N222UA

Part: ACTUATOR — FAULTED (ZONE 800) · airframe 90,874 hrs · 12,065 cycles

DOOR FLIGHT LOCK 3R STATUS MESSAGE DUE TO HISTORY, COMPLIED WITH *DM* REF. MX FAULT MSG 52-11330 FIM 52-11 TASK 806 FOR FAULT ISOLATION, REPEAT WRITE-UP, AFTER FAULT ISOLATION, REMOVED AND REPLACED DOOR LOCK ACTUATOR IAW AMM 52-11-26-400-801 OPS TEST GOOD.

Part: MODULE — INOPERATIVE (ZONE 200) · airframe 90,661 hrs · 12,019 cycles

POWER SUPPLY - BATTERY PACK CAPACITY CHECK PROCEDURE - EMERGENCY PATH LIGHTS INOP IN SEAT 18G, 28G, AND 30D REPLACED FLOOR PROXIMITY LIGHT ASSEMBLY ON SEAT 18G, 28G, AND 30D REFER AMM 33-51-05. OPS CHECK GOOD.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 90,661 hrs · 12,019 cycles

POWER SUPPLY - BATTERY PACK CAPACITY CHECK PROCEDURE - EMERGENCY BATTERY PACK FOR EMERGENCY POWER SUPPLY M33098 OVERDOOR 2R FAILED FUNCTIONAL TEST REPLACED BATTERY PACK AT POWER SUPPLY M33098 OVERDOOR 2R. OP CHECK GOOD REF AMM 33-51-06. OP CHECK GOOD

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 90,661 hrs · 12,019 cycles

POWER SUPPLY - BATTERY PACK CAPACITY CHECK PROCEDURE - EMERGENCY PATH LIGHTS INOP IN SEAT 18G, 28G, AND 30D DUPLICATE WRITE UP. WORK PERFORMED ON LOG PAGE #6651473 DUPLICATE LOG PAGE. WORK PERFORMED ON LOG PAGE #6651473

Part: SKIN — GROUND DAMAGE (ZONE 100) · airframe 90,544 hrs · 11,995 cycles

AIRCRAFT AFT FUSALAGE CONTACTED LAV TRUCK AT LAV SVC HATCH. MULTIPLES DENTS AREAS AROUND LAV SERVICE DOOR ON THE STRINGERS THAT REQUIRED OPEN UP FOR FURTHER INSPECTION FOR DAMAGE. REF. SRM 53-00-01-1A-1. SEE ATTACHED PHOTOS FOR LOCATION OF DAMAGE. SKIN AND INTERNAL STRINGER. AS REQUIRED IMAGES OF AREA 1 AND A EXTERIOR PIC OF AERA 1 . COMPLIED WITH AVO15686 STEPS 1. THROUGH 5. PERFOMED VISUAL INSPECTION, NO OTHER DAMAGE NOTED, GAINED ACCESS, CLEANED AREA, STRIPPED PAINT AND BLENDED OUT SCRATCHES ON SKIN. REQUEST AN INSPECTOR PERFORM HFEC INSPECTIONS REF. AVO15686 STEPS 6. THROUGH 9. ACCOMPLISHED ALL HFEC AS REQUIRED IN STEPS 6-9 OF AVO 15686 REV A. NO FURTHER DEFECTS NOTED. ACCOMPLISHED STEP 10 OF AVO 15686 REV A, ULTRASONIC THICKNESS CHECK LOWEST REMAINING THICKNESS IN AREA 1 IS 0.094" AND AREA 2 IS 0.096" SEE PICTURES FOR GRIDS THE DENT AT AREA ONE IS SMOOTH AND FREE OF OTHER DAMAGE, THE DENT MEASURES 1.60" X 1.70" WITH A DEPTH OF 0.035" FOR A W/Y = 45.7 WHICH IS WITHIN ALLOWABLE DAMAGE LIMITS REF. SRM 53-00-01-1A-1 DETAIL E. SEE AVO15686 REV. B STEP 11. AND 12. VERIFIED DENT IN AREA 1 MEASURES 1.6" X 1.7" WITH A DEPTH OF .035" A/Y OF 45.7 THE DENT AT AREA TWO IS SMOOTH AND FREE OF OTHER DAMAGE, THE DENT MEASURES 5" X 8" WITH A DEPTH OF 0.080" FOR A W/Y 62.5, STRINGER 48L FOLLOWS THE SHAPE OF DEC/W AVO15686 REV. E AND EC/RA #: 5300-03280 REV.A, PART -1, STEPS 1-25.

Part: STRINGER — DENTED (ZONE 100) · airframe 90,539 hrs · 11,994 cycles

REF. LOG PAGE # 6361899 STRINGER 49R IS DAMAGED BETWEEN STA. 1958 AND STA. 1979CUT OUT DAMAGED SECTION OF STRINGER REF. SRM 53-70-03-2R-1 REPAIR 1 PARAGRAGH 4.C. REQUEST ON INSPECTOR PERFORM HFEC INSPECTION OF CUT EDGES AND ALL INITAL FASTENER HOLES IN REPAIR AREA OF STRINGER PER PARAGRAGH 4. D. AND E. P ERFORMED HFEC INSP OF STRINGER EDGE CUTS AND ALL RELATED FASTENERS HOLES AS REQUIRED PER SRM 53-70-03-2R-1 REAPAIR 1 PARA 4.D. AND E WITH NO RELEVANT INDICATIONS. REF 777NDTM PT 6-51-00-01 PR 2 AND PT 6-51-00-02 PR 3. VERIFIED MATERIAL FOR STRINGER REPAIR PART 1 AND 2 FABRICATE FROM .071 7075-0 BARE SHEET ( PO# 7334192345 ) REF. SRM 53-70-03-2R-1 REPAIR 1 FIG.202. VERIFIED STRINGER REPAIR MATERIAL FOR PART 1 AND 2 AS .071 REF. SRM 53-70-03-2R-1 REPAIR 1 FIG.202. VERIFIED MATERIAL OF REPLACEMENT SECTION OF STRINGER FABRICATE FROM .056 7075-0 BARE SHEET REF. SRM 53-70-03-2R-1 REPAIR 1 FIG.202. VERRIFIED "FILLER MATERIAL" PO # 3978832 7075-0-056 BARE VERIFIED -4 FILLER 0.056" 7075-O BARE HAS BEEN HEAT TREATED TO 7075-T6 AND -1 & -2 REPAIR J SECTIONS 0.071" HAVE HEAT TREATED REF. SRM 53-70-03-2R-1 REPAIR 1.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 88,579 hrs · 11,572 cycles

SUPPORT TASK - CABIN DR L2 EXIT SIGN FOUND DIM DURING DEEP CYCLE (POWER FROM EMER PWR PACK M33096). WORK TRANSFER NON ROUTINE WO.4474361. CABIN DR L2 EMER LT POWER BATTERY PACK ( M33096) REPLACED AND INSTALLATION TEST CARRIED OUT WITH RESULT NORMAL AS PER AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 88,579 hrs · 11,572 cycles

SUPPORT TASK - CABIN DR L3 FWD EXIT IDENTIFIER FOUND DIM DURING DEEP CYCLE (POWER FROM EMER PWR PACK M33400). WORK TRANSFER NON ROUTINE WO.4474375 AND ORIGINATED BY EMP V920592. CABIN DR L3 EMER LT POWER BATTERY PACK ( M33400) REPLACED AND INSTALLATION TEST CARRIED OUT WITH RESULT NORMAL AS PER AMM 33-51-06. WORK ACCOMPLISHED BY MECH V920592 AND INSPECTED BY V896963 .

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 88,579 hrs · 11,572 cycles

SUPPORT TASK - CABIN DR R3 EXIT SIGN FOUND DIM DURING DEEP CYCLE (POWER FROM EMER PWR PACK M33404). WORK TRANSFER NON ROUTINE WO.4474384. CABIN DR 3 EMER LT POWER BATTERY PACK (M33404) REPLACED AND INSTALLATION TEST CARRIED OUT WITH RESULT NORMAL AS PER AMM 33-51-06.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 88,579 hrs · 11,572 cycles

SUPPORT TASK - CABIN DR R2 EXIT SIGN FOUND DIM DURING DEEP CYCLE (POWER FROM EMER PWR PACK M33097). WORK TRANSFER NON ROUTINE WO.4474373. CABIN DR R2 EMER LT POWER BATTERY PACK ( M33097) REPLACED AND INSTALLATION TEST CARRIED OUT WITH RESULT NORMAL AS PER AMM 33-51-06.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 88,579 hrs · 11,572 cycles

SUPPORT TASK - LLAR BACK-UP LIGHT FOUND DIM DURING DEEP CYCLE (POWER FROM PWR PACK M023). WORK TRANSFER NON ROUTINE WO.4474388. LLAR EMER LT POWER BATTERY PACK ( M023) REPLACED AND INSTALLATION TEST CARRIED OUT WITH RESULT NORMAL AS PER AMM 33-51-06.

Part: BATTERY — NO TEST (ZONE 200) · airframe 87,551 hrs · 11,324 cycles

POWER SUPPLY - BATTERY PACK CAPACITY CHECK PROCEDURE - EMERGENCY LIGHTS AT 2L DOOR (INSIDE) AND FWD MID GALLEY GO OUT AFTER A FEW MINUTES REPLACED BATTER AT POWER SUPPLY M33096 PER AMM 33-51-06-960-802 CK OK POWER SUPPLY - BATTERY PACK CAPACITY CHECK PROCEDURE - EMERGENCY LIGHTS AT 2L DOOR (INSIDE) AND FWD MID GALLEY GO OUT AFTER A FEW MINUTES REPLACED BATTER AT POWER SUPPLY M33096 PER AMM 33-51-06-960-802 CK OK PARTS USED: 99-3351-3-0015,QTY :1

Part: BATTERY — NO TEST (ZONE 200) · airframe 87,551 hrs · 11,324 cycles

POWER SUPPLY - BATTERY PACK CAPACITY CHECK PROCEDURE - 1R DOOR SLIDE LIGHT AND ASSOCIATED INTERIOR LIGHTS INOP REPLACED BATTERY PACK AT POWER SUPPLY M33094 PER 33-51-06-960-802 CK REPLACED BATTERY PACK AT POWER SUPPLY M33094 PER 33-51-06-960-802 CK OK PARTS USED: AD-D717-01-100,QTY :1

Part: BATTERY — NO TEST (ZONE 200) · airframe 87,551 hrs · 11,324 cycles

POWER SUPPLY - BATTERY PACK CAPACITY CHECK PROCEDURE - 1L DOOR SLIDE LIGHT (EXTERIOR) INOP R&R BATTERY PACK FOR EMERGENCY POWER SUPPLY M33424 REF AMM 33-51-06-960-802. OPS CHECK GOOD PARTS USED: 99-3351-3-0015,QTY :1

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 87,551 hrs · 11,324 cycles

POWER SUPPLY - BATTERY PACK CAPACITY CHECK PROCEDURE - 3R DOOR SLIDE AND ASSOCIATED INTERIOR LIGHTS INOP REPLACED BATTERY PACK AT POWER SUPPLY M33401 REF AMM 33-51-06-960-802 CK OK PARTS USED: AD-D717-01-100,QTY :1

Part: PANEL — BROKEN · airframe 87,547 hrs · 11,323 cycles

PDA 1 PANEL 196JR DEPARTED AC UPON LANDING AND DAMAGED PANEL 198JR. PANEL FOUND ON RUNWAY AFTER LANDING IN HNL. REF LP 9565702 REMOVED REMAINING HINGES ATTACHED TO THE PLANE PER AMM 53-46-01-000-801. FOUND FOLDING STRUT FITTING ASSEMBLY DAMAGED (CRACKED). REMOVED ASSEMBLY, AFT GAP OF PANEL TO ACFT SKIN NOT WITHIN LIMITS. ENLARGING GAP REQ TO BE IN TOLERANCE. PANEL GAP REQ IS 0.14 +/- .06. GAP NOW IS 0.047. REF AMM TASK 53-46-01-400-801 FOR INSTALLATION OF PANEL.

Part: PUMP — FAILED (FUEL SYS) · airframe 86,994 hrs · 11,196 cycles

FUEL SCAVENGE PUMP FAIL INFLIGHT FAULT HISTORY SHOWS "CENTER TANK FUEL SCAVENGE WAS NOT COMPLETED". THIS OCCURED ON THE 22 AND 24TH JULY. MAINTENACE MESSAGE IS 28-11081. REF FIM 28-22 TASK 901. CHECKED FAULT HISTORY, FOUND MAINT MESSAGE HIT ON PREVIOUS LEG. CENTER TANK HAD LESS THAN 2,400LBS WITH 2,200LBS AFTER LANDING. MESSAGE DID NOT HIT ON FOUR CONSECUTIVE LEGS. NO FURTHER MAINT ACTION REQUIRED. ENGINEERING RECOMMENDS: PERFORM FUEL TANK SUMP DRAIN VALVE - WATER REMOVAL/SAMPLING, AMM TASK 12-11-02-680-801, WATER SCAVENGE JET PUMP CHECK, AMM TASK 28-22-13-200-801, IF DEBRIS IS FOUND AND REMOVED PERFORM FUEL SCAVENGE SYSTEM - FUNCTIONAL TEST, AMM TAS K 28-22-00-720-805. ALSO IT IS RECOMMENDED TO PERFORM A MICROBIAL GROWTH TEST. IT IS IMPORTANT THAT A THOROUGH REMOVAL OF WATER IS ACCOMPLISHED.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 84,527 hrs · 10,610 cycles

EMER LT BATTERY PACK AT DR 4R FOUND CAPACITY FUNCTION CHECK FAIL (M33409) REF HX NR WO.2295764, ORIG BY V920586 EMER LT BATTERY PACK AT DR 4R REPLACED AND INSTALLATION TEST RESULT NORMAL IAW AMM 33-51-06 (M33409) ACCOMPLISHED BY MECH V920586, INSP V896992

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 84,527 hrs · 10,610 cycles

EMER LT BATTERY PACK AT DR 3L FOUND CAPACITY FUNCTION CHECK FAIL REF HX NR WO.2295784, ORIG BY V920586 EMER LT BATTERY PACK AT DR 3L REPLACED AND INSTALLATION TEST RESULT NORMAL IAW AMM 33-51-06 ACCOMPLISHED BY MECH V920586, INSP V896992

Part: BATTERY PACK — DISCHARGED (DOOR 3R) · airframe 84,527 hrs · 10,610 cycles

EMER LT BATTERY PACK AT DR 3R FOUND CAPACITY FUNCTION CHECK FAIL REF HX NR WO.2295839, EMER LT BATTERY PACK AT DR 3R REPLACED AND INSTALLATION TEST RESULT NORMAL IAW AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (DOOR 2R) · airframe 84,527 hrs · 10,610 cycles

EMER LT BATTERY PACK AT DR 2R FOUND CAPACITY FUNCTION CHECK FAIL REF HX NR WO.2295789, ORIG BY V920586 EMER LT BATTERY PACK AT DR 2R REPLACED AND INSTALLATION TEST RESULT NORMAL IAW AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 84,527 hrs · 10,610 cycles

EMER LT BATTERY PACK (M33099) AT DR 2L FOUND CAPACITY FUNCTIONAL CHECK FAIL REF HX NR WO.2295826, ORIG BY V920586 EMER LT BATTERY PACK AT DR 2L REPLACED AND INSTALLATION TEST RESULT NORMAL IAW AMM 33-51-06 (M33099)

Part: LIGHT — INOPERATIVE (SEAT 20G,21G,22G) · airframe 83,783 hrs · 10,426 cycles

FOUND PAX SEAT 20G 21G 22G 32G FLOOR PROXIMITY LIGHT LAMPS INOP - ORIGINATED BY EMP V916788 ON HAECO NR 9461070, SUPPORT TASK. PERFORMED BY EMP V903179, IDT BY V903189. REPLACED THE PAX SEAT 20G 21G 22G 32G FLOOR PROXIMITY LIGHT ASSY AND PERFORMED OP TEST FOUND NORMAL. REFER AMM 33-51-05-960-802 REV 98. IDT BY V903189.

Part: BATTERY — FAILED (R3 DOOR) · airframe 83,783 hrs · 10,426 cycles

FOUND R3 DOOR SECTIONS OF EMERGENCY LIGHTS INOP - ORIGINATED BY EMP V916788 ON HAECO NR 9461070, SUPPORT TASK. PERFORMED BY EMP V903179, IDT BY V903189. PERFORMED T/S FOUND M3 3405 POWER SUPPLY BATTERY PACK FAILED, REPLACED THE BATTERY PACK AND PERFORMED OP TEST FOUND NORMAL, REFER AMM 33-51-06-960-802 REV 98. IDT BY V903189.

Part: BATTERY — FAILED (R2 DOOR) · airframe 83,783 hrs · 10,426 cycles

FOUND R2 DOOR SECTIONS OF EMERGENCY LIGHTS INOP - ORIGINATED BY EMP V916788 ON HAECO NR 9461070, SUPPORT TASK. PERFORMED BY EMP V903179, IDT BY V903189. PERFORMED T/S FOUND M3 3098 POWER SUPPLY BATTERY PACK FAILED, REPLACED THE BATTERY PACK AND PERFORMED OP TEST FOUND NORMAL, REFER AMM 33-51-06-960-802 REV 98. IDT BY V903189.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,664 hrs · 9,631 cycles

B777-33-3-7031 - SEAT 47-53 - AND AFT GALLY FWD PARTITION AREA EMER LT FOUND DIM. EMER LT POWER SUPPLY BATTERY REPLACED AND TEST NORMAL AS PER AMM 33-51-06.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 80,664 hrs · 9,631 cycles

B777-33-3-7031 - SEAT 27-36 AND CREW REST DOORWAY AREA EMER LT FOUND DIM - REFER TRANSFER NON-ROUTINE ZHA501993 AND ORIGINATED BY EMP V935378 M33404 EMER LT POWER SUPPLY BATTERY REPLACED AND TEST NORMAL AS PER AMM 33-51-06 ADD EMP:V896992 IDT INSPECTED OKAY BY HX 195273 ADD EMP:V896958

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 79,505 hrs · 9,329 cycles

R4 EMERGENCY BATTERY FAILED OPS CHECK ON T/C NO. 97-1011-1-6904 REMOVED AND REPLACED R4 BATTERY PACK P/N AD-D717-01-1 S/N 180833 REF 777 MM 33-51-06-960-802. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EXTERIOR LIGHT) · airframe 79,489 hrs · 9,326 cycles

B777-33-3-7030 L/H NO.3 DOOR EXTERIOR EMER LT FOUND UNILLUMINATE REFER NR LP 9130048 L/H NO.3 DOOR EXTERIOR EMER LT REPLACED AND OP TEST RESULT NORMAL AS PER AMM 33-51-04 ADD EMP:V927706 IDT BY HX 195306

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 79,489 hrs · 9,326 cycles

B777-33-3-7030 R/H NO.4 DOOR EXTERIOR EMER LT FOUND ILLUMINTED REFER NR LP 9130049 R/H NO.4 DOOR EXTERIOR EMER LT REPLACED AND OP TEST RESULT NORMAL AS PER AMM 33-51-04

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,489 hrs · 9,326 cycles

SUPPORT TASK DR R3 EMERGENCY LT PWR SUPPLY (M33401) INOP REFER NR LP 9131097 DR R3 EMERGENCY LT PWR SUPPLY (M33401) REPLACED AND OP TEST FOUND NORMAL AS PER AMM 33-51-06 ADD EMP:V896992

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,489 hrs · 9,326 cycles

SUPPORT TASK LLAR EMER LT FOUMS UNILLUMINATED REFER NR LP 9131122 LLAR EMER LT CHARGER REPLACED AND OP TEST RESULT NORMAL AS PER AMM 33-29-01

Part: ENGINE — SURGES (NR 2) · airframe 76,682 hrs · 8,987 cycles

2822-2 ESN 222036 EXPERIENCED SURGE DURING TAKEOFF RUN AT 60KTS. ON RETURN TO GATE GRUMM REPORTED METAL IN TAILPUPE. ACCOMPLISH BORESCOPE INSPECT HPC STG 5,6,9,AND HPT STG 1 AND 2. REF AMM72-00-00 P6XX CFG2. IF SIGNS OF IMPACT, INSPECT OTHER STAGES. PERFORMED HPC BORESCOPE INSPECTION IAW AMM72-00-00-290-833-N02, FOUND ALL 5TH AND 6TH STAGE BLADES DAMAGED BEYOND AMM LIMITS, SIGNS OF INGESTION. ALSO, INSPECTED 1ST STAGE LPC AND FOUND SEVERAL BLADE TIPS BENT INWARD AND OUTWARD. INSPECTED FAN BLADES, NO VISUALLY PERCEIVED DAMAGE FOUND. ENGINE MUST BE TOMC AND ESC GROUP. REPLACED BEFORE FURTHER FLIGHT.

Part: ENGINE — SURGES (NR 1) · airframe 75,693 hrs · 8,875 cycles

E1 SURGE, DATA PRINT AND EMAIL. E1 SN 222210 (TSI=380 HRS). HAD A SILENT SURGE REPORTED BY AHM IN CRZ T/803-29 IAD-NRT. PLEASE SEND DATA FOR ENGINEERING REVIEW (1) REF AMM 31-61-00 PG201. ACCESS MCDU MAINT PGS CHAP71 PER. EPCS PG 1 & 2, AND L ENG EXCD. FIND ALL AUTO & MAN EVENT SNAP SHOTS REGARDING SURGE, PRESS "SEND" TO ACARS AND PRINT. (2) FROM MAT MAIN MENU, GO TO COND MONITORING REPORT "INFLIGHT SHUTDOWN" REPORT. PRINT 9 PGS. (IFSD REPORT TRIGGERED BY CMC SURGE MSG) (3) WRITE ACFT NUMBER ON PRINTED PAGES AND E-MAIL TO [email protected] & [email protected]. THX. WHQLM-EMC ARSHAD. CARRIED BY ELB PERFORMED VISUAL INSPECTION OF THE INLET, EXHAUST AND BLEED PORT PER STEP C12&13 OF FIM 71-05-00-810-819-N00. ADDITIONALLY CHKD CONNECTIONS OF PB LINES AND IP CHK VLV. NO DEFECT FOUND. INBD PILOT HAS ALEADY REPORTED MCDU MAINT. PGS CH71 VIA ACARS. SENT CONF SENT COND. MONITORING REPORT FOR IFSD BY E-MAIL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 73,290 hrs · 8,597 cycles

M/D LLAR EMER LT BATTERY 1EA FOUND LOW CAPACITY. REPLACED THE CABIN LLAR EMERGENCY LT PWR PACK BATTERY AND OP TEST CARRIED OUT, FOUND NORMAL AS PER AMM 33-51-06-960-802 REV 83.

Part: LIGHT — BROKEN (CABIN) · airframe 73,290 hrs · 8,597 cycles

M/D A4 GALLEY LT 1EA LWR EMER LT FOUND BROKEN. REPLACED THE CABIN A4 GALLEY LT SIDE 1EA LWR EMERGENCY LIGHT AND OP TEST CARRIED OUT, FOUND NORMAL AS PER AMM 33-51-05-960-802 REV 83.

Part: LIGHT — BROKEN (CABIN) · airframe 73,290 hrs · 8,597 cycles

M/D MID GALLEY, 5EA LWR EMER LIGHTS FOUND BROKEN. REPLACED THE CABIN MID GALLEY 5EA LWR EMERGENCY LIGHTS AND OP TEST CARRIED OUT, FOUND NORMAL AS PER AMM 33-51-05-960-802 REV 83.

Part: LIGHT — BROKEN (CABIN) · airframe 73,290 hrs · 8,597 cycles

M/D A & B ZONE CTR PARTITION, 4EA LWR EMER LIGHTS FOUND BROKEN. REPLACED THE CABIN ZONE A & B CTR PARTITION TOTAL 4EA LOWER EMERGENCY LT AND OP TEST CARRIED OUT, FOUND NORMAL AS PER AMM 33 -51-05-960-802 REV 83.

Part: BATTERY — LOW (CABIN) · airframe 73,290 hrs · 8,597 cycles

FOUND CABIN RT NR 3 DOOR AREA EMERGENCY LT PWR SUPPLY M33401 LOW CAPACITY. REPLACED THE CABIN R3 DOOR AREA EMERGENCY PWR SUPPLY BATTERY M33401 AND OP TEST CARRIED OUT, FOUND NORMAL AS PER AMM 33-51-06 -960-802 REV 83.

Part: HOUSING — BROKEN (CABIN) · airframe 73,290 hrs · 8,597 cycles

M/D L1 & L4 DOOR AREA 2EA EXIT IDENT'S HOUSING FOUND BROKEN. REPLACED THE CABIN L1 FWD & L4 DOOR AFTER AREA 2EA EXIT INDICATORS AND OP TEST CARRIED OUT, FOUND NORMAL AS PER AMM 33-51-01-960-802 REV 83.

Part: BATTERY — LOW (CABIN) · airframe 73,290 hrs · 8,597 cycles

FOUND CABIN LT NR 3 DOOR AREA EMEERGENCY PWR SUPPLY M33400 LOW CAPACITY. REPLACED THE CABIN L3 DOOR AREA EMERGENCY PWR SUPPLY BATTERY M33400 AND OP TEST CARRIED OUT, FOUND NORMAL AS PER AMM 33-51-06 -960-802 REV 83.

Part: LIGHT — BROKEN (CABIN) · airframe 73,290 hrs · 8,597 cycles

M/D L2 FWD & AFT L3 DOOR FWD EXIT IDENT 3EA FOUND BROKEN. REPLACED THE DOOR L2 FWD & AFT L3 DOOR FWD EXIT INDICATOR LIGHT AND OP TEST CARRIED OUT, FOUND NORMAL AS PER AMM 33-51-01-960- 802 REV 83.

Part: BATTERY PACK — LOW (CABIN) · airframe 73,290 hrs · 8,597 cycles

FOUND CABIN LT NR 3 DOOR AREA EMERGENCY POWER SUPPLY M33406 LOW CAPACITY. REPLACED THE CABIN L3 DOOR AREA EMERGENCY POWER SUPPLY BATTERY M33406 AND OP TEST CARRIED OUT, FOUND NORMAL AS PER AMM 33-51-06 -960-802 REV 83.

Part: BATTERY — LOW (CABIN) · airframe 73,290 hrs · 8,597 cycles

FOUND CABIN RT NR 4 DOOR AREA EMERGENCY LT PWR SUPPLY M33409 LOW CAPACITY. REPLACED THE CABIN R4 DOOR AREA EMERGENCY LIGHT PWR SUPPLY BATTERY M33409 AND OP TEST CARRIED OUT, FOUND NORMAL AS PER AMM 33-51-06 -960-802 REV 83.

Part: LENS — MISSING (CABIN) · airframe 73,290 hrs · 8,597 cycles

M/D DOOR 1 CTR PARTITION 1EA CTR LWR EMER LIGHT LENS FOUND MISSING. REPLACED THE CABIN DOOR 1 CTR PARTITION 1EA CTR LWR EMERGENCY LT AND OP TEST CARRIED OUT, FOUND NORMAL AS PER AMM 33-51-05-960- 802 REV 83.

Part: BATTERY PACK — LOW (CABIN) · airframe 73,290 hrs · 8,597 cycles

FOUND CABIN RT NR 1 DOOR AREA EMERGENCY LT PWR SUPPLY M33094 LOW CAPACITY. REPLACED THE CABIN RT NR1 DOOR AREA EMERGENCY LIGHT PWR SUPPLY BATTERY M33094 AND OP TEST CARRIED OUT, FOUND NORMAL AS PER AMM 33-51-06-960-802 REV 83.

Part: BATTERY — LOW (CABIN) · airframe 73,290 hrs · 8,597 cycles

FOUND CABIN LT NR1 DOOR AREA EMERGENCY LT POWER SUPPLY M33093 LOW CAPACITY. REPLACED THE CABIN L1 DOOR AREA EMERGENCY LIGHT POWER SUPPLY BATTERY M33093 AND OP TEST CARRIED OUT, FOUND NORMAL AS PER AMM 33-51-06-960-802 REV 83.

Part: LIGHT — BROKEN (CABIN) · airframe 71,102 hrs · 8,361 cycles

AFT GALLEY RT AISLE WALL EEL LIGHT AND EDGE TRIM BROKEN. REPLACED EEL LIGHT AND TRIM.

Part: LIGHT — ODOR (SEAT 23HJK) · airframe 69,704 hrs · 8,202 cycles

ROW 23HJK ELECTRICAL ODOR. CEILING LIGHTS AT 25 HJK INOPERATIVE. REMOVED AND REPLACED CEILING LIGHT. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 68,062 hrs · 8,006 cycles

ZONE ''C'' DOOR 3 LT CEILING AREA EMERGENCY LT INOP. M33405 BATTERY REPLACED AND EMERGENCY LT SYSTEM FUNCTIONAL TEST FOUND ''C'' ZONE DOOR 3 LT CEILING AREA EMERGENCY LT ''NORMAL'' REF AMM 33-51-00-710-801 REV 79.

Part: LIGHT — BROKEN (CABIN) · airframe 68,062 hrs · 8,006 cycles

PARTITION 4EA EMERGENCY LIGHT FOUND BROKEN. PARTITION 4EA EMERGENCY LIGHT REPLACED & FUNCTIONAL TEST C/O FOUND NORMAL REF AMM 33-51-00-710-801 REV 79.

Part: LIGHT — BROKEN (CABIN) · airframe 68,062 hrs · 8,006 cycles

M/D GALLEY 2EA EMERGENCY LIGHT FOUND BROKEN. M/D GALLEY 2EA EMERGENCY LIGHT REPLACED & FUNCTIONAL TEST C/O FOUND NORMAL REF AMM 33-51-00-710-801 REV 79.

Part: LIGHT — INOPERATIVE (SEAT 36D) · airframe 68,062 hrs · 8,006 cycles

SEAT 36D EMERGENCY LIGHT INOPERATIVE. SEAT 36D EMERGENCY LIGHT REPLACED & FUNCTIONAL TESTED GOOD IAW AMM 33-51-00-710-801, REV.79.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,003 hrs · 7,540 cycles

EXIT PATH LIGHT OUT AT 20D. REPLACED EMER EXIT PATH LIGHT LENS AT 20D IAW AMM 33-51-05. ALL OPERATIONS NOW NORMAL.

Part: ENGINE — OVERTEMP (NR 1) · airframe 60,909 hrs · 7,209 cycles

VIA ACARS ENG 1 EGT LIMIT EXCEEDED ON TAKEOFF, RED BOX AROUND EICAS ENG1 EGT. FOUND PEAK EGT OF 699 DEGREES, OVER TAKEOFF EGT LIMIT OF 675 DEGREES FOR 14.4 SECONDS, AT OR ABOVE 695 DEGREES FOR 2.8 SECONDS. ENG REPLACED IAW REQUIREMENT.

Part: PANEL — DAMAGED (RT WING) · airframe 55,434 hrs · 6,627 cycles

DAMAGE REPORTED TO RT WING TE PANEL 651AB. IAW SRM57-51-01-101X PANEL REPAIRED IAW SHEET METAL SHOP & INSTALLED PANEL.

Part: PANEL — DENTED (RT WING) · airframe 55,426 hrs · 6,626 cycles

DAMAGE REPORTED TO RT WING TE PANEL 651AB. INSPECTED PANEL 651AB & FOUND TWO EACH DENTS OF 8 X 3 & 6 X 3 INCHES. PERFORMED VISUAL INSPECTION FOR CRACKS & DELAMINATION, ALL OK. PANEL REMOVED FOR REPAIR. PANEL IN SHEET METAL SHOP.

Part: CONNECTOR — DIRTY (RT ENGINE) · airframe 54,642 hrs · 6,542 cycles

RIGHT ENG WOULD NOT SHUT DOWN ON ARRIVAL. MX MG 73-60212 NOT ACTIVE. ACCOMPLISHED FIM TASK 73-22-802 IAW WD 76-21-71. WHILE ACCOMPLISHING WIRING CHECKS FOUND OPEN LINE DUE HIGH RESISTANCE BETWEEN PLUGS D71024P & DM76001C PINS 3 & 4 TO 1 & 14. DISCONNECTED & CLEANED CONNECTOR D71074P J PINS 1 & 2. RECONNECTED 71024P & D71074P & NOW 28VDC BETWEEN PINS 1 & 14 ON DM76001C. RECONNECTED DM761001C & ACCOMPLISH ENG TEST 3 & SHUTDOWN NORMAL. TO CONFIRM CONNECTORS THAT WERE DISCONNECTED & RECONNECTED ARE WD 76-21-71 D71024P, D71074P & DM76001C.

Part: BLANKET — TORN (RT NACELLE) · airframe 53,835 hrs · 6,455 cycles

RT NACELLE STRUT HEAT BLANKET TORN ABOVE NR 1 HEAT SHIELD. EVIDENCE OF HEAT DAMAGE TO STRUT STRUCTURE. REPLACED HEAT BLANKET IAW AMM 54-54-01. REPLACED LOWER SPAR WEB STRUCTURE IAW SRM 51-40-0 2. REPLACED CHORD, FRAME, & BULKHEAD IAW SRM 51-20-01 & DRAWING 313W3810.

Part: RFU — FAULTY (SATCOM) · airframe 53,404 hrs · 6,403 cycles

SATCOM SYS PASSES FIM TEST BUT SHOWS A RFU INTERNAL FAULT. REPLACED RFU, CHECKED OKAY.

Part: VALVE — FAILED (AC BAY) · airframe 52,569 hrs · 6,313 cycles

PACK MODE RT PACK AIR CYCLE MACHINE HAS FAILED, OR RT ECONOMY COOLING VLV FAILED OPEN, OR BOTH RT CONDENSER INLET TEMP SENSORS FAILED. RT PACK IS OPERATING IN A NON NORMAL MODE HEAT EXCHANGER ONLY COOLING MODE. REPLACED RT PACK LOW LIMIT VLV IAW AMM. DUE TO MATERIAL INTERROGATION MESSAGE. OPERATED MAINT GROUND SYSTEM TEST AIR ON, PASSED ALL PARAMETERS RT PACK CHECKED NORMAL

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 52,569 hrs · 6,313 cycles

CABIN ALTITUDE AUTO LOSS OF INPUT FROM, OR FAILURE OF BOTH ASCPC'S, OR LOSS OF INPUT OR FAILURE OF BOTH OFV'S, OR A COMBINATION OF THE ABOVE THAT RESULTS IN LOSS OF COMPLETE AUTOMATIC CONTROL, OR MANUAL MODE SELECTED FOR BOTH OFV'S. CAUTION IAW PTT SEQ 5692013 OUTFLOW VLV FWD LT IAW AMM 21-31-03, OPERATIONS CHECKED GOOD, NO FAULTS NOTED.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 52,563 hrs · 6,311 cycles

BLEED PRSOV LEFT MESSAGE DUE TO CHRONIC BLEED PRSOV LEFT MESSAGES, PLEASE PERFORM A PNEUMATIC SYSTEM HEALTH CHECK IAW SERVICE TIP 36-UA1 FOR PRSOV MUSCLE LINE FROM PRSOV TO PRSOV CONT. R & R PRSOV IAW AMM 36-11-09. ALSO, REPLACED PRSOV CONTROLLER IAW 36-11-18-401 PRECAUTIONARY.

Part: AIR FILTER — CLOGGED (CABIN) · airframe 52,422 hrs · 6,295 cycles

RECIRCULATING MESSAGE ON EICAS ALL CABIN RECIRCULATING FILTERS MUST BE REPLACED. ONE IN MID GALLEY CEILING FOUND COMPLETELY PLUGGED WITH INSULATION MATERIAL, REPLACED UPPER RECIRCULATING AIR FILTERS. LOWER RECIRCULATING FILTERS STILL NEED TO BE REPLACED. REPLACED ALL 4 LOWER RECIRCULATING AIR FILTERS.

Part: AIR FILTER — DIRTY (CABIN) · airframe 52,422 hrs · 6,295 cycles

RECIRCULATING MESSAGE ON EICAS. REPLACED UPPER RECIRCULATING AIR FILTERS.

Part: SEAL — DAMAGED (LIFE VEST) · airframe 52,261 hrs · 6,275 cycles

SEAT 2A LIFE VEST COMPARTMENT SEAL DAMAGED. REPLACED SEAL.

Part: SEAL — DAMAGED (LIFE VEST) · airframe 52,261 hrs · 6,275 cycles

SEAT 1C LIFE VEST COMPARTMENT SEAL IS DAMAGED. REPLACED SEAL.

Part: SHUTOFF VALVE — FAULTY (RT A/C PACK) · airframe 51,650 hrs · 6,201 cycles

RT A/C PACK LOWER FLOW CONTROL STATUS MESSAGE. REPLACED VALVE REF AMM, NO HELP ITEM DF.

Part: CONTROL VALVE — WARNING MESSAGE (A/C PACK) · airframe 51,650 hrs · 6,201 cycles

PACK FCV LOWER RIGHT STATUS MSG.

Part: WARNING MESSAGE — ILLUMINATED · airframe 51,010 hrs · 6,122 cycles

BLEED OFF ENG RT EICAS. MX MESSAGE 36-10350. HPSOV MOVES FREELY. CLEANED HPFAC CONNECTOR. MESSAGE SHOWING NOT ACTIVE. MX MESSAGE 36 -10360. TROUBLESHOT IAW FIM 36-11, TASK 804. AFTER GROUND TEST 36 AIR SUPPLY CNTL SYS, SYS TEST, RT AIR SUPPLY CNTL SYS. MESSAGE NOT ACTIVE NOW. NO FURTHER MESSAGE. NO HISTORY.

Part: FMU — FAULTY (NR 2 ENGINE) · airframe 50,423 hrs · 6,052 cycles

AFTER ENG SHUTDOWN EICAS MESSAGE FUEL VALVE RT SHOWED. REPLACED RT ENG FMU IAW AMM.

Part: CONTROL VALVE — FAILED (LT A/C PACK) · airframe 49,845 hrs · 5,989 cycles

EICAS STATUS MESSAGE FOR LEFT A/C PACK FLOW CONTROL VALVE. REPLACED LEFT FLOW CONTROL VALVE PER MM. PERFORMED GROUND TEST, MESSAGE WENT AWAY AND TEST PASSED.

Part: WIRE — DAMAGED (AC SYSTEM) · airframe 49,816 hrs · 5,986 cycles

MSG 21-24001 LATCHED IN CRUISE. REPLACED LOWER FLOW CONTROL VALVE PER MM 21-51-02 PG 401 AND LEFT CTC PER MM 21-61-01 PG 401, CABIN TEMP CONT SYSTEM AIR ON TEST FAILED WITH MSG 21-24001, 21-23082 AND 21-23070. STILL STATUS MSG 'PACK FCV LWR L' SHOWS. REMOVED CTC WRANG OUT WIRES TO CTC TORQUE MOTOR. FOUND WIRING EXPOSED FOR RETURN AND SUPPLY AND TWISTED TOGETHER. ISOLATED WIRES UNLATCHED FAULT. PASSED AIR ON TEST NEED TO REPAIR WIRES AND RUN TEST.

Part: CONTROL VALVE — FAULTY (NR 2) · airframe 49,803 hrs · 5,985 cycles

NR 1 PACK OVERHEAT AT OUTLET OR LEFT PACK COMPRESSOR OUTLET OR LEFT PACK FLOW CONTROL VALVES (FCV) ARE CLOSED DUE TO FCVS FAILED CLOSED, FCVS LATCHED CLOSED BY CABIN TEMP CONTROLLER (CTC) BECAUSE OF FAULT, OVERHEAT, OR PACK CONTROL SWITCH COMMANDED OFF, OR NO PNEUMATIC AIR AVAILABLE TO PACK. CREW COMMENTS: OCCURRED AFTER STATUS MSGPACK FCV LWR L SAME AS INBOUND TO PEK PROBLEM MSG-2125502 INACTV ER INTER MSG-2124001 LATCHD CL MODE. RPLC'D LEFT LOWER FLOW CONTROL AND SHUT OFF VALVE IAW MM. ALSO REPLACED COMPRESSOR DISCHARGE TEMP SENSOR IAW MM 21-52-41. DUE TO FIM 21-51 TASK 806. SYSTEM TESTED OKAY.

Part: SHUTOFF VALVE — FAULTY (CREW REST) · airframe 49,706 hrs · 5,975 cycles

CREW REPORTS LOWER LOBE CREW REST AREA AIR FLOW CHIME SOUNDING CONTINOUSLY, UNABLE TO RESET. LOWER LOBE CREW REST SOV LOCKED OUT PER MEL. POSSIBLE HOT AIR TYPE ODOR IN AREA OF DOOR 3R. RECIRC FANS TURNED OFF & ODOR DID DISSIPATE SLIGHTLY. REPLACED RELAY K21011, PER FORMED TEST AND SHUTOFF VALVE SHOWS IN WRONG POSITION. REPLACED LLAR SHUTOFF VALVE PER MM 21-29-11, OPS CHECKS NORMAL AND MESSAGE CLEARED AND TEST PASS. ADJUSTED SWITCH S21291 ALSO. 041384DOOR SWITCH WAS NOT CONTACTING DOOR, AFTER ADJUSTMENT NOW ACTUATES NORMALLY. RAN ENTERTAINMENT SYSTEM, PACKS, DOOR HEATERS AND PACKS AND NO ODORS DETECTED. LOWER REST AREA AIRFLOW, OPS CHECKS NORMAL AND ALL WARNINGS RESET. REF WDM 21-29-11, FIM 21-29 TASK 802, 21-00 TASK 808.21-00 TASK 807-808. LOWERED CEILING PANELS ABOVE DOOR 3RT AND LEFT AND IN CENTER ISLE AND NO ODOR OR DEFECTS NOTED.

Part: SHUTOFF VALVE — FAULTY (CREW REST) · airframe 49,559 hrs · 5,961 cycles

CREW REST LOWER LOWER LOBE ATTENDANT REST SHUTOFF VALVE IS NOT IN THE COMMANDED POSITION. REPLACED SHUTOFF VALVE PER MM, OPS CHECKED GOOD AND NO LEAKS. ALL MESSAGES CLEAR AND TEST PASSED.

Part: SEAL DEPRESSOR — DAMAGED (CARGO DOOR) · airframe 49,446 hrs · 5,948 cycles

AFT CARGO DOOR SEAL DEPRESSOR IS DAMAGED IN THE AFT UPPER CORNER. REPLACED DAMAGED DEPRESSOR SEAL SECTION REF TO IPC 52-37-51-005 DETAIL C ITEMS 440 AND 460. REPAIR COMPLIES WITH SRM 53-00-15 PG 201.

Part: IDG — FAILED (RIGHT) · airframe 48,969 hrs · 5,900 cycles

RIGHT GENERATOR DRIVE DISPLAYED AFTER TAKEOFF. DISCONNECTED IDG PER FM PROCEDURES, APU ON AND POWERING BUSSES. REPLACED RT IDG PER MM, CHECKED NORMAL.

Part: MODULE — FAULTY (RIGHT) · airframe 48,917 hrs · 5,894 cycles

FMC R RIGHT FLIGHT MANAGEMENT COMPUTER (FMC) FAULT. FAILURE IN GUIDANCE, NAVIGATION, PERFORMANCE, OR OTHER RELATED FMC FUNCTION. STATUS MSG-3151024 LATCHD DC HARD. REPLACED CMF CORE MODULE PROCESSOR. INSTALL NEW DATA BASE UPDATES, OP CHECKS GOOD.

Part: BUTTON — MISSING (CONTROL PANEL) · airframe 48,801 hrs · 5,884 cycles

RED BUTTON MISSING ON FIRE CONTROL PANEL. REPLACED RED BUTTON.

Part: ANTI-ICE VALVE — FAILED (LT ENGINE) · airframe 48,801 hrs · 5,884 cycles

LEFT ENGINE ANTI-ICE VALVE FAILED IN CLOSED POSITION. VALVE REPLACED. PERFORMED TEST PER TASK 30-21-00-730-806-003. TESTED GOOD.

Part: FIRE DETECTOR — FAULTY (RT ENGINE) · airframe 48,195 hrs · 5,817 cycles

ON ARRIVAL OVERHEAT CIRCUIT R1 STATUS MESSAGE. REPLACED BOTH RIGHT ENG LOWER AFT FIRE DET ELEMENTS, OPS CK NORMAL.

Part: LUG — BROKEN (FIRE LOOP) · airframe 48,195 hrs · 5,817 cycles

LUG TO LWR AFT FIRE LOOP BROKEN ON O/B SIDE OF NR 2 ENGINE. REPLACED BOTH LOWER AFT ENGINE FIRE DETECTORS, OPS CHECKED NORMAL.

Part: FIRE LOOP — INOPERATIVE (RT ENGINE) · airframe 48,195 hrs · 5,817 cycles

ON ARRIVAL FIRE LOOP 1 ENGINE R STATUS MESSAGE CHECK MAT ACTIVE. DF 0606 RIGHT ENGINE FIRE LOOP 1 INOPERATIVE. COMPLIED WITH MEL REQUIREMENTS. REPLACED BOTH RIGHT ENGINE LOWER AFT FIRE DETECTIVE ELEMENTS, OPS CHECKED NORMAL PER MM.

Part: PRECOOLER — BLOWN (NR 1 ENGINE) · airframe 48,051 hrs · 5,801 cycles

FOUND NR 1 ENGINE PRECOOLER BLOWN. IT DAMAGED MULTIPLE HEAT BLANKETS ON SAME ENGINE REVERSER. NR 1 ENGINE PRECOOLER LEAKING. REMOVED NR 1 ENGINE PRECOOLER PER MM. NEW PRECOOLER IN AREA. REPLACED PRECOOLER ASSY.

Part: LIGHT — IMPROPER PART (CABIN) · airframe 48,027 hrs · 5,799 cycles

PER FCD#3330-01031 FOUND INCORRECT HALOGEN BULBS P/N 9203 INSTALLED AT ALL 4 POSITIONS AND MAINT TEXT: MANDATORY PLACARDS MISSING ABOVE LLAR STA1466 AND STA 1522. ACP FCD 330-01031 PER EG 7521. RELAMPED BULBS AND ADDED PLACARDS.

Part: LAMP — INOPERATIVE (CARGO BAY) · airframe 48,027 hrs · 5,799 cycles

FWD LIGHTS IN AFT CARGO CMPT ABOVE LLAR ARE INOP. FOUND 4 EA LIGHTS OUT DURING COMPLETION OF EG7521 FCD 3330-01031 INOPED PER MEL. REPLACED LAMPS, OPS GOOD.

Part: VANE — CRACKED (NR 1 ENGINE) · airframe 47,749 hrs · 5,766 cycles

NR 1 ENGINE HAS FOD DAMAGE AT 9TH STAGE LPT VANES. FOUR VANES WITH CRACKS BETWEEN .125 INCH TO 500 INCH LONG IN AREAS B AND C. FOUR WITH PLATFORM MAT'L MISSING (AREA D), AND THREE WITH THE MAT'L MISSING LARGEST OF WHICH IS .500 LG X .375 DEEP PER AMM. NO CRACKS OR DAMAGE IN (AREA 'D') ALLOWED. REMOVED ENGINE.

Part: UNKNOWN — MALFUNCTIONED (FLAPERON) · airframe 47,531 hrs · 5,736 cycles

FLAPERON ACT STATUS: MSG 27-10302 ACTIVE & LATCHED. ACP'D FIM 27-11 TASK 816 STEP C. FOUND WIRE CHECKS GOOD. REF STEP C.(3), REPLACED ACE-L2 (M2712 2) PER MM27-02-02. LRU REPLACEMENT TEST CHECKS OK BUT FLAPERON POSITION SYSTEM TEST FAILS WITH MSG 27-16039, FLAPERON PCU RIB RAM TRANSDUCER POS SIGNAL OUT OF RANGE. REF FIM 27-11 TASK 878.

Part: PCU — FAULTY (FLAPERON) · airframe 47,531 hrs · 5,736 cycles

FLAPERON ACTUATOR STATUS MSG-REPEAT. REPLACE RIGHT INBOARD FLAPERON PCU PER AMM. SYSTEM OPS CHECK NORMAL.

Part: VALVE — FAULTY (LT ENGINE) · airframe 47,158 hrs · 5,696 cycles

LEFT ENGINE BLEED FAN AIR MODULATING VALVE (FAMV) FAILED TO OPEN OR CLOSED OR LEFT AIR SUPPLY AND CABIN PRESSURE CONTROLLER FAILURE. STATUS MSG-3610180 LATCHED AP MODE. REPLACED NR 1 ENGINE FAN AIR VALVE PER MM. PERFORMED OPERATIONAL TEST ON MAT AND RAN ENGINE. OPERATIONAL TEST GOOD.

Part: VALVE — FAULTED (NR 1) · airframe 46,860 hrs · 5,662 cycles

BLEED FAMV LT ON STATUS PAGE. TRIED RUNNING NR 1 ENG WITH NO HELP. REMOVED AND REPLACED NR 1 ENG FAMV, OP CHECKED PER MM

Part: SDU — FAULTY (SATCOM) · airframe 46,511 hrs · 5,624 cycles

SATCOM HIGH GAIN FAILED. SATCOM SYSTEM BECAME INOPERATIVE LOW AND HIGH GAIN REPLACED SDU PER AMM.

Part: VALVE — FAILED (BLEED SYSTEM) · airframe 46,446 hrs · 5,616 cycles

BLEED FAN AIR MODULATION RIGHT EICAS MESSAGE DISPLAYED. MSG02- LATCHED FAN AIR MODULATING VALVE (RIGHT) RVDT CIRCUIT IS OPEN OR SHORTED. MSG-3610532 LATCHD QT MSG-3610532 LATCHED QT. REPLACED FAMV PER MM.

Part: MONITOR — FAILED (SEAT 21H) · airframe 45,754 hrs · 5,535 cycles

SEAT MONITOR AT 21H OVERHEATED AND HAD ELECTRICAL ODOR. CREW TURNED OFF SWITCH UNDER SEAT TO TURN OFF POWER TO 21HJ. VIDEO MONITOR AT 21H. REMOVED AND REPLACED. FUNCTION TESTED AND OPERATION IS SATISFACTORY.

Part: MODULE — MALFUNCTIONED (WX RADAR SYS) · airframe 45,431 hrs · 5,496 cycles

WEATHER RADAR HAS HEAVY STROBE AT AN 8 MILE ARC. REPLACED LEFT AIMS COMM 2 MODULE. WEATHER RADAR SYSTEM OP'S CHECKED GOOD.

Part: PEEP SIGHT — MISINSTALLED (COCKPIT DOOR) · airframe 45,378 hrs · 5,488 cycles

COCKPIT DOOR PEEP HOLE APPEARS TO BE INSTALLED IN REVERSE. REPLACED FLT DECK DOOR PEEK HOLE.

Part: LIGHT — BROKEN (CABIN) · airframe 45,326 hrs · 5,484 cycles

DOOR 4LT EMERGENCY LIGHT ASSY BROKEN. REPLACED DOOR 4LT UPPER EMERGENCY EXIT LIGHT ASSY, OP CHECKS GOOD ON GROUND.

Part: DATALINK — FAULTED (SATCOM) · airframe 44,839 hrs · 5,427 cycles

SATCOM SYSTEM FAILS OR NO BUSS ACTIVITY. ADVISORY MESSAGE 2368893 ACTIVE ES HARD. REPLACED SATCOM DATA UNIT PCN 583-9200 PER MM, OP CHECKED FAIL DUE TO LNA-DIPLEXER HAS A FAULT MSG23-60091 OR FIM 23-15 TASK 807. COMPLETED STEP C OF THE FIM.

Part: CONTROL PANEL — MALFUNCTIONED (WX RADAR SYSTEM) · airframe 44,823 hrs · 5,423 cycles

WEATHER RADAR SHOWS THIN BAND OF GREEN RETURN AT 6 NM IN WEATHER WITH GAIN IN AUTO WITH REF TO FIM. REPLACED RECEIVER CONTROL PANEL PER MM. RECEIVER SYS TEST NORMAL.

Part: VALVE — FAILED (THRUST REVERSER) · airframe 44,568 hrs · 5,391 cycles

NR 1 ENG T-R SYC LOCK VALVE IS NOT IN COMMANDED POSITION. ITEM HAS MULTIPLE HIT IN FAULT HISTORY. REF J-C2-2020 ITEM 7. RPLC'D SYNC LOCK VALVE PER MM ON NR 1 ENG SYNC LOCK VALVE FAILED OPERATIONAL TEST. FOUND C-B P23 ON PANEL P110 POPPED. RESET C-B. SYNC LOCK LOCK AND T-R ISO VALVE DEACTIVATED REV LOCKOUT PINS INSTALLED. CK CONNECTOR SUSPECT SHORTED. RELAY K78106 DOES NOT BREAK DOWN TO P-N IF NEEDED. NO HISTORY UNTIL SYNC LOCK FAILED ACK JOB CARD. REVERSED MEL AND RAN ENGINE OPERATED REVERSER 4 TIMES CHECKS GOOD.

Part: ACTUATOR — LEAKING (VARIABLE STATOR) · airframe 44,290 hrs · 5,361 cycles

NR 1 ENGINE VARIABLE STATOR VANE ACTUATOR LEAKING FUEL AFTER 5 MIN ENGINE RUN. REPLACED VARIABLE STATOR VANE ACTUATOR.

Part: TERMINAL — INOPERATIVE (COCKPIT) · airframe 42,611 hrs · 5,168 cycles

PAC CT INOP AT DEPARTURE. CT IS INOP. CP IN AFT CAB IN OPERATIONAL. IFE SYSTEM OPERATIONAL. ONLY CREW TERMINAL INOP. REMOVED AND REPLACED CT NO HELP. P/N ON RD-FA1051-01. S/N ON D761024, S/N OFF E688751. FOUND CT OK. PERFORMED ALL TEST, CT WORKING PROPERLY.

Part: SHADE — BROKEN (COCKPIT) · airframe 42,577 hrs · 5,164 cycles

ONE BROKEN WINDOW SHADE ON FLIGHT DECK. REPLACED CRACKED WINDOW SHADE ON CAPTAIN'S SIDE.

Part: SKIN — DAMAGED (BS 157-164) · airframe 40,775 hrs · 4,964 cycles

EXTERNAL FUSELAGE SKIN HAS DAMAGE AT S-45R LAP JOINT, STA 157.00 TO STA 164.00. EXTERNAL FUSELAGE SKIN REPAIRED AT S-45R LAP JOINT, STA 157.00 TO STA 164.00, THIS REPAIR APPROVED FOR STATIC STRENGTH ONLY, PENDING THE RESULTS OF A DAMAGE TOLERANCE ANALYSIS, A NEW 8100-9 MUST BE RECEIVED BY 3-25-2013 (729 DAYS) THAT FINDS COMPLIANCE TO 14 CFR 25.571, OR THE ACFT BECOMES UNSERVICEABLE. CONTACT EG WITH ANY AND ALL DEVIATIONS. REF UA-EVA-80695 A, A NEW 8 100-9 MUST BE RECEIVED BY 3-25-2013, THAT FINDS COMPLIANCE TO 14 CFR 25.571, OR ACFT BECOMES UNSERVICEABLE.

Part: SKIN — DAMAGED (BS 157 S34-39R) · airframe 40,775 hrs · 4,964 cycles

EXT FUSE BS 157 STR 34R & 39R, LIGHTNING STRIKE REPAIR AREA HAS EXCESSIVE MATERIAL REMOVED. ORIG THICKNESS .08 0 INCH THICK, U-S INSP FOUND .0562 INCH REMAIN. MAJOR REPAIR ACCOMPLISHED: UPPER DOUBLER REPAIR DONE, REINSTALLED EQUIPMENT IN E&E COMPARTMENT. REFERENCE UA-EVA-80695-A.

Part: ENGINE — SMOKE (RIGHT) · airframe 40,723 hrs · 4,959 cycles

REPORTED SMOKE FROM RIGHT ENGINE ON TAKEOFF. CREW DID A VISUAL CHECK FROM CABIN - SAW NOTHING. NOTHING ON DOWNLINKS FROM THE ACFT. ALL INDICATORS IN COCKPIT NORMAL. ALL IN AGREEMENT AT THIS TIME TO MONITOR AND CONTINUE ON TO ORD.

Part: DRIVE ASSY — INOPERATIVE (WEATHER RADAR) · airframe 40,380 hrs · 4,907 cycles

WEATHER RADAR FAIL BOTH RADAR SYS INOPERATIVE. REPLACED DRIVE ASSY, BOTH SYS PASS MAT TEST.

Part: MOTOR — MALFUNCTIONED (FUEL BOOST PUMP) · airframe 39,886 hrs · 4,841 cycles

LT WING MAIN AFT BOOST PUMP HSG VALVE PLATE WILL NOT PROPERLY CLOSE DURING PUMP REMOVAL. FUEL PUMP INSTALLED, OPS CKS GOOD, LEAK CKS GOOD, OK FOR SVC IAW MT 28-UA11. REPLACED LT MAIN AFT BOOST PUMP HOUSING. REMOVED AND REPLACED LT AFT BOOST PUMP. OPS CHECK AND LEAK CHECK GOOD.

Part: GUARD — DAMAGED (EMERGENCY LIGHTS) · airframe 39,816 hrs · 4,835 cycles

COCKPIT EMERGENCY LIGHTS SWITCH GUARD TURNS OFF LIGHTS WHEN CLOSED. REPAIRED GUARD AND OPERATES NORMAL.

Part: HEAT EXCHANGER — LEAKING (NR 2 ENGINE) · airframe 38,454 hrs · 4,676 cycles

NR 2 ENG BLEED AIR HEAT EXCHANGER LT LOWER BROKEN, LEAKING HOT BLEED AIR SEVERELY. REPLACED WITH NEW PRECOOLER, NO LEAK FOUND.

Part: CHECK VALVE — FAILED (FUEL BOOST) · airframe 38,087 hrs · 4,637 cycles

IAW CREW, WITH CTR TANK FUEL AND MAIN TANKS EQUAL AT 61.6 ON DEPARTURE,THE LT MAIN TANK FUEL QTY INCREASED TO 64.9 WITH THE RT STILL AT 61.6. FUEL FLOW WAS EVEN FOR ENG 1 AND 2. WITH CTR TANK FUEL USED AND TANK TO ENGINE FUEL FLOW NORMAL AND FUEL BALANCE MAINTAINED. REPLACED LT MAIN FWD AND AFT BOOST PUMP DISCHARGE CHECK VALVES IAW MM. OPS CHECKS GOOD.

Part: RIB — DAMAGED (HYDRAULIC DOOR) · airframe 38,009 hrs · 4,631 cycles

FOUND RIB DAMAGE IN SIDE HYD DOOR AREA. REPAIRED RIB DAMAGE IAW MM.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 38,009 hrs · 4,631 cycles

'C' HYD SYS LEAK. LEAK IN LINES ON C-ADP PUMPS. IDENTIFIED LINES ALL ON AOG. 1 STOCKED (Y6258)1 N-S (S2904). INSTALLED BOTH 3'' HYD LINES ON CTR HYD NR 1 ADP ACCOUNT OF HYD LEAK. BOTH LINES TORQUED. NEED TO SVC CTR SYST. HYD FLUID AND THEN LEAK CHECK LINES. SERVICED CTR SYS AND LEAK CHECKED LINES OK.

Part: PROBE — FAULTY (NR 2 ENGINE) · airframe 37,565 hrs · 4,589 cycles

ACFT RTBL WITH CORRELATED TO ENG CONTROL R. REPLACED INLET P2-T2 PROBE. OPS CHECKS OK.

Part: EEC — MALFUNCTIONED (RT ENGINE) · airframe 37,565 hrs · 4,589 cycles

ENG CONTROL R RT ENG ELEC ENG CONTROL MSG. REPLACED EEC AND TEST IAW MM. RAN ENGINE 2 AT IDLE AFTER EEC REPLACEMENT. GOT CHANNEL A FAULT TCA THERMOCOUPLE OUT OF RANGE REPORTED BY EEC. M73010 ORDERED TO LLCK DROP. INSTALLED NEW TC. TESTS OK.

Part: COUPLER — FAULTY (HF SYSTEM) · airframe 37,312 hrs · 4,569 cycles

HF LT DOES NOT STAY TUNED..TUNES FINE THEN AFTER A FEW XMISSIONS..RETUNES. SUPPLEMENTAL DATA UPDATE REMOVED AND REPLACED L HF COUPLER. NEEDS OP CHK AND COAX CONNECTOR SAFETY WIRING.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 37,153 hrs · 4,551 cycles

SEAT 2F EMERGENCY LIGHTS INOP. REPLACED Y HARNESS IN SEAT. OPS NORMAL.

Part: CONTROL VALVE — FAULTY (A/C PACK) · airframe 37,083 hrs · 4,543 cycles

PACK FCV L ONE (BUT NOT BOTH) OF THE TWO LEFT PACK FLOW CONTROL VALVES (FCV) ARE NOT IN THE COMMANDED POSITION. STATUS MSG-2124001 LATCHD ER MODE MSG-2124001 LATCHD ER MODE. REPLACED LT PACK FCV, OP CKS OKAY.

Part: CONTROLLER — FAULTY (FLOW CONTROL VAL) · airframe 37,082 hrs · 4,542 cycles

LT PACK FLOW CONTROL VALVE (BUT NOT BOTH) OF THE TWO LEFT PACK FLOW CONTROL VALVES ARE NOT IN THE COMMANDED POSITION. STATUS MSG-2124001 LATCHD ER MODE MSG-2124001 LATCHD ER MODE. FOUND CONTROLLER TO BE FAULTY. REPLACED CABIN PRESSURE CONTROLLER. RESET AND OPS GOOD.

Part: CONTROL VALVE — MALFUNCTIONED (A/C PACK FLOW) · airframe 36,993 hrs · 4,530 cycles

PACK FLOW CONTROL VALVE LT ONE (BUT NOT BOTH) OF THE (2) LT PACK FLOW CONTROL VALVES (FCV) ARE NOT IN THE COMMANDED POSITION. STATUS MSG-2124001 LATCHED ER MODE MSG-2124001 LATCHED ER MODE. REPLACED LT LWR FLOW CONTROL VALVE. LT PACK CKS GOOD. NO FAULTS.

Part: VALVE — LEAKING (APU FUEL) · airframe 36,287 hrs · 4,447 cycles

FUEL DRIPPING FROM APU FUEL VENT. FUEL LEAKING FROM FWD DRAIN LINE 50-60 DROPS PER MIN. NO LEAK WITH APU OFF. SUSPECT SURGE CONTROL VALVE ACTUATOR. THE FUEL PUMP SHAFT SEAL, IGV ACTR & SCV HAVE TELL TALE WITNESS DRAINS TO EASILY IDENTIFY A FAULTY UNIT. EACH HAS AN ALLOWABLE 1CC IAW MIN RATE. RPR OR RPL AS NEEDED. VERIFIED SURGE VALVE WAS SOURCE OF FUEL. REPLACED SURGE VALVE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 36,091 hrs · 4,427 cycles

EMERGENCY LIGHT OVHD SWITCH WIRE BROKEN. SWAPPED THE SWITCH GUARD WITH THE "STANDBY PWR" SWITCH ON THE "MAINT ELECTRICAL PWR ONLY" PANEL. NEEDS PCN 585-5361. WHEN USING THE "STANDBY PWR" THE SWITCH NEEDS TO MOVED MANUAL AS THE AUTO POSITIONING FUNCTION OF SWITCH IS INOP.

Part: SATCOM — MALFUNCTIONED (LEFT) · airframe 35,672 hrs · 4,383 cycles

SATCOM SYSTEM SATCOM SYSTEM FAILS OR NO BUS ACTIVITY. STATUS MSG01- ACTIVE CLIMB HARD; SATELLITE DATA UNIT (LEFT) HAS NO OUTPUT ON ANY BUSS. MSG-2368801 ACTIVE CL HARD. FOUND LT SATCOM CB TRIPPED. REPLACED SDU. BITE TEST NORMAL. CONTACTED SAMC 777 CONTROLLER VIA SATCOM, ALL NORMAL.

Part: TURBINE BLADES — DAMAGED (ENGINE) · airframe 35,548 hrs · 4,371 cycles

HPT BLADE BURN. DAMAGE AT HPT TURBINE BLADES 2EA HAVING MATERIAL BURN THROUGH IN AREA B BEYOND LIMITS. R & R ENGINE.

Part: DETECTOR — FAULTY (RIGHT) · airframe 35,412 hrs · 4,353 cycles

ICE DETECTOR, RT ICE DETECTOR FAILURE. GROUND TEST CARRIED OUT. TASK 804 OF AIRFOIL COWL ICE PROTECTION SYS TEST FAILED. RT ICE DETECTOR REPLACED AGAIN. OPS CHECK OK, NO STATUS MSG MAT TEST PASSED.

Part: CIRCUIT CARD — DEFECTIVE (FIRE WARNING) · airframe 33,900 hrs · 4,201 cycles

STATUS MSG B4 START OVHT CIRC R2-R1 FIRE LOOP 2 ENG R. REPLACED RT FIRE DETECTION CARD A10 AND SYSTEM OPS CHECK NORMAL.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 33,632 hrs · 4,172 cycles

FLOOR PROXIMITY EMERGENCY PATH MARKING LIGHT INOP ON CLOSET WALL JUST AFT OF SEAT 9D. ONE EACH LIGHT ONLY INOP. LOCATED ON WALL CORNER JUST AFT OF 9D, RELAMP NO HELP. SUSPECT WIRE ISSUE. TRIED NEW LIGHT ASSY, NO HELP. STILL SUSPECTS WIRING. FOUND CONNECTOR ABOVE CLOSET NOT PROPERLY SEATED. RESEATED CONNECTOR. CKS OKAY.

Part: STARTER — FAILED (APU) · airframe 33,477 hrs · 4,155 cycles

APU CONTROL APUC DETECTED FAILURE OF REDUNDANT CONTROL FUNCTION OR LOSS OF ONE ARINC 629 CHANNEL. STATUS REPLACED APU STARTER. INSTALLATION TEST CHECKS NORMAL. APU OPS NORMAL.

Part: PROCESSOR — MALFUNCTIONED (FUEL QUANTITY) · airframe 32,854 hrs · 4,088 cycles

LEFT WING WOULDN'T ACCEPT FUEL. REPLACED FUEL QUANTITY PROCESSOR UNIT. BOTH SAME SOFTWARE AND TEST CARRIED, BUT NO HELP. FUELED MANUAL. INSTALLED NEW SIGNAL CONDITION ASSEMBLY AND TESTED PER, NO HELP. REPLACED REFUELING PANEL. REFUELING SYSTEM & ALL VALVES OPERATE NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,707 hrs · 3,756 cycles

EMERGENCY LIGHT AT SEAT 18G IS OUT. LAMP FOUND INOP. REPLACED LAMP. OP TESTS OKAY.

Part: GROUND WIRE — SHORTED (CONTROL UNIT) · airframe 28,161 hrs · 3,578 cycles

SPOILERS EICAS MESSAGE DISPLAYED. OUTBOARD SPOILERS INOP. MAINT MESSAGE 27-10500 SPOILER POWER CONTROL UNIT NR 1. AFTER EXTENSIVE TROUBLE SHOOTING AND PART REPLACEMENT. FOUND HIGH RESISTANCE SHORT TO SHIELD-GROUND. REF WDM 27-61-15 PG2 IN AREA AT RECEPTACLE D2139J. REPLACED NR 1 SPOILER CONTROL HARNESS OP CHECKED GOOD. AC OK FOR SERVICE.

Part: MOTOR — MALFUNCTIONED (TE FLAPS) · airframe 26,222 hrs · 3,376 cycles

FLAP-SLAT CONTROL 1 STATUS MESSAGE. SUSPECT ELECTRIC MOTOR. REPLACED ELECTRIC MOTOR. PERFORMED PRIMARY FLAP MAT TEST. TEST PASSED AND MSG CLEARED. IN ADDITION, PERFORMED SECONDARY FLAP TEST PASSED. RAN FLAPS IN ALT 3 TIMES NO FAULTS. ACFT OK FOR SERVICE.

Part: CONNECTOR — UNSECURE (EMERGENCY LGIHT) · airframe 25,029 hrs · 3,245 cycles

EEL AT FIRST CLASS SEAT 3E INOP. SECURED EEL CONNECTOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,029 hrs · 3,245 cycles

EEL AT FIRST CLASS SEAT 2E INOPERATIVE. RECONNECTED

Part: LIGHT — BROKEN (SEAT 1E) · airframe 24,635 hrs · 3,203 cycles

SEAT 1E HAS ONE EEL LIGHT BROKEN.

Part: FIRE WARNING — ILLUMINATED (APU) · airframe 24,505 hrs · 3,187 cycles

DURING PUSH-BACK, CREW HAD AN APU FIRE WARNING INDICATION. 08-31-07 REPLACED APU. ALSO, ACCOMPLISHED APU FIRE EXTINQUISHUNG BOTTLE REPLACEMENT PER MM 26-22-01-401. SUSPECT INTERNAL APU FAILURE: SYMPTOMS CONSISTENT WITH T1 BLADE FAILURE.

Part: CYLINDER — UNRELIABLE (DOOR 4R SQUIB) · airframe 23,565 hrs · 3,074 cycles

FOUND DOOR 4R EPAS DOOR CYLINDER SQUIB TO HAVE NO EXPIRATION DATE. [07-06-07] REPLACED EPAS DOOR ASSIST CYCLINDER SQUIB WITH ONE THAT HAS AN EXPIRATION DATE & AIRPLANE OK FOR SERVICE.

Part: BATTERY PACK — UNRELIABLE (EMERGENCY LIGHT) · airframe 23,565 hrs · 3,074 cycles

FOUND 4R DOOR BATTERY PACK SERVICEABLE DATE SMUDGED AND HARD TO READ. [07-06-07] REPLACED EPAS BATTERY PACK ASSY PER MMOV 52-11-20 CONFIG 1 AND CONFIG 2. AIRCRAFT READY FOR SERVICE.

Part: PCU — LEAKING (RUDDER) · airframe 23,032 hrs · 3,008 cycles

ARRIVAL CHECK FOUND RUDDER UPPER POWER CONTROL PACKAGE HYD HEAVY LEAK. [SUP 05-18-07] REPLACED UPPER RUDDER POWER CONTROL UNIT. REF MM 27-21-11 P401. COMPLETED OPERATIONAL CHK AND LEAK CHECK . BOTH CHECKED OK.

Part: LIGHT — DAMAGED (SEAT 2E AFT) · airframe 22,910 hrs · 2,994 cycles

EMERGENCY LIGHT DAMAGED AT SEAT 2E. REPLACED AFT EMERGENCY LIGHT ON SEAT 2E. OPS CHECK GOOD.

Part: CHARGER — FAULTY (MASTER BATTERY) · airframe 16,163 hrs · 2,159 cycles

RECEIVED BATTERY CHARGER FAULT. MECHANICS FOUND CIRCUIT BREAKER FOR MAIN BATTERY CHARGER TRIPPED. THE BATTERY AND CHARGER WERE REPLACED PER MM 24-31-01 AND 24-31-02. REMOVED BATTERY PN 263BA101-2 SN 1049A HAS BEEN SENT TO THE VENDOR FOR REPAIR. BATTERY CHARGER PN 263BC101-2 SN 1088 HAS PASSED ALL SHOP TESTS. ONE PRIOR REPORT ON PREVIOUS LEG 22AUG05 OF MAIN BATTERY LOW VOLTAGE WHERE BATTERY WAS REPLACED. NO OTHER REPORTS IN LAST 12 MONTHS. ENGINEERING CONSIDERS THIS AN ISOLATED CASE.

Part: FILLER — MISSING (L/E SLAT) · airframe 3,626 hrs · 530 cycles

SLATS NR 1 & 14 FILLERS WERE MISSING FROM SPANWISE BULB SEALS. MAJOR REPAIR ACCOMPLISHED. FILLERS INSTALLED.