N725SW

Part: STRIP — DETACHED (CABIN) · airframe 77,249 hrs · 45,656 cycles

EGRES STIP DETACHED ; / [01] REATTACHED EGRESS STRIP IAW AMM 33-51-15.ALL WORK PERFORMED BY 72111.

Part: VALVE — LOOSE (#1 ENGINE) · airframe 77,088 hrs · 45,567 cycles

SUPPLEMENTAL INFORMATION: HYDRAULIC QTY DROPPED 1% EVERY 2 MINUTES. LANDED WITH 50% HYDRAULIC QTY IN SYSTEM A ; / [01] FOUND A SYSTEM HYDRAULIC RETURN LINE FROM #1 ENG TR ISOLATION VALVE LOOSE. RE TORQUED PER AMM 20-50-11; NO LEAKS NOTED. SERVICED A SYSTEM HYDRAULICS PER AMM 12-12-00.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 76,400 hrs · 45,155 cycles

EMERGENCY SLIDE FWD ENTRY DOOR NEEDS READJUSTING ; / [01] READJUSTED FWD ENTRY SLIDE SKIRT PER. SIP AMM

Part: HANDLE — UNSECURE (R1 DOOR) · airframe 75,785 hrs · 44,804 cycles

FRONT SERVICE DOOR MANUAL RELEASE HANDLE FLAP NOT CORRECTLY STOWED. / RE-SECURED FRONT SERVICE DOOR MANUAL RELEASE HANDLE PER S.I.P.

Part: LIGHT — LOOSE (CABIN) · airframe 75,070 hrs · 44,385 cycles

FLOOR TACK LIGHTING NEAR SEAT 1C IS LIFTING FROM THE FLOOR. RESECURED FLOOR TRACK LIGHTING, PER SIP.

Part: NUT PLATE — BROKEN (LT WING) · airframe 74,837 hrs · 44,257 cycles

LEFT WING PANEL 521GB NUTPLATE CHANNEL BROKEN AT FASTENER LOCATION ALONG AFT EDGE OF PANEL; THIRD FASTENER FROM INBOARD / REMOVED AND REPLACED BROKEN NUTPLATE CHANNEL PER SRM 51-40-02

Part: RIB — CRACKED (VERTICAL STAB) · airframe 74,711 hrs · 44,181 cycles

DORSAL FIN FWD SUPPORT ATTACH RIB CRACKED / REMOVED AND REPLACED 1 EACH RIB AT DORSAL FIN FWD SUPPORT PER B737-700 SRM 51-40-02-0G-0

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 74,711 hrs · 44,181 cycles

LEFT WING REAR SPAR FIXED TRAILING EDGE LOWER SUPPORT BRACKET 2EA CRACK & SHEARED RIVETS INB .& OUB. OF PYLON LOWER FIXED FAIRING TIP MKD DOTS 60-003 / REMOVED AND REPLACED BRACKETS I/B AND O/B ;AT LEFT WING REAR SPAR FIXED T/E LOWER SUPPORT PYLON LOCATION AS PER REF B737-700 SRM 51-40-02-0G-0 (SL 16697)

Part: SUPPORT ANGLE — CRACKED (R/H WING) · airframe 74,711 hrs · 44,181 cycles

RIGHT WING ACCESS PANEL 651GB SUPPORT ANGLE;SHOW SIGNS OF SURFACE CRACK AT UPPER INB AREA.(MKD 26-002) / REMOVED AND REPLACED SUPPORT ANGLE P/N 115A2752-18 AT RT WING ACCESS PANEL 651 GB PER B737-700 SRM 51-40-02-0G-0

Part: ATTACH ANGLE — CRACKED (RT WING TE) · airframe 74,711 hrs · 44,181 cycles

RT WING T/E DEFLECTOR CONTROL RIB I/B ATTACH ANGLE CRACKED. / REMOVED AND REPLACED ANGLE AT R/WING T/E DEFLECTOR CONTROL RIB I/B ATTACH AS PER SRM 51-40-02-0G-0. MG 443 10/21/2020

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 74,553 hrs · 44,078 cycles

EMERGENCY PULL HANDLE NOT COVERED ON FORWARD SERVICE DOOR. RE-PACKED FORWARD SERVICE DOOR SLIDE, PER MT 725-61-06.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 74,553 hrs · 44,078 cycles

EMERGENCY PULL HANDLE NOT COVERED ON FORWARD GALLEY DOOR (ENTRY). RE-PACKED FORWARD ENTRY AND GALLEY SLIDES, PER MT 725 -61-06.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 74,009 hrs · 43,728 cycles

LH STA. 540 FRAME FITTING; SOB SLOT FILLET SEALANT AND VAPOR BARRIER IS FOUND TO BE INSUFFICIENT PER TASKCARD# 571-I-14608-NG STEPS 2.B.(1)(A) AND 2.B.(2)(A). SEALANT IS MISSING WITH VOIDS AND VAPOR BARRIER IS CRACKERD. NOT TO LEVEL SHOWN IN TASKCARD. / WORK PERFORMED BY TANK TIGER' REPAIR. REFERENCE MT 5710-E 1462 NG AND MT 5710-1-4608-NG.

Part: FITTING — CRACKED (RT MLG WW) · airframe 74,009 hrs · 43,728 cycles

RH STA. 540 FRAM FITTING; SOB SLOT FILLET SEALANT AND VAPOR BARRIER IS FOUND TO BE INSUFFICIENT PER TASK CARD # 5710-I-14608-NG STEPS 2.B.(3)(A) AND 2.B.(4)(A). SEALANT IS MISSING AND VAPOR BARRIER IS CRACKED. NOT TO LEVEL SHOWN IN TASKCARD. / WORK PERFORMED BY 'TANK TIGER' REPAIR W.O# 1202R545 AND M/M 28-11-00. REFERENCE MT 5710-E-14623-NG; MT 5710-I-4608-NG

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,821 hrs · 43,607 cycles

R1 DOOR SIDE EMERGENCY LIGHTS INOP / R&R BATTERY PACK REF AMM 33-51-04 OPS CHECK NORMAL

Part: BATTERY — FAILED (CABIN) · airframe 71,866 hrs · 42,344 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 71,866 hrs · 42,344 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669. R&R BATTERY PER AMM.

Part: WEB — CRACKED (R/H WING) · airframe 71,866 hrs · 42,344 cycles

RIGHT WING ANGLED WEB SUPPORT COMMON TO INBOARD SIDE OF DEFLECTION CONTROL RIB CRACKED / REMOVED AND REPLACED RIGHT WING ANGLED WEB SUPPORT COMMON TO INBOARD SIDE OF DEFLECTION CONTROL RIB PER SRM 51-40-02

Part: LIGHT — LOOSE (CABIN) · airframe 71,369 hrs · 42,031 cycles

LT EMERGENCY ELECTRIC LIGHT STRIP LOOSE BETWEEN ROW 7 TO ROW 8. CLEANED AND REATTACHED PHOTO STRIP AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 70,632 hrs · 41,567 cycles

LT EMERGENCY AISLE LIGHTENING LOOSE AT ROW 8. SECURED LIGHT PER SIP.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 69,621 hrs · 40,909 cycles

LOWER BULKHEAD STIFFENER CRACKED AT BS 663, LBL 5. R&R STIFFENER IAW SRM & DWG.

Part: WEB — CORRODED (LEFT WING) · airframe 69,621 hrs · 40,909 cycles

PRIORITY LEVEL 1: L/H WING; REAR SPAR WEB; TANK 1 AFT BOOST PUMP LOCATION; CORROSION FOUND AT LOWER BONDING JUMPER ATTACH POINT. MARKED IN RED. / REMOVED CORROSION ON L/H WING REAR SPAR WEB LOWER BOOST PUMP ATTACH POINT; VERIFIED MATERIAL LOSS; ORIGINAL MATERIAL IS .680. REMAINING IS .572 LOSS OF .108. OUT OF LIMITS IAW SRM 57-20-10-1A-3. REPARIED IAW AAR EA 180668 IR AND SWA EA 1-757-15739 REV IR.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,621 hrs · 40,909 cycles

STRINGER CLIP CRACKED AT BS 259+2, STR 6L. R&R CLIP IAW SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,621 hrs · 40,909 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT STA LEADING EDGE 114.55. R&R RIB IAW SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,621 hrs · 40,909 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT STA LEADING EDGE 114.55. R&R RIB IAW SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,621 hrs · 40,909 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT LEADING EDGE STA 96.96. R&R RIB IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,621 hrs · 40,909 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS 500D, STR 22L. R&R GUSSET IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,621 hrs · 40,909 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS 500D, STR 21L. R&R GUSSET IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 69,621 hrs · 40,909 cycles

CREASE BEAM INNER CHORD CORRODED AT BS 716, RBL 63. R&R CREASE BEAM IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,621 hrs · 40,909 cycles

LOWER CABIN SEAT TRACK SURFACE CORRODED AT BS 877, LBL 24.5. R&R SEAT TRACK PER DWG AND SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,621 hrs · 40,909 cycles

SEAT TRACK CORRODED BETWEEN BS 400 TO BS 480, LBL 44.5. REPAIRED SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 69,621 hrs · 40,909 cycles

CABIN SEAT TRACK LBL 44.5 BS 500C LOWER TRACK SURFACE CORRODED. / BLENDED AND REMOVED CORROSION ON SEAT TRACK AT STA 500C LBL 45 REMOVED .045' MATERIAL MAXIMUM ALLOWED .040' OUT OF LIMITS IAW SRM 53-00-52. REMOVED AND REPLACED SEAT TRACK FROM STA 480 TO STA 520 LBL 45 ON N/R X835151

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 69,621 hrs · 40,909 cycles

STRINGER CLIP CRACKED BETWEEN BS 208.25 TO BS 259, STR 12L. R&R CLIP IAW SRM AND DWG.

Part: FITTING — CORRODED (AFT CARGO BAY) · airframe 69,621 hrs · 40,909 cycles

AFT CARGO EQUIPMENT BAY INNER STRUCTURE STA 996 BETWEEN STR 24L AND 25L AT WATER DRAIN HAS SIGNS OF CORROSION. / EVALUATED CORROSION FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED SRM LIMITS. REMOVED AND REPLACED -18 FITTING PER SRM 51-40-02-0G-0 AND DWG 147A7443 REV B

Part: BEAM — CRACKED (R1 DOOR) · airframe 69,621 hrs · 40,909 cycles

R1 DOOR INTERNAL NR 4 LOWER BEAM CRACKED NEAR FORWARD-INBOARD FASTENER HOLE COMMON TO HANDLE BOX HOUSING. R&R NR 4 LOWER BEAM IAW EO, SRM, AND DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 69,621 hrs · 40,909 cycles

AFT CARGO COMPARTMENT BULKHEAD SUPPORT ATTACH ANGLE CRACKED AT BS 867, STR 26L. R&R ANGLE PER SRM.

Part: FLOOR PANEL — PULLED (CABIN) · airframe 69,621 hrs · 40,909 cycles

PASSENGER CABIN FLOOR PANEL 231ZF UPPER SURFACE HAS MULTIPLE LINES OF PULLED FIBERS. / FABRICATED FLOOR PANEL 231ZF PER SAMPLE ORIGINAL IAW B 737-700 SRM 53-00-50-2R-0 REV 66; BOE. DWG 144A5810 ID: 001 REV:- BAC5085 REV E 21-FEV-2018. CURED IN OVEN E0-01 1-18-19 FOR 1 HR @140F (WN1680) (A46012)(A93390)

Part: FLOOR PANEL — PULLED (CABIN) · airframe 69,621 hrs · 40,909 cycles

PASSENGER CABIN FLOOR PANEL 231XF UPPER SURFACE HAS MULTIPLE LINES OF PULLED FIBERS. / FABRICATED FLOOR PANEL 231XF PER ORIGINAL SAMPLE. IAW B737-700 SRM 53-00-50-2R-0 REV 66; BOE-DWG 144A5810-7; BAC5085 REV E 21FEC2018. CURED IN OVEN E0-01 1-18-19 FOR 1HR @140F (WN1680) (A46012) (A93390)

Part: FLOOR PANEL — PULLED (CABIN) · airframe 69,621 hrs · 40,909 cycles

PASSENGER CABIN FLOOR PANEL 241DF UPPER SURFACE HAS MULTIPLE LINES OF PULLED FIBERS. / FABRICATED FLOOR BOARD 241DF PER SAMPLE IAW SRM SRM 53-00-50-2R-0; PER DRAWING 144A5810-9 & BAC 5085. CURED IN OVEN E0-01 1-18-19 1HC 140 DEGREE

Part: FLOOR PANEL — PULLED (CABIN) · airframe 69,621 hrs · 40,909 cycles

PASSENGER CABIN FLOOR PANEL 242DF UPPER SURFACE HAS MULTIPLE LINES OF PULLED FIBERS. / FABRICATED FLOORBOARD 242DF PER SAMPLE IAW SRM 53-00-50-2R-0; PER DRAWING 144A5810-3 & BAC 5085; CURED IN OVEN F0-01; 1-18-19 FOR 1HR AT 140

Part: FLOOR PANEL — PULLED (CABIN) · airframe 69,621 hrs · 40,909 cycles

PASSENGER CABIN FLOOR PANEL 241AF UPPER SURFACE HAS MULTIPLE LINES OF PULLED FIBERS. / FABRICATED FLOORBOARD 241AF PER SAMPLE IAW SRM 53-00-50-2R-0 PER DRAWING 144A5810-8 AND BAC5085. CURED IN OVEN E0-01; 1-18-19 FOR 1 HR AT 140.

Part: FLOOR PANEL — CORRODED (FLIGHT DECK) · airframe 69,621 hrs · 40,909 cycles

FLIGHT COMPARTMENT PANEL 211AF UNDERSIDE HAS CORROSION AROUND THE EDGES AS MARKED. / REPLACED FLIGHT COMPARTMENT PANEL 211AF IAW BOEING DWG #141A0631 REV. D P/N 141A5133U15 ATAG#A58519 NO LIMITS PUBLISHED IN SRM.

Part: FLOOR PANEL — PULLED (CABIN) · airframe 69,621 hrs · 40,909 cycles

PASSENGER CABIN FLOOR PANEL 232RF HAS A LINE OF PULLED FIBERS. / FABRICATED FLOOR PANEL 232RF PER ORIGINAL SAMPLE IAW B737-700 SRM 53-00-50-2R-0 REV 66; BAC5085 REV E 21FEC2018; BOE. DWG 144A5810-4; CURED IN OVEN E001 1-18-19 FOR 1 HR @ 140F (A93390)(WN1680) (A46012)

Part: STRIP — CORRODED (FWD CARGO BAY) · airframe 69,621 hrs · 40,909 cycles

FWD CARGO COMPARTMENT #2 L/H FLOOR TO SIDEWALL CAP STRIP IS CORRODED (STA 435 TO STA 500A) / REPLACED CAP STRIP ON TABLE; PART #453A1611-11 ISSUE TAG# A54487 IAW AIPC 25-52-10-01 ITEM 80. CAP STRIP INSTALLED ON CARD NO. JPANEL-121-CLOSE

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 69,621 hrs · 40,909 cycles

RIGHT WING FUEL ACCESS PANELS; PANEL 633AB HAS AREA OF CORROSION [MARKED] / EVALUATED RIGHT WING FUEL ACCESS PANEL 633AB AREA OF CORROSION FOUND NO DAMAGE LIMITS GIVEN FOR PANEL SURFACE. ORDERED AND RECIEVED SERVICABLE PANEL FOR RIGHT WING FUEL ACCESS PANEL 633AB IAW B737 SRM 51-10-02-0G-0 STEP 9C AND IPC 28-11-11-02 ATAG# RH 0133

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,621 hrs · 40,909 cycles

RT HORIZONTAL STABILIZER LEADING EDGE PANEL 341B 9TH RIB FROM INBOARD CRACKED. R&R RIB IAW SRM AND DWG.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 69,621 hrs · 40,909 cycles

LT HORIZONTAL STABILIZER RIB AT STAB STATION 129.5, 3RD VERTICAL STIFFENER CRACKED. R&R STIFFENER IAW SRM & DWG.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 69,621 hrs · 40,909 cycles

LT WING OUTBOARD AFT FLAP DELAMINATED ON TOP SIDE AT INBOARD END. REPAIRED AFT FLAP IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 69,621 hrs · 40,909 cycles

LT STABILIZER COMPARTMENT DOOR BONDING WIRE ATTACH TO FRAME CORRODED AT BS 1040. R&R FRAME IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,621 hrs · 40,909 cycles

LT HORIZONTAL STABILIZER RIB AT STAB STATION 129.5 4TH VERTICAL STIFFENER CRACKED. R&R RIB IAW SRM & DWG.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 69,621 hrs · 40,909 cycles

LT MAIN LANDING GEAR HORIZONTAL PRESSURE DECK WEB CRACKED AT BS 665, LBL 31. REPAIRED WEB IAW EA.

Part: CARGO TRACK — CORRODED (AFT CARGO BAY) · airframe 69,621 hrs · 40,909 cycles

AFT CARGO COMPARMENT FLOOR SUPPORT UPPER SURFACE HAS CORROSION AT STA:927+7; LBL: 3. / REMOVED AND REPLACED -13 CARGO TRACK LBL 3 STA 927 TO FACTORY SPLICE AT STA 887 PER DWG 147A7500 REV - AND SRM 51-40-02-0G-0.

Part: PANEL — DELAMINATED (RT WING) · airframe 69,621 hrs · 40,909 cycles

RIGHT PYLON PANEL 441EL IS DELAMINATED AT LOWER CORNER / REPAIRED AND APPLIED DECORATIVE FINISH TO RIGHT PYLON PANEL 441EL AT LOWER CORNER IAW B737 SRM 51-70-04-2R-6; B737 AMM 51-21-72-370-801 AND B737 AMM 51-21-73-370-803 REV 67. A11445; A01035; A99165; A44703

Part: CARGO TRACK — CORRODED (AFT CARGO BAY) · airframe 69,621 hrs · 40,909 cycles

AFT CARGO COMPARTMENT; FLOOR SUPPORT HAS CORROSION AT STA 927+7; RBL:14 / REMOVED AND REPLACED -14 CARGO TRACK STA 947 TO FACTORY SPLICE AT STA 887 PER DWG 147A7500 REV - AND SRM 51-40-02-0G-0

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 69,621 hrs · 40,909 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT BS 787+3. R&R CARGO TRACK PER SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,621 hrs · 40,909 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS 500D, STR 19R. R&R GUSSET IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,621 hrs · 40,909 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,621 hrs · 40,909 cycles

FORWARD CARGO COMPARTMENT FLOOR STRUCTURE UNDER RT SIDE BAFFLE CLIP CRACKED AT BS 500C. R&R BAFFLE CLIP IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FWD CARGO BAY) · airframe 69,621 hrs · 40,909 cycles

FORWARD CARGO COMPARTMENT BILGE STA 500A TO 500B BL0 TFTS AIRPHONE ANTENNA SUPPORT HAS CORROSION / EVALUATED CORROSION ON FWD CARGO STA 500A-500B BL 0 TFTS AIRPHONE ANTENNA SUPPORT OUT OF LIMITS REPLACED W/ NEW SUPPORT IAW AIPC 53-42-00-24 REF ITEM 110 AND SRM 51-40-02-0G-0 APPLIED CIC AS NECESSARY IAW AMM 51-21-91-620-802

Part: PANEL — CRACKED (LT WING) · airframe 69,621 hrs · 40,909 cycles

LEFT WING #3 SLAT AT ACTUATOR ATTACH FITTING; COVE PANEL 523DB IS CRACKED. / REPLACED COVE PANEL AT #3 SLAT ACTUATOR AREA I-A-W B737-700 SRM 51-40-02-0G & BOEING DWG # 114A5030 TY : DWG REV:E; ID: 0003

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 69,621 hrs · 40,909 cycles

FORWARD CARGO COMPARTMENT AFT BULKHEAD LT SIDE BULKHEAD SUPPORT ANGLE CORRODED ON UPPER AND LOWER SURFACE. R&R ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 69,621 hrs · 40,909 cycles

AFT CARGO COMPARTMENT; RH 'Z' ANGLE AT STA. 727B+14; SCREW HOLE HAS CORROSION. / EVALUATED AFT CARGO R/H 'Z' ANGLE STA 727B+14 FOUND TO BE OUT OF LIMITS 100% MATERIAL LOSS I/A/W SRM 53-00-53-1A-2. FABRICATED AND INSTALLED NEW 'Z' ANGLE FROM STA 727-767 I/A/W SRM 51-40-02-0G-0 AND DWG 146A 7502 REV A. APPLIED CIC TO NEW 'Z' ANGLE I/A/W 51-21-91-620-802

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 69,621 hrs · 40,909 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT BS 767+5, RBL 8. R&R BEAM PER EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,621 hrs · 40,909 cycles

FORWARD CARGO COMPARTMENT FLOOR STRUCTURE LT SIDE Z-ANGLE CORRODED BETWEEN BS 425 TO BS 500D. R&R Z ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 69,621 hrs · 40,909 cycles

AFT CARGO COMPARTMENT LT "Z" ANGLE CORRODED BETWEEN BS 727D TO BS 727E. R&R "Z" ANGLE IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,621 hrs · 40,909 cycles

FORWARD CARGO COMPARTMENT FLOOR STRUCTURE UNDER LT SIDE Z-ANGLE BAFFLE CLIP CRACKED AT BS 500C. R&R BAFFLE CLIP IAW SRM AND DWG.

Part: ANGLE — CORRODED (FWD CARGO BAY) · airframe 69,621 hrs · 40,909 cycles

FORWARD CARGO COMPARTMENT FLOOR STRUCTURE R/H SIDE AFT SHIELD (Z-ANGLE) IS PUNCTURED AND CORRODED / REPLACED PUNCTURED SHIELD W/ NEW SHIELD P/N 143A8126U31 I/A/W BOEING DWG 143A0080 SHEET 6 AND SRM 51-40-02-0G-0. APPLIED CIC TO NEW PART AS NECCESSARY I/A/W AMM 51-21-91-620-802.

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 69,621 hrs · 40,909 cycles

AFT CARGO COMPARTMENT; RH FWD SHIELD FROM STA. 767 TO STA. 787 HAS CORROSION. / REMOVED AND REPLACED AFT CARGO FWD SHIELD PER DWG # 146A0081 REV C AND SRM 51-40-07-0G-0 STA 767 TO STA 792

Part: ANGLE — CORRODED (FWD CARGO BAY) · airframe 69,621 hrs · 40,909 cycles

FORWARD CARGO COMPARTMENT FLOOR STRUCTURE R/H SIDE Z-ANGLE HAS CORROSION STA 500A TO 500D / EVALUATED FWD CARGO R/H 'Z' ANGLE STA 500A-500D FOUND TO BE OUT OF LIMITS I/AW SRM 53-00-53-1A-2 USING AAR TOOL # 36646 CAL DUE 02OCT19. FABRICATED & INSTALLED NEW 'Z' ANGLE I/A/W SRM 51-40-02-0G-0 AND BOEING DWG 143A7501 SHEET 3 REV A. APPLIED CIC TO NEW 'Z' ANGLE STA 500A-500D I/A/W AMM 51--21-91-620-802.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 69,621 hrs · 40,909 cycles

AFT CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: PANEL — ELONGATED (RT WING) · airframe 69,621 hrs · 40,909 cycles

RIGHT WING LEADING EDGE PANEL 621XB HAS SCREW HOLE THAT IS ELONGATED. MARKED / REPAIRED AND APPLIED DECORATIVE FINISH TO RIGHT WING LEADING EDGE PANEL 621XB OF ELONGATED SCREWHOLE (AS MARKED) IAW B737-700 SRM 51-70-04-2R-9 REV 66 AND B737 AMM 51-21-99-300-01 REV 67 A33188; A35994; A11393; A44703

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 69,621 hrs · 40,909 cycles

AFT CARGO; LH SIDE FLOOR TO SIDEWALL CAP STRIPS HAVE CORROSION / REPLACED 3EA CAP STRIPS ON TABLE; PART #453A2611-8 453A2611-10 AND 453A2611-4 IAW AIPC 25-52-10-02 ITEM NUMBER 90;100 AND 105. CAP STRIPS CORROSION FOUND TO BE OUT OF LIMIT DUE TO NO PUBLISHED SRM LIMITS. CAP STRIPS INSTALLED ON CARD NO JPANEL-141-CLOSE

Part: SCUFF PLATE — CORRODED (AFT CARGO) · airframe 69,621 hrs · 40,909 cycles

AFT CARGO; AFT SCUFF PLATE HAS CORROSION / EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED SRM LIMITS. REPLACED SCUFF PLATE ON TABLE. SCUFF PLATE INSTALLED ON WORK INSTRUCTION NO. 753-140-00-02Y

Part: SPLICE STRAP — CORRODED (AFT CARGO BAY) · airframe 69,621 hrs · 40,909 cycles

AFT CARGO; FLOOR SPLICE STRAP AT STA 727D HAS CORROSION ON UPPER AND LOWER SURFACE. / AFT CARGO FLOOR SPLICE STRAP @ STA 727D CORROSION OUT OF LIMIT DUE TO NO PUBLISHED LIMITS IN SRM. REPLACED STRAP ON TABLE; PART # 146A9401-8 ISSUE TAG# A54494 IAW AIPC 53-42-11-30 ITEM 5. STRAP INSTALLED ON CARD # JPANEL-141-CLOSE

Part: SPLICE STRAP — CORRODED (AFT CARGO BAY) · airframe 69,621 hrs · 40,909 cycles

AFT CARGO; FLOOR SPLICE STRAP AT STA 767 HAS CORROSION ON UPPER AND LOWER SURFACE. / EVALUATED CORROSION FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED SRM LIMITS FOR FLOOR STRAP. REPLACED STRAP ON TABLE. PART # 146A9401-4 ISSUE TAG# WN8493 IAW AIPC 53-42-11-30 ITEM 30. STRAP INSTALLED ON CARD NO. JPANEL-141-CLOSE.

Part: SPLICE STRAP — CORRODED (AFT CARGO BAY) · airframe 69,621 hrs · 40,909 cycles

AFT CARGO; FLOOR SPLICE STRAP AT STA 887 HAS CORROSION ON UPPER AND LOWER SURFACE. / EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED LIMITS IN SRM. REPLACED FLOOR SPLICE STRAP ON TABLE. STRAP INSTALLED ON CARD NO JPANEL-141-CLOSE

Part: SCUFF PLATE — CORRODED (AFT CARGO) · airframe 69,621 hrs · 40,909 cycles

AFT CARGO; FWD SCUFF PLATE HAS CORROSION / EVALUATED CORROSION FOUND TO BE OUT OF LIMITS DUE TO NO PUBLISHED LIMITS IN SRM. REPLACED SCUFF PLATE ON TABLE. SCUFF PLATE INSTALLED ON WORK INSTRUCTION NO. 753-140-00-02Y.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 69,621 hrs · 40,909 cycles

AFT CARGO FLOOR PANEL 140CF HAS CORROSION AROUND PERIMETER OF FLOOR PANEL / REPLACED AFT CARGO PNL 140CF ON TABLE W/ P/N 453A2610-1 SI #7252490 ATAG# WN7676 I/A/W AIPC 25-52-10-02 ITEM #160 PANEL INSTALLED ON JPANEL-141-CLOSE.

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 69,621 hrs · 40,909 cycles

AFT CARGO; RH SIDE FLOOR TO SIDEWALL CAP STRIPS HAVE CORROSION / REPLACED 3EA CAP STRIPS ON TABLE. PART #453A2611-9; 453A2611-11; AND 453A 2611-3 IAW AIPC 25-52-10-02. CAP STRIPS INSTALLED ON CORD NO JPANEL-141-CLOSE

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 69,621 hrs · 40,909 cycles

AFT CARGO DOOR CUTOUT FORWARD CORNER SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 69,621 hrs · 40,909 cycles

AFT CARGO; CAP STRIPS FOR FLOOR PANEL 140CF HAS CORROSION / REPLACED 3 EA PANEL 140CF CAPSTRIPS ON TABLE PAST NUMBERS 453A2611-6; 453A2611-7 AND 453A2611-5 IAW AIPC 25-52-10-02. CAPSTRIPS INSTALLED ON CARD NO. JPANEL-141-CLOSE

Part: SKIN — CRACKED (LE SLAT) · airframe 69,621 hrs · 40,909 cycles

LT WING NR 8 SLAT NOSE SKIN CRACKED AROUND ACTUATOR RIB FASTENER HOLES. R&R SKIN IAW SRM.

Part: HOOK — LOOSE (L1 DOOR) · airframe 68,381 hrs · 40,127 cycles

L1 DOOR EMERGENCY ESCAPE SLIDE BAR LOOSE IN HOLDER. SECURED HOOK IAW SIP.

Part: BATTERY PACK — FAILED (CABIN) · airframe 68,217 hrs · 40,019 cycles

AFT RT EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 68,217 hrs · 40,019 cycles

AFT LT EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK. R&R BATTERY PACK PER MM.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,066 hrs · 39,917 cycles

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

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 67,129 hrs · 39,356 cycles

UPON RE-INSPECTION OF FORWARD CARGO DOOR CENTER SCUFF PLATE SPEED TAPE CONDITION; FOUND CENTER SCUFF PLATE CREASED FROM IMPACT DAMAGED AND MULTIPLE CRACKS ON FORWARD EDGE OF CENTER SCUFF PLATE / REMOVED AND REPLACED FWD CARGO SCUFF PLATE. REF AMM 53-11-02.

Part: CONTROL UNIT — FAILED (COCKPIT) · airframe 66,289 hrs · 38,790 cycles

DRIVE ELECTRONIC UNIT RIGHT FAILED IN FLIGHT. DIVERTED. RESEATED THE 2 DRIVE ELECTRONIC UNIT IAW AMM.

Part: ANGLE — BROKEN (LOWER EXT FUSELA) · airframe 66,204 hrs · 38,740 cycles

RIGHT FORWARD WING TO BODY FAIRING HAS BROKEN ATTACH ANGLE AT BS 540.(MARKED) / ANGLE WAS REMOVED AND REPLACED PER SRM 51-10-02 SEE ADDED SUB TASKS FOR INDIVIDUAL SIGN OFFS

Part: DOUBLER — CRACKED (WHEEL WELL RH) · airframe 66,204 hrs · 38,740 cycles

RIGHT TURBOFAN EXIT HAS CRACKED DOUBLER IN RIGHT WHEEL WELL OPENING. / REMOVED AND REPLACED DOUBLER PER BOEING DRAWING #111A1512

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 65,966 hrs · 38,584 cycles

FORWARD GALLEY UPPER EMERGENCY FLASHLIGHT STRAP BROKEN. R&R STRAP PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 65,967 hrs · 38,584 cycles

L1 DOOR EMERGENCY EVAC SLIDE COMPARTMENT LOOSE. SECURED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,759 hrs · 37,832 cycles

LT OVERWING EXIT LIGHT INOP. RESECURED LIGHT BATTERY PACK PER MM.

Part: STRINGER — TORN (FUSELAGE) · airframe 64,639 hrs · 37,753 cycles

VERTICAL STRINGER TORN AT BS 1074, STR. 17R. REPAIRED STRINGER PER SRM & EA.

Part: SKIN — DAMAGED (BS 1073.5) · airframe 64,639 hrs · 37,753 cycles

SKIN DAMAGED AT BS 1073.5, STRINGER 16R. REPAIRED THE SKIN IAW EA.

Part: SKIN — TORN (BS 1074) · airframe 64,639 hrs · 37,753 cycles

SKIN TORN AT BS 1074, STRINGER 17R. REPAIRED THE SKIN IAW SRM & EA.

Part: BULB — OVERHEATED (EMERGENCY LIGHT) · airframe 63,262 hrs · 36,913 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT BULB OVERHEATED. REPLACED THE BULB IAW AMM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,261 hrs · 36,912 cycles

AFT CARGO BAY SHIELD CORRODED BETWEEN BS 767 TO BS 787, RBL 23. R&R SHIELD PER SRM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,261 hrs · 36,912 cycles

L2 DOOR, LOWER SILL WEB CORRODED BETWEEN BS 951 TO BS 992, LBL 48. R&R WEB PER SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,261 hrs · 36,912 cycles

R2 DOOR LOWER SILL WEB CORRODED BETWEEN BS 951 TO BS 992, RBL 48. R&R WEB PER SRM & DWG.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 63,261 hrs · 36,912 cycles

MAIN WHEEL WELL PRESSURE DECK BEADED WEB CRACKED AT BS 665, RBL 41. REPAIRED THE PRESSURE DECK WEB IAW ER AND EA,

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,261 hrs · 36,912 cycles

FORWARD ENTRY DOORWAY LOWER THRESHOLD SUPPORT OUTBOARD ANGLE CORRODED AT BS 316. REPAIRED ANGLE PER SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,261 hrs · 36,912 cycles

L1 DOORWAY LOWER THRESHOLD SUPPORT ANGLE CORRODED BETWEEN BS 310 TO BS 340. R&R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,261 hrs · 36,912 cycles

L1 DOORWAY LOWER THRESHOLD, MIDDLE SUPPORT ANGLE CORRODED BETWEEN BS 310 TO BS 340. R&R ANGLE PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,261 hrs · 36,912 cycles

CABIN FLOOR SUPPORT INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 45. R&R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,261 hrs · 36,912 cycles

CABIN FLOOR SUPPORT INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 45. R&R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,261 hrs · 36,912 cycles

CABIN FLOOR SUPPORT INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 297, BL 0. R&R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,261 hrs · 36,912 cycles

CABIN FLOOR SUPPORT INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 27. R&R INTERCOSTAL IAW SRM.

Part: DOOR FRAME — CRACKED (BS 294) · airframe 63,261 hrs · 36,912 cycles

FORWARD GALLEY DOORWAY FORWARD FRAME CRACKED AT LOWER AT BS 294, WL 208. REPAIRED FRAME PER ER AND EA

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,261 hrs · 36,912 cycles

FLOORBEAM TEE CHORD CORRODED AT BS 986, BETWEEN LBL 51 TO RBL 51. R&R TEE CHORD IAW SRM AND EA.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 63,261 hrs · 36,912 cycles

FORWARD GALLEY DOORWAY LOWER THRESHOLD ATTACH ANGLE CORRODED BETWEEN BS 297 TO BS 328. R&R ANGLE IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,261 hrs · 36,912 cycles

FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED. R&R WEB IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,261 hrs · 36,912 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 23. R&R SUPPORT PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,261 hrs · 36,912 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED. R&R WEB IAW SRM.

Part: SIDEWALL SUPPORT — CORRODED (BS 727-807) · airframe 63,261 hrs · 36,912 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO 807, LBL 23. R & R THE SIDEWALL SUPPORT IAW SRM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 62,881 hrs · 36,662 cycles

R1 DOOR LOWER EMERGENCY LIGHT LENS MISSING. INSTALLED LENS IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 61,348 hrs · 35,757 cycles

FORWARD GALLEY RT LOWER EMER EXIT SIGN BROKEN. R & R SIGN IAW AMM.

Part: RIVET — SHEARED (EVAC SLIDE) · airframe 61,348 hrs · 35,757 cycles

L1 DOOR EMER EVAC SLIDE COVER GIRT BAR FWD HINGES RIVET SHEARED. R & R SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 61,174 hrs · 35,661 cycles

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

Part: LINK ASSY — LOOSE (LT WING) · airframe 60,304 hrs · 35,181 cycles

LEFT WING NR 2 FLAP SUPPORT, FAIRING LINK ASSEMBLY LOOSE. R & R LINK ASSEMBLY IAW AMM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 60,304 hrs · 35,181 cycles

LEFT WING INBD TE FLAP, LOWER SURFACE DELAMINATED. REPAIRED FLAP IAW SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 59,160 hrs · 34,536 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 59,119 hrs · 34,516 cycles

L1 DOOR EVACUATION SLIDE GIRT BAR LOOSE. SECURED GIRT BAR IAW MM.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 59,034 hrs · 34,475 cycles

R2 DOOR EMER EXIT SIGN LENS FELL OFF. RELAMPED LIGHT ASSEMBLY IAW AMM.

Part: PANEL — CRACKED (FUSELAGE) · airframe 57,075 hrs · 33,374 cycles

UPPER WING TO BODY PANEL 195CL CRACKED. REPAIRED PANEL IAW SRM.

Part: PANEL — CRACKED (FUSELAGE) · airframe 57,075 hrs · 33,374 cycles

UPPER WING TO BODY PANEL 195CR CRACKED. REPAIRED PANEL IAW SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 57,075 hrs · 33,374 cycles

FUSELAGE FRAME GUSSET CRACKED AT STATION 520D, STRINGER 19L. R & R GUSSET IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 57,075 hrs · 33,374 cycles

FITTING CRACKED AT BS 663, LBL 24. REPAIRED FITTING IAW EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 57,075 hrs · 33,374 cycles

RIGHT ACFT BAY AFT BULKHEAD STIFFENER CRACKED AT BS 663. R & R STIFFENER IAW SRM & DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,075 hrs · 33,374 cycles

STRINGER CORRODED AT BS 540, STRINGER 23R. R & R STRINGER IAW SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 57,075 hrs · 33,374 cycles

CHORD SPLICE CRACKED AT BS 540, BETWEEN STRINGER 22R TO 23R. REPAIRED SPLICE IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 57,075 hrs · 33,374 cycles

WEB CRACKED AT BS 663, BETWEEN LBL 24.92 TO 45.64. REPAIRED WEB IAW EA.

Part: PRESSURE PANEL — CRACKED (MLG WW) · airframe 57,075 hrs · 33,374 cycles

VERTICAL PRESS WEB CRACKED AT BS 663, BETWEEN LBL 40.00 TO RBL 45.64. REPAIRED WEB & EA.

Part: SKIN — CRACKED (LT WING) · airframe 57,075 hrs · 33,374 cycles

LEFT WING LE LOWER SKIN CUT OUT CRACKED AT STATION 666. REPAIRED SKIN IAW SRM.

Part: RIB — CRACKED (RT WING) · airframe 56,360 hrs · 32,948 cycles

RIGHT WING UPPER FIXED PANEL BETWEEN SPOILER 7 & 8 CRACKED OTBD WING PANEL BEAM RIB CRACKED. R & R RIB IAW SRM.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 56,360 hrs · 32,948 cycles

RIGHT WING UPPER FIXED PANEL BETWEEN SPOILER NR 7 & 8 OTBD ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM & EA.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 56,288 hrs · 32,900 cycles

L1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: COVER — LOOSE (EXIT SIGN) · airframe 55,474 hrs · 32,437 cycles

RIGHT LIGHT EMERGENCY EXIT SIGN COVER LOOSE. SECURED COVER IAW SIP.

Part: RETAINING CLIP — LOOSE (L1 DOOR) · airframe 54,152 hrs · 31,623 cycles

L1 DOOR EMERGENCY EVAC SLIDE COVER GIRT BAR AFT RETAINER CLIP LOOSE. SECURED CLIP IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,152 hrs · 31,623 cycles

RT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.

Part: ACTUATOR — LEAKING (RT ELEVATOR TAB) · airframe 54,152 hrs · 31,623 cycles

RT ELEVATOR TAB CONTROL LOCKING ACTUATOR LEAKED. R & R ACTUATOR IAW AMM.

Part: FASTENER — LOOSE (R2 DOOR) · airframe 54,152 hrs · 31,623 cycles

R2 DOOR EMERGENCY EVAC SLIDE COVER LOWER SUPPORT FASTENERS LOOSE. R & R FASTENER ASSEMBLY IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,152 hrs · 31,623 cycles

LT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.

Part: RETAINING CLIP — LOOSE (R1 DOOR) · airframe 54,152 hrs · 31,623 cycles

R1 DOOR EMERGENCY EVAC SLIDE COVER GIRT BAR FWD RETAINER CLIP LOOSE. SECURED CLIP IAW SRM.

Part: TRANSMITTER — FAULTY (TE FLAP) · airframe 54,184 hrs · 31,642 cycles

DECLARED EMERGENCY ON LANDING. WHEN ASKING FOR FLAPS 30Ï¿½, FLAPS WOULD NOT EXTEND BEYOND 5Ï¿½ ON THE FWD PANEL INDICATOR. R & R TRANSMITTER IAW MM.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 53,661 hrs · 31,327 cycles

LT AFT EMERGENCY BATTERY PACK INOPERATIVE. R & R POWER SUPPLY IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 53,661 hrs · 31,327 cycles

RT AFT EMERGENCY BATTERY PACK INOPERATIVE BETWEEN ROW 16 TO ROW 18. R & R POWER SUPPLY IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 53,661 hrs · 31,327 cycles

LT AFT EMERGENCY SIGN INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 53,661 hrs · 31,327 cycles

RT FWD OVER DOOR EMERGENCY SIGN INOPERATIVE. RELAMPED SIGN IAW AMM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,438 hrs · 31,174 cycles

RT HORIZONTAL BS 92.7 RIB SECTION CRACKED ON RIB WEB AT 3RD VERTICAL STIFFENER FROM FWD SPAR. REPAIRED RIB IAW EA & SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,438 hrs · 31,174 cycles

RT HORIZONTAL STABILIZER BS 92.7 RIB SECTION CRACKED ON RIB WEB AT 2ND VERTICAL STIFFENER FROM FWD SPAR. R & R RIB IAW ER & EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,438 hrs · 31,174 cycles

RT HORIZONTAL STABILIZER BS 92.7 RIB SECTION CRACKED ON RIB WEB AT 1ST VERTICAL STIFFENER FROM FWD SPAR. REPAIRED RIB IAW SWA SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,438 hrs · 31,174 cycles

LT NR 1 WINDOW FRAME ASSEMBLY CRACKED AT UPPER AFT HOLE. R & R FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,438 hrs · 31,174 cycles

NR 1 RT COCKPIT WINDOW FRAME CRACKED IN THE UPPER OTBD CORNER VERTICAL FLANGE UPPER HOLE. R & R FRAME IAW ACO.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 53,438 hrs · 31,174 cycles

SPLICE STRAP CRACKED AT BS 727B, BETWEEN LBL 24.75 TO RBL 45.5. REPAIRED SPLICE IAW EA.

Part: LENS — BROKEN (CABIN) · airframe 53,438 hrs · 31,174 cycles

G1 GALLEY EMERGENCY LIGHT LENS ON LOWER RT SIDE LENS BROKEN. R & R LENS IAW AMM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,438 hrs · 31,174 cycles

RT HORIZONTAL STABILIZER BS 92.7 RIB SECTION CRACKED AT VERTICAL STIFFENER LOCATIONS. REPAIR RIB IAW SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 53,438 hrs · 31,174 cycles

SPLICE STRAP CRACKED AT BS 727B BETWEEN LBL 24.75 TO RBL 45.5. REPAIRED SPLICE IAW EA.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 53,438 hrs · 31,174 cycles

SPLICE STRAP CRACKED AT BS 727B BETWEEN RBL 24.75 RBL 45.5. REPAIRED SPLICE IAW EA.

Part: STRAP — CRACKED (FUSELAGE) · airframe 53,438 hrs · 31,174 cycles

SPLICE STRAP CRACKED AT BS 727B BETWEEN LBL 24.75 TO RBL 45.5. REPAIRED FLANGE IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,438 hrs · 31,174 cycles

FRAME CRACKED AT BS 400, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,438 hrs · 31,174 cycles

FRAME CRACKED AT BS 360 STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,438 hrs · 31,174 cycles

FRAME CRACKED AT BS 400, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,438 hrs · 31,174 cycles

FRAME CRACKED AT BS 867 STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,438 hrs · 31,174 cycles

FRAME CRACKED AT BS 747, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,438 hrs · 31,174 cycles

FRAME CRACKED AT BS 727D STRINGER 8. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,438 hrs · 31,174 cycles

FRAME CRACKED AT BS 500C STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,438 hrs · 31,174 cycles

FRAME CRACKED AT BS 907 STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,438 hrs · 31,174 cycles

FRAME CRACKED AT BS 827 STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,438 hrs · 31,174 cycles

FRAME CRACKED AT BS 727D STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,438 hrs · 31,174 cycles

FRAME CRACKED AT BS 867 STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,438 hrs · 31,174 cycles

FRAME CRACKED AT BS 787, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,438 hrs · 31,174 cycles

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

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,438 hrs · 31,174 cycles

LT NR 3 WINDOW FRAME E-F POST SECOND LOWER CORNER FASTENER HOLE CRACKED. R & R FRAME IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,438 hrs · 31,174 cycles

R1 DOOR EMERGENCY LIGHT INOPERATIVE. R & R BULBS IAW MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,438 hrs · 31,174 cycles

RT NR 3 WINDOW FRAME E-F POST SECOND LOWER CORNER FASTENER HOLE CRACKED. R & R FRAME IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,438 hrs · 31,174 cycles

LT EMERGENCY BULLNOSE LIGHT INOPERATIVE BETWEEN ROW 16 TO ROW 18R. R & R BULBS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,666 hrs · 29,559 cycles

LEFT OVERWING EXIT LOWER EMERGENCY LIGHT BULBS INOP. RELAMPED (WITH 3 NEW BULBS) AND OP CHECKED GOOD LEFT OVERWING EXIT, LOWER EMERGENCY LIGHT IAW SWA B737 MM 33-51-0.

Part: FLAP — PUNCTURED (LT WING) · airframe 50,666 hrs · 29,559 cycles

LEFT I/B FLAP PUNCTURED. REMOVED AND REPLACED FLAP IAW AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 50,443 hrs · 29,421 cycles

LEFT EEPLS LOOSE AT ROW 8. SECURED EEPLS PER MM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 49,348 hrs · 28,741 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED AT STA 133.15. REPAIRED SKIN PER SRM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 47,693 hrs · 27,796 cycles

R-1 DOOR ESCAPE SLIDE COVER FWD GIRT BAR STOWAGE HOOK IS LOOSE. SECURED HOOK PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,693 hrs · 27,796 cycles

EXTERIOR EMERGENCY EXIT LIGHT AFT OF THE L1 DOOR IS INOP. REMOVED AND REPLACED BULB PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 47,693 hrs · 27,796 cycles

EXTERIOR EMERGENCY EXIT LIGHT AFT OF THE R2 DOOR IS INOP. REMOVED AND REPLACED BULB PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 47,693 hrs · 27,796 cycles

RT WING O/B AFT FLAP UPPER SURFACE I/B END DELAMINATED. REMOVED AND REPLACED AFT FLAP IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,693 hrs · 27,796 cycles

EMERGENCY LIGHT AT BULLNOSE PANEL ROW 16ABC IS INOP. REMOVED AND REPLACED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,693 hrs · 27,796 cycles

LT OVERWING EXIT SIDEWALL LIGHT IS INOP. REMOVED AND REPLACED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,541 hrs · 27,701 cycles

DURING SCHEDULED SPV CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP AT ROW 13. REMOVED AND REPLACED LAMP PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 44,344 hrs · 25,855 cycles

AFT O/B EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,237 hrs · 25,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,237 hrs · 25,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER EA.

Part: FLOORBEAM — WORN (FUSELAGE) · airframe 44,237 hrs · 25,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM WORN AT BS 887, BETWEEN LBL 22 TO RBL 4. REPAIRED BEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,237 hrs · 25,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 32. REMOVED AND REPLACED BEAM PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 44,237 hrs · 25,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 14R. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,237 hrs · 25,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER EA.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 44,237 hrs · 25,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX FUEL TANK STIFFENER CRACKED AT BS 549, RBL 14. REMOVED AND REPLACED STIFFENER PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,237 hrs · 25,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER EA.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 44,237 hrs · 25,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX FUEL TANK STIFFENER CRACKED AT BS 549, LBL 41. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 44,237 hrs · 25,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX FUEL TANK STIFFENER CRACKED AT BS 549, LBL 14. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 44,237 hrs · 25,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX FUEL TANK STIFFENER CRACKED AT BS 549, LBL 32. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 44,237 hrs · 25,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX FUEL TANK STIFFENER CRACKED AT BS 549, LBL 6. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 44,237 hrs · 25,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX FUEL TANK STIFFENER CRACKED AT BS 549, RBL 41. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 44,237 hrs · 25,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX FUEL TANK STIFFENER CRACKED AT BS 549, RBL 32. REMOVED AND REPLACED STIFFENER PER SRM.

Part: STIFFENER — CRACKED (CENTER WING BOX) · airframe 44,237 hrs · 25,792 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX FUEL TANK STIFFENER CRACKED AT BS 549, RBL 6. REMOVED AND REPLACED STIFFENER PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 41,694 hrs · 24,301 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — WORN (CABIN) · airframe 41,201 hrs · 24,019 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS WORN AT ROW 11. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 40,850 hrs · 23,824 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE IN CASE. SECURED PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,192 hrs · 23,438 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 39,659 hrs · 23,110 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: FUSE — INOPERATIVE (CABIN) · airframe 38,645 hrs · 22,462 cycles

LT EMERGENCY EXIT DOOR LIGHT INOP. REMOVED AND REPLACED LIGHT FUSE PER MM.

Part: CONTAINER — LOOSE (EVAC SLIDE) · airframe 38,406 hrs · 22,322 cycles

R2 DOOR EMERGENCY EVAC SLIDE STORAGE CONTAINER LOOSE. SECURED CONTAINER PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 37,516 hrs · 21,785 cycles

L1 DOOR EMERGENCY EVACUATION SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: FITTING — LOOSE (GIRT BAR) · airframe 367,010 hrs · 21,290 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR GIRT BAR AFT RETAINING CLIP LOOSE. SECURED CLIP PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 367,010 hrs · 21,290 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR GIRT BAR AFT RETAINING CLIP LOOSE. SECURED CLIP PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 367,010 hrs · 21,290 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR GIRT BAR FWD RETAINING CLIP LOOSE. SECURED CLIP PER MM.

Part: ACTUATOR — FAULTY (NLG) · airframe 36,252 hrs · 21,028 cycles

DURING CLIMB NLG EXTENDED WITHOUT COMMAND WHEN GEAR HANDLE MOVED TO OFF POSITION. REMOVED AND REPLACED NLG LOCK ACTUATOR PER MM.

Part: FITTING — CORRODED (LT MLG) · airframe 35,671 hrs · 20,668 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: FITTING — CORRODED (RT MLG) · airframe 35,671 hrs · 20,668 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 34,866 hrs · 20,185 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,739 hrs · 20,113 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 33,910 hrs · 19,621 cycles

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

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 33,910 hrs · 19,621 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 32,899 hrs · 18,994 cycles

L2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: FUSE — BLOWN (CABIN) · airframe 32,754 hrs · 18,912 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 6 ABC. REMOVED AND REPLACED FUSE PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,992 hrs · 18,433 cycles

DURING SCHEDULED MV2 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 31,657 hrs · 18,241 cycles

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

Part: LENS — LOOSE (EMERGENCY LIGHTS) · airframe 31,479 hrs · 18,141 cycles

L1 DOOR EMERGENCY EXIT LIGHT SIGN LENS LOOSE. SECURED LENS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,282 hrs · 17,450 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 771, RBL 3. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,282 hrs · 17,450 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM UPPER CAP CORRODED AT BS 986.5, LBL 52 TO RBL 52. REPAIRED FLOORBEAM PER SWA EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 29,471 hrs · 16,994 cycles

DURING SCHEDULED HC2 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 29,471 hrs · 16,994 cycles

DURING SCHEDULED HC2 CHECK, LEFT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 29,471 hrs · 16,994 cycles

DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,044 hrs · 16,218 cycles

DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF LIMITS (L1 DOOR) · airframe 24,602 hrs · 14,261 cycles

DURING SCHEDULED RON CHECK, L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATED OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: TIRE — SEPARATED (MLG WHEEL) · airframe 24,485 hrs · 14,187 cycles

NR 3 MAIN TIRE TREAD SEPARATED. FOUND NR 3 KRUEGER FLAP, RIGHT INBOARD T/E AFT FLAP & RIGHT INBOARD T/E MIDFLAP DAMAGED. REMOVED AND REPLACED NR 3 & NR 4 MAIN TIRE/WHEEL ASSY, NR 3 KRUEGER FLAP & RIGHT INBOARD T/E AFT FLAP PER MM. REPAIRED RIGHT INBOARD T/E MIDFLAP PER SWA EA & SRM.

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 24,375 hrs · 14,128 cycles

DURING SCHEDULED HC2 CHECK, NR 2 ENGINE HAS 2 EACH COMPRESSOR SPOOL BLADE TIP CORNERS MISSING MATERIAL BEYOND LIMITS. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 22,021 hrs · 12,818 cycles

L2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED L2 COCKPIT WINDOW PER MM.

Part: SIGN — LOOSE (EMERGENCY EXIT) · airframe 18,902 hrs · 11,051 cycles

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

Part: LIGHT — ACTIVATED (CABIN FLOOR) · airframe 18,310 hrs · 10,740 cycles

EEPLS INOP AT FWD END. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — LOW (L1 DOOR) · airframe 17,647 hrs · 10,377 cycles

L1 DOOR EVACUATION SLIDE PRESS IND LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 17,341 hrs · 10,217 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT PRESS BULKHEAD OIL CANNED AT BS 1016, STR 1L. REPAIRED BULKHEAD PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 14,959 hrs · 8,907 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,525 hrs · 8,650 cycles

EEPLS INOP AT ROW NR 2. REMOVED AND REPLACED EEPLS LIGHT ASSY PER MM.

Part: LENS — MISSING (CABIN) · airframe 14,349 hrs · 8,538 cycles

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

Part: SLIDE — LOOSE (FWD ENTRY DOOR) · airframe 13,283 hrs · 7,944 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE LOOSE IN CONTAINER. SECURED SLIDE PER MM.

Part: PLACARD — MISSING (EVAC SLIDE) · airframe 12,277 hrs · 7,374 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE INSPECTION PLACARD MISSING. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — OUT OF ADJ (AFT ENTRY DOOR) · airframe 9,644 hrs · 5,896 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: ROD — WORN (RH ELEVATOR) · airframe 9,492 hrs · 5,810 cycles

DURING SCHEDULED SERVICE CHECK, RH ELEVATOR TAB FAILED FREE PLAY CHECK. R&R ELEVATOR TAB CONTROL ROD END & # 1 HINGE BUSHING PER MM.

Part: WEB — CRACKED (RH MLG W/W) · airframe 9,044 hrs · 5,534 cycles

DURING SCHEDULED C1 CHECK, FOUND RH MLG W/W AFT WEB CRACKED. R&R WEB PER SRM.

Part: COVER — LOOSE (CABIN) · airframe 8,641 hrs · 5,322 cycles

EEPLS TRACK COVER LOOSE AT FWD CABIN. SECURED EEPLS COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 8,151 hrs · 5,029 cycles

EEPLS TRACK COVER MISSING. INSTALLED TRACK COVER PER MM.

Part: FITTING — ELONGATED (ELEVATOR TAB) · airframe 7,826 hrs · 4,850 cycles

DURING SCHEDULED C4 CHECK, FOUND LT ELEVATOR TAB ATTACH FITTING MAST OUTBD INPUT ROD LUG BOLT HOLE ELONGATED. REMOVED AND REPLACED ELEVATOR TAB PER MM.

Part: BOTTLE — DISCHARGED (SLIDE)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE BOTTLE PRESSURE LOW. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: LIGHT — LOOSE (CABIN)

FWD EEPLS TRACK LOOSE. RESECURED EEPLS TRACK PER MM.