N76529

Part: ADIRU — FAULTED (ZONE 100) · airframe 47,311 hrs · 17,042 cycles

AFTER T/O LNAV WOULD NOT TRACK COURSE OR GO TO A FIK. TOMC RESET AIRBORN NO HELP FLAGGING FOR SDR PERFORMED FMCS L/R BITE PROCEDURE REF FIM 34-61 TASK 801. FOUND FMC R REPORTING FMC L FAULT. FAULT FMC-L PRES POS LAT RATE. PER FIM 34-61 TASK 824. ADIRS BITE PROCEDURE SHOWS NO FAULTS. DFCS BITE PROCEDURE, SHOWS MGS 22-11822 AS STATED IN HISTORY. BOTH CDS BITE PROCEDURE IN FLIGHT FAULTS REPORTING FMC. REF LOG 7417431 FOR WORK PERFORMED.REMOVED AND REPLACED TAT PROBE REF AMM 34-21-06-000-801/34-21-06-400-801. INSTALLATION TEST PASSED.

Part: SKIN — CRACKED (ZONE 100) · airframe 47,271 hrs · 17,025 cycles

BROKEN DOUBLER AT PREVIOUS REPAIR OF POWER RECEPTACLE SURROUND SKIN. INSTALLED REPAIR PARTS AT POWER RECEPTACLE AREA IAW SRM 53-10-15-2R-4, REPAIR 4.

Part: BEAM — CRACKED (ZONE 800) · airframe 47,267 hrs · 17,023 cycles

R1 SERVICE DOOR HANDLE TORQUE BOX LOWER SUPPORT BEAM CRACKED NEAR TORQUE BOX FWD ATTACH BOLT. R & R LOWER INNER SKIN & LOWER BEAM IAW SRM 51-40-02-0G-0 & DWG 141A6516 AND DWG 141A6535.

Part: BEAM — CRACKED (ZONE 800) · airframe 47,267 hrs · 17,023 cycles

R1 SERVICE DOOR HANDLE TORQUE BOX UPPER SUPPORT BEAM CRACKED NEAR TORQUE BOX FWD ATTACH BOLT. INSTALLED UPPER BEAM AND STOP FITTING NR 3 AT R1 DOOR PENDING SKIN IAW SRM 51-40-02-0G-0, DRAWING 141A6516 AND DRAWING 141A6535.

Part: SKIN — CRACKED (ZONE 300) · airframe 47,271 hrs · 17,025 cycles

CRACK FOUND ON RT HORIZONTAL STAB LOWER SKIN AT HSS 120.30, INBD ROW, 11 INCHES FROM REAR SPAR. CRACK LENGTH: 1 INCH. REMOVED PREVIOUS REPAIR , FABRICATE NEW DOUBLER & INSTALLED NEW REPAIR PARTS IAW SRM 55-10-01-2R-11, REPAIR 11, PAGE 7, TABLE 204.

Part: UNKNOWN — ODOR (CABIN) · airframe 47,148 hrs · 16,966 cycles

3/4 FA REPORTED BURNING OIL SMELL AROUND ROW 7 LAST HALF OF FLIG HT FLIGHT ATTENDANTS FILLED OUT ODOR IN PLANE FORM 46-6020. INBOUND CREW DID NOT REPORT ODOR. ONCOMING O/B CREW CREATED LOG. ONE F/A REPORTED NOT SMELLING ANYTHING AND THAT AN INBOUND PILOT ALSO DIDNT CONFIRM SMELL AT LOCATION REPORTED. FOLLOWED CONDITIONAL INSPECTION REF AMM TASK 05-51-26-800-801-C1. REQUESTED ENGINE RUNS ALONG WITH CONDITIONAL INSPECTION. ALL AND INSPECTION REQUIREMENTS COMPLIED WITH. COULD NOT DUPLICATE. OK TO CONTINUE.

Part: NONE — NONE (NONE) · airframe 46,655 hrs · 16,716 cycles

BIRD STRIKE LEFT LEADING EDGE ON LANDING INSPECTED BIRD STRIKE PER AMM 05-51-18-210-807 . CLEANED AREA. NO DEFECTS NOTED .

Part: LENS — OUT OF POSITION (ZONE 200) · airframe 46,598 hrs · 16,690 cycles

EMERGENCY EXIT ROW LIGHTS OUT OF CORRECT SEQUENCE. REPOSITIONED EMERGENCY LIGHT LENS AT ROW 21 ABC TO CORRECT CONFIG. REF. AMM 33-51-11. EMERGENCY LIGHTS TEST NORMAL.

Part: BRAKE — FAULTED (ZONE 700) · airframe 46,221 hrs · 16,510 cycles

NUMBER 1 BRAKE REQUIRES REPLACEMENT DUE TO POSSIBLE LOCKING UP ON LANDING REMOVED AND REPLACED #1 MLG BRAKE PER AMM 32-41-41-000/400-801. OPS AND LEAK CHK GOOD.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 46,195 hrs · 16,498 cycles

MULTIPLE EMERGENCY LIGHTS INOPERATIVE THOUGHOUT CABIN. REMOVED BATTERY PACK IAW AMM 33-51-06-960-805. INSTALLED SERVICEABLE BATTERY PACK IAW AMM 33-51-06-960-805. PERFORMED EMERGENCY LIGHTS OPS CHECK IAW 33-51-00. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 46,195 hrs · 16,498 cycles

SEAT ROW 7-14ABC EMERGENCY LIGHTS INOPERATIVE. REMOVED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06. INSTALL EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06. EMERGENCY LIGHTS OPS CHECK IAW 33-51-00. OPS CHECKS GOOD.

Part: SLIDE — OUT OF ADJUST (ZONE 800) · airframe 45,797 hrs · 16,304 cycles

DOOR 2R SLIDE HAS EXCESS MATERIAL SHOWING BELOW DOOR THAT NEEDS ADJUSTING RESECURED DOOR 2R SLIDE GIRT MATERIAL REF AMM 25-66-01. OKAY FOR CONTINUED SERVICE.

Part: SLIDE — FAULTED (ZONE 800) · airframe 45,703 hrs · 16,258 cycles

EMERGENCY ESCAPE SLIDE INSPECTION {B737-25-3-1066} - R2 DOOR SLIDE OUT OF TIME. REMOVED R 2 DOOR SLIDE REF AMM 25-66-01, OK TO INSTALL NEW SLIDE. FLAGGING FOR CLEARANCE ACP RII VERIFICATION OF DOOR R2 SLIDE PN REF IPC 25-66-00-16 FIG. ITEM 390. PN 5A3307-9 SN BNG35695 IS OK TO INSTALL R2 POSITION. RII PER GMM 09-25-05. REPLACED DOOR R 2 DOOR SLIDE REF AMM 25-66-01-400-803. NO COMPONENT FOUND ACP RII VERIFICATION OF DOOR R2 SLIDE INSTALLATION REF AMM 25-66-01-400-801 AND 25-66-01-400-803. NO DEFECTS NOTED. RII PER GMM 09-25-05.

Part: SWITCH — FAULTY (ZONE 100) · airframe 45,557 hrs · 16,194 cycles

STAB OUT OF TRIM WITH A/P ON DURING CLIMB NO TRIM WITH A/P ENGAG ED CHECKED DFCS BITE TEST, AND FAULT HISTORY.BY FLT LEG. CHANNEL A SHOWS LEG 01 MSG 22-11177 AND 22-11186. CHQNNEL B NO FAULTS. PERF. LRU REPLACMENT TEST MSG22-11167 PRESENT (SPEED/STAB CHAN-A STAB TRIM CLUTCH) STAB TRIM WHEEL DOES NOT MOVE. REQ. FURTHER TROUBLESHOOTING. FIM 22-14 TASK 818. STABILIZER RIGGING TEST FAILED TEST 54.03, STAB FAILED TO MOVE TO STAP POS.PLEASE REPLACE R384 RELAY NEXT AND RE-ACCOMPLISH AMM 22-11-00-820-805 AND 22-11-81-710-801.REF FIM 22-15 TASK 821 FOR ADDITIONAL TROUBLESHOOTING IF R384 IS NO HELP.SFOLM POZAS PER FIM 22-12 TASK 803, PERFORMED STAB RIG TEST AMM 22-11-00-820-805. FAILED. NO MOVEMENT OF STAB WITH AUTOPILOT. STRANGE HUM BELOW FO FOOTWELL. PERFORMED STAB TRIM MOTOR AUTOPILOT TEST 22-11-81-710-801. NO MOVEMENT OF STAB WITH ADD EMP:U181360 AUTOPILOT. CHANGED R384 RELAY WDM 22-13-11-3 AND PERFORMED STAB TRIM MOTOR AUTOPILOT TEST AGAIN. FAILED. HUM REMAINS. LOCATED HUM AS FO COLUMN SWITCHING UNIT. SUSPECT FAILED PART. ON ORDER. REPLACED F/O COLUMN CUTOUT SWITCH IN REF TO AMM 27-41-51/401. OPS TEST PASS. PARTS USED: 29-2741-9-0007.ROTABLE PARTS CHG:TT # 1973186 SN OFF 2185 PN OFF 29-2741-9-0007.SWITCH, COLUMN OFF 29-2741-9-0007 2185 ON 29-2741-9-0007 4344 PERFORMED STAB TRIM MOTOR AUTOPILOT TEST REF AMM TASK 22-11-81-710-801 & STAB RIGGING TEST REF AMM TASK 22-11-00-820-805. ALL TEST PASS.

Part: GIRT BAR — FAULTED (ZONE 800) · airframe 45,190 hrs · 16,037 cycles

DOOR 1R HAS EXTRA GIRT BAR MATERIAL SHOWING. REMOVED SLIDE AND REPACKED SLIDE PACK GIRT MATIRIAL. REINSTALLED SLIDE AND VERIFIED SAFTEY PIN REMOVED. REF AMM 25-66-01. VERIFIED INSTALLATION OF DOOR 1R SLIDE. SLIDE SAFETY PIN REMOVED AND STOWED. REF. AMM 25-66-01/ GMM 09-25-05

Part: STRUCTURE — DAMAGED (ZONE 600) · airframe 45,173 hrs · 16,030 cycles

RII INSPECTION REQUIRED RIGHT WING LOWER CHORD DAMAGED AT STRIKER PLATE LOCATION STA 540 RBL 40.875 OUT OF LIMITS . VERIFIED REPAIR MATERIAL REF SRM 57-10-13-2R-3 TABLE 201. OK TO REF: SRM 57-10-13-2R-3 STEP 4 F - ACCOMPLISHED HFEC 737 NDT PART VERIFIED FLAP PEEN INTENSITY AND COVERAGE - OK TO CONTINUE. FABRICATE REPAIR PARTS. 6-51-00-00 PROCEDURE 23, NO DEFECTS NOTED. MATERIAL ID 7075 T6 .125 PO# 3919569 FOR ITEM 1 STRAP AND ITEM 4 REMOVED DAMAGE AS PER SRM 57-10-13-2R-3 REPAIR INSTRUCTIONS PERFORMED FLAP PEEN AS PER INTRUCTION 4 (H FILLER AS PER SRM 57-10-13-2R-3 TABLE 201 4(A)(B)(C) REQUIRES HEFC AS PER INSTRUCTIONS 4(D) VERIFIED PARTS INSTALLED AND SECURE FABRICATED PARTS ALODINED AND PRIMED AS PER SRM 51-20-01 AND FABRICATED PARTS ALODINED AND PRIMED AS PER SRM 51-20-01 AND FABRICATED PARTS ALODINED AND PRIMED AS PER SRM 51-20-01 AND VERIFIED PARTS INSTALLATION, ALODINED AND PREME REF SRM INSTALLED PNEUMATIC DOOR AND AJUSTED LATCHES DOOR SECURED AND INSTALLED AS SRM 57-10-13-2R-3 INSTALLED AS SRM 57-10-13-2R-3 INSTALLED AS SRM 57-10-13-2R-3 57-10-13-2R-3 OK TO CONTINUE CREATED ESFR 1038275 REPAIRED AS PER SRM 57-10-13-2R-3.

Part: TIRE — FAILED (ZONE 700) · airframe 45,173 hrs · 16,030 cycles

01 MLG TIRE FOUND BEYOND AMM LIMITS. MUST BE REPLACED PRIOR TO T HE NEXT FLIGHT. #1 MAIN TIRE BLOWN. REMOVED AND REPLACED #1 MLG WHEEL ASSY IAW AMM 32-45-11.

Part: FLAP SYSTEM — FAULTED · airframe 45,066 hrs · 15,984 cycles

FLAPS STUCK IN BETWEEN 2 AND 5 PILOTS INFORMED FLAP 4KNOT OVERSPEED, FLAPS 15, 5 SECONDS, 2500FT. PERFORMED FSEU BITE. FOUND FAULT CODE 27-51351 TE FLAP UCM UNCOMMANDED MOTION OF THE TRAILING EDGE FLAP SYSTEM. PERFORMED TRAILING EDGE FLAP LOAD RELIEF GROUND TEST. TEST PASSED. CONTINUE FIM 27-51 TASK 830 STEP D(9). UNLOCKING FOR MX PERFORMED FIM 27-51 TASK 830. NO FAULTS FOUND. PERFORMED PHASE 1 INSPECTION OF FLAP/SLAT OVERSPEED REF AMM 05-51-08. NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECK OF FLAP SYSTEM REF AMM 27-51-00. OPS CHECK GOOD FLAPS EXTEND AND RETRACT NORMALLY.

Part: DOOR — WARNING MESSAGE (2AFT DOOR) · airframe 40,628 hrs · 14,040 cycles

2AFT DOOR LIGHT CAME ON DURING INITIAL T/O ROLL OPERATED THE 2R DOOR AND PROX SWITCH, FOUND NO ISSUES WITH NOTED WITH EITHER DOOR REF. AMM TASK 12-25-12-640-801. CREW WAS SWITCH OR ROLLERS/CATCHES. OPERATED THE 2L DOOR AND PROX SWITCH, NOT CERTAIN OF WHICH LIGHT CAME ON DURING TAKE OFF ROLL DUE TO FOUND NO ISSUES WITH SWITCH OR ROLLERS/CATCHES. LUBRICATED ALL LIGHT ON AND EXTINGUISHED VERY QUICKLY. THIS IS WHY BOTH AFT BEARINGS AND OPENED AND CLOSED DOORS NORMALLY, NO ISSUES WERE DOORS WERE EXAMINED. OK TO CONTINUE.

Part: ADIRU — FAULTY (R ADIRU) · airframe 40,076 hrs · 13,841 cycles

FMC NAV STATUS IRS L ONLY. NO FAULT LT. FO NO MAG COMP OR HDG B UG.FO TCAS FAIL. ON R ADIRU FOUND FAULT 34-21009 "ENTER HEADING" FAULT ON LAST GOOD. PERFORMED LAND VERIFY TEST PER AMM 22-11-00-700-801. ALL LEG. PER FIM 34-21 TASK 808 FAULT CLEARED AFTER HEADING IS TEST PASSED FULL CAT CAPABILITY RETAINED. PARTS USED: ENTERED. NO MAINT REQUIRED PER FIM. NO OTHER FAULTS FOUND. 60-3421-9-0001,QTY :1 REMOVED AND REPLACED R ADIRU PER AMM 34-21-01. ALL OPS CHECKS ROTABLE PARTS CHANGE WAS INDICATED - TT # 1760096 SN OFF 3003 UNIT, ADIRU, AI OFF 60-3421-9-0001 3003 ON 60-3421-9-0001 1449

Part: LIGHT — BROKEN (CABIN) · airframe 39,737 hrs · 13,728 cycles

EMER ESCAPE LT MISSING LENS COVER LIGHT IS JUST FWD OF 1B PIC ONLY EMER ESCAPE LT IS ALSO MISSING THE LIGHT BULBS. BULB ALSO MISSING , RELAMPED LIGHT AND INSTALLED LENS COVER. OPS CHK GOOD.

Part: LIGHT — DAMAGED (11ABC) · airframe 38,181 hrs · 13,154 cycles

SEAT MOUNTED EMERGENCY LIGHT AT 11ABC DAMAGED. REMOVED AND REPLACED LIGHT ASSY REF MM 33-51-11. OPS CK OK. VERIFIED IDT REQUIREMENTS FOR EMEGENCY PATH LIGHTING AT ROW 11ABC.

Part: SKIN — NONE (STA 188) · airframe 37,999 hrs · 13,096 cycles

BIRD STRIKE UNDER CAPT NOSE FOUND SMALL DENT JUST FWD OF FWD E&E DOOR LOCATED A LITTLE FWD STA 188, MEASURED 2"W 1.5L & .046D, PER SRM 53-00-01-1A-1 WITHIN LIMITS D < .125 & W/Y RATIO > 30 ACCOMP ACFT BIRD STRIKE INSP PER MM 05-51-18 LOCATED ON FUSELAGE CENTER LINE ADD EMP:U113787

Part: WARNING LIGHT — FALSE INDICATION (AFT ENTRY DOOR) · airframe 36,478 hrs · 12,564 cycles

AFT ENTRY DOOR LIGHT AS TAKEOFF POWER WAS APPLIED CYCLE THE LEFT AFT DOOR SEVERAL TIMES SHOWED INDITION NORMAL , OK TO CONTINUE.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,138 hrs · 11,402 cycles

ON ARRIVAL FOUND DENT , RIGHT SIDE FUSELAGE APPROX 3 FEET AFT OF DOOR 1R, EVEN WITH BOTTOM OF DOOR. IN ZONE 43 . DENT IS APPROX .500L X .250W X .100D . RE-EVALUATED DENT. DENT IS SMOOTH WITH NO GOUGES OR CRACKS. DENT IS BETWEEN STRINGER 16 & 17. 2" AFT OF BS 360. 3" BELOW STRINGER 16. L=.500" W=.250" D=.100" Y=2.5 5300-06801. BE LESS THAN 3" OF SKIN SPLICE. NEED TO CREATE DIP REF EC/RA DENT IS OUT OF LIMITS, REF SRM 53-00-01 ALLOWABLE DAMAGE MUST ACCOMLISHED HFEC AS REQUIRED ON EXTERNAL SKIN ONLY REF NDT MANUAL PT 6 51-00-00-23. NO CRACKS FOUND AT THIS TIME. ALLOWABLE DAMAGE MUST NOT BE WITHIN 3" OF A SKIN SPLICE. NEED TO CREATE A DIP REF EC/RS 5300-06801. ENTRY SHOULD READ...DENT IS OUT OF LIMITS, REF SRM 53-00-01 PLACING ON DIP. COMPLETED INTERIM REPAIR: PART 1 PER ECRA 5330-06801. SEE UPDATES ABOVES. PER DIP ACCOMPLISH A DAILY INSPECTION PER PART 2. ACCOMPLISH INSPECTION PER PART 2A EVERY 2 DAYS. ACCOMPLISH IMPROVED INTERIM REPAIR PER PART 1A ON OR BEFORE 3/14/2021. G1 GALLEY MAY NEED TO BE REMOVED FOR ACCESS TO ACCOMPLISH THIS IMPROVED INTERIM REPAIR PER PART 1A. ENSURE INSTALLATION. M&L UPDATED TO PROVIDE INOUGH GROUND TIME FOR G2 GALLEY REMOVAL AND ACCOMPLISHED PART 1 STEPS 1-4, PER EC/RA 5300-06801. DENT , RIGHT SIDE FUSELAGE APPROX 3 FEET AFT OF DOOR 1R, EVEN WITH BOTTOM OF DOOR. IN ZONE 43 . DENT IS APPROX .500L X .250W X .100D. PLACING ON DIP. COMPLETED INTERIM REPAIR: PART 1 PER ECRA 5330-06801. SEE UPDATES ABOVES. PER DIP

Part: SKIN — DENTED (FUSELAGE) · airframe 33,138 hrs · 11,402 cycles

DENT WITH A GOUGE FOUND ON R SIDE FUSELAGE APPROX 3 FT AFT OF 1R, BETWEEN STRINGER 15&16, 1" BELOW STRINGER 15, 1.5" AFT OF BS 360. L=.600" W=.500" D=.020. Y=25 BLEND OUT GOUGE TREAT PRIME AND PAINT DENT REF SRM 53-00-01 AND ECRA 5330-06801. MANUAL PT 6 51-00-00-23. NO CRACKS FOUND AT THIS TIME. ACCOMLISHED HFEC AS REQUIRED ON EXTERNAL SKIN ONLY REF NDT PLACING ON DIP. COMPLETED INTERIM REPAIR: PART 1 PER ECRA 5330-06801. SEE UPDATES ABOVES. PER DIP ACCOMPLISH A DAILY INSPECTION PER PART 2. ACCOMPLISH INSPECTION PER PART 2A EVERY 2 DAYS. ACCOMPLISH IMPROVED INTERIM REPAIR PER PART 1A ON OR BEFORE 3/14/2021. G1 GALLEY MAY NEED TO BE REMOVED FOR ACCESS TO ACCOMPLISH THIS IMPROVED INTERIM REPAIR PER PART 1A. ENSURE INSTALLATION. TO PROVIDE INOUGH GROUND TIME FOR G2 GALLEY REMOVAL AND DENT WITH A GOUGE FOUND ON R SIDE FUSELAGE APPROX 3 FT AFT OF 1R, BETWEEN STRINGER 15&16, 1" BELOW STRINGER 15, 1.5" AFT OF BS 360. L=.600" W=.500" D=.020. Y=25. TOMC-APPROVAL FROM SC1ELBYC COMMENT DENT WITH A GOUGE FOUND ON R SIDE FUSELAGE APPROX 3 FT AFT OF 1R, BETWEEN STRINGER 15&16, 1" BELOW STRINGER 15, 1.5" AFT OF BS 360. L=.600" W=.500" D=.020. Y=25. PLACING ON DIP. COMPLETED INTERIM REPAIR: PART 1 PER ECRA 5330-06801. SEE UPDATES ABOVES. PER DIP ACCOMPLISH A DAILY INSPECTION PER PART 2. ACCOMPLISH INSPECTION PER PART 2A EVERY 2 DAYS. ACCOMPLISH IMPROVED INTERIM REPAIR PER PART 1A ON OR BEFORE 3/14/2021. REVIEWED RECORDS UPDATE RECORDS UPDATE QC REVIEWED RIR: (PART 2) DAI

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 30,981 hrs · 10,696 cycles

CABIN IN AUTO GAVE CABIN WARNING AT FL330 CABIN ALTITUDE REACHED 10K CREW REPORTED NO FAULTS ONLY HEARD CABIN ALT WARNING HORN AND SAW CABIN ALT LIGHT AND CABIN ALT AT 10000 FT AND OUTFLOW VALVE PARTIALLY OPEN, WENT TO MANUAL MODE AND RECOVERED CABIN ALT. ACCOMPLISHED BITE CHECKON BOTH DCPC AND FOUND CODE 58 MANUAL SWITCH ON BOTH CONTRLLERS, NO OTHER FAULTS, ACCMPLISHED BITE CK ADD EMP:107430 OF BOTH PACK CONTROLLERS NO FAULTS NOTED CONTACTED TOMC WITH FINDINGS PANEL, PRESS, C OFF 29-2131-9-0006 8148 ON 29-2131-9-0006 6729 CONTROLLER, CAB OFF 58-2131-9-0002 0317 ON 58-2131-9-0002 0453 PER SAMC REPLACED BOTH CABIN PRESSURE CONTROLLERS REF AMM21-31- 01-000-801 AND CABIN PRESSURE CONTROL MODULE REF AMM21-31-02-000 -801. TESTED GOOD REF AMM21-31-00-700-802 AND AMM21-31-00-700-80 2. CKS OK.. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1281742 SN OFF 8148 TT # 1040906 SN OFF 0317 ENTERED FOR PARTS UPDATE ROTABLE PARTS CHANGE WAS INDICATED - TT # 1228060 SN OFF 6430 CONTROLLER, CAB OFF 58-2131-9-0002 6430 ON 58-2131-9-0002 6142

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,205 hrs · 7,814 cycles

LEFT OVERWING AFT EMERGENCY LIGHT INOPERATIVE. FOUND THE POWER SUPPLY M1670 AT FAULT IAW WDM 33-51-13, PG 9, SHT 2. REPLACED THE POWER SUPPLY IAW AMM 33-51-06-960-806, OPS TESTED NORMAL.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 23,139 hrs · 7,784 cycles

CABIN ALTITUDE HORN WENT OFF, CLIMBING THRU 30K. CABIN ALTITUDE LIGHT ALSO ON CONTROLLABLE IN MANUAL. EMERGENCY DECLARED. REMOVED AND REPLACED NR 1 CABIN PRESSURE CONTROLLER IAW AMM 21-31-00 AND TESTED, SYSTEM TESTED OK, NO FAULTS NOTED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 22,873 hrs · 7,698 cycles

EMERGENCY LIGHT LENS MISSING AT FWD CABIN NEAR CLOSET 712 REMOVED AND REPLACED MONUMENT LIGHT REF IPC 25-20-23 ITEM 165. CKS GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,772 hrs · 7,659 cycles

MID EMERGENCY LIGHT INOPERATIVE. REMOVED & INSTALLED A SERVICEABLE EMERGENCY BATTERY CHARGER ASSY. OPS CHECKED GOOD, NO FAULTS NOTED.

Part: LIGHT — BROKEN (CABIN) · airframe 21,412 hrs · 7,184 cycles

15C EEL LITE BROKEN. REMOVED AND REPLACED BROKEN EEL LIGHT ON SEAT 15C. REF AMM 33-51 -11. OPS CK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,412 hrs · 7,184 cycles

21C SEAT LIGHT INOP. REMOVED AND REPLACED INOP SEAT EMERG LIGHT AT SEAT 21C. OPS CK NORMAL REF AMM 33-51-11.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 20,542 hrs · 6,905 cycles

CRACK FOUND AT RT HORIZONTAL STAB LOWER SKIN AT STA 129.5 APPROX 18" FROM T/E AND .375 I/B OF I/B FASTENER ROW. CRACK LENGTH 1.125" CUTOUT AREA AT RT HORIZONTAL STAB LOWER SKIN STA 129.5 PER B737-800 SRM 55-10-01 FIG 204 REPAIR 11, HFEC INSP AT CUTOUT AREA PER 51-00-00-23, FABRICATED FILLER AND DOUBLER PER SRM 55-10-01, TREATED AND PRIMED FILLER AND DOUBLER AND SKIN PER SRM 51-20-01. INSTALLED FILLER AND DOUBLER REPAIR PER B737-800 SRM 55-10-01 FIG 204 REPAIR 11 SHEET 213. DIP REQUIREMENTS FOR RE-INSPECTION INITIATED ON ELB.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 20,542 hrs · 6,905 cycles

CRACK FOUND AT RT HORIZONTAL STAB LOWER SKIN AT STA 175.5 APPROX 9.5" FROM L/E AND .200 I/B OF I/B FASTENER ROW. CRACK LENGTH .500". CUTOUT CRACKED AREA AT RT HORIZONTAL STAB STA 175.5 PER B737-800 SRM 55-10-01 FIG 204 REPAIR 11, HFEC INSP AT CUTOUT AREA PER 51-00-00-23. FABRICATED FILLER AND DOUBLER PER SRM 55-10-01. TREATED AND PRIMED FILLER AND DOUBLER PER SRM 51-20-01. INSTALLED FILLER AND DOUBLER REPAIR PER SRM B737-800 SRM 55-10- 01 FIG 201 REPAIR 11 SHEET 213. DIP REQUIREMENTS FOR RE-INSP INITIATED AND ACCOMPLISHED ON ELB LP 3779530.

Part: ENGINE — FAILED (NR 2) · airframe 19,109 hrs · 6,438 cycles

NR 2 ENGINE SHUTDOWN BY CREW AFTER OIL TEMP CLIMBED INTO YELLOW AND THEN WENT INTO RED. SHORTLY AFTER, OIL FILTER BYPASS AND OIL QTY DECREASE. ENGINE WINDMILL APPROX 45 MINS. REPLACED NR 2 ENGINE IAW W/C 29-7100-1-4900, 29-7100-1-0900, & AMM 71-00-02-400-801-FOO.

Part: FILTER — ODOR (RECIRC FAN) · airframe 6,539 hrs · 2,162 cycles

AT ROWS 4 AND 20 AND 21, THERE WAS A BURNING ODOR OF ELECTRIC WIRE BUT NO SMOKE. PERFORMED TASK 05-51-26-800-801 C1 NO TROUBLE FOUND PERFORMED HIGH POWER RUN ON BOTH ENGINES NO PROBLEM FOUND OPERATION OF BOTH PACKS AT VARIOUS TEMPS CHECKS NORMAL. R & R BOTH RECIRCULATION FAN FILTERS IAW AMM 21-25-01-000-801, OK TO CONTINUE.

Part: CONTROL LEVER — FAILED (COCKPIT) · airframe 2,369 hrs · 754 cycles

AFTER TAKEOFF WITH THE GEAR LEVER IN THE OFF POSITION ALL GEAR LIGHTS WERE EXTINGUISHED. DURING CLIMB AT 13572 GEAR UNSAFE RED LIGHTS ILLUMINATED FOR ALL 3 GEARS. AT 14132 WERE UNSAFE LIGHTS EXTINGUISHED. NO ABNORMAL YAW, VIBRATION, OR NOISE OBSERVED DURING EVENT. REMOVED AND REPLACED LANDING GEAR CONTROL MODULE LEVER IAW 32-31-11. PERFORMED LANDING GEAR TEST IAW AMM 32-32-00. OPS CHECK GOOD NO DEFECTS NOTED. ROTABLE PARTS CHANGE WAS INDICATED - TT 1431907 S/N OFF 03733 MODULE, LANDING OFF 29-3231-9-0010 3733 ON 29-3231-9-0010 0323

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 1,728 hrs · 562 cycles

AFTER TAKEOFF WENT TO RAISE THE GEAR AND WITH GEAR HANDLE IN UP POSITION ALL 3 RED GEAR LIGHTS STAYED ON. MOVED GEAR HANDLE TO OFF POSITON AND 3 RED GEAR LIGHTS STILL STAYED ON. CHECKED THE 5 ROWS OF CIRCUIT BREAKERS ON P6-3 ALL WERE IN AFTER 1 TO 1.5 MINUTES LIGHTS WENT OUT A/C SOUNDED AND FLEW LIKE GEAR CAME UP NORMAL. PERFORMED FIM TEST 32-09 TASK 801 NO DEFECTS NOTED. SWUNG GEAR SEVERAL TIMES NO DEFECTS NOTED A/C OK TO CONTINUE.