500.;[02] VERIFIED AND INSPECTED STEP#1.

Part: CHANNEL — CORRODED (BS 727D-727E) · airframe 65,755 hrs · 39,229 cycles

AFT CARGO COMP. R/H Z CHANNEL BETWEEN ST 727D TO ST 727E; LBL 21 HAVE LIGHT CORROSION AROUND NUTPLATE HOLES (6';7';8';16' AND 18). (228-006) AFT CARGO COMP. R/H Z CHANNEL BETWEEN ST 727D TO ST 727E RBL 21 HAVE LIGHT CORROSION AROUND NUTPLATE HOLES (6'7'8'16' AND 18). (228-006)<[01] FAULT TO BE ACCOMPLISHED ON TTG8Q00SV07E.;[02] VERIFIED STEP#1.

Part: CHANNEL — CORRODED (BS 727C-727D) · airframe 65,755 hrs · 39,229 cycles

AFT CARGO COMP. R/H Z CHANNEL BETWEEN ST 727C TO ST 727D; LBL 21 HAVE LIGHT CORROSION AROUND NUTPLATE HOLE (10). (228-005) AFT CARGO COMP. R/H Z CHANNEL BETWEEN ST 727C TO ST 727D RBL 21 HAVE LIGHT CORROSION AROUND NUTPLATE HOLE (10). (228-005)<[01] FAULT TO BE ACCOMPLISHED ON TTG8Q00SV07E.;[02] VERIFIED STEP#1.

Part: CHANNEL — CORRODED (BS 727E-747) · airframe 65,755 hrs · 39,229 cycles

AFT CARGO COMP. R/H Z CHANNEL BETWEEN ST 727E TO ST 747; LBL 21 HAVE LIGHT CORROSION AROUND NUTPLATE HOLE (10). (228-007) AFT CARGO COMP. R/H Z CHANNEL BETWEEN ST 727E TO ST 747 RBL 21 HAVE LIGHT CORROSION AROUND NUTPLATE HOLE (1'2'5'6'8'10 AND 14'). (228-007)<[01] FAULT TO BE ACCOMPLISHED ON TTG8Q00SV07E.;[02] VERIFIED STEP#1.

Part: CHANNEL — CORRODED (BS 727E-747) · airframe 65,755 hrs · 39,229 cycles

AFT CARGO COMP. L/H Z CHANNEL BETWEEN ST 727E TO ST 747; LBL 21 HAS LIGHT CORROSION AROUND NUTPLATE HOLE (10'). (228-003)<[01] FAULT TO BE ACCOMPLISHED ON TTG8Q00SUZCR.;[02] VERIFIED STEP#1.

Part: CHANNEL — CORRODED (BS 767-787) · airframe 65,755 hrs · 39,229 cycles

AFT CARGO COMP. L/H Z CHANNEL BETWEEN ST 767 TO ST 787; LBL 21 HAVE LIGHT CORROSION AROUND NUTPLATE HOLE (18'). (228-004)<[01] REMOVED AND REPLACED NEW Z CHANNEL AT AFT CARGO COMP. BETWEEN STA 767 TO STA 787 LBL 21.PER B 737-700 DWG#146A7500 AND SRM 51-40-02-0G-0.;[02] VERIFIED AND INSPECTED STEP#1.

Part: CHANNEL — CORRODED (BS 727C-727D) · airframe 65,755 hrs · 39,229 cycles

AFT CARGO COMP. L/H Z CHANNEL BETWEEN ST 727C TO ST 727D; LBL 21 HAVE LIGHT CORROSION AROUND 2 NUTPLATE HOLES (14' AND 18'). (228-001)<[01] FAULT TO BE ACCOMPLISHED ON TTG8Q00SUZCR.;[02] VERIFIED STEP#1.

Part: ATTACH ANGLE — CRACKED (BS 663) · airframe 65,755 hrs · 39,229 cycles

FASTENER HOLES CRACKED ON LEFT VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 19; 25 & 33 POSITION. FASTENER HOLES CRACKED ON LEFT VAPOR BARRIER UPPER ATTACH ANGLE AT LBL 19 25 & 33 POSITION.<[01] REMOVED AND INSTALLED NEW LT VAPOR BARRIER UPPER SUPPORT ANGLE P/N # 111A1322U5 IN REF B 737-700 SRM 51-40-02-0G-0; 51-80-01-0G-0 AND DWG # 111A1322U5;[02] VERIFIED REPLACEMENT OF ANGLE STEP ONE.

Part: FLOORBEAM — CRACKED (BS 540 LBL46) · airframe 65,755 hrs · 39,229 cycles

CABIN FLOOR STRUCTURE; PANEL BREAK UPPER STRAP CRACKED AT STA. 540 LBL46<[01] REMOVED AND REPLACED PANEL BREAK ASSEMBLY AT STA 540. LBL 46 AS PER REF B737 SRM 51-40-02-0G-0.;[02] CORRECTING PREVIOUS STEP: REMOVED AND REPLACED PANEL BREAK ASSEMBLY UPPER PLATE AT STA 540. LBL 46 AS PER REF B737 SRM 51-40-02-0G-0 AND DWG 143A5240.;[03] VERIFIED 2 REPLACEMENT OF PANEL BREAK UPPER PLATE (STRAP).

Part: PANEL — DAMAGED (ZONE 100) · airframe 65,755 hrs · 39,229 cycles

FOUND ELONGATED HOLES ON PANEL 551GB<[01] APPLIED REPAIR AT PANEL#551GB PER B737SRM 57-51-01-2R-1 51-70-04-2R-0PARAGRAPH(4.N.2) MATERIAL USED RESIN 3804 PO#2066364 FIBER GLASS PO#1690463. TOOL USED<BR>TEMPERATURE CONTROL ID:160354 DUE DATE:03/07/25 VACUMM GAGE ID:173240 DUE DATE:05/30/24.APPLIED TOP COAT AT PANEL#551GBON REPAIR AREA PER B737 AMM 51-21-99-300-802 PAINT USED PO#2055785.;[02] VERIFIED PANEL REPAIRED

Part: SEAT TRACK — CORRODED (BS 360) · airframe 65,755 hrs · 39,229 cycles

SEAT TRACK AT LBL 24.75; STA 360+11 FOUND EXFOLIATED.<[01] REMOVED AND REPLACED EXFOLIATED SEAT TRACK BETWEEN STA 360+11 AND STA 480 LBL 24.75 AS PER B737-700 SRM 51-40-02-0G-0; DWG#: 141A5300 AND DWG#: 143A5300.;[02] VERIFIED AND INSPECTED STEP#1.

Part: FLOOR SUPPORT — CORRODED (BS 268 BL 0) · airframe 65,755 hrs · 39,229 cycles

CORROSION ON FLIGHT DECK FLOOR INTERCOSTAL UPPER SURFACE B.S. 268.25 B.L. 0 W.L. 208. (DOT 51-001)<[01] REMOVED AND REPLACED INTERCOSTAL (SUPPORT CHANNEL) AT FLIGHT DECK FLOOR BETWEEN STA 260 AND STA 270 BL 0 REF B737-700 SRM 51-40-02-0G-0 AND DWG# 141A5210.;[02] VERIFIED INTERCOSTAL REPLACED; (SUPPORT CHANNEL).

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 65,755 hrs · 39,229 cycles

CABIN FLOOR PANEL #231XF DELAMINATED<[01] RECEIVED NEW FLOOR PANEL#231XF; THIS PANEL WILL BE INSTALL ON TTG8Q00SBTX5.;[02] VERIFIED TTG8Q00SBTX5.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 65,755 hrs · 39,229 cycles

CABIN FLOOR PANEL #241DF DELAMINATED<[01] RECEIVED NEW FLOOR PANEL# 241 DF; THIS PANEL WILL BE INSTALL ON TTG8Q00SBTUH.;[02] VERIFIED TTG8Q00SBTUH

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 65,755 hrs · 39,229 cycles

FWD CARGO CUTOUT FWD SCUFF PLATE CRACKED<[01] RECEIVED WELDED FWD CARGO FWD SCUFF PLATE FOR OUTSIDE VENDOR J.L WELDIND INC PO#2059779 ; THIS SCUFF PLATE WILL BE INSTALL ON TTG8Q0037XG5;[02] ADD STEP #1 SRM 53-30-15-2R-1FOR WENDING;[03] VERIFIED SCUFF PLATE RECIEVED AND INSTALL TO BE ACCOMPLISHED ON TTG8Q0037XG5

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 65,755 hrs · 39,229 cycles

CABIN FLOOR PANEL #241AF DELAMINATED<[01] RECEIVED NEW FLOOR PANEL 241AF ; THIS PANEL WILL BE INSTALL ON TTG8Q00SBTUP;[02] VERIFIED STEP 1

Part: SUPPORT — CRACKED (ZONE 100) · airframe 65,755 hrs · 39,229 cycles

FUSELAGE SUPPORT STRUCTURE CRACKED UNDER WTB PANEL #191AR<[01] REMOVED AND REPLACED SUPPORT STRUCTURE (FRAME) UNDER WTB PANEL# 191AR REF B737-700 SRM 51-40-02-0G-0 AND DWG# 116A3110 AND 116A3010.;[02] VERIFIED CORRECTIVE ACTION STEP 1

Part: PIVOT ASSY — CRACKED (LT RAM AIR DOOR) · airframe 65,755 hrs · 39,229 cycles

LEFT RAM AIR DOOR LINKAGES ARE WORN. THE LINKAGE PIVOT FITTING IS CRACKED THROUGH.<[01] REMOVED AND REPLACED LT RAM AIR DOOR LINKAGES AND HARDWARE REF SRM 51-40-20-0G-0.;[02] VERIFIED STEP 1

Part: INLET — CRACKED (NR 1 ENGINE) · airframe 65,755 hrs · 39,229 cycles

# 1 ENGINE INLET COWL OUTER BARREL LOWER SKIN ANTI-ICE AIR GRILL OUTLET CRACKED AT 6 O'CLOCK. MARKED DOT 251-006<[01] ENG 1 INLET COWL WILL BE REPLACE USING TASK CARD 7111-E-17062-NG (REP - INLET COWL AND CRUSHABLE WEAR SPACERS) [TTG8Q00S71ZL];[02] VERIFIED STEP 1

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 65,725 hrs · 39,213 cycles

LH HORIZONTAL FRONT UPPER SLIDING SEAL IS CRACKED.<[01] REMOVED LH HORIZONTAL FRONT UPPER SLIDING SEAL. REF AMM 53-31-31. INSTALLATION STILL REQUIRED.;[02] 01 - REMOVED AND REPLACED PER [AMM 53-31-31-401 CONFIG 1-NG (STABILIZER TO BODY FRONT SPAR SLIDING SEAL - REMOVAL/INSTALLATION - PERMANENT)]

Part: SIGN — LOOSE (CABIN) · airframe 65,645 hrs · 39,162 cycles

EXIT SIGN OVER FWD GALLEY DOOR FELL OFF<[01] 04 - REPAIRED PER [EA EA-GENERAL (EA ATTACHED TO AN AIRCRAFT FAULT)] OK TO CONTINUE PER EA -21-133-00720 MUST BE REPAIRED IN 30 FLT CYCLES

Part: BRACKET — LOOSE (GIRT BAR) · airframe 65,515 hrs · 39,086 cycles

FORWARD SERVICE DOOR GIRT BAR BRACKET IS LOOSE<[01] RESECURED FORWARD SERVICE DOOR GIRTBAR BRACKET PER S.I.P

Part: SLIDE — LOOSE (L1 DOOR) · airframe 65,276 hrs · 38,929 cycles

L1 SLIDE LOOSE; DID NOT DEPLOY<[01] RESECURED SLIDE FOR L1 DOOR IAW MT 725-61-06. A/C OK FOR SERVICE.

Part: LAMP — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,316 hrs · 38,320 cycles

EMERGENCY EXIT ROW SIDEWALL LIGHT FO SIDE INOP<[01] R&R RH SIDE ROW EMERGENCY EXIT LAMP &FUSE REF A.M.M 33-51-01;OPS CHECK GOOD AT THIS TIME

Part: BATTERY — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,179 hrs · 38,242 cycles

FORWARD GALLEY EMERGENCY FLASHLIGHT-BLINKING POWER LIGHT INOP<[01] REMOVED AND REPLACED FWD GALLEY UPPER EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-64-00; OPS CHECK GOOD.

Part: GIRT BAR — LOOSE (ZN 200 FUS TOP) · airframe 64,037 hrs · 38,151 cycles

FORWARD ENTRY DOOR. RIGHT GIRT BAR; REPORTED LOOSE. PERFORMED A VISUAL AND OPS CHECK OF FORWARD ENTRY DOOR GIRT BAR PER AMM 25-66-01 OPS CHECKS GOOD.<[01] PERFORMED A VISUAL AND OPS CHECK OF FORWARD ENTRY DOOR GIRT BAR PER AMM 25-66-01; OPS CHECKS GOOD.

Part: HOOK — LOOSE (ZN 800 DOOR) · airframe 63,536 hrs · 37,805 cycles

FWD SVC DOOR GIRT BAR STOWAGE HOOK LOOSE<[01] RESECURED FWD SVC DOOR GIRT BAR STOWAGE HOOK RIVETS PER <BR>MM 25-66-00

Part: POWER SUPPLY — INOPERATIVE (ZN 200 FUS TOP) · airframe 62,926 hrs · 37,412 cycles

EMER LIGHTS 9/ 12 CBA AND RH AFT OF WING GROUND ILLUMINATION LTS INOP<[01] R/R STA727C+13 EMER LIGHT POWER SUPPLY PER AMM 33-51 -06 OPS CHECK GOOD.

Part: LENS — MISSING (R/H CABIN) · airframe 60,426 hrs · 35,769 cycles

ROW 18 DEF EMERGENCY LIGHT LENS MISSING. / [01] REPLACED MISSING EMERGENCY LIGHT LENS IAM AMM 33-51-03

Part: ANGLE — CRACKED (PAX CABIN) · airframe 60,134 hrs · 35,574 cycles

CRACK ANGLE FLOOR STRUCTURE AT BS 291.5 TO BS 294.5 AT LEVEL STR17R AT PASSENGER CABIN 2022-257561 / [01] REPLACED ANGLE FLOOR STRUCTURE AT BS 291.5 TO BS 294.5 AT LEVEL STR17R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG #141A8310 REV. -. SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED ANGLE FLOOR STRUCTURE AT BS 291.5 TO BS 294.5 AT LEVEL STR17R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG #141A8310 REV. -. RII ; SEE INDIVIDUAL SIGN OFFS BELOW.

Part: FLOOR PANEL — MISSING (FWD GALLEY) · airframe 60,134 hrs · 35,574 cycles

MISSING MATERIAL FLOOR PANEL 221BF ON CORNER AREA AT FWD GALLEY AREA 2022-207360 / [01] REPLACED FLOOR PANEL 221BF AT FWD GALLEY AREA IAW B737-700 AMM 53-21-00-400-801;[02] REPLACED FLOOR PANEL 221BF AT FWD GALLEY AREA IAW B737-700 AMM 53-21-00-400-801

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 60,134 hrs · 35,574 cycles

DELAMINATED FLOOR PANEL 231AF AT PASSENGER CABIN 2022-207399 REPAIRED FLOOR PANEL 231AF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 60,134 hrs · 35,574 cycles

CORROSION FLOOR PANEL 221BF SLEEVE AT FWD GALLEY AREA (20 EA) 2022-207359 / [01] REPLACED FLOOR PANEL 221BF AT FWD GALLEY AREA IAW B737-700 AMM 53-21-00-400-801;[02] REPLACED FLOOR PANEL 221BF AT FWD GALLEY AREA IAW B737-700 AMM 53-21-00-400-801

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 60,134 hrs · 35,574 cycles

PERFORATION FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT 2022-207311 / [01] FABRICATED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWING: 453A2610 SHEET 9 REV E. MATERIAL USED P/N: 2024T3-071 P.O: 2021 210316.;[02] FABRICATED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWING: 453A2610 SHEET 9 REV E. MATERIAL USED P/N: 2024T3-071 P.O: 2021 210316.

Part: FLOOR PANEL — CRACKED (AFT GALLEY) · airframe 60,134 hrs · 35,574 cycles

CRACK ON FLOOR PANEL 242XF OF AFT GALLEY AREA 2022-207323 / [01] REPLACED FLOOR PANEL 242XF OF AFT GALLEY AREA I.A.W B737-700 AMM 53-21-00-400-891 STEP 3.F ITEM 10 AND FLOOR PANEL 242XF WILL BE INSTALLED ON CARD: TTG8Q00B8SWC;[02] CERTIFIED WORK PERFORMED.

Part: FLOOR PANEL — DETERIORATED (AFT CARGO BAY) · airframe 60,134 hrs · 35,574 cycles

DETERIORATED FLOOR PANEL 140AF AT AFT CARGO COMPARTMENT 2022-207314 / [01] FABRICATED FLOOOR PANEL 140AF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWING 453A2610 SHEET 4 REV C MATERIAL USED: P/N: A90RG1W 48144 P.O: 2021 237448;[02] FABRICATED FLOOOR PANEL 140AF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWING 453A2610 SHEET 4 REV C MATERIAL USED: P/N: A90RG1W 48144 P.O: 2021 237448

Part: FLOOR PANEL — DETERIORATED (FWD CARGO BAY) · airframe 60,134 hrs · 35,574 cycles

DETERIORATED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT 2022-207293 / [01] FABRICATED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWING: 453A1610 SHEET 7 REV C MATERIAL USED P/N: 2024T3-071 P.O: 2021 210316.;[02] FABRICATED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWING: 453A1610 SHEET 7 REV C MATERIAL USED P/N: 2024T3-071 P.O: 2021 210316.

Part: BRACKET — BROKEN (RH WING) · airframe 60,134 hrs · 35,574 cycles

BROKEN SPAR LOWER BRAKET LOC ON OUTBOARD SIDE STRUT BOX AREA AT RT PYLON 2022-207304 / [01] REPLACED BRACKET AND FASTENERS LOCATED ON OUTBOARD SIDE STRUT BOX AREA AT RT PYLON IAW B737-700 SRM 52-40-02;[02] CORRECTED STEP 1<BR>REPLACED BRACKET AND FASTENERS LOCATED ON OUTBOARD SIDE STRUT BOX AREA AT RT PYLON IAW B737-700 SRM 51-40-02;[03] REPLACED BRACKET AND FASTENERS LOCATED ON OUTBOARD SIDE STRUT BOX AREA AT RT PYLON IAW B737-700 SRM 51-40-02

Part: BULKHEAD — ELONGATED (AFT CARGO BAY) · airframe 60,134 hrs · 35,574 cycles

ELONGATED HOLE BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT 2022-207266 / [01] FABRICATED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWING 453A2510 SHEET 12 REV - MATERIAL USED: A60SG4W 60144 P.O: 2022 104980;[02] FABRICATED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWING 453A2510 SHEET 12 REV - MATERIAL USED: A60SG4W 60144 P.O: 2022 104980

Part: PLATE — CRACKED (LH WING PANEL) · airframe 60,134 hrs · 35,574 cycles

CRACK PLATE ASSY TRAILING EDGE ACCESS PANEL 542 BB LT WING 2022-207265 / [01] REPLACED PLATE ASSY TRAILING EDGE ACCESS PANEL 542 BB LT WING IAW B737-700 SRM 51-40-02-0G-0;[02] REPLACED PLATE ASSY TRAILING EDGE ACCESS PANEL 542 BB LT WING IAW B737-700 SRM 51-40-02-0G-0

Part: PLATE — CRACKED (LH WING PANEL) · airframe 60,134 hrs · 35,574 cycles

CRACK PLATE ASSY TRAILING EDGE OUTBARD EDGE ACCESS PANEL 542BB LT WING 2022-207267 / [01] REPLACED PLATE ASSY TRAILING EDGE OUTBARD EDGE ACCESS PANEL 542BB LT WING IAW B737-700 SRM 51-40-02-0G-0;[02] REPLACED PLATE ASSY TRAILING EDGE OUTBARD EDGE ACCESS PANEL 542BB LT WING IAW B737-700 SRM 51-40-02-0G-0

Part: PANEL — CRACKED (LH WING) · airframe 60,134 hrs · 35,574 cycles

CRACK FUEL TANK INDICATOR HOUSING ACCESS PANEL 532CB AT LT WING 2022-207272 / [01] REMOVED AND REPLACED MEASURING STICK 3 AND HOUSING IAW B737-700 AMM:28-44-11-400-801 TOOL USED:TORQUE P/N:QD1R50 S/N:0416041420 D/D:22/FEB/23;[02] REMOVED AND REPLACED MEASURING STICK 3 AND HOUSING IAW B737-700 AMM:28-44-11-400-801 TOOL USED:TORQUE P/N:QD1R50 S/N:0416041420 D/D:22/FEB/23<BR>NO LEAK WAS FOUND;[03] CORRECTED STEP 1 AND 2 <BR>REMOVED AND REPLACED MEASURING STICK 3 AND HOUSING IAW B737-700 AMM:28-44-11-400-801 TOOL USED:TORQUE P/N:QD1R50 S/N:0416041420 D/D:22/FEB/23 <BR>NO LEAK WAS FOUND <BR>SEE INDIVIDUAL SIGN OFF BELOW;[04] CERTIFIED STEP 3 COMPLETE <BR>LEAK NOT FOUND

Part: PLATE — CRACKED (RH WING PANEL) · airframe 60,134 hrs · 35,574 cycles

CRACK PLATE ASSY TRAILING EDGE OUTBOARD CENTER EDGE ACCESS PANEL 642BB RT WING 2022-207270 / [01] REPLACED PLATE ASSY AND FASTENERSON TRAILING EDGE OUTBOARD CENTER EDGE ACCESS PANEL 642BB RT WING IAW B737-700 SRM 51-40-02-0G-0;[02] REPLACED PLATE ASSY AND FASTENERSON TRAILING EDGE OUTBOARD CENTER EDGE ACCESS PANEL 642BB RT WING IAW B737-700 SRM 51-40-02-0G-0

Part: BULKHEAD — ELONGATED (AFT CARGO BAY) · airframe 60,134 hrs · 35,574 cycles

ELONGATED HOLE BULKHEAD PANEL 142MW AT AFT CARGO COMPARTMENT 2022-207268 / [01] FABRICATED BULKHEAD PANEL 142MW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWING #453A2510 SHEET: 5 REV: -; MATERIAL USED P/N: A60SG4W PO: 2022-104980;[02] TASK COMPLETED

Part: PLATE — CRACKED (RH WING PANEL) · airframe 60,134 hrs · 35,574 cycles

CRACK PLATE ASSY TRAILING EDGE OUTBOARD FWD EDGE ACCESS PANEL 642BB RT WING 2022-207269 / [01] REPLACED PLATE ASSY TRAILING EDGE OUTBOARD FWD EDGE ACCESS PANEL 642BB RT WING IAW B737-700 SRM 51-40-02-0G-0;[02] REPLACED PLATE ASSY TRAILING EDGE OUTBOARD FWD EDGE ACCESS PANEL 642BB RT WING IAW B737-700 SRM 51-40-02-0G-0

Part: PLATE — CRACKED (RH WING) · airframe 60,134 hrs · 35,574 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 243 LOWER SURFACE AT RT WING 2022-207218 / [01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 243 LOWER SURFACE AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A2001; SHEET 30; REV. A.;[02] TASK COMPLETED

Part: WEB — CRACKED (FWD GALLEY) · airframe 60,134 hrs · 35,574 cycles

CRACK INNER CHORD LOCATED BS303.9 AT LBL55 AT FWD GALLEY AREA 2022-207235 / [01] REPLACED INNER CHORD LOCATED BTW BS 360 AND BS 270 AT LBL55 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02 DWG:141A8110 SHEET:9 REV:A P/N: 654A0004-1073 P.O: 2023000639 SEE INDIVIDUAL SING OFFS BELOW;[02] JOB CERTIFIED AS RII.

Part: PANEL — CRACKED (LH WING) · airframe 60,134 hrs · 35,574 cycles

CRACK ACCESS PANEL HOLES 561BB AT LT WING 2022-207243 / [01] TOOL USED: HOT BONDER P/N:HCS9200B S/N:18175478 DUE DATE:05-AUG-22.;[02] TOOL USED:SCALE P/N: SCA-301 S/N:AE-412127 DUE DATE:14-MAR-23.;[03] TOOL USED: HOT BONDER P/N:HCS9200B S/N:18196127 DUE DATE:16-JAN-23.;[04] TOOL USED MULTIMETER P/N: FLUKE 1587 ; S/N: 38200035 ; DUE DATE: 08-SEP-22;[05] REPAIRED ACCESS PANEL 561BB AT LT WING IAW B737-700 SRM 51-70-04-2R-09 REPAIR 09. TOOL USED: CALIPER P/N 500-464; S/N: 15331932; DUE DATE: 26-OCT-22. SEE INDIVIDUAL SIGNOFFS BELOW.;[06] JOB COMPLETED

Part: PANEL — CRACKED (LH WING) · airframe 60,134 hrs · 35,574 cycles

CRACK ACCESS PANEL HOLES 561AB AT LT WING 2022-207242 / [01] TOOL USED: HOT BONDER P/N:HCS9200B S/N:18175478 DUE DATE:05-AUG-22.;[02] TOOL USED:SCALE P/N: SCA-301 S/N:AE-412127 DUE DATE:14-MAR-23.;[03] TOOL USED MULTIMETER P/N: FLUKE 1587 ; S/N: 38200035 ; DUE DATE: 08-SEP-22;[04] REPAIRED ACCESS PANEL 561AB AT LT WING IAW B737-700 SRM 51-70-04-2R-09 REPAIR 9 TOOL USED: CALIPER P/N: 500-464; S/N: 15331932; DUE DATE: 26-OCT-22. SEE INDIVIDUAL SIGNOFFS BELOW.;[05] TASK COMPLETED

Part: FLOORBEAM — CORRODED (FWD GALLEY FLOOR) · airframe 60,134 hrs · 35,574 cycles

CORROSION FLOOR BEAM LOCATED BS312 AT LBL16 AND WL208.1 AT FWD GALLEY AREA 2022-207236 / [01] TOOL EDDY CURRENT USED P/N: NORTEC 600D S/N: 60009161631 AND DUE DATE: 03-DEC-22.;[02] REPAIRED FLOOR BEAM LOCATED BS312 AT LBL16 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-17; REPAIR 17. THIS REPAIR IS CATEGORY A. SEE INDIVIDUAL SIGNOFF BELOW.;[03] REPAIRED FLOOR BEAM LOCATED BS312 AT LBL16 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-17; REPAIR 17. THIS REPAIR IS CATEGORY A. SEE INDIVIDUAL SIGNOFF BELOW... RII ITEM

Part: INTERCOSTAL — CRACKED (FWD GALLEY) · airframe 60,134 hrs · 35,574 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS312 TO BS328 AT RBL30 FWD GALLEY AND LAV 2022-207226 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS312 TO BS328 AT RBL30 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 141A5400 REV:-;[02] CORRECTIVE STEP 1<BR>REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS312 TO BS328 AT RBL30 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 141A5400 REV:-. SEE INDIVIDUAL SIGNSOFF BELOW.;[03] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,134 hrs · 35,574 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS294.5 TO BS312 AT RBL15 FWD GALLEY AND LAV 2022-207227 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS294.5 TO BS312 AT RBL15 FWD GALLEY IAW B737-700 SRM 51-10-02 AND B737-700 SRM 51-40-02 AND DRAWING DRAWING 141A5400 REV A AND DRAWING 141A5410 REV A;[02] CORRECTED STEP <BR>REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS294.5 TO BS312 AT RBL15 FWD GALLEY IAW B737-700 SRM 51-10-02 AND B737-700 SRM 51-40-02 AND DRAWING DRAWING 141A5400 REV A AND DRAWING 141A5410 REV A .SEE INDIVIDUAL SIGN OFF BELOW;[03] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ANGLE — CORRODED (FWD GALLEY) · airframe 60,134 hrs · 35,574 cycles

CORROSION INNER CHORD LOCATED BS328 AT RBL58 AND WL208.1 AT FWD GALLEY AREA 2022-207221 / [01] TOOL USED PN. 35DL; SN. 091419910; DUE DATE. 26-JAN-23;[02] REPLACED INNER CHORD LOC. BS328 AT RBL58 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEET 25 REV: B. SEE INDIVIDUAL SIGN-OFF BELOW;[03] REPLACED INNER CHORD LOC. BS328 AT RBL58 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEET 25 REV: B. SEE INDIVIDUAL SIGN-OFF BELOW. COMPLETED RII

Part: FLOORBEAM — CORRODED (FWD GALLEY FLOOR) · airframe 60,134 hrs · 35,574 cycles

CORROSION FLOOR BEAM LOCATED BS344 AT LBL9 AND WL208.1 AT FWD GALLEY AREA 2022-207215. [05] REPAIRED FLOOR BEAM BTW BS 328 TO BS 360 LBL 11.10 WL208.1 AT FWD GALLEY AREA I.A.W B737-700 SRM 53-10-51-2R-9 REPAIR 9 REPAIR IS CATEGORY: A DOES NOT REQUIRE INSPECTIONS SEE INDIVIDUAL SING OFF BELOW.;[06] REPAIRED FLOOR BEAM BTW BS 328 TO BS 360 LBL 11.10 WL208.1 AT FWD GALLEY AREA I.A.W B737-700 SRM 53-10-51-2R-9 REPAIR 9 REPAIR IS CATEGORY: A DOES NOT REQUIRE INSPECTIONS;

Part: PLATE — CRACKED (LH WING) · airframe 60,134 hrs · 35,574 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL ORSS 243 LOWER SURFACE AT LT WING 2022-207199 / [01] REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE LOCATED AT LEVEL ORSS 243 LOWER SURFACE AT LT WING IAW B737-700 SRM 51-40-02 AD DRAWING 115A2001 SHEET 30 REV. A. PURCHASE ORDER 2022-144386. TOOL USED CALIPER P/N 500-197-30; S/N A21043164; DUE DATE: 01/SEP/22;[02] CORRECTED STEP 1<BR>REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE LOCATED AT LEVEL ORSS 243 LOWER SURFACE AT LT WING IAW B737-700 SRM 51-40-02; SRM B737-700 51-10-02 AND DRAWING 115A2001 SHEET 30 REV. A. PURCHASE ORDER 2022-144386. TOOL USED CALIPER P/N 500-197-30; S/N A21043164; DUE DATE: 01/SEP/22;[03] TASK COMPLETED

Part: FLOORBEAM — CORRODED (AFT GALLEY) · airframe 60,134 hrs · 35,574 cycles

CORROSION ON FLOOR BEAM 986.5 RBL 5 AND WL 208. AFT GALLEY AREA 2022-207214 / [01] TOOL USED: ULTRASONIC THICKNESS GAUGE; PN:45MG; SN: 130064101; DUE DATE: 11-MAY-22;[02] EDDY CURRENT EQUIPMENT P/N: NORTEC500D; S/N: N500X12101V022235; DUE DATE: 03-JUN-22.;[03] TOOL USED P/N FPK-PRO-104 S/N PRO-3384 DUE DATE: 24 MAY 22;[04] REPAIRED FLOOR BEAM BS 986.5 LOC. AT THE RBL 1 TO RBL 9 AND WL 208.1 AFT GALLEY AREA I.A.W B737-700 SRM 53-70-51-2R-6 ALTERNATIVE 1; PARAGRAPH 4; TABLE 201 FIGURE 202; SEE INDIVIDUAL SIGN OFFS BELLOW.;[05] JOB COMPLETE

Part: PANEL — CRACKED (RH WING) · airframe 60,134 hrs · 35,574 cycles

CRACK ACCESS PANEL 661BB AT RT WING 2022-207240 / [01] TOOL USED:CALIPER P/N:500-464 S/N:15331926 DUE DATE 28-SEP-22;[02] TOOL USED: HOT BONDER P/N:HCS9200B S/N:18175478 DUE DATE:05-AUG-22;[03] TOOL USED:SCALE P/N: SCA-301 S/N:AE-412127 DUE DATE:14-MAR-23.;[04] TOOL USED: HOT BONDER P/N:HCS9200B S/N:18196127 DUE DATE:16-JAN-23.;[05] TOOL USED MULTIMETER P/N: FLUKE 1587 ; S/N: 38200035 ; DUE DATE: 08-SEP-22;[06] REPAIRED ACCESS PANEL 661BB AT RT WING IAW B737-700 SRM 51-70-04-2R-09 REPAIR 9. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] TASK COMPLETED

Part: FLOORBEAM — CORRODED (AFT GALLEY) · airframe 60,134 hrs · 35,574 cycles

CORROSION ON FLOOR BEAM 986.5 LBL 44 AND WL 208.1 AFT GALLEY AREA 2022-207220 / [04] REPAIRED FLOOR BEAM 986.5 LBL 55.8 BTW LBL 64 AND WL 208.1 AFT GALLEY AREA I.A.W B737-700 SRM 53-70-51-2R-6 REPAIR 6 TABLE 204 FIGURE: 205. THIS REPAIR IS CATEGORY AND NOT REQUIRED ANY INSPECTIONS SEE INDIVIDUAL SING OFF BELOW.;[05] CORRECTED STEP 4 REPAIRED FLOOR BEAM 986.5 LBL 55.8 BTW LBL 64 AND WL 208.1 AFT GALLEY AREA I.A.W B737-700 SRM 53-70-51-2R-6 REPAIR 6 TABLE 204 FIGURE: 205. THIS REPAIR IS CATEGORY A AND NOT REQUIRED ANY INSPECTIONS

Part: ANGLE — CORRODED (FWD GALLEY FLOOR) · airframe 60,134 hrs · 35,574 cycles

CORROSION ANGLE - SUPPORT LOCATED BS312 TO BS328 AT RBL59 AND WL208.1 AT FWD GALLEY AREA 2022-207238. REPLACED ANGLE - SUPPORT LOCATED AT INNER CHORD BTW BS294.5 TO BS328 AT RBL59 AND WL208.1 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A8310 REV:- SHEET 23.

Part: SUPPORT ANGLE — CRACKED (LH WING) · airframe 60,134 hrs · 35,574 cycles

CRACK SUPPORT ANGLE LOWER SURFACE REAR SPAR LOCATED AT LEVEL ORSS 281 AND ORSS 329 LT WING 2022-207190 / [01] REPLACED SUPPORT ANGLE ( BEAM ASSY ) P/N : 115A3758-9 PO: 2022 143854 LOC. LOWER SURFACE REAR SPAR AT LEVEL ORSS 281 AND ORSS 329 LT WING IAW B737-700 SRM 51-10-02 ; 51-40-02 AND DWG # 115A3700 REV :- DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM AND CRACK MEASURE IS: 0.700? TOOL USED; DIGITAL CALIPER P/N: 500-197-30 S/N:A21143429 DUE DATE: 11-OCT-22;[02] REPLACED SUPPORT ANGLE ( BEAM ASSY ) P/N : 115A3758-9 PO: 2022 143854 LOC. LOWER SURFACE REAR SPAR AT LEVEL ORSS 281 AND ORSS 329 LT WING IAW B737-700 SRM 51-10-02 ; 51-40-02 AND DWG # 115A3700 REV.

Part: PANEL — CRACKED (RH WING) · airframe 60,134 hrs · 35,574 cycles

CRACK ACCESS PANEL 661AB HOLES AT RT WING 2022-207241 / [01] TOOL USED: CALIPER P/N:500-464 S/N:15331926 DUE DATE 28-SEP-22;[02] TOOL USED: HOT BONDER P/N:HCS9200B S/N:18175478 DUE DATE:05-AUG-22.;[03] TOOL USED:SCALE P/N: SCA-301 S/N:AE-412127 DUE DATE:14-MAR-23.;[04] TOOL USED MULTIMETER P/N: FLUKE 1587 ; S/N: 38200035 ; DUE DATE: 08-SEP-22;[05] REPAIRED ACCESS PANEL 661AB AT RT WING IAW B737-700 SRM 51-70-04-2R-09 REPAIR 9. SEE INDIVIDUAL SIGNOFFS BELOW.;[06] TASK COMPLETED

Part: FLOORBEAM — CORRODED (FWD GALLEY FLOOR) · airframe 60,134 hrs · 35,574 cycles

CORROSION FLOOR BEAM LOCATED BS294.5 AT RBL9 TO RBL13 AND WL208.1 AT FWD GALLEY AREA 2022-207229 REPAIRED FLOOR BEAM LOC. BS294.5 AT RBL9 TO RBL13 AND WL208.1 AT FWD GALLEY AREA; IAW SRM 53-10-51-2R-16 THIS REPAIR IS CATEGORY A. REPAIRED FLOOR BEAM LOC. BS294.5 BTW RBL41 TO LBL40 AND WL208.1 AT FWD GALLEY AREA; IAW SRM 53-10-51-2R-16 ALTERNATIVE A; THIS REPAIR IS CATEGORY A;

Part: WEB — CRACKED (FWD GALLEY) · airframe 60,134 hrs · 35,574 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS277 TO BS294.5 AT BL0 FWD GALLEY AND LAV 2022-207232 / [01] REPLACED NEW WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS277 TO BS294.5 AT BL0 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 20 REV - AND SRM 51-10-02 PARAGRAPH 9;[02] CORRECTIVE STEP 1<BR>REPLACED NEW WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS277 TO BS294.5 AT BL0 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 20 REV - AND SRM 51-10-02 PARAGRAPH 9. SEE INDIVIDUAL SIGNSOFF BELOW.;[03] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: WEB — CRACKED (FWD GALLEY) · airframe 60,134 hrs · 35,574 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS312 TO BS328 AT LBL46 FWD GALLEY AND LAV 2022-207233 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS312 TO BS328 AT LBL46 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 141A5400 REV:-;[02] CORRECTIVE STEP 1<BR>REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS312 TO BS328 AT LBL46 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 141A5400 REV:-. SEE INDIVIDUAL SIGNSOFF BELOW.;[03] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: FLOORBEAM — CORRODED (FWD GALLEY FLOOR) · airframe 60,134 hrs · 35,574 cycles

CORROSION FLOOR BEAM LOCATED BS328 AT RBL19 TO RBL22 AND WL208.1 AT FWD GALLEY AREA 2022-207225. REPAIRED FLOOR BEAM LOCATED BS328 AT LBL6 TO RBL60 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-7 REPAIR 7 ALTERNATIVE 2. THIS REPAIR IS CATEGORY A.

Part: FLOORBEAM — CORRODED (FWD GALLEY FLOOR) · airframe 60,134 hrs · 35,574 cycles

CORROSION FLOOR BEAM LOCATED BS328 AT RBL42 AND WL208.1 AT FWD GALLEY AREA 2022-207223 ; REPAIRED FLOOR BEAM LOCATED BS328 AT LBL 6 TO RBL 60 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-7 REPAIR 7 ALTERNATIVE 2 THIS REPAIR IS CATEGORY A.THIS REPAIR IS DOCUMENTED ON FAULT TTG8Q00C3N3L.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,134 hrs · 35,574 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS344 TO BS360 AT RBL32 FWD GALLEY AND LAV 2022-207219 REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS344 TO BS360 AT RBL32 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 39 AND SRM 51-10-02 PARAGRAPH 9.REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS344 TO BS360 AT RBL32 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 33 AND SRM 51-10-02 PARAGRAPH 9.

Part: FLOORBEAM — CORRODED (AFT GALLEY) · airframe 60,134 hrs · 35,574 cycles

CORROSION ON FLOOR BEAM 986.5 BTW RBL 39 TO RBL 44 AND WL 208.1 AFT GALLEY AREA 2022-207216 / [01] TOOL USED PN:35DL; SN:091419910; DUE DATE:26-JAN-23.;[02] ET TOOL USED: PN: PHASEC 3D; SN: 587435 /03; DUE DATE: 22 -DEC -22;[03] REPAIRED FLOOR BEAM 986.5 BTW RBL 30.00 TO RBL 50.00 AND AT WL 208.1 AFT GALLEY AREA IAW EA 22-153-01411-WIP1 BARCODE (TTG8Q00CEYZ4) AND EA 22-153-01411 BARCODE (TTG8Q00CL5RG) SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPAIRED FLOOR BEAM 986.5 BTW RBL 30.00 TO RBL 50.00 AND AT WL 208.1 AFT GALLEY AREA IAW EA 22-153-01411-WIP1 BARCODE (TTG8Q00CEYZ4) AND EA 22-153-01411 BARCODE (TTG8Q00CL5RG) RII. SEE INDIVIDUAL SIGN OFF BELOW.

Part: STRINGER — CRACKED (PAX CABIN) · airframe 60,134 hrs · 35,574 cycles

CRACK STRINGER BETWEEN BS294.5 TO BS303.9 STR15L AT PASSENGER CABIN 2022-207139 / [01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN:210136503; DUE DATE: 11-APR-23;[02] TOOL MEASUREMENT ULTRASONIC THICKNESS USED P/N: 45MG S/N: 130060401 DUE DATE: 26-JAN-23.;[03] REPAIRED STRINGER BETWEEN BS294.5 TO BS303.9 STR15L AT PASSENGER CABIN IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; THIS REPAIR IS CATEGORY A. NO FURTHER ACTION OR INSPECTION REQUIRED. SEE INDIVIDUAL SIGNOFF BELOW;[04] REPAIRED STRINGER BETWEEN BS294.5 TO BS303.9 STR15L AT PASSENGER CABIN IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; THIS REPAIR IS CATEGORY A. NO FURTHER ACTION OR INSPECTION REQUIRED. SEE INDIVIDUAL SIGNOFF BELOW AS RII

Part: STUB FRAME — CRACKED (PAX CABIN) · airframe 60,134 hrs · 35,574 cycles

CRACK FRAME STUB LOCATED BS 294.5 AND BETWEEN STR8R TO STR9R AT PASSENGER CABIN 2022-207148 / [01] REPLACED FRAME STUB LOCATED BS 294.5 AND BETWEEN STR8R TO STR9R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED FRAME STUB LOCATED BS 294.5 AND BETWEEN STR8R TO STR9R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGNOFF BELOW.. RII ITEM

Part: LIGHT — BROKEN (AFT GALLEY) · airframe 60,134 hrs · 35,574 cycles

BROKEN LAVATORY B ASSY EMERGENCY EXIT LIGHT AT AFT GALLEY AREA 2022-207125 / [01] REPLACED LAVATORY B ASSY EMERGENCY EXIT LIGHT AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-801 P/N 702409DME1007;[02] REPLACED LAVATORY B ASSY EMERGENCY EXIT LIGHT AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-801 P/N 702409DME1007

Part: TIE CLIP — CRACKED (PAX CABIN) · airframe 60,134 hrs · 35,574 cycles

CRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN 2022-207141 / [01] REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A1110 SHEET 18 REV: -. ;[02] REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A1110 SHEET 18 REV: -. SEE INDIVIDUAL SING-OFF BELOW.<BR>RII;[03] CORRECTED STEP 1.REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN IAW SRM B737-700 51-10-02; SRM B737-700 51-40-02 AND DWG 141A1110 SHEET 18 REV: -. ;[04] CORRECTED STEP 2. REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN IAW SRM B737-700 51-10-02; SRM B737-700 51-40-02 AND DWG 141A1110 SHEET 18 REV: -.

Part: BATTERY PACK — INOPERATIVE (PAX CABIN) · airframe 60,134 hrs · 35,574 cycles

INOP EMERGENCY EXIT LIGHT BATTERY BTW BS 597 TO BS 616 LT SIDE AT PASSENGER CABIN (1EA) 2022-207119 / [01] REPLACED EMERGENCY EXIT LIGHT BATTERY BTW BS 597 TO BS 616 LT SIDE AT PASSENGER CABIN; TEST IS OK IAW AMM 33-51-06-960-805.;[02] TASK COMPLETED <BR><BR>TEST OK

Part: WEB — CRACKED (FWD GALLEY) · airframe 60,134 hrs · 35,574 cycles

CRACK WEB INTERCOSTAL LOCATED BETWEEN BS294.5 TO BS303.9 STR16L AT FWD GALLEY AREA 2022-207128 / [01] TOOL USED EDDY CURRENT INSTRUMENT P/N NORTEC500D S/N N500X12101U102020 DUE DATE 01-JUN-22;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 190023010 DUE DATE: 14-FEB-23;[03] REPLACED WEB INTERCOSTAL LOCATED BETWEEN BS294.5 TO BS303.9 STR16L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 141A8180 SHEET 27 REV C. SEE INDIVIDUAL SING-OFFS BELOW.;[04] REPLACED WEB INTERCOSTAL LOCATED BETWEEN BS294.5 TO BS303.9 STR16L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 141A8180 SHEET 27 REV C. SEE INDIVIDUAL SING-OFFS BELOW.<BR>RII

Part: BATTERY PACK — INOPERATIVE (PAX CABIN) · airframe 60,134 hrs · 35,574 cycles

INOP LOWERED CEILING PANEL BATTERY EMERGENCY EXIT LIGHT AT AFT GALLEY AREA (2EA) 2022-207118 / [01] REPLACED BATTERY EMERGENCY EXIT LIGHT AT AFT GALLEY AREA (2EA); TEST IS OK IAW AMM 33-51-06-960-805.;[02] TASK COMPLETED<BR><BR>TEST OK

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 60,134 hrs · 35,574 cycles

CRACK LEADING EDGE SUPPORT ANGLE LOC BTW STR 2RT AND STR 2LT BS 1016 AT VERTICAL STABILIZER 2022-207126 / [01] REPLACED SUPPORT ANGLE (SPRING) LOC. BTW STR 2R AND STR 2L BS 1016 AT VERTICAL STABILIZER IAW: B737-700 SRM 51-40-02 AND DWG 176A3101; SHEET: 4; REV: - AND DWG: 176A3001; SHEET: 23; REV: D. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT ANGLE (SPRING) LOC. BTW STR 2R AND STR 2L BS 1016 AT VERTICAL STABILIZER IAW: B737-700 SRM 51-40-02 AND DWG 176A3101; SHEET: 4; REV: - AND DWG: 176A3001; SHEET: 23; REV: D.RII . SEE INDIVIDUAL SIGN OFF BELOW

Part: STUB FRAME — CRACKED (PAX CABIN) · airframe 60,134 hrs · 35,574 cycles

CRACK STUB FRAME LOCATED 294.5 AT LEVEL STR17R AT PASSENGER CABIN 2022-207142 / [01] REPLACED STUB FRAME LOC. BS 294.5 AT LEVEL STR 15R TO STR 17R AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM:9 AND DWG:141A8370 SHEET:9 REV:D AND DWG:141A8430 SHEET:4 REV:B;[02] CORRECTED STEP 1: REPLACED STUB FRAME LOC. BS 294.5 AT LEVEL STR 15R TO STR 17R AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM:9 AND DWG:141A8370 SHEET:9 REV:D AND DWG:141A8430 SHEET:4 REV:B;[03] REPLACED STUB FRAME LOC. BS 294.5 AT LEVEL STR 15R TO STR 17R AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM:9 AND DWG:141A8370 SHEET:9 REV:D AND DWG:141A8430 SHEET:4 REV:B

Part: BRACKET — CORRODED · airframe 60,134 hrs · 35,574 cycles

RUST ON AFT SERVICE DOOR GIRT BAR FITTING BRACKET AT PASSENGER CABIN (1EA) 2022-207120 / [01] REPLACED ON AFT SERVICE DOOR GIRT BAR FITTING BRACKET AT PASSENGER CABIN (1EA) IAW B737-700 AMM 25-66-02-400-801;[02] REPLACED ON AFT SERVICE DOOR GIRT BAR FITTING BRACKET AT PASSENGER CABIN (1EA) IAW B737-700 AMM 25-66-02-400-801

Part: STRINGER — CRACKED (PAX CABIN) · airframe 60,134 hrs · 35,574 cycles

CRACK STRINGER 16L BETWEEN BS294.5 TO BS303.9 AT PASSENGER CABIN 2022-207127 / REPAIRED STRINGER 16L BETWEEN BS294.5 TO BS303.9 AT PASSENGER CABIN B737-700 SRM 53-00-03-2R-1 REPAIR 1; THIS REPAIR IS CATEGORY A. NO FURTHER ACTION OR INSPECTION REQUIRED. REPAIRED STRINGER 16L BETWEEN BS277 TO BS303.9 AT PASSENGER CABIN IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; THIS REPAIR IS CATEGORY A. NO FURTHER ACTION OR INSPECTION REQUIRED.

Part: FRAME — CRACKED (FWD GALLEY) · airframe 60,134 hrs · 35,574 cycles

CRACK FRAME ON BS 312 AT LEVEL STR6L FWD GALLEY AND LAV 2022-207130 / [01] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 210138203; DUE: 11-APR-23;[02] INSPECTION REJECT IN STEP 12 SEE TTG8Q00CDDUS;[03] REPAIRED FRAME LOC. ON BS 312 AND BTW STR 5L TO STR 6L FWD GALLEY AND LAVATORY IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1 PARAGRAPH 4; FIGURE 203. MATERIAL USED P/N: 7075T0-0.063?; P/O: 2022-124059 1. SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPAIRED FRAME LOC. ON BS 312 AND BTW STR 5L TO STR 6L FWD GALLEY AND LAVATORY IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1 PARAGRAPH 4; FIGURE 203. MATERIAL USED P/N: 7075T0-0.063?; P/O: 2022-124059 1. RII .SEE INDIVIDUAL SIGN OFF BELOW.

Part: PLATE — CRACKED (LH WING) · airframe 60,134 hrs · 35,574 cycles

CRACK CORRUGATED PLATE LOCATED AT LEVEL ORSS261 TRAILING EDGE AT LT WING 2022-207040 / [01] REPLACED CORRUGATED PLATE LOCATED AT LEVEL ORSS261 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-20-01 AND DWG 115A2001-59 SHEET 29 REV -;[02] REPLACED CORRUGATED PLATE LOCATED AT LEVEL ORSS261 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-20-01 AND DWG 115A2001-59 SHEET 29 REV -

Part: ANGLE — CRACKED (LH WING) · airframe 60,134 hrs · 35,574 cycles

CRACK ANGLE LOCATED TRAILING EDGE AT ORSS 271 APPROX LOWER SURFACE AT LT WING 2022-207039 / [01] REPLACED ANGLE AND FASTENERS LOCATED ON TRAILING EDGE AT ORSS 271 APPROX LOWER SURFACE AT LT 2WING IAW B737-700 SRM 51-40-02;[02] CORRECTED STEP 1: REPLACED ANGLE AND FASTENERS LOCATED ON TRAILING EDGE AT ORSS 271 APPROX LOWER SURFACE AT LT WING IAW B737-700 SRM 51-40-02 SRM 51-10-02;[03] CERTIFIED WORK PERFORMED.

Part: ANGLE — CRACKED (RH WING) · airframe 60,134 hrs · 35,574 cycles

CRACK ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 271 RT WING 2022-207017 / [01] REPLACED ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 271 RT WING IAW: B737-700; SRM 51-40-02 AND SRM 51-10-02; ITEM 9; SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 271 RT WING IAW: B737-700; SRM 51-40-02 AND SRM 51-10-02; ITEM 9; SEE INDIVIDUAL SIGN OFF BELOW.

Part: PLATE — CRACKED (RH WING) · airframe 60,134 hrs · 35,574 cycles

CRACK CORRUGATED PLATE LOCATED AT LEVEL ORSS 261 TRAILING LOWER EDGE AT RT WING 2022-207023 / [01] REPLACED CORRUGATED PLATE LOCATED AT LEVEL ORSS 261 TRAILING LOWER EDGE AT RT WING IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 115A2001; SHEET 29; REV -.;[02] TASK COMPLETED

Part: WEB — CRACKED (RH WING) · airframe 60,134 hrs · 35,574 cycles

CRACK WEB LOCATED BETWEEN ORSS 261 AND ORSS 280 TRAILING EDGE AT RT WING 2022-207020 / [01] INSTALLED NEW WEB WITH FASTENERS LOCATED BETWEEN ORSS 261 AND ORSS 280 TRAILING EDGE AT RT WING I.A.W B737-700 SRM 51-40-02 AND DWG 115A2512 REV: A.;[02] CORRECTED STEP 1<BR>REPLACED WEB LOCATED BETWEEN ORSS 261 AND ORSS 280 TRAILING EDGE AT RT WING I.A.W B737-700 SRM 51-10-02 ITEM 9 ; SRM 51-40-02 AND DWG 115A2512 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED WEB LOCATED BETWEEN ORSS 261 AND ORSS 280 TRAILING EDGE AT RT WING I.A.W B737-700 SRM 51-10-02 ITEM 9 ; SRM 51-40-02 AND DWG 115A2512 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.

Part: STRAP — CRACKED (FWD SERVICE DOOR) · airframe 60,134 hrs · 35,574 cycles

CRACK INDICATION ON FWD SERVICE DOOR BEAR STRAP BTW BS 291.5 TO BS 294.5 AT LEVEL S-8R TO S-9R PASSENGER CABIN 2022-207062 PERFORMED REOAIR IWA EA 22-153-01299;[06] PERFORMED PERMANENT REPAIR ON FWD SERVICE DOOR BEAR STRAP BTW BS 291.5 TO BS 294.5 AT LEVEL S-8R TO S-9R PASSENGER CABIN IAW EA 22-153-01299. SEE INDIVIDUAL SIGNS OFF BELOW. RII;[07] PERFORMED PERMANENT REPAIR ON FWD SERVICE DOOR BEAR STRAP BTW BS 291.5 TO BS 294.5 AT LEVEL S-8R TO S-9R PASSENGER CABIN IAW EA 22-153-01299.

Part: ANGLE — CRACKED (LH WING) · airframe 60,134 hrs · 35,574 cycles

CRACK ANGLE LOCATED TRAILING EDGE AT LEVEL ORSS 276 AT LT WING 2022-207038 / [01] REPLACED ANGLE LOCATED TRAILING EDGE AT LEVEL ORSS 276 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9;[02] TASK COMPLETED

Part: ANGLE — CRACKED (LH WING) · airframe 60,134 hrs · 35,574 cycles

CRACK ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 271 UPPER SURFACE LT WING 2022-207037 / [01] REPLACED ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 271 UPPER SURFACE LT WING IAW SRM B737-700 51-10-02 ITEM 9 AND 51-40-02;[02] REPLACED ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 271 UPPER SURFACE LT WING IAW SRM B737-700 51-10-02 ITEM 9 AND 51-40-02

Part: SKIN — CRACKED (RH HOR STAB) · airframe 60,134 hrs · 35,574 cycles

CRACK INDICATIONS FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 10.0 INCH FROM REAR SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.200 INCH 2022-206920 REPAIRED RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 10.0 INCH FROM REAR SPAR; INBD SIDE OF RIB IAW B737-700 SRM 55-10-01-2R-11 REPAIR 11 FIGURE 204 SHEET 2 DETAIL:B AND SRM 51-40-02.THIS REPAIR IS CATEGORY B. CRACK LENGTH IS 1.200 INCH. [03] REPAIRED RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 10.0 INCH FROM REAR SPAR; INBD SIDE OF RIB IAW B737-700 SRM 55-10-01-2R-11 REPAIR 11 FIGURE 204 SHEET 2 DETAIL:B AND SRM 51-40-02.THIS REPAIR IS CATEGORY B. CRACK LENGTH IS 1.200 INCH.

Part: SKIN — CRACKED (LH HOR STAB) · airframe 60,134 hrs · 35,574 cycles

CRACK INDICATIONS FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 18.0 INCH FROM REAR SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.250 INCH 2022-206921 REPAIRED HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 18.0 INCH FROM REAR SPAR; INBD SIDE OF RIB. IAW B37-700 SRM 55-10-01-2R-11 REPAIR 11. THIS REPAIR IS CATEGORY B. SEE INDIVIDUAL SIGNOFF BELOW.;[04] REPAIRED HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 18.0 INCH FROM REAR SPAR; INBD SIDE OF RIB. IAW B37-700 SRM 55-10-01-2R-11 REPAIR 11. THIS REPAIR IS CATEGORY B.

Part: SKIN — CRACKED (LH WING) · airframe 60,134 hrs · 35,574 cycles

CRACK LEADING EDGE SKIN SLAT ACTUATOR 2 AT LT WING 2022-206875 / [01] TOOL EDDY CURRENT USED P/N: NORTEC 600D S/N: 190023010 AND DUE DATE: 14-FEB-23.;[02] TOOL USED RADIUS GAUG P/N: 2204A3 S/N: AE-408652 DUE DATE: 29-JAN-23;[03] REPAIRED LEADING EDGE SKIN SLAT ACTUATOR 2 AT LT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 ALTERNATIVE 1 FIGURE 202. SEE INDIVIDUAL SIGNOFF BELOW.;[04] REPAIRED LEADING EDGE SKIN SLAT ACTUATOR 2 AT LT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 ALTERNATIVE 1 FIGURE 202. SEE INDIVIDUAL SIGNOFF BELOW. COMPLETED RII

Part: STRAP — CRACKED (AFT CARGO BAY) · airframe 60,134 hrs · 35,574 cycles

CRACK ON STRAP LOCATE BTW BS767 TO BS787 AND STR25L TO STR25R AT AFT CARGO COMPARTMENT 2022-206781 REPLACED STRAP LOCATE BTW BS767 TO BS787 AND STR25L TO STR25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG 146A7500-16. P/N: 146A9401-4ATSMRO PO:2022 142949.REPLACED STRAP LOCATE BTW BS767 TO BS787 AND STR25L TO STR25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG 146A7500-16. P/N: 146A9401-4ATSMRO PO:2022 142949.REPLACED STRAP LOCATE BTW BS767 TO BS787 AND STR25L TO STR25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG 146A7500-16. P/N: 146A9401-4ATSMRO PO:2022 142949.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 60,134 hrs · 35,574 cycles

CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2022-206730 / [01] TOOL USED DIGITAL CALIPER P/N 500-196-30; S/N A21033522; DUE DATE 01-NOV-22.;[02] REPAIRED SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGNOFFS BELOW.;[03] REPAIRED SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGNOFFS BELOW.

Part: PANEL — NONE (FUSELAGE) · airframe 59,119 hrs · 34,956 cycles

WING TO BODY PANEL 193D HAD FRETTING DAMAGE ; / [01] R AND R PANEL 193D PER AMM 53-51-21

Part: SEAT TRACK — CORRODED (BS 727A LBL 45) · airframe 58,567 hrs · 34,627 cycles

PASSENGER CABIN SEAT TRACK LBL 45 STA 727A+16.5'' WL 208 HAS CORROSION ON UPPER SURFACE ; / [01] REMOVED CORROSION FROM SEAT TRACJ STA 727A + 16.5' LBL 45. UPPER SURFACE IAW 51-10-02-0G-0; USED 10X MAGNIFYING GLASS.; [02] VERIFIED MATERIAL LOSS STA 727A + 16.5' LBL 45 UPPER SURFACE IAW SRM 53-00-52-1A-1. FOUND TO BE WITHIN LIMITS. DEPTH .016' MAX ALLOWED .020'. AAR TOOL 36307 CAL DUE DATE 06/14/22.; [03] VERIFIED STEPS 1. AND 2.; [04] OK TO RESTORE FINISH.; [05] TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1. COMPLETED ALL STEPS 1-5.; [06] INSPECTION CW.

Part: SEAT TRACK — CORRODED (BS 727A LBL 45) · airframe 58,567 hrs · 34,627 cycles

PASSENGER CABIN SEAT TRACK LBL 45 STA 727A+12'' WL 208 HAS CORROSION ON LOWER SURFACE<REMOVED CORROSION AT SEAT TRACK STA 727A+12 UPPER AND LOWER SURFACES AND PERFORMED 10X MAGNIFYING GLASS I/A/W SRM 51-10-02-0G-0 VERIFIED MATERIAL LOSS AT SEAT TRACK AT STA 727A+12 LBL 45 ON BOTTOM OF SEAT TRACK LOSS OF .023 MAXIMUM LOSS IS .040 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22 VERIFIED MATERIAL AT SEAT TRACK STA 727A+12 LBL45 LOSS OF .010 ON UPPER SURFACES MAXIMUM IS .020 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22 VERIFIED STEPS 1. THRU 3. OK TO RESTORE FINISH. TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1.

Part: SEAT TRACK — CORRODED (BS 727A LBL 24) · airframe 58,567 hrs · 34,627 cycles

PASSENGER CABIN SEAT TRACK LBL 24 STA 727A+13' WL 208 HAS CORROSION ON LOWER SURFACE ; / [01] REMOVED CORROSION AT SEAT TRACK LBL24 STA 727A+ 13 WL208 AND PERFORM 10 X MAGNIFYING GLASS I/A/W SRM 51-10-02-0G-0; [02] VERIFIED MATERIAL LOSS AT SEAT TRACK STA 727A +13 LOSS ON .018 MAXIMUM CLEANUP IS .040 ON BOTTOM OF SEAT TRACK IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22; [03] VERIFIED STEPS 1. AND 2.; [04] OK TO RESTORE FINISH.; [05] TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1. COMPLETED ALL STEPS 1-6.; [06] INSPECTION CW.

Part: SEAT TRACK — CORRODED (BS 727C LBL 45) · airframe 58,567 hrs · 34,627 cycles

PASSENGER CABIN SEAT TRACK LBL 45 STA 727C+4' WL 208 HAS CORROSION ON LOWER SURFACE<REMOVED CORROSION FROM SEAT TRACK STA 727C + 4' LOWER SURFACE IAW SRM 51-40-02-0G-0. USED 10X MAGNIFICATION GLASS. VERIFIED MATERIAL LOSS ON SEAT TRACK STA 727C + 4' LBL 45 ON LOWER SURFACE IAW SRM 53-00-52-1A-1. DEPTH .02' MAX ALLOWWED .040'. AAR TOOL 36307 CAL DATE DUE 06/14/22. VERIFIED STEPS 1. AND 2. OK TO RESTORE FINISH. TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1.

Part: SEAT TRACK — CORRODED (BS 685 LBL 45) · airframe 58,567 hrs · 34,627 cycles

PASSENGER CABIN SEAT TRACK LBL 45 STA 685+41' WL 208 HAS CORROSION ON UPPER AND LOWER SURFACE ; / [01] REMOVED CORROSION AT SEAT TRACK 685+41 LBL45 AND PERFORMED 10X MAGNIFYING GLASS I/A/W SRM 51-10-02-0G-0; [02] VERIFIED MATERIAL AT SEAT TRACK STA 685+41 LBL45 <BR>ON BOTTOM OF TRACK LOSS OF .024 MAXIMUM IS .040 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06\14\22; [03] VERIFIED MATERIAL AT SEAT TRACK STA 685+41 ON UPPER SURFACES LBL45 LOSS OF .008 MAXIMUM IS .020 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22; [04] VERIFIED STEPS 1. THRU 3.; [05] OK TO RESTORE FINISH.; [06] TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1.

Part: SEAT TRACK — CORRODED (BS 685 LBL 24) · airframe 58,567 hrs · 34,627 cycles

PASSENGER CABIN SEAT TRACK LBL 24 STA 685 WL 208 HAS CORROSION ON UPPER AND LOWER SURFACE<REMOVED CORROSION AT LBL24 STA 685 WL 208 AT UPPER AND LOWER SURFACE AND CHECKED WITH 10X MAG IAW SRM 51-10-02-0G-0 MATERIAL. LOSS AT LBL 24 STA 685 WL 208 AT CROWN IS.014 AND LOWER BOTTOM IS .024 WITHIN LIMITS IAW SRM 53-00-52-1A-1 LOSS AT LBL 24 STA 685 WL 208 AT CROWN IS .014 MAX ALLOWABLE IS .020 WITHIN LIMITS IAW SRM 53-00-52-1A-1. LOSS AT LBL 24 STA685 WL 208 AT SEAT TRACK BOTTOM IS .024 MAX ALLOWABLE IS .040 WITHIN LIMITS IAW SRM 53-00-52-1A-1 TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1.

Part: SEAT TRACK — CORRODED (BS 685 LBL 45) · airframe 58,567 hrs · 34,627 cycles

PASSENGER CABIN SEAT TRACK LBL 45 STA 685 WL 208 HAS CORROSION ON UPPER AND LOWER SURFACE<REMOVED CORROSION AT SEAT TRACK LBL45 STA 685 AND PERFORMED 10X MAGNIFYING. GLASS I/A/W SRM 51-10-02-0G-0 VERIFIED MATERIALS LOSS AT SEAT TRACK STA 685 LBL45 ON BOTTOM OF SEAT TRACK LOSS OF .017 MAXIMUM CLEAN UP IS .040 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22 VERIFIED MATERIAL LOSS AT SEAT TRACK 685 LBL 45 UPPER SEAT TRACK LOSS OF .018 MAXIMUM CLEANUP IS .020 IS WITH IN LIMITS I/A/W SRM 53-00-52-1A-1. OK TO RESTORE FINISH. TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1.

Part: SEAT TRACK — CORRODED (BS 616 LBL 24) · airframe 58,567 hrs · 34,627 cycles

PASSENGER CABIN SEAT TRACK LBL 24 STA 616+17' WL 208 HAS CORROSION ON UPPER AND LOWER SURFACE<REMOVED CORROSION AT SEAT TRACK STA 616+17 LBL 24 UPPER AND LOWER SURFACE AND PERFORMED 10X MAGNIFYING GLASS I/A/W SRM 51-10-02-0G-0 VERIFIED MATERIAL LOSS AT STA 616+17 LBL24 ON UPPER SURFACES OF SEAT TRACK LOSS OF .011 MAXIMUM IS .020 IS WITHIN LIMITS IAW SRM 53-00-52-1A-1. VERIFIED MATERIAL LOSS ON SEAT TRACK SEA 616+17 LBL24 LOSS OF .015 MAXIMUM. IS .040 ON BOTTOM OF SEAT TRACK IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22 VERIFIED STEPS 1. THRU 3. OK TO RESTORE FINISH. TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1.

Part: SEAT TRACK — CORRODED (BS 639 LBL24) · airframe 58,567 hrs · 34,627 cycles

PASSENGER CABIN SEAT TRACK LBL 24 STA 639+23' WL 208 HAS CORROSION ON UPPER AND LOWER SURFACE<REMOVED CORROSION AT SEAT TRACK STA 639+23 LBL24 ON UPPER AND LOWER SURFACES AND PERFORMED 10X MAGNIFYING GLASS I/A/W SRM 51-10-02-0G-0 VERIFIED MATERIAL LOSS AT SEAT TRACK AT STA 639+23 LBL 24 ON UPPER SURFACES LOSS OF .010 MAXIMUM IS .020 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22 VERIFIED MATERIAL LOSS AT LOWER SURFACES OF SEAT TRACK LOSS OF .015 MAXIMUM LOSS IS .040 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22 VERIFIED STEPS 1. THRU 3. OK TO RESTORE FINISH. TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1.

Part: SEAT TRACK — CORRODED (BS 663 LBL 45) · airframe 58,567 hrs · 34,627 cycles

PASSENGER CABIN SEAT TRACK LBL 45 STA 663 WL 208 HAS CORROSION ON UPPER AND LOWER SURFACE<REMOVED CORROSION AT SEATTRACK LBL45 STA 663 WL208 AND PERFORMED 10X MAGNIFYING GLASS I/A/W ARM 51-10-02-0G-0 0N UPPER AND LOWER SURFACE VERIFIED MATERIAL LOSS ON SEAT TRACK STA 663 LBL 45 UPPER SURFACE OF TRACK LOSS OF .008 MAXIMUM CLEAN UP IS .020 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 VERIFIED MATERIAL LOSS AT STA 663 LBL45 ON LOWER SURFACE OF SEAT TRACK LOSS OF MATERIAL IS .012 MAXIMUM CLEAN UP IS .040 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22 VERIFIED STEPS 1. THRU 3. OK TO RESTORE FINISH. TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1.

Part: SEAT TRACK — CORRODED (BS 685 LBL 24) · airframe 58,567 hrs · 34,627 cycles

PASSENGER CABIN SEAT TRACK LBL 24 STA 685+41' WL 208 HAS CORROSION ON UPPER AND LOWER SURFACE<REMOVED CORROSION ON UPPER AND LOWER SURFACES OF SEAT TRACK STA 685+41 LBL24 AND PERFORMED 10X MAGNIFYING GLASS I/A/W SRM 51-10-02-0G-0 VERIFIED MATERIAL LOSS AT SEAT TRACK STA 685+41 LBL 24 ON BOTTOM OF SEAT TRACK LOSS OF .015 MAXIMUM LOSS IS .040 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22 VERIFIED MATERIAL ON UPPER SURFACE OF SEAT TRACK LOSS OF .012 MAXIMUM CLEANUP IS .020 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE VERIFIED STEPS 1. THRU 3. OK TO RESTORE FINISH. TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1.

Part: SEAT TRACK — CORRODED (BS 616 LBL 45) · airframe 58,567 hrs · 34,627 cycles

PASSENGER CABIN SEAT TRACK LBL 45 STA 616+19' WL 208 HAS CORROSION ON UPPER AND LOWER SURFACE<REMOVED CORROSION. AT SEAT TRACK STA 616+19 LBL45 UPPER AND LOWER SURFACES AND PERFORMED 10X MAGNIFYING GLASS I/A/W SRM 51-10-02-OG-0 VERIFIED MATERIALS LOSS AT SEAT TRACK 616+19 LBL 45 LOSS OF .018 ON BOTTOM OF SEAT TRACK MAXIMUM LOSS IS .040 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22 VERIFIED MATERIAL LOSS ON SEAT TRACK STA 616 +19 LBL 45 ON UPPER SURFACES LOSS OF .011 MAXIMUM IS .020 IS WITHIN LIMITS I/A/W SRM 53-00-52-1A-1 AAR TOOL 36307 DUE 06-14-22 VERIFIED STEPS 1. THRU 3. OK TO RESTORE FINISH. TREATED AND PRIMED SEAT TRACK IAW SRM 53-00-52 -1A-1.

Part: ATTACH ANGLE — CRACKED (BS 663 BULHEAD) · airframe 58,567 hrs · 34,627 cycles

BS 663 LOWER CHORD COMMON TO FUEL TANK CRACKED AT RBL 8, CUT & REMOVED ATTACH ANGLE IAW SRM 57-10-10-2R-5 REPAIR 5. PERFORMED DVI OF REPAIR AREA & UNDERLYING STRUCTURE. NO DEFECTS IAW SRM 57-10-10-2R-5. HFEC IAW NDT PART 6 51-00-00 PROC 16. NO DEFECTS. FABRICATED REPAIR PARTS IAW SRM 57-10-10-2R-5, REPAIR 5. TREATED AND PRIMED REPAIR PARTS & CUT EDGE IAW SRM 57-10-10-2R-5 REPAIR 5. INSTALLED REPAIR PARTS IAW SRM 57-10-10-2R-5 REPAIR 5. BONDING CHECKED GOOD. APPLIED CIC TO REPAIR AREA IAW SRM 57-10-10-2R-5 REPAIR 5. PERFORMED LEAK CHECK IAW AMM 28-11-00-400-801. NO LEAKS.

Part: ATTACH ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 58,567 hrs · 34,627 cycles

FOUND CRACK INDICATION IN A/C BAY AT STA 663 VAPOR BARRIER ATTACH ANGLE LBL 10<CUT AND REMOVED ATTACH ANGLE IAW SRM 57-10-10-2R-5 REPAIR 5 FIG 202. PERFORMED DVI OF REPAIR AREA & UNDERLYING STRUCTURE. NO DEFECTS IAW SRM 57-10-10-2R-5, REPAIR 5. HFEC IAW NDT PART 6 51-00-00 PROC 16. NO DEFECTS. FABRICATED REPAIR PARTS IAW SRM 57-10-10-2R-5 REPAIR 5. TREATED & PRIMED REPAIR PARTS & CUT EDGE IAW SRM 57-10-10-2R-5 REPAIR 5. INSTALLED REPAIR PARTS IAW SRM 57-10-10-2R-5 REPAIR 5. BONDING CHECKS GOOD. APPLIED CIC TO REPAIR AREA IAW SRM 57-10-10-2R-5 REPAIR 5. LEAK CHECK IAW 28-11-00-400-801 NO LEAKS.

Part: HMU — FAULTY (#2 ENGINE) · airframe 58,230 hrs · 34,446 cycles

NUMBER 2 ENG .N-1 4% LOWER THAN #1 .WOULD NOT ATTAIN FULL CLIMB POWER ; NUMBER 2 ENG. N-1 ;4% LOWER THAN #1 WOULD NOT ATTAIN FULL CLIMB POWER / [01] REF W/O 13684334 LINE #11 TASK CARD 773-11-00 HAS BEEN C/W FUEL PUMP AND HMU WERE REPLACED WITH THIS TASK CARD. RAN END TO T/O POWER NO DEFECTS NOTED

Part: PUMP — FAULTY (RIGHT) · airframe 58,230 hrs · 34,446 cycles

NUMBER 2 ENG .N-1 4% LOWER THAN #1 .WOULD NOT ATTAIN FULL CLIMB POWER ; NUMBER 2 ENG. N-1 ;4% LOWER THAN #1 WOULD NOT ATTAIN FULL CLIMB POWER / [01] REF W/O 13684334 LINE #11 TASK CARD 773-11-00 HAS BEEN C/W FUEL PUMP AND HMU WERE REPLACED WITH THIS TASK CARD. RAN END TO T/O POWER NO DEFECTS NOTED

Part: CONTROL UNIT — FAULTED (E&E BAY) · airframe 57,216 hrs · 33,865 cycles

ON TAKEOFF REJECTED TO @ 92 KNTS DUE TO VERY STRONG INTENSITY BURNING ELECTRICAL SMELL. F/A'S SAID THEY SMELLED IT FROM ROW 3 FWD TORNADO FLT DECK / PERFORMED CONDITIONAL INSPECTION AS PER AMM 05-51-56 AND FIM 21-00 TASK 806 R/R BPCU PRECAUTIONARY L/P 0567667 R/R FWD GALLEY COFFEE MAKER PRECAUTIONARY AS PER AMM 25-30-01 IN FWD GALLEY NO OTHER ISSUES OR DEFECTS WERE FOUND AT THIS TIME RAR 93185

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 57,216 hrs · 33,865 cycles

ON TAKEOFF REJECTED TO @ 92 KNTS DUE TO VERY STRONG INTENSITY BURNING ELECTRICAL SMELL. F/A'S SAID THEY SMELLED IT FROM ROW 3 FWD TORNADO FLT DECK / PERFORMED CONDITIONAL INSPECTION AS PER AMM 05-51-56 AND FIM 21-00 TASK 806 R/R BPCU PRECAUTIONARY L/P 0567667 R/R FWD GALLEY COFFEE MAKER PRECAUTIONARY AS PER AMM 25-30-01 IN FWD GALLEY NO OTHER ISSUES OR DEFECTS WERE FOUND AT THIS TIME RAR 93185

Part: LENS — INCORRECT (R/H OVERWING) · airframe 56,912 hrs · 33,695 cycles

RT OW EMERGENCY EXIT LOWER LENSE INCORRECT. INSTALLED CURRENT RT OW EMERGENCY EXIT LOWER LENSE COVER PER 33-51-01.

Part: LAMP — MISSING (EMERGENCYLIGHT) · airframe 56,912 hrs · 33,695 cycles

RIGHT OW EXIT LOWER EMER EXIT SIGN LENSE IS MISSING. INSTALLED EMERG LIGHT LAMP PER AMM 33-51-01. OPS CHECK NORMAL.

Part: COVER — LOOSE (EMERGENCY SIGN) · airframe 56,575 hrs · 33,492 cycles

'EXIT/SALIDA' LIGHT COVER NEAR FWD GALLEY DOOR POPPED OFF, WILL NOT STAY ON. INSTALLED NEW EXIT LIGHT COVER, PER AMM 33-51-02.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 55,206 hrs · 32,646 cycles

CRACK LEADING EDGE RIB AT LE STA 105.26 RT HORIZONTAL STAB / REPLACED LEADING EDGE RIB AT LE STA 105.26 RT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 186A1001 REV B

Part: LATCH — BROKEN (A/C DOOR) · airframe 55,206 hrs · 32,646 cycles

BROKEN PRESSURE ACCESS DOOR 192DR LATCH BOLT AT AIR CONDITIONING BAY (1 EA) / REPLACED LATCH PRESSURE ACCESS DOOR 192DR AT AIR CONDITIONING BAY (1E/A) I.A.W B737-700 51-40-02 AND SRM B737-700 51-10-02 PARAGRAPH 9

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,206 hrs · 32,646 cycles

INOP EMERGENCY LIGHT BATERRY PACKS M1672 AND M1668 AT PASSENGER CABIN (2 EA) / REPLACED EMERGENCY LIGHT BATTERY PACKS M1672 AND M1668 AT PASSENGER CABIN (2EA) IAW B737-700 AMM 33-51-06-960-805 (U008)

Part: SUPPORT — CRACKED (LT WING) · airframe 55,206 hrs · 32,646 cycles

CRACK TRAILING EDGE SUPPORT STRUCTURE AT LEVEL ORSS 297 AT LT WING (1EA) / REPLACED SUPPORT STRUCTURE AT LEVEL ORSS 297 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG #115A3712 REV.A

Part: LENS — CRACKED (CABIN) · airframe 55,206 hrs · 32,646 cycles

CRACK ON EXIT LIGHT LENS ON HEADER PANEL RH AT AFT GALLEY AREA (1 EA) / REPLACED EXIT LIGHT ON HEADER PANEL RH AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-801

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK ANGLE - SUPPORT LOCATED AT BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT / REPLACED ANGLE SUPPORT LOCATED AT BS867 AT LEVEL STR.26L AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 ITEM 9; 51-40-02 AND DWG #149A8102 REV.-

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS 727C TO BS 787 AT LEVEL STR 25L AND LBL 22 AT AFT CARGO COMPARTMENT WL 152.8 / PERFORMED REPAIR ON SUPPER ZEE LOCATED FROM BS 727 TO BS 807 AT LEVEL STR 25L LBL 22 AND WL 152.8 AFT CARGO COMPARMENT IAW B737-700 SRM 53-00-53-2R-6 REPAIR 6 AND DRAWING #146A1500

Part: BRACKET — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK BRACKET LOCATED AT BS 727 BTW STR 27R TO STR 27L AT AFT CARGO COMPARTMENT / REPLACED BRACKET LOCATED AT BS727 BTW STR 27R TO STR 27L AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG #144A2600 SHEET 486 REV A AND SRM 51-10-02

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS 727D TO BS 767 AT LEVEL STR 25R AND RBL 22 AT AFT CARGO COMPARTMENT WL 152.8 / REPLACED SUPPORT ZEE SECTION LOCATED BETWEEN BS 727 TO BSJ767 AT LEVEL STR 25RH RBC 22 AND WL 152.8 AFT CARGO COMPARTMENT IAW SRM 737-700 51-10-02 PARAGRAPH 9 AND DRAWING # 146A7500 REV

Part: WEB — CORRODED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CORROSION INTERNAL STRUCTURE WEB LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 27R AND RBL 5 AT AFT CARGO COMPARTMENT WL 152.8 / REPLACED INTERNAL STRUCTURE WEB LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 27R AND RBL 5 AT AFT CARGO COMPARTMENT WL 152.8 IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 146A8130 REV B.

Part: STIFFENER — DAMAGED (BS 907) · airframe 55,206 hrs · 32,646 cycles

ELONGATED HOLE INTERNAL STRUCTURE VERTICAL STIFFENER AT BS 907 AT AFT CARGO COMPARTMENT / REPLACED VERTICAL STIFFENER AT BS 907 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-10-02 PARAGRAPH 9.

Part: STRAP — CORRODED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CORROSION INTERNAL STRUCTURE STRAP AT BS 887 BTW STR 25R TO STR 27L BT W RBL 21 TO LBL 9 AT AFT CARGO COMPARTMENT / REPLACED INTERNAL STRUCTURE STRAP AT BS 887 BTW STR 25R TO STR 27L BTW RBL 21 TO LBL 9 AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-40-02; SRM 51-10-02 PARAGRAPH DRAWING # 146A7500- SHEET 61; REV -

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK INDICATION ON FRAME AROUND FASTENER HOLE COMMON TO SUPPORT BRACKET BS 500C BTW STR 8R AND STR 9R AT PASSENGER CABIN / REPAIRED FRAME LOCATED AT BS 500C BTW STR8R AND STR9R AT PASSENGER CABIN IAW EA N.1-A53-12114 REV 4

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK INDICATION ON FRAME AROUND FASTENER HOLE COMON TO SUPPORT BRACKET AT BS 400 BTW STR8L AND STR9L AT PASSENGER CABIN ( / PERFORMED PERMANENT REPAIR ON FRAME BS 400 BTW STR 8L AND STR 9L IAW EA #1-A53-12114 RVE 4

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK INDICATION ON FRAME AROUND INBOARD FASTERNER HOLE COMMON TO SUPPORT BRACKET AT BS 440 BTW STR 8L AND STR 9L AT PASSENGER CABIN / PERFORMED PERMANENT REPAIR ON FRAME BS 440 BTW S-8L TO S-9L IAW EA # 1-A53-12114 REV 4

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK INDICATION ON FRAME AROUND FASTENER HOLE COMMON TO SUPPORT BRACK ET BS 500A BTW STR 8R AND STR 9R AT PASSENGER CABIN / REPAIRED FRAME BST 500A BETWEEN STR 8 AND STR 9RH SIDE AT PASSENGER CABIN IAW EA#1-A53-12114 REV 4

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK INDICATION ON FRAME AROUND FASTERNER HOLE COMMON TO SUPPORT BRACKET AT BS 727B BTW STR 8L AND STR 9L AT PASSENGER CABIN / PERFORMED PERMANENT REPAIR ON FRAME LOC ON BS 727B BTW STR 8L TO STR 9L AT PASSENGER CABIN IAW EA #1-A53-12114 REV #4

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK ANGLE - CLIP LOCATED FWD FACE OF BS 500B AND STRINGER 26L AT FWD CARGO COMPARTMENT / REPLACED ANGLE-CLIP LOCATED FWD FACE OF BS 500B AND STRINGER 26L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505 REV 'B' (U031)

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK INDICATION ON FRAME AROUND FASTENER HOLE COMMON TO SUPPORT BRACK ET BS 440 BTW STR 8R AND STR 9R AT PASSENGER CABIN (1 EA) / REPAIRED FRAME BST 440 BETWEEN STR 8 AND STR 9 RH SIDE AT PASSENGER CABIN IAW EA #1-A53-12114 REV 4

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK INDICATION ON FRAME AROUND FASTENER HOLE COMMON TO SUPPORT BRACKET BS 360 BTW STR 8R AND STR 9R AT PASSENGER CABIN (1 EA) / REPAIRED FRAME BST 360 BETWEEN STR 8 AND STR 9RH SIDE AT PASSENGER CABIN IAW EA#1-A53-12114 REV 4

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK INDICATION ON FRAME AROUND INBOARD FASTENER HOLE COMMON TO SUPORT BRACKET AT BS 827 BTW STR8L AND STR9L AT PASSENGER CABIN / PERFORMED PERMANENT REPAIR ON FRAME LOC ON BS 827 BTW STR 8L TO STR 9L AT PASSENGER CABIN IAW EA #1-A53-12114 REV 4

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK ANGLE - CLIP LOCATED BS 400 AND STRINGER 26R FWD CARGO COMPARTMENT / REPLACED ANGLE - CLIP LOCATED BS400 AND STRINGER 26R FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG 143A7505 REV 'B'

Part: ANGLE — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK ANGLE - CLIP LOCATED ON BS 400 AND STRINGER 26L FWD CARGO COMPARTMENT / REPLACED ANGLE-CLIP LOC ON BS 400 AND STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM '9' AND DWG 143A7505 SHEET 2 REV B (U131)

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK INDICATION ON FRAME AROUND FASTENER HOLE COMMON TO SUPPORT BRACK ET BS 480 BTW STR 8R AND STR 9R AT PASSENGER CABIN / REPAIRED FRAME BST 480 BETWEEN STR 8 AND STR 9RH SIDE AT PASSENGER CABIN IAW EA#1-A53-12114 REV 4

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK INDICATION ON FRAME AROUND INBOARD FASTENER HOLE COMMON TO SUPORT BRACKET AT BS 787 BTW STR8L AND STR9L AT PASSENGER CABIN / PERFORMED PERMANENT REPAIR ON FRAME BS 787 BTW S-8L TO S-9L IAW EA # 1-A53-12114 REV 4

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK SUPPORT ANGLE LOCATED AT BS693 AT BL0 FLOOR STRUCTURE (2E/A) AT PASSENGER CABIN / REPLACED SUPPORT ANGLE (2E/A) LOCATED AT BS 693 AT BL0 FLOOR STRUCTURE AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 273A9111 REV. 'B'

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK INDICATION ON FRAME AROUND FASTENER HOLE COMMON TO SUPPORT BRACK ET BS 827 BTW STR 8R STR 9R AT PASSENGER CABIN / REPAIRED FRAME BST 827 BETWEEN STR 8 AND STR 9 RH SIDE AT PASSENGER CABIN IAW EA#1-A53-12114 REV 4

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK SUPPORT ANGLE LOCATED AT BS540 BETWEEN RBL24.5 TO LBL24.5 (2E/A) CENTER SECTION / REPLACED SUPPORT ANGLE LOCATED AT BS 540 BETWEEN RBL 24.5 TO LBL 24.5 (2EA) IAW B737-700 SRM 51-40-02 AND DWG 143A0060 REV 'B'

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK INDICATION ON FRAME AROUND FASTERNER HOLE COMMON TO SUPPORT BRACKET AT BS 500C BTW STR 8L AND STR 9L AT PASSENGER CABIN / REPAIRED FRAME LOCATED AT BS500C BETWEEN STR 8L AND STR9L AT PASSENGER CABIN IAW EA N. 1-A53-12114 REV 4

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK INDICATION ON FRAME AROUND INBOARD FASTENER HOLE COMMON TO SUPORT BRACKET AT BS 747 BTW STR8L AND STR9L AT PASSENGER CABIN / PERFORMED PERMANENT REPAIR ON FRAME BS 747 BTW S-8L TO S-9L IAW EA #1-A53-12114 REV.4

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK INDICATION ON FRAME AROUND FASTENER HOLE COMMON TO SUPPORT BRACKET BS 747 BTW STR 8R AND STR 9R AT PASSENGER CABIN / REPAIRED FRAME BST 747 BETWEEN STR 8 AND STR 9RH SIDE AT PASSENGER CABIN IAW EA#1-A53-12114 REV 4

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK INDICATION ON FRAME AROUND FASTENER HOLE COMMON TO SUPPORT BRACKET BS 727D BTW STR 8R AND STR 9R AT PASSENGER CABIN / REPAIRED FRAME BST 727D BETWEEN STR 8 AND STR 9RH SIDE AT PASSENGER CABIN IAW EA#1-A53-12114 REV 4

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK INDICATION ON FRAME AROUND INBOARD FASTENER HOLE COMMON TO SUPORT BRACKET AT BS 727D BTW STR8L AND STR9L AT PASSENGER CABIN / PERFORMED PERMANENT REPAIR ON FRAME BS 7270 BTW STR 8L TO STR 9L IAW EA #1-A53-12114 REV 4

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK INDICATION ON FRAME AROUND INBOARD FASTERNER HOLE COMMON TO SUPPORT BRACKET AT BS 867 BTW STR 8L AND STR 9L AT PASSENGER CABIN / PERFORMED PERMANENT REPAIR ON FRAME LOC ON BS 867 BTW STR 8L TO STR 9L AT PASSENGER CABIN IAW EA #1-A53-12114 REV 4

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK INDICATION ON FRAME AROUND FASTENER HOLE COMMON TO SUPPORT BRACK ET BS 787 BTW STR 8R AND STR 9R AT PASSENGER CABIN / REPAIRED FRAME BST 787 BETWEEN STR 8 AND STR 9RH SIDE AT PASSENGER CABIN IAW EA#1-A53-12114 REV 4

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK INDICATION ON FRAME AROUND FASTERNER HOLE COMMON TO SUPPORT BRACKET AT BS 500A BTW STR 8L AND STR 9L AT PASSENGER CABIN / PERFORMED PERMANENT REPAIR ON FRAME BS 500A BTW S-8L AND S-9L IAW EA # 1-A53-12114 REV 4

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK INDICATION ON FRAME AROUND INBOARD FASTERNER HOLE COMMON TO SUPPORT BRACKET AT BS 520 BTW STR 8L AND STR 9L AT PASSENGER CABIN / REPAIRED FRAME LOCATED AT BS 520 BTW STR8L AND STR9L AT PASSENGER CABIN IAW EA N. 1-A53-12114 REV 4

Part: GUSSET — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK GUSSET LOCATED ON BS 500D AND STRINGER 19R FWD CARGO COMPARTMENT / REPLACED GUSSET LOCATED ON BS 500D AND STRINGER 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DRAWING 143A7902 REV -

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK INDICATION ON FRAME AROUND FASTENER HOLE COMMON TO SUPPORT BRACK ET BS 400 BTW STR 8R AND STR 9R AT PASSENGER CABIN (1 EA) / REPAIRED FRAME BST 400 BETWEEN STR 8 AND STR 9RH SIDE AT PASSENGER CABIN IAW EA#1-A53-12114 REV 4

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CRACK INDICATION ON FRAME AROUND INBOARD FASTERNER HOLE COMMON TO SUPPORT BRACKET AT BS 480 BTW STR 8L AND STR 9L AT PASSENGER CABIN / PERFORMED PERMANENT REPAIR ON FRAME BS 480 BTW STR 8L TO STR 9L IAW EA #1-A53-12-114 REV 4

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 55,206 hrs · 32,646 cycles

CORROSION FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT / REPLACED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND DRAWING 453A2610 REV E

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 55,206 hrs · 32,646 cycles

CRACK FRONT SPAR INSPAR RIB LOCATED STA 120.30 STIFFENER 3 RT HORIZONTAL STAB / PERFORMED PERMANENT REPAIR LOCATED FRONT SPAR INSPAR RIB LOCATED STA 120.30 STIFFENER 3 RT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5. THIS REPAIR IS CATEGORY A

Part: ACCESS DOOR — CORRODED (LOWER FUSELAGE) · airframe 55,206 hrs · 32,646 cycles

CORROSION ACCESS DOOR 311BL INTERNAL LOCATED ON 4 INCH LOWER EDGE; 9 INCH AFT EDGE AND 13 INCH UPPER EDGE AT LOWER FUSELAGE / REPLACED ACCESS DOOR 311BL AFT LOWER FUSELAGE IAW AMM B737-700 52-49-11-400-802 AND SRM B737-700 51-10-02 ITEM 9

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 55,206 hrs · 32,646 cycles

CRACK INSPAR RIB STAB STA 120.30 AND 15.5 INCH FROM FRONT SPAR LT HORIZONTAL STAB / PERFORMED PERMANENT REPAIR ON INSPAR RIB STAB STA 120.30 AND 15.5 INCH FROM FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 55,206 hrs · 32,646 cycles

CRACK INSPAR RIB STAB STA 120.30 AND 26 INCH FROM FRONT SPAR LT HORIZONTAL STAB / REPAIRED INSPAR RIB STAB STA 120.30 AND 26 INCH FROM FRONT SPAR LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R REPAIR 5. THIS REPAIR IS CATEGORY A

Part: SKIN — CRACKED (LE SLAT) · airframe 55,206 hrs · 32,646 cycles

CRACK LEADING EDGE SKIN SLAT 5 AT THE ACTUATOR RIB AT RT WING (1 EA) / REMOVED AND REPLACED SLAT 5 RT WING DUE TO CRACKS ON REPAIR AREA ARE NOT PERMITED. I.A.W B737-700 AMM 27-81-21-400-801 AND AMM 27-81-00-820-803 POS:5 TAG/GRB: 619101 P/N OFF:114A5040-A S/N OFF:001553 P/N ON: 114A5040-A S/N ON:001531

Part: FLOOR PANEL — ELONGATED (FWD CARGO) · airframe 55,206 hrs · 32,646 cycles

ELONGATED HOLE FLOOR PANEL 120CF AT FWD CARGO COMPARTMENT / REPLACED FLOOR PANEL #120CF AT FWD CARGO COMPARTMENT I.A.W. AMM B737-700 25-52-01-201-801 AND DRAWING #453A1610 REV. D DUE TO ALLOWABLE DAMAGE NOT FOUND FOR ELONGATED HOLE NEW PANEL FABRICATED FROM 0.090' CANOLITE P.O. #2020-138497

Part: SKIN — CRACKED (LE SLAT) · airframe 55,206 hrs · 32,646 cycles

CRACK LEADING EDGE SKIN SLAT 3 AT THE ACTUATOR RIB AT LT WING (1 EA) / PERFORMED PERMANENT REPAIR ON SKIN SLAT 3 IAW EA #20-157-00416 REV IR EA #57-0376-20 REV #0

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 55,206 hrs · 32,646 cycles

CRACK SEAL - PLATE ACCESS PANEL 333AB AT LT HORIZONTAL STAB / REPLACED SEAL PLATE ON ACCESS PANEL 333AB AT LT HORIZONTAL STAB. I.A.W B737-700 SRM 51-10-02- 0G-0 ITEM 9 AND SRM 51-40-02

Part: PLATE — CORRODED (FWD CARGO) · airframe 55,206 hrs · 32,646 cycles

CORROSION BILGE AREA PLATE BS 787 RBL 25 FWD CARGO COMPARTMENT (1 EA) / REPLACED PLATE LOCATED BILGE AREA BS 787 RBL 25 FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 REV C DRAWING 453A2611

Part: ANGLE — CORRODED (BS 460) · airframe 54,011 hrs · 31,895 cycles

UPPER CARGO DOOR SILL CLIP CORRODED AT BS. 460, RBL 66. / REPAIRED CLIP PER EA & ER.

Part: DOOR FRAME — CORRODED (BS 460) · airframe 54,011 hrs · 31,895 cycles

FORWARD CARGO DOOR UPPER DOOR FRAME WEB CORRODED AT BS. 460, STR. 19R. / REPAIRED WEB PER EA & ER.

Part: SIGN — BROKEN (CABIN) · airframe 54,011 hrs · 31,895 cycles

OVERHEAD EMERGENCY EXIT SIGN BROKEN. / R&R EXIT SIGN HOUSING PER MM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 53,835 hrs · 31,782 cycles

FORWARD GALLEY EMERGENCY FLASH LIGHT POS #1 SAFETY STRAP BROKEN. / R&R STRAP IAW AMM.

Part: PANEL — OUT OF TOLERANCE (LOWER EXT FUSELA) · airframe 53,238 hrs · 31,374 cycles

193B PANEL HOLES OUT OF LIMITS / REMOVED AND REPLACED 193B PANEL REF AMM 53-51-21.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 53,231 hrs · 31,367 cycles

R1 DOOR EMERGENCY ESCAPE SLIDE CAME LOOSE. R&R SLIDE PER MT.

Part: ESCAPE ROPE — OUT OF ADJUST (COCKPIT) · airframe 53,179 hrs · 31,337 cycles

CAPTAIN'S ESCAPE ROPE DOOR OUT OF ADJUST. ADJUSTED ROPE DOOR PER SIP.

Part: WEB — DENTED (FLIGHT DECK FLOO) · airframe 53,036 hrs · 31,236 cycles

FOUND COCKPIT FLOOR SKIN CREASED ALONG CHANNEL AT STA 258; LBL 15.33'. DAMAGE MEASURES L = 9; W = 3'; AND D = 0.078'. MOD / REPAIRED COCKPIT FLOOR STA 258 LBL 15.33 IAW SWA EA 1-A53-33179

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,092 hrs · 28,740 cycles

L1 DOOR EMERGENCY LIGHTS INOP IN GALLEY AREA. R&R BATTERY PACK PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 49,025 hrs · 28,694 cycles

LT WING OUTBOARD AFT FLAP INBOARD AFT CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM AND AMM.

Part: STRINGER — CRACKED (LT WING) · airframe 49,025 hrs · 28,694 cycles

LT WING FIXED LEADING EDGE PANEL STRINGER CRACKED BETWEEN KRAS 206.32 TO KRAS 224. R&R STRINGER IAW SRM AND DWG.

Part: PLATE — CRACKED (LT WING) · airframe 49,025 hrs · 28,694 cycles

LT WING TRAILING EDGE INBOARD OF SAIL TAIL WAFFLE PLATE CRACKED AT FASTENER HOLE. R&R WAFFLE PLATE IAW SRM.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 49,025 hrs · 28,694 cycles

FORWARD CARGO DOOR SURROUND FORWARD CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 49,025 hrs · 28,694 cycles

LT WING TRAILING EDGE AT SAIL TAIL UPPER AFT BULB SEAL SUPPORT ANGLE CRACKED. R&R ANGLE IAW SRM.

Part: RIB — CRACKED (RT WING) · airframe 49,025 hrs · 28,694 cycles

RT WING FIXED TRAILING EDGE PANEL SUPPORT RIB CRACKED LOCATED. R&R RIB IAW SRM AND DWG.

Part: SKIN — CRACKED (RT WING) · airframe 48,478 hrs · 28,361 cycles

RT WING NR 5 LEADING EDGE SLAT SKIN CRACKED AT ACTUATOR ATTACH POINT. REPAIRED NR 5 SLAT SKIN PER SRM.

Part: STIFFENER — CRACKED (RT WHEEL WELL) · airframe 48,027 hrs · 28,071 cycles

RIGHT MAIN WHEEL WELL STA 663 RBL 26 STIFFENER CRACKED OUTBD OF TURBINE EXHAUST DUCT / REPLACED STIFFENER AT 663 RBL 26 REF SRM 51-40-02

Part: RADOME — DELAMINATED (FWD FUSELAGE) · airframe 47,320 hrs · 27,616 cycles

RADOME DELAMINATED. / R&R NOSE RADOME IAW AMM 53-52-00. SAM 115 ROBBED PARTS TAG - P/N OFF: 1001002-2 P/N ON: 1001001-1 S/N OFF: 9307205-C S/N ON: 0107103C (ROBBED FROM A/C 968)

Part: VAPOR BARRIER — CRACKED (LT WHEEL WELL) · airframe 45,699 hrs · 26,625 cycles

CRACK IN LEFT W/W MOISTURE BARRIER MOD. / APPLIED INTERIM REPAIR PER SRM 57-10-10-2R-2. FWD SIDE OF BULKHEAD

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 45,323 hrs · 26,405 cycles

RIGHT EMERGENCY EXIT ROW VERTICAL EXIT SIGN COVER MISSING AT ROW 12. R & R THE LIGHT ASSEMBLY IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 45,304 hrs · 26,393 cycles

L1 DOOR ESCAPE SLIDE OUT OF POSITION. REPOSITIONED THE SLIDE IAW MT.

Part: COVER — BROKEN (CABIN) · airframe 44,867 hrs · 26,129 cycles

FORWARD GALLEY EMERGENCY EXIT LIGHT COVER BROKEN. R&R LIGHT ASSEMBLY IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 44,675 hrs · 26,013 cycles

R2 DOOR EXIT SIGN LOOSE. R&R SIGN ASSEMBLY IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 42,781 hrs · 24,877 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER TC.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 42,706 hrs · 24,836 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW AMM & MAINTENANCE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,592 hrs · 24,753 cycles

M1670 LOWER EMER EXIT LIGHT ASSEMBLY INOPERATIVE BETWEEN ROW 9 - 12. R & R LIGHT ASSEMBLY IAW AMM.

Part: TIE CLIP — CORRODED (FUSELAGE) · airframe 42,592 hrs · 24,753 cycles

TIE CLIP CORRODED AT BS 867, STRINGER 25L. R & R TIE CLIP IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 42,592 hrs · 24,753 cycles

AFT LAVATORY SERVICE PANEL SKIN CORRODED AT AFT & LOWER EDGES UNDER PAN. REPAIRED SKIN IAW EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,592 hrs · 24,753 cycles

INTERCOSTAL CORRODED AT BS 312, RBL 11. R & R INTERCOSTAL IAW SRM & DWG.

Part: STRUCTURE — CORRODED (R2 DOOR) · airframe 42,592 hrs · 24,753 cycles

R2 DOOR CHORD CORRODED AT THRESHOLD. R & R CHORD IAW SRM & DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 42,592 hrs · 24,753 cycles

AFT CARGO FLOOR STRAP CORRODED AT BS 887. REPAIRED STRAP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 42,592 hrs · 24,753 cycles

STRINGER CLIP CRACKED AT BS 500D, STRINGER 19L. REPAIRED CLIP IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,592 hrs · 24,753 cycles

FLOOR STRUCTURE CORRODED AT BS 772, LBL 3. R & R SUPPORT IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 42,592 hrs · 24,753 cycles

FORWARD CARGO THRESHOLD WEB CORRODED. R & R WEB IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 42,592 hrs · 24,753 cycles

STRINGER CLIP CRACKED AT BS 500C, STRINGER 19L. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 42,592 hrs · 24,753 cycles

STRINGER CLIP CRACKED AT BS 500D, STRINGER 19R. R & R CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 42,592 hrs · 24,753 cycles

STRINGER CLIP CRACKED AT BS 500C, STRINGER 19L. R & R CLIP IAW SRM & DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 42,592 hrs · 24,753 cycles

LOWER BULKHEAD CHORD FASTENER HOLE CRACKED AT BS 540, BETWEEN STRINGER 22R - 23R. REPAIRED CHORD IAW EA.

Part: LENS — MISSING (EXIT SIGN) · airframe 41,994 hrs · 24,402 cycles

FORWARD EMER EXIT SIGN COVER LENS MISSING. INSTALLED LENS IAW SIP.

Part: BRACKET — LOOSE (L1 DOOR) · airframe 41,836 hrs · 24,306 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR BRACKET IAW MT.

Part: COVER — LOOSE (CABIN) · airframe 41,529 hrs · 24,134 cycles

RIGHT OVERWING EMER EXIT LIGHT COVER LOOSE. SECURED COVER IAW MM.

Part: LENS — CRACKED (EXIT SIGN) · airframe 40,305 hrs · 23,422 cycles

R2 DOOR EMER EXIT SIGN, LENS COVER CRACKED. R & R COVER IAW MM.

Part: SIGN — LOOSE (CABIN) · airframe 39,644 hrs · 23,037 cycles

L1 DOOR EXIT SIGN LOOSE. R & R SIGN ASSEMBLY IAW MM.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 38,838 hrs · 22,560 cycles

L2 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,461 hrs · 21,789 cycles

M01669 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW WDM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,461 hrs · 21,789 cycles

M01673 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW WDM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,461 hrs · 21,789 cycles

M01670 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW WDM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 37,461 hrs · 21,789 cycles

M01672 EMER LIGHTING BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW WDM.

Part: PLATE — CRACKED (RT WING) · airframe 37,461 hrs · 21,789 cycles

RIGHT WING WIGGLE PLATE CRACKED. R & R WIGGLE PLATE IAW SRM.

Part: SIGN — BROKEN (CABIN) · airframe 36,872 hrs · 21,436 cycles

RIGHT OVERWING EXIT SIGN BROKEN. R & R SIGN IAW MM.

Part: LENS — MISSING (CABIN) · airframe 36,714 hrs · 21,348 cycles

R2 DOOR EXIT SIGN LENS MISSING. INSTALLED LENS IAW SIP.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 35,984 hrs · 20,942 cycles

R2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM & MT.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 35,904 hrs · 20,903 cycles

LEFT HORIZONTAL STABILIZER STAB STATION 92.70 APPROXIMATELY 20 INCHES FROM FRONT SPAR CRACKED ON LOWER VERTICAL STIFFENER. REMOVED STABILIZER IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 35,904 hrs · 20,903 cycles

FLOOR SUPPORT STRUCTURE CRACKED AT BS 540, LBL 0. R & R SUPPORT IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,904 hrs · 20,903 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,904 hrs · 20,903 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,904 hrs · 20,903 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: ATTACH FITTING — BROKEN (RT WING) · airframe 35,904 hrs · 20,903 cycles

RIGHT WING TE RIB AT REAR SPAR ORSS 275 BULB SEAL FITTING ATTACH BRACKET UPPER FLANGE BROKEN. R & R FITTING IAW SRM & DWG 2.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,904 hrs · 20,903 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: FITTING — LOOSE (R2 DOOR) · airframe 35,904 hrs · 20,903 cycles

R2 DOOR EMER EVAC SLIDE FWD FLOOR FITTING LOOSE. SECURED FITTING IAW AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 35,344 hrs · 20,583 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: LENS — DAMAGED (EXIT SIGN) · airframe 35,095 hrs · 20,443 cycles

L1 DOOR EXIT SIGN LENS DAMAGED. REPAIRED COVER IAW SWA EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,186 hrs · 19,311 cycles

L2 DOOR EMERGENCY EXIT EXTERNAL LIGHT INOPERATIVE. R&R BULB IAW AMM.

Part: FITTING — LOOSE (R1 DOOR) · airframe 32,205 hrs · 18,754 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. SECURED CLIP IAW MM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 31,166 hrs · 18,161 cycles

RT MAIN WHEEL WELL FWD VERTICLE PRESSURE WEB CRACKED 1" AT BS 663.75, RBL 32.83 FWD OF SPOILER CONTROL VALVE. REPAIRED PER SRM 57-10-10-2R-3 REPAIR 3 FIG 204. REFER TO SAM 326 FRO SIGN OFFS. FACT AS A RESULT OF POST REPAIR INSPECTION

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 31,166 hrs · 18,161 cycles

RIGHT MAIN WHEEL WELL FWD VERTICLE PRESSURE WEB CRACKED 3" AT BS 663.75, RBL 43.80 JUST BELOW CEILING. REPAIRED PER SRM 57-10-10-2R-3 REPAIR 3 FIG 204, REFER TO SAM 326 FOR SIGN OFFS. FACT AS A RESULT OF POST REPAIR INSPECTION

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 31,166 hrs · 18,161 cycles

LEFT MAIN WHEEL WELL FWD VERTICLE PRESSURE WEB HAS 1" CRACK AT BS 663.75, LBL 38.00 JUST BELOW CEILING. REPAIRED PER SRM 57-10-10-2R-3, REPAIR 3 FIG 204, REFER TO SAM 326 FOR SIGN OFFS.

Part: LIGHT — BROKEN (CABIN) · airframe 30,748 hrs · 17,909 cycles

EXIT LIGHT ON ROW 10, CAPT SIDE SIDEWALL, BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM OPS GOOD CLEARING # 81636 MEL CLEARED ON L/P 8612346.

Part: LIGHT — BROKEN (CABIN) · airframe 30,748 hrs · 17,909 cycles

EXIT LIGHT ON ROW 10, CAPT SIDE SIDEWALL, BROKEN. REMOVED AND REPLACED EMERGENCY LIGHTT LENS SECURED C/W EA 1-A33-0130 OK TO CONTINUE ON MX NOTE # 81192 REPAIR/REPLACE/ON BEFORE 30 CYCLES.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 30,710 hrs · 17,889 cycles

FWD KEEL BEAM PANEL HAS A FWD OUTBOARD BRACKET CRACKED. REMOVED AND REPLACED PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,602 hrs · 17,827 cycles

EMERGENCY EXIT LIGHT ON AFT GALLEY AREA WALL AT AFT ENTRY DOOR INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY AT AFT ENTRY DOOR PER M/M. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,483 hrs · 17,748 cycles

FORWARD RIGHT JUST AFT OF THE FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 30,371 hrs · 17,676 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SIGN — MISSING (CABIN) · airframe 29,855 hrs · 17,324 cycles

RIGHT EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,051 hrs · 16,834 cycles

RIGHT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHTS INOP BETWEEN ROW 8 TO ROW 13. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 29,051 hrs · 16,834 cycles

R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RECONNECTED CONNECTOR PER SWPM & AMM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 29,051 hrs · 16,834 cycles

RIGHT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STA 129.50. REMOVED AND REPLACED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 29,051 hrs · 16,834 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STA 92.70. REPAIRED RIB IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,051 hrs · 16,834 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138.7. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,051 hrs · 16,834 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.9. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 29,051 hrs · 16,834 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,051 hrs · 16,834 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147.9. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 29,051 hrs · 16,834 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.9. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,051 hrs · 16,834 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 175.5. REPAIRED SKIN PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 28,621 hrs · 16,590 cycles

EMERGENCY LIGHT TRACK COVER CRACKED AT ROW 9. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 28,621 hrs · 16,590 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES PER MM.

Part: BRACKET — LOOSE (EVAC SLIDE) · airframe 27,793 hrs · 16,125 cycles

L2 DOOR EMERGENCY EVAC SLIDE BRACKET LOOSE. SECURED BRACKET PER MM.

Part: COVER — BROKEN (CABIN) · airframe 26,352 hrs · 15,278 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EMERGENCY EXIT LIGHT COVER BROKEN AT ROW 11. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 24,423 hrs · 14,142 cycles

L2 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,276 hrs · 14,053 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 1. RELAMPED EEPLS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 24,067 hrs · 13,938 cycles

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

Part: WINDOW — ARCED (COCKPIT) · airframe 23,713 hrs · 13,745 cycles

DIVERSION - R1 COCKPIT WINDOW ARCED DURING FLIGHT. REMOVED AND REPLACED R1 WINDOW SHIELD AND HEAT CONTROLLER PER MM.

Part: COVER — MISSING (CABIN) · airframe 23,205 hrs · 13,468 cycles

EEPLS COVER MISSING AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: COVER — BROKEN (CABIN) · airframe 23,057 hrs · 13,382 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EEPLS COVER BROKEN AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 22,889 hrs · 13,288 cycles

EMERGENCY EXIT LIGHT COVER MISSING AT ROW 1. INSTALLED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 22,259 hrs · 12,914 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER MISSING AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: COVER — WORN (CABIN) · airframe 21,836 hrs · 12,669 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS COVERS WORN BETWEEN ROW 1 TO ROW 20. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 21,544 hrs · 12,497 cycles

AFT GALLEY EMERGENCY FLASHLIGHT BATTERY VOLT LOW. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — MISSING (CABIN) · airframe 21,474 hrs · 12,460 cycles

EEPLS LENS MISSING AT ROW 2. INSTALLED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 21,474 hrs · 12,460 cycles

EEPLS LENS MISSING AT ROW 1. INSTALLED LENS PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 21,464 hrs · 12,454 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS MISSING AT ROW 1. INSTALLED EEPLS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 20,776 hrs · 12,033 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 3. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 19,647 hrs · 11,345 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EMERGENCY LIGHT COVERS CRACKED BETWEEN ROW 3 TO ROW 14. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 19,647 hrs · 11,345 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EMERGENCY LIGHT COVERS CRACKED BETWEEN ROW 15 TO ROW 23. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 19,206 hrs · 11,063 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,358 hrs · 9,961 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP. RELAMPED PER MM.

Part: COVER — CRACKED (CABIN) · airframe 17,314 hrs · 9,929 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS TRACK COVER CRACKED. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 17,280 hrs · 9,902 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,127 hrs · 9,812 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 2L. REMOVED AND REPLACED EEPLS PER MM.

Part: WIRE — EXPOSED (EMERGENCY LIGHT) · airframe 16,929 hrs · 9,699 cycles

FWD EEPLS WIRE EXPOSED AT ROW 1. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 16,837 hrs · 9,649 cycles

EEPLS LIGHT STRIP LOOSE AT ROW 1. SECURED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 162,223 hrs · 9,275 cycles

FOUND FWD EEPLS LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — CRACKED (CABIN) · airframe 14,883 hrs · 8,463 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS CRACKED AT ROW 4 ABC. REMOVED AND REPLACED LENS PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 14,524 hrs · 8,261 cycles

L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 14,516 hrs · 8,253 cycles

L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER MT.

Part: LENS — CRACKED (CABIN) · airframe 12,840 hrs · 7,249 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS CRACKED AT ROW 5 ABC. REMOVED AND REPLACED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 11,888 hrs · 6,691 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,830 hrs · 4,945 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 8,820 hrs · 4,940 cycles

EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 6,194 hrs · 3,381 cycles

EEPLS TRACK LOOSE AT FWD END. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 5,922 hrs · 3,240 cycles

EEPLS TRACK COVER MISSING AT ROW 23. INSTALLED COVER PER MM.

Part: FAN — FAULTY (E & E BAY) · airframe 3,368 hrs · 1,864 cycles

DIVERSION, ACRID ELECTRICAL ODOR IN CABIN. GASPER FAN & RECIRCULATION FAN SWITCHES TURNED OFF, ODOR DISSIPATED. REMOVED AND REPLACED EQUIPMENT COOLING FAN PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 154 hrs · 91 cycles

DURING SPV, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERIES PER MM.

Part: SLIDE — DISLODGED (R2 DOOR) · airframe 124 hrs · 75 cycles

R2 DOOR EVAC SLIDE FELL OUT, DID NOT DEPLOY. REINSTALLED R2 DOOR EVAC SLIDE PER MM.