N33262

Part: AOA — FAULTED (ZONE 100) · airframe 74,742 hrs · 26,371 cycles

SPD LIM FLAG CAPT PFD NO VERTICAL FD GUIDANCE INTMT STICK SHAKER CA SIDE. REMOVED AND REPLACED CAPT AOA SENSOR REF AMM 34-21-05 OPS CHECK GOOD.

Part: AOA — FAULTED (ZONE 100) · airframe 73,931 hrs · 26,070 cycles

SPD LIM ON CA PFD W/ INTRMTNT VERT FD CMD BAR INTRMTNT STICK SHA KER AND SPEED TAPES REF L/P 4414719 FOR PART REPLACEMENT REMOVED AND REPLACED CAP AOA SENSOR REF AMM 34-21-05. OPS CHECK GOOD. ALL TESTS PASSED.ROTABLE PARTS CHG:TT # 1915849 SN OFF 2217 PN OFF 29-3412-9-0001SENSOR, ANGLE O OFF 29-3412-9-0001 2217 ON 29-3412-9-0001 2226.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 72,870 hrs · 25,668 cycles

SEAT 32C AND 35 C SEAT MOUNTED EMER. LIGHTS INOP. REPLACED BOTH SEATS EMER. LIGHT ASSY PER AMM. OPE' CHK OK.

Part: SKIN — CRACKED (ZONE 100) · airframe 72,579 hrs · 25,562 cycles

LH #3 WINDOW FRAME, E-F POST THIRD (LOWER CORNER) FASTHER HOLE WITH CRACK SIGNAL INDICATION, DIRECTION OF INDICATION 9 O''CLOCK POSITION. (REF: AAR NR 1000016743) REPAIRED LH NO. 3 WINDOW FRAME IAW EA 5310-08195 OP 003, AAR RFD EA NO. 240547 & ECRA 5310-08430 PART 1, STEP 1, REF: AAR RFD NR 1000016743 REF LP NO. 9518614 & 9520275 FOR DIP REQUIREMENTS. ITEM NOT IDENTIFIED AS RII PER GMM 09-25-05. HIS ITEM GENERATED FOR REPORTING PURPOSES ONLY.

Part: BONDING STRAP — CORRODED (LH WING) · airframe 72,579 hrs · 25,562 cycles

CORROSION BENEATH THE TWO FUEL BOOST PUMP BONDING STRAPS AT FRONT SPAR LEFT WING. (REF: AAR NR 1000016757)

Part: SKIN — CRACKED (ZONE 300) · airframe 72,579 hrs · 25,562 cycles

LH HORIZONTAL STABILIZER, LOWER SKIN, ONE CRACK INDICATION AT STA 101.9, LENGTH 1 1/2 INCHES, 12 INCHES INFRONT REAR SPAR. (REF: AAR NR 1000016457)

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 72,579 hrs · 25,562 cycles

EMERGENCY LIGHTS BATTERY PACK M1695 FAILS CAPACITY CHECK (REF. A AR NR 1000016319).REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK M1695 IAW B737 A.M.M. 33-51-06-60-805, TEST OK.

Part: SKIN — CRACKED (ZONE 300) · airframe 72,579 hrs · 25,562 cycles

RH HORIZONTAL STABILIZER, LOWER SKIN, ONE CRACK INDICATION AT STA 129.5, LENGTH 1 3/4 INCHES, 27 INCHES INFRONT REAR SPAR. (REF: AAR NR 1000016458)

Part: SKIN — DENTED (ZONE 800) · airframe 72,579 hrs · 25,562 cycles

PER CUST REQ REMOVE AND REPLACE FWD CARGO DOOR EXTERNAL SKIN LOG PAGE NO. 7476253 (REF. AAR NR 1000016455). DENTS FOUND AT FWD CARGO DOOR STA 453.5 1" X 1/16"ENTRY BY HDN CONTRACT MX FAA #2760825.

Part: SKIN — DENTED (ZONE 800) · airframe 72,579 hrs · 25,562 cycles

PER CUST-REQ REMOVE AND REPLACE AFT CARGO DOOR EXTERNAL SKIN LOG NO. 5665769 (REF. AAR NR 1000016454).

Part: LIGHT — INCORRECT (G4 GALLEY- NEXT) · airframe 71,278 hrs · 24,970 cycles

EMERGENCY LIGHTS- R2 DOOR EXIT LOCATOR LIGHT MOUNTED TO G4 GALLEY IS MOUNTED INCORRECTLY. FOUND INCORRECT LENS INSTALLED AND LIGHT BASE BROKEN. REPLACED 00-0595-3-2273,QTY :2 00-0583-3-6868,QTY :2 29-3351-3-0011,QTY BROKEN EXIT LOCATOR LIGHT ON G4 GALLEY ADJACENT TO R2 DOOR IAW :1 AMM 33-51-01-960-802. OPS CHK GOOD IAW AMM 33-51-14-960-802. REF CONFIG DWG 3351DD15945E FOR CORRECT LENS.PARTS USED: VERIFIED IDT REQUIREMENTS PER GMM AND AMM

Part: LIGHT — INCORRECT (LAV D) · airframe 71,278 hrs · 24,970 cycles

EMERGENCY LIGHTS- LAV D FORWARD EPL LIGHT HAS INCORRECT LENS INSTALLED. REPLACED FORWARD LAV MOUNT EPL LIGHT LENS ON LAV D IAW AMM 33-51-00-710-801. 33-51-14-960-802. REF IFM(CMM) 25-40-09 LIGHT L21-1 ON WIRE DIAGRAM FOR CORRECT LIGHT P/N. NO REF FOR THIS LIGHT IN CONFIG DWG 3351DD15945E FOR CORRECT LENS. OPS CHK GOOD IAW AMM VERIFIED IDT REQUIREMENTS PER GMM AND AMM

Part: LENS — INCORRECT (AFT GALLEY NEAR) · airframe 71,278 hrs · 24,970 cycles

EMERGENCY LIGHTS- L2 DOOR EXIT LOCATOR LIGHT MOUNTED TO G4 GALLEY HAS INCORRECT LENS. REPLACED EXIT LOCATOR LIGHT LENS ON G4 GALLEY ADJACENT TO L2 DOOR IAW AMM 33-51-01-960-802. OPS CHK GOOD IAW AMM 33-51-14-960-802. REF CONFIG DWG 3351DD15945E FOR CORRECT LENS. VERIFIED IDT REQUIREMENTS PER GMM AND AMM

Part: CHECK VALVE — MISSING (LH PACK) · airframe 71,015 hrs · 24,856 cycles

LEFT PACK LIGHT IS ON WITHOUT MASTER CAUTION RECALL ACCOMPLISHED BITE OF PACK TEMP CONTROLLERS REF FIM 21-62 TASK 801. LEFT TEMP CONTROLLER FAULTING TCV. FOUND FAN BYPASS CHECK VALVE DOOR MISSING. REF FIM 21-53 TASK 820 FOUND BYPASS CHECK VALVE DOOR MISSING. REF LOG 7197306 FOR PDA LOGPAGE. ADDED MFG DDP C/W PER MEL. REMOVED AND REPLACED DIFFUSER ASSY PER AMM 21-51-03-400-804-002. OPS CHECK GOOD, NO LEAKS NO RECALL LIGHTS NOTED. ENSURE DISPATCH DEVIATION PROCEDURE IS REVERED BEFORE RETURNING THE AIRCRAFT TO SERVICE. PERFORMED PACK TEMPERATURE CONTROL - BITE PROCEDURE IAW FIM 21-62-801. NO FAULTS NOTED.

Part: DOOR LATCH — UNKNOWN (1L DOOR) · airframe 69,043 hrs · 23,922 cycles

EXTERIOR DOOR LATCH HANDLE OPENED DURING FLIGHT UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V919611 PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC RELATED WORK ORDER 000000003076662 AND PRTR ROWE, ANDREW (V919611) PER CREW AT DOOR 1L HEARD NOISE HEARD AFTER TAKEOFF.CREW LOOKED THROUGH ENTRY DOOR WINDOW AND FOUND EXTERIOR HANDLE IN VIEW. OPERATED ENTRY DOOR SEVEAL TIMES PER AMM 52-11-00-860-801 AND -802 OPS CK GOOD. ROWE, ANDREW (V919611) PER CREW AT DOOR 1L HEARD NOISE HEARD AFTER TAKEOFF.CREW LOOKED THROUGH ENTRY DOOR WINDOW AND FOUND EXTERIOR HANDLE IN VIEW. OPERATED ENTRY DOOR SEVEAL TIMES PER AMM 52-11-00-860-801 AND -802 OPS CK GOOD. ADD EMP:V919611

Part: HOUSING — BROKEN (COACH SEAT AISLE) · airframe 68,855 hrs · 23,839 cycles

SEAT 37ABC EMERGENCY AISLE PATH UNDER SEAT LIGHT HOUSING OFTEN FOUND BROKEN AND WIRES BECOME PULLED OUT OF HOUSING AND SHORTING OUT CAUSING FUSE ON BATTERY PACKS TO BLOW. AS A CONSEQUENCE, MULTIPLE AISLE PATH LIGHTS RENDERED INOP.

Part: FASTENER — MISSING (L WING PNL 551BT) · airframe 68,345 hrs · 23,615 cycles

PDA 3 LT WING PANEL 551BT HAS 11 FASTENERS MISSING IN A ROW I/B SIDE. VERIFIED NUT PLATES ARE THERE AND NOT STRIPPED. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V925544 PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC RELATED WORK ORDER 000000003069066 AND PRTR JONES, ALLEN (V925544) INSTALLED MISSING FASTENERS. OK FOR CONTINUED SERVICE JONES, ALLEN (V925544) INSTALLED MISSING FASTENERS. OK FOR CONTINUED SERVICE ADD EMP:V925544

Part: FASTENER — MISSING (LT WING PANEL 55) · airframe 68,324 hrs · 23,602 cycles

MUTIPLE FASTENERS APPEAR TO BE MISSING ON TOP OF LEFT WING NEAR EMER EXIT UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V925544 PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC RELATED WORK ORDER 000000003069066 AND PRTR JONES, ALLEN (V925544) INSTALLED MISSING FASTENERS IN PANEL 551BT. OK FOR CONTINUED SERVICE. JONES, ALLEN (V925544) INSTALLED MISSING FASTENERS IN PANEL 551BT. OK FOR CONTINUED SERVICE. ADD EMP:V925544

Part: TIRE — DAMAGED (1&2) · airframe 65,193 hrs · 22,268 cycles

LEFT TIRE BLOW OUT NORMAL LANDING AND TAXI 1 TIRE FLAT AND SEIZED ON BRAKE. SUSPECT WHEEL BEARING FAILURE. ADDED PICTURES. HUBCAP AND ATTACHING HARDWARE REMOVED AND REMOVED 1 BLOWN TIRE AND WHEEL ASSEMBLY USING UNCONVENTIONAL PICTURE REMOVED WHEEL DELIVERED TO HANGAR. MEANS. INNER RACE OF INNER BEARING SIEZED TO AXLE. REMOVED LH MLG AXEL ASSY IAW 32-11-85-000-801. ADD EMP:U181398,U150635 INSTALLED 1 MLG AXLE IAW B737 AMM 32-11-85-420-801 UP TO AND 1 AND 2 BRAKES REPLACED SN OFF 7395 AXLE, MLG, ASSY OFF 29-3211-9-9050 7395 ON 29-3211-9-9150 4176 NUMBER 1 AND NUMBER 2 TRANSDUCERS REPLACED REF LOG PAGES 8133122 INSTALLED NEW 1 AND 2 MLG TIRES, REF LOG PGS 8117269 AND AND 8133118. 8133069 COMPLETED LT GEAR AXLE INSTALL PER 32-11-85-420-801, FROM STEP F(14) THRU COMPLETION. ADD EMP:U138140

Part: BRAKE — DAMAGED (#!) · airframe 65,109 hrs · 22,229 cycles

#1 BRAKE DAMAGED DUE TO SUSPECTED WHEEL BEARING FAILURE. REPLACED NUMBER # 1 BRAKE IAW 32-41-41. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1935536 SN OFF 1388 BRAKE, MLG, CAR OFF 60-3241-9-0001 1388 ON 60-3241-9-0001 4389

Part: LIGHT — BROKEN (ROW 15,20) · airframe 64,174 hrs · 21,860 cycles

SEAT MOUNTED EMERGENCY EXIT LIGHTS (RED) BROKEN AT ROW 15, 20 ADDED PARTS. NONE IN STOCK. 99-3350-3-0009. REPLACED LIGHT ASSY AT BOTH LOCATIONS REF AMM 33-51-11-960-802, BOTH CHECK GOOD ACP INSPECTION OF ROW 15 AND 20, FOUND SECURED, LIGHTS OPERATE NORMAL REF AMM 35-51-11-960-802

Part: SKIN — DENTED (B.S 182 STR 12R) · airframe 64,082 hrs · 21,821 cycles

FOUND DENT AT UPPER EXTERNAL FUSELAGE SKIN AT B.S 182 STR 12R JUST ABOVE F/O PITOT PROBE RT SIDE REF AAR N/R 9636184 REPAIRED DENT AT FUSELAGE SKIN STA 182 STR 12R JUST ABOVE F.O PITOT PROBE PER EC/RA 5331-02776 NEV IR AND RES WI 2017692-32. REFER TO ELB LP 7265535 AND 7265686 FOR DTA DIPS CREATED FOR REPETITIVE INSP / PERMANENT REPAIR. ADD EMP:V891438 REPAIRED DENT AT FUSELAGE SKIN STA 182 STR 12R JUST ABOVE F.O PITOT PROBE PER EC/RA 5331-02776 NEV IR AND RES WI 2017692-32. REFER TO ELB LP 7265535 AND 7265686 FOR DTA DIPS CREATED FOR REPETITIVE INSP / PERMANENT REPAIR.

Part: NONE — CRACKED (RBL 40-45.64) · airframe 64,082 hrs · 21,821 cycles

CRACK FOUND ON CENTER WING REAR SPAR VERTICAL PRESSURE WEB BETWEEN RBL 40 TO RBL 45.64 (BETWEEN WL 200.6 AND 192.0) CRACK LENGTH : 0787" STA 663. (REF AAR NR 9635556) ACCOMPLISHED REPAIR AT CENTER WING REAR SPAR VERTICAL PRESSURE WEB BETWEEN RBL 40 TO RBL 45.64 (BETWEEN WL 200 AND 192) STA 663 IAW B737-800 SRM 57-10-10-2R-3 FIGURE 204. ADD EMP:V913144

Part: BULKHEAD — CRACKED (LBL 40.00-45.64) · airframe 64,082 hrs · 21,821 cycles

CRACK FOUND ON CENTER WING REAR SPAR VERTICAL PRESSURE WEB BETWEEN LBL 40.00 & LBL 45.64 ( BETWEEN WL 200.6 & 192.0 ) CRACK LENGTH : 1.575" REF. AAR N/R: 9635555 REMOVED DAMAGED AREA . FABRICATED NEW FILLER AND DOUBLERS. INSPECTED BY: V915555 INSTALLED NEW FILLERS AND DOUBLERS ON CENTER WING REAR SPAR VERTICAL PRESSURE WEB AND LOWER ANGLE AS PER B737-800 SRM 57-10-10-2R-3,REPAIR 3,FIG. 204.ALTERNATIVE 2,PAGE 15 AND SRM 57-10-10-2R-6 REPAIR 6 FIG. 202.REF. AAR N/R: 9635555 ADD EMP:V920362

Part: BEAM — CRACKED (R1 DOOR) · airframe 64,082 hrs · 21,821 cycles

RI DOOR CRACKED AT LWR FWD CORNER NEXT TO CENTER BOX. (REF AAR NR 9635753) PARTIALLY REMOVED THE BRACKET AND FASTENERS AT R1 DOOR AT THE BOEING SRM 51-40-02 REV 73 DATED 10 JUL 2021. NEW BEAM WAS LWR FWD CORNER NEXT TO CENTER BOX IN REF WITH BOEING SRM 51- INTALLED ON THE R1 DOOR AS PER BOEING SRM 51-40-02 REV 73 DATED 40-02 REV 73 DATED 10 JUL 2021. THEN, REMOVED THE CRACKED BEAM 10 JUL 2021. IN THE R1 DOOR AS PER BOEING SRM 51-40-02 REV 73 DATED 10 JUL 2021. LOCATED AND DRILLED THE NEW BEAM ON THE R1 DOOR AS PER ADD EMP:V925560

Part: BEAM — CRACKED (R1 DOOR) · airframe 64,082 hrs · 21,821 cycles

RI DOOR CRACKED AT LWR FWD CORNER NEXT TO CENTER BOX. (REF AAR NR 9635753) PARTIALLY REMOVED THE BRACKET AND FASTENERS AT R1 DOOR AT THE BOEING SRM 51-40-02 REV 73 DATED 10 JUL 2021. NEW BEAM WAS LWR FWD CORNER NEXT TO CENTER BOX IN REF WITH BOEING SRM 51- INTALLED ON THE R1 DOOR AS PER BOEING SRM 51-40-02 REV 73 DATED 40-02 REV 73 DATED 10 JUL 2021. THEN, REMOVED THE CRACKED BEAM 10 JUL 2021. IN THE R1 DOOR AS PER BOEING SRM 51-40-02 REV 73 DATED 10 JUL 2021. LOCATED AND DRILLED THE NEW BEAM ON THE R1 DOOR AS PER ADD EMP:V925560

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,394 hrs · 21,153 cycles

CABIN BATTERY PACK M1676 IS INOPERABLE, SPT 7000518.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,394 hrs · 21,153 cycles

CABIN BATTERY PACK M1670 IS INOPERABLE, SPT 7000519.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,394 hrs · 21,153 cycles

FWD RT EMERGENCY LIGHT BATTERY PACK AND CHARGER BAD M1674, SPT 7 000516.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,394 hrs · 21,153 cycles

FWD LT EMERGENCY BATTERY M1675 IS BAD, SPT 7000517.

Part: CONTROL CABLE — OUT OF LIMITS (AILERONS) · airframe 56,079 hrs · 18,732 cycles

FLIGHT CONTROLS BINDING, AILERONS COULD NOT MOVE PAST 11:00 O`CLOCK POSITION. HAPPENED AT 500AGL, FOUND THE FIRST OFFICER`S CONTROL YOKE CATCHES AT THE 11 OCLOCK POSITION WHEN MOVED FROM THE CENTER POSITION. COMPLETED A DETAILED INSPECTION IAW FIM. FOUND THE AILERON CABLES AA AND AB 50 PERCENT LOW. TENSIONED THE CABLES TO CORRECT VALUE IAW AMM 27-11-00-820-801. ACCOMPLISHED FIM TASK 27-11-00-810-813, FOUND TO MOVE FREELY AFTER STEP 2,(D) 2 A.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,540 hrs · 18,105 cycles

EMERGENCY LIGHTS INOPERATIVE FROM ROWS 22 TO 38. REMOVED AND REPLACED POWER SUPPLY AND BATTERY IAW AMM 33-51-06-960-806, OPS NORMAL.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 54,540 hrs · 18,105 cycles

EMERGENCY EXIT SIGN DOES NOT TURN OFF AT ROW 22A WITH EMERGENCY LIGHTS ARMED, EXIT AND FLOOR LIGHT COME ON AND FLICKER. AFT ROW 22. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AND BATTERY. OPS CHECKED NORMAL.

Part: LENS — UNSECURE (EXIT SIGN) · airframe 54,013 hrs · 17,877 cycles

EXIT SIGN FELL OFF DOOR 2L . INSTALLED SERVICEABLE EMERGENCY EXIT LENS.

Part: THERMOCOUPLE — FAULTY (NR 2 ENGINE) · airframe 53,637 hrs · 17,734 cycles

NR 2 ENGINE OVER REDLINE, 5 SEC, JUST AFTER LIFTOFF. REDUCED THROTTLE AND TEMP CAME BACK TO NORMAL. EMERGENCY DECLARED. REPLACED THE T495S4 THERMOCOUPLE PROBE IAW AMM 77-21-01

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,415 hrs · 17,653 cycles

EMERG LIGHTS ON EXT OF RT SIDE OF A/C INOP. REPLACED M1695 AND M1671 POWER SUPPLY AND BATTERY PACK. OPS CHKS GOOD REF AMM 33-51-06.

Part: SKIN — DENTED (L1 DOOR) · airframe 50,989 hrs · 16,664 cycles

ON ARRIVAL, OBSERVED A DENT WITH MATERIAL DISPLACEMENT 37" AFT OF DOOR 1L. 22"AFT OF PRODUC TION SPLICE. AND 23" ABOVE SKIN LAP. DEPTH OF DENT IS .058" AND DEPTH OF GOUGES ARE .009 - .012 APPROXIMATELY. BLENDED GOUGES AND PERFORMEDEDDY CURRENT, NO CRACKS NOTED. REMAINING MATERIAL IS .033" DENT DIMENSIONS ARE W-2.9", L - 3.4 " D - .058". REF. SMRM 53-00-01 ALLOWABLE DAMAGE 1 PAGE 130. DAMAGE IS AT STA 380, STRINGERS 7L - 8L. SEE NON ROUTINE 498766 4 FOR ALODINE AND PAINT. PERMANENT REPAIR WITHIN 50 FLIGHT HRS. REPAIRED IN ACCORDANCE WITH EC/RA 5331-02125. SEE ATTACHED 44-00 08 FOR ALL WORK ACCOMPLISHED.DIP INITIATED, REPAIRED THE DENT AT BS 380 STR 7L-8L WITHIN 50 FLT HRS IAW AMM 53-00-01 ALL DMG 1 PG 130 AREA B.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 48,838 hrs · 15,918 cycles

LEFT HORIZONTAL STAB LOWER SKIN HAS A CRACK AT STATION 157.10. REPAIRED IAW SRM 55-10-01 REPAIR 11. ISSUED A DIP IAW SRM 55-10 -01 REPAIR 11 STEP 5 TABLE 204. PERFORM A DETAILED VISUAL INSPECTION & EXTERNAL LOW FREQUENCY EDDY CURRENT, LFEC, INSPECTION AT 56,000 TOTAL FLIGHT CYCLES & EVERY 9,000 FLIGHT CYCLES THEREAFTER. DIP 48158 INIT 56K FC TCFC. UNIT WILL AUTO ITO TO RIR 1683. R & R EVERY 9,000 FC.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 48,838 hrs · 15,918 cycles

RIGHT STABILIZER LOWER SKIN HAS A CRACK INDICATION AT APPROX STAB STATION 157.10, 23" AFT OF STAB FRONT SPAR. INSTALLED REPAIR DOUBLER IAW SRM 55-10-01 REPAIR 11. DIP INITIATED TO INSPECT THE EXTERNAL DOUBLER AT 56,000 TOTAL COMPONENT FLIGHT CYCLES WITH REPEAT INSPECTIONS EVERY 9,000 FLIGHT CYCLES.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 48,838 hrs · 15,918 cycles

ONE CRACK FOUND AT APPROX STABILIZER STATION 101.90, 20 INCHES FROM REAR SPAR, 2.5 INCHES INBD OF DRAIN HOLE, LT STABILIZER. INSTALLED REPAIR DOUBLER IAW SRM 55-10-01 REPAIR 11. DIP INITIATED TO INSPECT THE EXTERNAL DOUBLER AT 56,000 TOTAL COMPONENT FLIGHT CYCLES WITH REPEAT INSPECTIONS EVERY 9,000 FLIGHT CYCLES.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 47,120 hrs · 15,302 cycles

INBOARD SEAT TRACK IS CORRODED BETWEEN STATIONS 500C + 500D, SEAT ROWS 7 & 8 ABC, LBL 24. BLENDED & EVALUATED CORROSION ON INBD SEAT TRACK. DETERMINED OUT OF LIMITS IAW SRM 53-00-52. MATL ID BAC 1510-1304 + BAC 1520-27897178-T6511. FABRICATED SEAT TRACK SECTION & 2 EA SPLICES IAW SRM 53-00-5 2. LOCATED, DRILLED & INSTALLED IAW SRM SDR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 47,120 hrs · 15,302 cycles

OUTBOARD SEAT TRACK IS CORRODED BETWEEN STATIONS 500C & 500D, SEAT ROWS 7 & 8 ABC. BLENDED, EVALUATED CORROSION ON OTBD SEAT TRACK. DETERMINED TO BE OUT OF LIMITS IAW SRM 53-2-52. MATL ID BAG 1570-1304 AN OC 1520-2787 717B-7651 1 FDAB 1 SEAT TRACK SEAT SEER 2 SPLICES IAW SRM 53- 00-52. LOCATED, DRILLED & INSTALLED IAW SRM 53-00-2.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,120 hrs · 15,302 cycles

SUPPORT TASK, FOUND BATTERY PACK AT FS 952, WL 290, LBL 14 WILL NOT HOLD CHARGE. R & R TWO BATTERY PACKS. OPERATIONS CHECKED GOOD ALL IAW AMM 33-51-06 AT STATION 952, WL 290 & LBL 14.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,120 hrs · 15,302 cycles

SUPPORT TASK, FOUND BATTERY PACK AT FS 952, WL 290, RBL 14 WILL NOT HOLD CHARGE. R & R TWO BATTERY PACKS. OPERATIONS CHECKED GOOD ALL IAW AMM 33-51-06 AT STATION 952, WL 290 & LBL 14.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,120 hrs · 15,302 cycles

BATTERY PACK AT FS 500C+8, WL 213, RBL 67 WILL NOT HOLD CHARGE. R & R BATTERY PACK. OPERATIONS CHECKED GOOD IAW AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,120 hrs · 15,302 cycles

FOUND BATTERY PACK AT FS 565, WL 213, RBL 68 WILL NOT HOLD CHARGE. R & R BATTERY PACK. OPERATIONS CHECKED GOOD AMM-33-41-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,120 hrs · 15,302 cycles

FOUND BATTERY PACK AT FS 727C+13, WL 212, LBL 68 WILL NOT HOLD CHARGE. R & R BATTERY PACK. OPERATIONS CHECKED GOOD IAW AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,120 hrs · 15,302 cycles

BATTERY PACK AT FS 565, WL 213, LBL 68 WILL NOT HOLD CHARGE. R & R BATTERY PACK. OPERATIONS CHECKED GOOD IAW AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,120 hrs · 15,302 cycles

FOUND BATTERY PACK AT FS 322, WL 291, RBL 7 WILL NOT HOLD CHARGE. R & R BATTERY PACK. OPERATIONS CHECKED GOOD IAW AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,120 hrs · 15,302 cycles

FOUND BATTERY PACK AT FS 322, WL 291, LBL 7 WILL NOT HOLD CHARGE. R & R BATTERY PACK. OPERATIONS CHECKED GOOD IAW AMM 33-41-06.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,120 hrs · 15,302 cycles

FOUND BATTERY PACK AT FS 727C+13, WL 212, RBL 68 WILL NOT HOLD CHARGE. R & R BATTERY PACK. OPERATIONS CHECKED GOOD IAW AMM 33-51-06.

Part: ANTI-SKID VALVE — FAILED (LANDING GEAR) · airframe 40,615 hrs · 13,059 cycles

ANTI-SKID INOP LIGHT CAME ON AFTER TAKEOFF AND REMAINED ON THROUGHOUT FLIGHT. LIGHT EXTINGUISHED AFTER LANDING. R & R LEFT INBD ANTI-SKID VALVE IAW AMM 32-42-31, OPS AND LEAK CHECK GOOD. ACFT OK TO CONTINUE.

Part: RING — BROKEN (LT WING) · airframe 36,535 hrs · 11,622 cycles

LEFT WING NR 7 DRIP STICK RED OUTER RING IS BROKEN. REPLACED OUTER RING PER VENDOR CMM 28-40-11. OK TO CONTINUE. 29-2844-3-0001, 29-2844-3-0004 AND 00-0594-3-2990.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,710 hrs · 10,623 cycles

SUPPORT TASK RIGHT FRAME CRACKED AT STATION 380 BETWEEN STRINGE R 8 AND 9, PER EA 5310-04716 REV B STEP 4. REPAIRED IAW EA 5310-04716 REV B.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,274 hrs · 10,104 cycles

SEAT ROWS 14-21 & LT WING OVERWING EXIT EMERGENCY LIGHTS INOP. NEED BATTERY PACK 29-3351-3-0013 NIS MSY. ROBBED BATTERY PACK FROM SAME LOCATION FROM A/C 521, S/N 72027. REF LP 8618647. INSTALLED BATTERY PACK, OP CHECKS OK.

Part: FAN — INOPERATIVE (LT PACK) · airframe 10,784 hrs · 3,074 cycles

THE FLIGHT ATTENDANTS REPORTED GRAY SMOKE IN THE CABIN IN THE AREA AROUND THE OVERWING EXIT WHILE ENROUTE. THE ENTERTAINMENT SYSTEM WAS SECURED, CABIN LIGHTS WERE TURNED OFF AND THE IFE CIRCUIT BREAKERS WERE PULLED. THE SMOKE DISSIPATED AND THE FLIGHT WAS CONTINUED TO ITS ORIGINAL DESTINATION OF AUA WHERE IT LANDED WITHOUT FURTHER INCIDENT. THE LT RECIRCULATION FAN WAS RUN WITH THE IFE SYSTEM OPERATING FOR OVER TWO HOURS AND THE SMOKE COULD NOT BE DUPLICATED. THE LT RECIRCULATION FAN WAS REMOVED AND REPLACED IAW MM 21-25-02 AS A PRECAUTIONARY MEASURE.

Part: BATTERY — WEAK (MEGAPHONE) · airframe 9,386 hrs · 2,625 cycles

INSPECTION FOUND AFT PASSENGER CABIN MEGAPHONE WEAK. THE MEGAPHONE WAS REPLACED.