N781WN

Part: FLOOR PANEL — SPLIT (AFT CARGO) · airframe 74,908 hrs · 44,392 cycles

AFT CARGO BIN FLOOR HAS A SPLIT / [01] FOUND AFT CARGO FLOOR PANEL 140BF WITH 2 CRACKS 15? AND 9?. OK TO CONTINUE PER MEL25-16-01 SP1B. AUTH 104453;[02] WORKING MEL 25-16-01. R+R AFT CARGO BIN FLOOR IAW AMM 25-52-10. THIS CLEARS MEL 25-16-01.

Part: NONE — DETERIORATED (LH WING) · airframe 74,585 hrs · 44,178 cycles

LEFT WING OB AFT FLAP SEPARATED AT TE APPROX 4 AT IB END. LEFT WING OB AFT FLAP SEPARATED AT TE APPROX 4 AT IB END. / [01] DISBOND MEASURES AT 5' INBD TO OTBD AND 3.5'FORE AND AFT APPLIED SEALANT 5-95 TO VOID AND APPLIED SPEED TAPE TO AFFECTED AREA

Part: MODULE — FAULTED (EMERGENCY LIGHTS) · airframe 74,455 hrs · 44,087 cycles

EMERGENCY EXIT LIGHTS WILL NOT EXTINGUISH WITH SWITCH OFF / [01] REMOVED AND REPLACED AFT ATTENDANT PNL LIGHTING MODULE REF AMM 25-25-11. PERFORMED EMERGENCY LIGHT OPS CHECK FOUND WORKING NORMAL PER AMM 33-51-00.

Part: MODULE — DAMAGED (EMERGENCY LIGHTS) · airframe 74,457 hrs · 44,089 cycles

EMERGENCY EXIT LIGHTS WILL NOT EXTINGUISH WITH SWITCH OFF / [01] REMOVED AND REPLACED AFT ATTENDANT PNL LIGHTING MODULE REF AMM 25-25-11. PERFORMED EMERGENCY LIGHT OPS CHECK FOUND WORKING NORMAL PER AMM 33-51-00.

Part: HOLDER — LOOSE (R1 DOOR) · airframe 74,401 hrs · 44,056 cycles

FORWARD SERVICE DOOR EMERGENCY SLIDE BRACKET IS LOOSE. / [01] RE-SECURED SLIDE GIRT BAR HOLDER REF. SIP.

Part: PANEL — ELONGATED (FUSELAGE) · airframe 74,272 hrs · 43,971 cycles

SEVERAL 193B PANEL FASTENER HOLES ARE ELONGATED AND HAS WORN THROUGH THE COMPOSITE MATERIAL. / [01] R&R 193 PANEL

Part: LIGHT — INOPERATIVE · airframe 73,660 hrs · 43,565 cycles

RIGHT WING EMERGENCY EXIT EXTERIOR EMERGENCY LIGHT INOP / [01] REMOVED AND REPLACED RT WING EMERGENCY EXIT EXTERIOR EMERGENCY LIGHT REF AMM 33-51-04. OPS CHECK GOOD

Part: PANEL — CRACKED (FUSELAGE) · airframe 72,535 hrs · 42,842 cycles

WING TO BODY 193D PANEL HAS SEVERAL HOLES WITH CRACKS EMANATING FROM FASTNER HOLES.(MARKED) / [01] REMOVED AND REPLACED WING TO BODY 193D PANEL PER AMM 53-51-21 FIG 1

Part: PANEL — CRACKED (FUSELAGE) · airframe 72,535 hrs · 42,842 cycles

WING TO BODY 194E PANEL HAS SEVERAL HOLES WITH CRACKS EMANATING FROM FASTNER HOLES.(MARKED) / [01] REMOVED AND REPLACED WING TO BODY 194E PANEL PER A AMM.53-51-21. FIG 1

Part: PANEL — ELONGATED (FUSELAGE) · airframe 72,535 hrs · 42,842 cycles

WING TO BODY 193D PANEL HAS SEVERAL ELONGATED FASTNER HOLES.(MARKED) / [01] REMOVED AND REPLACED 193D PANEL PER AMM 53-51-21 FIG 1

Part: PANEL — ELONGATED (FUSELAGE) · airframe 72,535 hrs · 42,842 cycles

WING TO BODY 194E PANEL HAS SEVERAL ELONGATED FASTENER HOLES.(MARKED) / [01] REMOVED AND REPLACED WING TO BODY FAIRING PANEL 194E PER AMM 53-51-21 FIG 1

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 71,983 hrs · 42,507 cycles

L/H LOWER WING TO BODY PANEL AFT OF L/H MAIN GEAR W/W PANEL 193CL IS DELAMINATED ; DELAM DIMENSIONS ARE APPROXIMATELY 12? Y 9.5? / [01] REPLACED PANEL PER MM 53-51-21

Part: GIRT BAR — LOOSE (L2 DOOR) · airframe 71,634 hrs · 42,283 cycles

SUPPLEMENTAL INFORMATION: AFT ENTRY DOOR GIRT BAR LOOSE ; / [01] RESECURED AFT ENTRY GIRT BAR PER SIP

Part: DOOR — OUT OF ADJUST (R2) · airframe 71,377 hrs · 42,145 cycles

AFT SERVICE DOOR HANDLE RAISES UP 4 FEW INCHES WHEN THE AIRCRAFT PRESSURIZES ; / [01] FOUND AFT GALLEY SERVICE DOOR HORIZONTAL CONTOL ROD OUT OF RIG. ADJUSTED CENTER CONTROL ROD I/A/W AMM 52-41-00. PREFORMED ADJUSTMENT TEST. I/A/W AMM 52-13-00. PRESSURIZED AIRCRAFT. NO MOVEMENT OD HANDLE NOTED.

Part: PANEL — CRACKED (WING) · airframe 71,082 hrs · 41,979 cycles

LEADING EDGE PANEL 621YB HAS 1IN CRACK ALONG OUTBD FWD EDGE. CRACK IS ALONG THE INBD-AFT EDGE. OK TO CONTINUE ON MX NOTE PER MPM 53-05-09A. REINSPECT EVERY 3 DAYS, WITH PERMANENT REPAIR WITHIN 20 DAYS. AUTHORIZATION CODE 22789. R&R PAL REF AMM 57-41-02.

Part: ANGLE — CORRODED (FWD CARGO) · airframe 70,552 hrs · 41,684 cycles

FWD CARGO COMPARTMENT AFT BULKHEAD LWR TRANSITION ANGLE;SHOW SIGNS OF SURFACE CORROSION IN SEVERA AREAS ; / PART REPLACED WITH NEW TRANSITION ANGLE P/N 143A9485-35 INSTALLATION WILL BE ACCOMPLISH T/C TTG8Q004EBSC; VERIFIED 1

Part: CAP — CORRODED (BS 847-947) · airframe 70,552 hrs · 41,684 cycles

FOUND SEVERAL EXFOLIATION CORROSION SPOTS ON AFT CARGO CAP STRIPS FROM STA 847 THROUGH STA 947.5 ; / LOCATED AND DRILLED CAP STRIP PER B737-700 SRM 51-40-05-0G-0.;PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW B737 NDT P4 51-00-00 PROC.3; MIN THK NOTED 0.038'<BR>TOOL USED MG27 BC:172139;REMOVED CORROSION FROM CAPSTRIPS FROM AFT CARGO FROM STA 847 THRU STA 947.5 RBL 21. AS PER B737-700 SRM 51-10-02-0G-0.;RECEIVED SERVICEABLE AFT CARGO CAP STRIP P/N 453A2611Y3; REF. TASK CARD TTG8Q004EYM2 FOR INSTALLATION.;VERIFIED STEP 1;VERIFIED STEPS 4 AND 5. TASK COMPLETE.

Part: CAP — CORRODED (BS 727-787) · airframe 70,552 hrs · 41,684 cycles

FOUND EXFOLIATION CORROSION SPOTS ON AFT CARGO CAP STRIPS RT SIDE FROM STA 727+4 THROUGH STA 787 ; / PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW B737 NDT P4 51-00-00 PROC.3; MIN THK NOTED 0.039'<BR>TOOL USED MG27 BC:172139;REMOVED CORROSION AT AFT CARGO CAP STRIPS FROM STA 727+4' THRU STA 787 RBL 21. AS PER B737-700 SRM 51-10-02-0G-0.;RECEIVED 2EA SERVICEABLE AFT CARGO CAP STRIPS FOR RT SIDE FROM STA 727+4 TO STA 787; P/N'S 453A2611-9 AND 453A2611-11. REF. TASK CARD TTG8Q004EYM2 FOR INSTALLATION.;VERIFIED STEP 1;VERIFIED STEP 4

Part: CAP — CORRODED (BS 727-847) · airframe 70,552 hrs · 41,684 cycles

FOUND SEVERAL EXFOLIATION CORROSION SPOTS ON AFT CARGO CAP STRIPS LT SIDE FROM STA 727+4 THROUGH STA 847. ; / PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW B737 NDT P4 51-00-00 PROC.3; MIN THK NOTED 0.041'<BR>TOOL USED MG27 BC:172139;REMOVED CORROSION FROM CAPSTRIPS FROM AFT CARGO FROM STA 847 THRU STA 727+4' LBL 21. AS PER B737-700 SRM 51-10-02-0G-0.;RECEIVED SERVICEABLE CAP STRIPS FOR AFT CARGO COMPARTMENT LEFT SIDE FROM STA 727+4 THROUGH STA 847. REPLACEMENT WILL BE ACCOMPLISHED ON TASK CARD TTG8Q004EYM2.;VERIFIED STEP 4;VERIFIED STEP 1

Part: BONDING JUMPER — MISSING (L2 DOOR) · airframe 70,552 hrs · 41,684 cycles

AFT ENTRY DOOR SLIDE COMPARTMENT MISSING FWD AND AFT BONDING JUMPERS AND STUDS ON BACKING PAN / AFT ENTRY DOOR SLIDE COMPARTMENT P/N 416A2200-11A WAS MODIFIED ON AIRCRAFT PER ACO 6933-25 TO REMOVE BONDING JUMPERS AND STUDS.; VERIFIED STEP 1

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 70,552 hrs · 41,684 cycles

MAIN CABIN FLOOR PANEL 241DF DELAMINATED AT UPPER SURFACE ; / STEP 2 COMPLIED WITH RII INSPECTION;COMPLETE;VERIFIED 1 AND 2;COMPLETE;PREPARED FOR REPAIR DAMAGED AREA TA FLOOR PANEL #241DF PER B737SRM 54-00-50-2R-1;REPAIRED DAMAGED AREA AT FLOOR PANEL #241DF PER B737 SRM54-00-50-2R-1 MATERIAL USED RESIN 50A PO#1692653 FIBERGLASS PO#1480720

Part: FLOOR PANEL — DAMAGED (COCKPIT) · airframe 70,552 hrs · 41,684 cycles

FLIGHT COMPARTMENT FLOOR PANEL 211AF ONE ENLONGATED FASTENER'S HOLE ; / APPLIED TOPCOAT TO FLOOR PANEL 211AF AS PER B737-700 AMM 51-21-73-370-804;LOCATED AND DRILLED NEW FLOOR PANLEL 141A5133U15 AS PER B737-700 SRM 51-40-05-0G-0.;RECIEVED FLOOR PANEL 211AF P/N: 141A5133-15. REF. TASK CARD TGG8Q0032JEA FOR PANEL INSTALLATION.;VERIFIED STEP 1;VERIFIED STEPS 3 AND 4

Part: SIGN — CRACKED (SEAT ROW 10) · airframe 70,552 hrs · 41,684 cycles

MAIN CABIN SEAT ROW 10 L/H EXIT SING CRACK ; / REMOVED AND REPLACED MAIN CABIN SEAT ROW #10 L/H EXIT SIGN AS PER B-737-700 AMM 33-51- 01-960-802.; VERIFIED 1

Part: FLOOR PANEL — DETERIORATED (AFT CARGO) · airframe 70,552 hrs · 41,684 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140AF IS DETERIORATED. [200-010] ; / AFT CARGO FLOOR PANEL 140AF WILL BE INSTALLED ON TASK CARD TTG8Q004EYM2.;FABRICATED AFT CARGO COMPARTMENT FLOOR PANEL 140AF PER B737-700 AMM 25-52-01-201-801.;REMOVED PANEL 140AF;REMOVED PANEL 140AF AS PER B737-700 AMM 25-52-10-000-801;VERIFIED STEP 5;VERIFIED STEPS 1 THRU 3

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 70,552 hrs · 41,684 cycles

FWD CARGO COMP FLOOR PANEL 120CF CRACKED ; / FABRICATED FLOOR PANEL #120CF AS PER REF B737-700 AMM 25-52-01-201-801;FLOOR PANEL INSTALLATION WILL BE ACCOMPLISH ON T/C TTG8Q004EBSC;VERIFIED STEPS 1 TO 3;REMOVED FLOOR PANEL PER AMM25-52-01-201-801

Part: FLOOR PANEL — DETERIORATED (AFT CARGO) · airframe 70,552 hrs · 41,684 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140BF IS DETERIORATED. [200-011] ; / AFT CARGO FLOOR PANEL 140BF WILL BE INSTALLED ON TASK CARD TTG8Q004EYM2.;FABRICATED AFT CARGO COMPARTMENT FLOOR PANEL 140BF PER B737-700 AMM 25-52-01-201-801.;REMOVED PANEL 140BF;REMOVED PANEL 140BF AS PER B737-700 AMM 25-52-10-000-801;VERIFIED STEP 5. TASK COMPLETE.;VERIFIED STEPS 1 THRU 3

Part: DOOR — OUT OF RIG (R2) · airframe 70,552 hrs · 41,684 cycles

R-2 DOOR OUT OF RIG (HITTING ON BOTH FWD LATCH CRANKS) ; / FINALIZED R-2 DOOR ADJUSTMENT IN REF B737 AMM 52-41-00-820-801.;PERFORMED (R2) GALLEY SERVICE DOOR ADJUSTMENT CHECK UP TO AND INCLUDING STEP 2.M.(3)(C)(4) PG.12 IN REF B737 AMM 52-41-00-820-801;RE-INSTALLED LINING AT R-2 DOOR IN REF B737-7 AMM 52-41-31-400-802.;REMOVE AND REPLACED R-2 DOOR UPPER AND LOWER LATCH RECEIVERS IN REF B737-7 AMM 52-41-00-820-801 AND ACCOMPLISHED R-2 DOOR ADJUSTMENT IN REF B737 AMM 52-41-00-820-801.;REMOVED R-2 DOOR LINING IN REF B737-7 AMM 52-41-31-000-802.;REMOVED AND REPLACED R2 DOOR BOTH UPPER AND LOWER FWD LATCH RECEIVERS IN REF B737-7 AMM 52-41-00-820-801.;VERIFIED REMOVAL AND REPLACEMENT R2 DOOR BOTH UPPER AND LOWER FWD LATCH RECEIVERS IN REF B737-7 AMM 52-41-00-820-801.;VERIFIED STEP 4.<BR>PERFORMED (R2) GALLEY SERVICE DOOR ADJUSTMENT CHECK UP TO AND INCLUDING STEP 2.M.(3)(C)(4) PG.12 IN REF B737 AMM 52-41-00-820-801;OK TO RE-INSTALL LINER REMOVED ON STEP 1;VERIFIED STEP 6;VERIFIED STEPS 9 AND 10

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 70,304 hrs · 41,540 cycles

BATTERY PACKS POWER SUPPLIES FAILED CAPACITY TEST AT FOLLOWING LOCATIONS M1673;M1672;M1675 M1674. R AND R 'D BATTERY PACKS POWER SUPPLIES AT FOLLOWING LOCATIONS M1673;M1672;M1675; M1674 PER AMM335106

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,869 hrs · 41,289 cycles

RIB AT STAB STA. 78.29 CRACKED / REMOVED AND REPLACED RIB AT STA. 78.29 PER SRM 51-40-02

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,869 hrs · 41,289 cycles

RIVET PULLED AT RIB STAB STA. 114.55 LOWER SIDE AND RIB CRACKED. / REMOVED AND REPLACED RIB AT STA 119.55 PER SRM 51-40-02

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,869 hrs · 41,289 cycles

R/H HORIZONTAL STAB; RIB AT STATION 101.9 CRACKED AT 4TH VERTICAL STIFFNER AFT OF FRONT SPAR HFEC VERIFIED PER 737 NDT PART 6 PROCEDURE 23 / REMOVED CRACKED RIB. THEN REPAIRED AND REINSTALLED SERVICEABLE RIB IAW SRM 55-10-09-2R & SRM 51-40-02

Part: PLATE — CRACKED (AFT CARGO DOOR) · airframe 68,255 hrs · 40,302 cycles

AFT CARGO DOOR AFT LWR BEARING PLATE CRACKED / REMOVED AND REPLACED PER AMM 52-31-00.

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,310 hrs · 39,694 cycles

L/H MLG FWD TRUNNION SUPPORT FITTING; LOWER I/B LUG BORE EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,310 hrs · 39,694 cycles

L/H MLG FWD TRUNNION SUPPORT FITTING LOWER OUTBOARD HAT SIDE LUG SHOWS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,310 hrs · 39,694 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING; UPPER O/B_LUG FACE EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,310 hrs · 39,694 cycles

LEFT WING MLG FWD TRUNNION SUPPORT FITTING UPPER INBD LUG FACE SHOWS SIGNS OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,310 hrs · 39,694 cycles

LEFT WING MLG FWD TRUNNION SUPPORT FITTING LOWER OTBD LUG FACE SHOWS SIGNS OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,310 hrs · 39,694 cycles

LEFT WING MLG FWD TRUNNION SUPPORT FITTING LOWER INBD LUG FACE SHOWS SIGNS OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,310 hrs · 39,694 cycles

L/H MLG FWD TRUNNION SUPPORT FITTING LOWER INBD HAT SIDE LUG SHOWS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,310 hrs · 39,694 cycles

LEFT WING MLG FWD TRUNNION SUPPORT FITTING UPPER OTBD LUG FACE SHOWS SIGNS OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (LT MLG) · airframe 67,310 hrs · 39,694 cycles

L/H MLG FWD TRUNNION_SUPPORT FITTING UPPER I/B LUG EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,310 hrs · 39,694 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING LOWER I/B LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,310 hrs · 39,694 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING UPPER I/B LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (RT MLG) · airframe 67,310 hrs · 39,694 cycles

R/H MLG FWD TRUNNION SUPPORT FITTING LOWER O/B_LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER WA 1-A57-3246 REV 11

Part: REFERENCE UNIT — FAULTY (E&E BAY) · airframe 67,026 hrs · 39,509 cycles

DIVERSION/DECLARED EMERGENCY-------------------------------------------------------------AT FL400 INDICATED AIR SPEED DISAGREE FLAG ON PRIMARY FLIGHT DISPLAY +- 5-6 KTS BETWEEN CAPTAIN/FIRST OFFICER/STANDBY AIR SPEED. DURING DESCENT CAPTAINS AIR SPEED GRADUALLY DECREASED TO 45KT, FIRST OFFICERS STANDBY INDICATED 250KT. CAPTAINS ALTITUDE 300-500FT HIGH. ELECTRONIC ENGINE CONTROL SYSTEM / SHIFTED TO ALTITUDE MODE. CAPTAIN AIR SPEED & ALTITUDE REMAINED ERRONEOUS UNTIL 5000-8000FT WHEN THEY SEEMED NORMAL. / FOUND FAULTY LEFT AIR DATA INERTIAL REFERENCE UNIT PER AMM.

Part: SENSOR — NO TEST (E&E BAY) · airframe 67,026 hrs · 39,509 cycles

DIVERSION/DECLARED EMERGENCY-------------------------------------------------------------AT FL400 INDICATED AIR SPEED DISAGREE FLAG ON PRIMARY FLIGHT DISPLAY +- 5-6 KTS BETWEEN CAPTAIN/FIRST OFFICER/STANDBY AIR SPEED. DURING DESCENT CAPTAINS AIR SPEED GRADUALLY DECREASED TO 45KT, FIRST OFFICERS STANDBY INDICATED 250KT. CAPTAINS ALTITUDE 300-500FT HIGH. ELECTRONIC ENGINE CONTROL SYSTEM / SHIFTED TO ALTITUDE MODE. CAPTAIN AIR SPEED & ALTITUDE REMAINED ERRONEOUS UNTIL 5000-8000FT WHEN THEY SEEMED NORMAL. / R&R LEFT ANGLE OF ATTACK SENSOR PER AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 66,588 hrs · 39,231 cycles

R1 DOOR GIRT BAR R/H STOWAGE HOOK NOT SECURE ENOUGH TO RETAIN GIRT BAR. / REPOSITIONED SLIDE IAW AMM.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 66,040 hrs · 38,875 cycles

L2 DOOR EMERGENCY EXIT SIGN LIGHT BURNED OUT BULB. R&R BULB PER AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,040 hrs · 38,875 cycles

EMERGENCY EXIT LIGHT ON FORWARD LAV HAD SEGMENT INOP. RELAMPED LIGHT PER AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,040 hrs · 38,875 cycles

EMERGENCY EXIT LIGHT BATTERY PACK M1669 DID NOT CHARGE. R&R BATTERY PACK M1669 PER AMM.

Part: STRAP — CORRODED (ESCAPE HATCH) · airframe 66,040 hrs · 38,875 cycles

R/H EMERGENCY EXIT HATCH ESCAPE STRAP ANCHOR CORRODED. / R&R STRAP PER AMM.

Part: STRAP — CORRODED (ESCAPE HATCH) · airframe 66,040 hrs · 38,875 cycles

L/H EMERGENCY EXIT HATCH ESCAPE STRAP ANCHOR CORRODED. R&R STRAP PER AMM.

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 66,040 hrs · 38,875 cycles

PANEL 193AR HAS DELAMINATED AREA ON OUTER SKIN (MID SPAN) / PANEL 193AR DELAMINATED AREA ON OUTER SKIN (MIDSPAN) WAS REPAIRED IAW SRM 51-70-05-2R-1 56144U 08/12/2019

Part: SEAT TRACK — CORRODED (BS 370-480) · airframe 66,040 hrs · 38,875 cycles

SEAT TRACK CROWN CORRODED BETWEEN BS. 370 TO BS. 480, LBL 45. R&R SEAT TRACK IAW SRM AND DWG.

Part: STIFFENER — CRACKED (WHEEL WELL LH) · airframe 66,040 hrs · 38,875 cycles

L/H BS663 LOWER VAPOR BARRIER VERTICAL STIFFENER IS CRACKED IN THE RADIUS AT LBL25 WL145 / REMOVED L/H BS 663 CRACKED VERTICAL STIFFNER BS 663 LBL 25 WL 145 PER SRM 51-40-02-0G-0. LOCATED; DRILLED AND DEBURRED NEW STIFFNER PER SRM 51-40-05-0G-0; DWG 111A1000; OK TO INSTALL. LEAD 269 13AUG19 INSP 15 13AUG19 INSTALLED VERTICAL STIFFNER ON L/H BS 663 VAPOR BARRIER; LBL 25 WL 145 PER SRM 51-40-02-0G-0. DWG 111A1000.

Part: ANGLE — CRACKED (BS 663) · airframe 66,040 hrs · 38,875 cycles

LOWER VAPOR BARRIER COMPOSITE BULKHEAD UPPER ATTACH ANGLE CRACKED AT BS. 663, LBL 9. REPAIRED ANGLE PER ER AND EA.

Part: SKIN — OBSTRUCTED (AFT FUSELAGE) · airframe 66,040 hrs · 38,875 cycles

ACCESS SKIN AT BS1016 BL0 AS REQUIRED TO FACILITATE PRESSURE WEB REPAIR / REPAIRED SKIN AT B.S 1016 BL 0 PER ATS ER 19-04184 REV IR AND SWA EA# 1-753-35478 REV IR

Part: WEB — CORRODED (BS 351-360) · airframe 66,040 hrs · 38,875 cycles

E-BAY VERTICAL WEB CORRODED BETWEEN BS. 351 TO BS. 360, STR. 28L. / R&R WEB PER SRM & DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 66,040 hrs · 38,875 cycles

L/H HORIZONTAL STABILIZER REMOVABLE LEADING EDGE RIB AT LEADING EDGE STA. 123.85 CRACKED. R&R RIB IAW SRM AND DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 66,040 hrs · 38,875 cycles

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

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 66,040 hrs · 38,875 cycles

AFT CARGO BAY FLOOR SPLICE HAS CORROSION AT BS767+6 WL156 RBL10 TO LBL10 / RECEIVED NEW ACB FLOORSPLICE AT 767+6 ON PO# 717082 NEW PART WILL BE INSTALLED ON JPANEL-141-CLOSE

Part: STRAP — CORRODED (AFT CARGO COMPT) · airframe 66,040 hrs · 38,875 cycles

AFT CARGO BAY FLOOR SPLICE HAS CORROSION AT BS727D+6 WL156 RBL10 TO LBL10 / RECEIVED NEW ACB SPLICE STRAP FOR B.S727D+6 ON PO# 724358 NEW PART WILL BE INSTALLED ON CARD# JPANEL-141-CLOSE

Part: BRACKET — CRACKED (AFT CARGO COMPT) · airframe 66,040 hrs · 38,875 cycles

AFT CARGO BAY; LOWER BULKHEAD SUPPORT PLATE IS CRACKED AT BS867 LBL10 WL163 / REMOVED AND REPLACED CRACK DAMAGED BRACKET WITH NEW BRACKET AT BS 867 LBL10 WL163 ALL IAW SRM 51-10-02-0G-0 SRM 51-40-05-0G-0 SRM 51-40-02-0G-0 AND IPC 53-42-51-06 43656R 17AUG19

Part: SUPPORT — CORRODED (BS 727-767) · airframe 66,040 hrs · 38,875 cycles

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

Part: CRADLE — CRACKED (FWD FLASHLIGHT) · airframe 66,040 hrs · 38,875 cycles

FORWARD EMERGENCY FLASHLIGHT BRACKET CRACKED AT FASTENER HOLE. R&R FLASHLIGHT BRACKET IAW SIP AND DWG.

Part: SHIELD — CORRODED (BS 847-867) · airframe 66,040 hrs · 38,875 cycles

AFT CARGO BAY SHIELD AFT OF THE DOOR CORRODED BETWEEN BS. 847 TO BS. 867, RBL 23. / R&R SHIELD IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 867-885) · airframe 66,040 hrs · 38,875 cycles

AFT CARGO BAY, R/H FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS. 867 TO BS. 885, RBL 21. / R&R SUPPORT PER SRM & DWG.

Part: SUPPORT PLATE — CORRODED (BS 727-847) · airframe 66,040 hrs · 38,875 cycles

AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS. 727 TO BS. 847, LBL 23. / R&R SUPPORT PLATE IAW SRM & DWG.

Part: STRINGER CLIP — CORRODED (BS 767) · airframe 66,040 hrs · 38,875 cycles

STRINGER CLIP CORRODED AT BS. 767, STR. 26L. R&R STRINGER CLIP IAW SRM & DWG.

Part: DOUBLER — CHAFED (AFT FUSELAGE) · airframe 66,040 hrs · 38,875 cycles

FUSELAGE EXTERNAL SKIN HAS CHAFING DAMAGE ON EXISTING REPAIR DOUBLER BS 853 TO BS 861 BETWEEN STR 2L AND STR 2R (CONTACT ENGINEERING). / REPAIRED DAMAGE ON FUSELAGE EXTERNAL SKIN ON EXISTING REPAIR DOUBLER BS 853 TO BS 861 BETWEEN STR 2L AND 2R PER ER #19-04143 REV IR AND EA #1-753-35512 REV IR

Part: STRINGER CLIP — CORRODED (BS 787) · airframe 66,040 hrs · 38,875 cycles

STRINGER CLIP CORRODED AT BS. 787, STR. 26L. R&R STRINGER CLIP IAW SRM & DWG.

Part: WEB — CORRODED (BS 847-867) · airframe 66,040 hrs · 38,875 cycles

AFT CARGO BAY VERTICAL WEB CORRODED ON FORWARD END BETWEEN BS. 847 TO BS. 867, STR. 27R. R&R WEB IAW SRM & DWG.

Part: SKIN — DAMAGED (AFT FUSELAGE) · airframe 66,040 hrs · 38,875 cycles

FUSELAGE EXTERNAL SKIN HAS CHAFING DAMAGE AT DORSAL FIN FOOTPRINT BS 867 TO BS 872 BETWEEN STR 1 AND STR 2L. / REPAIRED DAMAGE ON FUSELAGE EXTERNAL SKIN AT DORSAL FIN FOOTPRINT BS 867 TO BS 872 BETWEEN STR 1 AND STR 2L PER ER #19-04143 REV IR AND EA #1-753-35512 REV IR

Part: SHIELD — CORRODED (BS 420-440) · airframe 66,040 hrs · 38,875 cycles

FORWARD CARGO BAY SHIELD FORWARD OF CARGO DOOR CORRODED BETWEEN BS. 420 TO BS. 440, RBL 23. / R&R SHIELD PER SRM & DWG.

Part: ANGLE — CORRODED (BS 665) · airframe 66,040 hrs · 38,875 cycles

UPPER SURFACE OF CREASE BEAM WEB ATTACH ANGLE CORRODED AT BS. 665, RBL 66. / R&R ATTACH ANGLE IAW SRM AND DWG

Part: SEAT TRACK — CORRODED (BS 540-727B) · airframe 66,040 hrs · 38,875 cycles

SEAT TRACK CROWN CORRODED BETWEEN BS. 540 TO BS. 727B, RBL 25. R&R SEAT TRACK CROWN IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (BS 540-727B) · airframe 66,040 hrs · 38,875 cycles

SEAT TRACK CROWN CORRODED BETWEEN BS. 540 TO BS. 727B, LBL 45. / R&R SEAT TRACK CROWN IAW SRM AND DWG.

Part: SKIN — DAMAGED (CENTRE FUSELAGE) · airframe 66,040 hrs · 38,875 cycles

BROKEN NUTPLATE COMMON TO FWD ADF ANTENNA STA 693; BETWEEN STR 1-2 R/H. (MARKED) / DAMAGE TO SKIN PANEL COMMON TO ADF ANTENNA REPAIRED IAW EA #1-453-35504 REV IR AND ER# 19-04165 REV IR.

Part: SEAT TRACK — CORRODED (BS 480-520) · airframe 66,040 hrs · 38,875 cycles

SEAT TRACK CROWN CORRODED BETWEEN BS. 480 TO BS. 520, LBL 45. R&R SEAT TRACK IAW DWG AND SRM.

Part: WEB — CORRODED (CARGO THRESHOLD) · airframe 66,040 hrs · 38,875 cycles

FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS. 440 TO BS. 494, RBL 23. / R&R WEB PER SRM AND DWG.

Part: WEB — CORRODED (CABIN) · airframe 66,040 hrs · 38,875 cycles

***CORROSION*** ON UPPER SURFACE OF CREASEBEAM WEB; STA 673; RBL 66; WL 208. (MARKED) / REPAIRED DAMAGE ON UPPER SURFACE OF CREASE BEAM WEB. BS 673; RBL66; WL208 PER ER # 19-04177 REV IR AND EA# 1-753-35381 REV IR.

Part: SEAT TRACK — CORRODED (BS 484-520) · airframe 66,040 hrs · 38,875 cycles

IOUS REPAIRED SEAT TRACK CROWN CORRODED BETWEEN BS. 484 TO BS. 520, RBL 25. / R&R SEAT TRACK IAW DWG AND SRM.

Part: SEAT TRACK — CORRODED (BS 480-520) · airframe 66,040 hrs · 38,875 cycles

SEAT TRACK CROWN CORRODED BETWEEN BS. 480 TO BS. 520, LBL 25. R&R SEAT TRACK IAW DWG AND SRM.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 66,040 hrs · 38,875 cycles

FWD CARGO BAY; FWD CORNER SCUFF PLATE IS CRACKED / REMOVED REPAIRED AND REINSTALLED FORWARD CARGO BAY FWD CORNER SCUFF PLATE IAW EA 1-A53-2076 REV II.

Part: RETAINER — CRACKED (RIGHT WING) · airframe 66,040 hrs · 38,875 cycles

RT WING UPPER T/E PANEL JUST AFT OF #2 PYLON; HORIZ. SEAL RETAINER IS CRACKED. / REMOVED AND REPLACED SEAL RETAINER RT WING UPPER TE PANEL JUST AFT OF #2 PYLON; IAW SRM 51-40-02-0G-0 AND FASTENERS AFT OF #2 PYLON; IAW SRM 51-40-02-0G AND FASTENERS IAW AIPC 57-50-00-25 89813U 07-26-19

Part: FRAME — CRACKED (BS 312) · airframe 66,040 hrs · 38,875 cycles

312 FRAME CRACKED L/H ABOVE L1 DOOR CUTOUT. REPAIRED FRAME PER ER AND EA.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 66,040 hrs · 38,875 cycles

LOWER COMPOSITE BULKHEAD CRACKED AT BS. 663, LBL 45. / R&R BULKHEAD VAPOR BARRIER IAW SRM & DWG.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 66,040 hrs · 38,875 cycles

BOTH AFT CABIN DOOR EXIT LIGHT LENS DISCOLORED. R&R LENS PER AMM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 66,040 hrs · 38,875 cycles

LOWER COMPOSITE BULKHEAD CRACKED AT BS. 663, RBL 20. REPAIRED BULKHEAD IAW SRM.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 66,040 hrs · 38,875 cycles

AFT ENTRY CENTER LINE EXIT LIGHT LENS DISCOLORED. R&R LENS PER AMM.

Part: ANGLE — CRACKED (BS 663) · airframe 66,040 hrs · 38,875 cycles

LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE CRACKED AT BS. 663, RBL 10. / R&R ANGLE IAW SRM.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 66,040 hrs · 38,875 cycles

FORWARD ENTRY CENTER LINE EXIT LENS DISCOLORED. R&R LENS PER AMM.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 66,040 hrs · 38,875 cycles

L1 DOOR EXIT LIGHT LENSES DISCOLORED. R&R LENSES PER AMM.

Part: PRESSURE DECK — CRACKED (MAIN CABIN) · airframe 66,040 hrs · 38,875 cycles

UPON COMPLETION OF CCN:753-201-00-02 FOUND CRACKS ON HORIZONTAL PRESSURE DECK AT BS 667 LBL 32 WL 201 AND BS 667 LBL 41 WL 201 / REPAIRED CRACKS ON HORIZONTAL PRESSURE DECK BS 667 LBL 32 WL201 + BS 667 LBL14 WL201 IAW SRM 53-40-51-2R-2 REPAIR 2.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 64,988 hrs · 38,212 cycles

L1 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER SIP.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 64,817 hrs · 38,106 cycles

RT PHOTOLUMINESCENT STRIP DAMAGED AT 1ST SECTION. INSTALLED STRIP IAW AMM.

Part: CLAMP — LOOSE (R1 DOOR) · airframe 63,903 hrs · 37,525 cycles

R1 DOOR GIRT BAR CLIPS LOOSE. ADJUSTED GIRT BAR CLAMPS IAW SIP.

Part: COVER — UNSECURE (CABIN) · airframe 63,894 hrs · 37,519 cycles

REAR GALLEY EMERGENCY EXIT LIGHT COVER FELL OFF. R&R LIGHT ASSEMBLY PER MMM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 63,577 hrs · 37,312 cycles

RT HORIZONTAL STABILIZER RIB AT STA 129.5 CRACKED AT FORWARD LOWER OUTBOARD END. R&R RIB IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 63,577 hrs · 37,312 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STA 120.3, 2ND STIFFENER FROM THE FRONT, LOWER FLANGE. REPAIRED RIB PER SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 63,577 hrs · 37,312 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STAB STA 120.3, 3RD STIFFENER FROM FRONT. REPAIRED RIB IAW SRM.

Part: SLIDE — UNSECURE (L2 DOOR) · airframe 62,675 hrs · 36,712 cycles

L2 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER MT.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 61,443 hrs · 35,918 cycles

RIGHT OVERWING EMERGENCY LIGHT LENS LOOSE. R & R THE LENS IAW AMM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 61,391 hrs · 35,888 cycles

R2 DOOR SLIDE HAD LOW PRESSURE. R & R THE SLIDE IAW MT.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 60,939 hrs · 35,600 cycles

BULKHEAD WEB CRACKED AT BS 663, BETWEEN RBL 38 AND RBL 60. REPAIRED THE BULKHEAD WEB IAW EA.

Part: SWITCH — FAULTY (EMERGENCY LIGHTS) · airframe 60,368 hrs · 35,236 cycles

CABIN EMERGENCY EXIT LIGHTS ILLUMINATED ON TAKEOFF. R & R THE SWITCH IAW WDM AND AMM.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 60,368 hrs · 35,236 cycles

RIGHT EMERGENCY EXIT LIGHTS FAULTY. REPAIRED A WIRE IAW AMM.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 60,368 hrs · 35,236 cycles

LEFT EMERGENCY LIGHT FAULTY. REPAIRED A WIRE IAW AMM.

Part: LIGHT — DIM (CABIN) · airframe 59,849 hrs · 34,902 cycles

LT OVERWING EMERGENCY EXIT LIGHT IN FRONT OF EXIT HATCH DIM. RELAMPED LIGHT PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,606 hrs · 34,748 cycles

LT OVERHEAD BIN EMERGENCY LIGHT INOP BETWEEN ROW 4 TO ROW 12. R&R BATTERY PACK IAW AMM AND WDM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 59,606 hrs · 34,748 cycles

RT MID DOOR EMERGENCY PASSENGER CABIN ESCAPE HATCH LIGHT INOP. RECONNECTED CONNECTOR IAW AMM AND WDM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 59,606 hrs · 34,748 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STATION 105. R&R RIB IAW SRM AND DWG.

Part: STRINGER — CRACKED (RT WING) · airframe 59,606 hrs · 34,748 cycles

RT WING INBOARD FIXED LEADING EDGE STRINGER CRACKED AT OUTBOARD AFT FASTENER HOLE BETWEEN WS 180 TO WS 204. R&R STRINGER IAW SRM AND DWG.

Part: PLATE — CRACKED (LT WING) · airframe 59,606 hrs · 34,748 cycles

LT WING WIGGLE PLATE CRACKED AT ORSS 261. R&R WIGGLE PLATE IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,606 hrs · 34,748 cycles

FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME IAW ER AND EA.

Part: WEB — DELAMINATED (WHEEL WELL LH) · airframe 59,606 hrs · 34,748 cycles

(COSTOMER REQEST) 663 L/H LOWER EXISTING REPAIR IS DELAMINATED / INSTALLED REPAIR IN 3 BAYS IAW SRM 57-10-10-2R-2 IN BAYS 1;2 AND 4. REMOVED DELAMINATED EXISTING REPAIR AND REPAIRED IAW SRM 57-10-10-2R-2 AT BS 663 I/H LWR VAPOR BARRIER

Part: DOOR — CORRODED (LOWER EXT FUSELA) · airframe 59,606 hrs · 34,748 cycles

CORROSION ON LAV SERVICE DOOR AROUND GROUND STRAP AND HINGES / REPLACED LAV SERVICE DOOR IAW ATS ER 17-03146 IR AND SWA EA 1-752-2086 IR. REMOVED CORROSION IN AN AREA OF 1.5'X1.5'X.028. FOUND TO BE OUT OF LIMITS IAW SRM 52-40-01-1A-4

Part: ANGLE — CRACKED (ECS BAY RH) · airframe 59,606 hrs · 34,748 cycles

ANGLE ON FWD SIDE OF BS 663 CRACKED AT RBL 9 APPROX. WL156 / REMOVED CRACKED ANGLE + REPLACED WITH NEW P/N 111A130106 IAW SRM 51-40-02-0G-0; 51-40-05-0G-0 AND BOEING DWG 111A1000

Part: ANGLE — CRACKED (ECS BAY LH) · airframe 59,606 hrs · 34,748 cycles

ANGLE ON FWD SIDE OF BS 663 CRACKED AT LBL 9 APPROX. WL156 / REMOVED CRACKED STIFFENER (ANGLE) ON FWD SIDE OF BS 663 LBL 9 WL156 IAW SRM 51-40-02. LOCATED; DRILLED AND INSTALLED NEW ANGLE IAW SRM 51-40-05-0G-0; SRM 51-40-02 AND BOEING DRWG# 111A1000 REV B

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 59,606 hrs · 34,748 cycles

INTERCOSTAL CRACKED AT FLOOR BOARD HOLES BS 312-328 RBL 29 WL 208 / REMOVED DAMAGED INTERCOSTAL AND REPLACED WITH NEW PART# 141A541OU12 PO# 593172 IAW SRM 51-40-02-0G-0 AND BOEING DWG# 141A5400 AT LOCATION BS 312-328 RBL 29 WL 208 56433C 01JULY17

Part: FLOOR SUPPORT — CRACKED (BS 294-312) · airframe 59,606 hrs · 34,748 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 294.5 TO 312, RBL 16. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 59,606 hrs · 34,748 cycles

FORWARD SERVICE DOOR STUB FRAME CRACKED AT BS 294, RBL 55. REPAIRED STUB FRAME IAW ER AND EA.

Part: WEB — DAMAGED (CABIN) · airframe 59,606 hrs · 34,748 cycles

CREASE BEAM WEB AT BS 332.10 TO BS 344; RBL 55 WL 208 HAS DAMAGE / REPAIRED DAMAGED CREASE BEAM WEB AT BS 332.10 TO 344. RBL 55 WL 208 IAW ATS ER 17-03162 REV IR AND SWA EA 1-753-31451 REV IR

Part: WEB — CORRODED (BS 986) · airframe 59,606 hrs · 34,748 cycles

L2 DOOR UPPER SURFACE OF CABIN FLOOR WEB CORRODED AT BS. 986, LBL 39. R & R THE FLOOR WEB IAW SRM AND DWG.

Part: BRACKET — CRACKED (#2 ENGINE) · airframe 59,606 hrs · 34,748 cycles

#2 ENGINE OUTBOARD FAN COWL BRACKET FORWARD OF AFT HOLD OPEN ROD IS CRACKED / REMOVED & REPLACED #2 ENGINE; OUTBOARD FAN COWL BRACKET FORWARD OF AFT HOLD OPEN ROD. REF SRM 51-40-02-0G-0 PARA 5 & PARA 9 & CMM 71-13-30

Part: PANEL — DELAMINATED (R/H WING) · airframe 59,606 hrs · 34,748 cycles

R/H WING PANEL # 621 RB HAS DELAMINATED CORNER AT FWD INBOARD CORNER / REPAIRED DELAMINATED CORNER AT FWD INBOARD CORNER ON R/H WING PANEL #621RB. IAW SRM 57-41-01-2R-1 AND IAW SRM 51-70-04-2R-13

Part: ANGLE — CORRODED (FUSELAGE) · airframe 59,606 hrs · 34,748 cycles

***CORROSION*** INNER CHORD & ANGLE CORRODED SEVERAL AREAS AT FWD ENTRY DOOR SILL STA 306-STA 335; WL 208; LBL 57 / REMOVED CORROSION FROM MOPSILL 3.0' X .65' X .012 PER SRM 51-10-02; ORIGINAL THICKNESS .090' REMAINING .078'; REMOVED CORROSION FROM ANGLE 1'X3'X.012' PER SRM 51-10-02; ORIGINAL THICKNESS .080'; REMAINING .068'; BOTH OUT OF LIMITS PER SRM 53-10-15-1A-1; REMOVED AND REPLACED MOSILL AND ANGLE PER SRM 51-40-02; DWG# 141A8110

Part: DOOR SILL — CORRODED (BS 305-345) · airframe 59,606 hrs · 34,748 cycles

FORWARD GALLEY DOOR SILL CORRODED BETWEEN BS 305 TO 345, RBL 57. REPAIRED IAW SRM AND DWG.

Part: PANEL — CRACKED (FUSELAGE) · airframe 59,606 hrs · 34,748 cycles

PANEL # 195 CL HAS CRACK AT AFT END AT BEND / REPAIRED CRACK AT AFT END OF PANEL #195CL PER SRM 53-40-70-2R-1 AND SRM 51-70-05-2R-10

Part: STRAP — CORRODED (FUSELAGE) · airframe 59,606 hrs · 34,748 cycles

***CORROSION*** AFT CARGO DOOR LOWER MAIN SILL STRAP AT APPROX. BS 785 HAS SEVERAL AREAS OF CORROSION / REMOVED AND REPLACED LOWER MAIN SILL STRAP AT STA 785 I.A.W. SRM 51-40-02-0G-0 AND DWG# 146A8120

Part: INTERCOSTAL — DAMAGED · airframe 59,606 hrs · 34,748 cycles

INTERCOSTAL BETWEEN FLOOR BEAMS; AT STA 312 & STA 328; LBL 42 DAMAGED AT TOP CHORD / REMOVED & REPLACED INTERCOSTAL IAW SRM 51-40-02 & DWG. #141A5400 BS312-328 LBL42

Part: INTERCOSTAL — DAMAGED · airframe 59,606 hrs · 34,748 cycles

INTERCOSTAL BETWEEN FLOOR BEAMS; AT STA 328 & STA 344; LBL 42 DAMAGED AT TOP CHORD / INTERCOSTAL BETWEEN FLOOR BEAMS AT STA 328 & 344 LBL 42 HAD DAMAGE 1.3'X1' AND OUT OF LIMITS IAW SRM 53-10-51-1A-1 REMOVED DMAAGED INTERCOSTAL IAW SRM 51-40-02-0G-0 LOCATED & DRILLED NEW INTERCOSTAL PART #141A5410.16 IAW SRM 51-40-05-0G-0 AND BOEING DWG 114A5400 AND SRM 51-40-02-0G-0

Part: PANEL — DELAMINATED (LEFT WING) · airframe 59,606 hrs · 34,748 cycles

LOWER LEADING EDGE ACCESS PANEL 521VB HAS DELAM AT CORNER (MARKED) / REPAIRED DELAM AT CORNER ON LOWER LEADING EDGE ACCESS PANEL 521VB IAW SRM 57-41-01-2R-1 AND IAW SRM 51-0-04-2R-13

Part: WEB — CORRODED (FUSELAGE) · airframe 59,606 hrs · 34,748 cycles

AFT CARGO BIN BILGE AREA VERTICAL WEB CORRODED BETWEEN BS 767 TO BS 777, RBL 4. R&R WEB IAW SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 59,606 hrs · 34,748 cycles

AFT CARGO BIN BILGE AREA VERTICAL WEB CORRODED AT BS 793, RBL 4. R&R WEB IAW SRM AND DWG.

Part: PANEL — DELAMINATED (LEFT WING) · airframe 59,606 hrs · 34,748 cycles

LOWER LEADING EDGE ACCESS PANEL 521WB HAS DELAM AT CORNER (MARKED) / REPAIRED DELEN AT CORNER ON LOWER LEADING EDGE ACCESS PANEL 521WB IAW SRM 57-41-01-2R-1 AND IAW SRM 51-70-04-2R-13

Part: PANEL — DELAMINATED (LEFT WING) · airframe 59,606 hrs · 34,748 cycles

LOWER LEADING EDGE ACCESS PANEL 521DB HAS DELAM AT CORNER (MARKED) / REPAIRED DELAM AT CORNER ON LOWER LEADING EDGE ACCESS PANEL 521DB IAW SRM 57-41-01-2R-1 AND IAW SRM 51-70-05-2R-10

Part: PANEL — CORRODED (NLG WHEEL BAY) · airframe 59,606 hrs · 34,748 cycles

PANEL 114AC HAS CORROSION AROUND MOUNTING HOLES INTERIOR SIDE. / REPLACED PANEL 114AC WITH SERVICABLE PANEL IAW AMM 53-14-01 PERFORMED LEAK CHECK ON PANEL 114AC IAW AMM 05-51-91-790-801 LEAK CHECK GOOD

Part: FLOORBEAM — CORRODED (BS 951) · airframe 59,606 hrs · 34,748 cycles

CABIN FLOORBEAM CORRODED AT BS 951.5, BETWEEN RBL 33 TO RBL 39.5, ON LOWER SURFACE OF UPPER FLANGE. R & R THE FLOORBEAM SUPPORT ANGLE IAW SRM AND DWG.

Part: PANEL — DELAMINATED (LEFT WING) · airframe 59,606 hrs · 34,748 cycles

LOWER LEADING EDGE ACCESS PANEL 521NB HAS DELAM AT CORNER (MARKED) / REPAIRED DELAM AT CORNER ON LOWER LEADING EDGE ACCESS PANEL 521NB IAW SRM 57-41-01-2R-1 AND IAW SRM 51-70-05-2R-10

Part: SPLICE — CORRODED (FUSELAGE) · airframe 59,606 hrs · 34,748 cycles

AFT CARGO BIN FLOOR SUPPORT SPLICE CORRODED AT BS 887, BETWEEN LBL 20 TO RBL 20. R&R SPLICE IAW SRM AND DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 59,606 hrs · 34,748 cycles

AFT CARGO BIN LT Z CHANNEL CORRODED BETWEEN BS 727A TO BS 807. REPAIRED Z CHANNEL IAW DWG & SRM.

Part: INTERCOSTAL — CORRODED (CABIN FLOOR) · airframe 59,606 hrs · 34,748 cycles

***CORROSION*** FOUND ON CABIN FLOOR INTERCOSTAL AROUND FASTENER HOLE ON UPPER AND LOWER SURFACES OF UPPER FLANGE. STA959 RBL 30 / EVALUATED DAMAGE ON CABIN FLOOR INTERCOSTAL FASTENER UPPER @ LOWER FOUND TO BE OUT OF LIMITS PER SRM 53-70-51; FIG. 103. DET. A REMOVED AND REPLACED SUPPORT STRIFFENER (NEW PART REPLACEMENT 147A576505) ON BS 959; RBL 30; IAW SRM 51-40-02-0G-0 AND DWG. 187A5760

Part: WEB — CORRODED (BS 986-1016) · airframe 59,606 hrs · 34,748 cycles

R2 DOOR UPPER SURFACE OF CABIN FLOOR WEB CORRODED BETWEEN BS 986 TO 1016, BETWEEN RBL 37 TO RBL 45. R & R THE WEB IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (CABIN) · airframe 59,606 hrs · 34,748 cycles

***CORROSION*** FOUND ON CABIN FLOOR INTERCOSTAL AROUND FASTENER ON UPPER SURFACE OF UPPER FLANGE. STA 951.5 RBL 30 / REMOVED AND REPLACE SUPPORT FLOOR ON NON ROUTINE CARD DEFECT NUMBER N096830

Part: BEAM — ELONGATED (RIGHT WING) · airframe 59,606 hrs · 34,748 cycles

TOP OF WING T/E PANEL ATTACH POINT TO GUIDE ARM HAS ELONGATED MOUNT BOLT HOLES; R/H WING APPROX. RSS 284; AFT OF R/H ENG PYLON SAIL FIN / REPAIRED TOP OF WING T/E PANEL ATTACH POINT TO GUIDE ARM ELONGATED MOUNT BOLT HOLES. RIGHT WING RSS289; AFT OF R/H ENG PYLON SAILFIN IAW SRM57-51-02-2R-1 REPAIR 1. AND SRM57-51-02-2R-4 REPAIR 4 AND EA: 1-A57-3523 REV-.

Part: FRAME — CRACKED (BS 480) · airframe 59,606 hrs · 34,748 cycles

FRAME CRACKED AT BS 480, STRINGER 8L. REPAIRED THE FRAME IAW EA.

Part: FRAME — CRACKED (BS 867) · airframe 59,606 hrs · 34,748 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,606 hrs · 34,748 cycles

FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER EA.

Part: BRACKET — CRACKED (RIGHT WING) · airframe 59,606 hrs · 34,748 cycles

I/B ATTACH BRACKET CRACKED; FOR I/B AUX TRACK ON #8 L/E SLAT; WHERE TRACK ATTACHES TO LOWER SEAL PLATE / REMOVED AND REPLACED #8 L/E SLAT; I/B AUX TRACK LOWER SEAL PLATE I/B ATTACH BRACKET IAW SOPM 20-50-01

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,606 hrs · 34,748 cycles

FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,606 hrs · 34,748 cycles

FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (BS 440) · airframe 59,606 hrs · 34,748 cycles

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

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 59,606 hrs · 34,748 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT HSS 123.85. REPAIRED RIB IAW SRM & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,606 hrs · 34,748 cycles

FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,606 hrs · 34,748 cycles

FRAME SUPPORT BRACKET CRACKED AT BS 867, STR 8R. REPAIRED FRAME ER EA.

Part: SUPPORT BRACKET — CRACKED (BS 747) · airframe 59,606 hrs · 34,748 cycles

FRAME SUPPORT BRACKET CRACKED AT BS 747, STRINGER 8R. REPAIRED THE FRAME SUPPORT BRACKET IAW EA.

Part: WEB — CORRODED (AFT CARGO THRESH) · airframe 59,606 hrs · 34,748 cycles

***CORROSION*** AFT CARGO BAY THRESHOLD WEB HAS CORROSION FROM STA 803-836 RBL 30 / REMOVED CORROSION OF AFT CARGO BAY THRESHOLD WEB IN AN AREA OF 6'X2.5'X.009' OF AN ORIGINAL THICKNESS OF 0.045' FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 FIG 103 DETAIL D. REMOVED AND REPLACED AFT CARGO BAY THRESHOLD WEB. IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A8340 SH 9 REV 9

Part: FRAME — CRACKED (BS 727D) · airframe 59,606 hrs · 34,748 cycles

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

Part: FLOORBEAM — CORRODED (BS 986.5) · airframe 59,606 hrs · 34,748 cycles

FLOORBEAM UPPER ANGLE CAP CORRODED AT BS 986.5, LBL 43. REPAIRED THE FLOORBEAM ANGLE CAP IAW SRM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 59,606 hrs · 34,748 cycles

FLOOR PANEL 222AF HAS DAMAGE 5' FROM O/B EDGE UPPER SURFACE / REPAIRED DAMAGE 5' FROM O/B EDGE UPPER SURFACE OF FLOOR PANEL 222AF PER SRM 53-00-50-2R-1

Part: CHANNEL — CORRODED (BS 736-767) · airframe 59,606 hrs · 34,748 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CHANNEL CORRODED BETWEEN BS 736 TO 767, BETWEEN RBL 23 TO RBL 25. R & R THE CHANNEL IAW SRM & DWG.

Part: SUPPORT BRACKET — CRACKED (BS 500C) · airframe 59,606 hrs · 34,748 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,606 hrs · 34,748 cycles

FRAME SUPPORT BRACKET CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER EA.

Part: SILL DRAIN — CORRODED (ASD THRESHOLD) · airframe 59,606 hrs · 34,748 cycles

***CORROSION*** AFT SERVICE DOOR LOWER SILL (MOPSILL) INNER CHORD HAS CORROSION FROM STA 957-994 / REMOVED CORROSION FROM AFT SERVICE DOOR MOPSILL INNER CHORD BS 957-994 IN AN AREA 24'X2'X.025' AND FOUND OUT OF LIMITS IAW SRM 53-70-15-1A-1. REMOVED AND REPLACED AFT SERVICE DOOR MOPSILL INNER CHORD IAW SRM 51-40-02-0G-1 AND DQG 147A8501 REV-

Part: GUSSET — CRACKED (FUSELAGE) · airframe 59,606 hrs · 34,748 cycles

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

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 59,606 hrs · 34,748 cycles

FLOOR PANEL 221DF HAS DAMAGE 11' FROM O/B EDGE UPPER SURFACE / REPAIRED DAMAGE 11' FROM O/B EDGE UPPER SURFACE ON FLOOR PANEL 221DF PER SRM 53-00-50-2R-1

Part: GUSSET — CRACKED (FUSELAGE) · airframe 59,606 hrs · 34,748 cycles

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

Part: SHIELD — CORRODED (BS 768.5-785.5) · airframe 59,606 hrs · 34,748 cycles

AFT CARGO BAY RT FORWARD SHIELD FORWARD OF CARGO DOOR, FOUND CORRODED BETWEEN BS 768.5 TO 785.5. R & R THE SHIELD IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (BS 952-983) · airframe 59,606 hrs · 34,748 cycles

L2 DOOR LOWER SILL INNER STRUCTURE CORRODED BETWEEN BS 952 TO 983. R & R THE DOOR SILL IAW SRM & DWG.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 59,606 hrs · 34,748 cycles

CABIN FLOOR PANEL 222DF IS DAMAGED AROUND INSERT HOLE FWD O/B (MARKED) / REPAIRED DAMAGE AROUND INSERT HOLE FWD O/B AND INSTALLED INSERT SLP5182A3-1 AND SLA5182A3-300-2; RESIN BMS 5-1076 LOT#AKAP4730K ON CABIN FLOOR BOARD 222DF PER SRM 53-00-50-2R-2; BOEING DWG 141A5810 SHT 185 REV:B

Part: FLOORBEAM — CORRODED (BS 986.5) · airframe 59,606 hrs · 34,748 cycles

FLOORBEAM UPPER CAP CORRODED AT BS 986.5, BETWEEN RBL 35.5 TO RBL 40. R & R THE FLOORBEAM ANGLE CAP SRM.

Part: GUSSET — CRACKED (BS 500D) · airframe 59,606 hrs · 34,748 cycles

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

Part: SHIELD — CORRODED (FUSELAGE) · airframe 59,606 hrs · 34,748 cycles

AFT CARGO FLOOR CLOSEOUT PANEL SHIELD CORRODED AT BS 854, RBL 20. R&R SHIELD IAW DWG & SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,606 hrs · 34,748 cycles

FRAME SUPPORT BRACKET CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,606 hrs · 34,748 cycles

FRAME SUPPORT BRACKET CRACKED AT BS 827, STR 8R. REPAIRED FRAME IAW EA.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 59,606 hrs · 34,748 cycles

AFT CARGO FLOOR PANEL TEE SPLICE CORRODED AT BS 772. R&R TEE SPLICE PER SRM AND DWG.

Part: BRACKET — ELONGATED (LEFT WING) · airframe 59,606 hrs · 34,748 cycles

TOP OF L/H WING T/E PANEL ATTACH BRACKET MOUNT HOLES ARE ELONGATED; RSS 272; JUST I/B OF #5 SPOILER / REPAIRED TOP OF L/H WING T/E PANEL ATTACH BRACKET MOUNT HOLES AT RSS 272 JUST I/B OF #5 SPOILER IAW SRM 57-51-02-2R-4 REPAIR 4.

Part: SPLICE — CORRODED (FLOOR PANEL) · airframe 59,606 hrs · 34,748 cycles

AFT CARGO FLOOR PANEL TEE SPLICE CORRODED AT BS 727D. R&R TEE SPLICE PER SRM AND DWG.

Part: FITTING — BROKEN (LOWER EXT FUSELA) · airframe 59,606 hrs · 34,748 cycles

PANEL #192E FWD R/H ATTACH FITTING IS BROKEN / REMOVED FWD R/H ATTACH FITTINGS ON PANEL #192E IAW SRM 51-40-02-0G-0 STEP D;3;5 AND 6. LOCATED; DRILLED AND INSTALLED FWD R/H ATTACH FITTING IAW SRM 51-40-05-0G-0 STEP (4)1; SRM 51-40-02-0G-0; BOEING DRAWING 149A7701 REV.A.

Part: PLATE — CRACKED (AFT CARGO COMPT) · airframe 59,606 hrs · 34,748 cycles

AFT CARGO AFT NET TIE DOWN PLATE CRACKED / REMOVED & REPLACED AFT CARGO AFT NET TIE DOWN PLATE IAW SOPM 20-50-01

Part: PLATE — CRACKED (AFT CARGO COMPT) · airframe 59,606 hrs · 34,748 cycles

AFT CARGO FWD NET TIE DOWN PLATE CRACKED / REMOVED AND REPLACED AFT CARGO FWD NET TIE DOWN PLATE IAW SOPM 20-50-01

Part: SLIDE — LOOSE (R1 DOOR) · airframe 59,231 hrs · 34,520 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. REINSTALLED SLIDE IAW MT.

Part: LENS — DISCOLORED (EMERGENCY LIGHT) · airframe 58,974 hrs · 34,369 cycles

RIGHT OVERWING EMERGENCY LIGHT LENS DISCOLORED. R & R THE LENS IAW MM.

Part: LIGHT — LOOSE (EXIT SIGN) · airframe 58,562 hrs · 34,113 cycles

R2 DOOR EMERGENCY EXIT SIGN LIGHT LOOSE. R&R LIGHT IAW AMM.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 58,272 hrs · 33,927 cycles

L1 DOOR EGRESS EXIT SIGN LENS FELL OFF. R&R SIGN BASE PER AMM.

Part: COVER — LOOSE (R2 DOOR SLIDE) · airframe 57,566 hrs · 33,519 cycles

R2 DOOR EMERGENCY SLIDE COVER LOOSE. SECURED THE SLIDE COVER IAW MT.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 57,507 hrs · 33,485 cycles

L2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: PLATE — CRACKED (LT WING) · airframe 55,837 hrs · 32,486 cycles

LEFT WING LOWER TE PANEL ATTACH WIGGLE PLATE, INBD OF ENG STRUT CRACKED. R & R WIGGLE PLATE IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 55,837 hrs · 32,486 cycles

RIGHT WING OTBD ANGLE CRACKED FOR FIXED UPPER TE PANEL AT NR 6 CANOE. R & R ANGLE IAW SRM.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 55,837 hrs · 32,486 cycles

LEFT WING INBD FLAP, UPPER SURFACE TE WEDGE DELAMINATED. REPAIRED WEDGE IAW EA.

Part: PLATE — LOOSE (L2 DOOR) · airframe 55,837 hrs · 32,486 cycles

L2 DOOR FWD SLIDE MOUNT PLATE BRACKET LOOSE ON DOOR. R & R MOUNT PLATE IAW SRM.

Part: FLAP TRACK — LOOSE (TE FLAP) · airframe 55,837 hrs · 32,486 cycles

LEFT WING OTBD AFT FLAP, OTBD TRACK ATTACH LOOSE. R & R FLAP TRACK IAW AMM.

Part: FLAP TRACK — LOOSE (TE FLAP) · airframe 55,837 hrs · 32,486 cycles

LEFT WING OTBD AFT FLAP, SECOND ATTACH TRACK LOOSE AT FLAP. R & R FLAP TRACK IAW AMM.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 55,837 hrs · 32,486 cycles

LEFT WING TE UPPER PANEL, BETWEEN NR 5 & 6 SPOILERS AFT SUPPORT BRACKET, CRACKED AT UPPER OTBD FASTENERS. R & R BRACKET IAW SRM.

Part: FLAP TRACK — LOOSE (TE FLAP) · airframe 55,837 hrs · 32,486 cycles

LEFT WING OTBD AFT FLAP, INBD TRACK ATTACH LOOSE. R & R FLAP TRACK IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,837 hrs · 32,486 cycles

RIGHT CTR INTERCOSTAL CRACKED AT BS 540. R & R INTERCOSTAL IAW SRM.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 53,597 hrs · 31,190 cycles

R1 DOOR OVERHEAD EXIT SIGN INOPERATIVE. RE-CONNECTED CONNECTOR IAW WDM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,597 hrs · 31,190 cycles

RIGHT NR 3 WINDOW FRAME, CRACKED IN OTBD AT SECOND LOWER HOLE CORNER FASTENER HOLE. REPAIRED FRAME IAW EA.

Part: RIB — DAMAGED (LT HORIZ STAB) · airframe 53,597 hrs · 31,190 cycles

LEFT HORIZONTAL STABILIZER INSPAR RIB LOWER FLANGE DAMAGED AT STATION BS 101.9. REPAIRED FLANGE IAW ER & EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,597 hrs · 31,190 cycles

RIGHT HORIZONTAL STABILIZER 92.7, RIB CRACKED AT THE SECOND FROM REAR VERTICAL STIFFENER. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,597 hrs · 31,190 cycles

RIGHT HORIZONTAL STABILIZER 92.7, RIB CRACKED AT THE FIRST FROM REAR VERTICAL STIFFENER. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,597 hrs · 31,190 cycles

RIGHT HORIZONTAL STABILIZER 92.7, RIB CRACKED AT THE THIRD FROM REAR VERTICAL STIFFENER. REPAIRED RIB IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 53,597 hrs · 31,190 cycles

MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, LBL 41. REPAIRED WEB IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 53,597 hrs · 31,190 cycles

MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, RBL 35. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 53,597 hrs · 31,190 cycles

RIGHT WING NR 6 SLAT, LOWER SKIN CRACKED COMMON TO AFT SPAR, BETWEEN THE ACTUATOR RIBS. REPAIRED SKIN IAW SRM.

Part: SENSOR — FAULTY (TE FLAP) · airframe 52,236 hrs · 30,430 cycles

DIVERSION, TE FLAPS WILL NOT EXTEND WHEN FLAP LEVER MOVED TO POS 5. FLAP POSITION INDICATOR SHOWED RT FLAP AT UP & LT FLAP BETWEEN 1 & UP. R & R NR 3 FLAP SKEW SENSOR IAW MM.

Part: LENS — MISSING (CABIN) · airframe 49,979 hrs · 29,156 cycles

R2 DOOR LOWER EMER EXIT LIGHT LENS MISSING. R & R LIGHT ASSEMBLY IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 49,529 hrs · 28,912 cycles

R1 DOOR EMER EXIT SIGN INOPERATIVE. R & R LIGHT ASSEMBLY IAW MM.

Part: COVER — MISSING (CABIN) · airframe 48,757 hrs · 28,472 cycles

RIGHT EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER IAW SIP.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 48,008 hrs · 28,033 cycles

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

Part: RETAINER — OUT OF ADJUST (L1 DOOR) · airframe 47,854 hrs · 27,949 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINERS OUT OF ADJUSTMENT. ADJUSTED RETAINER ASSEMBLY IAW SIP.

Part: BATTERY — FAILED (CABIN) · airframe 47,088 hrs · 27,480 cycles

AFT LT EMERGENCY BATTERY PACKS FAILED TEST. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 47,088 hrs · 27,480 cycles

AFT RT EMERGENCY BATTERY PACKS FAILED TEST. R&R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 47,088 hrs · 27,480 cycles

AFT LT EMERGENCY BATTERY PACKS FAILED TEST. R & R BATTERY IAW MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 46,889 hrs · 27,354 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOW PRESSURE. R&R SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,889 hrs · 27,354 cycles

LT OVERHEAD BIN EMERGENCY EXIT LIGHT INOPERATIVE BETWEEN ROW 11 TO ROW 12. RELAMPED LIGHT IAW MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,889 hrs · 27,354 cycles

SKIN CRACKED AT STATION 540, STRINGER 22R. REPAIRED SKIN IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 46,889 hrs · 27,354 cycles

SEAT TRACK CRACKED AT STATION 727B, LBL 25.75. REPAIRED SEAT TRACK IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 48,057 hrs · 28,066 cycles

RT NR 1 WINDOW FRAME CRACKED IN OTBD UPPER CORNER. REPAIRED FRAME IAW EA.

Part: SLAT — CRACKED (LT WING) · airframe 46,889 hrs · 27,354 cycles

LT WING NR 2 SLAT CRACKED LOWER SIDE AT ACTUATOR RIB. REPAIRED SLAT IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 46,889 hrs · 27,354 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 46,889 hrs · 27,354 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 46,889 hrs · 27,354 cycles

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

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 46,889 hrs · 27,354 cycles

LT HORIZONTAL STABILIZER SKIN CRACKED AT IN SPAR RIB 175.50. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 46,699 hrs · 27,241 cycles

RT HORIZONTAL STABILIZER SKIN CRACKED IN LOWER STAB SKIN 41" OTBD OF FUSELAGE 10" FWD OF AFT SPAR. REPAIRED SKIN IAW SRM.

Part: SIGN — LOOSE (CABIN) · airframe 46,147 hrs · 26,920 cycles

L2 EMERGENCY EXIT LIGHTED SIGNS LOOSE. R & R SIGNS IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 46,147 hrs · 26,920 cycles

R2 EMERGENCY EXIT LIGHTED SIGNS LOOSE. R & R SIGNS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,777 hrs · 26,691 cycles

RIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED & REPLACED LIGHT IAW AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 45,173 hrs · 26,339 cycles

FORWARD ENTRY DOOR LOWER EMERGENCY EXIT LENS NOT STAYING ON BASE. SECURED LIGHT PER EA.

Part: FAIRING — DAMAGED (RT WING) · airframe 44,222 hrs · 25,725 cycles

RIGHT INBOARD CANOE HAS DAMAGE FROM FLAP OPERATING ROD BRACKETS SEPARATING. PERFORMED REPAIR PER EA.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 43,784 hrs · 25,454 cycles

L2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,856 hrs · 24,294 cycles

LT OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 22. RELAMPED LIGHT PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 40,746 hrs · 23,613 cycles

RT EEPLS BROKEN. REMOVED AND REPLACED EEPLS PER MM.

Part: SIGN — CRACKED (CABIN) · airframe 40,135 hrs · 23,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD LAVATORY EXTERIOR O/B EMERGENCY EXIT SIGN CRACKED. REMOVED AND REPLACED SIGN IAW MM.

Part: SIGN — CRACKED (CABIN) · airframe 40,135 hrs · 23,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND G1 GALLEY EMERGENCY EXIT SIGN CRACKED. REMOVED AND REPLACED SIGN IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 40,135 hrs · 23,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND R2 EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LENS IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,135 hrs · 23,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,135 hrs · 23,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,135 hrs · 23,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500A, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.

Part: FITTING — CORRODED (L2 DOOR) · airframe 40,135 hrs · 23,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS IAW MM.

Part: FITTING — CORRODED (R2 DOOR) · airframe 40,135 hrs · 23,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,135 hrs · 23,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,135 hrs · 23,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 360, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,135 hrs · 23,248 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500C, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.

Part: ATTACH FITTING — CORRODED (L1 DOOR) · airframe 40,135 hrs · 23,248 cycles

DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR ATTACH FITTING CORRODED AT BS 342, WL 208, LBL 55. REMOVED AND REPLACED FITTING IAW SOPM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 38,805 hrs · 22,486 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR LOW. REMOVED AND REPLACED SLIDE PER MM.

Part: COVER — BROKEN (CABIN) · airframe 37,590 hrs · 21,773 cycles

FWD ENTRY EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 36,707 hrs · 21,253 cycles

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

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,288 hrs · 21,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT CARGO FLOORBEAM SUPPORT CORRODED BS 772, RBL 7.5. REMOVED AND REPLACED BEAM PER EA.

Part: SKIN — CRACKED (TE FLAP) · airframe 36,288 hrs · 21,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD AFT FLAP LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,288 hrs · 21,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT CARGO FLOORBEAM SUPPORT CORRODED BS 772, LBL 7.5. REMOVED AND REPLACED BEAM PER EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,288 hrs · 21,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT CARGO FLOORBEAM SUPPORT CORRODED BS 772, RBL 2.5. REMOVED AND REPLACED BEAM PER EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 36,288 hrs · 21,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING O/B AFT FLAP INBOARD AFT CORNER DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: LIGHT — DAMAGED (CABIN) · airframe 36,288 hrs · 21,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND EEPLS PEELED. REMOVED AND REPLACED EEPLS PER MM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,288 hrs · 21,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT CARGO FLOORBEAM SUPPORT CORRODED BS 772, LBL 12. REMOVED AND REPLACED BEAM PER EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,288 hrs · 21,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT CARGO FLOORBEAM SUPPORT CORRODED BS 772, LBL 2.5. REMOVED AND REPLACED BEAM PER EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,288 hrs · 21,001 cycles

DURING SCHEDULED 10Y CHECK, FOUND AFT CARGO FLOORBEAM SUPPORT CORRODED BETWEEN BS 727 TO BS 736B, RBL 13. REMOVED AND REPLACED BEAM PER SRM AND BAC DWG.

Part: OVERHEAT SENSOR — FAULTY (MLG WW) · airframe 35,680 hrs · 20,642 cycles

DIVERSION - INTERMITTENT WHEEL WELL LIGHT AND FIREBELL AT CRUISE. REMOVED AND REPLACED WHEEL WELL OVERHEAT DETECTOR PER MM.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,281 hrs · 20,425 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,281 hrs · 20,425 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 34,345 hrs · 19,868 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT MID CABIN EMERGENCY EXIT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,345 hrs · 19,868 cycles

DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR FWD UPPER CORNER. REMOVED AND REPLACED FRAME SECTION PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 34,345 hrs · 19,868 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 34,345 hrs · 19,868 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 33,357 hrs · 19,266 cycles

L1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: LENS — BROKEN (CABIN) · airframe 33,074 hrs · 19,090 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 31,249 hrs · 18,005 cycles

RT OVERWING EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 31,249 hrs · 18,005 cycles

RT OVERWING EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 30,690 hrs · 17,675 cycles

L1 DOOR EMERGENCY EXIT SLIDE FELL OUT, DID NOT DEPLOY. SECURED SLIDE PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 30,121 hrs · 17,336 cycles

DURING SCHEDULED 8Y CHECK, FOUND FWD CENTER TANK SHEAR TIE CORRODED AT BS 540 LBL 54.6 TO RBL 32.4. REMOVED AND REPLACED TIE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,121 hrs · 17,336 cycles

DURING SCHEDULED 8Y CHECK, FOUND UPPER FLOORBEAM CORRODED AT BS 986.5 BETWEEN RBL 32 TO RBL 44. REMOVED AND REPLACED BEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 30,121 hrs · 17,336 cycles

DURING SCHEDULED 8Y CHECK, FOUND UPPER FLOORBEAM CAP CORRODED AT STATION 986.5 BETWEEN LBL 7 TO RBL 7. REMOVED AND REPLACED PER SWA EA.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 29,029 hrs · 16,701 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 27,285 hrs · 15,629 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 133.15. REPAIRED SKIN PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 27,285 hrs · 15,629 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 27,285 hrs · 15,629 cycles

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

Part: GLOWSTRIP — WORN (CABIN) · airframe 27,285 hrs · 15,629 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 13 DEF. REMOVED AND REPLACED STRIP PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 27,285 hrs · 15,629 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 133.15. REPAIRED SKIN PER SRM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 23,418 hrs · 13,405 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 6 ABC. SECURED STRIP PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,112 hrs · 13,234 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,112 hrs · 13,234 cycles

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

Part: COVER — MISSING (CABIN) · airframe 22,248 hrs · 12,749 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS LIGHT COVER MISSING AT ROW 6 DEF TO ROW 13 DEF. INSTALLED EEPLS LIGHT COVER PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 21,673 hrs · 12,414 cycles

R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: LATCH — BROKEN (L2 DOOR) · airframe 21,532 hrs · 12,335 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH BROKEN. REMOVED AND REPLACED EVAC SLIDE LATCH PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,170 hrs · 12,121 cycles

DURING SCHEDULED MV1 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 18,948 hrs · 10,889 cycles

PHOTOLUMINESCENT FLOOR TRACK COVER MISSING. REMOVED AND REPLACED PHOTLUMINESCENT FLOOR TRACK SECTION PER MM.

Part: FASTENER — MISSING (L1 DOOR SLIDE) · airframe 18,420 hrs · 10,593 cycles

DURING SCHEDULED 5Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE COVER MISSING FASTENERS. INSTALLED FASTENERS PER SRM.

Part: FLOORBEAM — CORRODED (CABIN FLOOR) · airframe 18,420 hrs · 10,593 cycles

DURING SCHEDULED 5Y CHECK, FOUND LONGITUDINAL FLOORBEAMS CORRODED AT BS 727D, LBL 3 & BS 772 TO BS 774, LBL 17. REPAIRED FLOORBEAMS PER SWA EA.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 18,070 hrs · 10,400 cycles

R2 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 15,269 hrs · 8,789 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 14,530 hrs · 8,380 cycles

R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,530 hrs · 8,380 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD RIGHT EEPLS INOP. RELAMPED EEPLS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,530 hrs · 8,380 cycles

DURING SCHEDULED C1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT AT ROW 3 ABC, INOP. RELAMPED PER BULL NOSE LIGHT PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,598 hrs · 7,338 cycles

DURING SCHEDULED MS, FOUND EMERGENCY EXIT LIGHT AT ROW 13 DEF INOP. RELAMPED PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 12,546 hrs · 7,303 cycles

DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: CDU — FAULTY (COCKPIT) · airframe 12,222 hrs · 7,101 cycles

DURING CRUISE AT FL 370, SMOKE WAS FOUND COMING FROM RIGHT FWD CONTROL PEDESTAL. DIVERTED TO MCI. REMOVED AND REPLACED CDU PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 11,627 hrs · 6,776 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER WHEN OPENING THE DOOR. REINSTALLED SLIDE PER MM.

Part: CLIP — LOOSE (GIRT BAR) · airframe 11,321 hrs · 6,614 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE GIRT BAR CLIP ATTACH RIVET SHEARED. REPAIRED GIRT BAR CLIP PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,117 hrs · 5,942 cycles

DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW NR 21 DEF. RELAMPED EXIT LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 8,942 hrs · 5,282 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BALLAST — FAULTY (CABIN) · airframe 8,942 hrs · 5,282 cycles

DURING SCHEDULED C4 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM.

Part: SLIDE — LOOSE (AFT SVC DOOR) · airframe 8,027 hrs · 4,787 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,741 hrs · 4,623 cycles

DURING SCHEDULED BC3 CHECK, FOUND OVERHEAD BIN BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW NR 9 ABC. RELAMPED EXIT LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 5,088 hrs · 3,021 cycles

DURING SCHEDULED RON, FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF THE CONTAINER. REINSTALLED SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 4,287 hrs · 2,543 cycles

DURING SCHEDULED C4 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED IN FWD CABIN. R&R COVERS PER MM.

Part: SWITCH — FAULTY (MLG W/W) · airframe 1,798 hrs · 1,097 cycles

DIVERSION, LANDING GEAR AURAL WARNING HORN SOUNDED INTERMITTENTLY DURING FLIGHT. ALL SYSTEMS FUNCTIONING NORMAL. REMOVED AND REPLACED FLAP - LANDING GEAR WARNING SWITCH PER MM. RESET PSEU LATCHES AND RAN BITE CHECK WITH NO FAULTS.

Part: BLADE — DAMAGED (NR 1 ENGINE) · airframe 280 hrs · 170 cycles

AIR TURNBACK, DURING ROTATION RECEIVED NUMEROUS BIRD STRIKES TO AIRCRAFT. ON RETURN TO ALB, NR 1 ENG VIBRATION GAUGE READ 3.0, APPROACHED 4.0 AT FL 240,THRUST LEVER REDUCED TO KEEP VIBRATION LEVEL TO BELOW 4.0. SMELL IN CABIN. PERFORMED BIRD STRIKE INSP PER MM NR 1 AND 2 ENG SHOWED EVIDENCE OF CORE INGESTION. REMOVED AND REPLACED NR 1 ENG FAN BLADE SET PER MM. AMENDED SDR 2028 NR 2 ENG BORESCOPED NO DAMAGE NOTED, NR 1 ENG ON 10 CYCLE FLYBACK BORESCOPE INSPECTION.