N648UA

Part: INDICATOR — FAULTED (FUEL QTY) · airframe 125,761 hrs · 19,366 cycles

SUSPECTED FUEL LEAK, RT ENGINE, FL370 FUEL COFIG WITH IN 5 MIN INSPECTED ENGINE 2 FOR EXTERNAL FUEL LEAK,WITH FAN COWLS,THRUST REVERSERS AND CORE COWL OPEN NO FUEL LEAK WAS NOTED, DRAINS WERE ALSO INSPECTED. ENGINE COWLS AND THRUST REVERSERS WERE CLOSED & REACTIVATED AS REQUESTED, PERFORMED BITE OF FQIS & FOUND ONE FAULT, RM TU 5 CONTAMINATED G. ALSO PERFORMED A DIP OF RH FUEL TANK WITH THE FOLLOWING READINGS, STICK 5 READING 10.1 WITH A ROLL OF 0.5 LT WING DOWN & PITCH OF 0.5 NOSE UP. FUEL READING IN THE COCKPIT WAS 34.6 IAW AMM 28-44-00, 71-11-04,71-11-06, & 78-31-00, REV 145. DEFERED RIGHT FQIS INOP, DEFER RIGHT FQIS PER MEL 2841P. PLACARD INSTALLED. RT FUEL QTY VERIFIED USING FUEL STICK METHOD.

Part: IDG — FAULTED (NR 1 GEN) · airframe 124,281 hrs · 19,175 cycles

AT CRUISE L GEN DRIVE CAME ON FOLLOWED QRH AND DISCONNETED GENREF LP 4495210 DUPLICATE ITEM "L GEN DRIVE. RAN FLIGHT MANUAL CHECKLIST, DISCONNECTED AND STARTED APU REF NON-NORMALS 2.60.34" LP 4495210 TRANSFERRED TO THIS LP AND CLEARED REF LP 4495696 OVERFLOW SERVICE ADAPTER FOUND LEAKING OIL SUSPECT IDG BURNED UP DUE TO LOW OIL. IDG REPLACEMENT REQUIRED TOMC LOCKS FOR REPAIR CONFIRMATION UPON OIL DRAINING IN PREP FOR CHANGE FOUND IDG OIL WAS FULL NEED TO FURTHER T/S IF IDG REPLACEMENT IS REQUIRED OR NOT. CURRENT BPCU FAULT POINTS TO PRESSURE SWITCH WIRING OR GCU PERFOMED BITE CHECK OF BPCU, FOUND MSG IDG/PRESSURE SW WIRING. CONTINUED TO FIM 24-20 TASK 804. PERFORMED WIRING CHECKS,NO FAULTS. FIM'S NEXT RECOMENDATION REPLACEMNT OF GCU ACCOMPLISHED ELSEWHERE ON THIS LOGPAGE. PER TOMC REQUEST REPLACED IDG REF AMM 24-11-01-404-001-006, SERVICED IDG REF AMM 12-13-03, DRY MOTORED ENGINE REF AMM 71-00-00-862-053-N00 AND RESERVICED IDG. REMOVED AND REPLACED LEFT GCU (ENG 1)(M144) OPS CHECK GOOD REF AMM 24-22-02. VERIFIED INSTALLATION COMPLETED INSTALLATION CHECKS FOR LT IDG PER AMM 24-11-00 DISCONNECT AND LOAD TESTS PASSED.

Part: COVER — BROKEN (ZONE 200) · airframe 124,104 hrs · 19,150 cycles

IT WAS FOUND THE SEAT 43D WITH EPL COVER BROKEN. WAS REMOVED AND REPLACED THE EPL COVER REF CMM 25-21-53. ITEM OK FOR SERVICE.PARTS USED: 58-2523-3-0048,QTY :1

Part: DOOR — MISSING (ZONE 400) · airframe 123,934 hrs · 19,131 cycles

PDA 2 RIGHT ENGINE, INBORD SIDE PYLON PANEL 446BL MISSING PHOTO ADDED REQUEST CDL 54D.PANEL MISSING. NO ITHER DAMAGE FOUND DISPATCH DESK: 82 NAME: MJ DATE: 14-MAR-25- CDL 54D APPROVED. REF GMM 02-30-95, PANEL IS CAT 2. PLACED #2 PYLON PANEL 446BL ON CDL. STICKER APPLIED. SEE LP 4170096 ALSO INSTALLED NEW STRUT ACCESS PANEL 446BL WITHOUT ROTARY LATCHES.

Part: TAT PROBE — FAULTED (ZONE 100) · airframe 123,825 hrs · 19,113 cycles

TAT PROBE AUTOTHROT DISC COMPLIED WITH QRH REM/REPL TAT PROBE SENSOR IAW B767-3 AMM 34-12-02-404-008. TAT PROBE TESTS GOOD IAW AMM 34-12-02-864-027. REM/REPL (AIR/GND) RELAYS K411 & K514 REF. B767-3 SSM 30-33-01-101 AS A PRECAUTIONARY MEASURE. REM/REPL (AIR/GND) RELAY K517, REF. B767-3 SSM 30-33-01-101.

Part: ACCESS PANEL — MISSING (ZONE 400) · airframe 123,791 hrs · 19,109 cycles

PDA 2 REFERENCE LP 4049048: PANEL NACELLE STRUT ACCESS ENG N2 MISSING PANEL 436 BL REPLACED 436 BL PANEL ON E2 INBOARD PYLON NACELL. REF AMM 54-53-98.

Part: BOTTLE — LOW PRESSURE (L2 DOOR SLIDE) · airframe 122,852 hrs · 18,988 cycles

DOOR 2L SLIDE PRESSURE GAUGE IN RED PERFORMED SCAPE SLIDE CHECK REF TASK 25-66-98-206-001 AND FOUND GAGE NEEDLE IN THE CORRECT POSITION. GOOD FOR SERVICE.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 122,862 hrs · 18,989 cycles

EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - FOUND EXTERNAL LIGHT INOP POSITION STA 1197 LH. REMOVED AND REPLACED THE EXTERNAL EMERGENCY LIGHT POSITION STA 1197 LH AS PER AMM-TASK 33-51-06-902-082, CHECKED OK.

Part: ACCESS DOOR — MISSING (NR 1 NACELLE) · airframe 121,667 hrs · 18,845 cycles

ENG 1 OUTBOARD NACELLE STRUT ACCESS DOOR 436BL MISSING ON ARRIVAL. PLESE REFER TO LOG 8447087 FOR ACTION.

Part: IDG — WARNING LIGHT (FD) · airframe 121,667 hrs · 18,845 cycles

DEBRIEFED FLIGHT CREW, CREW STATES L GEN DRIVE LIGHT ILLUMINATED ON OVERHEAD IN FLIGHT. PILOTS SELECTED L IDG DISCONNECT SW TO DISCONNECT IDG R BEING 11. 24-20 TASK 804, NO FAILURES/FAULTS DISCOVERED. FOUND SIGNIFICANT OIL LEAKS INSIDE LH ENGINE COWLINGS AND ON IDG OIL PLUMBING. SUSPECT SUDDEN OIL LOSS TRIGGERED FAILURE OF IDG. RECCOMEND IDG REPLACEMENT. PERFORMED BITE OF BPCU AND FOUND MULTIPLE FAULTS ON BPCU FOR THE PICS ATTACHED OF AUTO EVENT AND BITE RESULTS. PICS CONTINUED AUTO EVENT PERFORMED FIM 24-20 TASK 801 AND FOUND MULTIPLE MGS ON BPCU FOR LEFT GENERATOR SYSTEM. SOME FAULTS FOUND WERE IDG HIGH RISE TEMP PERFORM CORRECTIVE ACTION AS REQUIRED. IDG PARTS INFORMATION LEFT GEN POWER SYSTEM: SVC IDG, IDG/PRESSURE SW WIRING, UNDER WHICH COINCIDES WITH AUTO EVENT WHICH DISPLAYED A 10 DEGREE C ATTACHED. FREQ TRIP, IDG/PMG WIRING, DISCONNECT TRIP, IDG NOT DIFFERENCE IN IDG RISE TEMPS BETWEEN L AND R WITH L BEING 21 AND DISCONNECTED. PERFORMED TROUBLESHOOTING FOR MESSAGES REF FIM 00-0586-3-1071 IDG REMOVED REF AMM 24-11-01. NEW IDG INSTALLED UP TO 24-11-01 SUBTASK 24-11-01-424-022-006. QAD REQUIRES TORQUE AS WELL AS ALL UNIONS. PRESSURE FILL COUPLINGS NEEDS REPLACEMENT, DRAIN COUPLIMG REPLACED REF AMM 20-10-20 PARTS USED:

Part: PANEL — DAMAGED (T.E FLAP) · airframe 120,462 hrs · 18,698 cycles

DURING ACCOMPLISHMENT OF 2SC FOUND T.E FLAP MECHANISM PANEL 196JR WITH SIGNS OF MISALIGMENT. REMOVED INBOARD FLAP TORQUE TUBE SLOT DOOR PERFORM IAW CDL REF # T.E FLAP MECHANISM PANEL 196JR REMOVED PLACED ON MEL CDL 27B DDP 27B. C/W. ADD EMP:U162722,U399319 DISPATCH DESK: 81 NAME: MK DATE: 13-MAR-24- TOMC APPROVES CDL 27B THIS IS TO ADD PICTURE REQUESTED FROM TOMC. THIS IS TO ADD PICTURE REQUESTED FROM TOMC. ALSO CRACKED DOOR REMOVED IS NUMBER 196HR. PANEL 196GR(76-5300-3-0033) IS REMOVED UPPER PANEL 196 GR REF AMM 53-51-21. BRACKET, SEAL AND HARDWARE ARE ON A PLATIC BAG INSIDE COCKPIT... CRACKED. SEE PICS. STRAP ON BACK OF PANEL 196JR(654T0513-1676)IS REPAIRED DAMAGED AREA IN REFERENCE TO SRM 51-70-05 AND 51-70-03 REF PREVIOUS ENTRY FOR REPAIR OF PANEL. PANEL NUMBER REPAIRED I PANELS 196GR AND 196JR WERE REMOVED AND REPAIRED. REINSTALLED NEEDS OLD ASSY THAT WAS REMOVED IN GIG TO SEE WHICH PART IS NEED S 196GR. PANELS 196GR AND 196JR. FLAP MECHANISM CDL STAYS. ED FOR REPAIR.

Part: CLAMP — MISINSTALLED (ANTI-ICE VALVE) · airframe 119,960 hrs · 18,630 cycles

L STRUT DUCT LEAK INDICATION DURING CLIMB THRU FL180 DURING TROUBLESHOOTING, FOUND THE NO.1 ENGINE THERMAL ANTI-ICE VALVE AFT CLAMP INCORRECTLY INSTALLED AND NOT MATED PROPERLY TO THE DUCT AND VALVE FLANGE. PHOTO ATTACHED. REMOVED BOTH ANTI-ICE VALVE MOUNTING CLAMPS TO CORRECTLY REINSTALL VALVE. INSTALLED AND TORQUED THE AFT MOUNTING CLAMP. PHOTO ATTACHED. WORK PERFORMED IAW AMM 30-21-03. NEED TO INSTALL THE FORWARD CLAMP AND RETEST THE VALVE. DUE TO AIRCRAFT REPOSITIONING, TURNED OVER TO SWINGS. FWD CLAMP HANDED TO SWING SHIFT ETOPS SUPERVISOR C.L. REMOVED UPPER CONECTING ROD AND LINE ATTATCHED TO DUCTING FOR MORE FREEDOM OF MOVEMENT OF THE DUCT IN HOPE OF EASIER CONNECTION OF CLAMP. NO SUCESS, NEEDS MORE TIME. HARDWARE LEFT IN FLIGHT DECK. SEE ATTACHED PHOTO INSTALLED CONNECTING ROD, LINE ATTATCHED TO DUCTING AND ANTI-ICE MOUNTING CLAMP IRW AMM 30-21-03. LEAK CHECK OKAY.

Part: SKIN — CORRODED (STA1111,S-16L) · airframe 119,892 hrs · 18,612 cycles

GEN ITEM: 63-5310-1-2630 CABIN LEFT SIDE AT STATION 1111 S-16L HAS CORROSION ON THE SKIN UNDER THE STRINGER, JUST BELOW LOWER FORWARD CORNER SECTION OF WINDOW, MARKED WITH STREAMER REPAIRED AIW REA 47585REA01. SEE PARTIAL WORK SHEET NO 14 1-4 FOR ALL WORK ACCOMPLISHED. REF UNITED EC/RA NO 5330-07159. REF NON -ROUTINE 165631-0200-0219 FOR DETAILS

Part: SKIN — CORRODED (STA1562-1582) · airframe 119,892 hrs · 18,612 cycles

GEN ITEM: 63-5310-1-2507 B767-53-3-7058 CORROSION ON INTERNAL FUSELAGE SKIN STA 1560 STRINGER 39L-39R AROUND THE TOILET SERVICE PANEL. REPAIRED THE AREA STA 1562-1582 IAW EC/RA 5300-0349, REA 47585FA B04, EC/RA 5360-01749, REA 47585FAB03. REF NON-ROUTINE 165631- 0100-0246 FOR DETAILS

Part: PLATE — CORRODED (STA1373-1395) · airframe 119,892 hrs · 18,612 cycles

GEN ITEM: 63-3810-1-2801 AFT POTABLE WATER SERVICE PANEL HAS CORROSION IN MULTIPLE SPOTS MARKED REF AMES NR 165631-0100-0038 REMOVED DAMAGED PANEL AND FOUND TO BE OUT OF LIMITS AND REPLACED WITH NEW PANEL IAW B767 SRM 52-40-01-1A-7 AND SRM 51-40-02 PARA GRAPHS 4 AND 7.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 119,892 hrs · 18,612 cycles

GEN ITEM: 63-5300-1-2003 R2 DOOR AREA LOWER AFT CORNER IN-BETWEEN STATIONS 1518-1538 HAS FLOOR SUPPORT STRUCTURE WITH CORROSION, MARKED WITH STREAMER (T. GREGORY V921207) REPAIRED R2 DOOR AREA LOWER CORNER STA 15818-1538 FLOOR SUPPORT STRUCTURE IAW AMES REA DOC. 47585REA03 AND UNITED EC/RA #5320-02 989. SEE PARTIAL WORK ACCOMPLISHED ON BACK OF N/R AND PWS 73 PAG ES 1 AND 2.

Part: STRINGER — CORRODED (STA1535-1562) · airframe 119,892 hrs · 18,612 cycles

CORROSION F/S 1544 STR 39R.

Part: SHEAR TIE — CORRODED (STA1540) · airframe 119,892 hrs · 18,612 cycles

CORROSION ALC FS 1540 SHEAR TIE BETWEEN STR 38L & 39L AFT SIDE. BLENDED CORROSION ON STA 1540 SHEAR TIE AT STR 38L-39L FOUND TO 2 TOOL TAG NO 10371. BE OUT OF LIMITS MATERIAL LOSS .010" ALLOWABLE LIMITS .006" REMOVED AND REPLACE SHEAR TIE WITH PN: 140T21024585 IAW B767-300 SRM 53-00-07-1A-2 FIG 101 DETAIL II 51-40-02 PARA 4, 7, DWG 140T210

Part: BRACKET — CORRODED (STA 1540) · airframe 119,892 hrs · 18,612 cycles

CORROSION ALC FS 1540 SHEAR TIE BETW EEN STR 38R & 39R AFT SIDE. BLENDED CORROSION ON SHEAR TIE AT STA 1540 STR 38R-39R MATERIAL LOSS .025" ALLOWABLE DAMAGE .006" FOUND TO BE OUT OF LIMITS REMO VED AND REPLACE SHEAR TIE WITH PN: 140T21-02U585 IAW B767-300 SR M 51-40-02 PARA 4, 7, SRM 53-00-07-1A-2 FIG 101 DETAIL II DWG

Part: FRAME — CORRODED (STA1560) · airframe 119,892 hrs · 18,612 cycles

CORROSION ON INTERNAL FUSELAGE FRAME LOWER CHORD STA 1560 STRINGER 39R-39L FWD OF LAV SERVICE PANEL. REF AMES NR 165631-0100-0247 BLENDED CORROSION LWR CHORD AT STA 1562 MATERIAL LOSS 100% OUT O F LIMITS REPLACED LWR CORD I.A.W B767-300 SRM 51-40-02 PARA 7 SE E PARTIAL WORK ACCOMPLISHED

Part: SEAT TRACK — BROKEN (STA1329) · airframe 119,892 hrs · 18,612 cycles

GEN ITEM: ZONE 250CW CLOSE SEAT TRACK @STA 1329 UPPER FLANGE IS BROKEN AT FASTNER HOLE . REF AMES NR 165631-0200-0235 #5300-03047 FOR ANODINE OF SEAT TRACK REPAIR PART. SEE PARTIAL W SEAT TRACK UPPER FLANGE FOUND TO BE OUT OF LIMITS. REPAIRED SEAT ORK ACCOMPLISHED ON BACK OF N/R AND PWS NO. 76 PAGES 1-4. ESFR 1 TRACK AT STA 1229-1395 LBL11 IAW B767-300 SRM 53-00-52-2R-1 REP 034684 AIR 1. REF. AMES REA DOC. 47585REA07 AND EC/RA

Part: SKIN — CRACKED (R1 DOOR) · airframe 119,892 hrs · 18,612 cycles

WHILE PERFORMING EA 5315-01152 OP 002 FOUND CRACK INDICATION AT LOWER HOLE THROUGH SKIN SURFACE AT R1 DOOR LOWER AFT CORNER. REF AMES NRC 165631-0200-0049.

Part: SHEAR TIE — CORRODED (STA1562) · airframe 119,892 hrs · 18,612 cycles

GEN ITEM: 53-5310-1-2638 ALC F/S 1562 I/B OF STR 38L SHEAR TIE EXFOLIATED. LEFAIVE REF AMES NR 165631-0100-0231 PARA 7 SFR# 1034683 SEE PARTIAL WORK ACCOMPLISHED REMOVED CORROSION AT STA 1562 FWD AND AFT SHEAR TIE MATERIAL LOS S 100% FOUND OUT OF LIMITS INSTALLED NEW SHEAR TIE AT STA 1562 F ROM STR 38L-STR 38R I.A.W B767-300 SRM 53-00-03, SRM 51-40-02

Part: FITTING — CORRODED (RT HORIZ STAB) · airframe 119,892 hrs · 18,612 cycles

REF AMES NRC 165631-0300-0073 - REMOVE R/H O/B HORIZONTAL STABILIZER PIVOT HINGE TO FOM. CORROSION WAS LOCATED ON THE R/H HORT STAB PIVOT CORROSION WAS REPAIRED IAW AMES REA DOC 47585REA01 AND UNITED EC/RA #5510-03210 REMOVED AND REINSTALLED PIVOT HINGE IAW B767 AMM 20-11-00-910-80 2 CORROSION WAS LOCATED ON THE R/H HORT STAB PIVOT CORROSION WAS R EPAIRED IAW AMES REA DOC 47585REA01 AND UNITED EC/RA #5510-03210 REMOVED AND REINSTALLED PIVOT HINGE IAW B767 AMM 20-11-00-910-80 2 ADD EMP:V921193

Part: KEELBEAM — CORRODED (BS 785) · airframe 119,892 hrs · 18,612 cycles

GEN ITEM; 63-2060-1-2610; KEEL BEAM FS785 CORROSION UNDER 5 NUT PLATES "MARKED" REF AMES NR 165631-0100-0072. 03046 SEE BACK + PARTIAL WORKSHEETS #40 1 OF 2, 2 OF 2 FOR PARTI BLENDED + EVALUATED KEEL BEAM FS785 UNDER 5 NUT PLATES ON PANEL AL WORK COMPLETED. SUPPORT STRAP. FOUND TO BE OUT OF LIMITS IAW B767 SRM 53-50-12-1 A. REMOVED + REPLACED IAW B767 SRM 51-40-02 PARA 9 + EC/RA 5300- NO ADDITIONAL REMARKS.

Part: STRINGER CLIP — CRACKED (STA1219 STR21R) · airframe 119,892 hrs · 18,612 cycles

REMOVED AND REPLACED STRINGER CLIP AT STA 1219 STR 21R REMOVED AND REPLACED STRINGER CLIP AT STA 1219 STR 21 R I/A/W SR M 51-40-02 PAR 9 BOEING DRW 140T2101 AND ECRA 5300-03045. REF AMES NR 165631-0200-0230. REMOVED & REPLACED STRINGER CLIP AT STA 1219 STR 21R IAW SRM 51-40-02 PARA 9, AMES DOC #47585FAB01, BOEING DWG 140T2101, + EC/RA 5300-03045 SEE BACK FOR PARTIAL WORK COMPLETED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 119,892 hrs · 18,612 cycles

FUSELAGE SKIN HAS 2EA CRACKS ON VERTICAL FASTENER ROW MEASURING 1" LONG AND .250 LONG LOCATED AT LFS 1702, BETWEEN S-10L AND S-11L (VERI FIED WITH HFEC) REF AMES NR 165631-0300-0008 REMOVED DAMAGE. FABRICATED AND INST ALLED DOUBLER 1 AND FILLER 3 IAW SRM 53-00-01 REPAIR 29. TH IS IS A CATEGORY B REPAIR REQUIRING SUPPLEMENTAL INSPECTION AS G IVEN IN TABLE V FIG 201 SHEET 10 NO ADDITIONAL REMARKS.

Part: PANEL — CORRODED (AFT LAV) · airframe 119,892 hrs · 18,612 cycles

AFT LAV WATER SERVICE PANEL HAS CORROSION UNDER LATCHES AFT LAV SERVICE PNL WAS REPLACED WITH THE LATCHES. THE CORROSION WAS 100% MATERIAL LOSS I.A.W B767-300 SRM 52-40-01-1A-4 ALLOWAB LE DAMAGE 4 DETAIL IV DWG 146T3244

Part: INTERCOSTAL — CORRODED (STA 287 LBL 30) · airframe 119,892 hrs · 18,612 cycles

CORROSION AT STA 287 LBL 30 JUST AFT OF COCKPIT DOOR ENTRY.

Part: STRINGER CLIP — CORRODED (STR16R, STA1285) · airframe 119,892 hrs · 18,612 cycles

STRINGER CLIP ON STR 16R AT STA 1285 HAS CORROSION FLAGGED.

Part: CHARGER — MALFUNCTIONED (SEAT 16A-33A) · airframe 118,870 hrs · 18,470 cycles

B767-33-3-7000 - LHS OVERHEAD EXIT SIGNS AND EMER AISLE LT ON SEAT 16A-33A DIM TRANSFER REF HXWO 1996055 AND ORIGINATED BY EMP V920570 EMER POWER SUPPLY (M737) REPLACED AND TEST NORMAL AS PER AMM33-51-07 ATTACHED FORM 44-0008 ITEM 1 TO 2.

Part: BRACKET — BROKEN (LEFT WING) · airframe 118,790 hrs · 18,458 cycles

LEFT WING EXTERNAL INSPECTION {B767-06-3-0217} - FOUND SUPPORT BRACKET BROKENB/DAMAGED. SEE PHOTO. ADDED PHOTO. PANEL 652DB REMOVED BROKEN BRACKET 2767 CYCLES, OR 551 DAYS WHICH IS REMAINING TIME BEFORE NEXT "C" CHECK. WHICHEVER COMES FIRST. DIP TO ACCOMPLISH INSPECTION PER PART 2 OF EC/RA 5700-03923 REV B ONCE EVERY 14 DAYS AND ACCOMPLISH PART 3 BEFORE 10,393 HRS, CARRY APPROVED PER ECRA 5700-03923 REV B. ACCOMPLISH INSPECTION TOMC-APPROVAL FROM SC1ELBYC COMMENT PER PART 2 ONCE EVERY 14 DAYS AND ACCOMPLISH PART 3 BEFORE 10393 HOURS, 2767 CYCLES, OR 551 DAYS WHICHEVER COMES FIRST WHICH IS THE TIME REMAINING TILL NEXT C-CHECK. C/W HFEC PER ECRA 5700-03923 REV B. NO CRACKS NOTED. FABRICATED CHANNEL AND MATCHED DRILLED HOLES TO NEW PART REF COMPLETED INSTALLATION OF CHANNEL REF ECRA 5700-03923 REV B QC ECRA 5700-03923 REV A, PART 1 INTERIM REPAIR STEP 1 A. B. INTERIM REPAIR PART 1 STEPS 1 AND 2, NEEDS TO BE PLACED ON DIP REQUIRES HFEC INSP STEP 1 C. OF BEND RADIUS TO VERIFY NO CRACKS PER STEP 3. EXIST. RECORDS UPDATE. HC TOMCQC REV PERFORMED PER ECRA 5700-03923 REV C PART 1 INTERIM REPAIR IS NOW CONSIDERED A PERMANENT REPAIR. NO FURTHER ACTIONS REQUIRED. QC REVIEW RIR : 14 DAYS T/A : 10,393 FH OR 2,767 FC OR 551 DAYS (NEXT C CK)...HC

Part: STUD — LOOSE (SEAT 2D) · airframe 118,119 hrs · 18,368 cycles

DURING CABIN CHECK WAS FOUND SEAT 2D WITH FOWARD STUD ANCRA LOOSE. THE STUD ANCRA WAS INSTALED IN THE SEAT 2D REF IFM 25-25-95, GOOD FOR SVC. OBSERVED PASSENGER SEAT INSTALLATION ALL FUNCTIONS NORMAL. SEAT 2D SAFETY AND SECURED.

Part: BLADES — DAMAGED (NR 2 ENGINE) · airframe 117,127 hrs · 18,219 cycles

NR 2 ENG HAD SEVERAL COMPRESSOR STALLS DURING CLIMB. EGT EXCEEDANCE OBSERVED. HAD THE THROTTLE BACK AT IDLE AND ENGINE STABILIZED. RETURNED TO HKG. IAW FIM 71-05 FAULT TREE 803, FOR T/SHOOTING. CHECKED INLET, EXHAUST. CHECKED MCDS, EPCS PERFORMANCE & EGT EXCEEDANCE PAGE. RT ENG PIMU BITE PROCEDURE CARRIED OUT, RESULT NORMAL IAW FIM 71-05 FAULT TREE 803, STEP 2 ENGINE TURBINE EXHAUST BORESCOPE INSPECTION PERFORMED IAW FIM 71-05 FAULT TREE 803. 71-01-00. AREA FOUND PARTICLES AND COLLECTED, STEP 3 N1 ROTOR TURN FREELY, RESULT FOUND 5TH, 6TH, 10TH STAGE HPC BLADES DAMAGED STEP 4 & STEP 5 RESULT NORMAL, STEP 6 NO UNUSUAL LIMIT IAW AMM 72-00-00 MATERIAL FOUND.

Part: LIGHT — INOPERATIVE (AFT DR SLIDE) · airframe 117,127 hrs · 18,218 cycles

AFT DOOR LH SLIDE EMERGENCY LIGHT FOUND INOP TRANSFER REF. NON-ROUTINE WO.1298586 & ORIGINATED BY EMP V920580 AFT DOOR LH SLIDE EMERGENCY LIGHT LAMP REPLACED AND TEST NORMAL PER AMM 33-51-06 WORK ACCOMPLISHED BY MECHANIC V920580 INSPECTED BY V898561

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 117,127 hrs · 18,218 cycles

EMER CHARGER ASSY (M738) FOUND NO POWER OUTPUT. EMER CHARGER ASSY (M738) REPLACED AND TEST NORMAL PER AMM 33-51- 07

Part: LAMP — INOPERATIVE (SLIDE LIGHT) · airframe 117,127 hrs · 18,218 cycles

AFT DOOR LH SLIDE LIGHT FOUND INOPERATIVE. AFT DOOR LT SLIDE LIGHT LAMP REPLACED AND TEST NORMAL.

Part: PITOT TUBE — FAULTED (FIRST OFFICER'S) · airframe 117,122 hrs · 18,217 cycles

IAS DISAGREE EICAS B THE AIRSPEED DIFFERENCE BETWEEN THE AIR DATA COMPUTERS IS GREATER THAN 5 KNOTS AND THE RADIO ALTITUDE IS GREATER THAN 400 FEET FO AIRSPEED UNRELIABLE DISAGREED WITH CPT AND STANDBY INSTRUMENTS 30+ KNOTS LESS CAPT STBY. PERFORMED F/O PITOT SYSTEM FLUSH PER AMM 34-11-00, NO MORE DEBRIS COLLECTED AT ALL POINTS. REINSTALLED PITOT PROBE PER AMM 34-11-01 AND PRESSURIZED SYSTEM FOR LEAK CHK PER AMM 34-11-00, NO LEAKS NOTED, LEAK RATE TEST PASSED. PRESSURIZED F/O'S AND LEFT AUX 1 PITOT PROBES AND COMPARED F/O'S AIRSPEED TO THE STBY A/S INDICATOR, BOTH MATCHED AT ALL SETTINGS. A/C OK FOR SERVICE.

Part: MODULE — DAMAGED (PACKING DAMAGED) · airframe 115,499 hrs · 18,005 cycles

L HYD QTY LOW QTY SHOWING .48 SECURED L HYD PUMPS AS PER CHECKL IST. FOUND EVIDENCE OF HYDRAULIC LEAKEAGE ON LEFT ENGINE. AFTER 78-34-01-05 ITEM 320. REPLACED PACKING PER AMM 78-34-01 AND AMM ENGINE COWLS OPEN, NOTED HYDRAULIC LEAKEAGE COMING FROM UPPER 12-12-01 FOR HYD SERVICE TO FULL LEFT SYSTEM. CHECK GOOD. PART OF ENGINE. FOUND PACKING PART NUMBER NAS1612-8 DAMAGED ON VALVE MODULE DIRECTIONAL CONTROL THRUST REVERSER. REF. IPC ADD EMP:U235671,U381077

Part: LANDING GEAR — NONE (NA) · airframe 113,833 hrs · 17,696 cycles

PER CREW VERBAL, AFTER TAKE OFF AND GEAR RET. WE HAD MASTER CAUTION WITH GEAR DISAGREE AND GEAR DOORS EICAS. AT SAME TIME AMBER DOORS AND AMBER GEAR ANOUNCIATOR LIGHTS ILLUMINATED. RAN QRH CHECKLIST AND SUBSEQUENTLY LOWERED GEAR WICH PRODUCED NORMAL INDICATION GEAR DOWN. CAPT CALER, U168150.

Part: FAIRING — MISSING (FAIRING 447DB) · airframe 113,567 hrs · 17,631 cycles

PDA 3 #2 ENGINE PYLON AFT FAIRING 447DB INBD MISSING 1EA SCREW IN AFT METAL PAN. INSTALLED SCREW AT FAIRING INBD PAN 447DB UPPER FWD FASTENER POSITION.

Part: HOSE — DAMAGED (RT HYD SYSTEM) · airframe 112,376 hrs · 17,413 cycles

RH ENGINE PYLON STRUT HYD HOSE TEMPORARY INSTALLED PER GPM 01-13 -015.DUE TO NO AVAILABILITY OF SOLID LINE. PER GPM 01-13-003 INT ERIM REPAIR MUST BE REPLACED WITH PERMENAT IN 50 FLIGHT HOURS.TH E REPAIR MUST BE CHECKED FOR INTEGRITY AT EACH MAINTENACE OPPORT UNITY PER GMM 05-30-15 DIP ITEM FOR TEMP RPR OF HYD LINE. INSTALLED TE MP HYD HOSE PER GPM 01-13-003 AND GPM 01-0-13-3.THIS INTERMI RPR MUST BE REPLACED BY PERMENANENT REPAIR WITH IN 50 FLT, HOURS RH ENGINE PYLON STRUT HYD HOSE TEMPORARY INSTALLED PER GPM 01-13 -015 DUE TO NO AVAILABILITY OF SOLID LINE PER GPM 01-13-003 PAR C.10. MUST BE REPLACED WITH NEW LINE WITHIN 500 FLYING HOURS.REF L/P 6379394 AND IPC 78-34-52-02 ITEM 145 MFG# 312T4100-34 NOTE: PART BEING SENT TO SMB SHOP FOR FABRICATION TOMC-APPROVAL FROM SC1ELBYC COMMENT Q/C REVIEWED. Q/C REVIEWED. RECORDS UPDATE......SS T/A : 500 F/H.......SS

Part: ACTUATOR — FAILED (OUTFLOW VALVE) · airframe 111,734 hrs · 17,313 cycles

CABIN AUTO INOP EICAS B THERE IS A FAILURE OF THE NO. 1 AND 2 AUTOMATIC PRESSURIZATION C ONTROLLERS OR THE PILOT CHANGED TO MANUAL PRESSURIZATION CONTROL . 0 UPDATE TO INDICATE FLT 0252 DELAY. CONTROLERS SHOW AC MOTOR FAILURE. REPLACED OUTFLOW ACTUATOR PER AMM 21-31-04. CHECKS OK. UPDATED WITH RORABLE PART NUMBERS ROTABLE PARTS CHANGE WAS INDICATED - TT # 1300978 SN OFF 4329 IPC REFERENCE # 21-31-03-10 ACTUATOR, CABIN OFF 75-2133-9-0001 4329 ON 75-2133-9-0001 1678

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 111,219 hrs · 17,226 cycles

REFERENCE CID 507699 EMERGENCY BATTERY LIGHT PACK AT BS 1197 AT ROW 32A INOPERABLE. REPLACED EMERGENCY LIGHT BATTERY PACK AT BS 1197 ROW 32A, IAW AMM 33-51-07. OPERATIONAL CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 111,219 hrs · 17,226 cycles

REFERENCE AERSALE CID 507698 EMERGENCY BATTERY LIGHT PACK AT BS 1340 AT ROW 40A INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK AT BS 1340 ROW 40A, IAW AMM33-51-07. OPERATIONAL CHECKED GOOD. WORK ACCOMPLISHED ON AERSALE CID 507698 BY V931306 AND INSPECTED BY ASI QC-50 ADD EMP: V931306.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 111,219 hrs · 17,226 cycles

REFERENCE CID 507693 EMERGENCY BATTERY LIGHT PACK AT BS 998 ROW 24A INOPERABLE. REPLACED EMERGENCY LIGHT BATTERY PACK AT BS 998 ROW 24A, IAW AMM 33-51-07. OPERATIONAL CHECK GOOD.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 102,394 hrs · 16,013 cycles

DURING ACCOMPLISHING EA2500-04990 OP 15 SEAT TRACK REWORK AT RBL54. FOUND ONE BOLT HOLE SEM 0.51" AT STA844. BOLT HOLE SIZE 0.312" SEAT TRACK BEAM AT STA 786 TO STA 899 RBL54 REPAIRED PER SRM 53-00-51 REPAIR 3 FIG 201 AND EC/RA 2500-06090 REV -. FORM 44-0008 ATTACHED ITEM 1 TO ITEM 30 ACCOMPLISHED

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 102,394 hrs · 16,013 cycles

B767-53-3-6087 MAIN DECK FLOORBEAM UPPER SURFACE RBL 55 STA 325 FOUND CORROSION. REPAIRED PER SRM 53-00-51 REPAIR 1 FIG 201 FORM 44.0008 ITEM 1-24 ACCOMPLISHED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 102,394 hrs · 16,013 cycles

B767-53-3-6050 CABIN STA 742-754 RBL 20 SEAT TRACK CROWN FOUND CORROSION AS MARKED. REPAIRED PER SRM 53-00-52 REPAIR 2 FIG 201. FORM 44.0008 ATTACHED ITEM 1 TO 25 ACCOMPLISHED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 102,394 hrs · 16,013 cycles

B767-53-3-6252 CABIN STA 1461 LBL 1 TO LBL 28 FLOORBEAM FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 53-00-51. REPAIR 1 FIG 201. ATTACHED FORM 44.0008 ITEM 1 TO ITEM 29 ACCOMPLISHED.

Part: STRINGER — CRACKED (BS 1809.5) · airframe 102,394 hrs · 16,013 cycles

BS 1809.5, STRINGER 12AR, ONE FASTENER HOLE FOUND CRACKED, REPAIRED IAW EC/RA 5300-02458.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 102,394 hrs · 16,013 cycles

CABIN STA 735-745 LBL 20 SEAT TRACK FOUND CORROSION CRACK CABIN STA 735-745 LBL20. SEAT TRACK REPAIRED PER SRM 53-00-52 REPAIR 2 FIG 201 FORM 44-0008 ATTACHED ITEM 1 TO 25 ACCOMPLISHED.

Part: FLOORBEAM — CORRODED (BS 347) · airframe 102,394 hrs · 16,013 cycles

MAIN DECK FLOORBEAM UPPER SURFACE, RBL 35 - 55, BS 347 WAS FOUND CORRODED. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIG 201, REPAIR 1.

Part: SEAT TRACK — CORRODED (BS 325) · airframe 102,394 hrs · 16,013 cycles

MAIN DECK SEAT TRACK BS 325, RBL 11 FOUND CORRODED AND CRACKED. REPLACED THE SEAT TRACK IAW SRM 51-10-02, AND SRM 51-40-02.

Part: FAN — FAILED (RECIRCULATION) · airframe 100,600 hrs · 15,737 cycles

COCKPIT CREW REPORTED ELECTRICAL ODOR IN THE COCKPIT. NO SMOKE NOTICED. AFTER A FEW SECONDS THE LT RECIRCULATOR FAN INOPERATIVE LIGHT ILLUMINATED. COCKPIT CREW SWITCHED OFF THE LT RECIRCULATION FAN. REPLACED RECIRCULATION FAN IAW MM

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 99,572 hrs · 15,600 cycles

EXTERIOR EMERGENCY LIGHT ON FUSELAGE JUST AFT OF LT WING IS INOPERATIVE. REPLACED THE LAMP AND ACCOMPLISHED SUCCESSFUL OPERATIONAL CHECK IAW AMM 3 3-50-00.

Part: STRUT — BROKEN (NLG DOOR) · airframe 96,051 hrs · 15,105 cycles

AFTER TAKEOFF ACFT EXPERIENCED A VIBRATION IN AREA OF NLG. ACFT RETURN TO FIELD. FOUND NLG LT AFT DOOR ATTACH STRUT BROKEN. REPLACED & ADJUSTED THE LT AFT NLG DOOR OPERATOR STRUT ASSEMBLY IAW AMM 32-22-04. JACKED NOSE IAW AMM 07-11-02 & SWUNG GEAR TO VERIFY ADJUSTMENT & FAIR OF DOOR.

Part: SHUTOFF VALVE — BROKEN (FUEL SYSTEM) · airframe 95,542 hrs · 15,032 cycles

FUEL PUMPS, UNWANTED, INTO RT WING TANK AT 150 LBS PER MINUTE WITH FUEL IN CTR TANK & CTR PUMPS ON. REPLACED THE RT TANK ENG SHUTOFF, SPAR VLV DUE TO ENTIRE FLANGE BROKEN OFF VLV, CAUSING FUEL TO BE PUMPED INTO RT WING TANK.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 92,839 hrs · 14,666 cycles

SEAT MOUNTED EMER EXIT LIGHT INOPERATIVE AT SEAT 20 LT. SECURED CONNECTOR. LIGHT OPERATIONS CHECKED NORMAL.

Part: WIRE — BROKEN (CABIN) · airframe 92,397 hrs · 14,605 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT SEAT ROW 30 LT. FOUND BROKEN WIRE UNDER SEAT IN THE PANEL FOR SEAT ELECTRONICS BOX, WIRE BROKEN AT CONNECTOR. LIFE VEST REMOVED & PANEL OPENED. NEED NEW SOCKET & WIRE CRIMPED ON WIRE.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 92,397 hrs · 14,605 cycles

EMERGENCY EXIT FLOOR LIGHT INOPERATIVE AT CTR AISLE JUST FWD OF SEAT ROW 19. SECURED CONNECTOR. FLOOR EEL OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 92,397 hrs · 14,605 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT SEAT ROW 23 LT. SECURED CONNECTOR, OPERATIONS CHECKED OK.

Part: FAN — CLOGGED (NR 2) · airframe 91,460 hrs · 14,470 cycles

CREW REPORTS CARGO DETECTION AIR STATUS MSG DURING CLIMB. FOUND AFT FAN 2 EXHAUST CLOGGED. REMOVED BLOCKAGE FOUND INTERMITTENT RELAY K331. REPLACED IAW AMM 26.16.21 & FWD FAN 1. OPERATIONS CHECKED GOOD, NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: UNKNOWN — MALFUNCTIONED (RT ENGINE) · airframe 31,339 hrs · 14,452 cycles

RETURN TO FIELD DUE TO LOSS OF RT GEN DRIVE.

Part: WARNING MESSAGE — ACTIVATED (COCKPIT) · airframe 90,376 hrs · 14,324 cycles

DIVERSION TO CDG DUE TO FUEL FILTER MESSAGE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 90,144 hrs · 14,288 cycles

HORIZONTAL OUTWARD CREASE AT BS 1724 BETWEEN STRINGER 17R TO STRINGER 19R FUSE EXTERIOR SKIN. REMOVED DAMAGED SKIN, FABRICATED & INSTALLED A REPAIR DOUBLER BETWEEN BS 1664 - 1680 & BETWEEN STRINGER 17R - STRINGER 20R IAW REO G17222, REV IR & SRM 53-00-01, REPAIR 14 & ECRA 5380-01103.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,144 hrs · 14,288 cycles

C53-222-02 MAIN CABIN FLOOR BEAM UPPER CORD AT STATION 324 RB L57 IS CORRODED. REPAIRED STATION 324 MAIN CABIN FLOOR BEAM IAW B767 SRM 53-00-51 REPAIR 1 & ECRA 5310-05998.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 90,144 hrs · 14,288 cycles

AFT PIT FRAME AT BS 1329, WEB & FITTING ARE CRACKED AT LOWER CARGO DOOR OPENING. REMOVED CRACK DAMAGE ON WEB, FABRICATED A REPAIR DOUBLER & TAPERED FILLER & INSTALLED IAW TIMCO REO G17129, REV A & ECRA 5360-01362 AT RBL 42.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 90,144 hrs · 14,288 cycles

OUTWARD CREASE BETWEEN BS 1693 TO 1700 BETWEEN STRINGER 18L & STRINGER 19L. REMOVED DAMAGED SKIN, FABRICATED & INSTALLED A REPAIR DOUBLER BETWEEN BS 1665 - 1680 & BETWEEN STRINGER 18L - STRINGER 20L IAW REO G17222, REV IR & SRM 53-00-01, REPAIR 14 & ECRA 5380-01103 IAW ECRA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 90,144 hrs · 14,288 cycles

PREVIOUS BLENDS EXCEED SRM LIMITS BS 412 & BS 434, STRINGER 35L - STRINGER 36L. COMPLIED WITH ECRA 5310-05 997 FOR FUSELAGE DOUBLER AT STATION 412 - 434, STRINGER 35L - 36L.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 90,144 hrs · 14,288 cycles

AFT PIT BULK CARGO DOOR FRAME FOUND CORROSION OUT OF LIMITS. REMOVED & FABRICATED PN 146T1281 4 FRAME WEB & 146T8211 2 FLOOR STIFFENER IAW DRAWING 146T1281 & 146T8211. NO DEVIATIONS NOTED.

Part: STRUCTURE — CRACKED (LT PYLON) · airframe 90,144 hrs · 14,288 cycles

LT 1 PYLON OTBD DRAIN HOLE AT NACELLE STATION 156 IS CRACKED. ALSO FOUND TWO EACH CRACKS AT THE INBD DRAIN HOLE, NACELLE STATION 156. STOP DRILLED ENDS OF CRACKS, FABRICATED TWO EACH DOUBLERS & FILLERS & INSTALLED IAW SRM 54-53-01, REPAIR 10.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 90,144 hrs · 14,288 cycles

FLOOR BEAM 246 FWD FACE STIFFENER CRACKED LBL 40, BS 246. R & R STIFFENER AT FLOOR BEAM 246 FWD FACE LBL 40, BS 246 IAW B767-300 SRM 53 -10-51 REPAIR 4.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 90,144 hrs · 14,288 cycles

FLOOR BEAM 246 FWD FACE STIFFENER CRACKED LBL 23 BS 246. CRACKED STIFFENER R & R IAW B767-300 SRM 51-40-02 & SRM B767 53-10-51 REPAIR 3 TIMCO NR 20003.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,144 hrs · 14,288 cycles

MAIN CABIN FLOOR BEAM FOUND CORRODED AT STATION 303 & RBL 41. REMOVED DAMAGED SECTION & REPAIRED FLOOR BEAM T CORD IAW SRM 53-00-51 REPAIR 1, STATION 303, RBL 41 & WL 199.5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 90,144 hrs · 14,288 cycles

FWD CARGO FLOOR BEAM T CAP FOUND CORRODED BEYOND LIMITS AT STATION 654 - 121, STRINGER 33L - 34L. ACCOMPLISHED REPAIR 4 OF SRM53-00-07 FIG 201 1-10.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 90,144 hrs · 14,288 cycles

FLOOR BEAM 246 FWD FACE STIFFENER CRACKED LBL 11 BS 246. CRACKED STIFFENER R & R IAW B767-300 SRM51-40-02 & B767-300 SRM 53-10-51 REPAIR 3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,144 hrs · 14,288 cycles

C53-221 MAIN CABIN FLOOR BEAM STATION 287, BL 0, LBL 20 FOUND CORRODED. CORROSION FOUND OUT OF LIMITS AT STATION 287, BL 0, LBL 20. REPAIRED BEAM IAW SRM53-00-51REPAIR 4 IAW NR21219.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,144 hrs · 14,288 cycles

FLOOR BOARD SUPPORT AT STATION 1524 - 1540, LBL 80 FOUND CORRODED BEYOND LIMITS SPLASH GUARD. REMOVED DAMAGE, FABRICATED EXTRUSION & INSTALLED IAW DRAWING 146T0051 & SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 90,144 hrs · 14,288 cycles

MAIN CABIN FLOOR SUPPORT STATION 288 - 295, RBL 80 FOUND CORRODED, FOUND DAMAGE OUT OF LIMITS. R & R WITH NEW SPLASH GUARD IAW DRAWING 141T 8310 & SRM 51-40-02.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 90,144 hrs · 14,288 cycles

BS 246 FLOOR BEAM FWD FACE STIFFENER IS CRACKED AT RBL 11. INSPECTED THE MID CHORD & FLOOR BEAM WEB FOR CRACKS IN THIS LOCATION IAW ROUTINE TASK CARD 611003311, STEP 3, NOTE 1, NO CRACKS NOTED. REMOVED STIFFENER, FABRICATED REPLACEMENT STIFFENER 5 SUPPORT IAW DRAWING 141T5104 ON NR 21241 & INSTALLED IAW SRM 53-10-51, RPR 3.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 90,144 hrs · 14,288 cycles

MAIN CABIN FLOOR BEAM FOUND GOUGED AT BS 893 RBL 10. GOUGE EXCEEDED LIMITS IAW SRM53-00-51. REMOVED DAMAGE & REPAIRED IAW SRM 53-00-51 REPAIR 3.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 90,144 hrs · 14,288 cycles

MAIN CABIN FLOOR BEAM AT BS 920 LBL 33 IS FOUND GOUGED. GOUGE FOUND OUT OF LIMITS. REMOVED DAMAGE & REPAIRED IAW SRM53-00-51 REPAIR 3 CAT A REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,144 hrs · 14,288 cycles

CORROSION FOUND ON MAIN CABIN FLOOR BEAM BS 850 LBL 55. CORROSION EXCEEDED LIMITS IAW SRM53-00-51. REMOVED & REPAIRED DAMAGED BEAM IAW SRM53-00- 51 RPR3.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 90,144 hrs · 14,288 cycles

MAIN CABIN RT UNDER FLOOR SEAT TRACK SUPPORT CORRODED AT BS 859, RBL 55. INSTALLED REPAIR IAW B767-300 SRM 53-00-51 REPAIR 3 PAGE 204.

Part: INDICATOR — MISSING (R2 DOOR) · airframe 89,513 hrs · 14,203 cycles

DOOR 2R ARM INDICATOR BY HANDLE NOT ENGAGING. VERIFIED R2 DOOR CLOSES & ARMS CORRECTLY. MISSING YELLOW FABRICATED POP UP. DEFERRED IAW MEL 5211D. OK TO CONTINUE.

Part: ISOLATION VALVE — FAULTY (THRUST REVERSER) · airframe 89,413 hrs · 14,190 cycles

AT CRUISE ALTITUDE THE LT REVERSER AMBER LIGHT ILLUMINATED BRIEFLY THREE TIMES IN A ROW THEN EXTINGUISHED. REPLACED LT ENGINE THRUST REVERSER ISOLATION VALVE IAW AMM78-34-05 & TESTED OK.

Part: BLADE — NICKED (NR 1 ENGINE) · airframe 89,315 hrs · 14,178 cycles

NR 12 1ST STAGE FAN BLADE ON NR 1 ENGINE HAS 1-16TH INCH NICK 12 INCHES FROM ROOT ON LE. ACCOMPLISHED BLEND REPAIR IAW AMM 72-31-02 & EDDY CURRENT INSPECTION IAW NTM PART 6-72-31-401.

Part: ADC — FAULTY (NR 1) · airframe 89,268 hrs · 14,173 cycles

FIRST OFFICERS ALTIMETER CONSISTENTLY 150 FEET LOWER THAN CAPTAINS ALL ALTITUDES WHOLE FLIGHT. R & R CAPTAIN`S ADC. OPERATIONS CHECKED NORMAL. TEST 30-40 PASSED. IDT REQUIRED FOR PITOT-STATIC QUICK DISCONNECT-RECONNECT.

Part: SEAL — BROKEN (FLASHLIGHT) · airframe 88,991 hrs · 14,137 cycles

FLASHLIGHT SEAL BROKEN RT OVERWING EXIT. REPLACED SEAL,

Part: CONTROLLER — FAULTY · airframe 88,898 hrs · 14,125 cycles

BITE TEST ZONE CONTROLLER, FAULTING CONTROLLER.

Part: BATTERY — FAULTY (APU) · airframe 88,757 hrs · 14,106 cycles

APU BATTERY CHARGER NOT CHARGING. REPLACED APU BATTERY & CHARGER IAW MM, 24-31-04 & 24-31-05, ALL OPS & INDICATORS NOW NORMAL.

Part: PACKING — LEAKING (N2 ENG FUEL PUMP) · airframe 88,750 hrs · 14,105 cycles

NR 2 ENGINE FUEL PUMP LINE TO FCOC LEAKING AT FUEL PUMP. REPLACED PACKING. NO LEAK PRESENT ON ENGINE RUN.

Part: CONTROL PANEL — FAILED (WX RADAR) · airframe 88,673 hrs · 14,095 cycles

NO HSI DISPLAYS, TEST FAILED AFTER EFIS SELF TEST. (1=CAPT, 2=1ST OFF). REPLACED WEATHER CONTROL PANEL IAW AMM.

Part: WIRE — EXPOSED (EMERGENCY LIGHTS) · airframe 88,665 hrs · 14,094 cycles

EXPOSED WIRE ON FLOOR AT SEAT 30A. NO DAMAGE TO WIRES FOUND, REROUTED AND SECURED.

Part: OVEN — CONTAMINATED (GALLEY) · airframe 88,496 hrs · 14,072 cycles

PLASTIC BURNING ODOR. FOUND MELTED PLASTIC FROM A PLASTIC TRAY, REMOVED TRAY AND PLASTIC TRACE.

Part: OVEN — ODOR (GALLEY) · airframe 88,496 hrs · 14,072 cycles

AFTER ENGINE SHUTDOWN, F/A`S SMELLED A PLASTIC BURNING ODOR WITH NO SMOKE. CLEANED WARMING OVEN, CHECKED OPERATION. OK, NO ODOR FOUND.

Part: INSULATION — DAMAGED (CABIN) · airframe 88,486 hrs · 14,070 cycles

PRESSURIZED PNEU DUCT FROM APU, FOUND NO LEAKS. OPS CHECKED BULK AND AFT CARGO HEATING SYS, FOUND NO LEAKS. OPS CHECKED ADP, FOUND NO LEAKS. INSULATION BLANKET ON PNEU DUCT UNDER SEAT 36 AND 37 AB FOUND DAMAGED. REPLACED INSULATION BLANKET.

Part: INSULATION — DAMAGED (BLEED DUCT) · airframe 88,486 hrs · 14,070 cycles

CREW REPORTED FLOOR AND SIDEWALL AREA AROUND ROWS 36 AND 37 ARE ABNORMALLY HOT. TURNED OFF AFT CABIN TRIM AIR, NO HELP. DAMAGED BLEED DUCT INSULATION BLANKET WAS REPLACED, NO LEAKS DETECTED.

Part: BLADE — NICKED (NR 2 ENGINE) · airframe 87,843 hrs · 13,988 cycles

NR 2 ENGINE FAN BLADE NR 19 HAS NICK 4 INCHES FROM BLADE TIP. PERFORMED PRELIMINARY BLADE BLEND. ACCOMPLISHED HFEC AS REQUIRED REF MM AND NDT MANUAL PART 672-31-401. STILL REQUIRES ADDITION .020" BLENDING REF MM 72-31-02 AT BLADE NR 19. BLENDED BLADE ADDITIONAL .020 IAW MM.

Part: BLADE — NICKED (NR 2 ENGINE) · airframe 87,843 hrs · 13,988 cycles

NR 2 ENGINE FAN BLADE, NR 38 HAS A NICK IN THE L/E ONE INCH FROM TIP. PERFORMED PRELIMINARY BLADE BLEND ON BLADE NR 38.

Part: SKIN — DENTED (BS 289 S25R) · airframe 87,841 hrs · 13,987 cycles

DENT ON FUSELAGE SKIN AT BS 289 AND STRINGER 25R. FOUND WITHIN LIMITS REF SRM 53-00-01 A D1.

Part: PAWL — BROKEN (R2 DOOR SLIDE) · airframe 87,642 hrs · 13,961 cycles

FOUND R2 DOOR OUTSIDE SLIDE ARMING MECHANISM PAWL BROKEN. ARMING PAWL REPLACED IAW AMM.

Part: CONTROL PANEL — FAULTY (WEATHER RADAR) · airframe 87,360 hrs · 13,924 cycles

PWS INOP LIGHT DOES NOT TEST. REPLACED WX RADAR CONT PANEL, OPS CHECK NORMAL.

Part: SMOKE DETECTOR — FAULTY (NR 1) · airframe 87,343 hrs · 13,922 cycles

EICAS MESSAGE - FWD SMOKE DET 1. FORWARD SMOKE DETECTOR NR 1 REPLACED AND OP CHECK OKAY.

Part: FILTER — DEFECTIVE (COCKPIT) · airframe 87,325 hrs · 13,920 cycles

INFLIGHT COCKPIT AIR NOISE TOO LOUD RECIRC FANS NOISY. REPLACED RECIRC HEPA FILTERS.

Part: LENS — DAMAGED (SWITCH) · airframe 87,191 hrs · 13,894 cycles

RIGHT GENERATOR DRIVE DISCONNECT SWITCH MISSING BALE WIRE FROM SWITCH BODY TO LENS CAP. LENS CAP FITTED WITHOUT BALE WIRE, SWITCH OPS ARE NORMAL. REPLACED RIGHT GEN DRIVE LENS AND REPLACED GUARD, SAFETIED BOTH DISC SWITCHES.

Part: COUPLER — NOT SEATED (LT ADC) · airframe 87,043 hrs · 13,875 cycles

SPLIT BETWEEN ALTIMETERS BEYOND 40FT LIMIT. RESEATED QUICK COUPLERS ON LEFT ADC, ALL INDICATIONS WERE WITHIN LIMITS.

Part: CONTROL VALVE — FAULTY (RECIRC FAN) · airframe 87,043 hrs · 13,875 cycles

COCKPIT FAR TOO MUCH NOISE WITH PACKS ON. CANNOT HEAR CHECKLIST OR ATC GROUND AND IN AIR. REPLACED AIR RECIRCULATION FAN CONTROL VALVE, OPS CHECK GOOD.

Part: VALVE — LEAKING (WATER DRAIN) · airframe 86,884 hrs · 13,849 cycles

AFT WATER DRAIN LINE CONTINUES TO DRIP AFTER VALVE IS CLOSED. 643-0044 ON AOM V5969. REPLACED FILLING - DRAIN WATER VALVE, CHECK NO LEAKS.

Part: STRUCTURE — DAMAGED (LT WING LE FLAP) · airframe 86,859 hrs · 13,846 cycles

ACCOMPLISHED BIRD STRIKE CONDITIONAL INSPECTION. DAMAGES FOUND ON LT WING OUTBOARD FLAP LOWER SIDE AT 32 INCHES FROM OUTBOARD AFT EDGES OF FLAP. REPLACED LEFT WING OUTBOARD FLAP IAW AMM-27-51-20 RIG AND OPS CHECKED OK.

Part: STOP — DETACHED (GALLEY) · airframe 86,804 hrs · 13,837 cycles

CONTAINER REAR STOP BLOCK DETACHED LOCATION 402, LEFT SIDE OF BUS GALLEY. RESECURED STOP BLOCK.

Part: SCREW — MISSING (VERTICAL STAB) · airframe 86,767 hrs · 13,830 cycles

ONE SCREW STICKING OUT AND POSSIBLY ONE MISSING ON THE LEFT SIDE OF THE VERTICAL STAB. REPLACED MISSING SCREWS AND TWO EACH NUT PLATES.

Part: SWITCH — FAILED (HYD SYSTEM) · airframe 86,675 hrs · 13,815 cycles

CENTER ELEC HYD PUMP DOES NOT PROMPT AN EICAS WHEN TURNED OFF. REPLACED C2 SWITCH BASE ASSY IAW SWPM 20-84-14, WD 29-11-31 AND MM 29-11-00 CENTER HYD SYS TEST. NO FAULTS FOUND EICAS AND PRESSURE LIGHT NORMAL.

Part: GENERATOR — FAULTY (APU) · airframe 86,399 hrs · 13,777 cycles

APU GENERATOR TRIPS. ON GROUND APU GENERATOR KICKED OFF. REPLACED APU GENERATOR.

Part: LATCH — OUT OF ADJUST (NR 1 PYLON) · airframe 86,134 hrs · 13,739 cycles

NR 1 ENGINE PYLON ACCESS INBD & OUTBD DOORS HAVE 6 EA LATCHES OPEN ON AIRCRAFT ARRIVAL. LATCHES NEED TO BE ADJUSTED. REPLACED 7 EA LATCHES, AND 8 LATCH STRIKERS.

Part: RELAY — FAULTY (EVAC SLIDE) · airframe 85,927 hrs · 13,713 cycles

SQUIB TEST 1 EMERGENCY ESCAPE R DOESN'T ILLUMINATE. REMOVED & REPLACED K3 RELAY SLIDE DOOR TEST RELAY REF WDM 25-65-12. WPB 73611 OPS CHECKED NORMAL.

Part: FILTER — FAULTY (CABIN) · airframe 85,840 hrs · 13,700 cycles

ELECTRIC SMOKE SMELL, RTFL. AFTER TAKEOFF, F/A REPORTED ELECTRICAL SMELL-CARD BOARD BURNING SMELL IN THE MID CABIN AREA. BUSINESS CLASS AND ECONOMY PLUS SECTIONS. ONCE UTILITY BUSES TURNED OFF, SMELL DISSIPATED. F/A DIRECTED MM TO SMELL FROM MID CABIN GALLEY, UNABLE TO DETECT ANY TYPE OF ELECTRIC ODOR FROM AC CABIN. OPS CHECKED ALL GALLEY OVENS AND HOT PLATES UNABLE TO DUPLICATE SMELL. REMOVED BOTH LEFT AND RIGHT PREFILTERS AND CHARCOAL FILTERS REF 21-25-02. PER TOMC PERFORM HI PWR RUNS WITH BLEEDS ON AND OFF & CHECK FOR BURNING SMELL IN CABIN. ACCOMPLISHED HIGH POWER RUN WITH BLEEDS ON AND BLEEDS OFF ALSO PACKS ON AND OFF. NO SMELLS NOTED.

Part: OIL COOLER — FAULTY (NR 2 ENGINE) · airframe 85,701 hrs · 13,681 cycles

NR 2 ENGINE-TS AOC MSGS, AOC? 6448-2 ESN 727790 - ENGINE IS DOWNLINKING CH A&B AOC TR CHECK FAIL MSG 351-23. REMOVED NR 2 ENGINE AIR-OIL COOLER. REF AMM 79-21-09 TASK 79-21-09-004-801. REF EG7491-2, REPLACE NR 2 ENGINE AIR-OIL COOLER (HEAT EXCHANGER).

Part: YAW DAMPER — FAULTY (LEFT) · airframe 85,669 hrs · 13,676 cycles

LEFT YAW DAMPER INOPERATIVE. TROUBLESHOT TO BAD LEFT YAW DAMP MODUAL REPLACE SAME AS PER AMM. OPS CHECKS NORMAL. AC REMAINS CAT FULL CAPABLE. INSTALLED BORROWED PART PN 99-222 1-9-0001 SN 0937 MG PN 285T0013-123.

Part: DRIVE ASSY — FAILED (WEATHER RADAR) · airframe 85,538 hrs · 13,657 cycles

WXR FAIL DISPLAYED ON HSI. WXR FAIL ANT DISPLAYED ON HSI IN WXR TEST POS. REMOVED AND REPLACED WX ANT DRIVE ASSY, OPS CHECK GOOD.

Part: SENSOR — FAULTY (FUEL SYSTEM) · airframe 85,489 hrs · 13,651 cycles

FUEL TEMP INDICATION ON FUEL PANEL BLANK. REPLACED FUEL TEMP SENSOR TS168, OPS NORMAL.

Part: SLIDING WINDOW — FAULTY (COCKPIT) · airframe 85,258 hrs · 13,618 cycles

RIGHT SIDE WINDOW HEAT INOPERATIVE. REPLACED WINDOW HEAT CONTROLLER PER MM 30-41-01 PG 401, NO HELP. REINSTALLED ORIGINAL WINDOW HEAT CONTROLLER. INSPECTED WIRES AND LUGS FOR LOOSENESS AND NO DEFECTS NOTED REF WDM 30-41-01. NR 2 WINDOW HEAT CONTROLLER SHOWED FAULT FOR NR 2 WINDOW. REPLACED NR 2 FO SLIDING WINDOW AMM. OPERATIONAL CHECK GOOD AMM.

Part: SWITCH — STUCK (FUEL PUMP) · airframe 85,204 hrs · 13,610 cycles

LEFT FWD FUEL PUMP SWITCH STUCK IN 'ON' POSITION. REPLACED SWITCH.

Part: SWITCH — DIRTY (FAN) · airframe 84,681 hrs · 13,542 cycles

RT RECIRCULATION FAN LIGHT FAILS TO TEST. LIGHT WORKS BY OPERATING THE RECIRCULATION FAN SWITCH. THE LIGHT DID NOT WORK WHEN USING THE LIGHT TEST SWITCH. CLEANED SWITCH, OPS CHECK NORMAL

Part: BULB — INOPERATIVE (ESCAPE SLIDE) · airframe 84,610 hrs · 13,534 cycles

RIGHT EMERGENCY ESCAPE SLIDE RIGHT TEST ONE INOPERATIVE. RESEATED BULB IN TEST PANEL, OPS CHECKED GOOD.

Part: ACTUATOR — LEAKING (RUDDER) · airframe 83,713 hrs · 13,416 cycles

HYDRAULIC FLUID LEAKING FROM BOTTOM OF TAIL AT 10 DROPS PER SECOND. RUDDER RATIO ACTUATOR LEAKING. REPLACED RUDDER RATIO CHANGER ACTUATOR IAW MM. OPS AND LEAK CHECKED NORMAL.

Part: CONTROL UNIT — FAULTY (AILERONS) · airframe 83,641 hrs · 13,406 cycles

WITH HYD ON, RIGHT INBOARD AILERON BANGING AND SHAKING ACFT. REPLACED RIGHT 3R SCM, TEST PASSED.

Part: OIL SYSTEM — LEAKING (APU ENGINE) · airframe 83,641 hrs · 13,406 cycles

APU FAULT TWICE. FOUND NO OIL IN APU TANK, AND APU COMPARTMENT OIL SOAKED. REPLACED APU PER MM.

Part: STIFFENER — CRACKED (BS 246 FLOORBEAM) · airframe 83,589 hrs · 13,398 cycles

BS 246 FLOORBEAM VERTICAL STIFFENER ON FWD SIDE AT RBL 16 CRACKED IN RADIUS. FABRICATED AND REPLACED VERTICAL STIFFENER, REPAIRED AFT MOUNTING BRACKET AND PULLEY BRACKET PER SRM'S. OPS CHECKED GOOD PER AMM. MAJOR REPAIR

Part: TRACK — WORN (R1 DOOR) · airframe 83,589 hrs · 13,398 cycles

R1 DOOR UPPER FWD TRACK WORN. REPLACED DOOR UPPER TRACK PER SRM. REPLACED TROLLEY ROLLERS PER AMM. ACCOMPLISHED DOOR ADJUSTMENT AND TEST PER AMM, OPS CHECKED GOOD.

Part: STRUCTURE — CORRODED (BS 955, RBL 12) · corrosion level 2 · airframe 83,589 hrs · 13,398 cycles

CORROSION ON CANTED DECK AT STA 955, RBL 12. REMOVED CORROSION PER SRM. ACCOMPLISHED HFEC OF HOLES PER NDTM 51-00-19, PRT 6, NO CRACKS NOTED. ACCOMPLISHED FHRS FOR THICKNESS PER NDTM 51-00-16, PRT 6. FLAP PEENED AREA PER SRM 51-20-06, ECRA 5710-02234, AND EA PT67-57-001.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 83,589 hrs · 13,398 cycles

EMERGENCY LIGHT CEILING ABOVE SEATS 6AB INOP. REMOVED AND REPLACED LIGHT BULB IAW 33-51-04.

Part: OXYGEN MASK — MISINSTALLED (PAX COMPARTMENT) · airframe 83,589 hrs · 13,398 cycles

PASSENGER CABIN, PAX O2 MASKS IMPROPERLY PACKED. REPACKED ALL PASSENGER O2 MASKS.

Part: SHEAR TIE — CORRODED (BS 1562 S39L/R) · corrosion level 2 · airframe 83,589 hrs · 13,398 cycles

FUSELAGE BS 1562 BETWEEN STRINGERS S-39L-39R SHEAR TIE CORRODED. REMOVED AND REPLACED SHEAR TIE REF SRM51-40-02.

Part: FLOORBEAM — CORRODED (BS 1153) · corrosion level 2 · airframe 83,589 hrs · 13,398 cycles

AFT CARGO BAY, BS 1153, RBL 23 - 42, FLOORBEAM CAP CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-00-07. FABRICATED NEW FLOORBEAM CAP IAW SRM 51-40-05 AND INSTALLED IAW SRM 51-40-02.

Part: PANEL — UNSECURE (SEAT 26K) · airframe 83,470 hrs · 13,379 cycles

OVERHEAD OXYGEN PANEL HANGING DOWN AT SEAT 26K. SECURED PANEL.

Part: CONTROL PANEL — SMOKE (CARGO DOOR) · airframe 83,459 hrs · 13,376 cycles

FWD CARGO DOOR CONTROL PANEL. SMOKE OBSERVED COMING FROM PANEL DURING DOOR OPERATION. AFTER COMPLETION OF LM3415 AND NO WIRE DAMAGE IS CONFIRMED, INOPERATIVE FWD CARGO DOOR ELECTRICAL FUNCTION PER MEL 5230AB PROCEDURES. ACCOMPLISHED REQ OF LM3415. NO WIRE DAMAGE CONFIRMED. FWD CARGO DOOR ELECT FUNCTIONS INOP PER MEL 5230AB.

Part: WIRE — PULLED (WINDOW HEAT) · airframe 82,949 hrs · 13,312 cycles

LEFT SIDE WINDOW HEAT INOP. FOUND GND WIRE AT LEFT WINDOW 2 CONNECTOR D5872P POS 2 WIRE W624-101O-20 HAD PULLED OUT OF SOCKET, RETERMINATED AND SECURED WIRE. WINDOW HEAT TEST OKAY.

Part: CABLE — SMOKE (FOOD CART) · airframe 82,887 hrs · 13,304 cycles

FOOD CART CONTROLLER CORD 'N51' STARTED SMOKING. CREW SELECTED SWITCH TO OFF, OPENED CB AND DISCONNECTED CART CORD. SMOKE DISSIPATED. RESET CB &CONNECTED CART RAN FOR 15 MINS, INSPECTED PIGTAIL AND CONNECTORS, NO SIGN OF DAMAGE OR SMOKE-SUSPECT POSS PROBLEM IS CART OR FOOD IN CART-TAGGED CART FOR INSP BEFORE RE-USE, PULLED CB AND PLACARDED. REPLACED CART CONTROLLER & CABLE, NO HELP. RESET CB, OPS CHECK OKAY. UNABLE TO DUPLICATE FAULT.

Part: GENERATOR — CRACKED (APU) · airframe 82,790 hrs · 13,292 cycles

APU SHUT DOWN ON ITS OWN. FAULT LIGHT ON. FOUND LARGE CRACK IN APU GENERATOR CASING, CAUSING APU OIL LOSS. APU GENERATOR REPLACED AS PER AMM, ALL CHECKED OKAY.

Part: RVDT — FAULTY (LE SLAT) · airframe 82,565 hrs · 13,261 cycles

AFTER FLAP EXTENSION, GOT FLAP SLAT ELEC STATUS MSG AND DURING FLAP SLAT RETRACTION GOT T/E CAUTION LIGHT. REPLACED M548 SLAT TRANSDUCER RVDT PER MM 27-81-11 PAGE 412 AND ACP TESTS PER MM 27-51-00 PAGE 501 AND MM 27-81-00 PAGE 501 SYS PASSED OKAY.

Part: SATCOM — FAULTY (COCKPIT) · airframe 82,558 hrs · 13,260 cycles

NO COMM DISPLAYED ON ACARS DISPLAY UNIT OVER OCEAN. ACARS SENDS OK IN VHF RANGE. CREW COMMENTS: SATCOM CONSTANTLY REQUESTING LOGON. SAMC TEXT: MAINTENANCE REPORT SATCOM SYSTEM INOP HIGH & LOW GAIN. AFTER SAT AND ACARS SYSTEM RESET IDU SHOWS SATCOM ALWAYS IN SEARCH MODE WITH NO COMM DISPLAY. DEFERRED SATCOM AND PULLED CB HFSAT SATCOM AND SATCOM HG. REPLACED BOTH RADIO FREQ UNIT AND ALSO SATCOM DATA UNIT.

Part: RESTRICTOR — DETERIORATED (CABIN) · airframe 82,357 hrs · 13,234 cycles

BLEED AIR LEAK. EXCESSIVE AIR NOISE ABOVE CROSS AISLE JUMP SEAT AFT OF FWD GALLEY. INSPECTED DUCTING ABOVE CEILING, ALL CONNECTIONS LOOK GOOD AND FLOW IS GOOD. FURTHER INSP FOUND AIRFLOW RESTRICTORS DETERIORATED AT THE PLENUM FOR THE OVERHEAD AIR OUTLET ABOVE THE FWD JUMP SEAT. AIRFLOW AND NOISE IS HIGHER BUT NOT EXCESSIVE AND IS ACCEPTABLE. PARTS NEEDED 214T3436-203 4EA. REPLACED THE RESTRICTORS. AIRFLOW IS ACCEPTABLE.

Part: SLAT SYSTEM — FALSE INDICATION · airframe 82,208 hrs · 13,206 cycles

WITH FLAPS BETWEEN 1 AND 5, GET "M548 OTBD SLAT PDU RVDT MISRIG" FAULT ON UNIT. OPERATED FLAPS THROUGH FULL RANGE OF OPERATION TWICE. COULD NOT DUPLICATE PROBLEM.

Part: INDICATOR — DEFECTIVE (COCKPIT) · airframe 82,187 hrs · 13,203 cycles

CABIN PRESSURIZATION VSI RATE GOING FROM 0 TO 2000 FPM RAPIDLY. REPLACED CABIN PRESS INDICATOR, OPS NORMAL.

Part: BLADE — NICKED (COMPRESSOR) · airframe 81,160 hrs · 13,058 cycles

NR 1 ENGINE HAS 2 BLADES NICKED. BLENDED BLADES.

Part: TIE BOLT — BROKEN (MAIN WHEEL) · airframe 80,871 hrs · 13,015 cycles

THE 3R MAIN WHEEL TIE BOLT BROKEN. REPLACED MAIN WHEEL ASSY PER MM.

Part: TIE BOLT — BROKEN (MAIN WHEEL) · airframe 80,871 hrs · 13,015 cycles

THE 2F MAIN WHEEL TIE BOLT BROKEN. REPLACED MAIN WHEEL ASSY PER MM.

Part: BRAKE — DAMAGED (MLG) · airframe 80,871 hrs · 13,015 cycles

THE 2F MAIN BRAKE ASSY DAMAGED DUE TO MAIN WHEEL ASSY TIE BOLT BROKEN. THE 2F MAIN BRAKE ASSY REPLACED AS PER MM.

Part: IDG — FAULTY (NR 2) · airframe 80,714 hrs · 12,995 cycles

RT GEN OFF LIGHT ON IN FLT. P6-4 RH FUEL BOOST CB POPPED. CREW REPORTED HAPPENED JUST AFTER RT GENERATOR TRIPPED. RAN BOTH PUMPS WHILE DOING ENGINE RUN FOR GENERATOR CHANGE. OPS CHECKED NORMAL. REPLACED IDG AND GCU PER MM. RAN NR 2 ENG AND OPS NORMAL.

Part: VALVE — STUCK (CABIN AIR) · airframe 80,348 hrs · 12,931 cycles

ONE TRIM AIR VALVE APPEARS STUCK. AUX FWD VALVE STUCK OPEN, DEFFERED PER MEL PROCEDURE 2. REPLACED TRIM AIR VALVE. OPS NORMAL.

Part: START VALVE — FAULTY (NR 1 ENGINE) · airframe 80,079 hrs · 12,886 cycles

NR 1 ENG START VALVE WILL NOT OPEN USING COCKPIT START SWITCH. REPLACED OF LEFT ENGINE START SWITCH, NO HELP START VALVE DOES NOT OPERATE. REPLACE NR 1 ENG START VALVE AND RESEATED NR 1 ENG N2 SPEED CARD, ENG STARTS NORMAL AND START SWITCH OPERATION NORMAL.

Part: BRAKE — SMOKE (MLG) · airframe 80,380 hrs · 12,939 cycles

ATC REPORTED SMOKE FROM LEFT WHEEL MOUNT AFTER LANDING AND FOD ON RUNWAY. REPLACED 1 AFT TIRE AND BRAKE.

Part: SWITCH — ARCED (LAVATORY DOOR) · airframe 79,821 hrs · 12,843 cycles

ELECTRICAL ODOR NOTICED IN FRONT LAV AREA WHILE SITTING HERE AT GATE. FOUND FWD LAV DOOR SWITCH ARCED, REPLACED SWITCH, OPERATION NORMAL.

Part: WIRE — DAMAGED (CABIN) · airframe 79,578 hrs · 12,809 cycles

LT OVERWING SLIDE EMERGENCY LIGHT L396 INOP. REPAIRED WIRING AT LAMP ASSY PER WDM, OP CHECKS GOOD.

Part: CIRCUIT CARD — FAULTY (RT ENGINE) · airframe 79,070 hrs · 12,735 cycles

RTBL, RT ENG SPEED CARD STS MSG WITH ENGINE RUNNING. FOUND POPPED CB "D24" (ENGINE SPEED SENSE R1) ON P11-4 PANEL, CB WILL NOT RESET. REPLACED N2 SPEED CARD PER MM.

Part: SKIN — DAMAGED (THRUST REVERSER) · airframe 78,974 hrs · 12,720 cycles

NR 1 ENGINE FAN EXIT ACOUSTIC LINER HAS A FOUR INCH CUT. DAMAGE IS LOCATED AT THE 5 O'CLOCK POSITION ON THE INNER C DUCT INNER SKIN. THIS DAMAGE IS ON THE REVERSER COWL INNER AIRSTREAM HALF. SEE SRM 54-33-01 PG2 ITEM 9 FOR SKIN DAMAGE LOCATION. DAMAGE IS 3.25 INCHES IN TOTAL LENGTH WITH 2.5 INCH OF THAT DAMAGE THROUGH SKIN SURFACE. ACCOMPLISHED INTERIM REPAIR PER UA-EVA-80738.

Part: FAIRING — OUT OF RIG (LT ENGINE) · airframe 78,974 hrs · 12,720 cycles

LEFT ENG OUTER SUPPORT STATOR VANE MISSING AEROFOIL SHAPED FAIRING. INBOARD SIDE OF ENGINE LOWER INTERMEDIATE STRUT FAIRING LOCATED AT 5.30 POSITION IS MISSING THE UPPER FAIRING SKIN. OK TO CF PER MM. MUST BE REPLACED BEFORE THE 51ST HOUR OF OPERATION PER MM. REPLACED MISSING FAIRING PER MM.

Part: SIGN — MISSING (CABIN) · airframe 78,780 hrs · 12,691 cycles

EMERGENCY EXIT SIGN MISSING ABOVE REAR OVERWING EXIT AT SEAT ROW 21 SEAT A. REPLACED SIGN COVER.

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 78,777 hrs · 12,690 cycles

NR 1 ENG BLEED, RTFL. LEFT DUCT PRESS SHOWING 5 PSI IN CRUISE AFTER SURGING DURING CLIMB. LEFT ENG BLEED OFF LIGHT ON. ACCOMPLISHED MM, PNEUMATIC SYSTEM HEALTH CHECK, PRSOV FAILED CHECK. REPLACED PRSOV PER MM9, TESTED NORMAL DURING HIGH POWER ENG RUN.

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SY) · airframe 78,777 hrs · 12,690 cycles

L DUCT PRESS FLUX. L DUCT PRESS CYCLING DURING DESCENT. VALVE LOCKED CLOSED. WORK WITH CH1548. 1 EA RELAY 562-1833 SHPD AOM D0403. REPLACED PRSOV PER MM. ACP ENGINE RUN, OPS CHECK NORMAL.

Part: EEC — FAULTY (LT ENGINE) · airframe 78,621 hrs · 12,666 cycles

LT ENG EEC C1 AND C2 DISPLAYED. RAN LT ENGINE TWICE. ONLY EICAS MESSAGE DISPLAYED IS EEC C1. BITE TESTED LEFT PIMU. NO FAULTS OR MESSAGES. NO PREVIOUS HISTORY. DEFERRED. REPLACED LT ENGINE EEC PER MM. RAN ENGINE TWICE, BOTH 'A' AND 'B' CHANNEL OPS NORMAL.

Part: EEC — FAULTY (LT ENGINE) · airframe 78,631 hrs · 12,668 cycles

LEFT ENGINE CONTROL MESSAGE, RTFL. EEC WAS PREVIOUSLY REPLACED AT POSITION 1 PRIOR TO FLT AT IAD FOR EEC C1 MESSAGES. REPLACED EEC ALT STATOR & LT ENGINE.

Part: FAIRING — CRACKED (THRUST REVERSER) · airframe 78,105 hrs · 12,593 cycles

NR 1 ENG OTBD REV 3 EA BLOCKER DOOR FAIRINGS CRACKED THRU FASTENERS. MFG AND INSTALLED NEW MOST LOWER END BLOCKER DOOR FILLER FAIRING AND MFG 2 EA. TEMPORARY 2ND AND 3RD FROM BOTTOM BLOCKER DOOR FILLER FAIRINGS ON NR 1 ENG OTBD REVERSER. WILL CREATE NEW ITEM FOR 2ND AND 3RD PANELS.

Part: FAIRING — CRACKED (THRUST REVERSER) · airframe 78,105 hrs · 12,593 cycles

NR 2 ENG INBD REV 4 EA BLOCKER DOOR FAIRINGS CRACKED THRU FASTENERS, MARKED WITH TAPE. REMOVED 4 EA BLOCKER DOOR FAIRINGS. INSTALLED NEW FAIRING IN NR 2 POSITION AND DRILLED NEW ONE FOR NR3 POSITION. INSTALLED NR3 FAIRING MFG AND DRILLED 4 AND 5 FAIRING IAW TMA 54220.

Part: CONTROLLER — FAULTY (BLEED SYSTEM) · airframe 78,105 hrs · 12,593 cycles

LOW PRESSURE AND BLEED LIGHT. REPLACED CONTROLLER & REGULATOR ON NR1 ENG PRECAUTIONARY FOR LOW PRESSURE AND BLEED LIGHT. ACCOMPLISHED RUN-UP IAW MM, WITH BOTH BLEEDS ISOLATED, PACKS ON DUCT PRESSURES WERE NORMAL & WITHIN PLUS OR MINUS 2 PSI OF EACH OTHER. SHIFTS OCCURED NORMAL IN EACH DIRECTION.

Part: DRIVE UNIT — DAMAGED (TE FLAPS) · airframe 77,946 hrs · 12,569 cycles

SCRAPING SOUND IN MID CABIN FLOOR AREA. FOUND RT INBOARD FLAP DRIVE UNIT GRINDING. POWER DRIVE CONTROL UNIT SUSPECT. PART ON HAND. REPLACED FLAP CONTROL UNIT. NO SCRAPING NOISE HEARD.

Part: VALVE — FAULTY (NR 1) · airframe 77,388 hrs · 12,492 cycles

'L ENG HPSOV' UPPER EICAS MSG WITH LEFT ENG BLEED SELECTED OFF. MSG GOES AWAY WITH WHEN BLEED SELECTED ON. REPLACED L HPSOV, NO HELP. AFTER SEVERAL CYCLES WITH ENG RUNNING BLEED SWITCH ON NO DUCT PSI ALSO BLEED SWITCH OFF LIGHT ILLUMINATED.

Part: VALVE — FAULTY (POS 2) · airframe 77,388 hrs · 12,492 cycles

RT ENG (BLEED) OFF LIGHT ON AND RT ENG BLEED OFF EICAS MESSAGE, WIT RUNNING, ENG BLEED SWITCH ON, LT AND RT ISOLATION VALVES CLOSED, AC PACK SELECTED ON, AND DUCT PSI IS ZERO. OFF LIGHT STAYS ON WHEN N1 IS ABOVE. REPLACED RT ENG PRSOV. OPS NORMAL.

Part: CONTROLLER — FAULTY (POS 2) · airframe 77,388 hrs · 12,492 cycles

NR 2 ENGINE BLEED INOP WITH ENGINE BLEED SWITCH ON. REPLACED HIGH STAGE REGULATOR AND CONTROLLER AND HIGH STAGE VALVE. OPS NORMAL.

Part: FAN — FAULTY (SUPPLY) · airframe 77,371 hrs · 12,489 cycles

FWD EQ SUP FAN 1 STATUS MESSAGE. REPLACED FAN, NO HELP. FAN RUNS FOR 6-7 MINUTES AND STOPS. REPLACED VIBRATION MONITOR PER AMM, NO HELP. REPLACED FAN AGAIN. OPERATIONS NORMAL.

Part: CONTROLLER — FAULTY (PRIORITY VALVE) · airframe 77,371 hrs · 12,489 cycles

PRIORITY VALVE EICAS MESSAGE CAME ON AT 1000 FT & WENT OUT AFTER 30 SEC AND REPEATED THEN STAYED OUT. REPLACED PRV CONTROLLER PER MM. ACCOMPLISHED ENG HIGH PWR RUN. BLEED COMES ON MOMENTARILY AT 50 PERCENT N1.

Part: PRIORITY VALVE — FAULTY (RT ENGINE) · airframe 77,363 hrs · 12,488 cycles

RIGHT ENG PRV LIGHT MOMENTARILY ON TAKEOFF ROLL AND TWICE IN DESCENT WITH REDUCED POWER. REPLACED RT ENG PRV AS PER MM. ALL OPS AND IND NORMAL. PROBLEM RECURRED ON NEXT SEGMENT. REPLACED PRV NR 2 ENGINE IAW AMM. RAN ENGINE FOUND LIGHT FOR ENGINE STILL FLICKERS AFTER 55 N1. REMOVED AND REPLACED RIGHT ENG BLEED AIR CONTROL CARD ASSY AS PER MM, PERFORMED ENG RUN, OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 77,262 hrs · 12,473 cycles

EMERGENCY LIGHT INOP FWD OF DR2L. REPLACED BATTERY PACK, CHECKS GOOD.

Part: WIRE — MISWIRED (EMERGENCY LIGHTS) · airframe 76,718 hrs · 12,403 cycles

EMERGENCY LIGHT SWITCH AT THE AFT F/A PANEL DOES NOT WORK WHEN EMERGENCY SWITCH IN THE FLIGHT DECK IS IN THE ARM MODE. REMOVED CONN D1650 AT AFT F/A PANEL, (WITH FL DK SW IN ARM) FOUND PINS 24 AND 25 HAVE NO CONTINUITY WHEN EMER LIGHT SW ACTIVATED. FOUND "EMERGENCY LIGHTS. OFF-WING ESCAPE LT" CB ON P11-6 TRIPS WHENEVER AFT F/A EMERGENCY LIGHT SWITCH ON WITH FLT DECK EMERGENCY LIGHT SWITCH TO ARM POS. REPLACED "AFT ATTEND. EMERGENCY LIGHT SWITCH" AT P22 -- STILL NO HELP. FOUND SHORT BETWEEN PIN 12 CONN, D5086J AND PIN 30 CONNECTOR D5154J AT P25 IAW WDM. POSSIBLE MISWIRING AT TB162. :COA 661101 WRITTEN 13DEC07 & ACP BY GSO. FOUND WIRE W1064-043-22 CONNECTED TO YA12 ON TB162 INSTEAD OF Z10 ON TB162, RECONNECTED IAW WDM, OPS CK OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 76,718 hrs · 12,403 cycles

FLOOR EEL AT LH AISLE BY AFT LAV INOP. NEED TO REMOVE DOGHOUSE AFT OF SEAT 39AB FOR ACCESS TO FEEDER CABLE RUN. REMOVED STORAGE UNIT BEHIND SEAT 39AB TO REPLACE ESCAPE PATH LIGHT STRIP. REPLACED BATTERY BEHIND LT AIR GRILL AT LOCATION PLACARD. OPS CHECKED NORMAL.

Part: EEC — FAULTY (LT ENGINE) · airframe 76,635 hrs · 12,390 cycles

LEFT ENG CONTROL STATUS MESSAGE. MESSAGES 'EEC CHL A CONTROL', EEC CHL B LOSS POWER, EEC CHL B CHL FAIL, EEC CHL B CONTROL, EEC CHL B FAULT CAT 2, 352-29, 350-16 & 350-14. REPLACED EEC ALTERNATOR & THE EEC CONTROL PER MM. ERASED ALL MESSAGE & PERFORMED EEC TEST AND TEST 6 IDLE RUN. ALL OPS NORMAL, NO MESSAGES.

Part: WINDOW — FAULTY (POSITION L2) · airframe 76,385 hrs · 12,355 cycles

EICAS MESSAGE; WINDOW HEAT DISPLAYED WINDOW HEAT INOP LIGHTS ILLUMINATED POSITION 6. INOPERATIVE LIGHT DID NOT EXTINGUISHED WHEN SWITCH WAS RECYCLED TO OFF THEN ON. LT NR 2 WINDOW HEAT INOPERATIVE. ACCOMPLISHED WINDOW HEAT CONTROL UNIT BITE PROCEDURE. L2 WINDOW AMBER FAULT LIGHT ILLUMINATED. ACCOMPLISHED WIRING CHECKS IAW TABLE 101, SUSPECT WINDOW AT FAULT. REPLACED L2 SLIDING WINDOW, ADJUSTED IAW SAME REFERENCE, OPS CHECKED GOOD. ACCOMPLISHED WINDOW HEAT TEST IAW MM. OPS CHECKED GOOD.

Part: PLUNGER — OUT OF ADJUST (E/E DOOR) · airframe 76,195 hrs · 12,331 cycles

RECEIVED DOOR EICAS, RTFL. ACFT RETURNED WITH AN E&E DOOR LIGHT ON THE OVERHEAD PANEL ADJUSTED DOOR PLUNGER IAW AMM. LIGHT OFF AND DID NOT COME BACK ON.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 76,195 hrs · 12,330 cycles

LT WING OVERWING EMERGENCY CTR LIGHT IS INOP. RELAMPED LT OVERWING EMERGENCY LIGHT IAW MM. LT WING OVERWING EMERGENCY LIGHT, NOW OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 76,195 hrs · 12,330 cycles

LT WING OVERWING EMERGENCY CTR LIGHT IS INOPERATIVE. RELAMPED LT OVERWING EMERGENCY LIGHT IAW MM. LT WING OVERWING EMERGENCY LIGHT NOW OPS NORMAL IAW MM.

Part: PLUNGER — DISENGAGED (DOOR 2R) · airframe 76,195 hrs · 12,330 cycles

R-2 DOOR INT HANDLE DISENGAGED, PLUNGER STUCK. ACP SMC008 ON NONROUTINE CARD 2215N00452. REMOVED AND REPLACED R2 DOOR INTERIOR HANDLE PLUNGER IAW AMM. OPS CHECK GOOD

Part: REHEATER — FAULTED (LT CONDENSER) · airframe 76,195 hrs · 12,330 cycles

LEFT CONDENSER RE-HEATER FAULTY. REMOVED DEFECTIVE UNIT AND REPLACED LEFT HAND CONDENSER REHEATER. OPS NORMAL.

Part: FUEL CELL — CORRODED (BS 955) · airframe 76,195 hrs · 12,330 cycles

CORROSION AT STA 955, BL0, TOP OF CENTER FUEL TANK. SUPPLEMENTAL DATA UPDATE ACP REPAIR PER PEMCO EA PD87-57-010 AND UAL EVA 74059. THE REPAIR IS MINOR PER EVA. CF9066 IS CREATED TO TRACK FOR 8100-9 WITHIN 24 MONTHS.

Part: BLOWER — FAULTY (CARGO BAY) · airframe 76,195 hrs · 12,330 cycles

PRODUCTION REQUEST AFT CARGO SMOKE DET. SYS , BOTH PRIMARY AND SECONDARY BLOWERS INOPERATIVE. REMOVED AND REPLACED PRIMARY AND SECONDARY AFT CARGO SMOKE DETECTOR BLOWER PER MM. REMOVED AND REPLACED NR 1 BLOWER AFT CARGO SMOKE DET. DELAY RELAY K334 IAW FIM. OPS CHECK GOOD IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,195 hrs · 12,330 cycles

L4 EMERGENCY EXIT LIGHT LOWER INOP. TROUBLESHOT AND FOUND DOOR 4L PATH LIGHT STRIP BAD, REPLACED LIGHT PATH STRIP AND OPS CHECK. OPS CHECK GOOD. WORK WAS ACP ON PEMCO NR 2215N00284.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,195 hrs · 12,330 cycles

EMERGENCY LIGHT STRIPS INOP ON SEAT ROWS 13AB, 8JK, AND 30KJ. RELAMPED EMERGENCY LIGHTS AT 8JK AND PERFORMED EMERGENCY LIGHTS TEST ON 8JK 13AB AND 30KJ IAW G767 AMM.

Part: WIRE — DAMAGED (IDG) · airframe 76,183 hrs · 12,326 cycles

EICAS MSG R GEN OFF DISPLAYED. GEN OFF & FIELD OFF LIGHTS ILLUM & FAILED TO RESET. FUEL WAS SUFFICIENT FOR APU OPERATION FOR THE REST OF FLIGHT. DISCONNECTED IDG AND TAPED OVER IDG DISCONNECT AND LOW PRESS SWITCH. IDG REPLACED. TROUBLESHOT AND FOUND DAMAGE ON WIRE W3538-202R-18, PIN 10 AT D10966. REPAIRED DAMAGED WIRE. PERFORMED OPS CHECK ON NR 2 IDG, OPS CHECK GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 76,126 hrs · 12,318 cycles

FLOOR PROXIMITY EMERGENCY LIGHT IS INOP AT ROW 19 CROSS AISLE. SECURED BATTERY CONNECTOR. CHECKS GOOD.

Part: CONNECTOR — DEFECTIVE (EMERGENCY LIGHTS) · airframe 76,126 hrs · 12,318 cycles

FLOOR PROXIMITY EMERGENCY LIGHT AT FWD ENTRY CROSSAISLE IS INOPERATIVE. REPLACED CONNECTOR. TESTS OKAY.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 76,126 hrs · 12,318 cycles

FLOOR PROXIMITY EMERGENCY LIGHT IS INOP AT THE LT AISLE MID LAV. SECURED BATTERY CONNECTOR. CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,126 hrs · 12,318 cycles

FLOOR PROXIMITY EMERGENCY LIGHTS ARE INOP AT LT AISLE NEXT TO THE FWD LAV. REPLACED LIGHT ASSY. TESTS OK.

Part: LIGHT — OBSTRUCTED (CABIN) · airframe 76,126 hrs · 12,318 cycles

CARPETING IS COVERING THE FLOOR PATH (EEL) LIGHTS AT LEFT FWD AISLE NEXT TO FWD LAV. AT RIGHT FWD AISLE NEXT TO FWD GALLEY. AT LEFT AISLE MID LAV. AT RIGHT AISLE MID LAV. SUPPLEMENTAL DATA UPDATE TRIMMED CARPETS AT LEFT AND RIGHT AISLE NEXT TO MID LAVS, FWD AISLE NEXT TO CLOSET AFT OF MAIN ENTRY DOOR AND FWD AISLE NEXT TO GALLEY.

Part: IDG — FAULTY (RIGHT) · airframe 75,999 hrs · 12,297 cycles

RT GEN FAILURE, RTFL SWAPPED GCU. NO HELP. THE IDG RELATED TO THE RTFL WAS CONFIRMED TO HAVE A HARD FAULT RELATED TO ONE OF THE ROTOR DIODES. THE FAILURE OF THE DIODE PREVENTS THE UNIT FROM PRODUCING ELECTRICAL POWER BECAUSE IT PREVENTS THE ROTOR FROM PRODUCING THE REQUIRED EXCITATION MAGNETIC FIELD. REPLACED IDG, LEAK CHECK AND RESERVICED AT ENG RUN.

Part: WIRE — SHORTED (GALLEY CART) · airframe 75,962 hrs · 12,289 cycles

OVEN M61 C/B POPPED, RTFL. FOUND CBS POPPED. FOUND SHORTED PIGTAILS FOR CARTS. REPLACED P61 & P62 PIGTAILS. OPS CHECK OK. RAN ALL OVENS IN ALL GALLEY S FOR 30 MIN OPS CHECK OK.

Part: SHUTOFF VALVE — FAULTED (BLEED SYSTEM) · airframe 75,683 hrs · 12,251 cycles

UNABLE TO START ENGINES DUE TO APU DUCT PRESS AT 20PSI. IAW SAM CYCLED "S23" AND "S24" CB'D AT P11-6 PANEL, NO HELP. FOUND SHUTOFF VALVE FAULTED.

Part: ADC — MALFUNCTIONED (RIGHT) · airframe 75,557 hrs · 12,234 cycles

ADC FAILURE, RTFL. CREW REPORTS SHORTLY AFTER ROTATION AND GEAR RETRACTION, APPEARED TO HAVE A RT AIR DATA SYS FAIL. F/O'S AIRSPEED IND, AND ALTIMETER WOUND UP, GOT FALSE AIRSPEED WARNINGS, RUDDER RATIO, TCAS, AND NUMEROUS OTHER AIR DATA DEPENDENT SYS FAILURES. SHORTLY AFTER THIS OCCURRED, ALL RETURNED TO NORMAL. APPROX 15 MINS LATER, RT AIR DATA FAILED AGAIN. WHEN SWITCHED TO ALT AIR DATA SOURCE, ALL OPS ARE NORMAL. REPLACED RT ADC. PERFORMED PITOT AND STATIC TEST IAW MM. ALL INDICATIONS IN FLT DECK ARE NORMAL WITH NO FLAGS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,535 hrs · 12,230 cycles

LEFT EXIT EMERGENCY LIGHT JUST AFT OF THE FLAP INOP. FOUND LIGHT AFT OF THIS LIGHT ALSO INOP. RELAMPED BOTH BUT NO HELP. T-S REF WDM, RANG ALL 4 (5A) FUSES IN M738 RANG GOOD, M738 IS LOCATED AT SEAT 37ABC. BATTERY PACK M738 TO BE REPLACED IS BY STA 1349 (LEFT AIR GRILL). REPLACED BATTERY PACK, GROUND CHECK NORMAL.

Part: SKIN — PUNCTURED (RT WING TE FLAP) · airframe 75,535 hrs · 12,230 cycles

RT INBD T/E FLAP HAS PUNCTURE ON TOP SIDE. PUNCTURE WITHIN LIMITS IAW SRM. SEALED WITH SPEED TAPE, INSPECT EACH "A CHECK". DO A REPAIR NO LATER THAN THE NEXT "C CHK". SHOP 273 WILL NEED T/E AFT FLAP REMOVED FOR IN SHOP REPAIR. 5 SHIFT SLOT RQSTD FOR TE FLAP REMOVAL AND REPAIR. DAMAGE IS APPROX .750 INCH. RECHECKED T/E REPAIR NO FURTHER DAMAGE IN SURROUNDING AREA.

Part: ADC — FAULTY (POSITION 2) · airframe 75,491 hrs · 12,224 cycles

FO ALT, AIRSPEED AND VSI HAVE OFF FLAGS. OK WHEN AIR DATA ALTN SELECTED. ALSO TCAS FAIL ON HSI. AIR DATA COMPUTER REPLACED. REMOVED AIR DATA P/N. INSTALLED NEW AIR DATA. ALL TESTS PASS WITH SUCCESS.

Part: ACTUATOR — FAULTY (RT WING AILERON) · airframe 75,424 hrs · 12,215 cycles

RT AILERON LOCK OUT ACTUATOR. NEED TO REPLACE RT AILERON LOCK OUT ACTUATOR. IT DID HIT AGAIN. REPLACED RT AILERON LOCKOUT ACTUATOR. OPS CHECKED GOOD.

Part: ACTUATOR — FAULTY (AILERONS) · airframe 75,336 hrs · 12,203 cycles

LT & RT AILERON LOCKOUT MSGS. DUE TO REPEAT WRITE UP OF AILERON LOCKOUT NEED TO REPLACE THE RT & LT AILERON LOCKOUT ACTUATORS. REPLACED THE RT & LT AILERON LOCKOUT ACTUATORS. FUNCTION TESTS OK.

Part: ACTUATOR — FAILED (ELEVATOR) · airframe 75,187 hrs · 12,180 cycles

RT CENTER ELEVATOR PCA FAILS SINGLE HYD SOURCE OP CHECK. RT ELEV MOVES 4-5 SECONDS SLOWER NOSE UP THAN LT SIDE. REPLACED CENTER SYSTEM RT ELEVATOR PCA. OPS GOOD.

Part: WINDOW — CRAZED (COCKPIT) · airframe 74,435 hrs · 12,080 cycles

THE 1ST OFFICER'S FIXED SIDE-AFT WINDOW'S VISIBILITY IS AFFECTED BY DEFECTS, REPLACE FIRST AVAILABLE. CREW COMMENTS: WITH CERTAIN ANGLES OF LIGHT WINDOW VISIBILITY REDUCED. THE 1ST OFFICERS FIX SIDE AFT WINDOW VISIBILITY AFFECTED REPLACE OR REPAIR FIRST MAINT OPS WITHIN 150 FLT HRS. REPLACED WINDOW PER MM. FINAL TORQUE TO BE DONE NO SOONER THAN 1130 AM 3-17-10. WINDOW SEALED AND ELEC CONNECTED.

Part: WINDOW — CRAZED (COCKPIT) · airframe 74,435 hrs · 12,080 cycles

CAPTAIN'S FIXED SIDE-FORWARD WINDOW'S VISIBILITY IS AFFECTED BY DEFECTS. REPLACE FIRST AVAILABLE. CREW COMMENTS: WITH CERTAIN LIGHT ANGLES WINDOW VISIBILITY REDUCED. CAPTAINS FIX SIDE FORWARD WINDOW VISIBILITY IS AFFECTED BY DEFECTS REPLACE OR REPAIR FIRST MAINT OPS WITHIN 150 FLT HRS. REPLACED CAPT WINDOW PER MM. FIRST AND SEC. TORQUE ACCOMPLISHED FINAL TORQUE TO BE DONE NO SOONER THAN 10 AM ON 3-17-10. WINDOW SEALED AND ELEC HOOKED UP.

Part: LAP JOINT — CORRODED (FUSELAGE) · airframe 74,171 hrs · 12,040 cycles

CABIN BLANKETS SATURATED WITH H2O ROW 24. FOUND AFTER PRESSURIZING. LOW AND HIGH GAIN ANT, ADF ANTENNA AND LAP JOINT. REMOVING INTERIOR TO AGAIN ACCESS TO LAP JOINT AREA AND WET INSULATION. INSPECTED AREA. FOUND NO OBVIOUS DEFECTS. REMOVED OLD SEALANT AND RESEALED. FOUND CORROSION UNDER LT SIDE HIGH GAIN ANTENNA WHEN IT WAS REMOVED. REMOVED CORROSION IAW GNMM. CLEANED AREA AND TREATED IAW GNMM. PRIMED AREA IAW GNMM.

Part: VALVE — STUCK (CABIN TEMP) · airframe 74,155 hrs · 12,035 cycles

CHRONIC IMPOSSIBLE TO CONTROL CABIN TEMP IN AUTO OR MANUAL OR STANDBY MODES. ACFT VERY COLD. FOUND TRIM AIR PRESSURE REGULATING VALVE STUCK CLOSED. REPLACED VALVE AND ACCOMPLISHED CHECKS.

Part: AMPLIFIER — INOPERATIVE (SATCOM) · airframe 73,825 hrs · 11,973 cycles

SATCOM INOPERATIVE. AMPLIFIER FOUND FAULTY. REPLACED AMPLIFIER, OP'S CHECKED OK. CALLED SAMC ON SATCOM, ALL CHECKED NORMAL.

Part: WARNING LIGHT — ILLUMINATED (FUEL CONFIG) · airframe 73,821 hrs · 11,972 cycles

FUEL CONFIGURATION LIGHT ON IN FLIGHT. ACCOMPLISHED SERVICE TIP. NO FUEL MOVEMENT NOTED FROM RT TO LT MAIN FUEL TANKS AT THIS TIME. UNABLE TO VERIFY FUEL MOVEMENT BETWEEN RT AND LT MAIN TANK.

Part: CLAMP — BROKEN (NR 1 ENGINE) · airframe 73,812 hrs · 11,967 cycles

NR 1 ENGINE FWD CLAMP ON IP VALVE HAS BROKEN LINKS. LINKS FOUND BROKEN. REPLACED CLAMP.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,812 hrs · 11,967 cycles

RT AISLE EMERGENCY LIGHTS INOP ROW 23 THRU 26. REPLACED BATTERY PACK AND PWR SUPPLY, OPS CHECKED OK.

Part: VALVE — FAULTY (BLEED SYS) · airframe 73,714 hrs · 11,949 cycles

LT BLEED AIR DUCT PRESSURE FLUCTUATES WILDLY AT TAKEOFF & CLIMB. THRUST NORMAL AT CRUISE POWER. REMOVED AND REPLACED PRSOV. RPL HIGH PRESSURE CONTROLLER (P/N 773289-15 (S/N 133), RPL PRV CONTROLLER (P/N 792755-8 (S/N 166). NO HELP. ACP'D PNEUMATIC HEALTH CHK. FOUND NEWLY INSTALLED PRSOV FAILED THE CK. RPL'D PRSOV. NO LEAKS NOTED, NO FAULTS NOTED. OPS CK NORMAL.

Part: CONTROLLER — FAULTY (NR 1) · airframe 73,558 hrs · 11,924 cycles

L HPSOV FLUCTUATES WITH THROTTLES AT IDLE IN DESCENT. DURING PNEUMATIC HEALTH CHECK FOUND HPSOV SLUGGISH AND CONTROLLER FAILING TO COMMAND VALVE CLOSURE. REPLACED VALVE AND CONTROLLER. ALL CHECKS NORMAL.

Part: CHARGER — FAULTY (CABIN) · airframe 72,704 hrs · 11,802 cycles

EXTERIOR EMERGENCY LIGHT INOP AT FUSELAGE AFT OF LT TRAILING EDGE. RELAMP, NO HELP. NEED MORE TIME TO T-S. REPLACED BATTERY CHARGER M738, OP CHECKS NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 72,704 hrs · 11,802 cycles

EXTERIOR EMERGENCY LIGHT INOP AT DOOR 2L. RELAMP, NO HELP. NEED MORE TIME TO T-S. REPLACED BATTERY CHARGER M738, OP CHECKS NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 72,704 hrs · 11,802 cycles

SEAT MOUNTED EMERGENCY EEL LIGHT INOP FROM SEAT ROW 19ABC TO 23ABC. EEL LIGHT COMES ON BUT MOMENTARILY. REPLACED BATTERY AT SEAT 22 ABC, M737, SECURED CONNECTORS M1559.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 72,704 hrs · 11,802 cycles

EXTERIOR EMERGENCY LIGHT INOP AT DOOR 1L. RELAMPED, OPS CHECKED OKAY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,704 hrs · 11,802 cycles

SEAT MOUNTED EMERGENCY EEL LIGHT INOP FROM SEAT ROW 19ABC TO 23ABC. EEL LIGHT COMES ON BUT MOMENTARILY. ORDERED BATTERY PACK. BATTERY LOCATION AT SEAT 22ABC. REPLACED BATTERY AT SEAT 22ABC, M737, SECURED CONNECTORS M1559.

Part: IDG — FAILED (RT ENGINE) · airframe 72,653 hrs · 11,794 cycles

EICAS MSG R GEN DRIVE DISPLAYED. GEN DRIVE LIGHT ILLUM. GEN DRIVE DISCONNECTED. ACP'D BPCU BITE AND CHECKED SCAVENGE FILTER (CLEAN FILTER AND DPI NOT POPPED). RESET AND RAN, NO HELP. REPLACED R ENG IDG AND ALL OPS GOOD. ENG RAN AND NO LEAKS APPARENT.

Part: VALVE — LEAKING (LT ENGINE) · airframe 72,631 hrs · 11,790 cycles

FUEL RUNNING LEAK ON THE FLOW DIVIDER AREA LEFT ENGINE. DURING CHECK FOUND LEAK COMING FROM THE FUEL DISTRIBUTION VALVE. REPLACED VALVE AND TRANSFER TUBE PACKINGS. WET MOTORED ENGINE, NO MORE LEAKS FOUND.

Part: STARTER — FAILED (NR 1 ENGINE) · airframe 72,631 hrs · 11,790 cycles

OBSERVED SPARKS AND OIL LEAKING FROM PNEUMATIC STARTER DURING WET MOTORING FOR FUEL LEAK CHECK. REPLACED PNEUMATIC STARTER, OPS CHECK OK.

Part: O-RING — CUT (HYD PUMP) · airframe 72,424 hrs · 11,760 cycles

HYD QTY DECREASED. QTY STABLE WITH EDP DEPRESSURIZED & ACMP OFF. POS 2 (01=L,02=R). CREW COMMENTS: WITH R PUMPS ON R HYD QTY SYS DECREASED FAST R HYD QTY LT ON. FOUND THE EDP DIFFERENTIAL PRESS INDICATOR LEAKING. FOUND THE O-RINGS WORN/CUT. REPLACED O-RINGS. SERVICED RT HYDRAULIC SYSTEM TO FULL. NO LEAKS WERE NOTED. CLEANED PYLON WITH SOAP AND WATER.

Part: GCU — FAULTY (RT) · airframe 72,276 hrs · 11,732 cycles

RT GEN FIELD OFF LIGHT WON'T RESET. SWAPPED GOOD GEN CONT UNIT, RAN ENG GEN FIELD LIGHT CAME ON AFTER ENG SHUT DOWN. BITE CHK BPCU FAULT MSG. SHORTED PMG, GEN-FIELD, AND WIRING-GEN. FOUND GENERATOR CONTROL UNIT WAS TRIPPED INTERMITTENTLY.

Part: PUMP — INOPERATIVE (NR 2 ENGINE) · airframe 72,149 hrs · 11,713 cycles

FUEL DRIPPING FROM NR 2 ENG AFTER SHUTDOWN, APPROX 70 DPM. INSPECTED NR 2 ENG FUEL LEAK. LEAK APPEARS TO BE COMING FROM VENT HOLE AT FWD LOWER RT SIDE OF FUEL PUMP. STEADY STREAM AFTER SHUT-DOWN. WILL NEED TO REPLACE FUEL PUMP. RECEIVED BOOST PUMP, NEED FUEL PUMP ON W7109 ETA 0658 FLT 705. FUEL PUMP REMOVAL COMPLETE. COMPLETED INSTALLATION OF NEW PUMP AND SAME FMU. LEAK CHECKED GOOD. OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 72,145 hrs · 11,712 cycles

LEFT AFT EXT EEL DOOR SLIDE LIGHT INOPERATIVE. REPLACED BATTERY PACK M738, TEST OKAY.

Part: FUEL TANK — LEAKING (RT WING) · airframe 71,334 hrs · 11,586 cycles

WEEP HOLE INSIDE OF NR 2 ENGINE ON WING LEAKING FUEL AT 80 DROPS PER MINUTE. ACP TANK 2 AND RT WING TANK ENTRY FOUND FUEL SEEPING INTO DRY BAY FROM LOWER FWD O/B SECTION. RESEALED AND LEAK CHECKED WITH 19K FOB. ALL CHECKS OKAY.

Part: ACTUATOR — FAULTY (AILERON) · airframe 71,201 hrs · 11,562 cycles

AILERON LOCKOUT EICAS AND OVERHEAD LT ON. REPLACED RT OTBD AILERON LOCKOUT ACTUATOR.

Part: PUMP — FAULTY (CENTER TANK) · airframe 70,554 hrs · 11,472 cycles

AFTER 3 HRS IN CRUISE RT FUEL QTY 2000LBS LWR THAN LT QTY. REPLACE CTR RT OVERRIDE PUMP REF RT FUEL TANK QUANTITY IMBALANCE. REPLACED CTR RT OVERRIDE PUMP. NEEDS LEAK AND OPS TEST. ACCOMPLISHED OVERRIDE JETTISON OP'S CHECK. LEAK CHECK GOOD.

Part: HYDRAULIC LINE — LEAKING (NR 1 PYLON) · airframe 70,461 hrs · 11,461 cycles

NR 1 ENG, OIL DRIPPING FROM LARGE DRAIN TUBE BOTTOM OF REVERSER COWL. FOUND EVIDENCE OF ACTIVE HYD LEAK INSIDE NR 1 PYLON ACCESS PLATE RT OF PYLON. FOUND TORQUE OF HYD B-NUTS AT INSIDE OF DISCONNECT PANEL OK. APPEARS TO BE COMING FROM ABOVE AND AFT OF ACCESS PLATE OPENING. TIGHTENED SUPPLY LINE. CLEANED ENTIRE AREA, MOTORED AND RAN ENG, CYCLED ALL FLIGHT CONTROLS AND NR 1 REV. NO EVIDENCE FOUND AFTER RUN.

Part: BATTERY — FAULTY (RT SQUIB) · airframe 70,009 hrs · 11,398 cycles

RIGHT EMERGENCY ESCAPE SQUIB WON'T TEST. REPLACED BATTERY FOR RT SYSTEM. OPS CHECKS NORMAL ON GROUND.

Part: ANTI-ICE VALVE — FAULTY (NR 1 ENGINE) · airframe 69,660 hrs · 11,347 cycles

LEFT ENG ANTI-ICE VALVE DISAGREE LIGHT ILLUMINATED WITH SWITCH IN THE "ON" POSITION. REPLACED NR 1 ENGINE INLET THERMAL ANTI-VALVE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,471 hrs · 11,320 cycles

EXTERIOR EMERGENCY LIGHTS INOP. REPLACED BULB. OPS CHECK GOOD AND ALLOWED BATTERIES TO CHARGE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,471 hrs · 11,320 cycles

RT MID CLOSET FLOOR EEL INOP. REPLACED RT MID CLOSET FLOOR EEL LIGHT BAR AND OPS CHECK GOOD.

Part: SKIN — DELAMINATED (LT ELEVATOR) · airframe 69,471 hrs · 11,320 cycles

LT INBD ELEVATOR UPPER SURFACE OB END DELAMINATED. REMOVED DELAMINATED PLIES AND INSTALLED REPAIR.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 69,471 hrs · 11,320 cycles

CRACKS FOUND ON NR1 PYLON CLOSEOUT ANGLE, 2ND FASTENER FROM INBD EDGE AT 0:00 POS AND 0900 POS. MAJOR REPAIR ACCOMPLISHED: STOPPED DRILLED CRACKS AND INSTALLED FILLER AND STRAP DOUBLER REPAIR.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 69,471 hrs · 11,320 cycles

CRACK ON UPPER FWD RADIUS ON PANEL CUTOUT NR 2 PYLON INBOARD SIDE, PANEL 446BL. MAJOR REPAIR ACCOMPLISHED, STOP DRILLED 2 EA CRACKS. INSTALLED REPAIR DOUBLERS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,279 hrs · 11,286 cycles

EEL FLOOR PATH LIGHTING AT RT MID LAV ARE INOP. REPLACED EEL LIGHT, CHECKS GOOD.

Part: POWER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 69,279 hrs · 11,286 cycles

EMERGENCY FLOOR PATH LIGHTING LEFT AISLE FIRST LIGHT IN FIRST CLASS CABIN IS INOP. REPAIRED POWER FEED LINE. OPS CHECKS GOOD.

Part: CONNECTOR — BROKEN (FUEL FLOW) · airframe 69,279 hrs · 11,286 cycles

CREW REPORTED FUEL CONFIGURATION EICAS ON DESCENT. FOUND ENTIRE CONNECTOR BROKEN AT THE DIFFERENTIAL PRESSURE SWITCH, D11000. REPLACED NR 1 ENG FUEL FLOW CONNECTOR. NR 1 ENGINE, 5 MINUTE IDLE RUN ACCOMPLISHED. NO LEAKS NOTED.

Part: BLADE — DAMAGED (ENGINE) · airframe 68,940 hrs · 11,230 cycles

NUMEROUS FAN BLADES HAVE SMALL NICKS & DENTS ON BOTH NR 1 & NR 2 ENGINES.

Part: FAN BLADE — DENTED (ENGINE) · airframe 68,940 hrs · 11,230 cycles

NUMEROUS FAN BLADES HAVE SMALL NICKS & DENTS ON BOTH NR 1 & NR 2 ENGINES. ALL DAMAGED FAN BLADES BLENDED ON BOTH NR 1 & NR 2 ENGINES.

Part: HYDRAULIC LINE — CRACKED (HYDRAULIC SYS) · airframe 68,827 hrs · 11,212 cycles

HYDRAULIC PROBLEM. RTFL. FOUND HYDRAULIC LANDING GEAR UP TUBE ASSY CRACKED. ALSO 2 OTHER TUBES INTERFERING AND DAMAGING. REPLACED TUBES OKAY. LEAK CHECK CARRIED OUT NO FAULTS FOUND. SURROUNDING AREA CLEANED OKAY.

Part: STARTER — MALFUNCTIONED (LT ENGINE) · airframe 68,500 hrs · 11,160 cycles

L ENG START VALVE WON'T OPEN. START VALVE MALFUNCTIONED. REPLACED STARTER AND STARTER VALVE. ALL CHK NORMAL.

Part: ACTUATOR — FAULTY (RT A/C PACK) · airframe 67,809 hrs · 11,053 cycles

RIGHT PACK INOP LIGHT ON. S/D* FOUND FAULTY ACTUATOR. REPLACED ACTUATOR PER MM 21-53-04, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: MICROPHONE — INOPERATIVE (OXYGEN MASK) · airframe 67,809 hrs · 11,053 cycles

CAPTAIN'S OXYGEN MASK MIC INOP. *S/D* SUSPECT PRE FLIGHT CHECKS. REPLACED NR 1 O2 BOX. AC OK FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (MAIN OIL FILTER) · airframe 67,605 hrs · 11,024 cycles

CREW REPORTS: RT ENG "OIL FILTER MSG AT ENGINE START, MSG CLEARED AFTER ENG START TOOK 15 SEC , OAT WAS 15C & OIL TEMP WAS BELOW 35C". DEFERRED. MAIN OIL FILTER TO BE REPLACED WITHIN 50 FLIGHT HOURS. MAIN OIL FILTER SUBSEQUENTLY REPLACED AT ORD. RAN ENGINE - NO LEAKS, NO FILTER MESSAGE.

Part: COMPRESSOR — STALLED (LT ENGINE) · airframe 67,375 hrs · 10,989 cycles

LEFT ENGINE COMPRESSOR STALL WHEN THROTTLES ADVANCED. ALSO OCCURRED DURING REVERSER OPERATION. UNABLE TO FIND ANY DAMAGE TO ACCOUNT FOR THE REPORTED STALL. ADDITIONALLY, NO SURGE FLAG WAS SET. BECAUSE OF REPEATED POWERPLANT INTERFACE MANAGEMENT UNIT (PIMU) FAULTS THE EEC WAS REPLACED. SUBSEQUENT HIGH POWER RUNS, AND ACCEL-DECEL CHECKS WERE OK WITH NO STALL OR SURGE. THE AIRCRAFT RETURNED TO SERVICE WITH NO FURTHER PROBLEMS.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 67,307 hrs · 10,976 cycles

EMERGENCY ESCAPE PATH LIGHTING COMES ON FROM ROW 28 TO DOOR 2R (ONLY ON RIGHT SIDE OF A-C). AFTER TROUBLESHOOTING FOUND FAULTY POWER SUPPLY. REPLACED POWER SUPPLY M734 AND OPS CHECKS OK. AC OK FOR SERVICE.

Part: MODULE — MALFUNCTIONED (LEFT) · airframe 67,038 hrs · 10,934 cycles

RUDDER RATIO & AILERON LOCKOUT EICAS MSG. FLIGHT DIVERTED. REPLACED LT STAB TRIM AILERON LOCKOUT MODULE (SAM). SHOP FINDINGS: NFF

Part: LIGHT — INTERMITTENT (ROW 23 AFT) · airframe 67,038 hrs · 10,934 cycles

EXIT LIGHTS 23-AFT ON OFF UNCOMMANDED. AFTER TROUBLE SHOOTING UNABLE TO DUPLICATE PROBLEM. AC OK FOR SERVICE.

Part: CIRCUIT CARD — FAULTY (E&E BAY) · airframe 66,825 hrs · 10,902 cycles

FWD EQUIPMENT VAL EICAS MSG ON WHILE TAXIING OUT. SUSPECT EQUIPMENT COOLING CARD. REPLACED EQUIP COOL CARD IN P50 PNL M867, RAN ENGINES OPS NORMAL. AC OK FOR SERVICE.

Part: ASPIRATOR — LEAKING (EVAC SLIDE)

LEAKING ASPIRATOR. SUPPLEMENTAL DATA UPDATE, POSSIBLE MANUFACTURER DEFECT. REPLACED ASPIRATOR.

Part: SLIDE — DEFECTIVE (R2 DOOR) · airframe 66,618 hrs · 10,867 cycles

NEW SLIDE FOR DOOR 2 RT BECAME UNRAVELED. SLIDE IS IN ACFT NOT INSTALLED. SUSPECT IMPROPERLY PACKED SLIDE. REPLACED SLIDE PER MM 25-66-01. AC OK FOR SERVICE.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 66,583 hrs · 10,858 cycles

LT ENGINE APPROACH IDLE OUT OF LIMITS.

Part: CIRCUIT CARD — MALFUNCTIONED (CABIN TEMP) · airframe 66,425 hrs · 10,834 cycles

UNABLE TO CONTROL TEMPERATURE IN ANY PART OF ACFT USING AUTO, TRIM AIR OFF, OR STANDBY SYSTEM. AFTER EXTENSIVE TROUBLE SHOOTING FOUND FAULTY COOLING CARD. REPLACED EQUIPMENT COOLING CARD M867 RAN ENGINES OP CHECKED GOOD. AC OK FOR SERVICE.

Part: ASPIRATOR — LEAKING (DOOR SLIDE)

ASPIRATOR LEAKS. REPLACED ASPIRATOR LEAK CHECKED GOOD. AC OK FOR SERVICE.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 66,134 hrs · 10,792 cycles

EMERGENCY PATH LIGHTS IN COACH ON THE RIGHT SIDE COMES ON INTERMITTENTLY.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 65,348 hrs · 10,673 cycles

EMERGENCY STRIP LIGHTING BETWEEN ROWS 15 AND 25 CONTINOUSLY FLICKER ON AND OFF. COULD NOT DUPLICATE. OPS CHECKS GOOD.

Part: UNKNOWN — UNKNOWN · airframe 65,085 hrs · 10,633 cycles

NR 2 ENG 'ENG EEC C1' MESSAGE APPEARED ON EICAS. ENGINE OPERATION ABNORMAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 64,202 hrs · 10,495 cycles

EMERGENCY LIGHT PATH IN FRONT OF MIDDLE LT LAVATORY INOP. RECONNECTED PATH CONNECTOR.

Part: SMOKE DETECTOR — INOPERATIVE (LT LAVATOR) · airframe 64,054 hrs · 10,471 cycles

MID LEFT LAVATORY HAS INOP SMOKE DETECTOR. REPLACED SMOKE DETECTOR. OP CHECKS OK FOR SERVICE.

Part: SLIDE — INOPERATIVE (RIGHT) · airframe 63,993 hrs · 10,461 cycles

RIGHT EMERGENCY ESCAPE SLIDE TESTS INOP DURING SQUIB TEST. REPLACED OFF WING ESCAPE SYS. EMERGENCY BATTERY FOR RIGHT SIDE. (M962) ESCAPE SLIDE SQUIBS TEST NORMAL

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 63,582 hrs · 10,393 cycles

FLIGHT DECK EMERGENCY LIGHT FAILS TO COME ON DURING TEST. 10-11-07 REPLACED EMERGENCY LIGHT ASSY. OP CHECKED OK .

Part: WIRE — EXPOSED (CABIN) · airframe 63,116 hrs · 10,307 cycles

SOME EMERGENCY LIGHT STRIP WIRES EXPOSED. REINSTALLED EEL LIGHTS WITH EXPOSED WIRING. OP CHECKED OK FOR SERVICE.

Part: BRAKE — FIRE (NR 1 MLG) · airframe 63,087 hrs · 10,302 cycles

ON ARRIVAL HAD BRAKE FIRE ON NR 1 FWD MLG BRAKE ASSY.

Part: LIGHT — UNSECURE (CABIN) · airframe 63,028 hrs · 10,292 cycles

EMERGENCY FLOOR LIGHTS 2EF SOME LIGHTS ARE INOP. [08-14-07] SECURED LIGHT STRIP. OP CHECKS OK FOR SERVICE.

Part: LIGHT — UNSECURE (CABIN) · airframe 63,028 hrs · 10,292 cycles

EMERGENCY STRIP LIGHTING IN FIRST CLASS IS LOOSE. [08-14-07] RESECURED STRIP LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,028 hrs · 10,292 cycles

THE 27A EMERGENCY FLOOR LIGHTS INOPERATIVE. [08-14-07] FOUND CUT IN CABLE ASSY. SPLICED CUT STRIP. TESTS OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,979 hrs · 10,285 cycles

EEL INOP IN AISLE AFT OF MED 1L. REPAIRED FLOOR-MOUNTED EEL PER MM 33-51-10.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 62,964 hrs · 10,282 cycles

FLOOR MOUNTED EEL LIGHTS INOP RIGHT SIDE IN F-C. FLOOR MOUNTED CONNECTOR HAS BEEN DAMAGED. [08-14-07] FLOOR MOUNTED CONNECTOR HAS BEEN DAMAGE BY CLEANERS. -RPR-:REPAIRED FLOOR-MOUNTED EEL PER MM 33-51-10.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 62,651 hrs · 10,225 cycles

FWD PIT CARGO FLOORBEAM FRAME WEB HAS GOUGES ON FWD FRAME AT STA 654 AND LBL29. REMOVED DAMAGED SECTION OF WEB. FABRICATED AND INSTALLED A REPAIR DOUBLER.

Part: ACCESS PANEL — CRACKED (NR 2 PYLON) · airframe 62,651 hrs · 10,225 cycles

NR 2 PYLON FWD OF ACCESS PNL NR 442BR WEB FWD OF FUEL FEED LINE IS CRACKED. INSTALLED DOUBLER REPAIR.

Part: WIRE — PINCHED (BS 857) · airframe 62,651 hrs · 10,225 cycles

MAIN CABIN EMERGENCY EXIT LIGHT WIRES ARE PINCHED. REPAIRED PINCHED WIRES TO L977 AT STA 857, LBL 85 PER WDM 33-51-14 AND BSWPM 20-10-13. OPS TESTS GOOD PER MM 33-51-01 ON NON ROUTINE E2116I.

Part: BUSHING — MIGRATED (RT STRUT) · airframe 62,651 hrs · 10,225 cycles

RIGHT STRUT, DIAGONAL BRACE ATTACH FITTING, INBOARD BUSHING MIGRATED. [08-08-07] REPLACED BUSHINGS PER MM 54-53-90, REPAIR 4. AIRCRAFT OK FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (RT PYLON) · airframe 62,651 hrs · 10,225 cycles

RIGHT PYLON STRUT OUTBOARD MIDSPAR FITTING, OUTBOARDD LUG BUSHING MIGRATED. [08-08-07] REMOVED AND REPLACED BUSHINGS PER SRM 54-53-90, REPAIR 3. MID-SPAR FITTING OK FOR SERVICE.

Part: BUSHING — MIGRATED (RT PYLON) · airframe 62,651 hrs · 10,225 cycles

RIGHT PYLON STRUT, INBOARD MIDSPAR FITTING, INBOARD LUG BUSHING MIGRATED. [08-08-07] REMOVED AND REPLACED BUSHINGS PER SRM 54-53-90, REPAIR 3. AIRCRAFT OK FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (LT PYLON) · airframe 62,651 hrs · 10,225 cycles

LEFT PYLON INBOARD MIDSPAR FITTING, INBOARD LUG BUSHING MIGRATED. [08-08-07] REMOVED AND REPLACED BUSHINGS PER SRM 54-53-90, REPAIR 3.

Part: SHIM — MIGRATED (NR 2 PYLON) · airframe 54,432 hrs · 8,849 cycles

NR 2 PYLON LOWER AFT SPAR FITTING FOR THE DIAGONAL BRACE HAS SHIM MIGRATION. [08-08-07] REMOVED 4 EACH FASTENERS AT AFT LOWER SPAR FITTING PER SRM 51-40-02. NO GAP OR FURTHER SHIM MIGRATION NOTED. INSTALLED NEW FASTENERS PER MM 54-51-95 AND SEALED AREA. AIRCRAFT OK FOR SERVICE.

Part: BUSHING — MIGRATED (NR 2 ENGINE) · airframe 62,651 hrs · 10,225 cycles

NR 2 ENG, UPPER LINK INBOARD BUSHING MIGRATED AT FWD POINT. [08-07-07] REPLACED BUSHING DURING C-CHECK NR 12 VISIT. ALSO INSTALLED 2 EA REPAIR WASHERS. AIRCRAFT OK FOR RETURN TO SERVICE.

Part: LATCH — BROKEN (EVAC SLIDE) · airframe 62,651 hrs · 10,225 cycles

LEFT OVERWING SLIDE COMPARTMENT NR 3 LATCH BROKEN (MISSING DRIVE PIN AND REAR SPRING). [07-31-07] REPLACED NR 3 LATCH AT LT OVERWING SLIDE COMP DOOR IAW 25-65-09 INSTALLATION TEST OF LATCH GOOD IA W 25-65-09. SLIDE PROBLEM ROOT CAUSE: VIBRATION CAUSES FRETTING IN THE LATCH ASSY & EVENTUAL FRACTURE.

Part: PANEL — DELAMINATED (LT PYLON) · airframe 62,638 hrs · 10,221 cycles

LEFT INBOARD PYLON PANEL IS DELAMINATED & MISSING RIVETS. [07-10-07] REMOVED LEFT INBD PYLON PANEL & CREATED DOUBLER REPAIR PER SRM. INSTALLED DOUBLER, REINSTALLED PANEL. INSTALLED LEADING EDGE FASTENERS TO COMPLETE INSTALLATION OF PANEL. SUSPECT VIBRATION LED TO RIVETS PULLING THROUGH PANEL & UNBOUND PANEL BEGAN TO DELAMINATE.

Part: DOOR — MISSING (LT MLG) · airframe 61,246 hrs · 9,976 cycles

LEFT MLG SHOCK STRUT DOOR FOUND MISSING. A/C FERRIED TO GSO FOR DOOR REPLACEMENT. ACCOMPLISHED DOOR INSTALL AND RIG CHECK. INSPECTED DOOR INSTALLATION PER MM32-12- 00. CORRECTLY INSTALLED. A/C RETURNED TO SERVICE. DOOR EXPERIENCES AIR LOADS DURING LANDING & TAKEOFF. SUSPECT VIBRATION CAUSED FAILURE OF DOOR MOUNTING.

Part: WARNING LIGHT — ILLUMINATED · airframe 60,209 hrs · 9,796 cycles

WITH NORMAL CONFIGURATION FORWARD EQUIPMENT VALVE EICAS MESSAGE AND LIGHT. VALVE IDENTIFIED AS E&E COOLING VALVE. CONDUCTED OP CHECK OF VALVE USING A-CHECK JOB CARDS. VALVE AND SYSTEM CHECKED OK.

Part: MOTOR — FAULTED (LOCKOUT ACTUATOR) · airframe 59,839 hrs · 9,741 cycles

"AIL LOCK" LIGHT WITH ASSOCIATED "AILERON LOCKOUT" EICAS ADVISORY LEVEL MESSAGE DISPLAYED DURING HIGH SPEED FLIGHT. CONFIRMED RT AILERON LOCKOUT ACTUATOR BAD. REPLACED PER MM27-11-44. FINAL CHECK GOOD. RETURN AC TO SERVICE. DAMAGED ACTUATOR MOTOR. SUSPECT VIBRATION & NUMBER OF CYCLES.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 59,141 hrs · 9,620 cycles

A -FWD EQPT OVHT- EICAS DISPLAYED, SELECTED STBY AND AFTER 7 MINS -FWD EQPT OVHT- MESSAGE RETURNED. APPARENTLY, EICAS MESSAGE APPEARED DUE TO HIGH AMBIENT TEMP AT IAD (99F), & INOP APU BLEED FOR AIRCONDITIONING ON GROUND. SUPPLIED GROUND A-C, RESET EQUIP COOLING SYSTEM, & MESSAGE DID NOT RETURN. HOT DAY & INOP APU CAUSED OVERHEAT.

Part: ADC — FAILED (E/E BAY) · airframe 58,906 hrs · 9,582 cycles

FLIGHT DIVERTED TO JFK DUE TO A FAILED AIR DATA COMPUTER. REPLACED LT ELECTRONIC ATTITUDE DIRECTION INDICATOR (EADI) PER MM 34-22-03, 401. CLEANED AIR VENTS ON RT EADI PER 34-22-00. OPS CKD BOTH EADI'S IN PRIMARY AND ALTERATE FOR APPROX 4 HRS. ALL SYS FUNCTIONED NORMALLY. SUSPECT SUBCIRCUIT FAILURE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,365 hrs · 9,350 cycles

FOUND A-ZONE AND MOST AFT LEFT EEL FLOOR LIGHTS OUT.

Part: SUPPORT — LOOSE (RT OWING SLIDE) · airframe 57,365 hrs · 9,350 cycles

RT OVERWING SLIDE LACING ATTACH NYLON FINGERS, 8 BROKEN, SUPPORTING TUBE LOOSE, LAYING ON SLIDE COMPARTMENT LWR SURFACE. ROOT CAUSE APPEARS TO BE OVER TIGHTENING DURING SLIDE OVERHAUL.

Part: PIN — CRACKED (LT MLG) · airframe 57,365 hrs · 9,350 cycles

DURING ULTRASONIC INSPECTION OF LT MLG BOGIE PIN, CRACK INDICATION WAS FOUND. INITIAL ULTRASONIC TEST INDICATED CRACKING. THEREFORE, THE PART WAS REPLACED WITH A NEW -5. SUBSEQUENT TESTING REVEALED THAT THE PART WAS NOT CRACKED.

Part: PIN — CRACKED (RT MLG) · airframe 57,365 hrs · 9,350 cycles

RT MAIN LANDING GEAR BOOGIE PIN SHOWS CRACK. INITIAL ULTRASONIC TEST INDICATED CRACKING. THEREFORE, THE PART WAS REPLACED WITH A NEW -5. SUBSEQUENT TESTING REVEALED THAT THE PART WAS NOT CRACKED.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 56,201 hrs · 9,158 cycles

NOSE WW BULKHEAD HAS DAMAGE. AUX NOSE JACK ACCIDENTALLY OVERLOADED. BOEING AOG TEAM PERFORMED PERMANENT STRUCTURE REPAIR TO STATION 287 BULKHEAD ASSY AND REPLACED DAMAGED SKIN PANEL.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 56,027 hrs · 9,117 cycles

NR 1 ENGINE COMPRESSOR STALL AND AUTO SHUTDOWN. ABORTED TAKEOFF AT 50 KIAS DUE TO COMPRESSOR SURGE. CAPT REPORTED STRONG X-WIND AT 20 GUSTING 33. FOUND METAL IN THE TAILPIPE. ENGINE REPLACED AT IAD. ENGINE RETURNED TO LESSOR ON 06/08/05 WITHOUT BEING DISASSEMBLED.

Part: RELAY — FAILED (NR 1 EVAC SLIDE) · airframe 55,355 hrs · 9,002 cycles

LEFT SQUIB ON NR 1 ESCAPE SLIDE WILL NOT TEST. REPLACED RELAYS K3, K4, K5, & K6 ON M1135 MODULE ABOVE LEFT AFT OVERWING DOOR PER WIRING DIAGRAM 25-65-11 AND PERFORMED REPETITIVE ITERATIONS OF SQUIB TEST. ALL CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (SLIDE LIGHT) · airframe 54,885 hrs · 8,928 cycles

POSITION 1 EMERGENGY ESCAPE SLIDE SQUIB LIGHT FAILED TO ILLUMINATE DURING TEST. DEFECT CAUSED BY LOW BATTERY. REPLACED LEFT HAND BATTERY PACK.

Part: BRAKE — SMOKE (MLG) · airframe 54,870 hrs · 8,925 cycles

HEAVY SMOKE COMING FROM 4F MAIN TIRE WHEN TAXIING INTO GATE. BRAKE MR 32357 DASH 2181 REPLACED. 4F TIRE REPLACED. 3F TIRE REPLACED AS MATE. CLEANED INSIDE 4F AXLE AND FOUND PAINT DISCOLORATION. OUTSIDE OF AXLE FOUND NO DAMAGE TO CADMIUM PLATING. ACCOMPLISHED BOROSCOPE OF 4F AXLE, FOUND DISCOLORATION OF GREEN PRIMER, ACCOMPLISHED HEAT DAMAGE INSP.

Part: ARM — CRACKED (TE FLAP) · airframe 54,432 hrs · 8,849 cycles

LT IB AFT FLAP, IB HINGE ARM CRACKED BOTH SIDES AT ATTACH POINT TO MAIN FLAP. REPAIRED & INSTALLED FITTING.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 54,432 hrs · 8,849 cycles

RIGHT WING INBOARD MAIN FLAP REAR SIDE LINKAGE SUPPORT FITTING CRACKED, INBOARD AND OUTBOARD SIDES. MAJOR REPAIR ACCOMPLISHED. REPAIRED & INSTALLED SUPPORT FITTING.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,432 hrs · 8,849 cycles

MID CABIN SEAT TRACK AT STA 725 AND STA 759, APPROX LBL 90, AFT END CRACKED. *S/D* DAMAGED SEAT TRACKS WERE REPLACED.

Part: CONNECTOR — LOOSE (EVAC SLIDE) · airframe 52,509 hrs · 8,512 cycles

LT OVERWING SLIDE SQUIB TEST FAILED. PROBLEM CAUSED BY LOOSE CONNECTORS. PROBLEM CLEARED BY RE-SEATING CONNECTORS ON BACK OF FLIGHT DECK PANEL.

Part: ENGINE — VIBRATION (NR 2) · airframe 52,470 hrs · 8,505 cycles

REPORTS OF VIBRATION NR 2 ENGINE. DUE TO REPORTS OF ENGINE VIBRATION THE ENGINE WAS BOROSCOPED, CHIP DETECTORS INSPECTED AND INLET AND EXHAUST CHECKED. NO DEFECTS NOTED. THE ENGINE THEN HAD A TRIM BALANCE AND RETURNED TO SERVICE.

Part: SQUIB — INOPERATIVE (ESCAPE SLIDE) · airframe 52,252 hrs · 8,470 cycles

LEFT OVERWING ESCAPE SLIDE SQUIB TEST LIGHT DOES NOT WORK WHEN PRESSED TEST NR 1. RESEATED PLUGS ON BACK OF TEST PANEL - -TESTS OK.

Part: RADAR — INOPERATIVE (WEATHER RADAR) · airframe 50,342 hrs · 8,161 cycles

RETURNED TO FIELD DUE TO INOP WEATHER RADAR. THE WX RADAR R-T. SHOP FINDINGS FOR THE REMOVED WX RADAR R-T WERE LOW POWER OUT. THIS CONDITION WAS CORRECTED IN THE SHOP BY REALIGNING THE FREQUENCY MULTIPLIER OF THE UNIT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 48,372 hrs · 7,830 cycles

EXTERIOR EMERGENCY LIGHT INOPERATIVE AFT OF LEFT WING. RELAMPED LIGHT.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 48,145 hrs · 7,791 cycles

EMERGENCY EXIT LIGHT FWD UPPER CORNER OF DOOR 2R AND 2L INOP. REPLACED BATTERY CHARGER AND BATTERY PACK ASSEMBLY.

Part: NUT — LOOSE (NR 1 ENGINE) · airframe 47,905 hrs · 7,750 cycles

A/C EXPERIENCED DROP IN NR 1 ENGINE OIL QTY AND PRESSURE. ENGINE WAS REMOVED FROM A/C AND HOC RUN PERFORMED AT TEST CELL. FOUND NR 1 & 2 OIL SCAVENGE TUBE LEAKING AT 'B' NUT. REPLACED TUBE. IDG CARBON SEAL AT THE MAIN GEAR BOX WAS REPLACED DUE TO THE IDG BEING REPLACED. NO HOC REPORTED AFTER TEST.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,429 hrs · 7,681 cycles

EEL PATH LIGHT STRIP AT RH MID-GALLEY IS INOP. REPAIRED DAMAGED SECTION.

Part: PROBE — MALFUNCTIONED (TAT)

AT FL 370, AUTO THROTTLE AND AUTO PILOT DISENGAGED. TCAS, GROUND PROXIMITY, FLIGHT DIRECTOR, AND TAT INOPERATIONAL. *S/D* REPLACED TAT PROBE AND ANOMALY WAS CORRECTED.

Part: SWITCH — MALFUNCTIONED (NR 2 ENGINE) · airframe 44,444 hrs · 7,159 cycles

NR 2 ENGINE BYPASS OIL LIGHT ILLUMINATED. FOUND OIL FILTER AND CHIP DETECTORS CLEAN. REPLACED OIL FILTER BYPASS SWITCH.

Part: HEAT EXCHANGER — MALFUNCTIONED (LT ENGINE) · airframe 43,031 hrs · 6,900 cycles

STATUS MSG LEFT ENGINE AIR OIL VALVE. SUITABLE EQUIPMENT MAY NOT BE AVAILABLE TO REPAIR ENGINE IN HAVANA. RETURNED TO MIA. REPLACED AIR-OIL HEAT EXCHANGER AND VALVE.

Part: CDU — FAILED (COCKPIT) · airframe 42,997 hrs · 6,894 cycles

RT FMC OVERHEATED SHORTLY AFTER DEPARTURE. A HOT PLASTIC SMELL WAS VERY EVIDENT IN THE COCKPIT. CAPT ELECTED TO RETURN TO IAD. RT FMC HMCDU OVERHEATED, HOT PLASTIC SMELL WAS VERY EVIDENT IN THE COCKPIT. RT HMCDU BECAME INOPERATIVE AND WAS VERY HOT TO TOUCH. REPLACED THE RIGHT HMCDU. SHOP FINDINGS: BURNED TRACE ON THE I/O CARD A5. SHOP REPORTED PREVIOUS HMCDU'S WITH OVERHEATED CARD A5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,462 hrs · 6,801 cycles

MAJOR CABIN FLOORBEAM CORRODED BS 340, RBL 88. CORROSION REMOVAL EXCEEDS SRM LIMITS. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM.

Part: SKIN — DENTED · airframe 42,458 hrs · 6,800 cycles

BULK CARGO DOOR EXTERNAL SKIN DENTED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,458 hrs · 6,800 cycles

BODY STATION 246 RBL 68 FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED FLOOR BEAM.

Part: BATTERY — INTERMITTENT (CABIN) · airframe 35,813 hrs · 5,623 cycles

REAR CABIN EMERGENCY EXIT FLOOR LIGHTING ON RIGHT SIDE BLINKS INTERMITENTLY. *S/D* APR 26 REPLACED BATTERY ASSY M1555 FOR AFT EEL LIGHTING, SYSTEM CHECKS OK. APR 28 AND 30- EEL LIGHTS BLINKING INTERMITTANTLY. MAY 01- REPLACED EEL LEAD-IN CABLE (P/N 5879-1), OP CHECKS GOOD. MAY 26- REPLACED BATTERY ASSY M1556.

Part: INDICATOR — STUCK (COCKPIT) · airframe 35,657 hrs · 5,598 cycles

CAPTAIN''S AIRSPEED INDICATOR STUCK AT 60 KTS. REJECTED TAKEOFF AT 90 KTS. RTB. *S/D* REPLACED CAPTAIN''S MACH AIRSPEED INDICATOR (MASI). ACFT HAS NO SIMILAR FAULTS SINCE MASI REPLACEMENT ON APRIL 13, 2000. UPDATED SHOP FINDINGS 5/16/2000 : TESTED OK. NO FAULTS FOUND. MOTOR BEARINGS WERE REPLACED PRECAUTIONARY.

Part: RELAY — FAILED (FLAP SHUTOFF) · airframe 35,003 hrs · 5,486 cycles

T/E FLAP DISAGREE LIGHT ON SHORT FINAL. FLAPS STOPPED AND REMAINED AT 23 DEGREES. AMBER ALERT. *S/D* A FAULTY T/E FLAP SHUTOFF VALVE RELAY (K351) CAUSED THE T/E FLAP SHUTOFF VALVE TO CLOSE WHICH INHIBITED FLAP MOVEMENT. WITH FLAP MOVEMENT INHIBITED AT 23 UNITS WHILE FLAP HANDLE IS IN THE 25 UNIT DETENT, THE FLAP SLAT ELECT UNIT (FSEU) DETECTED A DISAGREEMENT BETWEEN THE COMMANDED POSITION OF THE FLAP HANDLE AND ACTUAL FLAP POSITION. THIS CONDITION WILL CAUSE THE ''T/E FLAP DISAGREE'' EICAS MESSAGE WITH AMBER ALERT TO ILLUMINATE. THE SUBJECT K351 T/E FLAP SHUTOFF VALVE RELAY WAS REPLACED WITH NEW PART.

Part: BLEED VALVE — FAILED (NR 1 ENGINE)

NR 1 ENGINE NACELLE OVERHEAT. *S/D* ENGINE 2.95 STABILITY BLEED VALVE WAS OPEN ON TAKEOFF. REPLACED 2.95 STABILITY BLEED VALVE, 2.95 BLEED SOLENOID AND 2.95 BLEED PNEUMATIC RELAY VALVE. SOLENOID AND RELAY VALVES TESTED OK. THE 2.95 BLEED VALVE WAS FOUND LEAKING AT THE PISTON RING SEALS PW75-130, WHICH IS ACCOMPLISHED AT VALVE OVERHAUL IMPROVES VALVE PISTON RING SEALS.

Part: SLIDE — DEPLOYED (RT EMER EXIT)

RT WING SLIDE DEPLOYED INADVERTENTLY. SLIDE DOOR HAD 7 INCH HAIRLINE CRACK IN HONEYCOMB. THERE ARE THREE INNER HINGES BROKEN AND FOUR KEEPERS RUPTURED. *S/D* THE SLIDE INADVERTENTLY DEPLOYED WHILE PINNING THE INFLATION CYLINDER. THE DEPLOYMENT WAS HENCE OUT OF TYPICAL SEQUENCE. THE COMPARTMENT DOOR WAS NOT COMMANDED TO OPEN. THE SLIDE INFLATED INSIDE THE COMPARTMENT AND FORCED THE DOOR OPEN, THUS DAMAGING THE DOOR BY CRACKING THE HONEYCOMB, BREAKING THREE HINGES AND RUPTURING THE FOUR KEEPERS. THE ROOT CAUSE WAS HUMAN ERROR.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EMERGENCY EXIT FLOOR LIGHTS FLICKER ON AND OFF ON RIGHT SIDE BETWEEN ROWS 15 TO 20. *S/D* REPLACED EMERGENCY LIGHTS POWER SUPPLY, M1559.

Part: PRSOV — FAILED (RT ENGINE)

RETURNED TO EZE, DUE TO RIGHT ENGINE BLEED VALVE FAILURE. SUPPLEMENTAL DATA UPDATE PRSOV (PRESSURE REGULATING AND SHUTOFF VALVE) FAILED DUE TO CLOGGED MAIN INLET FILTER. REPLACED PRSOV.

Part: OVEN — FIRE (GALLEY)

A SMALL FIRE OCCURRED IN THE AFT GALLEY OVEN. *S/D* FOOD SPILLED ONTO THE BOTTOM OF THE OVEN INSERT RESULTING IN A SMALL FIRE. THE FIRE WAS EXTINGUISHED WITH A HALON FIRE EXTINGUISHER. THE OVEN WAS NOT DAMAGED AS A RESULT OF THIS INCIDENT, OPERATIONS CHECK NORMAL.

Part: FAN EXIT CASE — CRACKED (RT ENGINE)

THE RIGHT ENGINE CASE AND VANE ASSEMBLY FAN EXIT HAS A CRACK AT THE 5 O'CLOCK POSITION LOOKING FORWARD. THE CRACK EXTENDS OUTWARD ON THE CASE STIFFENER FLANGE. THE CRACK IS LOCATED ON THE B1 FLANGE. THE CRACK RUNS FROM THE OUTER DIAMETER OF THE FLANGE INTO AN UNUSED BOLT HOLE. A FAN EXIT CASE CRACK IS COMMONLY FOUND DURING ENGINE SHOP VISITS. THE CONDITION WILL BE MONITORED DURING SUBSEQUENT A-CHECKS. PART TOTAL CYCLES, 1,970.

Part: CIRCUIT BREAKER — TRIPPED (AC ELECT SYST)

THE C327 CIRCUIT BREAKER TRIPPED IN FLIGHT, CAUSING THE LOSS OF THE RIGHT 115 VOLT A/C TRANSFER BUSS.