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 M1671 WILL NOT HOLD A CHARGE

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

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

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

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

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.

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.

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

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

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

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#09 A-043 AFT CARGO COMPARTMENT RH Z ANGLE CORRODED AT STA 727B+10' TO 767 RBL 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#07 A-043 AFT CARGO COMPARTMENT LH Z ANGLE CORRODED STA 727E+10' TO 747 LBL 22 WL 156

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

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

FWD CARGO COMPARTMENT FLOOR PANEL 120AF 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.

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

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.

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

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.

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

(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

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

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 AT FCB; BS500A; AFTER FRAME RBL23; WL153.

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

FOUND EMERGENCY BATTERY PACK M1673 WILL NOT CHARGE

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

FOUND EMERGENCY BATTERY PACK M1671 WILL NOT CHARGE

FOUND EMERGENCY BATTERY PACK M1695 WILL NOT CHARGE

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.

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.

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

LEFT ENGINE EXHAUST STRUT LOWER HEAT SHIELD CRACKED.

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

BOTH FLASHLIGHTS UNDER FWD FA JUMPSEAT INOP

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.

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

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

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.

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

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.

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

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.

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

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 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

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.

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

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 AFT AND R/H INOP

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

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.

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.

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 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

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

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 847-867 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.

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 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.

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.

NOSEWHEEL TIRE VIBRATION ON TAKEOFF FOLLOWED BY LARGE VIBRATION ON ROTATION AND BURNING RUBBER SMELL.

NR 1 ENG SHOWS AN OIL SYSTEM CHIP COUNT INCREASE. INSPECTED ODMS SENSOR PER AMM 79-00-00-210-804-G00, ALL SCAVENGE SCREEN PLUGS PER AMM 79-21-04-211-801-G00, AND STARTER MCD PER AMM 80-11-09-200-8 01-G00. CONFIRM MAGNETIC OR NON-MAGNETIC FOR ALL FINDINGS. RESET ODMS TO ZERO PER AMM 71-00-00-700-802-G00. OPTION 4. FOUND METALLIC DEBRIS ON ODMS SENSOR, DEBRIS WAS FOUND TO BE GREATER THAN 0.004 INCHES REF AMM 79-00-00-210-804-G00 ST EP G.1(B) G. 2(B). INSTALLED OIL DEBRIS MONITORING SYSTEM SENSOR REF AMM 79-21-12-400-801-G00. VERIFIED O-RING AND INSTALLATION OF NR 1 ENGINE ODMS SENSOR. CHECKED STARTER MCD PER AMM 80-11-09-200-801-G00, NO DEBRIS NOTED.

PACKS ARE GOING TO HIGH FLOW; UNCONTROLLED. HOT OIL SMELL AND COCKPIT TEMP BECAME HOT. THEN PACKS WENT TO NORMAL FLOW AND ICE SHOT OUT OF VENTS. SUSPECT LEFT PACK IS UNCONTROLLABLE.

THIS LOGPAGE IS GENERATED FOR SDR REPORTING PURPOSES IAW GMM 04-20-16, REF LOGPAGE 7288541. LEFT MAIN LANDING SHEARED OFF DUE TO AIRCRAFT VEERED OF THE HARD SURFACE. LOG PAGE GENERATED FOR SDR REPORTING PURPOSES, ALL WORK PERFORMED BY THE BOEING COMPANY FAA REPAIR STATION BACR668L UNDER UNITED CONTRACT UAL-RE-2401657

REF LP 8301672. WHEN REPLACING MMR1 FOUND PUSHED BACK PIN IN MMR1 BENCHPLUG CONN D10719B POS B8. REF SSM 34-58-11 PIN IS ASSOCIATED WITH 'IR OUTPUT BUS 4' SIGNAL.. VERRIFIED PIN B8 ON D10719B LOOKS TO BE PUSHED IN (ATTEMPTED TO TAKE PHOTO BUT YOU CANNOT TELL VERY WELL.) ATTEMPTED TO PUSH PIN BACK OUT WITHOUT DISTURBING THE E1-2 RACK, NO SUCCESS. E1-1 AND E1-2 WILL NEED TO BE TAKEN OUT IN ORDER TO GET ACCESS TO BENCH PLUG D10719B REMOVED E1-1 RACK AND ALL CONNECTORS AND COAX CABLES ATTACHED TO RACK IN ORDER TO GET ACCESS TO CONNECTOR D10719B. REF IPC 50-50-51-30 REMOVED E1-2 AND REMOVED CONNECTOR D10719B FROM E1-2 RACK. FOUND PIN IN B08 HAS INCORRECT PIN. PICTURE ADDED WITH A08 (RED WIRE) RIGHT NEXT TO IT. FLAGGED FOR SDR FOR CONNECTOR D10719B MFR P/N BACC66H40F03AM01 THE B INSERT MFR P/N BACI10AH14 INSERT CONFIGURATION 120T2 ONLY 1 TYPE OF CONTACT IS ALLOWED TO BE USED P/N BACC47EF1 REFERENCE B7X7 SWPM 20-71-14 PAGE 126 CONTACT CURRENTY INSTALLED IN ADD EMP:U382127, POSITION B8 ON D10719B IS NOT P/N BACC47EF1 AND WILL REQUIRE REPLACMENT AND RE-TERMIANTION REPLACED AND RE-TERMINATED POS B8 PIN CONTACT IN D10719B BACKSHELL. REFERENCE B7X7 SWPM 20-71-14 PAGE 126. MMR GROUND TEST OK. REF AMM 34-31-42-000-801. INSTALLED E1 & E2 RACKS. REF IPC 50-50-51-30. REF SMM 34-58-11. RE TERMINATED PIN IN B8 ON CONNECTOR D10719. ADD FAULT:NONE INSPECTION NOT REQIERED, REPAIR IS A MINOR IAW GMM 03-20-20 SDR NOT REQUIERED PER GMM 04-20-16.

REF LP 8301672. WHEN REPLACING MMR1 FOUND PUSHED BACK PIN IN MMR1 BENCHPLUG CONN D10719B POS B8. REF SSM 34-58-11 PIN IS ASSOCIATED WITH ''IR OUTPUT BUS 4'' SIGNAL.. PLUG D10719B POSITION B8 ON D10719B IS NOT P/N BACC47EF1 AND WILL REQUIRE REPLACMENT AND RE-TERMIANTION VERRIFIED PIN B8 ON D10719B LOOKS TO BE PUSHED IN (ATTEMPTED TO REMOVED E1-1 RACK AND ALL CONNECTORS AND COAX CABLES ATTACHED TO REMOVED E1-2 AND REMOVED CONNECTOR D10719B FROM E1-2 RACK. ATTEMPTED TO PUSH PIN RACK IN ORDER TO GET ACCESS TO CONNECTOR D10719B. REF IPC PIN IN B08 HAS INCORRECT PIN. PICTURE ADDED WITH A08 (RED WIRE) THE B INSERT MFR P/N BACI10AH14 INSERT CONFIGURATION 120T2 ONLY BACK OUT WITHOUT DISTURBING THE E1-2 RACK, NO SUCCESS. E1-1 AND 50-50-51-30 RIGHT NEXT TO IT. 1 TYPE OF CONTACT IS ALLOWED TO BE USED P/N BACC47EF1 REFERENCE E1-2 WILL NEED TO BE TAKEN OUT IN ORDER TO GET ACCESS TO BENCH B7X7 SWPM 20-71-14 PAGE 126 CONTACT CURRENTY INSTALLED IN ADD EMP:U382127, REPLACED AND RE-TERMINATED POS B8 PIN CONTACT IN D10719B BACKSHELL. REFERENCE B7X7 SWPM 20-71-14 PAGE 126. MMR GROUND TEST OK. REF AMM 34-31-42-000-801. INSTALLED E1 & E2 RACKS. REF IPC 50-50-51-30. REF SMM 34-58-11. RE TERMINATED PIN IN B8 ON CONNECTOR D10719. ADD FAULT:NONE INSPECTION NOT REQIERED, REPAIR IS A MINOR IAW GMM 03-20-20 SDR NOT REQUIERED PER GMM 04-20-16.

GENERATOR DRIVE LIGHT COMES ON WITH ENGINE ABOVE IDLE IN FLIGHT DURING CLB RAN ENGINE. DRIVE LIGHT REMAINED ILLUMINATED AND OUT LIGHT CAME IDG REQS REPLACEMENT. REMOVED IDG REF AMM 24-11-11-000-801, ALL INSTALLED NEW IDG AT E2 REF AMM 24-11-11-400-801. STILL REQUIRE ALSO REQUIRED TEST NO. 4 AND NO. 9 FROM REF AMM ON. STEPS. SEE SEP LP FOR ELOTO. THE OPS TEST AMM 24-11-00-700-804. COMPLETED IDLE ENGINE RUN TASK 4, NO LEAKS NOTED. IDG OPS TESTS PER AMM 24-11-00-700-804. OPS CHECK SUCCESSFUL.

LEFT MAIN LANDING SHEARED OFF DUE TO AIRCRAFT VEERED OF THE HARD SURFACE. ALL WORK PERFORMED BY BOEING.

LOUD THUD AT 120 KNOTS ON T/O ROLL FOLLOWED BY HEAVY VIBRATIONS UNTIL GEAR RETRACTION. GEAR EXTENSION; LANDING AND ROLLOUT ALL NORMAL.

LE FLAP TRANSIT LIGHT AT 15000 MAINTENANCE MESSAGE: 27-81213 LE SLAT 7 INBOARD SENSOR SIGNAL [HISTORY]. NO CURRENT FAULT; BUT BITE CHECK INDICATES MOST ORIGINAL: FLIGHT CREW INDICATES THAT SLAT #7 WOULD NOT RETRACT SEE LOG PAGE HISTORY #8134788. FIM TASK WORK NEEDS TO BE DOES NOT AGREE WITH OTHER LE SLAT INBOARD SENSOR PREVIOUS LEGS WITH SAME INTERMITTENT FAULT: 27-81213. REF. FIM: WITH "IN TRANSIT" LIGHT INDICATION AT 15K. ABLE TO FULL EXTEND RE-VALIDATED. SIGNALS DETECTED BY: FLAP/SLAT ELECTRONICS UNIT (FSEU 27-81 TASK 819. AND CYCLE RETRACT ON GROUND. T/S REF WDM 27-81-22-1 FOUND A SHORT ON WIRE W6166-2025B-24 NEAR PLUG D40142P. REPAIRED REF SWPM 20-30-12. OPS CHECK GOOD REF AMM 27-81-00-700-801.

FOUND DAMAGED WIRE SEAT ROW 15ABC FWD BIN; 2 INCHES BEHIND CONNECTOR D14702

WHILE PERFORMING RIG CHECK ON RUDDER CONTROL ROD. DISCOVERED CRACK IN LOWER RUDDER TRAILING EDGE HINGE PN175A1207-4 REF IPC 55-40-51 FIG ITEM 1 REF LOGPAGE 2520929 FOR ORIG. DISCREPANCY. YAW DAMP DUTCH ROLL PROBLEM. WHILE PERFORMING RIG CHECK ON RUDDER CONTROL ROD. DISCOVERED CRACK IN LOWER RUDDER TRAILING EDGE HINGE PN175A1207-4 REF IPC 55-40-51 FIG ITEM 1

WHILE PERFORMING RIG CHECK ON RUDDER CONTROL ROD. DISCOVERED CRACK IN L/H L/H BRACKET PN 251A3426-2 REF. IPC 27-21-00 FIG ITEM 70 REF LOGPAGE 2520929 FOR ORIG. DISCREPANCY. YAW DAMP DUTCH ROLL PROBLEM. WHILE PERFORMING RIG CHECK ON RUDDER CONTROL ROD. DISCOVERED CRACK IN L/H L/H BRACKET PN 251A3426-2 REF. IPC 27-21-00 FIG ITEM 70. PERFORMED EA 24-155-01449. PERFORMED EA 24-155-01449. PERFORMED EA 24-155-01449.

WHILE PERFORMING RIG CHECK ON RUDDER CONTROL ROD. DISCOVERED CRACK IN UPPER RUDDER TRAILING EDGE HINGE PN175A1210-5 REF IPC 55-40-51 FIG ITEM 1 REF LOGPAGE 2520929 FOR ORIG. DISCREPANCY. YAW DAMP DUTCH ROLL PROBLEM. WHILE PERFORMING RIG CHECK ON RUDDER CONTROL ROD. DISCOVERED CRACK IN UPPER RUDDER TRAILING EDGE HINGE PN175A1210-5 REF IPC 55-40-51 FIG ITEM 1

CREW REPORTS; 23767; AFTER T/O NO HEADING DATA DISPLAYED ON EITHER SIDE

STAB OUT OF TRIM LITE ILLUM AT FL340 OTH PRIMARY AND B/U TRIM INOP COCKPIT OUT OF NORMAL CONFIGURATION, STAB TRIM S/WS ARE ON CUTOUT POSITION AND FLAP S/W IS ON INHIBIT POSITION REMOVED ABD REPLACED STAB TRIM MOTOR REF AMM 27-41-71-400-801 UP TP STEP G (5) STILL NEEDS BONDING CHECK. ACCOMPLISHED BONDING CHECK OF STAB TRIM MOTOR TO AIRCRAFT STRUCTURE IAW AMM 27-41-71-400-801 STEP G (5) BONDING CHECKED GOOD AND WITHIN LIMITS. REPLACED STABILZER TRIM MOTOR. IAW AMM 27-41-71-400-801. COMPLETED INSTALL OF THE STAB MOTOR OF AMM 27-41-71-400-801 UP TO TEST. COMPLETED INSTALLATION OF THE STABALIZER TRIM MOTOR IAW AMM 27-41-71-400-801 PERFOMED A STABILIZER TRIM MOTOR TEST IN REFERENCE TO B737 AMM 27-41-71-700-801 PERFORMED A STABILIZER TRIM MOTOR AUTOPILOT TEST IN REFERENCE TO B737 AMM 22-11-81-710-801 TEST PASSED

FUEL LEAK SURGE TANK DRAIN LEFT MAY BE C TANK FILLING L TANK RESET PURGE VALVE ON LEFT WING, SUMPED LEFT WING PURGE TANK, NO FUEL FOUND. ACP FIM28-21 TASK 833 C. 1-6 NO FUEL MIGRATION FOUND DURING TESTS. WING FUEL WAS GREATER THAN 6500 AMD CENTER TANK WAS GREATER THAN 1500 FOR EACH TEST FOR 30 MINUTES SINCE FIM TASK 28-21 TASK 833 WAS ACCOMPLISHED. AS PRECAUTIONARY, PERFORMED IDLE ENGINE RUN ON #1 ENGINE REF. AMM 71-00-00-910-803-G00, WITH CROSSFEED VALVE CLOSED, ONLY LEFT CENTER TANK TURNED ON, OTHER FUEL TANK SWITCHES IN THE OFF POSITION. RAN #1 ENGINE WITH 6.51 LBS LEFT WING AND 2.31 ON CENTER TANK. AFTER RUNNING #1 ENGINE FOR 25 MINUTES, ONLY CHANGE WAS 6.52 LBS ON LEFT WING AND 2.00 ON CENTER. ALSO, SUMPED BOTH LEFT AND RIGHT WING SURGE TANKS, NO EVIDENCE OF FUEL IN THE SURGE TANKS. DID NOT FIND SIGNS OF UNWANTED FUEL TRANSFER DURING THE ENGINE RUN, SUSPECT THERE WAS INTERMITTENT FAULT.

ENROUTE WITH CENTER PUMP, LOW PRESSURE LIGHT ILLUMINATION THE FIRE WARNING LIGHT ALSO ILLUMINATED. WITH CENTER PUMPS OFF, THE FIRE WARNING LIGHT EXTINGUISHED. NO OTHER ASSOCIATED FIRE LIGHTS ILLUMINATED. ON ENGINE SHUTDOWN AT GATE, FIRE WARNING LIGHT CAME ON AGAIN WITH MASTER CAUTION. NO OTHER FIRE LIGHTS ILLUMINATED. DID NOT CYCLE CENTER PUMPS ENROUTE. GROUNDED - YES. T/S & FOUND HISTORY IN COMPARTMENT OVERHEAT DETECTION CONTROL UNIT INDICATING MSG26-F0716 AN INTERMDIENT OPEN - BITE TEST OF DETECTION CONTROL UNIT PASSED. KEEL BEAM OVERHEAT DETECTOR CURRENTLY FLUXUATING BETWEEN 24 & 38 OHMS CONTINUALLY. SUSPECT LOWER ANTI-COLLISION LITE ASSY & PANELS 192K & 193B TO GAIN ACCESS. PANEL 193D PARTIALLY REMOVED. CONTINUED TO FULLY REMOVE PANEL 193D. INSPECTED AFT KEEL BEAM DETECTION LOOP & FOUND NO DEFECTS, ALL CONNECTIONS TIGHT, SECURED, & SAFETIED. ISOLATED CAUSE OF ERRATIC READINGS TO LENGTH OF WIRE BETWEEN D848 & PRESSURE SEAL IMMEDIATELY FWD. DISCONNECTED D848 FROM M272. LWR BEACON LIGHT CB RECONNECTED D848 REF AMM 26-18-02. RESISTANCE READINGS IN RANGE AFTER THAT.

AT 37000 MSL; THE AUTO FAIL LIGHT ILLUMINATED. THE AUTO FAIL LIGHT REMAINED ILLUMINATED IN ALTN MODE AND THE QRH DIRECTED US TO MANUAL MODE. PACKS AND BLEEDS OPERATED NORMALLY

LOUD NOISE AND VIBRATION FROM NOSE AREA PASSING 25000FT LOCKED FOR FERRY FLIGHT UNLOCKED FOR TECH UPDATES. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN FOUND FWD ACCESS DOOR LOOSE ON BOTH FWD ENDS. NO PRESSURIZATION ACCOMPLISHED ECRA 5240-02090 FOR FERRY FLIGHT. ACCOMPLISHED VISUAL INSPECTION OF ACCESS DOOR , SURROUNDING AREA AND HARDWARE , NO DISCREPANCIES FOUND. READJUSTED DOOR STOP PINS REF. AMM 52-48-31-400-801 AND IPC. 52-48-31-01 , MEASURED A DRAG VALUE OF 0.63. PRESSURIZED AIRCRAFT REF. AMM 05-51-91-790-801 , NO LEAKS NOTED.

ANTISKID INOP LIGHT ON ACCOMP FIM 32-42 TASK 840 , FOUND AACU FAULT PWR 1-4 , RPL AACU SERVICE AS PER AMM TASK 32-42-21-400-801 , PERFORMED BITE TEST AS PER ROTABLE PARTS CHANGE WAS INDICATED - TT # 1554706 SN OFF 0820 AMM 32-42-00-740-801. NO FAULTS NOTED , ALSO PERF AACU OPS TEST AS PER AMM 32-42-00-720-801. NO FAULTS NOTED TEST NORMAL. OK FOR FAULT

ALL EMER LIGHTS AFT OF ROW 20 INOP

CABIN PRESSURIZATION CYCLING +/- 500 FPM ON CABIN CLIMB GAUGE. INFO: STEADY AT CRUISE; FL 350 3 + 30 INTO FLIGHT SWITCHED TO ALTN CTRL ON CABIN PRESS PANEL.