N711HK

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,797 hrs · 46,925 cycles

AFT SERVICE DOOR SLIDE EMERGENCY LIGHT INOPERATIVE. REMOVED & REPLACED LAMP, IAW AMM 33-51-04.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 77,745 hrs · 46,890 cycles

FWD ENTRY LOWER EMERGENCY EXIT LIGHT LENS NOT SECURE. R & R FWD ENTRY LOWER EMERGENCY EXIT LIGHT LENS, IAW AMM 33-51-03.

Part: SCREW — MISSING (R2 DOOR SLIDE) · airframe 76,794 hrs · 46,304 cycles

SCREW TO AFT SERVICE DOOR SLIDE MISSING. REPLACED AFT SERVICE DOOR SLIDE AFT SCREW IAW AMM 25-66-01. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,991 hrs · 45,820 cycles

ONE LAMP AT FORWARD ENTRY EMERGENCY EXIT INDICATOR AND ONE BULB AT AFT CEILING LEFT INDICATOR DO NOT ILLUMINATE. / RELAMPED FORWARD ENTRY EMERGENCY EXIT INDICATOR AND AFT CEILING LEFT INDICATOR AND PERFORMED GOOD TEST OF NEW LAMPS PER AMM 33-51-01-960-801 93128U 22MAR20

Part: HOUSING — BROKEN (EXIT SIGN) · airframe 75,991 hrs · 45,820 cycles

AFT ENTRY DOOR EXIT SIGN HOUSING IS BROKEN IN 2 PLACES REPLACED AFT ENTRY DOOR EXIT SIGN HOUSING PER AMM 33-51-01-960-802. OPS CHECK IS GOOD.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 75,991 hrs · 45,820 cycles

PASSENGER CABIN L/H OVERWING EXIT SIGN HAS INOP BULB. RELAMPED PASSENGER CABIN L/H OVERWING EXIT SIGN AND PERFORMED GOOD FUNCTIONAL TEST AS PER AMM 33-51-01-960-801 STEP. 2.C.(1.A.2)(1.C)(2)(3)(4). 59132U 21MAR20

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 75,991 hrs · 45,820 cycles

PASSENGER CABIN R/H OVERWING EXIT, UPPER LOCATOR SIGN HAS INOP BULB. RELAMPED R/H OVERWING EXIT UPPER LOCATOR SIGN AND PERFORMED GOOD FUNCTIONAL TEST AS PER AMM. 33-51-01-960-801 STEP 2.C(1.A.4.)(1.C)(2)(3)(4). 59132U 21MAR20

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 75,991 hrs · 45,820 cycles

INTERCOSTAL COMMON TO STR25R BETWEEN BS500D AND BS520 IS CRACKED ON AFT END FABRICATED NEW INTERCOSTAL ON P.O# 787160-SWA LOCATED, DRILLED, APPLIED CHEMICAL CONVERSION COAT AND PRIMED ALL I.A.W BOEING DWGS. 143A9803, 143A7902 143A9803 AND SRM 51-40-05-0G-0. INSTALLATION WILL BE ACCOMPLISHED ON CUSTOMER CARD U133768 FUSELAGE 5097.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 75,991 hrs · 45,820 cycles

EMERGENCY EXIT LIGHTS ASSOCIATED WITH M1673 BATTERY PACK COME ON MOMENTARILY. / REMOVED AND REPLACED M1673 BATTERY PACK AND PERFORMED GOOD TEST OF NEW BATTERY PACK PER AMM 33-51-06-960-805. 93128U 22MAR20

Part: SKIN — CORRODED (FUSELAGE) · airframe 75,991 hrs · 45,820 cycles

***CORROSION*** ON LOWER BELLY SKIN OUTER SURFACE BS 500A+14 BETWEEN STR 28R-28L; BL0; WL 148 / REPAIRED FUSELAGE BELLY SKIN BS 500A+14 BETWEEN STR 28R-28L BL0 WL148 PER ER 20-02135 REV IR AND EA 1-753-36786 REV IR

Part: STRAP — CORRODED (AFT CARGO) · airframe 75,991 hrs · 45,820 cycles

AFT CARGO BAY STRAP UNDER INTERCOSTAL BETWEEN BS787 AND BS794 HAS CORROSION RBL19; WL155 / CORROSION ON ACB STRAP UNDER INTERCOSTAL BETWEEN BS787 AND BS794 FOUND TO BE OUT OF LIMITS. DUE TO NO SRM LIMITS. REMOVED AND REPLACED STRAP BS767+15' - 794+10' RBL19 WL155 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0. DWG 146A8120.

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 75,991 hrs · 45,820 cycles

AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE HAS AREAS OF CORROSION AROUND NUTPLATE HOLES BS727 TO BS847 LBL21, WL156 EVALUATED CORROSION ON ACB L/H FLOOR TO SIDEWALL SUPPORT, REMOVED .020" FROM ORIG .040", FOUND TO BE OUT OF LIMITS, IAW SRM 53-00-53-1A-2. LOCATED AND DRILLED NEW, FLOOR TO SIDEWALL SUPPORT, AND INSTALLED, IAW SRM 51-40-05-0G-0, DWG 146A7500, SRM 51-40-02-0G-0.

Part: WEB — CORRODED (FUSELAGE) · airframe 75,991 hrs · 45,820 cycles

AFT CARGO BAY SUBTHRESHOLD WEB HAS AREAS OF CORROSION BETWEEN BS792 TO BS847 RBL27 WL158 / CORROSION ON ACB SUBTHRESHOLD WEB FOUND TO BE OUT LIMITS PER SRM 53-60-15-1A-1. REMOVED AND REPLACED SUBTHRESHOLD BS 792-847 RBL 27 WL 158 PER SRM 51-40-02-0G-0. SRM 51-40-05-0G-0. DWG 146A8120; DWG 146A8340.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,991 hrs · 45,820 cycles

FCB STR25R HAS CORROSION ON END OF STRINGER AT BS535.5 WL156 / REPAIRED FCB STR25 R/H AT BS535.5 WL156 PER ER 20-02095 REV IR AND EA 1-753-36796 REV IR

Part: SPLICE STRAP — CORRODED (AFT CARGO FLOOR) · airframe 75,991 hrs · 45,820 cycles

AFT CARGO BAY FLOOR SPLICE STRAP HAS CORROSION AROUND NUT PLATES BS727D+6 WL156 RBL10 TO LBL10 / EVALUATED CORROSION ON SPLICE STRAP FOR ACB FLOOR SPLICE B.S 727D+6 RBL 10 TO LBL 10 FOUND OUT OF LIMITS DUE TO NO SRM LIMITS RECEIVED NEW FLOOR STRAP ON PO# 777687 NEW PART WILL BE INSTALLED ON CUST. CARD #JPANEL-141-CLOSE

Part: STRINGER — CORRODED (FUSELAGE) · airframe 75,991 hrs · 45,820 cycles

FCB STR23R HAS CORROSION ON END OF STRINGER AT BS535.5 WL164 / FOUND END OF STRINGER TO HAVE %100 MATERIAL LOSS IN A .5' X .5' AREA PER SRM 53-00-03-1A-1. REPAIRED PER ATS ER 20-02091 REV IR AND SWA EA # 1-753-36795 REV IR

Part: SHIELD — CORRODED (FUSELAGE) · airframe 75,991 hrs · 45,820 cycles

AFT CARGO BAY SHIELD FWD OF AFT CARGO DOOR OPENING HAS AREAS OF CORROSION AROUND NUT PLATES BS767 TO BS792, RBL21, WL158 CORROSION ON ACB SHIELD BS 767-792 RBL21, WL158 FOUND TO BE OUT OF LIMITS DUE TO NO SRM LIMITS. REMOVED AND REPLACED SHIELD PER SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, DWG 146A0081.

Part: WEB — CORRODED (FUSELAGE) · airframe 75,991 hrs · 45,820 cycles

AFT CARGO BAY VERTICAL WEB BETWEEN BS727A AND 727B, LBL3, WL147 HAS CORROSION AROUND RIVET BUCKTAILS EVALUATED CORROSION ON AFT CARGO BAY VERTICAL WEB BETWEEN BS727A AND 727B, LBL3, WL147 PART# 146A7505-5, FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN SRM, REPLACEMENT OF PARTS REQUIRED IAW SRM 51-10-02-0G-0, REMOVED AND REPLACED AFT CARGO BAY VERTICAL WEB BETWEEN BS727A AND 727B, LBL3, WL147 IAW DWG 146A7500 AND SRM 51-40-02-0G-0

Part: WEB — CORRODED (FUSELAGE) · airframe 75,991 hrs · 45,820 cycles

AFT CARGO BAY VERTICAL WEB JUST FWD OF BS927 LBL3, WL168 HAS CORROSION REMOVED DAMAGED WEB AND INSTALLED NEW WEB AT BS947-927 LBL3 WL168 IAW SRM 51-40-02-0G-0 AND DWG 147A7500 AND 147A7580 RECEIVED FABRICATED PART FROM OSS ON PO# 785391 5358C 15MAR20

Part: WEB — CORRODED (FUSELAGE) · airframe 75,991 hrs · 45,820 cycles

AFT CARGO BAY VERTICAL WEB AT BS945 RBL3 WL173 HAS CORROSION REMOVED DAMAGED WEB AND INSTALLED NEW WEB AT BS 947-927 RBL3 WL173 IAW SRM 51-40-02-0G-0 AND DWG 147A7500 AND 147A7580 RECEIVED FABRICATED PART FROM OSS ON PO# 785395 5358C 15MAR20

Part: WEB — CORRODED (FUSELAGE) · airframe 75,991 hrs · 45,820 cycles

AFT CARGO BAY VERTICAL WEB HAS CORROSION ON FWD END BETWEEN BS827 AND BS847 RBL6 WL153 REMOVED AND REPLACED ACB VERTICAL WEB BS 827-847, WL 153, RBL 6 IAW SRM 51-40-02, SRM 51-40-05, DWG # 146A8130, DWG # 146A8132.

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 75,991 hrs · 45,820 cycles

AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS AREAS OF CORROSION AROUND NUTPLATE HOLES BS727 TO BS767 RBL21; WL156 / CORROSION ON ACB R/H FLOOR TO SIDEWALL SUPPORT BS727-767; RBL21; WL156 FOUND TO BE OUT OF LIMITS DUE TO FOUND .020 REMOVED FROM ORIG .040 IN NUMEROUS 1' X 1' AREAS PER SRM 53-00-53-1A-2. REMOVED ACB R/H FLOOR TO SIDEWALL SUPPORT BS727-767 RBL21; WL156 PER SRM 51-40-02-0G-0; INSTALLED NEW ACB R/H FLOOR TO SIDEWALL SUPPORT ASSY BS727-767 RBL21; WL156 PER SRM 51-40-02-0G-0 AND DWG 146A7500. 59911U; 03/14/20

Part: FLOORBEAM — CORRODED (BS 757 R-LBL 10) · airframe 75,991 hrs · 45,820 cycles

AFT CARGO BAY FLOOR SPLICE STRAP HAS CORROSION AROUND NUT PLATES BS767+6 WL156 RBL10 TO LBL10 / EVALUATED CORROSION ON STRAP FOR ACB FLOOR SPLICE B.S 767+6 RBL 10 TO LBL 10 FOUND OUT OF LIMITS DUE TO NO LIMITS IN SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0 RECEIVED NEW FLOOR SPLICE ON PO#777784 NEW PART WILL BE INSTALLED ON CUST. CARD #JPANEL-141-CLOSE

Part: MOUNT — CORRODED (ANTENNA TRAY) · airframe 75,991 hrs · 45,820 cycles

FCB; ANTENNA TRAY MOUNT HAS CORROSION AROUND NUT PLATES BETWEEN BS500 AND BS500A BL0 WL148 / REMOVED AND REPLACED FCB ANTENNA TRAY MOUNT @ BS 500-500A BL0 WL 148 IAW SRM 51-40-02 AND DWG 143A3230

Part: WEB — CORRODED (FUSELAGE) · airframe 75,991 hrs · 45,820 cycles

AFT CARGO BAY VERTICAL WEB BETWEEN BS727A AND 727B, RBL3, WL147 HAS CORROSION AROUND RIVET BUCKTAILS REMOVED DAMAGED WEB AND INSTALLED NEW WEB AT BS 727A-727B RBL3 WL147 IAW SRM 51-40-02-0G-0 AND DWG 146A7505 AND 146A7500

Part: NUT PLATE — CORRODED (ANTENNA TRAY) · airframe 75,991 hrs · 45,820 cycles

FCB; ANTENNA TRAY MOUNT HAS CORROSION AROUND NUT PLATES BETWEEN BS500A AND BS500B BL0 WL148 / EVALUATED CORROSION TRAY FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN SRM REMOVED FCB ANTENNA TRAY MOUNT BETWEEN BS500A AND BS500B; BL0 PER SRM 51-40-02 ALL OTHER WORK WILL BE ACCOMPLISHED ON CUST.CARD# U133888 NO FURTHER ACTION REQUIRED ON THIS CARD

Part: SKIN — CRACKED (LE SLAT) · airframe 75,991 hrs · 45,820 cycles

#8 SLAT NOSE SKIN CRACKED AT ACTUATOR RIB ATTACH FASTENER (MARKED) / REPAIRED #8 SLAT NOSE SKIN CRACK AT ACTUATOR RIB ATTACH AREA IAW SRM 57-42-01-2R-8. 84036U; 18MAR20.

Part: INTERCOSTAL — DETERIORATED (FUSELAGE) · airframe 75,991 hrs · 45,820 cycles

DURING ACCOMPLISHMENT OF EA# 1-A53-33179 FOUND PREVIOUS REPAIR AT BS 270 INTERCOSTAL LBL 12-RBL 12 WL 208. / REPAIRED STA 270 INTERCOSTAL; LBL12 - RBL12; WL208 IAW EA 1-753-36758; REV IR; ER 20-02078. REV IR

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,991 hrs · 45,820 cycles

***CORROSION*** COCKPIT FLOOR STA 259; WL 208; LBL 10 TO RBL 8 TOP AFT FLOOR BEAM CHORD TOP SURFACE CORRODED. / REPAIRED CORROSION ON BS259.5 AFT CHORD LBL20-RBL20 WL208 AS PER EA# 1-753-36775 REV IR AND ER# 20-02074 REV IR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 75,991 hrs · 45,820 cycles

***CORROSION*** FUSELAGE EXTERNAL SKIN BS 947-1006 STR 2L-2R REPAIRED CORROSION DAMAGE ON FUSELAGE SKIN BS 947- 1006 STR 2L-2R PER ER 20-02114 REV IR AND EA 1-753-36761 REV IR

Part: FLOOR PANEL — DENTED (COCKPIT) · airframe 75,991 hrs · 45,820 cycles

COCKPIT REMOVABLE FLOOR PANEL 211AF IS DENTED. / FABRICATED COCKPIT REMOVABLE PANEL 211AF REPLACEMENT FROM 2024-T3 -C .040' LOT# 1398916-1 IAW DWG 141A5133 AND SRM 51-40-05-0G-0

Part: LIGHT — BROKEN (CABIN) · airframe 75,991 hrs · 45,820 cycles

R/H EXIT LIGHT IS BROKEN ON SIDEWALL 242YAW. REMOVED AND REPLACED R/H EXIT LIGHT LENS IAW B737-700 AMM 33-51-01-960-802

Part: STUD — DAMAGED (FUSELAGE) · airframe 75,991 hrs · 45,820 cycles

DAMAGED STUD ON 616 FRAME COMMON TO L/H OWE EXIT CUTOUT. (MARKED) / REPLACED DAMAGED STUD AT LH FR 616 OVERWING EXIT CUT OUT. IAW B737-700 SRM 51-40-02-0G-0 PARA 7D

Part: STUD — DAMAGED (FUSELAGE) · airframe 75,991 hrs · 45,820 cycles

DAMAGED STUD ON R/H 616 FRAME AT OWE EXIT; TOP STUD. / REPLACED DAMAGED STUD AT RH FR616 AT OVERWING EXIT; TOP STUD IAW B737-700 SRM 51-40-02-0G-0 PARA 7D

Part: LENS — CRACKED (CABIN) · airframe 75,991 hrs · 45,820 cycles

AFT ENTRY DOOR EXIT LENS IS CRACKED. REPLACED AFT ENTRY DOOR EXIT LENS PER AMM 33-51-01-960-802.

Part: STRAP — CORRODED (FUSELAGE) · airframe 75,991 hrs · 45,820 cycles

***CORROSION*** ON STRAP AT STA 636; LBL 66; WL 221; COMMON TO LOWER SILL WEB. (MARKED) / REPLACED CORRODED STRAP WITH A NEW STRIP BS636 WL221 LBL66. WORK ACCOMPLISHED IAW SRM 51-10-02-0G-0 SRM 51-40-02-0G-0; BOEING DWG #144A8201 REV-.

Part: WEB — DENTED (FUSELAGE) · airframe 75,991 hrs · 45,820 cycles

AFT CARGO BAY DOOR CLOSE OUT WEB 142KW IS WORN AND DENTED / RECEIVED NEW ACB CLOSEOUT WEB # 142KW ON PO # 782804 NEW PART WILL BE INSTALLED ON CUST. CARD # JPANEL-141-CLOSE

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,991 hrs · 45,820 cycles

CRACKED ANGLE STA 694 COMMON TO INTERCOSTAL, RBL 1, WL 207. (MARKED) REPLACED CRACKED ANGLE BS694 COMMON TO INTERCOSTAL RBL1 WL207. ALL WORK ACCOMPLISHED IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, BOEING DWG# 273A9110 REV-. AMM 20-60-02-100-801, AMM 20-60-07-913-801.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 75,991 hrs · 45,820 cycles

CRACKED ANGLE STA 695 ON INTERCOSTAL, LBL 24, WL 202. (MARKED) REPLACED CRACKED ANGLE BS695 COMMON TO INTERCOSTAL LBL24 WL202. ALL WORK ACCOMPLISHED IAW AMM 20-60-07-913-801, AMM 20-60-02-100-801, SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, SOPM 20-41-04, SOPM 20-43-03 BOEING DWG# 273A9110 REV-, BOEING DWG# 111A6000 REV A.

Part: FLOOR PANEL — DENTED (COCKPIT) · airframe 75,991 hrs · 45,820 cycles

FLIGHT DECK FLOOR IS DENTED AT B.S. 255; L.B.L. 14; W.L. 207.45 / REPAIRED FLIGHT DECK FLOOR DAMAGE AT BS 255; LBL 14. WL 207.45 PER EA #1-A53-33179 REV IR.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 75,689 hrs · 45,612 cycles

6 EACH CABIN EMERGENCY LIGHTING BATTERY PACKS FAIL CAPACITY TEST. REMOVED AND REPLACED 6 EACH CABIN EMERGENCY LIGHTING BATTERY PACKS AT LOCATIONS M1669, M1670,M1672,M1673,M1674 AND M1675 PER AMM 33-51-06 AND ENG DWG 33500005.

Part: SKIN — CORRODED (CENTRE FUSELAGE) · airframe 74,234 hrs · 44,716 cycles

REFERENCE NRC # D391825 AREA UNDER ADF ANTENNA HAS CORROSION SEVERAL SPOTS / DMA CLOSING LP: 0166158 COMPLIED WITH EA 1-753-35505 REV IR REFERENCE NRC # D384592 FOR LT TLD TRACKING CLEARING NUMBER 86646

Part: PLATE — CORRODED (FUSELAGE) · airframe 74,231 hrs · 44,714 cycles

AREA UNDER ADF ANTENNA HAS CORROSION IN SEVERAL SPOTS. / REWORK ACCOMPLISHED PER EA 1-753-35494 AND EA 1-753-35505. ADF BLANKING PLATE INSTALLED PER EA 1-753-35488. CONTINUED AIRWORTHINESS REQUIREMENTS TRACKING ON QMOD EA 1-753-36150.

Part: LIGHT — MISSING (CABIN) · airframe 74,231 hrs · 44,714 cycles

L/H OVERHEAD BIN EMERGENCY LIGHT LENS MISSING AT ROW 1. INSTALLED LIGHT IAW AMM.

Part: RIB — CRACKED (LOWER EXT FUSELA) · airframe 73,649 hrs · 44,351 cycles

LEFT WING TO BODY PANEL 195AL SUPPORT RIB CRACKED / REMOVED/REPLACED LEFT WING TO BODY PANEL 195AL SUPPORT RIB REF SRM 51-40-02

Part: PANEL — ELONGATED (LOWER EXT FUSELA) · airframe 73,061 hrs · 43,987 cycles

PANEL 193B ALL SCREW HOLES WORN AND ELONGATED. / COMPLIED WITH ON E.A. 1-753-34687

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 73,061 hrs · 43,987 cycles

AFT I/B FLASHLIGHT LED DOES NOT BLINK. R&R FLASHLIGHT PER AMM 25-64-00

Part: BRACKET — CRACKED (RT WING) · airframe 71,469 hrs · 42,994 cycles

RT WING FIXED TRAILING EDGE BULB SEAL RETAINING BRACKET FOR INBOARD FORE FLAP OUTBOARD END CRACKED. R&R BRACKET PER SRM.

Part: STRAP — MISSING (FLASHLIGHT) · airframe 71,274 hrs · 42,873 cycles

AFT LT GALLEY EMERGENCY FLASHLIGHT MISSING SAFETY STRAP. INSTALLED SAFETY STRAP IAW SIP & AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,660 hrs · 42,465 cycles

AFT LT EMERGENCY LIGHT INOP BETWEEN ROW 23 AND ROW 24. RELAMPED LIGHT IAW AMM.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 70,660 hrs · 42,465 cycles

SHEAR TIE DAMAGED AT BS 360, BETWEEN STR 26R TO STR 27R. R&R SHEAR TIE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 70,660 hrs · 42,465 cycles

SHEAR TIE CORRODED AT BS 360, RBL R2. R&R SHEAR TIE IAW SRM AND DWG.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 70,660 hrs · 42,465 cycles

STRINGER SPLICE SUPPORT CORRODED AT BS 360, STR 27R. R&R SPLICE IAW SRM AND DWG.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 70,660 hrs · 42,465 cycles

BUTT SPLICE CORRODED AT BS 360, BETWEEN STR 28R TO STR 27R. R&R BUTT SPLICE IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 70,660 hrs · 42,465 cycles

CHANNEL TIE CORRODED AT BS 360, BL 0. R&R CHANNEL TIE PER DWG & SRM.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 70,660 hrs · 42,465 cycles

STRINGER TIE CORRODED AT BS 360, STR 28R. R&R STRINGER TIE IAW ER AND EA.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 70,660 hrs · 42,465 cycles

STRINGER CORRODED BETWEEN BS 360 TO BS 364, STR 28L. R&R STRINGER IAW SRM & DWG.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 70,534 hrs · 42,383 cycles

AFT OUTBOARD EMERGENCY FLASHLIGHT INOP. R&R BATTERY PER MM.

Part: HOOK AND LOOP — LOOSE (R2 DOOR) · airframe 70,172 hrs · 42,146 cycles

R2 DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED LOWER HOOK AND LOOP IAW AMM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 70,038 hrs · 42,070 cycles

AFT GALLEY EMERGENCY FLASHLIGHT INOP. R&R BATTERY PER AMM.

Part: FITTING — LOOSE (R1 GIRT BAR) · airframe 69,643 hrs · 41,808 cycles

R1 DOOR GIRT BAR RETAINING FITTING LOOSE. SECURED THE FITTING IAW AMM.

Part: NONE — BROKEN (LEFT WING) · airframe 69,547 hrs · 41,754 cycles

LH WING PANEL 551GB INNER SUPPORT RODS UPPER CLIP ASSY BROKEN. / REMOVED AND REPLACED LH WING PANEL 551GB SUPPORT ROD UPPER ATTACH CLIP PER SRM 51-40-0G-0 AND DWG 115A5300 REV C.

Part: WEB — CRACKED (FUSELAGE) · airframe 69,547 hrs · 41,754 cycles

SUPPLEMENTAL INFORMATION: WHILE REPLACING CRACKED STRINGER CLIP AT STATION 294.5; STRINGER 13L FOUND INBOARD FRAME WEB FASTENER HOLE DRILLED OVERSIZE AND FILLER INSTALLED UNDER CLIP. / ACCOMPLISHED FRAME WEB REPAIR AT STA 294.5 AND STR 13L I.A.W E.A 180092 IR AND SWA EA 1-753-32036 IR

Part: BRACKET — CRACKED (RT WING) · airframe 69,547 hrs · 41,754 cycles

RT WING FORWARD FUEL FEED BRACKET CRACKED AT RIB 6 AT WING STA 228.25. R&R BRACKET IAW SRM AND DWG.

Part: PLATE — CRACKED (RT WING) · airframe 69,547 hrs · 41,754 cycles

RT WING TRAILING EDGE WIGGLE PLATE CRACKED AT STA 261. R&R WIGGLE PLATE IAW DWG AND SRM.

Part: BEAM — CRACKED (R1 DOOR FRAME) · airframe 69,547 hrs · 41,754 cycles

R1 DOOR CUTOUT UPPER FORWARD STUB BEAM FRAME CRACKED. R & R THE STUB BEAM IAW SRM AND DWG.

Part: STRAP — CORRODED (MAIN CABIN) · airframe 69,547 hrs · 41,754 cycles

PASSENGER CABIN CREASE BEAM R1 DOOR WAY BS 303.9 + 4'; TAPERED STRAP IS CORRODED THAT ATTACHES TO ANGLE / REMOVED CORROSION ON TAPERED STRAP COMMON TO R1 CREASE BEAM AT BS 303.9 + 4' IAW SRM 51-10-02-0G-0. VERIFIED LIMITS; ORIGINAL 'T' .200' LOSS OF .026'; REMAINING .174' OUT OF LIMITS IAW SRM 53-10-15-1A-2 REMOVED AND REPLACED STRAP IAW SRM 51-40-02-0G-0 AND BOEING DWG # 141A8316 REV E. A 46319

Part: STIFFENER — CRACKED (WNG-BODY FAIRING) · airframe 69,547 hrs · 41,754 cycles

MAIN WHEEL WELL WING TO BODY SUPPORT STRUCTURE PANEL SUPPORT STIFFENER CRACKED AT BS 663, BETWEEN, LBL 6 TO LBL 32. R & R THE STIFFENER IAW DWG.

Part: SPAR — CORRODED (LT WING) · airframe 69,547 hrs · 41,754 cycles

LEFT WING AFT SPAR CORRODED AT UPPER AND LOWER BONDING STRAP ATTACH POINTS FOR NR 1 FUEL BOOST PUMP. REPAIRED THE AFT SPAR IAW EA.

Part: PANEL — DELAMINATED (LT WING) · airframe 69,547 hrs · 41,754 cycles

#1 ENGINE PYLON PANEL 431ER; CORNER COMPOSITE IS DELAMINATED AS MARKED. / #1 ENGINE PYLON PANEL 431ER REPAIRED IAW B737 SRM 54-50-70-2R-02 PARA 4

Part: PANEL — CRACKED (MAIN CABIN) · airframe 69,547 hrs · 41,754 cycles

L1 DOOR FORWARD CUT-OUT COVE PANEL AROUND UPPER LATCH FITTING CRACKED. / REMOVED AND REPLACED L 1 DOOR FWD CUT OUT COVE PANEL VERIFIED NEW PANEL LOCATED AND DRILLED AND TOP COATED IAW SRM 51-40-02-0G-0 AND 51-40-05-0G-0 AND IPL 53-13-00-21 AND AMM 51-21-73-370-801

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 69,547 hrs · 41,754 cycles

AFT CARGO COMPARTMENT AFT CORNER SCUFF PLATE CRACKED / REPAIRED PER # 1-A53-2076 REV 11 AFT CARGO CPMPARTMENT AFT CORNER SCUFF PLATE.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 69,547 hrs · 41,754 cycles

AFT CARGO COMPARTMENT BS 947; RH SIDE BULKHEAD ANGLE IS CORRODED / AFT CARGO COMPARTMAENT RH SIDE BULKHEAD ANGLE ASSY. P/N 149A8118-26 AT BS947 WAS CORRODED OUT OF LIMITS. DOUBLER P/N 149A8118-15 ORG T .063' LOSS .025' REMAINING .038' ANGLE (BRACKET) P/N 149A8118-25 ORG T .080' LOSS .040' REMAINING 040' ALSO OUT OF LIMITS. ANGLE ASSY P/N 149A8118-26 WAS REMOVED AND REPLACED WITH NEW FABRICATED PART. SMAL # PO1530656L AND PO1530656L2; IAW BOEING DRW 149A8118 REV- AND SRM 51-40-02-0G-0

Part: SKIN — CRACKED (BS 293) · airframe 69,547 hrs · 41,754 cycles

R1 DOOR CUTOUT INTERNAL SKIN, 2 INCH CRACKED AT BS 293, STRINGER 9R FORWARD UPPER LATCH FITTING. REPAIRED THE SKIN IAW EA.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 69,547 hrs · 41,754 cycles

FWD CARGO COMPARTMENT FWD LOWER CORNER THRESHOLD SCUFF PLATE CRACKED / FWD CARGO FWD LOWER CORNER OF SCUFF PLATE CRACKED ; REPAIRED CRACKED SCUFF PLATE ON E.A 1-A53-2072 REV 11.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,547 hrs · 41,754 cycles

AFT CARGO COMPARTMENT INTERCOSTAL CORRODED BETWEEN BS 847 TO BS 867, LBL 20. R&R INTERCOSTAL IAW SRM AND DWG.

Part: ANGLE — CRACKED (AFT CARGO BAY) · airframe 69,547 hrs · 41,754 cycles

AFT CARGO COMPARTMENT BS 947 LOWER BULKHEAD ANGLE CORRODED / REMOVED AND REPLACED AFT CARGO COMPARTMENT STA 947 LOWER BULKHEAD ANGLE IAW BOEING DWG 149A8118 REV: A AND SRM 51-40-02-0G-0

Part: ANGLE — CRACKED (RT MLG WW) · airframe 69,547 hrs · 41,754 cycles

VERTICAL PRESSURE DECK WEB ANGLE WEB CRACKED AT BS 663, RBL 34. REPAIRED ANGLE IAW EA.

Part: SUPPORT ANGLE — CORRODED (MAIN CABIN) · airframe 69,547 hrs · 41,754 cycles

LEFT HAND; L1 DOOR SILL PLATE; SUPPORT STRUCTURE HAS MULTIPLE AREAS OF CORROSION / BLENDED OUT CORROSION AT L1 DOOR SILL PLATE SUPPORT ANGLE IAW B737 SRM 51-10-02. ORIGINAL THICKNESS 0080'; MATERIAL LOSS 0.020'. THE MATEIRAL REMAINING 0.060'; THE AREA FOUND TO BE OUT OF LIMIT IAW B737-700 SRM 53-80-15-1A-1. LOCATED AND DRILLED NEW ANGLE P/N: 141A842-20 IAW B737-700 SRM 51-40-05 AND DWG: 141A840 REV:-. INSTALLED NEW ANGLE IAW B737-700 SRM 51-40-02 AND DWG 141A8110 REV:- ATAG: WN 0016

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 69,547 hrs · 41,754 cycles

INTERCOSTAL CRACKED AT BS 309.9, STR 3L. R&R INTERCOSTAL IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 69,547 hrs · 41,754 cycles

INTERCOSTAL STRAP CRACKED AT BS 309.9, STR 3L. R&R STRAP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CORRODED (MAIN CABIN) · airframe 69,547 hrs · 41,754 cycles

R1 DOOR SILL; INBRD SUPPORT STRUCTURE; HAS MULTIPLE AREAS OF CORROSION / REMOVED CORROSION ON RA DOOR SUPPORT ANGLE IAW SRM 51-10-02-0G-0. 100% MATERIAL LOSS. OUT OF LIMITS IAW SRM 53-10-15-1A-2 REMOVED AND REPLACED ANGLE IAW SRM 51-40-02-0G-0 AND BOEING DWG # 141A8312 REV E.

Part: STRINGER CLIP — CRACKED (BS 309) · airframe 69,547 hrs · 41,754 cycles

FUSELAGE STRINGER CLIP CRACKED AT BS 309.9, STRINGER 13L. R & R THE STRINGER CLIP IAW EA.

Part: WEB — CORRODED (BS 847-867) · airframe 69,547 hrs · 41,754 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 847 TO 867. REPAIRED THE WEB IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,547 hrs · 41,754 cycles

LT CREASE BEAM WEB CORRODED BETWEEN BS 727E TO BS 747. R&R WEB IAW DWG AND SRM.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 69,547 hrs · 41,754 cycles

LEFT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL IS CRACKED. / REMOVED AND REPLACED LH HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL IAW B737-700 AMM 53-31-31-400-801.

Part: SHIELD — CORRODED (BS 767-794) · airframe 69,547 hrs · 41,754 cycles

AFT CARGO BAY FORWARD SHIELD CORRODED BETWEEN BS 767 TO 794, RBL 21. R & R THE SHIELD IAW SRM AND DWG.

Part: STIFFENER — BROKEN (HORZONTAL STAB) · airframe 69,547 hrs · 41,754 cycles

RIGHT HORIZONTAL STABILIZER INSPAR RIB HSS 230.70, FIRST VERTICAL STIFFENER BROKEN. REPAIRED THE STIFFENER IAW EA.

Part: ATTACH ANGLE — CORRODED (BS 727D) · airframe 69,547 hrs · 41,754 cycles

AFT CARGO BAY LT FRAME SIDEWALL ATTACH ANGLE CORRODED AT BS 727D, BETWEEN STRINGERS 24L TO 25L. R & R THE ATTACH ANGLE IAW SRM AND DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,547 hrs · 41,754 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB LEADING EDGE, HSS 105.26 CRACKED. R & R THE RIB ASSEMBLY IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,547 hrs · 41,754 cycles

AFT CARGO PIT LT Z ANGLE CORRODED BETWEEN BS 727B+2 TO BS 847, LBL 21. R&R Z ANGLE IAW SRM AND DWG.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 69,547 hrs · 41,754 cycles

RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL IS CRACKED / REMOVED AND REPLACED RH HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL IAW B737-700 AMM 53-31-31-400-801.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,547 hrs · 41,754 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB, LEADING EDGE HSS 114.55 CRACKED. R & R THE RIB ASSEMBLY IAW SRM AND DWG.

Part: BULKHEAD — ELONGATED (AFT CARGO BAY) · airframe 69,547 hrs · 41,754 cycles

AFT CARGO PIT FORWARD BULKHEAD RIGHT LOWER CHORD STA 727+4 RBL21 BOTTOM FASTENER HOLE IS ELONGATED / AFT CARGO PIT FWD BULKHEAD RH LWR CHORD STA 727 HAS ELONGATED HOLE. REPLACED CHORD FABRICATED ON SMAL PO 1526476L2 BOAG DWG 144A9401 REV A. INSTALLED IAW SRM 51-40-02 AND BOEING DWG 144A2600 REV-

Part: ANGLE — CRACKED (BS 947) · airframe 69,547 hrs · 41,754 cycles

AFT CARGO BAY RIGHT BAFFLE ANGLE CRACKED AT BS 947. R & R THE ANGLE IAW DWG AND SRM.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 69,547 hrs · 41,754 cycles

AFT CARGO PIT RIGHT Z-ANGLE STA 727B-2 TO 767 RBL21 HAS CORROSION AROUND FASTENER HOLES / REMOVED CORROSION ON RIGHT Z ANGLE IN AFT CARGO PIT STA 727 B-2' TO STA 767; RBL21 AND FOUND MATERIAL LOSS OUT OF LIMITS IAW B737 SRM 53-00-53-1A-2. ORIG T=.040' REM. T=.030'; MAT LOSS =.010' REMOVED AND REPLACED Z ANGLE FROM STA 727 TO 767 IAW B737 SRM 51-40-02-0G-0 AND BAE DWG: 146A7500; REV-.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 69,547 hrs · 41,754 cycles

AFT CARGO PIT RIGHT Z-ANGLE STA 887+4 TO 907+7 RBL23 HAS CORROSION AROUND FASTENER HOLES / REMOVED CORROSION ON RIGHT Z ANGLE IN AFT CARGO PIT STA 887+4' TO 907+7' AND REPLACED Z ANGLE FROM STA 887 TO STA 947 IAW B737 SRM 51-40-02-0G-0 AND BAR DWG 147A7501; REV A. ORIG T=.240'; REV.T=.027'; MAT LOSS =.013'.

Part: PANEL — ELONGATED (RT WING) · airframe 69,547 hrs · 41,754 cycles

RIGHT WING LEADING EDGE PANEL 621LB HAS AN ELONGATED HOLE (MARKED) N / REPAIRED AND APPLIED DECORATIVE FINISH TO RIGHTR WING LEADING EDGE PANEL 621LB OF ELONGATED HOLE IAW B737 SRM 51-70-04-2R-9 REV 63 AND B737

Part: NUT PLATE — BROKEN (FWD CARGO BAY) · airframe 69,547 hrs · 41,754 cycles

FORWARD CARGO PIT DOOR SURROUND FRAME STA 492 BETWEEN STR 20R-21R INNER FLANGE NUTPLATE STRAP IS BROKEN OFF / FWD CARGO PIT POOR SURROUND FRME STA 492 BETWEEN STR-20R-21R NUT PLATE STRIP CRACKED. REPLACED NUT PLATE STRIP FABRICATED FROM SMAL SRV RG #0220151310 AND DWG 143A8200 REV IT. INSTALLED NEW NUTPLATE STRIP IAW BOEING DWG 143A8200 REV H AND SRM 57-40-C2

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 69,547 hrs · 41,754 cycles

RIGHT WING PANEL 651GB, SEAL SUPPORT BRACKET CRACKED. R & R THE SUPPORT BRACKET IAW SRM.

Part: BULKHEAD — CRACKED (BS 663) · airframe 69,547 hrs · 41,754 cycles

RIGHT MAIN WHEEL WELL VERTICAL BULKHEAD CRACKED AT BS 663. REPAIRED THE BULKHEAD IAW SRM.

Part: RIB — CRACKED (LT MLG DOOR) · airframe 67,656 hrs · 40,527 cycles

LT MAIN GEAR CENTER DOOR VERTICAL RIB CRACKED 4 INCHES ABOVE LOWER AFT ATTACH POINT. R&R LT DOOR ASSEMBLY AMM.

Part: BRACKET — CRACKED (RT WING) · airframe 67,653 hrs · 40,525 cycles

RIGHT WING BRACKET CRACKED INBOARD SIDE OF FIXED TRAILING EDGE DEFLECTION SUPPORT BEAM. R & R THE BRACKET ASSEMBLY IAW SRM.

Part: FLANGE — BROKEN (LT WING) · airframe 67,653 hrs · 40,525 cycles

LEFT WING FIXED TRAILING EDGE UPPER PANEL SUPPORT BEAM FLANGE BROKEN WHERE RETAINER BOLTS AND SERRATED PLATE ASSEMBLY ATTACH. / REPAIRED PER SRM 57-51-02.

Part: ANGLE — CRACKED (LT WING) · airframe 67,653 hrs · 40,525 cycles

LEFT WING FIXED TRAILING EDGE UPPER PANEL WEB L ANGLE CRACKED AT SUPPORT BEAM ATTACH FASTENERS. / REPAIRED PER SRM 51-40-02.

Part: FITTING — DIRTY (R1 DOOR) · airframe 66,048 hrs · 39,535 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK DIRTY. CLEANED CLIPS PER SIP.

Part: RETAINING CLIP — LOOSE (R1 DOOR) · airframe 63,848 hrs · 38,226 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR LOOSE. SECURED CLIPS IAW MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 63,423 hrs · 37,974 cycles

AFT RT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 63,423 hrs · 37,974 cycles

AFT LT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 63,335 hrs · 37,925 cycles

L1 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW MM & MT.

Part: SKATE ANGLE — CRACKED (RT PYLON) · airframe 63,301 hrs · 37,901 cycles

RIGHT PYLON OTBD STRUT, FWD FAIRING STRUCTURE SKATE ANGLE, CRACKED AT NAC, STATION 235. REPAIRED SKATE ANGLE IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,301 hrs · 37,901 cycles

FRAME CRACKED AT BS 500D, BETWEEN STRINGER 18R - 20R. R & R FRAME IAW SRM & DWG.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 63,301 hrs · 37,901 cycles

PRESSURE DECK HORIZONTAL WEB, CRACKED AT BS 663.75, LBL 32. REPAIRED WEB IAW EA.

Part: ANGLE — CRACKED (RT WING) · airframe 63,301 hrs · 37,901 cycles

RIGHT WING TE ANGLE CRACKED, AT RSS 133, UPPER CHORD. R & R ANGLE IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,301 hrs · 37,901 cycles

WEB CRACKED, BETWEEN BS 344 - 360, BL 0. R & R WEB IAW DWG & SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,301 hrs · 37,901 cycles

WEB CRACKED, BETWEEN BS 344 - 360, LBL 11. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,301 hrs · 37,901 cycles

WEB CRACKED BETWEEN BS 277 - 294.5, BL 0. R & R WEB IAW DWG & SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,301 hrs · 37,901 cycles

WEB CRACKED, BETWEEN BS 312 - 328, LBL 46. R & R WEB IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,301 hrs · 37,901 cycles

WEB CRACKED BETWEEN BS 312 - 328, RBL 31. R & R WEB IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,301 hrs · 37,901 cycles

WEB CRACKED BETWEEN BS 344 - 360, RBL 12. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,301 hrs · 37,901 cycles

WEB CRACKED BETWEEN BS 328 - 344, LBL 46. R & R WEB IAW SRM & DWG.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,301 hrs · 37,901 cycles

FLOORBEAM CRACKED AT BS 294.5, RBL 51. REPAIRED FLOORBEAM IAW EA.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 63,301 hrs · 37,901 cycles

LEFT KEEL BEAM BRACKET CRACKED AT BS 540+2. R & R BRACKET IAW SRM.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,301 hrs · 37,901 cycles

AFT CARGO COMPARTMENT TRACK CORRODED, BETWEEN BS 747 - 887, RBL 13.84. REPAIRED CARGO TRACK IAW SRM.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 63,301 hrs · 37,901 cycles

AFT CARGO COMPARTMENT, TRACK CRACKED AT BS 727E, STRINGER 26R. REPAIRED TRACK IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,301 hrs · 37,901 cycles

FORWARD CARGO COMPARTMENT ANGLE, CRACKED AT BS 500C, STRINGER 26L. R & R ANGLE IAW SRM.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 63,301 hrs · 37,901 cycles

FORWARD CARGO COMPARTMENT, TRACK CRACKED AT BS 500, RBL 13.8. REPAIRED CARGO TRACK IAW SRM & DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,301 hrs · 37,901 cycles

LEFT WING NR 1 SLAT SKIN CRACKED ON LE AT STATION 451.97. REPAIRED SKIN IAW EA.

Part: ENGINE — FAILED (LEFT) · airframe 63,215 hrs · 37,847 cycles

AIR TURN BACK, IN FLIGHT SHUTDOWN, DECLARED EMER. NR 1 ENG FAILURE. R & R NR 1 ENG IAW MT.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 63,115 hrs · 37,790 cycles

APU DETECTION LIGHT ILLUMINATED IN FLIGHT. R & R ENG & APU FIRE CONTROL PANEL IAW AMM.

Part: COVER — BROKEN (CABIN) · airframe 62,301 hrs · 37,320 cycles

R1 SERVICE DOOR EXIT INDICATOR LIGHT COVER BROKEN. R & R INDICATOR IAW MM.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 60,364 hrs · 36,229 cycles

LEFT PHOTO LUMINESCENT STRIPS CRACKED AT ROW 1. R & R STRIPS IAW MM.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 60,364 hrs · 36,229 cycles

RIGHT PHOTO LUMINESCENT STRIPS CRACKED AT ROW 1. R & R STRIPS IAW MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 60,070 hrs · 36,050 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,108 hrs · 35,504 cycles

LEFT BULLNOSE EMER LIGHT INOPERATIVE AT ROW 6. RELAMPED LIGHT IAW MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 58,286 hrs · 35,016 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 58,286 hrs · 35,016 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 57,535 hrs · 34,570 cycles

FORWARD ENTRY LOWER EMER EXIT LIGHT BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 56,610 hrs · 34,029 cycles

LEFT EMERGENCY EXIT BULLNOSE LIGHT INOPERATIVE AT ROW 17. RECONNECTED CONNECTOR IAW WDM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 56,610 hrs · 34,029 cycles

STIFFENER CRACKED AT BS 663, LBL 27. REPAIRED STIFFENER IAW SRM & DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 56,610 hrs · 34,029 cycles

STRINGER CLIP CRACKED AT STATION 360, STRINGER 8R. R & R CLIP IAW SRM.

Part: SPAR — CRACKED (LT WING) · airframe 56,610 hrs · 34,029 cycles

LT WING FWD LOWER SPAR CRACKED AT WS 254 LOWER ROW OF VERTICAL FLANGE JUST OTBD OF RIB 7. R & R SPAR IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 56,610 hrs · 34,029 cycles

STIFFENER CRACKED AT STATION 663 FWD BULKHEAD, LBL 5. R & R STIFFENER IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 56,610 hrs · 34,029 cycles

LEFT HORIZONTAL STABILIZER STATION 129.50 RIB CRACKED ON LOWER FLANGE AT AFT RT FASTENER HOLE COMMON TO REAR SPAR. REPAIRED RIB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,610 hrs · 34,029 cycles

FUSELAGE FRAME CRACKED AT STATION 787, STRINGER 8R. REPAIRED FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,610 hrs · 34,029 cycles

FUSELAGE FRAME CRACKED AT STATION 440, STRINGER 8R. REPAIRED FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,610 hrs · 34,029 cycles

FUSELAGE FRAME CRACKED AT STATION 480, STRINGER 8R. REPAIRED FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,610 hrs · 34,029 cycles

FRAME CRACKED AT BS 500A, STRINGER 8R. REPAIRED FRAME IAW ER & EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 56,610 hrs · 34,029 cycles

RT HAND HORIZONTAL STABILIZER RIB AT STATION 92.70, NR 1 & NR 2 VERTICAL STIFFENERS CRACKED. REPAIRED RIB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,610 hrs · 34,029 cycles

FRAME CRACKED AT BS 440, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,610 hrs · 34,029 cycles

FRAME CRACKED AT BS 380, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,610 hrs · 34,029 cycles

FUSELAGE FRAME CRACKED AT STATION 867, STRINGER 8R. REPAIRED FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,610 hrs · 34,029 cycles

FUSELAGE FRAME CRACKED AT STATION 500A, STRINGER 8L. REPAIRED FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,610 hrs · 34,029 cycles

FUSELAGE FRAME CRACKED AT STATION 400, STRINGER 8R. REPAIRED FRAME IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,610 hrs · 34,029 cycles

FUSELAGE FRAME CRACKED AT STATION 360, STRINGER 8R. REPAIRED FRAME IAW SWA EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 56,610 hrs · 34,029 cycles

MAIN WW PRESS WEB CRACKED AT BS 665, RBL 40. REPAIRED WEB IAW SWA & EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 56,610 hrs · 34,029 cycles

MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, LBL 40. REPAIRED WEB IAW SRM.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 56,610 hrs · 34,029 cycles

LT COCKPIT NR 3 E - F WINDOW POST CRACKED AT 2ND FASTENER FROM BOTTOM. REPAIRED POST IAW ER & EA.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 56,610 hrs · 34,029 cycles

RT NR 3 E - F WINDOW POST CRACKED AT 2ND FASTENER HOLE FROM BOTTOM. REPAIRED POST IAW ACO.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,610 hrs · 34,029 cycles

RT WING NR 7 SLAT NOSE SKIN CRACKED AT THE ACTUATOR RIB. REPAIRED SKIN IAW SRM.

Part: FITTING — CRACKED (RT MLG WW) · airframe 55,616 hrs · 33,438 cycles

"B" SYSTEM HYDRAULIC QUANTITY AT REFILL, FOUND HYDRAULIC LEAK RT WW CEILING AFT. FOUR WAY HYDRAULIC CROSS FITTING CRACKED. R & R FITTING IAW SIP.

Part: LENS — MISSING (CABIN) · airframe 55,127 hrs · 33,147 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS IAW MM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 54,166 hrs · 32,610 cycles

INTERCOSTAL UPPER ANGLE CRACKED BETWEEN STA 380 TO STA 400, BL 0. R & R ANGLE IAW DWG AND SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,166 hrs · 32,610 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,166 hrs · 32,610 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,166 hrs · 32,610 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 54,166 hrs · 32,610 cycles

RIGHT EMERGENCY BULLNOSE LIGHT AT ROW 3 LOOSE. R & R LENS IAW AMM.

Part: LENS — LOOSE (CABIN) · airframe 54,166 hrs · 32,610 cycles

RIGHT EMERGENCY BULLNOSE LIGHT AT ROW 8 LOOSE. R & R LENS IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 53,204 hrs · 32,006 cycles

FAILED CAPACITY CHECK OUT PER 733-055-00-01. REMOVED AFT LEFT BATTERY PACK AT MW MO1673 & AFT RIGHT BATTERY PACK AT MW MO1672 AND REPLACED AT SAME LOCATION WITH NEW BATTERY PACK PER AMM. LEFT AFT AT MW MO1673 S/N OFF:26481, S/N ON:36937. SAME P/N

Part: HOOK — LOOSE (L1 DOOR) · airframe 52,171 hrs · 31,358 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM.

Part: OVERHEAT SENSOR — FAULTY (RT PYLON) · airframe 51,915 hrs · 31,195 cycles

DIVERSION -- RIGHT WING-BODY OVERHEAT ILLUMINATED ON CLIMBOUT, AFTER RIGHT SIDE ISOLATED WITH RIGHT PACK AND BLEED OFF WING BODY OVERHEAT EXTINGUISHED. REMOVED AND REPLACED RIGHT PYLON STRUT OVERHEAT DETECTOR PER MM.

Part: COVER — BROKEN (CABIN) · airframe 51,640 hrs · 31,028 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER AMM.

Part: LIGHT — CRACKED (CABIN) · airframe 50,791 hrs · 30,525 cycles

FWD EEPLS CRACKED. REMOVED AND REPLACED EEPLS PER M/M.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 50,487 hrs · 30,342 cycles

F/O'S COCKPIT WINDOW POST CRACKED. REMOVED AND REPLACED WINDOW POST PER BAC DRAWING & SRM.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 50,487 hrs · 30,342 cycles

COCKPIT LT WINDOW POST CRACKED. REMOVED AND REPLACED WINDOW POST PER SRM & BAC DRAWING.

Part: SIGN — BROKEN (R1 DOOR) · airframe 50,100 hrs · 30,113 cycles

R1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER M/M.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 50,090 hrs · 30,108 cycles

R2 DOOR LOWER EGRESS LIGHT LENS BROKEN. REMOVED AND REPLACED LENS ASSY PER AMM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 50,013 hrs · 30,063 cycles

R1 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 49,945 hrs · 30,024 cycles

EMERGENCY EXIT SIGN LENS BY FORWARD ENTRY DOOR IS BROKEN. REPLACED LENS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 49,058 hrs · 29,494 cycles

DURING SCHEDULED HC1 CHECK, LT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 49,058 hrs · 29,494 cycles

DURING SCHEDULED HC1 CHECK, RT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 48,175 hrs · 28,957 cycles

AFT GALLEY EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 47,266 hrs · 28,447 cycles

DURING SCHEDULED HC2 CHECK FOUND, RT HORIZONTAL STAB LOWER INSPAR SKIN CRACKED AT STA 101.9. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 47,071 hrs · 28,326 cycles

AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LENS — MISSING (CABIN) · airframe 45,530 hrs · 27,413 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 43,288 hrs · 26,081 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,288 hrs · 26,081 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM T-CAP CORRODED AT BS 967, LBL 5. REPAIRED T-CAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,288 hrs · 26,081 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM T-CAP CORRODED AT BS 967, RBL 5. REPAIRED T-CAP PER SRM.

Part: FLOORBEAM — CORRODED (CARGO BAY) · airframe 43,288 hrs · 26,081 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM CORRODED BETWEEN BS 793 TO BS 827, RBL 13.5. REPAIRED BEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 43,288 hrs · 26,081 cycles

DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM ANGLE CORRODED BETWEEN BS 967 TO BS 986.5. REPAIRED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (CARGO BAY) · airframe 43,288 hrs · 26,081 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO FLOORBEAM LOWER SURFACE CORRODED AT BS 772, RBL 14. REPAIRED BEAM PER EA.

Part: LENS — LOOSE (CABIN) · airframe 42,932 hrs · 25,866 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LOOSE AT ROW 8. SECURED LENS PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 41,707 hrs · 25,154 cycles

R1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,402 hrs · 23,173 cycles

DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT 3 DEF. REMOVED AND REPLACED LIGHT PER MM.

Part: SIGN — LOOSE (EMERGENCY LIGHT) · airframe 38,078 hrs · 22,968 cycles

MID CABIN OVERHEAD EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 36,076 hrs · 21,756 cycles

DURING SCHEDULED HC1 CHECK, FWD RIGHT CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 31,134 hrs · 18,852 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 31,134 hrs · 18,852 cycles

DURING SCHEDULED HC1 CHECK, LT OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 31,134 hrs · 18,852 cycles

DURING SCHEDULED HC1 CHECK, LT AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 31,134 hrs · 18,852 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT MLG FWD W/W STIFFENER CRACKED. REMOVED AND REPLACED MLG STIFFENER PER SRM.

Part: BATTERY — FAILED (CABIN) · airframe 31,134 hrs · 18,852 cycles

DURING SCHEDULED HC1 CHECK, LT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FLOORBEAM — CORRODED (BS 772) · airframe 29,487 hrs · 17,899 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT BS 772, RBL 2.5. REPAIRED FLOORBEAM PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 24,566 hrs · 15,086 cycles

FWD GALLEY SERVICE DOOR LOWER EMERGENCY EXIT LIGHT COVER, LOOSE. REINSTALLED COVER PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 24,176 hrs · 14,872 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EVACUATION SLIDE OUT OF ADJUST. RE-ADJUSTED SLIDE ASSY PER MM.

Part: HOOK — LOOSE (L1 DOOR GIRT BAR) · airframe 24,176 hrs · 14,872 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR STOW HOOK LOOSE. SECURED GIRT BAR STOW HOOK PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 23,807 hrs · 14,666 cycles

EEPLS COVER AT ROW 7 DEF AND ROW 8 DEF, LOOSE. SECURED EEPLS COVER PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 23,675 hrs · 14,604 cycles

L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,121 hrs · 13,748 cycles

DURING SPV, FOUND RT OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 22,025 hrs · 13,696 cycles

DURING SPV, FOUND RT OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,995 hrs · 13,680 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT LT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED AFT LT BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (PAX DOOR) · airframe 19,627 hrs · 12,375 cycles

DURING SCHEDULED A CHECK, FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 19,313 hrs · 12,184 cycles

OVERHEAD BIN BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW NR 1 ABC. SECURED LENS PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 16,980 hrs · 10,903 cycles

DURING SCHEDULED PM CHECK, FOUND EMERGENCY FLASHLIGHT INOP AT FWD CABIN. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 16,961 hrs · 10,894 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (AFT ENTRY DOOR) · airframe 16,961 hrs · 10,894 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: COVER — MISSING (CABIN) · airframe 16,446 hrs · 10,578 cycles

DURING SCHEDULED RON, FOUND EEPLS COVER MISSING AT ROW NR 6. INSTALLED COVER PER MM.

Part: ENGINE — FLAMED OUT (RIGHT) · airframe 16,159 hrs · 10,408 cycles

INFIGHT SHUTDOWN, DECLARED EMERGENCY, AIR TURNBACK, DURING CLIMB NR 2 ENGINE FLAMED OUT. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 12,432 hrs · 8,260 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED ( 19 EA ) IN CABIN. R&R EEPLS COVERS PER MM.

Part: SHAFT — WORN (ELEVATOR) · airframe 11,230 hrs · 7,547 cycles

DURING SCHEDULED C4 CHECK, RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR OUTPUT SHAFT PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 11,230 hrs · 7,546 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT ENTRY & AFT SVC DOORS EMERGENCY EVAC SLIDE GIRT ASSY OUT OF AJUSTMENT. ADJUSTED EMERGENCY EVAC SLIDE GIRT ASSY''''S PER MM.

Part: TRACK — BROKEN (CABIN) · airframe 11,230 hrs · 7,546 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK LOOSE AT FWD CABIN AND EEPLS COVER BROKEN AT ROW 11. SECURED EEPLS AND INSTALLED EEPLS COVER PER MM.

Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 11,230 hrs · 7,546 cycles

DURING SCHEDULED C4 CHECK, FOUND FWD SVC & FWD ENTRY DOORS EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUSTMENT. ADJUSTED EMERGENCY EVAC SLIDE GIRT ASSY''S PER MM.

Part: COVER — CRACKED (CABIN) · airframe 10,235 hrs · 6,953 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER CRACKED AT FWD SECTION. REMOVED AND REPLACED TRACK COVER PER MM.

Part: ACTUATOR — DEFECTIVE (NLG) · airframe 9,689 hrs · 6,611 cycles

AIR TURNBACK DURING T/O, NOSE GEAR WOULD NOT RETRACT WITH GEAR HANDLE PLACED IN UP POSITION. FWD PANEL INDICATES NOSE GEAR GREEN LIGHT & RED UNSAFE LIGHT. AFT OVERHEAD LIGHT SHOWS NOSE GEAR GREEN LIGHT ONLY. PERFORMED PSEU BITE CHECK, NO FAULTS FOUND. PERFORMED NOSE GEAR RETRACTION CHECK, OPS CHECK NORMAL PER MM. AT LAS, R&R NLG LOCK ACTUATOR AS PRECAUTIONARY MEASURE.

Part: FITTING — CRACKED (RT MLG WW) · airframe 8,239 hrs · 5,714 cycles

DURING SCHEDULED C1 CHECK, FOUND WING TO BODY FAIRING CASTING IN AFT O/B RIGHT W/W CRACKED. REPAIRED PER SWA RA.

Part: LIGHT — CRACKED (ROW 2,12,&22)

DURING SCHEDULED BC2 CHECK, FOUND EEPLS STRIPS CRACKED AT ROWS 2, 12, 22. REMOVED AND REPLACED LIGHT STRIPS PER MM.

Part: FUEL PUMP — FAILED (NR 1 ENGINE)

ENG NR 1 FAILED ON TAXI-OUT APPROXIMATELY 3 MIN AFTER ROLL BACK ON ENG NR 2. SOURCE OFF LT NR 1 ILLUMINATED MASTER CAUTION, LOCKED DOWN ENGINE INDIC AND SAW ENG FAIL ON NR 1. NO OTHER UNUSUAL INDICATIONS. REMOVED AND REPLACED NR 1 ENGINE FUEL PUMP AND HMU ASSY PER M/M. ENG RUN OP CK GOOD.