N3731T

Part: WIRE — DAMAGED (ZONE 200) · airframe 71,683 hrs · 33,666 cycles

(LOG 7414814) ROW 11 SEATS AB AND C REPORTED TELEVISIONS WENT OUT INFLIGHT AND A PUFF OF SMOKE WAS OBSERVED. FOUND DAMAGED WIRE ON WIRING HARNESS RD-KM7882-002. REMOVED AND REPLACED HARNESS IAW IS60978. ALL ITUS NOW ONLINE AND SOFTWARE DOWNLOADED. ALL SYS OPS CHECK GOOD.

Part: ELEC CONNECTOR — DAMAGED (ZONE 200) · airframe 71,351 hrs · 33,526 cycles

(LOG 7009483) DURING SVC FOUND EMERGENCY FLOOR PATH LIGHT AT ROW 21 INOP. FOUND PIN AT WALL CONNECTOR PUSHED IN, RESEATED CONNECTOR PIN, OPS NORMAL.

Part: PITOT TUBE — FAULTED (ZONE 100) · airframe 70,198 hrs · 33,010 cycles

ATB- DUE TO CAPTAIN'S AIRSPEED UNRELIABLE AFTER TAKEOFF. CORRECTIVE ACTION: MAINTENANCE REPLACED LEFT AOA SENSOR PER AMM 34-21 AND CAPTAINS PITOT TUBE PER AMM 34-11. LEAK AND OPS CHECK GOOD.

Part: SEAT — UNSECURE (ZONE 200) · airframe 69,028 hrs · 32,489 cycles

(LOG 4285456) SEAT 33DEF LOOSE FROM O/B TRACK. SECURED SEAT 33DEF INTO O/B TRACK.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,884 hrs · 32,422 cycles

(LOG 0510791) FUSELAGE / SKIN, SKIN DOUBLER AND BULKHEAD CHORD STA 500H TO 540 & S-26L TO S-26R / CORROSION, CRACK. REPAIRED PER ERA 619586-14.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 69,038 hrs · 32,493 cycles

(LOG 0510803) FUSELAGE / SKIN, SKIN DOUBLER AND BULKHEAD CHORD STA 500H TO 540 & S-26L TO S-26R / CORROSION, CRACK. REPAIRED PER ERA 619586-14.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,884 hrs · 32,422 cycles

(LOG 0511336) CORROSION ON LOWER CHORD OF FWD. WALL OF WINGBOX BTW. STA. 540 AND S-28R TO 28L BEHIND OF A/C MIXER INSIDE OF AIR CONDITION BAY AT FWD. CARGO COMPARTMENT. CARGO COMPARTMENT WAS REPAIRED PER ER/A 619586-14 REV. ORIGINAL SECTION I PERMANENT REPAIR.

Part: PRESSURE DECK — CRACKED (ZONE 100) · airframe 68,882 hrs · 32,421 cycles

(LOG 0499059) CRACKS ON LH VERTICAL PRESSURE DECK WEB WERE FOUND AS FOLLOW: THREE CRACKED HOLES IN THE ATTACH ANGLE, (HOLE 3,4 & 5), FOUR CRACKED HOLES IN VERTICAL PRESSURE DECK WEB (HOLES 1, 2, 3 & 4) AND TWO CRACKED HOLES IN THE VERTICAL STIFFENERS (HOLES 2 & 3). LH VERTICAL PRESSURE DECK WEB WAS REPAIRED PER ER/A 619577-14AD.

Part: SEAT TRACK — BROKEN (ZONE 200) · airframe 68,882 hrs · 32,421 cycles

(LOG 0497061) SEAT TRACK BROKE ON CROWN AREA ( 2 PLACES) BTW BSTA 500B AND 500E LBL 24.751. EAT TRACK (2 PLACES) BTW BSTA 500B AND 500E LBL 24.751 WERE REPAIRED PER B737-800 SRM 53-00-52-2R PROCEDURE 4 REPAIR 4.

Part: ACCESS DOOR — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,882 hrs · 32,421 cycles

(LOG 0491983) WORK SHOP INTERIOR SHEET METAL: CORROSION ON TRIM UNDER OF THE DOOR ACCESS A417 (1EA) AND A423 (1EA) AT GALLEY 4. TRIM UNDER OF THE DOOR ACCESS A417 (1EA) AND A423 (1EA) AT GALLEY 4 WERE REPLACED PER ER/A NO. 619671-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 619671-14 REV. 0 AND REV. 1.

Part: STRINGER — CORRODED (ZONE 100) · airframe 68,882 hrs · 32,421 cycles

(LOG 0488707) CORROSION ON STRINGER FLANGES UP/LOW SIDES BTW STA. 520 TO 540, S-27R (1EA) AND S-27L(1EA) INSIDE OF AIR CONDITION BAY AT FWD. CARGO COMPARTMENT. STRINGER BTW STA 520 T0 540 AND S-27R WAS REPAIRED PER B737-800 SRM 53-00-03-2R PROCEDURE 3 REPAIR 3.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,882 hrs · 32,421 cycles

(LOG 0480404) CORROSION ON SIDE PLATE UPPER AND LOWER SURFACE BTW STA 500 TO 500I LH SIDE AT FWD CARGO COMP. SIDE PLATE BTW STA 500 TO 500I LH SIDE AT FWD CARGO WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,882 hrs · 32,421 cycles

(LOG 0475424) CORROSION ON STRINGER TIP WAS FOUND BTW STA.520 TO 540 AND S-28R INSIDE OF AIR CONDITION BAY AT FWD. CARGO COMPARTMENT. STRINGER TIP BTW STA .520 TO 540 AND S-28R INSIDE OF AIR CONDITION BAY WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,882 hrs · 32,421 cycles

(LOG 0476429) CORROSION ON FLOOR STRINGER 13RBL BTW STA 787 TO STA 827 AT AFT CARGO COMPARTMENT. FLOOR STRINGER 13RBL BTW STA 787 TO STA 827 WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: FRAME — DENTED (ZONE 100) · airframe 68,882 hrs · 32,421 cycles

(LOG 0468100) DENT ON FRAME STA 500D AND BTW S26L AND S25L AT FWD CARGO COMP. FRAME STA 500D AND BTW S26L AND S25L WAS REPAIRED PER B737-800 SRM 53-30-07-2R PROCEDURE 1 REPAIR 1.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,882 hrs · 32,421 cycles

(LOG 0469656) CORROSION ON INTERCOSTALS BTW STA 500E TO STA 500I S-26L AT FWD CARGO COMPARTMENT. INTERCOSTALS BTW STA 500E TO STA 500I S-26L (4 EAS) AT FWD CARGO COMPARTMENT WERE FABRICATED AND REPLACED PER DWG 143A7505 REV. B AND B737-800 SRM 51-40-02-0G.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,882 hrs · 32,421 cycles

(LOG 0468187) CORROSION ON LH AFT DOOR FLOOR SUPPORT FROM STA 945 TO 990 APROX LBL 55. LH AFT DOOR FLOOR SUPPORT FROM STA 945 TO 990 APPROX LBL 55 WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,882 hrs · 32,421 cycles

(LOG 0469663) CORROSION ON FLOOR STRINGERS 3LBL/3RBL BTW STA 767 TO STA 777 AT AFT CARGO COMPARTMENT. REPAIRED PER B737-800 SRM 53-00-53-2R PROCEDURE 2 REPAIR 2.

Part: FRAME — DENTED (ZONE 100) · airframe 68,882 hrs · 32,421 cycles

(LOG 0468087) DENT ON FRAME STA 500D AND BTW S26L AND S25L AT FWD CARGO COMP. FRAME STA 500D AND BTW S26L AND S25L WAS REPAIRED PER B737-800 SRM 53-30-07-2R PROCEDURE 1 REPAIR 1.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,882 hrs · 32,421 cycles

(LOG 0467880) CORROSION ON FLOOR BEAM AT STA 986.5 FROM RBL 45 TO LBL 45. PAX CAB. FLOOR BEAM AT STA 986.5 FROM RBL 45 TO LBL 45. PAX CAB WAS REPAIRED PER B737-800 SRM 53-70-51-2R PROCEDURE 4 REPAIR 4.

Part: FRAME — DENTED (ZONE 100) · airframe 68,882 hrs · 32,421 cycles

(LOG 0468082) INITIAL INSPECTION: DENT ON FRAME STA 500D AND BTW S26L AND S25L AT FWD CARGO COMP. REPAIRED PER B737-800 SRM 53-30-07-2R PROCEDURE 1 REPAIR 1.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,882 hrs · 32,421 cycles

(LOG 0466259) INITIAL INSPECTION: CORROSION ON FLOOR BEAM OF STA 947.5 BTW LBL 50 AND RBL 50. FLOOR BEAM OF STA 947.5 BTW LBL 50 TO RBL 50 WAS REPAIRED PER B737-800 SRM 53-70-51-2R PROCEDURE 5 REPAIR 5.

Part: FLOORBEAM — CORRODED (ZOEN 200) · corrosion level 2 · airframe 68,882 hrs · 32,421 cycles

(LOG 0465748) CORROSION ON FLOOR SUPPORT OF STA 950 BTW LBL 51, LBL 46, LBL 40 AND LBL 24. NEW FLOOR SUPPORTS OF STA 950 BTW LBL 51, LBL 46, LBL 40 AND LBL 24 WERE DRILLED PER B737-800 SRM 51-40-05-0G & REMOTION AND INSTALLATION IS UNDER NRC 00468.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,882 hrs · 32,421 cycles

(LOG 0465368) CORROSION ON LH SIDE PLATES (UPPER AND LOWER SURFACE) BTW STA 727 TO STA 847 AT AFT CARGO COMPARTMENT. LH SIDE PLATES (UPPER AND LOWER SURFACE) BTW STA 727 TO STA 847 WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: FRAME — DENTED (ZONE 100) · airframe 68,882 hrs · 32,421 cycles

(LOG 0462798) DENT ON FRAME STA 500A BTW S26L AND S25L AT FWD CARGO COMP. FRAME STA 500A BTW S26L AND S25L WAS REPAIRED PER B737-800 SRM 53-30-07-2R REPAIR 1.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,882 hrs · 32,421 cycles

(LOG 0462363) CORROSION ON FLOORBEAM, STA 992 RBL 35-45 AND STA 992 LBL 35-45 AT PAX CABIN. R&R R2 WINDOW AND #1 HEAT CONTROL UNIT. REF B737 AMM 56-12 AND 30-41. LEAK AND OPS CHECK GOOD OKAY FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,882 hrs · 32,421 cycles

(LOG 0457437) CORROSION ON FLOOR SUPPORT AT RBL 53 BTW STA 291.5 AND STA 345 IN PAX CABIN. FLOOR SUPPORT (CHORD)AT RBL 53 BTW STA 260 AND STA 360 IN PAX CABIN (W1) WAS REPLACED PER B737-800 SRM 51-40-02-0G PAR.4.B AND SRM 51-40-02-0G.

Part: FRAME — CRACKED (ZONE 200) · airframe 68,882 hrs · 32,421 cycles

(LOG 0455961) CRACK (0.250 IN LENGTH) ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA. 867 BTW S-8L & S-9L. FUSELAGE FRAME STA 867 BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.

Part: FRAME — CRACKED (ZONE 200) · airframe 68,882 hrs · 32,421 cycles

(LOG 0455149) CRACK (0.625 IN LENGTH) ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 380 BTW S-8R & S-9R AND CRACK (0.125IN LENGTH) ON FUSELAGE FRAME AT OUTBOARD FASTENER HOLE STA 380 BTW S-8R & S-9R. RH FUSELAGE FRAME STA 380 BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B. )

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,882 hrs · 32,421 cycles

(LOG 0455125) CORROSION ON FLOOR SUPPORT AT RBL 11 BTW STA 312 AND STA 328 IN PAX CABIN. FLOOR SUPPORT AT RBL 11 BTW STA 312 AND STA 328 IN PAX CABIN WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: FRAME — CRACKED (ZONE 200) · airframe 68,882 hrs · 32,421 cycles

(LOG 0455951) CRACK (0.125 IN LENGTH) ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 500C. BTW S-8L & S-9L. FUSELAGE FRAME STA 500C BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.

Part: FRAME — CRACKED (ZONE 200) · airframe 68,882 hrs · 32,421 cycles

(LOG 0455948) CRACK (0.500 IN LENGTH) ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 400 BTW S-8L & S-9L. FUSELAGE FRAME STA 400 BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.

Part: FRAME — CRACKED (ZONE 200) · airframe 68,882 hrs · 32,421 cycles

(LOG 0455944) CRACK (0.796 IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 380 BTW S-8L & S-9L AND CRACK (0.125IN LENGTH) ON FUSELAGE FRAME AT OUTBOARD FASTENER HOLE STA 380 BTW S-8L & S-9L. FUSELAGE FRAME STA 380 BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.

Part: FRAME — CRACKED (ZONE 200) · airframe 68,882 hrs · 32,421 cycles

(LOG 0455956) CRACK (0.500 IN LENGTH) ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 727B. BTW S-8L & S-9L. FUSELAGE FRAME STA 727B BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.

Part: FRAME — CRACKED (ZONE 200) · airframe 68,882 hrs · 32,421 cycles

(LOG 0455181) CRACK (0.500 IN LENGTH) ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 500D. BTW S-8R & S-9R. RH FUSELAGE FRAME STA 500D BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.

Part: FRAME — CRACKED (ZONE 200) · airframe 68,882 hrs · 32,421 cycles

(LOG 0455208) CRACK (0.125 IN LENGTH) ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 867. BTW S-8R & S-9R. RH FUSELAGE FRAME STA 867 BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.

Part: PLATE — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,882 hrs · 32,421 cycles

(LOG 0456232) CORROSION ON RH SIDE PLATES (UPPER AND LOWER SURFACE) BTW STA 727 TO STA 767 AT AFT CARGO COMPARTMENT. RH SIDE PLATE BTW STA 727 TO STA 767 AT AFT CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: FRAME — CRACKED (ZONE 200) · airframe 68,882 hrs · 32,421 cycles

(LOG 0455202) CRACK (0.250 IN LENGTH) ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 827. BTW S-8R & S-9R. RH FUSELAGE FRAME STA 827 BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.

Part: SKIN — BROKEN (ZONE 100) · airframe 68,882 hrs · 32,421 cycles

SHIP 3731 - BROKEN CUTOUT SKIN OF EXTERNAL POWER RECEPTACLE FWD EDGE. SUMMARY OF NRC 00024: SKIN OF EXTERNAL POWER RECEPTACLE FWD EDGE WAS REPAIR PER B737-800 SRM 53-10-15-2R-5. (LP #0454660)

Part: WEB — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 68,882 hrs · 32,421 cycles

(LOG 0454562) CORROSION ON WEB OF LOWER SILL AREA AT AFT CARGO COMPARTMENT DOOR SURROUND STRUCTURE. WEB OF LOWER SILL AREA AT AFT CARGO COMPARTMENT DOOR SURROUND STRUCTURE WERE REPLACED PER B737-800 SRM 51-40-02-0G.

Part: SKIN — DAMAGED (ZONE 100) · airframe 68,882 hrs · 32,421 cycles

(LOG 0454672) BROKEN CUTOUT SKIN OF EXTERNAL POWER RECEPTACLE FWD EDGE. SKIN OF EXTERNAL POWER RECEPTACLE FWD EDGE WAS REPAIRED PER B737-800 SRM 53-10-15-2R-5.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 68,882 hrs · 32,421 cycles

(LOG 0452990) CORROSION ON FLOOR SUPPORT AT LBL 53 AND STA 344 IN PAX CABIN. FLOOR SUPPORT AT LBL 53 AND STA 344 IN PAX CABIN WAS REPLACED PER B737-800 SRM 51-40-02-0G.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 67,259 hrs · 31,716 cycles

(LOG 0102471) EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:11D. RESERCURED. EMERGENCY LIGHT AT 11D IAW B737 AMM 33-51. OK FOR SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 67,025 hrs · 31,607 cycles

(LOG 9593504) AT ABOUT 1000' AGL WHILE ON APPROACH TO TPA, THE FA, SMELLED A ELECTRICAL AND THEN A CHEMICAL SMELL IN THE FWD GALLEY AREA, UPON LANDING, THE SMELL DISSIPATED. FOUND PED POWER RECEPTACLE 1 A&B CHARRED. C/W NOGO ODI FOR ATA 2172. OK FOR SERVICE.

Part: PLATE — BROKEN (NOT REPORTED) · airframe 64,972 hrs · 30,593 cycles

(LOG 9688812) DURING INSPECTION FOUND AFT CARGO NET TIE DOWN BROKEN. R+R'D TRACK FITTING PER IPC 25-52-51-09 ITEM 32. OPS CHECK GOOD.

Part: NONE — NONE · airframe 61,874 hrs · 29,206 cycles

(LOG 2076116) DURING INSPECTION FOUND EMERGENCY FLOOR LIGHTING DAMAGED. 20D EMERGENCY FLOOR LIGHT REPAIRED PER B737 AMM 33-51. OPS CHECK OK.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,983 hrs · 28,798 cycles

(LOG 1930827) DURING INSPECTION ELONGATED HOLES WERE FOUND (3EAS) ON FUSELAGE SKIN LH SIDE AT NLG JACK POINT AREA. PERMANENT REPAIR ON HOLES (3EAS) OF FUSELAGE SKIN LH SIDE AT NLG JACK POINT AREA WAS PERFORMED PER ETI-37-21-484 REV. 3 AND ER/A 593769-14.

Part: FAIRING — DAMAGED (WNG-BDY FAIRING) · airframe 60,965 hrs · 28,788 cycles

(LOG 1927749) DURING CCK AT QRO, WHILE PERFORMING EM 5352-01035-02 INSPECTIONS TO THE LOWER AFT WING TO BODY FAIRING PANEL 194E AND SUPPORT STRUCTURE, ELONGATED HOLES (QTY 7) WERE FOUND COMMON TO THE NUT HOLES ON THE STA 727+2.7 & 727C SUPPORT FRAMES. MAINTENANCE REPAIRED DAMAGE PER ETI 37-21-475 REV 3 AND ERA 593629-14AD.

Part: MODULE — INOPERATIVE (NR 1) · airframe 60,951 hrs · 28,779 cycles

SHIP 3731 -ATB- DUE TO ENGINE FAULT LIGHT ILLUMINATED WITH BOTH EECS IN ALT. ALSO HAVE A CAPT. ALTITUDE AND AIRSPEED DISAGREE. ON APPROACH HAD A FLAP DISAGREE MESSAGE. FOUND CAPTAIN'S PITOT LINE DISCONNECTED FROM ADM. REPLACED CAPTAIN'S PITOT AND STATIC ADMS. REPLACED LEFT AOA SENSOR. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: DISPLAY — INOPERATIVE (NR 1) · airframe 60,951 hrs · 28,779 cycles

SHIP 3731 -ATO- AT >80 KNOTS DUE TO ENG MASTER CAUTION SIX PACK LIGHT ILLUMINATED. CORRECTIVE ACTION: PERFORMED EEC 1-2 BITE CHECKS, ADIRU 1-2 BITE CHECKS, FMC 1-2 BITE CHECKS AND EAU BITE CHECK. ALL NO TROUBLE FOUND. DEU-2 FAULT CODE 31-60012 OBSERVED THIS LEG. REPLACED DEU-2. REPLACED FIRST OFFICER'S 6 PACK LIGHT SWITCH PRECAUTIONARY. OPS CHECKS GOOD.

Part: FAN — FAILED (RECIRCULATION) · airframe 59,618 hrs · 28,199 cycles

LOG 6876130 AT TOP OF DESCENT FA REPORTED SMELLING SMOKE OR SOMETHING BURNING AFTER ONLY A FEW MINUTES OF ATTEMPTING TO DETERMINE. THE SOURCE THEY REPORTED THE SMELL WENT AWAY. REPLACED RIGHT RECIRC FAN PER B737 AMM 21-25.

Part: SELECTOR VALVE — LEAKING (MLG BRAKES) · airframe 59,441 hrs · 28,107 cycles

DE/HYD, DUE TO LOSS OF 'B' HYDRAULIC SYSTEM QUANTITY/FLUID. CORRECTIVE ACTION: MAINTENANCE REPLACED THE ALTERNATE BRAKE SELECTOR VALVE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,840 hrs · 27,256 cycles

(LOG 6988196) DURING INSPECTION FOUND EMERGENCY LIGHT INOP FROM ROW 23 TO ROW 33. R/R EMERGENCY LIGHT BATTERY PACK ZONE M1672 PER B737 AMM 33-51. OPS CHECK OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 57,828 hrs · 27,251 cycles

(LOG 6988186) DURING INSPECTION FOUND EMERGENCY EXIT LIGHS AT SEAT ROWS 10-16 INOPERATIVE. REPLACED BATTERY AT EMERGENCY POWER SUPPLY M1676 PER B737 AMM 33-51. ALL LIGHTS OPS OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,257 hrs · 26,533 cycles

(LOG 5375275) DURING INSPECTION FOUND FWD EMERGENCY LIGHTS BATTERY AND CHARGER AT FWD LT GALLEY LOCATION BAD. REPLACED EMERGENCY LIGHT BATTERY AND CHARGER AT LOC M1675 PER AMM 33-51. OPS CK GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 56,257 hrs · 26,533 cycles

(LOG 5375276) DURING INSPECTION FOUND FWD EMERGENCY LIGHTS BATTERY AND CHARGER AT FWD RT GALLEY LOCATION BAD. REPLACED EMERGENCY LIGHT BATTERY AND CHARGER AT LOC M1674 PER AMM 33-51. OPS CK GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 56,039 hrs · 26,452 cycles

DURING INSPECTION FOUND MISSING RED FWD EMERGENCY LIGHTING COVER FIRST CLASS. MAINTENANCE INSTALLED LENS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,099 hrs · 25,272 cycles

CORROSION ON FLOORBEAM STA Y= 986.5 RBL 43 PAX CABIN. AREA WAS REPAIRED PER ER/A 571518-14 REV ORIG AND ETI 37-18-507 REV 5 ASSOCIATED ER/A 00-571518.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,097 hrs · 25,271 cycles

CRACKED RIB ON RT HORIZONTAL STABILIZER FROM STAB STA 92.70 (EHV). CRACKED RIB AT RT HORIZONTAL STABILIZER (STA 92.70) WAS REPAIRED PER SRM 55-10-09 REPAIR 5 AND REPAIR 4.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 53,097 hrs · 25,271 cycles

CRACK ON FWD SERVICE DOOR JAMB FWD EDGE ABOVE LONG 17R. AREAS WERE REPAIRED PER ER/A 571460-14 REV ORIGINAL AND ER/A 571461-14 REV. ORIGINAL, ETI -37-18-505 REV 1 AND ETI 37-18-485 REV ORIGINAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,097 hrs · 25,271 cycles

CRACK ON FRAME STA 500A STR 8R AND STR 9R PAX CABIN. AREA WAS REPAIRED PER ERA 571123-14AD REV ORIG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,097 hrs · 25,271 cycles

CRACK ON FRAME STA 500C STR 8R AND STR 9R PAX CABIN. AREA WAS REPAIRED PER ERA 571123-14AD REV ORIG. (ET) (HFEC) INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND AFTER TRIM OUT PER ER/A 571123-14AD REV ORIGINAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,097 hrs · 25,271 cycles

CRACK ON FRAME STA 827 SRT 8L AND SRT 9L PAX CABIN. FRAME WAS REPAIRED PER ERA 571123-14AD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,097 hrs · 25,271 cycles

CRACK ON FRAME STA 500D SRT 8L AND SRT 9L PAX CABIN. FRAME WAS REPAIRED PER ER/A 571123-14AD REV ORIGINAL SECTION L. DETAILED VISUAL INSPECTION AND HFEC INSPECTION WERE ACCOMPLISHED NO CRACKS WERE FOUND AFTER TRIM OUT PER ER/A 571123-14AD REV ORIGINAL SEC L & NDT MANUAL PART 6, 51-00 AND ASSOCIATED ER/A 00-571123.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,097 hrs · 25,271 cycles

CRACK ON FRAME STA 480 SRT 8L AND SRT 9L PAX CABIN. FRAME WAS REPAIRED PER ER/A 571123-14AD REV ORIGINAL DETAILED VISUAL INSPECTION AND HFEC INSPECTION WERE ACCOMPLISHED NO CRACKS WERE FOUND AFTER TRIM OUT PER ER/A 571123-14AD REV ORIGINAL ASSOCIATED ER/A 00-571123..

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,097 hrs · 25,271 cycles

INITIAL INSPECTION, CORROSION ON INTERCOSTAL AT FLOOR STRUCTURE AT AFT CARGO COMPARTMENT BTW STA 847-787 AND RBL13.84. LEVEL CORROSION 2, FLOOR STRUCTURE AT AFT CARGO COMPARTMENT BTW STA 767 TO 887 AND RBL13.84 WAS REPLACED PER SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,097 hrs · 25,271 cycles

INITIAL INSPECTION: CRACK ON FRAME STA 727B STR 8R AND STR 9R PAX CABIN. FRAME REPAIRED PER ER/A 571123-14AD REV ORIG. NO CRACKS WERE FOUND AFTER TRIM OUT PER ER/A 571123-14AD REV ORIGINAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,097 hrs · 25,271 cycles

INITIAL INSPECTION: CRACK ON FRAME STA 440 STR 8L AND STR 9L PAX CABIN. FRAME WAS REPAIRED PER ER/A 571123-14AD REV ORIG NO CRACKS WERE FOUND AFTER TRIM OUT PER ER/A 571123-14AD REV ORIGINAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,097 hrs · 25,271 cycles

INITIAL INSPECTION: CRACK ON FRAME STA 727D STR 8R AND STR 9R PAX CABIN. FRAME WAS REPAIRED PER ER/A 571123-14AD REV ORIG. NO CRACKS WERE FOUND AFTER TRIM OUT PER ER/A 571123-14AD REV ORIGINAL.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,097 hrs · 25,271 cycles

OUT LIMIT ON SIDEPLATE LT STA 727E TO 727F AT AFT CARGO COMPARTMENT. LEVEL CORROSION 2 AREA WAS REPAIRED PER SRM 53-00-53 REPAIR 6 FIG 203 AND 51-40. NO CRACKS WERE FOUND AFTER REMOVING DAMAGE.

Part: BULKHEAD — BROKEN (LT MLG WW) · airframe 53,097 hrs · 25,271 cycles

DURING INSPECTION FOUND BROKEN REAR SPAR, BULKHEAD LOWER LEFT WEB AND WEB BTW LBL 10-LBL 15 AT LT MLG WHEEL WELL, STATION 663. WEB BTW LBL 10 & LBL 15 AT LT MAIN LANDING GEAR WHEEL WELL STATION 663 WAS REPAIRED PER 57-10-10 REPAIR 2.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,097 hrs · 25,271 cycles

DURING INSPECTION FOUND CORROSION OUT OF LIMITS RT SIDE PLATE STA 727D TO 767 AT AFT CARGO COMPARTMENT. RT SIDE PLATE STA 727D TO 767 WAS REPLACED PER SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,097 hrs · 25,271 cycles

DURING INSPECTION FOUND CORROSION ON INTERCOSTAL BTW STA Y=311 TO S=325 BTW 7 AND 8 O'CLOCK. INTERCOSTAL WAS REPLACED PER SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,097 hrs · 25,271 cycles

DURING INSPECTION FOUND CORROSION ON FLOORBEAM STA Y= 947 AND RBL 50 PAX CABIN. FLOORBEAM STA Y= 947 AND RBL 50 PAX CABIN WAS REPAIRED PER SRM 53-70-51 REPAIR 5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,097 hrs · 25,271 cycles

DURING INSPECTION FOUND CORROSION ON FLOORBEAM STA Y= 947 AND RBL 50 PAX CABIN. FLOORBEAM STA Y= 947 AND RBL 50 PAX CABIN WAS REPAIRED PER SRM 53-70-51 REPAIR 5. FLOORBEAM STA Y= 947 AND RBL 50 PAX CABIN WAS REPAIRED PER SRM 53-70-51 REPAIR 5.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,097 hrs · 25,271 cycles

(LOG 0719379) DURING INSPECTION FOUND CORROSION OUT -LIMIT AREAS ON FLIGHT DECK FLOORS FROM STA= 244 LBL 1 AND STA= 251 LBL 1. FLIGHT DECK FLOORS FROM STA= 244 LBL 1 AND STA= 251 LBL 1 WERE REPAIRED PER SRM 53-10-51 REPAIR 2.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,530 hrs · 25,069 cycles

DURING INSPECTION FOUND AFT LEFT OVERHEAD AND LEFT SIDE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE R&R AFT LEFT OVHD EMERGENCY BATTERY PACK PER AMM 33-51-06-960-805. OPS CHK GOOD.

Part: RELAY — FAILED (ANTI SKID SYS) · airframe 50,019 hrs · 24,128 cycles

DURING FLIGHT, ANTI-SKID LIGHT ILLUMINATED. CREW DECLARED EMERGENCY PRIOR TO LANDING. FLIGHT LANDED WITHOUT FURTHER EVENT. MAINTENANCE REPLACED THE RELAY R627 IAW WDM 32-41-11.

Part: HINGE — CORRODED (LAV SERVICE DOOR) · airframe 48,685 hrs · 23,703 cycles

DURING INSPECTION FOUND CORROSION AFT HINGE ON AFT TOILET SERVICE DOOR ON LOWER FUSELAGE. MAINTENANCE REMOVED AND REPLACED HINGE ON AFT TOILET SERVICE DOOR. ON LOWER FUSELAGE AS PER SRM 51-40-02.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 48,685 hrs · 23,703 cycles

CRACK AT LOWER SKIN ON LE STA 133.15 AT LT HORIZONTAL STABILIZER. PERFORMED REPAIR ON LOWER INSPAR SKIN LOCATED BETWEEN LE STA 128 TO LE STA 138 AT LT HORIZONTAL STABILIZER AS PER SRM.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 42,548 hrs · 21,502 cycles

DURING INSPECTION, FOUND EMERGENCY ESCAPE PATH LIGHTS AT SEATS 24 AND 32 ARE INOPERATIVE. MAINTENANCE REPLACED WIRE HARNESS AT SEAT 32, R & R TERMINAL END ON SEAT 24. OPS TEST OK.

Part: SKIN — DAMAGED (BS 354) · airframe 39,976 hrs · 20,634 cycles

DURIING INSPECTION, FOUND DAMAGE AT FUSELAGE SKIN AT BS 354 BELOW S27L. MAINTENANCE REPAIRED IAW ERA 528892-14.

Part: SKIN — DENTED (BS 354) · airframe 39,975 hrs · 20,633 cycles

DURING INSPECTION FOUND DENT ON THE SKIN LOCATED AT BS 354 AND S29L. MAINTENANCE REPAIRED IAW ERA 528892.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,420 hrs · 19,363 cycles

DURING INSPECTION, FOUND EMERGENCY LIGHT BATTERY PACKS FAILED TIME TEST. MX REPLACED BATTERY PACKS IAW AMM 33-51.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,699 hrs · 19,472 cycles

DURING INSPECTION, FOUND FRAME CRACKED AD2009-01-02. MX REPAIRED IAW ERA 506369-14AD.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 33,045 hrs · 18,106 cycles

DURING EMERGENCY LIGHT CHECK, FOUND FWD EMERGENCY EXIT OVERWING DOOR LIGHT INOP. REPLACED BALLAST AND TESTS OK.

Part: SLIDE — FOULED (R1 DOOR) · airframe 31,755 hrs · 17,638 cycles

WHILE PERFORMING OPN 68050 R1 DOOR SLIDE DEPLOYMENT DOOR DID NOT OPEN FULLY. FOUND MANUAL INFLATION CABLE WRAPPED IN DOOR STRUCTURE PREVENTING DOOR FROM OPENING PROPERLY. REPLACED SLIDE.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 29,894 hrs · 16,957 cycles

LEFT FWD OVERWING HATCH, EMERGENCY EGRESS EXIT SIGN HAS 3 OF 4 BULBS INOPERATIVE. RELAMPED CHECKS OK.

Part: CONNECTOR — LOOSE (CABIN) · airframe 28,110 hrs · 16,246 cycles

EMERGENCY EGRESS AISLE LIGHTING INOPERATIVE BETWEEN ROWS 4-10. RE-SECURED LIGHT CONNECTOR AT SEAT 4C AND 10D, SYSTEM NOW CHECKS OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,055 hrs · 16,223 cycles

EMERGENCY EGRESS AISLE LIGHTING BETWEEN ROWS 1 AND 4 ARE INOPERATIVE. MX REPLACED EMERGENCY LIGHT POWER SUPPLY, CHECKS GOOD.

Part: ENGINE — UNSERVICEABLE (NR 1) · airframe 21,306 hrs · 13,553 cycles

NR 1 ENGINE INFLIGHT SHUTDOWN GOING THROUGH 10000 FT. ACFT MADE AN AIRTURN BACK TO SEA. ON ARRIVAL TO THE GATE, FOUND TURBINE BLADES IN TAILPIPE. MCC/OCC NOTIFIED. REPLACED NR 1 ENGINE.

Part: FILTER — DEFECTIVE (NR 1 ENGINE) · airframe 20,367 hrs · 13,197 cycles

AIR TURNBACK, OIL FILTER BYPASS CAUTION LIGHT LEFT ENG CAME ON IN CLIMBOUT. REDUCED THRUST - LIGHT WENT OUT WHEN THRUST REDUCED TO IDLE. INSPECTED CHIP DETECTORS, NO DEBRIS FOUND. INSPECTED AND REPLACED BOTH THE MAIN AND SCAVANGE OIL FILTERS PER M/M, ALL ITEMS LEAK CHECK OK. NO MESSAGE RETURNED ON ENGINE RUN. FWD TO MEL 79-00-02.

Part: BULB — BLOWN (LT FUSELAGE) · airframe 3,278 hrs · 4,086 cycles

IR-LT EXTERIOR EMERGENCY LIGHT JUST AFT OF WING INOP CA-RELAMPED SAME. OPS CKS NML.

Part: BOLT — LOOSE (COCKPIT WINDOW) · airframe 3,131 hrs · 3,893 cycles

CREW LOCKED THEMSELVES OUT OF COCKPIT EQUIPPED WITH SECURITY DOOR. F/O SLIDING WINDOW FAILED TO OPEN FROM OUTSIDE, REMOVED F/O WINDOW AND FOUND LOWER BEARING BOLT BACKED OUT PREVENTING EMERGENCY HANDLE FROM OPERATING PROPERLY. TIGHTENED SAME.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 2,061 hrs · 2,542 cycles

LEFT EXTERIOR LOWER AFT EMERGENCY EGRESS LIGHT INOP. RELAMPED SAME PER AMM, OPS CHECKS GOOD.

Part: STARTER — FAILED (NR 1 ENGINE) · airframe 1,239 hrs · 1,547 cycles

NR 1 ENG STARTER SHEARED ON INITIAL START. REPLACED NR 1 ENG STARTER AND SERVICED. WINDMILLED ENG AND NO LEAKS ON DUCT. OPN CHECKS NORMAL.

Part: COMPUTER — FAILED (STALL YAW) · airframe 455 hrs · 573 cycles

DURING CLIMB YAW DAMP LIGHT ILLUMINATED AND YAW DAMP SWITCHED OFF. CREW FELT AIRCRAFT WAS UNSAFE AND DECLARED AN EMERGENCY. REPLACED NR 1 STALL WX/YAW COMPUTER.