737 MAX
Incident Reports

DURING EXTERNAL INSPECTION FOUND #2 ENGINE PYLON CRACK LOWER SKIN AFT. CRACK IS APPROX. 8.5 INCHES LONG.

ON DESCENT LE FLAPS TRANSIT LIGHT ILLUMINATED. PERFORMED FIM 27-81 TASK 821. OPS CHECKED LE FLAPS. LE FLAPS TRANSIT LIGHT REMAINS EXTINGUISHED. NO PREVIOUS HISTORY. OK FOR SERVICE. PERFORMED FIM 27-81 TASK 821. OPS CHECKED LE FLAPS. LE FLAPS TRANSIT LIGHT REMAINS EXTINGUISHED. NO PREVIOUS HISTORY. OK FOR SERVICE.

ROLL AUTHORITY ON FINAL 7NM 1500FT PER DFCS BITE SEE PHOTOS. REF AMM 22-11-00 PER FIM 22-11 TASK D79. PER AMM22-11-25-710-801 TEST PASS NO FAULTS . ADD EMP:U102168 NEED TO CONTINUE WITH FIM 22-11-D79. PERFORMED AMM 27-11-00-710-801, OPS CHECK IS GOOD. PERFORMED AMM 27-61-00-710-801, OPS CHECK IS GOOD. BOTH REQUIRED PER FIM 22-11 D 79. AMM TASKS 22-11-25-710-801, 22-23-00-710-802, 27-11-00-730-801, 27-21-00-700-805 & 27-21-00-700-807 STILL NEED TO BE ACCOMPLISHED PER FIM 22-11 D 79. ATTEMPTED TO PERFORM LAND VERIFY TEST TO NARROW DOWN TROUBLESHOOTING. ACFT IS FAILING DUAL STAB AND SUBSEQUENTLY MACH TRIM TESTS AND GIVING HARD FAULT OF 22-11191 MT CMD MON. ADDING FCC PART PRECAUTIONARY. ABOVE UPDATE FOR MESSAGE 22-11191 TRANSCRIBED TO LOGPAGE 9215536 SEE REFERENCED LOGPAGE FOR DISPOSITION PERFORMED AUTOPILOT AILERON ACTUATOR TEST IN REFERENCE TO B737 AMM 22-11-25-710-801 TEST PASSED PERFORMED YAW DAMPER SYSTEM TEST IN REFERENCE TO B737 AMM 22-23-00-710-802 SYSTEM TEST PASSED UPDATED FOR SDR PERFORMED AILERON TRIM RESPONSE TEST IN REFERENCE TO B737 AMM 27-11-00-730-801 TEST PASSED ADD EMP:U388284, PERFORMED RUDDER TRIM SYSTEM TEST IN REFERENCE TO B737 AMM 27-21-00-700-807 TEST PASSED PERFORMED RUDDER TRAVEL TEST IN REFERENCE TO B737 AMM 27-21-00-700-805 TEST PASSED ALL TESTS IN B737 FIM 22-11 TASK D79 HAVE BEEN COMPLETED WITH NO FAULTS FOUND ADD EMP:U388284, COMPLETED B737 FIM 22-11-D79 WITH NO FAULTS FOUND SPOKE WITH TOMC OK TO CLEAR FCC A REPLACED ON LOGPAGE 9204147

FA'S REPORT THAT R1 DOOR IS DIFFICULT TO CLOSE FULLY. CLOSES WITH HANDLE IN CORRECT POSITION, BUT CAN LEAVE OPEN GAP AT UPPER RIGHT CORNER. REQUIRES MULTIPLE ATTEMPTS TO ENSURE IT CLOSES COMPLETELY. GROUNDED - YES. VERIFIED R1 DOOR CLOSED W/ AN OPEN GAP AT UPPER R/H CORNER INTERMITTENTLY. FOUND GUIDE ARM ADJUSTMENT JAMNUT LOOSE. ADJUSTED GUIDE ARM REF AMM 52-41-00 STEP 2.(I). OPS CHECK GOOD DOOR OPERATES AS INTENDED. SKIN CLEARANCE AND FLUSHNESS CHECK GOOD. ACCOMPLISHED GALLEY SERVICED DOOR SYSTEM TEST REF AMM 52-41-00-700-801. TEST PASSED. VERIFIED GUIDE ARM ADJUSTMENT JAMNUT IS TIGHTENED.

WHILE IN CRUISE FL380 A SLIGHT BURNING SMELL BECAME PRESENT IN COCKPIT AND CABIN. SMELL QUICKLY BECAME VERY INTENSE IN CABIN AND COCKPIT. BOTH QRC AND QRH COMPLETED FOR SMOKE/FIRE OR FUMES. 02 MASKS CONT...DONNED SMELL DISSIPATED SHORTLY BEFORE LANDING AND DID NOT RETURN. NO VISIBLE SMOKE INDICATIONS WERE EVER PRESENT. NO 30DH - CH21/CH36

11C EMERGENCY EXIT LIGHT INOP. WIRE BROKEN PLACING 11C EMERGENCY LIGHT ON MEL 3351A. VERIFIED THAT THE ADJACENT EMERGENCY LIGHT IS OPERATIVE. TOMC APPROVED ,OK TO DEFER PER MEL 3351A APPLIED MEL 3351A. PLACED INOP PLACARD ON EMERG LIGHT SWITCH T/S PER MERIDIAN 1072994 CMM REF 25-21-65. FOUND RECEPTACLE ON HARNESS PART NUMBER BR9631-28 MISSING, REQUIRES NEW HARNESS. ADD EMP:U393350 HARNESS IS NIS @ EWR. ALSO MISSING ARE FLOOR PROXIMITY EMERGENCY LIGHT MISSING, PART NUMBER BR9644-21FS, OUTBOARD SHROUD ASSY MISSING, PART NUMBER 1078850-305BWC, AND INNER SHROUD ASSY MISSING, PART NUMBER 1044199-301BTD. *DM* ASSIST: {HRNSS/29-2542-3-0042, EPL CLOSEOUT/42-2521-3-0084, RACEWAY SHROUD/42-2521-3-0092, & LT MODULE/99-3350-3-0008 PREV ORDERED (MODULE DUPED M&E+MFG: I CANXD MFG#BR9644-21FS)}.INCREASED M/H TO MATCH GRND TIME @ 3 REMOVED AND REPLACED EMERGENCY PROXIMATELY LIGHT AND WIRE HARNNESS AT SEAT ROW 11ABC PER AMM 33-51-11-960-801.PARTS USED: 29-2542-3-0042,QTY :1 99-3350-3-0008,QTY :1

L1 DOOR LOWER HINGE COVER BINDING UP DOOR ON OPENING. GROUNDED - YES. PERFORMED GVI OF L1 DOOR, FRAME, SURROUNDING AREA. OPS CK'D DOOR FROM INSIDE AND OUT MULTIPLE TIMES. NO DEFECTS FOUND. OPERATES AS IT SHOULD.

STAB TRIM UNCOMMANDED NOSE DOWN TRIM DURING LANDING ROLLOUT. MAI N ELEC TRIM NOT APPLIEDTALKED TO PILOTS. STAB ON LAND ROLLOUT WITH AUTO PILOT OFF TRIM STARTED TO GO FULL DOWN. PILOT MADE SURE HAND WAS OFF ELECTRIC TRIM. WHEN NOTICED WAS OFF THEY HOT TRIM CUT OUT AMD THE TRIM STOPPED. NO FUALTS IN HISTORY AND NO FULTS IN EXSITING OR INBOUND. UPDATED TO REPORT SDR FOUND NO FAULTS IN INBOUND FLIGHT DECK EFFECTS OR FAULT HISTORY PEROFORMED STABALIZER TRIM MOTOR TEST IN REFERENCE TO B737 AMM 27-41-71-700-801 TEST PASSED AWAITING ESC TO REVIEW QAR DATA FOR FURTHER DIRECTION PERFORMED DIGITAL FLIGHT CONTROL SYSTEM SPEED TRIM/STAB TRIM DISCRETE BITE TEST IN REFERENCE TO B737 AMM 22-11-00-740-815 TEST PASSED STILL AWAITING ESC RESPONSE FOR FURTHER DIRECTION AFTER QAR DATA REVIEW VERIFIED BOTH FCC'S IN GROUND MODE 28 VOLTS ON BOTH FCC A AND B ON PIN B3. PER ESC REQUEST PERFORMED AN ANGLE OF ATTACK SENSOR SYSTEM TEST IN REFERENCE TO B737 AMM 34-21-05-730-801 TEST PASSED PERFORMED DFCS BITE FOR THE ADIRU AND SMYD IN REFERENCE TO B737 AMM 22-11-00-740-801 TEST PASSED PERFORMED AN OPERATIONAL TEST OF THE STALL WARNING SYSTEM IN REFERENCE TO B737 AMM 27-32-00-710-802 OPERATIONAL TEST PASSED NO FAULTS FOUND CONFIRMED BOTH FCCS INSTALLED ARE 822-1604-102 REFERENCE B737 IPC 22-11-33-03 AS REQUESTED REPLACED FCC A IN REFERENCE TO B737 AMM 22-11-33-400-801 CONFIRMED CORRECT SOFTALL ABOVE ACTIONS COMPLIED WITH PER ESC INSTRUCTIONS. REPLACED BOTH FCCS ALL OPERATIONAL TESTS PASSED OK TO CLOSE ITEM

PER INBOUND CAPTAIN, AT ALTITUDE IN CRUISE, EXPERIENCED UN COMMANDED ROLL RIGHT. MAX ROLL AUTHORITY LIMIT STOP WAS REACHED. AIRCRAFT WAS AT FL 340, 255KTS ON ARRIVAL. THEY WERE APPROACHING A WAYPOINT THAT REQUIRED A SLIGHT RT TURN. AUTOPILOT STARTED THE RIGHT TURN AND CONTINUED UNTIL AIRCRAFT REACHED 33 DEGREES OF BANK. THE AUTOPILOT THEN COMMANDED YOKE TO LEFT TO CORRECT BUT THE PLANE CONTINUED TURNING RIGHT. AT THIS POINT "ROLL AUTHORITY" WAS ANNUCIATED. PILOTS THEM DISCONNECTED AUTOPILOT AND MADE EXCESSIVE LEFT ON YOKE TO REGAIN WINGS LEVEL. PILOTS STATED THEY EXPERIENCED BUFFETING/SHUDDERING THROUGH THE AIRFRAME. THEY STATED IT SEEMED LIKE A SPOLIER WAS UP. THEY DONT THINK IT WAS WAKE TURBULENCE OR MOUNTAIN WAVE TURBULENCE. ACCESSED MY BOEING FLEET TO FIND MAINTENANCE MESSAGES. NONE FOUND. ACCOMPLISHED SEVERE OR UNUSUAL TURBULENCE, EXCESSIVE MANEUVER CONDITIONAL INSPECTION ON LOG PAGE 9133363 FOLLOWED FIM 22-11 TASK D79. PREFORMED ALL OPS CHECKS LISTED. ALL OPS CHECKS GOOD, FOUND NO DISCREPANCIES. ACCOMPLISHED DFCS BITE TESTS REF AMM 22-11-00-740-814 AND LAND VERIFY TEST PASSED. HOWEVER A RELATED FAULT WAS FOUND IN LEG 01. FAULT MSG 22-11715, "ROLL AUTHORITY" MATCHES THE DATE AND FLIGHT PARAMETERS. NEED TO ACCOMPLISH FIM TASK 22-11 TDUE TO UNCOMMANDED ROLE WE HAVE C/W FIM TASK 22-11-C37, AND 22-11-D79. REF LOG PAGE 9133363 FOR SEVER TURBULANCE INSPECTION C/W. A/C HAS BEEN RETURNED TO SERVICE AND READY FOR T-HOP.

UPPER FWD DOOR STOP FITTING ON L2 DOOR REQUIRES REPLACEMENT DUE TO BEING OUT OF LIMIT PER SRM 52-10-90-1A1 AD1. REMOVED FITTING FOR REPLACEMENT. HOLES AND COUNTERSINKS FOR HOLES COMMON TO FITTING REQUIRE INSPECTION. HOLES AND COUNTERSINKS FOR HOLES COMMON TO FITTING REQUIRE INSPECTION. VERIFIED RII REQUIREMENTS, PERFORMED HOLE PROBE INSPECTION REF NDTM PART 6 51-00-00 PROCEDURE 16. NO DEFECTS NOTED. DRILLED FITTING OFF OF DOOR, CLEANED AND DEBURRED FITTING. REQUEST OK TO INSTALL FITTING. DRILLED FITTING OFF OF DOOR, CLEANED AND DEBURRED FITTING. REQUEST OK TO INSTALL FITTING. VERIFIED RII REQUIREMENTS OK TO INSTALL FITTING

TWO AFT GALLEY FLASHLIGHTS WILL NOT TEST

#1 ENG FILTER BYPASS INFLIGHT, INFLIGHT SHUTDOWN. GROUNDED - YES. ACCOMPLISHED TSR 716465 UP TO STEP 7. FOUND MAGNETIC METAL MATERIAL IN THE SCAVENGE FILTER AND ON THE ODMS SENSOR. ODMS POD WAS USED AND THE SCAVENGE FILTER ROUTED TO AOG ENGINEERING FOR ANALYSIS. ALL SCAVENGE SCREENS WERE REMOVED AND FOUND NO DEBRIS. INSTALLED ALL SCAVENGE SCREENS AND SCAVENGE FILTERS IAW TSR. MAINTENANCE MESSAGE:79-42890 DESCENT, OIL FILTER IMPENDING BYPASS FAULT CODE: 79330251. REQUIRES TROUBLESHOOTING. COMPLETED 70 PERCENT RUN FOR 10 MINUTES INSPECTED ODMS AND SCAVENGE SCREENS, NO PARTICLES FOUND. INSTALLED ODMS REF AMM 79-21-12-400-801-G00 AND SCAVENGE SCREEN PLUGS REF AMM 79-21-04-400-801-G00. LEAK CHK GOOD. ACCOMPLISHED INFLIGHT WINDMILLING INSPECTION REF AMM 71-00-00-200-807-G00. TSR 716465 COMPLETE. FINDINGS REPORTED TO AOG ENGINEERING CONSULTED AND ADVISED RETURN TO SERVICE. REF LOGPAGE 60787795 FOR SIGNIFICANT EVENT PROCESS COMPLETED AND AIRCRAFT RETURN TO SERVICE AUTHORIZATION BY SEAMC.

IAS DISAGREE AT 100KTS F/O 100KTS.CA 70 KTS RTO.RETURNING TO GAT E ACCOMPLISHED PITOT STATIC SYSTEM FLUSHING REF AMM34-11-00-170-802. FOUND TO DEBRIS DURING FLUSHING PROCESS. FOUND MAINT MESSAGE 31-03120. REPLACED #2 ADM NO HELP. LATER FOUND MAINT MESSAGE 31-03120 SWAPPED #1 & #2 ADIRS. FAULT DID ADD EMP:344425 NOT FOLLOW. RETURNED ADIRS TO ORIGINAL POSITIOMS. FOUND NO DEBRIS DURING FLUSH PROCESS. REF FIM 31-65 TASK B70 & FIM 31-65 TASK B74. UPDATED LABOR HOURS REMOVED AND REPLACED RH AOA SENSOR IAW B737 AMM 34-21-05. OPS CHECK GOOD. REMOVED AND REINSTALLED ORIGINAL RH ADM IAW B737 AMM 34-21-04. OPS CHECK GOOD.PARTS USED: 29-3412-9-0001,QTY :1 ADD EMP:U348571 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1460359 SN OFF 6558 SENSOR, ANGLE O OFF 29-3412-9-0001 6558 ON 29-3412-9-0001 9256 VERIFIED ALL PITOT AND STATIC PORTS COVERS REMOVED, AND QDS RECONNECTED. OPS CHECK NORMAL. UPDATE ROTABLE PART CHANGED ROTABLE PARTS CHANGE WAS INDICATED - TT # 1325600 SN OFF 3217 MODULE, AIR DAT OFF 42-3413-9-0001 3217 ON 42-3413-9-0001 7799

FOUND DENT REF LP 8972873, AVO13111A HAS BEEN COMPLETED. INSPECTION HAS EMAILED ENGINEERING OF THEIR FINDING STRINGER INSPECTED NO DAMAGE NOTED. VERIFIED ALL STEPS OF AVO COMPLETE ACCOMPLISHED DETAILED VISUAL INSPECTION OF REPAIR AREA REF AVO13111 STEP 15 AND 16 STEPS WORKED ON PER AVO13111 REV. B - ACCOMPLISHED STEP 17, WILL NOT BE REPLACING S-29 AS ADVISED IN STEP 18. ACCOMPLISHED GVI OF S-29 AND FOUND NO DAMAGE. ALL STEPS OF AVO13111 REV. B HAVE BEEN COMPLIED WITH SENT ALL FINDINGS TO ESC FOR FURTHER REPAIR 2 DENTS, DENT 1 IS LOCATED FWD OF E & E DOOR, AT BS 316 AND O/B OF S29-C. DENT 2 IS LOCATED BS 314 AND 8" O/B OF S-29-C. PERFORMED STEP 14-A-C AND E-K OF AVO 13111 REV B. CUT DAMAGE OUT AT 2 LOCATIONS. PERFORMED INSURANCE CUTS ON BOTH DAMAGE CUT OUTS, REF AVO 1311 REVB, STEP 14-D. COMPLIED WITH INSPECTION OF AVO13111 STEP 14. NO DISCREPANCIES NOTED,INCLUDING STEP 14.D. HFEC, INCLUDING INSURANCE CUT. NO LIMITING DEFECTS NOTED DURING INSPECTION REF AVO13111 STEPS 15 AND 16 INSTALLED TCAS ANTENNA IAW EC/RA 5330-07331 STEP 28 AND 34-45-02-400-801. REQ INSP. BONDING MEASURES 0.82 MILLI OHM. PREV ABOVE STATEMENT REQUIRES INSPECTION VERIFIED THE ECRA 5330-073371 REV ORIGINAL. ARE COMPLETED SIGN OFF UP TO AND INCLUDED SPET 30. INSTALLED INTERIM REPAIR DOUBLER/TRIPLER REF EC/RA 5330-07331.

ENG 2 HYD LOW PRESS LT WAS FIRST INDICATION OF LOSSZOF ALL QTY I N SYS B. CREW REPORTED THAT FIRST INDICATION WAS ENGINE 2 HYDRAULIC ENGINE DRIVEN PUMP LOW PRESSURE LIGHT ON. CREW RAN QRH SHUT DOWN NUMBER 2 EDP THEN RAN ALTERNATE PROCEDURES. WHEN CREW COMPLETED QRH THEY FOUND SYSTEM B HYDRAULIC RESERVOIR WAS AT 0. CREW REPORTED THAT NUMBER2 ELECTRIC DRIVEN PUMP WAS ON FOR SOMETIME AFTER RESERVOIR WAS EMPTY. ATTEMPTED TO FILL HYD SYST B RESERVOIR BY HAND PUMP METHOD. FLUID STARTED LEAKING FROM ENG 2 FWD DRAIN MAST. CLOSED ENG 2 PYLON VALVES WITH FIRE HANDLE IN FLIGHT DECK. TAGGED FIRE HANDLE WITH LOTO TAG

FMC 2 PGM FAULT 34-62001 FAULT WAS 34-62001 FMC-2 PGM FAULT DETECTED BY: FLIGHT MANAGEMENT COMPUTER (FMC)-1. REF TSM 34-61-882, DUE TO FMC DISAGREE MESSAGE REPLACED FMC-2 REF AMM TASK 34-61-02-000-801 & TASK 34-61-02-000-801. PICTURE INCLUDED OF INSTALLED FMC. FMC REMOVED WAS PN 176200-01-01 SN 019415. OPS CHECKED OK.

EMERGENCY LIGHT BATTERY PACK M1671 WILL NOT HOLD A CHARGE

L1 DOOR EMERGENCY SLIDE LIGHT INOP THE IMAGES ATTACHED ARE OF THE BACKSIDE OF THE FORWARD GALLEY/WINDSCREEN ON THE LEFT SIDE OF AIRCRAFT. THE RED SQUARE INDICATES THE AREA WHERE THE CHAFFED WIRE WAS FOUND. THE VERTICAL RECTANGLE IS THE LOCATION OF AN ALUMINUM BRACKET THAT SUPPORTS THE FRONT EDGE OF THE KICK PANEL. IT HAS A TAB WITH A SCREW SLOT AT THE TOP OF THE BRACKET THAT ATTACHES IT TO THE GALLEY WALL. THIS TAB WAS RUBBING AGAINST THE WIRING FOR THE SLIDE LIGHT.

EMERGENCY LIGHT BATTERY PACK M1676 WILL NOT HOLD A CHARGE

EMERGENCY LIGHT BATTERY PACK M2816 WILL NOT HOLD A CHARGE

EMERGENCY LIGHT BATTERY PACK M2335 WILL NOT HOLD A CHARGE

EMERGENCY LIGHT BATTERY PACK M1675 WILL NOT HOLD A CHARGE

EMERGENCY LIGHT BATTERY PACK M1695 WILL NOT HOLD A CHARGE

EMERGENCY LIGHT BATTERY PACK M1670 WILL NOT HOLD A CHARGE

FORWARD CARGO COMPARTMENT STA. 500I AFT BULKHEAD LOWER CENTER SUPPORT IS CORRODED. GROUNDED - YES. EVALUATED CORROSION OF SUPPORT, FOUND TO BE CORRODED MULTIPLE AREAS THAT EXCEED 10% WIDTH OF LOWER FLANGE, FOUND TO BE OUT OF LIMITS IAW B737-MAX SRM 53-00-53-1A-2 FIG. 103 SHEET 2 DETAIL A&B. REMOVED AND REPLACED LOWER CENTER SUPPORT IAW B737-MAX SRM 51-40-02 AND BAC DWG 143A9481 REV. A. REMOVED AND REINSTALLED FLOOR PANEL 120EF IAW B737-MAX AMM 5110-04. LOWER CENTER SUPPORT P/N 143A9485-35 P.O.# 1096478.2.

M1673 EMERGENCY EXIT LIGHT BATT PACK AT STA 952 WL 290 LBL 14 WILL NOT CHARGE.

M1672 EMERGENCY EXIT LIGHT BATT PACK AT STA 952 WL 291 RBL 14 WILL NOT CHARGE.

R/H HORIZONTAL STABILIZER UPPER FORWARD SLIDING SEAL HAS A VERTICAL CRACK ON THE FORWARD SIDE.

DOT A24-7 RH WING #12 SPOILER UPPER SKIN IS DELAMINATED ABOUT 2 INCHES O/B OF I/B EDGE AND 2 THROUGH 10 INCHES FWD OF AFT EDGE.

PROCEDURE - LIFE VEST SEAL WRONG SECURITY SEALS INSTALLED 6 EACH REMOVED 6 EACH FOUND WRONG TAGS SECURITY. INSTALLED SEALS ME 29-2521-3-0030.

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

AFT ENTRY LIGHT ILLUMINATED ON TAKEOFF ROLL DID NOT EXCEED 80 KTS, REJECTED TAKEOFF. OPENED AND CLOSED L2 DOOR IAW AMM 52-13-00, NO DEFECTS NOTED AT THIS TIME. DOOR SECURED CLOSED, LIGHT EXTINGUISHED. PERFORMED HIGH SPEED ENERGY STOP INSPECTION IAW AMM 05-51-07, NO DEFECTS NOTED. SPEED AT 80 KTS NO DAMAGE NOTED. REF LP 737-002-9548. PER COMPANY REQUEST ADJUSTED L2 DOOR PROX SWITCH SENSOR IAW AMM 52-71-11 PERFORMED OPS CHECK OF DOOR WARNING SYSTEM IAW AMM 52-71-00 OPS CHECK GOOD AT THIS TIME.

THROUGHOUT THE PASSENGER CABIN THERE ARE SEVERAL FLOOR PROXIMITY GLOW STRIPS THAT HAVE THE PART NUMBER TAGS STILL ATTACHED TO THE UPPER SURFACES.

NEITHER AUTOPILOT WILL ENGAGE AFTER SEVERAL ATTEMPTS DURING CLIM B AND CRUISE ACCOMPLISHED FIM TASK 22-11 TASK 933 FOR MAINT MSG 22-11176 UP TO STEP F.2. REMOVED AND REPLACED MAIN ELEC STAB TRIM RELAY R1193, REQUIRES LAND VERIFY. PERFORMED SPD/STB TRIM TEST LAND VERIFY TEST PER AMM 22-11-00-700-801. OPS CHK GOOD. ALL TEST PAASED WITH NO FAULTS

UPON LANDING, R2 EMERGENCY LIGHT ILLUMINATED AND EXIT LIGHT ILLUMINATED. BOTH LIGHTS WENT OUT AFTER APPROXIMATELY 15 SECONDS NO PRESSURIZATION ISSUES NOTED AND NO COCKPIT INDICATION PRESENT. GROUNDED - YES. R2 DOOR INSPED, NO DEFECTS NOTED.OPENED & CLOSED INSIDE & OUTSIDE HANDLES PRFM'D EMERGENCY LIGHT TEST IAW AMM 33-51-00-720-801. CHIK'D COCKPIT DEFECTS FOR DOOR & LIGHT INDITCATIONS NO DEFECTS NOTED.

2 MIN AFTE TAKEOFF AFT FA REPORTED A VERY LOUD VIBRATION AND NOI SE FOR 5 MIN. HISSING AFTEWARDS UPON INITIAL EVALUATION, FOUND DAMAGE TO UPPER RIGHT DOOR STOP AND HARDWARE. THREADED INSERT RETAINING CLIP/PIN IS MISSING, INSERT IS LOOSE. PHOTOS ATTACHED. LOCATION IS L2 DOOR AS REPORTED BY FA. ADJUSTED GUIDE ARM IN REFERENCE TO AMM 52-13-00-820-801. THE DOOR NO LONGER CONTACTS THE STOP FITTING IN TRANSITION. UPPER FOWARD STOP PIN ADJUSTED AND NEW STOP PIN CLIP INSTALLED IN REFERENCE TO AMM 52-13-00-820-801. INSPECTED AND VERIFIED GUIDE ARM ADJUSTED AND STOP PIN CLIP INSTALLED PER AMM 52-13-00-820-801. OK TO CONTINUE. ADJUSTED DOOR PER AMM 52-13-00-820-801 PERFORMED LEAK CHECK AND VERIFIED NO LEAKS, QC VERIFIED THAT NO WHISTELING OR HISSING NOTED DURING PRESSURIZATION LEAK CHECK.

STAB OUT OF TRIM LIGHT ILLUMINATED DURING CLIMB. ELECTRIC TRIM INOPERATIVE. MANUAL TRIM WORKED NORMALLY. NO CIRCUIT BREAKERS POPPED.

DOT#06 A-043 AFT CARGO COMPARTMENT RH FWD SHIELD CORRODED AT NUTPLATE HOLES TOP AND BOTTOM SIDES STA 767 TO 787 RBL 22 WL 156

DOT#07 A-043 AFT CARGO COMPARTMENT LH Z ANGLE CORRODED STA 727E+10' TO 747 LBL 22 WL 156

DOT#08 A-043 AFT CARGO COMPARTMENT FLOOR 'T' SPLICE PLATE CORRODED STA 767+5' BL 0 TO RBL 21 WL 156

DOT#09 A-043 AFT CARGO COMPARTMENT RH Z ANGLE CORRODED AT STA 727B+10' TO 767 RBL 22 WL 156

FWD CARGO COMPARTMENT FLOOR PANEL 120AF IS CORRODED AT FASTENER HOLES

FWD CARGO COMPARTMENT FLOOR PANEL 120DF IS CORRODED AT FASTENER HOLES

IRS-R FAULT LIGHT IS ON CHECKED FAULT MASSAGE: ADIRU-R INTERNAL FAULT. ADDED PARTS USED. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1522004 SN OFF 1048 UNIT, ADIRU, AI OFF 42-3421-9-0001 1048 ON 42-3421-9-0001 5385 REMOVED & REPLACED RT ADIRU (M1752) REF AMM 34-21-01, PERFORMED OPS TEST REF AMM 34-21-00-710-801 TESTS OK.

FWD CARGO COMPARTMENT FLOOR PANEL 120CF IS CORRODED AT FASTENER HOLES

NUMBER 2 ENG FAIL ON T/O ROLL...EGT WENT RED AT STABILIZED NO N1 N2...REJECT 60 KTS ENGINE #2 REMOVED AND REPLACED IAW ETASK 41-7100-1-0006. ALL CKS GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1579351 SN OFF 3315 ENGINE, BASIC, OFF 42-7200-9-0001 3315 ON 42-7200-9-0001 3248 JOBCARD COMPLETED

EMERGENCY LIGHTS UNABLE TO ILLUMINATE WHEN IN THE "ON" POSITION. GROUNDED - YES. REMOVED/REPLACED EMERGENCY EXIT LIGHT SWITCH IAW SYSTEM SCHEMATIC MANUAL 33-51-11-103. OPS CHECK GOOD.

ENGINE NUMBER ONE ENG ANTI ICE LIGHT ILLUMINATED IN FLIGHT. FOUND E1 PI SENSOR FAULT 36-21010. PLACED ON MEL IAW CARD 36070. REMOVED AND REPLACE PRSOV IAW 36-11-04. NO HELP WITH ISSUE. FURTHER TROUBLE SHOOTING REQ.

SMOKE AND FUMES IN THE CABIN AND COCKPIT DURING DEPARTURE. NO ENGINE ABNORMALITIES

LE FLAP TRANSIT LIGHT ILLUMINATED IN FLIGHT - DID NOT RESET AFTE R QRH PROCEDUREBEGAN TROUBESHOOTING PROCEDURE. FAULT SHOWS ON #1 LEADING EDGE FLAP WITH ASSOCIATED MTC MESSAGE 27-81216. UNABLE TO CLEAR FAULT THROUGH FSEU INTERROGATION. REF FIM TASK 27-81 822. FAULT REMAINS. PERFORMED UP TO STEP D3 (FSEU REPLACEMENT) WHILE INSPECTING LE FLAP RETRACT SENSOR 1, FOUND SPLICES HAD SLIGHTLY PULLED APART DUE TO WIRE BUNDLE SECURED TOO TIGHTLY. SUSPECT THAT COULD BE POSSIBLE ISSUE. REMOVED AND RESPLICED WIRES FOR LE FLAP RETRACT SENSOR 1 (S168) REF SWPM 20-30-12. DURING TESTING IT WAS A NO FIX. LEFT LE FLAP 1 IN TRANSIT LIGHT STILL ILLUMINATED AND FAULT STILL EXISTS. MAY NEED NEW FSEU OR FURTHER WIRING CHECKS ACCOMPLISHED. SUSPECT SWITCH S-168 IS BAD, MOVED FLAPS TO A POSITION WHERE ALL SENSORS WERE OFF THEIR TARGETS, USED A SCALE ON OTHER 3 RETRACT SENSORS TO SIMULATE THE TARGET, ALL THEIR RESPECTIVE LIGHTS WENT OUT, DID THE SAME THING TO S -168 NO CHANGE STILL SHOWED IN TRANSIT. REMOVED LE FLAP 1 RETRACT SENSOR S168 REF AMM 27-88-11/401, RESISTANCE CKS OF WIRES FROM S168 TO THE FSEU GOOD REF WDM 27-81-11-1, INSTALLED NEW SENSOR S168 NO FIX, T/S FURTHER AND FOUND BAD GROUND AT GD614AC. VERIFIED GROUND GD614-AC IS BAD. BRACKET NOT GROUNDED TO THE AC. PERFORMED WIRING CHECKS FROM SWITCH S168, TO. FSEU REF WDM 27-81-11, SWITCH CHECKS GOOD. REBITE CK OF FSEU GOOD IAW AMM 27-51-01/401.

ON CLIMB OUT; STRONG SMELL OF BURNING OIL

REJECT T/O 100-105KTS AIRSPEED DISAGREE CREW REPORTS FO AIRSPEED STOPPED ACCELERATING. CAPT AIRSPEED KEPT CLIMBING. THEN THEY REJECTED TAKEOFF. APPROX 20 KNOT DIFFERENCE. PERFORMED DETAILED INSPECTION OF THE PITOT AND STATIC DRAINS AS REQUIRED, FOUND NO EVIDENCE OF MOISTURE AND OR DEBRI REF AMM 34-11-00-210-801 AND AMM 34-11-00-210-802 MIANTENANCE MESSAGE 31-03120 " IAS DISAGREE", NO OTHER RELATED MESSAGES FOUND, PER FIM 31-65 TASK B70, REQUIRES PITOT STATIC SYSTEM FLUSHING ACP FIM 31-65 TASK B70 PITOT SYSTEM FLUSH. NO DEBRIS FOUND. RPL PITOT ADM IAW AMM34-21-04-400-801. ACP R/H PITOT SYSTEM LEAK TEST REF AMM34-11-11-790-807. LEAK CHECK OK. ALL OPS CHECK NORMAL.PARTS USED: 42-3413-9-0001,QTY :1 PARTS USED: ADD EMP:U330401 42-3413-9-0001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1722908 SN OFF 4122 IPC REFERENCE # IPC 34-11 COMPLIED WITH INSPECTIONS REF GMM 09-10-05. MODULE, AIR DAT OFF 42-3413-9-0001 2412 ON 42-3413-9-0001 8156

AT TOP OF DECENT F/A REPORTED SMOKE IN CABIN. IDENTIFIED SOURCE AS PAX CELL PHONE BATTERY. EXTINGUISHED IN CONTAINMENT BAG. DIVERTED TO PBI AS PRECAUTION. NO OVERWEIGHT LANDING.

(A125) CABIN; EMERGENCY LIGHTS INOP AT CEILING - ROW 2; ROW 4; LH ROW 9; LH ROW 12; AND R1 DOOR - EXIT SIGN AND OVERHEAD LIGHT

#1 ENGINE FLUCTUATING 1.3 % N1 AT CLIMB THRUST; ALSO EGT AND FUEL FLOW ALSO FLUCTUATING

FOUND EMERGENCY BATTERY PACK M1695 WILL NOT CHARGE

FOUND EMERGENCY BATTERY PACK M1671 WILL NOT CHARGE

CRACK ON BAFFLE CLIP AT FCB; BS460 AFT FRAME; LBL23; WL153

FOUND EMERGENCY BATTERY PACK M1673 WILL NOT CHARGE

CRACK ON BAFFLE CLIP FWD FRAME BS 460; LBL 23 AND WL 153

CRACK ON BAFFLE CLIP AT FCB; BS500A; AFTER FRAME RBL23; WL153.

CRACK ON BAFFLE; AT FCB; BS500B; FWD FRAME; RBL23; WL153 CRACK ON BAFFLE CLIP AT FCB BS500B FWD FRAME RBL23 WL153

CRACK ON BAFFLE CLIP AFT FRAME BS 440; LBL 23 AND WL 153

# 1 PYLON REQUIRES REMOVAL FOR THE REPAIR OF LOWER THE SUPPRESSOR SKIN CRACK

FWD GALLEY CA SIDE HAS FLUID LEAKING AROUND THE BOTTOM BY FORWARD DOOR AND AROUND THE 1ST ROW PASSENGER SEATS. ALSO HAS A BAD ODOR ASSOCIATED WITH IT. ITS BEEN REPORTED ON PREVIOUS PAGE.

TOO LOW GEAR WARNING AT 500 GEAR WAS DOWN.FULL CONFI G NORMAL LOCKING LOCKPAGE PERFORMED PSEU OPS CK IAW AMM 32-09-10-750-801 AND ALSO FIM TEST PASSED RESULTS TASK 31-51 TASK 806 ALL TEST PASSED OK TO CONTINUE UNLOCK TO CLEAR ALL LRU R&R AND TESTS REQ PASSED, OK TO CLEAR.

LEFT ENGINE EXHAUST STRUT LOWER HEAT SHIELD CRACKED.

ASSIGNED WO #2010108 T/C AD20222409-MULTI-21-2 CABIN ALTITUDE WARNING SWITCH S1153 TEST FAILED. GROUNDED - YES. REMOVED AND REPLACED CABIN ALTITUDE WARNING SWITCH S1153 IAW AMM 21-33-04. FUNCTIONAL TEST GOOD. NO DEFECTS AT THIS TIME.

BOTH FLASHLIGHTS UNDER FWD FA JUMPSEAT INOP

(A125) LEFT WING; #3 FLAP TRACK; CENTER CANOE FAIRING 542BB; O/B SIDE REPAIR OF THE WING SEAL HAS A CRACKED INTERNAL SUPPORT

RH CABIN SIDEWALL LIGHTS BETWEEN ROWS 21 AND 29 INOP. PLACED ON MEL 3321A. DEFERRED DIRECTLY BY TOMC REPLACED LIGHT ASSY'S BETWEEN ROWS 21 AND 29 M&E # 60-3321-3-0005, NO HELP. PHASE 2 TEST SHOWS NO COM 21-29 RIGHT. FURTHER AVIONICS T/S REQUIRED NEEDS SOFTWARE UPDATE *DM* ASSIST: ATTENDANT CONTROL PNL CONFIG CK AVAIL @ AMM 23-42-03-700-801; SOFTWARE LOAD @ 23-42-03-470-801; BITE IN AMM 23-42-03-740-801. INCREASED M/H & GRND TIME TO 3. REPLACED SIDEWALL LIGHT 323-21-00, OPS CHECKS GOOD

DUE TO WATER LEAK AT LAV D THE CENTER SECTION OF CARPET WAS FLOODED. CENTER SECTION OF CARPET TO 11 WINDOWS FWD OF AFT LAV. SCRUBS CLEANED AREA AND DRIED . INSPECTED AFT PIT FOUND NO SIGNS OF WATER PASSING THROUGH FLOOR AND NO ELECTRONICS IN AREA. REQUIRES IN DEPTH CLEAN UP WITHIN 7 DAYS INITIAL CLEAN UP COMPLETE, REQUIRES IN DEPTH CLEAN UP WITHIN 7 DAYS. AFFECTED AREA IS 727I THROUGH BS 950 TOMC APPROVED DIP DUE TO WATER SPILL IN AFT LAV LEFT LAV D, INITIAL CLEANUP ACCOMPLISHED REF EC/RA 2011-01000 REV AD, WITHIN 7 DAYS ACCOMPLISH LAV SPILL SECTION 2. B. IN DEPTH CLEANUP IN THE APPROXIMATE AREA FROM BS 727I THROUGH BS 950 AND LBL 30 AND RBL 30, NO WATER NOTED OUTBOARD OF INBOARD SEAT TRACKS OR IN CARGO PIT AREA. TOMC-APPROVAL FROM SC1ELBYC COMMENT REVIEWED CONTROL #:SOURCE DOCUMENT: 2011-01000 R TERMINATING LABOR HOURS: 0072 GROUND TIME: 0024 QC REVIEWED RECORDS UPDATE....RM TA M&E: 41-9925-8-0074 S/N: 7268 LIMIT: PERFORMED IN DEPTH CLEAN UP PER STEP 2B ECRA 2011-01000 REV AD. NO BLANKETS OR CONTAMINATION FOUND IN AFT CARGO PIT AREA. REF LOG PAGE #8566654 WATER WAS FROM AFT LAV D SINK. REF LOGPAGE #8629992 FOR SUPPLEMENTAL INSPECTION. SEE L/P 8629992 FOR SUPPLEMENTAL INSPECTION TOMCQC REV PERFORMED

ELECTRICAL PANEL ELEC LIGHT ILLUMINATED FOUND MAINTENANCE MESSAGE 24-F0504 PERFORMED FIM TASK 24-31 TASK 810 CYCLED SPCU CURCUIT BREAKER MESSAGE CLEARED, OK TO CONTINUE.

BATT DISCHARGE LIGHT IMAGE OF CURRENTLY INSTALLED APU START POWER UNIT. ADDITIONAL IMAGES ADDED. UNIT, APU START OFF 29-4941-9-0002 8135 ON 0000 UNIT, APU START OFF 29-4941-9-0002 8135 ON 29-4941-9-0002 8262 REMOVED AND REPLACED APU START POWER UNIT. PERFORMED INSTALLATION TEST, NO RELATED FAULTS OR MESSAGES PRESENT AT THIS TIME, INSTALLATION TEST PASS. REF AMM 49-41-71 PARTS USED: 29-4941-9-0002,QTY :1 PARTS USED: 29-4941-9-0002,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1362619 SN OFF 8135

CBS FWD GALLEY PULLED IN RESPONSE TO FAINT SMELL OF SMOKE AT COFFEE MAKERS SMOKE DISAPPEARED REMOVED THE GALLEY ELECTRICAL CONTROL PANEL AND INSPECTED WIRING , CONNECTORS AND CB'S ALSO REMOVED COFFEE MAKRES AND INSPECTED WIRING AND CONNECTORS NO EVIDENCE OF ARCING PRESENT. TURN ON COFFEE MAKRES NO SMELL AND PRESENT OF SMOKE. SMOKE/ ODOR. RAN OVENS NO DISCREPANCIES.

DUAL FMC RESET AT TOD 12NM W OF SLT. FMC RESTORED IN APPROX 30 S ECONDS REQUEST MEL FOR #1 FMC. DISPATCH DESK: 22 NAME: RW DATE: 12-JUL-24- NOC DESK: MAX NAME: KB DATE: 12-JUL-24-TOMC APPROVED FOR MEL 3461M PLACED #1 FMC ON ME PLACED IN #2 POSTION. STICKER INSTALLED. PERFORMED FMC OPS TEST WITH REF TO AMM 34-61-00-710-801 NO FAULTS FOUND. INTERROGATED FAULT HISTORY ON OMF AND FOUND MAINTENANCE MESSAGE 39-69001 *DM* DUE TO MSG 34-69001, SUGGEST FIM 34-61 TASK 836, SEE M/L FOR FMC 1 M1175, FMCS TRANSFER RELAYS R00475, & R00476, AS NEEDED. UPDATE SDR

R/H ELEVATOR FAIL SURFACE FRICTION AND BALANCE TEST PROCEDURE 27-31-00--700-803 STEP 13 G (1).

DURING ELEVATOR LUBE, FOUND BOTH COTTER PINS FOR T-BOLTS MISSING ON ELEVATOR TAB CONTROL RODS. REPLACED MISSING COTTER PINS REF IPC 27-31-34-01

N1 ENG VIB ABOVE 4.0 ON CLIMBOUT CREW REPORTS NO VIBRATION FELT , ENGINE SPINS FREELY, NO DAMAGE DEF PER MEL. #1 ENG VIBRATION INOP. HARNESS (ENG 1) 65007, IF NEEDED. 77-31-06/401. ESCPP ROHAN IN INLET OR EXHAUST. HAS HISTORY OF INDICATION PROBLEM JULY 01. APPROVED MEL CARD 7731A. #1 ENGINE VIBRATION INDICATION INOPERATIVE. *DM* DUE TO MSG 77-44620, SUGGEST FIM 77-00 TASK 919, SEE M/L ENGINEERING UPDATE: PLEASE T/S PER FIM 77-00 TASK 919 LIKE *DM* FOR TURBINE CENTRAL FRAME ACCELEROMETER (ENG 1) 65603, & HJ8A SUGGESTED. IF NFF, R&R THE TCF ACCELEROMETER PER AMM REPLACED ACCELEROMETET PER AMM TASK 77-31-06-400-801-G00. WILL PERFORM HPR TO OPS CHECK PERFORMED LPT AND HPT REF AMM TASK 71-00-00. NO ERATIC VIBRATIONS NOTED. OPS CK GOOD AT THIS TIME.

SEAT 12E LIFEVEST BOX HAS THE WRONG TYPE SEAL INSTALLED. UPDATED LOGPAGE WITH PHOTO. REPLACED LIFEVETS CONTAINER SEAL WITH CORRECT SEAL. COULD NOT EASILY BREAK SEAL PREVIOUSLY INSTALLED, AND HAD TO CUT IT OFF, WHICH WOULD AFFECT THE ABILITY TO ACQUIRE THE LIFEVEST IN AN EMERGENCY.PARTS USED: 29-2521-3-0030,QTY :1 PARTS USED: 29-2521-3-0030,QTY :1

SEAT 8A LIFEVEST BOX HAS THE WRONG TYPE SEAL INSTALLED. UPDATED LOGPAGE WITH PHOTO. REPLACED LIFEVEST BOX SEAL WITH THE CORRECT SEAL.PARTS USED: 29-2521-3-0030,QTY :1 PARTS USED: 29-2521-3-0030,QTY :1

SEAT 25E LIFEVEST BOX HAS THE WRONG TYPE SEAL INSTALLED. UPDATED LOGPAGE WITH PHOTO. REPLACED LIFEVEST BOX SEAL WITH CORRECT SEAL.

GRND CREW REPORTS GREY/BLACK SMOKE ON LEFT MAIN TIRE DURING PUSH BACK, ON ARRIVAL FOUND BRAKE DISC COMING APART, ONE COMPLETELY OUT. REMOVED AND REPLACED NR 2 BRAKE PER AMM 32-41-41. OPS CHECK GOOD, NO LEAKS NOTED.

FOUND GALLEY CART SEAL INSTALLED ON LIFE VEST CONTAINER AT SEAT 15C GALLEY CART SEALS HAVE A METAL CABLE IN THEM AND NEED TO BE CUT OFF, WE ARE FINDING THESE SEALS INSTALLED ON MANY SEATS. THIS IS A SAFETY ISSUE, INSTALLED CORRECT SEAL, OK FOR CONTINUED SERVICE

EMERGENCY LIGHT IN CEILING IS HANGING DOWN BY ELEC WIRES JUST FORWARD OF RAFT # 3 COMPARTMENT. GROUNDED - YES. RESECURED EMERGENCY AISLE LIGHT ASSEMBLY RETAINING RING IAW AMM 33-51-03.

EMERGENCY EXIT LIGHTS AFT AND R/H INOP

MANY SEATS HAVE INCORRECT LIFE VEST SECURITY SEALS INSTALLED THROUGHOUT THE CABIN. INCORRECT LIFE VEST SEALS WERE INSTALLED,NOT BRAKE AWAY,HAD TO CUT THE SEALS TO REMOVE. PASSENGER ACCESS WOUL HAVE BEEN MOST DIFFICULT IN TIME OF NEED. INSTALLED CORRECT SEALS TO AFFECTED LIFE VEST BOXES.

EMERGENCY EXIT LIGHTS L1507 X 2; L1515; L547 & L6 REMAINS ON WHILE P5 OVHD PNL SWITCH IS ON ARMED POSITION.

NUMBER 2 ENG BLEED DOES NOT OPEN OIL SERVICE ACCOMPLISHED AT MCO FOR FLT 2120 ON 02 JUL 08:46:06 ENGINE 1: 00 ENGINE 2: 00 ENGINE 3: 00 ENGINE 4: 00 APU: 00 CHECKED REF FIM 36-21 . DOWN POWERED A/C , RAN BOTH ENGINES BLEEDS ARE N ORMAL AND PACKS RUN NORMAL WITH ENGINE. R563 #2 ENGINE RUN/STOP RELAY REQUESTED TO BE REPLACED DUE TO FAULTD HITS AND DIVERSION. REMOVED AND REPLACED RELAY R563 REF SWPM 20-81-22. PERFORMED PSEU OPERATIONAL CHECK REF AMM 32-09-10-740-801. NO FAULTS NOTED AT THIS TIME. RAN #2 ENG AND CONFIRMED ENG BLEED OPERATIONAL. PERFORMED CABIN PRESSURE LEAK TEST ON N/W/W PANEL REF AMM 05-51-91-790-801. NO LEAKS NOTED AT THIS TIME.

AIRCRAFT EXPERIENCED 1000# FUEL IMBALANCE. #1 FUEL TANK 1000#S LESS THAN RIGHT. LANDED 3780# LEFT AND 4590# RIGHT. IMBALANCE OCCURRED 4060# LEFT AND 5090# RIGHT. ALL ENGINE INSTRUMENTS NORMAL. FUEL FLOWS MATCHED.

ENG 1 OVERHEAT LIGHT CAME ON DURING CLIMB OUT TESTED FIRE AND OVERHEAT SYSTEM WITH CORRECT INDICATIONS AND NO ABNORMALITIES. FAULT HISTORY SHOWS MESSAGES 26-00310 & 26-00020 INACTIVE #1 ENGINE. BITE CHK ENGINE/ APU FIRE DETECTION MODULE M279 IN THE E&E COMPARTMENT AND NO FAULTS # 1 ENGINE. #1 ENGINE WAS A OVERHEAT LIGHT ON NOT FIRE LIGHT. #1 ENGINE FIRE LIGHT CAME ON #1 N1-96.1 % ;MAXIMUM FOR THAT ALTITUDE. FIRE LIGHT EXTINGUISHED WHEN THRUST LEVER RETARDED FROM MAX CONTINOUS THRUST. SUSPECT BLEED LEAK. FOUND UPPER CDP GASKET PINCHED, DAMAGED AND LEAKING. REPLACED CDP GASKET, EGT HARNESES #1 AND 2 , REPLACED. EEC HARNESSES HJ8A AND HJ8B AND ASSOCIATED CLAMPS AND HEAT SHIELD BLANKET AROUND CDP DUCT. PERFORMED OPS CHECKS AS PER AMM 71-00-00, NO LEAKS NOTED,NO FAULTS NOTED ALL TESTS PASS. OK TO CONTINUE.

FOUND DELAMINATION ON L/H ELEVATOR TAB TRAILING EDGE AT 11.5 TO 15 FROM I/B EDGE MEASURING 2.7 LONG AND .10 WIDE. 1.5 AWAY FROM OTHER DAMAGE UNDER TTG8Q00UA17G. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 55-20-01-1A-3

FOUND AREA OF COMPOSITE DELAMINATION ON LEFT HAND ELEVATOR TAB TRAILING EDGE AT 16.75' TO 19.0' FROM INBOARD EDGE MEASURING 2.4 IN LONG AND A WIDTH OF 0.03 IN DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 55-20-01-1A-3

R/H EMERGENCY OVER WING FWD; AFT; AND CENTER AISLE EXIT SIGNS INOP. REMOVED AND REPLACED M1695 POWER SUPPLY AND BATTERY. REF. AMM 33-51-06.

FWD LAV HAS A WATER LEAK . WATER COMING FROM UNDE R THE PANELS A ROUND THE TOILET. LEAK IS NOT URINE. LEAK IS CLEAN WATER. POSITIONED WATER VALVE MEL APPLIED. WATER SHUTOFF. WATER HEATER SHUTOFF, CB PULLED UNDER SINK TO OFF. CLEANED UP SMALL AMOUNT WATER UNDER LAV SHROUD I.A.W. EXRA 2011-01000 NO LEAK NOTED FROM ANY VALVES PRIOR TO SHUTTING OFF WATER SYSTEM. E/E COMPARTMENT DRY NO LEAK NOTED UNDER FLOOR REACTIVATED FORWARD LAV WATER SYSTEM & REMOVED TOILET SHROUD. FLUSHED LAV SEVERAL TIMES NO LEAKS NOTED. RAN FAUCET FOUND NO LEAKS UNDER SINK. RETURNED ACFT TO NORMAL CONFIG. REF AMM 38-32-00-700-802

REF L/P 8335328, UNABLE TO CREATE NEW CLIENT CREDENTIALS FOR AID-FWD. FOUND EXISTING ACTIVE FAULT 46-52003.AIRCRAFT INTERFACE DEVICE-FORWARD (AID-FWD WA DOES NOT RESPOND TO NFS COMMANDST/S PER FIM 46-13 TASK 857, NO HELP. SUSPECT AID INOP. M&E 61-4613-9-0001 N.I.S CLE. REQUEST MEL 4613A FOR ONS SYSTEM INOP DUE TO AID FAULT APPROVED ITEM PLACED ON MEL. DDP C/W *DM*: {INTERFACE DEVICE M3501/61-4613-9-0001 PREV ORDERED.} FIM 46-13/857 COVERS MM46-52003 FAULT ISLN. PRECAUTIONARILY ORDERED AID PWR CB C4113 / 99-2451-3-0014 & NFS M2898 / 43-4613-9-0001. NOTE: M3501 S/W VERIF @ AMM46-103-52-470-801. ALSO BE AWARE THAT NFS R&R MAY INVOLVE CAPTURING FILES & GENERATING KEYS: SEE AMM 46+-13-01-000-801 AND 46-13-01-400-801 FOR DETAILS. AVIONICS EG UPDATE: PLEASE START BY REPLACING THE AID. UPDATING LABOR/GROUND TIME HOURS FOR AID REPLACEMENT. ECRA 4613-01576 CAN BE UTILIZED FOR THE AID REPLACEMENT REMOVED AND REPLACED AID IN REF ECRA 4613-01576.NO HELP. T/S REF. B737-8 FIM 46-13 TASK 857. VERIFIED PWR GOING TO AI WWU. ADD FAULT: 46-52003 PWR ON LIGHT & STATUS LIGHT SHOW SOLID RED. AI WWU WILL NOT ACCEPT SOFTWARE LOAD, SEE ATTACHED PHOTO. SUSPECT EITHER WIRING BETWEEN AI WWU & NFS OR INSTALLED AI WWU BAD FROM STOCK. WILL REQ. FURTHER TROUBLESHOOTING PARTS USED: 1569351,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1569351 SN OFF 0296 DEVICE, AIRCRAF OFF 61-4613-9-0001 0296 ON 61-4613-9-0001 1MAJOR REPAIR AND RII FLAGS ENTERED IN ERROR. SEE PREVIOUS ENTRY FOR WORK ACCOMPLISHED.

STA 847 RBL 19-28 WL 162, STIFFENER WAS REPLACED BY BOEING REF CONTRACT #UAL-RE-2401657 AND FRR 149-3. THE PURPOSE OF THIS LP IS TO COMPLY WITH GMM 4-20-05 AND COMPLETE AN SFR. SFR COMPLETE.

STA 727+20 WL 169 LBL 72, FRAME ASSY REPLACED BY BOEING REF CONTRACT UAL-RE-2401657 AND FRR 16-1. THE PURPOSE OF THIS LP IS TO COMPLY WITH GMM 4-20-05 AND COMPLETE AN SFR. SFR COMPLETE.

RIGHT PACK LIGHT ON DEPARTUR E CREW DEBRIEFED. RT PACK OFF LIGHT RESET AFTER SEVERAL MINUTES WHEN TURNED TO FULL HOT. LIGHT ILLUMINATED AFTER A BRIEF TIME OFF. QRH NO HELP. FOUND NOT ACTIVE FAULT CODE 21-55101. OPERATED RT PACK FOR 45 MINUTES REF. 21-51 TASK 820. PACK LIGHT DID NOT COME BACK ON. FOUND ACTIVE FAULTS 21-55001 & 21-55011 AFTER PERFORMING RIGHT AIR CON IBIT TEST REF. FIM 21-51 TASK 802 & FIM 21-51 R & R RT RAM AIR INLET ACTUATOR IAW AMM 21-51-21. FWD ACT. FAULT LIGHT WENT OUT BUT EXHAUST REMAINS, BOTH ACTIVE FAULTS REMAIN. SWAPPED LT & RT IASC WITH NO HELP. WHILE PERF. WIRING CHECKS, FOUND 28VDC AT BOTH INLET & EXHAUST RAM AIR ACTUATORS. ALSO FOUND INLET & EXHAUST FAULT LIGHTS ILLUMINATED ON FWD RIGHT ACTUATOR. R & R RT RAM AIR EXHAUST ACTUATOR IAW AMM 21-51-27. OPS CHECK GOOD.

STA 847-867 LBL 21 WL 160, INTERCOSTAL P/N 149A8109-127 WAS REPLACED BY BOEING REF CONTRACT UAL-RE-2401657 AND FRR-111-3. THE PURPOSE OF THIS LP IS TO COMPLY WITH GMM 4-20-05 AND COMPLTE AN SFR. SFR COMPLETE.