AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: LOST ABOUT 1QT OF OIL PER 15-20 MIN IN FLIGHT ON NUMBER 1 ENGINE; AIRCRAFT DIVERTED TO AND LANDED SAFELY AT CLT. PERFORMED TSI, FOUND OIL FILTER CAP O-RING CUT IN HALF. REMOVED AND REPLACED OIL TANK FILLER CAP, PER AMM 79-11-03. PERFORMED OPERTIONAL AND LEAKS NO LEAKS NOTED.

R/H HORIZONTAL UPPER SLIDING SEAL CRACKED FWD AND AFT SIDES

AIRCRAFT WAS GROUNDED: DURING FLIGHT AT CRUISE AT FL 210 USING ALL AUTOMATION CONTROL, WHILE REDUCING SPEED THE AUTO THROTTLE REDUCES THE POWER THEN THE GEAR HORN GOES OFF AND THE 3 GEAR RED LIGHTS COME ON. REMOVED AND REPLACED SPOILER CONTROL UNIT (AALA202504176310), PER AMM 27-61-45. ACCOMPLISHED PSEU CHECK AND TEST PER AMM 32-09-10. ACCOMPLISHED LMP TEST PER GPM 16-10. ACCOMPLISHED TSI MIC 0113390. ALL TEST PASSED. REMOVED AND REPLACED PSEU (AALA202504226211), PER AMM 27-61-45. ALL TEST PASSED.

AIRCRAFT WAS GROUNDED: DURING FLIGHT AT CRUISE AT FL 210 USING ALL AUTOMATION CONTROL, WHILE REDUCING SPEED THE AUTO THROTTLE REDUCES THE POWER THEN THE GEAR HORN GOES OFF AND THE 3 GEAR RED LIGHTS COME ON. (OPEN).

RIGHT HORIZONTAL STAB TO BODY UPPER FRONT SPAR SLIDING SEAL IS CRACKED.

AIRCRAFT WAS NOT GROUNDED: REPEAT WRITE UP: WHEN LEFT WING FORWARD FUEL BOOST PUMP IS TURN OFF THE LOW PRESSURE LIGHT DID NOT IMMEDIATELY ILLUMINATE. AFTER 1 MINUTE AND 30 SECONDS IT'S LOW PRESSURE LIGHT FINALLY ILLUMINATED ALONG WITH THE MASTER CAUTION AND SYSTEM ANNUNCIATOR FUEL LIGHTS. REPLACED PRESSURE SWITCH. PER MM 28-42-11.

LEFT HORIZONTAL STAB TO BODY UPPER FRONT SPAR SLIDING SEAL IS CRACKED.

AFTER #2 ENGINE START; DURING TAXI; WHILE STARTING #1 ENGINE; NO. 2 HAD UNCOMMANDED SHUTDOWN WITH NO INDICATIONS.

AIRCRAFT WAS GROUNDED: REPEAT RECURRING ISSUE WITH GEAR WARNING HORN GOES OFF WHEN THROTTLES PULLED BACK, ALONG WITH 3 RED GEAR LIGHTS. HORN CUTOUT WILL SILENCE THE HORN.HAD TO REDUCE SPEED IN CRUISE AND WHEN THRUST WAS REDUCED, THE HORN WENT OFF. REPLACED LRRA SYSTEMS 1 (AALA202504165893) AND 2 (AALA202504170737) ANTENNAS AND TESTED GOOD, PER AMM 34-31-11. PERFORMED J/C 09C21031001 OPERATIONAL TEST LANDING GEAR LOGIC MODULE OUTPUT TO THE AURAL WARNING MODULE, NO FAULTS NOTED.

BOTH CAPT & FO FD FAILED; MACH TRIM FAILED LIGHT ILL; A/P FAILED; A/T FAILED

ALL 4 WINDOW OVHT LIGHTS ILLUMINATED. COMPLIED W /FM PROCEDURE. LIGHTS REMAINED ILLUMINATED. FOUND ALL 4 CIRCUIT BREAKERS OPENED. RESET ALL CBS AND PERFORMED OPERATIONAL TEST FOR WINDOW HEAT TEST AND OVERHEAT TEST PER AMM 30-41-00-710-801. AS A PERCAUTION REMOVED AND REPLACED WINDOW PITOT HEAT MODULE PER AMM 30-00-02-400-801. OPERATIONAL CHECKED OK PER AMM 30-31-00-730-801.

#4 BRAKE CLIPS CRACKED/MISSING RIVETS R&R #4 BRAKE ASSY REF AMM 32-41-41. OPS/LEAK CK GOOD. PARTS USED: 60-3241-9-0001,QTY :1 ROTABLE PARTS CHG:TT # 1591018 SN OFF 1150 PN OFF 60-3241-9-0001 BRAKE, MLG, CAR OFF 60-3241-9-0001 1150 ON 60-3241-9-0001 8508

AIRCRAFT WAS GROUNDED: GEAR WARNING HORN COMES ON AND RED GEAR LIGHTS COME ON DURING DESCENT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED**(OPEN).

AIRCRAFT WAS GROUNDED: GEAR WARNING HORN COMES ON AND RED GEAR LIGHTS COME ON DURING DESCENT. **SUPPLEMENTAL REPORT FOR (AALA202504116493): FOUND POWER SYSTEM FAULTS ON PSEU. REMOVE AND REPLACED PSEU (AALA202504116493), PER AMM IAW 32-09-10. REMOVE AND REPLACED LANDING GEAR CONTROL MODUL (AALA202504177012), PER AMM 32-31-11**(CLOSED).

DOOR 1L GIRT BAR DIFFICULT TO ARM/DISARM CHECKED AND CLEANED FLOOR MOUNTED SLIDE BRACKETS AND CHECKED GIRT BAR RELEASE FOR SECURITY NO DIFFICULTY NOTED IN ARMING SLIDE ASSY IAW AMM TASK 03-25-66-200-801.

T/O ROLL APPROX 50KTS BOTH LEFT FWD OVERWING AND LEFT AFT OVERWI NG ILLUMINATED. CYCLED DOORS AND LIGHT EXTINGUISHED.OPS CHECK GOOD OF INDICATION. CLEARED FAULTS IN PSEU. NO FURTHER MESSAGES REF FIM 52-20 .

CREW REPORTED BURNING RUBBER SMELL AFTER LANDING

AIRCRAFT WAS GROUNDED: LANDING GEAR WARNING HORN AND GEAR UNSAFE LIGHTS ILLUMINATED MULTIPLE TIMES DURING DESCENT. REPLACED NUMBER 2 RADIO ALTIMETER.

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: WEATHER RADAR AND PWS FAILED MULTIPLE TIMES; AIRCRAFT DIVERTED TO AND LANDED SAFELY AT CTG. REMOVED AND REPLACED THE WEATHER RADAR TRANSCEIVER (AALA202504083644), PER AMM 34-41-41-401. OPERATIONAL CHECKED SUCCESSFUL. REMOVED AND REPLACED THE WEATHER RADAR PROCESSOR (AALA202504087761), PER AMM 34-41-42-401. OPERATIONAL CHECKED SUCCESSFUL.

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: WEATHER RADAR AND PWS FAILED MULTIPLE TIMES; AIRCRAFT DIVERTED TO AND LANDED SAFELY AT CTG. **SUPPLEMENTAL REPORT FOR (AALA202504083644): REMOVED AND REPLACED THE WEATHER RADAR TRANSCEIVER (AALA202504083644), PER AMM 34-41-41-401. OPERATIONAL CHECKED SUCCESSFUL. REMOVED AND REPLACED THE WEATHER RADAR PROCESSOR (AALA202504087761), PER AMM 34-41-42-401. OPERATIONAL CHECKED SUCCESSFUL**(CLOSED).

EMERGENCY LIGHTS OPERATIONAL CHECK EMERGENCY LIGHTS OPERATIONAL CHECK - PASSENGER ECONOMY FORWARD OF EMERGENCY DOORS SECTION LIGHT INOP. FOUND POWER SUPPLY M2335 TEST BUTTON INOP. REPLACED IN REFERENCE TO AMM 33-51-06. ALSO FOUND EXPOSED WIRE ON SEAT 15ABC CAUSING SHORTS. RETAPED BARE WIRE. OPS CHECK GOOD.PARTS USED: 99-3351-3-0009, QTY :1 29-3351-3-0031, QTY :1

AIRCRAFT WAS GROUNDED: GEAR WARNING HORN AND RED LIGHTS ON INTERMITTENTLY ON DESCENT FROM FL230 TO ABOUT 15000. PERFORMED BITE TEST ON BOTH LRRA TRANSCEIVERS, PER AMM 34-33-00 BITE TEST PASS. FOUND ALL SCREWS ON ALL 4 LRRA ANTENNAS LESS THAN 30 INCH LBS. HALF TURNED ALL SCREWS ON ALL 4 LRRA ANTENNA TO 30 INCH LBS, PER AMM 34-33-11. PERFORMED LRRA SYSTEM OPERTIONAL TEST GOOD, PER AMM 34-33-00.

POTENTIAL ESCAPE SLIDE ISSUE. EXCESSIVE MATERIAL SHOWING ATTACH ED TO GIRT BAR. DOOR 1R. SECURED EXCESSIVE MATERIAL ON GIRT BAR

#2 TIRE TREAD CAME OFF DURING TAKE OFF ROLL IN ATL CAUSING MULTIPLE POINTS OF DAMAGE AROUND THE LANDING GEAR. GROUNDED - YES. FOUND MULTIPLE POINTS OF DAMAGE FROM TIRE TREAD SEPARATION ON UPPER + LOWER AFT FLAP AND PANELS SURROUNDING L/H MLG. PERFORMED INSPECTION OF FUSELAGE, LANDING GEAR, #1 ENGINE AND COWLS, WHEEL WELL IAW AMM REF 05-51-59 AND 05-51-54. REMOVED AND REPLACED #2 AND #1 MLG TIRE REF AMM 32-45-11-400-801.

GIRT BAR 1L NOT LOCKING WHEN DISARMED READJUSTED GIRT BAR PER AMM 25-66-02. NO DEFECTS NOTED AT THIS TIME

MASTER CAUTION FIRE WARNING BELL CUTOUT MULTIPLE 6 PACK LIGHTS ILLUMINATED WITH ODOR DEBRIEFED CREW NO FIRE OR SMOKE NOTICED OR VISIBLE. PERFORMED CONDITIONAL INSP PER AMM 05-51-56. INSPECTED FWD GALLEY AREA INCLUDING COFFEE MAKERS AND OVENS NO ISSUES FOUND. RAN ACFT AIR COND PACKS AND NO FUMES OR SMOKE FOUND. PERFORMED FIRE OVERHEAT TESTS AND UNABLE TO DUPLICATE. SUSPECT INTERMITTANT FAULT ASSOCIATED WITH ENGINE AND APU FIRE DETECTION CONTROL MODULE. REMOVED AND REPLACED MODULE REF AMM 26-10-01. OPS CK GOOD. NO FURTHER FAULTS FOUND. OK TO CONTINUE.

CABIN ALT WARNING. NO PAX OXY DEPLOYED ALTIUDE CONTROLLABLE IN MANUAL AT 15000 AHM REPORTED MM 36-12021 E2 FAMV IS NOT IN COMMANDED POS. REPEAT FAULT ALSO REPORTED ON LOG PAGES 4287368 AND 4285383. DEBRIEFED CREW AND AFTER FOLLOWING QRH AND TURNING OFF E1 BLEED AND PACK 1 CREW SAW E2 BLEED SURGING BEFORE GETTING CABIN ALT WARNINGS. INSPECTED PRECOOLER KISS SEAL [6] AND VERIFIED INSTALLATION AND SECURITY. REF. AMM 36-12-03-400-801 STEP G (1). INSTALLED #2 ENG FAMV PER AMM 36-12-03-400-801 UP TO STEP I. REF AMM 36-12-03-400-801 FOR REMAINDER OF OPS CHECKS ON ENGINE 2 FAMV. LEAKS AND OPS CHECK GOOD.

#1 O/B TIRE DAMAGED BEYOND LIMITS. EVERBRIDGE: DURING LANDING ROLL, THE #1 MLG TIRE TREAD SEPARATED FROM THE TIRE ASSEMBLY WHICH RESULTED IN OUT-OF-LIMIT DAMAGE TO THE WING ACCESS PANEL, AND DENTS TO LOWER WING AND FLAP SURFACES. ALL 4 TIRES REMAINED INFLATED UPON ARRIVAL AT THE GATE. GROUNDED - YES. ACCOMPLISHED CONDITIONAL INSPECTION FOR TIRE TREAD LOSS REF AMM 05-51-54-210-801. FOUND LEFT HAND WING IB MAIN FLAP LOWER SKIN BENT. MEASURES 6" FWD TO AFT , 4" OB TO IB, 1/4" DEEP, CRACKED ACCESS PANEL 551DB CRACKED AND DENT ON LOWER IB PANEL 551FB, 12" LONG CRACK, 2" FWD TO AFT AND 4" OB TO IB DENT, 1/4" DEEP. CRACKED CLIP ASSEMBLY BY IB GROUND SPOILER ACTUATOR BRACKET. REQUIRES OP CHECK OF TRAILING EDGE FLAP SYSTEM AND SPEED BRAKE CONTROL SYSTEM TEST. SEE LOG PAGE 61084265 FOR MLG #1 & 2 TIRE REPLACEMENT. NEEDS FURTHER INSPECTION. DM 03/30/2025 4875729 REFMM 57-71-01 REPLACED CLIP ASSY AIPC 57-16-51-02 ITEM 290. SPEED BRAKE OPS TEST GOOD MM 27-62-00. FLAPS OPS CK GOOD. MM 27-51-00.

ELECTRICAL SMELL /NO SMOKE REAR OF AIRCRAFT DID NOT INCREASE DECLARED EMERGENCY RETURNED NO ABNORMAL INDICATION IN COCKPIT (CREW REPORTS NO OVERWEIGHT LANDING ) 67949

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO MIA DUE TO LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED. NUMBER 3 SLAT AMBER ON OVERHEAD PANEL. THE AIRCRAFT LANDED SAFELY AT MIA WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED SLAT PROXIMITY SENSOR S998 IAW AMM 27-88-11-400-801. OPERATIONAL CHECK GOOD.

FLAPS WOULD NOT EXTEND PAST 25 DEG

ENGINE CONTORL ALT LIGHT STAY IN ON LH SIDE

APU MAKING BACKFIRING NOISE. SKUNK SMELL IN FWD COCKPIT & MILD FUEL SMELL IN CABIN

AT 105 KNOTS DURING TAKEOFF GOT FIRE WARNING AND MASTER CAUTION LTS AND FIRE WARNING BELL. REJECTED THE TAKEOFF. AT 105 KNOTS DURING TAKEOFF GOT FIRE WARNING AND MASTER CAUTION LTS AND FIRE WARNING BELL. REJECTED THE TAKEOFF DID NOT SEE AND ENGINE OR APU FIRE HANDLE ILLUMINATED. FIRE TRUCK VISUALIZE CONFIRMS NO FIRE.

#1 SPOILER CRACK AT O/B AFT

#2 ENGINE ACOUSTIC SHROUD WAS FOUND TO HAVE CRACK AT 9 OCLOCK POSTION MEASURING APPROX. .750 FORWARD TO AFT. #2 ENGINE ACOUSTIC SHROUD WAS FOUND TO HAVE CRACK AT 9 OCLOCK POSTION MEASURING APPROX. .750 FORWARD TO AFT.

AIRCRAFT WAS NOT GROUNDED: REPEAT PREVIOUS WRITE UP: WITH 700 POUNDS OF FUEL IN THE CENTER TANK WE TURNED ON BOTH CENTER TANK FUEL PUMPS AFTER LEAVING 10000 FEET. THE LEFT CENTER FUEL PUMP LIGHT ILLUMINATED AND THE CENTER TANK FUEL INCREASED FROM 700 TO 930 POUNDS OF FUEL. DURING THE SAME TIME THE LEFT MAIN TANK FUEL DECREASED BY ABOUT A 400 POUND DIFFERENCE WITH THE RIGHT MAIN TANK FUEL. MAINTENANCE VERIFIED LEFT CENTER TANK BOOST PUMP INOPERATIVE. REMOVED AND REPLACED R54 RELAY, OPERTIONAL CHECK GOOD. PER AMM 25-22-18**(CLOSED).

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK RIGHT HAND SLIDING WINDOW WILL NOT OPEN, THE EMERGENCY LATCH ON OUTSIDE OF AIRCRAFT BENEATH THE WINDOW IS NOT FLUSH AND SLIGHTLY CROOKED. MAINTENANCE FOUND THE WINDOW FRAME HAD EXCESSIVE PRIMER / PAINT WHICH WAS REMOVED. MAINTENANCE ALSO LUBRICATED THE WINDOW SEAL AND ACCCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 56-12-11.

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AN THE AIRCRAFT DIVERTED TO ATL DUE TO AUTO PRESSURIZATION FAILURE. THE AIRCRAFT LANDED SAFELY AT ATL. AIRCRAFT WAS ON AN MEL FOR CABIN PRESSURE CONTROLLER #2 INOPERATIVE. MAINTENANCE REPLACED THE OUTFLOW VALVE PER AMM 21-31-03 (AALA202503086361) AND THE #2 CABIN PRESSURE CONTROLLER REF AMM 21-31-01 (AALA202503089000). ACCOMPLISHED SATISFACTORY LEAK AND OPERATIONAL CHECKS.

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AN THE AIRCRAFT DIVERTED TO ATL DUE TO AUTO PRESSURIZATION FAILURE. THE AIRCRAFT LANDED SAFELY AT ATL. AIRCRAFT WAS ON AN MEL FOR CABIN PRESSURE CONTROLLER #2 INOPERATIVE. MAINTENANCE REPLACED THE OUTFLOW VALVE PER AMM 21-31-03 (AALA202503086361) AND THE #2 CABIN PRESSURE CONTROLLER REF AMM 21-31-01 (AALA202503089000). ACCOMPLISHED SATISFACTORY LEAK AND OPERATIONAL CHECKS.

ACRID SMELL WHEN LH & RH RECIRC FANS ARE ON SMELL DISSIPATES WHEN TURNED OFF

BURNING SMELL ON FLT DECK AFTER REPORT FROM GROUND. NO SMOKE O BSVD. REF LOGPAGE 3812980. DUE TO APU AUTO SHUTDOWN. APPLIED FIM 21-00/830 STEP K. FAULT ISOLATION PROCEDURE (APU). NO SMELL FUMES OR SMOKE NOTED. OK FOR SERVICE PER FIM.

L2 DOOR HARD TO OPEN AND CLOSE HINGE AREA MAKES NOISE WHEN OPENING OR CLOSING. GROUNDED - YES. NO NOISE NOTED AT HINGE AREA, NOISE COMING FROM CONTACT BETWEEN DOOR LINER SEAL AND DOOR SURROUND SEAL, LUBRICATED SEALS WITH VASELINE (NO MORE NOISE). PERFORM AFT ENTRY DOOR SYSTEM TEST ALL FORCES WITHIN LIMITS DOOR IN RIG REF AMM 52-13-00.

SEAT FLOOR AISLE EMERGENCY PATH LIGHTS, ROWS 1AB THRU 5AB INOP. REPLACED EMERGENCY POWER SUPPLY CHARGER M1675 AT STATION 310 FWD CEILING PANEL JUST AFT OF FWD LAV A PER AMM TASK 33-51-06. SEE DWG 3351DD16408 FOR INFO ON ELP MAX 9 INSTALL FOUND POWER SUPPLY M2816 F2 FUSE BLOWN.REPLACED AND BLOWN AGAIN ,ISOLATED SEATS,AND FOUND ROW 4 BLOWNING THE FUSE, DISCONNECTED SEAT HARNESS UNDER SEAT 4A, SEE PHOTO ,NOW ALL LIGHTS WORK EXCEPT ROW 4B,PLACED ON MEL MEL 3351D APPROVED BY TOMC. AISLE 4B INOP. ALL OTHERS WORK. OK TO CONTINUE ON MEL SEAT 4B EMERGENCY PATH LIGHT IS INOP. FOUND BROKEN WIRE SHOTED TO GROUND, REPAIRED WIRE IAW SPWM 20-30-19

PDA 2 #4 TIRE THREAD SEPARATED FROM TIRE. UNKNOWN IF IT HAPPENED ON TAKE OFF OR LANDING.

EMERGENCY LIGHTS OPERATIONAL CHECK EMERGENCY LIGHTS OPERATIONAL CHECK - PAX SEATS 28 CBA -34CBA EMERGENCY PATH LIGHT NOT ILLUMINATING. INSPECTED CONNECTIONS OF WIRING FROM PAX SEAT 30 TO SIDEWALL F.S. 727K +10.00. REF UNITED DWG 3351DD16408. NO LOOSE CONNECTERS. FURTHER TROUBLESHOOTING REQUIRED. FURTHEST AFT AND FWD EMERGENCY PATHWAY LIGHTS AND ADJACENT LIGHTS ARE OPERATIVE. INOPERATIVE LIGHTS NOT ADJACENT ARE INOPERATIVE. REF MEM 33-51-03-01-01. PLACARD INSTALLED. REQUEST DEFERRAL. COMPLIED WITH DDP REMOVED AND REPLACED ALL 4 FUSES IN M1670 EMERGENCY LIGHT POWER SUPPLY. NO HELP. REF AWM 33-51-22-4. MORE TROUBLESHOOTING NEEDED. R&R M 1670 POWER SUPPLY ASSY NO HELP. REMOVED NEW PART AND INSTALLED ORIGINAL PART.REQUIRES FURTHER TROUBLE SHOOTING.

MILD TO MODERATE ELECTRICAL SMOKE SMELL IN FLIGHT DECK. LESS W ITH LT PACK OFF. FOUND TO BE LT PACK AT FAULT, PLACED LEFT PACK ON MEL, DDP C/W FOLLOWED FIM TASK 21-00 TASK 830 FOUND TO BE LT PACK AT FAULT, PLACED LEFT PACK ON MEL, DDP C/W DEFERRED DIRECTLY BY TOMC FOLLOWED FIM 21-00 TASK 830. FOUND MILD SWEET SMELL IN FLIGHT DECK WITH LEFT PACK RUNNING ON WARM. INSPECTED LT PACK BAY NO DEFECTS NOTED. INSPECTED APU COMPARTMENT AND APU INLET FOUND SPLASHED OF SUSPECTED DE ICE FLUID. CLEAN OFF FLUID AND REPLACED BOTH RIGHT AND LEFT RECIRCULATION AIR FILTERS AS PRECATIONARY REF AMM 21-25-01. OPERATED LEFT PACK NO UNSUAL FUMES OR ODORS NOTED AT THIS TIME IN THE FLIGHT DECK.

MAINT LIGHT ILL AS SOON AS MCD CLOSEDSTATUS PAGE SHOWS APU GEN FAULT MSG 49-41244 REQ TO MEL 4911A DISPATCH DESK: 93 NAME: NL DATE: 03-FEB-25- NOC DESK: 737 NAME: MM DATE: 03-FEB-25- MEL 4911A APPROVED. UPON CLEARING THIS MEL ITEM, CONTACT TOMC FOR ASSIGNMENT OF MEL CARD 49001 OR 49003 TO ACCOMPLISH APU ETOPS VERIFICATION FLIGHT. DDP CW. UPON CLEARING THIS MEL ITEM, CONTACT TOMC FOR ASSIGNMENT OF MEL CARD 49001 OR 49003 TO ACCOMPLISH APU ETOPS VERIFICATION FLIGHT REMOVED AND REPLACED APU STARTER GENERATOR IAW AMM 49-41-21/401, APU STILL DOESN'T START. FOUND 2 ACTIVE FAULT MESSAGES ONBOARD MAINTENANCE FUCTION. 49-41026 AND 49-41244. PERFORMED ADD EMP:U421939 TROUBLESHOOTING IAW FIM 49-40 TASK 806, CONTINUITY CHECK GOOD ON ALL WIRES BETWEEN P6 AND D11114B PER STEP D. (2) (C). NEXT STEPS ARE CHANGING APU START CONVERTER UNIT AND APU ELECTRONIC CONTROL UNIT. PARTS NOT IN STOCK AT SNA. DURING T/S NOTICED APU INLET DOOR NOT OPENING ON APU MANAGE OF REMOVED PART.

FOUND OVER HEAD PANEL EMERGENCY LIGHT NOT ARMED ILLUMINATION LIGHT INOP RELAMPED INDICATOR REF AMM 33-18-00

HYD PUMP B SIDE ELEC 1 LOW PRESS LIGHT ILLUMIN ATED IN FLIGHT UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. LOCKED LP. UNLOCKED. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. LOCKED LP. UNLOCKING FOUND ELECTRIC SIDE OF PUMP AND CONNECTOR WARM TO TOUCH AND PUMP SIDE COLD. PUMP SEIZED. REPLACED B SYSTEM PUMP, REMOVED AND INSPECTED CASE DRAIN FILTER. NO CONTAMINATION NOTED. REPLACED CASE DRAIN FILTER WITH NEW. REF MM29-11-21 AND MM29-11-41. OPS AND LEAK CHECKED GOOD.

AFT ENTRY DOOR LIGHT IN FLIGHT. DOOR HANDLE MOVE D 3 INCHES AND REQUIRED FA TO HOLD IT DOWN ACCOMPLISHED RIG/ADJUSTMENT CHECK OF AFT ENTRY DOOR REF AMM 52 -13-00-820-801 STEP 2A THROUGH AND INCLUDING 2N PG 12. FOUND UPPER GATE FLUSHNESS TO FUSELAGE EXCESSIVE AND ADJUSTED TO WITHIN LIMITS. ALSO FOUND UPPER AFT LATCH ROLLER RECEIVER AND FWD LOWER LATCH RECEIVER WITH EXCESSIVE ROLLER GAP AND ADJUSTED RECEIVERS TO WITHIN PROPER LIMITS STEP N. NEED TO CONTINUE WITH STEP O. ACP RII INSP OF L2 DOOR ADJ AND TEST REF AMM 52-13-00-820 UP TO AND INCLUDING STEP N. TPAQC UNLOCKING . COMPLETED DOOR RIG/ADJUSTMENT REF 52 13-00-820-801 FOUND ALL STOP PINS OUT OF ADJUSTMENT AND UPPER GATE NEEDED SMALL ADJUSTMENT TO GET HANDLE ( INNER ) IN LIMITS W TORQUE COMPLIED WITH INSPECTIONS OF L2 DOOR REF GMM 09-25-05 AND AMM 52-13-00-820-801. ACP DOOR RIG REF AMM 52-13-00-820-801 FOUND ALL DOOR STOP PINS OUT OF ADJUSTMENT AND UPPER GATE OUT OF ADJUSTMENT MADE ADJUSTMENTS ALONG WITH PREVIOUS FINDINGS FROM MAINTENECE ALL ITEMS APPROVED BY INSPECTION AC OK FOR FERRY FLIGHT FOR DOOR CK

ENG 1 OVERHEAT LIGHT IS ON PASSING 25K ENG OVRHT LIGHT CAME ON DID IMMEDIATE ACTIONS REDUDC ED PWR WENT OUT T/S REF FIM TASK 26-11. ALL FAULTS IN OMF SHOW NOT ACTIVE. FOUND ENGINE/APU FIRE DETECTION MODULE, M279 FAULTING THE BOX. REPLACED ENGINE/APU FIRE DETECTION MODULE, M279 REF AMM 26-10-01. OPS CK AND TESTS NORMAL PARTS USED: 1424347,QTY :1ROTABLE PARTS CHANGE WAS INDICATED - TT # 1424347 SN OFF 1620 MODULE, FIRE DE OFF 42-2610-9-0001 1620 ON 42-2610-9-0001 1239

PROBE HEAT LIGHT COMES ON TEMP PROBE LT ON IN FLIGHT PIC ADDED R&R TOTAL TAT PROBE IAM AMM TASK 34-21-06-000-801/400-801, R&R WINDOW/PITOT HEAT MODULE IAW AMM TASK 30-00-02-400-801. PERFORMED SYSTEM TEST PITOT PROBE, AOA SENSOR AND TAT PROBE HEAT IAW AMM TASK 30-31-00-730-801. ALL TEST PASS, NO MX MSG ON DISPLAY. APPLIED SEALANT ,OPS CKD OK REF. AMM34-21-06-400-801.

FWD ENTRY DOOR OPEN LT ILLUMINATED ON T/O AT 80 KTS. T/O REJECTE D. VERIFIED L1 DOOR WAS CLOSED UPON COMING BACK TO THE GATE, CYCLED L1 ENTRY DOOR INDICATION IS NORMAL AS PRECAUTIONARY REQUEST MEL FOR DOOR INDICATION INOP DISPATCH DESK: 41 NAME: ATE: 28-JAN-25- TOMC OK VERIFIED THAT L1 DOOR IS CLOSED AND LOCKED. OK TO CONTINUE ON MEL. FAULT CODE 52-71111 PRESENT AT FAULT HISTORY ADDED PHOTO NO TIME FOR T/S *DM* REF FIM 52-20 TASK 801 FOR MSG 52-71111. ADDED SENSOR (S199) AND PSEU (M2061) IN CASE NEEDED. PARTS UPDATED. T/S PER FIM 52-20 TASK 801 AND WDM 52-71-11. VERIFIED CORRECT GAP ADJUSTMENT OF S199 PER AMM 52-71-11-820-801, GAP CHECKS OK. AS PRECAUTIONARY WILL REQUIRE S199 FORWARD ENTRY DOOR SENSOR REMOVAL AND REPLACEMENT WITH GAP ADJUSTMENT. MEL REMAINS. FAULT HISTORY SHOWS PSEU FWD ENTRY DOOR SENSOR IS TARGET FAR DURING TAKEOFF. MAINTENANCE MESSAGE 52-71111 NOT ACTIVE. ADJUSTED FWD ENTRY DOOR INDICATION SENSOR S199 IAW AMM 52-71-11-820-801. DOOR OPS CKS NORMAL. FLIGHT DECK LIGHT INDICATIONS OPERATE NORMAL. NO FURTHER FAULTS NOTED.

DOOR 2L GIRT BAR BRACKET S ARE TOO LOOSE. BAR IS EASILY BUMPED O UT OF PLA CE AND IS UNSAFE. ADJUSTED BOTH GIRT BAR RETAINER HOOKS, OPS CHECK GOOD. REF AMM 25-66-01

WHILE T/S LAV RT LIGHT PROBLEN FOUND BUNDLE W3144 NEAR CONNECTOR D15864 BURNED. SEVERAL WIRES BROKE. TOTAL 11 WIRES DAMAGED ON CONNECTOR D15864. 3 BROKEN, 8 CHARRED AND CHAFFED DAMAGED WIRES CIRCUIT BREAKERS PULLED TO DEACTIVATE ALL LAVS REF AMM 25-40-00-040-802. REF SWPM 20-30-13, REPAIRED DAMAGED WIRES W3144-0730-18, W3144-0850-20, W3144-0851-20, W3144-0856-22, W3144-0857, W3144-0867-20, W3144-0868-20, AND W3144-2703R&B-22 BY SEALED SPLICE IAW SWPM 20-30-12. WIRE W3144-0874-18 FOUND MINOR DAMAGE TO INSULATION REPAIRED WITH TAPE&TIES, REMAINING WIRES IN BUNDLE CLEANED REF SWPM 20-10-04 AND INSPECTED WITH NO DAMAGE NOTED. RESECURED BUNDLE AND APPLIED CHAFF PROTECTION REF SWPM 20-10-26.

WORK ORDER 92849, NR00001: MULTIPLE SMOKED FASTENERS ON THE R/H WING JUST INBOARD OF THE #2 ENGINE PYLON WHEN PRESSING ON PANEL IT APPEARS THAT THE FASTENERS ARE LOOSE AND MAYBE SHEARED. ACCOMPLISHED REPAIR ON RH WING LOWER FIXED TRAILING EDGE PANEL I/B OF #2 PYLON IAW B737-800BCF SRM 51-70-04.

LEFT NOSE WHEEL TIRE, INBOARD WHEEL HALF DISINTEGRATED UPON LANDING. WILL REQUIRE FURTHER INSPECTION OF AIRCRAFT FOR DAMAGE.

FA REPORTS DOOR R1 DIFFICULT TO DISARM CREW REPORTS THAT IT'S NOT THE ARMING BRACKET BUT THE AFT GIRT BAR STOW BRACKET IS HOLDING THE GIRT BAR LOOSELY. ADJUSTED THE TENSION ON BRAKET GRIP. CHECKS GOOD.

EMERGENCY LIGHTS OPERATIONAL CHECK EMERGENCY LIGHTS OPERATIONAL CHECK - NONE OF SEATS IN FIRST CLASS WORK DURING EMERGENCY LIGHT TEST. SEE PHOTO. REPLACED FUSE IN SLOT F2 REF AMM 33-51-06-960-801. OPS CHECK OK.

SIDEWALL LIGHT WILL NOT TURN OFF 11F SIDEWALL LIGHT AT SEAT 11F IS STROBING. LIGHT IS NIS LAS. PULLED AND COLLARED C/B PANEL P92 C/B E-11 WDO LT RIGHT. CLOSED AND SECURED E&E BAY DOOR. REQUEST MEL 3321A. DDP CW AND PLACARDED. UPDATED PARTS REQUIRED. LIGHT DEACTIVATED - TOMC APPROVED DEFERRED SIDEWALL LIGHT AT 11F PER MEL 3321A. C/B P92 E11 PULLED AND COLLORED. DDP C/W AND PLACARDED. *DM* ASSIST: {LT ASSY/60-3321-3-0007 PREV ORDERED.} IF INSUFF FOR RECOVERY, PLEASE UPDATE LP W/REQD PART NBRS & REFERENCE SOURCE REPLACED R/H ROW 11 FED SIDEWALL LIGHT REF: AMM 33-21-00. DURING OPS CHECK, THE LIGHT DID NOT RESPOND AS EXPECTED TO THE SELECTED SETTINGS, IT DID NOT TURN OFF WHEN OFF WAS SELECTED. LIGHT IS NOT FLICKERING ANYMORE. COMPLIED WITH MEL 3321A, PULLED AND COLLARED C/B P92 E11 PERFORMED ACP SOFTWARE LOADING PER AMM TASK 23-42-03-470-801. TEST WINDOW LIGHTS PER AMM TASK 33-21-00-960-801. TESTED GOOD.

ON ETOPS WALK AROUND INSPECTION FOUND #1 TIRE DELAMINATED WITH DAMAGE TO THE INBOARD L/H FLAP AND MLG OUTBOARD DOOR FAIRING. GROUNDED - YES. ACCOMPLISHED TIRE BURST CONDITIONAL INSPECTION REF AMM 05-51-54-210-801. FOUND MLG TIRE 1 DAMAGED. MLG TIRE 1 AND 2 REPLACED IAW AMM 32-45-11. DURING INSPECTION FOUND L/H INBOARD AFT FLAP DAMAGED, REF LOG PAGE 60814711. ALSO FOUND L/H MLG INNER DOOR DAMAGED REF LOG PAGE 60814712. SEAMC ASHRAF NOTIFIED.

ON ETOPS WALK AROUND INSPECTION FOUND #1 TIRE DELAMINATED WITH DAMAGE TO THE INBOARD L/H FLAP AND MLG OUTBOARD DOOR FAIRING. GROUNDED - YES. ACCOMPLISHED TIRE BURST CONDITIONAL INSPECTION REF AMM 05-51-54-210-801. FOUND MLG TIRE 1 DAMAGED. MLG TIRE 1 AND 2 REPLACED IAW AMM 32-45-11. DURING INSPECTION FOUND L/H INBOARD AFT FLAP DAMAGED, REF LOG PAGE 60814711. ALSO FOUND L/H MLG INNER DOOR DAMAGED REF LOG PAGE 60814712. SEAMC ASHRAF NOTIFIED.

DOOR 1L GIRT BAR DIFFICULT TO SECURE IN BRACKET SLIDE ATTACHMENT UNEVEN PER FLT CREW, INCORRECT DOOR LOCATION, CORRECT DOOR LOCATION IS 1R REMOVED, ADJUSTED SLIDE SKIRT ND REINSTALLED SLIDE REFERENCE AMM 25-66-01 ADD EMP: U129300 C/W GMM RII REMOVED AND RE-INSTALL SLIDE TO RE POSITION THE SKIRT

ANTI SKID INOP LIGH CAME ON AFTER TAKEOFF AND WENT OUT AFTER AB OUT 25 MINUTES SEE LOG PAGES 3520220, AND 3525590 FOR WHEEL 1&2 ANTISKID TRANSDUCERS CHANGED.REMOVED LEFT MLG ANTISKID WHEEL SPEED TRANSDUCER PER AMM 32-42-11-000-801. E16 E18 C/B OPEN AT P6-3 PANEL. REPLACED LEFT MLG TRANSDUCER AND IN AXLE ADAPTER AS PER AMM 32-42-11-400-801. AWAITING OPS CHECK. WITNESSED NORMAL OPERATION OF #1MLG ANTISKID TRANSDUCER. PERFORMED WHEEL #1 ANTISKID TRANSDUCER OPS TEST IAW AMM32-42-00-710-803. OPS TEST NORMAL, AND FAULT MSG CLEARED. RETURNED ACFT BACK NORMAL CONFIGURATION.

THE EMERGENCY LIGHT MOUNTED ON THE CEILING AT ROW 3 IS INOPERABLE. REQUESTING DEFERRAL FOR THE INOP LIGHT, PART NIS IN BOS TOMC APPROVED C/W MEL FOUND THE EMERGENCY AISLE LIGHT (EAL) ELECTRICAL CONNECTOR IS DISCONNECTED. RECONNECTED ELECTRICAL CONNECTOR, OPS CHK OK. REF. AMM. 33-51-03-960-802

RIGHT WING LOWER FIXED LEADING EDGE; WING STATION 204.25; INBOARD OF NACELLE STRUT; HAS A DELAMINATION AT THE TRAILING EDGE. MARKED.

RIGHT WING LOWER FIXED LEADING EDGE; WING STATION 204.25; INBOARD OF NACELLE STRUT; HAS A DELAMINATION AT THE TRAILING EDGE. MARKED.

CABIN WRITE UP- FWD GALLEY EMER LIGHT STRIP INTERMITTENT. GROUNDED - YES. REF AMM 33-51-00 AND 33-51-01. FA NOTES STATE LIGHT INTERMITTENTLY FLICKERED DURING FLIGHT BUT DID NOT SPECIFY WHICH LIGHT. REMOVED ALL FWD GALLEY EMERGENCY LIGHTS AND MANIPULATED HARNESSES AND SHOOK ASSYMBLIES. UNABLE TO DUPLICATE DEFFECT. MONITORED FWD GALLEY EMERGENCY LIGHTS FOR A LONG TIME AND NEVER SAW THE LIGHTS COME ON UNCOMMANDED. ALL EMERGENCY LIGHTS PASS OPERATIONAL TEST AND COME ON WHEN COMMANDED. UNABLE OT DUPLICATE DISCREPANCY.

LEFT WING ANTI ICE VALVE FAIL PERFORMED FIM 30-11 TASK 808 FOUND NO FAULTS. ALSO PERFORMED OPS CHECK PER AMM 30-11-11-710-801. OPS CHECK GOOD. OK TO CONTINUE AT THIS TIME.

LEFT HYDRAULIC PRESSURIZATION MULE FITTING COUPLINGS DUST CAPS ARE NOT INSTALLED. INSTALLED DUST CAPS ON LEFT HYDRAULIC PRESSURIZATION MULE FITTINGS REF AMM 29-11-08.

LEFT HYDRAULIC PRESSURIZATION MULE FITTING COUPLINGS DUST CAPS ARE NOT INSTALLED. INSTALLED DUST CAPS ON LEFT HYDRAULIC PRESSURIZATION MULE FITTINGS REF AMM 29-11-08.

LEFT WING ANTI ICE VALVE FAIL PERFORMED FIM 30-11 TASK 808 FOUND NO FAULTS. ALSO PERFORMED OPS CHECK PER AMM 30-11-11-710-801. OPS CHECK GOOD. OK TO CONTINUE AT THIS TIME.

RAMP REPORTS #3 MLG TIRE DAMAGED UPON ARRIVAL. GROUNDED - YES. TIRE TREAD LOSS. REPLACED #3 MLG TIRE REF AMM 32-45-11. TIRE TREAD DAMAGED RH INBD MAIN TE FLAP/FLAP TORQUE TUBE, RH INBD TE AFT FLAP/PUSHROD ASSY AND RH LOWER INBD FIXED TE PANEL.

CABIN WRITE UP- FWD GALLEY EMER LIGHT STRIP INTERMITTENT. GROUNDED - YES. REF AMM 33-51-00 AND 33-51-01. FA NOTES STATE LIGHT INTERMITTENTLY FLICKERED DURING FLIGHT BUT DID NOT SPECIFY WHICH LIGHT. REMOVED ALL FWD GALLEY EMERGENCY LIGHTS AND MANIPULATED HARNESSES AND SHOOK ASSYMBLIES. UNABLE TO DUPLICATE DEFFECT. MONITORED FWD GALLEY EMERGENCY LIGHTS FOR A LONG TIME AND NEVER SAW THE LIGHTS COME ON UNCOMMANDED. ALL EMERGENCY LIGHTS PASS OPERATIONAL TEST AND COME ON WHEN COMMANDED. UNABLE OT DUPLICATE DISCREPANCY.

E2 ESN 60A202 HAD POWER FLUCTUATIONS ON CLIMB DURING FERRY FLIGHT FROM EWR TO CLE. SUBJECT A/C A/R BACK INTO EWR. PLEASE DOWNLOAD THE CEOD DATA USING EC/RA 7321-01747. PLEASE REPORT FINDINGS AND ACTION IN THIS LOG PAGE. ESCPP@UNITED.COM; 847-700-8324 OPTION 4. CARRIED BY ELB ACCOMPLISHED ECRA 7321-01747 AND UPLOADED #2 ENGINE CEOD DATA. AS PER FIM 73-20 TASK 927 PERFORMED WIRING CHECKS BETWEEN #2 ENG FMU DP55A TO CH.A EEC DP5A REF WDM 73-25-21-1. CONTINUITY CHECKS GOOD AND NO SHORTS NOTED WITH MEGGER. ALSO CHECKED CH.A FMU RESISTANCE VALUES, ALL WITHIN LIMITS PER THE FIM. PERFORMED A HIGH POWER RUN WITH NO DEFECTS NOTED ON #2 ENGINE.

LH WINGLET CRACK . REMOVED LEFT WINGLET LOWER BLADE PER AMM TASK 57-31-21-000-80. INSTALLED 4 COUNTERSUNK RIVETS IN NEW SCIMATAR WINGLET IAW SRM 51-40-02. INSTALLED NEW LH WINGLET PER AMM TASK 57-31-21-400-802. PLANE RESTORED TO ORIGINAL CONFIGURATION.

AFTER LANDING FOUND THE CABIN EMERGENCY LIGHTS CIRCUIT BREAKER POPPED WHILE THE PASSENGERS WERE DEPLANING. GROUNDED - YES. REF AMM 20-60-01-860-801 INSPECTED BEHIND P6-5 & C/B CAB EMERGENCY LT'S - RESET C/B ALSO REF WDM 33-51-11-2 P.2 (C/B STAYS IN) PERFORMED OPS CK OF EMERGENCY LT'S REF AMM 33-51-00-710-801 ALL LT'S ILLUMINATED NORM IN TEST. C/B STAYS IN.

MASTER CAUTION WITH SPOILERS LIGHT ILLUMINATED WITH FLAPS 30 SELECTED.

LEFT ENG ANTI-ICE LIGHT ILLUMINATED INFLIGHT PASSING 10000 REM AINED ON. NNC RAN FLLX FOUND 4 CIRCUIT BREAKERS OPEN. 1)ENGINE 1 STBY ALTN PWR CHAN A. 2)ENG 1 IGN L AND ALTN PWR CHAN A. 3)BLEED AIR VALVES CB. ALL PICTURES ATTACHED. PERFORMED EEC BITE TEST FOR ENGINE ONE AND TEST PASSED. RESET ALL CIRCUIT BREAKERS PERFORMED ENGINE RUN. NUMBER ONE ENGINE, ANTI ICE DISAGREE LIGHT ILLUMINATED, AND CIRCUIT BREAKERS FOR IGNITION POPPED AGAIN (IGN L AND ALTN PWR CHAN A). REPLACED PRSOV PER AMM TASK 36-11-04. ACP FIM TASK 361-104-41 R&R IASC REF AMM 21-61-22 OP CHECKS GOOD.

LOW PRESSURE LIGHT ELEC 2 PUMP ON FOR INITIAL EVAULATION CYCLED CB C8 ON P92 PANEL. NO HELP. UPON FOLLOW UP WITH PILOTS, THEY STATED NO PRESSURE INDICATION FROM ELEC 2 PUMP SYSTEM A INDICATION. ONLY WITH ENGINE RUNNING HAD PRESSURE INDICATION. UPON OPENING OF P92 PANEL FOUND CB F3 POPPED FOR ELEC HYD PUMP SYS A. RESET BREAKER AND OPERATED PUMP, WHICH QUICKLY RESULTED IN CIRCUIT BREAKER TO POP AGAIN. DISCONNECTED D2664 FROM PUMP, CB DID NOT POP. 'B' PHASE LEG IN PUMP IS OPEN, REF WD29-11-12. REMOVED ELECTRIC HYDRAULIC PUMP A IN REF AMM 29-11-21-000-801 REPLACED A SYSTEM ELECTRIC HYD. PUMP REF. AMM 29-11-21-400-801. OPS CHECKED AND LEAK CHECK. NO LEAKS TESTED GOOD. REPLACED A SYSTEM ELECTRIC HYD. PUMP REF. AMM 29-11-21-400-801. OPS CHECKED AND LEAK CHECK. NO LEAKS TESTED GOOD.

RNAV APPROACH B AUTOPILOT LNAV+ VNAV ENGAGED AT 1500 AGL FLT DIRECTOR BARS DISPLAYED RNAV PATH BUT AIRCRAFT AUTOPILOT COMMANDED 20 DEGREES LEFT BANK AND 5 DEGREES PITCH UP. PILOT REPORTS DISCREPANCY WENT AWAY WHEN DISENGAGED B AUTOPILOT.

INFO ONLY CB P18-3 B-10 LIGHTING R AFT EMER CHGR POPPED.

ENG 1 HYD A SYSTEM LOW PRESSURE PER CREW: ABOUT A HOUR TO FLIGHT THE OVER HEAD PRESS ON ENGINE 1 LOW HYD PRESSURE LIGHT. CREW NOTICED HYD ON LEFT QTY WENT UP TO 106 % AND STEADLY WENT DOWN TO 10% AT LANDING. READS NOW AT GATE 19 RF, CREW REMEMBERS AT DEPARTURE LEFT WAS AT 97%. REMOVED AND REPLACED #1 ENG IAW W.C. 41-7100-1-0006 OPS AND LEAK CKS GOOD.

F/O FWD WINDOW ARC'D THEN WINDOW CRACKED AT 22,000'. PRESSURE NORMAL(

#1 ENGINE STACK FIRE AFTER SHUTDOWN INSPECTED #1 ENGINE TAILPIPE PER EA M-23-172-03308-ETOPS AND NO DAMAGE FOUND OIL CONSUMPTION RATE IS WITHIN LIMITS OF 0.1 QPH MOC MAYFIELD NOTIFIED POWERPLANT ENGINEERING FOR FOLLOW UP. A/C OK TO CONTINUE.

#4 BRAKE FIRE; NO HARD BRAKING AFTER LANDING DRY CHEMICAL FIRE EXTINGUISHING AGENT WAS USED ON BRAKES #3 AND #4

STRONG EXHAUST SMELL FRO M LEFT PACK.STRONG JET F UEL/EXHAUST SM ELL IN WHE EL AND FIRST CLASS.SMELL COMING FROM APU BLEED, RAN BOTH PACKS WITHOUT APU BLEED, NO SMELL IN CABIN. PLACARDED APU INOP MEL 4911A DISPATCH DESK: 23 NAME: RWB DATE: 19-DEC-24- NOC DESK: OM7 NAME: CO DATE: 19-DEC-24- TOMC APPROVED SMELL COMING FROM APU BLEED, RAN BOTH PACKS WITHOUT APU BLEED, NO SMELL IN CABIN. PLACARDED APU INOP MEL 4911A. NO OIL LEAKS NOTED FROM APU. UPUN CLEARING THIS MEL ITEM, CONTACT TOMC FOR ASSIGMENT OF MEL CARD 49001 TO ACCOMPLISH APU ETOPS VERIFICATION FLT. REF FIM 49-52 TASK 801. RAN PACKS ON APU AIR, EXHAUST / OIL SMELL STARTED WHEN PACKS WERE TURNED ON BUT DISSAPATED LESS THAN 5 MINUTES AFTER LT AND RT PACKS WERE RUNNING. CYCLED PACK TEMPS FROM COLD TO HOT SMELL DID NOT RETURN. HAD PACKS RUNNING FOR 20 MINUTES. STILL HAD ODOR USING APU BLEED DURING PART POWER RUNS FOR OTHER MAINTENANCE. REF LOG PAGE 3235772 NGS INOP, SUGGEST REPLACING NGS FILTER MODULE 61-4711-9-0001, NIS TPA AND SYSTEM AT THIS TIME. NGS IS STEP C.7 ON FIM 49-52 TASK 801 FOR APU OIL SMELL. REMOVED AND REPLACED NGS AIR SEPARATION MODULE (REF AMM TASK 47-11-01). OPS CHECKS GOOD. NO LEAKS FOUND. RAN PACKS FOR 30 MINUTES AN00-0609-3-2703,QTY :1 00-0604-3-1688,QTY :1 00-0608-3-1698,QTY :1 61-4711-9-0001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1933095 SN OFF 7281 MODULE, AIR SEP OFF 61-4711-9-0001 7281 ON 61-4711-9-0001 7256

PC GROUND AIR DOOR IS MISSING. ****MUST PERFORM -PARTS DEPARTED A/C COND INSP REF AMM 05-51-59****

RH HORIZONTAL STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL IS CRACKED.

PANEL 231JF PANEL ASSY - PASSENGER CABIN FLOOR HAS MISSING FIBERS. REMOVED AND REPLACED FLOORBOARD PER AMM 53-21-00.

L1 DOOR GIRT BAR AFT HOOK HAS SHEARED FASTNER.

LH PACK LIGHT. RESET PACK LIGHT RETURNED.THE FOLLOWING AIR/GND RELATED MSG'S ALL REPORTED AGAIN INBOUND, 21-55340, 21-55341 & 36-00021, THE FIM FOR THESE MESSAGES HAVE BEEN C/W PREVIOUSLY,IT WAS SUBSEQUENTLY REPLACED AND THE AIRCRAFT FLEW FOR 10 DAYS WITHOUT A LT PACK ISSUE. PLEASE REF AMM 21-51-21-400-801 SUBTASK 21-51-21-710-002 AND ENSURE CORRECT OPERATION OF LT PACK RAM AIR INLET/OUTLET DOORS,ITS POSSIBLE THE NEWLY INSTALLED UNIT MAY HAVE FAILED. PARTS, INCLUDING A PSEU HAVE BEEN REQUESTED. PERFORMED TEST FOR RAM AIR INLET ACTUATOR. LEFT RAM AIR INLET DOOR DOES NOT MOVE OPEN/CLOSED. REFAMM 21-51-21-400-801. AC SYSTEM IBIT SHOWS PASS, BUT L RAM ACTUATOR DOOR STILL DOES NOT OPERATE. R & R L1 RAM AIR ACTUATOR IN REF TO AMM 21-51-21-000/400-801. OPS CHECK GOOD,TEST PASSED. ACTUATOR WORKS, BUT INLET DOOR STILL HAS DISAGREEMENT WITH COMMAND.CONTINUE T/S POSSIBLE RELAY. L/H ACTUATORS WORK DURING IBIT. BUT DO NOT ACTUATE WHEN PLACED IN AIR MODE. FOUND MM 21-55340; 21-55341; 36-00021 IN HISTORY. SWAPPED CONTROLLERS AND ACCESSORY UNITS, NO HELP. SLAVED IN PSEU, NO HELP. FOUND SHORT TO GND WHEN IN AIR MODE AT D158388 AT J5. ISOLATED. RAN NEW WIRE BTW D14386 PIN 1 AND SM5.REPLACED EMI PIGTAILS. ALL WIRING DONE IAW SWPM 20-10. AIR/GND NOW OPCHECKS GOOD IAW 21-61-22-400-801

FWD ENTRY DOOR LIGHT ILLUMINATED ON TAKEOFF COMPLIED WITH DDP. CYCLED DOOR SHUT, LATCHED AND OPEN. OPERATES NORMALLY. TASK 05-41-08-210-806 AND 807. PER FIM 52-10-801 OMF SHOWS NO ACTIVE MAINTENANCE MESSAGES,OPERATIONAL TEST OF DOOR WARNING SYSTEM PER AMM 52-71-00. OPS CHECK NORMAL.

FUEL PUMPS LOW PRESSURE LIGHT IS ON CTR R APON BLOCKING AT GATE DEN, FOUND CB FOR CNTR RIGHT BOOST PUMP LOCKED OUT. CNTR LEFT BOOST PUMP ON MEL WAS NOT LOCKED OUT. PULLED AND LOCKED OUT LEFT CNTR BOOST PUMP CB. RT BOOST PUMP OPS NORMAL.

AFT GALLEY EMERGENCY LIGHT SWITCH HAS RED LIGHT ON REPORTED BY FLIGHT ATTENDANT

FOUND UPPER ANTI COLLISION LIGHT INOP. PARTS UPDATED NEED SNORKEL TO ACCESS LIGHT ASSY FROM TOP TO CHANGE. NO ACCESS FROM CABIN. REMOVED AND REPLACED ANTI COLLISION LIGHT DRIVER MODULE ASSEMBLY REF AMM TASK 33-44-01-960-807. UPPER LIGHT TURNS ON FOR ONE FLASH WHEN TURNED ON BUT WILL NOT CONTINUE FLASHING REQUIRES FURTHER TROUBLESHOOTING.

LEFT WINGLET LOWER BLADE FRAME HAS CRACK

BIRDSTRIKE, EXCEPT AT ENGINE INLET BIRDSTRIKE ON TAKEOFF 110KNOTS. ABOVE FO WINDSHIELD. ENGINE INS T NORMAL.NO SMELL IN CABIN PERFORMED BIRD STRIKE CONDITIONAL INSPECTION REF 05-51-18-210-801, CLEANED BIRD REMAINS DIRECTLY ABOVE FO'S WINDSHIELD, APPEARED TO BE SMALL BIRD. FOUND NO DMG OR DEFECTS. NO OTHER BIRD STRIKES FOUND ON ANY OTHER PART OF AIRCRAFT, A/C OK FOR RETURN TO SERVICE

CONT CAB TEMP SPIKED ON CLIMBOUT AND AGAIN ON DESCENT RESULTING IN STRONG ODOR THROUGHOUT CABIN.