N24706

Part: PROXIMITY SENSOR — FAULTED (ZONE 700) · airframe 83,318 hrs · 30,503 cycles

OVR HD LEFT GEAR GREEN LIGHT REMAINED ILLUMINATED AFTR TAKEOFF AND WOULD NOT RETRACT INDICATION. PREFORMED PSEU BITE FOUND FAULT CODE 32-61007. REF FIM 32-61 TASK 801 DEPINNED THE SENSOR AND REMOVED OLD SENSOR ROUTED NEW HARNESS AND INSTALLED NEW SENSOR S1006 UP TO AND INCLUDING STEP 3.F(6)(A). IAW AMM 32-61-31-400-801, NEXT STEP IS CLEAREANCE MEASUREMENT AND OPS CHECK. PERFORMED SENSOR (S0302) CLEARANCE MEASURMENT AND BITE CHECK IAW AMM 32-61-31-400-801 FROM STEP 3.F(6)(B) TO COMPLETION, BITE CHECK GOOD.

Part: HOOK — DEFORMED (ZONE 800) · airframe 82,963 hrs · 30,339 cycles

ESCAPE SLIDE PACK BUSTLE LOOSE L1 VISUALLY INSPECTED L1 ESCAPE SLIDE BUSTLE PER AMM 25-61-01 GIRT LENGTH WITHIN LIMITS. FOUND "J" HOOK SLIGHTLY DEFORMED ADJUSTED TO PROPER CONFORMITY MEASUREMENT.

Part: SELECTOR — OUT OF POSITION (HYD SYSTEM) · airframe 82,772 hrs · 30,246 cycles

HYD SYS A AND B BOTH LOST QTY DURING FLT ABOUT 1PERCNT EVERY 10 MIN FLIGHT CREW LOGGED QUANTIES AND TIMES CREW ALSO INDICATED PRESSURE ON BOTH SYSEMS WERE CONSISTANT AND NORMAL. INFO: CDS BITE SHOWED NO ASSOCIATED FAULTS FOUND RSERVOIR FILL SELECTOR VALVE ON THE B SYSTEM POSITION. MOVED SELECTOR TO THE CLOSED POSITION. PERFORMED DEU 1 & 2 SELF TEST PROCEDURE. PERFORMED DEU 1 & 2 BITE TEST. NO FAULTS PRESENT AT THIS TIME. BOTH DEU 1 & 2 TEST PASSED. PERFORMED HYD RESERVOIR PRESSURIZATION SYSTEM LEAKAGE TEST. TEST PASSED. PERFORMED EXTERIOR WALK AROUND TO CHECK FOR LEAKS. NO LEAKS NOTED AT THIS TIME. FOUND RESERVOIR FILL SELECTOR VALVE ON THE B SYSTEM POSITION. MOVED SELECTOR TO THE CLOSED POSITION. PERFORMED A 5 MINUTE ENGINE RUN 1 & 2 ENGINES, NO FAULTS NOTED AT THIS TIME. RAN HYDRAULIC SYSTEMS A & B, CYCLED FLIGHT.

Part: WIRE — BROKEN (ZONE 200) · airframe 82,578 hrs · 30,161 cycles

FOUND ROW 23ABC PATHWAY EMERGENCY LIGHT INOP REF AMM 33-51-11 RELAMPED SEAT EMERGENCY LIGHT AND REPLACED ASSEMBLY, NO HELP DF PER MEL TOMC APPROVES C/W DDP FOUND SEAT WIRE HARNESS WITHBROKEN LOCKING TAB AND DISCONNECTED UNION AT BASE OF SEAT 23ABC REF 737 SWPM 20-42-01 UNPINED REPLACED CONNECTOR AND REPINNED AND SECURED. LIGHT RESTORED.

Part: LIGHT — NO TEST (ZONE 200) · airframe 82,519 hrs · 30,134 cycles

EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - FOUND SEAT 24 ABC LOWER SEAT EMERGENCY LIGHT INOP. SECURED CONNECTOR D12054 AT SEAT ROW 24 ABC. ALL EMER LIGHTS CHECK OK REF WDM 33-51-22

Part: NONE — NONE (NONE) · airframe 82,393 hrs · 30,071 cycles

INPUTING ESFR

Part: SKIN — DAMAGED (ZONE 100) · corrosion level 2 · airframe 81,825 hrs · 29,829 cycles

INSPECT (GENERAL VISUAL) LAVATORY SERVICE PANEL(S) FOR, BUT NOT LIMITED TO: {B737-38-3-0129} - FASTENERS PULLING THRU LAV PANEL FRAME STRUCTURE LOCKING FOR MX FERRY FLIGHT 2 SEPARATE AREAS OF BULGING METAL AT LOWER FWD AND AFT CORNERS OF LAV DOOR REPAIR. FWD AREA APPROX 6 X 7 OF BULGING AREA WITH APPROX 6-10 RIVETS PULLING THRU. BULGE HEIGHT APPROX .250 HIGH. AFT AREA APPROX 4X6 WITH ANOTHER EXTRA PICTURE SHOWING NO DAMAGE TO INTERIOR STRUCTURE AND ONLY FWD AND AFT LOWER CORNERS TOTAL OF EIGHT RIVETS PULL THROUGH ONLY THROUGH FIRST PLY AND NO DAMAGE TO STRUCTURE OR BACK SIDE OF THE RIVETS THAT HAVE PULLED THROUGH PICTURE OF EIGTH RIVETS 6-10 RIVETS PULLING THRU. BULGE HEIGHT APPROX .200 HIGH. ACCOMPLISHED STEP 7. HFEC INSP OF BLENDED AREA REF NDT PART6, 51-00-00 PROC23, STEP 8 HOLE PROBE HFEC INSP OF FASTENER HOLES REF NDT PART6, 51-00-00, PROC16. NO NOTABLE CRACK INDICATIONS NOTED. REF AVO13671. UNLOCKING FOR UPDATES ACCOMPLISHED STEP 9, ULTRASONIC INSP FOR REMAINING THICKNESS REF NDT PART 4, 51-00-00 PROC.3. COMPLIED WITH AVO13671 STEPS 1.- 6., INSPECTED AREA, NO OTHER DAMAGE NOTED, REMOVED LAV SERVICE PAN AND FASTENERS, REMOVED CORROSION, REPAIRS ACCOMPLISHED IAW EC/RA5300-03174.

Part: NONE — NONE (NONE) · airframe 81,809 hrs · 29,823 cycles

REMOVED L1 DOOR ESCAPE SLIDE TO F.O.M. RENDER SAFE ESCAPE SLIDE CHECKLIST COMPLETE REINSTALLED L1 DOOR ESCAPE SLIDE I.A.W. AMM 25-66-00. SLIDE PACK NEVER OPENED. REMOVE AND REPLACE COMPLETE VERIFIED INSTALLATION AND OPPERATION. QC#U223821

Part: FITTING — CRACKED (STA 727 & S-18A) · airframe 78,284 hrs · 28,238 cycles

AT D1 CHECK IN IAH, CRACKS WERE FOUND DURING EA 5310-07660 OP 1 & 2 INSPECTION OF STA 727 & S-18A WEB AT LH UPPER, LH LOWER AND RH LOWER HOLE LOCATIONS. AN INTERIM REPAIR WAS ACCOMPLISHED REPLACING THE CRACKED FITTINGS AND OVERSIZING FASTENER HOLES DUE TO HOLE QUALITY. THE INTERIM REPAIR IS PENDING FINAL REPAIR EVALUAT ION. ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF THE LATEST REVI SION OF EC/RA 5310-08189 ON OR BEFORE JANUARY 13, 2025. ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF THE LATEST REVI SION OF EC/RA 5310-08189 ON OR BEFORE JANUARY 13, 2025.

Part: STRINGER — CORRODED (STR22R, STA1006) · airframe 78,284 hrs · 28,238 cycles

FOUND CORROSION ON STR 22R AT STA 1006 R/H SIDE UNDER AFT WET AREA...REF BAM N/R# 1517657 FOR WORK ACCOMPLISHED PART 2 OF THE LATEST REVISION OF EC/RA 5330-07118 ON OR BEFORE 09-FEB-2025. INTERIM REPAIR ACCOMPLISHED AT FUSELAGE SKIN STA 1006 BETWEEN S-21R & S-24R - ACCOMPLISH INITIAL INSPECTION REQUIREMENTS PER TOMC APPROVED DIP CARRY. IAH MX PERFORMED INTERIM REPAIR PER TOMC-APPROVAL FROM SC1ELBYC COMMENT PART 1 REF ECRA 5330-07118. PLACED ON DIP TO ACCOMPLISH INITIAL INSPECTION REQUIREMENTS PER PART 2 OF THE LATEST REVISION OF EC/RA 5330-07118 ON OR BEFORE 09-FEB-2025.

Part: UNKNOWN — DAMAGED (R2 DOOR) · airframe 78,284 hrs · 28,238 cycles

DAMAGE FOUND ON R2 DOOR CUT-OUT OUTER CHORD IN TWO SPOTS BTWN STA 965 TO STA 983 LOG PAGE CREATED FOR SFR REPORTING. SFR #1033393 CREATED. REPAIR COMPLETED AT IHC HEAVY D CHECK VISIT ON BAM NR 1482301 & 1482299 PER ECRA 5370-01086. DIP LP 5432529 & 5432657 CREATED FOR PERMANENT REPAIR. GOOD LPG. CREATED FOR SFR REORTING ,SFR 1033393 CREATED,REPAIR COMPLE TED AT IHC HEAVY D CHECK VISIT ON BAM NR 001482301 & 001482299 PER ECRA 5370-01086. DIP LPG 5432529 & 5432657 CREATED FOR PERMANENT REPAIR.

Part: WEB — DAMAGED (R2 DOOR) · airframe 78,284 hrs · 28,238 cycles

ELONGATED HOLES AT R2 DOOR WEB ABOVE R2 Z-ANGLE BTWN STA 887 TO STA907. REMOVED DAMAGED SECTION OF WEB, FABRICATED REPAIR PIECES,TREATE D,PRIMED,INSTALLED REPAIR PIECES, REINSTALLED WEB IN REF TO ECRA 5311-03044 NEED DIP INFO. GENERATED DIP FOR FURTHER INSPECTIONS....REF L/P# 5403629 FOR DI P INFORMATION

Part: NONE — MISSING (LEFT WING INBD A) · airframe 76,091 hrs · 27,238 cycles

TRAILING EDGE FLAP BULB SEAL LEFT WING INBOARD FLAP LOWER SEAL IS MISSING UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. INSTALL LIFT WING TRAILING EDGE BULB SEAL PER AMM 27-81-11-910-801-C1

Part: NONE — MISSING (LT WING IB AFT F) · airframe 76,091 hrs · 27,238 cycles

THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 9/05/22. TRAILING EDGE FLAP BULB SEAL LEFT WING INBOARD FLAP LOWER SEAL IS MISSING. INSTALL LEFT WING TRAILING EDGE BULB SEAL. OPS CHECKS GOOD.

Part: FITTING — CRACKED (BS 540) · airframe 69,881 hrs · 24,825 cycles

SHEAR FITTING AT STA 540 LBL 6.14 IS CRACKED. L/P 6471112 SUPPOR T TASK REMOVED AND REPLACED SHEAR FITTING IAW B737-700. SRM 51-40-02 AN D ECRA NO. 5714-01047.SSFR REPORT, FORM 46-0024, ENTERED BY UAL U358176, 1/27/20 INSPECTION ACCEPTED

Part: FITTING — CRACKED (BS 540) · airframe 69,881 hrs · 24,825 cycles

SHEAR FITTING AT STA 540 RBL 32.40 IS CRACKED. L/P 6471109. SUPP ORT TASK REMOVED AND REPLACED SHEAR FITTING IAW B737-700. SRM 51-40-02 AN D ECRA NO. 5714-01049. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U358176, 1/27/20 INSPECTION ACCEPTED

Part: FITTING — CRACKED (BS 540) · airframe 69,881 hrs · 24,825 cycles

SHEAR FITTING AT STA 540 LBL 54.60 IS CRACKED. L/P 6471114. SUPP ORT TASK REMOVED AND REPLACED SHEAR FITTING IAW 737-700. SRM 51-40-02 AND DWG NO. 111A2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INS PECTION U358176, 1/27/20 INSPECTION ACCEPTED

Part: FITTING — CRACKED (BS 540) · airframe 69,881 hrs · 24,825 cycles

SHEAR FITTING AT STA 540 RBL 40.87 IS CRACKED. L/P 6471110. SUPP ORT TASK REMOVED AND REPLACED SHEAR FITTING IAW B737-700. SRM 51-40-02 AN D DWG 111A2000.

Part: FITTING — CRACKED (BS 540) · airframe 69,881 hrs · 24,825 cycles

SHEAR FITTING AT STA 540 RBL 6.14 IS CRACKED. L/P 6471106 . SUPP ORT TASK REMOVED AND REPLACED SHEAR FITTING IAW B737-700. SRM 51-40-02 AN D DWG. 111A2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPE CTION U358176, 1/27/20 INSPECTION ACCEPTED

Part: FITTING — CRACKED (BS 540) · airframe 69,881 hrs · 24,825 cycles

SHEAR FITTING AT STA 540 RBL 15.04 IS CRACKED. L/P 6471107. SUPP ORT TASK REMOVED AND REPLACED SHEAR FITTING IAW B737-700. SRM 51-40-02 AN D ECRA NO. 5714-01048.

Part: FITTING — CRACKED (BS 540) · airframe 69,881 hrs · 24,825 cycles

SHEAR FITTING AT STA 540 RBL 54.60 IS CRACKED. L/P 6471111. SUPP ORT TASK REMOVED AND REPLACED SHEAR FITTING IAW B737-700. SRM 51-40-02 AN D ECRA NO. 5714-01050.

Part: FITTING — CRACKED (BS 540) · airframe 69,881 hrs · 24,825 cycles

SHEAR FITTING AT STA 540 LBL 15.04 IS CRACKED. L/P 6471113. SUPP ORT TASK REMOVED AND REPLACED SHEAR FITTING IAW B737-700. SRM 51-40-02 AN D DWG 111A2000.

Part: THERMOCOUPLE — FAILED (RT ENGINE) · airframe 67,471 hrs · 23,857 cycles

R-ENG EGT OVERTEMP DURIN G CLIMB THRU 15000 FT. ARC TURNED AMBE R. MAX EG T SEEN WAS 918C. ENG 2 BITE TEST, MSG NMBR: 77-20872 THE TOP LEFT EGT SIGNAL 77-21-00-810-804-F00 THE TOP LEFT EGT SIGNAL (T495S4) IS OUT OF RANGE - FAULT ISOLATION (T495S4)IS OUT OF RANGE. REF FIM TASK TASK FIM 71-06-00-810-804 STEP E 2 A. ALSO FOUND MAINTENANCE MSG 77-20862 DURING EEC BITE TEST . REF REF MM 77-21-01-200-801-F00, FOUND CJ10 HARNESS FAIL INSULATION TEST AND S4 PROBE INSULATION SHORTED TO GROUND. RESISTANCE TEST GOOD, REMOVED AND REPLACED CJ10 HARNESS AND S4 PROBE REF MM 73-2 1-06 AND MM 77-21-01, NEED TO PERFORM FADEC SYSTEM TEST REF MM 7 3-21-00 ADD EMP:344019 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1143802 SN OFF 7634 PROBE, THERMOCO OFF 29-7721-9-9001 7634 ON 29-7721-9-9001 0909 INSPECTION NOT REQUIRED ACP, FADEC EEC TEST AND TEST 12 ACTUATORS TEST AND ACPD IDLE RUN #1 AND #2 ENGINES. OPS CKS GOOD, NO FAULTS NOTED.

Part: CIRCUIT BREAKER — TRIPPED (WASTE DISPOSAL) · airframe 67,225 hrs · 23,755 cycles

ALL 3 TOILETS ARE NOT FLUSHING. FOUND VACUUM WASTE CB POPPED ON P18-3 PANEL. PER FIM 38-30-00-810-811 CB 1423 WAS NOT CLOSED ON ARRIVAL. VERIFIED M1188 MODULE AT AFT GALLEY SECURE, LCM IN AFT PIT SECURE AND HARNESS, ALL LAV HARNESS SECURE UNDER SINKS. SYSTEM OPS CHKD BY ALMOST ENTIRE PAX LOAD AND NO FAULTS. LCM BITE OK. WATER PX NOMINAL. OK FOR SVC PER VERIFICATION IN FIM TASK.

Part: FRAME — CRACKED (BS 235) · airframe 61,745 hrs · 21,454 cycles

INNER PART OF FRAME AT BS 235.8 IS CRACKED AT FASTENER HOLE FOR EXTERNAL POWER RECEPTACLE BOX ATTACH LOCATION. INSTALLED A REPAIR IAW EC/RA 5310-07150. BS 235.8 FROM RBL 30 TO RBL 40.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 61,745 hrs · 21,454 cycles

PERFORMED HFEC AT CENTER WING REAR SPAR VERTICAL PRESSURE WEB AND FOUND CRACK AT APPROX WL 196.0 AND LBL 42.0 . INSTALLED REPAIR PER EC/RA 5710-02610 AND SRM 57-10-10, REPAIR 3, ALTERNATIVE 2.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,376 hrs · 20,511 cycles

LAST 4 ROWS ON LEFT SIDE EMERGENCY AISLE LIGHTING IS INOPERATIVE. R & R EMERGENCY BATTERY PACK REF AMM 33-51-06-9 60-805. LOCATED AT RT SIDE OVERHEAD AFT GALLEY CEILING. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE · airframe 59,376 hrs · 20,511 cycles

EMERGENCY LIGHTS NOT ARMED, LIGHT INDICATOR BULBS BURNED OUT. RELAMPED, CKS GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,266 hrs · 19,670 cycles

RIGHT OVERWING EXIT, EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED & ADJUSTED THE LIGHT RECEPTACLE IAW AMM 33-51-06-960-805. SYS CHECKED GOOD IAW AMM 33-51-06-960-805, PN 767.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 55,338 hrs · 18,914 cycles

DAMAGED FASTENER HOLES ON INTERIOR SURFACE AT STATION 540 BULKHEAD CHORD BETWEEN STRINGER 22R & 23R, FIVE EACH MARKED. REPAIRED OVERSIZED FASTENER HOLES BY INSTALLING FREEZE PLUG, DOUBLER & TRIPLER IAW ECRA 5310-06416.

Part: SLIDE — UNKNOWN (R2 DOOR) · airframe 53,639 hrs · 18,265 cycles

INBOUND CREW PIREP SOMETHING HANGING FROM SLIDE. REMOVED SLIDE FROM DOOR & ACCIDENTALLY BLOWN ON REINSTALLATION IN SHROUD. REPLACED SLIDE ASSEMBLY R2 DOOR & REINSTALLED GIRT BAR ASSEMBLY IAW MM 25-66-01401. SAFETY PIN REMOVED & STOWED IN POUCH. DOOR & GIRT BAR OPERATIONS CHECKED NORMAL.

Part: SLIDE — UNWANTED DEPLOY (L2 DOOR) · airframe 53,515 hrs · 18,217 cycles

IN FLIGHT CLIMBING TO FL400 AFT LT DOOR SLIDE DEPLOYED & AFT DOOR LIGHT ILLUMINATED. ACFT REMAINED PRESSURIZED. DIVERTED TO NEAREST AIRPORT. INSPECTED L2 DOOR IAW AMM 52-13-00-200-801 AFT ENTRY DOOR CHECK & 52-13-00-700-805 AFT ENTRY DOOR SYS TESTED ONE TIME AW A00 4974. DOOR OPERATIONS CHECKED SMOOTH & NORMAL. REPLACED DOOR 2L SLIDE & COVER ASSEMBLY IAW MM 25-66-01-400-803.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,847 hrs · 16,460 cycles

EMERGENCY LIGHTS ROWS 3-7 INOPERATIVE, TROUBLESHOT AND REPLACED BATTERY PACK IN SIDEWALL. OPS CHECKED GOOD IAW AMM 33-51-06-960-805.

Part: FRAME — CRACKED (BS 787) · airframe 47,443 hrs · 15,985 cycles

FRAME BS 787, CRACKED AT FASTENER, RADIUS GOOD. REPAIRED IAW EA 5310-04716, REV C, OP1 SEE FLEET CYCLE FOR ALL WORK PERFORMED.

Part: FLOORBEAM — CORRODED (BS 947.5) · airframe 47,490 hrs · 16,000 cycles

BS 947.5 FLOORBEAM AT RBL 48 UNDER AFT OTBD LAV MOUNT CORRODED. REPAIRED FLOORBEAM IAW SRM 53-70-51 AND ECRA 5321-01805.

Part: FRAME — CRACKED (BS 907) · airframe 47,443 hrs · 15,985 cycles

FRAME BS 907, CRACKED AT BRACKET FASTENER RADIUS GOOD. REPAIRED FRAME AT 907 IAW ECRA 5310-0557.

Part: FLOOR SUPPORT — CORRODED (BS 260-270) · airframe 47,443 hrs · 15,985 cycles

FLOOR SUPPORT INTERCOSTAL CORRODED FROM STA 260-270 RBL5 -LBL5. R & R IAW EC/RA 5321-01566.

Part: FRAME — CRACKED (BS 827) · airframe 47,443 hrs · 15,985 cycles

FRAME BS 827, CRACKED AT BRACKET FASTENER. RADIUS GOOD. ALL WORK COMPLETE.

Part: INTERCOSTAL — CORRODED (BS 260) · airframe 47,443 hrs · 15,985 cycles

BS 260 LATERAL INTRECOSTAL CORRODED AT LBL 10 - RBL 10. REPAIRED IAW ECRA 5321-01807.

Part: FRAME — CRACKED (BS 907) · airframe 47,443 hrs · 15,985 cycles

FRAME BS 907, CRACKED AT FASTENER, RADIUS GOOD. REPAIRED IAW ECRA5310-05570.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 47,443 hrs · 15,985 cycles

LEFT HORIZONTAL STAB LOWER SKIN SURFACE SHOWS CRACK INDICATION WITH C- SCAN AT STA 129.50 2 EA CRACKS MEASURED WITH HFEC CRACK LENGTH 1.5 AND .25 MARKED INSTALLED REPAIR REF SRM 55-10-01, REPAIR 11.

Part: INTERCOSTAL — CORRODED (BS 270) · airframe 47,443 hrs · 15,985 cycles

BS 270, LATERAL INTERCOSTAL CORRODED AT LBL10-RBL10. REPAIRED INTERCOSTAL IAW ECRA 5321-01566.

Part: FRAME — CRACKED (BS 867) · airframe 47,443 hrs · 15,985 cycles

FRAME BS 867, FRAME CRACKED AT FASTENER HOLE BETWEEN STR 8 AND 9R. FRAME REPAIRED IAW EA 5310-04716 REV C, OP 1, FIG 3.

Part: FRAME — CRACKED (BS 867) · airframe 47,443 hrs · 15,985 cycles

FRAME 867L CRACKED AT BRACKET FASTENER, RADIUS GOOD REPAIRED IAW EA 5310-04716, REV C, OP1.

Part: FRAME — CRACKED (BS 827) · airframe 47,443 hrs · 15,985 cycles

FRAME 827R CRACKED AT FASTENER BETWEEN STR 8 AND STR 9R. REPAIRED FRAME 827 R IAW EA 5310-04716 REV C, OP 1, FIG 3.

Part: FRAME — CRACKED (BS 747) · airframe 47,443 hrs · 15,985 cycles

FRAME 747, RT CRACKED AT FASTENER RADIUS GOOD REPAIRED IAW EA 5310-04716, REV C.

Part: FRAME — CRACKED (BS 500A) · airframe 47,443 hrs · 15,985 cycles

FRAME 500A L CRACKED AT BRACKET FASTENER BETWEEN STR 8L AND 9L. REPAIRED FRAME 500A L IAW EA 5310-04716.

Part: FRAME — CRACKED (BS 440) · airframe 47,443 hrs · 15,985 cycles

FRAME 440L CRACKED AT FASTENER BETWEEN STR 8 AND STR 9L, FRAME 440L. FRAME REPAIRED IAW EA 5310-04716.

Part: FRAME — CRACKED (BS 727D) · airframe 47,443 hrs · 15,985 cycles

SUPPORT TASK FRAME AT STA 727D L CRACKED AT FASTENER HOLE BETWEEN STR 8 AND 9L. REPAIRED FRAME IAW EA 5310-04716.

Part: FRAME — CRACKED (BS 727B) · airframe 47,443 hrs · 15,985 cycles

SUPPORT TASK FRAME 727B L CRACKED AT FASTENER HOLE BETWEEN STR 8 AND 9L. REPAIRED FRAME 727B L IAW EA 5310-04716.

Part: FRAME — CRACKED (BS 480) · airframe 47,443 hrs · 15,985 cycles

FRAME 480 L CRACKED AT FASTENER HOLE BETWEEN STR 8 AND STR 9 L. REPAIRED FRAME 480L IAW EA 5310-04716.

Part: FRAME — CRACKED (BS 727D) · airframe 47,443 hrs · 15,985 cycles

FRAME 727D R CRACKED AT FASTENER HOLE AT ATTACH BRACKET BETWEEN STR 8R AND 9R REPAIRED FRAME 727D R IAW EA 5310-04716.

Part: FRAME — CRACKED (BS 787) · airframe 47,443 hrs · 15,985 cycles

FRAME 787L, CRACKED AT BRACKET FASTENER, RADIUS GOOD REPAIRED IAW EA 5310-04716, REV C, OP 1.

Part: FRAME — CRACKED (BS 520) · airframe 47,443 hrs · 15,985 cycles

FRAME 520R CRACKED AT FASTENER, RADIUS GOOD REPAIRED IAW EA 5310-04716.

Part: FRAME — CRACKED (BS 480) · airframe 47,443 hrs · 15,985 cycles

FRAME 480R CRACKED AT FASTENER, RADIUS GOOD REPAIRED IAW EA5310-04716.

Part: FRAME — CRACKED (BS 727) · airframe 47,443 hrs · 15,985 cycles

FRAME 727BR CRACKED AT FASTENER , RADIUS GOOD REPAIRED IAW EA 5310-04716.

Part: FRAME — CRACKED (BS 400) · airframe 47,443 hrs · 15,985 cycles

FRAME 400R, CRACKED AT FASTENER , RADIUS GOOD REPAIRED IAW EA 5310-04716.

Part: FRAME — CRACKED (BS 440) · airframe 47,443 hrs · 15,985 cycles

FRAME 440R CRACKED AT FASTENER, RADIUS GOOD REPAIRED IAW EA 5310-04716.

Part: LENS — MISSING (EXIT SIGN) · airframe 44,949 hrs · 15,108 cycles

OVERWING EXIT ABOVE DOOR AT ROW 20 MISSING. INSTALLED OVERWING EXIT LENS P/N 29-3351-3-0025. OK FOR SERVICE WPB 2779242.

Part: MECHANISM — FAULTY (AILERON) · airframe 38,666 hrs · 12,842 cycles

THE AILERONS ARE VERY STIFF TO MOVE THROUGHOUT FULL TRAVEL. REMOVED AND REPLACED AILERON TRANSFER MECHANISM IAW 737 AMM 27-11-61. ROTABLE PARTS CHANGE WAS INDICATED - TT 1054666, S/N OFF 01332.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,935 hrs · 11,133 cycles

CABIN STATION 500 AT S9R PASSENGER SERVICE UNIT RAIL BRACKET TO FRAME CRACKED. REPAIRED FRAME REF EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,935 hrs · 11,133 cycles

CABIN STATION 400 BETWEEN S8L AND S9L HAS PASSENGER SERVICE UNIT RAIL ATTACH BRACKET TO FRAME CRACKED. REPAIRED FRAME REF EA 5310-04498.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,935 hrs · 11,133 cycles

CABIN STATION 747 AT S9L PASSENGER SERVICE UNIT RAIL BRACKET TO FRAME CRACKED. REPAIRED FRAME REF EA 5310-04498.

Part: ATTACH BRACKET — CRACKED (CABIN) · airframe 33,935 hrs · 11,133 cycles

PASSENGER SERVICE UNIT (PSU) RAIL ATTACHMENT BRACKET TO FRAME CRACKED AT CABIN STATION 747 BETWEEN S8L AND S9L. CUT OUT DAMAGE AND INSTALLED REPAIR ANGLES IAW ECRA 5310-04498.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 33,935 hrs · 11,133 cycles

CABIN FLOOR SUPPORT STA 380 TO 400 BL 0 CRACKED. REMOVED AND REPLACED FLOOR SUPPORT STA 380-400 BL 0 REF SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 33,935 hrs · 11,133 cycles

CABIN FLOOR SUPPORT STA 380 TO 400 RBL 13 CRACKED. REMOVED AND REPLACED CABIN FLOOR SUPPORT PER SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 33,935 hrs · 11,133 cycles

PAX CABIN FLOOR STRUCTURE SUPPORT HAS CRACKED INTERCOSTAL BETWEEN STA 344 AND STA 360 AT BL 0. REMOVED AND REPLACED INTERCOSTAL IN REF TO SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 33,935 hrs · 11,133 cycles

PAX CABIN FLOOR STRUCTURE HAS CRACKED INTERCOSTAL BETWEEN STA 312 AND STA 328 AT ABOUT LBL46. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,008 hrs · 9,820 cycles

INSPECTION FOUND AFT HALF SECTION OF AISLE PATH LIGHTING INOPERATIVE DURING RON. THE BATTERY PACK FOR M1672 CHARGER WAS FOUND AT FAULT, REF W/D 33-51-11. THE BATTERY PACK WAS REPLACED.

Part: COFFEEMAKER — MALFUNCTIONED (AFT GALLEY) · airframe 27,194 hrs · 8,913 cycles

AN ODOR OF BURNING INSULATION WAS EVIDENT WHEN BREWING COFFEE IN THE AFT GALLEY WHILE EN ROUTE TO IAH. THE COFFEEMAKERS WERE TURNED OFF AND CIRCUIT BREAKERS WERE PULLED. THE AIRCRAFT ARRIVED AT IAH WITHOUT FURTHER PROBLEM. BOTH AFT GALLEY COFFEEMAKERS WERE REMOVED AND REPLACED. OPERATIONAL CHECKS WERE GOOD.

Part: INTERCOSTAL — CORRODED (STA 947-967) · airframe 24,601 hrs · 8,018 cycles

INSPECTION FOUND INTERCOSTAL CORRODED AT STA 947-967, RBL 36. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (STA 986.5) · airframe 24,601 hrs · 8,018 cycles

INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 35 TO RBL 35. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01268.

Part: INTERCOSTAL — CORRODED (STA 986.5-1016) · airframe 24,601 hrs · 8,018 cycles

INSPECTION FOUND INTERCOSTAL CORRODED AT STA 986.5-1016, LBL 33. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW ECRA 5321-01268.

Part: STRUCTURE — CORRODED (STA 992.8-1040) · airframe 24,601 hrs · 8,018 cycles

INSPECTION FOUND CHORD AT R-2 DOOR CORRODED AT STA 992.8 TO 1040, LBL 63. THE CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND BOEING DRAWING 147A8540.

Part: CHARGER — INOPERATIVE (ROW 15-20) · airframe 11,840 hrs · 3,872 cycles

THE EMERGENCY LIGHTS ON SEATS AT ROWS 15-20 WOULD NOT ILLUMINATED WHEN TESTED. TROUBLESHOOTING FOUND M1672 AND M1670 BATTERY CHARGERS FAILED. THE BATTERY CHARGERS WERE REMOVED AND REPLACED IAW MM 33-51-06 AND OPERATION OF THE LIGHTS TESTED GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 11,654 hrs · 3,805 cycles

INSPECTION FOUND EMERGENCY AISLE PATH LIGHTING INOPERATIVE FROM 15AB TO 21AB. THE BATTERY CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-06.

Part: MONITOR — INOPERATIVE (CABIN)

THE FLIGHT ATTENDANT OBSERVED SMOKE AT ROW 21 A-C WHILE EN ROUTE TO IAH. THE VIDEO SCREEN AT ROW 21 WAS ERRATIC. THE VIDEO SYSTEM WAS TURNED OFF AND VIDEO CIRCUIT BREAKERS WERE PULLED. THE SMOKE CEASED AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE VIDEO MONITOR AT ROW 21ABC FAILED. THE VIDEO MONITOR WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. A FUNCTIONAL CHECK OF THE SONY PAVES SYSTEM WAS PERFORMED AND NO DISCREPANCIES WERE FOUND.