N641UA

Part: DISPLAY — MALFUNCTIONED (ZONE 200) · airframe 132,512 hrs · 20,340 cycles

IFE SCREEN IS INTERMIT ENT. GOES BACK AND FORTH BETWEEN STARTUP AND SHUTDOWN. FA REPORTS CREW TERMINAL IS GHOSTING AND SELECTS ITEMS WITH NO COMMAND. CLEANED SCREEN, COULD NOT REPLICATE FAULT. IFE SYS OPS CHK GOOD. REF 44-25-00

Part: SKIN — GROUND DAMAGE (ZONE 100) · airframe 131,815 hrs · 20,248 cycles

LOADER CAME IN CONTACT WITH THE ACFT AT THE AFT CARGO DOOR, DAMAGE IS LOCATED APPROX. BS 1373, ABOVE STRINGER 29R ON FUSELAGE SKIN WITH PULLED FASTENERS ON SKIN. INSPECTION OF UNDERLYING STRUCTURE REVEALED BOWED FRAME. DAMAGE DEMENSIONS ARE 3.6"X 1.1". BLENDED DAMAGE IAW SRM 51-10-02 AND SRM 53-00-01-1A-1 , REQUESTING HFEC SURFACE INSP TO VERIFY ALL DAMAGE REMOVED AND UT INSP TO VERIFY HOW MUCH MATERIAL REMOVED FOR INITIAL DAMAGE ANALYSIS PERFORMED HFEC COMMON TO THE BLENDED AREA, NO FURTHER DEFECTS NOTED. ALSO PERFORMED ULTRA SOUND REMAINING THICKNESS CHECK, CHEM-MILLED SKIN SHOWS NOMINAL THICK OF 0.185" LOWEST REMAINING THICKNESS OF 0.167" 3.6" BY 1" GOUGE DAMAGE BLENDED WITHIN LIMITS , ONLY REMOVED 10% MATERIAL AND 15% ALLOWED REF SRM 53-00-01-1A-1 TABLE 1 , DETAIL 2 DENT ALSO WITHIN LIMITS AND MEASURES 4.8" WIDE AND 9.1" LONG AND 0.110" DEEP A/Y=43 REF SRM 53-00-01-1A-1 TABLE 1 , DETAIL 3 COMPLETED STEPS 1, 2 AND 3 OF AVO 15518 REV A. DISTANCE TO NEAREST FASTENER IS .275" AND 22.375" TO THE CUTOUT EDGE. DENT MEASURES 9.1"X4.8"X.110". PREVIOUS UPDATE WAS ENTERED IN INCORRECT LP. REF LP 6164228 FOR CORRECT LP. REF AVO15518 REV A. STEP 5. REQUEST INSPECTION FOR REMAINING THICKNESS ON GRID PATTERN. ACP PER AVO 15518 STEP 5. REF PT 4 NTM 51-00-10.

Part: SHEAR TIE — DAMAGED (ZONE 100) · airframe 131,815 hrs · 20,248 cycles

WHEN REMOVING DAMAGED SHEAR TIE FOUND DAMAGE TO FRAME AT BS 1373 BETWEEN S-28R AND S-27R , ACCOMPLISHED HFEC OF CUT OUT AREA STEP 7 REF AVO 15518 REV A. NO CRACKS INDICATED. REF AVO 15518 REV A. COMPLIED WITH STEP 8 WITH A .040 INSURANCE CUT. COMPLETED STES (10)&(11) OF AVO 15518 REV.A, NO CRACKS FOUND. PER AVO 15518 REV A STEP 6, PERFORMED DAMAGE TRIM OUT WITH 2D EDGE MARGIN FOR FILLER. ACCOMPLISHED DUE TO 2D EDGE MARGIN . HFEC SURFACE C/W FOR STEP 7 WITH NO CRACK INDICATION. REF. NDT B767 6-51-00-19. COMPLETED STEP 8 OF AVO 15518 REV A .040 INSURANCE CUT. COMPLIED WITH FRAME DAMAGE STEP 12 - A, B, AND C. PER AVO 15518 REV. C. TRIM RADIUS ARE .50". MANTAINED 63 RA MICROINCHES OR BETTER SKIN ROUGHNESS AND MANTAINED MINIMUM EDGE MARGIN ABOVE 2D. CUT OUT DIMENSIONS ARE L-1.8" X W-0.95". PER STEP 12- D WILL NEED INSPECTION TO PERFORM SURFACE HFEC OF THE TRIMMED EDGE. REF 767 NDT MANUAL PART 6, 51-00-19. C/W AVO15518 REV. C STEP 12.D. PERFORMED HFEC INSPECTION OF THE TRIMMED EDGE. REF 767 NDT MANUAL PART 6,VERIFIED INSTALLATION OF FRAME REPAIR IAW ECRA 5360-02026 AND GMM 09-25-05

Part: CABLE — DISCONNECTED (DOOR SLIDE) · airframe 131,633 hrs · 20,226 cycles

L1 DOOR ESCAPE SLIDE DEPLOYMENT CABLE FOUND DISCONNECTED FROM GIRT BAR. UPON FURTHER INVESTIGATION WITH SLIDE REMOVED FOUND GIRT BAR OUTSIDE OF GIRT BAR HOLDER. REMOVED AND INSPECTED SLIDE NO DAMAGE FOUND, REINSTALLED L1 DOOR SLIDE REF AMM 25-66-01-404-072. C/W GMM 09-25-05 RII FOR INSTALLATION OF L1 DOOR MOUNTED ESCAPE SLIDE PACK REF AMM 25-66-01-404-072

Part: UNKNOWN — ODOR (GALLEY) · airframe 131,570 hrs · 20,219 cycles

BURNING ODOR IN AFT GALLEY AND FA REPORTED UNUSUAL SOUND. REMOVED ALL CARTS FROM AFT GALLEY TO PERFORM A DETAILED INSPECTION IAW AMM 25-31-91-202-001 AND CHECKED OVENS FOR DEFECTS OR ANY BURNING. OPERATED CHILLERS FOR 15MINS IAW AMM 25-31-00-705-001 AND 25-33-00-206-001 TO CHECK FOR ANY ABNORMAL ODORS OR SOUNDS IN AFT CARGO AND NONE WERE FOUND. RAN APU FOR 10MINS IAW AMM 49-11-00-802-002, SHUTDOWN AND APU OPERATED WITHOUT SHUTTING OFF OR MAKING NOISE. NO FURTHER DEFECTS RELATED TO ODOR OR SOUNDS AT THIS TIME. OK TO CONTINUE.

Part: SLIDE — NOT REPORTED (ZONE 800) · airframe 129,832 hrs · 20,003 cycles

FOR TRACKING PURPOSES INFORMATION ONLY, L1 DOOR ESCAPE SLIDE REPLACEMENT SCHEDULED UPDATING SERVICEABLE PARTS TAG FOR L1 DOOR ESCAPE SLIDE TRACKING TAG # 1425358, AS REQUIRED. PARTS USED: 76-2500-9-0001, QTY :1 ROTABLE PARTS CHG:TT # 1425358 SN OFF 1495 PN OFF 76-2500-9-0001.SLIDE, B767S, F OFF 76-2500-9-0001 1495 ON 76-2500-9-0001 0278

Part: SHROUD — DAMAGED (ZONE 200) · airframe 129,807 hrs · 20,000 cycles

SEAT 48F EMERGENCY EXIT LIGHT DAMAGED REMOVED AND REPLACED DAMAGED LIGHT ASSEMBLY REF IFM 25-21-53.

Part: CHILLER — SMOKE (ZONE 900) · airframe 129,680 hrs · 19,986 cycles

AFT CHILLERS SMOKING WITH SMELL REF TO LP 4024883 THIS CHILLER WAS REPLACED FOR THE SAME ISSUES.. REF LOGPAGE 4024883, ISOLATED ISSUE TO AFT GALLEY UPPER CHILLER. INSPECTED BOTH UPPER AND LOWER CANNON PLUGS AND ASSC'D WIRE HARNESSES FOR SIGNS OF BURNING OR ARCING, NONE FOUND. ALSO, ISOLATED GALLEY VENT FAN 1 AND 2 FOR T/S, NO ABNORMALTIES NOTED. FOUND BAD ODER PRESENT WHEN ONLY UPPER CHILLER WAS RUNNING. ODOR DISSAPATED AFTER PULLING UPPER CHILLER CB'S. ODOR DID NOT RETURN. THIS LOG IS CLOSED. SEE 4024883 FOR MEL REOPENINING.

Part: CHILLER — FAULTY (ZONE 900) · airframe 129,698 hrs · 19,988 cycles

AFT CHILLERS CAUSING SMOKE CB PULLED SMOKE AND ELECTICAL ODOR DISAPATED VERIFIED NO SMOKE OR ODOR WITH CHILLER DEACTIVATED REQ TOMC APRVL TO DEF BOTH CHILLER IN AFT GALLEY DDP C/W CB PULLED AND SECURED NOC.NEF 2520NB APPROVED DEFERRED AFT GALLEY CHILLER PER NEF DID OPS CHECK OF AFT GALLEY CHILLER PER AMM 25-33-00-730-801 ISSUE COULD NOT BE DUPLICATED RAN CHILLER FOR 1 HOUR OPS CHECKED GOOD NO SMELL OR BREAKERS POPPED R&R AFT GALLEY CHILLER IN CARGO PIT DUE TO SMELL OF SMOKE IN AFT OF AIRCRAFT AND BREAKER BEING POPPED REF AMM 25-33-02 OPS CHECKED GOOD. REOPEN IAH U066009 02MAR25 FOR: CLOSED PREMATURELY ODOR RETURNED PRIOR TO DEPARTURE. MX HAS ISOLATED AND CHECKED WIRING, NO DEFECTS, CHILLER IS DEFECTIVE AND REQUIRES REPLACEMENT PER MX. ODOR IS NOT PRESENT WITH CHILLER DEACTIVATED AND NO ODOR PRESENT. OPS MGR NOTIFIED 3/2 ES. FOUND AFT GALLEY UPPER CHILLER CAUSING FOUL ODOR. WAS ABLE TO ISOLATE BY PULLING CBS FOR BOTH UPPER AND LOWER CHILLERS, CONFIRMED ONLY UPPER CHILLER AT FAULT. INSP'D CONNECTOR PLUGS AND ASSREMOVED AND REPLACED AFT UPPER GALLEY CHILLER REF AMM 25-33-02. VERIFIED NORMAL OPERATION AND COOLING. NO SMOKE OR ODOR NOTED.

Part: OVEN — ODOR (ZONE 900) · airframe 129,663 hrs · 19,984 cycles

ON ARIVAL AT 18K AFT FA REPORTED SMOKE IN AFT GALLY. SHUT OFF OVEN AND IT GOT BETER DEBRIEFED FLT AND CABIN CREW, ELECTRICAL SMELL NOTICED IN AFT GALLEY AREA AND MORE NOTICEABLE ABOVE AFT CTR F/A SEATS. MX DID NOT SEE OR SMELL ANYTHING UNUSUAL IN ACFT AND ALL C/B'S IN AFT GALLEY WERE FOUND IN NORMAL POSITION. CREW FILLED OUT SMOKE/ODOR QUESTIONAIRE FORM 46-6020. RAN CHILLERS AND OVENS AND LOWERED AFT GALLET CEILING. ONLY FOUND STRANGE SMELL IN OVEN 710 AND EVIDENCE OF OLD FOOD BURNED IN OVEN. REMOVED AND REPLACED OVEN 710 IRW 767 25-31-00. OPS CHECK GOOD AT THIS TIME. ISPECTION IRW 767 AMM 05-51-56

Part: UNKNOWN — ODOR (GALLEY) · airframe 129,663 hrs · 19,984 cycles

SMOKE AFT GALLEY, REF LOG 4015078. LOG NEEDS TO BE SIGNED OF WITH REFERENCE TO CONDITIONAL INSPECTION SMOKE OR ODOR IN THE FLIGHT DECK AND OR CABIN, AMM 05-51-56/201 CONDITIONAL INSPECTION COMPLIED ON LP 4015078

Part: CEILING PANEL — OUT OF POSITION (ZONE 200) · airframe 128,921 hrs · 19,886 cycles

LEFT AFT ENTRY DOOR ON EICAS. CLOSED SENSOR S204 SHOWING FAR WITH DOOR VERIFIED CLOSED. REPOSITIONED MOVABLE CEILING PANEL, ALL INDICATIONS NOW GOOD. VERIFIED DOOR OPEN CLOSED OPERATION. CLOSED SENSOR S204 SHOWING FAR WITH DOOR VERIFIED CLOSED. REPOSITIONED MOVABLE CEILING PANEL, ALL INDICATIONS NOW GOOD.

Part: SNUBBER — FAULTY (ZONE 800) · airframe 128,877 hrs · 19,879 cycles

L AFT ENT DOOR EICAS.SENSOR FOR AFT LEFT DOOR SHOWS. NEED SECOND DEFERRAL MEL CARD 33260 TARGET SHOWS FAR UNABLE TO DO PSEU SENSOR TEST TO CHECK SENSOR POSITION. UPON INSPECTION OF DOOR LATCHING MECHANISM, FOUND DOOR LATCH PIN DOES NOT EXTEND FULLY INTO LATCH POSITION. MEL 5271C MEL REJECTED, PLEASE FIX FOUND THAT EXTERIOR HANDLE WAS NOT FLUSH WHEN DOOR IS CLOSED AND HANDLE IN CLOSED POSTION. INTERIOR HANDLE IS FLOPPY AND NOT FULLY LATCH WITH LATCH PIN NOT IN FULLY LATCH POSTION TO SENSOR. WAS ABLE TO PUSH EXTERIOR HANDLE IN TO BE FLUSHED AND FOUND BOTH INTERIOR AND EXTERNAL HANDLES TO LATCH WITH LATCH PIN IN FULLY LATCH POSTION TO DOOR SENSOR. SUSPECT DOOR RIGGING PROBLEM. WHEN CLOSING FROM INSIDE UNABLE TO GET INTERIOR HANDLE TO LATCH FULLY CLOSED. ABLE TO GET INTERIOR HANDLE TO LATCH CLOSE BY APPLYING PRESSURE TO DOOR. WHEN HANDLE IS FULLY LATCH AND FLUSH TARGET SHOWS NEAR. REFER POG PAGE 3077510 FOR PSEU REPLACEMENT GAINED ACCESS TO HANDLE MECHANISM WHEN OPENING INTERIOR HANDLE SPRING HYDRAULIC SNUBBER FEELS WEAK AND NOT ALLOWING INTERIOR HANDLE TO LATCH, CLOSED WHEN CLOSING HANDLE. SUSPECT SPRING HYDRAULIC SNUBBER TO BE FAULTY SUGGEST TO RE-RIG SPRING HYDRAULIC SNUBBER OR REPLACE USING AMM TASK 52-11-31-404-012. REMOVED AND REPLACE LT AFT DOOR SPRING HYDRAULIC SNUBBER REF AMM 52-11-31/401. PERFORMED OPS CHECK NORMAL AND TESTED LT AFT DOORVERIFED INSTALL OF SNUBBER AT DOOR 4 LEFT PER AMM 52-11-31-401 VERIFED CYCLE OF LIGHT IN COCKPIT PER AMM 52-71-00-735-072 NO DEFECTS

Part: SIGN — DETACHED (ZONE 200) · airframe 128,815 hrs · 19,871 cycles

OVERWING EMERG. EXIT SIG N FALLING OFF AT SEATS 30 F-K EMERGENCY SIGN WAS REINSTALLED INTO PLACE OPS OK FOR SERVICE

Part: UNKNOWN — ODOR (COCKPIT) · airframe 128,779 hrs · 19,867 cycles

STRONG SCENT OF ELEC SMOKE IN COCKPIT PERFORM AMM 05-51-56-940-801-C1 OF INTIAL INSPECTION UP TO AND INCLUDING 1.D.(8). FOUND NO SIGNS OF SMOKE OR SMOKE SMELL.

Part: UNKNOWN — ODOR (ZONE 200) · airframe 128,779 hrs · 19,867 cycles

FLIGHT ATTENDANTS INFORM ED US THEY COULD SMELL SMOKE THROUGHT T HE CABIN AND IN THE AFT GALLEY PERFORMED INSPECTION REF AMM 05-51-56-940-801-C1. COMPLETED INSPECTION UP TO STEP 1.D.8 NO SIGNS OF SMOKE OR DAMAGE.

Part: CONTROLLER — INOPERATIVE (HPSOV) · airframe 128,619 hrs · 19,846 cycles

R HPSOV EICAS CAUTION ON TAKEOFF PERFORMED AIR SUPPLY CONTROL SYSTEM BITE TEST REF AMM 36-23-00. REMOVED HPSOV FOR REPLACEMENT. REF AMM 36-11-07 PERFORMED FIM 36-10 FT 865. ALL BLOCKS PASSED. BLOCK 6 SHOWED BITE TEST SHOWS HPSOV AND HPC FAULT. THE VERIFY TEST SHOWS NO FAULTY HPSOV CONTROLLER. CHANGING HPSOV ALSO AS A PRECAUTION. FAULTS. SEE ATTACHED PICTURE INSTALLED HPSOV UP TO STEP G. (HIGH PRESSURE SHUTOFF VALVE R AND R HIGH PRESSURE VALVE CONTROLLER IN REF AMM 36-11-08. INSTALLATION TEST) REF AMM 36-11-07-424-014-002. PARTS USED: REQUIRES HIGH POWER RUN TO ESTABLISH CLEARED FAULT AS REFERENCED 76-3612-9-0003,QTY :1 1203626,QTY :1 IN THIS LOGPAGE. PARTS USED: 00-0593-3-1982,QTY :1 ADD EMP:U401682,U409810 00-0594-3-1790,QTY :1 76-3612-9-0003,QTY :2 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1203626 SN OFF 0614 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1562199 SN OFF 1188 VALVE, SHUTOFF, OFF 76-3611-9-0001 0614 ON 76-3611-9-0001 0834 CONTROLLER, HIG OFF 76-3612-9-0003 1188 ON 76-3612-9-0003 4105 PERFORMED INSTALLATION TEST OF RH HPSOV REF AMM 36-11-07, OPS HIGH POWER RUN REF AMM 71-00-00, BLEEDS OPS CHECK NORMAL. CHECK AND LEAK CHECK GOOD. PERFORMED INSTALLATION TEST OF HPC REF AMM 36-11-08, LEAK CHECK GOOD. PERFORMED AIR SUPPLY DISTRIBUTION OPS CHECK REF AMM 36-11-00, NO DEFECTS. PERFORMED ADD EMP:U352085,U334238

Part: TRANSMITTER — FAULTED (NR 1 HYD SYSTEM) · airframe 128,468 hrs · 19,825 cycles

L HYD QTY EICAS STATUS PG SHOWED 0.0RF OVRHD PANEL QYT LT TROUBLESHOT PER FIM 29-11 TREE 823. COMPARED HYD QUANTITY READING IN FLIGHT DECK WITH READING ON REMOTE SERVICING PANEL. READINGS WITHIN LIMITS. REMOVED AND REPLACED HYDRAULIC FLUID QUANTITY MONITORING UNIT IRW AMM 29-33-01.PARTS USED: 1869947,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1869947 SN OFF 0209 IPC REFERENCE # 29-33-01-01 MONITOR, HYDRAU OFF 76-2932-9-0002 9004 ON 76-2932-9-0002 0511 REMOVED AND REPLACED THE LH RESERVOIR HYDRAULIC FLUID QUANTITY TRANSMITTER PER FIM 29-11 TASK 832 IRW AMM 29-33-02. CLEANED AND INSPECTED CANNON PLUG AT TRANSMITTER. NO DISCREPANCIES NOTED. PERFORMED ENGINE 1 AND 2 ENGINE RUN WITH U346472. FAULT DID NOT REOCCUR. OPS CHECK GOOD AT THIS TIME.PARTS USED: 1567550,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1567550 SN OFF 5035 IPC REFERENCE # 29-11-20-01 TRANSMITTER, HY OFF 99-2936-9-9002 5034 ON 99-2936-9-9002 9020 PHOTOS DURING ENGINE RUN ADD REF LOG PAGE 9566427 FOR CONFERMATION FLIGHT.

Part: PUMP — UNKNOWN (HYD SYSTEM) · airframe 127,487 hrs · 19,705 cycles

R ELEC HYD DEMAND PUMP AUTO INOP THE PUMP RH DEMAND OPS NORMAL IN ON POSITION. REQUEST DEFERRAL MEL 2911K APPROVED FOR MEL 2911K PLACED RH ELEC HYD DEMAND PUMP ON MEL 2911K AS REQUESTED. DDP FOLLOWED. THIS IS NOT A SDR REPORTABLE EVENT PER THE GMM. ATTEMPTING TO UNSELECT SDR FLAG UPDATED SDR WITH ZEROS IN ATTEMPT TO CLEAR INADVERTENT SELECTION OF SDR. NOT SDR EVENT PER GMM *DM* MX NOTE, PLACING A ELECTRIC HYD PUMP 75-2914-9-0001 ON ORDER IN CASE NEEDED AFTER T/S-ING. WORK PERFORMED BY U029187 PERFORMED FIM TASK 29-11-809 RIGHT ELECT HYD DEMAND PUMP AUTO OPERATE AS REQUIRED. NO FAULT MESSAGES

Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR) · airframe 126,883 hrs · 19,632 cycles

BULK CARGO DOOR INDICATION LIGHT AND EICAS MESSAGE ON COCKPIT. RESET BULK CARGO DOOR LIGHT AND EICAS MESSAGE, DOOR CHECKED CLOSED BEFORE DEPARTURE REF 52-71 FAULT TREE 808.

Part: SUPPORT FRAME — CORRODED (BS 522-544 RBL24) · airframe 126,187 hrs · 19,543 cycles

GENERATING ITEM: 166320-0100.0168, SUPPORT TASK: FLC UPPER FRAME CHORD CORRODED @ F.S. 522-544 RBL24.26. REMOVED AND REPLACED FLC UPPER FRAME CHORD SRM 523-544 RBL 24-46 IAW B767 SRM 51-40-02 PARA 7.

Part: FAILSAFE — CORRODED (BS 569) · airframe 126,187 hrs · 19,543 cycles

GENERATING ITEM: 63-5310-1-2503, FLC DOOR CUTOUT LWR SILL F/S 569 FAIL SAFE STRAP HAS CORROSION AT CARGO STOP AFT FASTENER LOCATION, TAG# 8138. LEFAIVE REMOVED AND REPLACED FAIL SAFE STRAP IAW B767 SRM 51-40-02 SECTIONS 4 & 7.

Part: DOOR SILL — CORRODED (FWD CARGO) · airframe 126,187 hrs · 19,543 cycles

GENERATING ITEM: 63-5310-1-2503, FLC DOOR CUTOUT LWR SILL F/S 498 FLOOR STUB FRAME END SPLIT RBL 40-42, TAG# 8122. LEFAIVE.

Part: PANEL — CORRODED (CARGO BILGE) · airframe 126,187 hrs · 19,543 cycles

FLC BILGE CORRODED F.S 497-537 RBL 25-38. REMOVED AND REPLACED BILGE PANEL PN 143T5014U17 AT F/S 497-537 RBL 25-38 IAW B767 SRM 51-40-02 PARA 7.

Part: DOOR SILL — CORRODED (BS 553-560) · airframe 126,187 hrs · 19,543 cycles

FLC DOOR CUTOUT LWR SILL F/S 553-560 INNER CHORD EXFOLIATED. TAG# 7125 (N/R 0100-0147 SAME AREA) LEFAIVE. REMOVED AND REPLACED FLC DOOR CUTOUT LOWER SILL INNER CHORD PN-143T5204-4 AT F/S 553-560 IAW B767 SRM 51-40-02 PARA 7 WORK COMPLETION EC/RA 5300-03068.

Part: FLOOR SUPPORT — CORRODED (BS 551 RBL 41) · airframe 126,187 hrs · 19,543 cycles

FLC DOOR CUTOUT LWR SILL F/S 551 RBL 41 STRAP UPPER SURFACE CORROSION AT SCREW HOLE, BLENDED, FOUND TO BE OUT OF LIMITS. REMOVED & REPLACED PANEL SUPPORT IAW B767 SRM 51-40-02, AMES DOC# 47594FAB02.UNITED EC/RA 2552-01302.

Part: FLOOR SUPPORT — CORRODED (BS 544-566 RBL23) · airframe 126,187 hrs · 19,543 cycles

FLC BS 544-5 66 RBL 23.20 FLOOR SUPPORT INTERCOASTAL IS CORRODED. REMOVED & REPLACED INTERCOSTAL AT STA 544-566 RBL 23.20 IAW B767 SRM 51-40-02 UNITED EC/RA 5328-01000.

Part: DOOR SILL — CORRODED (FWD CARGO) · corrosion level 2 · airframe 126,187 hrs · 19,543 cycles

FLC DOOR CUTOUT LWR SILL F/S 6 10 RBL 40 - 42 FLOOR BEAM CHORD LWR LEG SPLIT, REPLACED FLOOR BEAM CHORD AT FS 610 EBL 40-42 IAW B767 SRM 51-40 -02 PARAGRAPH 7.

Part: FLOOR SUPPORT — CORRODED (FWD CARGO) · corrosion level 2 · airframe 126,187 hrs · 19,543 cycles

FLC DOOR CUTOUT LWR SILL F/S 5 41 RBL 42 FLOOR WEB SUPPORT EX FOLIATED, REMOVED AND REPLACED FLOOR SUPPORT INTERCOASTALL @ F/S 541 RBL42 IAW B767-300 SRM 51-40-02 PAR 7 AND AMES DOC 47594 FAB 04 REV: IR.

Part: SUPPORT ANGLE — CORRODED (CARGO FLOOR) · airframe 126,187 hrs · 19,543 cycles

GEN ITEM 63-5310-1-2503 /// FLC DOOR CUTOUT LWR SILL F/S 598 RBL REMOVED AND REPLACED SUPPORT ANGLE @ F/S 589 RBL 42 IAW B767-300 SRM 51-40-02 PAR 7

Part: DOOR SILL — CORRODED (BS 556-562) · airframe 126,187 hrs · 19,543 cycles

GEN ITEM; 63-5310-1-2503 /// FLC DOOR CUTOUT LWR SILL FS 556-562 RBL 37 FLOOR INTERCOSTAL HAS CORROSION AROUND NUTPLATE PLUS 1 N UTPLATE IS MISSING TAG NO 7127. REMOVED AND REPLACED STRAP PN-143T5014-33 AT FLC DOOR CUTOUT LOWER SILL F/S 556-562 RBL 37 IAW B767 SRM 51-40-02 PARA 7.

Part: PANEL — CORRODED (CARGO BAY BILGE) · airframe 126,187 hrs · 19,543 cycles

GEN ITEM; 166320-0100-0137 /// SUPPORT TASK, FLC BILGE PANEL CORRODED FS 537-600 RBL 25-38.

Part: WEB — CORRODED (CARGO FLOOR) · airframe 126,187 hrs · 19,543 cycles

GEN ITEM 166320-0100-0137 /// SUPPORT TASK : FLC BILGE PANEL CORRODED @ FS 600-632 RBL 25-38.

Part: ANGLE — CORRODED (FLC FLOOR) · airframe 126,187 hrs · 19,543 cycles

FLC DOOR CUTOUT LOWER SILL F/S 536 INNER CHORD AND BEAM "L" ANGLE HAVE UPPER SURFACE FRETTING, TAG #8126. REF AMES (ILN) NRC 166320-0100-0142. REMOVED AND REPLACED "L" ANGLE AT F/S 536 IAW B767 SRM 51-40-02, PAR 7.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 126,187 hrs · 19,543 cycles

FLC DOOR CUTOUT LOWER SILL F/S 566 RLB 41 "L" ANGLE UPPER SURFACE HAS CORROSION. REF AMES (ILN) NRC 166320-0100-0148. REMOVED AND REPLACED "L" ANGLE AT F/S 566, RBL 41 IAW B767 SRM 51-40-02, PAR 7. REF AMES (ILN) NRC 166320-0100-0148.

Part: WEB — CRACKED (NR 1 NACELLE) · airframe 126,187 hrs · 19,543 cycles

#1 PYLON MOST AFT CLOSE OUT WEB IS CRACKED. REF AMES (ILN) NRC 166320-0400-0166. NEW CLOSEOUT WEB P/N 313T3355U233 INSTALLED (M&E 76-7831-3-0155). SEE PARTIAL WORK ACCOMPLISHED ON BACK FOR MORE DETAILS, IAW B767-300 SERM 51-40-02. FORM 46-0024 COMPLETED (SSFR). REF AMES (ILN) NRC 166320-0400-0166.

Part: HEAT SHIELD — CRACKED (#1 PYLON) · airframe 126,187 hrs · 19,543 cycles

#1 PYLON HEAT SHIELD PAN ASSY UPPER WEB CRACKED NEAR DRAIN HOLE AND AT AFT END. REF AMES (ILN) NRC 166320-0400-0175. NEW WEB FABBED AND INSTALLED IAW AMES DOC # 47594FAB01 AND UNITED EC/RA 5456-01044. FORM# 46-0024 C/W. REF AMES (ILN) NRC 166320-0400-0175.

Part: PLATE — WORN (NR 2 NACELLE) · airframe 126,187 hrs · 19,543 cycles

#2 I/B PYLON PANEL 447AL HAS WEAR MARK INTO PANEL AROUND 2 FWD HOLES. ALSO, FLAT SEAL IS NOT CORRECT SEAL. BULB SEAL SHOULD GO THE LENGTH OF THE PANEL. REF AMES (ILN) NRC 166320-0400-0050. #2 I/B PYLON PANEL 447AL BLENDED AND FOUND TO BE OUT OF LIMITS. PARTIAL WORKSHEET #70 1 OF 1. REF AMES (ILN) NRC NEW PANEL WAS FABRICATED IAW B767 DWG DOC #313T3200. SEAL WAS 166320-0400-0050. FOUND TO NOT NEED REPLACED AND WAS REINSTALLED IAW B767 SRM 51-40-02 AND B767 SRM 51-30-03. SEE PARTIAL WORK ON BACK SEE

Part: ANGLE — CRACKED (NR NAC HEAT SHLD) · airframe 126,187 hrs · 19,543 cycles

NR 1 PYLON HEAT SHIELD PAN ASSY UPPER WEB STIFFENER ANGLE CRACKED ( ANGLE LOCATION IS JUST AFT OF DRAIN HOLE) REPORTED BY V921225 NEW ANGLE P/N 313T3355-315UAL WAS FABBED ON CRO WO# C/W. 166323-0400-0003. HOLES LOCATED AND WAS INSTALLED ON NR 0400-0162 AND 0400-0175. HOLE LOCATION IAW B767 SRM 51-40-05. SEE PARTIAL WORK ON BACK FOR MORE DETAILS. FORM 46-0024 (SSFR)

Part: FLOOR SUPPORT — CORRODED (BS 478-497 RBL30) · airframe 126,187 hrs · 19,543 cycles

GEN ITEM; 166320-0100-0137 FLC FLOOR SUPPORT INTERCOASTAL CORRODED @ F.S. 478-497 RBL 30.95 PART WAS REMOVED ON NR 0100-0137 ENT RY NO 5

Part: ACCESS PANEL — MECHANIC ERROR (#7 SLAT) · airframe 126,187 hrs · 19,543 cycles

WHILE GIVING OK TO CLOSE, FOUND NR 7 SLAT INTERNAL ACCESS PANEL 612DB TO HAVE A MISDRILLED FASTENER HOLE. REPORTED BY V932171 FABRICATED NEW PART FOR #7 SLAT PANEL 612DB IAW BOEING DWG# 114T3161. INSTALLED ON J/C 166319-0600-0090. SEE BACK AND PARTIAL WORKSHEET #68 FOR WORK ACCOMPLISHED. REF AMES (ILN) NRC 166320-0600-0092.

Part: WEB — CORRODED (LAVATORY A) · airframe 126,187 hrs · 19,543 cycles

CORROSION ON TOP OF FLOOR STRUCTURE AT AFT IB CORNER OF LAV A AT STA 280.

Part: ANGLE — CRACKED (#1 PYLON) · airframe 126,187 hrs · 19,543 cycles

#1 PYLON INSIDE I/B ARROW HEAD PANEL AT AFT END, L ANGLE IS CRACKED. REF AMES (ILN) NRC 166320-0400-0162. REMOVED DAMAGED ANGLE AND INSTALLED NEW PN 313T3355-287 UAL. SEE CWO NO 166327-0400-0002 FOR PART FAB IAW B767-300 SRM 51-40-02. SEE PARTUIAL WORK ON BACK PWS NO 20 PG 1 OF 1 FOR MORE DETAILS FORM 46-0024 (SSFR) ON NON ROUTINE 166320-0400-0162 FOR DETAILS

Part: STRAP — CRACKED (#1 PYLON) · airframe 126,187 hrs · 19,543 cycles

#1 PYLON AFT V WEB AFT STRAP WHERE STRINGER PANEL ATTACHES IS CRACKED. INSTALLED NEW STRAP PN 313T3380-660 IAW B767-300 SRM 51-40-02. S EE PARTIAL WORK ACCOMPLISHED FOR MORE DETAILS FORM 46-0024 (SSFR ) SEE NON-ROUTINE 166320-0400-0168 FOR DETAILS

Part: ANGLE — CRACKED (R1 DOOR) · airframe 126,187 hrs · 19,543 cycles

GEN ITEM: 63-5310-1-2623. FLOOR SUPPORT BRACKET LOOKS CUTOUT/ BROKE IN TWO PLACES UNDER FLOOR BOARD 2ND IB AT R1 DOOR AT STA 287. REMOVED AND REPLACED BROKEN CAP ANGLE AT STA 287 RBL 39.25 IAW B767 SRM 51-40-02 PARA 7.

Part: FLOOR SUPPORT — CORRODED (BS 524-541 RBL34) · airframe 126,187 hrs · 19,543 cycles

FLC FLOOR SUPPORT INTERCOSTAL CORRODED F.S. 524-541 RBL 33.08.

Part: FLOOR SUPPORT — CORRODED (BS 500-520 RBL25) · airframe 126,187 hrs · 19,543 cycles

FLC INTERCOSTAL CORRODED AT F.S. 500-520 RBL 24.75.

Part: FLOORBEAM — CORRODED (BS 566 RBL38-39) · airframe 126,187 hrs · 19,543 cycles

FLC DOOR CUTOUT LWR SILL F/S 566- RBL 38 & 39 FLOOR WEB SUPPORT ANGLE HAS EXFOLIATION AT NUTPLATES.

Part: FLOOR SUPPORT — CORRODED (BS 588-610) · airframe 126,187 hrs · 19,543 cycles

SUPPORT TASK FLC FLOOR SUPOORT INTERCOSTAL @ F.S 588-610 RBL 33.08 IS CORRODED.

Part: INTERCOSTAL — CORRODED (BS 546-566) · airframe 126,187 hrs · 19,543 cycles

SUPPORT TASK, FLC F.S 546-566 RBL 31.96 FLOOR SUPPORT INSTERCOSTAL IS CORRODED.

Part: SKIN — CRACKED (BS 335 S20R) · airframe 126,187 hrs · 19,543 cycles

EA 5315-01152 SEQ 1331, R1 DOOR CUTOUT FUSELAGE SKIN AFT LOWER CORNER STA 335 JUST ABOVE STRINGER 20R LOWER HOLE HAS CRACK INDICATIONS IN BOTH THE SKIN AND BEAR STRAP WHILE PERFORMING HFEC SCAN.

Part: FLOOR SUPPORT — CORRODED (BS 522 RBL 40) · airframe 126,187 hrs · 19,543 cycles

FLC DOOR CUTOUT LWR SILL F/S 520 RBL 40 FLOOR SUPPORT LWR SURFACE EXFOLIATED.

Part: SKIN — CRACKED (BS 335 S20L) · airframe 126,187 hrs · 19,543 cycles

EA 5315-01152 L1 DOOR LOWER AFTER CORNER FUSELAGE SKIN ONLY AT STA 335 JUST ABOVE STRINGER 20L LOWER FASTENER HOLE HAS A CRACK INDICATION WHILE PERFORMING HFEC OPEN HOLE SCAN.

Part: INTERCOSTAL — CORRODED (BS 588-610) · airframe 126,187 hrs · 19,543 cycles

FLC FLOOR SUPPORT INTERCOSTAL IS CORRODED @ F.S. 588-610- RBL 24.76 (143T5019-32).

Part: FLOOR SUPPORT — CORRODED (STA522-544) · airframe 126,187 hrs · 19,543 cycles

FLC FLOOR SUPPORT @ F.S 522-544 RBL 24.75 IS CORRODED AND SPLIT. REMOVED AND REPLACED FLC FLOOR SUPPORT AT STA 522-544 RBL 24.75 IAW B767 SRM 51-40-02 PARA 7

Part: SHEAR TIE — CORRODED (STA1540) · airframe 126,187 hrs · 19,543 cycles

BS 1540 SHEAR TIE CORRODED- AFTSIDE OF FRAME BETWEEN S-39L & S-39R. DOCUMENTED ON AMES NR 166320-0100-0274. REMOVED AND REPLACED SHEAR TIE PN-140T21026585 ON AFT SIDE OF FR AME LOCATED AT STA 1540 BETWEEN S-39L-S-39R IAW B767 SRM 51-40-0 2 PARA 4 & 7

Part: LIGHT — UNKNOWN (SEAT 30D) · airframe 125,209 hrs · 19,408 cycles

BE PINNACLE TOURIST CLASS SEAT INSPECT {B767-25-3-0075} - IT WAS FOUND EMERGENCY ESCAPE PATH LIGHT SEAT 30D WITH LENS BROKEN REMOVED AND REPLACED EMERGENCY ESCAPE SEAT LIGHT ASSEMBLY # 30D REFER AMM 33-51-10/201. CHECKED OK GOOD FOR SERVICE.

Part: ELT — NONE · airframe 125,209 hrs · 19,408 cycles

DURING A CHECK WAS FOUND ELT ON FWD RH FLIGHT ATTENDANT SEAT WITH BATTERY EXPIRED. PHOTO ADD. REMOVED AND REPLACED ELT ON FWD RH FLIGHT ATTENDANT SEAT, REF AMM 25-60-99. GOOD FOR SVC.

Part: ELT — NONE (LH FA SEAT) · airframe 125,209 hrs · 19,408 cycles

DURING A CHECK WAS FOUND ELT ON AFT LH FLIGHT ATTENDANT SEAT WITH BATTERY EXPIRED. PHOTO ADD. REMOVED AND REPLACED ELT ON AFT LH FLIGHT ATTENDANT SEAT, REF AMM 25-60-99. GOOD FOR SVC. PARTS USED: 99-2560-9-9001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1729736 SN OFF 5782 TRANSMITTER, EM OFF 99-2560-9-9001 5782 ON 99-2560-9-9001 6101

Part: ENGINE — FAILED (ENG 1) · airframe 124,868 hrs · 19,363 cycles

NO1 ENG FAILURE AT V2 LOUD BANG HEARED NO FIRE INDICATION BUT RAN FIRE CHECKLIST. REMOVED AND REPLACED #1 ENGINE, ALL OPS CHECKS AND LEAK CHECKS GOOD AT THIS TIME.

Part: MODULE — FAULTY (RIGHT) · airframe 124,543 hrs · 19,309 cycles

FL350 NORMAL CRUISE.. FLAP INDICATE POS 1 HANDLEUP.VISUALLY CONF IR MED UP. FLAP/SLAT ELEC T/S AS PER FIM TASK REF. 27-51 FAULT TREE 836. FOUND RIGHT FLAP REMAINS FULLY CAT CAPABLE. PARTS USED: 1444363,QTY :1 STABILIZER POSITION MODULE FAULTY. R & R FSPM AS PER MM REF. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1444363 SN OFF 1148 27-58-01, OPS CKS OK. PERFORMED AN AUTOPILOT SYSTEM TEST AS PER IPC REFERENCE # NONE MM REF. 22-10-00/501, OPS CKS. OK. A/C CAT STATUS UNCHANGED. A/C

Part: LAMP — INOPERATIVE (SLIDE LIGHT) · airframe 124,322 hrs · 19,275 cycles

R/H MID DOOR GND SLIDE LIGHT 1EA INOP L391, REPLACED R/H MID DOOR L391 GND SLIDE LIGHT LAMP AND LIGHT TEST FOUND NORMAL REF AMM33-51-06 -902-082 REV 138.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 124,322 hrs · 19,275 cycles

INSTALL FOUND THE 41LK 35LK CEILING PANEL EMERGENCY LIGHT CONNECTORS LOOSE, REPLACED 41LK 35LK CEILING PANEL EMERGENCY LIGHT CONNECTORS AND 41LK 35LK CEILING EMERGENCY LIGHT TEST FOUND PASS AS PER SWPM 20-61-28 REV 81 & AMM 33-51-05 -002-039 REV 138.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 124,322 hrs · 19,275 cycles

AFT DOOR LEFT SIDE LOWER EXIT IDENTIFIER INOP, PERFORMED TROUBLE SHOOTING AND REPLACED M1561 POWER SUPPLY AND TEST POWER SUPPLY M1561 FOUND PASS AS PER FIM 33-51 FAULT TREE 812 REV 138 & AMM 33-51-07-402-010 REV 138.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 124,322 hrs · 19,275 cycles

21D 21F SEAT EMERGENCY LIGHT DAMAGE. REPLACED 21D 21F SEAT EMERGENCY LIGHT AND 21D 21F SEAT EMERGENCY LIGHT INSTALLATION TEST FOUND NORMAL AS PER CMM 25-21-53 REV 1 & AMM 33-51-10-962-1 04 REV 138.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 124,322 hrs · 19,275 cycles

TEST FOUND L1 AND R1 DOOR EXIT SIGN INOP, PERFORMED TROUBLE SHOOTING FOUND BATTERY FAILED, REPLACED NEW BATTERY AND TEST ''PASS'' REF FIM 33-51 FAULT TREE 808 REV 138, AMM 33-51-07-022-001 & AMM 33 -51-07-422-012 REV 138.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 124,322 hrs · 19,275 cycles

FOUND 4F-1RC LAVATORY EMERGENCY LIGHT COVER CRACKED, REPLACED 4F-1RC LAVATORY EMERGENCY LIGHT AND LIGHT TEST FOUND PASS OF NEW LIGHT AS PER AMM 33-51-10-962-173 REV 138.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 124,322 hrs · 19,275 cycles

30AB CEILING PANEL EMERGENCY LIGHT INOP. REPLACED 30AB CEILING PANEL EMERGENCY LIGHT LAMP AND LAMP TEST FOUND PASS AS PER AMM 33-51-05-002-039 REV 138.

Part: HOUSING — DAMAGED (EMERGENCY LIGHT) · airframe 124,322 hrs · 19,275 cycles

VCC EXIT SIGN TERMINAL DAMAGE, REPLACED VCC EXIT SIGN HOUSING AND TEST FOUND PASS AS PER AMM 33-51-01-402-030 REV 138.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 124,322 hrs · 19,275 cycles

OVERWING EGRESS LIGHT L394 TEST FAILED, REFER TO NR NO. 9403497, SPEC NO. B767-33-3-7004. REPLACED OVERWING EGRESS LIGHT L394 LAMPS AND LIGHT TEST NORMAL REF AMM 33-51-06-902-082 REV 138.

Part: SKIN — DAMAGED (BS 387 S38-39R) · airframe 124,322 hrs · 19,275 cycles

SKIN BS 387 S38-39R REPAIRED IAW ECRA 5311-02932. INDICATED AS DAMAGE AREA #2 ON ECRA 5311-02932. ACCOMPLISH AN INSPECTION OF REPAIR INSTALLED ON FUSELAGE SKIN AT BS 385 & S38R IAW LATEST REVISION OF ECRA 5311-02932 PART 2 ON OR BEFORE REACHING 37,500 TOTAL FLIGHT CYCLES PER LATEST REVISION OF ECRA 5311-02932 PART 2 ON OR BEFORE REACHING 37,500 TOTAL FLIGHT CYCLES. DIP ITEM CREATED PER ECRA 5311-02932 PART 1. ACCOMPLISH AN INSPECTION OF REPAIR INSTALLED ON FUSELAGE SKIN AT BS 385 & S38R

Part: WIRE — SHORTED (NR 2 IDG) · airframe 118,394 hrs · 18,275 cycles

UPON ARRIVAL TO ACP BITE 24-20-00-810-801. AND RECORD YOUR FINDING. NEED TO CONNECT DRIVE AND INSPECT TERMINAL CONNECTIONS TO RIGHT IDG. RUN ENGINE AND CHECK FOR VOLTS AND FREQS. ALSO, CHECK FOR ADDITIONAL EICAS MSG. CARRIED BY ELB LOCKED LP . CONTACT TOMC WITH UPDATES UNLOCKED LP TO UPDATE BPCU SHOWS MSG''S "SERVICE IDG" "IDG/PRESSURE SW WIRING" "DISCONNECT TRIP" FAULTS. AUTO EVENT ON ELEC PAGE (P61) SHOWS "R GEN DRIVE" FAULT. SERVICED RIGHT IDG ADDED APPROX 1.5 PINTS. IDLE RUN #2 ENGINE IDG CKS NORMAL WITH 45 PERCENT LOAD FOR APPROX 5 MIN. SEE FIM TASK 24-20-00-810-804 PAGE 47. NEED TO PERFORM WIRING CHECKS PER FIM 24-20-00-810-804 PARA.BJ. SFOLM LEE D256A PIN C6 IS GOOD AND GND IS CONFIRMED ON PIN 10.PLEASE MEGG ER PIN 9 TO PIN 10 TO CK FOR INTERMITTENT SHORTS.SFOLM POZAS UPDATE TO FIM WIRING CHECKS,IF CONTINUITY FROM D10964 PIN 9 TO ACCOMPLISHED WIRING CHECKS PER FIM 24-2000-810-804 ITEM BJ. GOOD GCU M146 AND PIN 9 OF D10964; CHECKS GOOD. PIN 10 OF D10964 IS CONTINUITY BETWEEN PIN 9 AND 10 ON IDG. RANG BETWEEN PIN C6 ON A GOOD GROUND. MEGGERED BETWEEN PIN 9 AND 10 AND SHOOK WIRE BUNDLES IN AREA WITH NO DISCREPENCIES. NO PROBLEMS FOUND. NEXT STEPS OF FIM ARE TO REPLACE P5 PANEL AND IF CONTINUES REPLACE GCU. RE-CHECKED WIRING AND FOUND A SHORT TO GROUND ON PIN 9.FOUND W3538-003-18 AND W3538-301Y-18 WIRES MAKING CONTACT WITH BRACKET AT 7 O''CLOCK POSITION JUST AFT OF CONN D10964. 24-11-00-715-006. 20-10-13. NEED TO TEST RIGHT IDG OPERATION REF AMM REF WDM 24-11-21 PG1 SHT2,

Part: OXYGEN GEN — MISSING (SUPPLEMENTAL) · airframe 114,803 hrs · 17,770 cycles

IDTINSPECTION REQUIRED REFERENCE WORK CARD 63-3500-1-2100 F/C FWD CENTER, LEFT CLOSET SUPPLEMENTAL OXYGEN UNIT MISSING O2 GENERATORS INSTALLED 2 EACH O2 GENERATORS AS REQUIRED REF AMM 35-35-98-000-801C1. OK FOR SERVICE.

Part: LIGHT — DAMAGED (NLG) · airframe 114,621 hrs · 17,747 cycles

PDA 2 FOUND RIGHT NOSE LANDING LAMP SMASHED ON ARRIVAL AT LHR, GLASS MISSING. RIGHT NOSE TAXI LIGHT RELAMPED PER AMM 33-42-01-962-021. OP TEST OK.

Part: NOT REPORTED — CRACKED (FUSELAGE) · airframe 112,387 hrs · 17,448 cycles

STA 1809 STR 5R & 7R FOUND 2EA CRACK APPROX 7/8" & 1.5" AS MARKED. STA 1809 STR 5R & 7R REPAIRED AS PER EC/RA5310-07532 REV-.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 112,386 hrs · 17,448 cycles

REF N/R 9130579. STA 1809 FWD OUTER CHORD FOUND CRACKED AT RT S5R AND S7R. INTERIM REPAIR ACCOMPLISHED AS PER ECRA 5310-07 532 PART 1. AS PER ECRA 5310-07532 PART 1 STEP 2 INITIATE A DIP TO ACCOMPLISH REPEAT INSPECTION PER ECRA 5310-07532 PART 2 BEFOR E THE A/C REACHES 37,500 TTL FLT CYC. REPEAT THE INSPECTION AT I NTERVALS NOT TO EXCEED 6,000 FLT CYCLES. DIP INITIATED TO ACCOMPLISH THE INSPECTION PER ECRA 5310-07532 P ART 2 BEFORE THE AIRCRAFT REACHES 37,500 TTL FLT CYC. REPEAT THE INSPECTION AT INTERVALS NOT TO EXCEED 6,000 FLT CYCLES. OK TO CARRY REPAIR INSPECTION REQUIREMENT TO BE ACCOMPLISHED PRI OR TO 37500 TOTAL FLT CYC''S WITH REPEAT INSPECTIONS EVERY 6000 F LT CYCLES THEREAFTER TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 112,387 hrs · 17,448 cycles

REF NR LP 9131303 B767-53-3-6095 CABIN BS 852 RBL 74 FLR SUPPORT FOUND COR CABIN FLOOR BEAM RBL 74 BETWEEN STA 782 - 888 REPAIRED AS PER SR M 53-00-51 REPAIR 3 FIG 201 INSPECTED AND APPROVED.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 112,387 hrs · 17,448 cycles

CABIN - STA 999, RBL 33 FLOOR T-CHORD FOUND CRACK. CABIN STA 943 TO STA 999 RBL 33 FLOOR UPPER CHORD REPAIRED PER SRM 53-00-51 REPAIR 3 FIG 201.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 112,386 hrs · 17,448 cycles

REF NR LP 9131536, B767-53-3-6095, CABIN - STA 999, RBL 33 FLOOR T-CHORD FOUND CRACK. CABIN STA 943 TO STA 999 RBL 33 FLOOR UPPER CHORD REPAIRED PER SRM 53-00-51 REPAIR 3 FIG 201. RII INSPECTED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 112,387 hrs · 17,448 cycles

CABIN STA 287 RBL 52 TO RBL 54 FLOORBEAM UPPER CHORD CORRODED. CABIN STA 287 BETWEEN RBL 25'' TO RBL 88'' REPAIRED PER SRM 33-00- 51 REPAIR 1 FIG 201.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 112,072 hrs · 17,404 cycles

THE CREW REPORTED A CENTER HYDRAULIC QUANTITY LOSS THROUGH DURATION OF FLIGHT. ON GATE ARRIVAL, HYDRAULIC FLUID WAS FOUND COMING FROM LEFT INBOARD TE FLAP TRACK FAIRING NEAR THE LEFT GEAR. MX FOUND A FLEX LINE LEAKING ON LEFT MLG EXTENSION AND RETRACTION SYSTEM. THE FLEX LINE WAS REPLACED AND SYSTEM WAS SERVICED.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 109,554 hrs · 17,047 cycles

EMERGENCY LIGHTS AT SEATS 24AB THRU 33AB INOPERATIVE. TROUBLESHOT FOUND THE BATTERY PACK AND CHARGER BAD, REMOVED AND REPLACED AND OPS CHECKED GOOD.

Part: ALTIMETER — OUT OF TOLERANCE (COCKPIT) · airframe 109,391 hrs · 17,023 cycles

AT/FL330 STBY ALT WAS INDICATING 500 FT HIGH. REMOVED AND REPLACED STANDBY ALT AS PER AMM 43-13-06-344-031, OPS CHECK GOOD ON GROUND. OKAY FOR SERVICE

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 108,033 hrs · 16,822 cycles

EMERGENCY FLOOR LIGHTS OUT ON LEFT AISLE ROWS 24-33. REPLACED POWER SUPPLY AND BATTERY PACK REF AMM 33-51-07.

Part: LENS — MISSING (CABIN) · airframe 107,206 hrs · 16,694 cycles

EMERGENCY CEILING LIGHT FIRST CLASS GALLEY MISSING COVER. REPLACED LENS COVER.

Part: FLOORBEAM — CORRODED (BS 287) · airframe 106,959 hrs · 16,655 cycles

FLOORBEAM CORRODED AT BS 287, RBL 30 - 80. CORROSION REMOVED IAW SRM 51-10-02, BLEND OUT FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101. THE FLOORBEAM UPPER TEE WAS REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201.

Part: ANCHOR FITTING — CORRODED (BS 1417) · airframe 106,959 hrs · 16,655 cycles

BULK CARGO DOOR CUTOUT LOWER EDGE AREA BS 1417, ANCHOR NUT FOUND CORRODED. REPAIRED IAW SRM 51-10-02 AND SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 106,959 hrs · 16,655 cycles

STA 654-121 LBL 43 FLOORBEAM SURFACE WAS CORRODED. FLOORBEAM REPLACED AS PER SRM 51-10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 106,959 hrs · 16,655 cycles

FLOORBEAM FOUND CORRODED AT STA 303 RBL 50. FLOORBEAM REPAIRED AS PER SRM 53-00-51 REPAIR FIG 201.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 106,959 hrs · 16,655 cycles

CABIN FLOORBEAM CRACKED AT STA 325 RBL 20. CABIN FLOORBEAM AT STA 325 LBL 2" TO RBL 57" UPPER FLANGE REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 CRACK LENGTH 0.37" ATTACH MAINTENANCE WORK SHEET FORM 44.0008 ITEM 1-30 ACCOMPLISHED.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 106,959 hrs · 16,655 cycles

FLOOR SUPPORT CRACKED AT STA 786 LBL 11. CABIN STA 786 LBL 11 FLOORBEAM UPPER CHORD CRACKED AREA (CRACK LENGTH 1.5IN). REPAIRED AS PER SRM 53-00-51 REPAIR 3 FIG 201 DETAIL II AND FORM 44.0008 ATTACHED ITEM 1-25 ACCOMPLISHED.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 106,959 hrs · 16,655 cycles

NR 2 PYLON RT SKIN FOUND CRACKED AT PANEL 426BR. CUTOUT POSITION NR 2 PYLON RT SKIN AT PANEL 426BR CUTOUT CRACKED AND REPAIRED IAW SRM 54-53-01, REPAIR 6, FIG 201.

Part: FLOORBEAM — CRACKED (BS 1461) · airframe 106,959 hrs · 16,655 cycles

BS 1461, RBL 31 FLOORBEAM UPPER FWD FLANGE FOUND CRACKED. REPAIR IAW SRM 53-00-51, REPAIR 2, FIG 201.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 106,959 hrs · 16,655 cycles

CABIN AT BS 1562 LBL 50 FLOORBEAM UPPER CHORD FLANGE CORROSION. REMOVED AS PER SRM 51-10-02, BLEND OUT AREA MEASURED DEPTH 0.042 " (ORI THK 0.100") X WIDTH 1" X LENGTH 1" OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMITS AND FLOORBEAM UPPER CHORD FLANGE CORRODED AREA REPAIRED AS PER SRM 53-00-51 REPAIR 2 FIG 2 01 AND FORM 44.0008 ATTACHED ITEM 1-20 ACCOMPLISHED.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,546 hrs · 15,782 cycles

CORROSION FOUND BEYOND LIMITS AFT CARGO PIT FLOOR STRUCTURE, STATION 1153, STRINGER 32L - 32R. R & R PSE CARGO FLOOR STRUCTURE T CAP, PN 146T1060-2 IAW DWG 146T1204 SH 3 & SRM 51-40-02. NO FURTHER INSPECTIONS REQUIRED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 100,546 hrs · 15,782 cycles

AFT PIT BS 1197+88, RBL 40.5 - 42.5 UPPER T CAP FRAME CRACKED. R & R T CAP, PN 146T1061-1 IAW DWG 146T1060 & SRM 51-40-02 PH4.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 100,546 hrs · 15,782 cycles

MAJOR REPAIR, NLG WW RT AFT OTBD, CORNER CHORD CRACKED 11 INCHES FROM THE TOP. REPAIR WAS ACCOMPLISHED IAW SRM 51-70-12 FIG 1 SHEET 4 IAW EA 5300-01606 REV A OP 4 ITEM 2.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 100,379 hrs · 15,759 cycles

EMERGENCY SCAPE SQUIB TEST 1 LIGHT DOES NOT ILLUMINATE WHEN TEST BUTTON PUSHED. DURING ETOPS PDC CHECK. FOUND NO VOLTAGE AT K1 RELAY. REPLACED BATTERY PACK ASSEMBLY M961, M962 & TIME DELAY MODULE M1 IN MODULE M1135. SQUIB TEST CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 98,063 hrs · 15,450 cycles

EMERGENCY EXIT LIGHT INOPERATIVE. CEILING BETWEEN SEAT ROWS 37 & 38 RT. REPLACED LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 95,743 hrs · 15,126 cycles

COCKPIT EMERGENCY LIGHT DOES NOT ILLUMINATE WITH P5 EMERGENCY LIGHT SWITCH ON. REPLACED OVERHEAD EMERGENCY LIGHT ASSEMBLY. WORKED FOR A WHILE & THEN BATTERY RAN DEAD, LEFT OLD LIGHT ASSEMBLY FOR TROUBLESHOOTING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 95,743 hrs · 15,126 cycles

EMERGENCY ESCAPE PATH LIGHT AT SEAT 8B INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY ON MOUNTED SEAT, OPERATIONS CHECKED GOOD.

Part: SOCKET — DIRTY (CABIN) · airframe 95,743 hrs · 15,126 cycles

EXT EMERGENCY LIGHT, DOOR SLIDE ILLUMINATED LIGHT INOPERATIVE AT DOOR 2R. REMOVED LAMP, CLEANED LIGHT SOCKET & LAMP BASE. INSTALLED LAMP & OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 95,743 hrs · 15,126 cycles

COCKPIT EMERGENCY LIGHT DOES NOT ILLUMINATE WITH P5 EMERGENCY LIGHT SWITCH ON. REPLACED OVERHEAD EMERGENCY LIGHT ASSEMBLY. WORKED FOR A WHILE & THEN BATTERY RAN DEAD, LEFT OLD LIGHT ASSEMBLY FOR TROUBLESHOOTING.

Part: RELAY — FAILED (LT ENGINE) · airframe 95,244 hrs · 15,055 cycles

LT IDG VLV STATUS MESSAGE. TROUBLESHOT IAW FIM 24-20-00 PG 105, BLOCK 1 & 2 ARE BOTH, NO NEED TO START AT BLOCK 3, FIG 102, PG 106. ALSO PERFORMED BITE ON PBCU, NO IDG FAULTS, NR 1 ENG, IDG OIL SERVICED, SCAVENGE FILTER DPI IS GOOD. CHECKED WIRING & CONNECTORS, IAW SERVICE TIP 24-20-00 PG 100. REPLACED K1033 RELAY IAW 24-11-11. NEED TO ACCOMPLISHED HIGH POWER RUN. ACCOMPLISHED RUN, NOT HIGH POWER, NO EICAS MESSAGE AFTERWARD.

Part: DOOR — OBSTRUCTED (L2) · airframe 95,244 hrs · 15,055 cycles

2L WILL NOT ARM. REMOVED DEBRIS FROM DOOR SILL

Part: SLIDE — FAULTY (L1 DOOR) · airframe 95,143 hrs · 15,042 cycles

L1 DOOR SLIDE, RT SIDE RETAINING CABLES RELEASED, SLIDE REMOVED FROM DOOR. R & R L1 DOOR SLIDE IAW AMM.

Part: PROXIMITY SWITCH — FAULTY (LE SLAT) · airframe 95,091 hrs · 15,035 cycles

LE SLAT ASYM EICAS WHEN FLAPS LOWERED TO 1. BITE TEST ON PSEU BOX HAD FAULTED NR 5 SLAT INBD PROX SWITCH 286. REPLACED PROX SWITCH & ACP LE SLAT SENSOR OPERATION TEST. SYS TESTED NORMAL, EICAS MSG CLEARED.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 95,067 hrs · 15,032 cycles

DIVERSION DUE TO LE SYMMETRY ISSUE COUPLED WITH MAIN FLAPS UNABLE TO ADVANCE BEYOND 20 DEGREES. IN THIS CONDITION AIRCRAFT IS UNABLE TO EXECUTE A AUTO LAND AS REQUIRED IAW FOM FOR CONDITIONS AT ETA.

Part: RELAY — FAULTY (FUEL PUMP) · airframe 95,022 hrs · 15,026 cycles

RT CTR FUEL PUMP DOES NOT TEST PROPERLY. CLEANED RELAY K633, TESTED GOOD.

Part: RELAY — FAULTY (AC BAY) · airframe 94,934 hrs · 15,014 cycles

FWD EQUIP VLV EICAS MESSAGE. TROUBLE SHOT IAW AMM 21-58 FAULT FREE 939 FIG 4. GOT TO STEP 20 FOUND K1007 RELAY TO BE AT FAULT. REPLACED K1007 RELAY, CHECKED GOOD.

Part: FAN — INOPERATIVE (RIGHT) · airframe 94,767 hrs · 14,990 cycles

RT RECIRCULATING FAN INOPERATIVE. TRIED RESET BUT NO HELP. LT RECIRCULATING FAN OPERATION GOOD. RT RECIRCULATING DEFERRED DUE TIME.

Part: ISOLATION VALVE — STUCK (BLEED AIR SYS) · airframe 94,739 hrs · 14,987 cycles

LT ISOL BLEED VALVE STUCK IN CLOSED POSITION UNABLE TO CROSSBLEED START. TROUBLE SHOT FOUND LT BLEED ISO VALVE INOPERATIVE. REPLACED & OPERATIONS CHECKED GOOD.

Part: CIRCUIT CARD — FAULTY (EQUIP COOLING) · airframe 94,701 hrs · 14,982 cycles

EQUIPMENT COOLING VALVE EICAS MESSAGE & LIGHT ON IN AUTO AFTER NR 2 ENGINE START. REPLACED NR 2 ENG SPEED CARD, NO HELP. REPLACED EQUIPMENT COOLING INDICATION CARD M867 IAW AMM. EQUIPMENT COOLING VALVE OPERATIONS CHECKED NORMAL.

Part: INSULATION — OUT OF POSITION (R2 DOOR) · airframe 94,412 hrs · 14,945 cycles

INSULATION ON DOOR 2R IS STARTING TO BLOCK WINDOW. REPOSITIONED INSULATION.

Part: CLOSEOUT PANEL — DAMAGED (LE SLAT) · airframe 94,412 hrs · 14,945 cycles

RT INBD LE SLAT DAMAGED. R&R SLAT CLOSURE PANEL IAW ECRA 5743-01160.

Part: APU — FAULTY (APU BAY) · airframe 94,410 hrs · 14,944 cycles

APU NO START 3 TRIES HANGS AT 40%. REPLACED APU.

Part: UNKNOWN — MALFUNCTIONED (COOLING SYS) · airframe 94,386 hrs · 14,941 cycles

EICAS MESSAGE 'FWD EQPT VAL` DISPLAYED. EQUIPMENT COOLING 'VALVE' LIGHT ILLUMINATED.'STBY' SELECTED & 'VALVE' LIGHT REMAINED ILLUMINATED. ON RETURN TO BLOCKS VALVE LIGHT ON CONTINUOUS. SHUT PACKS & MOVED TO STBY & AUTO VALVE LIGHT RESPONDED NORMALLY WITHIN DESIGNATED 30 SECONDS. CLEANED & RESET RELAY K1325 & RESET ENGINE REPLACED CARDS ON P50 130365ALL T-S ACCOMPLISHED IAW MM. FIG 105 OPERATION NOW NORMAL.

Part: STARTER — SLOW (APU) · airframe 94,330 hrs · 14,934 cycles

AUXILIARY POWER UNIT SHUTDOWN ON PUSHBACK. AUXILIARY POWER UNIT FAULT MAINTENANCE MESSAGE. RESTART GOOD. ACCOMPLISHED SEVERAL SUCCESSFUL AUXILIARY POWER UNIT STARTS. RAN PACKS & STARTED ENGINES. NO AUXILIARY FAULTS OR SHUTDOWNS. REPLACED AUXILIARY POWER UNIT STARTER FOR SLOW ACCELERATION DURING AUXILIARY POWER UNIT START IAW MM.

Part: SENSOR — FAULTY (BLEED AIR SYS) · airframe 94,330 hrs · 14,934 cycles

AIR SUPPLY BITE MODULE SHOWING FAULT FOR RT ENGINE PRV EXIT PRESSURE SENSOR M1843. PRESSURE INDICATION IS SHOWING 168 PSI WITH NO BLEED PRESSURE APPLIED. REPLACED SENSOR M1843.

Part: NUT — LOOSE (LAVATORY) · airframe 94,297 hrs · 14,929 cycles

ONE INCH STANDING H2O LT SIDE MID CABIN LAV 111. RE-SECURED LOOSE WING NUT TO WATER FILTER IN LAV 2R.

Part: SKIN — DAMAGED (LT WING SLAT) · airframe 94,297 hrs · 14,929 cycles

SKIN ABOVE LEFT WING PEELING. PERFORMED REPAIR TO LEADING EDGE SLAT IAW SRM 51-70-10 REPAIR 4.

Part: OUTFLOW VALVE — MALFUNCTIONED · airframe 94,221 hrs · 14,919 cycles

FWD EQUIPMENT VALVE EICAS ON ENG START. REPLACED FWD OVERBOARD VALVE V169, REINSTALLED RELAYS K1325, K1326 (P87PNL) OPS CHECKED SYS WITH ENGINE START, REACTIVATED ALL RELATED SYSTEMS. OPS CHECK GOOD REF- FIM 21-58-00, FIM 31-01-87. AC RETURNED TO NORMAL.

Part: SPEAKER — FAILED (COCKPIT) · airframe 93,819 hrs · 14,872 cycles

NR 2 COCKPIT SPEAKER DEFECTIVE. LOUD HUM FROM LOWER SPEAKER. INSTALLED NEW SPEAKER, SPEAKERS WORK NORMAL.

Part: CHARGER — FAILED (MASTER) · airframe 93,819 hrs · 14,872 cycles

MAIN BATTERY CHARGER EICAS MESSAGE DISPLAYED. R & R BATTERY CHARGER IAW AMM, OPS CHECKED GOOD. R & R MAIN BATTERY IAW AMM 24-31-01, OPS CHECKED GOOD, NO FAULTS PRESENT.

Part: IGNITION UNIT — FAULTY (APU) · airframe 93,621 hrs · 14,847 cycles

APU AT ALTITUDE WILL NOT START. APU HANGS BETWEEN 30 TO 50 PERCENT DURING START. APU STOPS AT 26 PERCENT. THREE ATTEMPTS. APU WILL NOT START TEST ECU SHOW INGNITION FAULT. REPLACED IGNITION UNIT AND APU STARTED SEVERAL TIMES.

Part: RELAY — FAILED (VALVE) · airframe 93,472 hrs · 14,830 cycles

FWD EQUIPMENT VALVE EICAS AFTER SECOND ENGINE START. REMOVED AND REPLACED K1007 RELAY PER MM 21-58-00.

Part: SPEAKER — FAULTY (1ST OFFICER'S) · airframe 93,421 hrs · 14,822 cycles

HIGH PITCHED WAVERING TONE COMING FROM F/O'S SPEAKER. REPLACED SPEAKER, OPS CHECKED NORMAL AND CHECKED CONNECTION ON AUDIO SELECT PANEL, NO HIGH PITCH NOISED NOTED AT THIS TIME.

Part: SKIN — DAMAGED (NR 8 SPOILER) · airframe 93,198 hrs · 14,793 cycles

NR 8 SPOILER HAS A HOLE THRU THE BOTTOM SKIN AND INTO THE CORE ON THE NR 8 SPOILER PANEL. DAMAGE DIMENSIONS ARE 4" BY 1" BY 1". DAMAGE 4" BY 1" BY 1-2" DEEP & DOES NOT PENETRATE UPPER SKIN. ACCOMPLISHED INTERIM REPAIR IAW ECRA5770-01023 TAPE REINSPECTION REQUIRED EVERY 100 HOURS, PERM REPAIR TO BE ACCOMPLISHED BEFORE NOV 01 2013. MF2741 CREATED TO MONITOR.

Part: SWITCH — DAMAGED (FUEL SYSTEM) · airframe 93,092 hrs · 14,780 cycles

RIGHT CENTER FUEL SWITCH SLOW. REPLACED SWITCH ASSY.

Part: LATCH — DAMAGED (LT PYLON DOOR) · airframe 93,036 hrs · 14,773 cycles

LEFT PYLON HYDRAULIC BAY ACCESS DOOR AFT 4TH LATCH DAMAGED. REMOVED AND REPLACED LATCH, OPS NORMAL.

Part: ACCUMULATOR — LOW PRESSURE (BRAKE SYS) · airframe 92,904 hrs · 14,755 cycles

BRAKE ACCUMULATOR PRESSURE BLED DOWN QUICKLY WITHOUT PUMPS ON. TROUBLESHOT PER FIM 32-41-00. FOUND ACCUMULATOR PRECHARGE LOW. SERVICED ACCUMULATOR PER AMM AND OPS CHECKED GOOD, NO LEAKS NOTED.

Part: SWITCH — UNSECURE (BOOST PUMP) · airframe 92,817 hrs · 14,743 cycles

CENTER OVERHEAD RIGHT BOOST PUMP SWITCH IS HANGING DOWN FROM THE PANEL. REPLACED SWITCH ASSEMBLY, OPS CHECKED NORMAL.

Part: COVER — MISSING (INSTRUMENT PANEL) · airframe 92,703 hrs · 14,728 cycles

ENGINE BOTTLE NR 2 DISCHARGE LIGHT COVER IS MISSING. REPLACED COVER, ALL OPS NOW NORMAL.

Part: LIGHT — UNSECURE (CABIN) · airframe 92,618 hrs · 14,717 cycles

EMERGENCY LIGHTING STRIP IN FIRST CLASS GALLEY FLOOR IS LOOSE. SECURED EMERGENCY LIGHTING STRIP, OKAY NOW.

Part: WINDOW — WARNING MESSAGE (R3) · airframe 92,607 hrs · 14,715 cycles

RIGHT SIDE WINDOW EICAS MESSAGE, RESET DID NOT WORK. WINDOW HEAT CONTROLLER FAULTED R3 WINDOW. REMOVED AND REPLACED R3 WINDOW AS PER AMM 56-11-10, OPS CHECKED NORMAL IAW 30-41-00.

Part: SEAL — BROKEN (FIRE EXTING) · airframe 92,605 hrs · 14,714 cycles

WATER FIRE EXTINGUISHER AT LOCATION 534 SEAL IS BROKEN. DEFERRED WATER FIRE EXTINGUISHER INOP IN AFT GALLEY RIGHT SIDE IAW MEL 2626N. EXTINGUISHER INSTALLED IN FWD CABINET BY COCKPIT. REPLACED SEAL.

Part: CRADLE — FAULTY (INTERPHONE SYS) · airframe 92,178 hrs · 14,654 cycles

NO CHIME OR CALL LIGHT AFT INTERCOM. FOUND RIGHT AFT INTERPHONE CRADLE AT FAULT DISCONNECTED CRADLE AND HANDSET, 2L INTERPHONE LIGHT AND CHIME OPS NORMAL.

Part: INDICATOR — INOPERATIVE (STAB TRIM) · airframe 91,957 hrs · 14,627 cycles

STAB TRIM INDICATOR ON BOTH SIDES FLUCTUATING UP & DOWN WHILE TAXIING. APPROX 1-2 UNITS ON F/O. REPLACED RIGHT STAB POSITION TRANSMITTER. FOUND NO INDICATION. PART BAD. INSTALLED ORIGINAL TRANSMITTER. OPS CHECKED NORMAL.

Part: CONNECTOR — DAMAGED (STAB TRIM) · airframe 91,957 hrs · 14,627 cycles

BOTH STAB TRIM INDICATOR SHOWING MOVEMENT DURING TAXI. CLEANED CONNECTORS AT RIGHT AND LEFT STAB POSITION TRANSMITTERS IAW WD 27-48-11. ACCOMPLISHED AMM POSITION SYSTEM TEST AS PER MM 27-48-00-735-053. NORMAL FUNCTIONS NOTED.

Part: CIRCUIT CARD — FAULTY (MLG) · airframe 91,957 hrs · 14,627 cycles

FOUND PSEU FAULTING CARD O12. REPLACED PSEU CARD 012 PER MM, CHECKED OKAY.

Part: RELAY — FAULTY (RT ENGINE) · airframe 91,648 hrs · 14,585 cycles

DURING ENGINE RUN, LEFT ENGINE N2 WAS AT 64, RIGHT ENGINE N2 WAS 69. PULLING POSITION AIR-GND 2 CB CAUSED ENGINE 2 N2 TO MATCH ENGINE 1. SUSPECT AIR-GROUND RELAY PROBLEM, POSSIBLY K205 OR K207. REPLACED RELAYS K205 AND K207. RUNS OK NO IDLE DISAGREE.

Part: SKIN — DAMAGED (LE SLAT) · airframe 91,648 hrs · 14,585 cycles

RIGHT WING INBD SLAT HAS DAMAGE APPROX 5 FT OUTBD OF INBD END SLAT ON UNDER SIDE 2 INCHES FROM TRAILING EDGE. CF990 RIGHT WING INBD SLAT REQUIRES REPLACEMENT. BEGAN REMOVAL OF RIGHT WING INBD SLAT PER AMM. CONTINUED TO ITEM 2E(7) OUTBD AUX TRK BOLT & ROLLER REMOVED, CRT TRK & INBD AUX TRK NUTS REMOVED, BOLT & ROLLER IN PLACE. CONTINUE WITH REMAINDER OF 2E (7) TO END.

Part: MODULE — FAULTY (APU) · airframe 91,597 hrs · 14,579 cycles

APU ALTITUDE NO START - VERIFICATION APU HANGS BETWEEN 30 TO 50% DURING START. TRIED 3 APU STARTS FL380 TAT-41RPM PEAK 40% THEN APU FAULT EICAS. ACP'D BITE TEST OF APUCU. FAULTED "PT SENSOR". REPLACED FLOW SENSING MODULE IAW AMM. APU START NORMAL.

Part: CIRCUIT CARD — FAULTY (RT EEC) · airframe 91,541 hrs · 14,571 cycles

IDLE DISAGREE, 1 N1 24.5 2 N1 30.1. COMPLIED WITH MEL. INSTALLED DEFERRED NO. ADJACENT TO UPPER EICAS CRT. TROUBLESHOT PER FIM 73-21-00, SUSPECT RT ENGINE EEC DISCRETES CARD ASSY. REMOVED AND REPLACED RIGHT ENGINE EEC DISCRETES CARD, RAN BOTH ENG. N1 AT 25.7 AND 25.1, N2 65 STEADY AND FUEL FLOW 1.5 STEADY. OPS CHECK PER AMM, NORMAL.

Part: UNKNOWN — MALFUNCTIONED (AC BAY) · airframe 91,490 hrs · 14,563 cycles

LEFT PACK TEMP EICAS. LIGHT OUT IN STBY. ITEM HAS PREVIOUS HISTORY AND COMPRESSOR SENSOR HAS BEEN REPLACED ALREADY. ACCOMPLISHED BITE CHECK PER MM 21-51-00 FIG 103 AND SHOWS COMPRESSOR SENSOR. REF SHT 8 PG 116 NEXT STEP IS WIRING CHECKS. RECYCLED SYSTEM BREAKERS WITH RERACK OF PACK CONTROL BOXES BITE CHECK PER MM. GOOD GROUND OPERATED SYSTEM OPS CHECK GOOD.

Part: ENGINE — VIBRATION (NR 1) · airframe 91,066 hrs · 14,500 cycles

NR 1 ENGINE VIBRATION. REPLACED NR 1 ENGINE MAIN OIL SCREEN. NO METAL FOUND.

Part: SLAT — CRACKED (NR 6) · airframe 90,604 hrs · 14,437 cycles

FOUND GOUGE IN NR 6 SLAT 4 1-2 INCHES LONG ON INSIDE OF SLAT 38 1-2 INCHES INBOARD OF OUTER EDGE. CRACKED AT START OF GOUGE. PERFORMED INTERIM REPAIR PER EC-RA 5740-02328 PART 1, INSPECTED SPEED TAPE FOUND INTACT. REPAIR WILL REQUIRE 48 HOUR HOLD FOR HOT BOND REPAIR AS PER SHEET METAL CREW. REMOVED NR 6 SLAT REF MM 27-81-01 AND REMOVED AND REPLACED TO SHOP 273 UNDER R29933.

Part: DISPLAY — FAULTY (COCKPIT) · airframe 91,021 hrs · 14,492 cycles

LOWER EICAS SCREEN BLANK. REPLACED PER MM.

Part: BLADE — NICKED (LT ENGINE) · airframe 90,669 hrs · 14,446 cycles

NICK IN LEFT ENGINE FAN BLADE 24. ACP BLEND OF BLADE 24 ON NR 1 ENGINE PER MM. REQUIRES HFEC INSP WITHIN 6 CYCLES (BLADE HAS WHITE DOT APPLIED) NR 1 ENGINE FAN BLADE 24 HFEC INSP REF NTTM PT6 72-31-401. NO CRACK INDICATIONS.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 90,485 hrs · 14,420 cycles

SEAT 22AB, FLOORBOARD SOFT. SOFT SPOT IS 12 INCH IN DIMENSION IN CENTER OF AISLE

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 90,477 hrs · 14,419 cycles

FLIGHT DECK EMERGENCY EXIT LIGHT ILLUMINATED WITH EMERGENCY LIGHTS OFF (DISARMED). RESET BATTERY PACK, ACCOMPLISHED OPS CHECK. LIGHT OPS CHECKS SATISFACTORY.

Part: CONTROLLER — FAULTED (LT A/C PACK) · airframe 90,433 hrs · 14,413 cycles

FWD CABIN TEMP EICAS ON. VALVE CLOSED PER PROCEDURE 1, ALSO VISUALLY VERIFIED CLOSED. REPLACED LEFT PACK CONTROLLER BOX PER MM, OPS CHECK NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 90,160 hrs · 14,378 cycles

EMERGENCY FLOOR EMERGENCY LIGHT INOPERATIVE AFT OF COACH CLASS DIVIDER. SECURED CONNECTION, OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 90,160 hrs · 14,378 cycles

EMERGENCY LIGHTS AT CEILING NEAR SEATS 21K, 8K, AND AFT OF 14AB INOPERATIVE. RELAMPED AND OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 90,160 hrs · 14,378 cycles

EMERGENCY LIGHT AT R2 DOOR CAVITY AFT INOPERATIVE. RELAMPED, OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 90,160 hrs · 14,378 cycles

EMERGENCY LIGHT AT L2 DOOR CAVITY FWD AND AFT INOPERATIVE. RELAMPED, OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 90,160 hrs · 14,378 cycles

EMERGENCY LIGHT AT SEAT 36JK, 38JK AND 39JK INOPERATIVE. RELAMPED, OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 90,160 hrs · 14,378 cycles

EMERGENCY LIGHT AT SEATS 35AB AND 37AB INOPERATIVE. RELAMPED, OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 90,160 hrs · 14,378 cycles

EMERGENCY LIGHT AT L1 DOOR CAVITY FWD INOPERATIVE. RELAMPED, OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 90,160 hrs · 14,378 cycles

EMERGENCY LIGHT AT R1 DOOR CAVITY FWD INOPERATIVE. RELAMPED, OPS NORMAL.

Part: STRUCTURE — NICKED (RT NACELLE) · airframe 90,137 hrs · 14,375 cycles

RIGHT NACELLE NICKED JUST AFT OF OIL SERVICE DOOR 1 INCH LONG. BLENDED AREAS OF DAMAGE ON AFT EDGE OF OIL SERVICE DOOR CUTOUT IN LOCATION OF LATCHES. DEPTH OF BLEND ON TOP WAS .100 DEEP AND .050 ON BOTTOM AREA.

Part: CONNECTOR — DIRTY (CARGO BOTTLE) · airframe 89,938 hrs · 14,347 cycles

CREW REPORTS CARGO BOTTLE 1 EICAS MESSAGE WITH DISCHARGE LIGHT ILLUMINATED. TROUBLESHOT PER FIM 26-23-00 FIG 103 AND WD 26-23-11. REMOVED CONNECTOR D1448 AND OHMED OUT BOTTLE PRESSURE SWITCH, SWITCH OHMED OK. CLEANED CONNECTOR AND TESTED SWITCH WITH TEST SWITCH, OP CHECKED OK.

Part: APU — MALFUNCTIONED · airframe 89,228 hrs · 14,245 cycles

APU FAILED TWICE WHEN PNEU WAS IN USE. CHECKED CHIP DETECTORS ON APU, ALL GOOD. SERVICE WITH OIL. REPLACED APU BATTERY CHARGER IAW AMM, OPS CHECKED GOOD. RAN APU UNDER LOAD FOR 1 HALF HOUR RAN GOOD. APU AUTO SHUTDOWN AFTER OPERATING FOR 3 MINUTES. 5TH AUTO SHUTDOWN IN 3 DAYS. REPLACED GENERATOR FILTER DIFFERENTIAL PRESSURE SWITCH IAW MM, RAN AND SHUTDOWN MULTIPLE TIMES, CHECKED OK.

Part: PRESSURE SWITCH — FAULTY (FUEL PUMP) · airframe 89,183 hrs · 14,239 cycles

CREW REPORTS LEFT CENTER OVERIDE FUEL PUMP LOW PRESSURE LIGHT NOT ILLUMINATED WITH PUMP SWITCH OFF. FOUND PROBLEM WITH LT CENTER OVERRIDE PUMP PRESSURE SWITCH REMOVED AND INSTALLED PER MM. OPER TEST PER MM PERFORMED. TESTED OK. NO LEAKS FOUND.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 89,049 hrs · 14,223 cycles

NR 1 ENGINE HYDRAULIC PUMP HAS EVIDENCE OF A HYD LEAK. CLEANED AREA MOTORED ENGINE CHECKED HYD PUMP AND FITTINGS, NO LEAKS NOTED.

Part: AUDIO PANEL — FAULTY (POSIT 1) · airframe 89,026 hrs · 14,220 cycles

CAPTAIN'S RADIO - AND OR PANEL HAS SOME TYPE OF FAULT THAT KEEPS THE RADIO TUNED AND MIC OPEN. REPLACED CAPTAIN'S RTP ASSY, NOW OKAY.

Part: PROCESSOR — MALFUNCTIONED (FUEL SYSTEM) · airframe 88,911 hrs · 14,205 cycles

FUEL CONFIGURATION ADVISORY MESSAGE DISPLAYED. REPLACED FUEL PROCESSOR PER MM, OPS CHECKED OKAY FOR SERVICE.

Part: RING — GOUGED (THRUST REVERSER) · airframe 88,911 hrs · 14,205 cycles

NR 2 ENGINE OUTBD CASCADE SUPPORT RING GOUGED AT VARIOUS LOCATIONS ON INNER SURFACE. REMOVED DAMAGED RING ASSY. REPLACED RING ASSY.

Part: THRUST REVERSER — DAMAGED (NR 2 ENGINE) · airframe 88,860 hrs · 14,199 cycles

NR 2 ENGINE RIGHT THRUST REVERSER HALF C-DUCT (ALF) HAS A PREVIOUS REPAIR THAT IS COMING LOOSE UP INTO THE SECONDARY GAS PATH. REPLACED NR 2 ENGINE RIGHT REVERSER OUTBOARD SLEEVE PER MM. NEW SLEEVE OFF OF A-C 6444, OPS CHECK GOOD.

Part: CONTROLLER — FAULTY (BLEED AIR SYS) · airframe 88,851 hrs · 14,198 cycles

RT ENG HPSOV EICAS CAME ON DURING DESCENT. LOCKED OUT HPSOV HAS HISTORY. RPL'D HPSOV CONTROLLER. ALSO FOUND CROSSTHREADED ELBOW AT THE PRV CONTROLLER, RPL'D ELBOW. ACPD HIGH POWER RUN BLEED SYSTEM OKAY.

Part: ENGINE — MALFUNCTIONED · airframe 88,760 hrs · 14,187 cycles

REVIEW OF EHM DATA SHOWS A SIGNIFICANT SHIFT IN THE ENGINE PARAMETERS, TROUBLESHOOTING HAS BEEN ACCOMPLISHED WITH NFF. REVIEW OF EHM DATA SHOWS A SIGNIFICANT SHIFT IN THE ENGINE PARAMETERS, TROUBLESHOOTING HAS BEEN ACCOMPLISHED WITH NO FINDINGS THAT CAN ACCOUNT FOR THE SHIFT. REMOVE THE ENGINE PER AMM 71-00-02 PG BLK 401 C01. WILL INSTALL ESN 727884. THIS ENGINE WILL NEED TO BE CONVERTED FROM A "564" CONFIG TO A "606" CONFIGURATION.

Part: BAND — BROKEN (NR 1 ENGINE) · airframe 88,741 hrs · 14,184 cycles

LEFT SIDE V-BAND BROKEN ON NR 1 ENGINE, PART # IS IN DISPUTE, NEED BOEING VERIFICATION. INSTALLED LT SIDE V-BAND ROBBED. OPS OK CLOSED AND SECURED COWLINGS.

Part: TAPE — BURNED (ANTI-ICE SYS) · airframe 88,715 hrs · 14,178 cycles

PLUMBING INSTALLATION SECT 43 DRAIN HOSE FOR B119 HEATER TAPE BURNED. REPLACED HEATER TAPE, OPS CHECK GOOD.

Part: TAPE — BURNED (DRAIN LINE) · airframe 88,715 hrs · 14,178 cycles

SECTION 43 DRAIN HOSE FOR B119 HEATER TAPE IS BURNED. ON NR 3811N01354 INSP 868 RMV AND RPL HEATER TAPE BN9 PLUMBING SEC 43 DRAIN HOSE IAW B767-300, OPS CHK GOOD.

Part: LINE — BURNED (POTABLE WATER) · airframe 88,715 hrs · 14,178 cycles

SUPPLY LINE FOR POTABLE WATER BURNED AT STATION 790. REPLACED THE B234 SUPPLY LINE AT STA 790.

Part: LINE — BURNED (POTABLE WATER) · airframe 88,715 hrs · 14,178 cycles

POTABLE WATER SUPPLY LINE HAS BURN DAMAGE AT STA 1495. RMV'D & RPLC'D POTABLE WATER SUPPLY LINE.

Part: WEB — CRACKED (NR 2 PYLON) · airframe 88,715 hrs · 14,178 cycles

NR 2 PYLON FWD UPPER SPAR DRAIN WEB AT NAC STA 175.5 COMMON TO FUEL TUBE CUTOUT IS CRACKED AT NUT PLATE HOLE. TRIMMED OUT DAMAGE & ACP NDT FOR CRACKS, NONE FOUND. FABRICATED AND INSTALLED DOUBLER REPAIR PER EA PD67-54-020 & ECRA 5453-01048.

Part: FASTENER — FAULTY (FUSELAGE) · airframe 88,715 hrs · 14,178 cycles

FUSELAGE CROWN STA 218.9 LBL 12.5 & STA 233.9 LBL 14.4 HAS 1 EACH BLIND FASTENER INSTALLED IN EACH LOCATION. BLIND FASTENERS REMOVED AND REPLACED WITH BLIND FASTENERS DUE TO NO ACCESS PER REO(EVA) G11456 AND UA-EVA-60126. CUT ACCESS HOLES IN DRIPSHIELD & INSTALLED SOLID FASTENERS REF ECRA 2514-01006 & EA PD67-53-060.

Part: GUARD — CORRODED (L1 DOOR) · corrosion level 2 · airframe 88,715 hrs · 14,178 cycles

CORROSION ON FASTENER HOLES CREASE BEAM AT L1 DOOR FROM BS 192-345 AT LBL 82. (N-R 3811N00437). MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION REF SRM 51-10-02 & FOUND MATERIAL LOSS OUT OF LIMITS. REMOVED & REPLACED EXISTING CREASE BEAM SPLASH GUARD WITH A NEW & PLUG REPAIRED SIX PILOT HOLES REF EC-RA 5360-01182 & EA PD67-53-061. MINOR REPAIR.

Part: CREASE BEAM — CORRODED (BS 292-345) · corrosion level 2 · airframe 88,715 hrs · 14,178 cycles

CORROSION AROUND FASTENER HOLES ON CREASE BEAM AT L1 DOOR FROM BS 292-345 LBL 82. WORK ACP ON PTT SEQ 7152119. CREASE BEAM REPAIRED ON BASE N-R 3811N00437.

Part: SPLASH GUARD — DAMAGED (FUSELAGE) · airframe 88,715 hrs · 14,178 cycles

DOOR 1LT CREASE BEAM SPLASH GUARD REPAIR MUST RECEIVE A NEW 8100-9 SHOWING COMPLIANCE TO 14 CFR 25.571 & 26.43(D) AND THE DAMAGE TOLERANCE INFORMATION INCORPORATED IN THE AIRCRAFT MAINT PROGRAM WITHIN 24 MONTHS FROM 15FEB2012 FOR THE REPAIR APPROVAL TO REMAIN VALID AFTER 15FEB2014.

Part: BOLT — DAMAGED (LT WING) · airframe 88,715 hrs · 14,178 cycles

LT WING BOLT LOCATED AT WS 416.2, STR 18L COMMON TO RIB NR 9 AND P-N 112T5373-9 FITTING HAS THREAD DAMAGE, REF EVA IMC-00713 AND IMC-00733 FOR HISTORY. REMOVED AND REPLACED BOLT WITH NEW ONE.

Part: SHIM — MIGRATED (LWS 404) · airframe 88,715 hrs · 14,178 cycles

LEFT WING AT RIB NR 9, STR 18L, WS 404, SHIM HAD MIGRATED. ACCOMPLISHED PERMANENT REPAIR 85625 REPLACED DISCREPANT FASTENER AND MIGRATED SHIM. REMOVED SEALANT TO ACCESS SHIM AND FOUND ADDITIONAL MIGRATION. TRIMMED SHIM AND DETERMINED DIMENSIONS. FABRICATED AND INSTALLED SOLID SHIM.

Part: CONNECTOR — BURNED (NR 1 PYLON) · airframe 88,715 hrs · 14,178 cycles

NR 1 PYLON CONNECTOR TO MOTORIZED ISOLATION VALVE IS BURNED BETWEEN PINS. REMOVED & REPLACED CONNECTOR & BACKSHELL REF BOEING SWPM20-61-00 AND WDM78-34-11. PERFORMED OPS CHECK OF SYSTEM. CHECKS GOOD.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 88,715 hrs · 14,178 cycles

KEEL BEAM CORRODED ON UPPER SURFACE AROUND 2 EACH NUT PLATES AT STA 997.9 - 1002 RBL 10. BLENDED UPPER AREA OF KEEL BEAM 0.020' MATERIAL REMOVED FOUND TO BE WITHIN LIMITS PER SRM 53-50-12.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 88,715 hrs · 14,178 cycles

KEEL BEAM CORRODED ON UPPER SURFACE AROUND NUT PLATE AT STA 1002 LBL 10. BLENDED KEEL BEAM UPPER SURFACE, MATERIAL LOSS 0.066", FOUND TO BE WITHIN LIMITS PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 88,715 hrs · 14,178 cycles

BS 287 FLOORBEAM RT UPPER T-CAP REPAIR HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. RMV'D EXISTING REPAIR, FABBED AND INSTALLED T-CUP, 2 EA ANGLES, AND 1 EA STRAP PER SRM 51-40-02 ON PEMCO NR 3811N00414.

Part: PROBE — FAULTY (LT EEC) · airframe 88,703 hrs · 14,176 cycles

L ENG EEC MODE ON EICAS ON L ENG START RETURN TO GATE. DEF IAW MEL 7321AF IN AGREEMENT WITH TOMC ENG DESK TONI MP ACCOMPLISHED. -INF- :MSG 350-24 T2P2 PROBE HEAT. (PARTS: 585-1473 0154ED2 PROBE *SPA* LOB: N).

Part: UNKNOWN — UNKNOWN · airframe 88,589 hrs · 14,162 cycles

ON DESCENT GOT STATUS R ENG CONTROL AND R ENG EEC C1. PIMU SHOWS CH A AND CH B B25 TR-CK FAIL. 2.5 BLEED VALVE ACTUATOR CONNECTION CHECKED AND CLEANED, TEST 15 EEC GROUND TEST OF ENGINE CONTROL SYSTEM ACTUATORS CARRIED OUT IAW AMM PAGE 586D AND FIM 71 PIMU MESSAGE INDEX. NIL FAULTS OBSERVED DURING AND AFTER TEST.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 88,569 hrs · 14,157 cycles

INTERIOR EMERGENCY AISLE LIGHTS AND EXIT SIGN LIGHT ARE INOPERATIVE. REPLACED POWER SUPPLY, LIGHTS CHECKED OK.

Part: CONTROL PANEL — MALFUNCTIONED (AUDIO) · airframe 88,569 hrs · 14,157 cycles

CAPTAIN'S AUDIO PANEL TRANSMIT LIGHTS INOPERATIVE. REPLACED CAPTS AUDIO CONTROL PANEL.

Part: LINE — LEAKING (NR 2 ENGINE) · airframe 88,476 hrs · 14,144 cycles

NR 2 ENGINE TCC ACTUATOR PRESSURE HARD LINE REF IPC 75-32-00-002 ITEM 1 AND MANIFOLD OIL COOLER INLET RETURN HARD LINE REF IPC 75-32-00-002 ITEM 70 BOTH CHAFING THROUGH AT CLAMPS AND PRESSURE LINE LEAKING FUEL. REPLACED BOTH LINES REF STATED IPC (PCN 280-4075 AND 280-4076). ACP'D DRY MOTOR LEAK CHECK AND TEST 15 ACT LEAK CHECK WITH NO LEAKS NOTED. ENG TEST 3 CHECKS OK.

Part: SEAL — LEAKING (COCKPIT WINDOW) · airframe 88,419 hrs · 14,136 cycles

CAPTS SIDE WINDOW HAS A HIGH PITCHED SQUEAL FOREWARD SIDE. REPLACED WINDOW SEAL. PRESSURIZED ACFT TO 4 PSID, NO LEAKS NOTED.

Part: FASTENER — MISSING (NACELLE) · airframe 88,167 hrs · 14,099 cycles

RIGHT ENGINE HAS LOOSE RIVETS. TAPED OVER 2 EACH MISSING FASTENERS & LOOSE RIVETS ON THE RT ENG. OUTBOARD CORE COWL LEADING EDGE ROB STRIP AT 3 O'CLOCK POS PER EVA UAEZA81463, NEED RECHECK TAPE BEFORE EACH DEPARTURE & PERMANENT REPAIR IN 75 FLIGHT HRS. REPLACED FASTNERS ON CORE COWL.

Part: FAN — FAULTY (E&E BAY) · airframe 88,153 hrs · 14,097 cycles

FWD EQ EXH FAN MSG. FOUND FAN BAD PER FIM. REMOVED EXHAUST FAN PER AMM. NEED TO INSTALL FAN. REPLACED FAN.

Part: ACTUATOR — LEAKING (RT ELEVATOR) · airframe 88,133 hrs · 14,094 cycles

RIGHT ELEVATOR PANEL LEAKING HYD FLUID. OPEN PANEL ON RT ELEVATOR ACTUATORS AND FOUND NO ACTIVE LEAK. REPLACED RT INBD ELEV PCA PER MM.

Part: BRACKET — DAMAGED (NACELLE) · airframe 88,018 hrs · 14,075 cycles

NR 2 ENGINE PYLON HYDRAULIC ACCESS BAY LOWER BULB SEAL RETAINERS ARE BROKEN BETWEEN NACELLE STATION 237.39 AND FORWARD OF NACELLE STATION 319.85 (FORWARD 2 RETAINERS). REMOVED DAMAGED SUPPORT BRACKET, MANUFACTURED NEW BULB SEAL SUPPORT ZEE ANGLE BRACKET & INSTALLED.

Part: OXYGEN MASK — NO TEST (COCKPIT) · airframe 87,679 hrs · 14,025 cycles

F/O'S O2 MASK TEST SWITCH STICKS IN TEST POSITION. REPLACED O2 MASK BOX PER MM.

Part: CONTROL QUADRANT — DIRTY (AILERON) · airframe 87,124 hrs · 13,943 cycles

CREW ACCOMPLISHING CONTROL CHECK CONTROL WHEEL BINDS WHEN TURNING TO THE LEFT AT APROX 4 UNITS. ACP AILERON CONTROL CHECK PER MM. ALSO CLEANED AND LUBED RIGHT AND LEFT LCCA QUADRANT. OPERATED SEVERAL TIMES, OP CHECKS OKAY.

Part: VALVE — FAULTY (BLEED AIR SYS) · airframe 87,120 hrs · 13,941 cycles

L ENG PRV EICAS. SAMC TEXT: ON LT ENG START WENT OUT THEN BACK ON, ON RT ENG START. REPLACED PRV ON NR 1 ENG.

Part: WARNING SYSTEM — ACTIVATED (BLEED AIR SYS) · airframe 87,089 hrs · 13,937 cycles

L ENG HPSOV EICAS & BLEED LT AFTER ENG START.

Part: O-RING — LEAKING (NR 1 ENGINE) · airframe 86,901 hrs · 13,912 cycles

NR 4 BEARING MCD OIL LEAKAGE BEYOND ALLOWABLE LIMITS WITH MAG PROBE. REMOVED ON NR 1 ENGINE (APPROX 90 DROPS PER MINUTE, MAX ALLOW 10 DROPS). REPLACED O-RING CHECKS GOOD.

Part: IDG — FAULTY (LT ENGINE) · airframe 86,323 hrs · 13,828 cycles

IDG TERMINAL INSULATION SHOWING SIGNS OF ARCING AND BURNT LEFT ENGINE. CLEANED DIRT FROM HARNESS INSPECTED AND FOUND NO SIGNS BURNING OR ARCING. IDG FEEDER LUG CKS OK, FOUND IDG LUG LOOSE. REPLACED NR 1 ENG IDG PER MM.

Part: SLIDING WINDOW — DEFECTIVE (COCKPIT) · airframe 86,315 hrs · 13,827 cycles

1ST OFFICER'S FIXED SIDE-FORWARD WINDOW'S VISIBILITY IS AFFECTED BY DEFECTS. REPLACE FIRST AVAILABLE. IN THE SUN SCRATCHES VISIBILITY IS AFFECTED. CREW VERBALLY CONFIRMED THAT 1ST OFFICERS NR 2 SLIDING WINDOW IS THE AFFECTED WINDOW. REPLACED FIRST OFFICERS SLIDING WINDOW, ALL CHECKS OKAY.

Part: WINDSHIELD — SCRATCHED (COCKPIT) · airframe 86,315 hrs · 13,827 cycles

CAPTAIN'S WINDSHIELD'S VISIBILITY IS AFFECTED BY DEFECTS, REPLACE FIRST AVAILABLE. CREW COMMENTS: SCRATCHES AFFECT VISIBILITY SCRATCHES FROM WINDSHIELD WIPER. REPLACED CAPTAINS 1L WINDOW REF MM AND INSPECTION, ALL OPS CHECK SATISFACTORY.

Part: BULB — LOOSE (FWD LAVATORY) · airframe 86,297 hrs · 13,822 cycles

ODOR IN AFT GALLEY, FLIGHT DIVERTED. FOUND LIGHT ASSY IN FWD LAV CAUSING CIRCUT BREAKER TRIPPED. ACCOMPLISHED PACK BURN PRECAUTIONARY. NO INDICATIONS OIL CONTAMINATION AT THIS TIME. REMOVED COLLAR ON CIRCUT BREAKER FOR TROUBLSHOOTING. USING WDM 33-24-11 ISOLATED PROBLEM TO RETURN TO SEAT LIGHT IN LT FWD LAVATORY POPPING CIRCUT BREAKER. FOUND TAB ON LIGHT ASSY OF LT FWD LAVATORY RETURN TO SEAT LIGHT BROKEN AND A 387 BULB LOOSE TO SEAT ITSELF ACROSS THE POWER AND GROUND SIDE WITH ITS BODY, CAUSING A SHORT. REMOVED LIGHT BULB AND CIRCUT BREAKER, OPS NORMAL.

Part: HANDSET — INOPERATIVE (CABIN) · airframe 86,020 hrs · 13,783 cycles

MID CABIN PA INOP. REPLACED MID CABIN PA HANDSET, OPERATIONAL CHECKS GOOD.

Part: AMU — FAULTY (ACARS) · airframe 86,020 hrs · 13,783 cycles

ACARS WENT NO COMM WHEN OUT REACH OF VHF. RESET SYSTEM, OPS CHECK GOOD. DUE TO CREW REFUSAL. REPLACE ACARS MANAGEMENT UNIT. REPLACED ACARS MANT UNIT PER MM.

Part: SDU — MALFUNCTIONED (COCKPIT) · airframe 86,020 hrs · 13,783 cycles

DUE TO CREW REFUSAL REPLACE SDU. REPLACED SAT DATA UNIT PER MM.

Part: TRANSCEIVER — FAULTY (HF COMM) · airframe 85,980 hrs · 13,777 cycles

RT HF DOES NOT TRANSMIT. CYCLED RT HF CB, NO HELP. NO HF WILL NOT TRANSMIT. NO TIME TO T-S FURTHER PRIOR DEPT. ITEM HAS HISTORY. SUSPECT TRANSCEIVER AT FAULT. LEFT HF, OPS NORMAL. REPLACED RT HF TRANSCEIVER PER MM, ALL OPS NOW NORMAL.

Part: CONTROL PANEL — FAULTY (AUTOPILOT) · airframe 85,889 hrs · 13,765 cycles

MCP SPEED IAS-MACH WINDOW'S FIRST DIGIT STUCK AT .9. REPLACED AUTOPILOT MODE CONTROL PANEL, OPS CHECK NORMAL.

Part: RELAY — FAULTY (LT ENGINE) · airframe 85,889 hrs · 13,765 cycles

L ENG EEC MODE EICAS MSG. CHECKED ENGINE FAULTS, RAN ENGINE FOUND NO EPR INDICATION ON THE LEFT ENGINE. TROUBLESHOT FOUND AS PER ELECTRICAL SCHEMATIC PAGE. REPLACED RELAY CARD. OP'S CHECK NORMAL NOW. RAN ENGINE PERFORMED TEST AS MM.

Part: REHEATER — CRACKED (AC PACK) · airframe 85,889 hrs · 13,765 cycles

RT PACK HAS 4 INCH CRACK ON BOTTOM OF REHEATER. REPLACED REHEATER PER MM. PACK DISCHARGE TEMP NOW READS 2 DEGREES. ALL OTHER PACK PARAMETERS CHECK NORMAL.

Part: REHEATER — CRACKED (AC PACK) · airframe 85,889 hrs · 13,765 cycles

CABIN WILL NOT COOL WITH APU AIR. REPLACED RT PACK REHEATER PER MM DUE TO HAD 4 INCH CRACK. REPLACED LT PACK REHEATER AND LOW LIMIT VALVE DUE TO NOT FULLY CLOSING PER MM. RAN PACKS AND L PACK DISCHARGE TEMP WAS 11 DEG AND R PACK WAS 5 DEG. ALL PACK PARAMETERS CHECK NORMAL.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 85,889 hrs · 13,765 cycles

CABIN ALTITUDE AUTO 1 STATUS MESSAGE. COMPLIED WITH MEL. REPLACED NR 1 PRESS CONTROLLER PER MM, TESTS OKAY.

Part: CONTROLLER — FAULTY (AC PACK) · airframe 85,889 hrs · 13,765 cycles

"L PACK BITE" MESSAGE WOULD NOT CLEAR. L PACK TEMP CONTROLLER FAULTS LT RAM AIR INLET ACT, SWAPPED LT & RT TEMP CONTROLLERS. PROBLEM WENT TO RT SIDE. PUT BACK TO ORIGINAL POSITION. REPLACED L PACK TEMP CONTROLLER, OP CHECK'S NORMAL.

Part: CONTROLLER — INOPERATIVE (COCKPIT) · airframe 85,889 hrs · 13,765 cycles

ZONE TEMPERATURE CONTROLLER INOPERATIVE. REPLACED ZONE TEMP CONTROLLER PER MM, BITE TEST PASSED.

Part: OXYGEN BOTTLE — LOW PRESSURE (CABIN) · airframe 85,873 hrs · 13,763 cycles

PSX PORTABLE OXYGEN CYLINDER(S) PRESS IS LOW OR ZERO. CREW COMMENTS: BOTTLE AT 2R USED. DF O2 BOTTLE INOP AT DOOR 2R DUE TO NO SPARE IN FRA. REPLACED O2 BOTTLE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 85,748 hrs · 13,746 cycles

FLIGHT DECK EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OP CHECKS NORMAL.

Part: CABLE — DISCONNECTED (CABIN) · airframe 85,748 hrs · 13,746 cycles

PER A-CHECK SEAT 25AB EEL INOPERATIVE. FOUND SEAT CABLE DISCONNECTED, SECURED CABLE OP CHECK NORMAL.

Part: MODULE — FAULTY (STABILIZER TRIM) · airframe 85,395 hrs · 13,693 cycles

EICAS MSG STAB TRIM DISPLAYED, & STAB TRIM LIGHT ILLUMINATED. STABILIZER TRIM OPERATES AT ONE-HALF SPEED. CREW COMMENTS: COMES ON INTERMITTENTLY WHEN TRIMMING WITH CONT WHEEL OR PEDESTAL. WITH STAB IN NEUTRAL, STAB L/E UP LIMIT SW WITH FLAPS RETRACTED AT M519 SHOWS OPEN, AT M520 AND M521 SHOWS CLOSED, MOVED STAB FULL NOSE DOWN (L/E UP) AND M520 AND M521 L/E UP LIMIT OPENED, REPLACED AND ADJ M519. OPERATIONAL TEST NORMAL.

Part: PROBE — FAULTY (ENGINE) · airframe 85,358 hrs · 13,686 cycles

CREW REPORTING "L ENG EEC MODE" DISPLAYED ON TAXI OUT. RTN TO GATE LT ENG EICAS MESSAGE, PIMU BITE SHOWS "P2T2 PROBE HT" ON BOTH CHANNELS. ACCOMPLISHED TROUBLE SHOOTING PER 71. PIMU MSG INDEX FOR MESSAGE 350-24. REPLACED PT2-TT2 PROBE PER MM. INSTALLED 2ND PROBE PER MM, ACCOMPLISHED ENG GROUND RUN X2 ALL OPS & INDICATIONS NOW OK.

Part: COMPUTER — FAULTY (STAB TRIM) · airframe 85,219 hrs · 13,664 cycles

EICAS MSG STAB TRIM DISPLAYED AND STAB TRIM LIGHT ILLUMINATED. SUPPLEMENTAL DATA UPDATE STABILIZER TRIM RATE NORMAL. CREW COMMENTS: STAB TRIM CAUTION LIGHT AND EICAS MSG CAME ON IN CLIMB-OUT. TRIM APPEARED NORMAL. FOUND HORIZONTAL STABILIZER PRIMARY TRIM CHANNEL LEFT INOP, DEFERRED HORIZONTAL STAB TRIM CHANNEL LEFT PER MEL. STAB TRIM CHANNEL RIGHT OK AND BOTH ALT STAB TRIMS CHECKED OKAY. REPLACED LEFT FCC. OPS NORMAL.

Part: STRUCTURE — LEAKING (FUSELAGE) · airframe 85,219 hrs · 13,664 cycles

CREW REPORTS WATER DRIPPING FROM OVERHEAD STOWBINS AT ROWS 33H, 34H AND 37J. FOUND LEFT SATCOM ANTENNA LEAKING BETWEEN ANTENNA AND SKIN. REMOVED ANTENNA. ACCOMPLISHED PRESSURIZATION CHECK OF FUSELAGE PER MM. FOUND MINOR LEAK AT LT SATCOM ANTENNA. REMOVED ANTENNA. REMOVED CEILING PANELS. RE-INSTALLED ORIGINAL PORT HIGH GAIN ANT AND SEALED. REPLACED WET INSULATION. REPLACED LT SATCOM ANTENNA.

Part: INSULATION — SATURATED (CABIN) · airframe 85,219 hrs · 13,664 cycles

CREW REPORTS WATER DRIPPING FROM OVERHEAD STOWBINS AT ROWS 33H, 34H, AND 37J. FOUND THREE SECTIONS OF INSULATION SATURATED IN THE OVERHEAD. CLIPS AND SOME INSULATION ON AOG B2699, M6021, E3702, L5994. FOUR PANELS WET ON RT SIDE AT 1200, 1240, 1260, 1400 LOCATIONS. REMOVED WET INSULATION MADE REPLACEMENT INSULATION PANELS AND INSTALLED PANELS. NEEDS FINAL SECURING AT STATION 1400-1420.

Part: SENSOR — FAULTED (APU) · airframe 84,901 hrs · 13,618 cycles

APU SHUTDOWN ON ENGINE START. APU INOP PREV HIT INDICATED SURGE. CLEANED CONNECTORS TO SCV & FLOW SENSE MODULE. REVERSE FLOW DISPLAYED ON ECU, REPLACED INLET TEMP SENSOR IAW MM AND PT TRANSDUCER. OPS TESTED NORMAL.

Part: CONNECTOR — DIRTY (APU SURGE VALVE) · airframe 84,800 hrs · 13,606 cycles

APU SURGING AND AUTO SHUTDOWN 2 TIMES AT GATE. CLEANED CONNECTORS TO APU SURGE VALVE AND FLOW SENSE MODULE ASSY. RESET APUC. ACCOMPLISHED APU BLEED OPS CHECK.

Part: O-RING — LEAKING (RT CASE DRAIN) · airframe 84,669 hrs · 13,587 cycles

RT SIDE CASE DRAIN FILTER ACMP AFT FAIRING LEAKING 1 DROP IAW SECOND WITH NO PRESSURE. REPLACED RT CASE DRAIN FILTER O-RING, LEAK CHECK OK.

Part: COAX — FAILED (STAB TRIM) · airframe 84,369 hrs · 13,547 cycles

UNSCHEDULED STAB TRIM DISP. CHANGED THE STAB COAX CABLE.

Part: DAMPER — FAULTY (RIGHT) · airframe 83,681 hrs · 13,450 cycles

RT YAW DAMPER INOPERATIVE. ACCOMPLISHED YAW DAMPER SYS BITE. SYS TESTED NORMAL. STORED FLIGHT LEG FAULTS IN RT YAW DAMPER MODULE FAULTING RT YAW DAMPER ACTUATOR. LT YAW DAMPER MODULE HAS NO FAULTS.

Part: PANEL — LOOSE (CABIN) · airframe 83,637 hrs · 13,441 cycles

LOUD BANG IN CABIN, RTFL. PER MM AND CG SUPERVISOR CANS FOUND NOT SECURE IN FWD CARGO PIT CAUSING "BANG". DUE TO VIBRATION HISTORY REMOVED CARGO CEILING AND SIDEWALL PANELS LOCATED UNDERNEATH SEATS 2K AND 6K. NO DEFECTS NOTED. FOUND LARGE PANEL LOCATED BEHIND SEAT AND CURTAIN MISSING ALL FASTENERS. PANEL WAS ONLY SECURED BY VELCRO STRIP. REPLACED 8EA MISSING PLASTIC RIVETS PART 27SR0030.

Part: GEARBOX — FOD (TE FLAPS) · airframe 83,561 hrs · 13,429 cycles

ON FLAP EXTENSION SELECTED FLAPS 5 AND FLAPS EXTENDED TO 15 WITH HANDLE IN 5 DETENT. OPERATED IN ALT TO FLAPS 20 FOR LANDING. OPENED COVERS AT CONTROL STAND FOR FLAP CONTROL LEVER AND REMOVED 2 PIECES OF PLASTIC TY RAPS AND 1 TRIM SCREW THAT WAS INTERFERING WITH THE FLAP CONTROL GEARBOX AND RVDT 1 AND REMOVED DEBRIS AND ACCOMPLISHED FLAP OPS CHECK.

Part: BLADE — DAMAGED (NR 1 ENGINE) · airframe 83,050 hrs · 13,360 cycles

NUMBER 1 ENGINE HIGH VIB FELT IN AIRFRAME OR THROTTLE. LT ENG VERY LOUD ON CLIMB OUT (LT VIB 3.0 RT VIB 1.2). NORMAL AT CRUISE LT VIB 1.5 RT 0.5. MAX VIB ON CLIMBOUT WAS 3.0 NOT 30. SLIGHT VIBRATION FELT ON YOKE IN CLIMB. NORMAL IN CRUISE, VIBS DID FOLLOW THROTTLE MOVEMENT. ALL OTHER ENG PARA'S NORMAL. REF: MM FOR TROUBLESHOOTING. (X.X RANGE 0.0 TO 5.0, ABNORM ABOVE 4.0).

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 83,006 hrs · 13,354 cycles

IN SEAT EMERGENCY LIGHTS INOP AT SEATS 26AB AND 32HJ. RELAMPED, NO HELP. ADJUSTED & RELAMPED. NOW OP CKS ARE GOOD.

Part: SHUTOFF VALVE — FAULTY (POSITION 2) · airframe 82,825 hrs · 13,325 cycles

RIGHT ENGINE HPSOV EICAS ONTO ROLL AT ABOUT 1.4 EPR WENT AWAY ON ABORT IDLE THRUST. BLEED AIR CONTROLLER FAULTS HPSOV. DEFERRED NR2 HPSOV IAW MEL 3611R. REPLACED NR 2 HPSOV IAW MM.

Part: ACTUATOR — LEAKING (LT ELEVATOR) · airframe 82,464 hrs · 13,278 cycles

EVIDENCE OF HYD FLUID ON BOTTOM OF LT ELEVATOR. INSPECTED AND FOUND LT ELEVATOR MIDDLE PCA FOR RT HYD SYS LEAKING. REPLACED LT SIDE ELEVATOR PCA (MIDDLE ONE). ACTUATOR IN AND SECURED. CLOSING UP.

Part: VANE — DAMAGED (THRUST REVERSER) · airframe 82,460 hrs · 13,276 cycles

NR 1 ENGINE, REPLACE REV CASCADE VANE SEGMENTS 8 AND 9 ON THE LT REV HALF REFERENCE MM. NO DAMAGE ALLOWED. REPLACED CASCADE SEGMENT.

Part: CONTROLLER — MALFUNCTIONED (BLEED AIR SYS) · airframe 82,460 hrs · 13,276 cycles

LEFT ENG BLEED OFF LIGHT ON WITH SWITCH IN ON POSITION, NO DUCT PRESS, ADVANCED POWER, NO CHANGE. PRSOV WOULD NOT OPEN. CYCLED LEFT BLEED CONT CB S11, DID NOT HELP. REPLACED RELAYS K1115 AND K1116. CAPT RAN ENGINE LEFT ENGINE PRSOV BLEED LIGHT EXTINGUISHED, OPS CHECK OK. REPLACED PRSOV, NO HELP. CONTINUED ASSISTANCE WITH PRSOV, NO HELP. LT BLEED FAILED AGAIN. REPLACED LT ENG PRSOV. OPS CKS NORMAL. LT ENG BLEED CYCLED ON OFF AT IDLE DESCENT SOME W EICAS MSG SOMETIMES NOT. ON RUN FROM IDLE TO BLEED SHIFT BLEED WOULD NOT MOVE ABOVE BLD SHIFT BLEED POPPED ON AND WAS NORMAL AFTER THAT, COULDN'T DUPLICATE. ACCOMPLISHED HEALTH CHECK, PRSOV FAILED HEALTH CHECK, REPLACED PRSOV, OPS CHECK NORMAL.

Part: SPAR — CRACKED (NR 1 PYLON) · airframe 81,207 hrs · 13,103 cycles

NR 1 PYLON UPPER SPAR WEB LOWER SURFACE CLOSE- OUT TEE FITTING PN 311T3157-1 AT MID-SPAR FITTING NAC STA 237 HAS 1.5 INCH CRACK VERIFIED BY NDT. HFEC VERIFIED STOP DRILL, ROTO PROBE INSP BOLT HOLES REF NDT PT6. INSTALLED REPAIR SPLICE AND FILLER REF EA AND MARKED REPAIR. REINSTALLED CLOSEOUT FITTING.

Part: LIGHT — INOPERATIVE (OVRWING EXIT) · airframe 81,207 hrs · 13,103 cycles

LOWER EMERGENCY EXIT LIGHT ON RT FWD OVERWING EXIT DOOR INOPERATIVE. RELAMPED LOWER EMERGENCY EXIT LIGHT ASSY. OPS CHECKED LIGHT ASSY. OPS CHECKED GOOD.

Part: MODULATING VALVE — FAULTY (HYD PUMP) · airframe 80,585 hrs · 13,007 cycles

C HYD DEM PUMP EICAS. PUMP WILL ONLY DELIVER NO MORE THAN 2000 PSI. REPLACED ADP REF MM. NO HELP. APU NOW SURGING WITH ADP IN AUTO AND IN MANUAL WITH NO HYD PRESSURE, NO PRESS LIGHT IN AUTO, BUT IN MANUAL LIGHT COMES ON. CHECKED CONNECTOR D488 PINS 6, 12 HAD 28 VDC PINS 3, 4 ARE GROUND. ADP MODULATING VALVE REPLACED, NO CHANGE. TRIED NEW OVERSPEED CARD M1057, NO CHANGE. PUT BACK OLD OVERSPEED CARD M1057. DOES NOT COME ONLINE PERIOD. FOUND INDICATION TO BE READING NORMAL ON APU BLEED.DUE TO HISTORY REPLACED M1057, GROUND CHECKS NORMAL.

Part: CONTROL VALVE — FAULTY (APU BLEED SYS) · airframe 80,516 hrs · 12,995 cycles

APU BLEED READING BETWEEN 12 18 PSI. APU BLEED INOPERATIVE. REPLACED SURGE CONTROL VALVE.

Part: PUMP — MALFUNCTIONED (JETTISON SYS) · airframe 80,144 hrs · 12,939 cycles

FUEL IMBALANCE. REPLACED RT JETTISON PUMP AND DIFFUSER. OPS CHECK OK AND NO LEAKS.

Part: TRANSCEIVER — FAULTY (HF SYSTEM) · airframe 79,887 hrs · 12,905 cycles

RT HF SLOW TO TUNE. ATC NOT HEARING OUR TRANSMISSIONS. REPLACED RT HF TRANSCEIVER, NO HELP. SUGGEST REPLACED RT HF COUPLER M242. REPLACED RT HF COUPLER. OPS CHECK GOOD. GOOD COMMUNICATION WITH NEW YORK ARINC ON RIGHT AND LEFT HF RADIOS.

Part: WIRE — BROKEN (LE SLAT) · airframe 79,683 hrs · 12,875 cycles

L/E SLAT ASYM EICAS, RTFL. FOUND WIRE BROKEN AT SPLICE OF SENSOR 279 OF NR 4 OTBD SLAT. REPLACED SPLICE AND CHK IAW MM. OPS CHK OK NOW. SLAT DISAGREE REPAIRED.

Part: SATCOM — FAULTY (COCKPIT) · airframe 79,640 hrs · 12,867 cycles

SATCOM INOP. REPLACED SDU & RFU. AFTER INSTALLATION SYS BITE CHKS GOOD BUT UNABLE TO ESTABLISH RADIO COMM USING SATCOM SYSTEM. ACCOMPLISHED RADIO CALL FOR BOTH CHANNEL CALLED SAMC, OPS CKD GOOD.

Part: ACTUATOR — MALFUNCTIONED (APU DOOR) · airframe 79,550 hrs · 12,853 cycles

APU WON'T START. STATUS MSG, APU DOOR. REPLACED INLET DOOR ACTUATOR, OPS CHECKS NORMAL.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 78,774 hrs · 12,737 cycles

LEFT CTR ADP LEAKING HYD FLUID. APPEARS TO BE A CAPPED FITTING ON INBOARD BOTTOM OF PUMP. REMOVED CENTER HYD SYS ADP. CONTINUING ADP INSTALLATION. INSTALLED ADP, OP CHECKS GOOD.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 78,774 hrs · 12,737 cycles

TOWER REPORTED THICK SMOKE COMING FROM APU. APU SUBSEQUENTLY AUTO SHUT DOWN. REMOVED APU. COMPLETED INSTALLATION OF NEW APU.

Part: OIL FILTER — FAULTY (LT ENGINE) · airframe 77,454 hrs · 12,534 cycles

LEFT ENGINE HAS OIL FILTER BYPASS WARNING MSG HISTORY. REPLACED FILTER. CHECKED MAGNETIC CHIP DETECTORS.

Part: PROCESSING UNIT — FAULTED (FUEL QTY) · airframe 77,065 hrs · 12,477 cycles

STATUS MSG FUEL QTY CHANNEL. REPLACED FUEL QTY PROCESSOR. ORIGINAL QTY PROCESSOR FAULTED CHANNEL 1 AND 2. AMR PROCESSOR FAULTS CHANNEL 1 ONLY. CHANNEL 2 OK AND QTY VERIFIED.

Part: PANEL — DAMAGED (RT WING) · airframe 76,759 hrs · 12,434 cycles

RT WING LOWER WING FIXED TRAILING EDGE PANEL 651VB HAS A 1.5 INCH CRACK RUNNING FORE TO AFT. CRACK IS LOCATED 5.5 INCHES FROM INNER EDGE OF PANEL AND 0.75 INCHES OUTBOARD OF NEAREST FASTENER. REMOVED TRAILING EDGE RT WING PANEL. ROUTED PANEL TO SHOP 273. PANEL REPAIRED BY SHOP 273.

Part: SKIN — DAMAGED (RUDDER) · airframe 76,304 hrs · 12,360 cycles

FOUND LIGHTNING STRIKE EXIT DAMAGE ON RUDDER TRAILING EDGE. DAMAGE IS LOCATED APPROXIMATELY 8 FEET UP FROM LOWER EDGE. DAMAGE IS A SEMI CIRCULAR DELAMINATED ARE MEASURING 2 INCH BY 1.25 INCH, CONTAINED IN CENTER IS A .75 BY 1.25 INCH AREA OF EXPOSED AND DAMAGED PLIES. DAMAGE DOES NOT PENETRATE THROUGH TO OTHER SIDE, BUT HAS A FASTENER IN THE CENTER OF THE DAMAGED AREA. REPAIRED RUDDER EDGE, PRIMED.

Part: SKIN — DAMAGED (RUDDER) · airframe 76,304 hrs · 12,360 cycles

FOUND LIGHTNING STRIKE EXIT DAMAGE ON RUDDER TRAILING EDGE. DAMAGE IS LOCATED APPROXIMATELY 8 FEET UP FROM LOWER EDGE. DAMAGE IS A SEMI CIRCULAR DELAMINATED ARE MEASURING 2 INCH BY 1.25 INCH, CONTAINED IN CENTER IS A .75 BY 1.25 INCH AREA OF EXPOSED AND DAMAGED PLIES. DAMAGE DOES NOT PENETRATE THROUGH TO OTHER SIDE, BUT HAS A FASTENER IN THE CENTER OF THE DAMAGED AREA. REPAIRED RUDDER EDGE, PRIMED.

Part: SMOKE DETECTOR — NO TEST (LAVATORY) · airframe 75,836 hrs · 12,295 cycles

AC-3 LAV SMOKE DETECTOR DOES NOT TEST. REPLACED AC-3 LAV SMOKE DETECTOR. OPS CHECKS NORMAL.

Part: LATCH — DAMAGED (EVAC SLIDE) · airframe 75,836 hrs · 12,295 cycles

LEFT WING OVERWING SLIDE DOOR, NR 3 LATCH HAS GROOVE IN SLIDER. REPLACED LT OVERWING SLIDE DOOR NR 3 LATCH. OPS CHECKS GOOD.

Part: LATCH — GOUGED (EVAC SLIDE) · airframe 75,836 hrs · 12,295 cycles

RT OVERWING SLIDE COMPARTMENT DOOR NR 2 LATCH GOUGED. REPLACED RT OVERWING SLIDE COMPARTMENT DOOR NR 2 LATCH.

Part: ACTUATOR — FAULTY (RT ENGINE) · airframe 75,825 hrs · 12,293 cycles

DURING START OF RT ENG, 'R FUEL SPAR VAL' EICAS MSG AND SPAR VLV LIGHT ILLUMINATED. ENG SUBSEQUENTLY SPOOLED DOWN. REPLACED ENG FUEL SHUTOFF ACTUATOR AND ACP ENG OPS CHECK.

Part: WIRE — BURNED (CONTROL PANEL) · airframe 75,794 hrs · 12,287 cycles

FWD CARGO COMPARTMENT P35 POPPING CB`S AS FOLLOW: C171, C173, C167, C168 & C169. FOUND 24 WIRES BURNED OUT UNDER PNL PDU 7L. ALL WIRES ISOLATED AND AFFECTED PDU'S ELECT PLUGS REMOVED AND ISOLATED. FWD CARGO HDG SYS INOP. STARTED TO IDENTIFY WIRES WITH LABELS. REPAIRED AND OPS CHECKED GOOD.

Part: CIRCUIT BREAKER — TRIPPED (BUFFER BOX) · airframe 75,399 hrs · 12,231 cycles

BURNING ELECTRICAL SMELL IN FWD CABIN NEAR VIDEO CONTROL EQUIPMENT WITH BUFFER BOX CB`S J15 AND J16 REPORTED TRIPPED BY FLT CREW. RESET J15 & J16 CB'S ON BUFFER BOX OPS CK OK.

Part: CIRCUIT CARD — FAULTY (PSEU) · airframe 74,939 hrs · 12,153 cycles

AFTER TAKEOFF AIR-GND DISAGREE STATUS MSG. RTFL. REPLACED ENTIRE PROXIMITY SWITCH ELEC UNIT WITH ALL CARDS AND NLG SWG OPS OK. REF SCHEMATIC:32-09-03 AND 32-09-02. REPLACED RELAYS K203, K293, K219 AND K209. AIR-GND RELAY TEST FAILS STEP I(3) AND I(7) FOR SYSTEM 1, PG 507-508 OF MM 32-09-02. SYSTEM 2 OPERATES OKAY. ACCOMPLISHED FIM 32-09-00 FIG103A. FIM SUGGESTS ADJUSTING SENSOR CLEARANCE (BLOCK 43, PG 116). HOWEVER, SENSORS ARE SLUGGED PER BLOCK 8 SO THERE IS NO ADJUSTMENT. ACP TEST REF MM32-09- 02, NO FAULTS. CHRONIC AIR-GRD MSG, SUGGEST REPLACED DRIVE R CARD IN PSEU REF MM32-09-06. REPLACED DRIVE R CARDS PER MM 32-09-06. OP CKS GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 74,939 hrs · 12,153 cycles

AFTER T/O, AIR-GND DISAGREE STATUS MSG. RTFL.

Part: LIGHT — UNSECURE (GALLEY) · airframe 74,336 hrs · 12,049 cycles

FWD GALLEY X-AISLE EEL LIGHT INOP. SECURED EEL STRIP TO PWR SUPPLY, OPS CHECKS GOOD.

Part: LIGHT — UNSECURE (ROWS 1-2AB) · airframe 74,336 hrs · 12,049 cycles

EEL LIGHTS LEFT SIDE FC ROWS 1AB & 2AB INOP. SECURED EMERGENCY LIGHTS TO POWER SUPPLY RIBBON. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (LAVATORY) · airframe 74,336 hrs · 12,049 cycles

EEL LIGHT ADJACENT TO LAV AT DOOR 1L INOP. SPLICED EEL LIGHT STRIP TO CKT PWR. OPS CHECKS GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 74,336 hrs · 12,049 cycles

EMERGENCY LIGHT ADJACENT DOOR 1R INOP. SECURED LOOSE CONNECTOR. OPS CHECK OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,389 hrs · 11,889 cycles

RIGHT FWD CABIN EEL INOPERATIVE.

Part: ASPIRATOR — LEAKING (CABIN)

LEAKING ASPIRATOR. THERE IS NO PHYSICAL DAMAGE TO THE ASPIRATOR. REPLACED ASPIRATOR.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 73,166 hrs · 11,856 cycles

DURING GEAR RETRACTION, HAD A C-HYD SYS PRESSURE AND AIR DEMAND PUMP EICAS ALONG WITH A C-HYD SYS.

Part: BLADE — CRACKED (COMPRESSOR) · airframe 72,700 hrs · 11,783 cycles

CRACK FOUND IN THE 5TH STAGE COMPRESSOR BLADE ROOT OF THE NR 1 ENGINE. REPLACED ENGINE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 72,530 hrs · 11,756 cycles

APU GEN OFF EICAS MSG WITH ASSOC SWITCH LIGHT ILLUMINATED.

Part: LIGHT — FAULTY (COCKPIT DOOR) · airframe 72,123 hrs · 11,695 cycles

EMERGENCY EXIT LIGHT AT FLIGHT DECK DOOR IS ON WITH STANDBY SWITCH IN OFF POSITION.

Part: BLADE — BENT (LT ENGINE) · airframe 71,501 hrs · 11,595 cycles

ONE BLADE ON LEFT ENGINE BENT OVER 90 DEGREES. REPLACED BLADE NR 37 DUE TO BENT AND OPPOSITE BLADE NR 18 PER MM 72-31-02. THREE OTHER BLADES NR 35, 36, 38 ARE CF'D. ACCOMPLISHED RII INSPECTION OF NR 35 36 AND 38 BLADES PER MM 72-31-02, OK FOR FINAL .020\ INSURANCE BLEND. ACCOMPLISHED BLENDING .020' PER MM 72-31-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,309 hrs · 11,568 cycles

FLOOR EEL STRIP AT SEATS 13 AND 14 AB INOP.

Part: BLADE — FAILED (ENGINE) · airframe 70,588 hrs · 11,453 cycles

ECM HAS DETECTED PARAMETERS SHIFT AT BOTH TAKEOFF AND CRUISE. ENGINE REPLACED. SHOP TEARDOWN REVEALED HEAVY HPC BLADE DAMAGE. THE DAMAGE WAS A RESULT OF FAILURE IN A 5TH STAGE DISK KNIFE EDGE. A 5-INCH SECTION OF THE FRONT KNIFE EDGE FRACTURED, CAUSING A 2-INCH SECTION OF THE STAGE-5 BLADE LEADING EDGE TO LIBERATE, AND SUBSEQUENT DOWNSTREAM BLADE DAMAGE.

Part: UNKNOWN — UNKNOWN (FUEL SYSTEM) · airframe 70,383 hrs · 11,420 cycles

CREW COMMENTS: FUEL OVERBURN BY 6000 PLUS POUNDS.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,155 hrs · 11,381 cycles

LEFT SIDE EEL IS INOP FROM SEAT 27 TO AFT GALLEY. REPLACED BATTERY & EEL CHECKS GOOD.

Part: WARNING SYSTEM — ACTIVATED (L/E SLAT) · airframe 70,042 hrs · 11,359 cycles

RTFL DUE TO L/E SLAT DISAGREE MESSAGE. EVENT RECURRED ON NEXT FLIGHT OUT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 70,040 hrs · 11,358 cycles

LEFT SIDE EXTERIOR EMERGENCY LIGHTS (L388): (L389): (L313 ): (L395): AND (L642) INOP.

Part: MECHANISM — OUT OF POSITION (OVERWING SLIDE) · airframe 70,040 hrs · 11,358 cycles

LEFT OVERWING SLIDE INFLATION CYLINDER PULL FORCE MECHANISM BALL IS IN THE WRONG POSITION, BALL IS IN FRONT OF THE RETAINER SPRING, NOT BEHIND IT AS REQUIRED.

Part: LATCH — OUT OF TOLERANCE (OVERWING SLIDE) · airframe 70,040 hrs · 11,358 cycles

LEFT OVERWING SLIDE DOOR LATCHES NR 1, 2, 3 & 4 FAIL EDGE MARGIN TEST.

Part: HANDLE — OBSTRUCTED (ESCAPE HATCH) · airframe 70,040 hrs · 11,358 cycles

RIGHT AFT EMERGENCY ESCAPE HATCH AUTO ARM AND AUTO FIVE SWITCHES DID NOT MOVE TO THE (UP) POSITION, DURING TEST.

Part: BATTERY — FAULTY (FLASHLIGHT) · airframe 69,472 hrs · 11,264 cycles

EMERGENCY FLASH LIGHT BETWEEN 1L & 1R FLIGHT ATTENDANT SEAT DOES NOT BLINK. [08-08-07] REPLACED BATTERY AND SEAL. AIRCRAFT OK FOR SERVICE.

Part: ASPIRATOR — LEAKING (EVAC SLIDE) · airframe 67,282 hrs · 10,898 cycles

BOTH ASPIRATORS LEAKING BETWEEN JET PLATE ASSEMBLY AND SENSING TUBE. REPLACED BOTH ASPIRATORS. SUSPECT SIDE LOAD ON ASPIRATORS DURING PACKING CAUSED LEAKS.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,321 hrs · 10,904 cycles

EMERGENCY OVERWING EXIT SIGNS INOP ALL POSITIONS. REPLACED BATTERY AND BASE; OPS CHECKED OK .

Part: WARNING LIGHT — ILLUMINATED (TAT PROBE) · airframe 66,008 hrs · 10,696 cycles

TAT PROBE LIGHT ILLUMINATED JUST AFTER TAKEOFF. [5-1-07] REPLACED THE TOTAL AIR TEMPERATURE SENSOR. OP CHECKS OK. CAUSE SUSPECTED TO BE INTERNAL ELECTRICAL SHORT IN SENSOR CIRCUIT.

Part: FAN — FAILED (COCKPIT) · airframe 65,162 hrs · 10,576 cycles

ELECTRICAL BURNING ODOR IN FLIGHT DECK. FOUND FAILED FORWARD EQUIPMENT COOLING EXHAUST FAN. REPLACED EQUIPMENT COOLING EXHAUST FAN. FOUND FAN IMPELLER ROUGH TO ROTATE. ALSO, A SMALL RADIAL PLAY OF THE IMPELLER WAS ALSO NOTICED WHILE HOLDING THE FAIRING.

Part: FITTING — CRACKED (NR 2 PYLON) · airframe 63,108 hrs · 10,261 cycles

NR 2 PYLON MIDSPAR FITTING LOWER TANG AT INBOARD CLOSEOUT ANGLE HAS 2 EACH CRACKS COMING OUT OF THE INBOARD BOLT HOLE. 2 CRACKS EMANATING FROM INBD BOLT HOLE OF CLOSEOUT ANGLE INSTALLED OVER NR 2 PYLON MIDSPAR FITTING LOWER TANG WAS FOUND. THE CLOSEOUT ANGLE WAS REPLACED (BUT NOT THE FITTING.)

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 63,108 hrs · 10,261 cycles

CLOSEOUT ANGLE BELOW MID SPAR FITTINGS OF NR 2 PYLON HAS CRACKS FROM INBOARD AND OUTBOARD ENDS. INBD AND OUTBD ENDS ON CLOSEOUT ANGLE BELOW MID SPAR FITTINGS OF NR 2 PYLON WERE FOUND CRACKED. THE CLOSEOUT ANGLE WAS REPLACED USING 767-300 SRM 51-40-02.

Part: STIFFENER — GOUGED (WS 825) · airframe 63,108 hrs · 10,261 cycles

LT WING STIFFENER GOUGED BEYOND LIMITS AT WS 825 REAR SPAR. THE LEFT WING STIFFENER, P/N 112T1237-1, WAS FOUND GOUGED BEYOND LIMITS AT WS 825 REAR SPAR. NO DAMAGE WAS REPORTED ON THE ADJACENT STRUCTURES. THEREFORE, THE GOUGED WAS LIKELY CAUSED BY FOD. REPLACED STIFFENER PER BAC DWG 112T1237 AND SRM 51-40-2.

Part: ATTACH FITTING — MISDRILLED (RT WING AILERON) · airframe 63,108 hrs · 10,261 cycles

RIGHT WING INBOARD AILERON, INBOARD SECTION LEADING EDGE ATTACH FITTING MISDRILLED. S/D* THE SUBJECT FITTING WAS MISDRILLED DURING INSTALLATION. REPAIRED PER TIMCO REO-G11452.

Part: FAILSAFE — CORRODED (BS 1562 S39L&R) · airframe 63,104 hrs · 10,260 cycles

CORROSION ON STA 1562 FAIL-SAFE, P/N 146T1223-30, BETWEEN STR 39L & 39R. REPAIRED BL 0 AREA CORROSION AT STA 1562 FAILSAFE CHORD WITH A REPAIR ANGLE AND FILLER PER TIMCO REO(EVA) G11428 AND UA EVA 60127. REPAIR IS FAA APPROVED AND PERMANENT.

Part: BULKHEAD — CRACKED (BS 1809) · airframe 63,104 hrs · 10,260 cycles

BS 1809 BULKHEAD RT SIDE, FWD OUTER CHORD, INBD FLANGE HAS A CRACK COMING OUT OF THE FASTENER HOLE. DAMAGE FOUND AS A RESULT OF ROUTINE INSPECTION, MANDATED PER AD 2005-11-02. REPAIRED PER AD REQUIREMENTS.

Part: SEAT TRACK — BROKEN (BS 789-808) · airframe 63,104 hrs · 10,260 cycles

MAIN SEAT TRACK OUTBD LT SIDE STA 786-808, LBL 88 INBD NODES BROKEN OFF FROM TRACK. DAMAGED SEAT TRACK REMOVED/REPLACED PER SRM.

Part: HINGE FITTING — CRACKED (LT INBD FLAP) · airframe 63,104 hrs · 10,260 cycles

LEFT INBD FLAP-CENTER HINGE FITTING CRACKED ON INBD AND OTBD FLANGES. THE SUBJECT HINGE FITTING WAS FOUND CRACKED ON THE INBOARD AND OUTBOARD FLANGE. REPAIRED PER 767-300 STRUCTURAL REPAIR MANUAL 57-53-02.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 63,104 hrs · 10,260 cycles

AFT PIT FLOORBEAM AT STA 1197+132 BETWEEN STR 33R TO 33L IS CORRODED AT 6 LOCATIONS. CORRODED FLOORBEAM REPAIRED PER SRM. DAMAGE FOUND BY ROUTINE INSPECTION.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 63,104 hrs · 10,260 cycles

AFT PIT FLOORBEAM AT STA 1197 BTWN STR 33L- 33R IS CORRODED TOP AND BOTTOM OF T-CAP, SEVERAL LOCATIONS. CORRODED FLOORBEAM REPAIRED PER SRM. DAMAGE FOUND BY ROUTINE INSPECTION.

Part: APU — SHUTDOWN (APU BAY) · airframe 60,248 hrs · 9,799 cycles

DIVERTED DUE TO AUXILIARY POWER UNIT AUTO-SHUTDOWN WITH LEFT GENERATOR DEFERRED INOPERATIVE. UPON LANDING APU FOUND 4.0 QUARTS LOW. MM ADDED OIL. ENGINEERING MONITORING OIL CONSUMPTION. TO DATE CONSUMPTION IS .014 QT/HOUR. LIMIT IS .20 QT/HR. SAMC REQUESTED ALITUDE START AND RAN APU ONE HOUR AT ALTITUDE WITH NO OIL CONSUMPTION. CAUSE OF LOW OIL QTY UNKNOWN. 0.3 OF QT USED SINCE EVENT WITH .001 QT/HR.

Part: WEDGE — DELAMINATED (L/E SLAT)

TRAILING EDGE WEDGE SKIN DELAMINATED, SLAT NR 6 MAJOR REPAIR ACCOMPLISHED. REPLACED T/E WEDGE.

Part: PSEU — MALFUNCTIONED (COCKPIT) · airframe 51,862 hrs · 8,383 cycles

WITH GEAR UP AND GEAR HANDLE OFF, THREE GREEN LIGHTS AND TAIL SKID LIGHT ILLUMINATED. LANDING GEAR MONITOR AND WARNING ELEX STATUS MESSAGES ILLUMINATED. REPLACED PSEU AND ELEX WARNING POWER SUPPLY MODULE.

Part: SKIN — GOUGED · airframe 50,712 hrs · 8,183 cycles

EXTERNAL FUSELAGE SKIN GOUGED AT STA 595, STRINGER 1L. BLENDED GOUGE. FABRICATED AND INSTALLED DOUBLER AND FILLER.

Part: POSITION SWITCH — FAILED (NR 9 SLAT) · airframe 38,584 hrs · 6,007 cycles

L/E SLAT ASSYMETRY EICAS MESSAGE DISPLAYED WHEN FLAP LEVER SELECTED TO 1. DIVERTED TO JFK. *S/D* SLAT MOVEMENT WAS INHIBITED BY THE FLAP/SLAT ELECT UNIT (FSEU) WHEN IT RECEIVED A SLAT POSITION LOGIC SIGNAL FROM THE PROXIMITY SWITCH ELECT UNIT INDICATING A SLAT ASYMMETRIC CONDITION. THE ASYMMETRIC LOGIC SIGNAL ORIGINATED FROM A FAILED SLAT POSITION SWITCH (S303) LOCATED ON THE RIGHT WING, NR 9 SLAT, INBOARD SWITCH. THE SUBJECT S303 POSITION SWITCH WAS REPLACED WITH A NEW SWITCH. THE SLAT SYSTEM WAS OPERATIONALLY CHECKED OK PER MM 27-88-06. AS PRECAUTION, THE FSEU WAS REPLACED PER MM 27-51-01.

Part: ACTUATOR — FAILED (LT MLG TRUCK)

LEFT MAIN GEAR WOULD NOT RECYCLE AFTER CLIMB-OUT. RECYCLED GEAR, LEFT MAIN WOULD NOT RECYCLE. DIVERTED LHR, OVERWEIGHT LANDING. CHECK VALVE IN TRUCK POSITION ACTUATOR PRESSURE LINE WAS MALFUNCTIONING, ALLOWING BYPASS AND PREVENTING UNLOCK ACTUATORS TO BUILD UP UNLOCK PRESSURE. REPLACED TRUCK POSITION ACTUATOR.

Part: SLIDE — WILL NOT TEST (LEFT)

LEFT OVERWING SLIDE SYSTEM WILL NOT TEST IN EITHER SYSTEM 1 OR 2. *S/D* ACCOMPLISHED CHECK PER MEL 25 360. GROUND CHECK GOOD. SYSTEM RETURNED TO NORMAL. REPLACED RELAYS K1, K5.

Part: COMPRESSOR VANE — BROKEN (APU)

APU AUTO SHUTDOWN AT DEPARTURE TIME. *S/D* FOUND APU DRIVEN COMPRESSOR DEWHISTLER VANE BROKEN. IMPELLER FOD. APU REPLACED.

Part: COMPRESSOR — STALLED (RT ENGINE)

AIRCRAFT RETURNED TO FIELD DUE TO RIGHT ENGINE COMPRESSOR STALL AND HIGH EGT. *S/D* COMPRESSOR STALL IS ATTRIBUTED TO THE N2 COMPRESSOR FAILURE. THE ENGINE WAS REMOVED FROM THE AIRCRAFT. THE ENGINE IS NOT YET DISASSEMBLED.

Part: PSEU — MALFUNCTIONED (FLIGHT DECK)

AIRCRAFT RETURNED TO BLOCKS WITH EICAS AMBER ADVISORY MESSAGE FOR RIGHT OVERWING SLIDE. REPLACED PSEU DUE TO ANNUNCIATOR PANEL LIGHT NOT ACCOMPANYING EICAS ADVISORY MESSAGE. SUSPECT FAULTY DRIVER CARD.