N3735D

Part: CONNECTING ROD — DISCONNECTED (ZONE 800) · airframe 73,114 hrs · 33,683 cycles

R1 DOOR WILL NOT OPEN. FOUND TORQUE TUBE CONNECTING ROD DISCONNECTED. REPLACED H/W. DOOR OP CK NORMAL. R1 SLIDE REMOVED & REPLACED TO FOM REFER AMDS WORKCARD 2560-4427. A/C OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 73,108 hrs · 33,681 cycles

FOUND AFT LEFT EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY M1673 IAW AMM 33-51. OPS CHECKED NORMAL.

Part: WINDOW — CRACKED (ZONE 200) · airframe 69,734 hrs · 32,163 cycles

(LOG 0619502) CRACK ON UPPER AFT CORNER OF LH WINDSHIELD (OUTER AREA) AT COCKPIT CABIN . UPPER AFT CORNER OF LH WINDSHIELD (OUTER AREA) AT COCKPIT CABIN WAS REPAIRED PER PER ERA NO. 619132-14AD.

Part: SKIN — DENTED (ZONE 300) · airframe 69,734 hrs · 32,163 cycles

(LOG 0614343) DURING DENT EVALUATION, PAINT ON RUDDER SKIN RH SIDE BTW RUD STA 102.2 AND RUD STA 129.7 WAS REMOVED, AND A PREVIOUS REPAIR WAS FOUND IN THE SAME AREA. AREA ON RUDDER SKIN RH SIDE BTW RUD STA 102.2 AND RUD STA 129.7 WAS REPAIRED PER B737-800 S.R.M. 51-70-04-2R GENERAL PROCEDURE PAR. 4 IN REFERENCE B737-800 S.R.M. 55-40-01-2R PROCEDURE 1 REPAIR 1 PAR 4 AND TABLE 201 AND RUDDER BALANCE PROCEDURE WAS PERFORMED PER B737-800 SRM 51-60-07-0G.

Part: STRINGER — CRACKED (ZONE 100) · airframe 69,734 hrs · 32,163 cycles

(LOG 0605745) CRACK ON STRINGER 27RH BTW STA 727 AND STA 727A (FWD EDGE) AT AFT CARGO COMPARTMENT. STRINGER 27RH BTW STA 727 AND STA 727A (FWD EDGE) AT AFT CARGO COMPARTMENT WAS REPAIRED PER ER/A 620742-14 REV. ORIGINAL SECTION I.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,734 hrs · 32,163 cycles

(LOG 0602723) CORROSION ON LH SIDE PLATE AT FWD CARGO COMPARTMENT BTW STA 360 TO STA 500H. LH SIDE PLATE AT FWD CARGO COMPARTMENT BTW STA 360 TO STA 500H WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,734 hrs · 32,163 cycles

(LOG 0599368) CORROSION ON SIDE PLATES LH FROM STA 727 TO STA 847 AT AFT CARGO COMPARTMENT. SIDE PLATES LH FROM STA 727 TO STA 847 AT AFT CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,734 hrs · 32,163 cycles

(LOG 0600360) CORROSION ON SIDE PLATE FROM STA 727 TO STA 767 RH SIDE AT AFT CARGO COMPARTMENT. SIDE PLATE FROM STA 727 TO STA 767 RH SIDE AT AFT CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: ACCESS DOOR — CRACKED (ZONE 100) · airframe 69,734 hrs · 32,163 cycles

(LOG 0598655) CRACK ON FLANGE OF EXTERNAL POWER RECEPTACLE ACCESS. FLANGE OF EXTERNAL POWER RECEPTACLE ACCESS WAS REPAIRED PER B737-800 SRM 53-10-15-2R PROCEDURE 5 REPAIR 5.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,734 hrs · 32,163 cycles

(LOG 0597673) CORROSION ON RH SIDE PLATE AT FWD CARGO COMPARTMENT BTW STA 490 TO STA 500I. RH SIDE PLATE AT FWD CARGO COMPARTMENT BTW STA 490 TO STA 500I WAS FABRICATED DWG 143A8126 REV.G AND REPLACED PER B737-800 SRM 51-40-02-0G.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 69,734 hrs · 32,163 cycles

(LOG 0592855) CRACK OF 0.560IN LENGTH ON LH THE ATTACH ANGLE AT THE DRAIN HOLE/SLOT. ATTACH ANGLE AT THE DRAIN HOLE/SLOT LH WAS REPAIRED PER B737-800 SRM 57-10-10-2R REPAIR 6.

Part: ATTACH ANGLE — DAMAGED (ZONE 100) · airframe 69,734 hrs · 32,163 cycles

(LOG 0592858) CRACK OF 0.315IN LENGTH ON RH THE ATTACH ANGLE AT THE DRAIN HOLE/SLOT. ATTACH ANGLE AT THE DRAIN HOLE/SLOT WAS REPAIRED PER B737-800 SRM 57-10-10-2R REPAIR 6 PAR 4 ASSOCIATED AA 5714-01004 ADDED FOR AC 3735.

Part: FRAME — CRACKED (ZONE 200) · airframe 69,734 hrs · 32,163 cycles

(LOG 0591870) CRACK WAS FOUND OF 0.13IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 787. BTW S-8R & S-9R. FRAME AT INBOARD FASTENER HOLE ON STA 787. BTW S-8R & S-9R. WAS REPAIRED PER CARD AD 2526-01236-02B.

Part: FRAME — CRACKED (ZONE 200) · airframe 69,734 hrs · 32,163 cycles

(LOG 0591941) CRACK WAS FOUND OF 0.23IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 827. BTW S-8R & S-9R. FRAME AT INBOARD FASTENER HOLE ON STA 827. BTW S-8R & S-9R WAS REPAIRED PER CARD AD 2526-01236-02B.

Part: FRAME — CRACKED (ZONE 200) · airframe 69,734 hrs · 32,163 cycles

(LOG 0591808) CRACK WAS FOUND OF 0.32IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 867. BTW S-8R & S-9R. FRAME AT INBOARD FASTENER HOLE ON STA 867. BTW S-8R & S-9R WAS REPAIRED PER CARD AD 2526-01236-02B.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 69,734 hrs · 32,163 cycles

(LOG 0592267) CORROSION ON FLOOR BEAM STA 947.5 AND RBL 48 AT W2 CPAX . FLOOR BEAM STA 947.5 AND RBL 48 AT W2 CPAX WAS REPAIRED PER B737-800 SRM 53-70-51-2R REP. 5.

Part: FRAME — CRACKED (ZONE 200) · airframe 69,734 hrs · 32,163 cycles

(LOG 0589476) CRACK WAS FOUND OF 0.31IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 727B. BTW S-8L & S-9L. FRAME AT INBOARD FASTENER HOLE ON STA 727B BTW S-8L & S-9L.. WAS REPAIRED PER AMDS 2526-01236-02A.

Part: FRAME — CRACKED (ZONE 200) · airframe 69,734 hrs · 32,163 cycles

(LOG 0589533) CRACK WAS FOUND OF 0.21IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 827. BTW S-8L & S-9L. FRAME AT INBOARD FASTENER HOLE ON STA 827 BTW S-8L & S-9L. WAS REPAIRED PER AMDS 2526-01236-02A.

Part: FRAME — CRACKED (ZONE 200) · airframe 69,734 hrs · 32,163 cycles

(LOG 0589342) CRACK WAS FOUND OF 0.25IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 867. BTW S-8L & S-9L. FRAME AT INBOARD FASTENER HOLE ON STA 867 BTW S-8L & S-9L . WAS REPAIRED PER AMDS 2526-01236-02A.

Part: FRAME — CRACKED (ZONE 200) · airframe 69,734 hrs · 32,163 cycles

(LOG 0590237) CRACK WAS FOUND OF 0.28IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 400. BTW S-8L & S-9L. FRAME AT INBOARD FASTENER HOLE ON STA 400. BTW S-8L & S-9L. WAS REPAIRED PER AMDS 2526-01236-02A.

Part: FRAME — CRACKED (ZONE 200) · airframe 69,734 hrs · 32,163 cycles

(LOG 0590309) CRACK WAS FOUND OF 0.12IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500F. BTW S-8L & S-9L. NO CRACKS WERE FOUND PER B737 NDT MANUAL PART 6 ASSOCIATED AA 2526-01236 ADDED FOR AC 3735.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 69,734 hrs · 32,163 cycles

(LOG 0590907) MISSING MATERIAL ON SEAT TRACK RBL 44 (OUTBOARD) ON STA 727J + 5 IN. SEAT TRACK RBL 44 (OUT BOARD) ON STA 727J + 5 IN WAS REPAIRED B737-800 SRM 53-00-52-2R PROCEDURE 5 REPAIR 5.

Part: FRAME — CRACKED (ZONE 200) · airframe 69,734 hrs · 32,163 cycles

(LOG 0590743) CRACK WAS FOUND OF 0.500IN OF LENGTH ON RH FUSELAGE FRAME AT INBD FASTENER HOLE ON STA 500F BTW S-8R & S-9R. FRAME AT INBD FASTENER HOLE ON STA 500F BTW S-8R & S-9R WAS REPAIRED PER CARD AD 2526-01236-02B.

Part: FRAME — CRACKED (ZONE 200) · airframe 69,734 hrs · 32,163 cycles

(LOG 0589206) CRACK WAS FOUND OF 0.13IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500C. BTW S-8R & S-9R. FRAME AT INBOARD FASTENER HOLE ON STA 500C BTW S-8R & S-9R. WAS REPAIRED PER AMDS 2526-01236-02B.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 69,734 hrs · 32,163 cycles

(LOG 0586603) INITIAL INSPECTION: CORROSION ON FLOOR BEAM STA 986.5 AND LBL34 TO LBL 44 ALSO RBL 11 TO RBL 45 AT CAB. PAX (W-2). FLOOR BEAM STA 986.5 AND LBL34 TO LBL 44 ALSO RBL 11 TO RBL 45 AT CAB. PAX (W-2). WAS REPAIRED PER B737-800 SRM 53-70-51-2R PROCEDURE 4 REPAIR 4

Part: THROTTLE — FAULTED (LT ENGINE) · airframe 69,068 hrs · 31,887 cycles

SHIP 3735 -ATO- DUE TO LEFT ENGINE THROTTLE RESPONSE ISSUES AND APPROACHING N1 OVERSPEED. CORRECTIVE ACTION: REPLACING LEFT THROTTLE RESOLVER ASSEMBLY.

Part: DOOR FRAME — DAMAGED · airframe 68,389 hrs · 31,580 cycles

AIRCRAFT 3735, AROUND FOUND DAMAGE TO FWD LOWER PORTION OF FWD CARGO DOOR FRAME JUST ABOVE SCUFF PLATE. CORRECTIVE ACTION: REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER ER/A 616656-14. (LP 0254391)

Part: INDICATION SYS — FALSE INDICATION (FUEL SYSTEM) · airframe 68,316 hrs · 31,542 cycles

DIVERTED TO SLC DUE TO LEFT FUEL QUANTITY DECREASING. MAINTENANCE HAD FUELING ADJUST FUEL QUANTITY AND PERFORMED FQIS BITE PER FIM 28-41-00. NO FAULTS ON MAIN TANK.

Part: BATTERY PACK — INOPERATIVE (UNKNOWN) · airframe 66,724 hrs · 30,818 cycles

(LOG 4131440) ON SVC CHECK FOUND THE AISLE ON SEATS 1-4 CD INOP. REMOVED AND REPLACED HE M1675 EMERGENCY LIGHT BATTERY PACK AND CHARGER PER B737 AMM 33-51-06. OPS CHECK OF ROW 1-3. AISLE LIGHTS OPS GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 66,733 hrs · 30,822 cycles

(LOG 4131441) ROW 4CD HAS A BROKEN HARNESS FOR THE AISLE EMERGENCY LIGHT. REPAIRED WIRES AT SEAT 4CD IAW B737 SWPM 20-10-13. EMERGENCY LIGHTS @ 4CD TEST NORMAL.

Part: CONTROL UNIT — DEFECTIVE (X) · airframe 65,458 hrs · 30,236 cycles

SHIP 3735 -ATB- DUE TO AN ELECTRICAL ODOR IN COCKPIT AND CABIN AFTER TAKEOFF. CORRECTIVE ACTION: R/R SPCU PER B737 AMM 24-34. OPS CHECK NORMAL.

Part: NONE — NONE · airframe 65,402 hrs · 30,213 cycles

(LOG 9427166) DURING INSPECTION FOUND DURING TOW EMERGENCY LIGHT WOULD NOT TURN OFF. FOUND AFT LIGHT MODULE M1886 WITH DAMAGED CONNECTION AT TERMINAL 3C ON SWITCH AND SWITCH ALSO DAMAGED INTERNALLY. REPLACED MODULE M1886 AND TESTED PER B737 AMM 33-51. NOW EMERGENCY LIGHTS OPS NML.

Part: NONE — NONE · airframe 64,279 hrs · 29,662 cycles

SHIP 3735 -ATO- DUE TO SMOKE/ODOR. CORRECTIVE ACTION: C/W NO-GO PROCEDURES, PERFORMED HIGH POWER ENGINE RUNS WITH NTF AND REPLACED RECIRC. FILTERS.

Part: BATTERY — INOPERATIVE · airframe 63,962 hrs · 29,489 cycles

(LOG 9296430) DURING INSPECTION FOUND AISLE EMERGENCY LIGHTS INOP AT SEAT ROWS 19-22 DEF. INSTALLED NEW BATTERY IN POWER SUPPLY M1671. REF B737 AMM 33-51-06 . OPS CKS GOOD.

Part: NONE — NONE · airframe 61,798 hrs · 28,543 cycles

(LOG 1969778) DURING INSPECTION FOUND L/H FAIRING SUPPORT STRUCTURE FOR PANELS 193D AND 194E HAS DAMAGE AT NUT PLATE HOLES. C/W ER/A 594467-14AD REV ORIGINAL .

Part: NONE — NONE · airframe 61,798 hrs · 28,543 cycles

(LOG 1969789) DURING INSPECTION FOUND R/H FAIRING SUPPORT STRUCTURE POR PANELS 193D AND 194E HAS DAMAGE AT NUT PLATE HOLES. C/W ER/A 594467-14AD REV ORIGINAL.

Part: SHROUD — DAMAGED (EMERGENCY LIGHT) · airframe 61,251 hrs · 28,308 cycles

(LOG 1864678) DURING INSPECTION FOUND FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM SEAT MOUNTED PATH LIGHT INOP AT SEAT 22D. REMOVED AND REPLACED BUMPER AND LIGHT SHROUD. REF CMM 25-27-79. LIGHT OPS CHK NML PER B737 AMM 33.

Part: BUSHING — CORRODED (LT TRUNNION) · corrosion level 2 · airframe 60,646 hrs · 28,076 cycles

DURING INSPECTION FOUND LEFT TRUNNION FITTING, LOWER I/B LUG HAS CORROSION IN BORE AND ON I/B FACE. REPLACED BUSHING PER B737 SRM 57-20-90 REPAIR 2.

Part: BUSHING — CORRODED (RT TRUNNION) · corrosion level 2 · airframe 60,646 hrs · 28,076 cycles

(LOG 1801043) DURING INSPECTION FOUND RIGHT TRUNION FITTING, LOWER O/B LUG HAS CORROSION IN BORE, AND I/B AND O/B FACE. REPLACED BUSHING PER B737 SRM 57-20-90 REPAIR 2.

Part: BUSHING — CORRODED (LT TRUNNION) · corrosion level 2 · airframe 60,646 hrs · 28,076 cycles

(LOG 1801031) DURING INSPECTION FOUND LEFT TRUNION FITTING, UPPER I/B LUG HAS CORROSION IN BORE AND ON THE I/B FACE. REPLACED BUSHING PER B737 SRM 57-20-90 REPAIR 2.

Part: BUSHING — CORRODED (LT TRUNNION) · corrosion level 2 · airframe 60,646 hrs · 28,076 cycles

(LOG 1801029) DURING INSPECTION FOUND LEFT TRUNION FITTING, LOWER O/B LUG HAS CORROSION IN BORE. REPLACED BUSHING PER B737 SRM 57-20-90 REPAIR 2.

Part: BUSHING — CORRODED (RT TRUNNION) · corrosion level 2 · airframe 60,646 hrs · 28,076 cycles

DURING INSPECTION FOUND RIGHT TRUNION FITTING, UPPER O/B LUG HAS CORROSION IN BORE, AND I/B AND O/B FACE. REPLACED BUSHING PER B737 SRM 57-20-90 REPAIR 2.

Part: BUSHING — CORRODED (LT TRUNNION) · corrosion level 2 · airframe 60,646 hrs · 28,076 cycles

(LOG 1801033) DURING INSPECTION FOUND LEFT TRUNION FITTING, UPPER O/B LUG HAS CORROSION IN BORE AND ON THE I/B FACE. REPLACED BUSHING PER B737 SRM 57-20-90 REPAIR 2.

Part: BUSHING — CORRODED (RT TRUNNION) · corrosion level 2 · airframe 60,646 hrs · 28,076 cycles

(LOG 1801041) DURING INSPECTION FOUND RIGHT TRUNION FITTING, LOWER I/B LUG HAS CORROSION IN BORE AND I/B AND O/B FACE. REPLACED BUSHING PER B737 SRM 57-20-90 REPAIR 2.

Part: BUSHING — CORRODED (RT TRUNNION) · corrosion level 2 · airframe 60,646 hrs · 28,076 cycles

(LOG 1801141) DURING INSPECTION FOUND RIGHT TRUNION FITTING, UPPER I/B LUG HAS CORROSION IN BORE AND ON O/B FACE. REPLACED BUSHING PER B737 SRM 57-20-90 REPAIR 2.

Part: BUSHING — WORN (HANGER) · airframe 60,646 hrs · 28,076 cycles

(LOG 1799852) DURING INSPECTION FOUND LOWER HANGAR LINK ATTACH BUSHINGS WORN ON A/C. REPLACED R/S LOWER ATTACH BUSHINGS PER CMM 57-15-01.

Part: BEARING — CORRODED (NLG) · airframe 60,646 hrs · 28,076 cycles

DURING INSPECTION FOUND LOWER LEFT SIDE BEARING FOR NOSE GEAR, LOCATED BOTTOM LEFT SIDE OF WHEEL WELL, CORRODED BEARING, AT EDGES, VISIBLE . CLEANED AND CHECKED PER BOEING DWG 141A7501.

Part: BUSHING — WORN (HANGER) · airframe 60,646 hrs · 28,076 cycles

DURING INSPECTION FOUND LOWER HANGAR LINK ATTACH BUSHINGS WORN ON A/C. REPLACED R/S LOWER ATTACH BUSHINGS PER CMM 57-15-01.

Part: BUSHING — WORN (HANGER) · airframe 60,646 hrs · 28,076 cycles

(LOG 1799849) DURING INSPECTION FOUND UPPER HANGER LINK ATTACH BUSHINGS WORN ON A/C. REPLACED UPPER ATTACH BUSHINGS PER BOEING DWG 144A1650. R/S UPPER ATTACH BUSHING PER BOEING DWG 144A1650.

Part: BUSHING — WORN (HANGER) · airframe 60,646 hrs · 28,076 cycles

(LOG 1799887) DURING INSPECTION FOUND UPPER HANGAR LINK ATTACH BUSHINGS WORN ON A/C. REPLACED UPPER ATTACH BUSHINGS PER BOEING DWG 144A1650.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,548 hrs · 27,030 cycles

DURING INSPECTION FOUND ROW 23-33 SEAT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK M1672. OPS OK. REF AMM 33-51.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 57,301 hrs · 26,510 cycles

(LOG 6749914) EXIT SIGN ABOVE 22CD DAMAGED. REMOVED AND REPLACED LIGHT ASSY PER B737 AMM 33-51, OPS CHECKS OK.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 58,494 hrs · 27,001 cycles

(LOG 1210584) DURING HCK AT QRO, OIL CAN CONDITIONS WERE FOUND COMMON TO AN EXISTING REPAIR ON AFT PRESSURE BULKHEAD (APB) AT BS 1016 AND BL 0 AND RBL 20 AT WEBS 148A2281-6. MAINTENANCE REPAIRED DAMAGE PER ERA 572491-14.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 53,986 hrs · 25,143 cycles

DURING INSPECTION FOUND OIL-CANNING EFFECT ON AFT PRESSURE BHD. PRESSURE BHD WAS REPAIRED PER ER/A 572491-14AD REV ORIGINAL AND ETI-37-18-521 REV 4.

Part: BULKHEAD — CANNING (FUSELAGE) · airframe 53,986 hrs · 25,143 cycles

DURING INSPECTION FOUND OIL-CANNING EFECT ON AFT PRESSURE BHD BS 1016 UPPER SIDE BTW STR S-1R-3R. PRESSURE BHD REPAIRED PER ER/A 572491-14AD REV ORIGINAL AND ETI-37-18-521 REV 4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,986 hrs · 25,143 cycles

(LOG 0795961) DURING INSPECTION FOUND CORROSION AT FLOORBEAM STA 986 LT SIDE. FLOORBEAM STATION 986 WAS REPAIRED PER ERA 572508-14 REV. ORIGINAL AND ETI-37-18-520 REV. 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,986 hrs · 25,143 cycles

(LOG 0795957) DURING INSPECTION FOUND CORROSION AT FLOORBEAM STA 986 RT SIDE. FLOORBEAM STATION 986 WAS REPAIRED PER ERA 572508-14 REV. ORIGINAL AND ETI-37-18-520 REV. 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,986 hrs · 25,143 cycles

(LOG 0790747) DURING INSPECTION FOUND CORROSION ON TIE TRACK (FLOOR SUPPORT) FROM 792 TO 847 BTW S26RBL AND S27RBL ON AFT CARGO COMPARTMENT. TIE TRACK (FLOOR SUPPORT) FROM 792 TO 847 BTW S26RBL AND S27RBL WAS REPLACED PER SRM 51-40-02.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,986 hrs · 25,143 cycles

(LOG 0789867) DURING INSPECTION FOUND CORROSION OUT OF LIMITS ON RT ZEE CHANNEL SUPPORTS SIDEPLATE AT FLOOR STRUCTURE FROM STA 727 TO STA 767 AT AFT CARGO COMPARTMENT. RT SIDE PLATE FROM STATION 727 TO STA 767 WAS REPLACED PER SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,986 hrs · 25,143 cycles

(LOG 0789085) DURING INSPECTION FOUND CRACK ON INTERCOSTAL BTW STATION 747 TO 767 AND S-25R TO S-26R AT AFT CARGO COMPARTMENT. INTERCOSTAL BTW STATION 747 TO 767 AND S-25R TO S-26R WAS REPLACED PER SRM 51-40-02.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,986 hrs · 25,143 cycles

(LOG 0787698) DURING INSPECTION FOUND CORROSION ON LT ZEE CHANNEL SUPPORTS SIDEPLATE AT FLOOR STRUCTURE FROM STA 727D TO STATION 847 ON AFT CARGO COMPARTMENT. LT SIDEPLATE AT FLOOR STRUCTURE FROM STA 727D TO STA 847 WAS REPLACED PER SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,986 hrs · 25,143 cycles

(LOG 0784596) DURING INSPECTION FOUND CRACK ON FRAME STATION 440 BTW S-8R TO S-9R AT PAX CABIN. FRAME STATION 440 BTW S-8R TO S-9R AT PAX CABIN WAS REPAIRED PER ETI-37-18-536 REV 1 AND ERA 572106-14AD REV. ORIGINAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,986 hrs · 25,143 cycles

(LOG 0784599) DURING INSPECTION FOUND CRACK ON FRAME STATION 500D BTW S-8L TO S-9L AT PAX CABIN. FRAME STATION 500D BTW S-8L TO S-9L PAX CABIN WAS REPAIRED PER ETI-37-18-536 REV 1 AND ERA 572106-14AD REV. ORIGINAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,986 hrs · 25,143 cycles

(LOG 0784605) DURING INSPECTION FOUND CRACK ON FRAME STATION 380 BTW S-8R TO S-9R AT PAX CABIN. FRAME STATION 380 BTW S-8R TO S-9R AT PAX CABIN WAS REPAIRED PER ETI-37-18-536 REV 1 AND ER/A 572106-14AD REV. ORIGINAL.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,986 hrs · 25,143 cycles

(LOG 0784771) DURING INSPECTION FOUND CORROSION ON FWD CARGO RT SIDE PLATE SUPPORT ZEE FROM STATION 500B TO 500I. RT SIDE PLATE SUPPORT ZEE FROM STATION 500B TO 500I WAS REPLACED PER SRM 51-40-02 PAR 4 AND 51-40-05.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,986 hrs · 25,143 cycles

(LOG 0784604) DURING INSPECTION FOUND CRACK ON FRAME STATION 500A BTW S-8R TO S-9R AT PAX CABIN. FRAME STATION 500A BTW S-8R TO S-9R AT PAX CABIN WAS REPAIRED PER ETI-37-18-536 REV 1 AND ERA 572106-14AD REV. ORIGINAL.

Part: BULKHEAD — BROKEN (LT MLG WW) · airframe 53,986 hrs · 25,143 cycles

DURING INSPECTION FOUND BROKEN BEYOND OF THE PREVIOUS REPAIR ON BULKHEAD STATION 663 LOCATED BTW STIFFENERS LBL 6-10 LOWER LEFT WEB, LT MLG WHEEL WELL. BULKHEAD LOWER LEFT WEB, LT MLG WHEEL WELL WAS REPAIRED PER SRM 57-10-10 REPAIR 2.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,986 hrs · 25,143 cycles

(LOG 0773126) DURING INSPECTION FOUND CRACK ON INTERCOSTAL BTW STATION 947 AND 967 50RBL. INTERCOSTAL WAS REPLACED PER SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 53,986 hrs · 25,143 cycles

(LOG 0772030) DURING INSPECTION FOUND CRACK INTERCOSTAL ON STATION 317 31 RBL ALSO CRACK INTERCOSTAL ON STA 321 AND 336, 45 LBL AT FWD WET AREA. INTERCOSTALS WERE REPLACED ON STA 317, 31 RBL ALSO ON STA 321 AND 336, 45 LBL AT FWD WET AREA PER SRM 51-40-02.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,986 hrs · 25,143 cycles

(LOG 0765693) DURING INSPECTION FOUND CORROSION ON WEB BTW STATION 793 TO 847 STR 25R AT AFT CARGO COMPARTMENT. WEB BTW STA 793 TO 847 STR 25R AT AFT CARGO COMPARTMENT WAS REPLACED PER SRM 51-40-02.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,937 hrs · 25,126 cycles

ON EMER LTS TEST FOUND ROWS 16, 17, 18INOP. FOUND BATTERY PACK M1695 INOP. R&R CHARGER & BATTERY PER AMM 33-51.

Part: SIGN — INOPERATIVE (CABIN) · airframe 53,232 hrs · 24,863 cycles

DURING INSPECTION FOUND OVERHEAD EXIT SIGN ABEAM OVERWING EXITS REPORTED TO BE NONFUNCTIONAL. REPLACED OVERHEAD EXIT SIGN IN REF AMM 33-51. OPS CHECK NORMAL.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 52,506 hrs · 24,598 cycles

DURING INSPECTION, FOUND THE EMERGENCY LIGHT LENS UNSECURE. MAINTENANCE SECURED THE LENS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,205 hrs · 24,484 cycles

DURING INSPECTION, FOUND THE EMERGENCY EXIT SIGNS AT THE R1 & R4 DOORS , ROWS 1 DEF TO 10 DEF AND 23DEF TO 33DEF INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK M1672 IAW AMM 33-41.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 51,270 hrs · 24,166 cycles

DURING INSPECTION, FOUND THE ROW 24 SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE BEHIND THE SIDEWALL PANEL BY ROW 24. REPAIRED WIRE IAW SWP 20-90-03. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,270 hrs · 24,166 cycles

DURING INSPECTION FOUND EMERGENCY LIGHT RO 16 TO 22 SEAT MOUNTED INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51. OPS CHECKED GOOD.

Part: FITTING — CORRODED (GIRT BAR) · airframe 49,597 hrs · 23,580 cycles

DURING INSPECTION, FOUND FWD AND AFT L2 DOOR GIRT BAR FITTINGS CORRODED. MAINTENANCE REPLACED THE GIRT BAR FITTINGS.

Part: FITTING — CORRODED (GIRT BAR) · airframe 49,597 hrs · 23,580 cycles

DURING INSPECTION, FOUND FWD AND AFT R2 DOOR GIRT BAR FITTINGS CORRODED. MAINTENANCE REPLACED THE FITTINGS.

Part: LIGHT — DAMAGED (CABIN) · airframe 44,581 hrs · 21,826 cycles

DURING INSPECTION FOUND 10D AFT EMERGENCY LIGHT DAMAGED. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSY. OPS CHECKED OK.

Part: FRAME — CRACKED (BS 480) · airframe 39,998 hrs · 20,253 cycles

DURING INSPECTION, FOUND A CRACK IN THE FRAME AT THE AIR CONDITIONING RAIL SUPPORT BRACKET BETWEEN S8-9R BS 480. MAINTENANCE REPAIRED IAW ERA 507336-14.

Part: OVEN — SHORTED (GALLEY) · airframe 39,955 hrs · 20,238 cycles

DURING FLIGHT, THE FORWARD GALLEY OVEN EXPERIENCED ELECTRICAL SHORT WITH SPARKS AND SMOKE. PULLED THE CIRCUIT BREAKER, SMOKE AND ODOR WENT AWAY. MAINTENANCE REMOVED OVEN, INSPECTED AREA, NO SMOKE NOTED. REPLACED OVEN IAW AMM 25-31-88. RAN OVEN FOR 20 MINS, OPS TESTED OK.

Part: SKIN — DAMAGED (BS 330-350) · airframe 38,850 hrs · 19,836 cycles

DURING INSPECTION, FOUND EXTERNAL SKIN DAMAGE AT BS 330-350 ABOVE STRINGER 23 RT. MAINTENANCE REPAIRED SKIN DAMAGE IAW ERA 526306-14, REV A AND PRI 526306-14, REV A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,850 hrs · 19,836 cycles

DURING INSPECTION, FOUND DAMAGE TO FUSELAGE SKIN FORWARD OF CARGO DOOR. MAINTENANCE REPAIRED DAMAGE IAW ERA 526306-14, REV A, SECTION II, PERMANENT REPAIR.

Part: SKIN — DAMAGED (BS 330) · airframe 38,850 hrs · 19,836 cycles

DURING INSPECTION FOUND DAMAGE TO RT FUSELAGE AT BS 330.62. MAINTENANCE COMPLIED WITH ERA 526306-14, REV A, SECTION II PERMANENT REPAIR.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 36,582 hrs · 19,039 cycles

DURING TEST FOUND EMERGENCY BATTERY PACK M2335 FAILED CAPACITY CHECK. MAINTENANCE REPLACED BATTERY PACK IAW MM 33-51-06. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (SEAT 3C) · airframe 35,369 hrs · 18,572 cycles

DURING INSPECTION FOUND PASSENGER SEAT 03C, EMERGENCY SEAT MOUNTED LIGHTING INOPERATIVE. MX REPAIRED EMERGENCY LIGHT AT SEAT 3C. OPS TESTED OK.

Part: SEAT TRACK — DAMAGED (BS 521 LBL 45) · airframe 33,135 hrs · 17,760 cycles

PASSENGER CABIN SEAT TRACK AT BS 521 LBL 45 DAMAGE. REPAIRED SEAT TRACK IAW SRM 53-00-52-2, R-4, REF 2587 1-2400-0006.

Part: SEAT TRACK — WORN (BS 521 RBL 45) · airframe 33,135 hrs · 17,760 cycles

PASSENGER CABIN SENT TRACK AT BS 521, RBL 45, REPAIRED SEAT TRACK IAW SRM 53-00-52-2R-4, REF 25871-2700-0002.

Part: SEAT TRACK — WORN (BS 521 RBL 24) · airframe 33,135 hrs · 17,760 cycles

PASSENGER CABIN SEAT TRACK AT BS 521, RBL 24. REPAIRED SEAT TRACK IAW SRM 53-00-52-2R-4, REF 25871-2700-0003.

Part: FLOORBEAM — CORRODED (BS 312) · airframe 33,135 hrs · 17,760 cycles

FLOORBEAM TEE CAP LBL-12 STA 312 HAS CORROSION REF AMM 51-05-01. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED IAW ER A 507330-14, REV C, REF NRC 25871/2700/0008.

Part: SEAT TRACK — WORN (BS 521 LBL 24) · airframe 33,135 hrs · 17,760 cycles

PASSENGER CABIN SEAT TRACK AT BS 521, LBL 24. REPAIRED SEAT TRACK IAW SRM 53-00-52-2R-4, REF 25871-2700-0001.

Part: SEAT TRACK — CRACKED (BS 727B RBL 24.7) · airframe 33,135 hrs · 17,760 cycles

SEAT TRACK FLANGE STA 727B RBL 24.75 CRACKED. REPAIRED IAW ERA 507333-14 REV ORIG. AT IND ON NR1353415.

Part: SEAT TRACK — CRACKED (BS 727B RBL 45.5) · airframe 33,135 hrs · 17,760 cycles

SEAT TRACK FLANGE BS 727B RBL 45.5 CRACKED. REPAIRED IAW ERA507333-14 REV ORIG. AT IND ON NR1353414.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 33,135 hrs · 17,760 cycles

SEAT TRACK FLANGE CRACKED AT BS 727B LBL 24.75. REPAIRED IAW ERA 507333-14, REV ORIG AT IND ON NR1353413.

Part: SEAT TRACK — CRACKED (BS 727B) · airframe 33,135 hrs · 17,760 cycles

SEAT TRACK FLANGE CRACKED AT BS 727B, LBL 45.5. REPAIRED IAW ERA 507333-14 REV ORIG AT IND ON NR1353416.

Part: FRAME — DAMAGED (BS 500A S8L) · airframe 33,135 hrs · 17,760 cycles

MAIN CABIN FRAME BS 500A, STR 8L, DAMAGED. REPAIRED IAW ERA 507331-14AD AT IND ON NR1353452.

Part: FRAME — DAMAGED (BS 727B) · airframe 33,135 hrs · 17,760 cycles

MAIN CABIN FRAME STA 727B, DAMAGED. REPAIRED IAW ERA 507331-14AD AT IND ON NR1353453.

Part: FRAME — CRACKED (BS 380 S8L) · airframe 33,135 hrs · 17,760 cycles

MAIN CABIN FUSELAGE STA 380 LT SIDE FRAME CRACKED AT RIVET. LOCATION ABOVE STR 8. REPAIRED IAW ERA 507331-14AD AT IND ON NR1353419.

Part: FRAME — CRACKED (BS 480 STR 8L) · airframe 33,135 hrs · 17,760 cycles

PASSENGER CABIN STA 480 AT STR 8L FRAME CRACKED AT INBD FASTENER PF PSU RAIL BRACKET. REPAIRED IAW ERA 507337-14 AD REV ORIG. AT IND AAR ON NR1353304.

Part: FRAME — CRACKED (BS 520) · airframe 33,135 hrs · 17,760 cycles

MAIN CABIN BS 520 AT STR 8 FRAME CRACKED AT F/B FASTENER OF PSU RAIL BRACKET. REPAIRED IAW ERA 507331-14AD AT IND ON NR1353305.

Part: FRAME — CRACKED (BS 440 S7-8R) · airframe 33,135 hrs · 17,760 cycles

MAIN CABIN FRAME BS 480 IS CRACKED AT RIVET BTW STR 7R AND 8R. REPAIRED IAW ERA 507336-14AD REV ORIG. AT IND ON NR1353284.

Part: FRAME — CRACKED (BS 400 S7-8R) · airframe 33,135 hrs · 17,760 cycles

MAIN CABIN FRAME BS 400 IS CRACKED AT RIVET BTW STR 7R AND STR8R. REPAIRED IAW ERA 507331-14AD AT IND ON NR1353283 NR1353283.

Part: FRAME — CRACKED (BS 440 S7-8L) · airframe 33,135 hrs · 17,760 cycles

MAIN CABIN FRAME STA 440 IS CRACKED AT RIVET BTW STR 7L &8L. REPAIRED IAW ERA 507331-14AD AT IND ON NR 1353285.

Part: FLOORBEAM — CORRODED (BS 312 LBL 12) · airframe 33,135 hrs · 17,760 cycles

FLOORBEAM TEE CAP LBL 12, BS 312 HAS CORROSION. REPAIRED IAW ERA 507330-14 REV, ORIG AT IND ON NR1353165.

Part: FLOORBEAM — CORRODED (BS 328) · airframe 33,135 hrs · 17,760 cycles

FLOORBEAM BS 328, RBL 10 TO RBL 58 HAS CORROSION. REPAIRED IAW SRM 53-10-51, REPAIR 7.

Part: SKIN — CORRODED (BS 500) · airframe 33,058 hrs · 17,727 cycles

FUSELAGE SKIN CORRODED BELOW FWD ANTENNA. REPAIRED IAW ER/A 507334-14, REV ORIG 507334-14.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 28,902 hrs · 16,194 cycles

DURING PSV FOUND RT FWD WHEEL WELL BULKHEAD CRACKED (VAPOR BARRIER) JUST OUTBOARD OF KEEL. REPAIRED PER B737 SRM 57-10-10 AVIATION PARTNERS BOEING.

Part: SKIN — GOUGED (BS 807 S25-26L) · airframe 26,521 hrs · 15,227 cycles

GOUGE ON LOWER FUSELAGE SKIN APPROX STA.807 BETWEEN STR 25L AND 26L. DAMAGE REPAIRED IAW ERA-486014-14.

Part: UNKNOWN — ODOR (CABIN) · airframe 25,907 hrs · 14,984 cycles

FLIGHT ATTENDANTS SMELLED PLASTIC SMELL IN FORWARD GALLEY, 20 MINUTES BEFORE LANDING. COFFEEMAKERS AND OVENS HAD BEEN OFF, WITH NO C/B POPPED. CREW SELECTED THE GALLEY POWER TO OFF AND THEN DID NOT SMELL ANYTHING AFTER LANDING. E&E INVESTIGATED GALLEY AND E&E COMPARTMENT, NO SMELL NOTED (2010-D0884)(DL738101945).

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,740 hrs · 6,684 cycles

AFT OVERWING RIGHT EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK.

Part: THERMOSTAT — LEAKING (NR 2 ENGINE) · airframe 3,385 hrs · 4,119 cycles

ON TAKEOFF RIGHT DUCT PRESSURE DROPS TO 10 PSI. REPLACED 450 DEGREE THERMOSTAT.