N824SY

Part: PLACARD — TORN (ZONE 200) · airframe 53,323 hrs · 30,547 cycles

PUSH PLACARD AT F/O SIDE EMERGENCY EXIT IS TEARING. R & R PUSH PLACARD IAW AMM 11-23-01.

Part: BALLAST — FAILED (ZONE 200) · airframe 52,895 hrs · 30,331 cycles

LEFT WING #1 EMERGENCY EXIT LIGHT FAILED REPLACED BALLAST ASSY OPS OK USING REF AMM 25-21-20 AND REF AMM 33-21-00

Part: LIGHT — UNSECURE (ZONE 200) · airframe 52,899 hrs · 30,329 cycles

ROW 12 ABC, EMERGENCY PATH LIGHTING IS BUCKLEING ADHEARED EMERGENCY PATH LIGHTING STRIP TO FLOOR REF AMM 33-51-15 OPS CHECK GOOD

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 52,872 hrs · 30,323 cycles

NO SMOKING/FASTENED SEATBELT LIGHTS INOP AT SEATS 2ABC,8ABC,12ABC,16ABC,23ABC,23DEF, AND 27DEF. RELAMPED NO SMOKING/FASTEN SEAT BELT LIGHT REF. MM 33-25-00. OPS CHECKS GOOD. OK FOR SERVICE.

Part: SKIN — DENTED (ZONE 200) · airframe 52,509 hrs · 30,167 cycles

FOUND DENT BETWEEN STA. 1006 AND 1013 BETWEEN STRINGERS 13L AND 14L DEPTH .160". DENT IS OUT OF LIMITS PER SRM 53-00-01 TABLE 2. NO CRACKS NOTED IN PAINT. REPAIRED DAMAGED FUSELAGE SKIN @ STA 1006 TO 1013, STR 13L TO 14L PER ER 25-02325 REV P1 AND ENG-53SCA-11709 REV. 00.

Part: STRINGER — DENTED (ZONE 200) · airframe 52,509 hrs · 30,167 cycles

WORK ORDER 96686, NR00009: MCI EMP#56711 - DENT FOUND ON STR 13L AT STA 1006+4 - RESOLUTION: MCI EMP# 57309R - REMOVED AND REPLACED STR 13L BS990-1016 WITH REPLACEMENT ITEM#HFAB53-STR-010, PO#10443621, IAW B737 SRM 51-40-02-0G

Part: SKIN — DENTED (ZONE 200) · airframe 52,509 hrs · 30,167 cycles

FOUND DENT BETWEEN STA. 1006 AND 1013 BETWEEN STRINGERS 12L AND 13L. DENT IS OUT OF LIMITS PER SRM 53-00-01 TABLE 2 NO CRACKS NOTED IN PAINT. REPAIRED DAMAGED FUSELAGE SKIN @STA 1006-1013 STR 12L TO 13L PER ER 25-02325 REV. P1 AND ENG-53SCA-11709 REV 00.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 52,508 hrs · 30,166 cycles

INOPERATIVE EMERGENCY EXIT LIGHT ON FWD RIGHT OVERWING EMERGENCY EXIT DOOR. REMOVED AND REPLACED LAMP IAW AMM 33-51-01. OPS CHECK GOOD.

Part: LIGHT — UNSECURE (ZONE 200) · airframe 52,337 hrs · 30,102 cycles

ROW 12 LEFT SIDE ISLE PATH LIGHT STRIP IS LOSE AND CAUSING A TRIPPING HAZARD - RESOLUTION: ROW 12 PATH STRIP SECURED REF AMM 25-27-00 OK FOR SERVICE

Part: BULB — INOPERATIVE (ZONE 200) · airframe 37,774 hrs · 12,956 cycles

L/H AFT EMERGENCY EXIT LIGHT INOP. R&R AFT L/H EMERGENCY EXTERIOR LIGHT BULB IAW AMM 33-51-04

Part: ENGINE — BIRD INGESTION (NR 2) · airframe 52,282 hrs · 30,079 cycles

DEFECT 809058: BRID STRIKE DURING CLIMB. LOUD BANG, YAW, FLIGHT ATTENDANTS REPORTED MOMENTARY BURNING SMELL IN CABIN. - RESOLUTION: PERFORMED BIRD STRIKE INSPECTION OF A/C IAW AMM 05-51-18, LOCATED STRIKE INSIDE #2 ENG INLET. INSPECTED #2 ENG INLET IAW AMM 71-00-00 NO DAMAGED FOUND IN OR AND ENG CLEANED/ REMOVED DEBRIS IAW AMM 72-00-00. OK FOR SERIVE

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 52,007 hrs · 29,975 cycles

15DEF EMERGENCY EXIT WINDOW LIGHT INOP - RESOLUTION: RELAMPED 15DEF WINDOW LIGHT IAW AMM 33-21-00. OPS CHECK GOOD

Part: OVEN — DIRTY (ZONE 900) · airframe 51,987 hrs · 29,986 cycles

AFT OVEN INSERT NEEDS TO BE CLEANED. SMOKES EXCESSIVELY WHEN USED - RESOLUTION: CLEANERS NOTIFIED

Part: BATTERY PACK — FAULTED (ZONE 200) · airframe 51,281 hrs · 29,673 cycles

DURING EMERGENCY BATTERY PACK OPS CHECK, R/H EMER DOOR AREA LIGHT IS GONE BEFORE 15MINUTES. R&R EMERGENCY BATTERY PACK FOR R/H EMER DOOR LIGHT REF AMM 33-51-06 OPS CHECK GOOD.

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 51,195 hrs · 29,641 cycles

DEFECT 755519: BOTH FWD GIRT BARS ARE TIGHT AND DIFFICULT TO ENGGE AND DISENGAUGE . RESOLUTION: ADJ CLAMPS ON BOTH L1 & R1 GIRT BARS. OPS CK NORMAL AT THIS TIME. REF: AMM 25-66-00.

Part: RETAINER — TIGHT (ZONE 800) · airframe 51,096 hrs · 2,965 cycles

DEFECT 755502: 1R GIRT BAR BRACKET ON RIHT SIDE IS TOO TIGHT. RESOLUTION: ADJUSTED GIRT BAR FLAP NOW CKS OK REF AMM 25-66-00

Part: LIGHT — UNSECURE (ZONE 200) · airframe 51,083 hrs · 29,601 cycles

DEFECT 798999: EMERGENCY EXIT LIGHT FLOOR STRIP LOOSE. RESOLUTION: SECURED STRIP REF AMM 25-27-00.

Part: SAFETY PIN — MISSING (ESCAPE SLIDE) · airframe 50,581 hrs · 29,413 cycles

WORK ORDER 80463 NR00010: INITIAL INSPECTION: MISSING SAFETY PIN OF ESCAPE SLIDE PACK OF R1 DOOR.

Part: BATTERY — DISCHARGED (ZONE 200) · airframe 50,553 hrs · 29,397 cycles

THREE EMERGENCY LIGHTS INOP IN CABIN UNDER BAG BINS FWD OF RT. LAV. CHARGED UP EMERGENCY POWER SUPPLY BATTERY PACKS. PERFORMED BATTERY PACK CAPACITY TEST. PASSED CAPACITY TEST OF 15 MINUTES. ALL LIGHTS WORK. REPLACED BAD EMERGENCY LIGHT BULB AT ROW 11. REF AMM 33-51-06.

Part: TRUNNION — CORRODED (ZONE 100) · airframe 50,545 hrs · 29,394 cycles

WORK ORDER FS240109: RT MLG FWD TRUNNION HOUSING FITTING HAS CORROSION ON OB FACE 3 LOCATIONS. - - RESOLUTION: REPAIRED RH MLG FORWARD TRUNNION SUPPORT FITTING IAW B737-NG-800-SRM-57-20-90-2R-2

Part: TRUNNION — CORRODED (ZONE 100) · airframe 50,545 hrs · 29,394 cycles

WORK ORDER FS240109: LT MLG FWD TRUNNION HOUSING FITTING HAS CORROSION ON OB FACE 4 LOCATIONS. - - RESOLUTION: REPAIRED LH MLG FORWARD TRUNNION SUPPORT FITTING IAW B737-NG-800-SRM-57-20-90-2R-2

Part: APU — SHUTDOWN · airframe 50,357 hrs · 29,314 cycles

APU SHUTDOWN AT FL39000. DIVERSION TO OMA. APU LOW PRESSURE LIGHT ILLUMINATED. PERFORMED FIM 49-65 TASK 801. NO CURRENT FAULTS NOTED. OKAY FOR SERVICE.

Part: SLIDE — MISRIGGED (L1 DOOR) · airframe 49,677 hrs · 29,051 cycles

1L DOOR RIGHT BRACKET TOO TIGHT AND HARD TO DISARM. REPACKED DOOR SLIDE IN REF TO AMM 25-66-01. OPS CHECK GOOD.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 49,462 hrs · 28,958 cycles

UPPER POST CRACK BETWEEN WIND 1R AND 2R WAS FOUND CRACKED ON A WINDOW CHANGE. PERMANENT REPAIR INSTALLED REF 737-53-1336-01-GRP3CFG1&2-RH. WORK COMPLETED ON W/O 85892 AND ATS JOB 728977.

Part: WINDOW — ARCED (R1) · airframe 49,430 hrs · 28,946 cycles

R1 WINDOW HAS DELAM AND SHOWS SIGNS OF ARCING ON TOP AT BOTH CORNERS. REMOVED R1 WINDOW REF AMM 56-11-11, INSTALLED R1 WINDOW UP TO STEP 8, SUBTASK 56-11-11-420-028. CONT. WITH R1 WINDOW INSTALL PER AMM 56-11-11-420-028. GLAIR SHIELD AND DU'S INSTALLED. WINDOW IS SEALED WAITING CURE TIME. VARIFIED THAT WINDOW TAP BOARD.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 49,430 hrs · 28,946 cycles

POST WAS FOUND CRACKED ON A WINDOW CHANGE. PERMEANT REPAIR INSTALLED REF 737-53-1336-01-GRP3CFG1&2-RH. WOK COMPLETED ON W/O 85892 AND ATS JOB 728977

Part: HOOK — LOOSE (GIRT BAR) · airframe 49,320 hrs · 28,907 cycles

DEFECT 761468 - CLIP THAT HOLDS 1R GIRT BAR IS LOOSE. ADJUSTED CLIP ON 1R GIRT BAR IAW AMM 25-66-00

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 49,312 hrs · 28,904 cycles

DEFECT 761468: - CLIP THAT HOLDS 1R GIRT BAR IS LOOSE - RESOLUTION: ADJUSTED CLIP ON 1R GIRT BAR IAW AMM 25-66-00.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,771 hrs · 28,588 cycles

DEFECT 7638788: - 1L GIRT BAR DIFFICULT TO ARM.. - RESOLUTION: PEFOREMD OPS TEST OF L1 GIRT BAR. REF AMM 25-66-00-710-801 NO DEFECTS NOTED ATH THIS TIME.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,306 hrs · 28,368 cycles

DEFECT 758718: ORANGE GLOW ON HEAT ELEMENT LI WINDOW. - - - RESOLUTION: OPS CHECK GOOD REF AMM 30-41-00. COULD NOT DUPLICATE DEFECT. L1 WINDOW HEAT SYSTEM IS GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,927 hrs · 28,157 cycles

DEFECT 702276: DURING COCKPIT PREFLIGHT FOUND LEFT PACK AMBER LIGHT ILLUMINATED. PACK LIGHT WOULD NOT EXTINGUISH UNDER MEL 21-32. FOLLOWING TAKEOFF AND CLIMB TO 7000' AND AFTER COMPLETING THE LEFT PACK INOP SUPPLEMENTARY AND MEL PROCEDURE, THE RIGHT BLEED TRIP LIGHT ILLUMINATED. DECLARED EMERGENCY. 702277: AIR RETURN TO MSP OVERWEIGHT LANDING NORMAL TOUCH DOWN & ROLLOUT NO ISSUES NOTED- - - RESOLUTION: R&R'D LEFT TEMP CONTROL VALVE ALONG WITH SENSE LINE OFF THE ACM PER AMM 21-51-10 LEAK CHECK AND OPS CHECK GOOD. THIS CLEARS MEL 21-1-1-A. PERFORMED OVERWEIGHT LANDING INSPECTION IAW AMM 05-51-35 NO DAMAGE FOUND. OK FOR SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,476 hrs · 27,966 cycles

DEFECT 706725: EXCESS MATERIAL FALLING OUT OF SLIDE ON DOOR L1. - - - RESOLUTION: REPOSITIONED L1 SLIDE IN BUSSEL REF AMM 25-66-01 OK FOR SERVICE

Part: UNKNOWN — UNKNOWN · airframe 47,128 hrs · 27,843 cycles

DEFECT W/O 76340 NR00012: L1 DOOR SLIDE GIRT BAR RETAINING CLIP LOOSE ON AFT SIDE. RESOLUTION: REMOVED L1 SLIDE REF AMM 25-66-01. REMOVED AND REPLACED RETAINING CLIP FASTENERS REF SRM 51-40-02. INSTALLED L1 DOOR SLIDE IAW AMM 25-66-01 ACCOMPLISHED RII OF DOOR SLIDE INSTALLATION.

Part: INTERCOSTAL — DAMAGED (BS 827-847 S25L) · airframe 47,021 hrs · 27,802 cycles

DEFECT JC 8022558 NR 00352: FOUND Z CHANNEL BAFFLE (INTERCOSTAL) FROM FR 827-847 STRG 25L TO HAVE NUT PLATE HOLE BLOWN OUT. (NO ED FOR NUT PLATE RIVET) MARKED. RESOLUTION: REMOVED AND REPLACED INTERCOSTAL FS 827-847 / 25L IAW 737-800 SRM 51-40-02-0G-0 AND BOEING DWG 146A7502.

Part: STRAP — CORRODED (BS 1016) · airframe 47,021 hrs · 27,802 cycles

CORROSION ON STRAP BS 1016, RBL 3, WL 207. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0. REMOVED AND REPLACED THE STRAP IAW SRM 51-40-02-0G-0, AND DWG 147A5700, REV B, CAUSE OF CORROSION TO BE MOISTURE.

Part: STRAP — CORRODED (BS 1016) · airframe 47,021 hrs · 27,802 cycles

CORROSION ON STRAP BS 1016, RBL 18, WL 207. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-1002-0G-0. REMOVED AND REPLACED THE STRAP IAW SRM 51-40-02-0G-0, AND DWG 147A5700, REV B. CAUSE OF CORROSION TO BE MOISTURE.

Part: FRAME — DENTED · airframe 47,021 hrs · 27,802 cycles

DEFECT TC 00163 NR 00335: WHILE INSPECTING THE INSTALLATION OF NEW LH ZEE CHANNEL FOUND STA 827 FRAME DAMAGE NEAR ZEE CHANNEL ATTACH FASTENER HOLE (MARKED). RESOLUTION: UPON DAMGE INVESTIGATION STA 827 FRAME ABOVE STR 25L FOUND TO BE DENTED. DENTS ARE NOT PERMITTED IAW 737-SRM 53-00-07-1A-1 ON INNER CORD. REPAIRED DAMAGE IAW B737 SRM 53-60-07-2R-2 REPAIR 2, REPAIR IS CAT B IAW B737- SRM 53-60-07-ER-2 REPAIR 2 TABLE 203 THRESHOLD INSPECTION 50,000 FLIGHT CYCLES, METHOD HIGH FREQUENCY EDDY CURRENT (HFEC) DETAILED INSPECTION INTERVAL 10,000 FLIGHT CYCLES.

Part: ATTACH ANGLE — CRACKED (BS 827) · airframe 47,021 hrs · 27,802 cycles

ATTACH ANGLE BS 827, RBL 20, WL 160 CRACKED AT FLANGE. REMOVED ATTACH ANGLE IAW SRM 51-40-02-06-0 REV 77. INSTALLED A NEW ANGLE IAW SRM 51-40-02-06-0 REV 77 AND DWG 146A0081 REV A.

Part: WEB — CORRODED (BS 784-787) · airframe 47,021 hrs · 27,802 cycles

AFT CARGO WEB ASSY UNDER SHIELD FWD OF CARGO DOOR AT STA 787-784 RBL 20 WL 160 HAS CORROSION AROUND FASTENERS HOLES. CORROSION ON WEB FOUND TO BE OUT OF LIMITS STA 787 TO 794 RBL 20 WL160 IAW SRM 53-60-15-1B-1. REV 77. REMOVED WEB ASSY IAW SRM 51-40-02-06-0 REV 77. INSTALLED SERVICEABLE WEB ASSY LOT # 5175037-1 IAW SRM 51-40-02-06-0 REV 77 AND BOEING DWG 146A8120 REV: -

Part: STRAP — CORRODED · airframe 47,021 hrs · 27,802 cycles

DEFECT TC 532400000 NR 00314: CORROSION OUT OF LIMITS ON LOWER STRAP BS 840-860 RBL 20 WL 160 (DOOR SURROUND STRUCTURE PSE) RESOLUTION: CORROSION ON LOWER STRAP BS 840-860 RBL 20 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 PAR 4 F-1 REMOVED AND REPLACED STRAP IAW SRM 51-40-02-06-0 REV 77 AND BOEING DWG 146A8128 REV: -

Part: WEB — CORRODED · airframe 47,021 hrs · 27,802 cycles

DEFECT JC 802558 NR 00310: WEB ASSY BS 847-857 RBL 20 WL 160 UNDER SHIELD FWD OF CARGO DOOR. RESOLUTION: CORROSION ON WEB ASSY BS 847-857 RBL 20 WL 160 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1. REMOVED WEB ASSY IAW SRM 51-40-02-0G-0. INSTALLED NEW WEB IAW SRM 51-40-02-0G-0 REV: 77. INSTALLED NEW WEB ASSY.

Part: ATTACH FITTING — CRACKED · airframe 47,021 hrs · 27,802 cycles

DEFECT TC 531400002 NR 00304: ATTACH CLIP BS 807 RBL 20 WL 160 IS CRACKED RESOLUTION: REMOVED CRACKED ATTACH CLIP BS 807 RBL 20 WL 160 IAW SRM 51-40-02-06-0 REV 77. INSTALLED CLIP LOT # 5124722 IAW SRM 51-40-02-06-0 REV 77 AND BOEING DWG 146A8120 REV:-

Part: WEB — CORRODED · airframe 47,021 hrs · 27,802 cycles

DEFECT TC 532400000 NR 00288: AFT CARGO LOWER MAIN SILL WEB AT STA 787-847 RBL 20 WL 158 HAS CORROSION AROUND MULTIPLE FASTENER HOLES (MARKED). RESOLUTION: CORROSION ON AFT CARGO LOWER MAIN SILL WEB FOUND TO BE OUT OF LIMITS IAW 53-60-15-1A-1 STEP 4-6-2-B, REMOVED LOWER MAIN SILL WEB IAW SRM 51-40-02-06-00 REV 77. INSTALLED NEW WEB IAW LOT # 51-24-832-1 IAW SRM 51-40-02-06-0 REV 77. AND BOEING DRAWING 146A8120 REV: -

Part: BRACKET — CORRODED (BS 500E S23-24L) · airframe 47,021 hrs · 27,802 cycles

CORROSION ON SUPPORT BRACKET AT FWD CARGO COMPARTMENT STA 500E BETWEEN STR 24L AND STR 23L. RESOLUTION: DAMAGE ON SUPPORT BRACKET AT FWD CARGO COMPARTMENT STA 500E BETWEEN STR 24L AND STR23L FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS - REMOVED AND REPLACED SUPPORT BRACKET IAW B737 SRM 51-40-02-0G-0 AND BOEING DAMGE #417A2150 ID: 0008 REV B.

Part: SUPPORT BEAM — CORRODED (BS 500H S23-24L) · airframe 47,021 hrs · 27,802 cycles

CORROSION ON SUPPORT BRACKET AT FWD CARGO COMPARTMENT STA 500H BETWEEN STR 24L AND STR 23L. DAMAGE ON SUPPORT BRACKET AT FWD CARGO COMPARTMENT STA 500H BETWEEN STR 24L AND STR 23L FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-40-02-0G-0 AND DWG #417A2150 ID:0008 REV B.

Part: SUPPORT BRACKET — CORRODED (BS 500G S23-24L) · airframe 47,021 hrs · 27,802 cycles

CORROSION ON SUPPORT BRACKET AT FWD CARGO BAY BS 500G, S23-24L DAMAGE ON SUPPORT BRACKET FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS. REMOVED AND REPAIRED SUPPORT BRACKET IAW SRM 51-00-02-0G-0 AND DWG 417A2150, REV B.

Part: SUPPORT BRACKET — CORRODED (BS 500F S23-24L) · airframe 47,021 hrs · 27,802 cycles

DAMAGE ON SUPPORT BRACKET AT FWD CARGO COMPARTMENT STA 500F BETWEEN STR 24L AND STR 23L FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-40-02-06-0 AND DWG #417A2150 REV B.

Part: CHANNEL — CORRODED (BS 500A-500D) · airframe 47,021 hrs · 27,802 cycles

CORROSION ON FWD COMPARTMENT LH Z CHANEL STA 500A TO STA 500D. REPAIRED Z CHANNEL FROM STA 500+10" TO 500 IAW B737 SRM 53-00-53-2R-6 REPAIR 6, SRM 51-40-05-0G AND DWG 143A7501.

Part: SHIELD — CORRODED (BS 420-440) · airframe 47,021 hrs · 27,802 cycles

CORROSION ON FWD CARGO COMPARTMENT RH Z CHANNEL BETWEEN STA 420 AND STA 440. REMOVED AND REPLACED ON FWD CARGO COMPARTMENT RH 2 CHANNEL "SHIELD" IAW B737 SRM 51-40-02-0G-0 PAR 4, AND DWG 143A0080.

Part: SKIN — DAMAGED · airframe 47,021 hrs · 27,802 cycles

DEFECT JC 802558 NR 00265: REPAIR AT STA 1016+6 BETWEEN STR 13L & STR14L. RESOLUTION: ACCOMPLISHED REPAIR AT STA 1016+6 BETWEEN STR 13L AND 14C IAW SCA ENG-53SCA-11093 REV 00.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 47,021 hrs · 27,802 cycles

DEFECT TC 530500000 NR 00194: RH VERTICAL PRESSURE WEB 663 IS CRACKED. ACCOMPLISHED REPAIR AT RH VERTICAL PRESSURE WEB BS 663 IAW SRM 57-10-10-2R-3, PAR 5.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 47,021 hrs · 27,802 cycles

LEFT VERTICAL UPPER PRESSURE WEB BS 663 WAS CRAKCED. ACCOMPLISHED REPAIR IAW SRM 57-10-10-2R-3, PAR 5.

Part: BRACKET — CORRODED (BS 947) · airframe 47,021 hrs · 27,802 cycles

DEFECT TC 531400002 NR 00146: CORROSION AFT CARGO AFT LOWER BULKHEAD SUPPORT HAS CORROSION STA 947 WL 160 LBL 5.RESOLUTION: REMOVED AND REPLACED AFT LOWER BULKHEAD SUPPORT P/N 149A8118U29 IAW B737-800 SRM 51-40-02-0G-0 AND DWG 149A8118 REV A AT BS 947 WL 160 LBL 5

Part: WEB — CORRODED · corrosion level 2 · airframe 47,021 hrs · 27,802 cycles

DEFECT TC 531400002 NR 00149: AFT CARGO THRESHOLD HAS CORROSION AROUND FASTENER HOLES STA 807-847 RBL 35 WL 158. RESOLUTION: CORROSION ON AFT CARGO BAY THRESHOLD WEB FOUND TO BE OUT OF LIMITS IAW 53-60-15-1A-1 FIG 103 DETAILED. REMOVED THRESHOLD WEB IAW SRM 51-40-02-06-0 REV 77. INSTALLED NEW WEB IAW SRM 51-40-LOT # 5124706-1 IAW SRM 51-40-02-02-06-0 REV 77 AND BOEING DWG 146A8340 REV -. REMOVED WEB IAW SRM 51-40-02-06-0 REV 77. INSTALLED WEB LOT # 5125106 IAW SRM 51-40-02-06-0 REV 77 AND BOEING DWG 146A8340 REV.0.

Part: STRINGER — DENTED · airframe 47,021 hrs · 27,802 cycles

DEFECT TC 00265 NR 00329: UPON REMOVAL OF EXISTING SKIN REPAIR S-13L AT APPROX. BS 1021 FOUND STRINGER DENTED OUT OF LIMITS. RESOLUTION: EXISTING SKIN REPAIRS STRINGER 13L DENT AT APPROX STA 1021 FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-00-03-1A-1 STEP 4 (A) 2 (C). REMOVED AND REPLAACED WITH NEW STRINGER ITEM # 69-78188-16 IAW B737 SRM 51-40-02-006-0 AND SRM 53-00-03-2R-1.

Part: STRAP — CORRODED · airframe 47,021 hrs · 27,802 cycles

DEFECT TC 531400002 NR 00151: CORROSION OUT OF LIMITS ON AFT CARGO FLOOR STRAP (DOOR SURROUND STRUCTURE PSE) RBL 25 WL 158 STA. 787-847. RESOLUTION: CORROSION ON AFT CARGO DOOR FLOOR STRAP AT STA 747-847 RBL 25 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 FIG 103 DETAIL D. REMOVED STRAP IAW SRM 51-40-02-06-0 REV 77. INSTALLED NEW STRAP IAW SRM 51-40-02-06-0 REV: 77 AND BOEING DWG 146A8120 REV: -

Part: FLOOR SUPPORT — CORRODED (BS 767) · airframe 47,021 hrs · 27,802 cycles

CORROSION ON AFT CARGO INTERCOSTAL AFT OF RT ZEE CHANNEL AT BS 767. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED THE INTERCOSTAL BS 737 - 787 RBL30, WL 158 IAW SRM 51-40-00-02-0G-0 AND DWG 146A8123. CAUSE OF CORROSION WAS MOISTURE.

Part: CHANNEL — CORRODED (BS 727) · airframe 47,021 hrs · 27,802 cycles

CORROSION AFT CARGO LH ZEE AT BS 727+6 LBL 25 WL 158. REMOVED AND REPLACED CHANNEL IAW SRM 51-40-02-0G-0, SRM 53-0053-2R-5, AND DRAWING 146A7500, REV B.

Part: FLOOR SUPPORT — CRACKED (BS 312-328 RBL32) · airframe 47,021 hrs · 27,802 cycles

DEFECT: INTERCOSTAL BTW STA312 AND STA328 RBL31.5, 208 WATERLINE HAS CRACK AROUND FASTENER HOLE. RESOLUTION: DAMAGE ON INTERCOSTAL AT STA312-328 RBL 31.5 FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-00-04-10-1. REMOVED AND REPLACED INTERCOSTAL AT STA312-328 RBL31.5 IAW B737 SRM 51-40-02-0G-0 AND BOEING DRAWING 141A5400 REV.

Part: TRACK — CORRODED · corrosion level 2 · airframe 47,021 hrs · 27,802 cycles

DEFECT TC 531400002 NR 00159: *CORROSION* FLOOR STRUCTURE (CARGO TIE DOWN TRACK) @ STA. 787-797 RBL 15 AND WL 158. RESOLUTION: REPLACED DAMAGED SECTION OF CARGO TIE DOWN TRACK FS 787-797 RBL 15 IAW 737-800 SRM 53-00-53-2R-3 REPAIR 3.

Part: SHIELD — CORRODED · airframe 47,021 hrs · 27,802 cycles

DEFECT TC 531400002 NR 00148: CORROSION OUT OF LIMITS ON AFT CARGO SHIELD AFT OF THRESHOLD WEB (DOOR SURROUND STRUCTURE PSE) RBL 25 WL 158 STA. 847-867. RESOLUTION: CORROSION ON AFT CARGO AFT SHIELD OF THRESHOLD WEB TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE FOU IN SRM. REMOED SHIELS IAW SRM 51-40-02-06-0 REV 77. INSTALLED NEW SHIELD LOT#5124789-1 IAW SRM 51-40-02-06-0 REV 77 AND BOEING DWG 146A0081 REV A.

Part: SHIELD — CORRODED · corrosion level 2 · airframe 47,021 hrs · 27,802 cycles

DEFECT TC 531400002 NR 00145: AFT CARGO SHIELD FWD OF THRESHOLD AT RBL 25 WL 158 HAS CORROSION OUT OF LIMITS. RESOLUTION: CORROSION ON SHIELD FWD OF THRESHOLD WEB RBL 25 WL 158 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE IAW SRM 53-60-15-1A-1. REMOVED SHIELD IAW SRM 51-40-02-06-0 REV 77. INSTALLED NEW SHIELD IAW SRM 51-40-02-00-0 AND BOEING DWG 146A0081 REV A.

Part: CHANNEL — CORRODED (BS 970) · airframe 47,021 hrs · 27,802 cycles

CORROSION ON R2 MOP SILL STA 970. REMOVED AND REPLACED MOP SILL RH BTW STA 887 TO STA 1006 IAW B737-800 SRM 51-40-02-0G-0

Part: FLOORBEAM — CORRODED (BS 986 RBL 45) · airframe 47,021 hrs · 27,802 cycles

CORROSION ON FLOORBEAM BS 986 RBL 45. CORROSION ON FLOORBEAM WAS REPAIRED IAW SRM 57-30-51-2R-6, PAR 4, FIG 205.

Part: FLOORBEAM — CORRODED (BS 986 LBL45) · airframe 47,021 hrs · 27,802 cycles

CORROSION ON BS 986 FLOORBEAM LBL45. CORROSION ON 986 FLOOR BEAM LBL45 WAS REPAIRED IAW B737-800 SRM 53-70-51-2R-6 PAR. 4, FIG. 205 AND TABLE 204.

Part: STRAP — CORRODED (BS 1008) · airframe 47,021 hrs · 27,802 cycles

CORROSION ON STRAP BS 1008 LBL5, WL 208. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0. REMOVED AND REPLACED THE STRAP IAW SRM 51-40-02-0G-0 AND DWG 147A5700, REV B,

Part: FLOOR SUPPORT — CORRODED (BS 294-312 LBL12) · airframe 47,021 hrs · 27,802 cycles

DEFECT: TASKCARD 533800000 NRTC 00079 CORROSION INTERCOSTAL STA 294.5-312 LBL 12 RESOLUTION: DAMAGE ON INTERCOSTAL AT STA 294.5-312 LBL12 FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-00-04-1A-1. REMOVED AND REPLACED INTERCOSTAL AT STA 294.5-312 LBL12 IAW B737 SRM 51-40-02-6G-0 AND DRAWING 141A5600 REV B. CAUSE OF CORROSION: MOISTURE. NO PREVIOUS BLENDING REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 294-312 LBL12) · airframe 47,021 hrs · 27,802 cycles

CORRODED INTERCOSTAL BS 294.5-312 LBL12. DAMAGE ON INTERCOSTAL AT BS 294.5-312 LBL12 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04-1A-1. REMOVED AND REPLACED INTERCOSTAL IAW 51-40-026G-0 AND DRAWING 141A5600 REV B. CAUSE OF CORROSION: MOISTURE. NO PREVIOUS BLENDING REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 947-967) · airframe 47,021 hrs · 27,802 cycles

DEFECT TC 533800000 NR 00082: CORROSION ON FLOOR SUPPORT STA 947.5-967 LBL 45, WL208. RESOLUTION: FLOOR SUPPORT STA 947.5-967 LBL 45 FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-A. REMOVED AND REPLACED FLOOR SUPPORT AT STA 947.5-967 LBL 45 IAW SRM 51-40-02-0G-0 AND BOEING DRAWING 147A5650 REV: -

Part: FLOOR SUPPORT — CORRODED (BS 328-344 LBL46) · airframe 47,021 hrs · 27,802 cycles

CORROSION ON INTERCOSTAL STA 328-344 LBL 46. REMOVED AND REPLACED INTERCOSTAL P/N 141A5410U16 AT MAIN CABIN STAT 328-344 LBL 46 PER B737-800 SRM 51-40-02-0G AND DWG #141A5400. CAUSE OF CORROSION TO BE MOISTURE.

Part: INTERCOSTAL — CORRODED (BS 312-328) · airframe 47,021 hrs · 27,802 cycles

DEFECT TC533800000 NR 00078: CORROSION ON INTERCOSTAL STA 312-328 LBL 12, WL 208. RESOLUTION: REMOVED AND REPLACED INTERCOSTAL STA 312-328 LBL 12 PER B737 SRM 51-40-02-0G-0 STEP 7 AND BOEING DWG 141A5400

Part: IDG — MALFUNCTIONED (NR 2) · airframe 42,918 hrs · 25,912 cycles

GEN OFF BUS LIGHT AND SOURCE OFF LIGHT ILLUMINTED AT CRUZE GEN WOULD NOT RESET. CREW FOLLOWED THE QRH, UNABLE TO RECONNECT GEN 2 TO THE TRANSFER BUS. DUE TO #2 GEN OFF LIGHT STARTED APU IN FLIGHT AT 37000 , AFTER 3 MINUTES APU INOP LIGHT ILLUMINTED AND APU DROPPED OFF LINE. DID NOT ATTEMPT RESTART. REPLACED #2 ENG IDG REF AMM 24-11-11 OPS CHECK GOOD LEAK CHECK GOOD. PERFORMED FIM 49-60 TASK 801 AND FOUND FAULT 49-91007 LOW OIL PRESSURE. PERFORMED FIM 49-90 TASK 803 AND NO CURRENT FAULTS APU STARTED NORMAL SEVERAL TIMES. REMOVED & REPLACED APU LOW OIL PRESSURE SWITCH. APU OPS CHECK GOOD. REF: AMM 49-94-22. OK FOR SERVICE

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,365 hrs · 23,567 cycles

FOUND 13F EXIT DOOR LAMP INOP. R&R THE BULB AT 13F EXIT DOOR. OP CHK GOOD. OK FOR SVC.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,252 hrs · 23,127 cycles

AFT LT OVERWING EXIT DOOR LIGHT INOP. REPLACED LIGHT ASSY. OPS CHECKS GOOD.