N656UA

Part: OVEN — DIRTY (ZONE 900) · airframe 126,354 hrs · 19,461 cycles

OVEN 109 BLACK RESIDUE ON HEATING ELEMENT. SMOKED WHEN TURNED ON . STOPPED WHEN TURNED OFF REQUESTED NEF, DDP FOLLOWED AND CB OVEN 109 OPEN AND SECURED. DEFERRED IAW NEF 25178; CIRCUIT BREAKER OPEN AND SAFETY. REMOVED AND REPLACED OVEN AT POSITION 109 IAW AMM 25-31-00, OPS CHECKED GOOD.

Part: SWITCH — LOOSE (ZONE 200) · airframe 125,664 hrs · 19,378 cycles

EMER LIGHT SWITCH ASSEMBLY LOOSE. ADJUSTED EMERGENCY LIGHT SWITCH ASSEMBLE REF AMM TASK 33-51-08-004-002;ASSY SECURE.

Part: HOUSING — BROKEN (ZONE 200) · airframe 124,900 hrs · 19,284 cycles

EMERGENCY AISLE LIGHT SHROUD BRACK BROKEN AND HANGING FROM UNDER SEAT 36F. REMOVED AND REPLACED BRACKET. REF, AMM 33-50-00. PARTS USED: 58-2523-3-0048, QTY :1

Part: INDICATOR — FAULTED (ZONE 200) · airframe 124,694 hrs · 19,259 cycles

CABIN ALTITUDE DIFFERENTIAL GAUGE READS 8.8 PSI WHICH IS IN AMB ER BAND. FL370 CABIN PRESSURE CONTROLLER BITE PROCEDURE CARRIED OUT AS PER FIM 21-31 FAULT TREE 803. NO FAULTS FOUND. CABIN PRESSURE INDICATION TEST CARRIED OUT AS PER AMM 21-33-00-705-025 FOUND DIFF PRESS INDICATION FOUND TO BE 0.45PSI ON GROUND, AMM LIMITS STATE 0.35PSI /-. AS PER FIM TASK 21-33 FAULT TREE 806, INSPECTED DIFFERENTIAL PRESSURE SENSOR. DUE TO NO SPARES WE R&R CABIN PRESSURE INDICATOR AS PER BLOCK 11. CABIN PRESSURE LEAKAGE TEST CARRIED OUT AS PER AMM 05-51-24-782-001. DIFF PRESS TAKEN UP TO 4PSI SEVERAL TIMES. ALL READINGS CORRECT AND OUTFLOW VALVE MOVEMENT CHECKS GOOD. EXTERNAL AIRCRAFT WINDOWS, DOORS AND HATCHES CHECKED USING ACOUSTIC IMAGER. CHECKS GOOD. UPON COMPLETION OF INITIAL TROUBLE SHOOTING, CABIN ALT AUTO 2 SATUS MESSAGE DISPLAYED. AS PER FIM TASK 21-33 FAULT TREE 803 BLOCK 21. CABIN PRESSURE CONTROLLER LIGHT IS DISPLAYED. AS PER BLOCK 42 R&R CABIN PRESSURE CONTROLLER. POST INSTALLATION TEST CARRIED OUT WITH NO FAULTS. NO FURTHER MAINT REQUIRED.

Part: BOTTLE — NOT REPORTED (ZONE 800) · airframe 124,688 hrs · 19,258 cycles

OVER WING EMERGENCY ESCAPE SLIDE DEACTIVATION REF AMM 25-65-00-042-001. INSTALLED SAFETY PIN ON RIGHT OVERWING INFLATION CYLINDER REF AMM 25-65-00-042-001. PULLED CBS AND TAGGED K14, 15, 16 & 17 AND K17 & 18 ON P6. AS WELL AS C6, 7, 8, & 9; G17, 18, 26 & 27; P 35 & 36 ALL ON P11. INSTALLED SAFETY PIN ON LEFT INFLATION CYLINDER REF AMM 25-65-00-042-001 DISCONECTED EMERGENCY BATTERIES FOR BOTH LEFT AND RIGHT SLIDES REF AMM 25-65-00-042-001 DEACTIVATED RIGHT WING SPOILER SQUIB ACTUATOR REF AMM 25-65-00-042-001 REARMED OVER THE WING ESCAPE SYSTEM REF AMM 25-65-00-442-010 UP TO STEP 2 ARM/FIRE SWITCH CHECK. PERFORMED ARM FIRE SWITCH CHECK UP TO STEP H8 REF AMM 25-65-00-726-054. ACCOMPLISHED RII PER GMM 09-25-05. COMPLETED OVERWING SLIDE RE-ARM PER AMM TASK 25-65-00-442-010 OPS CHECK GOOD INSPECTED AS REQUIRED IAW GMM9-25-05 COMPLETION OF SLIDE RE-ARM REF: AMM TASK 25-65-00-442-010.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 124,559 hrs · 19,242 cycles

REAR SLIDE DOOR PRESSURE LOW. DOOR 2R INPECTED R2 DOOR SLIDE PRESSURE FOUND NON THE LIMITS AT THE HIGH END PER MM 25-66-02-206-001.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 124,276 hrs · 19,207 cycles

R1 DOOR SLIDE PRESSSURE IS LOW DOOR 1R SLIDE PRESSURE WAS FOUND SERVICEABLE. THIS LP WAS ENTERED IN ERROR, DOOR WITH DISCREPANT SLIDE PRESSURE IS DOOR R2. SEE LP 4245458. REF AMM 25-66-99.

Part: SKATE ANGLE — CRACKED (RT WING) · airframe 120,529 hrs · 18,732 cycles

GEN ITEM: 63-0600-1-2803 (B767-06-3-7290) THE I/B SKATE ANGLE IS CRACKED, LOCATED ON THE UPPER I/B EDGE OF WHERE PANEL 447DR ATTACHES TO THE LOWER SURFAC E OF THE RIGHT WING.#6173 REF AMES NR 167037-0400-0059 REPAIRED I/B SKATE ANGLE ON THE #2 ENG INBD EDGE IAW B767 BOEING DOCUMENT # 112T7001 AND REA DOCUMENT# 47601REA10 SEE PARTIAL WO RK ACCOMPLISHED AND ECRA 5458-01003

Part: SKATE ANGLE — CRACKED (UPPER I/B EDGE P) · airframe 120,528 hrs · 18,732 cycles

GEN ITEM: 63-0600-1-2803 (B767-06-3-7290) THE I/B SKATE ANGLE IS CRACKED, LOCATED ON THE UPPER I/B EDGE OF WHERE PANEL 447DR ATTACHES TO THE LOWER SURFAC E OF THE RIGHT WING.#6173 REF AMES NR 167037-0400-0059 REPAIRED I/B SKATE ANGLE ON THE #2 ENG INBD EDGE IAW B767 BOEING DOCUMENT # 112T7001 AND REA DOCUMENT# 47601REA10 SEE PARTIAL WO RK ACCOMPLISHED AND ECRA 5458-01003

Part: FLOORBEAM — CORRODED (BS 720 LBL 48) · airframe 120,529 hrs · 18,732 cycles

GEN ITEM: 63-5330-1-2610 FLOOR BEAM CAP CORRODED AT STA720 LBL48 MARKED FLAGGED #2196 T.K ELLY REMOVED CORRODED FLOOR BEAM CAP AT STA 720 FROM LBL 48- RBL 48 A ND INSTALLED SERVICEABLE NEW UPPER CHORD, PN 143T1060T33 IAW 767 -300 SRM 51-40-02 PAR 7. SEE NON-ROUTINE 167037-0100-0139 FOR DE TAILS

Part: STRINGER — CORRODED (BS 1302 S35L) · airframe 120,529 hrs · 18,732 cycles

STRINGER-35L IS CORRODED AT LFS-1302 . REPAIRED STRINGER 35L AT F.S.1302 IAW AMES REA DOC NO 47601REA08 AND UNITED EC/RA NO 5360-01767. SEE NON-ROUTINE 167037-0100-018 7 FOR DETAILS

Part: WEB — CRACKED (BS 676 RBL48) · airframe 120,529 hrs · 18,732 cycles

GEN ITEM: 63-5330-1-2610 FLOOR WEB AT STA676 RBL 48 IS CRACKED MARKED FLAGGED #2197 T.KEL LY REMOVED & REPLACED WEB STA 676 RBL 48 IAW B767 SRM 51-40-02 PARA 4 AND 9. SEE NON-ROUTINE 167037-0100-0141 FOR DETAILS

Part: SKIN — CRACKED (RT NACELLE) · airframe 120,529 hrs · 18,732 cycles

1 1/2 INCH CRACK IN THE UPPER AFT CORNER OF THE CUTOUT, FOR THE FWD ACCESS PANEL, ON THE O/B SIDE OF THE RIGHT ENGINE PYLON.#6204 REF AMES NR 167037-0400-0184. CRACK IN UPPER AFT CORNER OF CUTOUT REPAIRED IAW B767 SRM 54-53- 01-2R-G REPAIR 6 SEE PARTIAL WORK ACCOMPLISHED AND PARTIAL WORKS HEET 21 PAGE 1-3

Part: SKIN — CRACKED (BS 335 S20R) · airframe 120,529 hrs · 18,732 cycles

GENERATING ITEM EA 5315-01152 LOWER AFT CORNER OF R1 DOOR FUSELAGE SKIN AND BEAR STRAP STA 335 STRINGER 20R HAS CRACK INDICATION WHILE PERFORMING HFEC OPEN HOLE SCAN. INSTALLED REPAIR PARTS IAW SRM 53-10-01-2R-1, REPAIR 1 53-10-01-2R-1, REPAIR 1, FIG 201, SHT 7. REPAIR IS CAT B & REQ R ALL WHICHEVER LATER, REF SRM 53-10-01-2R-1, REPAIR 1, TABLE 202, FIG 201, SHT 3. MODIFIED R1 DOOR LWR SCUFF PLATE IAW B767 SRM E-INSP AT 37500 FC FROM A/C DELIVERY OR 6000 FC FROM REPAIR INST CUT OUT CRACKED AREAS IAW SRM 53-10-01-2R-1, REPAIR 1. HFEC AREA, NO FINDINGS IAW B767 NDTM 51-00-19 & 51-00-16 PART 6.AFTER INTIAL INSP. REPAIR REQUIRES RE-INSP AT 3000 FC INTERVALS. THE ABOVE REPAIR CAT B INSP THRESHOLD 37,500 FLT CYCLES TOMC-APPROVAL FROM SC1ELBYC COMMENT AFTER ACFT DELIVERY OR 6,000 MAX FLT CYCLES FROM THE REPAIR INSTALLATION, REPEAT INSPECTION AT INTERVAL 3,000 FLT CYCLES PER TABLE 202 OF SRM 53-10-01-2R-1 ..TOMC MO COMPLIED WITH FINAL INSP OF THIS REPAIR.

Part: SHEAR TIE — CORRODED (BS 1285 S38-39R) · corrosion level 2 · airframe 120,529 hrs · 18,732 cycles

AFT LOWER CARGO HAS CORROSION AT SHEAR TIE BL-5 STATION 1285 IN- BETWEEN S-39R AND S-38R, MARKED WITH STREAMER 2369 (T. GREGORY V 921207) REMOVED AND REPLACED SHEAR TIE AT BL-5 STA 1285, STR 38R IAW B767 SRM 51-40-02 PARA4. ACCOMPLISHED AT AMES BY V946986 & V931871 ON AMES NRC 167037-0100-0191.

Part: STRINGER — CRACKED (BS 1542 S38R) · airframe 120,529 hrs · 18,732 cycles

WHILE WORKING N/R 0100-0205 FOUND STRINGER 38R AT BS 1542 CRACKED JUST FWD OF DRAIN HOLE IN STRINGER. REPAIRED STR 38L FROM STA 1530-1550 IAW SRM 53-00-03-2R-2 REPAIR 2 DETAIL II PG. 7

Part: STRINGER — CRACKED (BS 1530-1562) · airframe 120,529 hrs · 18,732 cycles

GEN ITEM: 167037-0100-0205 WHILE WORKING SKIN CORROSION ON N/R 0100-0205, FOUND STRINGER 39 R AT STA 1544 CRACKED NEAR TANK SUPPORT. REPAIRED STR 39R FROM STA 1530-1562 IAW SRM 53-00-03-2R-2 REPAIR 2 DETAIL 11 PG. 7.

Part: SHEAR TIE — CORRODED (BS 1540 S39L-39R) · corrosion level 2 · airframe 120,529 hrs · 18,732 cycles

WHILE WORKING SKIN CORROSION ON N/R 0100-0205, FOUND SHEAR TIE CORRODED AT STA 1540 BL 0 BETWEEN STR 39R-39L. BLENDED & CHECKED LIMITS FOUND TO BE OUT OF LIMITS. REMOVED & RE PLACED SHEAR TIE AT STA 1540 BETWEEN STR 39R-39L IAW SRM 51-40-02 PARA 4 & 9 .

Part: SHEAR TIE — CORRODED (BS 1540 S38-39L) · corrosion level 2 · airframe 120,529 hrs · 18,732 cycles

CORROSION BS 1540 SHEAR TIE BETWEEN STR 38L & 39L, BLENDED & CHECKED LIMITS, FOUND TO BE OUT OF LIMITS. REMOVED & RE PLACED SHEAR TIE AT STA 1540 BETWEEN STR 38L & 39L IAW SRM 51-40-02 PARA 4 & 9.

Part: SKIN — CORRODED (BS 1544 S39L-R) · airframe 120,529 hrs · 18,732 cycles

CORROSION ALC F/S 1544 SKIN BETWEEN STR 39R & 39L AT DRAIN AREA, TAG 5368. 7 NDTM 51-00-19 PT 6, NO FINDINGS. REPAIRED AREA IAW UAL ECRA 53 ECRA 5330-07196 PT 2 TO BE PERMANENT. INSP PER PART 2 OF THE LA REPEAT INSP AT INTERVALS NOT TO EXCEED 9000 FC THEREAFTER. 30-07196 PT 1 & AMES EWO 47601REA06. REPAIR REQS REPEAT INSP PER TEST REV OF ECRA 5330-07196 ON OR BEFORE 37500 TOTAL FC. PERFORM REF AMES NR 167037-0100-0205. REMOVED CORROSION & FOUND OUT OF L IMITS PER 767-300 SRM 53-00-01 & 53-60-01-01-1. HFEC AREA.

Part: SHEAR TIE — CORRODED (BS 1540, S38-39R) · corrosion level 2 · airframe 120,529 hrs · 18,732 cycles

CORROSION F/S 1540 SHEAR TIE O/B OF STR 39R, TAG 6257. BLEND & CHECKED LIMITS FOUND TO BE OUT OF LIMITS. REMOVED & REPL ACED SHEAR TIE AT STA 1540 BETWEEN 39R & 38R STR IAW B767 SRM 51 -40-02 PARA 4 & 9.

Part: FLOORBEAM — CORRODED (BS 325 LBL 55) · corrosion level 2 · airframe 120,529 hrs · 18,732 cycles

CORROSION ON TOP SIDE OF FLOORBEAM IN UPPER CABIN STA 325 LBL 55. THIS IS A CATEGORY A REPAIR. FLOORBEAM AT STA 325 LBL 55 WAS RE PAIRED IAW SRM 53-00-51-2R-4 REPAIR 4.

Part: SKIN — CRACKED (#1 PYLON) · airframe 120,529 hrs · 18,732 cycles

GEN ITEM: 63-54-1-2805// INNER SKIN CRACK AT AFT UPPER CORNER ON NO1 PYLON AT ACCESS PANEL 436BR CUTOUT (M) 2328. STOPPED DRILL CRACK FABRICATED AND INSTALLED REPAIR DOUBLER INST ALLED RUB STRIP IAW B767 SRM 54-53-01-2R-7 REPAIR 7. SEE PARTIAL WORK ACCOMPLISHED AND PARTIAL WORKSHEET NO 34 PAGES 1-3 FOR DET AILS. REF NON-ROUTINE 167037-0400-0183 FOR DETAILS

Part: FLOORBEAM — CORRODED (BS 303 LBL42-60) · corrosion level 2 · airframe 120,529 hrs · 18,732 cycles

CORROSION ON TOP SIDE OF FLOOR BEAM IN UPPER CABIN STA 303 LBL 42. THIS REPAIR IS A CATEGORY A REPAIR. FLOORBEAM AT STA 303 LBL 42 -60 WAS REPAIRED IAW B767-300 SRM 53-00-51-2R-4 REPAIR 4.AND PWS #5 PAGES 1-8 OF 8.

Part: ATTACH ANGLE — CRACKED (NR 2 NACELLE) · airframe 120,529 hrs · 18,732 cycles

REMOVED AND REPLACED #2 PYLON IB AFT FAIRING ATTACHED ANGLE IAW B767-300 SRM 51-40-02 PARA 7

Part: FLOOR SUPPORT — CRACKED (CARGO BAY) · airframe 120,529 hrs · 18,732 cycles

FABRICATED DOUBLER AND FILLER INSTALLED ON AFT END OF FLOOR SUPPORT IAW B767 SRM 51-70-11-0G-0 AND DWG 146T5002 146T5006 SEE PART IAL WORK ACCOMPLISHED AND PARTIAL WORK SHEET 96 FOR DETAILS.

Part: FLOORBEAM — CORRODED (BS 654 LBL44) · airframe 120,529 hrs · 18,732 cycles

THE FLOOR BEAM CAP CORRODED AT STA 654+121 LBL 44.

Part: ANGLE — CORRODED (CARGO FLOOR) · airframe 120,529 hrs · 18,732 cycles

GEN ITEM: 63-5330-1-2610 PDU DRIVE STRUCTURE CORRODED AT STA654+70 RBL23 MARKED FLAGGED.

Part: STRINGER — CORRODED (BS 1395 S39L) · corrosion level 2 · airframe 120,529 hrs · 18,732 cycles

REF AMES NR 167037-0100-0212 GENERATING ITEM: 167037-0100.0167, STRINGER 39L STA 1395 FOUND CORRODED. WORK WITH N/R 0100-0167. REMOVED AND REPAIRED STR 39L STA 1395 IAW B767-300 SRM 53-00-03- 2R-2 DETAIL IV.

Part: SHEAR TIE — CORRODED (BS 1395) · corrosion level 2 · airframe 120,529 hrs · 18,732 cycles

AFT LOWER CARGO SHEAR TIE HAS CORROSION AT STATION 1395 BL-0 APPR OXIMATELY, AFT LOWER CARGO SHEAR TIE HAS BEEN FOUND TO BE OUT OF LIMITS, RE MOVE AND INSTALL OF NEW SHEAR TIE HAS BEEN INSTALLED ON N/R 1670 37-0100-0212 ENTRY #7.

Part: SHEAR TIE — CORRODED (BS 1285 S39L/R) · corrosion level 2 · airframe 120,529 hrs · 18,732 cycles

AFT LOWER CARGO HAS CORROSION AT SHEAR TIE BL-0 IN-BETWEEN S-39R AND S-39L STA 1285, REMOVED AND INSTALLED NEW SHEAR TIE BETWEEN STR 39R AND 39L AND BS 1285 IAW B767 SRM 51-40-02 PARA 4. WORK COMPLETED AND IAW DWG 146T121 0 SHT 2.

Part: BRACKET — CORRODED (POT WATER BOX) · corrosion level 2 · airframe 120,529 hrs · 18,732 cycles

AFT LOWER CARGO AT STATION 137 3 HAS CORROSION BL-0 TO S-38L ON SUPPORT STRUCTURE IN FRONT OF POTABLE WATER SERVICE BOX, REMOVED AND REPLACED 2 EACH CLIPS PN-146T3006-23 AND 146T3006-24 IN ALC AT STATION 1373 BL-0 TO S-38L IAW B767 SRM 51-40-02 PARA 7.

Part: SKIN — CORRODED (RT WING UPPER) · corrosion level 2 · airframe 120,529 hrs · 18,732 cycles

RIGHT WING UPPER SKIN AT OVER WING FUEL FILL PORT IS CORRODED. FOUND R/W UPPER SKIN FILL PORT TO BE OUT OF LIMITS PER B767-300 ACCOMPLISHED ON BACK OF NR AND PWS #27 PAGES 1 AND 2. REF AMES SRM 57-20-01, ALLOWABLE DAMAGE 1, TABLE 1. MIN REMAINING (ILN) NRC 167037-0600-0077. THICKNESS .205" FROM A NOM .266". REPAIRED AREA IAW AMES REA DOC #47601REA04 AND UNITED EC/RA 5723-01054. SEE PARTIAL WORK

Part: WEB — CORRODED (CABIN FLOOR) · corrosion level 2 · airframe 120,529 hrs · 18,732 cycles

CORROSION ON TOP SIDE OF FLOORBEAM CLOSEOUT WEB AND JUST FWD ON ADJACENT WEB IN UPPER CABIN STA 285 LBL 42 (M) 4615 REMOVED DAMAGE FROM WEB AT STA 285 100% MATERIAL LOSS VERIFIED M ATERIAL AND FABRICATED NEW WEB AND INSTALLED AT STA 285 IAW SRM 53-00-51-1A-1 ALLOWABLE DAMAGE DETAIL II,

Part: BRACKET — CORRODED (#1 PYLON) · airframe 120,529 hrs · 18,732 cycles

AN ANGLE SUPPORT BRACKET IS DAMAGED, LOCATED AT THE INTERIOR UPPER AFT CORNER OF 437BL ACCESS, OB SIDE IF NO 1 PYLON. REMOVED AND REPLACED BRACKET P/N 313T3380-133 IAW B767 SRM 51-40-02 PAR 7 AND PAR 9 AND BOEING DWG 313T3380. REF AMES (ILN) NRC167037-0400-0090.

Part: BRACKET — WORN (NR 2 ENGINE) · airframe 120,529 hrs · 18,732 cycles

NUMBER 2 ENGINE I/B FAN COWL HAS EXCESSIVE PLAY AT HLD OPEN ROD STOWAGE BRACKET (6222) STOWAGE BRACKET DAMAGED AND FOUND TO BE OUT OF LIMITS IAW B767 SRM 54-23-90-1A-1. NEW REPLACEMENT BRACKET FABRICATED IAW B767 ENGINEERING DWG 314T3114 AND NEW BRACKET INSTALLED IAW B767 SRM 51-40-02 PARAGRAPH 7. REF AMES (ILN) NRC 167037-0400-0207.

Part: DOOR FRAME — GOUGED (BS 1433-1443) · airframe 120,529 hrs · 18,732 cycles

GEN ITEM: 63-5230-1-2103 BULK CARGO DOOR LOWER FRAME HAS EXISTING REPAIR THAT IS GOUGED M ARKED FLAGGED #9268 REMOVED AND REPLACED GOUGED REPAIR PART ON THE BULK CARGO DOOR LOWER FRAME WITH A NEW REPAIR PART IAW B767 SRM 51-70-11-0G-0 AND SRM 51-40-02, PG 9. REF AMES (ILN) NRC 167037-0800-0011.

Part: BRACKET — WORN (FAN COWL) · airframe 120,529 hrs · 18,732 cycles

NO 2 ENG O/B FAN COWL HOLD OPEN ROD HAS EXCESSIVE PLAY AT STOWAGE BRACKET (REFERENCE STREAMER) FABRICATED NEW PLATE PN 314T3114-35 INSTALLED PLATE AMD GROMMET IAW B7567 SRM 51-40-02 PARA 7. REFERENCE NON-ROUTINE 167037-0400 -0203 FOR DETAAILS

Part: INSULATION — MISSING (STA 1979 - 2017) · airframe 119,591 hrs · 18,585 cycles

**POTENTIAL CHRONIC LVL 0 **DUE TO FLIGHT ATTENDENTS OBERSERVATI ON THAT THE L AFT LAV GETS VERY HOT WHEN THE APU IS RUNNING, PLE ASE INSPECT AFT LAV FOR POSSIBLY APU AIR LEAK WHEN RUNNING. REPA IR ALL FAULTS FOUND. ORDLM MARTINEZ 09/28/2023 CARRIED BY ELB REPLACEMENT. SEE ELECTRONIC LOG PAGE.5888261.APU DUCT ASSBLY MISSING INSULATION BLANKETS FROM STATION 1979 THRU 2017. REQUIRES REPLACED MISSING DUCT BLANKET REF LOG 5888261. PARTS USED: 76-3611-3-0110,QTY :1 76-3611-3-0111,QTY :1 76-3611-3-0026,QTY :1

Part: CONTROLLER — FAULTY (APU) · airframe 119,464 hrs · 18,564 cycles

IMMEDIATELY AFTER APU SHUTDOWN FLT ATTENDANTS REPORTED HOT AFT L LAV +SMELLED SMOKE IN LAV SMOKE/ODOR IN THE PLANE QUESTIONAIRE FILLED OUT BY FLT CREW PERFORMED INITIAL INSPECTION AS PER REF AMM 05-51-56. NO DEFECTS NOTED. A/C OK TO CONTINUE ADD EMP:U375129,U397288,U395275 REF LOGPAGE 5788519 - APU SHUTDOWN DURING PUSHBACK - PERFORMED APU BITE TEST AND FOUND FAULT 36. REMOVED AND REPLACED APU CONTROLLER PER AMM 49-61-05-004-001. RAN APU WITH FULL LOAD ND PERFORMED #1 ENGINE START NO FAULTS FOUND ON APU AT THIS TIME. PARTS USED: 75-4962-9-0001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1665171 SN OFF 1770 CONTROLLER, APU OFF 75-4962-9-0001 1770 ON 75-4962-9-0001 0013

Part: LATCH — UNKNOWN (PSU) · airframe 119,418 hrs · 18,558 cycles

ROW 36 CENTER OVERHEAD PANEL FELL DOWN FOUND PSU LATCH OPEN, ARMED LATCH AND CLOSED PSU PER AMM 25-23-01.

Part: FUEL CAP — MISSING (WING) · airframe 119,418 hrs · 18,558 cycles

FUEL CAP LEFT MISSING AT WING FUEL STATION. REPLACED FUEL CAP REF IPC 28-21-01-01.

Part: SLAT SYSTEM — WARNING MESSAGE (WING) · airframe 119,204 hrs · 18,532 cycles

LE SLAT DISAGREE AT FLAP 25. GO AROUND. QRH. FLAPS 20 LAND. LAND AT 147 KIAS. AB 3. BETWEEN POSITIONS 1 AND 5 LE SLAT DISAGREE FOR FRACTION OF A SECOND BEFORE DISAPPEARING. NO DISAGREE FROM POSITION 5 ALL THE WAY TO 30. NO DISAGREE FROM 30 BACK TO UP. CYCLED FLAPS A SECOND TIME. DURING SECOND CYCLE BETWEEN POSITION 1 TO 5 AGAIN RETURNED FLAPS TO UP POSITION WITH ALTERNATE FLAPS. RETURNED RECEIVED TE DISAGREE ON SECOND CYCLE. AGAIN FOR FRACTION OF A NORMAL FLAP LEVER TO NORMAL POSITION. TURNED OFF ALTERNATE FLAP SECOND. ALL OTHER POSITIONS AND RETURNING TO UP POSITION WORKED OVER RIDES. TURNED HYDRAULICS ON. CYCLED FLAPS TO 15 FOLLOWED BY NORMALLY. FLAPS 30 USING NORMAL FLAPS. WHEN MOVING FROM UP POSITION TO 15 ACCOMPLISHED THE FLAP AND SLAT PRIMARY DRIVES AND POSITION DISAGREE LIGHTS, AND NO STATUS OR MAINT MSGS RECORDED. MAINT MSG WAS RECORDED, AND SUSPECT THESE MSGS WERE ACTIVATED OPERATING PRESSURE WITHIN LIMITS PER AMM 29-11-00/001, STEP 3.C. INDICATING SYSTEMS TEST, AND LEADING EDGES OPERATED NORMAL IN ACCOMPLISHED BITE TEST OF THE FSEU, NO RELEVANT L.E. FAULTS CONCURRENT TO THE LEADING EDGE DISAGREE MSG, ALL USING CENTER ALSO, OPERATED THE FLAP SLAT USING THE ALTERNATE ELECTRIC SYST, ALL CYCLES PER AMM 27-51-00-705-508. WITH ALL CENTER SYSTEM FOUND. NO PREVIOUS HISTORY ON AIRCRAFT LOG RE L.E. SLAT SYST AT HYD SYSTEM, APPROX SAME TIME. ABLE TO CLEAR ALL MSGS ON THE FOUND NORMAL. PUMPS ON (ACMPS AND ADP) SLATS AND FLAPS OPERATED WITHOUT ANY THIS TIME. DURING TS, NOTED THA

Part: CHARGER — INOPERATIVE (M9043) · airframe 117,395 hrs · 18,291 cycles

B767-33-3-7000 - ZONE A SEAT 1-3 EEPL INOP TRANSFER REF HXWO 1594233 AND ORIGINATED BY EMP V920570 EMER LT PWR SUPPLY (M9043) REPLACED AND TESTED NORMAL AS PER AMM33-51-07 , EMER LT OP TEST CARRIED OUT AND FOUND NORMAL AS PER AMM33-51-00 WORK ACCOMPLISHED BY MECHANIC V920570 INSPECTED BY V898561 IDT INSPECTED BY HX161779 ADD EMP:V896963

Part: STIFFENER — CRACKED (RHW LES 664) · airframe 117,395 hrs · 18,291 cycles

B767-57-3-7014 RHW LES 664 FRONT SPAR STIFFENER FOUND CRACK TRANSFER TO NR WO.1500719 AND ORIGINATED BY V898549 RHW LES664 FRONT SPAR STIFFENER REPLACED AS PER SRM51-10-02 AND FASTENER INSTALLED AS PER SRM51-40-02 WORK ACCOMPLISHED BY MECHANIC V897473 INSPECTED BY V912779 RII INSPECTED BY HX147141 ADD EMP:V896853

Part: LAMP — BURNED (LH SLIDE L396) · airframe 117,395 hrs · 18,291 cycles

B767-33-3-7000 - LH SLIDE LIGHT (L396) EMER LT INOP TRANSFER REF HXWO 1490734 AND ORIGINATED BY EMP V920571 LH SLIDE LT (L396) LAMP AND LENS ASSY REPLACED & TESTED NORMAL AS PER AMM33-51-06 WORK ACCOMPLISHED BY MECHANIC V920570 INSPECTED BY V898561 IDT INSPECTED BY HX195306 ADD EMP:V896985

Part: POWER SUPPLY — INOPERATIVE (M1209) · airframe 117,395 hrs · 18,291 cycles

B767-33-3-7000 - EMER LIGHT POWER SUPPLY (M1209) INOP TRANSFER REF HXWO 1497793 AND ORIGINATED BY EMP V920570 EMER LT PWR SUPPLY M1209 REPLACED & TESTED NORMAL AS PER AMM33-51-07 WORK ACCOMPLISHED BY MECHANIC V920570 INSPECTED BY V898561 IDT INSPECTED BY HX206872 ADD EMP:V897802

Part: LAMP — INOPERATIVE (44A) · airframe 117,395 hrs · 18,291 cycles

B767-33-3-7000 - SEAT 44A EMER AISLE LIGHT INOP TRANSFER REF HXWO 1594230 AND ORIGINATED BY EMP V920570 SEAT 44A EMER AISLE LT LAMP REPLACED , LT ASSY RE-SECURED AND OP TEST CARRIED OUT AND FOUND NORMAL AS PER AMM33-51-05 WORK ACCOMPLISHED BY MECHANIC V920570 INSPECTED BY V898561

Part: POWER SUPPLY — INOPERATIVE (M737) · airframe 117,395 hrs · 18,291 cycles

B767-33-3-7000 - EMER LIGHT POWER SUPPLY (M737) INOP TRANSFER REF HXWO 1497707 AND ORIGINATED BY EMP V920570 EMER LT PWR SUPPLY M737 REPLACED AND TESTED NORMAL AS PER AMM33-51-07 WORK ACCOMPLISHED BY MECHANIC V920570 INSPECTED BY V898561 IDT INSPECTED BY HX206872 ADD EMP:V897802

Part: LAMP — INOPERATIVE (5A) · airframe 117,395 hrs · 18,291 cycles

B767-33-3-7000 SEAT 5A , 35AB , 27LK EMER LOWERED CEILING LT INOP TRANSFER REF HXWO 1490749 AND ORIGINATED BY EMP V920571 SEAT 5A , 35AB , 27LK EMER AISLE LT LAMP REPLACED & TESTED NORMAL AS PER AMM33-51-05 WORK ACCOMPLISHED BY MECHANIC V920570 INSPECTED BY V898561

Part: LAMP — BROKEN (SEAT 32KL) · airframe 117,395 hrs · 18,291 cycles

B767-33-3-7000 - SEAT 32KL EMER AISLE LIGHT INOP TRANSFER REF HXWO 1497705 AND ORIGINATED BY EMP V920570 SEAT 32KL EMER AISLE LT LAMP REPLACED AND TESTED NORMAL AS PER AMM33-51-05 WORK ACCOMPLISHED BY MECHANIC V920570 INSPECTED BY V898561

Part: LAMP — BURNED (L642) · airframe 117,395 hrs · 18,291 cycles

B767-33-3-7000 - LH O/WING ESCAPE LIGHT (L642) FWD SIDE INOP TRANSFER REF HXWO 1490756 AND ORIGINATED BY EMP V920571 LH O/WING ESCAPE LT (L642) LAMP REPLACED AND TESTED NORMAL AS PER AMM33-51-06 WORK ACCOMPLISHED BY MECHANIC V920570 INSPECTED BY V898561 IDT INSPECTED BY HX206872 ADD EMP:V897802

Part: LAMP — BURNED (DOOR 1L) · airframe 117,395 hrs · 18,291 cycles

B767-33-3-7000 - DOOR 1L EMER LIGHT (L313) INOP TRANSFER REF HXWO 1497654 AND ORIGINATED BY EMP V920570 DOOR 1L EMER DOOR LT (L313) LAMP REPLACED AND TESTED NORMAL AS PER AMM33-51-03 WORK ACCOMPLISHED BY MECHANIC V920570 INSPECTED BY V898561

Part: NONE — NONE (R MLG) · airframe 115,832 hrs · 18,069 cycles

PDA 1 RIGHT MAIN GEAR FWD JURY STRUT SPRING SNAPPED OFF DURING LANDING. PART RETREIVED BY PORT AUTHORITY AND RETURNED BACK TO MX. NOTIFIED LINE CONTROL AND TOMC. INSTALLED NEW RIGHT MAIN GEAR FWD JURY STRUT SPRING PER AMM 32-32-05-404-009; ADD EMP:U393384

Part: PANEL — MISSING (ENG #2 PYLON) · airframe 115,569 hrs · 18,032 cycles

PDA 2 DURING WALKAROUND FOUND PANEL MISSING FROM #2 ENGINE PYLON INBOARD SIDE. PHOTO ADDED. PERFORMED VISUAL INSPECTION OF A/C FOUND NO DAMAGE .INSTALLED PANEL P/N 311T3065-247 REF IPC. 54-53-01-01 SECURED FOR FLT.

Part: FLAP — INFLT SEPARATION (INBD AFT RH) · airframe 115,149 hrs · 17,978 cycles

PDA 1 RIGHT I/B AFT FLAP HAS A SECTION MISSING APPROXIMATELY 15 1/2 INCHES BY 60 INCHES. PER GMM 02-30-95, THIS CLASSIFY AS CATEGORY 1 PDA. FLAGGED AS SDR, SENT INFO TO ESC PER GMM 02-30-95 ACP MATING SURFACE INSPECTION AND PART NUMBER VERIFICATION, OK TO INSTALL.

Part: DUCT — LEAKING (BLEED SYS) · airframe 114,407 hrs · 17,855 cycles

MULTIPLE MOMENTARY R BLD DUCT LEAK MASTER CAUTIONS IN FLIGHT RE-ACCOMPLISHED TEST 26-18 FAULT TREE 804. TEST FAILED. NEEDS FURTHER TROUBLESHOOTING,, ROTABLE PARTS CHANGE WAS INDICATED - TT # 1345315 SN OFF 2369 IPC REFERENCE # 26-18-52-02 #5 ACCOMPLISHED 26-18 FAULT TREE 804 TEST FAILED. R BLEED DUCT LEAK LIGHT ON BLEED AIR PANEL AND R BLEED DUCT LEAK EICAS MESSAGE FAILED TO APPEAR. REPLACED M691 DUCT LK AND WHEEL WELL FIRE CARD IN P 54 PNL AS PER AMM TASK 26-10-01-024-024 & 26-10-01-424-025. CHECK BETWEEN TS214 AND TS215 ALSO BETWEEN TS215 AND TS216. CHECK IS OKAY. REMOVED PANELS 611CB 611JB 611NB AND 611PB FOR TROUBLESHOOTING UPDATING PARTS INFO REPLACED M691 DUCT LK AND WHEEL WELL FIRE CARD IN P 54 PNL AS REF SSM 26-18-01-102, FOUND WIRE BARELY HANGING FROM D10590 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1345315 SN OFF 6456 PER AMM TASK 26-10-01-024-024 & 26-10-01-424-025. NO FIX. CONNECTOR. JUMPERED FROM WIRE TO TS214 LOOP AND SYSTEM CHECKS CONTINUED FIM 26-18 FAULT TREE 804. CHECKED GROUND ON PIN 30, 7, NORMAL. WILL NEED D10590 CONNECTOR AND 16 AT CONNECTOR D10222. CHECKED OKAY. PERFORMED CONTINUITY CARD, ASSY, DUC OFF 64-2618-9-9001 6456 ON 64-2618-9-9001 0912 REPLACED CONNECTOR D10590 ACP SYSTEM TEST OPS NORMAL.

Part: BRAKE — FAILED (#6) · airframe 113,416 hrs · 17,660 cycles

NUMBER 6 BRAKE LEAKING FLUID AND CAUSING SMOKE REMOVED AND REPLACED #6 BRAKE REF AMM 32-41-08,OPS AND LEAK CHEAK OK. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1368206 SN OFF 0661 IDT CW ON MLG #6 BREAK ROD ,OK TO CONTINUE BRAKE, MLG, CAR OFF 76-3243-9-0002 0661 ON 76-3243-9-0002 0728

Part: RIB — DAMAGED (RH HORIZ STAB) · airframe 111,568 hrs · 17,273 cycles

RH HORIZONTAL STABILIZER TIP DAMAGED REMOVED DAMAGED TIP CAP (348AR) REPLACED TIP ASSY. REF AMM 55-11-01-404-005 THROUGH ITEM F 1E, WILL ALSO NEED EDGE SEAL. ACCOMPLISHED AMM55-11-01-404-005 PAGE 2OF2 ITEM F (1) (F)&(H) ACCOMPLISHED EDGE SEAL AND INSTALLATION OF TIP. REF 55-11-01-404-005

Part: FLOOR SUPPORT — CORRODED (BS 1197) · airframe 111,376 hrs · 17,242 cycles

REF AMES NR 0869. DURING PANEL INSTALL FOUND CORROSION ON FLOOR PANEL SUPPORT FRAME AT STA 1197+88 FLOOR PANEL SUPPORT FRAME BLENDED TO REMOVE CORROSION AT STA 119 7+88 ORIGINAL THICKNESS .063" MATERIAL REMOVED .030" REMAINING T HICKNESS .033". FOUND TO BE OUT OF LIMITS IAW B767-300 SRM 53-00 -07 ALLOWABLE DAMAGE 1 PG 106. FLOOR PANEL SUPPORT FRAME REPAIRED IAW B767 SRM 53-00-07 REPAIR 4 DETAIL VII.

Part: FLOORBEAM — CORRODED (BS 1197) · airframe 111,376 hrs · 17,242 cycles

REF AMES NR 0869. DURING PANEL INSTALL FOUND CORROSION ON FLOOR PANEL SUPPORT FRAME AT STA 1197+88 FLOOR PANEL SUPPORT FRAME BLENDED TO REMOVE CORROSION AT STA 119 7+88 ORIGINAL THICKNESS .063" MATERIAL REMOVED .030" REMAINING T HICKNESS .033". FOUND TO BE OUT OF LIMITS IAW B767-300 SRM 53-00 -07 ALLOWABLE DAMAGE 1 PG 106 TOOL TAG 2737. FLOOR PANEL SUPPORT FRAME REPAIRED IAW B767 SRM 53-00-07 REPAIR 4 DETAIL VII ADD EMP:V929460

Part: SKIN — CRACKED (STA 1680 S12R) · airframe 111,376 hrs · 17,242 cycles

REF AMES NR 0428. EA 5380-01178 REV A OP 2 R/H AFT EXTERIOR FUSE LAGE SKIN STA 1680 STRINGER 12R IS CRACKED (VERIFIED WITH HFEC S URFACE SCAN) REPAIRED FUSELAGE SKIN CRACK R/H STA 1680 STRINGER 12R IAW AMES REA DOC 47453REA02. SEE PARTIAL WORK ACCOMPLISHED ON BACK AND PW S PAGE 1 OF 1 ADD EMP:V931857

Part: SKIN — CRACKED (HORZ STAB) · airframe 111,376 hrs · 17,242 cycles

REF AMES NR 0460. THE FUSELAGE SKIN IS WORE THROUGH AND CRACKED AT THE FWD LWR EDGE OF THE CUTOUT FOR THE HOR STAB ON THE RIGHT SIDE REPAIRED FUSELAGE SKIN ON THE FWD LOWER EDGE OF CUTOUT FOR HORZ STAB IAW B767 SRM 53-60-01 REPAIR 3. SEE BACK AND PARTIAL WORKSH EETS 1 AND 2 FOR PARTIAL WORK ACCOMPLISHED ADD EMP:V921497

Part: FLOORBEAM — CORRODED (STA 1197) · airframe 111,376 hrs · 17,242 cycles

REF AMES NR 0867. DURING PANEL INSTALL FOUND CORROSION ON STATIO N 1197 FLOOR PANEL SUPPORT FRAME REMOVED CORROSION STA 1197+110 ORIGINAL THICKNESS .063" REMOVED .050" FOUND TO BE OUT OF LIMITS REPLACED INNER CHORD IAW B767 SR M 53-00-07 AND BOEING DWG 146T1060 REV F. SEE REVERSE AND PARTIA L WORKSHEETS (2)

Part: WARNING MESSAGE — FALSE ACTIVATION (HORIZONTAL STAB) · airframe 108,021 hrs · 16,659 cycles

HORIZONTAL STABILIZER TRIM CONTROL SYSTEM EICAS MESSAGE, UNSCHED STAB TRIM DISPLAYED, UNSCHED STAB TRIM LGT ON WITH AUTOPILOT OFF. NEITHER STAB TRIM CUTOUT SWITCH RE-ESTABLISHED CONTROLLED STAB TRIM, ONLY RECEIVED THE MESSAGE WHEN USING ALTERNATE TRIM SWITCHES. NO FAULT USING CONTROL WHEEL TRIM SWS. WHEN HAND FLYING. PERFORMED FIM TASK 27-09-00-815-813, PERFORMED TEST 65, NO FAULTS NOTED, TEST PASSED. PERFORMED TEST 30, TEST PASSED, NO FAULTS. AIRCRAFT REMAINS FULL CAPABILITY.

Part: COMPRESSOR — INOPERATIVE (POTABLE WATER) · airframe 106,802 hrs · 16,502 cycles

NO WATER IN GALLEYS AND LAVS WHEN AIRBORNE BUT WORKS ON GROUND WHEN LANDED REMOVED AND REPLACED THE H2O SYSTEM UNDERLOADER CHECK VALVE, FOUND BAD. PRESSURIZED THE SYSTEM WITH 1 ENG IDLE, OPS CHECK GOOD. H2O AIR COMPRESSOR INOP. REMOVED AND REPLACED THE AIR COMPRESSOR REF AMM 38-15-01-404-029. POTABLE WATER SYSTEM PRESSURE OPERATING NORMAL AT THIS TIME. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1122500 SN OFF 4895 IPC REFERENCE # 38-15-01-50.

Part: DUCT — BLOWN (LE SLAT) · airframe 105,147 hrs · 16,274 cycles

UPON INSPECTION OF SLAT NR 5 PRESSURE PANEL FOUND WING ANTI-ICE DUCT BLOWN. REMOVED & REPLACED NR 5 L/E SLAT ASSY IRW AMM TASK 27-81-02.

Part: CONTROL MODULE — MALFUNCTIONED (COCKPIT) · airframe 105,132 hrs · 16,272 cycles

GEAR HANDLE WOULD NOT MOVE PAST OFF POSITION JACKED A/C PER MM 07-11-01, PERFORMED OPERATIONAL TEST "MAIN GEAR EXT/RET SYSTEM" PER MM32-32-00-705-001. WITH NO ABNORMITIES NOTED AT THIS TIME. (4CYCLES). CHANGED LANDING GEAR CONTL LEVER MODULE FOR PRECAUTIONARY AS PER MAINT CONTL. R&R AS PER 32-31-01-004-001 OPS CHECKS NORMAL, OK FOR SERVICE. ROTABLE PARTS CHANGE WAS INDICATED TT 1064501 SN OFF 1047 IPC REFERENCE 32-31-01-01 MODULE, LANDING OFF 64-3231-9-0003 1047 ON 64-3231-9-0003 0763.

Part: LENS — BROKEN (CABIN) · airframe 103,510 hrs · 16,061 cycles

FLIGHT CREW LEFT RED EMERGENCY EXIT LIGHT LENS IN FLIGHT DECK. REPLACED BROKEN RED LENS FOR SEAT 20F EMERGENCY LIGHT. OPS CHECK NORMAL REF AMM 33-51-10.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 101,944 hrs · 15,855 cycles

EMERGENCY LIGHT ABOVE COCKPIT DOOR INOPERATIVE. REMOVED AND REPLACED LIGHT ASSY TESTS PASSED.

Part: SUPPORT BEAM — CRACKED (BS 500-566) · airframe 101,673 hrs · 15,815 cycles

FWD CARGO DOOR FRAME LOWER BEAM FOUND CRACKED AT RBL48, BS 500 & 566. A NEW SUPPORT BEAM WAS REINSTALLED IAW SRM 51-10-02 AND AMM 20-11-00.

Part: FLOORBEAM — CORRODED (BS 1518) · airframe 101,673 hrs · 15,815 cycles

BS 1518, BL 0 TO LBL 29 FLOORBEAM FOUND CORRODED. THE FLOORBEAM UPPER TEE WAS REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 101,082 hrs · 15,714 cycles

LENS IS MISSING FROM EMERGENCY LIGHT ON CEILING AT RT AISLE NEAR THE MIDDLE CROSS AISLE. REPLACED THE LENS.

Part: SIGN — DETACHED (EMERGENCY LIGHTS) · airframe 100,140 hrs · 15,562 cycles

EMERGENCY LIGHT MID ACFT, CAME DOWN AFTER LANDING. SECURED THE SIGN IAW AMM 33-15-02, OPS CHECKED GOOD.

Part: FAN — FAILED (EQUIP COOLING) · airframe 98,734 hrs · 15,359 cycles

FWD EQUIPMENT EXHAUST FAN STATUS MESSAGE DISPLAYED. AN ELECTRICAL ODOR WAS IN THE COCKPIT. FOUND FAN TO BE FAULTY. EXHAUST FAN BEARINGS ARE BAD . INTERNAL FAN RUBBING AGAINST FAN CASE. INSTALLED A NEW EXHAUST FAN IAW AMM 21-58-06, INSTALLED NEW VIBRATION MONITOR AND RESET IAW STEP 7, OPS CHECKED GOOD

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 97,532 hrs · 15,187 cycles

EMERGENCY EXIT SIGN IN FLIGHT DECK INOP. REPLACED LIGHT ASSY REF MM 33-51-01 PG 201.

Part: STRUCTURE — CORRODED (BS 520) · airframe 96,563 hrs · 15,049 cycles

INTERGRANULAR CORROSION IN FWD CARGO UPPER STRUCTURE BS 520, RBL 35. . REMOVED AND REPLACED IAW SRM 51-40-02 PARA 4 FIG 3 & 8, PARA 7D FIG 12 (DET 2), PARA 5 FIG 9 &10, PARA 9 FIG 16 AND DWG 143T8208.

Part: DOOR SILL — CORRODED (FWD CARGO) · airframe 96,563 hrs · 15,049 cycles

CORROSION AT FIVE AREAS ON THE FWD CARGO DOOR CUTOUT STRUCTURE LOWER MAIN SILL, BS 503, 508, 565.5, 597.5 AND 615.5 UPPER SURFACE.

Part: INTERCOSTAL — CORRODED (BS 478-500) · airframe 96,563 hrs · 15,049 cycles

FWD CARGO BAY BS 478 - 500 RBL 35 INTERCOSTAL CORRODED. REMOVED & REPLACED THE INTERCOSTAL IAW SRM 51-40-02 PA RA 7 FIG 12.

Part: CHANNEL — CORRODED (BS 478-500) · airframe 96,563 hrs · 15,049 cycles

FWD CARGO COMPARTMENT BS 478 - 500 RBL 25 CHANNEL CORRODED. REMOVED AND REPLACED THE CHANNEL.

Part: CHANNEL — CORRODED (BS 538-544) · airframe 96,563 hrs · 15,049 cycles

CORROSION FOUND ON FWD CARGO BAY CHANNEL AND RADIOUS BLOCK BS 544-5 38 RBL 40. REMOVED AND REPLACED THE CHANNEL & RADIUS BLOCK IAW SRM 51-40-02 PAR 7 FIG 12.

Part: CHANNEL — CORRODED (BS 478-500) · airframe 96,563 hrs · 15,049 cycles

FORWARD CARGO BAY BS 478 - 500 RBL 20 CHANNEL CORROSION. REMOVED AND REPLACED THE INTERCOSTAL.

Part: CHANNEL — CORRODED (FWD CARGO DOOR) · airframe 96,563 hrs · 15,049 cycles

U-CHANNEL IS CORRODED UNDER WEB AT FWD CARGO DOOR SURROUND BS 490, RBL 29. U-CHANNEL FOUND TO HAVE 100% MATERIAL LOSS AT FWD CARGO DOOR SURROUND. REMOVED & REPLACED THE CHANNEL IAW SRM 51-40-05 FIG 2, SRM 51-40-02 FIG 12 & DWG 143T5018.

Part: DOOR SILL — CORRODED (BS 550) · airframe 96,563 hrs · 15,049 cycles

CORROSION ON UNDER SIDE OF CARGO DOOR SILL BS 550 RBL 57. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15. LOCATED AN D DRILLED A NEW STRAP IAW SRM 51-40-05 FIG 2 & DWG 143T8 204.

Part: SHEAR TIE — CORRODED (BS 1540) · airframe 96,563 hrs · 15,049 cycles

CORROSION ON SHEAR TIE IN AFT CARGO BS 1540 AND BETWEEN STRINGERS 37 & 38R . FOUND TO HAVE 100% MATERIAL LOSS. REMOVED FABRICATED, LOCATED, DRILLED AND INSTALLED A NEW SHEAR TIE IAW SRM 51-40-02 PAR 4,7 FIG 3,8,12 SRM 51-30-01 PA R 7 FIG 7 AND SRM 51-40-05 PAR 4 FIG 3.

Part: WIRE — CHAFED (CABIN) · airframe 94,891 hrs · 14,817 cycles

BREAKER P36 ON P11 RESETS, BUT POPS WHEN SQUIB TEST 1 PRESSED. ON PUSHBACK & DURING POWER XFER BREAKER ALSO POPPED. REPLACED RT OFF WING ESCAPE SYS EMER BATTERY CHARGER ASSEMBLY. BREAKER P36 ON P11 STILL TRIPS DURING SQUIB TEST 1. ALSO TRIPS WITH CONNECTOR REMOVED FROM BATTERY. LT CONNECTOR OFF FOR TS. SIDEWALL GRILL ALSO OFF. REPAIRED CHAFED WIRE, SEE PTT SEQ 8916019.

Part: WIRE — CHAFED (CABIN) · airframe 94,891 hrs · 14,817 cycles

BREAKER P36 ON P11 RESETS, BUT POPS WHEN SQUIB TEST 1 PRESSED. ON PUSHBACK & DURING POWER XFER BREAKER ALSO POPPED. REPLACED RT SIDE OFF WING ESCAPE SYS EMER BATTERY CHARGER ASSEMBLY. BREAKER P36 ON P11 STILL TRIPS DURING SQUIB TEST 1. ALSO TRIPS WITH CONNECTOR REMOVED FROM BATTERY. LT CONNECTOR OFF FOR TS. SIDEWALL GRILL ALSO OFF. REPAIRED CHAFED WIRE SEE PTT SEQ 8916019.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 94,054 hrs · 14,694 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE AT CEILING, FROM FWD GALLEY CEILING RT SIDE, THROUGH SEAT ROW 8 RT. ALSO EXIT SIGN JUST FWD OF SEAT ROW 1 RT. SECURED CONNECTOR AT POWER SUPPLY M730. LIGHTS OPERATIONS NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 94,054 hrs · 14,694 cycles

EMERGENCY LIGHTS FWD ENTRY, LT EXIT IDENTIFIER, CROSS AISLE & LT EMER EXIT LIGHT REMAIN ON WITH EMER LIGHT SWITCH OFF. REPLACED BATTERY M1557 IAW MM 33-51-07. LIGHTS OPERATIONS CHECKED NORMAL.

Part: BATTERY — UNSECURE (CABIN) · airframe 93,669 hrs · 14,644 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE, CEILING ROWS 29 RT THROUGH AFT GALLEY RT SIDE. SECURED BATTERY AT M734. CEILING LIGHTS OPERATION CHECK NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 93,669 hrs · 14,644 cycles

SEAT MOUNTED EMER EXIT LIGHT INOPERATIVE AT SEAT ROW 36 RT. SECURED CONNECTOR, OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 93,669 hrs · 14,644 cycles

EXTERIOR EMER EXIT LIGHT INOPERATIVE, RT SIDE FUSELAGE AFT LIGHT. RELAMPED EXTERIOR EMER EXIT LIGHT IAW AMM 33-51-06.

Part: BATTERY — UNSECURE (CABIN) · airframe 93,669 hrs · 14,644 cycles

EMERGENCY EXIT SIGN INOPERATIVE AT AFT GALLEY WALL RT SIDE. SECURED BATTERY AT M734. EXIT SIGN OPERATIONS CHECKED NORMAL.

Part: BATTERY — UNSECURE (CABIN) · airframe 93,669 hrs · 14,644 cycles

EMERGENCY EXIT SIGN INOPERATIVE, RT SIDE CEILING AISLE JUST AFT OF SEAT ROW 39 RT. SECURED BATTERY AT M734. EXIT SIGN OPERATIONS CHECK NORMAL.

Part: TRUNNION — CORRODED (NLG) · corrosion level 2 · airframe 90,952 hrs · 14,279 cycles

CORROSION IN MULTIPLE AREAS. RT SIDE OF TRUNNION FITTING AT FASTENERS FWD E & E BAY BS 276. REMOVED CORROSION & REPAIRED DAMAGE ON RT NLG TRUNNION FITTING IAW ECRA 5340-01635.

Part: SHEAR TIE — MISREPAIRED (FUSELAGE) · airframe 90,952 hrs · 14,279 cycles

BS 1395 BETWEEN STRINGER 36L & 37L, REPAIRED SHEAR TIE DOES NOT HAVE A JOGGLE. R & R AFT CARGO SHEAR TIE BS 1395 BETWEEN STRINGER 36L & 37L IAW SRM 51-40-02 PAR 4 FIG 8 & DWG 146T1215.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,952 hrs · 14,279 cycles

CORROSION ON FRAME 1153 UPPER T CAP UPPER & LOWER SURFACE MULTIPLE AREAS IN AFT CARGO COMPARTMENT LBL 40 - RBL 45. R & R BS 1153 FRAME UPPER T CAP FROM LBL 40 TO RBL 40 IAW SRM 51-40-02 FIG 3, FIG 8 & FIG 12.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,952 hrs · 14,279 cycles

CORROSION ON STRINGER 34L BS 1329 - 1351 IN AFT CARGO COMPARTMENT. REMOVED CORROSION IAW SRM 51-10-02 FIG 1, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03 FIG 101 DETAIL I & II. REPAIRED DAMAGE TO STRINGER 34L BS 1307 TO 1361 IAW SRM 53-00-03 FIG 201 REPAIR 2.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,952 hrs · 14,279 cycles

CORROSION ON FRAME 1109 UPPER T CAP LOWER SURFACE LBL 44 EXCEEDS MAXIMUM ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-07 FIG 101 DETAIL VIII. R & R T CAP IAW SRM 51-40-02 PAR 4 & 7 FIG 3, 8 & 12, UPPER T CAP FABRICATED IAW DWG 146T1202.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,952 hrs · 14,279 cycles

CORROSION ON CABIN FLOORBEAM BS 266.5 RBL 80 FOUND TO BE 100% MATERIAL LOSS IAW SRM 53 -00-51 FIG 101. REMOVED & REPAIRED FLOORBEAM IAW SRM 53-00-51 FIG 201.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,952 hrs · 14,279 cycles

CORROSION ON FRAME 1197-44 UPPER T CAP LOWER SURFACE MULTIPLE AREAS IN AFT CARGO COMPARTMENT BS 1197 + 44 RBL 5 & LBL 44. MATERIAL REMOVAL IS .040 & IS OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DET VIII SEC D D. R & R UPPER T CAP IAW SRM 51-40-02 PAR 4 FIG 8 & 3. MARKED PART WITH PN 146T1060-1 IAW GMM 07- 35-05.

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,952 hrs · 14,279 cycles

CORROSION ON GUARD AT CREASE BEAM STATION 287.0 RBL 81. R & R NEW CREASE BEAM AT BS 287.0 RBL 81 IAW SRM 51-40-02 PAR 7 FIG 1 DUE TO 100 PERCENT MAT LOSS PN 141T8310-410 PO 435783.1.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,952 hrs · 14,279 cycles

CORROSION ON FRAME 1197 UPPER T CAP UPPER & LOWER SURFACE IN AFT CARGO COMPARTMENT LBL 40 RBL 40. R & R UPPER T CAP ON FRAME 197 LBL40 RBL40 IAW SRM 51-40-02 PAR 4B FIG 3 & PAR 7D FIG 12 & FIG 14. MATERIAL ID & FABRICATED INNER CHORD IAW SRM 53-60-07 FIG 1 ITEM 7 & GMM 07-35-05 PAR 8.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,952 hrs · 14,279 cycles

CORROSION ON 1219 FRAME CLIP BETWEEN STRINGER 38R - 39 IN AFT CARGO COMPARTMENT. REMOVED, FABRICATED & INSTALLED NEW FRAME CLIP BETWEEN STRINGER 38R-39R STATION 1219 IN AFT CARGO IAW SRM 51-40-02 PAR FIG 12.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,952 hrs · 14,279 cycles

CORROSION MAIN CABIN FLOORBEAM BS 325 RBL 48. REMOVED CORROSION ON FLOORBEAM UPPER CHORD BS 325 RBL 48 IAW SRM 51-10-02 PAR 1 5 FIG 1 & 5. ORIGINAL MATERIAL THICKNESS IS .125, MATERIAL REMOVED IS .036 & IS OUT OF LIMITS IAW SRM 53-00-51 FIG 101, 53-10-51 FIG 1 & DWG BAL 1506-3116. REPAIRED FLOORBEAM UPPER CHORD IAW SRM 53-00-51 REPAIR 1 FIG 201. THIS IS A CLASS A REPAIR.

Part: BATTERY — DISCHARGED (CABIN) · airframe 90,394 hrs · 14,194 cycles

RIGHT AISLE EMER CEILING LIGHTS INOPERATIVE BETWEEN SEATS 29 TO 37. REPLACED EMER LIGHT BATTERY IAW MM 33-51-00. OPERATIONS CHECKED OK.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 90,394 hrs · 14,194 cycles

LEFT AISLE SEAT EMER LIGHTS INOPERATIVE BETWEEN SEATS 34 TO 39. REPLACED BATTERY POWER CHARGER & BATTERY PACK ON ROW 38 LT. OPERATIONS CHECKED NORMAL IAW MM 33-51-00 & 33-51-07.

Part: FUSE — BLOWN (POWER SUPPLY) · airframe 90,394 hrs · 14,194 cycles

RIGHT EXIT EMER LIGHT SIGN ABOVE SEAT 39J INOPERATIVE. REPLACED POWER SUPPLY M734 FUSE IAW SSM 33-51-01 LIGHT L306. OPERATIONS CHECKED GOOD IAW AMM 33-51-0 0-501.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 90,196 hrs · 14,165 cycles

UPON LANDING & APU START, APU FAULT LIGHT ILLUMINATED. APU IGNITION EXCITER UNIT REPLACED, IGNITION LEAD REPLACED & IGNITER PLUG REPLACED. SYS RETURNED TO NORMAL OPERATIONAL STATE. FUNCTION TEST OF APU CARRIED OUT SUCCESSFULLY. FIVE ATTEMPTED STARTS TRIED BEFORE REPLACEMENT OF ABOVE PARTS. TWO GOOD STARTS ACHIEVED AFTER REPLACEMENTS. NO VERIFICATION FLIGHT REQUIRED. ACFT GOOD FOR SERVICE.

Part: EADI — FAULTY (COCKPIT) · airframe 89,434 hrs · 14,060 cycles

CAPTAIN'S EADI BLANKS. INSPECTED CAPT EADI FOUND NO PUSHBACK SOCKETS, SWAPPED EADI WITH FO, PROBLEM WENT TO FO, REPLACED CAPT EADI.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 88,839 hrs · 13,983 cycles

AFT CEILING EMERGENCY LIGHT RT SIDE COACH FOUR EACH IS INOPERATIVE. REPLACED BATTERY PACK IAW MM 33-51-07, CHECKED NORMAL.

Part: BRACKET — BROKEN (THRUST REVERSER) · airframe 87,802 hrs · 13,843 cycles

BRACKET SECURING PANEL IN LT ENG TAILPIPE BROKEN AT 5:30 POSITION. PLACED PANEL ON CF IAW INTERIM REPAIR IAW 78-31-14 PANEL WILL NEED REPLACED. IAW IPC 78-31-01-18B FOR POSSIBLE PARTS. PARTS 181-7618 315T3550-20.

Part: OXYGEN BOTTLE — LOW PRESSURE (CREW O2) · airframe 87,620 hrs · 13,820 cycles

CREW O2 READING 620 PS1. REMOVED O2 CYLINDER & SERVICED LOCALLY IAW MM, NO LEAKS NOTED.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 87,455 hrs · 13,799 cycles

APU BOTTLE DISCHARGE LIGHT WILL NOT ILLUMINATE DURING PREFLIGHT ANNUNCIATOR LIGHT TEST. DEFERRED IAW MEL 2622C, DAILY FLIGHT CHECK COMPLETE DDP, OK TO CONTINUE.

Part: GAUGE — INOPERATIVE (FUEL SYSTEM) · airframe 87,330 hrs · 13,780 cycles

CTR FUEL GAUGE AT FUELING BAY INOPERATIVE. R & R CTR FUEL GAUGE AT FUELING BAY, ALL OPERATIONS NORMAL AT THIS TIME.

Part: ACTUATOR — LEAKING (RUDDER) · airframe 87,282 hrs · 13,774 cycles

HYDRAULIC FLUID LEAKING ON TOP OF TAIL CONE FROM RUDDER DRAIN, FOUND ON WALK AROUND. DURING INSPECTION OF RUDDER PCA AREA, FOUND UPPER RUDDER PCA ACTUATOR LEAKING FROM ROD END .

Part: FLUID — LEAKING (HYDRAULIC SYS) · airframe 87,282 hrs · 13,774 cycles

HYD FLUID LEAKING ON TOP OF TAIL CONE FROM RUDDER DRAIN, FOUND ON WALK AROUND.

Part: ACTUATOR — LEAKING (RUDDER) · airframe 87,282 hrs · 13,774 cycles

HYD FLUID LEAKING ON TOP OF TAIL CONE FROM RUDDER DRAIN. DURING INSPECTION OF RUDDER PCA AREA, FOUND UPPER RUDDER PCA ACTUATOR LEAKING FROM ROD END .

Part: COVER — BROKEN (NLG DOOR) · airframe 86,783 hrs · 13,712 cycles

LT NOSE GEAR DOOR AFT HINGE COVER BROKEN OFF. COVER REMOVED & STOWED IN FLIGHT DECK, NO OTHER DAMAGE FOUND. ITEM DEFFERED IAW CDL 53A. PART NEEDED IPC 53-16-01-01 ITEM 392, PN 141T6976-42, PCN 160-2854. CAL M&E 64-5316-3-0010. PARTS: 160-2854 141T6976-2 HINGE.

Part: CONTROL VALVE — INOPERATIVE (ANTI SKID SYSTEM) · airframe 86,687 hrs · 13,697 cycles

SETTING PARKING BRAKE CAUSES ANTI-SKID OFF EICAS MESSAGE AND ANTI-SKID LIGHT ON OVERHEAD PANEL. R & R PARKING BRAKE CONTROL VALVE, ALL OPS AND LEAK CKS GOOD, OK TO CONTINUE.

Part: LIGHT — INOPERATIVE (SEAT 6J) · airframe 86,612 hrs · 13,689 cycles

SEAT 6J SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. INSTALLED OTTOMAN 6J REF SMC004 AND INSTALLED EMERGENCY ESCAPE PATH LIGHT, OPS CHECKED NORMAL.

Part: ACTUATOR — FAULTY (AILERONS) · airframe 86,420 hrs · 13,664 cycles

AILERON LOCK LIGHT ON AT HIGH SPEED. EICAS MESSAGE AILERON LOCKOUT DISPLAYED. OTBD AILERONS INDICATED NORMAL, LOCKED OUT. ACCOMPLISH CHRONIC REVIEW. REPLACED RT AILERON LOCKOUT ACTUATOR IAW AMM, TEST PASSED.

Part: SEAL — WORN (AIR DUCT) · airframe 86,411 hrs · 13,663 cycles

SIDE WALL AT 24A UNUSUALLY HOT AND HAS ODOR. REPLACED WORN OUT SEALS AT AIR SUPPLY DUCT.

Part: WIRE — SHORTED · airframe 86,343 hrs · 13,654 cycles

F/O RDMI FLAGS. FOUND SHORTED WIRE W161-223B-24 COMING OUT OF THE TB1 H5 BURNDY BLOCK, REMOVED WIRE 161-223B-24 FROM BURNDY BLOCK H5 RDMI. OPS CHECKED GOOD BEHIND ELECTRONICS RACK 1-6, SHORTED WIRE WILL BE REPAIRED ON OTHER SMC'S.

Part: CIRCUIT CARD — FAULTY (FIRE WARNING) · airframe 86,339 hrs · 13,653 cycles

FIRE BELL SOUNDS CONTINUOUSLY WITH NO FIRE LIGHTS OR EICAS STARTING AT NOSE WHEEL LIFTOFF. REPLACEED BELL-CHIME CARD. FIRE OVHT TESTED OK IAW MM 26-11-00, PG 501, MM26-17-00, PG 501, MM26-16-00, PG 501, AND MM26-15-00, PG 501.

Part: ACTUATOR — WARNING MESSAGE (LT AILERON) · airframe 86,307 hrs · 13,650 cycles

AILERON LOCKOUT MESSAGES, REPLACED LEFT AILERON LOCKOUT ACTUATOR IAW MM, OPS CHECKED GOOD.

Part: ACTUATOR — FAULTY (AILERONS) · airframe 86,228 hrs · 13,639 cycles

AILERON LOCKOUT EICAS MESSAGE & OVERHEAD LIGHT CAME ON AT 9,000. REPLACED THE RT WING OTBD LOCKOUT ACTUATOR IAW SERVICE TIP AMM 27-11-44 P 200A. ACCOMPLISHED LOCKOUT & MECHANISM TEST IAW AMM. CLEARED ALL EICAS STATUS MESSAGES. ACFT OK FOR SERVICE.

Part: LAMP — BURNED OUT (NAVIGATION PANEL) · airframe 85,926 hrs · 13,595 cycles

MODE CONTROL PANEL, ALL MODE RT HALF OF LIGHT BAR EXTINGUISHED WHEN SELECTED. LEFT NAVIGATION SWITCH, LEFT HALF BURNED OUT, REPLACED LAMP, LEFT NAVIGATION AND PERFORMED MCDP TEST O4, TESTED NORMAL.

Part: HOSE — LEAKING (LT MLG) · airframe 85,773 hrs · 13,576 cycles

LEFT MLG HAD A RUNNING HYD LEAK ON ARRIVAL. HYD LEAK TRACED TO THE BRAKE FLEX HOSE. R & R HOSE ASSY, BRAKES BLED. LEAK CHECKED SATISFACTORY. HYD QTY INDICATION CHECKED FULL.

Part: INDICATOR — FAULTY (FUEL QTY) · airframe 85,647 hrs · 13,561 cycles

AIR BUBBLE IN RT FUEL QTY GAUGE. REPLACED FUEL QTY GAUGE IAW MM28-41-00, GROUND CHECKED NORMAL.

Part: STRAP — BROKEN (FUSELAGE) · airframe 85,598 hrs · 13,555 cycles

AVIONICS DUO PACK RIGHT SIDE MID GALLEY HAS BROKEN STRAP THAT SECURES PACK IN PACK TRAY. AVIONICS DUO PACK REMOVED FROM STOW BIN AT MID GALLEY RIGHT SIDE. STRAP TAPED ON INSIDE OF PACK TRAY AND SECURE. WILL NEED NEW RIVET TO SECURE STRAP. ONE UNIT REMOVED. SECURED STRAP AND INSTALLED O2 UNIT.

Part: LINE — LEAKING (LAVATORY TANK) · airframe 85,552 hrs · 13,549 cycles

LAVATORY SERVICE REPORTED WHEN SERVICING LAVATORY WITH BLUE WATER, FLUID STARTED TO COME OUT OF DRAIN HOLE IN FRONT OF SERVICE PANEL. REPLACED FILL LINE FOR FWD TANK FROM FILTER TO PRECHARGE SHUTOFF VALVE IAW MM 20-11-00 AND LEAK CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 85,432 hrs · 13,533 cycles

EMERGENCY LIGHT AT SEAT 35B INOPERATIVE. REPLACED LAMPS, OPS NORMAL.

Part: SELECTOR PANEL — FAULTY (EICAS) · airframe 85,432 hrs · 13,533 cycles

EICAS DISPLAY SELECT PANEL TEST BUTTON DOES NOT WORK. REPLACED EICAS DISPLAY PANEL, TESTED OKAY.

Part: WARNING LIGHT — FALSE ACTIVATION (A/C PACKS) · airframe 85,432 hrs · 13,533 cycles

LT PACK BITE AND RT PACK BITE EICAS MAINTENANCE MESSAGES DISPLAYED. BITE CHECKED RT AND LT PACKS, MESSAGES GONE. CHECKED GOOD REF MM.

Part: ALTIMETER — INOPERATIVE (CAPTAIN'S) · airframe 85,432 hrs · 13,533 cycles

CAPTAIN`S ALTIMETER ANNUNCIATOR INOPERATIVE. REPLACED DEFECTIVE ALTIMETER. GROUND TESTED GOOD IAW MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 85,432 hrs · 13,533 cycles

EMERGENCY LIGHT AT SEATS 27, 30, 31, 34 & 37 JK ONE LAMP INOPERATIVE. REPLACED LAMP, OPS NORMAL.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 85,432 hrs · 13,533 cycles

EMERGENCY LIGHT AT SEAT 27JK MISSING LENS. REPLACED LENS. GROUND TESTED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 85,432 hrs · 13,533 cycles

EMERGENCY LIGHT AT SEAT 9HJ INOPERATIVE. REPLACED LAMPS, OPS NORMAL.

Part: LIGHT — INOPERATIVE (OVERWING) · airframe 85,432 hrs · 13,533 cycles

EMERGENCY LIGHT AT OVER WING EXIT LOWER NEAR SEAT 19HJ INOPERATIVE. TROUBLESHOT AND FOUND DEFECTIVE LIGHT. REPLACED OVERWING EXIT LIGHT ASSY. OP'S CHECKED GOOD.

Part: WINDOW FRAME — LOOSE (EMERGENCY EXIT) · airframe 68,180 hrs · 25,078 cycles

EMERGENCY EXIT WINDOW FRAME LOOSE. SECURED WINDOW FRAME.

Part: WIRE HARNESS — WORN (ELECTRICAL) · airframe 85,201 hrs · 13,505 cycles

ELECTRIC WIRE HARNESS INSULATION WORN AT P62. REPLACED PIGTAIL AT P62. OPS CHECKED WITH CART CONTROLLER TESTER, OPS CHECKED GOOD.

Part: WIRE — FAILED (GALLEY CART) · airframe 85,158 hrs · 13,500 cycles

P52 PIGTAIL SMOKING AND VERY HOT. ISOLATED BY PULLING CIRCUIT BREAKER AND DISCONNECTED PIGTAIL. SMOKE STOPPED AND PIGTAIL COOLED. NO ADDITIONAL ISSUES NOTED ALL LIGHTS OPERATING & GALLEY SYS NORMAL. SMOKE IN CABIN COND INSP ACCOMPL ACC AMM 05-51-56. CART CONTROLLER DEACTIVATED. REPLACED PIGTAILS ATP5. ACCOMPLISHED OPS CHECK WITH CART CONTROLLER TESTER, OPS CHECKED GOOD.

Part: CONNECTOR — BROKEN (WINDOW HEAT) · airframe 85,128 hrs · 13,495 cycles

LEFT SIDE WINDOW HEAT INOPERATIVE. FOUND J12 CONNECTOR BROKEN. INSTALLED NEW CONNECTOR AND TESTED SYSTEM IAW 30-41-00. NO DEFECTS NOTED.

Part: WINDOW — DEFECTIVE (COCKPIT L3) · airframe 85,128 hrs · 13,495 cycles

CAPTAIN'S AFT SIDE WINDOW AFT SIDE AREA HAS BUBBLES FORMING. REPLACED L3 WINDOW AND TESTED IAW 56-11-10. NO DEFECTS NOTED.

Part: BLOWER — FAULTY (LAVATORY) · airframe 85,128 hrs · 13,495 cycles

AFT LEFT, AFT LEFT CENTER AND RIGHT BUSINESS LAVS WILL NOT FLUSH. NO VACUUM, FORWARD SYSTEM. VACUUM AVAILABLE ABOVE 16K FEET. REMOVED AND REPLACED FWD SYSTEM 2 BLOWER PER MM, OPS CHECK NORMAL.

Part: AMPLIFIER — FAULTY (NR 1) · airframe 84,948 hrs · 13,472 cycles

REPLACED PA AMP AND AUDIO ACCY UNIT. PUT BACK OLD AUDIO ACCY UNIT. PA AMP MR23316 - 1 REPLACED WITH MR23316 - 30. REF LOG 8, PANASONIC DID SO WORK EARLIER TODAY, PLEASE HAVE THEM REPLACE THE PARTS OR RELOAD SOFTWARE FOR TROUBLESHOOTING PURPOSES. REPLACED AUDIO ACC UNIT, OPS CHECK NORMAL.

Part: IGNITER — FAULTY (NR 1 ENGINE) · airframe 84,840 hrs · 13,454 cycles

REPLACE IGNITER PLUGS (NR 1 ENGINE). REPLACED IGNITORS NR 1 ENGINE.

Part: WEB — CORRODED (CENTER WING) · corrosion level 2 · airframe 84,838 hrs · 13,453 cycles

LEFT MAIN WHEEL WELL, REAR SPAR WEB CORRODED AT BS 955, LBL 78. REPAIRED THE BS 955 LT SIDE CTR WING SECTION REAR SPAR BULKHEAD WEB & MODIFICATION OF FAILSAFE STRAP IAW REO-G15835, AND ECRA 5340-01497.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,838 hrs · 13,453 cycles

FUSELAGE SKIN SURFACE LOWER AREA, CORROSION BELOW FASTENER HOLE AT 1 IN ABOVE LOWER EDGE BS 962. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION ON SKIN LOWER AREA AND INSTALLED DISC FILLER IAW ECRA 5340-01497.

Part: SKIN — DAMAGED (BS 1725.5) · airframe 84,838 hrs · 13,453 cycles

LEFT FUSELAGE SKIN DAMAGED AT BS 1725.5 S24-27L. INSTALLED INTERIM REPAIR.

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 84,838 hrs · 13,453 cycles

LEFT HORIZONTAL STAB INBOARD, L/E AREA LOWER SKIN DAMAGED. REPAIRED LEFT HORIZONTAL STAB INBOARD LOWER PANEL SKIN FWD TORQUE BOX IAW REO-G15880 AND EC-RA 5510-02276.

Part: HOUSING — CRACKED (EVAC SLIDE) · airframe 84,838 hrs · 13,453 cycles

RIGHT OVERWING SLIDE COMPARTMENT, DISCONNECT HOUSING FOUND BROKEN-CRACKED, DURING SQUIB DATE CHECK. REMOVED RIGHT DISCONNECT CAM ASSEMBLY, REMOVED AND REPLACED RIGHT DISCONNECT HOUSING AND REINSTALLED CAM ASSEMBLY PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,838 hrs · 13,453 cycles

AFT CARGO COMPARTMENT LOWER BILGE, 2 EACH SHEAR TIES CORRODED ON AFT SIDE ALONG FASTENERS AT BS 1330, S-35L TO S-37L. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED SHEAR TIES FROM BS 1330, STR-35L TO S-37L PER BAC DWG 146T1212, REV E AND SRM 53-06-07 ON NON ROUTINE 44734.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,838 hrs · 13,453 cycles

AFT CARGO COMPARTMENT BILGE, SHEAR TIES CORRODED ON AFT (FASTENER) SIDE OF FRAME BENEATH PRESSURE WEB AT BS 1330, S-37L TO S-39L. MAJOR REPAIR ACCOMPLISHED. REMOVED & REPLACED SHEAR TIES AT BS 1330, S-39L TO S-37L BAC DWG 146T1212, REV E AND SRM 51-40-2.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,838 hrs · 13,453 cycles

AFT CARGO COMPARTMENT BILGE, SHEAR TIE CORRODED, ON AFT SIDE OF BS 1307 WEB, BETWEEN STR 38L-STR 37L. MAJOR REPAIR ACCOMPLISHED. REMOVED SHEAR TIE AND FABRICATED A NEW SHEAR TIE AND INSTALLED PER BAC DWG 140T2102, REV C AND SRM 51-40-2.

Part: SHEAR TIE — CORRODED (BS 1307 S38-39L) · corrosion level 2 · airframe 84,838 hrs · 13,453 cycles

AFT CARGO BILGE, SHEAR TIE IS CORRODED, ON AFT SIDE OF BS 1307 WEB BETWEEN S-38L TO S-39L. REMOVED AND REPLACED SHEAR TIE PER DWG 146T1211, REV F AND SRM 51-40-2. MAJOR REPAIR.

Part: SKIN — DENTED (CARGO DOOR) · airframe 84,838 hrs · 13,453 cycles

BULKPIT DOOR HAS 2 EA SKIN DENTS 2 IN FROM AFT EDGE, JUST ABOVE SCAB PATCH. AT C15 VISIT, RE-EVALUATED DENTS AND FOUND 3 TOTAL DENTS ABOVE EXISTING DOUBLER. ALL 3 DENTS ARE NOT WITHIN SRM 52-30-01 LIMITS, AND A OVER Y RATIOS ARE 17.14, 21.73 & 25. REMOVED EXISTING DOUBLER, CUT OUT DAMAGE SKIN, FABRICATED A DOUBLER AND FILLER AND INSTALLED PER SRM 52-30-01, RPR 6.

Part: SKIN — DENTED (CARGO DOOR) · airframe 84,838 hrs · 13,453 cycles

CARGO DOOR, LOWER FWD CORNER HAS NUMEROUS DENTS. EVALUATED FOUR DENTS AND FOUND TO BE OUT OF SRM 52-30-01 LIMITS. CUT OUT DAMAGED DOOR SKIN, FABRICATED AND INSTALLED A DOUBLER AND FILLER. CATAGORY 'B' REPAIR.

Part: YOKE — ODOR (COCKPIT) · airframe 84,656 hrs · 13,429 cycles

CREW REPORTS BURNING ELECTRIC ODOR FROM CAPT CONTROL WHEEL NEAR AILERON TRIM STICKER. MAINTENANCE CONFIRMS THAT ELECTRICAL ODOR IS COMING FROM PILOT YOKE. DOES NOT FEEL WARM TO THE TOUCH. SAMC TEXT: NO SMOKE OR HEAT EVER OBSERVED.

Part: TRIM SWITCH — FAULTY (COCKPIT) · airframe 84,656 hrs · 13,429 cycles

CREW REPORTS BURNING ELECTRIC ODOR FROM CAPT CONTROL WHEEL NEAR AILERON TRIM STICKER. DOES NOT FEEL WARM TO THE TOUCH. NO SMOKE OR HEAT EVER OBSERVED. REPORTED FROM PREVIOUS SHIFT SMELL SEEMED TO BE COMING FROM CAPT STAB TRIM SWITCH. OHM CHECKED FROM CONNECTOR D5131P, D5133P, TO CAPT STAB TRIM SWITCH, PIN TO PIN AND TO GRND, NO FAULTS. REPLACED CAPT STAB TRIM SWITCH DUE TO REPORT OF SMELL AT SWITCH AREA REF MM, OPS CHECKED GOOD, NO FAULTS OR ODOR NOTED. ACP CHECK AND METER WAS SENT.

Part: CDU — FAULTY (COCKPIT) · airframe 84,309 hrs · 13,378 cycles

L FMC MCDU IS BLANK, FLT DIVERTED. NO EICAS MSG DISPLAYED. SWITCHED TO RT FMC, NO HELP. TWO CDUS REQUIRED TO ENTER MNPS AIRSPACE. FOUND LEFT CDU AT FAULT. REPLACED CDU PER MM.

Part: PRESSURE SWITCH — FAULTY (HYDRAULIC SYS) · airframe 83,391 hrs · 13,256 cycles

LEFT ELEC HYD PUMP DOES NOT OPERATE IN AUTO. DEFERRED DUE TIME ON FUNCTION OPERATES NORMAL. REPLACED S26 PRESS SWITCH AND D54 CONNECTOR. OP CHECKS OKAY.

Part: DISPLAY — FAILED (UPPER EICAS) · airframe 83,320 hrs · 13,247 cycles

UPPER EICAS SCREEN FLICKERS OR GOES BLANK WITH ENGINES SUPPLYING ELECTRICAL POWER. REPLACED UPPER EICAS DISPLAY AND CB C4081. OPS CHECKED NORMAL.

Part: DISPLAY — FAILED (COCKPIT) · airframe 83,320 hrs · 13,247 cycles

LOWER EICAS BLANKED OUT AFTER SECOND ENGINE START. REPLACED EICAS DISPLAY SELECT PANEL. INSTALLED LOWER CRT IN UPPER POSITION AND INSTALLED NEW CRT IN LOWER POSITION. OPS CHECKED GOOD.

Part: INDICATOR — FAULTY (INSTRUMENT PANEL) · airframe 82,916 hrs · 13,193 cycles

STANDBY ENGINE INDICATOR BLANK WHEN SELECTED ON. REPLACED STANDBY ENGINE INDICATOR PER MM, OPS NORMAL.

Part: STRUCTURE — DAMAGED (LT NACELLE) · airframe 82,849 hrs · 13,183 cycles

LT ENGINE INNER INLET COWL HAS A HOLE APPROX 5-16THS BY 1-4 IN. LOCATION IS APPROX 10 O`CLOCK POSITION 7.5 IN FWD OF AFT END OF INLET COWL. REPAIRED PER SRM.

Part: UNKNOWN — FAULTED (WINDSHEAR SYSTEM) · airframe 81,933 hrs · 13,063 cycles

PREDICTIVE WINDSHEAR SYSTEM DOES NOT TEST CORRECTLY. REPLACED WEATHER TRANSCEIVER PER MM AND ACCOMPLISHED TEST, TEST PASSED. NEWLY INSTALLED RT UNIT FAILED, REINSTALLED ORIGINAL UNIT AND TESTS OKAY.

Part: AMU — FAULTY (NR 1) · airframe 81,859 hrs · 13,055 cycles

ACARS NO COM MULTIPLE OCCASSIONS DURING FLIGHT. REPLACED ACARS MANAGEMENT UNIT AS PER MM, OPS CHECKED NORMAL.

Part: CONTROL VALVE — ILLUMINATED (TE FLAPS) · airframe 81,646 hrs · 13,027 cycles

T/E FLAP DISAGREE FAULT WHEN FLAPS GO BETWEEN 1 & 5. REPLACED T/E FLAP CONTROL VALVE MODULE & BYPASS VALVE. REPLACED FLAP BYPASS VALVE. TESTED OK IAW MM.

Part: INDICATOR — FAULTED (TE FLAPS) · airframe 81,635 hrs · 13,026 cycles

FLAP NEEDLE SPLIT WHEN FLAPS DROPPED FROM 5 THRU 25, NEEDLES ALIGNED AT 25, SPLIT AT 30. CYCLED FLAPS AND DUPLICATED SPLIT AGAIN WHEN FLAPS DROPPED THRU EACH POSITION. FLAPS DRIVE SMOOTH HYDRAULICALLY, SUSPECT FLAP POSITION INDICATOR SYSTEM. REPLACED MODULE FLAPS ALT ELECTRIC INOPERATIVE. LOCKED UP AT 1. REPLACED K351 RELAY PER MM. FOUND NORMAL WPB29498 31271. TROUBLESHOT PER FIM. FOUND ELEC MOTOR POWERED IN BOTH DIRECTIONS AND SOUNDS LIKE ITS SPINNING BUT OUTPUT SHAFT DOES NOT TURN. REMOVED MOTOR PER MM. INSTALLED ALT TE FLAP ELECTRIC MOTOR PER MM. ACCOMPLISHED TEST OF ALT MOTOR, OP'S CHECKED GOOD.

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 81,635 hrs · 13,026 cycles

HYD LEAK IN NOSE WHEEL WELL AREA. FOUND WITH GEAR HANDLE IN UP POSITION LEAK IS BETWEEN THE LEFT SWIVEL FITTING & THE GEAR ACTUATOR. REPLACED O-RING ON THE UP FITTING UNION, NO LEAKS.

Part: STATIC INVERTER — MALFUNCTIONED · airframe 81,588 hrs · 13,020 cycles

STATIC INVERTER MALFUNCTIONED. REPLACED STATIC INVERTER, OP CHECKED GOOD AND PILOTS TESTED. ALL CHECKED GOOD.

Part: ACTUATOR — LEAKING (LT ELEVATOR) · airframe 80,957 hrs · 12,935 cycles

LT OUTBOARD ELEVATOR PCA HAS RUNNING LEAK FROM SHAFT SEAL. SHOULD READ LEAKING FROM LT CENTER ELEVATOR PCA. PCA REMOVED. COMPLETED INSTALLATION OF LT CTR ELEV PCA.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 79,576 hrs · 12,748 cycles

NR 1 ENG EDP WILL NOT DESELECT PRESSURE. REPLACED NR 1 ENGINE EDP, OPS CHECKED GOOD.

Part: COUPLER — DEFECTIVE (HF COMM) · airframe 79,186 hrs · 12,694 cycles

R HF INOPERATIVE. CARRIED OUT HF TEST. TONE OK. TRANSMISSION OKAY. TRANSCEIVER PREVIOUSLY REPLACED. WILL REQUIRE HF COUPLER, NO TIME (PCN 530-9045). REPLACED HF COUPLER, OP CHECKS GOOD.

Part: ACTUATOR — FAULTY (RUDDER TRIM) · airframe 79,186 hrs · 12,694 cycles

RUDDER TRIM ACTUATOR CHG. DUE TO RECENT HISTORY IF RUDDER TRIM PROBLEMS ACCOMPLISH THE FOLLOWING. REPLACE THE RUDDER TRIM ACTUATOR PER MM. THE PCN FOR THE RUDDER TRIM ACTUATOR IS 563-9038. PLEASE CHECK ONLINE IPC FOR CORRECT EFFECTIVITY. REPLACED RUDDER TRIM ACTUATOR PER MM.

Part: CONNECTOR — FAULTY (RUDDER TRIM) · airframe 79,178 hrs · 12,693 cycles

NO RUDDER TRIM INDICATION OR MOVEMENT WITH RUDDER TRIM KNOB ELECTR. CONNECTOR REMOVED & RECONNECTED RUDDER TRIM ACTUATOR TEST PERFORMED PER AMM. SYS OPS NORMAL.

Part: AUTOTHROTTLE SYS — MALFUNCTIONED (COCKPIT) · airframe 78,651 hrs · 12,621 cycles

AUTOTHROTTLE FAIL AT STATUS ON ADI IS BLANK. TMC APPEARS OK. LEG FAULT A-T DISC TMC 01310800 AND TEST FAILURE OF MCDP-TMC. REPLACED TMC. AUTOLAND TEST 02, 30, 40 PASSED.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 78,173 hrs · 12,550 cycles

LEFT HYD QTY LIGHT DURING ROLL OUT. SYSTEM QTY WHEN TO ZERO VERY RAPIDLY FOLLOWED BY L HYD PRIM SAMC TEXT: PUMP EICAS DURING TAXI IN. COMPLETED CHECK LIST AND SHUT DOWN PUMPS. ACC MAINT REPORT ENGINE DRIVEN HYD PUMP LEAK AT PUMP DEPRESSURIZATION SOLENOID. REPLACED EDP PER MM. REPLACED EDP PRESSURE-CASE DRAIN FILTERS PER MM. RUN ENGINE PER JRH, ACCMP'D LEAK CHECK. ALL OPERATIONS AND INDICATIONS NORMAL.

Part: CONTROLLER — MALFUNCTIONED (BLEED AIR SYS) · airframe 77,959 hrs · 12,515 cycles

RIGHT ENG BLEED LGT & R ENG HPSOV EICAS MSG DURING DESCENT WITH ENG BLEED SW ON & ENG RUNNING. REPLACED HPC CONTROLLER PER MM. ACP HIGH POWER ENGINE RUN, ALL INDICATIONS AND OPS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,752 hrs · 12,484 cycles

LH AFT MED EMERGENCY EXIT IDENTIFIER AND FLOOR STRIP NEXT TO LAV INOPERATIVE. REPLACED BATTERY PACK PER MM, OP CHECKS NORMAL.

Part: CABLE — BURNED (GALLEY) · airframe 77,752 hrs · 12,484 cycles

AFT GALLEY NEW TECH CART CABLES P52, P61 & P62 HAVE BURNT PINS. REPLACED CABLE ASSEMBLIES, OPS CHECK NORMAL.

Part: LENS — BROKEN (CABIN) · airframe 77,728 hrs · 12,479 cycles

SEAT 27ABC EMERGENCY LIGHT LENS BROKEN. REPLACED BROKEN LENS, OP CHECKS GOOD.

Part: LENS — MISSING (CABIN) · airframe 77,728 hrs · 12,479 cycles

SEAT 36ABC EMERGENCY LIGHT LENS MISSING. REPLACED BROKEN LENS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,199 hrs · 12,404 cycles

SEAT 26AB EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT AND OPS CHECK GOOD ON NON ROUTINE 23401.

Part: CABLE — DAMAGED (CABIN) · airframe 77,199 hrs · 12,404 cycles

FWD RT LIGHT BAR IS INOP. REPAIRED EEL CABLE USING CRIMPER TM13-0800C PER MM. OPS CHECK GOOD ON NON ROUTINE.

Part: HINGE FITTING — CRACKED (TE FLAP) · airframe 77,199 hrs · 12,404 cycles

LEFT WING INBOARD MAIN FLAP, TRAILING EDGE, AFT FLAP HINGE FITTING, INBOARD FLANGE CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE AND FABRICATED A REPAIR ANGLE AND FILLERS AND INSTALLED PER SRM.

Part: HEAT EXCHANGER — CRACKED (A/C PACK) · airframe 77,009 hrs · 12,376 cycles

LH PACK PRIMARY HEAT EXCHANGER WITH A 5" LONG HEAVILY BLOWING AIR WITH PACK ON. UPDATE HEAVY NOISE FOUND AFTER TOWING AND ARRIVAL TO THE GATE. REPLACED PRIMARY HEAT EXCHANGER AND PLENUM ASSY PER MM.

Part: WIRE — CHAFED (LT OVRWG SLIDE) · airframe 76,964 hrs · 12,371 cycles

LEFT WING SLIDE EICAS INTERMITTENT. REPEAT GRIPE. PSEU BITE SHOWS SAME FAULTS AS PREVIOUS. ADJUSTED S218 TARGET PER MM. REPAIRED CHAFED WIRE NR 216R-20 IN ADP BAY. SEU BITE AND SENSOR TESTS OK.

Part: SENSOR — FAULTY (LT WING SLIDE) · airframe 76,826 hrs · 12,352 cycles

LT WING SLIDE EICAS, FLIGHT DIVERTED. REPLACED S218 SENSOR IAW AMM, GROUND CHECKS NORMAL

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 76,433 hrs · 12,297 cycles

DOOR 1L SLIDE DOOR NOT SECURE. FOUND ESCAPE SLIDE PARTIALLY DETACHED FROM DOOR. DOOR 1L EMERGENCY ESCAPE SLIDE REMOVED. DOOR 1L PROPERLY CLOSED. REMOVED SLIDE NUMBER IS MR25708-225. REPLACED ENTRY DOOR ESCAPE SLIDE PACK AT DOOR 1L PER MM.

Part: SWITCH — FAULTED (OVERHEAT DETECT) · airframe 76,319 hrs · 12,281 cycles

LT ENG FIRE LOOP 2 STATUS MSG DISPLAYED. REPLACED FIRE-OVERHEAT TEST SWITCH ON P8 STAND FIRE-OVERHEAT TEST PANEL. OP CHECK SEVERAL TIMES AND CHECKED OKAY.

Part: MICROPHONE — FAULTY (OXYGEN MASK) · airframe 76,174 hrs · 12,259 cycles

2ND OBSERVERS OXYGEN MASK MIC WILL NOT TRANSMIT. REPLACED MASK ASSY, NO LEAKS NOTED. MIC STILL DOSEN'T TRANSMIT ON PA OR TO VHF.

Part: CONNECTOR — DIRTY (THRUST REVERSER) · airframe 76,124 hrs · 12,251 cycles

EICAS MESSAGE REVERSER ISOLATION VALVE DISPLAYED AND REVERSER ISOLATION LIGHT ILLUMINATED DURING REVERSE THRUST. REACTIVATED REVERSER. CLEANED CONNECTOR AT REVERSER ISOLATION VALVE. CHECKED OPERATION SEVERAL TIMES. REVERSER OPERATION NORMAL, NO FURTHER MESSAGES DISPLAYED OR FAULTS AT REVERSER CONTROL MODULE.

Part: CIRCUIT CARD — FAULTY (LT FIRE LOOP) · airframe 76,116 hrs · 12,250 cycles

LT ENGINE FIRE LOOP 2 DISPLAYED ON STATUS. FIRE TEST NO HELP. WON'T ERASE. REPLACED CARDS M684 AND M10274, LOOP RESISTANCE FROM CARD 684 PIN 19-20 1450 OHMS.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 76,116 hrs · 12,250 cycles

LEFT HYD SYS QTY INDICATES .68 RF ON STATUS AND EICAS PGS. FOUND LT SYS HYD QTY AT .40, SERVICED LT SYS TO FULL. FOUND EVIDENCE OF LARGE HYD LEAK IN TAIL. SUSPECT LT SYS RUDDER PCU OR LINE TO IT.

Part: FIRE DETECTOR — OUT OF LIMITS (LT NACELLE) · airframe 75,991 hrs · 12,231 cycles

LEFT ENG FIRE LP2 STATUS MSG. ACCOMPLISHED FIM. REPLACED CARD FILE M682 AND SWAPPED AFOLTS NR 1 WITH NR 2, NO HELP. REINSTALLED CARD TO ORIGINAL POS, FOUND DETECTOR TS681 OUT OF LIMITS PER FIM. ACCOMPLISHED CARD FILE REPLACEMENT IAW MM.

Part: CIRCUIT CARD — FAILED (NR 2) · airframe 75,991 hrs · 12,231 cycles

NR 2 ENG OVERHEAT LP2 AND OVERHEAT LP1 STATUS MESSAGE DISPLAYED LWR EICAS AFTER SWAPPING AFLOTS NR 1 AND NR 2 CARD PER FIM TO AID IN NR 1 ENG FIRE LP2 STATUS MSG. REPLACED NR 2 ENGINE AFOLTS CARD M10274 IAW MM, OP CHK GOOD.

Part: ACTUATOR — FAULTY (CABIN TEMP) · airframe 75,879 hrs · 12,218 cycles

TEMP UNCONTROLLABLE ALL CABINS AND CP. ALL TEMP CONTROLS FULL COLD OR BOTH PACKS STB C TEMPS 75. ZONE TEMP BITE OK. FOUND RT PACK RAM AIR EXHAUST DOOR ACTUATOR INOP. DOOR MOVES BY ITSELF. A ACTUATOR NO STOCK FRA. REMOVED EXHAUST DOOR PER CDL. DOOR AND ACTUATOR PLACED IN COCKPIT. PACK OPS OK.

Part: SENSOR — FAULTY (LT WING SLIDE) · airframe 75,562 hrs · 12,178 cycles

LEFT WING SLIDE EICAS OCCASIONALLY ILLUMINATES INFLIGHT. FOUND S218 SENSOR FAULTED ON PSEU.

Part: SENSOR — FAULTY (LT WING SLIDE) · airframe 75,440 hrs · 12,164 cycles

L WING SLIDE EICAS MSG. REPEAT EICAS MSG "LEFT WING SLIDE" WITH EMER DOORS LT ILLUM ON OVERHEAD PANEL. NEED TO ACP T-S PER MM. WARNING FOLLOW DEACTIVATION PROCEDURES** ACP COMPLETE OFF WING ESCAPE SLIDE SYSTEM ADJ. CHK'D GAPS ON LH WING SLIDE DOOR LOCKED AND SLIDE DOOR CL SENSORS ARE WITHIN LIMITS AND ADJUSTED PROPERLY. REPLACED DOOR LOCKED SENSOR (S198) IF NEEDED. REPLACED LEFT SLIDE COMPARTMENT DOOR LOCK SENSOR S198. SQUIB TEST NORMAL NO EICAS MSG.& OVERHEAD LIGHT WORKED NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 75,052 hrs · 12,111 cycles

EXTERIOR LIGHT AT AFT OF 2RMED INOP (767). RELAMPED (767) TWICE BUT NO HELP. REQUIRES ADDITIONAL TROUBLESHOOTING REPLACED BATTERY PACK, NO HELP. TRIED NEW BATT PACK & CHARGER AT POS M733 (STA 1406 BY SEATS 39JH), NO HELP. REPLACED CHARGER AT POS M733.

Part: BLOCKER DOOR — DAMAGED (THRUST REVERSER) · airframe 74,928 hrs · 12,094 cycles

NUMBER 2 FROM TOP BLOCKER DOOR DAMAGED ON THE RT ENGINE OTBD THRUST REVERSER HALF. REPLACED NR 2 ENG RT REVERSER BLOCKER DOOR.

Part: BLEED VALVE — FAULTY (NR 1 ENGINE) · airframe 74,361 hrs · 12,014 cycles

NR 1 ENGINE 2.5 BLEED VALVE NEEDS REPLACEMENT. NR 1 ENGINE 2.5 BLEED VALVE NEEDS REPLACEMENT. REPLACED NR 1 ENGINE 2.5 BLEED VALVE PER MM. COMPLETED INSTALLATION OF 2.5 BLEED VALVE IAW MM. ACCOMPLISHED TEST 3 AND TEST 6 IAW MM, TESTS OKAY, NO LEAKS NOTED.

Part: COUPLER — FAULTY (HF SYSTEM) · airframe 74,281 hrs · 12,000 cycles

RIGHT HF WILL NOT TRANSMIT AT ALL CREW STATIONS. TUNING TAKES MUCH LONGER THAN NORMAL. TRIED NEW TRANSCEIVER, NO HELP. ORIGINAL TRANSCEIVER RE-INSTALLED. REPLACED RT HF COMM ANTENNA COUPLER. ACP'D TEST IAW MM, GROUND CHECKS NORMAL.

Part: CIRCUIT BREAKER — FAILED (RUDDER SYS) · airframe 74,145 hrs · 11,983 cycles

RUDDER TRIM FAILED TO TRIM IN EITHER DIRECTION. SAMC TEXT: PLZ CHK RUDDER TRIM ACTUATOR. RESET CB P11 K16 & K17 RUDDER POSS & TRIM POSS. PERFORMED FIM 27-21-00 FIG 106, RUDDER TRIM WORKS NORMALLY, ALSO PERFORMED OPS TEST PER MM. TEST PASSED.

Part: PUMP — MALFUNCTIONED (MAIN BOOST) · airframe 73,765 hrs · 11,930 cycles

RT CTR PUMP NOT OVER RIDING MAIN PUMPS. FUEL OUT OF BALANCE. SUSPECT PUMP INOP. REPLACED RT OVERRIDE BOOST PUMP. TRANSFERRED FUEL FROM CTR TANKS TO WING TANKS AFTER LEAK AND OPS CHECKS.

Part: PUMP — INOPERATIVE (OVERRIDE BOOST) · airframe 73,750 hrs · 11,928 cycles

RIGHT CENTER PUMP NOT OVERRIDING MAIN PUMPS. FUEL OUT OF BALANCE. SUSPECT PUMP INOP. REPLACED RT OVERRIDE BOOST PUMP. TRANSFERRED FUEL FROM CENTER TANKS TO WING TANKS AFTER LEAK AND OPS CHECKS.

Part: STARTER — FAULTY (LT ENGINE) · airframe 73,730 hrs · 11,926 cycles

LT ENGINE. FIRST START ATTEMPT GOT 17 PERCENT N2 THEN SPOOL DOWN. SECOND ATTEMPT GOT START VALVE OPEN BUT NO ROTATION. SUSPECT STARTER SHAFT MAY BE SHEARED. REPLACED ENGINE 1 STARTER AND START VALVE. OPS CHECK GOOD.

Part: CIRCUIT CARD — FAULTY (TE FLAPS) · airframe 73,598 hrs · 11,906 cycles

DURING CLIMB AFTER FLAP RETRACTION, CAPTS ADI DISPLAYED THE STALL SPEED WHISKERS TILL FL200. ACCOMPLISHED FIM, NO FAULTS NOTED. BOTH STALL WARNING CARDS REPLACED ON APR-26. FAULT CHANGED TO LEFT SIDE ONLY. REPLACED LEFT STALL WARNING MODULE, ALL SUBSEQUENT TESTS PASSED.

Part: SENSOR — FAULTY (BLEED AIR SYS) · airframe 73,598 hrs · 11,906 cycles

RH ENG BLEED OVERHEAT MSG. RESET BLEED SWITCH. NO FURTHER INDICATION. REPEAT GRIPE. SECURED RT ENG HIGH PRESS SHUTOFF VALUE PER MEL ITEM 3611R. BITE CHECKED BLEED COMPUTER FOUND RIGHT ENG FAV AND FAS FAULTING ON PREVIOUS FLT. FAS SENSOR PCN 481-9007. ALSO SCREWS STRIPPED ON ACCESS DOOR. APPLIED MEL 3612D DISCONNECTED TEMP CONT PRESS LINE FROM FAN AIR VALVE AND CAPPED THE PRESS LINE AND LOCKED TO FULL OPEN POSITION. REPLACED RT ENG FAN AIR TEMP SENSOR. REACTAVATED FAN AIR VALVE PRESS SENSE LINE PER MEL3621D.

Part: CIRCUIT CARD — FAILED (STALL WARNING) · airframe 73,257 hrs · 11,859 cycles

STALL WARNING, RTFL. ACP FIM MM TASK TO FIG.103 SHT 4, BLOCK 7, REFERRED TO FIM MM PSEU BITE CHK FIG 103 SHT 3 BLOCK 2, CODE 007 CARD FAILED. REPLACED PSEU CIRCUIT CARD IAW MM AND CONT FIM. REPLACED L & R STALL WARNING MOD IAW MM. ACFT OK FOR SERVICE.

Part: TRANSCEIVER — FAILED (NR 1 VHF) · airframe 73,211 hrs · 11,851 cycles

LT VHF TRANSCEIVER INOPERATIVE. REPLACED TRANSCEIVER VHF NR 1 AND AUDIO SELECTOR PANEL. OPS CHECKS ARE GOOD .

Part: WIRE — OPEN (APU ECU DE OILER) · airframe 72,961 hrs · 11,807 cycles

APU BITE MX MESSAGE DISPLAYED ON ECS PAGE. ECU BITE SHOW DEOIL SOLENOID CIRCUIT FAILED. WIRES RANG OPEN FROM ECU. REPLACED DE-OIL SOLENOID VALVE, NO HELP. FOUND WIRE OPEN BETWEEN D4024P PIN 5 AND DE-OIL SOL CONNECTOR P11 PIN 1. FOUND WIRE FROM PIN 5 D4024P TO DIODE SEPARATED IN BUNDLE. SPLICED DIODE INLINE, APU ECU FAULT HISTORY ERASED IAW FIM.

Part: PANEL — LEAKING (RT WING) · airframe 72,961 hrs · 11,807 cycles

RT WING MID SEAM FWD OF PLATE 641FB IS LEAKING 24 INCHES IN 30 MINS, LOWER WING SURFACE. FUELED RT WING TO 33,000 LBS RT WING MID SEAM FWD OF PLATE 641FB IS LEAKING 24 INCHES IN 30 MINS. LOWER WING SURFACE. SEALED ON SMC24, FUELED AND LEAK CHECK GOOD

Part: APU — FAILED · airframe 72,459 hrs · 11,731 cycles

APU FAILED TWICE AT GATE. REMOVED AND REPLACED APU. OPS CHECKED APU AND ACCOMPLISHED PERFORMANCE TEST.

Part: EXHAUST VALVE — FAILED (FWD POSITION) · airframe 72,402 hrs · 11,718 cycles

FWD EQUIP VALVE DISPLAYED ON EICAS ON LANDING. SECURED INBD VALVE CLOSED AND REMOVED PLUG. NEED DUCT INSTALLATION FWD COMP AIR SUPPLY HEAT EXHAUST BYPASS VALVE. REPLACED FWD OVERBOARD EXHAUST VALVE. SYS CHECKS OK.

Part: STATIC INVERTER — MALFUNCTIONED (STANDBY) · airframe 72,183 hrs · 11,690 cycles

FLIGHT CREW REPORTS STANDBY INVERTER MESSAGE DISPLAYED. MSG IS INTERMITTANT, REPLACED STATIC INVERTER. ACCMP'D OP CK PASSED.

Part: SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 72,151 hrs · 11,686 cycles

T/E FLAP DISAGREE ON FINAL WITH 15 FLAPS. SUGGEST CK ALL T/E FLAP ROTARY ACTUATORS FOR TRIPS. ROTARY ACTUATORS OK. BITE CHECK FSEU NO FAULTS. OPERATED FLAPS THROUGH FULL CYCLES AND OPS NORMAL. FLAP DISAGREE WAS TROUBLESHOT TO THE M548 MODULE FOR THE OTBD SLAT POWER DRIVE UNIT OTBD SLAT POSITION TRANSMITTER. NEED TO ACCOMPLISH REPLACEMENT OF SLAT RVDT SENSOR. REPLACED M548 RVDT. OPS CK GOOD. NO RELATED MSGS. FSEU BITE CLEAN.

Part: OXYGEN MASK — UNSECURE (SEATS 35A & 35B) · airframe 72,104 hrs · 11,679 cycles

OXYGEN MASK COMPARTMENTS FELL OPEN AT 35A & 35B. REPACKED OXYGEN MASKS, INSPECTED OXYGEN GENERATOR AND CLOSED AND SECURED OXYGEN MASK DOOR IAW MM.

Part: WINDOW — OUT OF TOLERANCE (COCKPIT) · airframe 72,045 hrs · 11,670 cycles

LOUD SQUEAL AT F/O SLIDING WINDOW. CREW STATES LOUD SQUEAL IS COMING FROM RT SIDE ALONG HINGE ASSY. TAPED AREA AROUND AFT SIDE OF F/O'S SLIDING WINDOW. PLACED WINDOW ASSY IN LOB. STARTED INSTALLATION OF WINDOW 2R. INSTALLED WINDOW. F/O'S SLIDING WINDOW IS SQUEALING AGAIN. RMV'D FAULTY WINDOW. INSTALLED NEW NR 2 SLIDING WINDOW AND ADJUSTED. OP CHKS NORMAL.

Part: CHARGER — FAULTY (CABIN) · airframe 71,611 hrs · 11,609 cycles

EEL LIGHT INOP AT 19C THRU 22C. REPLACED BATTERY CHARGER. TESTS OKAY.

Part: PUMP — LEAKING (LT ENGINE) · airframe 71,512 hrs · 11,594 cycles

LEFT HYD QTY SLOWLY DECREASING NOW AT .32. FOUND HYD LEAK COMING FROM LEFT ENG DRIVEN PUMP BODY. PUMP REPLACED. LEAK CHECK PERFORMED OKAY. LEFT HYD SYS FILLED UP. ALL OPS NORMAL.

Part: PRESSURE SWITCH — DEFECTIVE (FUEL SYSTEM) · airframe 71,347 hrs · 11,572 cycles

CENTER FUEL PRESS LIGHT INOP. INOP RT CENTER FUEL PUMP. REPLACED RT CENTER OVERRIDE PUMP LOW PRESS SWITCH CHECK OKAY.

Part: CONNECTOR — CORRODED (FUEL SYSTEM) · airframe 71,209 hrs · 11,550 cycles

LT MAIN FQIS CONNECTOR M1944 ASSY IS CORRODED. INSTALLED NEW FQIS CONNECTOR M1944. OPS CHECKS GOOD. REF FUEL BITE.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 71,209 hrs · 11,550 cycles

CABIN FLOORBEAM FWD FACE VERTICAL STIFFENER CRACKED STA 246, RBL 11. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STIFFENER.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 71,209 hrs · 11,550 cycles

FLOORBEAM FWD FACE VERTICAL STIFFENER IS CRACKED STA 246, LBL 9. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE STIFFENER.

Part: SLIDE — UNSECURE (L2 DOOR) · airframe 71,209 hrs · 11,550 cycles

DOOR 2L SLIDE AFT SIDE IS PARTIALLY UNLACED. RELACED & REINSTALLED SLIDE.

Part: SHUTOFF VALVE — MALFUNCTIONED (A/C PACK) · airframe 70,723 hrs · 11,471 cycles

ON TAKEOFF LARGE L DUCT PRESS VARIATIONS. HI CABIN TEMP TO 87. HAD TO TURN OFF L PACK TO REG & GAIN CONTROL OF PRESS AND TEMP. TURNED L PACK BACK ON DUCT PRESS STABLE AND TEMP CONTROLLABLE. REPLACED LEFT PRSOV. RAN ENG TO POWER PER JRH, BLEED SYSTEM CHECKS NORMAL, PRESSURE STABLE, PACK OPERATION NORMAL.

Part: COOLING FAN — MALFUNCTIONED (E&E BAY) · airframe 70,563 hrs · 11,445 cycles

FWD EQ COOLING EX FAN MESSAGE DISPLAYED ON UPPER SCREEN. REPLACED FWD EQUIPMENT COOLING EXHAUST FAN AND ACCOMPLISHED OPERATIONAL CHECK.

Part: TERMINAL — LOOSE (IDG FEEDER CABLE) · airframe 70,537 hrs · 11,438 cycles

ELECTRICAL ISSUES NOTED. ACCOMPLISHED LT GENERATOR FEEDER CABLE & ELECTRICAL HARNESS CHECK. FOUND THE GENERATOR GROUND FEEDER CABLE TERMINAL LUG LOOSE AT THE IDG TERMINAL BLOCK END. CABLE PULLED OUT OF TERMINAL. INSTALLED NEW GROUND TERMINAL. ACCOMPLISHED ENG GRD RUN & GENERATOR CKS, ALL OPS & INDICATIONS NORMAL.

Part: FUEL TANK — LEAKING (RT WING) · airframe 70,522 hrs · 11,434 cycles

HEAVY FUEL SEEP RT WING. LOCATED LEAK INTERNALLY. CLEANED AND SEALED WITH A1-2 AND B1-2 AT 09:30 ON 8-16. SCRAPED AND RESEALED SEAM. NEEDS LEAK CHECK AFTER 12 HR CURE. LEAK CHECK, GOOD.

Part: VALVE — MALFUNCTIONED (E&E BAY) · airframe 70,442 hrs · 11,421 cycles

FWD EQUIP COOLING ISSUE, RTBL. TROUBLESHOT PER FIM 21-58 -00 FIG 105, REPLACED FAULTY INTERCONNECT VALVE NO HELP. TRIED NEW IND CARD M867, NO HELP. ORIGINAL REINSTALLED. FWD EQUIP VALVE AND VALVE LIGHT STILL ON. REPLACED RELAY K1006 AND K340, NO HELP. TROUBLESHOT PER FIM 21-58-00 NEEDS OVERRIDE VALVE. REPLACED OVERRIDE VALVE.

Part: CONTROL VALVE — FAULTY (AC PACK) · airframe 70,314 hrs · 11,399 cycles

RIGHT PACK INOP LIGHT ILLUMINATED. OK IN NORMAL STANDBY. CONTROLLER FAULTS RT RAM AIR ACTUATOR. SYSTEM OPERATES NORMALLY IN STANDBY. RANG WIRES FROM RELAY K49 TO RT RAM DR ACT AND RT PACK CNTLR TO RT RAM DR ACT. CHECKED GOOD. REPLACED PACK TEMP CONTROL VALVE. OPS CHECKED PACK, OPERATION NORMAL.

Part: VALVE — FAILED (RT AC PACK) · airframe 70,242 hrs · 11,384 cycles

RIGHT PACK OFF. REPLACED RIGHT PACK VALVE, OPERATIONAL NORMAL.

Part: EEC — FAULTY (NR 2 ENGINE) · airframe 69,524 hrs · 11,282 cycles

NR 2 ENGINE SILENT SURGE REPORTED. REPLACED EEC.

Part: LATCH — SHEARED (NR 2 ENGINE) · airframe 69,509 hrs · 11,279 cycles

NR 2 ENGINE COWL V BAND LATCH FOUND SHEARED ADJACENT TO TEE BOLT BRACKET. REPLACED INBOARD ENG COWL V BAND LATCH AND ADJUSTED, ALL OK. INSTALLED LOCK FASTENERS. A NEW BAND ASSY HAS TO BE INSTALLED NO LATER THAN C13 DUE 26NOV09.

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 68,690 hrs · 11,162 cycles

RIGHT ENG BLEED LIGHT & RT ENG HPSOV EICAS MSG DURING DESCENT WITH ENG BLEED SW ON & ENGINE RUNNING. REPLACED HPSOV.

Part: ANTI-ICE VALVE — FAULTY (RT ENGINE) · airframe 68,439 hrs · 11,123 cycles

RT ENG ANTI ICE VALVE LIGHT AND EICAS WHEN TURNED OFF, BOTH EXTINGUISH APPROX 45 SECS LATER. REPLACED RIGHT ENGINE ANTI-ICE VALVE. OPS CHECK NORMAL.

Part: ANTI-ICE VALVE — FAULTY (RT ENGINE) · airframe 68,439 hrs · 11,123 cycles

RT ENG ANTI ICE VALVE LIGHT AND EICAS WHEN TURNED OFF, BOTH EXTINGUISH APPROX 45 SECS LATER. REPLACED RIGHT ENGINE ANTI-ICE VALVE. OPS CHECK NORMAL.

Part: CHARGER — FAULTY (APU BATTERY) · airframe 67,657 hrs · 11,014 cycles

APU SHUTS DOWN WITH ELEC OR PNEUMATIC LOAD. REPLACED BATTERY CHARGER AS PER SERVICE TIP. CLEARED APU CONTROLLER OF ALL FAULTS. RAN ENG 3 TIMES TO PUT LOAD ON APU, AT MAX HAD 40 P.S.I. ALSO SERVICED APU OIL.

Part: INDICATOR — FAILED (ATTITUDE) · airframe 67,490 hrs · 10,985 cycles

SAI PROBLEM. RTFL. REPLACED STANDBY ATTITUDE IND AND STATIC INVERTER-ILS PROCESSOR. OPS NORMAL ON GROUND.

Part: IDG — FAULTY (RT ENGINE) · airframe 66,736 hrs · 10,883 cycles

RT ENGINE IDG FILTER DPI EXTENDED. REPLACED IDG. OP CHECK GOOD.

Part: IDG — UNDERSERVICED (RT ENGINE) · airframe 66,736 hrs · 10,883 cycles

RIGHT ENGINE IDG FILTER DPI EXTENDED. UNIT UNDERSERVICED. REPLACED IDG. OP CHECKS NORMAL.

Part: OIL FILTER — FAULTY (NR 2 ENGINE) · airframe 66,392 hrs · 10,833 cycles

R OIL FILTER BYPASS LIGHT ON FOR 1 MIN AFTER START. R OIL FILTER STATUS MSG REMAINS ON. REPLACED MAIN OIL FILTER. LEAK CHECKS OK.

Part: CONNECTOR — BROKEN (SATCOM) · airframe 65,690 hrs · 10,724 cycles

SATCOM UNAVAILABLE FOR ENTIRE FLIGHT. FOUND FAULTY CONNECTOR AT HIGH POWER RELAY, SHIELD BROKEN. REPLACED CONNECTOR, OP CHECKED GOOD. AC OK FOR SERVICE.

Part: VALVE — STICKING (BLEED SYSTEM) · airframe 65,690 hrs · 10,724 cycles

RIGHT ENG OVERHEAT LIGHT & RT ENG BLD OVERHEAT EICAS MSG DURING CRUISE & ENG OR WING ANTI-ICE SW OFF. *S/D* FOUND HIGH PRESSURE SHUT OFF VALVE STICKING. REPLACED HPSOV IAW MM36-11-07 AS A PRECAUTIONARY, CHANGED CONTROLLER IAW MM36-11-08, OP CHECK GOOD. AC OK FOR SERVICE.

Part: IDG — FAULTY (NR 2 ENGINE) · airframe 65,378 hrs · 10,676 cycles

RT GEN DRIVE LIGHT AND EICAS ILLUM. DISCONNECTED RT GEN PER IRREG, APU ON LINE. REPLACED RIGHT ENG. IDG IAW MM24-11-01 OP CHECKED GOOD, AC OK FOR SERVICE.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 65,357 hrs · 10,672 cycles

EMERGENCY PATH LIGHTS & WINDOW 'EXIT' LIGHTS FLASHING ON-OFF DURING FLIGHT. *S/D* SUSPECT BATTERY. REPLACED BATTERY PACK. AC OK FOR SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 65,216 hrs · 10,642 cycles

FWD LT OVERHEAD EXIT SIGN IS INOP. SUSPECT POWER SUPPLY. REPLACED POWER SUPPLY PER MM 33-51-07. AC OK FOR SERVICE.

Part: FRAME — DAMAGED (BS 1219 S37-38L) · airframe 65,216 hrs · 10,642 cycles

FRAME WEB AT STA 1219 BETWEEN STR 37 TO 38L HAS AN ELONGATED FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED, CUTOUT DAMAGE. INSTALLED NEW SHEARTIE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,216 hrs · 10,642 cycles

LEFT MID LAV EEL LIGHT BAR IS INOP. SUSPECT BROKEN LIGHT ASSEMBLY. REPAIRED LT MID LAV EEL LIGHT BAR IAW GNMM 2-0-15-005 OPS CHECKED GOOD IAW MM 33-51-00. AC OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,216 hrs · 10,642 cycles

RIGHT AFT LAV EEL LIGHT BAR IS INOP. SUSPECT BROKEN LIGHT ASSEMBLY. REPAIRED RT AFT LAV EEL LIGHT BAR IAW GNMM 20-51-005 AND OPS CHECKED GOOD IAW MM 33-51-10. AC OK FOR SERVICE.

Part: BATTERY PACK — MISSING (CABIN) · airframe 65,216 hrs · 10,642 cycles

EMERGENCY POWER SUPPLY MISSING (M1209) FOR RT FWD WING EXIT DOOR (VERTICALLY MOUNTED). SUSPECT BATTERY PACK IMPROPERLY INSTALLED. REPLACED BATTERY PACK PER MM 33-51-07. OPS CHECKS GOOD. AC OK FOR SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 65,216 hrs · 10,642 cycles

RIGHT AFT OVERWING EXTERIOR EMERGENCY LIGHT IS INOP. SUSPECT POWER SUPPLY. REPLACED POWER SUPPLY. OPS CHECKS GOOD, AC OK FOR SERVICE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,216 hrs · 10,642 cycles

CORROSION ON SHEARTIE AT STA 1219, STR 37L TO 38L. MAJOR REPAIR ACCOMPLISHED: REPLACED SHEAR TIE.

Part: TORQUE TUBE — CORRODED (FUSELAGE) · airframe 65,216 hrs · 10,642 cycles

CORROSION ON TORQUE TUBE BETWEEN STA 1263 AND STA 1285 AND STA 1285 AT LBL 6 TO RBL 16 IN AFT PIT. MAJOR REPAIR ACCOMPLISHED: REPLACED WEB.

Part: RUDDER — DAMAGED · airframe 65,216 hrs · 10,642 cycles

RUDDER DAMAGED ON TRAILING EDGE BY MANLIFT OPERATION, APPROX .25 INCH DEEP BY 6 INCH LONG. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA. INSTALLED LAY-UP REPAIR.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,216 hrs · 10,642 cycles

CORROSION ON SHEAR TIE IN BILGE AT STA 1197.66, BETWEEN STR 39L AND 39R. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW SHEAR TIE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,216 hrs · 10,642 cycles

CORROSION ON SHEAR TIE AT BS 1197+132, BETWEEN STR 38L-39L. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW SHEAR TIE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,216 hrs · 10,642 cycles

CORROSION ON SHEAR TIE AT BS 1197+132, BETWEEN STR 38R-39R. MAJOR REPAIR ACCOMPLISHED: REPLACED SHEAR TIE.

Part: SPRING — DEFECTIVE (R2 DOOR) · airframe 65,216 hrs · 10,642 cycles

R2 DOOR FWD DEPLOYMENT CABLE RETRACTOR STICKS, CABLE DOES NOT RETRACT. REPLACED GAS SPRING. OP CHECKS GOOD.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,216 hrs · 10,642 cycles

CORROSION ON SHEAR TIE AT STA 1241, STR 38 TO 39L. MAJOR REPAIR ACCOMPLISHED: REPLACED SHEAR TIE.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,216 hrs · 10,642 cycles

CORROSION ON SHEAR TIE AT STA 1241, STR 38R TO 39R. MAJOR REPAIR ACCOMPLISHED: REPLACED SHEAR TIE.

Part: SPRING — FAULTY (L1 DOOR) · airframe 65,216 hrs · 10,642 cycles

DEPLOYMENT BAR SNUBBER DOES NOT RETRACT BAR ON L1 DOOR. SUPPLEMENTAL DATA UPDATE, REPLACED GAS SPRING. OPS CHECKS GOOD.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,216 hrs · 10,642 cycles

CORROSION ON SHEAR TIE AT BS 1197+132, BETWEEN STR 39R-39L. MAJOR REPAIR ACCOMPLISHED: REPLACED SHEAR TIE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 65,216 hrs · 10,642 cycles

CORROSION UNDER NUTPLATE ON THE UNDERSIDE OF THE BILGE FRAME T-CAP AT BS 1197+132, LBL 18. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION. INSTALLED STRAP & ANGLE REPAIR.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 65,216 hrs · 10,642 cycles

CORROSION ON SHEAR TIE STA 1241, STR 39L TO 39R. MAJOR REPAIR ACCOMPLISHED: REPLACED SHEAR TIE.

Part: SPAR — CRACKED (NR 2 PYLON) · airframe 65,216 hrs · 10,642 cycles

NR 2 PYLON UPPER SPAR WEB IS CRACKED AT OTBD DRAIN HOLE, NAC STA 156. MAJOR REPAIR ACCOMPLISHED, ACCOMPLISHED HFEC AND FOUND 2 CRACKS APPROX .5 INCH LONG. STOP DRILLED CRACKS. FABRICATED AND INSTALLED A REPAIR DOUBLER.

Part: SEAT TRACK — CORRODED (BS 784-800) · airframe 65,216 hrs · 10,642 cycles

MAIN CABIN SEAT TRACK AT STA 784 TO STA 800, LBL 60 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED, CUT OUT DAMAGED SECTION OF SEAT TRACK. INSTALLED NEW SECTION.

Part: FLOORBEAM — CORRODED (BS 303) · airframe 65,216 hrs · 10,642 cycles

CABIN FLOORBEAM UPPER SURFACE CORRODED, BS 303, RBL 54. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF "T" CAP. INSTALLED "T" CAP AND ANGLE REPAIR.

Part: HOUSING — CRACKED (EVAC SLIDE) · airframe 65,216 hrs · 10,642 cycles

RIGHT EMERGENCY EXIT SLIDE DISCONNECT HOUSING IS BROKEN (CRACKED). FOUND DISCONNECT HOUSING CRACKED. REPLACED DISCONNECT HOUSING IAW MM 25-65-98 FREEDOM OF MOVEMENT CHECK GOOD IAW MM 25-65-04.AC OK FOR SERVICE.

Part: SUPPORT BRACKET — CRACKED (NLG TUNNEL) · airframe 65,216 hrs · 10,642 cycles

RT SIDE NLG TUNNEL AREA BS 246 FLOORBEAM HAS PULLEY SUPPORT BRACKET CRACKED AT RBL 15. REMOVED BRACKET AND INSTALLED NEW BRACKET.

Part: SUPPORT BRACKET — CRACKED (NLG TUNNEL) · airframe 65,216 hrs · 10,642 cycles

RT SIDE NLG TUNNEL AREA BS 246 FLOORBEAM SUPPORT BRACKET CRACKED RBL 26. REMOVED AND REPLACED BRACKET.

Part: CABLE — FRAYED (EMERGENCY EXIT) · airframe 65,216 hrs · 10,642 cycles

RT AFT EMERGENCY EXIT HATCH STEP FWD CABLE IS FRAYED. REPLACED CABLE IAW SRM 51- 40-02 AND OPS CHECKED GOOD IAW MM52-21-01.AC OK FOR SERVICE.

Part: LATCH — FAULTY (ESCAPE SLIDE) · airframe 65,216 hrs · 10,642 cycles

RT OVERWING EMERGENCY SLIDE NR 1 LATCH IS HARD TO OPERATE. SUSPECT FAULTY BEARING. REPLACED NR 1 HATCH AT RT OVERWING SLIDE COMPT DOOR PER MM 25-65-09 ALIGNMENT CHECK GOOD IAW MM 25- 65-09.AC OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 64,805 hrs · 10,582 cycles

ALL FOUR INTERIOR OVERWING EMERGENCY EXIT SIGNS INOP. REPLACED BATTERY PACK. OPS CHK'D OK.

Part: ASPIRATOR — UNSERVICEABLE (EVAC SLIDE)

ASPIRATOR LEAKING.

Part: SKIN — CRACKED (L/E SLAT) · airframe 63,412 hrs · 10,376 cycles

NR 8 SLAT LOWER SKIN CRACKED.

Part: AILERON — DAMAGED (RT WING) · airframe 63,147 hrs · 10,332 cycles

RETURN TO GATE DUE TO WING TO WING CONTACT. SUPPLEMENTAL DATA UPDATE RIGHT OUTBOARD AILERON DAMAGED DUE TO RT WING CONTACT WITH LT WING OF 6672.

Part: STARTER — MALFUNCTIONED (NR 2 ENGINE) · airframe 62,974 hrs · 10,304 cycles

NR 2 ENGINE STARTER BLEW DURING START. DAMAGED REVERSER & FAN COWL. 11-01-07 REPLACING STARTER & STARTER VALVE. OP CHECK OF STARTER INDICATES BOTH ARE GOOD FOR SERVICE. SUSPECT BEARING DETERIORATION & RELEASE OF ROTOR CAUSING RESULTANT IMBALANCE AND DISINTEGRATION.

Part: FIRE LOOP — FAULTY (NR 1 NACELLE) · airframe 62,882 hrs · 10,286 cycles

EICAS MSG "ENG 1 FIRE LP2" DISPLAYED AT SHUTDOWN.

Part: FEEDER CABLE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,372 hrs · 10,198 cycles

FLOOR MOUNTED EEL LIGHTS INOP, RT AISLE IN FIRST CLASS. REPLACED POWER STRIP IN FLOOR TRACK.

Part: SLIDE — OUT OF LIMITS (L1 DOOR) · airframe 60,908 hrs · 9,951 cycles

DOOR 1L SLIDE IS OUT OF LIMITS. [SUP 05-18-07] SLIDE SHOULD READ NO LESS THAN 2975 AT 70 DFG, IT IS CURRENTLY READING 2500. REPLACED SLIDE. A/C RETURNED TO SERVICE. SLIDE PROBLEM ROOT CAUSE: SUSPECT SEAL DETERIORATION AT FILL VALVE PRESSURE HOSE CONNECTION.

Part: SLIDE — WRONG PART (DOOR 1R) · airframe 60,852 hrs · 9,941 cycles

DOOR 1R SLIDE IS THE WRONG PART. [SUP 05-18-07] REPLACED DOOR 1R SLIDE ASSY PER AMM 25-66-01 WITH THE CORRECT SLIDE P/N. NEW SLIDE INSTALLED IS MR25708 (649-9059).

Part: FEEDER CABLE — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,079 hrs · 9,806 cycles

FOUND EMERGENCY EEL LIGHTS INOP FROM SEATS 15AB TO 27AB. REPLACED SEVERAL EEL STRIPS & CONNECTION CABLE. OPS CK OK.

Part: PROXIMITY SWITCH — FAILED (PSEU) · airframe 59,514 hrs · 9,712 cycles

TAKEOFF CONFIGURATION WARNING WITH EICAS -FLAPS- & -NOSE A-G DISAGREE- DISPLAYED. REPLACED PROXIMITY SWITCH ELECTRONICS UNIT. OP CHECKED OK.

Part: FLAP — MALFUNCTIONED (WING)

RETURNED TO THE FIELD DUE TO A FLAP CONTROL PROBLEM. AFTER TROUBLESHOOTING, DETERMINED A/C HAD LANDING GEAR MONITORING AIR-GROUND DISAGREE. REPLACED PROXIMITY SWITCH ELECTRONIC UNIT. ALL SYSTEMS CHEKED OK FOR SERVICE.

Part: PSEU — FAULTY (E/E BAY) · airframe 59,355 hrs · 9,680 cycles

RTFL FOR LANDING GEAR MONITOR MESSAGE AND MULTIPLE CONFIGURATION WARNINGS. AIRCRAFT NEEDS NEW PROXIMITY SWITCH ELECTRONICS UNIT BOX. REPLACED PSEU & AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (SEAT 10F) · airframe 59,106 hrs · 9,635 cycles

FOUR SEGMENTS OF FLOOR MOUNTED EMERGENCY STRIP LIGHTS ARE INOPERATIVE. THE FOUR SEGMENTS ARE LOCATED NEXT TO SEAT 10F, NEXT TO THE LAVATORY BETWEEN SEATS 10F AND 15F, NEXT TO THE LAVATORY BETWEEN SEATS 14B AND 15B, AND THE FIRST STRIP LIGHT AFT OF DOOR 1R.

Part: LIGHT — INOPERATIVE (SEATS 5AB, 5EF &) · airframe 59,106 hrs · 9,635 cycles

SEATS 5AB, 5EF, AND 7EF EEL LIGHT BARS WILL NOT ILLUMINATE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 59,106 hrs · 9,635 cycles

THE AFT LONG EEL LIGHT BAR IS INOPERATIVE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 59,106 hrs · 9,635 cycles

EEL LIGHT STRIP IN FRONT OF THE AFT RIGHT HAND LAV IS INOPERATIVE.

Part: ASPIRATOR — UNSERVICEABLE (SLIDE) · airframe 58,935 hrs · 9,606 cycles

DAMAGED SLIDE ASPIRATOR. REPLACED SLIDE. OK FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,730 hrs · 9,421 cycles

AFT LAV TANK EXHAUST VENT OUTLET SKIN HAS CORROSION DAMAGE. REMOVED ALL DAMAGE AND FABRICATED A REPAIR DOUBLER-FILLER AND INSTALLED.

Part: LATCH — FAILED (CABIN)

LT O/W SLIDE COMPT DOOR DISCONNECT HOUSING HAS FAIL CHECK. REMOVE AND REPLACE REF: UALB767 MM 25-65-98.

Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR) · airframe 52,726 hrs · 8,584 cycles

AFT CARGO DOOR EICAS MESSAGE. TRIED 4 TIMES, UNABLE TO DUPLICATE FAULT ON GROUND.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 50,860 hrs · 8,271 cycles

RETURNED TO BLOCKS TWICE DUE TO FLAP INDICATIONS.

Part: WINDOW — VIBRATES (COCKPIT) · airframe 50,515 hrs · 8,212 cycles

RETURNED TO FIELD WITH A COCKPIT WINDOW VIBRATION. THE VIBRATION WAS CAUSED BY A LOOSE TAPE THAT WAS APPLIED ON WINDOW 3L TO PROTECT UNCURED (SOFT) SEALANT. THE SEALANT WAS APPLIED WHEN THE EXISTING NR 3L WINDOW WAS REPLACED,

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 54,439 hrs · 8,870 cycles

FLIGHT ABORTED TAKEOFF DUE TO A COMPRESSOR STALL IN THE NR 1 ENGINE. ABORTED TAKEOFF AT 100 KIAS DUE TO COMPRESSOR SURGE. ENGINE REPLACED AT EZE. UA TURBINE SHOP FINDINGS: N2 WILL NOT ROTATE. ALSO, BORESCOPE INSPECTION REVEALED HEAVY HPC 5TH STAGE BLADE DAMAGE. ENGINE RETURNED TO LESSOR ON 06/06/05 WITHOUT BEING DISASSEMBLED.

Part: BOLT — MISSING (NR 2 BRAKE) · airframe 48,966 hrs · 7,958 cycles

RETURN TO FIELD DUE TO GEAR DISAGREEMENT EICAS MESSAGE. DAMAGE INCURRED FROM HANGING BRAKE ROD AFTER SEPARATION FROM BRAKE. ROD BELIEVED TO HAVE DETACHED FROM TORQUE ARM DUE TO MIGRATION OF BRAKE TORQUE ARM PIN. SAFETY BOLT BELIEVED TO HAVE COME LOOSE OR POSSIBLY NOT INSTALLED RESULTING IN KEEPER PIN DETACHMENT AND SUBSEQUENT PIN MIGRATION. BRAKE PIN AND KEEPER ASSEMBLY WERE FOUND AND REFLECTED NO DAMAGE INDICATIVE OF MATERIAL FAILURE.

Part: WIRE — WORN (EMERGENCY LIGHT) · airframe 48,683 hrs · 7,909 cycles

EMERGENCY EXIT LIGHTS - FLOOR STRIPS ON. ALSO FLASHING ON AND OFF. FOUND SEVERAL LOCATIONS WHERE STRIP WAS TORN AND PINS PUSHED IN. REPAIRED WITH SPLICE TOOL. OPS CK NORMAL.

Part: HINGE FITTING — CRACKED (T/E FLAP) · airframe 48,566 hrs · 7,891 cycles

RIGHT WING INBOARD FLAP AT CENTER HINGE FITTING IS CRACKED BROKEN. MAJOR REPAIR ACCOMPLISHED. REPAIRED FITTING PER SRM 51-40-2 AND 57-53-02, FIG 201.

Part: COMPRESSOR — STALLED (NR 2 ENGINE)

CANCELLED DUE TO NR 2 ENGINE COMPRESSOR STALL AT FL210. ENGINE SURGED ABOVE 1.25 EPR AND WAS REMOVED. SURGE CHECKS SHOWED NO IRREGULARITIES AND ENGINE PASSED TEST-21. PILOT REPORT STATED THAT AIRCRAFT HAD WAKE TURBULENCE DURING CLIMB.

Part: LIGHT — BURNED OUT (NAVIGATION PANEL) · airframe 46,163 hrs · 7,447 cycles

BOTH RED NAV LIGHTS ON LEFT WING ARE OUT. CLEANED CONNECTOR, REPLACED BOTH NAV LIGHTS.

Part: SENSOR — OUT OF TOLERANCE (OVERWING DOOR) · airframe 43,651 hrs · 7,036 cycles

LEFT HAND OVER WING SLIDE DOOR LIGHT FLICKERING IN CONJUNCTION WITH EICAS MESSAGE. ACCOMPLISHED PROXIMITY SENSOR CHECK ON LT OVERWING SLIDE DOOR IAW MM 52-71-00/501. FOUND SENSORS OUT OF TOLERANCE.

Part: CIRCUIT CARD — FAULTY (DOOR WARNING) · airframe 43,552 hrs · 7,015 cycles

FORWARD CARGO DOOR EICAS AND OVERHEAD CAUTION LIGHT ILLUMINATED INTERMITTENTLY. REPLACED PROXIMITY SENSOR CARDS

Part: BRACKET — LOOSE (EVAC SLIDE) · airframe 43,340 hrs · 6,972 cycles

'L WING SLIDE' EICAS MESSAGE DISPLAYED INTERMITTENTLY WITH EMERGENCY DOOR OVERHEAD LIGHTS FLICKERING. TARGET ASSY BRACKET FOUND LOOSE IN OFF WING SLIDE COMPARTMENT. SECURED BRACKET.

Part: CIRCUIT CARD — FAULTY (WARNING SYSTEM) · airframe 43,609 hrs · 7,026 cycles

FORWARD CARGO DOOR EICAS MESSAGE AND OVERHEAD CAUTION LIGHT ILLUMINATED INTERMITTENTLY. REPLACED PROXIMITY SENSOR CARDS

Part: VALVE — FAILED (E/E BAY) · airframe 42,457 hrs · 6,803 cycles

EQUIPMENT FAILURE ASSOCIATED WITH EQUIPMENT COOLING PROBLEM. INTERMITTENT HSI/ADI/TCAS/WX RADAR OCCURRED RIGHT AFTER TAKEOFF. SYSTEMS SOMEWHAT RESTORED ONCE FAN SELECTED TO OVERRIDE. REF INBD LOG1 FOR LOSS OF VARIOUS CRT'S W SOME A-P PROBLEMS. AS PER LCL DIRECTIVE, EQUIP CLG OVERBOARD EXH VLV TO BE REPLACED. REF MM21-58-05-401 ACPD TO STEP 12. UNABLE TO REMOVE VLV DUE TO EXCESSIVE SEALANT. SPOILERS ARE NOT DEACTIVATED. CONT OF AMIS ITEM 4576002: FINISHED INSTALLATION AS REQUIRED PER MM 21-58-05.

Part: STRINGER — PUNCTURED (FUSELAGE) · airframe 42,371 hrs · 6,786 cycles

STATION 358 STRINGER 3 RT IS PUNCTURED, LIGHTNING STRIKE DAMAGE. MAJOR REPAIR ACCOMPLISHED. STRINGER REPAIRED.

Part: SKIN — CHAFED (FUSELAGE) · airframe 42,371 hrs · 6,786 cycles

BODY STATION 1809.5 LT EXT FUSE SKIN HAS EXCESSIVE CHAFFING. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR DOUBLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,371 hrs · 6,786 cycles

BODY STATION 852 LBL 55 T-CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,371 hrs · 6,786 cycles

BODY STATION 1219 LBL 30 T-CAP CORRODED UNDER NUT PLATES. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED T-CAP.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 42,371 hrs · 6,786 cycles

BODY STATION 348 STRINGER 20R RBL 84 TOP OF FLOORBEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM SECTION AND SPLICES.

Part: SKIN — CHAFED · airframe 42,371 hrs · 6,786 cycles

BODY STATION 1809.5 RT EXTERNAL FUSELAGE SKIN HAS EXCESSIVE CHAFING WEAR. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLEDREPAIR DOUBLER.

Part: FUEL TANK — IMBALANCED (RIGHT) · airframe 38,867 hrs · 6,186 cycles

RT TANK INDICATION IS ROLLING BACK, AFTER APPROX 1 HOUR, 2500 LBS LOWER THAN LEFT TANK. CREW REPORTS PROGRESS PAGE MATCHES TOTALIZER AND IMBALANCE REMAINED FOR ENTIRE FLIGHT. CAPT TRIED BALANCING BY FEEDING BOTH ENGS WITH LT TANK.

Part: PUMP — MALFUNCTIONED (CENTER TANK) · airframe 35,427 hrs

WITH 1.1 FUEL IN CENTER TANK, WING GAUGES DISAGREE BY 2000 LBS. AFTER CENTER TANK EMPTY, 2000 LBS IMBALANCE REMAINED. FUEL USED SHOWED .3 DIFF, A-C REMAINED IN TRIM. X-FEED FUEL LEFT TO RIGHT WITH A-P DISCONNECTED A-C ROLLED TO RIGHT. *S/D* IMBALANCE WAS RESULT OF LOW OUTPUT FROM RIGHT OVERRIDE PUMP. PUMP WAS DIFFUSERLESS TYPE IN OVERRIDE POSITION. DIFFUSER TYPE PUMP INSTALLED AND OPERATION CHECK GOOD.

Part: BEARING — FAILED (MLG WHEEL) · airframe 34,598 hrs · 5,433 cycles

ACFT RETURNED TO BLKS WITH DRAGGING BRAKES. FOUND 2R TIRE ASSY WITH FAILED INNER BEARING. REPLACED 2R BRAKE ASSY, REPLACED 2R TIRE ASSY. REPLACED 1R TIRE ASSY. REPLACED AXLE ASSEMBLY. ACCOMPLISHED WHEEL BEARING FAILURE INSPECTION PER MM. *S/D* ACFT HAD 2R TIRE CHANGE AT IAD. WHEEL SPACER WAS LEFT OUT CAUSING WHEEL TO DRAG ON BRAKE AND INNER BEARING TO WOBBLE, OVERHEATING THE AXLE.

Part: SENSOR — OUT OF ADJ (CARGO DOOR) · airframe 32,828 hrs · 5,118 cycles

RTO DUE AFT CARGO DOOR LIGHT ON. *S/D* PERFORMED TROUBLESHOOTING TO DETERMINE THAT THE AFT CARGO LOCK PROXIMITY SENSOR SHOWED TARGET FAR WHEN DOOR WAS CLOSED. ADJUSTED TARGET IN ACCORDANCE WITH AMM 52-35-43. OPS CHECKED NORMAL. AIRCRAFT HAS HAD NO ADDITIONAL HITS SINCE THIS ACTION WAS ACCOMPLISHED.

Part: OVEN — FIRE (GALLEY) · airframe 32,328 hrs · 5,030 cycles

OVEN FIRE IN FLIGHT. DISCHARGED HALON EXTINGUISHER. *S/D* PAPER DEBRIS ON OVEN INSERT CAUSED SMALL FLAME-UP IN FLT. THE FIRE WAS EXTINGUISHED BY CREW USING HALON EXTINGUISHER. CHECKED OVEN AND GALLEY SURROUNDING AREA FOR DAMAGED, NO DAMAGE FOUND. CLEANED OVEN AND FAN SCREEN. RAN OVEN AT VARIOUS TIME SETTING, NO DISCREPANCY FOUND.

Part: PANEL — MALFUNCTIONED (COCKPIT) · airframe 32,234 hrs · 5,017 cycles

OVERHEAD INDICATION PANEL: ENTRY, EMER DOORS, CARGO DOORS, AND ACCESS DOORS ILLUMINATE WITH ASSOCIATED DOORS CLOSED. NO EICAS MESSAGES. STARTING LEFT ENG EXTINGUISHES INDICATOR LIGHTS. UPON ENG SHUT DOWN, ALL ABNORMALITIES RESUME. *S/D* TEST OF THE OVERHEAD INDICATION PANEL FOUND A FAULT IN THE F/O PITOT ANN CAPSULE. REPLACED F/O PITOT ANN CAPSULE. DEFECT HAS NOT BEEN NOTED SINCE REPLACEMENT WAS MADE.

Part: CARD — FAILED (LT EMER EXIT DR)

LEFT FORWARD EMERGENCY DOOR EICAS MESSAGE ILLUMINATED IN FLIGHT. *S/D* ACCOMPLISHED CHECK OF FWD LEFT EMERGENCY DOOR PER MM 52-21-01 AND MM 52-71-00. REPLACED M7 CARD AT PSEU PER MM 32-09-06. OPS CHECKS NORMAL.

Part: SENSOR — OUT OF ADJUST (EMER EXIT SLIDE)

RIGHT WING SLIDE EICAS MESSAGE DISPLAYED INTERMITTENTLY AT CRUISE. *S/D* CHECKED S199 AND S219 PROXIMITY SENSORS FOR TARGET CLEARANCES, FOUND S219 HAD EXCESSIVE GAP. SHIMMED SENSOR PER MM. REAMED SYSTEM PER MM, ALL INDICATIONS NORMAL.

Part: CONTROL ROD — OUT OF ADJUST (LT EMER EXIT)

EMERGENCY DOOR LIGHT ILLUMINATES INTERMITTENTLY AND EICAS MESSAGE LEFT WING SLIDE ILLUMINATES. *S/D* DOOR LATCH LINKAGE WAS FOUND OUT OF RIG. PERFORMED ADJUSTMENT PER MM. NO EICAS MESSAGE DISPLAYED AFTER RETURNING OVERWING SLIDE SYSTEM TO NORMAL.

Part: SENSOR — MALFUNCTIONED (EMER EXIT DOOR)

RIGHT WING SLIDE EICAS MSG DISPLAYED. ALSO, EMERGENCY DOOR LIGHT ILLUMINATED. DIVERTED TO BOS. *S/D* ACCOMPLISHED BITE CHECK OF PSEU AND FOUND SENSOR S199 FAULTED. REPLACED S199 PER MM5 AND ADJUSTED SENSOR PER MM, OPS CHECKS NORMAL.

Part: CONNECTOR — LOOSE (CABIN)

EEL FLOOR PATH LIGHTS ARE INOP ON RIGHT HAND SIDE FROM DOOR 1 RIGHT TO SEAT 6E. PROBLEM ORIGINATES AT CONNECTOR AT SEAT 1E. REPLACED EEL FEEDER STRIP FROM WALL AT 1 E AND F.

Part: EICAS MESSAGE — MALFUNCTIONED (COCKPIT)

LEFT WING SLIDE EICAS MESSAGE CAME ON INTERMITTENTLY ON TAXI OUT. *S/D* ACCOMPLISHED LT OFF-WING ESCAPE SYSTEM CHECK OF ADJUSTMENT OF SLIDE COMPARTMENT DOOR PROXIMITY SENSOR. THE SENSOR WAS FOUND WITHIN LIMITS. ACCOMPLISHED CHECK OF DOOR ADJUSTMENT AND DOOR LOCK SENSOR S198. ALL WAS FOUND WITHIN LIMITS. ACCOMPLISHED BITE OF PROXIMITY SENSOR BOX. NO DEFECTS NOTED. CAUSE UNKNOWN. RETURNED AIRCRAFT BACK TO NORMAL. AIRCRAFT TAXIED WITH NO MESSAGES.

Part: FIRE PANEL — MALFUNCTIONED (CABIN)

LEFT ENGINE OVERHEAT/FIRE TEST PANEL GAVE INDICATION INTERMITTENTLY. *S/D* FAULTY FIRE/OVERHEAT TEST PANEL GAVE INTERMITTENT INDICATON. REPLACED PANEL AND SYSTEM OPERATIONAL CHECKED NORMAL. PART IS NON-STOCK/NOT RECOVERABLE AND SPECIFIC COMPONENT FAILURE UNKNOWN.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT THRESHOLD LIGHT BY DOOR 2L AND 2R WILL NOT GO OUT. *S/D* REPLACED BATTERY PACK UNDER FLIGHT ATTENDANT JUMP SEAT AT SEAT 2R AND RECYCLED SYSTEM, OPS CHECK OK.

Part: SEAL — STICKING (APU FUEL CONTL)

FOUND FUEL IN APU OIL SYSTEM AND REPLACED APU PRECAUTIONARY. FUEL CONTROL WAS DISASSEMBLED AND CARBON SEAL ON THE SIDE OF THE FUEL CONTROL SHAFT SEAL WAS FOUND STICKING. SEAL WAS REPLACED.