N502UA

Part: SKIN — DENTED (FUSELAGE) · airframe 100,359 hrs · 28,411 cycles

DENT ON ENTERIOR SKIN FROM INSIDE OUT FED OF AFT DRAIN MAST APPROX STSTION 1590 C/W HFEC PER NDT MANUAL PART 6, OF FUSELAGE DENT , EXTERIOR SKIN- INSIDE OUT , FWD OF AFT DRAIN MAST AT APPROX STA-1590. NO CRACK INDICATIONS NOTED AT THIS TIME. PERFORMED INTERIM REPAIR PER PART 1. ACCOMPLISH PART 3 PERMANENT REPAIR WITHIN 2 FLIGHT CYCLES. DENT IS LOCATED STA 1590 AND BETWEEN S25R AND 26R. MEASUREMENTS ARE APROX .020" OUTWARDS 2"X1" IN LENGTH. ACCOMPLISH PART 3 PERMANENT REPAIR WITHIN 2 FLIGHT CYCLES TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED RECORD UPDATE QC REVIEWED C/W HFEC PER NDT MANUAL PART 6, OF FUSELAGE DENT .FWD OF AFT DRAIN MAST AT APPROX STA-1590. NO CRACK INDICATIONS NOTED AT THIS TIME. FOR PART 3 STEP 3 OF EC/RA #:5330-06635 TOMCQC REV PERFORMED ACCOMPLISHED PART 3 PERMANENT REPAIR PER ECRA 5330-06635 NO DAMAGE NOTED AT THIS TIME. REOPEN SFO U070265 26OCT19 FOR: CLOSED PREMATURELY ECRA 5330-06635 HAS BEEN REVISED WITH REV A FOR ADDITIONAL REQUIREMENTS. PER ECRA 5330-06635 REV A WILL REQUIRE IMPROVED INTERIM REPAIR 1A WITHIN 2 CYCLES. AFTERWARDS ACCOMPLISH PART 2 EVERY 10 CYCLES AND PERMANENT REPAIR TO BE DETERMINED BY ESC WITHIN 28415 CYCLES. DIP LIMIT Y REF ECRA 5330-06635A; INSP PER PART 2 AT 10 CYC INTERVALS AND AC C PERMANENT REPAIR PER PART 3 NOT TO EXCEED 28,415 TTL FLT CYC. RECORDS UPDATE CANNING 51-00-01 FOR CRKS. NO CRKS FOUND AND AREA IS INTACT WITH NO OIL INSPECTED AREA AROUND DENT AND ACPD NDT HFEC PER B757 NTM ABOVE INSP WAS ACPD DUE TO ECRA 533

Part: SKIN — CHAFED (FUSELAGE) · airframe 100,359 hrs · 28,411 cycles

B757-53-3-6075 SUPPORT BRACKET CHAFING INTO AFT FUSELAGE SKIN PA NEL STA 1797 STR 17L. RL030 REF ST ENG N/R 0079023 BLENDED AND CHECKED LIMITS TO CHAFING AT AFT FUSELAGE SKIN PANEL STA 1797 S-17L L=2.5 W=.75 D=.030 OUT OF LIMITS IAW B757-2 SRM 53-80-70 PG 106 FIG 201 REPAIR 4. REPAIRED SKIN PANEL AT STA 179 7 S-17L IAW B757-2 SRM 52-80-70 REPAIR 4 PG 106 FIG 201. ORIG MA T THICKNESS .056. WORK ACCOMPLISHED, INSPECTED. COMPLETED AND ACCEPTED ST ENG INSP

Part: DEPRESSOR — DENTED (CARGO DOOR) · airframe 100,359 hrs · 28,411 cycles

B757-52-3-6063 FWD CARGO DOOR,AFT DEPRESSOR IS DENTED IN 2EA PLA CES.(96-18) REF. ST. ENGINEERING N/R 0079119 FOUND 2EA DENTS OUT OF LIMITS.REMOVED AND REPLACED FWD CARGO DOO R AFT DEPRESSOR IAW B757-200 SRM 51-40-02 AND SRM 51-70-11,AREA FOD FREE AND BOEING DRAWING 143N6603 REV B. WORK ACCOMPLISHED BY MECH AND INSPECTED COMPLETED AND ACCEPTED BY ST ENG INSP

Part: PAN — GOUGED (PAX DOOR) · airframe 100,359 hrs · 28,411 cycles

B757-06-3-2303 L-2 PASSENGER DOOR,EXTERNAL HANDLE PAN IS GOUGED. (96-32) REF.ST. ENGINEERING N/R 0079201 BLENDED AND CHECKED LIMITS TO L2 PASSENGER DOOR EXTERNAL HANDLE PAN: L=1.3",W=.10" D=.008". OUT OF LIMITS IAW B757-200 SRM 52-10 -01 AD1,FIG 101,DETAIL VI.REMOVED AND REPLACED EXTERNAL DOOR HAN DLE PAN P/N:654N0243-44,BATCH NO. 0003589661,PO NO SAG 1952051 I AW BOEING DRAWING 143N6100 REV K.WORK ACCOMPLISHED BY MECH AND INSPECTED BY COMPLETED AND ACCEPTED BY ST ENG INSP

Part: HOUSING — DAMAGED (L1 DOOR HANDLE) · airframe 100,359 hrs · 28,411 cycles

SUPPORT TASK SECONDARY FINDING UPON REMOVAL OF L1 DOOR HANDLE ME CHANISM BOX FOUND 2EA DAMAGE (GOUGE) AT CENTER HOLE SLEEVE. REF ST ENG N/R 0079475

Part: DOOR FRAME — DENTED (CARGO DOOR) · airframe 100,359 hrs · 28,411 cycles

B757-52-3-6063 FWD CARGO DOOR,AFT CORNER FRAME IS DENTED IN CENT ER. (96-19) REF. ST. ENGINEERING N/R 0079120 CHECKED LIMITS TO DENT AT FWD CARGO DOOR AFT CORNER FRAME; L=.70 ", W=.40",D=.023" OUT OF LIMITS IAW B757-200 SRM 52-30-02 AD1,DE TAIL V.REOVED AND REPLACED LOWER AFT CORNER FRAME P/N: 654N0244- 601,BATCH 0003589372, PO NO SAG1952053 IAW BOEING DRAWING 143N66 03 REF F WORK ACCOMPLISHED BY AND INSPECTED COMPLETED AND ACCEPTED BY ST ENG INSP

Part: DEPRESSOR — DENTED (CARGO DOOR) · airframe 100,359 hrs · 28,411 cycles

B757-52-3-6065 AFT CARGO DOOR,AFT DEPRESSOR IS DENTED AND HAS CH AFING ALONG ENTIRE EDGE.(96-09) REF. ST. ENGINEERING N/R 0079110 REMOVED AND REPLACED AFT CARGO DOOR AFT DEPRESSOR P/N: 146N6603- 114,BATCH NO 0003589133,PO NO. SOS1920224 IAW BOEING DRAWING 143 N6603 REV A. WORK ACCOMPLISHED BY MECH AND INSPECTED COMPLETED AND ACCEPTED BY ST ENG

Part: CUSP WEB — CORRODED (BS 1020-1040) · airframe 94,400 hrs · 27,235 cycles

MAIN DECK RT FLOOR CUSP WEB HAS AREAS OF CORROSION BETWEEN BS 1020 & 1040. FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13, ALLOWABLE DAMAGE 1, FIG 101, DETAIL V1. REMOVED AND REPLACED THE CUSP WEB IAW DRAWING 144N5140, AND SRM 51-40-02, PG 7.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,355 hrs · 27,226 cycles

FWD CARGO FLOOR SUPPORT STR RBL 7.5 BETWEEN APPROX BS 635 TO BS 700 HAS CORROSION ON UPPER AND LOWER SURFACE IN MULTIPLE AREAS. ACCOMPLISHED SEVERED SECTION REPAIR ON FLOOR STRINGER BETWEEN STA 688-704 RBL 7.5 IAW SRM 53-00-53 REPAIR 1, STR WAS FOUND OUT OF LIMITS FROM STA 690 RBL 7.5 TO STA 700 L=16.0 W=1.30 D=.016 IAW SRM 53-00-53.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,355 hrs · 27,226 cycles

AFT CARGO FLOOR SUPPORT STR LBL 10.4 AT APPROX BS 1330 HAS CORROSION. ACCOMPLISHED REPAIR ON AFT CARGO FLOOR SUPPORT STRINGER AT LBL 1 0.4 STA 1330 IAW SRM 53-00-53 REPAIR 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,355 hrs · 27,226 cycles

AFT CARGO FLOOR SUPPORT STR LBL 2.9 BETWEEN APPROX BS 1340 AND BS 1445 HAS CORROSION IN MULTIPLE AREAS. REMOVED CORROSION ON AFT CARGO FLOOR SUPPORT STRINGER LBL 2.9 BET STA 1346 AND STA 1445. BLEND OUT FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53 AD1. REMOVED AND REPLACED FLOOR SUPPORT STRINGER AT AFT CARGO LBL 2.9 STA 1342 TO 1486 IAW SRM 51-40-02 PARA 4B PG 2 AND PARA 7D PG 6-7 AND DRAWING 146N53 90 REV D.

Part: FLOOR SUPPORT — CORRODED (BS1200 RBL2.9) · airframe 94,355 hrs · 27,226 cycles

AFT CARGO FLOOR SUPPORT STR RBL 2.9 BETWEEN APPROX BS 1200 TO BS 1290 HAS CORROSION IN MULTIPLE AREAS. REMOVED CORROSION 3EA AREA FLOOR STR RBL 2.9 BETWEEN STA 1200-1 290 DIMENSION L=5 INCH X W=.400 X D=.063. FOUND 100" OUT OF LIMITS IAW SRM 53-00-53 FIG 101 DETAIL V 1)L=2 INCH X W=400 X D=.003 2)L=1 INCH W=400 X D=.004 3)L=2.5 INCH X W=400 X D=.00 2, MAT ORIGINAL THICKNESS .063 IAW BAC1517-2226, FOUND AREA WITHIN LIMITS IAW SRM 53-00-53 FIG 101, DETAIL V PG 105. REMOVED AND REPLACED FLOOR SUPPORT STRINGER AT AFT CARGO BETWEEN S TA 1200-1340 RBL 2.9 IAW SRM 51-40-02 PG 6 & DWG 146N54 10.

Part: FRAME — DENTED (FUSELAGE) · airframe 94,355 hrs · 27,226 cycles

AFT CARGO FRAME DENTED FS 1440 STR 26L. ACMP PERMANENT REPAIR ON AFT CARGO FRAME UPPER FLANGE AT FS 1440 STR 26L IAW SRM53-00-07 FG 201 REPAIR 5.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,355 hrs · 27,226 cycles

AFT CARGO FLOOR SUPPORT STR LBL 10.4 BETWEEN APPROX BS 1200 TO BS 1290 HAS CORROSION IN MULTIPLE AREAS. BLENDED CORROSION AFT CARGO FLOOR SUPPORT STR LBL 10.4 BETWEEN APPROX BS 120 - BS 1290. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53 ALLOWABLE DAMAGE 1 FIG 101 DETAIL V. REMOVED AND REPLACED STR P/N 146N5416-14 PO TUA0000063 IAW SRM 51-40- 02 DWG 146N5416.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,355 hrs · 27,226 cycles

FWD CARGO FLOOR SUPPORT STR LBL 10.4 BETWEEN APPROX BS 635 TO BS 700 HAS CORROSION ON UPPER AND LOWER SURFACE IN MULTIPLE AREAS 209-138 FWD CARGO FLOOR STRINGER AT LBL 10.4 STA 689-704 & SPLICE AT STA 704 & SPLICE AT STA 704 LBL 10.4. FOUND OUT OF LIMITS IAW SRM 53-00-53-A1 L=2.0 W=.75 D=.030. ACCOMPLISHED PERMANENT REP AIR TO STRINGER AT STA 684-704 AND REPLACE SPLICE AT STA 704 LBL 10.4 IAW SRM 53-00-53-R1 FIG 201 AND DWG 140N2749.

Part: FITTING — CORRODED (FUSELAGE) · airframe 94,355 hrs · 27,226 cycles

UPON REMOVAL OF AFT CARGO RT TRANSITION PANEL BET .1440 TO 1530 FOUND SHEAR CLIP CORROSION AT STA 1444 S27R. FOUND SHEAR CLIP TO BE OUT OF LIMITS AT STA 1444 STR 27R L 200"W L 200" D=.020 IAW SRM 53-00-04. RECEIVED NEW FABRICATED SHEAR CLIP P/N 146N5421 TO BE INSTALLED ON CARD 0011769 COPY ATTACHED.

Part: CABLE — OUT OF ADJUST (OVERWING EXIT) · airframe 94,355 hrs · 27,226 cycles

LT FWD AND AFT OVER WING EMERGENCY EXIT HATCH PRESSURE BOTTLE MANUAL BACK-UP CABLE FAILED OPERATIONAL CHECK. COMPLIED WITH 757-2-SUA AMM 25-65-06-702-075 (ADJUSTED) DIMENSION AT STEP E17. OPS CHECK "GOOD" ON LT FWD AND AFT OVER WING EMER G EXIT HATCH PRESS BOTTLE MANUAL BACK UP CABLE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,355 hrs · 27,226 cycles

FWD CARGO FLOOR SUPPORT STR RBL 10.4 SURFACE IN MULTIPLE AREAS, TO INCLUDE SPLICE AT BS 700, 209-141. REMOVE CORR ON FLOOR SUPPORT IN FWD CARGO STR RBL 10.4 STA 635-7 00. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53 FIG 4101 L=12" X W=9" D=.015 (R&R FLOOR SUPPORT) PER SRM 51-40-02 & DWG 140N2749 AND REMOVED CORR ON SPLICE ON FLOOR SUPPORT STR STA 700 RBL 10.4 L=8" X 7" YA=.004 ORIGL MATL .071 AND DWG 140N2749 FOUND TO BE WITHIN LIMITS PER SRM 53-00-53 FIG 101 DETAIL V.

Part: FLOOR SUPPORT — CORRODED (BS 1200-1290) · airframe 94,355 hrs · 27,226 cycles

AFT CARGO FLOOR SUPPORT LBL 2.9, BETWEEN BS 1200 TO 1290 HAS CORROSION IN MULTIPLE AREAS. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-53, REPAIR 1, ITEM 4.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,355 hrs · 27,226 cycles

AFT CARGO FLOOR SUPPORT STR RBL 2.9 AT APPROX 1330 HAS CORROSION 209-104 AFT CARGO SUPPORT STR RBL 2.9 FROM STA 1200-1360 WILL BE REPLACED ON NR:0011583 NO ACTION REQUIRED. CORROSION WAS FOUND ON EXISTING REPAIR ANGLE AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-A1 FIG 101 DUE TO BEING ON EXISTING REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,355 hrs · 27,226 cycles

AFT CARGO FLOOR SUPPORT STR LBL 2.9 AT APPROX BS 1330 HAS CORROSION. ACCOMPLISHED PERMANENT REPAIR ON AFT CARGO FLOOR STR AT STR 133 0 LBL 2.9 IAW SRM 53-00-53 REPAIR 1 FIG 201 DETAIL X.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,355 hrs · 27,226 cycles

CORROSION ON MAIN CABIN FLOOR HAT CHANNEL BETWEEN STA 310-332 RBL 33.36 RG31. (MATL LOSS .025 ORG .025) BLENDED OUT DAMAGE AREA ON FLOOR HAT CHANNEL (SUPPORT) ON MAIN CABIN BETWEEN STA 310-STA 332 RBL 33-R BL 36. AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETIAL III. REMOVED, FABRICATED AND REPLACED (SUPPORT) I AW DWG 141N5162 SRM 51-40-02 PG 21 FIG 4.

Part: FLOOR SUPPORT — CORRODED (BS 1290) · airframe 94,355 hrs · 27,226 cycles

AFT CARGO FLOOR SUPPORT, RBL 2.9, BS 1290 HAS CORROSION. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-53, REPAIR 1, FIG 201.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 94,355 hrs · 27,226 cycles

UPON REMOVAL OF AFT CARGO RT TRANSITION PANEL BET 1440 TO 1530 FOUND INTERCOSTAL UPPER ANGLE WITH CORROSION BET STA 1440 AND 146 0 BET S26R AND 27R MARKED 0117-04 FOUND INTERCOSTAL UPPER ANGLE OUT OF LIMITS IAW SRM 53-0 0-04 AT STA 1440 TO 1460 STR 26R L=.300" W=1.00" D=.028, RECEIVE D NEW PART P/N 146N5215-1 ANGLE, TO BE INSTALLED ON CARD 0011769 COPY ATTACHED.

Part: ANGLE — CORRODED (BS 1825) · airframe 94,355 hrs · 27,226 cycles

APU AIR INLET ASSY AND INLET OPENING SECURING INTERNAL ATTACH FLANG HAS SEVERAL AREAS OF CORROSION AS VIEWED THRU ACCESS 311AL ABOVE THE HORIZTONAL STAB CENTER SECTION. BLENDED THE CORROSION IAW SRM 53-80-15, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-80-15. REMOVED AND REPLACED THE STRAP AND ANGLES IAW SRM 53-80 -15, REPAIR 2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,355 hrs · 27,226 cycles

AFT CARGO FLOOR SUPPORT STR RBL 10.4 AT APPROX BS 1330 HAS CORROSION 209-105. AFT CARGO FLOOR SUPPORT STR RBL 10.4 FROM STA 1200-1360 WILL BE REPLACED ON NR:0011577, NO ACTION REQUIRED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,355 hrs · 27,226 cycles

CORROSION ON MAIN CABIN FLOOR SUPPORT UPPER SURFACE BETWEEN STA 720-740 RBL-62. REMOVED MAIN CABIN FLOOR SUPPORT BETWEEN STA 720-740 RBL-62 AND INSTALLED NEW FLOOR SUPPORT PN 143N5522-2 BATCH 0003237235 POS G1890018 IAW SRM 51-40-02 PG 2 AND SRM 51-40-02 PG 7 AD DRAWING 143N5522. ORIGINAL MAT THICKNESS .056" BLEND OUT DIMENSIONS ON FLOOR SUPPORT L=8" W=2" D=.025" OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETIAL III.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 94,355 hrs · 27,226 cycles

CORROSION ON MAIN CABIN FLOORBEAM UPPER SURFACE AT STA 377 FROM LBL - 48 TO LBL - 63. ACCOMPLISHED PERMANENT BLEND REPAIR FOR 5EA AREAS FOUND WITH CORROSION ON FLOORBEAM UPPER SURFACE AT STA 377 BETWEEN LBL 45 TO LBL 63 IAW EC/RA 5310-07343.

Part: SEAT TRACK — GOUGED (BS1186 RBL24) · airframe 94,355 hrs · 27,226 cycles

MAIN DECK SEAT TRACK CROWN HAS DAMAGE AT STA 1186 RBL 24 AS MARKED. REMOVED DAMAGE (GOUGE) AT MAIN DECK SEAT TRACK CROW AREA AT BS 1186 AND 24 RBL, WITH DIMENSIONS L=1.5" W=0.5" D=.027", EVALUATED AND FOUND OUT OF LIMITS IAW SRM 53-00-52. ALLOW DAMAGE 1, ACCOMPLISHED SEAT TRACK REPAIR BTW BS 1180/1240 AND RBL 24 IAW SRM 53-00-52 REP 3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,355 hrs · 27,226 cycles

FWD CARGO FLOOR SUPPORT STR LBL 16 BETWEEN APPROX BS 700 TO BS 635 HAS CORROSION ON UPPER AND LOWER SURFACE IN MULTIPLE AREAS TO INCLUDE SPLICE AT BS 700, 209-137. FWD CARGO FLOOR STRINGER AND SPLICE AT LBL 16 STA 635-700 OUT OF LIMITS IAW SRM 53-00-53-A1 L=3.0 W=1.0 D=.030. INSTALLED PERMANENT REPAIR ON STRINGER AND REPLACED SPLICE IAW SRM 53-00-53-R1 AND DWG 140N2749.

Part: STRAP — CRACKED (FUSELAGE) · airframe 94,355 hrs · 27,226 cycles

MAIN CABIN FWD FLOOR SUPPORT STABILIZATION STRAP BETWEEN APPROX BS 365 AND BS 377, RBL 24 CRACKED. REMOVED AND REPLACED STABILIZATION STRAP AT STA 365 TO 377 RBL 24 IAW SRM 53-00-51 REPAIR 12.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 94,355 hrs · 27,226 cycles

AFT CARGO FLOOR SUPPORT STR LBL 10 AT APPROX BS 1460 HAS CRACK AND MISSING FASTENER, 209-097/096. REMOVED AND REPLACED AFT CARGO FLOOR SUPPORT STRINGER P/N 146N5 47U19 AT LBL 10 BS 1446-1495 IAW DWG 146N5390.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,355 hrs · 27,226 cycles

AFT CARGO FLOOR SUPPORT STR LBL 7.5 BETWEEN APPROX BS 1200 AND BS 1340 HAS CORROSION IN MULTIPLE AREAS. BLENDED CORROSION AT AFT CARGO FLOOR SUPPORT STR LBL 7.5 BETWEEN APPROX BS 1200 AND BS 1340. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53 AD1 FIG 101 DETAIL V DWG NR BAC1517-2226. REMOVED AND REPLACED STRINGER P/N 19-5310-3-0023 PO NR TVA000006 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,355 hrs · 27,226 cycles

AFT CARGO FLOOR SUPPORT STR RBL 16.1 AT APPROX BS 1330 HAS CORROSION 209-106. ACCOMPLISHED PERMANENT REPAIR ON AFT CARGO FLOOR STR AT STA 133 0 RBL 16.1 IAW SRM 53-00-53 REPAIR 1 FIG 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 94,355 hrs · 27,226 cycles

FWD CARGO FLOOR SUPPORT STR LBL 10.4 BETWEEN APPROX BS 700 TO BS 845 HAS CORROSION ON UPPER AND LOWER SURFACE IN MULTIPLE AREAS. ACCOMPLISH SEVERED SECTION REPAIR ON FLOOR STRINGER BETWEEN 700- 780 LBL 10.4 IAW SRM 53-00-53 REPAIR 1. STR WAS FOUND OUT OF LIMITS FROM STA 700-780 LBL 10.4 L=1200 W=1.0 D=.015 IAW SRM 53-00-53.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 94,355 hrs · 27,226 cycles

UPON REMOVAL OF AFT CARGO RT TRANSITION PANEL BET STA 1440 TO 1530, FOUND INTERCOSTAL BET STA 1440 AND 1460 BET S26R AND S27R HAS CORROSION (SAA-117-011) FOUND INTERCOSTAL WEB OUT OF LIMITS AT STA 1440 AND STA 1460 STR 26R, L=5.00" W=3.00" D=.013. INSTALLED ON CARD 011769, COPY ATTACHED SRM 53-00-53 FOR OUT OF LIMITS.

Part: SKIN — CORRODED (FUSELAGE) · airframe 94,297 hrs · 27,213 cycles

UPPER FUSELAGE SKIN HAS CORROSION AT APPX B STA 1787 BETWEEN S4R AND S6R JUST FWD OF APU INLET DOOR AS MARKED 034-001 B757-53-3-6 042. REMOVED APU INLET DOOR, REPLACED SURROUNDING SKIN STRAP. REINSTALLED APU INLET DOOR IAW SUA 49-15-08-004-001, SRM 51-40-02, AMM 49-15-08-404-008 AND DWG 148N3138.

Part: SPRING — DEFECTIVE (EMERGENCY EXIT) · airframe 94,297 hrs · 27,213 cycles

MAIN CABIN FORWARD RIGHT EMERG EXIT EXTERNAL HANDLE, HANDLE ACCESS COVER HAS NO SPRING RETURN 056-021 REMOVED RT FWD EMERGENCY EXIT DOOR. REMOVED AND REPLACED HANDLE ACCESS COVER SPRING AND REINSTALLED DOOR IAW AMM 52-2 2-01-902-001, SRM 51-40-02 & AMM 52-22-01- 402-074. OPS CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 1290) · airframe 94,297 hrs · 27,213 cycles

AFT CARGO FLOOR SUPPORT RBL 10.4 AT BS 1290 HAS CORROSION. BLENDED AND FOUND TO BE OUT LIMITS IAW SRM 53-00-53, ALLOWABLE DAMAGE 1, STEP V, FIG 101. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, PG 7, PAR 7D.

Part: ANGLE — CORRODED (BS 1440-1460) · airframe 94,297 hrs · 27,213 cycles

UPON REMOVAL OF AFT CARGO RH TRANSITION PANEL, FOUND THE LOWER ANGLE CORRODED BETWEEN BS 1440 TO 1460, STRINGER 27R.. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02, PG 1-10, AND DWG 146N8522.

Part: FLOOR SUPPORT — DAMAGED (BS 630) · airframe 94,297 hrs · 27,213 cycles

FWD CARGO FLOOR SUPPORT RBL 7.5, BS 630 DAMAGED. REMOVED AND REPLACED THE FLOOR SUPPORT BETWEEEN BS 612 TO 633 IAW SRM 53-00-53, REPAIR 1.

Part: SKIN — DENTED (BS 600-620) · airframe 94,297 hrs · 27,213 cycles

ONE DENT, LT FUELAGE SKIN BETWEEN BS 600 TO 620, STRINGER 17L. REPAIRED THE SKIN IAW ECRA 5330-06299, PART 1.

Part: FRAME — CORRODED (FUSELAGE) · airframe 94,297 hrs · 27,213 cycles

UPON REMOVAL OF AFT CARGO RT TRANSITION PANEL BET 1440 TO 1530 FOUND RT FRAME UPPER FLANGE HAS CORROSION AT STA 1480 S26R MARKED 0117-07. REMOVED CORROSION AT AFT CARGO RT FRAME UPPER FLANGE AT FS 1480 STR 26R MATER LOSS OUT OF LIMITS OUT OF LIMITS PER SRM 53-00-07. REPAIRED DAMAGED AREA IAW SRM 53-00-07 FG 201 REPAIR 5 CAT B PERMANENT REPAIR.

Part: FRAME — DENTED (BS 1560) · airframe 94,297 hrs · 27,213 cycles

AFT CARGO FRAME DENTED AT BS 1560, STRINGER 25L. ACOMPLISHED A CAT B PERMANENT REPAIR IAW SRM 53-00-07, REPAIR 5, FIG 201.

Part: FLOOR SUPPORT — CORRODED (BS 1640-1681) · airframe 94,297 hrs · 27,213 cycles

CORROSION FOUND ON THE MAIN CABIN FLOOR SUPPORT UPPER SURFACE AND ATTACHED GUSSET BETWEEN BS 1640 - 1681, BL-0. REMOVED THE CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 53-00-51, FIG 101, DETAIL I II, ALLOWABLE DAMAGE 1. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 146N5651.

Part: FCU — MALFUNCTIONED (NR 2 ENGINE) · airframe 93,618 hrs · 27,083 cycles

EICAS MESSAGE FOR CENTER RT FUEL PUMP, RT ENGINE SHUTDOWN. REMOVED AND REPLACED THE FUEL CONTROL UNIT ON THE RIGHT ENGINE IAW AMM 7 3-21-01, OPS CHECKED GOOD . LEAK CHECKED GOOD

Part: SENSOR — FAULTY (OVERWING SLIDE) · airframe 92,664 hrs · 26,901 cycles

RT OVERWING SLIDE DOOR LOCKED SENSOR FAULTED. REMOVED AND REPLACED RT OVERWING SLIDE DOOR LOCKED SENSOR S10374 AFTER TROUBLESHOOTING IAW AMM 52-71-00-825-211, 32-09-04 -004-001, 52-71-99-200-801C1, AND B757-2 WDM 20-30-12. ADJUSTMENT CHECKED GOOD IAW 52-71-00-825-211, AND PSEU SYSTEM TESTED GOOD IAW AMM 32-09-04-404-009. EICAS MESSAGE CLEARED.

Part: DOUBLER — CORRODED (LAVATORY SERVICE) · airframe 92,658 hrs · 26,899 cycles

AFT LAVATORY SERVICE CONNECTOR, INTERNAL AREA WHERE THE TEE PLUMBING ATTACHES, HAS BLUE WATER STAINS AND SIGNS OF CORROSION. CLEANED THE AFT LAVATORY SERVICE CONNECTOR IAW EC/RA 2011-01000, REV U. CORROSION ON DOUBLER HAS 100% MATERIAL LOSS AROUND CUT OUT FOR PLUMBLING. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-40-02, PAR 4, FIGS 3 & 8.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,658 hrs · 26,899 cycles

L2, R2, AND LEFT FORWARD OVERWING LOWER EMERGENCY EXIT SIGNS INOPERATIVE. RESEATED CONNECTOR D6660 ON LEFT EFD OVERWING SIGN IAW BSOPM 20-42-01 AND REMOVED AND REPLACED INVERTER M10826 IAW SRM 51-40-02, PG 7, AND BSWPM 20-42-01. OP CHECKED GOOD IAW AMM 32-51-00-715-039.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 92,658 hrs · 26,899 cycles

R1 DOOR UPPER EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-07-022-020, AND 33-51-07-862-054. OPS CHECKED GOOD IAW AMM 33-51-07-862-036.

Part: STRINGER CLIP — GOUGED (BS 1400) · airframe 92,658 hrs · 26,899 cycles

INBD FRAME TO STRINGER ATTACH ANGLE AT BS 1400, STRINGER 29L FOUND GOUGED. REMOVED AND REPLACED THE STRINGER CLIP IAW DWG 140N2003, SRM 51-40-02, AND 51-4 0-05.

Part: FRAME — CORRODED (BS 1400) · airframe 92,658 hrs · 26,899 cycles

BS 1400 FRAME IN AFT CARGO HAS CORROSION ON BOTH FWD AND AFT SIDES, STRINGERS 26L - 26R. BLENDED THE CORROSION ON THE FRAME AND WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00 -07, FIG 101. REMOVED, FABRICATED, LOCATED, DRILLED & INSTALLED A NEW FRAME IAW SRM 51-40-02, PARA 4 & 7, FIG 3, 8, & 12 & 51-40-05, TABLE II.

Part: INTERCOSTAL — CORRODED (BS 1400) · airframe 92,658 hrs · 26,899 cycles

AFT CARGO INTERCOSTAL, BS 1400 - 1420 BETWEEN STR 29-30R HAS CORROSION. REMOVED THE CORROSION IAW SRM 51-10-02, FIG 1. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53, FIG 1 01, DETAIL IV, REMOVED AND REPLACED THE INTERCOSTAL IAW B757-200 51- 40-02 PARA 4, PARA 7, FIG 3, FIG 12

Part: LAMP — INOPERATIVE (L2 DOOR SLIDE) · airframe 92,572 hrs · 26,882 cycles

L2 DOOR SLIDE LIGHT NOT ILLUMINATING. REPLACED THE LAMPS.

Part: TIRE — BLOWN (RT MLG) · airframe 91,501 hrs · 26,674 cycles

ON FINAL APPROACH PLACED THE GEAR HANDLE TO DOWN POSITION. RECEIVED GEAR DISAGREE EICAS. RT GEAR DID NOT EXTEND. ACCOMPLISHED ALT GEAR EXT CHKLST. RIGHT GEAR CAME DOWN NORMALLY. FOUND NR 7 TIRE BLEWOUT CAUSE DAMAGE OF HYDRAULIC LINES NEAR CEILING ARE ABOVE RT MAIN LANDING GEAR. FOUND R GEAR TILT PRESSURE SWITCH CANNON PLUG BROKEN. REMOVED AND REPLACED CANON PLUG D3208 IAW SWPM 20-61-11. REMOVED AND REPLACED 3 EA HYDRAULIC LINES THAT WERE DAMAGED IPC REF 32-32-51-16 ITEMS 680,550, AND 705. NO OTHER BROKEN OR DAMAGED LINES NOTED UPON CLOSE INSPECTION. PERFORM MAIN LANDING GEAR EXTENSION AND RETRACTION CHK, REF AMM 33-32-00 AND ECRA 3232-01115 OPS CHK GOOD NO FAULT NOTED.

Part: CONTROL MODULE — MALFUNCTIONED (SPOILERS)

ABORTED TAKEOFF APPROACHING 125 KTS DUE TO SPOILER ALERT MESSAGE. REQUESTED FIRE/RESCUE FOR HOT BRAKES, TOWED TO GATE REPLACED SPOILER CONTROL MODULE 1R IAW MM 27-09-00, ACCOMPLISHED TAKEOFF CONFIG WARNING CARD MODULE TEST, AND LANDING CONFIG WARNING CARD MODULE TEST, REF MM 31-51-04, NO FAULTS NOTED

Part: TRIGGER — DEFECTIVE (L2 DOOR) · airframe 88,254 hrs · 26,038 cycles

DOOR 2L POWER ASSIST TRIGGER & SUPPORT HOUSING, DO NOT TURN TOGETHER IAW EA 5200-01204. REPLACE TRIGGER IAW AMM 52-11-32-401, EMER POWER TRIGGER MECHANISM REMOVAL & INSTALLATION. REMOVAL OF EMER POWER RESERVOIR IS REQUIRED TO RPLACE TRIGGERS IAW AMM 52-11-30-401. R & R DOOR 2L TRIGGER FORK IAW MM 52-11-32. OPERATIONS OK.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 88,196 hrs · 26,026 cycles

1L WINDSHIELD SHATTERED AT FL 360, DIVERTED. REPLACED 1L WINDSHIELD IAW MM 56-11-01.

Part: SKIN — DENTED (FUSELAGE) · airframe 81,071 hrs · 24,664 cycles

DENT IN EXTERIOR SKIN AT STATION 1695, ABOVE STRINGER 15R. CUT OUT DAMAGED AREA, INSTALLED REPAIR DOUBLER IAW ECRA 5330-04717. NEED TO ACCOMPLISH A PERMANENT REPAIR ON OR BEFORE 24 MONTHS.

Part: IDG — LOW (LT ENGINE) · airframe 83,932 hrs · 25,212 cycles

LEFT GEN DRIVE ON UPPER EICAS ON TAKEOFF ROLL, TAKEOFF ABORTED. SERVICED LT IDG TO FULL, RAN LT ENG NO LEAKS NOTED, LFT GEN CHECKED OK. RE-CHECK IDG FLUID AFTER 25 FLIGHT HOURS. DPI CHECKED OK, BPCU SHOWED NEED OIL & CLEARED AFTER.

Part: IDG — LOW (LT ENGINE) · airframe 83,917 hrs · 25,209 cycles

LEFT GEN DRIVE ON UPPER EICAS ON TAKEOFF ROLL, ABORTED AT 85 KNTS. SERVICED LT IDG TO FULL, RAN LT ENG, NO LEAKS NOTED, CHECKED OK.

Part: IDG — MALFUNCTIONED (LT ENGINE) · airframe 82,735 hrs · 24,983 cycles

LT GEN KICKED OFF LINE ON TAKEOFF ROLL. REPLACED IDG IAW AMM 24-1 1-01, OPERATIONS LEAK CHECKED OK.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 81,884 hrs · 24,820 cycles

DOOR 2L SLIDE ARM LT INOPERATIVE, AFTER PUSH BACK. RELAMPED & OPERATIONS NOW NORMAL.

Part: PANEL — FAULTY (FUEL SYSTEM) · airframe 81,544 hrs · 24,755 cycles

FUEL QUANTITY PANEL DIGITS NOT TESTING PROPERLY.

Part: CONTACTOR — FAULTY (APU) · airframe 81,391 hrs · 24,726 cycles

APU WILL NOT START, APU INOPERATIVE. REPLACED CONT BREAKER, REPLACED APU BATTERY, REPLACED APU CONTROLLER 2117342-20, SERIAL OFF = 15, REPLACED APU DOOR ACTUATOR & NO HELP. IAW DF198 FOR APU DOOR MESSAGE. REPLACED APU BATTERY CHARGER 8-930-03, SERIAL OFF = 313, APU DOOR RELAY, APU START RELAY, NO HELP. ON ELECT PAGE BATTERY READS ZERO. REPLACED RELAY 563-0208 CONTACTOR. TROUBLE SHOT WIRING DIAGRAM, NORMAL OPERATIONS NOTED. RESTARTED APU NO FAULTS WERE NOTED. REPLACED CONTACTOR 563-0208 IAW MM 49-41-05

Part: STARTER — FAULTY (APU) · airframe 81,209 hrs · 24,691 cycles

APU FAULT WILL NOT START. LAST 5 STARTS APUC SHOWED START ABORT, 11% N1, BATTERY VOLTAGE DURING CRANK WAS 22 VOLTS DURING MX START ATTEMPT. APU DOOR NOT DISPLAYED. APU, REPLACED STARTER & STARTER CLUTCH ASSEMBLY, OPERATIONAL CHECKED GOOD.

Part: FIRE BOTTLE — MISSING (COCKPIT) · airframe 81,125 hrs · 24,675 cycles

NO FIRE EXTINGUISHER IN COCKPIT. REPLACED FIRE BOTTLE IN BRACKET IN COCKPIT.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 81,094 hrs · 24,669 cycles

FLAP BACK LIGHTING INOPERATIVE ON CENTER PEDESTAL. NEED TO REPLACE LIGHT PLATE ASSEMBLY PCN 563-0157. LIGHTING IS NOT POWERED BY STANDBY BUS OR BATTERY BUS. R & R LIGHT PLATE ASSEMBLY, OPERATIONS CHECKED GOOD.

Part: TRANSCEIVER — FAILED (WEATHER RADAR) · airframe 81,074 hrs · 24,665 cycles

WX RADAR FAILURE. REPLACED RADAR R-T, TESTED OKAY.

Part: FAN — SEIZED (CARGO BAY) · airframe 81,071 hrs · 24,664 cycles

LT EQUIPMENT VENT FAN MOTOR SEIZED IN AFT CARGO BIN. LT AFT EQUIPMENT VENT FAN R & R IAW AMM 21-26-01. IAW LOG PAGE 9620033.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,071 hrs · 24,664 cycles

CORROSION ON LOWER FRAME BS 1701 AT RBL3 TO RBL6. CUT OUT DAMAGED AREA ON FRAME FAIL SAFE CHORD. FABRICATED & INSTALLED REPAIR PARTS IAW ECRA5310-05860.

Part: SKIN — DENTED (FUSELAGE) · airframe 81,071 hrs · 24,664 cycles

DENT IN EXTERIOR SKIN AT STATION 1695, ABOVE STRINGER 15R. CUT OUT DAMAGED AREA, INSTALLED REPAIR DOUBLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 81,071 hrs · 24,664 cycles

FLOOR BEAM BS 1640 HAS CORROSION ON THE TOP FLANGE. REMOVED DAMAGED TEE CHORD AREA, FABRICATED & INSTALLED TEE REPAIR & SPLICE ANGLES IAW ECRA 5310-05861.

Part: SKIN — DENTED (FUSELAGE) · airframe 81,071 hrs · 24,664 cycles

DENT IN EXTERIOR SKIN AT BS 1695, ABOVE STRINGER 15R. CUT OUT DAMAGED AREA, INSTALLED REPAIR DOUBLER IAW ECRA 5330-04717.

Part: CABLE — OUT OF ADJUST (R4 DOOR) · airframe 81,071 hrs · 24,664 cycles

R4 DOOR POWER RESERVOIR CABLE TRAVEL CHECK NOT WITHIN LIMITS. ADJUSTED ACTUATOR CABLE & TESTED.

Part: CABLE — OUT OF ADJUST (L4 DOOR) · airframe 81,071 hrs · 24,664 cycles

L4 DOOR POWER RESERVOIR CABLE TRAVEL CHECK NOT WITHIN LIMITS. ADJUSTED CABLE TRAVEL IAW AMM 52-11-36. INSTALLED L4 DOOR POWER RESERVOIR BOTTLE IAW AMM 52-11-30.

Part: SKIN — DENTED (BS 1610) · airframe 81,071 hrs · 24,664 cycles

SMALL DENT NOTED, LT SIDE, APPROXIMATELY BS 1610, 8 INCHES ABOVE WATERLINE. DENT MEASURES 1.25 X 1.5". REF SRM 53-00-01. DENT IS SMOOTH AND DOES NOT IMPACT ANY STRINGER OR FASTENERS. OUTSIDE SRM LIMITS, REMOVED DAMAGED SKIN, INSTALLED REPAIR DOUBLER REF SRM 51-20-01.

Part: CONTROL PANEL — OUT OF POSITION (SWITCH PANEL) · airframe 80,582 hrs · 24,570 cycles

EMERGENCY EXIT SWITCH PANEL IS IN THE WRONG LOCATION SHOULD BE ABOVE ENGINE START PANEL. FOUND EMERGENCY PANEL PLACED WHERE ENG START PANEL SUPPOSE TO BE. RESWAPED PANELS, CHECKED OK.

Part: PROXIMITY SENSOR — INTERMITTENT (L1 DOOR) · airframe 80,413 hrs · 24,538 cycles

DOOR 1L SLIDE ARMED LIGHT INTERMITTENT. VERIFIED GIRT BAR ENGAGE SLIDE LIGHT INTERMITTENT. PLACARDED SLIDE LIGHT. CKD DOOR CKS OK. REPLACED PROXIMITY SENSOR S10214.

Part: LIGHT — UNSECURE (SEAT 8A) · airframe 80,265 hrs · 24,510 cycles

EMERGENCY LIGHT LOOSE AT SEAT 8A. SECURED LIGHT.

Part: CABLE — DAMAGED (EMERGENCY LIGHT) · airframe 79,887 hrs · 24,439 cycles

EMERGENCY LIGHT INOPERATIVE ON SEAT 23C. REPLACED SEAT CABLE. OP CHECKED GOOD.

Part: CONNECTOR — LOOSE (LT FUEL CONTROL) · airframe 77,209 hrs · 23,924 cycles

LEFT ENGINE PRI CONT STATUS MESSAGE. CREW SHUTDOWN ENGINE, FOLLOWING EPCS MESSAGES (P) FCU-EEC, (P) FCU-F-B INT, 350-20. CLEARED MESSAGES, UPON RESTART LT ENG PRI CONT RE-APPEARED WITH FCU-EEC. RETURNED TO BASE. FOUND CONNECTOR LOOSE ON FCU. CLEANED & SECURED CONNECTOR. RAN ENGINE TWICE PER JRH 2-5-1 NO DEFECTS NOTED DURING RUN.

Part: OVERHEAT SENSOR — LOOSE (AC BAY) · airframe 76,908 hrs · 23,866 cycles

EICAS MSG-EQPT OVHT & EQPT CLG FAN- OVERHEAT LIGHT ILLUMINATED. OVERHEAT LIGHT REMAINED ILLUMINATED WHEN ALTN WAS SELECTED. RIGHT PAC DISCHARGE TEMP BECAME LOOSE FROM DUCT CAUSING PAC TO OVERHEAT, AFTER TEMP INSTALLATION OF SENSOR PAC TEMP NORMAL AND EQT COOLING TEMP NORMAL DEFER ITEM CREATED TO INOP RT PAC PENDING REPAIR OF SENSOR. RAN ENGINE 3 ATTEMPTS USING ALL IGN PER JRH2-5-1. ALL INDICATIONS WHERE OK AND ENGINES STARTED NORMALLY.

Part: STATIC WICK — MISSING (RUDDER) · airframe 76,511 hrs · 23,790 cycles

A/C ENCOUNTERED LIGHTNING STRIKES. FOUND UPPER RUDDER STATIC WICK MISSING. REPLACED STATIC WICK.

Part: POTABLE WATER — CONTAMINATED · airframe 76,511 hrs · 23,790 cycles

WATER IN ENTIRE ACFT HAS FOUL ODOR AFFECTING TEA AND COFFEE BADLY. SERVICED WATER SYSTEM TWICE AND FLUSHED LINES IN INTERIOR OUT. WATER TASTES GOOD.

Part: FAN — NOISY (COCKPIT) · airframe 76,226 hrs · 23,736 cycles

RECIRC NEEDS TO BE DEFERRED FOR A-C ACCEPTANCE. VERY NOISY, INTERFERES W COCKPIT COMM RT RECIRC FAN INOP IN ADDITION AFT GALLEY CHILLER. PER MEL 2125E. ACCOMPLISHED SERVICE TIP PER MM 21-22-00, AUDIBLE LEVEL WITHIN LIMITS PER MM PARG (1-7).

Part: GIRT BAR — DIRTY (L1 DOOR) · airframe 75,923 hrs · 23,678 cycles

DOOR 1L WILL NOT ARM. CLEANED GIRT BAR AREA & CYCLED DOOR HANDLE. DOOR ARMED OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,834 hrs · 23,661 cycles

EMERGENCY LIGHT AT 8AB INOP. REPLACED EEL LIGHT, OPS CHECK OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,834 hrs · 23,661 cycles

EMERGENCY LIGHT AT SEAT 20AB INOP. REPLACED EEL LIGHT, OPS CHECK OKAY.

Part: LIGHT — LOOSE (CABIN) · airframe 75,834 hrs · 23,661 cycles

OVERHEAD EMERGENCY LIGHT NEAR ROW 15 INOP. LAMP LOOSE. SECURED LAMP, OPS CHECK OKAY.

Part: LIGHT — MALFUNCTIONED (L2 DOOR) · airframe 75,339 hrs · 23,567 cycles

DISARM LIGHT DOOR 2L ON ALL THE TIME. CYCLED DOOR ARM AND DISARM HANDLE. SLIDE LIGHT OPERATES NORMALLY.

Part: LIGHT — MISSING (CABIN) · airframe 75,135 hrs · 23,529 cycles

EEL LIGHTS MISSING ON SEATS 6B AND 10B AND 8B LOOSE. REPLACED MISSING LIGHTS AND SECURED LOOSE ONE, OPS CHECK GOOD.

Part: MECHANISM — OUT OF ADJUST (R4 DOOR) · airframe 74,819 hrs · 23,467 cycles

MAIN CABIN R-4 DOOR MODE SELECTOR LEVER FAILS MIDWAY CHECK. ADJUSTED MAIN CABIN R-4 DOOR MODE SELECTOR LOCKOUT MECHANISM AND LINKAGE TO GIRT BAR MECHANISM PER MM ON NON ROUTINE 26845.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 74,819 hrs · 23,467 cycles

EXTERNAL FUSELAGE SKIN LIGHTNING STRIKE 9 EACH AT BS 454 TO BS 458 AND STR 28R ARE OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. TRIMMED OUT DAMAGED SKIN AND FABRICATED A FREEZE PLUG, REPAIR DOUBLER AND FILLER PER TIMCO REO G14130, REV D & INSTALLED ON NON ROUTINE 25520. A NEW CF WILL BE GENERATED PER EVA 81428 FOR 24 MONTH DTA REQUIREMENT.

Part: ATTACH FITTING — DEFECTIVE (TE FLAP) · airframe 74,819 hrs · 23,467 cycles

LEFT WING OUTBOARD FLAP OUTBOARD FLAP TRACK, UPPER ATTACH FITTING TO FLAP MISSING 2 EACH MOUNT BOLTS. REF BOEING CMM 57-53-76, IPL FIGURE 1, SHEET 11 OF 18, ITEM'S 470 AND 473, 2 LOWER HI-LOKS. REMOVED FLAP AND INSTALLED MISSING FASTENERS, REFERENCE NON ROUTINE 25450. FASTENERS REPLACED AS PART OF OUTBOARD FLAP FRONT SPAR WEB REPAIR ACP'D ON 085625 NON ROUTINE 26543.

Part: LATCH — FRAYED (EVAC SLIDE) · airframe 74,819 hrs · 23,467 cycles

MAIN CABIN L-2 DOOR SLIDE HARNESS IS FRAYED. REMOVED AND REPLACED THE SLIDE HARNESS LATCH, P-N 416N2500-9 PER MM 25-66-01 ON NON ROUTINE 25422.

Part: PRESSURE DECK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,819 hrs · 23,467 cycles

MAIN CABIN BS 1680 AND RBL 31, EXISTING AFT PRESSURE DECK REPAIR DOUBLER IS CORRODED. FABRICATED, A TAPERED SHIM AND A FILLER PER TIMCO REO G14118, REV B AND INSTALLED ON NON ROUTINE 25856. THIS IS A CATEGORY A REPAIR, REF EVA 81386.

Part: LATCH — FRAYED (EVAC SLIDE) · airframe 74,819 hrs · 23,467 cycles

MAIN CABIN R-1 DOOR SLIDE HARNESS IS FRAYED. REMOVED AND REPLACED SLIDE HARNESS LATCH PER MM ON NON ROUTINE 25430.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 74,819 hrs · 23,467 cycles

THE FWD INTERCOSTAL, REF P-N 143N8338U26, NUMBER 11 AT R-2 DOOR CUTOUT SURROUND STRUCTURE IS CRACKED. REMOVED AND REPLACED INTERCOSTAL P/N 143N8338-26 ON NON ROUTINE 26063.

Part: HARNESS — FRAYED (EVAC SLIDE) · airframe 74,819 hrs · 23,467 cycles

MAIN CABIN L-4 DOOR SLIDE HARNESS IS FRAYED. REMOVED AND REPLACED HARNESS PER MM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 74,819 hrs · 23,467 cycles

EXTERNAL FUSELAGE SKIN AT BS 440, STR 18R TO STR 19R HAS LIGHTNING STRIKE OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SKIN AND FABRICATED AND INSTALLED A REPAIR DOUBLER AND FILLER PER TIMCO REO G14135, REV A ON NON ROUTINE 25858. PER EVA 81370, THIS REPAIR REQUIRES DTA ANALYSIS FROM BACO AND A NEW 8100-9 MUST BE ISSUED WITHIN 24 MONTHS FROM 04OCT 11. THIS ACFT WILL BECOME UNAIRWORTHY UNLESS A NEW FAA 8100-9 IS RECEIVED ON OR BEFORE 04OCT2013.

Part: FLOORBOARD — BUCKLED (CABIN) · airframe 74,819 hrs · 23,467 cycles

CABIN CARPET BUCKLE DOOR-2R MID-CABIN FWD GALLEY. CREW COMMENTS: GALLEY FLOOR HAS LARGE DENT NEAR DOOR 2R. TEMP REPAIR FOR FLOORBOARD 4357211-123 PG 801, STAINLESS STEEL SHEET USED WITH SEALANT. SHOULD RPLC FLOORBOARD AT NEXT C CHECK. REMOVED AND REPLACED FLOORBOARD P-N A357211-123 ON NON ROUTINE 25406.

Part: LINK — WORN (L2 DOOR) · airframe 74,819 hrs · 23,467 cycles

L2 DOOR UPPER HINGE LINK WORN. REMOVED AND REPLACED L2 DOOR UPPER HINGE LINK PER MM.

Part: PAN — GOUGED (R4 DOOR HANDLE) · airframe 74,819 hrs · 23,467 cycles

EXTERNAL DOOR HANDLE PAN ASSY IS GOUGED BEYOND LIMITS AT THE R4 DOOR. REMOVED & REPLACED HANDLE PAN ASSY PER SRM AND REINSTALLED HANDLE BOX PER SM-50-52-11-06-JD.

Part: COLLAR — WORN (L1 DOOR) · airframe 74,819 hrs · 23,467 cycles

L1 DOOR HOLD-OPEN LOCK WORN. REMOVED & REPLACED L1 DOOR HOLD OPEN LOCK COLLAR PER MM.

Part: LINK — WORN (L1 DOOR HINGE) · airframe 74,819 hrs · 23,467 cycles

L1 DOOR UPPER HINGE LINK WORN. REMOVED & REPLACED L1 DOOR UPPER HINGE LINK PER MM.

Part: BEARING — SEIZED (L2 DOOR) · airframe 74,819 hrs · 23,467 cycles

L2 DOOR EMERGENCY POWER ASSIST QUADRANT BEARINGS SEIZED. REMOVED QUADRANT & QUADRANT BEARING, CLEANED, REINSTALLED & LUBED BEARING. REINSTALLED QUADRANT PER MM AND GNMM 4-0-3-010 AND FOUND THE ACTUATION LEVER AND CAM ASSEMBLY TURNED FREELY PER MM.

Part: COLLAR — WORN (L2 DOOR) · airframe 74,819 hrs · 23,467 cycles

L-2 PASSENGER DOOR HOLD OPEN LOCK WORN. ORDERED HOLD OPEN LOCK COLLAR KIT P-N 654N0244-9. REMOVED & REPLACED L-2 DOOR HOLD OPEN LOCK COLLAR KIT PER MM ON NON ROUTINE 26515.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 74,819 hrs · 23,467 cycles

THE FORWARD INTERCOSTAL, REF P/N 143N8334U28, NUMBER 12 AT R-2 DOOR CUTOUT SURROUND STRUCTURE IS CRACKED. REMOVED & REPLACED DOOR FRAME (INTERCOSTAL WEB), P/N 143N8334U28, ON NON ROUTINE 26064.

Part: CYLINDER — OUT OF ADJUST (PAX DOOR) · airframe 74,819 hrs · 23,467 cycles

R4 DOOR, EMERGENCY POWER SPRING CYLINDER IS OUT OF ADJUSTMENT, NO RED BAND. ADJUSTED POWER SPRING CYLINDER PISTON RED BAND PER MM.

Part: LOCK — WORN (R1 HOLD OPEN) · airframe 74,819 hrs · 23,467 cycles

R1 DOOR HOLD OPEN LOCK WORN. REMOVED AND REPLACED DOOR HOLD OPEN LOCK PER MM.

Part: HARNESS — FRAYED (R2 DOOR SLIDE) · airframe 74,819 hrs · 23,467 cycles

MAIN CABIN R2 DOOR SLIDE HARNESS IS FRAYED. REMOVED & REPLACED MAIN CABIN R-2 DOOR SLIDE HARNESS PER MM.

Part: FRAME — DENTED (CARGO BAY) · airframe 74,819 hrs · 23,467 cycles

FORWARD CARGO BAY, MAIN FRAME4 DENTED ON INBOARD FLANGE. TRIMMED OUT DAMAGED AREA OF FLANGE, FABRICATED A REPAIR DOUBLER AND INSTALLED PER SRM 53-00-07, REPAIR 5. MAJOR REPAIR.

Part: CYLINDER — OUT OF ADJUST (R2 DOOR) · airframe 74,819 hrs · 23,467 cycles

R2 DOOR EMERGENCY POWER SPRING CYLINDER IS OUT OF ADJUSTMENT. ADJUSTED EMERGENCY POWER SPRING CYLINDER PISTON RED BAND PER MM.

Part: SHAFT — WORN (DOOR HOLD OPEN) · airframe 74,819 hrs · 23,467 cycles

R1 DOOR HOLD OPEN LOCK SPLINED SHAFT WORN AND DAMAGED. REMOVED & REPLACED HOLD OPEN LOCK SPLINE SHAFT PER MM AND OPS CHECKED GOOD.

Part: CYLINDER — OUT OF ADJUST (L2 DOOR) · airframe 74,819 hrs · 23,467 cycles

L2 DOOR EMERGENCY POWER SPRING CYLINDER PISTON IS OUT OF ADJUSTMENT. ADJUSTED POWER SPRING CYLINDER PISTON RED BAND PER MM.

Part: CYLINDER — OUT OF ADJUST (L1 DOOR) · airframe 74,819 hrs · 23,467 cycles

L1 DOOR EMERGENCY POWER SPRING CYLINDER IS OUT OF ADJUSTMENT. ADJUSTED POWER SPRING CYLINDER RED BAND PER MM.

Part: SKIN — DENTED (BS 400 S15L) · airframe 74,819 hrs · 23,467 cycles

BS 400 S15L SKIN IS DENTED AND CREASED. DENT FOUND TO BE OUT OF LIMITS PER SRM. CUT OUT DAMAGED SKIN AND FABRICATED A REPAIR DOUBLER AND FILLER AND INSTALLED PER SRM 53-0 0-01, REPAIR 2, TABLE V, MAJOR REPAIR.

Part: CABLE — LACK OF LUBE (RT OVERWING) · airframe 74,819 hrs · 23,467 cycles

THE RT AFT OVERWING MANUAL EMERGENCY BACKUP CABLE IS BINDING AND FAILED CHECK PER ROUTINE JIC 5R25I1366. LUBED RT AFT OVERWING MANUAL EMERGENCY BACKUP CABLE PER MM.

Part: INVERTER — FAULTY (NR 1) · airframe 74,559 hrs · 23,415 cycles

WHILE TROUBLE SHOOTING THE BATTERY CHARGER EICAS STATUS MESSAGE. FOUND THE STATIC INVERTER EXTREMELY HOT TO THE TOUCH. SUSPECT THE STATIC INVERTER IS CAUSING THE CHRONIC PROBLEM . REPLACED STATIC INVERTER PER MM, SYSTEM TESTED OKAY.

Part: LUG — DEFECTIVE (CABIN) · airframe 74,532 hrs · 23,410 cycles

ALL SIDEWALL LIGHTS AND FWD-AFT GALLEY LIGHTS ARE INOP. REPLACED K100075 & K100064, NO HELP. SUSPECT S10299. REPLACED LUG ON WIRE 9162-12 INSIDE P37 PANEL PER WDM. ALL SIDEWALL LIGHTS AND ENTRY & GALLEY LTS OP NORMAL WITH GROUND SVC OR FULL A-C POWER.

Part: APU — SMOKE (APU BAY) · airframe 74,532 hrs · 23,410 cycles

AT GATE IN SFO, APU WAS HASTILY SHUT DOWN WHEN MECH NOTICED HEAVY BLUE SMOKE COMING FROM THE EXHAUST. ACCOMPLISHED APU PERFORMANCE CHECK, OPERATION NORMAL. NO FAULTS.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,458 hrs · 23,396 cycles

DOOR 2L OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY AT DOOR 2L, OPS CHECKED NORMAL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,458 hrs · 23,396 cycles

EMERGENCY EXIT EXIT SIGN INOPERATIVE. BATTERY REPLACED, OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,458 hrs · 23,396 cycles

EMERGENCY LIGHT INOPERATIVE. RELAMPED, OPS CHECKED OK.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,458 hrs · 23,396 cycles

DOOR 2 GALLEY WALL MOUNTED EMERGENCY LIGHT INOPERATIVE. BATTERY REPLACED, OPS CHECKED NORMAL.

Part: FLOORBEAM — CORRODED (BS 324) · airframe 73,972 hrs · 23,300 cycles

FWD GALLEY FLOORBOARDS POPPING UP DUE TO FLOORBEAM CORROSION AT STA 324. MANUFACTURED AND INSTALLED FLOORBEAM REPAIR PER UA-EVA-80904.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,972 hrs · 23,300 cycles

SEAT 26 EMERGENCY LIGHT INOPERATIVE, PER A-CHECK. REPLACED LAMP ASSEMBLY, OPS CHECK OKAY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,972 hrs · 23,300 cycles

SEAT 24 EMERGENCY LIGHT INOPERATIVE, PER A-CHECK. REPLACED EMERGENCY LIGHT LAMP, CHECKED OKAY.

Part: STRUCTURE — DIRTY (R2 DOOR) · airframe 73,586 hrs · 23,227 cycles

CANNOT ARM DOOR 2R. CLEANED LOWER DOOR AREA DISARM AND ARM DOOR, OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (R4 DOOR) · airframe 73,495 hrs · 23,210 cycles

RT DOOR 4 EMERGENCY SLIDE LIGHT IS INOP. RELAMPED, OPS CK OK.

Part: FLOORBOARD — BUCKLED (CABIN) · airframe 73,464 hrs · 23,204 cycles

CABIN CARPET BUCKLE DR-2R MID-CABIN FWD GAL. GALLEY FLOOR HAS LARGE DENT NEAR DOOR 2R. TEMP REPAIR FOR FLOORBOARD 4357211-123, STAINLESS STEEL SHEET USED WITH SEALANT. SHOULD REPLACE FLOORBOARD AT NEXT 'C' CHECK.

Part: BALLAST — DEFECTIVE (EMERGENCY LIGHT) · airframe 71,636 hrs · 22,857 cycles

RT AFT OVER THE WING DOOR EMERGENCY EXIT SIGN LIGHT INOP. REPLACED SIGN ASSY DUE BALLAST DEFECTIVE, PN 11-5833-3, IAW MM. OPS CHECK GOOD.

Part: TERMINAL — LOOSE (WINDSHIELD) · airframe 70,786 hrs · 22,687 cycles

R1 WINDSHIELD NEED TO BE CHANGED DUE TO J1 TERM FOUND LOOSE. REPLACED WINDSHIELD PER MM, OPS OKAY.

Part: ACCESS PANEL — LEAKING (LT WING) · airframe 70,087 hrs · 22,555 cycles

FUEL LEAKING FROM FUEL TANK ACCESS DOOR LT WING. LT WING FUEL PLATE 541EB REMOVED DUE PLATE DOME NUT HSG CRACK. REPLACED FUEL PLATE IAW MM. NEW SEAL ON HAND. NEW PANEL SEALED AND INSTALLED NEED ADDITIONAL 3 HRS CURE TIME PRIOR TO REFUELING. OK FOR SERVICE.

Part: RESERVOIR — LOW PRESSURE (L4 DOOR) · airframe 69,786 hrs · 22,498 cycles

MED 4L PASSENGER DOOR EMERGENCY POWER RESERVOIR PRESSURE IS LOW AT 2,100 PSI. REPLACED RESERVOIR PER MM.

Part: LATCH — BROKEN (SLIDE COVER) · airframe 69,775 hrs · 22,496 cycles

DOOR 2L ESCAPE SLIDE COVER DOES NOT HAVE THE LATCH STRAP ENGAGED IN THE CENTER LATCH. REMOVED COVER, FOUND LATCH BROKEN, REMOVED LATCH.

Part: SKIN — CHAFED (L WING IB FLAP) · airframe 68,960 hrs · 22,335 cycles

LT WING IB FLAP OTBD SIDE CHAFING ON NR 5 SPOILER. MAJOR REPAIR ACCOMPLISHED: REPAIRED FLAP UPPER SKIN. ACP RII INSPECTION ON FLAP SKIN REPAIR.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 68,960 hrs · 22,335 cycles

MID GALLEY EMERGENCY LIGHTS INOPERATIVE. TROUBLESHOT AND FOUND WIRE BROKEN BELOW KICK STRIP AT MID GALLEY. REPAIR WIRE AT KICK STRIP, OPS CHECK.

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,990 hrs · 22,335 cycles

RT FWD OVERWING EXIT NORMAL FLOURESCENT LIGHT OUT. REPLACED FLOURESCENT LAMPS AND BALLAST ON AFT LIGHT. OPS CHECK GOOD.

Part: GATE — CORRODED (L1 DOOR) · airframe 68,960 hrs · 22,335 cycles

L1 DOOR LOWER GATE CORRODED AND CRACK. REMOVED AND REPLACED DOOR 1L LOWER GATE. OPS CHECK WILL BE ACP ON C-CK ROUTINE JC.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,960 hrs · 22,335 cycles

LT AFT OVERWING EXIT EMERGENCY EXIT LIGHT OUT. RELAMPED AND OPS CHECKED THE LT AFT OVERWING EXIT EMERGENCY EXIT LIGHT. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,879 hrs · 22,320 cycles

EMERGENCY LIGHT IN-OP AT DOOR NR 5 RT. REPLACED LIGHT BULB. OPS CHECKED OK FOR SERVICE.

Part: SLIDE — UNSERVICEABLE (CABIN)

LOWER TUBE BLEW ON OVERPRESSURE TEST. OP TUBE FAILURE SENT TO OEM.

Part: CONNECTOR — BROKEN (CABIN) · airframe 66,172 hrs · 21,800 cycles

PASSENGER CABIN SEAT 18AB EMERGENCY LIGHT INOP. FOUND MOLEX CONNECTOR BROKEN. REPLACED CONNECTOR REF BSWPM 20-64-17. OPS CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,172 hrs · 21,800 cycles

LEFT FWD OVERWING EXIT EMERGENCY LIGHT INOP. RELAMPED LT OVERWING EXIT EMERGENCY LIGHT AND OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,705 hrs · 21,524 cycles

EMERGENCY LIGHTS AT SEAT 15C AND 18C ARE INOP. REMOVED BOTH LIGHTS FROM THE SEATS. REPLACED 2EA LIGHT ASSYS.

Part: BALLAST — ODOR (GALLEY LIGHTS) · airframe 63,991 hrs · 21,389 cycles

NOTICED ODOR FROM MID GALLEY OVERHEAD LIGHTS. TURNED OFF SWITCH ODOR DISSIPATED. REPLACED 2EA BALLAST. OPS NORMAL.

Part: CONTROL UNIT — INTERMITTENT (L/E FLAP) · airframe 62,677 hrs · 21,138 cycles

LEADING EDGE FLAP DISAGREE INDICATION. RTFL SFO. FSEU INTERMITTENT FAILURES. REPLACED FSEU NR 3 AND RIGGED PDU TRANSMITTER AND LEFT SLAT TRANSMITTER. OPS CHECKED OK.

Part: BULB — WRONG PART (CABIN) · airframe 62,346 hrs · 21,076 cycles

DOOR 2L AND 2R LOWER EMERGENCY LIGHTS INOP. FOUND SMALL OVERHEAD EMERGENCY LIGHT IN MID GALLEY ON VERY DIMLY. IT HAD A 1308 BULB IN IT. SHOULD BE A 1317 BULB. RELAMPED WITH CORRECT BULB. ALL EMERGENCY LIGHTS AT DOOR 2L & 2R CHECKED OKAY.

Part: FLAP — DENTED (LT WING) · airframe 61,847 hrs · 20,982 cycles

LEFT WING, INBOARD FLAP, OUTBOARD LOWER TRAILING EDGE IS DENTED. PERFORMED REPAIR ON AREA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,903 hrs · 20,803 cycles

DOOR 3R SLIDE LIGHT WILL NOT ILLUMINATE. FOUND BATTERY PACK WEAK AND NOT CHARGING. REPLACED BATTERY PACK AND CHARGER. ALL SYSTEMS FUNCTION/TEST NORMALLY.

Part: SOCKET — BROKEN (EMERGENCY LIGHTS) · airframe 60,903 hrs · 20,803 cycles

EMERGENCY ESCAPE LIGHT INOP 18C, SEAT MOUNTED. FOUND DAMAGED SOCKET. REPAIRED SOCKET, RELAMPED OPS CHECK NORMALLY.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 60,903 hrs · 20,803 cycles

EMERGENCY ESCAPE LIGHT INOP 26C, SEAT MOUNTED.

Part: LIGHT — MISSING (CABIN) · airframe 60,067 hrs · 20,645 cycles

EMERGENCY LIGHT MISSING AT SEAT 15C.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,067 hrs · 20,645 cycles

EMERGENCY LIGHTS INOP AT SEAT 5B.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,022 hrs · 20,444 cycles

EEL STRIP AT ROW 15ABC INOPERATIVE. [06-22-07] REPLACED 15 ABC EEL STRIP. OPS CHECK OK.

Part: SILL — DIRTY (FUSELAGE) · airframe 58,953 hrs · 20,431 cycles

DOOR 3R WOULD NOT ARM. [06-20-07] CLEANED DEBRIS FROM DOOR SILL AREA. ATTRIBUTED THIS DISCREPANCY TO IMPROPER SKIRTING UNDERNEATH DOOR AND INADEQUATE CLEANING.

Part: PILOT VALVE — FAILED (ENGINE) · airframe 58,687 hrs · 20,380 cycles

RTFL DUE TO SMOKE IN COCKPIT. [SUP 06-06-07] FOLLOWED SOP AND SHUTDOWN UTILITY BUSSES, ODOR AND SMOKE DISSIPATED SLIGHTLY. INSPECTION OF NR 1 ENG FOUND EVIDENCE OF OIL COMING OUT OF 2.8 COMPRESSOR BLEEDS AT 6 O'CLOCK & OUT OF 8TH STG BLEED PNEUMATIC DUCTS. ALSO FOUND METAL DEBRIS IN 8TH STG CHECK VALVE. REPLACED PILOT VALVE AND HIGH STAGE VALVE. REPLACED NR 1 ENGINE. THE EXACT CAUSE OF THIS IRREGULARITY COULD NOT BE ESTABLISHED.

Part: FIRE LOOP — SHORTED (NR 1 NACELLE) · airframe 58,396 hrs · 20,319 cycles

NR 1 ENGINE NR 1 FIRE LOOP SHORT ABOVE FIRE WALL DISCONNECT SHORT APPEARS TO BE IN THE PYLON. [06-14-07] NR 1 ENGINE FIRE LOOP SHORT IN PYLON. ACCOMPLISHED SHIELDING REPAIR.

Part: RADAR — INOPERATIVE (WX SYSTEM) · airframe 55,614 hrs · 19,788 cycles

DIVERTED DUE TO INOP WEATHER RADAR. WX RADAR COMPLETELY INOP PER CREW, TRIED CYCLING RADAR OFF AND ON AND CYCLING CB F2 ON OVHD PNL WITH NOLUCK. REPLACED WX RADAR TRANSCEIVER.

Part: PDU — VIBRATION (TE FLAPS) · airframe 51,775 hrs · 19,004 cycles

RETURNED TO FIELD DUE TO AIRCRAFT VIBRATION. TE FLAP PDU DID NOT FUNCTION PROPERLY. REPLACED SUBJECT PDU.

Part: FRAME — DENTED (FUSELAGE) · airframe 51,076 hrs · 18,906 cycles

AFT PIT FUSELAGE FRAME IS DENTED AT STA 1480 STR 25L. CUT OUT DAMAGE AND ACP HFEC WITH NO CRACK INDICATION. PER GSO TIMCO REO G10464, FABRICATED RPR AND INSTALLED.

Part: SKIN — DENTED (FUSELAGE) · airframe 51,076 hrs · 18,906 cycles

FUSELAGE SKIN DENTED STA 600 STR 17L DENT IS APPROX 3 INCHES BY .067 DEEP. RMV DAMAGE AREA AND ACP HFEC WITH NO CRACK INDICATION FABRICATED REPAIR AND INSTALLED PER MM 53-30-92

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 51,076 hrs · 18,906 cycles

AFT CABIN FLOOR SHEAR WEB DOUBLER IS CORRODED STA 1681, RBL 48-55. REMOVED EXISTING REPAIR, REMOVED CORROSION INSTALLED DOUBLER REPAIR PER REO-G10512C AND SRM51-20-01

Part: FRAME — CORRODED (FUSELAGE) · airframe 51,076 hrs · 18,906 cycles

AFT PIT FRAME PREVIOUS REPAIR IS CORRODED AT STA 1600 - STR 25L TO 27L. REMOVED DAMAGE AND FABBED NEW PRODUCTION SPLICE AND ANGLE REPAIR AND INSTALLED PER REO-G10504B AND SRM51-40-02 AND EVA-50287.

Part: FRAME — DENTED (FUSELAGE) · airframe 51,076 hrs · 18,906 cycles

AFT PIT FUSELAGE FRAME IS DENTED AT STA 1520, STR 25L. REMOVED DAMAGE AND INSTALLED J ANGLE REPAIR PER RE0-G10463, EVA-50283, AND SRM51- 40-02.

Part: FRAME — GOUGED (FUSELAGE) · airframe 51,076 hrs · 18,906 cycles

FRAME STA 1520 FROM STR 22R TO 25R IS GOUGED FROM SCREWS IN 6 PLACES. REMOVED DAMAGE AND ACP HFEC NO CRACKS INDICATED. PER REO G10474 FABRICATED NESTLED ANGLE REPAIR AND INSTALLED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 51,076 hrs · 18,906 cycles

AFT CARGO INTERCOSTAL IS CORRODED BS 1360 TO 1380 RBL 26. REMOVED CORROSION AND FABRICATED INTERCOSTAL RPR AND INSTALLED PER SRM 53-00-04 AND BAC DWG 146N5427

Part: SKIN — DENTED (FUSELAGE) · airframe 51,076 hrs · 18,906 cycles

LEFT SIDE OF ACFT BETWEEN FR 740 & 760 STRS 15L AND 16L HAS 1 DENT. FABRICATED DOUBLER RPR PER SRM 53-00-01 AND INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 51,076 hrs · 18,906 cycles

FWD GALLEY STA 365 RBL 11 FLOORBEAM TOP IS CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS. FABRICATED ANGLE REPAIR IAW MM 53-00-98 AND INSTALLED PER MM 53-00-98

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 51,076 hrs · 18,906 cycles

AFT CABIN FLOOR SHEAR WEB IS CORRODED AT STA 1681 LBL 60. REMOVED CORROSION AND FABRICATED NEW TEE CAP. REPAIRED AND INSTALLED PER MM 53-00-98

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 49,308 hrs · 18,566 cycles

FLOORBEAM AT STA 324 RBL 60 IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED FLOORBEAM CHORD SPLICE REPAIR.

Part: LINE — RUPTURED (DOWNLOCK ACTUA) · airframe 37,693 hrs · 14,276 cycles

AT 8 MIN AFTER TAKEOFF THE LEFT HYDRAULIC QUANTITY EICAS MSG FOLLOWED BY LEFT HYD RSR AND LEFT HYD PRESS LIGHTS CAME ON. SUPPLEMENTAL DATA UPDATE REPLACED LEFT MLG DOWNLOCK ACTUATOR PRESSURE LINE.

Part: VALVE — FAILED (NLG) · airframe 37,431 hrs · 14,181 cycles

NOSE GEAR GREEN DOWN LIGHT FAILED ON APPROACH. *S/D* REPLACED NOSE DOOR SEQUENCE VALVE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,713 hrs · 13,911 cycles

FIVE FEET FORWARD OF DOOR 2 LEFT HAS A 14 INCH DENT WITH A 9 INCH CRACK IN SKIN. *S/D* REPAIRED PER SRM 53-00-01 FIGURE 204.

Part: SENSOR — FAILED (TEMP CONTROL) · airframe 36,530 hrs · 13,843 cycles

FLIGHT DECK TEMPERATURE UNCONTROLLABLE. *S/D* REPLACED THE RIGHT MIX MANIFOLD AND PACK TEMPERATURE SENSORS WITH NEW SENSORS. ALSO, REPAIRED BROKEN GROUNDING JUMPER AT THE RIGHT PACK TEMPERATURE SENSOR.

Part: UNKNOWN — ODOR (CABIN) · airframe 35,672 hrs · 13,529 cycles

WEAK ELECTRICAL SMELL IN THE MID GALLEY AREA. ODOR DISAPPEARED WHEN RT RECIRCULATION FAN SWITCHED OFF. *S/D* THE RECIRCULATION FANS AND GALLEY AREAS WERE CHECKED FOR POSSIBLE SOURCES OF THE SMELL. NO DISCREPANCIES WERE FOUND. HOWEVER, A PIECE OF PLASTIC WAS FOUND IN THE INLET IN THE AFT GALLEY OVEN. SINCE PLASTIC WAS REMOVED, NO ADDITIONAL WRITE-UPS FOR THE ODOR HAVE OCCURRED.

Part: SEQUENCE VALVE — DETERIORATED (NLG) · airframe 35,120 hrs · 13,302 cycles

UNABLE TO PERFORM NORMAL GEAR EXTENSION. ACCOMPLISHED MISSED APPROACH AND PERFORMED ALTERNATE EXTENSION PROCEDURE. *S/D* NOSE GEAR DOOR SEQUENCE VALVE HAD DETERIORATED O RING AND BACKUP RING REQUIRING LONGER THAN NORMAL THROW OF THE SPOOL VALVE. REPLACED DOOR SEQUENCE VALVE. (ORIGINAL VALVE).

Part: BATTERY PACK — DISCHARGED (CABIN)

SEVERAL EMERGENCY LIGHTS OUT, RT OVERWING AREA. REPLACED BATTERY PACK, AT STATION 985, IN THE RT PSU SPACER PANEL PER MM 33-51-07.

Part: TEMP SENSOR — FAILED (BLEED AIR)

WHEN SELECTING WING ANTI-ICE, BLEED WOULD BACK DOWN AND GET BLEED TRIP AND BLEED OFF LIGHT. SMELL IN CABIN. WHEN ANTI-ICE SHUTOFF, BLEED GOES BACK TO NORMAL CONDITION AND SMELL NOT NOTICED. *S/D* REPLACED FAN AIR TEMPERATURE SENSOR.

Part: INDICATOR — INOPERATIVE (FUEL SYST)

ON FINAL APPROACH, A FUEL CONFIGURATION MESSAGE ILLUMINATED. REPORTED AND ACTUAL FUEL DID NOT MATCH. *S/D* RIGHT LOWER WING FUELING LOAD SELECT INDICATOR WAS INOP. REPLACED THE LOAD SELECT INDICATOR PER 757MM 28-41-06. SYSTEM OPERATED NORMAL AFTER REPLACEMENT.

Part: SEALS — LEAKING (RT ENGINE)

RIGHT ENGINE OIL CONSUMPTION EXCEEDS LIMIT. *S/D* CARBON SEALS FOR STARTER AND FUEL PUMP REPLACED, OPERATIONS CHECK OK.

Part: T1 BLADE — FAILED (RT ENGINE)

RETURNED TO FIELD DUE TO NUMBER TWO ENGINE HIGH EGT. *S/D* FOUND TYPE 55 T1 BLADE FAILED IN FLIGHT. REMOVED RIGHT ENGINE AND REPLACED THE FAILED BLADE.