N817SY

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 66,124 hrs · 25,355 cycles

AFTER TAKEOFF, DURING AFTER TAKEOFF CHECKLIST, GEAR HANDLE MOVED FROM UP TO OFF, NOSE GEAR EXTENDED AND BOTH THE GREEN AND RED NOSE GEAR LIGHTS ILLUMINATED. RAN QRH, GEAR HANDLE MOVED TO UP POSITION DURING QRH PROCEDURE, NOSE GEAR RETRACTED AND ALL LIGHTS EXTINGUISHED. AIR RETURN FOR GEAR DISAGREE LIGHT. CREW DECLARED AN EMERGENCY. ON LANDING, ALL GEAR EXTENDED AND LOCKED NORMALLY. PERF. PSEU BITE IAW AMM 32-09-00-860-008, NOT FAULTS, PERF. FIM TSK. 32-30 TASK 811 NO FAULTS, PERF. FIM TASK32-61 TASK 804, NO FAULTS., PERF. AMM TASK 32-61-41-710-801 NO FAULTS NOTED. SUSPECT NLG WAS NOT UP AND LOCKED PRIOR TO SELECTING HANDLE TO OFF PO. PER FIM TASK 32-30 TASK 809 PG. 1 B. (1).

Part: FLOORBEAM — CORRODED (CABIN) · airframe 65,543 hrs · 25,167 cycles

CORROSION ON FLOOR BEAM UPPER CAP SURFACE AT STA 328 RBL 54 WL 208. REMOVED DAMAGED SECTION OF FLOOR BEAM UPPER FLANGE FROM BS 328 RBL 1.10" TO RBL 65 WL 208, PER SRM 53-10-51-28-7 PARA 4, FABRICATED-1 T-CHORD PER SRM 53-10-51-2R-7 AND INSTALLED, PER ER 20-03582 SRM 51-40-02-0G-0 AND SRM 53-10-51-2R-7 REP 7.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 65,543 hrs · 25,167 cycles

FLOOR PANEL 147A5810-145 IS DAMAGED AT THE AFT OUTBOARD INSERT AREA. REPAIRED DAMAGE AT THE AFT OUTBOARD IN SEAT AREA ON FLOOR PANEL 147A5810-145, IAW SRM 53-00-50-2R-Z.

Part: FRAME — DAMAGED (AFT CARGO) · airframe 65,543 hrs · 25,167 cycles

FRAME DAMAGED BS 500I LBL 25 WL 158 UPPER FLANGE. CUT OUT DAMAGED AREA OF FRAME BS 500I LBL 25 WL 158, IAW SRM 51-10-02-0G-0. REPAIRED AREA IAW SRM 53-30-07-2R-1 SRM 51-40-02-0G-0.

Part: BAFFLE — CORRODED (AFT CABIN) · airframe 65,543 hrs · 25,167 cycles

CORROSION ON BAFFLE AT STA 500G-500H, LBL 25, WL 156. REMOVED DAMAGED BAFFLE AT STA 500H-500G LBL 25 WL 156, IAW SRM 51-40-02. INSTALLED NEW BAFFLE P/N 143A7510-21 PO NR 807437, IAW SRM 51-40-02, DWG 143A7505 REV B.

Part: CHANNEL — CORRODED (FWD CARGO) · airframe 65,543 hrs · 25,167 cycles

FWD CARGO COMP LT ZEE CHANNEL CORROSION AT MULTIPLE FASTENER HOLES STA 500+15 TO STA 500I, LBL 24, WL 156. REMOVED DAMAGED SECTION OF LT ZEE CHANNEL FROM STA 500+15-500I LBL 24 WL 156 AND INSTALLED REPLACEMENT ZEE CHANNEL, IAW SRM 53-00-53-2R-5 DWG 143A7501 REV B SRM 51-40-02-0G-0. REPAIR ACCOMPLISHED FROM ORIGINAL REPAIR SPLICE AT STA 480+6 LBL 24.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 65,543 hrs · 25,167 cycles

FLOOR PANEL 147A5810-146 IS DAMAGED AT THE AFT OUTBOARD INSERT AREA. REPAIRED DAMAGE ON FLOOR PANEL 147A5810-146 AT AFT OUTBOARD INSERT AREA, PER SRM 53-00-50-2R-6.

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 65,543 hrs · 25,167 cycles

FWD CARGO COMPARTMENT AFT LT LOWER BULKHEAD PANEL SUPPORT CORROSION ON BOTTOM SURFACE STA 500I, LBL26, WL156. REMOVED DAMAGED BULKHEAD SUPPORT AT FWD CARGO AFT LT STA 500I LBL 26 WL 156 AND INSTALLED NEW BULKHEAD PANEL SUPPORT, IAW SRM 51-40-02, DWG 143A9481 P/N 143A9485Y23, PO NR 807125.

Part: SKATE ANGLE — WORN (VERTICAL STAB) · airframe 65,543 hrs · 25,167 cycles

RT AFT SKATE ANGLE IS WORN. ACCOMPLISHED BLEND REPAIR TO VERTICAL FIN CLOSURE ANGLE RT, BS 1032 TO BS 1104, PER ATS ER 20-03566 REV IR AND SCA EA 53-0068 REV 0.

Part: SUPPORT — CORRODED (FWD CARGO) · airframe 65,543 hrs · 25,167 cycles

FWD CARGO COMPARTMENT AFT LOWER BULKHEAD PANEL SUPPORT AREAS OR CORROSION STA 500I BETWEEN LBL 24 TO RBL 24, WL 156. REMOVED DAMAGED BULKHEAD PANEL SUPPORT AT FWD CARGO AFT RT 26-LH 26 STA 500I WL 156 AND INSTALLED NEW BULKHEAD PANEL SUPPORT, IAW SRM 51-40-02, DWG 143A9481 P/N 143A9485435, P/O 807144.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 65,543 hrs · 25,167 cycles

FLOOR PANEL 147A5810-71 IS DAMAGED AT THE AFT INSERT AREA AND FWD INSERT AREA. REPAIRED DAMAGE AT THE AFT + FWD INSERT AREA ON FLOOR PANEL 147A5810-71, IAW SRM 53-00-50-2R-1.

Part: FITTING — CORRODED (GALLEY) · airframe 65,543 hrs · 25,167 cycles

CORROSION ON G1 GALLEY INBOARD AFT LOWER FITTING. RECEIVED NEW INBOARD AFT LOWER FITTING ON G-1 GALLEY. INSTALLATION WILL BE ACCOMPLISHED ON CUSTOMER CARD NR 00012 CORROSION ON FITTING OUT OF LIMITS, DUE TO NO PUBLISHED LIMITS.

Part: SHEAR WEB — CORRODED (AFT CABIN) · airframe 65,543 hrs · 25,167 cycles

CORROSION ON AFT CABIN FLOOR SHEAR WEB STA 1016+3 WL 208 RBL 8.5. REPAIRED AFT CABIN FLOOR SHEAR WEB AT STA 1016+3 WL 208, IAW ATS ET 20-03552 REV IR AND SCA EA 53-0073 REV 00 RBL 8.5.

Part: SHEAR WEB — CORRODED (CABIN) · airframe 65,543 hrs · 25,167 cycles

CORROSION ON AFT CABIN FLOOR SHEAR WEB STA 1016 LBL 8 WL 208. REPAIRED AFT CABIN FLOOR SHEAR WEB AT STA 1016 LBL 8 WL 208, IAW ATS ER 20-03548 REV IR AND SCA EA 53-0072.

Part: CARGO TRACK — CORRODED (FWD CARGO) · airframe 65,543 hrs · 25,167 cycles

FWD CARGO COMPARTMENT TRACK TIE DOWN HAS SEVERAL AREAS OF CORROSION AROUND FASTENER HOLES, STA 500H+15-19, LBL 17, WL 156. REMOVED DAMAGED SECTION OF FWD CARGO COMPARTMENT TRACK TIE DOWN STA 500G+10-500I LBL 17 WL 156 AND REPLACED SECTION, IAW SRM 53-00-53-2R-3, SRM 51-40-02, DWG 143A7501.

Part: SHEAR WEB — CORRODED (CABIN) · airframe 65,543 hrs · 25,167 cycles

CORROSION ON AFT CABIN FLOOR SHEAR WEB, STA 1016+3.5 RBL 11 WL 208. REPAIRED AFT CABIN FLOOR SHEAR WEB AT STA 1016+3.5" RBL 11 WL 208, IAW ATS ER 20-03552 REV IR AND SCA EA 53-0073 REV 00.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 65,543 hrs · 25,167 cycles

STA 947.5, RBL 50 WL 208 FLOOR BEAM UPPER CAP HAS CORROSION. CORROSION ON STA 947.5 FLOOR BEAM UPPER CHORD RBL 50, WL 208 FOUND TO BE OUT OF LIMITS, IAW SRM 53-70-51-1A-1 FIG 104 DETAIL C. REMOVED DAMAGE AND REPAIRED, IAW SRM 53-70-51-2R-5.

Part: SHEAR WEB — CORRODED (CABIN) · airframe 65,543 hrs · 25,167 cycles

CORROSION ON AFT CABIN FLOOR SHEAR WEB STA 1016 RBL 24 WL 208. CORROSION ON AFT CABIN FLOOR SHEAR WEB STA 1016, RBL 24, WL 208. FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS, IAW SRM 53-70-51-1A-1. REMOVED AND REPLACED DAMAGED SHEAR WEB, IAW SRM 51-40-02-0G-0 AND BOEING DWG 147A5700.

Part: CHANNEL — CORRODED (L2 DOOR SILL) · airframe 65,543 hrs · 25,167 cycles

CORROSION ON L2 DOOR MOP SILL STA 947 TO STA 986 WL 208. CORROSION ON AFT ENTRY DOOR LOWER MAIN SILL INNER CHORD STA 947-986 WL 208, FOUND TO BE OUT OF LIMITS, IAW SRM 53-70-51-1A-1 FIG 103 DETAIL D. REMOVED AND REPLACED DAMAGED INNER CHORD, IAW SRM 51-40-02-0G-0 AND BOEING DWG 147A8501.

Part: SUPPORT ANGLE — CORRODED (THRESHOLD) · airframe 65,543 hrs · 25,167 cycles

CORROSION ON L1 DOOR LOWER SILL THRESHOLD SUPPORT ANGLE BS 316-344 LBL 68 WL 208. CORROSION DAMAGE ON L1 DOOR LOWER SILL THRESHOLD SUPPORT ANGLE BS 316-344 LBL 68 WL 208 FOUND TO BE OUT OF LIMITS, PER SRM 53-10-15-1A-1 STEP 4B FOG 108 DETAIL D. REMOVED AND REPLACED SUPPORT ANGLE, PER SRM 51-40-02 AND BOEING DRAWING 141A8110 REV A, ER 20-03573 REV IR AND SCA EA 53-0067 REV 00.

Part: SHEAR WEB — CORRODED (CABIN) · airframe 65,543 hrs · 25,167 cycles

CORROSION ON SHEAR WEB AT STA 986, LBL 32-46, WL 208. DAMAGE TO SHEAR WEB AT STA 986 LBL 32-46 WL 208 FOUND TO BE OUT OF LIMITS, DUE TO NO LIMITS FOUND IN SRM. REMOVED AND REPLACED WITH NEW PO NR 808105, IAW SRM 51-40-02-0G-0 AND DWG NR 147A5700.

Part: CHANNEL — CORRODED (R2 DOOR) · airframe 65,543 hrs · 25,167 cycles

CORROSION ON R2 DOOR MOP SILL STA 947 TO STA 986 WL 208. CORROSION ON AFT SERVICE DOOR LOWER MAIN SILL INNER CHORD STA 947-986 WL 208. FOUND TO BE OUT OF LIMITS, IAW SRM 53-70-51-1A-1 FIG 103 DETAIL D. REMOVED AND REPLACED DAMAGED INNER CHORD, IAW SRM 51-40-02-0G-0 AND BOEING DWG 147A8501.

Part: SHEAR WEB — CORRODED (CABIN) · airframe 65,543 hrs · 25,167 cycles

CORROSION ON SHEAR WEB AT STA 986, RBL 43, WL 208. REMOVED DAMAGED SHEAR WEB AT STA 986 RBL 43 WL 208 AN INSTALLED NEW SHEAR WEB P/N 147A5712-11 PO NR 808105, IAW SRM 51-40-02, DWG 147A5300.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 65,543 hrs · 25,167 cycles

CORROSION ON AFT CABIN FLOOR SUPPORT STA 947 TO STA 967 RBL 48 WL 208. REMOVED DAMAGED FLOOR SUPPORT (INTERCOSTAL) FROM AFT CABIN STA 947 TO 967 RBL 48 RBL 48 WL 208, PER SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW INTERCOSTAL ITEM NO 147A5660U22 PO NO 807575 AND INSTALLED, PER SRM 51-40-02-0G-0 AND DWG NR 147A5650 REV A.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 65,543 hrs · 25,167 cycles

CORROSION ON AFT CABIN FLOOR SUPPORT STA 947 TO STA 967 LBL 48 WL 208. REMOVED DAMAGED FLOOR SUPPORT (INTERCOSTAL) FROM AFT CABIN BS 947 TO BS 967 LBL 48 WL 208, PER SRM 51-40-02-0G-0. LOCATED, DRILLED NEW INTERCOSTAL ITEM NO 147A5660U22 PO NR 807575 AND INSTALLED, PER SRM 51-40-02-0G-0 AND DWG NR 147A5650.

Part: ATTACH ANGLE — CORRODED (SCUFF PLATE) · airframe 65,543 hrs · 25,167 cycles

CORROSION ON R1 DOOR SCUFF PLATE ATTACHED ANGLE AT STA 300 TO STA 328 WL 208. REMOVED DAMAGED ANGLE ON R1 DOOR SCUFF PLATE. ANGLE ATTACHED TO INNER CHORD, PER SRM 51-40-02-0G-0 AND INSTALLED A NEW ANGLE PER SRM 51-40-02-0G-0 AND DWG NR 141A8310.

Part: STUB FRAME — CRACKED · airframe 65,543 hrs · 25,167 cycles

STUB BEAM BS 296.4 RT CRACKED/BROKEN INBOARD FLANGE AT WL 208 RBL 62. REMOVED DAMAGE AREA AT STUB FRAME BS 296.4 INBOARD FLANGE AT WL 208 RBL 62, PER SRM 53-10-15-2R-7 PARA 4B, C MADE REPAIR PART ITEM (I) PER SRM 53-10-05-2R-7 ALODINE AND PRIMED, PER SOPM 20-44-04, 20-43-03 AND INSTALLED PER SRM 53-10-15-2R-7 FIG 201-203.

Part: WEB — CORRODED (AFT CARGO) · airframe 65,543 hrs · 25,167 cycles

AFT CARGO COMPARTMENT AREAS OF CORROSION ON LOWER MAIN SILL WEB STA 787+7 TO 848, RBL 24, WL 160. REMOVED DAMAGED AFT CARGO LOWER MAIN THRESHOLD SILL WEB + REPLACED WITH NEW P/N 146A8123U25, IAW SRM 51-40-02-0G-0 + BOEING DWG 146A8340.

Part: WEB — CORRODED (THRESHOLD) · airframe 65,543 hrs · 25,167 cycles

CORROSION ON AFT ENTRY DOOR SUB THRESHOLD WEB ON UPPER AND LOWER SURFACES IN MULTIPLE AREAS STA 954-988, LBL 50-53, WL 208. CORROSION FOUND ON AFT ENTRY DOOR SUB THRESHOLD WEB FOUND TO BE OUT OF LIMITS, DUE TO DAMAGE BEING WITHIN 20X OF FASTENER HOLE, IAW SRM 53-70-15-1A-1 FIGURE 103 DEATIL D. REMOVED AND REPLACED AFT ENTRY DOOR SUB THRESHOLD WEB STA 947-992, IAW SRM 51-40-02-0G-0 AND DWG 147A8501 SHEET 78 REV B.

Part: DOOR FRAME — CORRODED (SERVICE DOORWAY) · airframe 65,543 hrs · 25,167 cycles

FWD SERVICE DOOR LOWER SILL INNER CHORD HAS CORROSION FROM STA 297-332, RBL 64, WL 208. INSTALLED FWD SERVICE DOOR LOWER SILL INNER CHORD FROM BS 360 TO BS 259.5 RBL 64 WL 208, PER SRM 51-40-02-0G-0 PARA 4B 7D DWG NR 141A8310, 143A5900, AND ATTACHED ANGLE.

Part: DOOR FRAME — CORRODED (PAX DOORWAY) · airframe 65,543 hrs · 25,167 cycles

FWD ENTRY DOOR LOWER SILL INNER CHORD HAS CORROSION FROM STA 303.9-348.2, LBL 64, WL 208. CORROSION ON LOWER INNER CHORD BS 348-304 LBL 64 WL 208 FOUND TO BE OUT OF LIMITS, IAW SRM 53-10-15-1A-1 FIG 103 DETAIL D. REMOVED INNER CHORD, IAW SRM 51-40-02-0G-0. INSTALLED NEW INNER CHORD P/O 807579/1, IAW SRM 51-40-02-0G-0 AND BOING DWG 141A8110 REV A.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 65,543 hrs · 25,167 cycles

CORROSION ON PANEL BREAK FITTING BETWEEN STA 312 AND STA 328 RBL 10 WL 208. FOUND DAMAGE ON PANEL BREAK FITTING BETWEEN STA 312-STA 328 RBL 10 WL 208 TO BE OUT OF ALLOWABLE LIMITS, PER SRM 53-10-51-1A-1 FIG 105 DETAIL C. LOCATED AND DRILLED REPLACEMENT PANEL BREAK FITTING ITEM 141A5410U14 PO 806928, PER SRM 51-40-05-0G-0 AND BOEING DWG 141A5400 INSTALLED.

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 65,543 hrs · 25,167 cycles

AFT CARGO COMPARTMENT CORROSION AFT LOWER BULKHEAD PANEL SUPPORT STA 947.5, RBL 9, WL 179. REMOVED AND REPLACED AFT CARGO COMP AFT LOWER BULKHEAD PANEL SUPPORT STA 947.5 RBL 9 WL 179, IAW SRM 51-40-02-0G-0 AND DWG NR 149A8117. EVALUATED CORROSION FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE FOR THIS PART.

Part: SKIN — DENTED (LT WING SPOILER) · airframe 65,543 hrs · 25,167 cycles

LEFT WING NR 5 SPOILER UPPER SURFACE HAS A DENT 33" FROM OUTBOARD AND 15.5" FROM TRAILING EDGE. REPAIRED DENT ON NR 5 SPOILER UPPER SURFACE 33" FORM OUTBOARD EDGE AND 15.5" FORM TRAILING EDGE, PER SRM 57-70-01-2R-4 AND SRM 51-70-10-2R-4.

Part: SKIN — DENTED (LT WING SPOILER) · airframe 65,543 hrs · 25,167 cycles

LEFT WING NR 5 SPOILER UPPER SURFACE HAS A DENT 11" FROM OUTBOARD AND 13" FROM TRAILING EDGE. REPAIRED DENT ON UPPER SURFACE OF LT WING NR 5 SPOILER 11" FROM OUTBOARD EDGE AND 13" FROM TRAILING EDGE, PER SRM 57-70-01-2R-4 AND SRM 51-70-10-2R-2.

Part: FRAME — CORRODED (AFT CARGO) · airframe 65,543 hrs · 25,167 cycles

CORROSION FRAME BS 500D LBL 26 WL 156 INBOARD FLANGE. UPON FURTHER INVESTIGATION FOUND CORRODED AREA ON STA 500D LBL 26 INBOARD FLANGE TO ALSO BE DENIED. DAMAGE FOUND TO BE OUT OF LIMITS, IAW SRM 53-00-07-1A-1 STEP 4A. FORMED -1 REPAIR ANGLE FROM 7075-0 .063 LOT NR 5087735, HEAT TREATED BY OUTSIDE SERVICES PO 807410-SCA. INSTALLED REPAIR IAW SRM 53-30-07-2R-1.

Part: SUPPORT ANGLE — CORRODED (FWD CARGO BAY) · airframe 65,543 hrs · 25,167 cycles

FWD CARGO COMP LT FRAME LINING SUPPORT ANGLE HAS AREAS OF CORROSION, STA 500D, LBL 27-38, WL 156-164. CORROSION ON LT STA 500D SIDEWALL SUPPORT ANGLE FOUND TO BE OUT OF LIMITS, DUE TO NO ALLOWABLE LIMITS IN THE SRM. REMOVED AND REPLACED ANGLE PO 808042, IAW SRM 51-40-02-0G-0 BOEING DWG 143A1221 REV B.

Part: NUT PLATE — CORRODED (AFT CARGO) · airframe 65,543 hrs · 25,167 cycles

AFT CARGO COMPARTMENT CORROSION ON NUT PLATE STRIP ON BOTTOM OF FLOOR SILL STRAP INBOARD OF FWD SHIELD STA 787-787+6, RBL 20, WL 156. CORROSION ON STA 787-787+6 RBL 20 NUTPLATE STRIP FOUND TO BE OUT OF LIMITS, DUE TO NO ALLOWABLE DAMAGE IN THE SRM. REMOVED AND REPLACED P/O 807470, IAW SRM 51-40-02-0G-0 BOEING DWG 146A8340 REV C.

Part: ATTACH ANGLE — CORRODED (SCUFF PLATE) · airframe 65,543 hrs · 25,167 cycles

CORROSION ON L1 DOOR SCUFF PLATE ATTACHED ANGLE AT STA 312 TO STA 344 WL 208. CORROSION ON L1 DOOR SCUFF PLATE ATTACH ANGLE AT STA 312 TO 344 WL 208 FOUND TO BE OUT OF LIMITS DUE TO DAMAGE AT FASTENER HOLES, IAW SRM 53-10-15-1A-1 FIG 103 DETAIL D. REMOVED ATTACH ANGLE, IAW SRM 51-40-02-0G-0. INSTALLED NEW ATTACH ANGLE P/O 806888/2, IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A8110 REV A.

Part: BAFFLE — CORRODED (AFT CARGO) · airframe 65,543 hrs · 25,167 cycles

CORROSION AFT CARGO BAFFLE BS 747-767 RBL 25 WL 160 BOTTOM SIDE. REMOVED AND REPLACED BAFELE IN AFT CARGO BS 747-767 RBL 25 WL 160, IAW SRM 51-40-05 SRM 51-40-02 AND DWG NR 146A7502.

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 65,543 hrs · 25,167 cycles

AFT CARGO COMP CORROSION FWD SHIELD STA 767-787+6, RBL 22, WL 157. CORROSION ON AFT CARGO FWD SHIELD STA 767-787 FOUND TO BE OUT OF LIMITS, DUE TO NO ALLOWABLE DAMAGE IN THE SRM. REMOVED AND REPLACED PO 807782, IAW SRM 51-40-02-0G-0, BOEING DWG 146A0081 REV A.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 65,543 hrs · 25,167 cycles

LEFT HORIZONTAL STABILIZER TIP HAVE 4 EA FASTENER HOLES ELONGATED. REPAIRED 4 EA ELONGATED FASTENER HOLES ON LEFT HORIZONTAL STABILIZER TIP, IAW SRM 51-70-05-2R-9.

Part: SHIELD — CORRODED (AFT CARGO) · airframe 65,543 hrs · 25,167 cycles

AFT CARGO COMP CORROSION ON AFT SHIELD STA 847+7, RBL 23, WL 164. REMOVED AND REPLACED SHIELD WITH NEW, IAW SRM 51-40-02-0G-0 AND DWG 146A0081. SHIELD WAS REPLACED DUE TO NO PUBLISHED LIMITS IN SRM.

Part: COVER PLATE — CORRODED (TE FLAP) · airframe 65,543 hrs · 25,167 cycles

MAIN INBOARD MAIN FLAP COVER PLATE AND STRAP HAVE CORROSION AROUND FASTENER HOLES. REMOVED AND REPLACED RT MAIN FLAP INBOARD COVER PLATE, IAW SRM 51-40-08-0G-0 PAR 5 AND DWG 113A2001 REV H.

Part: SUPPORT — CORRODED (BULKHEAD) · airframe 65,543 hrs · 25,167 cycles

FWD CARGO COMP AFT LOWER BULKHEAD PANEL SUPPORT CORROSION STA 500I, RBL 25, WL 156. REMOVED AND REPLACED NEW BULKHEAD SUPPORT ON RT AT STA 500I RBL 25, IAW SRM 51-40-02-0G-0 + DWG 143A9481.

Part: CHANNEL — CORRODED (FWD CARGO) · airframe 65,543 hrs · 25,167 cycles

FWD CARGO COMP RT ZEE CHANNEL CORROSION AT MULTIPLE FASTENER HOLES STA 500A-STA 500I, RBL 24, WL 156. REMOVED AND REPLACED WITH REPLACEMENT LOT NR 5098219-1, IAW SRM 51-40-02-0G-0 DRG NR 143A7500. FWD CARGO COMPARTMENT STA 500A-500I RBL 24 WL 156.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,543 hrs · 25,167 cycles

CORROSION ON AFT CABIN FLOOR BEAM, STA 986, LBL 44 TO RBL 44, WL 208. CORROSION ON STA 986 FLOOR BEAM LBL 44-RBL 44 WL 208 FOUND TO BE OUT OF LIMITS, DUE TO NO SRM ALLOWABLE LIMITS FOR EXISTING REPAIRS. REMOVED AND REPLACED UPPER CHORD AND FASTENERS, PER 737-800 SRM 51-40-02 AS SHOWN IN 737-800 SRM 53-70-51-2R-4.

Part: SUPPORT ANGLE — CORRODED (FWD CARGO) · airframe 65,543 hrs · 25,167 cycles

FWD CARGO COMP RT FRAME LINING SUPPORT ANGLE HAS CORROSION, STA500D, RBL26, WL160. REMOVED AND REPLACED FWD CARGO COMP RT FRAME LINING SUPPORT ANGLE AT STA 500D, RBL 26, WL 160, IAW SRM 51-40-02-0G-0 AND BOEING DWG NR 143A1225 RIB PO NR 807144.

Part: WEB — CORRODED (AFT CARGO BAY) · airframe 65,543 hrs · 25,167 cycles

CORROSION AFT CARGO BS 847-857 RBL 24 WL 158 INTERCOSTAL/WEB TOP FLANGE AND BOTTOM OF FLANGE. REMOVED AND REPLACED INTERCOSTAL WITH A NEW FABRICATED INTERCOSTAL, IAW SRM 51-40-02-0G AND DWGS 146A8321 AND 146A8322 STA 847-857, RBL 24, WL 158.

Part: BAFFLE — CRACKED (CARGO BAY) · airframe 65,543 hrs · 25,167 cycles

CRACKED BAFFLE BS 500C-500D LBL 25 WL 156. REMOVED AND REPLACED WITH REPLACEMENT BAFFLE P/O 807474 STA 500C-500D LBL 25 WL 156, IAW SRM 51-40-02-0G-0 DRG 143A7505.

Part: BAFFLE — CORRODED (CARGO BAY) · airframe 65,543 hrs · 25,167 cycles

CORROSION ON BAFFLE STA 500H-500I, RBL 25, WL 156. REMOVED AND REPLACED BAFFLE STA 500H-500I RBL 25 WL 156 WITH REPLACEMENT P/O 807437, IAW SRM 51-40-02-0G-0 DRG NR 143A7505.

Part: CARGO TRACK — CORRODED (AFT CARGO BAY) · airframe 65,543 hrs · 25,167 cycles

AFT CARGO COMP CORROSION ON FLOOR RAIL STA 767+5, RBL 8, WL 156. FOUND CORROSION DAMAGE ON AFT CARGO BAY FLOOR RAIL AT BS 767+5, RBL 8 WL 156 TO BE OUT OF LIMITS, IAW SRM 53-00-53-1A-2 STEP 4A (2A) FIG 103 DETAIL D. REPAIRED DAMAGED AREA, IAW SRM 53-00-53-2R-2, MATERIAL USED BAC1510-1355 NR 7050T76511, LOT NR 5093194-1.

Part: BAFFLE — CRACKED (CARGO BAY) · airframe 65,543 hrs · 25,167 cycles

BAFFLE AT STA 500G-500H, RBL 25, WL 156 CRACKED. REMOVED AN REPLACED BADDLE STA 500G-500H RBL 25 WL 156 WITH REPLACEMENT P/O 807437, IAW SRM 51-40-02-0G-0 DRG 143A7505.

Part: BAFFLE — CORRODED (FWD CARGO BAY) · airframe 65,543 hrs · 25,167 cycles

CORROSION FWD CARGO BAFFLE BS 500B-C RBL 25 WL 158. REMOVED AND REPLACED BAFFLE WITH NEW BS 500B-500C RBL 25 WL 158, IAW SRM 51-40-02 BOEING DWG NR 143A7505 PO 807233.

Part: CHANNEL — CORRODED (AFT CARGO) · airframe 65,543 hrs · 25,167 cycles

AFT CARGO COMPARTMENT SEVERAL AREAS OF CORROSION LT ZEE CHANNEL ON BOTTOM WHERE NUTPLATES ATTACH STA 727A+10 TO STA 847, LBL 20, WL 156. REMOVED AND REPLACED AFT CARGO LT ZEE CHANNEL, IAW SRM 51-40-02 AND BDG 146A7500 P/O 786416-1 LOT NR 5093799-1 727A+10 TO 847 LBL 20 WL 156.

Part: CARGO TRACK — CORRODED (AFT CARGO BAY) · airframe 65,543 hrs · 25,167 cycles

AFT CARGO COMP CORROSION ON FLOOR RAIL STA 767+5, RBL 3, WL 156. FOUND CORROSION DAMAGE ON AFT CARGO BAY FLOOR RAIL AT BS 767+5 RBL 3 WL 156 TO BE OUT OF LIMITS, IAW SRM 53-00-53-1A-2 STEP 4A (2)(A), FIG 103 DETAIL D. REPAIRED DAMAGED AREA, IAW SRM 53-00-53-2R-2, MATERIAL USED, BAC 1510-1355 NR 7050T76511 LOT NR 5093194-1.

Part: BAFFLE — CRACKED (CARGO BAY) · airframe 65,543 hrs · 25,167 cycles

BAFFLE AT STA 500C-500D, RBL 25, WL 156 CRACKED. REMOVED AND REPLACED WITH REPLACEMENT BAFFLE P/O 807437 STA 500C-500D RBL 25 WL 156, IAW SRM 51-40-02-0G-0 DRG 143A7505.

Part: ANGLE — CORRODED (BAFFLE) · airframe 65,543 hrs · 25,167 cycles

FWD CARGO COMP FWD BAFFLE CLIP CORROSION AT STA 500H, LBL 25, WL 156. REMOVED AND REPLACED FCB FWD BAFFLE CLIP STA 500H LBL 25 WL 156 WITH REPLACEMENT P/O 807233, IAW SRM 51-40-02-0G-0 DRG 143A7505.

Part: FAIRING — ERODED (NR 8) · airframe 65,543 hrs · 25,167 cycles

NR 8 CANOE FAIRING 644AB HAS WIND EROSION DAMAGE ON FWD SEAL FASTENER HOLES. REPAIRED WIND EROSION AT FWD SEAL FASTENER HOLES ON NR 8 CANOE FAIRING 644AB, PER SRM 51-70-05-2R-10.

Part: FAIRING — ERODED (NR 8 CANOE) · airframe 65,543 hrs · 25,167 cycles

NR 8 CANOE FAIRING 644AB HAS WIND EROSION DAMAGE AT DRAIN HOLE. REPAIRED WIND EROSION AT DRAIN HOLE ON NR 8 CANOE FAIRING 644AB, PER SRM 51-70-05-2R-10.

Part: CHANNEL — CORRODED (AFT CARGO) · airframe 65,543 hrs · 25,167 cycles

AFT CARGO COMPARTMENT CORROSION RT FWD ZEE CHANNEL MULTIPLE AREAS WHERE NUTPLATES ATTACH ON BOTTOM STA 727I+5 TO STA 767, RBL 20, WL 156. AFT CARGO COMPARTMENT CORROSION RT FWD ZEE CHANNEL MULTIPLE AREAS WHERE NUTPLATES ATTACH ON BOTTOM STA 727I+5 TO STA 767, RBL 20, WL 156.

Part: CHANNEL — CORRODED (AFT CARGO BAY) · airframe 65,543 hrs · 25,167 cycles

AFT CARGO COMP CORROSION RT AFT ZEE CHANNEL STA 867, RBL 16, WL 166. REMOVED & REPLACED ZEE CHANNEL AT BS 867 RBL 16 ON AFT CARGO, IAW SRM 51-40-02 + DRAWING NR 146A7502.

Part: THRESHOLD — CORRODED (FWD CARGO DOOR) · airframe 65,543 hrs · 25,167 cycles

CORROSION FWD CARGO BAY SUB THRESHOLD HAS CORROSION AT STA 460+4", RBL 28, WL 156. FWD CARGO BAY SUB THRESHOLD AT BS 460+4 RBL 28 FOUND TO BE OUT OF LIMITS, IAW B737-800 SRM 53-30-15-1A-1 FIG 103 DETAIL D. REMOVED AND REPLACED SILL WEB, IAW B737-800 SRM 51-40-02-0G-0 AND BOEING DRAWING NR 143A8122 REV.

Part: SHIELD — CORRODED (FWD CARGO BAY) · airframe 65,543 hrs · 25,167 cycles

FWD CARGO COMP ENTRANCE AFT SHIELD HAS AREAS OF CORROSION STA 480+12 TO STA 500A, RBL 25, WL156. REMOVED AN REPLACED FCB AFT SHIELD WITH REPLACEMENT P/O 807062, IAW SRM 51-40-02-0G-0 AND DRG 143A0080.

Part: WEB — CORRODED (FUSELAGE) · airframe 65,543 hrs · 25,167 cycles

CORROSION ON WEB LOCATED BETWEEN STA 260 AND STA 270 BL 0 WL 208. REMOVED AND REPLACED WEB LOCATED BETWEEN STA 260-270 BL 0 WL 208 WITH ITEM NR 141A5211U1 PO NR 806895, IAW SRM 51-40-02 AND DWG NR 141A5210.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 65,543 hrs · 25,167 cycles

DURING QC WALK FOUND LEFT HORIZ STAB LEADING EDGE TO HAVE DENT AT LEADING EDGE STA 151.75. MEASURED DENT OF LEFT HORIZ LEADING EDGE AT STA 151.75 A=1.00 Y=.125 A/Y 6.7 DENT FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE AND INSTALLED REPIAR DOUBLER, IAW B737-800 SRM 55-10-01-2R-1 FIG 202 SHT 3.

Part: FAIRING — DAMAGED (NR 7 CANOE) · airframe 65,543 hrs · 25,167 cycles

NR 7 CANOE FAIRING 643AB HAS WIND EROSION DAMAGE AROUND FWD FASTENER HOLES. NR 7 CANOE FAIRING 643AB WIND EROSION DAMAGE AROUND FWD FASTENER HOLES REPAIRED, IAW B737 SRM 57-53-70-2R-3 TABLE 202 AND IAW B737 SRM 51-70-05-2R-8.

Part: MOUNT — ERODED (CANOE FAIRING) · airframe 65,543 hrs · 25,167 cycles

NR 1 FWD CANOE FAIRING 544AB HAS EROSION DAMAGE TO FWD BULB SEAL MOUNT SCREWS HOLES. NR 1 FWD CANOE FAIRING 544AB EROSION DAMAGE TO FWD BULB SEAL MOUNT SCREW HOLES REPAIRED, IAW B737 SRM 57-53-70-2R-3 TABLE 203 AND IAW B737 SRM 51-70-05-2R-10.

Part: SKIN — DAMAGED (WING) · airframe 65,543 hrs · 25,167 cycles

WING PANEL 621WB HAS DAMAGED FASTENER HOLE. REPAIRED DAMAGED FASTENER HOLE ON WING PANEL 621WB, IAW SRM 51-70-04-2R-9 PER SRM 57-41-01-2R-1 PARA 4B TABLE 202.

Part: SKIN — DAMAGED (WING) · airframe 65,543 hrs · 25,167 cycles

WING PANEL 521QB HAS DAMAGED FASTENER HOLE. REPAIRED WING PANEL 521QB, IAW SRM 51-70-04-2R-9, DAMAGED FASTENER HOLE.

Part: FAIRING — ERODED (NR 1 CANOE) · airframe 65,543 hrs · 25,167 cycles

NR 1 FWD CANOE FAIRING 544AB HAS EROSION DAMAGE TO FWD MOUNT HOLES. NR 1 FWD CANOE FAIRING 544AB EROSION DAMAGE TO FWD MOUNT HOLES REPAIRED, IAW B737 SRM 57-53-70-2R-3 AND IAW B737 SRM 51-70-05-2R-10.

Part: PANEL — DAMAGED (WING) · airframe 65,543 hrs · 25,167 cycles

WING PANEL 671DB HAS FASTENER HOLE DAMAGE. REPAIRED FASTENER HOLE DAMAGE ON WING PANEL 671DB, IAW SRM 51-70-04-2R-9 PER SRM 57-51-01-2R-1 PARA 4C TABLE 202.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 65,543 hrs · 25,167 cycles

FLOOR PANEL 221BF HAS DAMAGED INSERTS. UPON FURTHER INVESTIGATION FOUND DAMAGE ON UPPER SURFACE OF FLOOR PANEL 221BF. REPAIRED DAMAGE TO FLOOR PANEL 221BF AND REPLACED DAMAGED INSERTS, PER SRM 53-00-50-2R-2.

Part: PANEL — DAMAGED (WING) · airframe 65,543 hrs · 25,167 cycles

WING PANEL 651BT HAS DAMAGED FASTENER HOLES. REPAIRED WING PANEL 651BT DAMAGED FASTENER HOLES, IAW SRM 51-70-04-2R-9.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 65,543 hrs · 25,167 cycles

FLOOR PANEL 222BF HAS DAMAGED INSERTS. REPAIRED FLOOR PANEL 222BF HAD DAMAGED INSERTS, IAW SRM 53-00-50-2R-0.

Part: SKIN — CRACKED (WING) · airframe 65,543 hrs · 25,167 cycles

WING PANEL 551ET HAS CRACKED FASTENER HOLE. REPAIRED CRACKED FASTENER HOLE ON WING PANEL 551ET, IAW SRM 51-70-05-2R-8.

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY) · airframe 60,748 hrs · 23,486 cycles

AFT COFFEE MAKER SHUT OFF DUE TO POSSIBLE SMOKE. REMOVED AND REPLACED COFFEE MAKER IN AFT GALLEY. OPS CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,887 hrs · 23,144 cycles

DURING OPS CHECK EMER LIGHTS ROW 16 THREW 23 D,E,F, AND OUTSIDE AFT RIGHT SIDE OVER WING DOOR LIGHTS FAIL TEST. BATTERY PACK NEEDS REPLACEMENT. REPLACED BATTERY PACK. OPS CHECK GOOD.

Part: SKIN — CRACKED (NR 3 LE SLAT) · airframe 58,719 hrs · 22,764 cycles

NR 3 SLAT HAD A CRACK ON THE LOWER SKIN. R & R THE NR 3 L/E SLAT. OPS CHECKED AND FIT CHECKED GOOD,

Part: SKIN — CRACKED (NR 8 LE SLAT) · airframe 58,719 hrs · 22,764 cycles

NR 8 SLAT HAD A SMALL CRACK ON THE LOWER SKIN. REMOVED AND REPLACED THE NR 8 SLAT.

Part: SKIN — GOUGED (FUSELAGE) · airframe 57,690 hrs · 22,423 cycles

ON WALK AROUND FOUND 3' GOUGE IN FUSELAGE SKIN BELOW AFT CARGO DOOR CUTOUT. BLENDED DAMAGE. ACCOMPLISHED HFEC NO CRACKS FOUND. AND U.T. THICKNESS .086 REMAINING. FROM ORIGINAL .090. TREATED AND PRIMED. TOP COAT COMPLETED.

Part: DOME NUT — CRACKED (FUEL PANEL) · airframe 57,662 hrs · 22,415 cycles

ON WALK AROUND FOUND RIGHT FUEL TANK PANEL 632DB LEAKING. FOUND DOME NUT TO BE CRACKED ON FUEL PANEL 632DB. R&R RT WING FUEL PANEL 632DB. LEAK CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,637 hrs · 22,028 cycles

ROW 22 ABC AND AFT EMER. LIGHTS FAILED CAPACITY FUNCTIONAL TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,637 hrs · 22,028 cycles

ROW 22 DEF AND AFT EMER. LIGHTS FAILED CAPACITY FUNCTIONAL TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK.

Part: LIGHT — DAMAGED (ROW 10DEF) · airframe 55,867 hrs · 21,724 cycles

AT ROW 10 DEF 3 INCH SECTION OF EMERGENCY LIGHT IS DAMAGED. REPLACED THE LIGHT AND OPS CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,408 hrs · 20,799 cycles

AD DRIVEN, DURING NDT INSPECTION OF SKIN AND FASTENER HOLES AT STA 540 JUST BELOW STR 22L, FOUND CRACK INDICATION IN SKIN AT LOWER AFT FASTENER HOLE COMMON TO 540 UPPER CHORD. CIRCLED HOLE AND MARKED CRACK ENDS IN BLACK. REPAIRED CRACK TO FUSELAGE SKIN AT STATION 540 JUST BELOW STR 22L.

Part: ATTACH FITTING — CRACKED (RAM AIR DOOR) · airframe 53,408 hrs · 20,799 cycles

RT RAM AIR DOOR I/B AND O/B ATTACH FITTINGS CRACKED. REMOVED AND INSTALLED NEW RT RAM AIR DOOR I/B AND O/B ATTACH FITTINGS.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 53,408 hrs · 20,799 cycles

FWD WET AREA FLOOR BOARD 141A5810-135 DELAMINATED FWD OTBD. REPLACED FLOOR PANEL 141A5810-135.

Part: ACCESS PANEL — DELAMINATED (FUSELAGE) · airframe 53,408 hrs · 20,799 cycles

LOWER FUSELAGE FWD OF WHEEL WELL, ACCESS PANEL 193B INTERNAL SURFACE ON FWD LT CORNER IS DELAMINATED. REPAIRED LOWER FUSELAGE ACCESS PANEL 193B INTERNAL SURFACE. RESTORED FINISH.

Part: PLATE — PUNCTURED (CARGO BAY) · airframe 53,408 hrs · 20,799 cycles

FWD PIT LT SIDE PLATE HAS PUNCTURE AT STA 500A+4. REMOVED DAMAGED SECTION AT FWD PIT LEFT HAND SIDEPLATE FROM STA 480+10 TO 500B+10 FABRICATED AND INSTALLED NEW SECTION.

Part: SPACER — MISSING (LT WING) · airframe 53,408 hrs · 20,799 cycles

LT WING T/E AT LOWER ACCESS PANEL 561CB, O/B OF TRACK, NUTPLATE AND SPACER MISSING/DAMAGED. REMOVED PANEL SUPPORT STRUCTURE TO FOM. VERIFIED NEW WIGGLE STRIP SPACER, REMOVED DAMAGED WIGGLE STRIP SPACER & REPLACED W/NEW SPACER.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 53,408 hrs · 20,799 cycles

RT INBD AFT FLAP HAS DELAMINATION AT TRAILING EDGE. REPAIRED DAMAGED IMPACT PLY'S ON RT I/B AFT FLAP LOWER SURFACE.

Part: WIRE — DAMAGED (CABIN) · airframe 53,408 hrs · 20,799 cycles

EMERGENCY LIGHT, LOWER FWD OF RT OVERWING EXIT DOOR IS INOP. REPINNED WIRE W3142-0211-16 FROM PIN TO PIN 11 AND REPLACED FUSE AT M1694.

Part: FLOORBOARD — DAMAGED (FUSELAGE) · airframe 53,408 hrs · 20,799 cycles

FWD WET AREA FLOORBOARD 141A5810-347 FWD OTBD EDGE MISSING. REPAIRED FWD WET AREA FLOORBOARD 141A5810-347.

Part: ATTACH FITTING — CRACKED (RAM AIR DOOR) · airframe 53,408 hrs · 20,799 cycles

LT RAM AIR DOOR, LOWER ATTACH FITTING CRACKED. REMOVED AND REINSTALLED LT REINSTALLED LT RETRACTABLE LANDING LIGHT ASSEMBLE TO FOM. REMOVED AND INSTALLED NEW SHAFT SHAFT LOWER LINK ASSEMBLY SHAFT O/B ASSEMBLY, SHAFT O/B SUPPORT ASSEMBLY AND SHAFT SUPPORT ASSEMBLY AND SHAFT DRIVE FOR LT RAM AIR DEFLATOR DOOR.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 53,408 hrs · 20,799 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140BF HAS EDGE DAMAGE AND HAS NUMEROUS DENTS. FABRICATED AFT CARGO FLOOR PANEL 140BF.

Part: FLAP — DELAMINATED (LT WING) · airframe 53,408 hrs · 20,799 cycles

LEFT OUTBOARD AFT FLAP, LOWER INBOARD TRAILING EDGE HAS DELAMINATED. REPAIRED DELAMINATION TO LT T/E AFT FLAP. RESTORED FINISH.

Part: PLATE — PUNCTURED (CARGO BAY) · airframe 53,408 hrs · 20,799 cycles

FWD PIT LT SIDEPLATE HAS PUNCTURE AT STA 500G. REMOVED FWD PIT LT SIDE 2 ENGINE FROM STA 500E+10" TO 500. IDENTIFIED MATERIAL FOR NEW 2 ANGLE TO BE PART 1496-444. LOCATED AND DRILLED NEW 2 ANGLE. APPLIED ALODINE AND PRIME. INSTALLED NUT PLATES. APPLIED CIC. INSTALLED NEW 2 ANGLE.

Part: PLATE — TORN (CARGO BAY) · airframe 53,408 hrs · 20,799 cycles

AFT PIT RT SIDEPLATE ( Z ANGLE ) TORN AT STA 727J FRAME ATTACHMENT POINT. INSTALLED NEW AFT PIT RT SIDEPLATE ( Z ANGLE ) STA 727J.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 53,408 hrs · 20,799 cycles

INTERCOSTAL BETWEEN STA 312 AND 328 LBL 45 UPPER FLANGE HAS BROKEN FASTENER HOLE. REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 312 AND 328 LBL 456.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 53,242 hrs · 20,737 cycles

AFT LEFT EMERGENCY EXIT LIGHT COVER MISSING. REPLACED THE COVER IAW 33-51-00.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 53,188 hrs · 20,717 cycles

DURING TURN, F/A FOUND EMERGENCY EXIT LENS AT 13ABC NEAR THE FLOOR IS MISSING. REPLACED LENS. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,642 hrs · 20,529 cycles

EMERGENCY EGRESS STOW BIN LIGHT AT SEAT 4 ABC IS INOPERATIVE. REPLACED EEPLS LIGHT BULB IN STOW BIN AT SEAT 4 ABC. OPS CHECK GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,642 hrs · 20,529 cycles

CABIN, FRAME CRACKED AT STA 480 LT, BETWEEN STR 8L AND 9L. REPAIRED FRAME CRACK AT STA 480 LT BETWEEN STR 8L & 9L.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,642 hrs · 20,529 cycles

CABIN, FRAME CRACKED AT STA 440 RT, BETWEEN STR 8R AND 9R. REPAIRED FRAME CRACK AT STA 440 RT BETWEEN STR 8R & 9R.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 52,642 hrs · 20,529 cycles

CABIN FLOOR STRUCTURE, STA 540, LBL 2 PANEL BREAK FLOOR SUPPORT IS CRACKED. R & R PANEL BREAK AT STA 540, BL 0-LBL 24.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,642 hrs · 20,529 cycles

CABIN, FRAME CRACKED AT STA 500C RT, BETWEEN STR 8R AND 9R. REPAIRED CRACKED FRAME AT STA 500C RT BETWEEN STR 8R & 9R.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,642 hrs · 20,529 cycles

EEPLS FLOOR STRIP AT SEAT 10ABC IS INOPERATIVE. REPLACED EEPLS FLOOR STRIP. OPS TEST GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,642 hrs · 20,529 cycles

CABIN, FRAME CRACKED AT STA 400 RT, BETWEEN STR 8R AND 9R. REPAIRED FRAME CRACK AT STA 400 RT BETWEEN STR 8R & 9R.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,642 hrs · 20,529 cycles

CABIN, FRAME CRACKED AT STA 500A RT, BETWEEN STR 8R AND 9R. REPAIRED FRAME CRACKED AT STA 500A RT, BETWEEN STR 8R AND 9R.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,642 hrs · 20,529 cycles

CABIN, FRAME CRACKED AT STA 480 RT, BETWEEN STR 8R AND 9R. REPAIRED CRACKED AT STA 480 RT BETWEEN STR 8R & 9R.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 52,476 hrs · 20,462 cycles

EXIT SIGN COVER IS MISSING AT LT AFT OVERWING EXIT LOWER AFT SIGN, REPAIRED.

Part: SMOKE GOGGLES — CRACKED (COCKPIT) · airframe 52,099 hrs · 20,325 cycles

F/O SMOKE GOGGLES CRACKED. REPLACED SMOKE GOGGLES. OK FOR SERVICE.

Part: STRINGER — CORRODED (BS 986) · airframe 51,376 hrs · 20,086 cycles

FOUND CORROSION ON STRINGER 21L AT BS 986 WHERE GROUND JUNCTION BOX MOUNTS, REPAIRED.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 49,633 hrs · 19,317 cycles

ROW 14 DEF MISSING AFT EXIT EMERGENCY LIGHT COVER. REPLACED ROW 14DEF AFT EMERGENCY EXIT LIGHT COVER.

Part: SKIN — DAMAGED (BS 420) · airframe 49,164 hrs · 19,127 cycles

RIGHT SIDE LOWER FUSELAGE AFT OF FWD CARGO DOOR FS 420 AND R25 EVIDENCE OF LIGHTNING STRIKE. R & R 1 EA RIVET.

Part: SKIN — DAMAGED (BS 1016) · airframe 49,164 hrs · 19,127 cycles

RIGHT FUSELAGE HAS EVIDENCE OF LIGHTNING STRIKE FS 1016 AT STR 27R AFT EDGE OF SKIN. REPAIRED LIGHTNING STRIKE DAMAGE AT AFT EDGE OF BUTT JOINT.

Part: SKIN — DAMAGED (BS 727A) · airframe 49,164 hrs · 19,127 cycles

RIGHT SIDE LOWER FUSELAGE AFT OF RT WING FS 727A AND S24R SKIN EVIDENCE OF LIGHTNING STRIKE. REMOVED LIGHTNING STRIKE DAMAGE WITH RIVET REPAIR.

Part: SKIN — DAMAGED (BS 727C) · airframe 49,164 hrs · 19,127 cycles

RT SIDE LWR FUSELAGE AFT OF RT WING FS 727C AND R24 SKIN EVIDENCE OF LIGHTNING STRIKE. REPAIRED DAMAGE.

Part: SKIN — DAMAGED (BS 235) · airframe 49,164 hrs · 19,127 cycles

RIGHT SIDE LOWER FUSELAGE FWD OF FWD CARGO DOOR FS 235.8 AND BETWEEN R25-R26 EVIDENCE OF LIGHTNING STRIKE. REPAIRED LIGHTNING STRIKE DAMAGE WITH RIVET REPAIR.

Part: SKIN — DAMAGED (BS 268) · airframe 49,164 hrs · 19,127 cycles

RIGHT SIDE LOWER FUSELAGE FORWARD OF FORWARD CARGO DOOR FS 268.7 AND BETWEEN R26-R27 EVIDENCE OF LIGHTNING STRIKE. REMOVED DAMAGED RIVET AND INSTALLED NEW RIVET.

Part: SKIN — DAMAGED (BS 380) · airframe 49,164 hrs · 19,127 cycles

RT SIDE LOWER FUSELAGE AFT OF FORWARD CARGO DOOR FS 380 AND R25 EVIDENCE OF LIGHTNING STRIKE. R & R 1 EA RIVET.

Part: SKIN — DAMAGED (BS 727C) · airframe 49,164 hrs · 19,127 cycles

RIGHT SIDE LOWER FUSELAGE AFT OF RT WING FS 727C AND R24 SKIN EVIDENCE OF LIGHTNING STRIKE. FOUND TO BE OUT OF LIMITS. REPAIRED DAMAGE.

Part: SKIN — DAMAGED (BS 905) · airframe 49,164 hrs · 19,127 cycles

RT AFT LOWER FUSELAGE AT FS 905 AND ABOUT R24 POSITION SKIN HAS EVIDENCE OF LIGHTNING STRIKE. REPARED LIGHTNING STRIKE.

Part: SKIN — DAMAGED (BS 927) · airframe 49,164 hrs · 19,127 cycles

RIGHT AFT LOWER FUSELAGE AT BS 927 SKIN HAS EVIDENCE OF LIGHTNING STRIKE. REPAIRED SKIN.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 49,164 hrs · 19,127 cycles

LEFT HORIZONTAL STABILIZER TIP UPPER SIDE HAS EVIDENCE OF LIGHTNING STRIKE. R & R LT HORIZONTAL STABILIZER TIP WEDGE.

Part: SKIN — DAMAGED (BS 727) · airframe 49,164 hrs · 19,127 cycles

RIGHT SIDE LOWER FUSELAGE AFT OF RT WING FS 727 AND S24R SKIN EVIDENCE OF LIGHTNING STRIKE. REPAIRED LIGHTNING STRIKE.

Part: SKIN — DAMAGED (BS 727D) · airframe 49,164 hrs · 19,127 cycles

RT AFT LOWER FUSELAGE AT FS 727D AND R24 POSITION SKIN HAS EVIDENCE OF LIGHTNING STRIKE. DRILLED SKIN AND INSTALLED RIVET.

Part: SKIN — DAMAGED (BS 500B) · airframe 49,164 hrs · 19,127 cycles

RIGHT SIDE LOWER FUSELAGE AFT OF FWD CARGO DOOR FS 500B AND R25 SKIN EVIDENCE OF LIGHTNING STRIKE. R & R 1 EA RIVET.

Part: SKIN — DAMAGED (BS 727B) · airframe 49,164 hrs · 19,127 cycles

RIGHT SIDE LOWER FUSELAGE AFT OF RT WING FS 727B AND R24 SKIN EVIDENCE OF LIGHTNING STRIKE. LIGHTNING STRIKE DAMAGE AT 727C R24 FOUND TO BE OUT OF LIMITS. REPAIRED.

Part: SKIN — DAMAGED (BS 305) · airframe 49,164 hrs · 19,127 cycles

RIGHT SIDE LOWER FUSELAGE FORWARD OF FORWARD CARGO DOOR FS 305 S25R EVIDENCE OF LIGHTNING STRIKE. REPAIRED LIGHTNING STRIKE.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 49,164 hrs · 19,127 cycles

LEFT HORIZONTAL STABILIZER TIP UPPER AFT SIDE RIVETS 5 EA HAVE EVIDENCE OF LIGHTNING STRIKE. R & R 5 EA FASTENERS.

Part: SKIN — DAMAGED (BS 500G) · airframe 49,164 hrs · 19,127 cycles

RIGHT SIDE LOWER FUSELAGE AFT OF FWD CARGO DOOR STA 500G AND S25R SKIN EVIDENCE OF LIGHTNING STRIKE. R & R 1 EA RIVET.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 49,164 hrs · 19,127 cycles

LEFT HORIZONTAL STABILIZER TIP UPPER SIDE RIVETS 3 EA HAVE EVIDENCE OF LIGHTNING STRIKE. R & R 3 EA FASTENERS.

Part: SKIN — DAMAGED (BS 312) · airframe 49,164 hrs · 19,127 cycles

RIGHT SIDE LOWER FUSELAGE FORWARD OF FORWARD CARGO DOOR FS 312 AND R25 EVIDENCE OF LIGHTNING STRIKE. REPAIRED SKIN.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 49,164 hrs · 19,127 cycles

LEFT HORIZONTAL STABILIZER TIP UPPER SIDE AFT CORNER HAS BURN EVIDENCE OF LIGHTNING STRIKE. R & R UPPER STAB TIP SKIN DOUBLER.

Part: SKIN — DAMAGED (BS 178) · airframe 49,164 hrs · 19,127 cycles

RIGHT SIDE LOWER FUSELAGE AFT OF RADOME FS 178 BETWEEN R23-R24 HAS LIGHTNING STRIKE. R & R 1 EACH RIVET.

Part: SKIN — DAMAGED (BS 235) · airframe 49,164 hrs · 19,127 cycles

RIGHT SIDE LOWER FUSELAGE FWD OF FWD CARGO DOOR FS 235.8 AND BETWEEN R25-R26 HAS EVIDENCE OF LIGHTNING STRIKE. REPAIRED LIGHTNING STRIKE DAMAGE FS 235.8 BETWEEN STR 25 & 26.

Part: SKIN — DAMAGED (BS 727C) · airframe 49,164 hrs · 19,127 cycles

RIGHT SIDE LOWER FUSELAGE AFT OF RT WING FS 727C AND R24 EVIDENCE OF LIGHTNING STRIKE. FOUND TO BE OUT OF LIMITS. REPAIRED DAMAGE.

Part: SKIN — DAMAGED (BS 400) · airframe 49,164 hrs · 19,127 cycles

RIGHT SIDE LOWER FUSELAGE AFT OF FORWARD CARGO DOOR STA 400 AND R25 EVIDENCE OF LIGHTNING STRIKE. R & R 1 EA RIVET.

Part: SKIN — DAMAGED (BS 196-203) · airframe 49,164 hrs · 19,127 cycles

RT SIDE FORWARD LOWER FUSELAGE AFT OF RADOME BETWEEN FS 196.5-203 AND BETWEEN R23-R24 HAS LIGHTNING STRIKE. R & R 1 EACH RIVET.

Part: SKIN — DAMAGED (BS 767) · airframe 49,164 hrs · 19,127 cycles

RIGHT AFT LOWER FUSELAGE AT FS 767 AND ABOUT R24 POSITION SKIN HAS EVIDENCE OF LIGHTNING STRIKE. REPAIRED FUSELAGE.

Part: SKIN — DAMAGED (BS 178) · airframe 49,164 hrs · 19,127 cycles

RIGHT SIDE LOWER FUSELAGE AFT OF RADOME FS 178 BETWEEN R23-R24 SKIN HAS LIGHTNING STRIKE. DAMAGE REPAIRED.

Part: SKIN — DAMAGED (BS 325) · airframe 49,164 hrs · 19,127 cycles

RIGHT SIDE LOWER FUSELAGE FORWARD OF FORWARD CARGO DOOR STA 325 AND R26 EVIDENCE OF LIGHTNING STRIKE. R & R 1 EA RIVET.

Part: SKIN — DAMAGED (BS 727F) · airframe 49,164 hrs · 19,127 cycles

RIGHT FUSELAGE HAS EVIDENCE OF LIGHTNING STRIKE FS 727F +9" 1.5" ABOVE STR 21. REPAIRED.

Part: SKIN — DAMAGED (219-224) · airframe 49,164 hrs · 19,127 cycles

RIGHT SIDE LOWER FUSELAGE AFT OF RADOME HAS LIGHTNING STRIKE BETWEEN FS 224.8-219.5. REPAIRED LIGHTNING STRIKE DAMAGE TO FUSELAGE BETWEEN FS 224.8-219.5 STGR 25.

Part: SKIN — DAMAGED (BS 747) · airframe 49,164 hrs · 19,127 cycles

RIGHT FUSELAGE HAS EVIDENCE OF LIGHTNING STRIKE FS 747-1" 1.5" BELOW STRINGER 23R. DRILLED SKIN AND INSTALLED RIVET.

Part: SKIN — DAMAGED (BS 330) · airframe 49,164 hrs · 19,127 cycles

RIGHT SIDE LOWER FUSELAGE FORWARD OF FORWARD CARGO DOOR FS 330 AND R26 EVIDENCE OF LIGHTNING STRIKE. INSTALLED RIVET AFTER DRILLING OUT DAMAGE.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 48,113 hrs · 18,744 cycles

FWD WET AREA FLOORBEAM, BS 328 HAS CORROSION AT RBL 52. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED BLEND OUT.

Part: THRESHOLD — CORRODED (BS 986) · airframe 48,113 hrs · 18,744 cycles

AFT CABIN RT ON FRAME AT BS 986 JUST INBD OF R2 DOOR THRESHOLD, 2 EA AREAS OF CORROSION A250.004. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. REPAIR ENTIRE UPPER CHORD.

Part: FLOOR SUPPORT — CRACKED (BS 294-312) · airframe 48,113 hrs · 18,744 cycles

FWD WET AREA BS 294.5-312, RBL 15, FLOOR SUPPORT HAS A CRACK. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 48,113 hrs · 18,744 cycles

FWD WET AREA BETWEEN BS 328-344, LBL 11 FLOOR SUPPORT HAS CORROSION. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED FLOOR SUPPORT AND FABRICATED AND INSTALLED NEW FLOOR SUPPORT.

Part: STRINGER CLIP — CRACKED (BS 500I) · airframe 48,113 hrs · 18,744 cycles

STRINGER CLIP 26R CRACKED AT BS 500I. REMOVED DAMAGED STRINGER CLIP AND INSTALLED NEW.

Part: FLOORBEAM — CORRODED (BS 500I) · airframe 48,113 hrs · 18,744 cycles

FWD CARGO BAY AFT FLOOR PANEL LAND AT BS 500I LWR SURFACE CORRODED AT LBL 17.24 AND RBL 13.84. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW FLOOR PANEL RAIL.

Part: BAFFLE — CRACKED (BS 500E-500F) · airframe 48,113 hrs · 18,744 cycles

FOUND BAFFLE BETWEEN 500E-500F CRACKED. R & R BAFFLE.

Part: BAFFLE — CRACKED (BS 500A-500B) · airframe 48,113 hrs · 18,744 cycles

DURING GVI, FOUND BAFFLE BETWEEN BS 500A - 500B CRACKED. R & R BAFFLE.

Part: TEE FITTING — CORRODED (BS 992) · airframe 48,113 hrs · 18,744 cycles

L2 DOOR CUT-OUT FRAME TO INTERCOSTAL T-FITTING CORRODED, STA 992.8 AND STR 15L.

Part: FLOOR SUPPORT — CORRODED (BS 967-947) · airframe 48,113 hrs · 18,744 cycles

AFT CABIN LT BETWEEN BS 967 & 947.5 ON FLOOR SUPPORT JUST INBD OF L-2 DOOR THRESHOLD AREA OF CORROSION AROUND FASTENER HOLE A250-007. CORROSION REMOVED FOUND OUT OF LIMITS. R & R PART.

Part: STIFFENER — CRACKED (VERTICAL STAB) · airframe 48,113 hrs · 18,744 cycles

RIGHT STABILIZER NR 1 SPAR RIB STAB STA 92.7 FWD VERTICAL STIFFNER CRACKED AT LOWER FLANGE, REPAIRED.

Part: THRESHOLD — CORRODED (BS 967) · airframe 48,113 hrs · 18,744 cycles

AFT CABIN RT APPROXIMATELY STA 967 BY R-2 THRESHOLD FRAME HAS AREAS OF CORROSION AROUND FASTENER HOLE A250-002. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. R & R PART.

Part: DOOR FRAME — CORRODED (BS 787-847) · airframe 48,113 hrs · 18,744 cycles

AFT CARGO DOOR CUTOUT LOWER FRAME CORRODED FROM BS 787 - 847. R & R AFT CARGO DOOR CUTOUT LOWER FRAME.

Part: STIFFENER — CRACKED (VERTICAL STAB) · airframe 48,113 hrs · 18,744 cycles

RIGHT STABILIZER NR 1 INSPAR RIB AT STA 92.7 AFT VERTICAL STIFFNER CRACKED AT LOWER FLANGE, REPAIRED.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 48,113 hrs · 18,744 cycles

LEFT HORIZONTAL STABILIZER 1 INNER SPAR RIB AT STA 92.7, NR 3 VERTICAL STIFFENER IS CRACKED ON LWR END. REPAIRED CRACKED RIB.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 48,113 hrs · 18,744 cycles

LEFT HORIZONTAL STABALIZER NR 1 INNER SPAR RIB AT STABILIZER STA 92.7, NR 2 VERTICAL STIFFENER IS CRACKED ON LOWER END. REPAIRED CRACKED RIB.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 48,113 hrs · 18,744 cycles

FWD WET AREA BS 328-344, LBL 46, FLOOR SUPPORT HAS A CRACK. R & R THE FLOOR SUPPORT.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 48,113 hrs · 18,744 cycles

FWD WET AREA BETWEEN BS 344-360, BL 0, FLOOR SUPPORT HAS A CRACK. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 48,113 hrs · 18,744 cycles

FWD WET AREA BS 344-360, LBL 11, FLOOR SUPPORT HAS A CRACK. R & R THE FLOOR SUPPORT.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 48,113 hrs · 18,744 cycles

FWD WET AREA BETWEEN BS 312-328, LBL 46 FLOOR SUPPORT HAS A CRACK. R & R THE FLOOR SUPPORT.

Part: FLOOR PANEL — CORRODED (BS 877) · airframe 48,113 hrs · 18,744 cycles

BS 887 IN THE AFT BILGE, THE FLOOR PANEL SPLICE IS CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED NEW FLOOR PANEL SPLICE.

Part: FLOOR SUPPORT — CRACKED (BS 3612-328) · airframe 48,113 hrs · 18,744 cycles

FWD WET AREA BETWEEN BS 312-328, RBL 32 FLOOR SUPPORT HAS TWO CRACKS. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (BS 277-294) · airframe 48,113 hrs · 18,744 cycles

FWD WET AREA FLOOR SUPPORT BETWEEN STA 277 - 294.5 AT BL 0 IS CRACKED. R & R FLOOR SUPPORT.

Part: FRAME — CORRODED (BS 986) · airframe 48,113 hrs · 18,744 cycles

AFT CABIN LT AT BS 986 ON FRAME JUST INBD OF L2 DOOR THRESHOLD AREA AROUND FASTENER HOLE IS CORRODED A250.008. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED ENTIRE UPPER CHORD.

Part: CHANNEL — CRACKED (BS 500E) · airframe 48,113 hrs · 18,744 cycles

FWD CARGO BAY SIDEPLATE CHANNEL AT RBL 21 CRACKED AT STA 500E+8. CRACK EXTENDS SRM LIMITS. R & R SIDEPLATE CHANNEL.

Part: TRANSITION PANEL — CORRODED (BS 500I) · airframe 48,113 hrs · 18,744 cycles

DURING GVI IN FWD CARGO, FOUND CORROSION ON RT AFT END OF TRANSITION PANEL BS 500I. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. R & R SIDEPLATE CHANNEL.

Part: TRANSITION PANEL — CORRODED (BS 500I) · airframe 48,113 hrs · 18,744 cycles

DURING GVI, FOUND CORROSION IN FWD CARGO ON LT AFT END OF TRANSITION PANEL BS 500I. BLENDED CORROSION FOUND TO BE OUT OF LIMITS. REPLACED SECTION.

Part: CHANNEL — PUNCTURED (CARGO BAY) · airframe 48,113 hrs · 18,744 cycles

FWD CARGO BAY SIDEPLATE CHANNEL AT RBL 21, PUNCTURED AT BS 500A+4. R & R SIDEPLATE CHANNEL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,886 hrs · 18,649 cycles

FLOOR EMERGENCY LIGHTS INOPERATIVE ROW 1AC TO 4ABC. R & R EMERGENCY EXIT BATTERY PACK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,886 hrs · 18,649 cycles

R1 DOOR EMERGENCY LIGHT & OVERHEAD BIN EMERGENCY LIGHTS INOPERATIVE 2 FD & 3FD. R & R EMERGENCY EXIT BATTERY PACKS.

Part: COVER — UNSECURE (EMERGENCY LIGHTS) · airframe 45,828 hrs · 17,400 cycles

PLASTIC MOLDING OVER ELECTRICAL RUNNER BY 3C IS NOT ATTACHED TO THE FLOOR. R & R FLOOR TRACK EMERGENCY LIGHT LENS COVER AT SEATS 1C TO 4C APPROXIMATELY 10' STRIP. SECURITY CHECKS GOOD.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 45,635 hrs · 17,314 cycles

EXIT LIGHT COVER MISSING. INSTALLED NEW COVER.

Part: BATTERY PACK — FAILED (CABIN) · airframe 42,575 hrs · 16,166 cycles

ROW 11 RIGHT SIDE EMERGENCY BATTERY PACK FAILED CAPACITY CHECK.