N37263

Part: ANTI-ICE VALVE — FAULTED (ZONE 400) · airframe 74,921 hrs · 26,647 cycles

ENGINE COWL ANTI-ICE LIGHT ON AT 60KTS, ABORTED TAKEOFF, LIGHT WENT OUT 160.1 POWER WAS PULLED BACK AND LIGHT WENT OFF. CREW UNABLE TO SAY WHICH SYSTEM HAD THE AMBER LIGHT ILLUMINATED. CREW REPORTED UNABLE TO TELL WHICH SIDE, MAYBE RT BUT BOTH PILOTS UNABLE TO BE SURE. OPENED BOTH NR 1 AND 2 ENGINE COWLS , INSPECTED ANTI-ICE SWITCH & VALVE CONNECTIONS , NO DEFECTS NOTED . PERFORMED GVI OF DUCTS, HARDLINES & HARDWARE IN THE ANTI-ICE SYSTEM , NO DEFECTS NOTED . LEADS TO REQUEST HIGH POWER RUNS OFF THE GATE FOR TROUBLESHOOTING. REPLACED NR 2 ENGINE TAI VALVE, OPS CHECKED GOOD IAW AMM 30-21-11-400-80. OPS TESTED ANTI ICE AT POWER. LIGHT REMAINED DIM WITH SWITCH ON. NO FAULTS FOUND.

Part: LIGHT — DAMAGED (ZONE 200) · airframe 74,230 hrs · 26,309 cycles

(EPL) INSPECTION -ROW 22 EMERGENCY LIGHT DAMAGED. REMOVED AND REPLACED LIGHT WITH NEW ROW 22 EMERGENCY LIGHT CMM 25-23-54-4676.

Part: ELEC CONNECTOR — UNSECURE (ZONE 200) · airframe 74,123 hrs · 26,259 cycles

ROW 7 AISLE SEAT EMERGENCY EXIT LIGHT INOP. FOUND POOR CONNECTION UNDER MIDDLE SEAT. CLEANED AND RESEATED CONNECTION, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (ZONE 2000) · airframe 73,983 hrs · 26,200 cycles

EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - RIGHT OVERWING EXIT LIGHT SIGNS DO NOT TURN ON DURING OP CHECK. REMOVED AND REPLACED BATTERY PACK FOR RIGHT OVERWING EXIT LIGHT SIGNS. OPS CHECKS GOOD. REF AMM 33-51-06-960-804.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 73,142 hrs · 25,832 cycles

DURING THE ACCOMPLISHMENT OF THE WINDOW FRAME E-F REPAIR PER EA5 310-08195 REV. AOP 001 AT AAR-RFD, A CRACK WAS FOUND IN THE 3RD LOWER CORNER FASTENER HOLE OF THE LEFT HAND #3 WINDOW FRAME (P/N 141A8831-7). THE SUBSEQUENT CRACK REMOVAL PROCESS RESULTED IN A HOLE DIAMETER DECRA 5310-08520?. PERFORMED A REPAIR TO THE LEFT HAND #3 WINDOW FRAME E-F POST IN QC RECORDS UPDATE ACCORDANCE WITH EA5310-08195 REV. A OP 003 ALONG WITH THE ADDITIONAL REPAIR INSTRUCTIONS AND DEVIATIONS PROVIDED BY AAR-RFD EO # 250023. IAW ECRA 5310-08520 PART 1

Part: SKIN — CRACKED (ZONE 300) · airframe 73,142 hrs · 25,832 cycles

LH HORIZONTAL STABILIZER LOWER SKIN, ONE (1) CRACK FOUND AT STA 147.9 LOCATED AT 17 INCHES FROM TRAILING EDGE (REF: AAR NR 1000029021)

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 73,142 hrs · 25,832 cycles

PASSENGER CABIN, EMERGENCY LIGHT BATTERY PACK M1675 FAILS CAPACITY CHECK (REF: AAR NR 1000028948) REMOVED AND REPLACED EMERGENCY BATTERY PACK M1675 IAW B737 AMM 33-51-06-960-805. OPS TEST GOOD.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 73,142 hrs · 25,832 cycles

PASSENGER CABIN, EMERGENCY LIGHT BATTERY PACK M1694 FAILS CAPACITY CHECK (REF: AAR NR 1000028949) REPLACED PASSENGER CABIN, EMERGENCY LIGHT BATTERY PACK M1694 IAW B737 AMM 33-51-06-960-805. OPS CHECK GOOD. (WORK ACCOMPLISHED BY V934137 AND AAR QC A-15 V931575)

Part: ANTI-ICE VALVE — FAULTED (ZONE 400) · airframe 72,908 hrs · 25,730 cycles

ENG ANTI ICE CAUTION LIGHT ON T/O REJECT T/O AT 50KTS RESET BOTH ENGINES CB,S. RAN BOTH ENGINES AND PERFORMED ENGINE COWL TAI VALVE OPERATIONAL TESTS. BOTH GND CHK OK PER AMM 30-21-11-860-009 .

Part: MONITOR — UNKNOWN (ZONE 200) · airframe 72,581 hrs · 25,574 cycles

1B SEATBACK UNUSUALLY WARM OPPOSITE 2B VIDEO MONITOR NO BURNING SMELL AND MARK, NO MARK OF ANY SMOKE . SEAT 2B MONITOR IS COOLER THAN SEAT 2A MONITOR. PERFORMED SEAT 2B MONITOR OPS CHECK FOUND GOOD IAW AMM 44-25-00.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 72,306 hrs · 25,430 cycles

LEFT AFT OVERWING EXIT LOWER EMERGENCY LIGHT INOPERATIVE.SUPPORT TASK NSA EMX N/R 00215. REMOVED AND REPLACED BATTERY PACK AND EMERGENCY LIGHTS OPS CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 72,306 hrs · 25,430 cycles

R AFT OVERWING EXIT LOWER AND UPPER EMERGENCY LIGHT INOPERATIVE SUPPORT TASK EMX NR 00216. REMOVED AND REPLACED BATTERY PACK AND EMERGENCY LIGHT OPS CHECK GOOD.

Part: BATTERY PACK — WEAK (ZONE 200) · airframe 72,306 hrs · 25,430 cycles

AFT R/H EMERGENCY BATTERY PACK FOUND TO BE WEAK.SUPPORT TASK NSA EMX N/R 00154. REMOVED AND REPLACED BATTERY PACK AND EMERGENCY LIGHTS OPS CHECKS GOOD.

Part: BATTERY PACK — WEAK (ZONE 200) · airframe 72,306 hrs · 25,430 cycles

AFT L/H EMERGENCY BATTERY PACK FOUND TO BE WEAK. SUPPORT TASK NS A EMX N/R 00155. REMOVED AND REPLACED BATTERY PACK AND EMERGENCY LIGHTS OPS CHECKS GOOD.

Part: CONNECTOR — DAMAGED (ZONE 200) · airframe 72,306 hrs · 25,430 cycles

APPROXIMATELY 19 CONNECTORS FOR THE EEPL SEAT HARNESSES WERE FOUND BROKEN DURING THE INTIAL REMOVAL OF SEATS FROM CABIN. SUPPORT TASK NSA EMX N/R 00050. REMOVED AND REPLACES CONNECTORS FOR CABIN SEAT EEPL HARNESS THROUGH THE CABIN AS REQUIRED AND EMERGENCY LIGHTS OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (R1 DOOR) · airframe 70,590 hrs · 24,637 cycles

DURING OUTBOUND PVI FOUND EMERGENCY SLIDE LIGHT AFT OF R1 DOOR EXTERIOR INOP.SUPPORT TASK NSA EMX N/R 00149. REMOVED AND REPLACED R1 DOOR EMERGENCY SLIDE LIGHT LAMP AND OPS CHECK GOOD IAW UAL B737 AMM 33-51-- 04-960-801.

Part: BULB — BURNED OUT (R-1 DOOR) · airframe 70,543 hrs · 24,619 cycles

DURING OPS CHECKS R-1 DOOR EXT SLIDE LIGHT WAS INOP. R&R R-1 DOOR EMERGENCY SLIGHT LAMP AND OPS CHECKS GOOD IAW B737 AMM 33-51-04-960-801.

Part: FITTING — CRACKED (STA540,RBL15.04) · airframe 70,543 hrs · 24,619 cycles

B737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 15.04 IS CRACKED SUPPORT TASK NSA EMX NR 00094 REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL DATA WAS TRANSCRIBED FROM NSA EMX N/R 00094 AND HANAGR N/R 15.04 IAW B737-800 SRM 51--40-02 AND BAC DWG 111A2000 5428622. WORK ACCOMPLISHED BY V905004 AND INSPECTED BY V895955. REV ORIGINAL FOR WORK ACCOMPLISHED SEE NSA EMX N/R 00094 SSFR REPORT FORM 46-0024, ENTERED BY UAL INSPECTION U056569 AND HANGAR N/R 5428622 CIR C/W. DATE 12/07/2023.

Part: FITTING — CRACKED (STA540 LBL15.04) · airframe 70,543 hrs · 24,619 cycles

B737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 15.04 IS CRACKED SUPPORT TASK NSA EMX NR 00093 REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL DATA WAS TRANSCRIBED FROM NSA EMX N/R 00093, AND HANGAR 15.04 IAW 5737-800 SRM 51--40-02 AND BAC DWG 111A2000 REV N/R 5428621,

Part: CONTROLLER — FAULTED (BOTH 1 & 2 CPC) · airframe 69,117 hrs · 23,958 cycles

PRESS AUTO FAIL AND ALT NOT WORKING FAULTS WHEN TURNED ON AND FAULT CODE 059 REMAINS. ON INTIAL BOTH CABIN CONTROLLERS WERE FAULTING.DIDNT COMPLETE AFTER MOVING FROM MANUAL TO AUTO TO ALTN.NO EXISTING FAULTS. REF FIM TASK 21-31 TASK 824. FOUND CABIN PRESSURE CONTROLLER #1 CHANGED #1 CABIN PRESS CONTR SYSTEM TEST NEEDS TO BE IN RIGHT CONFIG. MANUAL WORKS AND AND #2 WITH FAULT "CONTRLR LRU FAIL. CODE 059". PERFORMED ROTABLE PARTS CHANGE WAS INDICATED - TT # 1686206 SN OFF 2021 VISUALLY CHECKED OUTFLOW VALVE NO DEFECT ON OUTFLOW NOTED. AFTER GROUND TEST REF FIMTASK 21-31-824 SYSTEM TEST OK. NO FAULTS FURTHER CHECKING NO EXISTING FAULTS NOTED. NOTED IN GROUND TEST.. BUT #2 CONTROLLER STILL SHOWED 01 PREV IPC REFERENCE # 21-20-00 R AND R BOTH #1 AND #2 CABIN PRESS CONTR REF AMM 21-31-01-000/400-801. PARTS USED: 29-2131-9-0003,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1762399 SN OFF 2028 CONTROLLER, CAB OFF 29-2131-9-0003 2028 ON 29-2131-9-0003 8457

Part: MOTOR — NONE (HORIZ STAB) · airframe 68,474 hrs · 23,651 cycles

CREW REPORTS DIFFICULTY REPOSITIONONG HORZ STAB. ACTUATOR. THE HORIZONTAL STABILIZER DOES NOT OPERATE ELECTRICALLY. WHEN ATTEMPTING TO MOVE STAB MANUALLY STAB CONTROL WHEEL IS DIFFICULT TO MOVE AND A RATCHING SOUND CAN BE FELT IN THE CONTROL WHEEL AND HEARD IN THE STABILIZER JACKSCREW COMPARTMENT BY THE THS ADD EMP:U138028 REF FIM 27-41 TASK 805 STAB TRIM DOES NOT MOVE FREELY.FOUND STAB TRIM MOTOR JAMED.REMOVED AND REPLACED STAB TRIM MOTOR REF AMM TASK 27-41-71-401.OPS CHK GOOD. PARTS USED: 29-2741-9-0011,QTY :1 1817647,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1817647 SN OFF 2408 MOTOR, STAB, HO OFF 29-2741-9-0011 2408 ON 29-2741-9-0011 5059

Part: RELAY — FAILED (STAB TRIM) · airframe 67,885 hrs · 23,394 cycles

STAB OUT OF TRIM LIGHT LIGHT ON MAIN ELECTRIC AND AUTO PILOT STAB TRIM FAIL. STAB OUT OF TRIM L IGHT SPEED TRIM FAIL LIGHTS ILLUMINATED. PLACED MAIN ELECTRIC AND AUTO PILOT TO CUTOFF AND USED MANUAL TRIM TO RETURN TO EWR. VERBAL FROM CREW. RIGHT AFTER TAKE OFF BOTH CAPT AND F/O''S AFTER MAINT ARRIVAL RETURNED STAB TRIM SWITCHES TO NORMAL AND ELECTRIC STAB TRIM SWITCHES DID NOT MOVE TRIM IN EITHER BOTH CAPT AND F/O TRIM SWITCHES WORK NORMALLY. NO FURTHER DIRECTION. CYCLED MAIN ELECTRIC AND AUTO PILIOT CUTOFF SWITCHES TROUBLESHOOTING ACCOMPLISHED. NO HELP. MANUAL TRIM WORKED NORMALLY. STAB OUT OF TRIM LIGHT AND T/S IAW FIM TASK 22-11 TASK 851, SSM 27-41-11 & WDM 27-41-11 & A/C OK TO CONTINUE.

Part: LIGHT — DAMAGED (21ABC) · airframe 67,418 hrs · 23,183 cycles

RED SEAT MOUNTED EMERGENCY LIGHT AT SEAT 21ABC DAMAGED. REMOVED AND REPLACED RED EMERGENCY LIGHT REF MM 33-51-11. OPS CK OK. LIGHT IS OPERATIONAL. NO DISCREPANCIES NOTED

Part: NONE — CORRODED (R 64 STAB) · airframe 67,153 hrs · 23,065 cycles

SPEED TRIM FAIL MASTER CAUTION ON DEPT BOX. LAND VERIFY TEST AND STAB TRIM TEST ALL PASS ON THE GROUND. REF FIMTSK 22-11 TASK 849. CURRENT STATUS FAULT HISTORY FOR LAST LEG CURRENT FAULTS STAB TRIM CUTOUT RELAY R64 LOCATED IN JUNCTION BOX J4. NEED TO RPL DUE TO HISTORY. REMOVED PANEL 114BW AND COVER FOR J4 JUNCTION REMOVED AND REPLACED R64 STAB TRIM CONT RELAY. OPS CHK GOOD. REF WDM 27-41-11-101. FIM 22-11 TASK 849. ADD EMP:392726

Part: SURGE VALVE — LEAKING (RH) · airframe 66,356 hrs · 22,712 cycles

263 1505-17 BZN-DEN DURING IRREGULAR FUELING OPERATION OF RT MAIN FUEL TANK DUE TO VTO ON MEL , THERE WAS A FUEL SPILL OUT OF RT WING TIP SURGE TANK VENT, LOCAL MAINTENANCE ESTIMATES FUEL SPILL WAS APPROXIMATELY 15 GALS. BZN FIRE DEPARTMENT ACCOMPLISHED CLEAN-UP & CONTAINMENT, NO FUEL ENTERED ANY DRAIN. FUEL WAS TRANSFERRED OUT OF RT MAIN & FILL VALVE CLOSED CORRECTLY.

Part: SKIN — DENTED (FWD CARGO DR) · airframe 66,297 hrs · 22,685 cycles

SUPPORT TASK FWD CARGO DOOR SKIN DENTED 17" FROM FWD EDGE AND 12" FROM TOP MRASURED DENT AS 3.8 X 3 X .080. W/Y = 37 WITHIN ALLOWABLE LIM ITS PER SRM 52-30-01 ALLOWABLE DAMAGE 1 DETAIL F. INSTALLED DE NT DOT PER GMM 07-01-55 RE-INSPECTED DENT, NO PROGRESSION NOTED, REF SRM 52-30-01 ALLOWABLE DAMAGE 1 DETAIL F. RE=EVALUATED AND INSPECTED DENT 3.8X3X.O8O W/Y=37.5 FOUND WITHIN LIMIT PER SRM 52-30-01 DMG REMAINS. LOG PAGE WAS CONVERTED TO ELB FORMAT ON DEC 06, 2016 AT 18161976 RE-INSPECTED,NO FURTHER DAMAGE NOTED IAW GMM 6-35-05. ADD EMP:N REFERENCE AAR RFD NR 99931285, DENT ON FWD CARGO DOOR FOUND TO B E OUT OF LIMITS. PERFORMED PERMANENT REPAIR OF FWD CARGO DOOR IA W B737 SRM 52-00-01-2R-2; THIS IS A GATEGORY A REPAIR (WORK ACCO MPLISHED BY V918170 & AAR QC A-13 V918050).

Part: BATTERY PACK — DISCHARGED (M1671) · airframe 66,297 hrs · 22,685 cycles

EMERGENCY LIGHTS INOP (REF AAR RFD NR 99935413). REPLACED BATTERY PACK M1671 AT ROW 27DEF IAW B737 AMM 35-51-06-960-805. TEST GOOD. WORK ACCOMPLISHED BY AAR RFD TECH V937427 AND AAR QC A-50 V931572.

Part: BEAR STRAP — CRACKED (FWD GAL) · airframe 66,297 hrs · 22,685 cycles

DURING NDT INSPECTION OF FWD GALLEY DOOR BEAR STRAP ON EA 5310-0 7694 REV A. A CRACK WAS NOTED ON THE INNER SURFACE OF THE BEAR S TRAP CRACK LENGHT MARKED ON SURFACE CRACK BETWEEN STRINGER 8R AND 9R BETWEEN STATION 291.5 AND 294.5 (REF AAR RFD NR 99935248) REQUIRES REPEAT INSPECTIONS PER TABLE 202 OF SRM 53-10-01-2R-6 REPEAT INSPECTIONS AT 12,000 FLIGHT CYCLES. WITH A THRESHOLD OF 50,000 TOTAL AIRCRAFT FLIGHT CYCLES AND REPAIRED FWD GALLEY DOOR BEAR STRAP IAW B737-800 SRM 53-10-01-2R-6 REPAIR 6. THIS IS A CATEGORY B REPAIR THAT ADD EMP:V916729 V914837

Part: NONE — CORRODED (STA986.5BL22) · airframe 66,297 hrs · 22,685 cycles

FOUND POSSIBLE CORROSION ON UPPER FLOOR BEAM BEAM AT STA 986.5, BL 22.5R (REF AAR NR 99935093)

Part: DOOR — LEAKING (L2) · airframe 63,618 hrs · 21,613 cycles

2L DOOR SQUEAL AND CBN NO PRESSURIZE UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. CONFIRMED L2 DOOR LEAKING AT LOWER CORNERS. AS PER LP 6274246 FOR TROUBLESHOOTING OF PRESSURIZATION ISSUE : PERFORMED CPC BITE, FOUND CODE 30 (LOW FLOW) ON CPC 1. FOLLOWING FIM 21-31-00-810-823, PERFORMED PACK OP CHECKS AND SINGLE PACK CONFIDENCE DECAY CHECK. PACKS OPERATED NORMAL AND DECAY WAS 150 SECONDS, LIMIT IS 100 SECONDS. NOTE: DFD SHOWS ENGINE BLEEDS OFF AT TAKEOFF. LOCKED FOR MAINTENANCE FERRY. FURTHER DETAILS AWAITED.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 63,037 hrs · 21,391 cycles

AUTO FAIL LT FL320 ALTN COULD NOT CONTROL CABIN EMERGENCY DESCENT CREW STATES AUTO FAIL LIGHT CAME ON SWITCHED TO ALTERNATE, NO RESPONSE FROM VALVE SWITCHED TO MANUAL. MAINT CABIN PRESS CONT FAULT CONTROLLER LRU FAIL DISPLAYED ON CONTROLLER 1 AND 2, FAULT CODE 059. FIM TASK 21-810-824 REPLACED CABIN PRESSURE CONTROLLERS 1 AND 2, AMM 21-31-01. PRESSURIZATION SYSTEM GROUND TEST, 21-31-00-700-802 IS GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT 1990425 SN OFF 0632 TT 1990054 SN OFF 9456 CONTROLLER, CAB OFF 29-2131-9-0003 0632 ON 29-2131-9-0003 9021 CONTROLLER, CAB OFF 29-2131-9-0003 9456 ON 29-2131-9-0003 2028.

Part: FUEL CELL — LEAKING (MAIN) · airframe 59,105 hrs · 19,880 cycles

FUEL SMELL AIRBORNE THROUGHOUT CABIN. STRONGEST ODOR OVER WING

Part: HANDLE — FROZEN (ENTRY DOOR) · airframe 59,086 hrs · 19,872 cycles

L1 DOOR EXTERIOR HANDLE WILL NOT PULL OUT FROZEN WITH ICE ICE THOWED OUT. HANDLE PULLS OUT OK NOW, INSPECTED HANDLE OK AMM 52-11-00-200-801, OPENED AND CLOSED WITH EXTERIOR AND INTERIOR HANDLE OK AMM 52-11-00-860-801/802/803/804.OK

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,358 hrs · 18,751 cycles

EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 7 - 14, 29 - 38, RT OVERWING EXITS AND RT AFT DOOR. FOUND BLOWN FUSES IN THE POWER SUPPLYS M1694, M1695, AND M1672. A BAD BATTERY AT M1676. REPLACED THE BATTERY CHARGERS M1694, M1695, M1672, AND REPLACED BATTERY AT M1676. ALL EMERGENCY LIGHTS, OP CHECK GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 53,271 hrs · 17,550 cycles

RIGHT AFT DOOR EMERGENCY EXIT LENS MISSING . SECURED THE LENS.

Part: FRAME — DENTED (FUSELAGE) · airframe 49,956 hrs · 16,271 cycles

FORWARD CARGO LT FRAME STATION 500E, JUST ABOVE SIDE PLATE THE FRAME IS SEVERELY DENTED ON TOP SIDE. IAW ECRA 5310-06802 COMPLIED WITH PART 1 INTERIM REPAIR. ITEM PLACED ON DIP IAW PART 1 STEP 17 OF ECRA 5310-06802.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,438 hrs · 15,022 cycles

NO EMER LIGHTING FROM 29 AFT. FOR SDR REPORTING. R & R BATTERY PACK FOR POWER SUPPLY IAW AMM 33-51-06 -960-805. OPERATIONS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 46,248 hrs · 14,954 cycles

EAT 15 ABC EMER LIGHT INOPERATIVE. R & R DAMAGED CONNECTOR AT SEAT ROW 15 ABC OTBD LEG. PN 172343-1 CONNECTOR. OPERATIONS CHECKED OF EMERG LIGHTING GOOD IAW AMM 33-51-00.

Part: ADIRU — MALFUNCTIONED (RIGHT) · airframe 45,554 hrs · 14,720 cycles

CLIMBING THROUGH 250 FOR 260 AUTOPILOT DISCONNECTED & WE HAD AN IRS LIGHT ON MASTER CAUTION, WITH A FAULT LIGHT ON THE OVERHEAD LT IRS. COMPLETED QRH WITH NO CHANGE. PLACED ON NO AUTO LAND STATUS DUE TO RT IRU. R & R, NO TIME TO PERFORM RTS. STICKER INSTALLED IAW MM 34-11-11 & 34-21-00. ROTABLE PARTS CHANGE WAS INDICATED TT 1705827 SN OFF 09316 IPC REFERENCE NR.

Part: BRAKE — DRAGGING (LT MLG) · airframe 43,688 hrs · 14,083 cycles

BRAKE DRAGGING ON LT INBD MAIN MOUNT DURING TAKEOFF ROLL. FUSE PLUG BLOWN, REJECTED TAKEOFF AT 50 KTS. R & R NR 1 & NR 2 TIRES, BRAKES, AB & AS CONTROLLER, NR 1 & NR 2 ANTI-SKID VLVS & LT BRAKE UPPER & LOWER FUSES. ALL SYS CHECKED NORMAL. TAXIED ACFT, NO DEFECTS FOUND.

Part: LENS — WRONG PART (CABIN) · airframe 43,318 hrs · 13,949 cycles

AFT CABIN WINDOW EMERGENCY EXIT PLACARDS REPORT MARKED INCORRECTLY WITHOUT ARROWS. REPLACED LENS FOR LT & RT AFT CABIN WINDOW EMERGENCY EXIT SIGNS IAW IPC 33-51-01 FIG 16.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 41,700 hrs · 13,393 cycles

COMPLETED C SCAN FOUND CRACK ON LT HORIZONTAL STAB LOWER SIDE AT STA 129.50 APPROXIMATELY 6 INCHES FWD OF PATCH, 16 INCHES AFT OF FWD SPAR. INSTALLED REPAIR IAW SRM 55-10-01 REPAIR 11.

Part: PRESSURE PANEL — CRACKED (BS 663)

DURING INSPECTION OF VERTICAL PRESSURE WEB AT BS 663, FOUND .25 INCH CRACK AT RBL 41, WL 194. REPAIRED PRESSURE WEB IAW SRM 57-10-10, REPAIR 3, ALTERNATE 2, PAGE 204, FIGURE 204.

Part: OVEN — MALFUNCTIONED (AFT GALLEY) · airframe 36,773 hrs · 11,639 cycles

IN CRUISE LEAD F/A CALLED AND STATED THAT THERE WAS A STRONG SMELL IN AFT GALLEY THAT SMELLED LIKE ELEC WIRING OR PLASTIC BURNING. TURNED OFF OVEN AND COFFEEMAKER. RAN QRH. NO SMOKE ONLY SMELL. SMOKE DID NOT DISSIPATE. DECLARED EMERGENCY AND DIVERT TO ATL. INSPECTED AFT GALLEY IAW 05-51-26-800-801-C1, FOUND NR 1 OVEN BAD. REF LOG 8961218 AND 8961219. OK TO CONTINUE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,611 hrs · 10,866 cycles

RT FUSELAGE STUB FRAME HAS CORROSION STA 706 + 10.5" ABOVE FLOOR. REMOVED CORROSION AND REWORKED AREA PER ECRA 5311-01529.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 34,611 hrs · 10,866 cycles

CABIN - CRACK AT STA 440, STRINGER 9R ACCOMPLISHED REPAIR AT STA 440 STR 9R REF EC/RA 5310-05385.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,611 hrs · 10,866 cycles

FLOORBEAM STA 328 HAS CORROSION AT RBL 53. INSTALLED REPAIR STRAP REF ECRA 5321-01764.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,611 hrs · 10,866 cycles

737-53-3-0737 FWD ENTRY FLOORBEAM AT STA 294 HAS CORROSION AT RBL 1.5. INSTALLED STRAP REPAIR REF ECRA 5321-01760.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,611 hrs · 10,866 cycles

737-53-3-0737 FLOORBEAM STA 328 RBL 11 TO RBL 53 HAS CORROSION. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP PER ECRA 5321-01763.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 34,611 hrs · 10,866 cycles

LT HORIZONTAL STABILIZER LOWER SKIN IS CRACKED. STAB STATION 128.75, 26 INCHES AFT OF FRONT SPAR. CUT OUT DAMAGED AREA, REPAIRED PER SRM 55-10-01 REPAIR 11.

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 34,611 hrs · 10,866 cycles

737-53-3-0714 ABB RT TIE DOWN RAIL CRACKED STA 727J. INSTALLED NEW SECTION OF RT CARGO TRACK AND SPLICES FROM STA 727+7.5 TO 758, PER SRM 53-00-53 REPAIR 3.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 34,611 hrs · 10,866 cycles

737-53-3-0714 ABB RT TIE DOWN RAIL CRACKED. 767 INSTALLED NEW SECTION OF RT CARGO TRACK AND SPLICES FROM STA 758 TO 887 PER SRM 53-00-53 REPAIR 3.

Part: FLOOR SUPPORT — BROKEN (FUSELAGE) · airframe 34,611 hrs · 10,866 cycles

737-53-3-0739 FLOOR SUPPORT BROKEN STA 540 BL 0 TO LT I/B SEAT TRACK CABIN FLOOR STRUCTURE. REPLACED BROKEN FLOOR SUPPORT REF SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,611 hrs · 10,866 cycles

737-53-3-0737 FWD ENTRY FLOORBEAM AT STA 344 HAS CORROSION AT LBL 2. REMOVED CORROSION AND REPAIRED PER SRM 53-10-51 REPAIR 9.

Part: FRAME — CRACKED (FUSELAGE) · airframe 34,611 hrs · 10,866 cycles

737-53-3-0734; CABIN - CRACK ON FRAME AT STA 380, STRINGER 9R. REPAIRED FRAME AT STA 380 BETWEEN STR 8R AND 9R PER EA 5310-04716 REV C OP 2.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 34,608 hrs · 10,864 cycles

DURING OPS CK OF R-1 DOOR EMER EXIT SIGN ON L/P 8823759 FOUND BATTERY PACK DEAD. REPLACED BATTERY, OPS CKS GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 34,608 hrs · 10,864 cycles

DURING EMER EXIT LIGHT TEST, O/W EXIT LIGHTS WENT OUT AFTER 5 SEC. REPLACED BATTERY PACK AND CHARGER, OPS CKS GOOD.

Part: PLATE — BROKEN (EXIT SIGN) · airframe 34,608 hrs · 10,864 cycles

EMER EXIT SIGN AT R-1 DOOR BROKEN BACKING PLATE. REPLACED EMER EXIT SIGN AT R-1 DOOR.

Part: UNKNOWN — MALFUNCTIONED (BRAKE SYSTEM) · airframe 31,208 hrs · 9,712 cycles

ANTI-SKID INOP-AUTOBRAKE DISARM (WHEN A/BRAKES ARMED ONLY) PARKING BRAKE ON LIGHTS ARE ILLUMINATED. COMPLIED WITH IAH MX TO RESET AUTOBRAKE & PARKING BRAKE C/B. NO HELP. REF N/R 4995703 & 4336994 AACU FLT FAULT "PWR A/B". ALSO CYCLED BRAKE SEVERAL TIMES WITH NO FAULTS FOUND, OK TO CONTINUE.

Part: SENSOR — FAILED (TE FLAP) · airframe 29,269 hrs · 8,977 cycles

TAKEOFF CONFIGURATION WARNING HORN SOUNDED DURING TAKEOFF AT ABOUT 50 KNOTS. TAKEOFF WAS REJECTED AT ABOUT 60 KNOTS. WARNING TEST BUTTON HAD BEEN TESTED WITH NO HORN RESULTING. AFTER REJECTION, NOTICED FLAPS WERE SPLIT L FLAP 7 R FLAP AT 5, HAD NOT NOTICED ANY SPLIT PRIOR TO TAKEOFF. PERFORMED FSEU BITE. FAULT: FLAP 2 SKEW. REMOVED AND REPLACED FLAP 2 SKEW SENSOR IAW B737 MM 27-59-01. PERFORMED FLAP SKEW FUNCTION TEST. ALL VALUES IN RANGE. FLAPS OPS CHECK NORMAL. ACFT OK TO CONTINUE. ROTABLE PARTS CHANGE WAS INDICATED - TT 1381344 S/N OFF 07701 SENSOR, FLAP SK OFF 29-2759-9-0002 S/N 7701 ON 29-2759-9-0002 S/N 2849

Part: BRAKE — LEAKING (NR 1) · airframe 15,044 hrs · 4,458 cycles

CLIMBING THROUGH 10,000, FUMES IN COCKPIT. REPLACED LEAKING NR 1 BRAKE PER AMM 32-41-41-400-801.