N598UA

Part: OVEN — SMOKE (AFT GALLEY) · airframe 77,063 hrs · 19,779 cycles

SMOKE AND FUMES COMING FROM AFT GALLEY OVENS DURING CLIMBOUT. AF T LAV SMOKE ALARMS BEGAN FLT ATT VERIFIED SMOKE SOURCE WAS OVEN 411. MEAL CONTAINED IN PLASTIC TOUCHING UPPER METAL PORTION OF MEAL CARIER. CONTROLLERS REPLACEMENTS ARE REQUIRED. REMOVED DIRTY OVEN INSERT AND MEALS FROM OVEN AND ADVISED PERFORMED TASK 05-51-56-202-001 SMOKE OR FUMES CABIN CONDITIONAL INSPECTION. NO RESIDUAL SMELL IN CABIN OR PACKS.

Part: SLIDE — UNSERVICEABLE (R1 DOOR) · airframe 75,964 hrs · 19,567 cycles

CATERER OPENED DOOR R1 FROM OUTSIDE AND DOOR ESCAPE SLIDE DETACHED FROM DOOR. DOOR ASSIST BOTTLE IS BLOWN FOR DOOR R1. SLIDE DID NOT DEPLOY. GIRT BAR STAYED ATTACHED TO FLOOR FITTINGS. FOUND DOOR IN DISARMED POSITION UPON INSPECTION. REMOVED SLIDE FROM DOOR R1 IAW AMM 25-66-01. SHOULD READ, DOOR WAS FOUND IN ARMED POSITION WHEN ARRIVED AT CATERING TRUCK. DOOR ASSIST BOTTLE CHANGE MOVED TO LP 3757576 REMOVED AND REPLACED SLIDE ASSY IAW AMM 25-66-01. ADD EMP:U303650 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1012349 SN OFF 1023 SLIDE, OFF 19-2566-9-0002 1023 ON 19-2566-9-0002 1142 PERFORMED RII INSPECTION REQD FOR R1 DOOR SLIDE CHANGE. NEW PART VERIFIED BY IPC. OK TO CONTINUE.

Part: CAP — LEAKING (FUEL PORT) · airframe 73,426 hrs · 19,085 cycles

A REPORT OF FUEL LEAK FROM LEFT OVERWING REFULING CAP DURING FLI GHT BY CREW...REF IPC 28-11-04-02,ITEM 10...TOMC MO REMOVED LEFT OVERWING FILL PORT PER AMM 28-11-04. NEW FILL PORT NEEDS TO BE INSTALLED. INSTALLED LT MAIN FUEL TANK OVER WING FUELING PORT REF MM 28-11- 04. SEE LOG PAGES 8172134, 8168347,8168341, 8168338 FOR TANK ENT RY WORK & IDT INSPECTIONS. ADD EMP:U068662 ACCOMPLISHED ALL CDCCL ITEMS ASSOCIATED WITH INSTALLATON OF LEFT FUEL TANL OVERWING FUELING PORT. REF AMM 28-11-04.

Part: FLOOR SUPPORT — CORRODED (BS 1343-1445) · airframe 71,203 hrs · 18,658 cycles

AFT CARGO FLOOR SUPPORT RBL 10.45 BETWEEN BS 1343.5 - 1445.6 CORRODED ON MULTIPLE AREAS BOTH UPPER AND LOWER SURFACES. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, PG & DWG 146N5390.

Part: FLOOR SUPPORT — CORRODED (BS 1343.5-1445.6) · airframe 71,203 hrs · 18,658 cycles

AFT CARGO FLOOR SUPPORT, RBL 16.1 BETWEEN BS 1343.5 AND 1445.6, CORRODED AT MULTIPLE AREAS, ON BOTH UPPER AND LOWER SURFACES, REMOVED THE CORROSION IAW SRM 51-10-02, AND SRM 53-60-53.FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, AD 1, DETAIL 5. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG 146N5390.

Part: FLOOR SUPPORT — CORRODED (BS 1440-1460) · airframe 71,203 hrs · 18,658 cycles

AFT CARGO FLOOR SUPPORT BETWEEN BS 1440 - 1460, RBL 24 HAS CORROSION. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, PG 39, AND DWG 146N5390.

Part: FLOOR SUPPORT — CORRODED (BS 634-705) · airframe 71,203 hrs · 18,658 cycles

)FWD CARGO FLOOR SUPPORT, BS 634 - 705, RBL 7.55, CORRODED AROUND NUTPLATES. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-53, REPAIR 1, FIG 201.

Part: FLOOR SUPPORT — CORRODED (BS 1200-1343.5) · airframe 71,203 hrs · 18,658 cycles

AFT CARGO FLOOR SUPPORT RBL 10.45 BETWEEN BS 1200 AND 1343.5 CORRODED AT MULTIPLE AREAS. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-53, REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (BS 634-705) · airframe 71,197 hrs · 18,657 cycles

FWD CARGO FLOOR SUPPORT AT BS 634 TO 705, RBL 10.45 HAS CORROSION AROUND NUTPLATES. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, FIG 101, DETAIL IV, ALLOWABLE DAMAGE 1. REMOVED AND REPLACED THE FLOOR SUPPORT SECTION IAW DWG 143N5320.

Part: FLOOR SUPPORT — CORRODED (BS 634-750) · airframe 71,203 hrs · 18,658 cycles

FWD CARGO FLOOR SUPPORT, BS 634 - 750, LBL 2.9, HAS CORROSION AROUND NUTPLATES. BLENDED AND FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53, FIG 101, DETAIL V, ALLOWABLE DAMAGE 1. REPAIRED IAW SRM 53-00-53, FIG 201, REPAIR 1.

Part: FLOORBEAM — CORRODED (BS 1676) · airframe 71,203 hrs · 18,658 cycles

SURFACE CORROSION ON THE MAIN CABIN FLOORBEAM ANGLE UPPER SURFACE AT BS 1676, LBL 53 - 04. BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, DETAIL III, ALLOWABLE DAMAGE 1. REMOVED AND REPLACED, THE FLOORBEAM ANGLE IAW DRAWING 146N5246.

Part: FLOOR SUPPORT — CORRODED (BS 1200-1343.5) · airframe 71,203 hrs · 18,658 cycles

AFT CARGO FLOOR SUPPORT, RBL 7.55, BS 1200 - 1343.5, CORRODED AT MULTIPLE AREAS ON BOTH UPPER AND LOWER SURFACES. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, PAR 4, PG 2, 3, PAR 7, PG 6 - 7, AND DWG 146N5390.

Part: FLOOR SUPPORT — CORRODED (BS 1497-1520) · airframe 71,203 hrs · 18,658 cycles

BULK CARGO FLOOR SUPPORT LBL 11.40, BS 1497 - 1520 GOUGEED AND CORRODED. REPAIRED IAW SRM 53-00-53, REPAIR 1.

Part: FRAME — DENTED (BS 540) · airframe 71,018 hrs · 18,621 cycles

FWD CARGO LOWER LOBE HAS A DENT ON FRAME AT BS 540, STRINGER 24L ACCOMPLISHED A MAJOR REPAIR IAW S AT-210118-5598-03A, AND ECRA 5310-07353 PART 1.

Part: WIRE — DAMAGED (PROXIMITY SENSOR) · airframe 71,018 hrs · 18,621 cycles

SLIDE LIGHT INOPERATIVE AT THE R4 DOOR. REMOVED AND REPLACED THE GIRT BAR PROXIMITY SENSOR S10224. OPS CHECKED GOOD IAW SWPM 20-30-12, AND AMM 25-66-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 71,018 hrs · 18,621 cycles

AFT CARGO FLOOR SUPPORT STR LBL 10.45 BETWEEN APPROX BS 1200 AN D BS 1343.5 HAS CORROSION ON MULTIPLE AREAS BOTH UPPER ABD LOWER SURFACES, 209-057. REMOVED CORROSION ON AFT CARGO FLOOR STRINGER BETWEEN STA 1200-1 343.5 LBL 10.45 FOUND TO BE OUT OF LIMITS IAW SRM 53-00- 53 FIG 101 DETAIL V ALLOWABLE DAMAGE 1 L=7.00 W=1.00 D=.021. REMOVED AND REPLACED NEW FLOOR STRINGER P/O SAG189017 IAW DWG 146N5390.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 71,018 hrs · 18,621 cycles

FOUND INTERCOSTAL AT STA 720 - 740, STR 24L - 25L WITH ELONGATED HOLES. REMOVED AND REPLACED INTERCOSTAL PART NR 143N5375-7 IN FWD CARGO STA 720-740 BETWEEN STR 24L - 25L IAW DRAWING NR 143N5375.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 71,018 hrs · 18,621 cycles

AFT CARGO FLOOR SUPPORT STR LBL 16.10 BETWEEN APPROX BS 1445 AND BS 1497 HAS CORROSION ON MULTIPLE AREAS BOTH UPPER AND LOWER SURFACES 209-042 REMOVED AND REPLACED AFT CARGO FLOOR SUPPORT LBL 16.10 BET BS 1445 & 1497 IAW SRM 51-40-02 PAR 4 PG 2 & 3 AND PAR 7 PG 6-7 AND DWG NO 146N5390.

Part: FLOOR SUPPORT — CORRODED (BS 634-705) · airframe 71,018 hrs · 18,621 cycles

FWD CARGO FLOOR SUPPORT AT BS 634 TO 705, RBL 16.10 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, FIG 101, DETAIL V. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1497-1520) · airframe 71,018 hrs · 18,621 cycles

BULK CARGO FLOOR SUPPORT RBL 2.90 FROM APPROX BS 1497 AND BS 1520 HAS CORROSION ON MULTIPLE AREAS BOTH UPPER AN D LOWER SURFACES. 209-032 BLENDED MULTIPLE ARESA OF CORROSION AT BULK CARGO FLR SUPPORT RB L 2.90 FROM APROX BS 1497 AND BS 1520. BLEND AREA 3" X 1" X .037 " AT BS 1510 FOUND TO BE OUT OF LIMITS IAW B757-200 SRM 53-00-53 FIG 101 DETAIL V. REPAIRED FLOOR SUPPORT (STRINGER AT BS 1510 I AW B757-200 SRM 53-00-53 PARA 4 FIG 201 DETAIL XII. SEE SUPPLEME NT NO.73809)

Part: FLOOR SUPPORT — CORRODED (BS 1497-1520) · airframe 71,018 hrs · 18,621 cycles

CARGO FLOOR SUPPORT RBL 11.40, BS 1497 AND 1520 CORRODED. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-53, AD 1, DETAIL V. REPAIRED IAW SRM 53-00-53, REPAIR 1.

Part: SHEAR TIE — CRACKED (BS 1300) · airframe 71,018 hrs · 18,621 cycles

SUSPECTED CRACKED SHEAR TIE AFT CARGO STA 1300 JUST ABOVE STRINGER 22 LEFT 20 AND 21 L/H. REMOVED AND REPLACED TIE SHEAR P/N 140N2002-331 BATCH 0002351315 PO NO SOS1870048 AT STA 1300 BETWEEN STR 21L-22L B757-200 SRM 5 1-40-02 PAG2 AND PER DWG 140N2002.

Part: SEAT TRACK — GOUGED (BS 486) · airframe 71,018 hrs · 18,621 cycles

GOUGE ON MAIN CABIN SEAT TRACK CROWN AT STA 486 RBL-25. RG61 BLENDED OUT GOUGE ON SEAT TRACK, FOUND TO BE OUT OF LIMITS IAW 7 57-200 SRM 53-00-52 FIG 101 DETAIL I ALLOWABLE DAMAGE I, COMPLIE D WITH PERMANANT REPAIR IAW 757-200 SRM 53-00-52 REPAIR 3.

Part: SEAT TRACK — GOUGED (BS 450) · airframe 71,018 hrs · 18,621 cycles

GOUGE ON MAIN CABIN SEAT TRACK CROWN AT STA 450 LBL-45. RG60 BLENDED OUT GOUGE ON SEAT TRACK FOUND TO BE OUT OF LIMITS IAW B7 57-200 SRM 53-00-52 FIG 101 DETAIL 1 ALLOWABLE DAMAG 1. COMPLIED WITH PERMANENT REPAIR IAW B757-200 SRM 53-00-53 REPAIR 3, L=1.0" D=0.2.

Part: PAN — GOUGED (R1 DOOR HANDLE) · airframe 71,018 hrs · 18,621 cycles

R1 DOOR, EXTERNAL HANDLE PAN HAS AN APPROX 1.4" LONG GOUGE. (JD116-945) BLENDED OUT GOUGE AREA ON R-1 DOOR EXTERNAL HANDLE PAN (L=2.0", W=0.4", D=.018"). AREA FOUND TO BE OUT OF LIMITS IAW B757-200 SR M 52-10-01 ALLOWABLE DAMAGE 1 FIG 101 DETAIL VI. REMOVED AND REPLACED 1EA HANDLE PAN IAW DWG 141N6200.

Part: FLOOR SUPPORT — CORRODED (BS 1445-1505) · airframe 71,018 hrs · 18,621 cycles

AFT CARGO FLOOR SUPPORT STGR RBL 16.10 BETWEEN APPROX. BS 1445 AND BS 1505 HAS CORROSION ON MULTIPLE AREAS BOTH UPPER AND LOWER SURFACES, 209-039. REMOVED CORROSION ON (4EA) AREAS ON AFT CARGO FLOOR SUPPORT STRI NGER RBL 16.10 STA 1452, 1475, 1480 & 1472 MAT LOSS OF 0.002", A LL BLEND OUT FOUND TO BE WITHIN LIMITS IAW B757 SRM 53-00-53 FIG 101 DETAIL V AND ACCOMPLISHED REPAIRED ON STA 1470 RBL 16.10" I AW B757 SRM 53-00-53 REPAIR 1. SEE SUPPLEMENT NO.75250.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 71,018 hrs · 18,621 cycles

FWD CARGO FLOOR STRINGER AT STA 634 TO STA 705 LBL 10.45 HAS CORROSION AROUND NUTPLATES. REMOVED CORROSION ON FWD CARGO FLOOR STR AROUND NUT PLATES FROM STA 634 TO STA 705 LBL 10.45 FOUND TWO AREAS (AREA 1 L=3.3" X W= .8" MAT REMAINING .027 AND AREA 4 L=3.0" W=.6 MAT REMAINING .027 ) OUT OF LIMITS IAW SRM 53-00-53 FIG 101. REMOVED AND RE PLACED FLOOR STR P/N 143N370-40 PO SAG189017 IAW DWG NO 143N001 0 AND SRM 51-40-02 PAG 2-7.

Part: FLOOR SUPPORT — CORRODED (BS 1497-1520) · airframe 71,018 hrs · 18,621 cycles

CARGO FLOOR SUPPORT RBL 7.55, BS 1497 & 1520 CORRODED. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-53, REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 71,018 hrs · 18,621 cycles

FWD CARGO FLOOR STRINGER AT STA 634 TO STA 705, LBL 16.10 HAS CORROSION AROUND NUTPLATES REMOVED CORROSION FROM FLOOR STRINGER AT FWD CARGO STA 634 TO STA 705 LBL 16.10 BLEND OUT AREA DIMENSION IS L=2.100" W=.800" D=. 019" & L=3.00" W=.800" D=.016" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53 FIG 101 DETAIL V ALLOWABLE DAMAGE 1 AND REPLACED FLOOR STRINGER SECTION IAW NR 143N5370.

Part: FLOOR SUPPORT — CORRODED (BS 634-705) · airframe 71,018 hrs · 18,621 cycles

FWD CARGO FLOOR SUPPORT, BS 634 TO 705, LBL 7.55 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, PAR 4, PG 2-3 & PAR 7, PG 6-7 AND DWG 143N5320.

Part: INTERCOSTAL — CORRODED (BS 740-760) · airframe 71,018 hrs · 18,621 cycles

FOUND A CORRODED INTERCOSTAL BETWEEN BS 740 - 760, STRINGER 24 - 25L. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, FIG 101, DETAIL V. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02, PAGE 2 & 4 AND DWG 143N5320.

Part: FLOOR SUPPORT — CORRODED (BS 1445-1497) · airframe 71,018 hrs · 18,621 cycles

AFT CARGO FLOOR SUPPORT, LBL 10.45, BETWEEN BS 1445 - 1497 CORRODED. REMOVED THE CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 53-00-53, A D1, DETAIL V, REPAIRED IAW SRM 53-00-53, REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (BS 1445 -1497) · airframe 71,018 hrs · 18,621 cycles

AFT CARGO FLOOR SUPPORT, LBL 2.90 BETWEEN BS 1445 AND 1497 CORRODED. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-53, REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (BS 1661-1680) · airframe 71,018 hrs · 18,621 cycles

SURFACE CORROSION ON MAIN CABIN FLOOR SUPPORT UPPER SURFACE BETWEEN BS 1661 - 1680, BL 0. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51, FIG 101. REMOVED AND REPLACED FLOOR SUPPORT IAW DWG PL146N5230, AND SRM 51-40-28.

Part: FLOOR SUPPORT — CRACKED (BS 1320-1340) · airframe 71,018 hrs · 18,621 cycles

MAIN CABIN AFT FLOOR SUPPORT UPPER SUPPORT ANGLE, BETWEEN BS 1320 - 1340, BL 0, FOUND CRACKED. INSTALLED A REPAIR IAW SRM 53-00-51, REPAIR 4, FIG 201.

Part: FLOOR SUPPORT — CORRODED (BS 365-377) · airframe 71,018 hrs · 18,621 cycles

CORROSION ON MAIN CABIN FLOOR SUPPORT UPPER SURFACE, BETWEEN BS 365 - 377, LBL 61. REMOVED & REPLACED THE FLOOR SUPPORT IAW DRAWING 141N5170.

Part: PIN — GOUGED (L2 DOOR SLIDE) · airframe 71,018 hrs · 18,621 cycles

L2 DOOR FWD SLIDE GUIDE PIN GOUGED. REMOVED AND REPLACED THE GUIDE PIN IAW SRM 51-40-0 2.

Part: FLOOR SUPPORT — CORRODED (BS 1640-1661) · airframe 71,018 hrs · 18,621 cycles

SURFACE CORROSION ON THE CABIN FLOOR SUPPORT UPPER SURFACE BETWEEN BS 1640 - 1661, RBL 57. REMOVED THE CORROSION IAW SRM 51-10-02 AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG 146N5230, AND SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 1580-1600) · airframe 71,018 hrs · 18,621 cycles

MAIN CABIN AFT FLOOR SUPPORT UPPER SUPPORT ANGLE BETWEEN BS 1580 -1600, BL 0 FOUND CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG 46N518 0, AND SRM 51-40-02, FIG 8.

Part: FLOOR SUPPORT — CRACKED (BS 1520-1540) · airframe 71,018 hrs · 18,621 cycles

MAIN CABIN AFT FLOOR SUPPORT BETWEEN BS 1520 AND 1540, BL 0 CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORTIAW DWG 146N5180.

Part: STRAP — CRACKED (BS 377) · airframe 71,018 hrs · 18,621 cycles

STABILIZATION STRAP SEVERED UNDER MAIN CABIN FLOORBEAM AT BS 377 LBL 45. REPAIRED THE STABILIZATION STRAP IAW REPAIR 12.

Part: FLOOR SUPPORT — CORRODED (BS 660-680) · airframe 71,018 hrs · 18,621 cycles

CORROSION ON MAIN CABIN FLOOR SUPPORT UPPER SURFACE, BETWEEN BS 660 - 680, LBL 20. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04, AD 1, PG 103, FIG 101, DETAIL II, REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG 143N5130, REV BA.

Part: FLOOR SUPPORT — CRACKED (BS 1200-1220) · airframe 71,018 hrs · 18,621 cycles

MAIN CABIN AFT FLOOR SUPPORT UPPER SUPPORT ANGLE, BETWEEN BS 1200 - 1220, BL 0 FOUND CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG 146N5180, AND SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 1420-1440) · airframe 71,018 hrs · 18,621 cycles

MAIN CABIN AFT FLOOR SUPPORT BETWEEN BS 1420 AND 1440, BL 0, CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 140N 2505.

Part: STRAP — GOUGED (BS 582) · airframe 71,018 hrs · 18,621 cycles

FWD CARGO CEILING STABILIZATION STRAP IS GOUGED AT BS 582, RBL 26. REPAIRED THE STRAP IAW SRM 53-00-51, REPAIR 12, DETA IL VII.

Part: TUBE — LEAKING (HYD SYSTEM) · airframe 70,033 hrs · 18,434 cycles

LEFT HYD SYS LEAK. EMERGENCY DECLARED. FOUND HYD FLUID PUDDLING UNDER #1 ENG. REF IPC 29-11-05-03, FOUND THE TUBE ASSY LEAKING FROM LOWER END OF RIGID LINE AT THE B-NUT. TIGHTENED B-NUT APPROX 1/4 TURN. STILL LEAKING. R & R THE TUBE ASSY.

Part: LENS — MISSING (EXIT SIGN) · airframe 69,205 hrs · 18,272 cycles

EMERGENCY EXIT SIGN LENS AT LAV M MISSING. REPLACED MISSING EXIT SIGN LENS AT LAV M. OPS CK GOOD.

Part: COVER — LOOSE (EMERGENCY LGIHT) · airframe 68,487 hrs · 18,132 cycles

SEAT 28C EMERGENCY LIGHT COVER LOOSE. TIGHTENED LIGHT COVER.

Part: SKIN — DENTED (FUSELAGE) · airframe 67,667 hrs · 17,970 cycles

FUSELAGE DENT AT STA BS 1691 BETWEEN STR 18R AND 19R. REMOVED THE DENT DAMAGE FROM FUSELAGE SKIN PANEL AND PERFORMED AN INTERIM REPAIR IAW SRM 53-00-01 REPAIR 3. ECRA NR 5330-05947 PROVIDES AN FAA APPROVED INTERIM REPAIR FOR THE DAMAGE SKIN ON OR BEFORE THE ACCUMULATION OF 67,900 TOTAL A/C FLIGHT CYCLES.

Part: CHANNEL — CORRODED (LAV SERVICE) · airframe 67,667 hrs · 17,970 cycles

SURFACE CORROSION ON INNER SIDE OF AFT LAV SERVICE PANEL AND INNER SKIN. INSTALLED DOUBLER AND REPLACED STIFFENER ON AFT LAV SERVICE PANEL PAN PER SRM 51-30-01 AND 51-40-02.

Part: DOUBLER — CORRODED (LAV SERVICE) · airframe 67,667 hrs · 17,970 cycles

FWD LAV DUMP VALVE UPPER SURFACE HAS BLUE WATER LEAK AND CORROSION. REMOVED REPLACED AND INSTALLED NEW RING ASSY DOUBLER AND SUPPORT ANGLE AT FWD LAV DUMP VALVE IRW SRM 51-40-05, 51-20-01 AND 51-40-02.

Part: STRUCTURE — CORRODED (RT WING) · corrosion level 2 · airframe 61,456 hrs · 16,757 cycles

RIGHT WING OVERFILL PORT CUT OUT HAS CORROSION. REMOVED CORROSION, INSTALLED .032" FABRICATED FILLER WASHER IAW SRM 57-20-01, REPAIR 6, STEP 4D, 4E, & 4F. ALL NDT & SHOT PEEN ACCOMPLISHED IAW ABOVE SRM, ALL CORROSION REMOVED.

Part: DOUBLER — DAMAGED (L4 DOOR) · airframe 61,456 hrs · 16,757 cycles

DOOR 4L HAS DAMAGE TO THE INTERNAL SKIN DOUBLER REPAIR. REMOVED, FABRICATED & INSTALLED NEW REPAIR DOUBLER ON R4 DOOR INNER STRUCTURE IAW ECRA 5210-02405 STEPS 5, 13 & 20 - 31.

Part: APU — FAULTY (APU BAY) · airframe 61,443 hrs · 16,754 cycles

APU ALTITUDE NO START, COLD SOAK FL 380. APU SHUTDOWN AFTER REACHING 95% SPEED AFTER 10 SECONDS. SERVICED APU TO FULL, APU STARTED. WHILE RUNNING, OBSERVED LARGE PLUMES OF SMOKE FROM EXHAUST. AUTO SHUTDOWN AFTER FIVE MINUTES. RECHECKED OIL LEVEL & FOUND NO OIL LEVEL IN SIGHT GLASS. REPLACED APU IAW AMM 49-11-01. LEAK CHECKED GOOD.

Part: SIGN — BROKEN (CABIN) · airframe 59,571 hrs · 16,396 cycles

EMERGENCY EXIT SIGN ON FWD WALL AT DOOR 1L BROKEN. REPLACED EMER EXIT LIGHT IAW AMM 33-51-10 PG 201 & WDM33-51-21 PG 4A. OPERATIONS CHECKED NORMAL.

Part: HYDRAULIC LINE — LEAKING (RT AILERON) · airframe 57,479 hrs · 15,998 cycles

ON PUSHBACK DISCOVERED HYD LEAK RT AILERON. SECURED HYD RETURN HYD ACTUATOR SPOILER LINE

Part: JUMPSEAT — DAMAGED (CABIN) · airframe 57,168 hrs · 15,937 cycles

2L FLIGHT ATTENDANT JUMP SEAT HAS SHARP PIECE PROTRUDING.

Part: BUMPER — DAMAGED (JUMPSEAT) · airframe 57,121 hrs · 15,928 cycles

2L FA JS HAS SHARP PIECE PROTRUDING, MISSING PIECE OF BUMPER. REMOVED SHARP PIECE. NEED TO REPLACE BUMPER.

Part: HANDLE — BROKEN (L2 DOOR) · airframe 57,050 hrs · 15,914 cycles

L2 DOOR WILL NOT ARM. PLASTIC DOOR HANDLE BROKEN. NO DEFECTS FOUND WITH DOOR, ARMS & DISARMS OK. REPLACED PLASTIC DOOR ASSIST HANDLE.

Part: HANDSET — INOPERATIVE (1L) · airframe 56,916 hrs · 15,888 cycles

HANDSET 1L INOPERATIVE. REPLACED HANDSET, CHECKED GOOD.

Part: TRANSCEIVER — FAULTY (COCKPIT) · airframe 56,853 hrs · 15,876 cycles

NO LAND 3 DISPLAY, UNABLE TO RESET. REPLACED CENTER RA TRANSCEIVER IAW MM, CHECKED GOOD. ACCOMPLISHED A CAT 3 AUTO LAND TEST IAW MM. TEST PASSED.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 56,842 hrs · 15,873 cycles

BOTH LT & RT FLOW CONTROL VLVS FAILED TO GO TO THE LOW FLOW POSITION. INDICATORS STAYED AT FULL OPEN MARK WHILE FMC DISCRETES ARE SHOWING LOW DURING PACK HIGH FLOW INHIBIT TEST IAW AMM. REPLACED BOTH FLOW CONTROL VLV'S.

Part: DUCT — DIRTY (AIR DISTRIBUTION) · airframe 56,812 hrs · 15,867 cycles

EXCESSIVE COCKPIT AIRFLOW NOISE OVERHEAD PANELS INTERFERES WITH VOICE COMM BETWEEN PILOTS. ACP SERVICE TIP AMM 21-22 -00 TO STEP 8. FOUND AIRFLOW TO BE HIGH AT 3800 FPM & CFM AT 380. TOTAL NOISE WITH RT RECIRCULATING OFF IS BELOW 70.5DB. NEEDS AIR DUCT CLEANING. CLEAN AIR DIST DUCTS IN THE CABIN & COCKPIT.

Part: LANYARD — UNSECURE (L2 DOOR SLIDE) · airframe 56,801 hrs · 15,865 cycles

L2 DOOR WILL NOT ARM. SECURED LOOSE LANYARD IN POUCH. ARM DISARM FUNCTION NOW NORMAL, SLIDE LIGHT CHECKED OKAY.

Part: FAN — NOISY (COCKPIT) · airframe 56,742 hrs · 15,854 cycles

RT RECIRCULATING FAN EXCESSIVELY NOISY INTERFERES WITH COCKPIT COMM. RECIRCULATING MESSAGE ON EICAS

Part: FAN — NOISY (RIGHT) · airframe 56,635 hrs · 15,833 cycles

RT RECIRC EXCESSIVELY LOUD.

Part: ANTENNA — FAULTY (RADAR ALTIMETER) · airframe 56,603 hrs · 15,827 cycles

FIRST OFFICER RADAR ALT FAILING. CHRONIC, DOWNGRADED AIRCRAFT TO AUTO LAND LIMIT "LAND 2". ACCOMPLISH SVC TIP 34-33- 02 ANTENNA RESIST TEST, REPLACE R-RA XMTR ANT M254 580-0685 IAW 34-33-02 IF RCVR ANT M255 IS LESS THAN 1 OHM IAW WDM34-33-21 P2. REPLACED RT RA TRANSMIT ANTENNA IAW MM. ACP ANTENNA TESTED & PASSED.

Part: SWITCH — DEFECTIVE (COCKPIT) · airframe 56,603 hrs · 15,827 cycles

RT ELEC HYD PUMP LIGHT DOES NOT ILLUMINATE "PRESS" WHEN DESELECTED, NO EICAS YELLOW CAUTION MESSAGE. BULBS ILLUMINATE WHEN TESTED, PUMP TURNS OFF NORMALLY WHEN SELECTED OFF, SYSTEM PRESSURE INDICATIONS OPERATE NORMALLY. REPLACED RT ELEC HYD PUMP SWITCH. OPERATIONS CHECKED NORMAL. ...

Part: MODULE — FAULTY (TE FLAP) · airframe 56,593 hrs · 15,825 cycles

TE FLAP DISAGREE, DUE TO TE FLAP DISAGREE & FINDING OF TE FLAPS MOVE TO SELECTED POSITION AT A RATE FASTER THAN NORMAL. PER 27-FAULT CODE INDEX PG 9 27-51-06-00, 27-51-07-00. REPLACE THE FLAP SLAT DEPRESSURIZATION MODULE IAW MM27-51-29-201 PCN 643-9093 REF IPC 27-51-29-001-80. REPLACED FLAP SLAT DEPRESSURIZATION MODULE IAW MM 27-51-29. OPERATIONS CHECKED FAILED.

Part: FSEU — FAULTY (TE FLAP) · airframe 56,583 hrs · 15,823 cycles

FLAPS STUCK BETWEEN 25 & 20. RETRACTED TO 0 AFTER ENGINE SHUTDOWN AT GATE. REPLACED FSEU 1 IAW MM, CHECKED GOOD. CYCLED FLAPS SEVERAL TIMES FULL DOWN & BACK UP, NO PROBLEMS.

Part: GIRT BAR — OBSTRUCTED (L4 DOOR) · airframe 56,435 hrs · 15,794 cycles

4L WILL NOT ARM. STOWED EXCESS STATIC LINE.

Part: REGULATOR — MALFUNCTIONED (ENGINE) · airframe 56,381 hrs · 15,783 cycles

ENGINE DUCT PRESSURES SPLIT DURING TAKEOFF OR CLIMB. ISOLATION VALVE CLOSED & BLEED SW SELECTED ON, RECORD DUCT PRESSURES. REPLACED PRESSURE REGULATING SHUTOFF VALVE, BLEED OPERATED NORMALLY DURING HIGH POWER RUN.

Part: B-NUT — LEAKING (FUEL-OIL COOLER) · airframe 56,366 hrs · 15,780 cycles

OIL LEAK FROM INLET PORT B-NUT OF FUEL OIL COOLER. REPLACED FUEL-OIL COOLER, RAN ENGINE NO LEAKS NOTED.

Part: OUTFLOW VALVE — FAULTY (POSIT 1) · airframe 56,237 hrs · 15,752 cycles

OVERBOARD EXHAUST VALVE NOT IN PROPER POSITION (NOT FULLY OPEN) REPLACED EQPT COOLING OVERBOARD EXHAUST VALVE IAW AMM.

Part: GIRT BAR — OBSTRUCTED (L4 DOOR) · airframe 56,223 hrs · 15,746 cycles

L4 DOOR WILL NOT ARM. CLEANED DEBRIS FROM DOOR WAY, OPS CHECKED NORMAL.

Part: SKIN — DAMAGED (BS 501-523) · airframe 56,218 hrs · 15,745 cycles

SKIN AT BS 501-523 S26L BL 0 DAMAGED. INSTALLED REPAIR. MAJOR REPAIR.

Part: SKIN — CRACKED (R4 DOOR) · airframe 56,218 hrs · 15,745 cycles

R4 DOOR INNER SKIN CRACKED AT ACCESS HOLE ABOVE LOWER HINGE. INSTALLED DOUBLER REPAIR IAW ECRA 5210-02405. MAJOR REPAIR.

Part: SKIN — DENTED (AFT CARGO DOOR) · airframe 56,218 hrs · 15,745 cycles

AFT CARGO DOOR DENTED. REPAIRED IAW SRM 52-30-01 REPAIR NR 4. MAJOR REPAIR.

Part: SKIN — DENTED (L1 DOOR) · airframe 56,218 hrs · 15,745 cycles

L1 DOOR HAS AN INTERIM REPAIR TO OUTER SKIN THAT REQUIRES PERMANENT REPAIR BY NEXT 'C' CHECK. REPAIRED DENT AT L1 DOOR OUTER SKIN IAW ECRA 5210-02403.

Part: SKIN — CRACKED (R2 DOOR) · airframe 56,218 hrs · 15,745 cycles

DURING DVI OF CABIN DOOR FOUND CRACK R2 DOOR INNER SKIN, OUTER SURFACE ON ROUND VIEW HOLE AT LOWER & AFT SURFACE OF THE DOOR. REPAIRED IAW ECRA 5210-02 401. THIS IS A CATEGORY A REPAIR AS DEFINED IN SRM 51-00-06.

Part: SPRING ASSY — FROZEN (R4 DOOR ASSIST) · airframe 56,218 hrs · 15,745 cycles

R4 DOOR POWER ASSIST TRIGGER FROZEN AND WILL NOT TURN IAW STEP 3, FIG 601, AMM 52-11-99. R & R SPRING CLIP AT POWER ASSIST TRIGGER. OPS CHECKED NORMAL.

Part: CONTROL VALVE — FAILED (RIGHT) · airframe 56,218 hrs · 15,745 cycles

ON CONDITION RT LOW LIMIT CONTROL VALVE. REPLACED CONTROL VALVE.

Part: CONTROL VALVE — FAILED (LEFT) · airframe 56,218 hrs · 15,745 cycles

ON CONDITION LEFT LOW LIMIT CONTROL VALVE. CONTROL VALVE REPLACED.

Part: PRESSURE DECK — CORRODED (BS 1681) · airframe 56,218 hrs · 15,745 cycles

AFT PRESSURE DECK BS 1681.8, PLUS 4 INCHES, RBL 55.0 FOUND TRACES OF CORROSION ON EXISTING DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED: REMOVED AND INSTALLED NEW DOUBLER IAW B757-200 SRM 51-40-08, PGS 5-7,51-20-05 PGS 201-203, 51-40-02 PGS 1&2 & ECRA 5330-04259. THIS IS A CAT A REPAIR AND NO FURTHER INSPECTIONS ARE REQUIRED.

Part: IMPELLER — FAILED (BOOST PUMP) · airframe 56,182 hrs · 15,734 cycles

LEFT AFT FUEL BOOST PUMP EICAS, FLT DIVERTED. REPLACED BOOST PUMP MOTOR IMPELLER IAW MM, OPS CHECKED OK.

Part: GREASE FITTING — DIRTY (RAT ACT ROD END) · airframe 56,125 hrs · 15,717 cycles

RAT DEPLOYMENT ACTUATOR ASSY UPPER AND LOWER GREASE FITTINGS WILL NOT TAKE GREASE. CLEANED FITTINGS. BOTH ROD ENDS TOOK GREASE.

Part: INDICATOR — FAILED (FUEL QTY) · airframe 56,125 hrs · 15,717 cycles

TOTAL FUEL QTY & FUEL TEMP INDICATION INTERMITTENT INOPERATIVE. REPLACED FUEL QUANTITY INDICATOR. OPS CHECKED GOOD.

Part: CONTROLLER — FAILED (COCKPIT) · airframe 55,546 hrs · 15,561 cycles

HMG FAILED ACK OPS CK. REPLACED HMG CONTROLLER.

Part: START VALVE — FAULTY (RT ENGINE) · airframe 55,238 hrs · 15,468 cycles

RIGHT ENGINE START VALVE WON'T OPEN DURING ENGINE START APU DUCT PRESS NORMAL. CONFIRMED START VALVE MANUALLY OPERATES. REMOVED & REPLACED NR 2 ENGINE START VALVE.

Part: LINE — CONSTRICTED (POTABLE WATER) · airframe 55,157 hrs · 15,443 cycles

NO WATER PRESSURE WITH APU & RT ENGINES RUNNING. FOUND PNEUMATIC FLEX LINE CONSTRICTED. NO AIR PRESSURE GOING TO WATER TANK. REMOVED PNEUMATIC FLEX LINE. INSTALLED NEW FLEX LINE AND CLAMPS.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 55,053 hrs · 15,413 cycles

EMERGENCY EXIT SIGNS AT FWD LEFT AND AFT RIGHT OVERWING EXITS ARE INOPERATIVE. REPLACED INVERTER, OPS NORMAL.

Part: HOUSING — LEAKING (SPOILER ACTUATOR) · airframe 54,908 hrs · 15,368 cycles

NR 3 SPOILER ACTUATOR LEAKING. LEAK IS COMING FROM PLUG ON BACK OF ACTUATOR BODY. SECURED LOOSE FITTING, ACCOMPLISHED LEAK CHECK NONE FOUND.

Part: UNKNOWN — UNKNOWN (FUEL QTY) · airframe 54,895 hrs · 15,363 cycles

FUEL QTY BITE MAINTENANCE MESSAGE DISPLAYED. SELF TEST GRIPES LM DENSITOMETER EXCITATION SHORTED. REPLACED FQPU, NO HELP. SUMPED LT AND RT MAIN TANKS. SMALL AMOUNT OF WATER REMOVED. FAULT STILL PRESENT. PERFORMED RESISTANCE CHECK, FOUND NO DEFECTS. BITE CHECKED FPQU FOUND NO FAULT. BITE CHECKED GOOD. NO FAULTS NOTED.

Part: LIGHT — INOPERATIVE (R3 DOOR) · airframe 54,841 hrs · 15,348 cycles

FOUND R3 DOOR OUTER EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT. CHECKED OK.

Part: LIGHT — UNSECURE (CABIN) · airframe 54,363 hrs · 15,223 cycles

CAPT'S INST PANEL FLOOD LIGHT CONTROL WILL NOT CONTROL INTENSITY OF (CAPT'S INST PANEL, CENTER INST PANEL) LIGHTS. LIGHTS DO NOT ILLUM BRT WITH LIGHT OVRD SWITCH ON. CTR FLOOR PANEL NEEDS RELAMP. SECURED LAMP IN CENTER FLUORESCENT HOLDER.

Part: CAP — MISSING (WINDOW HEAT) · airframe 54,136 hrs · 15,163 cycles

CAPTAIN`S FWD WINDOW MISSING CAP ON WINDOW HEAT. REPLACED MISSING CAP.

Part: START VALVE — FAULTY (RT ENGINE) · airframe 54,025 hrs · 15,140 cycles

RIGHT START CONT C/B POPPED DURING ENGINE START. REPLACED RIGHT ENGINE START VALVE PER AMM, GRD OPS CHECK.

Part: TRANSCEIVER — INOPERATIVE (HF COMM) · airframe 53,972 hrs · 15,128 cycles

L HF INOPERATIVE. CHECKED ON THE GROUND; INFLT-LONG TUNE CYCLE THEN UNABLE TO XMIT; RECEIVES OKAY :LT HF COUPLER NOT TUNING. REPLACED HF TRANSCEIVER PER MM.

Part: HANDSET — INOPERATIVE (CABIN) · airframe 53,959 hrs · 15,124 cycles

PHONE AT DOOR 1L INOP. REPLACED HANDSET AT DOOR 1L.

Part: FILTER ELEMENT — FAULTY (NR 2 IDG) · airframe 53,944 hrs · 15,121 cycles

NR 2 ENGINE IDG SCV FILTER ELEMENT FOR ETOPS SIGNIFICANT SYSTEM (GROUP 1). REMOVE AND REPLACE THE IDG SCAVENGE FILTER ELEMENT ON ENGINE NR 2 PER AMM. DO NOT ACCMP MAINTENANCE OF NR 1 AND NR 2 IDG AT SAME VISIT DUE TO ETOPS CRITICAL SYSTEM REQUIREMENTS. REPLACED NR 2 ENGINE IDG FILTER. NO PARTICLES NOTED, OPS CHECK GOOD, NO LEAKS NOTED.

Part: SEAL — LEAKING (NR 2 ENGINE) · airframe 53,748 hrs · 15,068 cycles

NR 2 HAS HIGH ENGINE OIL CONSUMPTION. FOUND OIL WETNESS AT DEOILER BREATHER OUTLET. NEED TO REPLACED DEOILER SEAL ASSY WITHIN 25 HOURS. REPLACED DE-OILER DRIVE SEAL, LEAK CHECKS GOOD. NEED TO CHECK NR 2 ENGINE OIL QTY AT EACH DEPARTURE.

Part: FUEL FILTER — FAULTY (NR 2 ENGINE) · airframe 53,635 hrs · 15,037 cycles

RIGHT ENGINE FUEL FILTER ISSUE, RTFL. REPLACED NR 2 ENGINE FUEL PUMP FILTER. ACP 5 MIN IDLE RUN. LEAK CHECK OK. MESSAGE CLEARED.

Part: MODULE — INOPERATIVE (YAW DAMPER) · airframe 53,340 hrs · 14,953 cycles

LEFT YAW DAMPER INOPERATIVE. REPLACED CSEU PWR SUPPLY MODULE M536 DUE TO "NO 26 VAC" FAULT ON YAW DAMP MODULE-L. YAW DAMP, RUDDER RATIO, POWER SUPPLY AND MCDP CURRENT FAULTS TEST 30 ALL PASS.

Part: SEAL PLATE — LEAKING (NR 3 SPOILER) · airframe 53,280 hrs · 14,937 cycles

HYD LEAK NR 3 SPOILER ACTUATOR. REPLACED SEAL PLATE ON SPOILER PCA ELECTRO HYD SERVO NR 3. NO FURTHER LEAKS NOTED.

Part: DRIVE ASSY — FAILED (WX RADAR SCANNER) · airframe 53,181 hrs · 14,910 cycles

WEATHER RADAR SYSTEM HAS UNCODED FAULT. AUTO TILT SWITCH INOPERATIVE IN MANUAL TILT ALL THE TIME REGARDLESS OF SWITCH POSITION. REPLACED ANTENNA DRIVE ASSEMBLY PER AMM.

Part: EXCITER — INOPERATIVE (APU ENGINE) · airframe 53,051 hrs · 14,871 cycles

APU HAD SHUTDOWN, FAULT LIGHT ILLUMINATED AND EICAS MESSAGE. APU FAULT DISPLAYED. THREE FAILED START ATTEMPTS ALL HUNG AT 25 PCT RPM BEFORE AUTO ABORT. FOUND NO SPARK ON APU ENGINE START, REPLACED EXCITER BOX AND LEAD, OPS CHECKED GOOD.

Part: SKIN — PUNCTURED (BS 640) · airframe 52,034 hrs · 14,580 cycles

FUSELAGE PUNCTURED BOTTOM LEFT APPROXIMATELY BS 640 AND WL 144. HOLE IS APPROX 1 INCH BY 1 INCH. HOLE LOCATION IS AT BS STA 668 AND ABOVE STRINGER 26L. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EG DOCUMENT.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 52,033 hrs · 14,579 cycles

DAMAGE ON FUSELAGE SKIN 1" X 1" HOLE. FUSELAGE PUNCTURED BOTTOM LEFT APROX STA 640 WL 144. HOLE IS APPROX 1 INCH BY 1 INCH. HOLE LOCATION IS AT BS STA 668 & ABV STR 26L RCV'D AVO1269 REV 2, REF ECRA 5300-01414. ACCMP'D PERMANENT REPAIR IAW EG DOCUMENT. CUT OUT DAMAGE STA 668 STR 26L PER AVO1269.

Part: JACK — DEFECTIVE (INTERPHONE) · airframe 51,940 hrs · 14,551 cycles

INTERPHONE AT 1L INOPERATIVE. REPLACED HANDSET JACK PER MM, OPS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (RT FIREWALL) · airframe 51,806 hrs · 14,509 cycles

RT ENG GENERATOR FEEDER CABLE PINS BURNED AND SEIZED IN CONNECTOR AND ENGINE SIDE CONNECTOR D1092 AT FIRE WALL DISCONNECT. WIRE HARNESS W5610 INSTALLED.

Part: BRACKET — CRACKED (LT WINDOW) · airframe 51,688 hrs · 14,479 cycles

WHILE ATTEMPTING TO ADJUST NR 2 LT OPENABLE WINDOW, FOUND LATCH HANDLE FWD STRIKER BRACKET CRACKED. REMOVED WINDOW. REPLACED WITH NEW BRACKET & REINSTALLED NR 2 LT WINDOW, RIGGED FOR FREE LATCH HANDLE.

Part: VALVE — FAULTY (RT A/C PACK) · airframe 51,466 hrs · 14,418 cycles

RT PACK OFF, FLIGHT DIVERTED. VERIFIED DRAIN LINES ARE CLEAR. REPLACED LOW LIMIT VALVE.

Part: PRESSURE SWITCH — FAULTY (SPEEDBRAKE SYS) · airframe 51,365 hrs · 14,389 cycles

AUTOSPEEDBRAKE EICAS MESSAGE CAME ON SHORT FINAL. REPLACED RIGHT GEAR TILT PRESSURE SWITCH S453, OPS CHECKED NORMAL.

Part: COMPUTER — FAULTY (AUTOPILOT SYS) · airframe 51,352 hrs · 14,386 cycles

NO LAND III DISPLAYED ON EICAS. AUTOPILOT BITE SHOWS NO INTERFACE FCC RIGHT TO RUDDER RATIO SERVO AUTOPILOT DOWNGRADED TO CATII SECOND DEFERAL CREATED FOR RIGHT FLIGHT DIRECTOR INOP. REPLACED R FCC PER MM AND ACCOMPLISHED A-P FLIGHT CONTROL TEST PER MM, ALL PASSED. RETURNED SYSTEM TO CAT III. SECOND DEFFERAL AGAINST RFD WAS NOT CREATED.

Part: SENSOR — FAULTY (LT PACK) · airframe 51,352 hrs · 14,386 cycles

EICAS MSG -L PACK TEMP-. PACK INOP LIGHT ON. LIGHT RE-ILLUM WHEN PACK RESET IN STBY. CREW COMMENTS: AUTO MODE INOP. CONCURRED WITH CREW, OPS CHECK LEFT PACK IN STBY MODE IS OPERATIONAL. -INF- :1EA 7540158 LAXCC4. RPL- :BITE CK SHOWS COMPRESSOR OUTLET SENSOR, RPL SENSOR PER MM, OPS CHK OKAY.

Part: CDU — FAULTY (COCKPIT) · airframe 51,260 hrs · 14,362 cycles

F/O CDU BLANK ON TAXIOUT. THIS IS 3RD HIT IN 2 DAYS, PLEASE REPLACE CDU. REPLACED CDU PER AMM. OPS CHECK NORMAL.

Part: ACTUATOR — LEAKING (LT AILERON) · airframe 51,169 hrs · 14,332 cycles

LT AILERON HYD LEAK FROM INBOARD PORTION OF AILERON TO OUTBOARD FLAP TRACK FAIRING. LEAKING FROM OUTBD AILERON ACT ROD END FOUND AT 3 DROPS PER MIN PER TOMC. LEFT OUTBD ACT TO BE RPLC'D WITHIN 75T. CURRENT PTT 51169.

Part: TRANSDUCER — INTERMITTENT · airframe 51,026 hrs · 14,296 cycles

NO LAND 3 DISP ON ASA WITH SYS ENGAGED IN CMD. SOURCE SELECT IN 2 (1=L ,2=C, 3=R) POS. CREW COMMENTS: LEFT AP SAME THING. FOUND FAULT FEEL POS-FCC C. FLIGHT FAULT CODES ARE FLT 5-132221,122221, FLT 22-132221, FLT 30-132221, FLT 40-122221, CARRIED OUT TRANSDUCER OUT TEST AND CENTER TRANSDUCER IS INTERMITTENT, NEED TO BE REPLACED PCN 564-0253, SEE AMM 22-00-02 PG 157 BLOCK 208, AND AMM 22-12-02 PG 401, WILL NEED TOOLING << -INF- :ALSO PER ABOVE AMM WILL NEED TO PUMP PITOT SYSTEM TO 350 KNOTS TO ADJUST SENSOR. SUGGEST A TWO SHIFT SLOT :2 SFT SLT RQSTD FOR REPLACEMENT OF TRANSDUCER. PARTS: 056-1735 B27039-13 KIT. 564-0253 U91B TRANSDUCER.

Part: FITTING — LEAKING (HYD LINE) · airframe 51,026 hrs · 14,296 cycles

FLUID LEAKING FROM LEFT AILERON AREA. SECURED LOOSE HYD LINE FITTING AFT OF LEFT OUTBOARD AILERON PCA.

Part: SEAL — FAILED (COCKPIT WINDOW) · airframe 51,011 hrs · 14,292 cycles

CAPTAIN'S WINDOW VERY HARD TO UNLOCK AFTER ACFT HAS BEEN FLOWN OR PRESSURIZED. DUE TO CAPT WINDOW NOT OPENING AFTER FLIGHT, ADJUSTED NR 2 WINDOW PER MM. AFTER RIG, PRESSUREIZED ACFT PER MM, AND CHECKED WINDOW FOR PROPER OPERATION. REPLACED WINDOW SEAL PER MM AND RIG CHECKED. ACCOMPLISHED CHECK OF CAPTAIN'S SLIDING WINDOW PER MM. ADJUSTED ARM LINK MEASURES 5.8 IN THE OPEN POSITION MEASURES 5.4 CLOSED PRESSURIZED AIRCRAFT, OPS CHECK OF WINDOW NORMAL.

Part: BLADE — DAMAGED (LT ENGINE) · airframe 50,972 hrs · 14,283 cycles

LEFT ENGINE HAS DAMAGE ON LEFT FAN BLADE. INSPECTED FAN BLADE-NO CRACKS OR TEARS. DAMAGE IS 5.25" IN FROM MID-SPAN. DAMAGE IS .031 DEEP. FIGURE 603 DAMAGE IS IN AREA 8. PER PAGE 609. BLENDED DAMAGED BLADE AS REQUIRED.

Part: RELAY — FAILED (RT AC PACK) · airframe 50,910 hrs · 14,267 cycles

COCKPIT AIR NOISE IS VERY LOUD. CHECKED FLIGHT DECK NOISE LEVEL PER SERVICE TIP 21- 22-00 PAGE 902 STEP 7. NOISE LEVEL INDICATED A GREATER THAN 3DB CHANGE WHEN RT RECIRCULATION FAN WAS SELECTED. FOUND THE RIGHT PACK STUCK IN HIGH FLOW. REPLACED CONTROL VALVE CARD M864, NO HELP. REPLACED RELAY K416, CHECKED OKAY.

Part: UNKNOWN — VIBRATION (YOKE) · airframe 50,716 hrs · 14,214 cycles

CREW REPORTED THAT AT 270 KTS FELT MILD VIBRATION IN YOKE ONLY. STOPPED AT 210 KTS, GEAR WAS UP, AND FLAPS AT 5. ACCOMPLISHED ELEVATOR COMPONENT CHECKS. ALL ELEVATOR COMPONENT WEAR CHECKED WITHIN LIMITS. ALSO INSPECTED NOSE GEAR DOOR SEALS AND GROUND POWER ACCESS DOOR, FOUND NO PROBLEMS.

Part: OXYGEN MASK — DEFECTIVE (COCKPIT) · airframe 50,668 hrs · 14,200 cycles

OXYGEN MASK DEFECTIVE AT3.(1=CAPT,2=1ST OFF,3=1ST OBS). CREW COMMENTS: F/O'S O2 MASK VERY HARD TO HEAR. SWITCHED WITH OBS MASK, NO HELP. BOTH TESTED OKAY IN OBS POSITION. REPLACED OXYGEN MASK PER AMM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 50,666 hrs · 14,199 cycles

EMERGENCY FLOOR LIGHTING INOP FROM DOOR 2L TO EXIT ROWS. SECURED LIGHT STRIP. SECURED CONNECTOR ON POWER SUPPLY, ALL CHECKS OK NOW.

Part: RECEPTACLE — DIRTY (FUEL SYSTEM) · airframe 50,450 hrs · 14,131 cycles

LEFT MAIN FUEL QTY BLANK AT LAX. TROUBLESHOOTING NEW FUEL QTY PROCESSOR, NO HELP. NEW FUEL QTY PROCESSOR INSTALLED BY MECHANIC. NO HELP. PROCESSOR SHOWS PRESENT FAULTS (LM HI Z SHIELD OPEN AT SPAR G01). ACP TROUBLESHOOTING PER MM. RANG OUT WIRES FROM FUEL QTY PROCESSOR M121 RACK CONN D2440C PINS A1, B2, C3 TO LEFT MAIN TANK FROM SPAR CONNECTOR D6880. ALL CHECKS SATISFACTORY. NEED TO CHECK WIRING IN TANK. CLEANED SPAR CONNECTOR RECEPTACLE AND PLUG. SELF TEST SHOWS NO FAULTS.

Part: SENSOR — FAULTY (AIRSPEED) · airframe 50,363 hrs · 14,101 cycles

CAPT & FO AIRSPEED SPLIT. ACCOMPLISHED CHECKS. NO DEFECTS FOUND. CAPT AND FO PITOT AND STATIC LEAK CHECKED GOOD. TRAPS OK AND NO OBSTRUCTION IN PROBES AND PORTS.

Part: ACM — SEIZED (RIGHT) · airframe 50,350 hrs · 14,098 cycles

RIGHT A/C PACK INOPERATIVE. ACM SEIZED, REPLACED RT ACM, OPS NORMAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,128 hrs · 14,029 cycles

FLOORBEAM AT BS 324 CORRODED AT RBL 44. MAJOR REPAIR ACCOMPLISHED: 324 FLOORBEAM UPPER CHORD REMOVED AND REPAIRED PER THE INSTRUCTIONS ON PEMCO PD 57-53-186 AND EVA 81314 WITHOUT DEVIATION.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 50,128 hrs · 14,029 cycles

TOOLING MARK ON FLOORBEAM WEB AFT SIDE AT STA 310, RBL 44. MAJOR REPAIR ACCOMPLISHED. BLENDED, FABBED AND INSTALLED DOUBLER, ANGLES AND SHIMS PER PEMCO EA PD57-53-197 AND EVA 81339 ON PEMCO NR 3365N00530.

Part: FLOORBEAM — CORRODED (BS 345) · airframe 50,128 hrs · 14,029 cycles

FLOORBEAM AT BS 345 CORRODED FROM BL 0 - RBL 45. MAJOR REPAIR ACCOMPLISHED REPLACED TEE'S, ANGLES, AND STRAPS PER SRM.

Part: FLOORBEAM — CORRODED (BS 1661) · airframe 50,128 hrs · 14,029 cycles

FLOORBEAM TEE CORRODED AT BS 1661 FROM BL 0 TO LBL15. REPLACED TEE'S AND STRAPS PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,128 hrs · 14,029 cycles

FLOORBEAM AT BS 365 CORRODED AT RBL 54. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION & FOUND MATERIAL LOSS OUT OF LIMITS OF SRM. REMOVED CORRODED SECTION OF FLOORBEAM UPPER CHORD. FABRICATED & INSTALLED REPAIR SPLICE ANGLES, STRAPS & NEW 'T' CHORD SECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 50,128 hrs · 14,029 cycles

FLOORBEAM AT BS 1640 BL 0 -RBL 50 CORRODED. REPAIR ACP PER SRM, REF WO 3365Z0273.

Part: SLIDE — UNSERVICEABLE (L2 DOOR) · airframe 50,128 hrs · 14,029 cycles

L-2 DOOR EVAC SLIDE SAFETY PIN ALIGNMENT HOLE ADJUSTMENT ALLEN SCREW HEAD BROKEN. REPLACED SLIDE AT DOOR 2L, SLIDE INTALLED ON TC 5R521I022, SLIDE RPL ON WO 3365Z001.

Part: LIGHT — UNSECURE (CABIN) · airframe 50,040 hrs · 14,001 cycles

EMERGENCY LIGHT STRIP ON FLOOR NEAR 12C COMING UP. SECURED LIGHT STRIP.

Part: CLOCK — OUT OF TOLERANCE (NR 2) · airframe 49,633 hrs · 13,882 cycles

FIRST OFFICERS CLOCK IS OUT OF TOLERANCE. REMOVED CLOCK AND INSTALLED CHRONOMETER, CHECKED OKAY.

Part: LIGHT — UNSECURE (SEAT 12C) · airframe 49,636 hrs · 13,883 cycles

EMERGENCY LIGHT AT SEAT 12C WILL NOT STAY DOWN. SECURED STRIP.

Part: TRANSFORMER — FAULTY (NR 1) · airframe 49,633 hrs · 13,882 cycles

HMG FAILS A-CHECK. MEASURED VOLTAGE IS 34.4 VDC. REQUIRED VOLTAGE IS 28VCD +-3. REPLACED HMG TRANSFORMER POWER SUPPLY T10060, HMG CHECKS OKAY.

Part: CONTROL PANEL — FAULTY (ENGINE START) · airframe 49,462 hrs · 13,834 cycles

RT ENGINE START SWITCH DIFFICULT TO MOVE FROM 'AUTO' TO 'GROUND'. REPLACED ENGINE START RAT CONTROL PANEL.

Part: GCU — FAULTY (RIGHT) · airframe 49,352 hrs · 13,808 cycles

RIGHT GENERATOR CONTROL CYCLING ON AND OFF AFTER LANDING. SERVICED IDG NR 2 OIL AND REPLACED GCU NR 2 PER AMM. GENERATOR NR 2 CHECKED OKAY ON 5 MIN IDLE RUN.

Part: MOTOR — FAULTY (BOOST PUMP) · airframe 49,207 hrs · 13,764 cycles

BOTH LT AND RT CENTER TANK PUMP LOW PRESSURE LIGHTS COME ON WHEN XFER FUEL FROM CENTER TANK. NEED TO INSP BOTH CENTER TANK PUMPS PICK UP TUBES FOR OBSTRUCTION. INSP CENTER TANK PLUMBING. NO DEFECTS FOUND. ALSO TRANSFER OF FUEL FROM CTR TO WING OPERATED PER MM. ACP AUTOSHUT OFF TEST. AUTO SHUTOFF OPERATES NORMAL. INSP CENTER TANK PICK UP TUBES FOR DEBRIS NONE FOUND. RT CTR PUMP AND PRESS SW REPLACED. TESTED CTR TANK PUMPS. PUMPS OPERATE NORMAL.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 48,896 hrs · 13,673 cycles

MCP IAS-MACH SWITCH INOP STAYS IN MACH ONLY. REPLACED MCP PER MM, ACP CATIII TEST PER MM. TEST PASSED.

Part: STARTER — FAULTY (NR 2 ENGINE) · airframe 48,898 hrs · 13,674 cycles

NR 2 ENG START, N2 FAILED TO ROTATE. GND SW AND VALVE LIGHT OK. REPLACED STARTER, ROTATED NORMAL, DUCT PRESSURES NORMAL.

Part: CONTROL VALVE — FAILED (APU BLEED SYS) · airframe 48,884 hrs · 13,670 cycles

WEAK APU PRESS FOR ENG START. 10 PSI DURING START. CROSSBLEED START OKAY. VALVE OPENS AND CLOSES NORMAL. LOW DUCT PRESS FROM APU. INOPED PER MEL PROCEDURES. REPLACED SURGE CONTROL VALVE PER MM. OP CHECKED OKAY.

Part: FEEDER CABLE — DAMAGED (CABIN) · airframe 48,764 hrs · 13,627 cycles

EEL LIGHT INOP AT FWD AFT LAV. REPAIRED EEL LIGHT FEEDER CABLE, OPS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,325 hrs · 13,491 cycles

EMERGENCY LIGHT STRIP INOP IN AFT CABIN AT ROW 32 ABC. REPLACED LIGHT AND OPS CHECKED GOOD.

Part: AUDIO PANEL — FAILED (COCKPIT) · airframe 47,949 hrs · 13,385 cycles

CAPT RADIO WILL TRANSMIT ON HF 2 WHEN USING PTT, YOKE & HAND MIC. REPLACED CAPT'S AUDIO SELECTOR PANEL REF AMM. OPS CHECKED ARE NORMAL.

Part: AUDIO PANEL — OUT OF TOLERANCE (COCKPIT) · airframe 47,954 hrs · 13,386 cycles

FIRST OBSERVERS AUDIO SELECTOR PANEL OUT OF TOLERANCE. REPLACED FIRST OBS AUDIO SELECTOR PANEL. OPS GOOD.

Part: SWITCH — INOPERATIVE (FIRE BOTTLE) · airframe 47,832 hrs · 13,350 cycles

NR1 BOTTLE DISCHARGE LIGHT WON'T STAY ON. REPLACED NR 1 BOTTLE DISCHARGE SWITCH. DISCHARGE LIGHT NOW STEADY IN TEST.

Part: CONTROL PANEL — FAULTY (SATCOM) · airframe 47,798 hrs · 13,342 cycles

CAPTAIN'S AUDIO SELECTOR PANEL RT SATCOM MIC SELECT WON'T LATCH. REPLACED AUDIO SELECT PANEL, OPS NORMAL.

Part: SEAL — LEAKING (NR 2 DEOILER) · airframe 47,599 hrs · 13,286 cycles

NR 2 ENG HIGH OIL CONSUMPTION EXCEEDS LIMIT. RAN ENGINES PERFORMED BAG AND BREATHER, NO FLUID LOSS FROM DRAINS NOTICED. WIPED COWL BEFORE RUN AND FOUND OIL LEAKAGE FROM DEOILER PORT AFTER RUN. REPLACED DEOILER SEAL AND RING. NO LEAKS NOTED.

Part: SHUTOFF VALVE — FAULTY (LT ENGINE) · airframe 47,540 hrs · 13,266 cycles

LEFT ENGINE BLEED AIR VALVE 'OFF 'LIGHT NOT ON WITH SWITCH 'ON' & ENG RUNNING. DUCT PRESSURE WAS NORMAL. AFTER LT ENGINE START BLEED REMAINED OPEN, ONLY HAD 10 PSI DUCT PRESSURE, HAD TO TURN OFF BLEED TO STA. PRSOV VALVE REPLACED IAW AMM. ON ENG RUN IAW NEW PROCEDURE FOUND PRSOV OFF. STAYED ON WITH ENG RUNNING.

Part: FLOOR SUPPORT — CORRODED (BS 1666) · airframe 46,930 hrs · 13,085 cycles

STA 1666 AT FLOOR LEVEL, SUPPORT CORRODED 8 INCHES TO THE RT OF WATER VALVE. (RT OF CTR LINE). CORROSION ON HAT SECTION STA 1666 IS BEYOND LIMITS. STARTED TO REMOVE CORROSION, UNABLE TO REMOVE ALL OF IT DUE TO ACCESSABILITY AND FLOORBOARD. NEED TO REMOVE GALLEY AND FLOORBOARD. CORROSION REPORTED TO BE BELOW AFT GALLEY FLOOR AREA. PICTURES ON RVI. ACP LOG 001 ON WU B4916W, 1666 FLOOR SUPPORT CORROSION. LOCATED & INSTALLED SIX EACH NUTPLATES, ACP PER AMT.

Part: GUARD — LOOSE (DOOR 3L) · airframe 46,847 hrs · 13,062 cycles

3L WILL NOT ARM. SECURED LOOSE WIRE GUARD THAT WAS INTERFERING WITH DOOR OPERATION.

Part: CONTROLLER — FAULTY (CABIN TEMP) · airframe 46,775 hrs · 13,035 cycles

ALL 3 ZONES INOP LIGHTS 3 EICAS TEMP INOP. REPLACED ZONE TEMP CONTROLLER, TESTS OK.

Part: CONNECTOR — DIRTY (HYD PUMP) · airframe 46,635 hrs · 12,990 cycles

CREW REPORTS RIGHT ELEC HYD PUMP INOP. CLEANED ELECTRICAL CONNECTOR AT ACMP - PUMP WORKS OKAY.

Part: HOSE — SHEARED (ASPIRATOR)

SLIDE RECEIVED IN PACKED CONDITION. UPON DISASSEMBLY, FOUND INFLATION HOSE FITTING SHEARED AT ASPIRATOR. NO OTHER DISCREPANCIES NOTED. SUSPECT IMPROPER PACKING CAUSED FAILURE OF HOSE FITTING TO EXCESS PRESSURE APPLIED DURING PACK. REPLACED INFLATION HOSE AND PACKED IAW UAL AND OEM PACKING INSTRUCTIONS.

Part: SHUTOFF VALVE — FAULTY (RIGHT) · airframe 46,520 hrs · 12,954 cycles

RT ENG BLEED AIR VALVE 'OFF' LIGHT NOT ON WITH SWITCH 'ON' & ENG RUNNING. DUCT PRESS WAS NORMAL. REPLACED PRSOV AND PRSOV REG IAW MM. CHECKS GOOD ON ENGINE RUN.

Part: HINGE — DAMAGED (OVERHEAD BIN) · airframe 46,453 hrs · 12,931 cycles

13ABC BIN INOP. NO EMERGENCY EQUIPMENT INSIDE. REPLACED RT HINGE.

Part: CONTROLLER — MALFUNCTIONED (RT ENG BLEED) · airframe 46,430 hrs · 12,924 cycles

RIGHT BLEED VALVE DID NOT CLOSE WITH SWITCH. ONLY CLOSED WHEN ISOLATION VALVE IS OPEN AND LT BLEED OPEN, DEFERRED. REPLACED RT ENG BLEED REVERSE FLOW CHECK CONTROL ASSY. OPS CHECKED GOOD, NO FAULTS.

Part: CIRCUIT CARD — FAILED (RT ECS) · airframe 46,357 hrs · 12,900 cycles

APU BLEED VALVE CLOSES EARLY (31 PERCENT N2) DURING ENG START ON THE RT ENG LT ENG START NORMAL REPLACED RT ECS BLEED CONF CARD IAW WD. ACCOMPLISHED ENGINE START. OP CHECKED OK.

Part: O-RING — LEAKING (SPOILER ACTUATOR) · airframe 46,185 hrs · 12,851 cycles

NR 5 FLT SPOILER ACTUATOR HAS A RUNNING LEAK AT OUTBOARD PLUG. ACTUATOR OUT OF STOCK SFO. STILL TRYING TO GET IPC BREAKDOWN OF ACTUATOR TO CHECK FOR POSSIBLE PLUG O-RING PACKING. ALSO LEFT HYD SYSTEM RESERVOIR WILL NEED SERVICING AT .87. REPLACED O-RING ON LEAKING PLUG, LEAK CHECK GOOD.

Part: HANDLE — SEPARATED (COCKPIT WINDOW) · airframe 46,046 hrs · 12,812 cycles

CAPTAIN'S SLIDING WINDOW HAND CRANK FELL OFF. NEEDS CLAMP UP BOLT ASSY. PN ABC7313. NHA TORQUE LIMITER 170-0030 ON ORDER. ACCOMPLISHED UA-EVA-74048.

Part: SHUTOFF VALVE — DEFECTIVE (BLEED AIR SYS) · airframe 45,947 hrs · 12,784 cycles

NR 2 ENG BLEED WILL NOT CLOSE WITH SWITCH IN OFF WHILE ENG RUNNING. SUSPECT BAD VALVE OUT OF STOCK. T-S PER FIM. REPLACED PRSOV PER MM AND RAN ENG FOR LEAK CHECKS, ALL INDICATIONS CHECK NORMAL.

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 45,941 hrs · 12,782 cycles

APU BLEED VALVE OPENING AND CLOSING ON GND WITH R ENG BLEED CYCLING ON OFF WITH ENG SHUTDOWN. DUPLICATED PROBLEM. ISOLATED TO RT PRSOV. REPLACED PRSOV AND NO APU BLEED CYCLING NOTED.

Part: CIRCUIT CARD — DEFECTIVE (WEU) · airframe 45,591 hrs · 12,673 cycles

WEU TEST FAILED WITH WARN ELEX 'B' CB CLOSED AND 'A' CB OPEN. REPLACED CARD M983, NO HELP. TRIED NEW POWER SUPPLY, NO HELP. NEEDS MORE TROUBLESHOOTING. REPLACED CARD M983, TESTS OKAY.

Part: STATOR — FAULTY (L ENGINE) · airframe 44,637 hrs · 12,400 cycles

CREW REPORTED AFTER LT ENG START, STS MSG L ENG SEC CONTROL AND LT ENG REV CONTROL. IAW SAM S-DWN ENGINE, CLEARED MESSAGES, EPCS SHOWED (P) PDIU-[EEC] AND (P) 35 4-29, AFTER CLEARING MESSAGES, BOTH MESSAGES CAME BACK AFTER RESTART. REPLACED PMA, CHECKS OK.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 44,474 hrs · 12,353 cycles

CAPTAIN'S O2 MASK ASSY HAS LEAK. REPLACED MASK ASSY.

Part: WINDOW — CRACKED (COCKPIT) · airframe 44,084 hrs · 12,249 cycles

WINDOW DEFECT COCKPIT 2R BUBBLE OR CRACK ON OUTER WINDOW. LOCATION CENTER RT. 1 INCH LENGTH. REPLACED NR 2R SLIDING WINDOW LAMINATE AND REINSTALLED WINDOW. REPLACED WINDOW 2L IAW MM. CB PULLED AND LOCKED OUT FOR 2R WINDOW HEAT. RESET CIRCUIT BREAKER.

Part: CIRCUIT CARD — FAULTY (FLOW CONTROL) · airframe 43,770 hrs · 12,162 cycles

LEFT PACK OFF LIGHT AND LEFT PACK UPPER EICAS MESSAGE WITH PACK ON. R & R FLOW CONTROL CARD AY M863, NO HELP. R & R NR1 PACK VALVE ASSY, SYS TEST NORMAL.

Part: CONTROL VALVE — FAULTY (AC PACK) · airframe 42,922 hrs · 11,927 cycles

RIGHT PACK PROBLEMS. REPLACED RT FLOW CONTROL & SHUTOFF VALVE. RT PACK BITE DISPLAYED WITH PTC FAULTING FLOW CONTROL VALVE. VERIFIED FLT DECK TEMP HELD DESIRED TEMP WITH APU PNEUMATICS.

Part: EEC — MALFUNCTIONED (RT ENGINE) · airframe 42,635 hrs · 11,859 cycles

CREW REPORTS R ENG PRI CONT MSG. LOST EPR INDICATION AND AUTOTHROTTLE. CYC EEC ALT SW AND REGAINED EPR IND AND AUTOTHROTTLE BUT STILL HAVE R ENG PRI CONT MSG. REPLACED RIGHT ENG EEC. NO MESSAGES. OK FOR SVC.

Part: CONTROL VALVE — MALFUNCTIONED (RT A/C PACK) · airframe 42,635 hrs · 11,859 cycles

RIGHT PACK OFF LIGHT ON STAND BY-CIRCUIT BREAKER-RECYCLING SWITCH NO HELP NO OTHER INDICATIONS CYCLED RT PACK CONTROL BREAKERS PRIOR TO APU START UP. RIGHT PACK CAME ON LINE OK WITH NORMAL INDICATIONS AND BLEED PRESSURE INDICATIONS. PACK RAN OK ON GROUND PRIOR TO DISPATCH FOR ONE HOUR. REPLACED FLOW CONTROL VALVE. WITH RIGHT PACK SWITCH OFF NO PACK OFF LIGHT OR EICAS MSG. RECYCLED RIGHT PACK SWITCH OPERATED NORMAL

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 42,470 hrs · 11,816 cycles

F/A REPORTS EMERGENCY FLASHLIGHT INOP AT AFT GALLEY. REPLACED BATTERY.

Part: EEC — MALFUNCTIONED (NR 2 ENGINE) · airframe 42,390 hrs · 11,794 cycles

CREW REPORTS AFTER ENG START, RT ENG SEC CNTL EICAS MSG DISPLAYED, AND WOULD NOT CLEAR. REPLACED AND TESTED EEC ON NR 2 ENGINE. RAN ENGINE, NO MESSAGES.

Part: VALVE — MALFUNCTIONED (COCKPIT TEMP) · airframe 42,228 hrs · 11,740 cycles

AFTER AIRBORNE, COCKPIT TEMP WENT FULL HOT AND PACK 1 OUT TEMP WAS 124 DEG STBY C IS OK. ACFT TO RETURN TO GSO. REPLACED FLT DECK TRIM VALVE. REPLACED FLIGHT DECK ZONE TEMP SELECTOR, ZONE TEMP CONTROLLER, OPS CHECK GOOD. PROBLEM RECURRED. REPLACED FLOW CONTROL & SHUTOFF VALVE.

Part: HEAT EXCHANGER — FAULTED (RIGHT) · airframe 42,175 hrs · 11,718 cycles

RT PACK INOP RT PACK OFF LIGHT ON. RT PAC INOP. REPLACED COMP OUTLET OVERHEAT SWITCH, REPLACED PACK OVERHEAT SWITCH. REPLACED COMP OUTLET SENSOR. ACCMP PACK RUN AND CHECK. RT PACK INDICATION 30 DEGREES IN NORM WITH TEMP SEL 12 O'CLOCK. LT PACK INDICATION 10 DEGREES. THE LONGER THE RT PACK RUNS, THE GREATER THE PACK OUTLET TEMP DIFF. REPLACED H-E'S2 & ACP MM21-00-99 P601 AFTER REPLACEMENT.

Part: CONTROLLER — FAULTY (A/C PACK) · airframe 42,154 hrs · 11,711 cycles

RT PACK TRIPPED & PACK TEMP EICAS MSG WITH AFT CABIN TEMP MSG, FLIGHT DIVERTED. REPLACED COCKPIT TEMP SENSOR. REPLACED PACK TEMP CONTROLLER.

Part: CONTROL VALVE — FAULTY (RT AC PACK) · airframe 42,155 hrs · 11,712 cycles

BITE ON RT PACK CONTROLLER SHOWS PACK TEMP CONTROL VALVE, RTFL. REPLACED PACK TEMP CONTROL VALVE. WITH BOTH PACKS RUNNING RT PACK FLOW CONTROL VLV VISUAL INDICATOR SHOWS VLV 3-4 OPEN AND LEFT FCV INDICATOR SHOWS FULL OPEN. REPLACED RT FLOW CONTROL VALVE. REPLACED RIGHT PACK LOW LIMIT VALVE AND LEAK CHECK. OP CHECK NORMAL (P/N 3289696-1 - S/N 85). REPLACED RIGHT PACK ACM.

Part: WIRE — DAMAGED (POWER RECEPTICAL) · airframe 42,090 hrs · 11,688 cycles

EXTERNAL POWER PLUG CAUGHT FIRE AT POWER RECEPTACLE. REPLACED 2 EA INTERCOSTAL, WORKING PAN INSTALLATION THEN WIRING CONNECTS. PAN INSTALLED & SOLD. WIRING ROUTED, E&E RESTORED. POWER IS BACK ON ACFT & WRKG MISC OPS. REVERSER SLEEVES SWAPPED BET 1 & 2 ENG & WIRING OPS CHECKS. FIX ACCOMPLISHED ON WU S9954L.

Part: SHUTOFF VALVE — FAULTY (BLEED AIR SYS) · airframe 41,858 hrs · 11,617 cycles

RT PACK RIGHT DUCT PRESS 5 PSI LEFT 16 PSI. REPLACED HIGH STAGE PILOT AND HIGH PRESSURE SHUTOFF VALVE. OPS CHECKED NORMAL WITH ENG RUN.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 41,637 hrs · 11,548 cycles

DOOR 4R EXTERIOR SLIDE LIGHT INOPERATIVE. RELAMPED DOOR 4R EXTERIOR SLIDE LIGHT.

Part: FUEL TANK — LEAKING (LT WING) · airframe 41,220 hrs · 11,416 cycles

ON WALK AROUND FOUND FUEL AT LEFT WING DRY BAY AREA. REMOVED SEALANT, RETORQUED BOLTS ON FIBERGLASS PANEL. RESEALED WITH A1-2 AND B1-2 AT 0615 HRS. LEAK CHECKED TANK WITH 14K AND NO LEAKS FOUND AFTER 1 HR.

Part: LINE — LEAKING (PNEUMATIC SYS) · airframe 41,023 hrs · 11,355 cycles

DURING CLIMB RIGHT PACK INOP PACK OFF AND ENGINE BLEED OFF LIGHTS ILLUMINATED SIMULTANEOUSLY. PERFORM BITE CHECK ON CONTROLLER. NO FAULTS NOTED.REPAIRED TWO LEAKS IN PNEUMATIC LINES. RPL OVERHEAT SWITCH PRECAUTIONARY. RAN PACKS ON APU AND NR 2 ENG BLEED, NO FAULTS NOTED.

Part: STRUCTURE — LEAKING (LT WING) · airframe 40,674 hrs · 11,255 cycles

FUEL LEAKING FROM NR 1 ENGINE PYLON SKATE SUPPORT AREA. FUEL LEAKING IN THE ENCLOSED AREA OF PYLON ABOVE THE AFT SUPPORT STRUT. APPEARS TO BE COMING FROM FASTENERS THRU THE STRUT SUPPORT STRUCTURE INTO THE WING. LOCATED LEAK. SEALED WITH A1-2 AND B1-2 AT 1500 ON 4-7. NEEDS LEAK CHECK AFTER 12HR CURE. LEAK CHECK GOOD.

Part: SERVO — UNRELIABLE (RT YAW DAMPER) · airframe 39,872 hrs · 11,031 cycles

2 YAW DAMPER DISPLAYED ON EICAS & YAW DAMP INOP LIGHT ON (1=L, 2=R). CREW COMMENTS: R YAW KICKED OFF. REPLACED YAW DAMPER SERVO RT. OPS CHECK GOOD.

Part: SERVO — UNRELIABLE (RT YAW DAMPER) · airframe 39,872 hrs · 11,031 cycles

TWO YAW DAMPER DISPLAYED ON EICAS & YAW DAMP INOP LIGHT ON (1=L, 2=R). CREW COMMENTS: R YAW KICKED OFF. REPLACED YAW DAMPER SERVO RT. OPS CHECK GOOD.

Part: BPCU — FAILED (ELECTRICAL SYS) · airframe 39,707 hrs · 10,985 cycles

JUST PRIOR TO REACHING CRUISE, BOTH UTILITY BUSSES TRIPPED. SINGLE RESET OF BOTH UTILITY BUSES NO HELP. UTILITY BUSSES RESET 4 TIMES, NO HELP. REPLACED BPCU. SYS OPS NORMAL, ALL BUSSES RESET AND FUNCTION NORMALLY.

Part: CONTROL UNIT — FAULTY (LT ENG) · airframe 39,690 hrs · 10,979 cycles

LT GEN DRIVE LIGHT INOP. REPLACED LT GCU AND REPLACE BPCU. RAN NR1 ENG, OPS CK GOOD .

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,291 hrs · 10,879 cycles

DOOR 4 RT EMERGENCY EXIT LIGHT INOP (EXT). RELAMPED EMERGENCY LIGHT, OPERATES NORMAL.

Part: ANTI-ICE VALVE — FAULTY (LT ENGINE) · airframe 39,132 hrs · 10,837 cycles

WHEN LT ENG ANTI-ICE SWITCHED ON, VALVE INTRANSIT LIGHT FAILED TO COME ON BRIEFLY. REPLACED TAI VALVE. TESTED, WORKS FINE.

Part: REGULATOR VALVE — FAILED (BLEED AIR SYS) · airframe 39,058 hrs · 10,817 cycles

WHILE RE-ACTIVATING NR 2 ENG HS-PILOT FOUND OVERPRESSURE INDICATOR POPPED. RESET, RAN ENG AT IDLE. PRESSURE INDICATING 18 PSI. REF MEL 3611D BY- 118169: ACP'D PNEUMATIC HEALTH CK ON NR 2 ENG ON H-S PILOT, HPSOV, PRC, AND PRSOV. PRSOV CONTROLLER FAILED REF PRESSURE, PRESS EXCEEDED LIMIT. REPLACED PRSOV REGULATOR AND HIGH STAGE PILOT. OPS CHECKS NORMAL.

Part: CONTROLLER — MALFUNCTIONED (BLEED AIR SYS) · airframe 39,058 hrs · 10,817 cycles

WHILE REACTIVATING NR 2 ENG HS-PILOT FOUND OVERPRESSURE INDICATOR POPPED. RESET, RAN ENG AT IDLE. PRESSURE INDICATING 18 PSI. REF MEL 3611D BY- 118169. ACP'D PNEUMATIC HEALTH CK ON NR 2 ENG ON H-S PILOT, HPSOV, PRC, AND PRSOV. PRSOV CONTROLLER FAILED REF PRESSURE, PRESS EXCEEDED LIMIT.

Part: IDG — FAULTY (RT ENGINE) · airframe 39,058 hrs · 10,817 cycles

RIGHT IDG MSG AND LIGHT. RTFL. RAN ENGINES FOUND DC-A 23 FOR NR 1 AND 13 FOR NR 2. AFTER DISCONNECTING APU GEN, NR 2 TRIPPED OFF AND WOULD NOT RESET. TRIED SWAPPING GCU'S BUT GEN WOULD NOT COME ONLINE SWAPPING BACK GCU'S GEN NR 2 CAME ONLINE BUT TRIPPED BEFORE TRYING TO TRANSFER POWER. TRIED NEW GPCU, BUT GEN NR 2 AGAIN DID NOT COME ONLINE AND WOULD NOT RESET. REPLACED NR 2 IDG, OPS NORMAL.

Part: MAIN BEARING — FAILED (NR 2 ENGINE) · airframe 39,043 hrs · 10,811 cycles

STRONG ODOR OIL SMELL ON TAKEOFF DISSIPATED ON CLIMBOUT. REPLACED NR 2 ENGINE. MAIN BEARING FAILURE.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 39,043 hrs · 10,811 cycles

STRONG ODOR - OIL SMELL ON TAKEOFF DISSIPATED ON CLIMBOUT. REPLACED NR 2 ENGINE.

Part: APU — DEFECTIVE · airframe 38,733 hrs · 10,733 cycles

APU INOP. FOUND APU OIL TANK EMPTY. SERVICED TO FULL. STARTED APU AND FOUND HEAVY SMOKE COMING OUT OF TAIL PIPE. AFTER APU SHUTDOWN FOUND HUGE QUANTITY OF OIL IN APU EXHAUST SECTION. REPLACED APU. OPS AND LEAK CHECK GOOD.

Part: SENSOR — MISSING (APU) · airframe 38,669 hrs · 10,711 cycles

APU FAILED TO START. FAULT LIGHT ILLUM AND EICAS MSG. APU FAULT DISPLAYED. SECOND ATTEMPT INDICATES (SLOW ACCEL, HUNG START). FOUND MISSING HARDWARE SENSOR ON LT SIDE OF APU PLENNUM. NONE STOCKED AT IAD. UNABLE TO DETERMINE IF THE LISTED PARTS WILL COMPLETE THE REPAIR AS IPC DOES NOT SHOW VIEW INSIDE THE PLENUM. THE APU WAS REPLACED.

Part: SEAL — LEAKING (NR 1 ENGINE) · airframe 38,403 hrs · 10,638 cycles

NR 1 ENG HIGH OIL CONSUMPTION EXCEEDS LIMITS. REPLACED NR 1 ENG DEOILER SEAL. RAN ENGINE. NO LEAKS. NO LEAKS EVIDENT FROM SHAFT SEAL DRAINS.

Part: TRANSCEIVER — FAILED (HF COMM) · airframe 38,365 hrs · 10,628 cycles

RADIO PROBLEM. SHOP REPORT: FOUND INTERMITTENT RX. RPL Q6 & Q7 IN RX. REPLACED RT HF TRANSCEIVER.

Part: UNKNOWN — UNKNOWN · airframe 38,021 hrs · 10,533 cycles

CREW REPORT: W-RUDDER TRIM ZEROED, AIRCRAFT ROLLS RIGHT ON ROTATION. LEVEL FLIGHT REQ 2.5 UNITS LEFT RUDDER. *S/D* ACCOMPLISHED OPS CHK OF RUD PER AM 27-21-00. ALSO CHECKED SYS PER AMM 27-21-00 ITEM THRU PG 524 ITEM I ALL CHECKS NORMAL. REF AMIS PTT SEQ 0212016 AND 0212005. RUD TRIM WITHIN LIMITS PER AMM 27-01-00 PG 501 PARA A. NO REPEATS SINCE ORIGINAL.

Part: SENSOR — FAULTY (DOOR 2R GIRT BAR) · airframe 37,809 hrs · 10,474 cycles

SLIDE LIGHT AT 2R IS DIM. GIRT BAR AFT SENSOR SHORTED. REPLACED GIRT BAR AFT SENSOR, OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,784 hrs · 10,468 cycles

EXTERIOR EMERGENCY EXIT LIGHT INOP, DOOR 4L. LAMP INOP. RELAMPED ASSY, OPS CHECKED NORMAL.

Part: LAMP — WEAK (R2 DOOR) · airframe 37,541 hrs · 10,402 cycles

DOOR "ARMED" LIGHT NOT BRIGHT ENOUGH AT DOOR 2R. FOUND A WEAK LAMP. REPLACED LIGHT ASSY PER WDM 25-66-11 AND CLEANED PROX SWITCHES AND OPS CK GOOD.

Part: HOSE — DAMAGED (OXYGEN MASK) · airframe 37,446 hrs · 10,377 cycles

OXYGEN MASK HOSE DEFECTIVE AT 2 (1=CAPT, 2=1ST OF, 3= 1ST OBS). CREW COMMENTS: HOSE IS BROKEN. BROKEN MASK HOSE (UNKNOWN DAMAGE). REPLACED HOSE ASSY, OPS CHECKED GOOD.

Part: MODULE — FAILED (CABIN PRESSURE) · airframe 37,177 hrs · 10,305 cycles

CABIN PRESSURIZATION PROBLEM CAUSED DIVERSION. MAIN PWR SUPPLY T1 AND FLEX CABLE BAD. A1 CARD (CPU) FAILS LRU TEST 140760. REPLACED CABIN PRESSURIZATION MODULE., OPS CHECKED NORMAL.

Part: FILTER — DIRTY (COOLING FAN) · airframe 36,961 hrs · 10,246 cycles

INTERMITTENT EQUIPMENT OVERHEAT LIGHT. FOUND EQUIPMENT FAN SYSTEM FILTER DIRTY. REPLACED EQUIPMENT COOLING FAN FILTER, OPS NORMAL.

Part: WARNING HORN — FAULTY (APU FIRE DETECT) · airframe 36,434 hrs · 10,095 cycles

APU FIRE WARNING HORN INOP. FOUND HORN FAULTY. REPLACED APU FIRE WARNING HORN.

Part: CONTROL PANEL — SHORTED (HMG) · airframe 36,418 hrs · 10,091 cycles

HMG FAILED OP CHECK. HMG CONTROL PANEL SHORTING. REPLACED HMG CONTROL PANEL, OPS CHECKED OK.

Part: IDG — LOW (ENGINE) · airframe 35,964 hrs · 9,961 cycles

RIGHT GEN DRIVE LIGHT IS OUT WITH ENGINE SHUTDOWN. POSSIBLY A LOW OIL CONDITION (OVERHEAT). SERVICED IDG AND ACCOMPLISHED TEST RUN OF RIGHT IDG, NO LEAKS NOTED AND IDG WAS INDICATING NORMAL. NO REPEATS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,933 hrs · 9,951 cycles

EMERGENCY ESCAPE PATH LIGHT AFT LAV DOOR THRESHOLD IS INOP. ACCOMPLISHED REPAIR OF ESCAPE LIGHT PATH LIGHTING.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,047 hrs · 9,674 cycles

FWD LEFT OVERWING EMERGENCY HATCH & AFT LEFT OVERWING EMERGENCY HATCH LIGHTS ARE INOPERATIVE. RELAMPED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,047 hrs · 9,674 cycles

NR 4R EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED.

Part: ENGINE — STALLED (NR 1) · airframe 34,201 hrs · 9,413 cycles

RTFL DUE TO NR 1 ENGINE STALL. NR 1 ENG, WINDMILLING INSPECTION WAS ACCOMPLISHED AS PART OF TROUBLESHOOTING. FILTERS AND CHIPS FOUND CLEAN AFTER FIRST RECHECK. REPLACED EEC ALTERNATOR STATOR AND ROTOR.

Part: OXYGEN BOTTLE — DEFECTIVE (CABIN) · airframe 33,818 hrs · 9,316 cycles

BOTH O2 BOTTLES FROM ROW 34 USED. ONE APPEARS TO BE DEFECTIVE. [08-08-07] REPLACED DEFECTIVE 02 BOTTLE IN OVERHEAD BIN AT SEAT 34ABC.

Part: UNKNOWN — LOOSE (L/E SLAT) · airframe 33,715 hrs · 9,293 cycles

SOMETHING ON RIGHT SLAT IS LOOSE AND FLAPPING. [08-08-07] APPLIED FIBERGLASS SLAT REPAIR.

Part: CARBON SEAL — LEAKING (NR 1 ENGINE) · airframe 32,743 hrs · 8,993 cycles

NR 1 ENGINE HIGH OIL CONSUMPTION EXCEEDS LIMIT. [SUP 06-06-07] DEOILER CARBON SEAL AND OTHER SEAL RINGS REPLACED TO CORRECT OIL CONSUMPTION. DEOILER CARBON SEAL P/N 7A0449; SEAL RING P/N 7T0541; PMA CARBON SEAL P/N 7T0530 AND SEAL RING 7T0536; STARTER CARBON SEAL P/N 7T0527.

Part: FAN — ODOR (CABIN) · airframe 29,878 hrs · 8,188 cycles

HAZE AND BURNING PLASTIC ODOR ON DEPARTURE. CLEARED IN CRUISE. RETURNED ON FINAL. THE BURNING SMELL WAS ATTRIBUTED TO A FAILED RH RECIRCULATION FAN. REPLACED FAN AND THE PROBLEM WENT AWAY.

Part: LIFE VEST — INCORRECT (SEAT 25D) · airframe 26,773 hrs · 7,328 cycles

INFANT LIFE VEST INSTALLED AT SEAT 25D.

Part: FRAME — DENTED (FUSELAGE) · airframe 23,470 hrs · 6,341 cycles

FRAME FLANGE AT BS 1540 AND STR 25L DENTED. INSTALLED NESTED J-ANGLE REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 23,468 hrs · 6,340 cycles

EXTERIOR FUSELAGE SKIN AT STA 600 TO 620 BETWEEN STR 15L AND 18L HAS 8 EACH DENTS. PARTIAL SKIN REPLACEMENT ACCOMPLISHED. PARTIAL SKIN PANEL REMOVED AND NEW SECTION SPLICED IN USING SPLICE DOUBLERS AND TRIPLERS.

Part: FRAME — DENTED (FUSELAGE) · airframe 23,468 hrs · 6,340 cycles

AFT PIT STA 1460 AND STR 25L, FRAME IS DENTED ON THE INBD FLANGE. INSTALLED NESTED J-ANGLE REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 23,468 hrs · 6,340 cycles

AREA 20 INCHES AFT OF DOOR 3 RIGHT IS DAMAGED. SKIN WAS HFEC INSPECTED FOR CRACKS AND A DOUBLER REPAIR WAS INSTALLED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 23,468 hrs · 6,340 cycles

EXTERIOR FUSELAGE 2 FT AFT OF EE DOOR FROM STA 540 TO 580 IS DAMAGED. DAMAGE CAUSED BY IMPACT. TEMPORARY BLIND FASTENER REPAIR WAS INSTALLED. THIS REPAIR WAS REMOVED AND REPLACED WITH ANOTHER EXTERNAL DOUBLER REPAIR INSTALLED WITH PERMANENT SOLID FASTENERS.

Part: SKIN — DENTED (FUSELAGE) · airframe 17,184 hrs · 4,616 cycles

FOUND SMALL DENT AFT OF DOOR 3 RIGHT, ABOUT 20 INCHES AFT OF DOOR 3 RIGHT OUTSIDE EMERGENCY LIGHT. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.

Part: SHUTOFF VALVE — LEAKING (ENGINE BLEED) · airframe 8,637 hrs · 2,402 cycles

ENGINE BLEED DUCT PRESSURE SPLIT. SUPPLEMENTAL DATA UPDATE TWO PRSOV SYSTEM FLEX LINES, HIGH PRESURE SHUTOFF VALVE, HIGH PRESSURE CONTROLLER AND MUSCLE LINE O-RING WERE REPLACED. HIGH POWER RUN ACCOMPLISHED, OPS CHECKED OK.

Part: SKIN — TORN (FUSELAGE) · airframe 8,490 hrs · 2,363 cycles

LOWER FUSELAGE SKIN TORN APPROX 10 INCHES BY 1.5 INCHES TWO FEET AFT OF E&E COMPARTMENT DOOR. STATION 510 BETWEEN S-27L AND S-28L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE. ACCOMPLISHED SKIN REPAIR AND INSTALLED EXTERNAL DOUBLER REPAIR.

Part: WARNING LIGHT — ILLUMINATED (TAT PROBE) · airframe 4,127 hrs · 1,201 cycles

AIRCRAFT DIVERTED TO HNL DUE TO TAT LIGHT ILLUMINATION. *S/D* C/B FOUND POPPED AND WAS RESET FOR TAT PROBE HT, SYSTEM WAS TESTED WITH NO FURTHER MESSAGES, AND VERIFICATION FLIGHT WAS ACCOMPLISHED.