N395DN

Part: SKIN — GROUND DAMAGE (ZONE 100) · airframe 69,370 hrs · 32,630 cycles

(LOG 0771210) DUE TO A BELT LOADER INCIDENT, IMPACT DAMAGE WAS SUSTAINED AT THE FORWARD CARGO DOOR SURROUND AT BS 440, S-24R. DAMAGE REPAIRED PER ERA 623606-14.

Part: SKIN — GROUND DAMAGE (ZONE 100) · airframe 69,370 hrs · 32,630 cycles

(LOG 0756499) BELT LOADER CONTACTED FORWARD CARGO SKIN AREA 7 TO 9 INCHES UP FROM FLOOR THRESHOLD ON FORWARD SIDE OF CARGO OPENING. REPAIRED DAMAGE PER ERA 623563-14.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0516002) DURING ROUTINE INSPECTION, EXTENSIVE CORROSION WAS FOUND ON THE L/H FRAME INNER CHORD (PN 141A8151-2) AT BS 303.90, BETWEEN STR 22L AND STR 23L, WL 170. MAINTENANCE REPAIRED DAMAGE PER ERA 620052-14.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 68,241 hrs · 32,164 cycles

(LOG 0515861) RH BS 663 VAPOR BARRIER UPPER ATTACH ANGLE CRACKED. REMOVED, FABRICATED -1 REPLACEMENT ANGLE P/N 2024T3#0,063 LOT. 5145130-1, -2 SPLICE ANGLE P/N 2024T3# 0,071 LOT 5157711-1 AND INSTALLED PER B737 SRM 57-10-10-2R PROCEDURE 5 AND SRM 51-40-02-0G.

Part: STUB FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0516184) CORROSION ON L/H STUB FRAME AT STA 303 WL 170. REMOVED AND REPAIRED DAMAGED L/H STUB FRAME @STA 303 WL 170 PER ER/A 620052-14 REV ORIGINAL.

Part: SHIELD — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0509329) CORROSION ON SHIELD FWD OF AFT CARGO BAY DOOR STA 767 TO STA 787 STR 25R. REMOVED & REPLACED SHIELD FWD OF AFT CARGO BAY DOOR @ STA767-STA 787 STR 25R IAW B737 SRM 51-40-02-0G & BOEING DWG# 146A0081 REV:A.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0509393) AFT CARGO BAY SUB THRESHOLD WEB HAS MULTIPLE AREA OF CORROSION. REMOVED AND REPLACED AFT CARGO SUB THRESHOLD WEB IAW B737 SRM 51-40-02-0G DRAWING# 146A8120 REV B.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0509255) CORROSION ON LOWER SILL WEB AT STA 767 TO STA 787 STR 25R WL 160. REMOVED AND REPLACED LOWER SILL WEB @ STA 767-787 STR 25R WL 160 IAW B737 SRM 51-40-02 & BOEING DWG# 146A8123 REV. C.

Part: SHEAR TIE — DAMAGED (ZONE 100) · airframe 68,241 hrs · 32,164 cycles

(LOG 0509226) STA 325.3 STR 24L TO STR 25L DAMAGED SHEAR TIE. REMOVED DAMAGED SHEAR TIE AND INSTALLED NEW SHEAR TIE AT STA 325.3 STR 24L TO STR 25L IAW B737 SRM 51-40-02-0G AND BOEING DWG # 141A0650.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0507655) FLOOR BEAM, UPPER SURFACE, STA 360. RBL 11, WL 208 CORRODED. C/W ER/A 619905-14 REV ORIGINAL.

Part: CARGO TRACK — DAMAGED (ZONE 100) · airframe 68,241 hrs · 32,164 cycles

(LOG 0507544) AFT CARGO BAY FLOOR TRACK DAMAGED ON SPLICE AT STA 747+9 RBL 13 WL 160. REMOVED AND REPLACED TRACK AND SPLICE REPAIR FROM STA 747 TO 767 RBL13 WL 180 PER B737 SRM 53-00-53-2R-3.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 68,241 hrs · 32,164 cycles

(LOG 0507531) DAMAGE ON SEAT TRACK CROWN STA 727F RBL 45. REPAIRED DAMAGED SEAT TRACK AT RBL45 FROM BS 727E+10 TO BS 727F+10 PER B737 SRM 53-00-52-2R-5.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 68,241 hrs · 32,164 cycles

(LOG 0516148) RH BS 663 VAPOR BARRIER UPPER ATTACH ANGLE CRACKED. REMOVED, FABRICATED -1 REPLACEMENT ANGLE P/N 2024T3#0,063 LOT. 5145130-1, -2 SPLICE ANGLE P/N 2024T3# 0,071 LOT 5157711-1 AND INSTALLED PER B737 SRM 57-10-10-2R PROCEDURE 5 AND SRM 5-40-02-0G. REMOVED, FABRICATED -1 REPLACEMENT ANGLE P/N 2024T3# 0,063 LOT. 5145130-1, -2 SPLICE ANGLE P/N 2024T3# 0,071 LOT 5157711-1 AND INSTALLED PER B737 SRM 57-10-10-2R PROCEDURE 5 AND SRM 51-40-02-0G.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0507651) CORROSION ON INTERCOASTAL BETWEEN STA 303 AND STA 312 STR 23L. REMOVED AND REPLACED INTERCOSTAL BTW STA-303 AND STA 312 STR 23L I.A.W. B737 SRM 51-40-02-OG AND DWG 141A8131 REV.E.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0509286) FWD CARGO AFT LWR BULKHEAD SUPPORT LBL 24 AND LBL 22 HAS CORROSION. REMOVED AND REPLACED FWD CARGO AFT LWR BULKHEAD SUPPORT PER B737 SRM 51-40-02-0G AND DWG# 143A-9481 REV A.

Part: SHIELD — GOUGED (ZONE 200) · airframe 68,241 hrs · 32,164 cycles

(LOG 0510807) SEAT TRACK GOUGED AT STA 847+7 LBL 45. ACCOMPLISHED REPAIR AT STA 847.7 LBL 45 SEAT TRACK MAIN CABIN IAW B737 SRM 53-00-52-2R.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

AIRCRAFT 3725, FLOOR BEAM, UPPER SURFACE, STA 312. LBL 12, 40, AND 46, WL 208 CORRODED. CORRECTIVE ACTION: COMPLIED WITH ER/A 619848-14 REV ORIGINAL. (LP 0503906)

Part: CARGO TRACK — DAMAGED (ZONE 100) · airframe 68,241 hrs · 32,164 cycles

AIRCRAFT 3725, FWD CARGO FLOOR RAIL AT LBL 18 AT STA.500E - 500I HAVE DAMAGE AROUND FASTNER HOLES. CORRECTIVE ACTION: EVALUATED DAMAGE ON FWD CARGO FLOOR RAIL AT LBL 18 STA 500E-500I FOUND TO BE OUT OF LIMITS PER B737 SRM 53-00-53-1A-2 PARA 4.A(2) DETAIL. D. REMOVED AND REPLACED RAIL SECTION FROM STA 500D+11 TO STA 500I, LBL 18 AT FWD CARGO PER B737 SRM 53-00-53-2R-3 PARA 4. TABLE 201 FIG 203. (LP 0503970)

Part: CARGO TRACK — DAMAGED (ZONE 100) · airframe 68,241 hrs · 32,164 cycles

AIRCRAFT 3725, FWD CARGO FLOOR RAIL AT RBL 22 AT STA.500E - 500I HAVE DAMAGE AROUND FASTENER HOLES. CORRECTIVE ACTION: EVALUATED DAMAGE ON FWD CARGO FLOOR RAIL AT RBL 13, STA 500E-500I FOUND TO BE OUT OF LIMITS PER B737 SRM 53-00-53-1A-2, PARA. 4.A (2) DETAIL. D. REMOVED AND REPLACED FLOOR RAIL SECTION FROM STA 500F+10" TO STA 500I, RBL 13 AT FWD CARGO PER B737 SRM 53-00-53-2R-3 TABLE 201 FIG 203. (LP 0503946)

Part: CARGO TRACK — DAMAGED (ZONE 100) · airframe 68,241 hrs · 32,164 cycles

AIRCRAFT 3725, FWD CARGO FLOOR RAIL AT LBL 4 AT STA. 500E - 500I HAVE DAMAGE AROUND FASTNER HOLES. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT STA 500D+10-500I LBL IAW B737 SRM 53-00-53-2R-2 ALT. 2 E. (LP 0503953)

Part: CARGO TRACK — DAMAGED (ZONE 100) · airframe 68,241 hrs · 32,164 cycles

AIRCRAFT 3725, FWD CARGO FLOOR RAIL AT RBL 18 AT STA. 500E - 500I HAVE DAMAGE AROUND FASTNER HOLES. CORRECTIVE ACTION: ACCOMPLISHED REPAIR AT FWD CARGO RAIL STA 500E-500I IAW B737 SRM 53-00-53-2R-2 ALT. 2 E. (LP 0503951)

Part: WEB — DAMAGED (ZONE 100) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

AIRCRAFT 3725, DAMAGE ON FWD CARGO SUB THRESHOLD WEB FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-30-15-1A-1 FIG. 103 DETAIL D. CORRECTIVE ACTION: REMOVED AND REPLACED FWD CARGO SUB THRESHOLD WEB WITH NEW REPLACEMENT IAW B737 SRM 51-40-02-0G AND DWG# 143A8330 REV A. (LP 0500544)

Part: CARGO TRACK — DAMAGED (ZONE 100) · airframe 68,241 hrs · 32,164 cycles

AIRCRAFT 3725, FWD CARGO FLOOR RAIL AT RBL 4 AT STA.500E - 500I HAVE DAMAGE AROUND FASTENER HOLES. CORRECTIVE ACTION: PERFORMED REPAIR ON FWD CARGO FLOOR RAIL RBL 4, STA. 500E-500I I.A.W. B737 SRM 53-00-53-2R-2. ALT. 2. (LP 0500537)

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0496869) CORROSION AT LOWER SILL WEB AT STA 827+11 STR 25R WL 160. REMOVED AND REPLACED LOWER SILL WEB STA 787+5-847 WITH NEW ITEM# 146A8123U25 IAW B737 SRM 51-40-02-0G DRAWING 146A8120 REV B.

Part: BAFFLE — CRACKED (ZONE 100) · airframe 68,241 hrs · 32,164 cycles

(LOG 0496782) FWD CARGO BAY BAFFLE RBL 25 BS500G-500H FOUND CRACKED. REMOVED AND REPLACED BAFFLE PART NO. 143A7510-22 ON RBL 25 BS500G-500H IAW SRM BOEING 737-800 SRM 51-40-02 AND DWG NO. 143A7505.

Part: SEAT TRACK — GOUGED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

AIRCRAFT 3725, GOUGE ON SEAT TRACK LOCATED AT STA 847+8", RBL 25 AND WL 208. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT TRACK SECTION FROM STA 827 TO STA 887 RBL 25 WL 208 PER B737 SRM 53-00-52-2R-5, FIG 202 TABLE 201. (LP 0500551)

Part: ANGLE — DENTED (ZONE 100) · airframe 68,241 hrs · 32,164 cycles

AIRCRAFT 3725, FWD CARGO STA 500D + 6 AT LBL 24 HAS DENT IN Z ANGLE. CORRECTIVE ACTION: REPLACED ZEE CHANNEL FROM STA 500-500E I.A.W B737 SRM 53-00-53-2R-5 AND DWG# 143A7500 REV- H. (LP 0503974)

Part: FRAME — DAMAGED (ZONE 100) · airframe 68,241 hrs · 32,164 cycles

AIRCRAFT 3725, AFT CARGO BAY FRAME DAMAGED AT STA 727E STR 23R WL 165. CORRECTIVE ACTION: REPAIRED DAMAGE AFT CARGO BAY FRAME AT STA 727E STR 23R WL 165 IAW SRM 53-60-07-2R PROCEDURE 3 REPAIR 3 ALTERNATIVE 1 FIGURE 204 DETAIL 1. (LP 0500499)

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0493314) CORROSION FOUND IN MULTIPLE AREAS ON FLOOR WEB @STA. 986, RBL 38 TO RBL 45, WL 208. REMOVED, REPLACED AND INSTALLED NEW FLOOR WEB BTW STA 986 TO 1016 RBL 38 TO RBL45 IAW B737 SRM 51-40-02-0G AND DWG 147A5700. REMOVED, REPLACED AND INSTALLED NEW FLOOR WEB BTW STA 986 TO 1016 RBL 38 TO RBL 45 IAW B737-800 SRM 51-40-02-0G AND DWG 147A5700.

Part: BAFFLE — DAMAGED (ZONE 100) · airframe 68,241 hrs · 32,164 cycles

(LOG 0496817) AFT CARGO BAY BAFFLE HAS TOOLING DAMAGE AT STA 727A+19 STR 25R. REMOVED AND REPLACED AFT CARGO BAY BAFFLE AT STA 727+19 STR 25R I.A.W B737 SRM 51-40-02-0G AND DRAWING # 146A7502.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0496847) CORROSION ON AFT CARGO BAY R/H ZEE CHANNEL 727A+11 - STA 727H +12 STR 25 WL 160. REMOVED AND REPLACED AFT CARGO BAY R/H ZEE CHANNEL STA. 727- STA 767 I.A.W B737 SRM 51-40-02-0G AND DWG # 146A7500.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0496750) CORROSION AT INTERCOSTAL BETWEEN STA 947.5 & STA 967 LBL24 WL208. REMOVED, REPLACED AND INSTALLED INTERCOSTAL BETWEEN STA 947.5 TO STA 967 LBL 24 WC-208 IAW B737-800 SRM 51-40-02-0G AND DWG 147A5650.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0496800) CORROSION ON FLOOR SUPPORT @STA. 967+4, LBL 28-48 WL 208. REMOVED, REPLACED AND INSTALLED FLOOR SUPPORT AT STA 967+4", LBL 28-48 IAW B737-800 SRM 51-40-02-0G AND DWG 147A5650.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 68,241 hrs · 32,164 cycles

AIRCRAFT 3725, GOUGES ON SEAT TRACK LOCATED AT STA 520, LBL 45 AND WL 208. CORRECTIVE ACTION: REMOVED DAMAGED SEAT TRACK FROM STA 520-500H+10 LBL 45 WL 208, FABRICATED AND INSTALLED NEW -1 SEAT TRACK SECTION IAW B737 SRM 53-00-52-2R PROC. 4 E. (LP 0500526)

Part: STRAP — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0496946) AFT GALLEY O/B FLOOR STRAP FROM STA 1016-1016+4" RBL18 WL208 HAS CORROSION. REMOVED, REPLACED AND INSTALLED NEW FLOOR STRAP ON AFT GALLEY O/B FROM STA 1006 TO 1016+14" RBL 18 WL-208 IAW B737-800 SRM 51-40-02-0G AND DWG 147A5714 AND DWG 147A5700 REV. A

Part: SILL DRAIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0498267) L2 DOOR (AFT ENTRY DOOR) MOP SILL HAS CORROSION FROM STA 947-986+3" LBL46-LBL55 WL208. REMOVED AND REPLACED L2 DOOR MOP SILL AT STA 887+8 TO 1016 WL 208 IAW B737 SRM 51-40-02-0G DWG# 147A8501.

Part: STRAP — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0496927) AFT GALLEY O/B FLOOR STRAP FROM STA 1016-1016+4" RBL27 WL208 HAS CORROSION. REMOVED, REPLACED AND INSTALLED STRAP ON AFT GALLEY O/B FLOOR FROM STA 1006 TO STA 1016+6" RBL 27 IAW B737-800 SRM 51-40-02-0G AND DWG 147A5714 REV. A. AND DWG 147A5700.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0498333) AFT GALLEY O/B FLOOR STRAP FROM STA 1016-1016+4" LBL18 WL208 HAS CORROSION. REMOVED AND REPLACED AFT GALLEY O/B FLOOR STRAP FROM STA 1016-1016+4" LBL 18 WL 208 IAW B737-800 SRM 51-40-02-0G PAR. 4, 7 AND DWG 147A5700 REV. A.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0493384) CORROSION AT AFT GALLEY FLOOR SUPPORT AT STA 947.5 +3 BETWEEN RBL 25 & RBL 48 WL208. REMOVED AND REMPLACED FLOOR SUPPORT I.A.W. B737-800 SRM 51-40-02-0G AND DWG 147A5650 REV E.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0498328) AFT GALLEY O/B FLOOR STRAP FROM STA 1016-1016+4" LBL27 WL208 HAS CORROSION. REMOVED AND REPLACED AFT GALLEY O/B FLOOR STRAP FROM STA 1016-1016+4" LBL 27 WL 208 IAW B737-800 SRM 51-40-02-0G-0 AND DWG 147A5714 REV. A.

Part: WEB — MECHANIC ERROR (ZONE 200) · airframe 68,241 hrs · 32,164 cycles

AIRCRAFT 3725, FOUND L/H FLOOR WEB WITH MIS-DRILLED HOLES @STA. 986+6, LBL 39, WL 208. CORRECTIVE ACTION: DAMAGE ON L/H FLOOR WEB AT STA 986+6 LBL 39 WL 208 FOUND TO BE OUT OF LIMITS DUE TO NO SRM LIMIT STATEMENT FINDINGS REMOVED AND REPLACED L/H FLOOR WEB AT STA 986-1016 WL 208 IAW B737 SRM 51-40-02-0G DWG# 147A5700. (LP 0503982)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

AIRCRAFT 3725, CORROSION ON SEAT TRACK STA. 727I+10" RBL 45, W.L. 208 FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-00-52-1A-1. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT TRACK SECTION STA. 727I+10 TO STA. 727J+10 IAW B737 SRM 53-00-52-2R-5. (LP 0500534)

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0489858) CORROSION FOUND IN MULTIPLE AREAS ON FLOOR WEB @STA. 986, RBL 38 TO RBL 45, WL 208. REMOVED, REPLACED AND INSTALLED NEW FLOOR WEB BTW STA 986 TO 1016 RBL 38 TO RBL45 IAW B737 SRM 51-40-02-0G AND DWG 147A5700.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0493394) FLOOR SUPPORT CORRODED STA 351 TO STA 354, RBL11, WL 208. REPLACED FLOOR SUPPORT AT RBL 11 BETWEEN STA 340 AND STA 360 IAW B737 SRM 51-40-02-0G AND DWG 141A5720 REV B.

Part: INTERCOSTAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0493320) CORROSION AT INTERCOSTAL BETWEEN STA 947.5 & STA 967 LBL48 WL208. REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 947.5 TO 967 LBL 48, WL 208 PER B737 SRM 51-40-02-0G AND DWG# 147A5650.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0493374) CORROSION AFT GALLEY FLOOR SUPPORT AT STA 907 +9 BETWEEN RBL 25 & RBL 48 WL208. REMOVED AND REPLACED FLOOR SUPPORT AT STA 987+9" BETWEEN RBL 25 TO RBL 48 WL 208 PER B737 SRM 51-40-02-0G AND DWG# 147A5760 REV. A.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0498280) CORROSION AFT GALLEY FLOOR SUPPORT BETWEEN STA 967 & STA 986.5 LBL16 WL208. REMOVED AND REMPLACED FLOOR SUPPORT BWT STA 967 TO STA 986.5 LBL 16 WL 208 IAW B737 SRM 51-40-02-0G AND DWG 140A9870 REV B.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0498351) FLOOR SUPPORT, UPPER SURFACE, STA 326.5, LBL 12, WL 208 CORRODED. REMOVED AND REPLACED FLOOR STRUCTURE AT STA 312 BTW 328 LBL 12 IAW B737-800 SRM 51-40-02-0G AND DWG 141A5400.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0489485) 947.5 FLOOR BEAM UPPER CHORD HAS CORROSION FROM LBL54-RBL54 WL208. REMOVED DAMAGE AND REPAIRED STA. 947.5 FLOOR BEAM UPPER CHORD LBL54-RBL54 WL 208 PER B737 SRM 53-70-51-2R-5.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0493351) CORROSION AT AFT GALLEY FLOOR SUPPORT BETWEEN STA 947.5 & STA 967 RBL16 WL208. REMOVED AND REPLACED FLOOR SUPPORT BETWEEN STA 947.5 AND STA 967 RBL 16 WL 208 PER B737 SRM 51-40-02-0G AND DWG# 147A5650 REV. E

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0493412) AFT GALLEY O/B ANGLE FROM STA 986.5-1016 RBL36 WL208 HAS CORROSION. REMOVED, REPLACED AND INSTALLED AFT GALLEY O/B WALL SUPPORT ANGLE FROM STA 986+6" TO STA 1006+6" RBL 36 IAW B737-800 SRM 51-40-02-0G AND DWG 147A5700.

Part: SILL DRAIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0493357) R2 DOOR MOP (AFT SERVICE DOOR) SILL HAS CORROSION FROM STA 947-986+3" RBL46-RBL55 WL208. REMOVED, REPLACED AND INSTALLED R2 MOOP SILL (AFT SERVICE DOOR) BTW STA 887+8" TO STA 1016 WL-208 IAW B737-800 SRM 51-40-02-0G AND DWG 147A8501.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0493435) CORROSION AT AFT CARGO BAY L/H ZEE CHANNEL 727A+11 - STA 727J STR 25 WL 160. REMOVED & REPLACED L/H ZEE CHANNEL FROM STA 727-STA 847 WITH SPCIC PLATES LOCATED @ STA 727E+6" & STA 727S+7" IAW B737 SRM 53-00-53-2R PROCEDURE 5, BOEING DWG# 146A7500 REV: C, 146A7502 REV:-, 146A7502 REV: B & B737 SRM 51-40-02-0G.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0498357) CORROSION AFT GALLEY FLOOR SUPPORT BETWEEN STA 967 & STA 986.5 RBL16 WL208. REMOVED AND REMPLACED FLOOR SUPPORT BWT STA 967 TO STA 986.5 RBL 16 WL 208 IAW B737 SRM 51-40-02-0G AND DWG 140A9870 REV: B.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

AIRCRAFT 3725, 986.5 FLOOR BEAM UPPER CHORD HAS CORROSION FROM LBL45-RBL45 WL208. CORRECTIVE ACTION: REMOVED DAMAGE AND REPAIRED STA. 986.5 FLOOR BEAM UPPER CHORD LBL 45 - RBL 45 WL 208 PER B737 SRM 53-70-51-2R-4. (LP 0500520)

Part: FLOOR SUPPORT — DAMAGED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0493406) INTERCOSTAL, UPPER SURFACE, STA 308, LBL 12, WL 208 CORRODED. REMOVED AND REPLACED INTERCOSTAL AT STA 294.5 BTW 312 LBL 11 IAW B737-800 SRM 51-40-02-0G AND DWG 141A5600 REV N.

Part: FLOOR SUPPORT — DAMAGED (ZONE 200) · airframe 68,241 hrs · 32,164 cycles

(LOG 0493387) FLOOR STRUCTURE UPPER SURFACE DAMAGED AT FASTENER HOLE, STA 365, RBL 11, WL 208. REMOVED AND REPLACED FLOOR STRUCTURE (INTERCOSTAL) RBL 11 BETWEEN STA 360 AND 380 IAW B737 SRM 51-40-02-0G AND DWG 141A5720.

Part: INTERCOSTAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0489390) CORROSION INTERCOSTAL BETWEEN STA 947.5 & STA 967 RBL48 WL208. REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 947.5 TO STA 967 RBL 48 WL 208 PER B737 SRM 51-40-02-0G AND DWG# 147A5650 REV. E.

Part: INTERCOSTAL — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0489386) CORROSION ON INTERCOSTAL BETWEEN STA 947.5 & STA 967 RBL25 WL208. REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 947.5 TO STA 967 RBL 25 WL 208 PER B737 SRM 51-40-02-0G AND DWG# 147A5650 REV. E.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0489393) FWD CARGO BAY L/H ZEE CHANNEL AT STA 500-500E IS REMOVED, THE ATTACHMENT STRUCTURE UNDERNEATH HAS CORROSION AT THE ANCHOR NUTS. EMOVED & REPLACED FWD CARGO FLOOR BAFFLES L/H STA 500-STA 500E IAW B737 SRM 51-40-02-0G & BOEING DWG #'S 143A7505 REV: A & 143A7505 REV: B.

Part: FRAME — CRACKED (ZONE 200) · airframe 68,241 hrs · 32,164 cycles

(LOG 0482661) (L/H) FUSELAGE FRAME CRACKED AT (STA 867), S-8L A/C RAIL SUPPORT BRACKET INBOARD FASTENER APPROX (.125") LONG. ACCOMPLISHED REPAIR PER CUSTOMER CARD # 2526-01236-02A.

Part: FRAME — CRACKED (ZONE 100) · airframe 68,241 hrs · 32,164 cycles

(LOG 0482810) (L/H) FUSELAGE FRAME CRACKED AT (STA 500A), S-8L A/C RAIL SUPPORT BRACKET INBOARD FASTENER APPROX (.125") LONG. REPAIR ACCOMPLISHED PER CUSTOMER CARD # 2526-01236-02A.

Part: FRAME — CRACKED (ZONE 200) · airframe 68,241 hrs · 32,164 cycles

(LOG 0482651) CUSTOMER CARD: 2526-01236-01A. (L/H) FUSELAGE FRAME CRACKED AT (STA 827), S-8L A/C RAIL SUPPORT BRACKET INBOARD FASTENER APPROX (.125") LONG. ACCOMPLISHED REPAIR PER CUSTOMER CARD # 2526-01236-02A.

Part: STRINGER CLIP — DAMAGED (STA 727C STR 25L) · airframe 68,241 hrs · 32,164 cycles

(LOG 0484013) AFT CARGO BAY STRINGER CLIP DAMAGED AT STA 727C STR 25L WL 160. REMOVED AND REPLACED AFT CARGO BAY CLIP AT STA 727C STR 25L WL160 IAW B737-800 SRM 51-40-02-0G AND DWG 146A1202.

Part: FRAME — CRACKED (BS 380) · airframe 68,241 hrs · 32,164 cycles

(LOG 0482792) CUSTOMER CARD: 2526-01236-01B. (R/H) FUSELAGE FRAME CRACKED AT (BS 380) S-8R A/C RAIL SUPPORT BRACKET INBOARD FASTENER APPROX (.25")LONG. ACCOMPLISHED REPAIR PER CUSTOMER CARD # 2526-01236-02B.

Part: FRAME — CRACKED (ZONE 200) · airframe 68,241 hrs · 32,164 cycles

(LOG 0482673) CUSTOMER CARD: 2526-01236-01A. (L/H) FUSELAGE FRAME CRACKED AT (STA 380), S-8L A/C RAIL SUPPORT BRACKET INBOARD FASTENER APPROX (.125") LONG. ACCOMPLISHED REPAIR PER CUSTOMER CARD # 2526-01236-02A.

Part: FRAME — CRACKED (S-8L A/C RAIL SU) · airframe 68,241 hrs · 32,164 cycles

(LOG 0482803) (L/H) FUSELAGE FRAME CRACKED AT (STA 727B), S-8L A/C RAIL SUPPORT BRACKET INBOARD FASTENER APPROX (.125") LONG. ACCOMPLISHED REPAIR PER CUSTOMER CARD # 2526-01236-02A.

Part: CARGO — DAMAGED (STA 727C STR 25L) · airframe 68,241 hrs · 32,164 cycles

(LOG 0484003) AFT CARGO BAY FRAME HAS DAMAGE AT STA 727C STR 25L WL 160. REPAIRED DAMAGE ON AFT CARGO BAY FRAME INNER UPPER CHORD AT STA 727C STR 25L WL160 IAW B737-800 SRM 53-60-07-2R REPAIR 2.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

AIRCRAFT 3725, CORROSION AT AFT CARGO BAY INTERCOSTAL STA. 787 - 794, RBL 25. CORRECTIVE ACTION: REPLACED AFT CARGO BAY INTERCOSTAL STA 787-794, RBL 25 PER B737-800 SRM 51-40-02-0G AND DWG 146A8320 REV A. (LP 0502233)

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 68,241 hrs · 32,164 cycles

(LOG 0510530) GOUGES ON SEAT TRACK LOCATED AT STA 727C, RBL 25 AND WL 208. REPAIRED SEAT TRACK RBL 25 BTW STA 727B AND 727D IAW B737-800 SRM 53-00-52-2R REPAIR 5.

Part: FRAME — DISTORTED (S8L STA 727B) · airframe 68,241 hrs · 32,164 cycles

(LOG 0483995) FRAME REPAIR AT S8L STA 727B DEVIATES FROM CUSTOMER CARD 2526-01236-02A. REPAIR ANGLE ENDS ON HOLES COMMON TO S9L CLIP. TRIMED EXCESS MATERIAL ON REPAIR DOUBLER PER CARD: 2526-01236-02A STEP 17 FIG 1 SHEET 2 OF 7.

Part: FRAME — NONE (ZONE 200) · airframe 68,241 hrs · 32,164 cycles

(LOG 0489326) FRAME REPAIR AT S8L STA 827 DEVIATES FROM CUSTOMER CARD 2526-01236-02A. REPAIR ANGLE ENDS ON HOLES COMMON TO S9L CLIP. TRIMED EXCESS MATERIAL ON REPAIR DOUBLER PER CARD: 2526-01236-02A STEP 17 FIG 1 SHEET 2 OF 7 AND SRM B737 51-40-02-0G.

Part: BRACKET — CHAFED (SUPPORT BRACKET) · airframe 68,241 hrs · 32,164 cycles

(LOG 0484050) AIR CONDITIONER SUPPORT BRACKET RIDES ON RIVET IN OUTBOARD ROW OF RIVETS AT STA 867 FRAME REPAIR STR 8L. REMOVED AND REPLACED FASTENER AT AIR CONDITIONER SUPPORT BRACKET STA 867 FRAME REPAIR IAW B737 SRM 51-40-02-0G.

Part: FRAME — NONE (ZONE 200) · airframe 68,241 hrs · 32,164 cycles

(LOG 0489336) FRAME REPAIR AT S8L STA 500A DEVIATES FROM CUSTOMER CARD 2526-01236-02A. REPAIR ANGLE ENDS ON HOLES COMMON TO S9L CLIP. TRIMED EXCESS MATERIAL ON REPAIR DOUBLER PER CARD: 2526-01236-02A STEP 17 FIG1 SHEET 2 TO 7 AT STA 500A STR. 9L. B737 SRM 51-40-02-0G.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

AIRCRAFT 3725, FLOOR BEAM, UPPER SURFACE, STA 328, RBL 40 TO 44 WL 208 CORRODED. CORRECTIVE ACTION: REPAIRED DAMAGE ON FLOOR BEAM, UPPER SURFACE, STA 328, RBL 40 TO 44 WL 208 IAW B737-800 SRM 53-10-51-2R PROCEDURE 8 ALTERNATIVE 2 H. (LP 0500503)

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

AIRCRAFT 3725, FLOOR BEAM, UPPER SURFACE, STA 344. LBL 4, AND 9, WL 208 CORRODED. CORRECTIVE ACTION: REPAIRED DAMAGED ON FLOOR BEAM, UPPER SURFACE, STA 344 LBL 4 AND 9, WL-208 IAW B737-800 SRM 53-10-51-2R PROCEDURE 8 ALTERNATIVE 3. (LP 0500508)

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

AIRCRAFT 3725, FLOOR BEAM, UPPER SURFACE, STA 328, RBL 11, WL 208 CORRODED. CORRECTIVE ACTION: REPAIRED DAMAGED ON FLOOR BEAM, UPPER SURFACE, STA 328, RBL 11, WL 208 IAW B737-800 SRM 53-10-51-2R PROCEDURE 8 ALTERNATIVE 2. (LP 0500505)

Part: SILL DRAIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0467368) R/H MOPSILL HAS SEVERAL AREAS OF CORROSION FROM STA 285 TO STA 344, WL 208. INSTALLED REPLACEMENT FWD SERVICE DOOR LOWER SILL INNER CHORD (MOP SILL) FROM STA 259.5 RH TO STA 360 RH. WL 208 IAW B737 SRM 51-40-02-0G, DWG 141A8310 REV D.

Part: SILL DRAIN — DAMAGED (ZONE 200) · airframe 68,241 hrs · 32,164 cycles

(LOG 0458827) TOOLING MARKS IN RADIUS OF L/H MOPSILL STA 280 TO STA 294, WL 208. REMOVED AND INSTALLED REPLACEMENT L/H MOPSILL STA. 280 TO STA 294, WL 208 I.A.W DWG #141A8110, REV:F, B737 SRM 51-40-02-0G.

Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,241 hrs · 32,164 cycles

(LOG 0458848) L1 DOOR THRESHOLD ANGLE ATTACHED TO MOPSILL, UPPER SURFACE BETWEEN STA 312 AND 344, WL 209 CORRODED. REMOVED AND INSTALLED REPLACEMENT L1 DOOR THRESHOLD ANGLE ATTACHED TO MOPSILL UPPER SURFACE BETWEEN STA 312 AND 344, WL 209 I.AW DWG# 141A8110 REV: E, B737 SRM 51-40-02-0G.

Part: SHIELD — DAMAGED (ZONE 100) · airframe 68,241 hrs · 32,164 cycles

(LOG 0463829) FWD CARGO R/H AFT SHEILD AT STA 500 TO 500A AT RBL 24 HAS SEVERAL MIS DRILLED HOLES. REPLACED FWD CARGO R/H AFT SHIELD AT STA 500 TO 500A AT RBL 24 PER B737-800 SRM 51-40-02-0G AND DWG 143A0080 REV A.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 67,963 hrs · 32,022 cycles

(LOG 4329569) WORKING WORKCARD 3350-7413, EMERG LIGHTS BATTERY FAILED CAPACITY CHECK. R/R EMERG LIGHT BATTERY PACK AT ROW 11F PER B737 AMM 33-51.

Part: PUMP — INOPERATIVE (FUEL BOOST) · airframe 67,215 hrs · 31,655 cycles

SHIP 3725 -DIV- DIVERTING TO DTW DUE TO LEFT CENTER BOOST PUMP INOP. RIGHT CENTER BOOST PUMP ON MEL. CORRECTIVE ACTION: FOUND UFI FAULT CODE 80. RESET UFI. REPLACED LEFT AND RIGHT CENTER FUEL BOOST PUMPS. OPS CHECKS GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 63,958 hrs · 30,178 cycles

(LOG 9422968) DURING INSPECTION FOUND EMER LIGHT ON OVERHEAD BIN INOP AT 20 RT. FOUND CONNECTOR ABOVE OVERHEAD BIN LOSE. SECURED CONNECTOR OPS OK.

Part: BATTERY PACK — INOPERATIVE · airframe 62,698 hrs · 29,589 cycles

(LOG 9269791) DURING INSPECTION FOUND RH SIDE FWD EMER LTS FAILED TEST. R/R BATTERY REF B737 AMM 33-51, OPS CHECKED GOOD.

Part: FUSE — INOPERATIVE · airframe 62,363 hrs · 29,422 cycles

(LOG 8836124) DURING INSPECTION FOUND ROWS 23-33DEF EMERGENCY AISLE LIGHTS INOP. REPLACED FUSE IN POWER SLED M1672 IAW B737 AMM 33-51. EMERGENCY AISLE PATH LIGHTS AT ROWS 23-33DEF, OPS CHECK GOOD.

Part: NONE — NONE · airframe 62,290 hrs · 29,393 cycles

(LOG 8850478) AT DEPARTURE FOUND 16D TRIPLE SEAT ASSY LOOSE FROM FLOOR TRACK. SECURED SEAT AND OPS CHECK NML PER B737 AMM 25-21.

Part: NONE — NONE · airframe 61,285 hrs · 28,962 cycles

(LOG 8278811) DURING INSPECTION FOUND SEAT ASSEMBLY 15DEF OUT OF SEAT TRACK. REINSTALLED SEAT ASSEMBLY REF B737 AMM 25-22.

Part: NONE — NONE · airframe 61,028 hrs · 28,851 cycles

(LOG 8328782) DURING INSPECTION FOUND EMERGENCY LIGHTS INOP AT ROWS 17 AND 18 (ABC) OVERWING HATCH LIGHTS. RELAMPED BULBS AT OVERWING HATCH LIGHTS ROWS 17ABC AND 18ABC. OPS CHK GOOD IAW B737 AMM 33-51.

Part: HEATER — BURNED (LT OVERWNG EXIT) · airframe 60,884 hrs · 28,795 cycles

SHIP 3725 -DIV/SMK- DIVERTED TO TAM DUE TO SMOKE/SMELL EVENT. FOUND LEFT AFT OVER-WING EMERGENCY EXIT DOOR AFT HEATING BLANKET BURNT. MAINTENANCE REPLACED LEFT AFT HATCH, AFT HEATING STRIP PER B 737 AMM 21-45. OPS CHECK OK.

Part: SEAT TRACK — CRACKED (BS 727H-727J) · airframe 60,500 hrs · 28,601 cycles

(LOG 1923337) DURING INSPECTION FOUND SEAT ROW 27B ADJUSTMENT CRACK ON SEAT TRACK WAS FOUND. EAT TRACK ON STA. 727H TO 727J AND LBL. 22 WAS REPAIRED PER B737-800 SRM 53-00-52-2R REPAIR 5.

Part: SKIN — NICKED (HORIZONTAL STAB) · airframe 60,500 hrs · 28,601 cycles

(LOG 1911757) DURING INSPECTION FOUND NICK ON LH HORIZONTAL STABILIZER LEADING EDGE STA LE 105. PERMANENT REPAIR ON LH HORIZONTAL STABILIZER LEADING EDGE STA LE 105 WAS PERFORMED PER B737-800 SRM 55-10-01-2R-1.

Part: SKIN — NICKED (HORIZONTAL STAB) · airframe 60,500 hrs · 28,601 cycles

(LOG 1911864) DURING INSPECTION FOUND NICK ON LH HORIZONTAL STABILIZER LEADING EDGE STA LE 133. PERMANENT REPAIR ON LH HORIZONTAL STABILIZER LEADING EDGE STA LE 133 WAS PERFORMED PER B737-800 SRM 55-10-01-2R-1.

Part: CHANNEL — CORRODED (BS 500G-500I) · corrosion level 2 · airframe 60,500 hrs · 28,601 cycles

(LOG 1911716) DURING INSPECTION FOUND CORROSION ON FLOOR SUPPORT CHANNEL FROM STA 500G TO 500I BTW RBL 22 TO 25.2 AT FWD CARGO COMPARTMENT.

Part: BULKHEAD — DAMAGED (BS 663) · airframe 60,500 hrs · 28,601 cycles

(LOG 1908575) DURING INSPECTION FOUND BROKEN VAPOR BARIER STA 663 AT RH WHEEL WELL FWD BULKHEAD FYT. VAPOR BARIER STA 663 AT RH WHEEL WELL FWD BULKHEAD WAS REPAIRED PER B737-800 SRM 57-10-10-2R-2.

Part: SKIN — NICKED (SPOILER) · airframe 60,500 hrs · 28,601 cycles

(LOG 1907974) DURING INSPECTION FOUND NICKS AT LOWER SURFACE OF SPOILER PANEL NO. 3. LOWER SURFACE OF SPOILER PANEL NO. 3 WAS REPAIRED PER B737-800 SRM 51-70-10-2R PROCEDURE REPAIR GENERAL.

Part: SKIN — DAMAGED (NR 6 SPOILER) · airframe 60,500 hrs · 28,601 cycles

(LOG 1906647) DURING INSPECTION FOUND SEVERAL NICKS AT LOWER SURFACE OF SPOILER PANEL NO. 6. LOWER SURFACE OF SPOILER PANEL NO. 6 WAS REPAIRED PER B737-800 SRM 51-70-10-2R PROCEDURE REPAIR GENERAL AND B737-800 SRM 57-70-01-2R PROCEDURE 1 REPAIR 1.

Part: SKIN — DAMAGED (NR 1 SPOILER) · airframe 60,500 hrs · 28,601 cycles

(LOG 1906683) DURING INSPECTION FOUND NICKS AT LOWER SURFACE OF SPOILER PANEL NO. 1. LOWER SURFACE OF SPOILER PANEL NO. 1 WAS REPAIRED PER B737-800 SRM 51-70-10-2R PROCEDURE REPAIR GENERAL AND B737-800 SRM 57-70-01-2R PROCEDURE 1 REPAIR 1.

Part: NONE — NONE · airframe 62,864 hrs · 29,694 cycles

(LOG 1906288) ELONGATED HOLES AND MISDRILLS FOUND DURING IDTV REMOVAL. DAMAGE REPAIRED PER ERA 593376-14.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 57,780 hrs · 27,404 cycles

DURING INSPECTION, FOUND LT OVERWING ESCAPE LIGHT INOPERATIVE BETWEEN DOORS. RESET FUSE ON POWER SUPPLY M1670. REF B737 WDM 33-51-13. LT OVERWING ESCAPE LIGHT NOW CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,637 hrs · 27,310 cycles

DURING INSPECTION, FOUND EMERGENCY LIGHT BATTERY FOR L1 DOOR EMERGENCY LIGHTS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51. OPS CHECKED GOOD.

Part: PANEL — MISSING (NOT REPORTED) · airframe 56,387 hrs · 26,792 cycles

(LOG 6243314) DURING SERVICE CHECK FOUND PANEL 194E MISING. REPLACED PANEL 194E.

Part: PLATE — MISSING (FUSELAGE) · airframe 54,481 hrs · 25,954 cycles

(LOG 5795013) DURING INSPECTION FOUND 2 LOWER ANTENNAS BASE PLATES ON LOWER AFT FUSELAGE APPEAR TO BE MISSING. MAINTENANCE REINSTALLED ANTENNA BASE PLATES CHECKS GOOD.

Part: CHILLER — ODOR (GALLEY) · airframe 53,696 hrs · 25,630 cycles

(LOG 0877436) INBOUND, CREW REPORTED ELECTRICAL ODOR FROM THE CHILLER. MAINTENANCE REPLACED FWD GALLEY CHILLER PER B737 AMM 25-31. OPS CK GOOD.

Part: SKIN — DENTED (LE SLAT) · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND DENT ON UPPER SURFACE AT RT WING TRAILING EDGE WEDGE SLAT NR 5. WING TRAILING EDGE WEDGE SLAT NR 5 WAS REPAIRED PER SRM 57-42-01-2R-4 AND SRM 51-70-10-2R-0.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CRACKED INTERCOSTAL STA 500F BTW S-25L/S-26L AT INTERNAL STRUCTURE FWD CARGO COMPARTMENT. INTERCOSTAL WAS REPAIRED PER ERA 570434-14 REV ORIG AND ETI-37-18-456 REV 1.

Part: INTERCOSTAL — DENTED (FUSELAGE) · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND BENTS ON INTERCOSTAL BELOW ZEE SIDE PLATE FROM STATION 500F TO 500G RBL 21 AT C1 CARGO CMPT. INTERCOSTAL WAS REPAIRED PER ERA 570434-14 REV ORIG AND ETI-37-18-456 REV 1.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CORROSION ON EXTERNAL FUSELAGE SKIN BTW STATION 500+5 TO 500+10 ALSO ON STA 500A+6 TO 500A+12 BTW S-27L AND S-27R. EXTERNAL FUSELAGE SKIN WAS REPAIRED PER ERA 570513-14 REV ORIG AND ETI-37-18-444 REV 3.

Part: SKIN — CORRODED (FUSELAGE) · airframe 52,572 hrs · 25,159 cycles

DURING HCK AT QRO, CORROSION WAS FOUND ON EXTERNAL FUSELAGE SKIN 143A3232-12 AT BS 500 +8 AND BS 500A + 12 AT FAYING SURFACES OF THE DEACTIVATED AIR PHONE ANTENNAS, BTW S-28R AND S-28L. MAINTENANCE REPAIRED DAMAGE PER ERA 570513-14.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CRACK ON BULKHEAD UPPER WEB STA 663 BTW RBL 22 TO RBL 50, WL 198 AT RT MLG WHEEL WELL. BULKHEAD UPPER WEB STA 663 BTW RBL 22 TO RBL 50 WAS REPAIRED PER ER/A 570235-14 REV ORIG AND ETI 37-18-436 REV 1.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 52,572 hrs · 25,159 cycles

DURING HCK AT QRO, SEVERAL CRACKS WERE FOUND AT THE RT CENTER WING REAR SPAR VERTICAL PRESSURE WEB. MAINTENANCE REPAIRED DAMAGE PER ERA 570235-14.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CORROSION ON LBL ZEE SUPPORT BTW STA 727 TO 747. ZEE SUPPORT LBL BTW STA 727 TO 747 WAS REPLACED PER SRM 53-60-53 FIG 2, 51-40-05, 51-40-08, 51-40-02 PAR 7C; 51-40-02 PAR 4, 51-20-01 PART 5, AMM 51-21-72-370-804 AND PS 900-2 NR 09.

Part: INTERCOSTAL — DENTED (FUSELAGE) · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND DENTS ON INTERCOSTALS BELOW ZEE SIDE PLATE FROM STA 500 TO 500F LBL 21 AT C1 CARGO CMPT. INTERCOSTALS BELOW ZEE SIDE PLATE FROM STATON 500 TO 500F LBL 21 AT C1 CARGO CMPT (C1) WERE REPLACE PER SRM 51-40-02.

Part: FRAME — DENTED (FUSELAGE) · airframe 52,572 hrs · 25,159 cycles

DURING HCK AT QRO, TWO DENTS WERE FOUND ON THE INBOARD FLANGE OF THE STA 500F FRAME, P/N 143A1200-31, BETWEEN S-24L - S-26L. MAINTENANCE REPAIRED DAMAGE PER ERA 570120-14.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CORROSION IN THE ZEE CHANNEL SIDEPLATE RBL 21.00 BTW STA 500A-500I AT INTERNAL STRUCTURE FWD CARGO COMPARTMENT. THE ZEE CHANNEL SIDEPLATE RBL 21.00 BTW STA 500A-500I WAS REPLACED PER SRM 51-40-02.

Part: FRAME — DENTED (FUSELAGE) · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND DENTS (2 E/A) IN FRAME STATION 500F BTW S-24L/S-26L AT INTERNAL STRUCTURE FORWARD CARGO COMPARTMENT. FRAME WAS REPAIRED PER ER/A 570120-14 REV ORIG AND ETI-37-18-434 REV 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CORROSION ON FLOOR SUPPORT IN STA Y= 887 BETWEEN STR 26LBL TO 25RBL AT AFT CARGO COMPARTMENT. FLOOR SUPPORT IN STA Y= 887 BETWEEN STR 26LBL TO 25RBL WAS REPLACED PER SRM 51-40-02.

Part: FRAME — DENTED (FUSELAGE) · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND DENT ON UPPER CHORD OF FRAME P/N 143A1200-41 AT STA 500C BETWEEN STRINGERS 24L AND 25L. MAINTENANCE REPAIRED PER ERA 570236-14.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CORROSION IN THE ZEE CHANNEL SIDEPLATE LBL 21.00 BTW STA 460-500I AT INTERNAL STRUCTURE FWD CARGO COMPARTMENT. MAINTENANCE REPLACED SIDEPLATE PER SRM 51-40-02 PAR 4 AND 7.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CORROSION ON RT "Z" FLOOR SUPPORT IN PROJECTION STR 25RBL BETWEEN STA. Y= 867 TO Y= 887 AT AFT CARGO COMPARTMENT. NEW SHIELD ON RT STA Y= 867 TO Y= 887 AT AFT CARGO COMPARTMENT WAS REPLACE PER SRM 51-40-02, 51-40-08 ,51-20-01 PAR 5 AND AMM 51-21-72-370-804.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CORROSION ON WEB IN PROJECTION STGR 25RBL BETWEEN STA Y= 847 TO Y= 867 AT AFT CARGO COMPRTMENT. WEB IN PROJECTION STGR 25RBL BETWEEN STA Y= 847 TO Y= 867 AT AFT CARGO COMPARTMENT WAS REPLACED PER DWG 146A8127 REV B AND SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CRACK ON FRAME STA 440 BTW S-8L TO S-9L AT PAX CABIN. FRAME STATION 440 BTW S-8L TO S-9L WAS REPAIRED PER ERA 570034-14 AD REV ORIGINAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CRACK ON FRAME STA 400 BTW S-8R TO S-9R AT PAX CABIN. FRAME STA 400 BTW S-8R TO S-9R WAS REPAIRED PER ERA 570034-14AD REV ORIG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CRACK ON FRAME STA 867 BTW S-8R TO S-9R AT PAX CABIN. FRAME STATION 867 BTW S-8R TO S-9R WAS REPAIRED PER ERA 570034-14AD REV ORIGINAL.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CORROSION ON FLOOR SUPPORT BTW STA Y 947 AND 967 LBL 48. CORROSION WAS REMOVED PER SRM 51-10-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CRACK ON FRAME STA 400 BTW S-8L TO S-9L AT PAX CABIN. FRAME STA 400 BTW S-8L TO S-9L WAS REPAIRED PER ER/A 570034-14 AD REV ORIGINAL.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CORROSION IN THE ZEE CHANNEL SIDEPLATE RBL 23.00 BTW STA 420 AND 440 AT INTERNAL STRUCTURE FWD CARGO COMPARTMENT. DAMAGEE ZEE CHANNEL SIDEPLATE RBL 23.00 BTW STA 420 AND 440 AT INTERNAL STRUCTURE FWD CARGO COMPARTMENT WAS REPALCED PER SRM 51-40-02 PAR 4 AND DWG 143A8126, REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CRACK ON FRAME STA 440 BTW S-8R TO S-9R AT PAX CABIN. FRAME STA 440 BTW S-8R TO S-9R WAS REPAIRED PER ERA 570034-14AD REV ORIG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CRACK ON FRAME STA 500C BTW S-8R TO S-9R AT PAX CABIN. FRAME STA 500C BTW S-8R TO S-9R WAS REPAIRED PER ERA570034-14 AD REV ORIGINAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CRACK ON FRAME STA 500A BTW S-8R TO S-9R AT PAX CABIN. CRACKED ON FRAME STA 500A BTW S-8R TO S-9R AT PAX WAS REPAIRED PER ERA 570034-14AD REV ORIGINAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CRACK ON FRAME STA 480 BTW S-8L TO S-9L AT PAX CABIN. FRAME STA 480 BTW S-8L TO S-9L AT PAX CABIN WAS REPAIRED PER ERA 570034-14AD REV ORIGINAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CORROSION OUT OF LIMITS ON FLOORBEAM STA 986 BTW BL 0 AND RBL 44 AT AFT WET AREA. REPAIR PERMANENT WAS ACCOMPLISHED ON FLOORBEAM STA 986 BTW BL 0 AND RBL 44 PER SRM 53-70-51-2R-4 SECTION 47, PARAGRAPH 4 A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CORROSION ON ZEE FLOOR SUPPORT STA 992 RBL=45 AT CABIN PAX FLOOR STUCTURE. ZEE FLOOR SUPPORT WAS REPLACED PER DWG 147A5710 ITEM 2 REV C AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CORROSION ON ZEE FLOOR SUPPORT STA 992 LBL=45 AT CABIN PAX FLOOR STUCTURE. ZEE FLOOR SUPPORT WAS REPLACED PER DWG 147A5710 ITEM 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CORROSION OUT OF LIMITS ON FLOORBEAM STA 986 BTW BL 0 AND LBL 44 AT AFT WET AREA. REPAIR WAS ACCOMPLISHED ON FLOORBEAM STA 986 BTW BL 0 AND LBL 44 PER SRM 53-70-51-2R-4 SECTION 47, PARAGRAPH 4 A.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CRACK IN RIB BTW FRONT SPAR AND REAR SPAR AT LEFT HORIZONTAL STAB STA 102.99. RIB WAS REPAIRED PER SRM 55-10-09 REPAIR 4.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CRACK IN RIB BTW FRONT SPAR AND REAR SPAR AT RIGHT HORIZONTAL STAB STA 92.99. RIB WAS REPAIRED PER SRM 55-10-09 FIG 202 REPAIR 4.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,572 hrs · 25,159 cycles

DURING INSPECTION FOUND CORROSION ON FLOOR STRUCTURE STA 230 AND LBL 8 AT FLIGHT COMPARTMENT. FLOOR STRUCTURE STA 230 AND LBL 8 WAS REPAIRED PER SRM 53-10-51 REP 2.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 51,077 hrs · 24,616 cycles

FOUND SKIN DAMAGE APPROXIMATELY TWO FEET AFT OF THE DOOR AT FLOOR LINE. REPAIRED IAW SRM 53-00-01, REPAIR 36.

Part: SKIN — DENTED (FUSELAGE) · airframe 53,870 hrs · 25,698 cycles

(LOG 0404703) WHILE IN ATL FOR A SCHEDULED MAINTENANCE VISIT, MTC FOUND A DENT COMMON TO THE FUSELAGE SKIN AT STA 380, S-16L. MAINTENANCE REPAIRED DENT PER ERA 565436-14.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 50,343 hrs · 24,362 cycles

PRES DURING FLIGHT AT 12000 MSL THE CABIN ALTITUDE WARNING LIGHT AND ALTITUDE HORN ACTIVATED. CREW CONTACTED ATC AND REQUESTED AN IMMEDIATE AND RAPID DECENT TO 9000 FEET HORN AND LIGHT WENT OUT. FLIGHT CONTINUED TO DESTINATION. MAINTENANCE PERFORMED A SINGLE PACK OPERATION CONFIDENCE CHECK PER B737 AMM 21-00-05. THE FLOW CONTROL VALVE WAS ALSO CHANGED AS A FURTHER PRECAUTION.

Part: LIGHT — BROKEN (ROW 22) · airframe 49,900 hrs · 24,189 cycles

DURING INSPECTION, FOUND THE EMERGENCY EXIT IN THE MID CABIN BROKEN. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSY AT SEAT ROW 22 IAW AMM 33-51. LIGHT CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,676 hrs · 23,469 cycles

DURING INSPECTION FOUND EMERGENCY LIGHT UNDER OVERHEARD BIN INOPERATIVE AT SEAT 10ABC. MAINTENANCE PERFORMED REPAIR PER NR 001-378:3350-7413/002.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 47,676 hrs · 23,469 cycles

DURING INSPECTION FOUND 2 EACH CRACKS FOUND ON UPPER FORWARD BULKHEAD IN LEFT MLG WHEEL WELL. MAINTENANCE REPAIRED PER SRM 57-10-10, REPAIR 3, ALTERNATIVE REP 2.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 47,676 hrs · 23,469 cycles

DURING INSPECTION FOUND 2 EACH CRACKS FOUND ON UPPER FORWARD BULKHEAD IN LEFT MLG WHEEL WELL. MAINTENANCE REPAIRED PER SRM 57-10-10, REPAIR 3, ALTERNATIVE REP 2.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 47,676 hrs · 23,469 cycles

DURING INSPECTION, FOUND TWO CRACKS ON THE UPPER FORWARD BULKHEAD IN LEFT MLG WHEEL WELL. MAINTENANCE REPAIRED THE BULKHEAD IAW SRM 57-10-10, REPAIR 3.

Part: FLOOR PANEL — DAMAGED · airframe 47,628 hrs · 23,450 cycles

AIRCRAFT SUSTAINED HEAT AND FIRE DAMAGE TO THE RIGHT SIDE OF THE AIRCRAFT BETWEEN BS 211.8 AND 243.7 AND STRINGERS 17 AND 247R. MAINTENANCE REPAIRED DAMAGED FLOOR WEB IAW ERA 552443-14.

Part: RECEPTACLE — FAILED (GROUND POWER) · airframe 47,626 hrs · 23,449 cycles

AIRCRAFT SUSTAINED HEAT AND FIRE DAMAGE COCKPIT FLOOR STIFFENER DUE TO ELECTRICAL FIRE ORIGINATING AT THE EXTERNAL GROUND POWER RECEPTACLE. MAINTENANCE REPAIRED DAMAGED STIFFENER IAW ERA 552502-14.

Part: SEAT TRACK — WORN (BS 520) · airframe 45,764 hrs · 22,829 cycles

DURING INSPECTION, FOUND BS 520, LBL 24 SEAT TRACK WORN FROM SEAT. MAINTENANCE INSTALLED A NEW SEAT TRACK IAW SRM 53-00-52, REPAIR 4.

Part: SEAT TRACK — WORN (BS 520) · airframe 45,764 hrs · 22,829 cycles

DURING INSPECTION, FOUND BS 520, RBL 45 SEAT TRACK WORN FROM SEAT. MAINTENANCE INSTALLED A NEW SEAT TRACK IAW SRM 53-00-52, REPAIR 4.

Part: SEAT TRACK — WORN (BS 520) · airframe 45,764 hrs · 22,829 cycles

DURING INSPECTION, FOUND BS 520, LBL 45, SEAT TRACK WORN FROM SEAT. MAINTENANCE REPAIRED THE SEAT TRACK IAW SRM 53-00-52, REPAIR 4.

Part: SEAT TRACK — WORN (BS 520) · airframe 45,764 hrs · 22,829 cycles

DURING INSPECTION, FOUND BS 520, RBL 24 SEAT TRACK WORN FROM SEAT. MAINTENANCE REPAIRED THE SEAT TRACK IAW SRM 53-00-52, REPAIR 4.

Part: LIGHT — BROKEN (SEAT 25F) · airframe 40,818 hrs · 21,157 cycles

DURING INSPECTION, FOUND EMERGENCY EXIT LIGHT ASSEMBLY AT 25F BROKEN. MAINTENANCE REPLACED LIGHT ASSY IAW MM 33-51. OPS NORMAL.

Part: FLOORBEAM — CRACKED (BS 727B) · airframe 39,144 hrs · 20,589 cycles

DURING INSPECTION, FOUND CABIN FLOORBEAM BS 727B SPILCE STRAP LBL24.75, RBL 24.75, LBL 45.50, AND RBL 45.50 CRACKED. MAINTENANCE REPAIRED IAW ERA 526847-14AD, REV ORIG.

Part: DIODE — FAILED (EMERGENCY LIGHTS) · airframe 38,781 hrs · 20,463 cycles

DURING INSPECTION FOUND EMERGENCY LIGHTS AT SEATS 26 AND 29 AT BOTTOM OF OVERHEAD BIN INOPERATIVE. MAINTENANCE FOUND BAD DIODE IN EMERGENCY BATTERY PACK. REMOVED AND REPLACED DIODE PER AMM 33-52. OPERATIONAL TEST OK.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,931 hrs · 19,407 cycles

DURING INSPECTION FOUND 33D EMERGENCY LIGHT INOPERATIVE. MX REPLACED WIRE HARNESS IAW WDM 33-51. OPS CHECK OK.

Part: WEB — DAMAGED (BS 360) · airframe 35,542 hrs · 19,268 cycles

DURING INSPECTION, FOUND FS 360 FRAME DAMAGED TO WEBAROUND SEVERAL FASTENER HOLES AND ONE LIGHTENING HOLE. MX C/W WEB REPLACEMENT IAW ERA 493220-14, REV D.

Part: FRAME — CRACKED (UNKNOWN) · airframe 39,144 hrs · 20,589 cycles

DURING INSPECTION, FOUND STRINGER 8R FRAMES CRACKED. MAINTENANCE REPAIRED IAW ERA 504524.

Part: FLOORBEAM — WORN · airframe 39,265 hrs · 20,628 cycles

DURING INSPECTION, WEAR WAS FOUND ON THE INBD FLANGE UPPER SURFACE OF THE FLOORBEAM UPPER TEE. MAINTENANCE REPAIRED IAW ERA 504527.

Part: FRAME — CRACKED (BS 727B S8R) · airframe 32,638 hrs · 18,188 cycles

FRAME BS 727B CRACKED BELOW STRINGER 8R. REPAIRED PER ERA 504524-14AD REV ORG.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,502 hrs · 17,029 cycles

EMERGENCY EGRESS AISLE LIGHTING INOPERATIVE AT ROWS 19, 21, 24 AND CENTER OVERHEAD. MAINTENANCE REPLACED THE BATTERY AND CHARGER M1670. CHECKS ARE GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,050 hrs · 16,865 cycles

EMERGENCY EGRESS AISLE LIGHTING INOPERATIVE AT ROWS 11-16. MAINTENANCE REPLACED THE BATTERY PACK AND THE SYSTEM NOW CHECKS OK.

Part: DOOR FRAME — DAMAGED (BS 360) · airframe 35,542 hrs · 19,268 cycles

DURING INSPECTION FOUND FUSELAGE L1 DOOR SURROUND STRUCTURE AT FS 360 DAMAGED. MX C/W PERMANENT REPAIR IAW ERA 493220-14, REV D.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 28,933 hrs · 16,810 cycles

ACS REPORTS GROUND DAMAGE INBOUND AT L1 DOOR AT STA 360-380 JUST BELOW FLOOR LEVEL. C/W ERA 493220-14 REV A.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 28,782 hrs · 16,758 cycles

LEFT LOWER AFT, OVERWING EMERGENCY EGRESS SLIDE LIGHT INOP. REPLACED POWER SUPPLY, CKS OK.

Part: VAPOR BARRIER — CRACKED (LT WHEEL WELL) · airframe 27,865 hrs · 16,402 cycles

LT VAPOR BARRIER WEB CRACKED AT AFT END OF ECS COMPARTMENT AND REPAIRED IAW SRM 57-10-10, REP 2.

Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 26,300 hrs · 15,786 cycles

EMERGENCY EGRESS AISLE LIGHT INOPERATIVE AT ROW 22 DEF. MAINTENANCE REPAIRED THE WIRE HARNESS ON SEAT ASSEMBLY AND THE SYSTEM NOW CHECKS OPERATIONAL (2010-D0856)(DL738101922).

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,064 hrs · 15,273 cycles

DURING EMERGENCY LIGHT FUNCTIONAL CHECK OPS 68052 FOUND FWD BATTERY PACK ONLY OPS FOR 4 MIN. REPLACED BATTERY PACK. CHECKS GOOD.

Part: CONTROLLER — MALFUNCTIONED (WINDSHIELD HEAT) · airframe 24,955 hrs · 15,232 cycles

F/O FWD WINDSHIELD SMOKING AT BOTH HEATER CONNECTION LOCATIONS, WHEN WINDOW HEAT APPLIED. CORRECTION: R & R F/O R1 WINDSHIELD, AND WINDOW HEAT CONTROLLER. CHECKS OK.

Part: ENGINE — CONTAMINATED (NR 1) · airframe 24,406 hrs · 15,036 cycles

ATB STRONG ODOR AND FUMES IN CABIN AND COCKPIT AFTER TAKEOFF. RETURNED TO DEPARTURE RAN ENG'S AND BOTH PACKS. OPERATED ALL GALLEYS. OPERATED ALL BLEEDS APU AND ENGINES. NO ODOR NOTED. FOUND CONSIDERABLE AMOUNT OF GLYCOL IN ENG INTAKES. SUSPECT ENG INGESTED GLYCOL. RAN PACKS FOR 20 MIN. NO SMELL NOTED.

Part: WINDOW — CRACKED (COCKPIT) · airframe 17,639 hrs · 12,447 cycles

CLIMBING THROUGH 12,000 CAPT SIDE NR 2 WINDOW CRACKED. PRESS WAS NOT LOST. REPLACED CAPT NR 2 SLIDING WINDOW PER MM. PRESSURIZED A/C, NO LEAKS. WINDOW HEAT CONTROLLER REPLACED AND CKS OK PER MM. PARTS HELD IN QUARANTINE CVG.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,593 hrs · 11,279 cycles

AFT EMERGENCY PATH LIGHT INOP. REPLACED POWER PACK FUSE, OPS CHK OK.

Part: CHILLER — OVERHEATED (FWD GALLEY) · airframe 6,066 hrs · 6,657 cycles

FUMES IN CABIN AT FL 350 INCREASING IN INTENSITY. SECURED GALLEY POWER AND ENTERTAINMENT SYSTEM. DIVERTING TO CLT. ISOLATED SMELL TO FWD GALLEY CHILLER DUE TO OVERHEAT FROM CLOGGED FILTER AND CLOGGED DUCT TO CHILLER. REPLACED CHILLER AND CLEANED DUCT.

Part: HMU — FAULTY (NR 2 ENGINE) · airframe 1,391 hrs · 1,833 cycles

DURING PREFLT, FOUND NR 2 ENG SHUT DOWN INADVERTENTLY AND WOULD NOT RESTART. FOUND HMU INOP. REPLACED HMU.

Part: PUMP — FAULTY (NR 2 ENGINE) · airframe 1,391 hrs · 1,833 cycles

NR 2 ENGINE SHUTS DOWN AFTER REACHING IDLE. T/S PER FIM 73-06-00-810-807 FOUND FUEL PUMP PRESSURE LOW PER AMM 73-11-01-200-802. REPLACED FUEL PUMP PER AMM 73-11-01-4. LEAK CHECK AND OPS CHECK OK.