N658UA

Part: SLIDE — NO DISCREPANCY (ZONE 800) · airframe 128,625 hrs · 19,770 cycles

DOOR 1R SLIDE RAFT PRESS GUAGE HAS CONDENSATION IS HARD TO READ. COMPLETED A GAS CYLINDER GAUGE CHECK IAW AMM 25-66 OPS CHECK GOOD OKAY TO CONTINUE

Part: SKIN — DELAMINATED (ZONE 600 AILERON) · airframe 128,471 hrs · 19,749 cycles

RIGHT WING OUTBOARD AILERON HAS DELAMINATIONDELAMINATED AREA TAP TESTED AND MAPPED. LOWER SURFACE DIMENSIONS OF DELAM MEASURE AT 18" IN LEGNTH BY 9" IN WIDTH. IT HAS AN EDGE DISTANCE 1.5" AND A TRAILING EDGE DISTANCE OF 5" UPPER SURFACE OF AILERON TAP TESTED AND DELAM MAPPED. DIMENSIONS OF THE DELAM MEASURE 12" LEGNTH BY 5" IN WIDTH. DISTANCE FROM INBOARD EDGE MEASURES 2.5". TRAILING EDGE DISTANCE MEASURES 6". PHOTOS ADDED FOR REFERENCE PART NUMBER OF AILERON ADDED. PHOTO OF DATA PLATE ADDED LOCKING FOR FERRY REMOVED RIGHT WING OUTBOARD AILERON REF AMM TASK 27-11-02-024-001 UP TO PARAGRAPH F. STEP (1). COMPLETED REMOVAL OF RH O/B AIL REF AMM 27-11-02, FROM STEP 2.F.(1) TO END OF PROCEDURE. ADD EMP:U223495,U346494 RH O/B AIL ROUTED TO IAH RAMS TEAM FOR REPAIR. UNLOCKING TAPPED TOP AND BOTTOM SKINS OF AILERON AND COULD NOT NOTE ANY DELAM/DISBOND, FROM IMAGES ASSUME WATER IN HONEYCOMB CELLS, CUT OUT AREA ON UPPER SKIN TO REMOVE WATER. COMPLIED WITH SRM 57-60-02-2R-1 AND SRM 51-70-17-0G-0 PARAGRAPHS 1.-3.B. REMOVED DAMAGED SKIN SECTION AND REMOVED WATER. COMPLIED WITH AVO ESC20250809-6458-1 ENLARGED CUTOUT AND REMOVED MOISTURE. DRY COOKED UPPER AND LOWER SECTION OF AILERON IN REF TO AVO15340 STEP 3A AND SRM 51-70-05, NEED TO ACCOMPLISH NDT PER AVO15340 STEP 3 THERMOGRAPHY C/W PER 767 NDT MANUAL PART 1, 51-01-01 AND NDT MANUAL PART9 51-00-01, NO WATER INDICATION AT THIS TIME REF AVO 15340 STEP 3 C/W STEP 4,A.B.C. OF AVO15340 . 6PLYS CUT AND REMOVED IN THE CRITICAL ADDED IMAGES.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 127,811 hrs · 19,660 cycles

DURING BODY BELOW AFT CARGO COMPARTMENT FLOOR (INTERNAL) CDP INSPECTION IT WAS FOUND SIGNS OF CORROSION AT STRINGER S-39R (UNDER STRINGER) LOCATED AT STA 1219. ALL OF STEPS OF ECRA 5360-01960 WERE PERFORMED WITHOUT ANY DEVIATION, NO MORE ACTION IS REQUIRED.FOR MORE INFORMATION SEE THE NR 2657427 ALL OF STEPS OF ECRA 5360-01960 WERE PERFORMED WITHOUT ANY DEVIATION.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 127,811 hrs · 19,660 cycles

BULK CARGO - FUSELAGE INTERNAL SKIN - DURING PRELIMINARY INSPECTION WAS FOUND STRINGER 39R WITH CORROSION AT STA 1542. IT WAS CREATED ESFR NECESSARY QC REVIEW AND APPROVAL. IT WAS CREATED ESFR NECESSARY QC REVIEW AND APPROVAL. PERFORMED INSPECTION AND APPROVED THE REPAIR AS PER EC/RA #5360-01961 AND ESFR NUMBER CREATED #1075. PERFORMED PERMANENT REPAIR AT STRINGER S-39R BETWEEN STA 1518 AND STA 1562 AS PER EC/RA #5360-01961. ITEM OK TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 127,811 hrs · 19,660 cycles

BODY BELOW AFT CARGO COMPARTMENT FLOOR (INTERNAL) INSPECTION: IT WAS FOUND SIGNS OF CORROSION BELOW FLOORBEAM AT BS 1131, S-34R IT WAS CREATED ESFR NECESSARY QC REVIEW AND APPROVAL. PERFORMED INSPECTION AND APPROVED THE REPAIR AS PER EC/RA #5360-01963, PERFORMED PERMANENT FLOORBEAM REPAIR AT BS 1131, S-34R AS PER EC/RA #5360-01963. ITEM OK TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 127,811 hrs · 19,660 cycles

FWD SERVICE DOOR AFTER CORNER - IT WAS FOUND A CRACK INDICATION IN TWO HOLES (LOWEST HOLES) AT 1 AND 2 O'CLOCK POSITION. THE CRACK IS PRESENT ON THE SKIN AND BEARSTRAP. PERFORMED REPAIR AS PER EC/RA #5310-08602. PERFORMED INSPECTION AND ALL STEPS OF THE REPAIR WERE ACCOMPLISHED AS PER B767-300 SRM 53-10-01-2R-1 AND EC/RA # 5310-08602.

Part: SKIN — CRACKED (ZONE 200) · airframe 127,811 hrs · 19,660 cycles

FWD ENTRY DOOR AFTER CORNER - IT WAS FOUND A CRACK INDICATION IN ONE HOLE (LOWEST HOLE) AT 11 O'CLOCK POSITION THE CRACK IS PRESENT ON THE SKIN AND BEARSTRAP. PERFORMED REPAIR AS PER SRM 53-10-01-2R-1. PERFORMED INSPECTION AND ALL STEPS WERE ACCOMPLISHED WITH NO DEVIATION IAW SRM 53-10-01-2R-1.

Part: WIRE — BROKEN (ZONE 200) · airframe 127,637 hrs · 19,637 cycles

R/H EMERGENCY DOOR LIGHT PANEL WIRE BROKEN.SEAT 20. REMOVED AND TERMINATED NEW LUGS ONTO EXIT SIGN ABOVE R OVER WING EXIT DOOR. IAW SWPM 20-30-11 AND WDM 33-51-14. REINSTALLED PANEL AND OPS CHECKED GOOD IAW AMM 33-51-00-715.

Part: SLIDE — FAILED (ZONE 800) · airframe 127,510 hrs · 19,621 cycles

REF WC 64-2560-1-3800, SCHEDULED MX, R&R L4 SLIDE DUE TO 2 SLIDES BAD FROM STOCK, REINSTALLED ORIGINAL SLIDE AT LOCATION L4, IAW WC 64-2560-1-3800. PARTS NIS @ EWR, DEFERRING SLIDE CHANGE, IAW TOMC. QC VERIFIED L4 WC 64-2560-1-3800

Part: IDG — FAULTY (NR 2) · airframe 126,465 hrs · 19,482 cycles

R GEN DRIVE EICAS LITE COMPLETED REMOVAL OF RH IDG IRT AMM 24-11-01-004-002-006. ALL UNIONS AND PARTS ARE LOCATED ON WORK TABLE NEXT TO ENGINE. ORDERED NEW O RINGS WAITING FOR THEM TO BE DELIVERED. START INSTALLATION OF R/H IDG REF AMM 24-11-01-404-001-006 UP TO INCLUDE STEP 3.H.(6).(E). USED ON FEEDER CABLES OF R/H ENG. IDG INSTALL REF. AMM 24-11-01. CONTINUED INSTALLATION ON IDG ON #2 ENG FROM REF. AMM 24-11-01-404-001-006 STEP H.(6)(I) THRU H. (9). COMPLETED RT ENG IDG INSTALLATION AND TEST, ALSO DISCONNECT FUNCTION REF AMM TASK 24-11-01-404-001-006. OPS NORMAL

Part: ACCESS PANEL — MISSING (LT NACELLE) · airframe 124,779 hrs · 19,257 cycles

PDA 2 ON AIRCRAFT ARRIVAL, LEFT ENGINE INBOARD PYLON PANEL 436AR MISSING. REPORTING SDR FOR PDA 2.

Part: ROLLER — DAMAGED (R2 DOOR) · airframe 124,741 hrs · 19,252 cycles

R-2 SERVICE DOOR (AFT. GALLEY) REQUIRES R.I.R. / D.V.I. OF AFT. ROLLER TRACK ASSY. EVERY 15 DAYS PER. EC/RA # 5211-01872 REV. [A]. PART # 2 (INSPECTIONS PROCEDURE) AND PART # 3 (PERMANENT REPAIR PROCEDURE) WITHIN 60 CALENDAR DAYS. [ACFT. # 6458]. REQUEST DIP APPROVAL PER EC/RA # 5211-01872 REV. [A]. ADD EMP:U406888 DIP 52-DIP REJECT. SDR NOT REQUIRED

Part: WIRE — SHEARED (PSU) · airframe 123,820 hrs · 19,131 cycles

PANEL CAME DOWN AT 33 DEF REDO 1 PIN OR REPLACEMENT OF MODULE PER WDM 35-21-14. HANDED OVER TO OPPOSITE CREW. PRELIMINARY INSPECTIONS OF 33DEF FOUND OXY MASK DEPLOYMENT WIRING FOR MODULE M00064 WITH WIRE BUNDLE W1170 AND WIRES121-20R AND W1170-122-20G OF CANNON PLUG D2996 WITH ONE WIRE PULLED OUT OF PIN AND ONE WIRE SHEARED. IT REQUIRES A SPLICE REPAIR AND ADD EMP:U381930 DOOR LATCH ACTUATOR REPLACED AS PER AMM 35-21-15 PB 401 AND WDM 35-21-14-1 PAGE 1. OPS CHECK PERFORMED AS PER 35-21-00-705-054. VERIFIED OXYGEN GENERATOR HOSES CONNECTED CORRECTLY AND SAFETY PIN IS REMOVED AT 33DEF.

Part: CONTROL MODULE — INTERMITTENT (STAB TRIM) · airframe 123,689 hrs · 19,111 cycles

UNSCHED STAB TRIM EICAS DURING TO ROLL X2 REMOVED AND REPLACED AND TESTED STAB TRIM CONTROL MODULE PER AMM 27-09-00.

Part: SEAL — MISSING (RT AILERON) · airframe 123,165 hrs · 19,039 cycles

R/H I/B AILERON, I/B LOWER SEAL MISSING. PICTURES ADDED. CONTACTING TOMC FOR DISPOSITION, NIL STOCK LHR. IPC REF 27-11-01-05 ITEM 155, PART NUMBER: 113T6105Y2 1 QUANTITY. INBD LOWER SEAL FOR INBD AILERON REPLACED I.A.W DWG 113T6100 SHEET 2, AILERON ACTUATED TO CHECK CLEARANCE. AIRCRAFT SERVICABLE RETURNED TO NORMAL.

Part: CYLINDER — UNKNOWN (OVRWG SLIDE) · airframe 121,777 hrs · 18,852 cycles

REF AMM 25-65-01-024 PARAG E (3): IF THE OFF WING ESC SYS OPERATED WITH THE REGULATOR SAFETY PIN INSTALLED, YOU MUST REPLACE THE INFLATION CABLE AND THE INFLATION CYLINDER. LEFT OFFWING ESCAPE SLIDE CYLINDER AND AND CABLE REPLACED AS PER AMM TASK 25-65-02-201 AND TASK 25-65-401 RESPECTIVELY. PARTS USED: 62-2565-3-0004,QTY :1 76-2565-9-9002,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1682720 SN OFF 1569 VERIFIED REPLACMENT OF LEFT OFFWING ESCAPE SLIDE CYLINDER AND AND CABLE REPLACED AS PER AMM TASK 25-65-02-201 AND TASK 25-65-401. ALL RIGGING VERIFIED AND LOCKING DEVICES REMOVED AS REF GMM 09-25-25 CYLINDER, ASSY, OFF 76-2565-9-9002 1569 ON 76-2565-9-9002 9923

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 121,769 hrs · 18,851 cycles

DURING OFF WING ESCAPE SLIDE INSPECPTION LEFT HAND WING SLIDE DOOR ACTATED OPEN. SLIDE AND BOTTLE NOT ACTIVATED. OFF-WING ESCAPE SYSTEM SPOLIER OVERRIDE ACTUATOR REPLACED IN UPDATE DUE TO PART HAVING ASSIGNED SERIAL NUMBER ACCORDANCE WITH AMM-25-65-20. SQUIB TEST TO BE ACTIONED. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1206998 SN OFF 9002 PARTS USED: 76-2565-9-9001,QTY :1 1206998,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1206998 SN OFF 0845 IPC REFERENCE # 25-65-20 ACTUATOR, EMERG OFF 76-2565-9-9001 9002 ON 76-2565-9-9001 1550 VERIFIED REPLACEMENT OF OFF-WING ESCAPE SYSTEM SPOLIER OVERRIDE PER AMM-25-65-20 AND LEFT WING OVERWING ESCAPE DOOR LATCH OPENING ACTUATOR PER AMM 25-65-404-012-001 VERIFIED ALL RIGGING AND REMOVAL OF LOCKING DEVICES LH ESCAPE SLIDE FWD DOOR ACTUATOR REPLACED IAW AMM LEFT OFF WING ESCAPE SLIDE PACK REPLACED AS PER AMM TASK LEFT WING OVERWING ESCAPE DOOR LATCH OPENING ACTUATOR REPLACED LEFT OVERWING ESCAPE SLIDE LATCH ACTUATOR REPLACED AS PER 25-65-10-404-016-001.

Part: ENGINE — DAMAGED (NR 2) · airframe 121,571 hrs · 18,821 cycles

UPON REACHING TO EPR LOUD BANG WITH SWERVE RIGHT . REJECTED T/O . NO FIRE. R REV ISLN VAL EICAS ENG2 SN. 724371 (TSI= 16306) SURGED AT T/OFF POWER, CHEK INLET, LOST N1, OIL PRESSURE IN RED 60 TO 70PSI PER FLIGHT CREW EXHAUST, TAIL PIPE FOR METAL, CHECK ALL CHIP DETECTORS. REF FIM 71-05 FAULT TREE 803 FOR FAULT ISOLATION AND T/SHOOTING. REPORT FINDINGS TO TOMC ENGINE CONTROLLER.WHQLM-EMC ARSHAD. 27AUG23. CAPT. U160941, CALLED TO SAY THAT IT WAS LOW SPEED 40-50 KNOTS ABORTED T/OFF, THRUST REVERSER AND RTO BRAKES WERE NOT USED. WHQLM-EMC ARSHAD. 28AUG23. REF EGC LOG PAGE 5587893 MOTOR IS SIEZE AND NEEDED TO BE RELACED. REF TASK CARD 76-7200-9-0001 FOR #2 ENGINE CHANGE SIGN OFFS. AMM72- 00-00-206-001-N01 5TH, 6TH, & 10TH STAGES OF THE HPC. 1ST & 2ND HPT BLADES. 1ST STG OUTER AIR SEAL DUCT SEGMENTS. LPT TRANSITION DUCT. 2ND STG OUTER AIR SEAL DUCT SEGMENTS. 3RD STG LPT BLADES. FOUND HEAVY DAMAGE AT EVERY STAGE, BLADES MISSING AND AP10 HOLE BLOCKED FROM DAMGE COULD NOT GET SCOPE IN. COLUD NOT TURN ENGINE FROM DRIVE PAD, LOCKED UP. CARRIED BY ELB LOG PAGE TRANSFERRED OF WING WITH ESN 724371. PARTS USED: 1916017,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1916017 SN OFF 4371 ENGINE, (PW4060 OFF 76-7200-9-0001 4371 ON 76-7200-9-0001 7686.

Part: PANEL — MISSING (NR 2 STRUT) · airframe 119,219 hrs · 18,501 cycles

PDA 1 REF LP 3518403. E2 INBD STRUT PNL 447AL BROKEAND PARTIALLY DEPARTED THE A/C INBD STRUT PNL 447AL INSTALLED WITH FIRE SEAL.

Part: SKIN — CRACKED (BS1809-1820) · airframe 116,687 hrs · 18,150 cycles

B767-53-3-7018 RH HORI STAB LOWER FAIRING QATTACH SKIN FOUND CRACK AT BS 1809-1820 , TRANSFER TO HX NRC WO 738612 AND ORIGINATED BY V896832 R/H HORI STAB LOWER FAIRING ATTACH SKIN AT BS1809-1820 BETWEEN STA 12AR TO STR 22R SKIN REPAIRED AS PER EC/RA 5381-01018 REV - WORK ACCOMPLISHED BY MECHANIC V897471 INSPECTED BY V898549 RII OK BY HX 146606 ADD EMP:V896834

Part: FRAME — CHAFED (BULK CARGO DOOR) · airframe 116,687 hrs · 18,150 cycles

B767-53-3-7006 BULK CGO DOOR LWR MID AREA DOUBLER FOUND CHAFING , TRANSFER TO HX NRC WO745751 AND ORIGINATED BY V898555 BULK CGO DOOR LOWER MID AREA FRAME CHAFING DOUBLER REMOVED AS PER SRM 51-70-11-0G-0 FIG 1 FORM 44.0008 WORSHEET AND DISCARD AS PER SRM 51-40-02 HFEC INSPECTION WAS CARRIED ITEM 1 TO ITEM 15 ACCOMPLISHED OUT AS PER 767 PART 6 51-00-19 REV 130 DATE NOV-2021 RESULT NO CRACK FOUND THE CHAFING AREA REPAIRED

Part: ACCESS PANEL — MISSING (WING) · airframe 116,307 hrs · 18,080 cycles

PDA 3 ACCESS PANEL 621 ADB MISSING DURING WALK AROUND. REPLACED ACCESS PANEL 621 ADB AS REQUIRED A/C OK TO CONTINUE.

Part: LIGHT — DAMAGED (SEAT 20D) · airframe 115,896 hrs · 17,996 cycles

STAR PRE-DEPARTURE CHECKLIST - EMERGENCY PARH LIGHT RED DAMAGED AT SEAT 20D REPLACED LIGHT ASSY, GRD OPS EMERGENCY PATH LIGHT SYS, NO DEFECTS NOTE

Part: SKIN — DEBONDED (RT WING TE FLAP) · airframe 115,209 hrs · 17,861 cycles

B767-06-3-7222 RHW I/B AFT FLAP UPPER AND BOTTOM SURFACE FOUND DISBOND - REFER NR LP 9130574. RHW I/B AFT FLAP DISBOND AREA PERFORMED REPAIR AS PER EC/RA 5752-01851 REV - REFER FORM 44-0008 ITEM 1-29 ACCOMPLISHED ADD EMP:V912779 RII INSPECTED OK BY HX198855 REF ECRA 5752-01851

Part: SPAR — DAMAGED (LT WING) · airframe 110,845 hrs · 17,158 cycles

LT WING L/E FRONT SPAR WEB FOUND DAMAGED AT OFSS1025 REF NRC 9131148 DVI SURROUNDING STRUCTURAL WITHIN 16'' NIL FINDINGS. HFEC INSP CARRIED OUT PER B767 NTM PART 6 51-00-19, NO CRACK FOUND AT TRIM MED EDGE. HFEC OPEN HOLE INSP CARRIED OUT AT EXISTING FASTENER LOCATIONS PER B767 NTM PART 6 51-00-16, NO CRACK FOUND. REPAIR PARTS INSTALLED.RESISTANCE BETWEEN SPAR WEB & WEB INNER SPLICE PER BAC5117-6 CARRIED OUT AND WITHIN AMM 20-10-21 LIMITS. OP CHECK & ADJUSTMENT TEST CARRIED OUT PER AMM 27-81-00, RESULT NORMAL. LEAK CHECK CARRIED OUT PER AMM 28-11-00, NO LEAK. NO.1 SLAT SENSOR SWITCH OP TEST CARRIED OUT PER AMM 27-88-01, RESULT NORMAL LHW FRONT SPAR WEB AT OFSS 1025 REPAIRED PER ECRA 5720-03122 ADD EMP:V897381 RII APPROVED BY HX147141 & NO.1 SLAT I/B AUX TRACK SENSOR TARGET IS INSTALLED PER DRAWING REQUIREMENTS

Part: SKIN — CORRODED (BS 1197) · airframe 110,845 hrs · 17,158 cycles

FUSELAGE SKIN PREVIOUS REPAIR DOUBLER SKIN FOUND SURFACE CORROSION AT STA 1197+120 BETWEEN STR 37L-38L CORROSION REMOVED PER SRM 51-10-02, ORG 0.065'' BLEND OUT AREA REMAIN 0.045'' WIDTH 2'' LENGTH 2'', CHECKED NOT WITHIN SRM53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. PREVIOUS DOUBLER REMOVED AND DISCARDED PER SRM 51-40-02. REPAIR PARTS MADE AND ISNTALLED PER SRM 53-00-01 REPAIR 14 FIG 201, WEIGH 0.75LB. ADD EMP:V897381 DIP REQUIRED PER SRM 53-00-01 REPAIR 14 FIG 201 TABLE V RII APPROVED BY HX106494 CARRY AS REQUIRED DUE TO CAT B REPAIR.

Part: STRINGER SPLICE — CORRODED (BS 1219-1225) · airframe 110,845 hrs · 17,158 cycles

CABIN STA 1219-1215 S-19R STRINGER SPLICE BRACKET FOUND CORRODED, REFERENCE NRC 9131413. CABIN STA 1219-1225 STR 19R STRINGER SPLICE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02. RII INSPECTED.

Part: FLOORBEAM — DAMAGED (BS 1087) · airframe 110,845 hrs · 17,158 cycles

CABIN - STA 1087 LBL 23 FLOOR BEAM FOUND FLOOR PANEL HOLE ELONGATED. (REF NR LP 9131027). CABIN STA 1087 LBL 23 FLOOR BEAM UPPER FLANGE REPAIRED AS PER SRM 53-00-51 REPAIR 2 FIG 201.

Part: STRINGER SPLICE — CORRODED (BS 1215-1219) · airframe 110,845 hrs · 17,158 cycles

STA 1219-1215 S-19R STRINGER SPLICE BRACKET FOUND CORRODED, THE STRINGER SPLICE WAS REPLACED IAW SRM 51-10-02 AND SRM 51-40-02.

Part: FLOORBEAM — DAMAGED (BS 1087) · airframe 110,845 hrs · 17,158 cycles

BS 1087, LBL 23 FOUND FLOORBEAM HOLE ELONGATED. . THE FLOORBEAM WAS REPAIRED AS PER SRM 53-00-51 REPAIR 2 FIG 201.

Part: CONTROL ROD — DAMAGED (LE SLAT) · airframe 109,266 hrs · 16,942 cycles

EICAS LE SLAT ASYM DEBRIEFED INBD FLIGHT CREW REPORTS NO OVERWEIGHT LANDING. REF FIM TASK 27-81-00-815-809 BLOCK 5, BITE TEST OF PSEU SHOWS INSPECTION FOUND OUTBOARD ROD ASSEMBLY BROKEN WITH DAMAGE TO THE WING LEADING EDGE ABOVE THE ROD MEASURING APPROX 2 AND 5/8 INCHES ACROSS AND 1 INCH LONG FAULT CODE 305 TARGET, INDICATING NR 7 LE SLAT RT OUTBD, ON CONTROL ROD. REMOVED PANELS 611KB AND 611NB FOR ACCESS. ALSO REMOVED DAMAGED 1-001. INSTALLED UPPER BOLT TO THE SLAT CONTROL ROD REF AMM 27-81-20-90 CORRECTION OF REF FOR INBOARD SLAT OUTBD ROD CONNECTION TO ACTUATOR REF 27-81-20-422-077. VERIFIED INSTALL OF ROD TO ROTARY ACTUATOR COMPLETED INSTALL OF ROD TO SLAT REF AMM 27-81-01-216-002, IPC 2 7-81-31-05, AND AMM 27-81-01-424-143. OPERATED SLATS THROUGH COMPLETE TRAVEL SEVERAL TIMES, ALL OPS SMOOTH AND NORMAL INDICATION

Part: WARNING LIGHT — FALSE ACTIVATION (TE FLAPS) · airframe 104,837 hrs · 16,347 cycles

FLAP DISAGREE AT FLAPS 5 EXTENSION. EMERGENCY DECLARED. TE FLAP DISAGREE SELF RESET AFTER PRESSURIZING ADP AND HYD ELEC PUMPS. FLAPS-SLATS FULLY EXTENDED AND ALL ROTARY ACTUATORS INSPECTED FOR OVERLOAD TRIP INDICATORS, NO FINDINGS. SEVERAL FLAPS-SLATS FULL FUNCTIONS PERFORMED, ALL NORMAL OPERATION. ALTERNATE ELECTRIC MODE ALSO TESTED AND FOUND WORKING "NORMAL" AS REPORTED BY INBOUND CREW.

Part: TRANSMITTER — OUT OF LIMITS (TE FLAPS) · airframe 104,652 hrs · 16,324 cycles

TE FLAP DISAGREE EICAS MSG ON APR LANDED F20 MSG ON APR WHEN FLAP LEV ER TO FLAPS 1 LANDED. EMERGENCY DECLARED. PERFORMED FSEU BITE REF FIM 27-51-00-815-808 AND NO CURRENT FAUL TS DISPLAYED. CYCLED FLAPS TO FULL TRAVEL WITH ELEC HYD PUMPS ON AND HAD A TRAILING EDGE FAULT LIGHT FOR 3-4 SECONDS ON MID WAY FROM 1 TO 5 APROX. AFTER THAT SECONDS FAULT LIGHTS GOES AWAY. FA ULT DID NOT REPEAT WITH ADP IN ON POSITION. FOUND #8 TRIPPED, PER FCD 2700-01993 STEP 11.00, TRIP INDICATOR WAS RESET. ADJUSTED #1 AND #8 T/E FLAP TRANSMITTERS PER B767 AMM 27-51-45-762-129. VALUES WITHIN LIMITS. REMOVED AND REPLACED HYD AIR PUMP "ON" TIME DELAY,(M305) REPLACED S35 CTR HYD SYSTEM S35 PRESSURE SWITCH REF B767AMM 29-109.OPS AND LEAK CHECKS GOOD. LUBED LEFT AND RIGHT TRAILING EDGE FLAPS AS REQUIRED PER FCD.

Part: ALTIMETER — INACCURATE (STANDBY) · airframe 104,482 hrs · 16,298 cycles

STANDBY ALTIMETER NEEDLE INDICATES 540, DIGITS INDICATE 100. REMOVED AND REPLACED THE STANDBY ALTIMETER IAW MM 34-13-06. OPS CHECKED GOOD.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 98,551 hrs · 15,478 cycles

NR 2 PYLON PANEL 426BR CUTOUT SKIN FOUND CRACKED. AD STRUCTURAL INSPECTION FINDING 76-5400-1-2512, NR 2 PYLON PANEL 426BR CUTOUT SKIN CRACKED. CRACK LENGTH 0.156", AREA REPAIRED IAW SRM 54-53-01, REPAIR 6, FIG 201, DETAIL III AND ATTACH FORM 44.0008 WORKSHEET ITEM 1 TO 14 WORK ACCOMPLISHED.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 98,551 hrs · 15,478 cycles

NR 1 PYLON PANEL 446BL CUTOUT SKIN FOUND CRACKED, AD STRUCTURAL INSPECTION FINDING. NR 2 PYLON PANEL 446BL CUTOUT SKIN CRACKED LENGTH 0.125" AND CRACKED AREA REPAIR IAW SRM 54-53-01, REPAIR 7, FIG 201, DETAIL I.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 98,551 hrs · 15,478 cycles

CABIN BS1518, LBL 1 TO RBL 3 FLOORBEAM FOUND CORROSION. CABIN FLOORBEAM AT BS1518, LBL1 TO RBL 3 UPPER CHORD CORROSION REMOVED IAW SRM 51-10-02. BLENDED AREA D 0.065", ORIGINAL THICKNESS 0.090", WITHIN 2" X 8" LENGTH OUT OF SRM 53-00-51. ALLOWABLE DAMAGE 1, FIG 101, LIMIT AND FLOORBEAM UPPER CHORD CORROSION. REMOVED AREA, REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201 AND FORM 44.0008 ATTACHED ITEM 1-18.

Part: HOUSING — BROKEN (EVAC SLIDE) · airframe 98,551 hrs · 15,478 cycles

LEFT OFF WING ESCAPE SLIDE CABLE SYS DISCONNECT HOUSING FOUND BROKEN AT THE ARM, AD FINDING IAW EA 2560-02662 REV A. FX LT OFF WING ESCAPE SLIDE CABLE SYS DISCONNECT HOUSING REPLACED & ADJUSTED IAW EA 2560-02662 REV A OP 001 & AMM 25-65-04.

Part: HOSE — KINKED (EVAC SLIDE) · airframe 98,551 hrs · 15,478 cycles

RIGHT FX OFF WING SLIDE CYLINDER INFLATION HOSE FOUND CONTAMINATED WITH HYD FLUID & KINKED AT CLAMPS AREA. REPLACED IAW AMM 25-65-02 & FORM 44.0008 ITEM 1 ACCOMPLISHED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 97,787 hrs · 15,372 cycles

EXTERIOR EMER EXIT LIGHT INOPERATIVE. RT SIDE OF FUSELAGE JUST FWD OF AFT CARGO DOOR. RELAMPED EXTERIOR EMER EXIT LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 97,373 hrs · 15,317 cycles

EXTERNAL EMERGENCY LIGHT AT R2 DOOR INOPERATIVE. RELAMPED, R & R AFT RT LIGHT ASSEMBLY. FOUND PUSHED BACK PIN AT CONNECTOR M733, SECURED IAW WDM 33-51-06. OPERATIONS NORMAL.

Part: SPAR — CRACKED (WING) · airframe 90,389 hrs · 14,367 cycles

ECRA 5710-02320, DURING A SPECIAL HOLD & THE ACCOMPLISHMENT OF EA 5710-02220 OP 03, A CRACK WAS DISCOVERED ON THE WING CTR SECTION, FRONT SPAR RING CHORD PN 111T2023-5. THE CRACK WAS FOUND AT A FASTENER HOLE, BETWEEN STRINGER 28L & 29L. THE REPAIR IAW ECRA 5710-02320 HAS RECEIVED FIRST STAGE APPROVAL. A NEW FORM 8100-9 SHOWING FULL COMPLIANCE WITH 14 CFR 26.43D & 25.571 MUST BE RECEIVED BEFORE 24 OCT 2015 FOR THE ACFT TO REMAIN AIRWORTHY.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 95,561 hrs · 15,061 cycles

EMERGENCY EXIT FLOOR LIGHT INOPERATIVE, JUST OUTSIDE OF AFT INBD LAVATORY. SECURED CONNECTOR. OPERATIONS CHECKED NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 95,561 hrs · 15,061 cycles

EMERGENCY EXIT FLOOR EEL INOPERATIVE JUST OUTSIDE OF AFT INBD LAVATORY. SECURED CONNECTOR, OPERATIONS CHECKED NORMAL.

Part: SCREEN — DIRTY (SMOKE DETECTOR) · airframe 94,514 hrs · 14,920 cycles

OUTBOARD LAVATORY AT DOOR 2R SMOKE DETECTOR TURNS ON WHEN POWER TO ACFT TURNED ON. HAPPENED A FEW TIMES, WAS ABLE TO RESET DETECTOR EACH TIME. FOUND MESH SCREEN DIRTY. CLEANED SCREEN IAW AMM 26-13-01. CYCLED ACFT POWER OFF & ON SEVERAL TIMES WITH NO SMOKE DETECTOR ALARM GOING OFF. HAD GREEN POWER INDICATOR ILLUMINATED EACH TIME.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 93,893 hrs · 14,835 cycles

EMERGENCY EXIT FLOOR EEL INOPERATIVE AT RT CTR LAVATORY. SECURED CONNECTOR. OPERATIONS CHECKED NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 93,829 hrs · 14,827 cycles

TRAILING EDGE FLAP DISAGREE ON INITIAL. LANDING FLAPS 20 VISUAL INSPECTION TE FLAPS SLATS PERFORMED WITH FLAPS EXTENDED, NO FINDINGS. FUNCTIONAL TEST IAW AMM 27-51-00 WITH NO FAULTS. FSEU BITE, NO TROUBLE FOUND.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 93,074 hrs · 14,721 cycles

CORROSION IN MAIN CABIN FLOOR T CAP BS 303 LBL 16 BS 303 BL 16. REPLACED UPPER T CORD IAW SRM 51-40-02 PAGE 4 PARA 7 FIG 2.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 93,074 hrs · 14,721 cycles

CORROSION OF FRAME ANGLE SHEAR TIE AT BS 1562 BL0 IN AFT CARGO COMPARTMENT. R & R SHEAR TIE AT BS 1562 BL0 IAW SRM 51-40-02 PARA 4 & 7 FIG 4, 7, 8 & 12 & SRM 53-00-07 FIG 101.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 93,074 hrs · 14,721 cycles

S37R CORRODED AFT OF BS 1540. REMOVED DAMAGE. FABRICATED & INSTALLED REPAIR PARTS IAW SRM 53-00-03 REPAIR 2.

Part: FLOORBEAM — PUNCTURED (FUSELAGE) · airframe 93,074 hrs · 14,721 cycles

AFT CARGO COMPARTMENT FLOORBEAM BS 1197+44 RBL 13 HAS A PUNCTURE IN WEB. REPAIRED IAW ECRA 5310-06238 REV A. THIS IS A PERMANENT REPAIR.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 93,074 hrs · 14,721 cycles

AFT PIT BS 1540 STRINGER 39R CORROSION. REMOVED DAMAGE, FABRICATED & INSTALLED REPAIR PARTS IAW SRM 53-00-03.

Part: FITTING — CORRODED (FUSELAGE) · airframe 93,074 hrs · 14,721 cycles

AFT PIT STRINGER 39L END FITTING AT AFT PRESS BULKHEAD: CORROSION. REMOVED DAMAGE. FABRICATED & INSTALLED REPAIR PARTS IAW SRM 51-40-05 & 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 93,074 hrs · 14,721 cycles

CORROSION ON FLOORBEAM IN MAIN CABIN FLOOR BS 287 FROM LBL 16 - 26 BS 287, BL 16 - 26. REMOVED CORROSION ON MAIN CABIN FLOORBEAM IAW SRM 51-10-02 PARA 15 FIG 1. 100% MATERIAL LOSS. FLOORBEAM OUT OF LIMITS IAW SRM 53-00-51 FIG 101. REPAIRED FLOORBEAM IAW SRM 53-00-51 FIG 201 REPAIR 1.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 93,074 hrs · 14,721 cycles

AFT CARGO COMPARTMENT BS 1395 SHEAR TIE BETWEEN STRINGER 38L - 39L CORRODED. R & R AFT CARGO COMPARTMENT SHEAR TIE IAW SRM 51-40-02 PAR 4 B & FIG 12.

Part: SKIN — DENTED (FUSELAGE) · airframe 93,074 hrs · 14,721 cycles

EXT FUSE SKIN BS 1720 - 1730 BETWEEN STRINGER 25R & 27R, DENT IN SKIN. REMOVED DAMAGE, HFEC, FABRICATED & INSTALLED REPAIR PARTS IAW ECRA 5330-04888.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 93,074 hrs · 14,721 cycles

MAIN CABIN BS 325 RBL 52 - 60 FLOORBEAM CORRODED. REMOVED DAMAGE, FABRICATED & INSTALLED REPAIR PARTS IAW SRM 53-00-51 REPAIR 2.

Part: BEAM — CORRODED (FUSELAGE) · airframe 93,074 hrs · 14,721 cycles

FORWARD CABIN WET AREA BS 325 LBL 16. CORROSION UNDER BEAM CAP AROUND FASTENER HOLE. REMOVED DAMAGE, FABRICATED & INSTALLED REPAIR PARTS IAW SRM 53-00-51 REPAIR 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 93,074 hrs · 14,721 cycles

CABIN FLOOR STRUCTURE BS 848 RBL 54.75 CORRODED. REMOVED DAMAGE, FABRICATED & INSTALLED NEW FLOORBEAM BS 838 TO 883 RBL 54.75 IAW SRM 53-00-51.

Part: ENGINE — VIBRATION (NR 2) · airframe 92,971 hrs · 14,706 cycles

NUMBER 2 ENG VIBRATION. ENG NR 2 NEEDS A VIBRATION SURVEY TEST NR 8 ACCOMPLISHED IAW MM 71-00-00-725-008-N00. COMPLETED VIBRATION SURVEY, VIBRATION WELL WITHIN LIMITS IAW JRH. HIGHEST READING WAS 1.6 AT 82 PER CENT N1 FAN IAW MM 72-31-00 PG 507.

Part: UNKNOWN — LEAKING (HYDRAULIC SYS)

FLIGHT CANCELLED DUE TO HYD LEAK. REMOVE UNDERWING PANEL TO SEARCH FOR SOURCE.

Part: WINDSHIELD WIPER — DAMAGED (WINDSHIELD) · airframe 91,212 hrs · 14,469 cycles

CAPTAIN`S SIDE WIPER BLADE FLEXES & APPEARS TO BE BROKEN. REPLACED CAPTAIN'S SIDE WIPER ARM & BLADE IAW AMM, CHECKED GOOD.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 90,932 hrs · 14,435 cycles

C2 HYD PUMP LEAKING. R & R C2 HYD ACMP PUMP, OPERATIONS & LEAK CHECKED GOOD.

Part: PIN — BROKEN (EVAC SLIDE) · airframe 90,932 hrs · 14,435 cycles

IAW EQ5099 TO R & R LT OVERWING SLIDE. IPC 25-65-08-01 LOCATING PIN ITEM 280 TWO EACH BROKEN. R & R OVERWING SLIDE LOCATING PINS AS REQUIRED.

Part: SPAR — CRACKED (WING) · airframe 90,389 hrs · 14,367 cycles

A CRACK WAS DISCOVERED ON THE WING CNTR SECTION FRONT SPAR RING CHORD PN 111T2023-5. THE CRACK WAS FOUND AT A FASTENER HOLE BETWEEN S28L & S29L. IAW PART 1 STEP 2 OF ECRA INITIATE A CF FOR TIME LIMIT ON FAA FORM 8100-9 TO BE RECEIVED BEFORE 24 OCT 2015. THE REPAIR PER ECRA 5710-02320 HAS RECEIVED FIRST STAGE FAA APPROVAL. A NEW FORM 8100-9 SHOWING FULL COMPLIANCE WITH 14 CFR 26.43D AND 25.571 MUST BE RECEIVED BEFORE 24 OCT 2015 FOR THE AC TO REMAIN AIRWORTHY. INF- :THE REPAIR IS BEING EVALUATED FOR DMG TOLERANCE & WILL LIKELY BE MADE PERMANENT WITH REPEATED INSPECTIONS. CONTACT ENGINEERING AFTER 24APR15 BUT PRIOR TO 24MAY15 FOR DISPOSITION.

Part: SHUTOFF VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 90,353 hrs · 14,361 cycles

DURING TROUBLESHOOTING OF NR 2 ENG IAW EM4271-2, FOUND LPT COOLING SHUTOFF VLV NOT FULLY CLOSING. FOUND HPT VLV IN THE OPEN POSITION WHEN SHOULD BE CLOSED IAW MM75-24-00-601. REACTIVATED & CHECKED THE TCC ACTUATION SYSTEM IAW AMM 75-24-00. RAN NR 2 ENG ACCOMPLISHED TEST NR 2 & NR 6 IAW 71-00-00.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 90,329 hrs · 14,356 cycles

CABIN ALT CONTROL KNOB ONLY ROTATES 10S DIGITS STUCK ON 2500. REPLACED CABIN PRESS CONTROL PANEL & ACP TEST PER SAME.

Part: CIRCUIT CARD — FAULTY (CARGO BAY) · airframe 90,278 hrs · 14,348 cycles

FWD CARGO PANEL DOOR CLOSED LIGHT INOPERATIVE WITH DOOR CLOSED. PUSHED TO TEST, WORKED NORMAL. DOOR CLOSED LIGHT SOCKET DEFECTIVE. DOOR OPEN LIGHT STAYS ON ALL THE TIME. REPLACED CARD NR 7 MR32030, DRIVER CARD, CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (CARGO BAY) · airframe 90,263 hrs · 14,346 cycles

FWD CARGO DOOR OPEN LIGHT AT PANEL TRIPPING J4 P36 CIRCUIT BREAKER.

Part: PROCESSING UNIT — FAULTY (FUEL SYSTEM) · airframe 90,136 hrs · 14,329 cycles

CENTER FUEL TANK QTY INOPERATIVE. FOUND FAULT "BITE DISPLAY BOARD FAILED G". R & R FUEL PROCESSOR UNIT IAW AMM 28-41-08, BITE CHECKED GOOD, INDICATIONS NORMAL.

Part: HEAT EXCHANGER — FAULTY (NR 2 IDG) · airframe 90,119 hrs · 14,326 cycles

STATUS MESSAGE RT IDG VALVE. R & R IDG AIR OIL HEAT EXCHANGER OF RT ENGINE.

Part: START VALVE — FAULTY (LT ENGINE) · airframe 90,022 hrs · 14,314 cycles

LT START VALVE WILL NOT OPEN, DEFERRED IAW MEL 8000C. REPLACED LT START VALVE IAW AMM, ENGINE MOTORING CHECKED OK.

Part: UNKNOWN — INOPERATIVE (CABIN) · airframe 89,937 hrs · 14,305 cycles

PIGTAIL NR 52 INOPERATIVE. SECURED PIGTAIL NR 52, OPERATIONS CHECKED NORMAL.

Part: INDICATION SYS — READS HIGH (CENTER FUEL CELL) · airframe 89,919 hrs · 14,303 cycles

CENTER FUEL QUANTITY READING 52000 LBS. FUEL STICK INDICATES CENTER TANK HAS 32000 LBS OF FUEL. REPLACED FISH YAW AM. OPERATIONS CHECKED YAW AM, ALL CHECKED NORMAL. STUCK TANK USING FUEL MANUAL 07-04-09 PG4, READ 21.2 WITH DENS OF 6.55. ALL CHECKED NORMAL WITH GAUGES.

Part: WIRE HARNESS — DAMAGED (FUEL QTY PROBE) · airframe 89,536 hrs · 14,252 cycles

CENTER TANK FUEL QTY INDICATION FLUCTUATED BETWEEN 1100 LBS AND 30800 LBS OVER APPROX 1.5 HRS. VERIFIED CENTER TANK FUEL LOAD USING DRIPSTICKS, CTR TANK FUEL QTY PLACED ON MEL 2841A. PROCESSOR PREVIOUSLY REPLACED AND FUEL TANK EXTERNAL WIRING CHECKED WERE FOUND GOOD. REPLACE LT AND RT AUX FUEL TANK WIRING HARNESSES. REPLACED AUX (CTR) FUEL TANK LT & RT QTY PROBE HARNESS.

Part: PUMP — MALFUNCTIONED (CENTER FUEL) · airframe 89,534 hrs · 5,346,007 cycles

TAXIING OUT, CENTER FUEL PUMPS CYCLING ON AND OFF. FOUND CENTER TANK FUEL LOAD AT 1100 LBS USING FUEL STICK METHOD. CENTER TANK PUMP OPS NORMAL.

Part: PROCESSOR — FALSE INDICATION (FUEL QTY) · airframe 89,346 hrs · 14,231 cycles

FMC MESSAGE FUEL DISAGREE PROG 2. CENTER TANK DISAGREES BY 20.0 LBS. SUMPED CENTER TANK TO ZERO. REPLACED FUEL QTY PROCESSOR IAW 28-41-08 AND ADDED KNOWN QTY TO CENTER TANK. ALL CHECKED NORMAL. PROCESSOR REPLACED DUE TO SHOP HISTORY OF CTR FUEL QTY PROBLEMS WITH NO TROUBLE FOUND. ACFT OK TO CONTINUE.

Part: RELAY — FAULTY (FUEL TRANSFER) · airframe 89,197 hrs · 14,211 cycles

CENTER FUEL PUMPS WILL NOT TRANSFER FUEL. R & R FUELING POWER TRANSFER RELAY, OPS CHECKED GOOD.

Part: OXYGEN MASK — UNSECURE (AREA 1C) · airframe 89,157 hrs · 14,206 cycles

PAX O2 MASK HAS FALLEN AT 1C. REPACKED O2 MASKS AT 1C.

Part: FAN — FAILED (EQUIP EXHAUST) · airframe 89,142 hrs · 14,204 cycles

FWD EQUIPMENT EXHAUST FAN INOPERATIVE WITH STATUS MESSAGE. REPLACED FWD EQUIPMENT EXHAUST FAN IAW AMM.

Part: CHARGER — FAILED (MASTER BATTERY) · airframe 89,109 hrs · 14,200 cycles

MAIN BATTERY CHARGER STATUS MESSAGE WILL NOT CLEAR. REPLACED BATTERY AND BATTERY CHARGER.

Part: MONITOR — FAULTED (FWD EQUIPMENT) · airframe 88,968 hrs · 14,182 cycles

FWD EQUIPMENT OVHT ON TAXI OUT. REPLACED FWD EQUIPMENT COOLING VIBRATION MONITOR. OPS CHECK GOOD, RESTORED AC TO NORMAL.

Part: HYDRAULIC SYSTEM — LEAKING · airframe 88,952 hrs · 14,180 cycles

HYDRAULIC FLUID LEAKING FROM BASE OF RUDDER AT A RATE OF 1 DROP EVERY 5 SECS.

Part: SENSOR — FAULTED (WINDOW HEAT) · airframe 88,945 hrs · 14,179 cycles

RIGHT FWD WINDOW EICAS MESSAGE. REPLACED WINDOW HEAT CONTROLLER. PERFORM FIM 30-41-00, PG 111, BLK 23 AND SWAP SENSORS TO SPARE. OPS CHECKS GOOD.

Part: ACTUATOR — STUCK (LT AILERON) · airframe 88,913 hrs · 14,175 cycles

LEFT INBD AILERON STUCK, FLT DIVERTED. FLT CREW ATTEMPTED TO MOVE AILERON. NO MOVEMENT NOTED. REPLACED LEFT INBD AILERON OTBD PCA IAW MM.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 88,392 hrs · 14,109 cycles

SEAT 1K LOWER EMERGENCY LIGHT LENS IS DAMAGED. REPLACED LENS.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,120 hrs · 14,076 cycles

WINDOW EICAS MSG DISPLAYED POSITION 3(1-L FWD,2=L SIDE,3= R FWD,4=R SIDE).INOP LIGHT ILLUM. INOP LIGHT DID NOT EXTINGUISH WHEN SWITCH WAS RECYCLED TO OFF THEN ON. FRM 30 41 02 -. CREW COMMENTS: CLIMBING THRU FL280 R FWD WINDOW HEAT INOP CHRONIC RAN C LIST, NO HELP. CHECK WIRING TO WINDOW ALL OK, CHECK CONDITION OF WINDOW NO BURNING MARKS PERFORMED BITE CHECK OF WHCU AS PER AMM (30-41-00 FIG 103 BLOCKS 1 THRU 3). COMPONENTS AND INTERFACE GOOD, SWITCH WINDOW HEAT ON, ALL INDICATIONS GOOD.

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 88,080 hrs · 14,071 cycles

RIGHT ENG HPSOV EICAS AND ASSOCIATED ENG BLEED LIGHT ON INTER DURING DESCENT. DUE HISTORY RIGHT ENG HPSOV SECURED CLOSED IAW MEL 3611R. AIR SYSTEM BITE PERFORMED. NO FAULTS. ONLY SATIS MESSAGE RIGHT ENG HPSOV. REPLACED HPSOV PER AMM 36-11-07 PG 401, NEED TO PERFORM HEALTH CHECK ADJUSTMENT AND TEST PER REF 36-00-99 PG 501. RPL- :IAW AMM 36-11-07 WITH REPLACEMENT OF HPSOV AIR SUPPLY SYSTEM BITE CHECK IAW AMM NEEDS TO BE PERFORMED. PERFORMED AIR SUPPLY BITE CHECK AND RAN NR 2 ENGINE NO EICAS MSG OR BLEED LIGHT.

Part: CONNECTOR — REVERSED (IGNITION SYS) · airframe 88,080 hrs · 14,071 cycles

LEFT ENGINE NR 2 IGNITION SYSTEM INOPERATIVE. FOUND M7196 NR 1 EXCITER BOX CONNECTOR SWAPPED WITH M7197 NR 2 EXCITER BOX CONNECTOR. WRONG IGNITION SYSTEM BEING TROUBLESHOT AND PARTS REPLACED. CORRECTED CONNECTOR POSITIONS AND REPLACED LEAD AND PLUG ON NR 1 SYSTEM. IF HIT AGAIN REPLACE EXCITER BOX. STARTED ENGINE THREE TIMES NORMAL.

Part: SHUTOFF VALVE — FAULTED (NR 2 ENGINE) · airframe 88,043 hrs · 14,065 cycles

RIGHT ENGINE HPSOV STATUS MESSAGE ANNUNCIATED DURING DESCENT AT HIGH ALTITUDE WENT OUT WHEN LEVELING OFF. HPSOV SECURED CLOSED. REPLACED HPSOV IAW AMM, BITE CHECKED GOOD.

Part: WINDOW — CRACKED (R1) · airframe 87,977 hrs · 14,057 cycles

R1 WINDOW CRACKED. REMOVED R1 WINDOW IAW MM. ACCOMPLISHED INSTALLATION OF WINDOW THROUGH STEP 12.

Part: PUMP — FAILED (FUEL SYSTEM) · airframe 87,945 hrs · 14,053 cycles

LEFT CENTER FUEL PUMP CIRCUIT BREAKER TRIPPED. REPLACED LT CENTER FUEL OVRD PUMP.

Part: BLADE — DENTED (NR 1 ENGINE) · airframe 87,924 hrs · 14,048 cycles

NR 1 ENGINE, NR 1 BLADE DENTED. REMOVED DENT FROM 22.5 INCH FROM ROOT AND 15-64TH DEEP PER MM 72-31-02. ACCOMPLISHED HFEC BLADE INSPECTION PER NDT PART 6 72-32-401. NO DEFECTS NOTED.

Part: PANEL — UNSECURE (CABIN) · airframe 87,798 hrs · 14,029 cycles

CEILING PANEL FIRST CLASS NEEDS TO BE SECURED. AFT LATCH BROKEN. REPLACED LATCH AND LANYARD. RE-INSTALLED CEILING PANEL.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 87,474 hrs · 13,987 cycles

EICAS MESSAGE TE FLAP DISAGREE DISPLAYED, TRAILING EDGE LIGHT ILLUMINATED, WHEN ANY TE FLAP POSITION SELECTED. FLAPS FAIL TO MOVE TO SELECTED POSITION. EXTENDED TO 20 USING ALT TE SYSTEM IAW CHECKLIST. FLAP SLAT SYSTEM CYCLED WITH NORMAL MODE WITHOUT ANY FURTHER REMARKS.

Part: WIRE — CUT (EMERGENCY LIGHT) · airframe 87,414 hrs · 13,978 cycles

RIGHT MID LAVATORY LOWER SIDE EMERGENCY LIGHT INOPERATIVE. FOUND 6 FT LONG FLOOR LAMP CONNECTOR END CUT OFF WHEN CARPET WAS INSTALLED. RELAMPED, CHECKED OKAY.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 87,414 hrs · 13,978 cycles

EMERGENCY LIGHT AT RT MID LAVATORY AND EXIT SIGNS BELOW BOTH RT OVERWING EXIT DOORS ARE INOPERATIVE. CHARGED BATTERY, OPS CHECKED GOOD.

Part: CONNECTOR — FAULTED (EMERGENCY LIGHT) · airframe 87,414 hrs · 13,978 cycles

DOOR 2 LEFT FWD LOWER SIDE EMERGENCY LIGHT INOPERATIVE. RESEATED CONNECTOR ON EMERGENCY BATTERY PACK, OP CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 87,414 hrs · 13,978 cycles

RIGHT WING EXIT LIGHT FWD SIDE INOPERATIVE. FOUND EXIT SIDE NOT CONNECTED BEHIND SIDEWALL, OPENED DADO PANEL AND CONNECTED CONNECTOR, EMERGENCY LIGHTS OP CHECKED GOOD ON GROUND.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 87,414 hrs · 13,978 cycles

LEFT WING EXIT LIGHT AFT SIDE INOPERATIVE. FOUND CONNECTOR BEHIND SIDEWALL PANEL DISCONNECTED, CONNECTED CONNECTOR BEHIND DADO PANEL, OP CHECKED GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 87,414 hrs · 13,978 cycles

DOOR 2 LEFT FWD EXIT SIGN INOPERATIVE. RESEATED CONNECTOR ON EMERGENCY BATTERY PACK, OPS CHECKED GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 87,414 hrs · 13,978 cycles

FWD DOOR NR 1 RT BOTTOM OF DOOR EMERGENCY LIGHT SIGN INOPERATIVE. REMOVED SIGN. ALL OTHER EMERGENCY LIGHTS OPERATE GOOD. REPLACED LIGHT ASSY. LIGHT OPS NORMAL AT THIS TIME.

Part: COVER — UNSECURE (PUMP SWITCH) · airframe 87,202 hrs · 13,947 cycles

RIGHT CENTER FUEL PUMP SWITCH WILL NOT TURN OFF. SECURED OVERHEAD PANEL COVER PLATE TO FUEL SWITCHES. OPS OK.

Part: CONNECTOR — FAULTY (FIRE BOTTLE) · airframe 86,781 hrs · 13,891 cycles

CARGO FIRE BTL DISCHARGE LIGHT DOES NOT TEST. REMOVED AND REINSTALLED CONNECTOR FROM LIGHT LENS FROM CARGO BOTTLE DISCHARGE LIGHT ASSY. LIGHT TEST NORMAL.

Part: CONNECTOR — MALFUNCTIONED (FIRE WARNING) · airframe 86,772 hrs · 13,889 cycles

CARGO FIRE BTL DISCHARGE LIGHT DOES NOT TEST. DEFERRED DUE TIME COMPLIED WITH REQUIREMENTS CONTAINED IN MEL 2620G. REMOVED AND REINSTALLED CONNECTORS FROM LIGHT LENS FROM CARGO BOTTLE DISCHARGE LIGHT ASSY LIGHT TEST NORMAL.

Part: LINE — LEAKING (BRAKE SYSTEM) · airframe 86,760 hrs · 13,886 cycles

RIGHT MAIN GEAR HAS HYDRAULIC LEAK FROM AREA ABOVE TOP OF STRUT. LEAKING AT A CONTINUOUS RATE. REPLACED BRAKE FLEX LINE REF IPC 32-41-62-005 ITEM 172, AND DAMAGED ELBOW ITEM 227 AND IT EM 230 (NUT) HAS BEEN SUBSTITUTED WITH PCN 710-2831. WAITING FOR ECRA TO BE ISSUED FOR THIS (NUT) SUBSTITUTION. LEAK CHECK HAS BEEN ACCOMPLISHED. NO LEAKS NOTED.

Part: SIGN — UNSECURE (CABIN) · airframe 86,735 hrs · 13,882 cycles

EXIT SIGN ON LEFT OVERWING FELL OFF. RE-INSTALLED AND TESTED SIGN AS PER MM.

Part: VALVE — FAULTY (BRAKE SYSTEM) · airframe 86,725 hrs · 13,879 cycles

BRAKE PSI DROPPED TO 2000 PSI IMMEDIATELY AFTER SETTING BRAKE. APPLIED MEL, PARK BRAKE VALVE CB 'F4' PULLED & COLLARED, ANTI-SKID AND AUTO BRAKES INOP PER MEL 3244E. -INF- :NO FURTHER BRAKE ACCUMULATOR PRESSURE DECAY WITH PARK BRAKE VALVE IN POSITION '2'. PARTS: (643-9272 MR29240 VALVE). REPLACED PARKING BRAKE VALVE. PERFORMED PARKING BRAKE SYSTEM TEST.

Part: SENSOR — FAULTY (LE SLAT) · airframe 86,716 hrs · 13,876 cycles

CREW REPORTS ON INITIAL FLAP RETRACTION, FLAP STUCK BETWEEN 1 DEG AND UP. L/E SLAT ASSY EICAS MSG DISPLAYED. REMOVED & REPLACED L/E SLAT SENSORS S285 & S298 IAW MM 27-88-01. PSEU BITE TEST GOOD IAW MM 27-88-01. PERFORMED GVI OF ROTARY ACTUATORS & BOTH PDU'S. NO VISUAL DEFECTS NOTED.

Part: LIMITER — OUT OF TOLERANCE (L1 DOOR) · airframe 86,715 hrs · 13,875 cycles

MAIN CABIN L1 DOOR LOAD LIMITER INDICATOR NUT OUT OF LIMITS, MORE THAN 1-8 INCH FROM HOUSING. REMOVED AND REPLACED MAIN CABIN L1 DOOR LOAD LIMITER IAW B767 AMM 52-11-21 LOAD LIMITER, OPS CHECK GOOD.

Part: LIGHT — DEFECTIVE (COCKPIT) · airframe 86,590 hrs · 13,858 cycles

F/O INST PANEL FLOOD LIGHTS WON`T LIGHT OR DIM WITH CONT KNOB. LIGHTS DO NOT ILLUM BRT WITH LGT OVRD SWITCH ON. REPLACED ASSY PER WS WD 33-11-11 AND OPS NORMAL.

Part: CAP — MISSING (WINDOW HEAT) · airframe 86,390 hrs · 13,832 cycles

WINDOW HT TERMINAL LUG BLOCK CAP MISSING. REPLACED CAP.

Part: FILTER — CLOGGED (GASPER DUCTS) · airframe 86,181 hrs · 13,800 cycles

VERY LOW AIRFLOW FROM BOTH PACKS. BORESCOPED ALL COCKPIT GASPER DUCTS FOR BLOCKAGE OR BROKEN DUCTS FOR APPROX 6FT, NO ISSUES NOTED. FOUND BOTH RECIRC FILTERS SEVERLY CLOGGED, PICS TAKEN. INCREASED AIRFLOW IN COCKPIT NOTICED AFTER FILTERS REPLACED. CLEANED SENSOR FILTERS.

Part: BLADE — NICKED (RT ENGINE FAN) · airframe 86,064 hrs · 13,785 cycles

NICK IN RIGHT ENG FAN BLADE AT ONE O’CLOCK FROM SPINNER MARK. REPAIRED BLADE PER AMM.

Part: FMU — FAULTED (NR 1 ENGINE) · airframe 85,732 hrs · 13,740 cycles

AFTER BOTH ENGINES STARTED, NR 1 ENGINE FUEL VALVE LIGHT FLICKERING DIMLY. NO EICAS MSG. SAMC TEXT: SHUT ENG DOWN, CYCLED CIRCUIT BREAKER P11-4 D25. ACCOMPLISHED NORMAL START, LIGHT STARTED FLICKERING AGAIN. REPLACED NR 1 ENGINE FMU REF MM. RAN ENGINE, OPERATIONAL CHECK NORMAL.

Part: SWIVEL — LEAKING (NLG) · airframe 84,276 hrs · 13,549 cycles

SIGNS OF HYDRAULIC FLUID IN NOSE LANDING GEAR AREA. FOUND EVIDENCE OF FLUID AROUND STEERING METERING VALVE (LOOKS LIKE SMALL WEEP THAT IS NOT NEW). CLEANED DOWN GEAR AND ACCOMPLISHED OPERATIONAL CHECK OF STEERING SYSTEM AND NO LEAKS AND NO WEAPAGE. REPLACED NOSE GEAR RETRACTION SWIVEL. PRESSURIZED RETRACTION ACTUATOR, NO LEAKS NOTED.

Part: CDU — FAILED (FMC) · airframe 84,127 hrs · 13,531 cycles

FMC PROBLEM. REPLACED CAPTAIN'S FMC COMPUTER DISPLAY UNIT, OP CHECKED GOOD ON GROUND CHECKS.

Part: STRUCTURE — LEAKING (CENTER TANK) · airframe 83,801 hrs · 13,488 cycles

FUEL LEAKING FROM CENTER TANK SEAM ABOVE THE LEFT AC PACK REHEATER (AREA WASHED AWAY). RESEALED SEAM.

Part: FITTING — LEAKING (CENTER TANK) · airframe 83,801 hrs · 13,488 cycles

FUEL LEAKING FROM LOWER RIGHT AFT SPAR TO FUSELAGE ATTACH FITTING (CENTER TANK). RESEALED FITTING RESEALED LEAKS IN CTR TANK, (SEE SEQ 8012030, 8012031, 8012032, 8012034-6).

Part: STRUCTURE — LEAKING (CENTER TANK) · airframe 83,801 hrs · 13,488 cycles

FUEL LEAKING FROM LEFT LOWER AFT SPAR TO FUSELAGE ATTACH FITTING (CENTER TANK). RESEALED FITTING & RESEALED SEAM IN CTR TANK.

Part: STRUCTURE — LEAKING (LT WING) · airframe 83,801 hrs · 13,488 cycles

FUEL LEAKING FROM LEFT LOWER WING ATTACH FITTING SEAM NEAR THE LEFT INBD CENTER TANK SUMP (SEALANT REMOVED). CLEANED AND RESEALED AREA INSIDE TANK. APPLIED SEALANT AT 0200 OF 26 FEB. OUTSIDE FITTING AND SEAM NEEDS TO BE RESEALED. RESEALED SEAM.

Part: STRUCTURE — LEAKING (RT WING) · airframe 83,801 hrs · 13,488 cycles

FUEL LEAKING FROM CENTER TANK SEAM JUST AFT OF THE RIGHT INBD TANK SUMP (PREVIOUSLY REPAIRED). CLEANED AND RESEALED AREA INSIDE TANK. SEALANT APPLIED 0200 OF FEB 26. OUTSIDE FITTING AND SEAM NEEDS TO BE RESEALED. RESEALED SEAM.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 83,801 hrs · 13,488 cycles

LT OBSERVERS RADIO CONTROL PANEL LIGHT PLATE INOP AND NONE OF THE RADIO SELECT BUTTONS ARE LIT. REPLACED CONTROL PANEL. LIGHTS AND OP CHECKED NORMAL.

Part: FLAP — MALFUNCTIONED (WING) · airframe 83,736 hrs · 13,478 cycles

TRAILING EDGE FLAP DISAGREE AT POSITION ONE USED ALTERNATE FLAP EXTENSION. ON ARRIVAL FSEU DISPLAYS FAULTS M548 OUTBD SLAT PDU RVDT MISRIG AND M603 FLAP LEVER RVDT MISRIG. RESET FLAPS TO SOWED USING ELECTRICAL SYSTEM AND CARRIED OUT MULTIPLE FLAP SLAT FUNCTIONS TO FULL EXTEND USING NORMAL SYSTEM. ALL OPERATES NORMALLY WITH NO VISIBLE SIGNS OF MISRIG OR FAULTS FROM EXTERNAL AND FLIGHT DECK. FURTHER FSEU TEST 164022 NOW INDICATES NO FAULTS WITH GREEN LED PASS LIGHT. PSEU FLAP SYSTEM 506 VERIFY DISPLAYS NO FAULTS. NO PREVIOUS HISTORY ON THIS DEFECT. AS PER FIM 27-51-00 FIG 104 SYSTEM CONSIDERED SERVICEABLE AND OK FOR FURTHER OPS.

Part: HYDRAULIC LINE — LEAKING (LT MLG) · airframe 83,729 hrs · 13,477 cycles

PIN HOLE IN LT MLG RETRACT LINE NEAR ACTUATOR. P/N 272T1200-316 TUBE. REMOVED LINE, HAD TO CUT ATTACHING LINE OFF AT LOWER AFT OUTBD END, LINE IS IN SHOP BEING MANUFACTURED, ALSO ORDERED ELBOW FOR UPPER FWD END TO LSVC DESK. REPAIRED LINE WITH RYNGLOCK AND REINSTALLED. LEAK CHECKS OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 83,647 hrs · 13,466 cycles

THE 19AB, 20AB EMER LIGHTS FLASH - *FIX DN. REPLACED POWER SUPPLY AND BATTERY ASSYS M1559 AND M737 AT SEAT 21A PER MM, TESTED AND OPS NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 83,533 hrs · 13,450 cycles

EEL LEFT CENTER FLOOR STRIP AND CENTER CROSS AISLE FLOOR STRIP ARE INOP. REPLACED EEL BATTERY BY SEAT 22A. OPS CHECKS NORMAL.

Part: UNKNOWN — LEAKING (LT ENGINE) · airframe 83,267 hrs · 13,415 cycles

OIL POOLED IN INLET OF LEFT ENGINE AND BEHIND FAN SECTION AND DRIPPING ONTO GROUND. INSPECTED ENGINE. SLIGHT POOLING IN INLET. OIL WETTING OR PUDDLING IN SPINNER AREA OK FOR SERVICE PER MM. OIL CONSUMPTION NORMAL.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 83,246 hrs · 13,413 cycles

OUTLFOW VALVE INOPERATIVE IN MANUAL MODE. CHECKED FOR VOLTAGE AT MOTOR. VOLTAGE PRESENT AT CLOSE AND OPEN CIRCUITS. REPLACED OUTFLOW VALVE ACTUATOR, PER AMM. AUTO AND MANUAL OPERATED NORMAL.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 83,206 hrs · 13,408 cycles

LAVATORY BY BUSINESS GALLEY, EMERGENCY LIGHT FLICKERS. CLEANED SECTION CONNECTORS AS PER AMM, ALL OPS OKAY. OPS CHECKED AND ALL OKAY.

Part: SLIDE — DETACHED (R1 DOOR) · airframe 83,060 hrs · 13,381 cycles

R1 DOOR SLIDE WAS PARTIALLY DEPLOYED. DOOR CHECK PERFORMED. FOUND DOOR SLIDE PARTIALLY DETACHED. REPLACED DOOR SLIDE PER MM.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 83,041 hrs · 13,378 cycles

ONE AREA OF EMER EXITS LIGHTS FLASHED ON AND OFF DURING DESCENT REPORTED BY PSGRS IN 19&20AB. RESEATED CONNECTOR ON AREA POWER SUPPLY, EMERGENCY LIGHTS OPS OK.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 83,039 hrs · 13,377 cycles

EMERGENCY LIGHTS CAME ON DURNG FLIGHT WITH SWITCH ARMED. OFF WHEN SWITCH IS OFF. FA REPORTS EMERGENCY LIGHTS ILLUMINATED CONTINUOUSLY AT 2R AND IN THE FWD PART OF AFT GALLEY. REPLACED POWER SUPPLY PER 33-51-07, OPS CHECKED OK.

Part: CONNECTOR — DIRTY (NR 1 ENGINE) · airframe 83,020 hrs · 13,374 cycles

IN CRUISE FLIGHT STATUS-MSG CAME ON L ENG EEC1. SAMC TEXT: ACTUAL FAULT CODE DOWNLINKED IS E352 BIT-14 FOR N1 RANGE FAIL CH-B. MAINT TEXT: PER TOMC ENG DOWNLOAD FAULTS 270A, 270B, 350A, 350B & 352B. ENG EEC NR 1 C1 & ENG NR 1 EEC C2 MSG. CLEANED ENG NR 1 N1 XDCR CONNECTOR. ACCP BITE REF 71-PIMU FIG 3 DURING ENGINE RUN, OK. NO STATUS MSG APPEARED OR FAULTS AT THE PIMU.

Part: LIGHT — UNKNOWN (UNKNOWN) · airframe 82,986 hrs · 13,368 cycles

EMERGENCY LIGHT AFT CABIN FLICKERS ROW 38 TO AFT GALLEY - ACCOMPLISHED CHECK OF LIGHTS AND CONNECTORS. ACCOMPLISHED OPS CHECK REF MM AND ALL OK.

Part: TRANSMITTER — ERRATIC (FUEL INDICATOR) · airframe 82,915 hrs · 13,358 cycles

IN CRUISE AT FL 360 WITH EPRS, N1 AND N2 BASICALLY MATCHED, NR 2 FF SHOWS ANYWHERE FROM 400 TO 1200#S HIGHER BURN THAN LEFT ENGINE. FF IS VERY ERRATIC ON RT ENGINE, BUT SEEMS TO BE VALIDATED BY THE HIGHER BURNOUT FROM THE RIGHT MAIN TANK. RT ENGINE FUEL FLOW TRANSMITTER WAS PREVIOUSLY REMOVED FOR FUEL FLOW FLUCTUATIONS.

Part: STRUCTURE — DAMAGED (RT WING TE FLAP) · airframe 82,414 hrs · 13,285 cycles

RIGHT INBD TRAILING EDGE FLAP DAMAGED. RT IB AFT FLAP WAS REPAIRED. REINSTALLED FLAP.

Part: CAP — DELAMINATED (RUDDER) · airframe 82,353 hrs · 13,275 cycles

RUDDER TIP DELAMINATED. REMOVED RUDDER CAP, ACCOMPLISHED 250 DEG PERMANENT REPAIR PER SRM. REPAIR COMPLETED AND PRIMER APPLIED. REINSTALLED AND SEALED. TOP COATED AND INSTALLED RUDDER CAP & EDGE SEALED.

Part: LIGHT — MISSING (FUEL PANEL) · airframe 81,587 hrs · 13,168 cycles

FUEL PANEL LIGHT IS MISSING. REPLACED MISSING LENS & BULB. FOUND BROKEN WIRE AT LIGHT ASSY. CAPPED WIRE. SECURED & CAPPED WIRE W047 2-A-A. NEEDS LIGHT ASSEMBLY REPLACED. UNIT IS HARD WIRED, NEED ENVIRONMENTAL SPLICES FOR INSTALLATION WITH POWER PLANE SIDE FOR HEAT SHRINK GUN. CAPPED WIRE IS UNDERNEATH LIGHT LENS. -INF- :LIGHT ASSY THAT WAS ON RES FOR 6458 NO LONGER AVAIL. ORDERED 563-0705 ON OSTF C2611. -INF- :LIGHT ASSY 563-0705 REQ FOR RPR, ALSO NEEDS LENS 563-4026 OSTF N6202. PCN:563-0705 PURCHASED FROM CO-IAH RCVD IN IADJL & ON RES PER - OPBLC 0047-20AUG. REPLACED LIGHT ASSY.

Part: NOZZLE — OBSTRUCTED (CARGO BAY) · airframe 81,368 hrs · 13,139 cycles

FWD SIDEWALL FIRE EXT NOZZLE PARTIALLY COVERED WITH PIT TAPE. REMOVED TAPE COVERING NOZZLE AND RETAPED.

Part: NOZZLE — OBSTRUCTED (CARGO BAY) · airframe 81,368 hrs · 13,139 cycles

BULK PIT CEILING FIRE EXT NOZZLE NEEDS RETAPING DUE PARTIALLY BLOCKING NOZZLE. REMOVED DAMAGED TAPE AND RETAPED.

Part: PCA — OUT OF ADJUST (RUDDER) · airframe 81,185 hrs · 13,103 cycles

PLANE NEEDS EXCESSIVE RT RUDDER TRIM, 3.5 UNITS. FFS MATCHED, L-EPR 1.27, R-EPR 1.22. ADJUSTED UPPER, MIDDLE AND LOWER PCA'S PER MM. ACCOMPLISHED INSPECTION OF THREE RUDDER ACTUATOR ADJUSTMENTS FOR SAFETY AND SECURITY, RIGS. ALL CHECKS OKAY.

Part: HOSE — BLOWN (MAIN BRAKE) · airframe 80,569 hrs · 13,012 cycles

RIGHT HYD QTY SHOWS .33. FOUND NR 7 MAIN BRAKE HOSE BLOWN. REPLACED NR 7 MAIN BRAKE HOSE PER MM. REFILLED HYD SYSTEM, OPS NORMAL.

Part: TRANSCEIVER — FAILED (WX RADAR) · airframe 80,475 hrs · 13,000 cycles

WX RADAR FAIL AND RT FLAG. REPLACED WEATHER RADAR TRANSCEIVER IAW AMM, OPERATION NORMAL.

Part: RUDDER — BINDING · airframe 80,157 hrs · 12,955 cycles

CREW REPORTED BOTH RUDDER PEDAL HEAVY AND BINDING. FOUND NO BINDING WITH HYD PRESS ON AND OFF. ACCOMPLISHED RUDDER PEDAL FORCE CHECK PER MM. FOUND ALL FORCES WITHIN LIMITS. AIRCRAFT TO BE TEST FLOWN FOR FURTHER EVALUATION.

Part: ROD — MISINSTALLED (RT MLG) · airframe 79,941 hrs · 12,924 cycles

WHEN CHANGING RT REAR TIRE ON RT MLG FOUND BRAKE ANTI ROTATION ROD ATTACH HARDWARE DAMAGED FROM BEING INSTALLED IMPROPERLY. REPLACED BRAKE ROD PER AMM.

Part: ACTUATOR — FAULTY (AILERON) · airframe 79,743 hrs · 12,897 cycles

THE "AIL LOCK" LIGHT ON AT LOW SPEED. EICAS MSG AILERON LOCKOUT DISPLAYED. OUTBD AILERONS DID NOT INDICATE NORMAL -LOCKED OUT- BOTH. CREW COMMENTS: AILERON LOCKOUT DISPLAYED AT 220 KNOTS FL140. REPLACED ACT PER MM.

Part: SLIDE — DAMAGED (CABIN) · airframe 79,720 hrs · 12,894 cycles

AFT ALIGNMENT PIN FOR OVERWING SLIDE ON RT DOOR BROKEN OFF. REMOVED RT OVERWING SLIDE.

Part: LIGHT — MISSING (CABIN) · airframe 79,559 hrs · 12,871 cycles

EEL LIGHT AT SEAT 10K'S VIDEO PANEL MISSING. INSTALLED NEW LIGHT. CHECKS GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 79,559 hrs · 12,871 cycles

SEAT EMERGENCY LIGHT AT SEAT 28B INOP. REPLACED SEAT MOUNTED EMERGENCY LIGHT LAMP ASSY AT 28AB, NO HELP. SUSPECT WIRING UNDER THE SEAT AT FAULT.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 79,559 hrs · 12,871 cycles

SEAT EEL LIGHTS FROM SEATS 19AB-23AB INOP. REPLACED BATTERY PACK ASSY. CHECKED OKAY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,559 hrs · 12,871 cycles

EMERGENCY EXIT SIGN ADJACENT TO MID GALLEY INOP. REPLACED BATTERY PACK. CHECKED, OKAY.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHT) · airframe 79,559 hrs · 12,871 cycles

EMERGENCY CEILING LIGHTS FROM SEATS 2AB- 8AB ARE INOP. REPLACED POWER SUPPLY, OPS CHECKED GOOD.

Part: PCA — MALFUNCTIONED (RT AILERON) · airframe 79,472 hrs · 12,859 cycles

RIGHT AILERON FLOATS WITH RT HYD SYSTEM DEPRESSURIZED. REPLACED AND OPS CHECKED THE RT INBD AILERON PCA PER MM. OPS CHECKED GOOD.

Part: FLOORBEAM — CORRODED (BS 853, LBL 75) · airframe 79,471 hrs · 12,858 cycles

CORROSION ALONG FLOOR SUPPORT STA 853, LBL 75 FOUND TO BE BEYOND ALLOWABLE LIMITS. MAJOR REPAIR ACCOMPLISHED: REMOVED AND REPLACED T-CAP AND SPLICE ANGLES BTWN STA 853 AND 888 ALONG LBL 75 IAW SRM REPAIR 3. APPLIED TOPCOAT IAW SRM. APPLIED CIC IAW SRM ON PEMCO NR 2493N00154 BY TECH 600177, INSP BY Q815.

Part: FLOORBEAM — CORRODED (BS 853, LBL 54) · airframe 79,471 hrs · 12,858 cycles

CORROSION ON FLOOR SUPPORT STA 853, LBL 54 BEYOND ALLOWABLE LIMITS IAW SRM. MAJOR REPAIR ACCOMPLISHED: REMOVED AND REPLACED TEE CAP BETWEEN STA 833 AND 920 IAW SRM REPAIR 3. APPLIED TOPCOAT IAW SRM, APPLIED CIC IAW SRM ON PEMCO NR 249N0 0154 BY TECH 600177, INSP BY Q815.

Part: O-RING — TORN (N2 ENG FUEL LINE) · airframe 79,417 hrs · 12,849 cycles

ON NR 2 ENG VISUAL INSP FOUND FUEL LEAK FROM FUEL OIL COOLER OUTLET HOSE LEAKING, FUEL ON FUEL PUMP INLET LINE CONNECTION. FOUND AND REPLACED TORN PACKING ON FUEL LINE, RAN NR 2 ENG AND NO LEAKS NOTED. FOUND FUEL LINE OK, JUST NEEDED TO REPLACE TORN O-RING.

Part: RELAY — FAULTY (LEFT) · airframe 79,175 hrs · 12,811 cycles

1 SPAR VALVE LIGHT FAILED TO ILLUMINATE WITH FUEL CONTROL SWITCH SELECTED (CUTOFF, RICH, RUN). EICAS MESSAGE (LT, RT) SPAR VALVE DISPLAYED. POS(1=LT,2=RT). TESTED OK. DID NOT LIGHT WITH ENG START OR SHUTDOWN. VALVE OPS OK. INDICATOR INOPERATIVE. SLAVED NEW SPAR VALVE ACTUATOR, NO HELP. SUSPECT K1 RELAY. REPLACED K1 RELAY IAW WDM, OPS CHECKED GOOD.

Part: DOOR — DAMAGED (R1) · airframe 79,173 hrs · 12,810 cycles

DOOR 1R AFT BUSTLE HAS A 2" GASH THAT PROTRUDES INTO THE CORE. REPAIRED BUSTLE.

Part: CIRCUIT BREAKER — INOPERATIVE (MID GALLEY) · airframe 79,165 hrs · 12,809 cycles

CREW REPORTED NO POWER AT THE MID GALLEY. CREW ALSO REPORTED MID GALLEY C/B ON P11-3 PANEL GRID U06 TRIPPED. REPLACED C/B U6 ON P11-3 AND MID GALLEY ELCU M1241 IAW MM. POWERED UP ALL GALLEYS FOR 15 MIN. ALL GOOD.

Part: WIRE — INOPERATIVE (GALLEY) · airframe 79,158 hrs · 12,808 cycles

GALLEY PIGTAIL-ELECTRICAL INOPERATIVE AT AFT CTR-AFT GAL 425. THE WIRE IS OVRHEATING AND SPARKING, REPLACED PIGTAIL AT N52. OPS NORMAL.

Part: LATCH — BENT (OVRWING SLIDE) · airframe 79,139 hrs · 12,805 cycles

FOUND RT OVER WING SLIDE FWD LINK-LATCH BENT AND FWD LATCH MISSING SPRING. REPLACED ALL DOOR LATCHES ON RT OFF WING ESCAPE SLIDE IAW MM. ACCOMPLISHED RII INSP OF THE RT WING SLIDE DOOR LATCHES IAW AMM.

Part: LIGHT — UNSECURE (CABIN) · airframe 77,909 hrs · 12,620 cycles

SEATS 24KJ, 25KJ AND 30AB HAVE EMERGENCY LIGHTS INOP. SECURED EMERGENCY LIGHTS, OPS CK OK.

Part: ACTUATOR — LEAKING (VSV) · airframe 77,767 hrs · 12,591 cycles

NR 2 ENG VARIABLE STATOR VANE ACTUATOR HAS FUEL STREAMING FROM DRAIN. REPLACED NR 2 ENG VSV ACTUATOR IAW MM.

Part: ACTUATOR — FAULTY (AILERONS) · airframe 77,611 hrs · 12,573 cycles

"AIL LOCK" LT ON AT HIGH SPEED. EICAS MESSAGE "AILERON LOCKOUT" DISPLAYED. OTBD AILERONS INDICATED MOVEMENT, UNLOCKED, BOTH. LIGHT CAME ON FOR 5 MIN AND THEN WENT OUT. PERFORMED SAM BITE. NO FAULT BALL ON LT AND RT SAM. NO AILERON LOCKOUT STATUS MESSAGE ON ARRIVAL. ACCOMPLISHED SERVICE TIPS. REPLACED AILERON LOCKOUT ACTUATOR. OPS CHECK CARRIED OUT OK AND ALL INDICATIONS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,532 hrs · 12,419 cycles

SEAT 8J EMERGENCY AISLE LIGHT INOP DUE TO OTTOMAN SEAT BROKEN. SEAT 8J EMERGENCY LIGHT REMOVED WIRES PROTECTED AND STOWED, NIL TIME TO REPAIR. NEED EEL HARNESS ASSY. REPLACED LIGHT ASSY.

Part: CONTROLLER — MALFUNCTIONED (APU GENERATOR) · airframe 75,948 hrs · 12,340 cycles

NO APU GEN AFTER GROUND START. APU FIELD LIGHT ON REAR PANEL. FOUND BPCU FAULTS "SHORTED PMG TRIP" AND "GEN-FIELD WIRING-GCU". REPLACED APU GCU, NO HELP. FOUND WIRE BETWEEN D264C PIN 4 AND D4040P PIN 4 OPEN. REPLACED APUC. CHECKED CONTINUITY FROM APU GEN D316 THROUGH OUT E2-4 SHELF M143 PMG HARNESS, FOUND CONNECTOR D4074J LOOSE. SECURED CONNECTOR. ACCOMPLISHED SUCCESSFUL APU GENERATOR OPERATIONAL CHECK.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 75,551 hrs · 12,290 cycles

ROW 19, (1) STRIP OF FLOOR LIGHTING CAME ON 2 HOURS INTO THE FLIGHT. CHECKED EMERGENCY LIGHT SYS IAW AMM, NO FAULTS FOUND. DUE TO PREVIOUS HISTORY, REPLACED POWER SUPPLY M1559. RECHECKED SYS, OPS NORMAL.

Part: ACTUATOR — STUCK (APU FUEL VALVE) · airframe 75,531 hrs · 12,288 cycles

UNABLE TO START APU 'APU FAULT' EICAS MSG. FOUND 'NO FLAME' MSG ON APU CONTROL BOX. PERFORMED FIM AND FOUND APU FUEL VALVE STUCK IN CLOSED POSITION. REPLACED APU FUEL VALVE ACTUATOR. APU OPS TEST PERFORMED, APU IS WORKING PROPERLY.

Part: WINDOW — CRAZED (COCKPIT) · airframe 75,137 hrs · 12,236 cycles

R2 AND L2 WINDOWS VERTICALLY CRAZED TO THE POINT OF RESTRICTING VISIBILITY. REPLACED BOTH L2 & R2 SLIDING WINDOWS.

Part: CIRCUIT CARD — FAULTY (FIRE DETECTION) · airframe 75,065 hrs · 12,225 cycles

RT ENG FIRE LP 1 ON STATUS PAGE. SAMC TEXT: CYCLED B22 ON P11 AND PERFORMED FIRE TEST FAULT CLEARED. CREW PUSHED POWER UP ON NR 2 ENG AND FAULT RE-APPEARED AND WENT AWAY WHEN BACK TO IDLE. REPLACED M683 CARD LOOP 1. RAN ENG, OPS CHECKS OKAY. NO FAULTS NOTED.

Part: SKIN — CORRODED (FUSELAGE) · airframe 74,270 hrs · 12,113 cycles

LEFT HIGH GAIN BEAM STEERING ANT AT FUSELAGE SKIN CORROSION DUE TO INADEQUATE SEALING. DURING SEALANT REMOVAL FOR CORROSION INSP FOUND SCRIBE MARKS AROUND 30 PERCENT OF ANTENNA PERIMETER. REPAIRED IAW SRM. ACCOMPLISHED HFEC AND ULTRASOUND, ALL FOUND OK. ALODINED BARE SKIN AREAS AND APPLIED FR PRIMER.

Part: ANTENNA — DAMAGED (ADF) · airframe 74,270 hrs · 12,113 cycles

WATER FALLING FROM OVRHD 22-23. R & R SATURATED INSULATION BLANKETS. REPLACED 2 EA ADF ANTENNAS AND LOW GAIN ANT. WORKING BOTH HIGH GAIN ANT REPLACED. RT INBD AILERON TRACKING B5971. WORKING INSULATION BLANKETS.

Part: REGULATOR — MALFUNCTIONED (OXYGEN MASK) · airframe 73,768 hrs · 12,039 cycles

CREW OXYGEN MASK PROBLEM. POSITION 1.(1=CAPT,2=FO, 3=1ST OBS,4=2ND OBS). CREW COMMENTS: HEAD HARNESS LEAKS ATTACHMENT POINT WITH REGULATOR WHEN SQUEEZING TRIGGERS TO INFLATE. REPLACED O2 MASK-REGULATOR. OP CHKS NORMAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 73,624 hrs · 12,018 cycles

2 FOOT SECTION OF EMERGENCY EXIT FLOOR LIGHTING IN FRONT OF L SIDE MID LAV BLINKING INTERMITTENTLY. RECONNECTED EMERGENCY LIGHT PLUG. CHECKED OKAY.

Part: STARTER — FAULTY (LT ENGINE) · airframe 73,550 hrs · 12,008 cycles

NO ROTATION ON LEFT ENGINE WHEN ATTEMPTING TO ENGAGE STARTER. REPLACED STARTER & STARTER VALVE. OPS ARE NORMAL.

Part: ENGINE — VIBRATION (NR 2) · airframe 73,499 hrs · 12,002 cycles

NR 2 ENG VIBRATION. NR 2 ENG EICAS VIB READS HIGH. HIGHEST READING 35 (X.X, RANGE 0.0 TO 5.0, ABNORMAL ON 767-322 IF ABOVE 4.0). EXCESSIVE VIBRATION NOT FELT IN AIRFRAME. 3.5 IS REACHED AT 1.11EPR. AT ALL OTHER EPR SETTINGS THE VIB IS LOWER. ACPD VISUAL INSPECTION OF ENG AND CHIP DETECTORS NO DEFECTS NOTED, NO OTHER HISTORY. FAN BLADES WERE LUBED, PERFORMED HIGH POWER RUN, ALL READINGS WERE WELL WITHIN LIMITS.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 72,813 hrs · 11,900 cycles

NEAR DOOR 2L EMERGENCY FLOOR PATH LIGHTING FLASHING ON AND OFF. REPLACED EMERGENCY LIGHT POWER SUPPLY (M1561). LIGHTS OPS CHECKED NORMAL.

Part: ACTUATOR — FAILED (AILERON) · airframe 72,701 hrs · 11,885 cycles

RIGHT AILERON LOCKOUT ACTUATOR FAILS LOCKOUT ACTUATOR AND MECHANISM TEST. RIGHT AILERON LOCKOUT ACTUATOR REPLACED. TESTED AILERON LOCKOUT SYSTEM, OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,701 hrs · 11,885 cycles

TWO EMERGENCY AISLE LIGHT ASSYS INOP AT 2B AND 7B. RELAMPED, NO HELP. NEED TO REMOVE SEAT 1A TO ACCESS POWER SUPPLY M735 FOR FURTHER T/S.

Part: COOLING FAN — MALFUNCTIONED (E&E BAY) · airframe 72,599 hrs · 11,870 cycles

STATUS MESSAGE, FWD EQ EXH FAN. REPLACED THE CENTER FAN CONTROL CARD, NO HELP. REPLACED FAN. MESSAGE GONE; FAN RUNS.

Part: FUSE — MALFUNCTIONED (EXTERNAL POWER) · airframe 72,516 hrs · 11,857 cycles

PER CREW ACFT WILL NOT ACCEPT GROUND POWER. REPLACED BUS POWER CONTROL UNIT. REPLACED ONE INTERLOCK FUSE, GND INDICATION OF EXTERNAL PWR NORMAL.

Part: STATOR — DAMAGED (ALTERNATOR) · airframe 72,422 hrs · 11,840 cycles

CREW REPORTS AFTER RT ENG START, EICAS MSG'S 'R ENG EEC C1','R ENG CNTL' STATUS MSG'S, AND 'RT ENG CNTL' ADVISORY MSG DISPLAYED. REPLACED ALTERNATOR STATOR FOR EEC RAN ENG ON A AND B CHANNELS NO MAINTENANCE OR STATUS MESSAGES.

Part: GCU — FAULTY (APU) · airframe 72,422 hrs · 11,840 cycles

APU GENERATOR INOPERATIVE. MM COMMENTS: APU GENERATOR SHUTDOWN AT DEPARTURE. RECYCLED SWITCH, NO HELP. REPLACED APU GCU. OPS CHECK NORMAL ON GROUND.

Part: CONNECTOR — CORRODED (LT MAIN TANK) · airframe 72,309 hrs · 11,822 cycles

CONNECTOR M1944 AT LEFT MAIN TANK, CORRODED, FAILED LOOP RESISTANCE CHECK. REPLACED BACKSHELL ASSY ON CONNECTOR M1944. BOND CHECKS, BITE CHECKS, AND LOOP RESISTANCE CHECKS GOOD.

Part: RAM AIR TURB — FAULTY (RAT) · airframe 72,309 hrs · 11,822 cycles

RAT DID NOT COMPLETELY DEPLOY AND PUSH BUTTON DID NOT STAY FLUSH, HAD UNLOCK LIGHT BUT NO PRESSURE LIGHT. (REFLY) RAT SYS TEST GOOD. MANUALLY DEPLOYED RAT 5 TIMES, ALL GOOD.

Part: CONNECTOR — CORRODED (LT AUX FQIS) · airframe 72,306 hrs · 11,822 cycles

FOUND CONNECTOR M1946 CORRODED, LEFT AUX FQIS. INSTALLED NEW M1946 BACKSHELL CONNECTOR KIT. ELECT AND BONDING CHECKS GOOD. LOOP RESIST TEST GOOD. READS 14.10 OHMS.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 72,309 hrs · 11,822 cycles

EMERGENCY EXIT FLOOR STRIP LIGHT BY G2 IS INOP. FOUND EMERGENCY LIGHT STRIP LOOSE AT CONNECTOR AT G2. REPAIRED AND OPS CHECKS GOOD.

Part: FLOORBEAM — CRACKED (BS 325 RBL 11) · airframe 72,309 hrs · 11,822 cycles

ELECTRONICS BAY, MAIN CABIN FLOORBEAM UPPER CHORD HAS EVIDENCE OF CRACK STARTING AT FASTENER'S HOLE, STA 325, RBL 11. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FLOORBEAM T-CAP, RBL 11 TO RBL 25. INSTALLED NEW SECTION T-CAP AND ANGLE DOUBLER REPAIR.

Part: STATIC INVERTER — MALFUNCTIONED · airframe 72,296 hrs · 11,818 cycles

"STBY INVERTER" EICAS, FLIGHT DIVERTED. DUE TO OVERHEAT DAMAGE REPLACED STANDBY INVERTER. ALSO REPLACED LEFT & RIGHT TRANSFORMER-RECTIFIERS. OPS CHECKS GOOD.

Part: GAUGE — LEAKING (EVAC SLIDE)

LOW PRESSURE. LEAKING FROM TOP OF GAUGE FAC THAT WAS BENT. REPLACED GAUGE.

Part: SOCKET — SHORTED (LAVATORY) · airframe 70,941 hrs · 11,598 cycles

FOUND AFT LEFT LAV DOME SOCKET SHORTED, REMOVED POWER WIRE AND SECURED. FOUND AFT LEFT LAV DOME SOCKET SHORTED, REMOVED POWER WIRE AND SECURED. NEEDS SOCKET, NOT STOCKED ORD. REPLACED LIGHT SOCKET, OP CHECKED OKAY.

Part: FEEDER CABLE — MISINSTALLED (NR 1 IDG) · airframe 70,367 hrs · 11,514 cycles

NR 1 ENG IDG FEEDER CABLES ARE INCORRECTLY ROUTED. REROUTED FEEDER CABLES FROM UPPER ENG AREA TO NR 1 IDG DISCONNECT. SECURED HARNESS.

Part: ENGINE — OIL CONSUMPTION (NR 2) · airframe 70,189 hrs · 11,492 cycles

OIL CONSUMPTION IS TRENDING UP. REPLACED NR 2 ENGINE FCOC. RUN CHECK NORMAL, NO LEAKS.

Part: START VALVE — FAILED (LT ENGINE) · airframe 70,173 hrs · 11,490 cycles

LEFT STARTER VALVE STAYED ON AFTER SW RTRND TO AUTO RAN QRCT. REPLACED LEFT STARTER VALVE. SATISFACTORY ENGINE START. RAN ENGINE PER JRH.

Part: CONNECTOR — LOOSE (E&E BAY) · airframe 69,786 hrs · 11,435 cycles

A-T FAILED TO ENGAGE. A-T MODE NOT DISPLAYED ON ADI. REPLACED EEC (P/N 791100-4-108, S/N 209), NO HELP. ALSO TRIED NEW ADC AND SWAPPED PIMUS, NO HELP. REPLACED AUTO THROTTLE SERVO MOTOR (S253T409-4, S/N 4), NO HELP MR 22324 OFF-4 ON-112. STILL HAVE NO INFC TMC EEC R PRIM AND SEC ON MCDP GRND TEST 30. RECHECKED WIRING FROM TMC TO EEC, CKS OK. TRIED NEW MCP, NO HELP. REPLACED K1040, NO HELP. FOUND OUTPUT BUSS FROM RT PIMU TO TMC INOP ON BOTH CHANNELS. SECURED CONNECTOR D5715P IN BACK OF E2-3 SHELF. ACP'D CAT III TEST. ALL TESTS PASSED. ACFT RETURNED TO CAT III STATUS.

Part: COVER — UNSECURE (DOOR 2L SLIDE) · airframe 69,768 hrs · 11,431 cycles

L2 DOOR SLIDE COVER LACING NOT SECURED. RESECURED L2 DOOR SLIDE LACING CABLE BALL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,341 hrs · 11,370 cycles

EXTERIOR EMERGENCY LIGHT AT DOOR 2L INOP. RELAMPED EMERGENCY LIGHT. OPS CHECK PASSED.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 68,878 hrs · 11,301 cycles

EMERGENCY ESCAPE PATH LIGHTING BESIDE 10FG WON'T COME ON DURING EMERGENCY LIGHT TEST. CABLE REPAIRED USING SPLICE CRIMPER METHOD. IT NOW OPS SATISFACTORY.

Part: UNKNOWN — UNKNOWN (AILERONS) · airframe 68,691 hrs · 11,273 cycles

THE "AIL LOCK" LIGHT ON AT HIGH SPEED. EICAS MSG "AILERON LOCKOUT" DISPLAYED. OUTBOARD AILERONS INDICATED MOVEMENT - UNLOCKED BOTH.

Part: DISPLAY — INTERMITTENT (COCKPIT) · airframe 68,261 hrs · 11,202 cycles

CAPTAINS ADI BLANKING INTERMITTENTLY. RTFL.

Part: ADI — FAULTY (COCKPIT) · airframe 68,261 hrs · 11,202 cycles

CAPTAINS ADI BLANKING INTERMITTENTLY. RTFL. LOSS OF ATTITUDE DEVIATION INDICATOR. REPLACED CAPTAIN'S ADI. OPS OK.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 67,037 hrs · 11,041 cycles

RESET AIR SUPPLY MODULE, RAN NR 1 ENGINE, NO DUCT PRESSURE INDICATED, BOX FAULTED PRSOV VALVE.

Part: FRAME — PUNCTURED (BS 1263 S39L/R) · airframe 67,060 hrs · 11,014 cycles

AFT PIT STA 1263 FRAME WEB HAS A PUNCTURE ABOVE STR 39L AND 39R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 51-70-13 AND SRM 51-40-02. AC OK FOR SERVICE.

Part: HOSE — KINKED (SLIDE BOTTLE) · airframe 67,060 hrs · 11,014 cycles

LT OVERWING SLIDE-BOTTLE PRESSURE HOSE IS KINKED SEVERAL SPOTS. SUSPECT HOSE MIS- STOWED DURING MAINTENANCE. REPLACED HOSE IAW SB 767-25-022. AC OK FOR SERVICE.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 67,060 hrs · 11,014 cycles

NR 2 PYLON UPPER WEB FUEL LINE CUTOUT SKIN CRACKED AT NAC STA 178. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR, ACCOMPLISHED REMOVED EXISTING REPAIR DOUBLER FROM NAC STA 172 TO 178. STOP DRILLED CRACK AND ACCMP'D HFEC TO VERIFY DAMAGE REMOVED. FABRICATED AND INSTALLED A REPAIR DOUBLER AND SPLICE TO INCORPORATE ENTIRE AREA.

Part: SHEAR TIE — CORRODED (BS 1241) · airframe 67,060 hrs · 11,014 cycles

AFT PIT LOWER FUSE FRAME SHEAR TIES HAVE CORROSION AT BS 1241 FROM STR 39R-35L. MAJOR REPAIR ACCOMPLISHED, REMOVED CORROSION AND REPLACED SHEAR TIES.

Part: FRAME — CORRODED (BS 1197) · airframe 67,060 hrs · 11,014 cycles

AFT CARGO COMPT AT BS 1197 AND LBL 20-25, FRAME T-CAP IS CORRODED AROUND NUT PLATE FASTENER HOLES. MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGED SECTION OF PIT FLOOR T-CAP. SPLICED IN NEW SECTION.

Part: DOOR FRAME — GOUGED (CARGO DOORWAY) · airframe 67,060 hrs · 11,014 cycles

AFT BULK PIT ACCESS DOOR BOTTOM FRAME HAS GOUGE ON REPAIR DOUBLER. MAJOR REPAIR ACCOMPLISHED, REMOVED DENTED DOUBLER. FABRICATED AND INSTALLED NEW DOUBLER.

Part: SHEAR TIE — CORRODED (BS 1395) · airframe 67,060 hrs · 11,014 cycles

AFT PIT FRAME SHEAR TIES HAVE CORROSION BS 1395 RBL 1 AND LBL 8. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGED SHEAR TIE. FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: FRAME — CORRODED (BS 1153) · airframe 67,060 hrs · 11,014 cycles

AFT CARGO COMPARTMENT AT BS 1153 AND LBL 8 -16, FRAME T-CAP IS CORRODED ON UNDERSIDE AND AROUND NUTPLATE. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGED SECTION OF CARGO FLOOR "T" CAP. SPLICED IN NEW SECTION.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 67,060 hrs · 11,014 cycles

AFT BULK PIT LOWER BILGE, FUSE FRAME HAS CORROSION ON LOWER AFT SIDE AT BS 1540 BETWEEN STR 38L-39L. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGED SHEAR TIE. FABRICATED AND INSTALLED NEW SHEAR TIE.

Part: FRAME — CORRODED (BS 1219) · airframe 67,060 hrs · 11,014 cycles

AFT CARGO COMPT AT BS 1219 AND RBL 33, FRAME T-CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED T-CAP.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 67,060 hrs · 11,014 cycles

EXTERNAL EMERGENCY LIGHT RT DOOR R4 INOP. REMOVED AND REPLACED BATTERY PACK OPS CHECKED GOOD. AC OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,060 hrs · 11,014 cycles

EXTERNAL EMERGENCY LIGHT RT OVERWING INOP. REMOVED AND REPLACED BATTERY PACK OPS CHECKED GOOD. AC OK FOR SERVICE.

Part: FRAME — CORRODED (BS 1197) · airframe 67,060 hrs · 11,014 cycles

AFT CARGO COMPT AT BS 1197 + 66 AT LBL 14 FRAME T-CAP IS CORRODED UNDER AND AROUND NUT PLATES. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED T-CAP.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 67,060 hrs · 11,014 cycles

EXTERNAL EMERGENCY LIGHT RT OVERWING INOP. REMOVED AND REPLACED BATTERY PACK OPS CHECKED GOOD. AC OK FOR SERVICE. REMOVED AND REPLACED BATTERY PACK AND OPS CHECKED GOOD. AC OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,060 hrs · 11,014 cycles

EXTERNAL EMERGENCY LIGHT LT AFT OF OVERWING SLIDE INOP. RELAMPED AND REPLACED BATTERY PACK OPS CHECKED GOOD. AC OK FOR SERVICE.

Part: FRAME — CORRODED (BS 1197) · airframe 67,060 hrs · 11,014 cycles

AFT PIT AT BS 1197+132 AND LBL 40 FRAME T-CAP IS CORRODED UNDER AND AROUND NUT PLATE. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED T-CAP.

Part: FRAME — CORRODED (BS 1197) · airframe 67,060 hrs · 11,014 cycles

AFT PIT AT BS 1197+88 AND LBL 40 FRAME T-CAP IS CORRODED UNDER AND AROUND NUT PLATE. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED T-CAP.

Part: STIFFENER — CRACKED (BS 246 FLOORBEAM) · airframe 67,060 hrs · 11,014 cycles

BS 246 FLOORBEAM AT APPROX RBL 16 HAS A CRACKED VERTICAL STIFFENER. MAJOR REPAIR ACCOMPLISHED, REMOVED AND REPLACED STIFFENER.

Part: SHEAR TIE — CORRODED (BS 1197 S39L-R) · airframe 67,060 hrs · 11,014 cycles

AFT CARGO PIT, BS 1197+66 BETWEEN S-39L-39R, SHEAR TIE IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REMOVED AND REPLACED SHEAR TIE.

Part: SHEAR TIE — CORRODED (BS 1197 S39L-R) · airframe 67,060 hrs · 11,014 cycles

AFT CARGO COMPARTMENT AT BS 1197+88 BETWEEN S-39L-39R SHEAR TIE IS CORRODED. MAJOR REPAIR ACCOMPLISHED, REMOVED AND REPLACED SHEAR TIE.

Part: FRAME — DAMAGED (BS 1351 S26-28R) · airframe 67,060 hrs · 11,014 cycles

FRAME IS TORN OUT STA 1351 BETWEEN STR 28R-26R. REPAIRED FRAME IAW SRM 53-00-01 FIG 201 DETAIL II AND SRM 51-40-02. AC OK FOR SERVICE.

Part: SLIDE — FAULTY (L1 DOOR) · airframe 67,060 hrs · 11,014 cycles

FOUND DOOR L1 SLIDE IS UNLACED.

Part: HOUSING — CRACKED (LT OWING SLIDE) · airframe 67,060 hrs · 11,014 cycles

LT OVERWING SLIDE COMPARTMENT DOOR DISCONNECT HOUSING CRACKED AT WELD SEAM.

Part: LIGHT — DAMAGED (CABIN) · airframe 66,952 hrs · 10,997 cycles

EEL LIGHTING INOP BY SEAT 14B. ACP PERMANENT REPAIR TO EEL LIGHT STRIP OPS CHECKED GOOD. AC OK FOR SERVICE.

Part: EXTINGUISHER — LEAKING · airframe 66,265 hrs · 10,900 cycles

WATER FIRE EXTINGUISHER LEAKING FLUID. SUSPECT FAULTY EXTINGUISHING RELEASE VALVE. REPLACED AFT WATER FIRE EXTINGUISHER. ACFT OK FOR SERVICE.

Part: ENGINE — VIBRATION (NR 2) · airframe 65,308 hrs · 10,754 cycles

ENG 2 VIBRATIONS SHIFTED UP FROM 0.2 TO 0.8 UNITS.

Part: CABLE — PULLED (CABIN) · airframe 64,652 hrs · 10,644 cycles

EEL LIGHT CABLE PULLED OUT OF TRACK FWD OF SEAT 1E.

Part: UNKNOWN — VIBRATION (NLG) · airframe 64,632 hrs · 10,644 cycles

RTFL UNDER AMBER ALERT DUE TO NOSE LANDING GEAR VIBRATION ON TAKEOFF.

Part: HOSE — CONTAMINATED (OVERWING SLIDE) · airframe 64,467 hrs · 10,612 cycles

RT OVERWING SLIDE INFLATION HOSE (FROM VESSEL TO AIRFRAME) COLLAPSED AND SPONGY. REPLACED SLIDE INFLATION HOSE DUE TO SPONGY & COLLAPSED CONDITION. HOSE ON OVERWING SLIDE INSTALLATION IS IN PROXIMITY OF HYDRAULIC SERVICING ACCESS CONNECTIONS. SPILLED HYD FLUID COMES IN CONTACT WITH THE HOSE AND DETERIORATES THE HOSE WALLS.

Part: UNKNOWN — LEAKING (HYD SYSTEM) · airframe 64,262 hrs · 10,571 cycles

CREW REPORTED THAT CENTER HYDRAULIC SYSTEM QUANTITY WAS DECREASING EN ROUTE. SYSTEM WAS TURNED OFF AND FLIGHT CONTINUED. AMBER ALERT WAS DECLARED, FLIGHT LANDED UNEVENTFULLY AND PROCEEDED TO THE GATE UNDER IT'S OWN POWER.

Part: APU — SHUTDOWN · airframe 64,146 hrs · 10,542 cycles

APU AUTO SHUTDOWN. [08-17-07] RESET APU ENGINE CONTROL UNIT. APU CK'S OK. AIRPLANE RETURNED TO SERVICE.

Part: WIRE — CROSSED (MLG) · airframe 63,887 hrs · 10,495 cycles

SPINNING NR 8 ANTISKID TRANSDUCER CAUSES THE NR 3 WHEEL BRAKE TO RELEASE, SHOULD RELEASE NR 4. STOPPING THE NR 8 TRANSDUCER CAUSES NR 7 BRAKE TO RELEASE, SHOULD RELEASE NR 8. FOUND WIRES TO TRANSDUCER CROSSED BETWEEN TRANSDUCER NR 7 AND NR 8. REINSTALLED WIRES REF WDM 32-42-11. TRANSDUCER SPIN TEST REF MM 32-42-00. NO FAULTS ON EICAS. TEST PASSED. AIRCRAFT OK FOR RETURN TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (APU) · airframe 63,745 hrs · 10,472 cycles

APU AUTO SHUTDOWN AFTER PUSHBACK. RESTART WAS NORMAL, BUT HAS HISTORY. [07-20-07] REPLACED APU CONTROL UNIT PER MM 49-61-05 AND P2 SENSOR PER MM 49-61-04. CK'D P2 SENSOR LINE FOR OBSTRUCTION, NONE FOUND. RAN APU FULLY LOADED WITH ELEC AND PNEUMATICS. NO FAULTS. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,664 hrs · 10,458 cycles

AFT LEFT EXTERIOR EEL LIGHT IS INOPERATIVE. RELAMPED AND LIGHT CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,664 hrs · 10,458 cycles

RIGHT FWD EEL FLOOR STRIP, EEL FLOOR STRIP BY THE RIGHT MID LAV & IN THE AFT GALLEY SMALL LEFT EEL FLOOR STRIP IS INOPERATIVE. [07-03-07] SECURED CONNECTOR. CHECKS GOOD.

Part: ASPIRATOR — LEAKING (SLIDE) · airframe 60,857 hrs · 9,982 cycles

ASPIRATOR LEAKING BETWEEN SENSING TUBE AND BARREL. SLIDE REPLACED. RETURNED TO SERVICE AFTER VISIT.

Part: ANGLE — CRACKED (NR 1 PYLON) · airframe 60,857 hrs · 9,982 cycles

NR 1 PYLON MIDSPAR CLOSEOUT ANGLE CRACKED AT BOTH INBD FASTENERS. STOPPED DRILLED CRACK. INSTALLED STRAP AND FILLER REPAIR.

Part: FLOORBEAM — PUNCTURED (FUSELAGE) · airframe 54,165 hrs · 8,956 cycles

E&E COMPARTMENT BS 246 FLOORBEAM WEB PUNCTURED APPROX RBL 45, WL 200. REPAIRED FLOORBEAM WEB.

Part: WIRE — BROKEN (RAM AIR TURNIBE) · airframe 54,165 hrs · 8,956 cycles

RAM AIR TURBINE FAILURE. DURING ROUTINE MAINTENANCE CHECK, A DISCREPANCY WAS NOTICED ON THE RAT SPEED SENSING. UPON FURTHER TROUBLESHOOTING, A WIRE INSIDE THE RAT SPEED SENSOR WAS FOUND BROKEN. AFTER REPAIR, THE RAT TEST WAS COMPLETED SUCCESSFULLY.

Part: LATCH — FAILED (CABIN)

LT OFFWING SLIDE LATCH CHECK FAILS TORQUE CHECK. TORQUE TO OPEN 200 IN/LBS, MAX ALLOWED 175.

Part: BEARING — FAILED (COOLING FAN) · airframe 52,900 hrs · 8,742 cycles

FLT CREW REPORTS ELECTRICAL ODOR AND LIGHT HAZE IN COCKPIT. THE FORWARD EQUIPMENT COOLING EXHAUST FAN FAILED. SHOP FINDINGS DETERMINED BEARING FAILURE TO BE THE ROOT CAUSE.

Part: CONTROL UNIT — MALFUNCTIONED (ELECTRICAL BUSS) · airframe 51,681 hrs · 8,531 cycles

ELECTRICAL UTILITY BUSS PROBLEM. LT AND RT UTILITY BUSS TRIPPED ABOUT 20 MINUTES OUT. UNABLE TO RESET AND THE AIRCRAFT RETURNED TO IAD. RELAYS K148 (SYS 1 AIR/GND) AND K10109 (UTIL/GALLEY PWR FLT RESET) WERE REPLACED AS A PRECAUTION. M116 BUSS POWER CONTROL UNIT (BPCU) ALSO REPLACED. THE DIRECT CAUSE OF THEN ANOMALY IS UNKNOWN; HOWEVER, IT HAS NOT RECURRED SINCE REPLACEMENT OF COMPONENTS.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 51,648 hrs · 8,526 cycles

FLIGHT RETURNED TO FIELD WITH CABIN PRESSURE FAULTS. THE EQUIPMENT COOLING OVERBOARD EXHAUST VALVE FAILED. THE VALVE WAS NOT DEACTIVATED PER THE MEL CAUSING A LOSS OF CABIN PRESSURIZATION ON THE SUBSEQUENT FLIGHT. THE VALVE WAS RE-DEFERRED PER THE MEL AND REPLACED AT THE NEXT MAINTENANCE OPPORTUNITY WITH NO FURTHER PROBLEMS. LINE QA IS CONDUCTING A INVESTIGATION INTO THE CIRCUMSTANCES.

Part: SCANNER — INOPERATIVE (WX RADAR SYS) · airframe 50,306 hrs · 8,282 cycles

FLIGHT DIVERTED DUE TO LOSS OF WEATHER RADAR. THE WEATHER RADAR SCANNER UNIT WAS DEFECTIVE . SCANNER WAS REPLACED.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 47,998 hrs · 7,923 cycles

LT SIDE OF CABIN EEL LIGHT FLOOR PATH LIGHTING IS INOP INCLUDING OVERWING EXIT MARKERS STARTING AT COACH SEATS. REPLACED BATTERY PACK. TESTS OK.

Part: WIRE — DEFECTIVE (EMERGENCY LIGHT) · airframe 45,847 hrs · 7,545 cycles

FROM SEAT 30F TO RIGHT AFT LAV AND AFT GALLEY CROSS AISLE FLOOR PROX LIGHTING INOP. REPLACED CABLE - LEAD WIRE.

Part: FAN — FAILED (CABIN) · airframe 45,363 hrs · 7,453 cycles

CREW REPORTED ELECTRICAL SMELL/SMOKE IN AIRCRAFT. THE RT RECIRCULATION FAN FAILED. THE FAN WAS REPLACED. THE SHAFT BEARINGS FAILED.

Part: DRIVE GEAR — SHEARED (OIL PUMP) · airframe 43,695 hrs · 7,186 cycles

NR 1 ENGINE SHUTDOWN DUE TO LOSS OF OIL PRESSURE AND HIGH TEMP. OIL PUMP DRIVE GEAR FAILURE. OIL PUMP DRIVE BEARING AND GEAR ASSY WERE FOUND LOOSE AND COCKED IN THE GEARBOX BEARING BORE. BEARING RETAINING SCREWS (ITEM 10 ) WERE BACKED OUT OF THE GEARBOX HOUSING AND LAYING IN THE BOTTOM OF THE GEARBOX. THIS RESULTED IN FRACTURE OF THE OIL PUMP DRIVE MODULE GEAR SHAFT IN THE WEB OF THE GEAR. THE FINAL ROOT CAUSE IS STILL BE INVESTIGATED. ENGINE WILL REQUIRE OVERHAUL OF ALL BEARINGS DUE TO LOSS OF OIL PRESSURE. MAIN GEARBOX WILL BE OVERHAULED.

Part: FRAME — CRACKED · airframe 41,635 hrs · 6,779 cycles

FWD CARGO DOOR, FWD FRAME IS CRACKED AROUND S152 SENSOR BRACKET. MAJOR REPAIR ACCOMPLISHED. REPAIRED FORWARD DOOR FRAME.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,635 hrs · 6,779 cycles

MAIN CABIN STATION 852 LBL 55, TRANSBEAM T-CAP UPPER CHORD CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. FABRICATED REPAIR SECTION AND INSTALLED.

Part: SKIN — CORRODED · airframe 41,635 hrs · 6,779 cycles

AFT CARGO, FUSE SKIN CORRODED BODY STATION 1197+117, ADJACENT TO STRINGER 37L, INTERNAL SKIN. MAJOR REPAIR ACCOMPLISHED. FABRICATED REPAIR DOUBLER.

Part: SHEAR TIE — CORRODED · airframe 41,635 hrs · 6,779 cycles

FWD PIT, BODY STATION 406 RIGHT HAND, SHEAR TIE BETWEEN STRINGER 36R AND STRINGER 35R, REQUIRES FABRICATION FOR SKIN REPAIR. MAJOR REPAIR ACCOMPLISHED. FABRICATED SHEAR TIE.

Part: SKIN — CHAFED · airframe 41,635 hrs · 6,779 cycles

RIGHT HAND FUSE SKIN STATION 1820, REAR EDGE OF H-STAB TO FUSE FAIRING SKIN HAS DEPTH CHAFFING FROM FAIRING. MAJOR REPAIR ACCOMPLISHED. FABRICATED REPAIR DOUBLER.

Part: SKIN — DENTED · airframe 41,635 hrs · 6,779 cycles

THREE EACH DENTS IN SKIN AT STATION 406, STRINGER 36R ARE OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. FABRICATED REPAIR DOUBLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,635 hrs · 6,779 cycles

MAIN CABIN STATION 852, RBL 55, TRANSBEAM UPPER CHORD CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. FABRICATED REPAIR SECTION AND INSTALLED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,635 hrs · 6,779 cycles

STA 830 LBL 11 UPPER CHORD CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SECTION AND SPLICES.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 41,635 hrs · 6,779 cycles

BS 287, RBL 14 - LBL 10, FLOORBEAM GOUGED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SECTION AND SPLICES.

Part: BEAM — CORRODED (FUSELAGE) · airframe 41,635 hrs · 6,779 cycles

STA 852-856 LBL 33 TRANSBEAM UPPER FLANGE CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED SECTION AND SPLICES.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 37,930 hrs · 6,152 cycles

APU NO START 3 ATTEMPTS. TWICE AT FL390 AND ONCE DESCENDING THRU FL290. MAX RPM 22 AND MAX EGT 10.

Part: UNKNOWN — ODOR (CABIN) · airframe 38,008 hrs · 6,163 cycles

OIL ODOR IN CABIN AFTER RT ENGINE START.

Part: FAN — FAILED (CABIN) · airframe 33,580 hrs · 5,350 cycles

CREW EXPERIENCED AN ODOR OF ELECTRICAL OR RUBBER TYPE OVERHEAT IN MAIN CABIN. THIS OCCURRED TWICE. *S/D* RIGHT RECIRCULATION FAN WAS OPERATING IMPROPERLY. RECIRC FAN WAS FOUND RUMBLING AND THEN SEIZING AFTER 2 MINUTES. FAN WAS REPLACED BY MVDMM AND NO FUTHER REPORTS OF ODOR HAVE BEEN REPORTED. COMPONENT SHOP SFOEC (154) FOUND THE FAN BEARING FAILED CAUSING THE IMPELLER RUBBING FAN HOUSING.

Part: OVEN — FAILED (GALLEY)

FLIGHT DIVERTED TO LHR UNDER AMBER ALERT DUE TO SMOKE AND ELECTRICAL FUMES IN MID GALLEY WITH VARIOUS ITEMS TURNED ON OR OFF. *S/D* LHR FOUND OVEN R41 SMELLING BADLY WHEN TURNED ON. PULLED AND COLLARED C-B FOR OVEN R41. AT COMPLETION ON FLT 953 IN ORD ON 6/25/99, REPLACED OVEN AND OPS CHECKS GOOD.

Part: OVEN — SMOKING (GALLEY)

RIGHT HAND MID-GALLEY OVEN FIRE. EXTINGUISHED FIRE WITH HALON EXTINGUISHER. ISOLATED ELECTRICAL SUPPLY BY TURNING-OFF LEFT UTILITY BUS. *S/D* AIRCRAFT CONNECTORS AND WIRING WERE INSPECTED AND FOUND TO BE SERVICEABLE. A NEW OVEN WAS INSTALLED AND OP CHECKED GOOD. THE REMOVED OVEN WAS INSPECTED BY THE HOME SHOP IN SFO AND FOUND TO HAVE PLASTIC DEBRIS MELTED ON AND ABOVE THE BAFFLE AND ON THE HEATING ELEMENT IN THE UPPER AREA OF THE OVEN. IT IS SUSPECTED THAT A PLASTIC BAG LEFT ON THE OVEN INSERT WAS DRAWN INTO THE OVEN HEATING AREA. OVEN INSERT PACKAGING, TRANSPORT AND LOADING PROCEDURES HAVE BEEN REVIEWED WITH UA CATERERS PER A SAFETY ALERT METER DTD 12/28/98.

Part: RETRACT MECH — MALFUNCTIONED (LANDING GEAR)

INITIAL LANDING GEAR EXTENSION RENDERED AMBER TAIL SKID AND GEAR LIGHTS AND EICAS GEAR DISAGREE MESSAGE. DID GO-AROUND, RECYCLED GEAR. SUBSEQUENT GEAR EXTENSION NORMAL.

Part: CONTROL VALVE — FAILED (TE FLAP)

TRAILING EDGE LIGHT ON DURING APPROACH AT POSITION 20. EXECUTED MISSED APPROACH. NEXT APPROACH FLAPS WORKED NORMALLY. *S/D* AN INTERMITTENT INTERNAL FAILURE IN THE TRAILING EDGE FLAP POWER DRIVE UNIT HYDRAULIC CONTROL VALVE MODULE ACTIVATED THE T/E FLAP FAILURE PROTECTION SYSTEM WHICH INHIBITS FLAP MOVEMENT. REPOSITIONING THE FLAP CONTROL LEVERS TO THE FULL RETRACT POSITION UNLATCHED THE FAILURE PROTECTION SYSTEM AND RESTORED FULL FLAP OPERATION. THE SUBJECT T/E FLAP PDU CONTROL VALVE WAS REMOVED, REPLACED, AND OPERATIONALLY CHECKED PER MM 27-51-32. ALL SYSTEMS CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

SECTION OF EMERGENCY TRACK LIGHTS FROM 6AB TO 13AB REMAIN ON WITH SWITCH ARMED AND OFF POSITIONS. REPLACED POWER SUPPLY. OPS CHECK OKAY.

Part: FILTER — DIRTY (RT ENGINE)

ABORTED TAKEOFF AT LHR AT 90 KNOTS DUE TO RT ENGINE BLEED OFF LIGHT ILLUMINATED AND EICAS MESSAGE RIGHT ENGINE BLEED OFF. *S/D* REPLACED RH PRSOV 02 JULY. SHOP FOUND INLET FILTER COMPLETELY CLOGGED, PREVENTING VALVE FROM OPENING.

Part: PITOT LINE — LOOSE (LT ADC)

TAKEOFF ABORTED APPROXIMATELY 90 KNOTS DUE TO NO CAPTAIN'S AIR SPEED INDICATION. *S/D* FOUND LOOSE PITOT ON LEFT ADC. SECURED PITOT LINE, AIRSPEED OPS NORMAL.

Part: WIRE — CHAFED (RT ENGINE)

RIGHT ENGINE BLEED OFF' EICAS AND BLEED OFF WARNING LIGHT DISPLAYED DURING CLIMBOUT. *S/D* MAINTENANCE FOUND WIRE CHAFED THROUGH AT PRESSURE REGULATING VALVE, CONTACTING ADJACENT METAL TUBING. REPAIRED WIRING AND SECURED.

Part: IDG — MALFUNCTIONED (LT ENGINE)

DIVERTED TO MIA UNDER AMBER ALERT DUE TO GENERATOR INDICATION PROBLEM. *S/D* THE LEFT ENGINE INTEGRATED DRIVE GENERATOR WAS BELIEVED TO BE AT FAULT. THE LEFT ENGINE IDG WAS REPLACED, OPERATIONS CHECK NORMAL. THE SHOP FOUND NOTHING WRONG WITH THE REMOVED IDG.

Part: COMPRESSOR BLADE — FAILED (RT ENGINE)

DURING CLIMB-OUT, THE RIGHT ENGINE EXPERIENCED HIGH EGT AND TWO COMPRESSOR STALLS. THE CREW INITIATED AN IN-FLIGHT SHUT DOWN. AIRCRAFT RETURNED TO MIAMI WITH AN UNEVENTFUL LANDING. THE HIGH PRESSURE COMPRESSOR FIFTH STAGE BLADE FAILED. THE ENGINE WAS REPLACED. PART TOTAL CYCLES, 2,473.

Part: BLADE — FAILED (NR 1 ENGINE)

ABORTED TAKEOFF AT LESS THAN 60 KNOTS DUE TO NR 1 ENGINE VIBRATION. THE HIGH PRESSURE COMPRESSOR EXPERIENCED A FIFTH STAGE BLADE FAILURE. THE ENGINE WAS REPLACED. PART TOTAL CYCLES, 2,471.

Part: LAMP — MALFUNCTIONED (LT EXT EEL)

LEFT EXTERIOR EMERGENCY LIGHTS WON'T TEST. REPLACED LAMPS.