N3742C

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 76,570 hrs · 30,656 cycles

(LOG 7469062) DURING SERVICE CHECK FOUND OVERWING EXIT DOOR EMERGENCY LIGHTS OUT AT 17A/18A. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1694 REF B737 AMM 33-51. OPS CHK GOOD.

Part: SKIN — CRACKED (ZONE 800) · airframe 76,487 hrs · 30,621 cycles

(LOG 1213937) GROUND POWER RECEPTACLE SURROUND STRUCTURE TAB BETWEEN DOOR HINGES IS CRACKED. REMOVED AND REPLACED DOUBLER AND TRIPPLER PER ER/A 585833-14 REV A SECTION II. COMPARED TO PRI REV 1, 2, 3, 4 AND 5. ALL WORK STEPS COMPLETE.

Part: SKIN — GROUND DAMAGE (ZONE 100) · airframe 76,487 hrs · 30,621 cycles

(LOG 7472984) AIRCRAFT SUSTAINED IMPACT DAMAGE; SECTION 41 LOWER LOBE FORWARD OF E&E DOOR. PERFORMED FRAME REPAIRS PER BOEING DRAWINGS 141A1501, 141A1502 AND 141A1503. SKIN INSTALLATION PER BOEING DRAWING 141A0650, 141A3501 AND 141A3502. ASSOCIATED REPAIRS C/W ON ER/A'S 585800-14 REV A, 628289-14 REV O, 628235-14 REV O AND 627805-14 REV O.

Part: SKIN — MECHANIC ERROR (ZONE 200) · airframe 76,452 hrs · 30,599 cycles

DURING THE LOCATION AND DRILLING OF SKIN P/N 141A3521Y33, 12 HOLES WERE MISDRILLED ON THE SKIN @ RBL 17 AND BS 178 - 188. TRIMMED OUT MINIMAL AMOUNT OF MATERIAL ONLY TO REMOVE MISDRILLED HOLES PER STEP 3 PN 628289-14 REV 0. REMOVED THE NECESSARY NUMBER OF FASTENER IN THE WITHIN THE REPAIR AREA. PERFORMED HFEC PER STEP 8 AND 9 OF PRI 628289-14 REV 1. FABRICATED REPAIR PARTS PER PRI 628289-14 REV 1. TREATED AND PRIMED AND INSTALLED PER PRI 628289-14 REV 1. INSTALLED REPAIR PER PRI 628289-14 REV 1. APPLIED TOP COAT PER DAL PS 900-3-6 #36. COMPLIED WITH ER/A 628289-14 REVISION ORIGINAL. COMPLIED WITH PRI'S 628289-14 REV 0, 1, AND 2. ALL STEPS MATCH, ALL RII STEPS COMPLIED WITH.

Part: BEAR STRAP — GROUND DAMAGE (ZONE 100) · airframe 76,452 hrs · 30,599 cycles

DUE TO IMPACT DAMAGE, FUSELAGE BEARSTRAP P/N 141A3522-3 FORWARD SECTION DAMAGED FROM STA 203.8 - 196.5. REPAIRED DAMAGED BEARSTRAP PER ER/A 628235-14 REV ORIGINAL COMPARED TO PRI 628235-14 REV 0 AND 1. IDENTIFIED REPAIR STEPS 10 AND 11 ADDED TO ER/A 628235-14 REV ORIGINAL. ALL STEPS COMPLIED WITH.

Part: SKIN — DAMAGED (ZONE 100) · airframe 76,452 hrs · 30,599 cycles

(LOG 1197892) AIRCRAFT TAIL NUMBER N3742C WAS SUBJECT TO IMPACT DAMAGE DUE TO HIGH WIND EVENT IN DENVER COLORADO. FUSELAGE SKIN PN 141A5321-11 WILL BE REPLACED AND SO IS THE BEARSTRAP PN 141A3522-3 FORWARD SECTION. WHILE THE SKIN PN 141A3521-11 IS RUNNING FROM STA 178 TO STA 259.50, THE BEARSTRAP PN 141A3522-3 IS RUNNING FROM STA 203.8 TO STA 351.20. REMOVAL OF THE ENTIRE BEARSTRAP REQUIRES REMOVAL OF THE NEXT SKIN SECTION FROM STA 259.50 TO STA 360. BEARSTRAP WILL BE SPLICED BASED ON OEM DISPOSITION. BEAR STRAP PN 141A3522-3 IS MADE OUT OF 2024-T3 0.080 CLAD SHEET. PERFORMED REPAIR IAW ERA 628235-14.

Part: FRAME — DAMAGED (ZONE 100) · airframe 76,452 hrs · 30,599 cycles

(LOG 1136825) FRAME 196.5, LOWER LOBE DAMAGED. COMPLETED INSTALLATION OF LOWER LOBE FRAME 196.5 PER BOEING DRAWING 141A1502.

Part: FRAME — DAMAGED (ZONE 100) · airframe 76,452 hrs · 30,599 cycles

(LOG 1136820) FRAME 203.8, LOWER LOBE DAMAGED. PROCURED LOWER CHORD AND WEB. POSITIONED PER BOEING DRAWING 141A1503. MATCH DRILLED PER BOEING B737 DRAWING 141A1503 (RJD 471692). INSTALLED LOWER LOBE FRAME 203.8 PER BOEING DRAWING 141A1503.

Part: FRAME — CRACKED (ZONE 100) · airframe 76,452 hrs · 30,599 cycles

(LOG 1136833) BHEC CRACK INDICATION IN STA 196.5 L/H FRAME SPLICE WEB. COMPLETED DRILLING SPLICE PLATE PER BOEING DRAWING 141A1502 (RJD 471692) OKAY TO TREAT AND PRIME (QC 5332). TREATED AND PRIMED (RJD 471692). INSTALLED SPLICE PLATE PER BOEING DRAWING 141A1502.

Part: FRAME — GROUND DAMAGE (ZONE 100) · airframe 76,452 hrs · 30,599 cycles

(LOG 1131559) REMOVED FRAME 188; LOWER LOBE, DUE TO IMPACT DAMAGE. INSTALLED FOR ALIGNMENT REF B737 DRAWING 141A1501 (RJD 471692). REMOVED WEB AND LOWER CHORD, DEBURRED AND PRIMED ALL BARE METAL . COMPLETED INSTALLATION OF FRAME 188 LOWER LOBE PER BOEING 737 DRAWING 141A1501.

Part: ELEC CONNECTOR — LOOSE (ZONE 200) · airframe 75,736 hrs · 30,275 cycles

EMERGENCY LIGHTS ABOVE LEFT SIDE EMERGENCY EXITS INOP. FOUND CONNECTOR D12008 @ M1694 LOOSE TO TOUCH. RE-SECURED. EMERGENCY LIGHTS OP CK NML REF B737 33-51-13 (WDM).

Part: FLOOR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 75,602 hrs · 30,211 cycles

(LOG 0854354) CORROSION FLOOR PANEL 140DF AT AFT CARGO COMPARTMENT. FABRICATED FLOOR PANEL 140DF AT AFT CARGO COMPARTMENT AS PER ER/A 624640-14 REV. ORIGINAL.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 75,412 hrs · 30,124 cycles

(LOG 0854328) CRACK INDICATION FOUND ON THE INNER CORNER RADIUS AND ON THE INTERNAL SURFACE OF RADIUS AREA OF THE NO 1 LH WINDOW FRAME. COMPLIED WITH ER/A 619132-14ADTR REV A PERFORMED PERMANENT REPAIR LOC ON N1 LH WINDOW FRAME AS PER ER/A 619132-14AD.

Part: LUG — CORRODED (ZONE 300) · corrosion level 2 · airframe 75,408 hrs · 30,122 cycles

(LOG 0848130) CORROSION LOCATED ON AFT FACE OF REAR LOWER LUG OF RH HORIZONTAL STABILIZER. PERFORMED REPAIR INSTRUCTIONS ON RH HORIZONTAL STABILIZER, AS PER ER/A 623846-14 REV. ORIGINAL.

Part: LUG — CORRODED (ZONE 300) · corrosion level 2 · airframe 75,408 hrs · 30,122 cycles

(LOG 0849062) CORROSION LOCATED ON AFT FACE OF REAR LOWER LUG AT LT HORIZONTAL STABILIZER. COMPLIED WITH ER/A 623847-14 REV ORIGINAL, THIS MATCHES WITH ALL STEPS ON PRI 623847-14 REV 0, 1 AND 2, IT HAS BEEN VALIDATED.PERFORMED REPAIR INSTRUCTIONS ON HORIZONTAL STABILIZER AS PER ER/A 623847-14 REV ORIGINAL.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 75,408 hrs · 30,122 cycles

(LOG 0848122) CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS767 TO BS787 AT LEVEL RBL19 AFT CARGO COMPARTMENT. REPLACED WEB INTERCOSTAL AND FASTENERS LOC. BETWEEN BS767 TO BS787 AT LEVEL RBL19 AFT CARGO COMPARTMENT AS PER B737-800 SRM51-40-02 DWG 146A0081.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 75,408 hrs · 30,122 cycles

(LOG 0848137) CORROSION EXTERNAL SKIN AT LEVEL BS 540 BTW STR 28R TO STR 28L AT LOWER FUSELAGE. PERFORMED REPAIR INSTRUCTIONS ON EXTERNAL SKIN AT LEVEL BS 540 BTW STR 28R TO STR 28L AT LOWER FUSELAGE AS PER ER/A 623918-14AD REV ORIGINAL.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 75,408 hrs · 30,122 cycles

(LOG 0848117) BURNED EMERGENCY LIGHTS EXIT ASSY ON POSITION MID FWD RH AT PASSENGER CABIN REPLACED EMERGENCY LIGHTS EXIT ASSY ON POSITION MID FWD RH AT PASSENGER CABIN AS PER B737-800 AMM 33-51.

Part: FRAME — DENTED (ZONE 100) · airframe 75,408 hrs · 30,122 cycles

(LOG 0848120) DENT FRAME BS 420 BTW STR 25L TO STR 26L AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON FRAME BS 420 BETWEEN STR 25 L TO 26 L AS PER B737-800 SRM 53-30-07-2R.

Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 75,408 hrs · 30,122 cycles

(LOG 0847672) CRACK CARGO TRACK CRACK 13.84 AT LEVEL BS 727E AFT CARGO COMPARTMENT. PERFORMED REPAIR CARGO TRACK SECTION LOCATED RBL 13.84 BTW BS727D PLUS 13INCH TO BS727F LESS 15 INCH AS PER B737-800 SRM53-00-53-2R PROCEDURE 3 REPAIR 3, SRM 51-40-02-0G-0 AND DWG 146A7501.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 75,408 hrs · 30,122 cycles

(LOG 0846091) CRACK SUPPORT ZEE BTW BS 727E TO 727F AT LEVEL OF STR 25R AFT CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR SUPPORT ZEE LOCATED BTW BS727 TO BS767 AT LEVEL STR 25R AFT CARGO COMPARTMENT AS PER B737-800 SRM 53-00-53-2R-6, REPAIR 6.

Part: SUPPORT CHANNEL — MECHANIC ERROR (ZONE 100) · airframe 75,408 hrs · 30,122 cycles

(LOG 0846086) DRILL MARK CHANNEL SUPPORT LBL 8.10 BTW BS 727J TO BS 747 AT AFT CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON CHANNEL SUPPORT BETWEEN BS727J AND BS747 ON LBL 8.10 AT AFT CARGO COMPARTMENT AS PER B737-800 SRM 53-00-53-2R PROCEDURE 2.

Part: WEB — CRACKED (ZONE 100) · airframe 75,408 hrs · 30,122 cycles

(LOG 0842519) SECONDARY FINDING CRACK WEB - INTERCOSTAL LOC BS500G AND STR26R AT FWD CARGO COMPARTMENT. REPLACED WEB - INTERCOSTAL, LOC BS500G AND STR26R AT FWD CARGO COMPARTMENT ASPER B737-800 SRM-51-40-02 AND B737-800 SRM-51-10-02 AND DWG: 143A7505.

Part: CARGO TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 75,408 hrs · 30,122 cycles

CORRODED CARGO TRACK 13.84 BTW BS 767 TO BS 827 AFT CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTIONS LOC. RBL 13.84 BTW STA 767 PLUS 11.5 INCH AND STA 887 AFT CARGO COMPARTMENT AS PER B737-800 SRM 53-00-53-2R-3 REPAIR 3 AND DWG: 146A7500.

Part: WEB — CRACKED (ZONE 100) · airframe 75,408 hrs · 30,122 cycles

(LOG 0842492) CRACK VERTICAL WEB - INTERCOSTAL BTW BS 807 AND BS 827 AT LEVEL OF STR 25R AFT CARGO COMPARTMENT. REPLACED VERTICAL WEB INTERCOSTAL BTW BS 807 AND BS 827 AT LEVEL OF STR 25R AFT CARGO COMPARTMENT AS PER B737-800 SRM 51-40-02 AND SRM 51-10-02 AND DWG 146A8120.

Part: SKIN — DENTED (ZONE 100) · airframe 75,408 hrs · 30,122 cycles

(LOG 0842820) DURING HEAVY MAINTENANCE VISIT AT MEXICANA MRO FACILITIES (MEX), A DENT + GOUGE DAMAGE HAS BEEN FOUND ON THE FUSELAGE SKIN, BETWEEN STA 360 / STA 380 AND STRINGERS S-17L / S-18L. REPAIRED DAMAGE PER ERA 597051-14.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 75,408 hrs · 30,122 cycles

(LOG 0836305) CORROSION WEB - INTERCOSTAL BTW BS 907 TO BS 927 AND BTW STR24L TO STR 23L AFT CARGO COMPARTMENT. REPLACED WEB INTERCOSTAL AND FASTENERS BTW BS 907 TO BS 927 AND BTW STR24L TO STR 23L AFT CARGO COMPARTMENT AS PER B737-800 SRM 51-40-02, SRM 51-10-02 AND AS PER DRAWING 147A7401, REV C.

Part: PLATE — CRACKED (ZONE 200) · airframe 75,408 hrs · 30,122 cycles

(LOG 0836303) CRACK FLOOR STRUCTURE PLATE ON BS 540 BTW RBL 24.75 AND BL 0 AT PASSENGER CABIN. REPLACED INTERCOSTAL PLATE AND FASTENERS LOC. FLOOR STRUCTURE ON BS 540 BTW RBL 24.75 AND BL 0 AT PASSENGER CABIN, AS PERB737-800 SRM 51-40-02-0G AND DWG 143A0060, SHEET 107, REV A.

Part: SEAT TRACK — BROKEN (ZONE 200) · airframe 75,408 hrs · 30,122 cycles

(LOG 0836321) BROKEN SEAT TRACK LBL 45.50 AT LEVEL BS 500C AT PASSENGER CABIN. PERFORMED PERMANENT REPAIR LOCATED PASSENGER CABIN, SEAT TRACK LBL 45.50 FROM BS500B TO BS500E AS PER B737-800 SRM 53-00-52-2R,REPAIR 4.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 75,408 hrs · 30,122 cycles

(LOG 0836315) CORROSION ANGLE - SUPPORT LOCATED BS947.5 AND BETWEEN RBL21 TO LBL 8.10 AFT CARGO COMPARTMENT. REPLACED ANGLE - SUPPORT AND FASTENERS LOC. BS947.5 AND BETWEEN RBL21 TO LBL 8.10 AFT CARGO COMPARTMENT AS PER B737-800 SRM 51-40-02-0G-0 , B737-800 SRM 51-10-02 -0G PARAGRAPH 9 AND DWG-149A8110 SHEET 7 REV A, REV. AND DWG-149A8117SHEET 4 REV C.

Part: RIB — CRACKED (ZONE 300) · airframe 75,408 hrs · 30,122 cycles

(LOG 0836349) CRACK ON RIB 105.26 ACCESS PANEL 331B LEADING EDGE LH HORIZONTAL STABILIZER. REPLACED RIB 105.26 ACCESS PANEL 331B LEADING EDGE LH HORIZONTAL STABILIZER AS PER B737-800 SRM 51-40-02 AND DWG 186A1001 ,REV A.

Part: FRAME — DENTED (ZONE 100) · airframe 75,408 hrs · 30,122 cycles

(LOG 0836337) DENT ON FRAME ON BS 767 STR 24L AT AFT CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON FRAME LOCATED ON BS 767 BTW STR23L TO STR25L ASPER B737-800 SRM 53-60-07-2R-3 REPAIR 3.

Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 75,408 hrs · 30,122 cycles

(LOG 0837670) CRACK CARGO TRACK RBL 13.84 AND AT LEVEL BS 727J AFT CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON CARGO TRACK LOC RBL 13.84 BETWEEN BS 727H MORE 12 INCHES TO BS 727J AFT CARGO COMPARTMENT AS PER B737-800 SRM 53-00-53-2R REPAIR 3.

Part: RIB — CRACKED (ZONE 300) · airframe 75,408 hrs · 30,122 cycles

(LOG 0836344) CRACK ON RIB 114.55 ACCESS PANEL 331B LEADING EDGE LH HORIZONTAL STABILIZER. REPLACED RIB 114.55 ACCESS PANEL 331B LEADING EDGE LH HORIZONTAL STABILIZER AS PER B737-800 SRM 51-40-02 AND DWG 186A1001.

Part: DOUBLER — CORRODED (ZONE 100) · airframe 75,408 hrs · 30,122 cycles

AIRCRAFT 3742, DURING H CHECK AT AEM (SAL), WHILE EXECUTION OF INSPECTIONS IN THE FWD CARGO COMPARTMENT (INTERNAL, CPCP) AS PER JOB CARD 5300-2594, CORROSION WAS FOUND AFFECTING SKIN DOUBLER PN 143A3233-2, LOCATED BETWEEN BSTA520/BSTA540 AND STR28R/STR28L. CORRECTIVE ACTION: REMOVED CORROSION AND DAMAGED AREA AND INSTALLED REPAIR PARTS PER ER/A 623918-14. (LP 0833788)

Part: FRAME — CRACKED (ZONE 200) · airframe 75,408 hrs · 30,122 cycles

(LOG 0828893) CRACK FRAME BS 827 BTW STR 8R TO STR 9R AT PASSENGER CABIN. COMPLIED WITH ER/A 624011-14AD REV ORIGINAL MATCHES WITH ALL STEPS ON PRI 624011-14 REV 0 AND PRI 624011-14 REV 1, IT HAS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON FRAME BS 827 BTW STR 8R TO STR 9R AT PASSENGER CABIN AS PER ER/A 624011-14AD REV ORIGINAL.

Part: FRAME — CRACKED (ZONE 200) · airframe 75,408 hrs · 30,122 cycles

(LOG 0828867) CRACK FRAME BS 827 BTW STR 8L TO STR 9L AT PASSENGER CABIN. COMPLIED WITH ER/A 624011-14AD REV ORIGINAL MATCHES WITH ALL STEPS ON PRI 624011-14 REV 0 AND PRI 624011-14 REV 1, IT HAS BEENVALIDATED. PERFORMED REPAIR INSTRUCTIONS ON FRAME BS 827 BTW STR 8L TO STR 9L AT PASSENGER CABIN AS PER ER/A 624011-14AD REV ORIGINAL.

Part: FRAME — CRACKED (ZONE 200) · airframe 75,408 hrs · 30,122 cycles

(LOG 0828886) CRACK FRAME BS 867 BTW STR 8R TO STR 9R AT PASSENGER CABIN. COMPLIED WITH ER/A 624011-14AD REV ORIGINAL MATCHES WITH ALL STEPS ON PRI 624011-14 REV 0 AND PRI 624011-14 REV 1, IT HAS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON FRAME BS 867 BTW STR 8R TO STR 9R AT PASSENGER CABIN AS PER ER/A 624011-14AD REV ORIGINAL SECTION 1.

Part: FRAME — CRACKED (ZONE 200) · airframe 75,408 hrs · 30,122 cycles

(LOG 0828826) CRACKED FRAME BS 867 BTW STR 8L TO STR 9L AT PASSENGER CABIN. COMPLIED WITH ER/A 624011-14AD REV ORIGINAL MATCHES WITH ALL STEPS ON PRI 624011-14 REV 0 AND PRI 624011-14 REV 1, IT HAS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON FRAME BS 867 BTW STR 8L TO STR 9L AT PASSENGER CABIN AS PER ER/A 624011-14AD REV ORIGINAL SECTION 1.

Part: STANCHION — CRACKED (ZONE 100) · airframe 75,408 hrs · 30,122 cycles

(LOG 0829147) DURING INSPECTION, A CRACK WAS FOUND RUNNING HORIZONTALLY ACROSS THE VERTICAL STANCHION (C-D POST) COMMON TO WINDOW FRAMES OF THE LH (P/N 141A8811-3) AND/OR RH (P/N 141A8811-4) NO. 1 DECK WINDOWS.REPAIRED PER ERA 619132-14.

Part: KEELBEAM — CRACKED (ZONE 100) · airframe 75,408 hrs · 30,122 cycles

(LOG 0828793) CRACK ON KEEL BEAM STR 27R INTERNAL STRUCTURE BTW BS 727 TO BS 727A AT AFT CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR LOC. KEEL BEAM STR 27R INTERNAL STRUCTURE BTW BS 727 TO BS 727A AT AFT CARGO COMPARTMENT AS PER B737-800 SRM 53-60-12-2R-1.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 75,408 hrs · 30,122 cycles

(LOG 0829143) CRACK INDICATION FOUND ON THE INNER CORNER RADIUS AND ON THE INTERNAL SURFACE OF RADIUS AREA OF THE NO 1 LH WINDOW FRAME. PERFORMED PERMANENT REPAIR ON N1 LH WINDOW FRAME AS PER ER/A 619132-14ADTR.

Part: FRAME — CRACKED (ZONE 200) · airframe 75,408 hrs · 30,122 cycles

(LOG 0828755) CRACK FRAME BS 480 BTW STR 8L TO STR 9L AT PASSENGER CABIN. COMPLIED WITH ER/A 624011-14AD REV ORIGINAL MATCHES WITH ALL STEPS ON PRI 624011-14 REV 0 AND PRI 624011-14 REV 1.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 75,408 hrs · 30,122 cycles

(LOG 0825579) CORROSION WEB - INTERCOSTAL LOC. BS 500C TO BS 500D AT LEVEL STR 26R FWD CARGO COMPARTMENT. REPLACED WEB AT BS 500C TO BS 500D AT LEVEL STR 26R FWD CARGO COMPARTMENT AS PER B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG D143A7505.

Part: CARGO TRACK — CRACKED (ZOEN 100) · airframe 75,408 hrs · 30,122 cycles

(LOG 0819595) CRACK CARGO TRACK LBL 17.24 AT LEVEL BS 767 AFT CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON CARGO TRACK LOCATED ON LBL 17.24 BTW BS 747 TO BS 787 IN AFT CARGO COMPARTMENT AS PER B737-800 SRM 53-00-53-2R PARAGRAPH 4 FIGURE 203 (SHEET 1 AND 2) AND DWG# 146A7500, REV C.

Part: WEB — CRACKED (ZONE 100) · airframe 75,408 hrs · 30,122 cycles

(LOG 0819559) CRACK WEB - INTERCOSTAL LOC. BS 500G TO BS 500H AT LEVEL STR 26L FWD CARGO COMPARTMENT. REPLACED WEB AT BS 500G TO BS 500H AT LEVEL STR 26L FWD CARGO COMPARTMENT AS PER B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 143A7505 REV R.

Part: STRINGER — CRACKED (ZONE 200) · airframe 75,408 hrs · 30,122 cycles

(LOG 0819530) CRACKED STRINGER 14L LOCATED BTW BS 294.5 AND BS 303.9 AT PASSENGER CABIN. PERFORMED PERMANENT REPAIR AT STRINGER 14L LOCATED BTW BS 294.5 AND BS 303.9 AT PASSENGER CABIN,REPAIR IS CATEGORY A, AS PER B737-800 SRM 51-40-02, AS PER B737-800 SRM 53-00-03-2R PROCEDURE 1, REPAIR 1.

Part: ANGLE — CRACKED (ZONE 100) · airframe 75,408 hrs · 30,122 cycles

(LOG 0819544) CRACK ANGLE - CLIP LOC. BS 500H FWD AREA AND AT LEVEL STR 26L FWD CARGO COMPARTMENT. REPLACED ANGLE - CLIP AT BS 500H AT LEVEL STR 26L FWD AREA AS PER B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 143A7505 REV A.

Part: ANGLE — CRACKED (ZONE 100) · airframe 75,408 hrs · 30,122 cycles

(LOG 0813228) CRACK ANGLE - CLIP LOC. BS 500H FWD AREA AND LEVEL STR 26R FWD CARGO COMPARTMENT. REPLACED ANGLE CLIP LOC. BS 500H FWD AREA AND LEVEL STR 26R FWD CARGO COMPARTMENT AS PER AS PER B737-800 SRM 51-40-02 AND AND B737-800 SRM-51-10-02 AND DWG: 143A7505.

Part: ANGLE — CRACKED (ZONE 100) · airframe 75,408 hrs · 30,122 cycles

(LOG 0813224) CRACK ANGLE - CLIP LOC. BS 500G FWD AREA AND STR 26R FWD CARGO COMPARTMENT. REPLACED ANGLE CLIP LOC. BS 500G FWD AREA AND STR 26R FWD CARGO COMPARTMENT AS PER B737-800 SRM 51-40-02 AND B737-800 SRM-51-10-02 PARAGRAPH 9, AND DWG: 143A7505.

Part: SHIELD — DAMAGED (ZONE 100) · airframe 75,408 hrs · 30,122 cycles

(LOG 0809589) ELONGATED HOLES ON SHIELD FLOOR STRUCTURE BTW BS 767 TO BS 794 AT LEV EL STR 25R AT AFT CARGO COMPARTMENT. REPLACED SHIELD FLOOR AND FASTENERS LOC AFT CARGO BTW BS 767 TO BS 794 AT LEVEL STG 25R AFT CARGO COMPARTMENT AS PER B737-800 SRM 51-40-02 AND AS PER B737-800 DRAWING -146A0081.

Part: ANGLE — CRACKED (ZONE 100) · airframe 75,408 hrs · 30,122 cycles

(LOG 0803528) CRACK BILGE AREA ANGLE CLIP ON BS 400 AT LEVEL STR 26R AT FWD CARGO COMPARTMENT. REPLACED CLIP AND FASTENERS LOCATED ON BS 400 AT LEVEL STR26R AT FWD CARGO COMPARTMENT AS PER B737-800 SRM 51-40-02 DWG 143A7505 SHEET 2.

Part: SKIN — CRACKED (ZONE 300) · airframe 75,408 hrs · 30,122 cycles

(LOG 0802129) CRACK EXTERNAL SKIN LOC LOWER SURFACE ON RIB 101.9 AND 19 INCHES FWD OF REAR SPAR AT RT HORIZONTAL STABILIZER. PERFORMED REPAIR CAT B ON RH HORIZONTAL STABILIZER LOWER SKIN LOC AT STA 101.9, 19 INCHES FWD OF REAR SPAR AS PER B737-800 SRM55-10-01-2R-11 REPAIR 11.

Part: BATTERY PACK — INOPERATIVE (ROW 19 & ROW 22) · airframe 75,095 hrs · 29,982 cycles

(LOG 6470452) DURING SVC CK, FOUND EEPLS LILGHTS BETWEEN ROW 19 AND ROW 22 INOP. R+R'D BATTERY PACK PER AMM 33-51. OP CHECKS GOOD.

Part: SIGN — DAMAGED (MID CABIN) · airframe 73,838 hrs · 29,438 cycles

(LOG 4757020) FOUND ON ARRIVAL EXIT SIGN DAMAGED. REMOVE AND REPLACE MID AISLE EXIT SIGN PER B737 AMM 33-511.

Part: TIRE — FAILED (NLG) · airframe 73,311 hrs · 29,210 cycles

SHIP 3742 -TIRE- RIGHT NLG TIRE TREAD SEPARATION ON TAKEOFF IAD. CORRECTIVE ACTION: REPLACED LT-RT NLG TIRES, E/E DOOR, LOWER TCAS ANTENNA AND FORWARD FUSELAGE DRAIN. PERFORMED LT-RT ENGINE BORESCOPES. AIRCRAFT RETURNED TO SERVICE.

Part: TIRE — FAILED (MLG) · airframe 73,318 hrs · 29,212 cycles

(LOG 5857551) FOUND 3 DENTS ON E/E DOOR FROM TIRE FAILURE. R/R E/E DOOR IAW B737 AMM 52-48. OPS CHECK NORMAL.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 72,200 hrs · 28,722 cycles

(LOG 0098446) COMPLY WITH PRI/ER/A 614152-14 LIGHTNING STRIKE REPAIR @ STA: 370 STR: 15L. C/W PRI 614152-14 REV. 3 (984172) (QC5290) C/W ER/A 614152-14 REV. ORIG SECTION I PERMANENT REPAIR.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 72,209 hrs · 28,726 cycles

(LOG 0098345) WHILE OVERNIGHT IN ATL, MTC ATTEMPTED TO REPAIR A DEFERRED LIGHTNING STRIKE DAMAGE TO THE FUSELAGE SKIN. THE DAMAGE IS LOCATED AT STA 370 AND STR 15L. DAMAGE REPAIRED PER ERA 614152-14.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 72,110 hrs · 28,671 cycles

(LOG 4342132) EMERGENCY FLOOD LIGHT ROW 13 DEF INOP. R/R CONNECTOR IAW B737 SWPM 20-61-12. OP CHK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,320 hrs · 28,311 cycles

(LOG 4892912) ON PREFLIGHT IN ANU FOUND ACCESS DOOR FOR HP EXTERNAL AIR MISSING. REMOVED HINGE REMNANTS REF B737 AMM 52-48(373750) PER ERA 611269-14 REV ORIG. C/W PERM. INST NEW ECS HIGH PRESSURE DOOR REF B737 AMM 52-48.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,521 hrs · 27,486 cycles

DURING INSPECTION FOUND EMER LIGHT INOP AT SEAT 28D. R/R EMER LIGHT AT SEAT 28D PER B737 AMM 33-51-11. OPS CH OK.

Part: BATTERY PACK — INOPERATIVE · airframe 68,254 hrs · 26,885 cycles

(LOG 9001907) DURING INSPECTION FOUND EMERGENCY LIGHT INOP AT OVER WING EXIT DOOR. REMOVED & REPLACED LEFT EMERGENCY EXIT BATTERY PACK IAW B737 AMM 33-51. OPS CHECK OK.

Part: NONE — NONE · airframe 67,028 hrs · 26,323 cycles

(LOG 2112864) DURING INSPECTION FOUND LH FWD FUSELAGE BETWEEN STA 360 AND STA 380 AND BETWEEN S-17L AND S-18L FUSELAGE DENTED. MAINTNENACE REPAIRED DENT PER ERA 597051-14.

Part: LIGHT — DAMAGED · airframe 66,767 hrs · 26,196 cycles

(LOG 8244810) DURING INSPECTION FOUND EMERGENCY LIGHT ON OUTSIDE OF LAV 204 MISSING LENS COVER. FOUND BASE OF LT IN POOR COND. R/R LIGHT ASSY PER B737 AMM 33-52. LIGHT CHKS GOOD.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 64,742 hrs · 25,259 cycles

(LOG 7535255) DURING INSPECTION FOUND RH AFT OVERWING EXIT LIGHT AND EXTERIOR EMERGENCY LIGHT RH AFT OF FLAP LIGHT WILL NOT ILLUMINATE. REPLACED FUSES ON EMERGENCY LIHT ASSY ROW 23F BOTH EXTERIOR EMERGENCY LIGHT OPS CHECK GOOD. REF B737 AMM 33-51.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,290 hrs · 24,496 cycles

(LOG 1519376) DURING INSPECTION FOUND EXTERNAL SKIN DAMAGED BELOW LOWER HINGE OV ELECTRICAL GROUND POWER DOOR. MAINTENANCE REPAIRED DAMAGE PER B737 SRM 53-10-15-2R REPAIR 5 AND ERA 585833-14.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,276 hrs · 24,490 cycles

(LOG 1514743) WHILE MTC WAS TRYING REPAIR EXTERNAL GROUND POWER DOOR PER B737-800 SRM 53-10-15-2R-5, MTC FOUND A DAMAGED FASTENER HOLE. WHILE ATTEMPTING TO LAYOUT THE REPAIR FASTENER PATTERN, MTC MISLOCATED AND DRILLED TWO (2) ADDED PILOT HOLES (0.125 DIA.) COMMON TO THE UPPER SKIN PANEL. MAINTENANCE REPAIRED DAMAGE PER ERA 585833-14.

Part: CONTROL MODULE — FAULTY (FIRE WARNING) · airframe 60,067 hrs · 23,158 cycles

(LOG 5270275) ON LANDING FIRE WARNING AND MASTER CAUTION CAME ON WITH BELL. NO FIRE HANDLE CARGO FIRE LIGHT . DEACTIVATED BELL WITH C/B AS BELL CAUTION DID NOT WORK. MAINTENANCE REMOVED AND REPLACED FIRE CTL MODULE IAW AMM 26-10-01. OPS NML.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 59,909 hrs · 23,097 cycles

DURING HCK AT QRO, CORROSION WAS FOUND AFFECTING THE AUX SILL CHORD-OUTER FLANGE AT BS 351 & PROJECTION OF S-23L. MAINTENANCE REPAIRED DAMAGE PER ERA 574933-14.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,919 hrs · 23,101 cycles

DURING INSPECTION FOUND CORROSION WAS FOUND ON CHORD-OUTER (E&E). AREA WAS REPAIRED PER: ERA 574933-14 REV ORIG AND ETI-37-19-303 REV 3.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 59,909 hrs · 23,097 cycles

DURING INSPECTION FOUND CRACK ON DOOR JAMB R1 FWD LOWER CORNER. CRACK ON DOOR JAMB R1 FWD LOWER CORNER WAS REPAIRED PER ERA 574840-14 REV ORIGINAL AND ETI-37-19-300 REV ORIGINAL AND ETI-37-19-302 REV 2 AND ER/A 574940-14 REV ORIGINAL.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 59,909 hrs · 23,097 cycles

DURING HCK AT QRO, A CRACK WAS FOUND AFFECTING THE FWD GALLEY DOOR SURROUND STRUCTURE LOWER SILL WEB 141A8311-2 AT BS 296 AND RBL 60. MAINTENANCE REPAIRED DAMAGE PER ERA 574940-14.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 59,909 hrs · 23,097 cycles

DURING INSPECTION FOUND CORROSION ON RAIL RBL 13.84 BTW STATION 727 TO 847 AT AFT CARGO COMPARTMENT FLOOR STRUCTURE. AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPLACED PER SRM 51-40-02 PAR 7 AND DWG 146A7501 REV C.

Part: SHIELD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,909 hrs · 23,097 cycles

DURING INSPECTION FOUND CORROSION ON SHIELD AT FLOOR STRUCTURE AT FWD CARGO COMPARTMENT BTW STA 500A-490 AND STR 25R. SHIELD AT FLOOR STRUCTURE WAS REPLACED PER SRM 51-40-02 PAR 7 AND DWG 143A8126-30 REV B.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 59,909 hrs · 23,097 cycles

DURING INSPECTION FOUND CRACKED RIB ON LT LE STA LES=133.15 AT LT HORIZONTAL STABILIZER. RIB ON LT LE STA LES=133.15 AT LT HORIZONTAL STABILIZER WAS REPAIRED PER ER/A 574803-14 REV ORIG AND ETI-37-19-301 REV ORIG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 59,909 hrs · 23,097 cycles

DURING INSPECTION FOUND CRACKED FLOOR SUPPORT ON STA Y=540 AND RBL 2 WING BOX AREA. FLOOR SUPPORT WAS REPLACED PER SRM 51-40-02.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 59,909 hrs · 23,097 cycles

DURING INSPECTION FOUND CRACK ON FWD FACE OF VAPOR STA Y=663 RBL 39 AT RT WHEEL WELL. CRACK ON FWD FACE OF VAPOR WAS REPAIRED PER SRM 57-10-10 REPAIR 2.

Part: BULKHEAD WEB — CRACKED (LT MLG WW) · airframe 59,909 hrs · 23,097 cycles

DURING INSPECTION FOUND CRACKED LOWER LT WEB STA 663, ON FWD BULKHEAD, BTW LBL 54.21 AND LBL 40.00, IN LT MLG WHEEL WELL. CRACKED LOWER LT WEB ON FWD BULKHEAD WAS REPAIRED PER SRM 57-10-10 REPAIR 2.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,909 hrs · 23,097 cycles

DURING INSPECTION FOUND CORROSION ON INTERCOSTAL STA 500I -500H AND STR 25R, STA 500I-500H AND STR 25L, STA 500F-500G STR 25R AT FWD CARGO COMPARTMENT. INTERCOSTAL OUTSIDE LIMITS WAS REPLACED PER SRM 51-40-02 PAR 4 AND DWG 143A7510 REV B.

Part: SKIN — WORN (WING) · airframe 59,909 hrs · 23,097 cycles

DURING INSPECTION FOUND WEAR ON LOWER SKIN AT SLAT 5 WEDGE AREA. WEAR AREA REPAIRED PER SRM 51-70-10 REPAIR 4.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,909 hrs · 23,097 cycles

DURING INSPECTION FOUND CORROSION ON INTERCOSTAL STATION 787 TO STATION 793 AT AFT CARGO COMPARTMENT. INTERCOSTAL STA= 787 TO STA= 793 AT AFT CARGO COMPARTMENT WAS REPLACED PER 146A8123 REV F AND SRM 51-40-02 PAR 7 AND SRM 51-40-02.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,909 hrs · 23,097 cycles

DURING INSPECTION FOUND CORROSION ON RT STRAP IN THE SETTLEMENT AREA OF SCUFF PLATE LOWER AND UPPER BETWEEN STA 787 TO 805. STRAP STATION 787 TO 805 WAS REPLACED PER DWG 146A8128 REV C AND SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,909 hrs · 23,097 cycles

DURING INSPECTION FOUND CRACK ON FRAME FROM STATION 400 BTW S8R TO S9R. MAINTENANCE REPAIRED CRACK PER ERA 574641-14AD REV ORIGINAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,909 hrs · 23,097 cycles

DURING INSPECTION FOUND CRACK ON FRAME FROM STATION 727B BTW S8L TO S9L. FRAME FROM STATION 727B BTW S8L TO S9L WAS REPAIRED PER ER/A 574641-14AD REV ORIGINAL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,909 hrs · 23,097 cycles

(LOG 0917649) DURING INSPECTION FOUND CRACK ON INTERCOSTAL (3 EAS)BTW STA 500G-500H S-25L, 500H-500G S-25R, 500A-500B S-25L AT FWD CARGO COMPARTMENT. INTERCOSTAL BTW STA 500G-500H S-25L, 500H-500G S-25R, 500A-500B S-25L AT FWD CARGO COMPARTMENT WERE REPLACED PER SRM 51-40-02 PAR. 4 E AND DWG 143A7510 REV.J.

Part: WEB — CRACKED (MLG WW) · airframe 59,909 hrs · 23,097 cycles

(LOG 0915555) DURING INSPECTION FOUND CRACK ON UPPER WEB AT WHEEL WELL LT SIDE. UPPER WEB AT WHEEL WELL LT SIDE WAS REPAIRED PER SRM 57-10-10 REPAIR 3.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 59,909 hrs · 23,097 cycles

(LOG 0914456) DURING INSPECTION FOUND CRACKED RIB AT FRONT SPAR LE STA. LES= 95.96 AT RT HORIZONTAL STABILIZER. RIB AT FRONT SPAR LE STA. LES= 95.96 AT RT HORIZONTAL STABILIZER WAS REPAIRED PER SRM 55-10-09 REPAIR 5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,909 hrs · 23,097 cycles

(LOG 0905638) DURING INSPECTION FOUND CORROSION ON FLOOR STRUCTURE BTW STATION 947 TO STATION 967, RBL 496. DAMAGED FLOOR SUPPORT BTW STA 947 TO STA 967 WAS REPLACED PER SRM 51-40-02.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 59,630 hrs · 22,997 cycles

(LOG 0846850) DURING INSPECTION FOUND EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. REPLACED LENSES AS REQ'D. OPS NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,741 hrs · 22,265 cycles

DURING INSPECTION, FOUND THE L4 EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE L4 DOOR EMERGENCY LIGHT IAW AMM 33-51. OPS CHECKED GOOD.

Part: SLIDE — DEFECTIVE (L2 DOOR) · airframe 56,412 hrs · 21,799 cycles

DOOR 2L HAS APPROXIMATELY ONE FOOT OF SLIDE MATERIAL SHOWING. REMOVED AND REPLACED DOOR L2 SLIDE IAW WORKCARD 2560-4426 TRANSFERRED GIRT BAR AND LATCH FROM OLD SLIDE ASSY. ALL RII C/W IAW CARD 2560-4426.

Part: SLIDE — NO TEST (L2 DOOR) · airframe 56,270 hrs · 21,752 cycles

L2 DOOR ESCAPE SLIDE FAILED TO INFLATE DURING AN OPS CHECK. MAINTENANCE REPLACED THE DOOR SLIDE IAW 2560-4426. OK FOR SERVICE.

Part: TERMINAL BLOCK — SMOKE (WINDOW) · airframe 55,828 hrs · 21,601 cycles

DURING FLIGHT, CREW REPORTED SMOKE FROM THE L2 WINDOW TERMINAL BLOCK DURING FLIGHT. THE CREW TURNED OFF WINDOW HEAT AND THE SMOKE DISSIPATED. MAINTENANCE REMOVED AND REPLACED L2 WINDOW PER AMM 56-12.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 55,421 hrs · 21,447 cycles

DURING INSPECTION, FOUND THE LEFT HORIZONAL STAB LOWER SKIN CRACKED AT HSS 129.5. MAINTENANCE REPAIRED THE SKIN IAW SRM 55-10-01, REPAIR 11.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 55,421 hrs · 21,447 cycles

DURING INSPECTION, FOUND THE LEFT HORIZONTAL STAB LOWER SKIN CRACKED AT HSS 129.5. MAINTENANCE REPAIRED THE SKIN IAW SRM 55-10-01, REPAIR 11.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,192 hrs · 21,014 cycles

DURING INSPECTION, FOUND THE RT AFT OVERWING EXIT LIGHT INOPERATIVE. MAINTENANCE R & R THE POWER SUPPLY M1671 IAW AMM 33-51. OPS CHECKED GOOD.

Part: SEAT TRACK — GOUGED (BS 520) · airframe 47,640 hrs · 18,809 cycles

DURING INSPECTION FOUND PASSENGER CABIN SEAT TRACK CROWN IS GOUGED AT BS 520, RBL 24. MAINTENANCE R & R SEAT TRACK IAW SRM 53-00-52, REPAIR 4.

Part: SEAT TRACK — GOUGED (BS 520) · airframe 47,640 hrs · 18,809 cycles

DURING INSPECTION, FOUND CABIN SEAT TRACK CROWN IS GOUGED AT BS 520, RBL 45. MAINTENANCE R & R THE SEAT TRACK IAW SRM 53-00-52, REPAIR 4.

Part: SEAT TRACK — GOUGED (BS 520) · airframe 47,640 hrs · 18,809 cycles

DURING INSPECTION, FOUND THE CABIN SEAT TRACK CROWN IS GOUGED AT BS 520, RBL 45. MAINTENANCE R & R THE SEAT TRACK IAW SRM 53-00-52, REPAIR 4.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,457 hrs · 18,752 cycles

DURING INSPECTION FOUND EMERGENCY LIGHTS INOPERATIVE FROM ROW 19DEF THRU DEF. MAINTENANCE REPLACED BATTERY CHARGER AT M01671 IAW AMM 33-51. OPS CHECK NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,040 hrs · 18,278 cycles

DURING INSPECTION FOUND EMERGENCY LIGHTS INOPERATIVE AT ROWS 19-22DEF. MAINTENANCE R & R BATTERY PACK AND CHARGER. OPS CHECKED NORMAL IAW AMM 33-51.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,040 hrs · 18,278 cycles

DURING INSPECTION FOUND EMERGENCY LIGHT ROWS 23-33 DEF INOPERATIVE. MAINTENANCE R & R BATTERY PACK IAW AMM 33-51. OPS CHECKED NORMAL.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 45,772 hrs · 18,178 cycles

DURING INSPECTION FOUND EMERGENCY LIGHT ROWS 23D-33D INOPERATIVE. MAINTENANCE REPLACED FUSES ON BATTERY CHARGER M1672. OPS CHECKED OK.

Part: FRAME — CRACKED (BS 500C) · airframe 38,901 hrs · 15,706 cycles

CABIN SIDEWALL FRAME CRACKED COMMON TO PSU RAIL SUPPORT AT STATION 500C S8R. REPAIRED IAW 509154-14AD.

Part: FRAME — CRACKED (BS 440) · airframe 38,901 hrs · 15,706 cycles

CABIN SIDEWALL FRAME CRACKED COMMON TO PSU RAIL SUPPORT CLIP AT BS 440 S8R. REPAIRED IAW ERA 509154-14AD.

Part: FRAME — CRACKED (BS 480) · airframe 38,901 hrs · 15,706 cycles

FRAME COMMON TO PSU RAIL SUPPORT CRACKED AT STA 480 S8R. REPAIRED IAW ERA 509154-14AD.

Part: FRAME — CRACKED (BS 500A) · airframe 38,901 hrs · 15,706 cycles

CABIN SIDEWALL FRAME CRACKED COMMON TO PSU RAIL SUPPORT CLIP AT STA 500A S8R. REPAIRED IAW ERA 509154-14AD.

Part: FRAME — CRACKED (BS 440) · airframe 38,901 hrs · 15,706 cycles

CABIN SIDEWALL FRAME CRACKED AT PSU SUPPORT CLIP, STA 440 S8L. REPAIRED IAW ERA 509154-14AD.

Part: FRAME — CRACKED (BS 727B) · airframe 35,598 hrs · 14,461 cycles

SIDEWALL FRAME CRACKED COMMON TO PSU RAIL SUPPORT ANGLE AT STA 727B S8R. REPAIRED IAW ERA 509154-14AD.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,239 hrs · 15,456 cycles

DURING INSPECTION, FOUND EMERGENCY LIGHTS AT OVER WING EXIT ON LT SIDE INOPERATIVE. MX REPLACED POWER SUPPLY FUSES. OPS CHECKED OK.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 37,917 hrs · 15,340 cycles

DURING TEST, ALL EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST. MX R & R BATTERY PACKS AND TESTED OK IAW AMM 33-51-09/201.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,203 hrs · 12,313 cycles

DURING LAYOVER CHECK, MX FOUND EMERGENCY PATH LIGHT AT 20DEF INOPERATIVE. MX REPLACED THE LIGHT HARNESS. OPS CHECK WAS GOOD. (DL738101663)

Part: PNEUMATIC SYSTEM — CONTAMINATED (A/C BAY) · airframe 13,286 hrs · 5,868 cycles

ABORTED T/O FOR SMOKE IN COCKPIT AND CABIN. PERFORMED OIL CONTAMINATION REMOVAL FROM AIR COND AND PNUEM SYS. NO SMELL OF CONTAMINATION NOTED. RAN PACKS AND ENGS TO T/O. NO SMOKE NOTED.