N562UA

Part: COMPUTER — FAULTY (AUTOPILOT SYS) · airframe 69,477 hrs · 25,521 cycles

AFTER TWO, CONTINUOUS LT & RT YAWING UP TO FL280 LIKE BOTH YAW DAMPERS INOPERATIVE BUT NO EICAS OR LIGHTS. R & R RT YAW DAMP COMPUTER IAW AMM 22-21-04, OPERATIONS CHECKED NORMAL. PERFORMED MCDP TEST 30 IAW AMM 22-00-02, NO FAULTS NOTED, AIRCRAFT REMAINS FULL CAPABILITY.

Part: CONNECTOR — LOOSE (CABIN) · airframe 69,412 hrs · 25,504 cycles

DOOR 1R OVERHEAD EXIT LIGHT INOPERATIVE. FOUND LOOSE CONNECTOR AT M730 POWER PACK. SECURED OPERATIONS CHECKED NORMAL IAW AMM.

Part: POWERPACK — INOPERATIVE (CABIN) · airframe 69,412 hrs · 25,504 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT SECTION FROM ROW 27 TO 36. REPLACED POWER PACK S735 IAW AMM 33-51-00 OPERATIONS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,412 hrs · 25,504 cycles

EMERGENCY EXIT LIGHT STRIP BY FIRST CLASS CLOSET INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT TAPE & COVER, OPERATIONS CHECKED NORMAL IAW AMM.

Part: POWERPACK — INOPERATIVE (CABIN) · airframe 69,412 hrs · 25,504 cycles

EMERGENCY EXIT LIGHT SECTION AT ROW 23 INOPERATIVE. REPLACED POWER PACK S735 IAW AMM 33-51-00 OPERATIONS CHECKED NORMAL.

Part: LIGHT — UNSECURE (ROW 20) · airframe 69,406 hrs · 25,502 cycles

EXIT PATH LIGHTING AT ROW 20 UNSECURE. SECURED EMERGENCY EXIT LIGHT COVER. LIGHTS TESTED OK.

Part: UNKNOWN — MALFUNCTIONED (AUTOPILOT SYS) · airframe 69,355 hrs · 25,485 cycles

PLANE YAWING BACK & FORTH DURING CLIMB. OSCILLATION STOPS WITH LT YAW DAMPER OFF.

Part: STARTER — SEIZED (NR 2 ENGINE) · airframe 69,041 hrs · 25,378 cycles

RT ENG HUNG START THEN RT ENG STARTER EICAS ON 2ND ATTEMPT. FOUND NR 2 ENG STARTER SEIZED. INSP GEARBOX AFTER OLD STARTER OFF, NO DAMAGE FOUND. INSTALLED NEW STARTER, OPERATIONS CHECKED GOOD. SECURED NR 2 ENGINE FAN COWLING.

Part: WIRE — BROKEN (CABIN) · airframe 68,881 hrs · 25,331 cycles

EMERGENCY EXIT LIGHT AT 21 ABC HAS A BROKEN ELECTRICAL WIRE. REPLACED CONNECTOR, OPERATIONS CHECKED OKAY.

Part: LENS — MISSING (L4 DOOR) · airframe 68,881 hrs · 25,331 cycles

AFT LT EXIT DOOR "ARMED" LIGHT MISSING. LENS ASSEMBLY IS MISSING, COULD NOT LOCATE. REPLACED DOOR 4 LEFT LENS CAP ASSEMBLY IAW AMM 52-11-96.

Part: SMOKE GOGGLES — DAMAGED (COCKPIT) · airframe 68,759 hrs · 25,292 cycles

FIRST OFFICER'S & CAPTAIN'S SMOKE MASKS ELASTIC STRETCHED OUT, UNABLE TO GET A TIGHT FIT. REPLACED BOTH SMOKE GOGGLES.

Part: COMPRESSOR — VIBRATION (POTABLE WATER) · airframe 68,626 hrs · 25,255 cycles

CREW REPORTS H20 COMPRESSOR VIBRATES. COMPLIED WITH MEL 3810B, CB K 21 IS COLLARED. PLACARD IS ON WATER GAUGE, DF123. ALL FAUCETS OPERATE NORMALLY WITH BLEED PRESSURE. REPLACED AIR COMPRESSOR PER AMM, OPS CHECKED OKAY.

Part: BLADE — NICKED (NR 1 ENGINE) · airframe 68,450 hrs · 25,192 cycles

NUMEROUS BLADES ON NR 1 ENGINE HAVE NICKS. REPAIRED BLADES IAW AMM, EDDY CURRENT ACCOMPLISHED.

Part: WINDOW — DELAMINATED (R3) · airframe 68,355 hrs · 25,165 cycles

R3 WINDOW DELAMINATED. DELAMINATION IS 2.875 INTO THE CLEAR VIEW OF THE WINDOW. REPLACED WINDOW.

Part: GAUGE — INACCURATE (WATER TANK) · airframe 68,237 hrs · 25,126 cycles

WATER TANK GAUGE IS NOT ACCURATE. FILLED AND DRAINED AND FILLED AGAIN POTABLE WATER TANK. FOUND GALLEY INDICATOR READING INCORRECTLY. REPLACED FWD GALLEY QTY IND IAW AMM. BOTH GALLEY AND SERVICE PANEL IND. READING ACCURATELY.

Part: INDICATOR — INACCURATE (COCKPIT) · airframe 67,896 hrs · 25,019 cycles

FWD CABIN TEMP DISPLAY READS INCORRECTLY AT 50 DEGREES. REPLACED ZONE TEMP INDICATOR, OPS CHECKED NORMAL.

Part: COVER — LOOSE (CABIN) · airframe 67,334 hrs · 24,852 cycles

FLOOR EEL STRIP CLEAR COVER IS LOOSE FROM ROW 30-35. SECURED EEL STRIP COVER.

Part: SMOKE GOGGLES — MISSING (COCKPIT) · airframe 67,258 hrs · 24,832 cycles

SMOKE GOGGLES MISSING AT OBSERVERS SEAT. INSTALLED SERVICEABLE SMOKE GOGGLES.

Part: SKIN — DENTED (BS 1610-1615) · airframe 67,221 hrs · 24,820 cycles

DENT ON RIGHT SIDE OF FUSELAGE BS 1610-1615 ON STR 17R. FOUND DENT TO BE OUT OF LIMITS, IAW SRM 53-00-01 DET III. REMOVED DAMAGE, INSTALLED DOUBLER PER SRM 53-00-01, FIG 201, REPAIR 2. MAJOR REPAIR.

Part: RADOME — ERODED (NOSE) · airframe 67,221 hrs · 24,820 cycles

RADOME, EXTERNAL SURFACE AND LIGHTING STRIPS ERODED AT APPROXIMATELY 12 AND 230 POSITIONS. REMOVED AND REPLACED AND ADJUSTED RADOME IAW MM. MAJOR REPAIR

Part: SMOKE DETECTOR — NO TEST (AFT CARGO) · airframe 67,221 hrs · 24,820 cycles

NR 3 AFT CARGO SMOKE DETECTOR FAILED SMOKE TEST. REMOVED AND REPLACED AFT CARGO SMOKE DETECTOR, OPS CHECKED GOOD IAW MM.

Part: SMOKE DETECTOR — NO TEST (AFT CARGO) · airframe 67,221 hrs · 24,820 cycles

NR 4 SMOKE DETECTOR FAILED SMOKE TEST. REMOVED AND REPLACED AFT CARGO AFT SMOKE DETECTOR, OPS CHECKED GOOD IAW MM 26-16-01.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 67,217 hrs · 24,819 cycles

RIGHT WING L/E DELAMINATED APPROX 15 INCHES LONG BY 12 INCHES WIDE. ON WING L/E UNDER NR 6 L/E SLAT. PER ECRA 5720-02361 ENSURED ALL WIRING IS CLEAN AND PROTECTED, EA9394 INJECTED, AND NO FURTHER DELAMINATION DETECTED AFTER INJECTION. REPAIRED RT LE PANEL IAW SRM. REPLACED RT FIXED LE PANEL IAW DWG 114N1203, 114N1601, SRM 51-40-02.

Part: ANNUNCIATOR — OUT OF POSITION · airframe 66,742 hrs · 24,654 cycles

DOOR ANNUNCIATOR LIGHT PANEL IS IN WRONG LOCATION, IS NEXT TO BT WHEN IT SHOULD BE AT TOP NEXT TO CIRCUIT BREAKER. RESTORED PANEL TO SPEC LOCATION.

Part: BONDING STRAP — BROKEN (ACCESS DOOR) · airframe 66,076 hrs · 24,423 cycles

EXTERNAL POWER ACCESS DOOR BONDING JUMPER BROKEN. REPLACED BONDING STRAP FROM POWER ACCESS DOOR.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 66,010 hrs · 24,397 cycles

EMERGENCY LIGHTS DAMAGED AT ROW 10 AND 39. REMOVED AND REPLACED LIGHT JUMPER HARNESS AND LEAD IN WIRE ASSY REF AMM 33-51-96, OPS CHECKED GOOD.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 64,225 hrs · 23,788 cycles

FLOOR EMERGENCY EXIT LIGHTING AT SEAT ROWS 8-11 LT INOP. SECURED LOOSE CONNECTOR AT SEAT 12, OPS CHECKS OKAY. ACP INSPECTION OF EEL CONNECTOR.

Part: SEQUENCE VALVE — FAULTY (NLG) · airframe 63,918 hrs · 23,678 cycles

GEAR DISAGREE ON FINAL. NOSE GEAR DOORS OPEN BUT NOSE GEAR NOT DOWN. ALT GEAR EXTEND SUCCESSFUL. REPLACED NOSE GEAR-GEAR OPERATED SEQUENCE VALVE. GEAR SWING NORMAL.

Part: LIGHT — LOOSE (CABIN) · airframe 63,579 hrs · 23,554 cycles

EMERGENCY EXIT LIGHT PULLED UP FROM FLOOR IN FRONT OF FWD CLOSET. SECURED EMERGENCY LIGHT, CHECKED OK.

Part: FEEDER CABLE — INOPERATIVE (CABIN) · airframe 63,353 hrs · 23,478 cycles

INOP EEL LIGHTS AT MID TO AFT CABIN. FOUND FEEDER CABLE FROM THE WALL CUT PROBABLY DURING CARPET INSTALLATION. REPLACED CABLE, OP CHECKS GOOD.

Part: BLADE — NICKED (RT ENGINE) · airframe 63,081 hrs · 23,378 cycles

APPEARS TO BE MULTIPLE NICKS ON SEVERAL FAN BLADES OF RT ENG AT 2-3 O'CLOCK POS FACING AFT. INSPECTED BLADES AND FOUND NUMEROUS BLADES WITH MINOR NICKS IN AREAS 2 AND 8. REPAIRED FIRST STAGE FAN BLADE PER AMM. ACCOMPLISHED EDDY CURRENT INSPECTION PER NDT 72-31-401 PART 6. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 62,833 hrs · 23,286 cycles

L2 DOOR LOWER EMERGENCY EXIT SIGN INOPERATIVE. REPLACED EMERGENCY LIGHT ASSY, OPS CHECKED GOOD.

Part: WIRE — DISCONNECTED (CABIN) · airframe 62,446 hrs · 23,143 cycles

EMERGENCY FLOOR LIGHT AT DOOR 1L WIRES DISCONNECTED. SECURED PER MM, EEL OPS CHECKS OKAY.

Part: TUBE — LEAKING (HYD SYSTEM) · airframe 61,574 hrs · 22,834 cycles

ON SHORT FINAL, C HYD QTY EICAS FLASHED TWICE. CENTER QTY SHOWING 35RF. FOUND STAB BRAKE RELEASE TUBE CRACKED. REMOVED AND REPLACED TUBE .

Part: CAP — MISSING (CABIN) · airframe 62,150 hrs · 23,044 cycles

EMERGENCY ESCAPE LIGHT END CAPS MISSING 6B, 9C & 13C. REPLACED CAPS.

Part: COVER — UNSECURE (CABIN) · airframe 61,996 hrs · 22,987 cycles

EMERGENCY LIGHT STRIP IN CABIN CAME OFF. SECURED COVER OVER LIGHT STRIP.

Part: WIRE — BROKEN (ELECTRICAL SYS) · airframe 61,832 hrs · 22,935 cycles

AFTER T-S FOUND BROKEN WIRE IN FWD EE PANEL P-32. WIRE IS MARKED AA AND W1132. IT LOOKS LIKE IT IS GOING ON THE RT UTIL BUS CB AT TOP OF P-32 PANEL. BROKEN WIRE REPAIR ON PTT 8322002 SECURED RT UTILITY BUS CB ON P32 PANEL REF 24-51-24.

Part: SLIDE — DISLODGED (R1 DOOR) · airframe 61,766 hrs · 22,911 cycles

THE 1R SLIDE LANYARD FELL OUT OF SLIDE PACK. SECURED LANYARD.

Part: THRESHOLD — DAMAGED (FUSELAGE) · airframe 61,532 hrs · 22,818 cycles

AFT CARGO PIT THRESHOLD - AFT SEVERAL INCHES OF THRESHOLD SCUFF PLATE ARE PULLED AWAY FROM SKIN. POSSIBLE BELT LOADER DAMAGE. REPORTED BY RAMP. FABRICATED REPAIR. HELD IN PLACE WITH 4 C CLAMPS.

Part: LIGHT — UNSECURE (COCKPIT) · airframe 61,532 hrs · 22,818 cycles

EMERGENCY EXIT LIGHT STRIP COMING UP 9C; END CAP IN COCKPIT CONTROL COLUMN. REINSTALLED CAP AND SECURED CLEAR TRIM.

Part: PROXIMITY SENSOR — FAULTY (GIRT BAR) · airframe 61,467 hrs · 22,794 cycles

DOOR 4L SLIDE GIRT BAR ENGAGED LIGHT DOES NOT GO OUT. SLIDE GIRT BAR MUST BE VERIFIED ENGAGED BY MAINT BEFORE EACH FLIGHT. REPLACED FWD GIRT BAR PROX SENSOR S10216. CHECKED OKAY.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 61,366 hrs · 22,757 cycles

CORROSION FOUND ON STR 20L AT STATION 757. MAJOR REPAIR ACCOMPLISHED, CUT AND REMOVED STRINGER 20L FROM STA 750-780 DUE TO 100% MATERIAL LOSS FROM CORROSION. FABRICATED REPLACEMENT SECTION OF STR 20L IAW BOEING DRAWING 143 N3110 USING PN 193N3110-6. REPAIR SPLICE FABRICATED IAW B757 SRM USING P/N BAC1498-203. TREATED AND PRIMED PARTS IAW MM AND TOP COATED PER MM. INSTALLED PARTS PER SRM.

Part: PLATE — CORRODED (FUSELAGE) · airframe 61,366 hrs · 22,757 cycles

CORROSION ON 8" X 12" PLATE AFT OF DOOR 4 RIGHT AT STA 1680. MAJOR REPAIR ACCOMPLISHED, ON PEMCO NR 2486N00309 PER PD57-53-109.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,366 hrs · 22,757 cycles

CORROSION ON CREASE BEAM STA 1020 - 1035, RBL 64 MAIN CABIN A FLOOR LINE. MAJOR REPAIR ACCOMPLISHED, REMOVED CORROSION, FABRICATED AND INSTALLED STRAP ON PEMCO NR 2486N00278 PER EA PD57-53-106.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 61,366 hrs · 22,757 cycles

FLOOR DECK HAS CORROSION FROM STA 1680 AFT AT BL 64. MAJOR REPAIR ACCOMPLISHED, ON PEMCO NR #2486N00310 PER EA PD57-53-109.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 61,366 hrs · 22,757 cycles

CORROSION ON STRINGER 21L AT STATION 751. MAJOR REPAIR ACCOMPLISHED, CUT STRING FROM STA 750- 780 DUE TO 100% MATERIAL LOSS FROM CORROSION. FABRICATED REPLACEMENT STRINGER PART NR 143N3110-67 IAW BOEING DRAWING NR 143N3110 AND REPAIR SPLICE FROM PART NR BAC1498-203 IAW B757 SRM(S). TREATED AND PRIMED IAW MM, TOP COATED PER MM. INSTALLED STRINGER REPAIR IAW B757 SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,366 hrs · 22,757 cycles

CORROSION ON FLOORBEAM AT BS 324, RBL 42 THRU 65. MAJOR REPAIR ACCOMPLISHED, CORROSION AT STA 324 WAS FOUND TO BE OUT OF LIMITS PER SRM. T-CHORD WAS REMOVED AND REPLACED PER INSTRUCTIONS IN EA PD 57-53-100 AND UA EVA80751 WITHOUT DEVIATION.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,366 hrs · 22,757 cycles

CORROSION FOUND ON INTERIOR SKIN SURFACE AND STRUCTURE UNDER DOME NUTS BETWEEN STR 19L TO 21L AND STA 750- 780. MAJOR REPAIR ACCOMPLISHED, REMOVED CORROSION FROM STA 750 - 780, STR 18L - 22L. INSTALLED DOUBLER OVER AREA AND NEW DOME NUT PLATES PER UAL EVA 80762 AND PEMCO EA PD57-53-107 ON PEMCO NR 2486N00189.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 61,366 hrs · 22,757 cycles

CORROSION FOUND ON STRINGER 19L AT STA 767. MAJOR REPAIR ACCOMPLISHED, REMOVED AND REPLACED STR 19L BTWN STA 750 - 780 PER SRM ON PEMCO NR 2486N00496.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 61,366 hrs · 22,757 cycles

CORROSION FOUND ON AFT SHEAR DECK AT STATION 1700 FROM RBL 10 - RBL 50. MAJOR REPAIR ACCOMPLISHED, REMOVED CORROSION AND FOUND AREA TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER PER INSTRUCTIONS ON EA PD 57-53-102 WITHOUT DEVIATION. THIS IS CONSIDERED A PERMANENT REPAIR.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 61,366 hrs · 22,757 cycles

CORROSION FOUND ON STR 20L AT STATION 757. MAJOR REPAIR ACCOMPLISHED, CUT AND REMOVED STRINGER 20L FROM STA 750-780 DUE TO 100% MATERIAL LOSS FROM CORROSION. FABRICATED REPLACEMENT SECTION OF STR 20L IAW BOEING DRAWING 143 N3110 USING P/N 193N3110-6. REPAIR SPLICE FABRICATED IAW B757 SRM AND 53-00-03 USING P/N BAC1498-203. TREATED AND PRIMED PARTS IAW MM AND TOP COATED PER MM. INSTALLED PARTS PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,366 hrs · 22,757 cycles

DURING HMV VISIT CORROSION WAS FOUND AT FUSELAGE SKIN SURFACE BS746 THRU BS780 BETWEEN S17L - S22L. MAJOR REPAIR ACCOMPLISHED, REPAIRED UNDER UA EVA 80762 WITHOUT DEVIATION. A NEW FORM 8100-9 SHOWING COMPLIANCE TO 14CFR 25.571 AND 26.43 (D) WITHIN 24 MONTHS FROM APR 12, 2011 IN ORDER FOR THE REPAIR TO REMAIN VALID AND ACFT TO REMAIN AIRWORTHY. DROP DEAD DATE IS APR 12, 2013.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,366 hrs · 22,757 cycles

CORROSION ON FLOORBEAM AT BS 367, RBL 5 THRU 65. MAJOR REPAIR ACCOMPLISHED, REPAIRED FLOORBEAM STA 365.25 T-CAP FROM LBL 8.5 TO RT FRAME JOINT AND REPAIRED FLOORBEAM WEB RBL 57.9 PER PEMCO EA PD57-53-104 ON PEMCO NR 2486N00275.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,366 hrs · 22,757 cycles

FUSELAGE SKIN AT BS 1610 STR 19 RT HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED, REPAIR WAS COMPLETED PER INSTRUCTIONS ON EVA 80750 WITHOUT DEVIATIONS DURING A HMV3 VISIT IN TPA. THIS REPAIR MUST RECEIVE A NEW FAA FORM 8100-9 SHOWING COMPLIANCE TO 14CFR 25.571 AND 26.43 (D) WITHIN 24 MONTHS FROM ORIGINAL ISSUANCE DATE OF APR 7 2011 TO REMAIN VALID AND AIRCRAFT TO REMAIN AIRWORTHY. DROP DEAD DATE IS APRIL 13TH, 2013.

Part: SKIN — DENTED (FUSELAGE) · airframe 61,366 hrs · 22,757 cycles

DENT REPORTED FWD OF DOOR 3R AT STATION 1630, STRINGER 19R, DENT 1" LONG. 5/32NDS DEEP SHARP, 3 QTR" WIDE. INSPECTED AND REPAIRED DENT PER UA-EVA-80517 AND SRM. HFEC ACP. PERMANENT REPAIR TO BE ACP WITHIN 50 FLT HRS. NEED A THREE SHIFT SLOT FOR REPAIR. NEED TO GAIN ACCESS THROUGH CABIN SIDEWALL. RE-ACP EXTERNAL HFEC INSP OF FUSELAGE SKIN AT DENT AREA DENT REPAIRED ON SKIN AT APPROX STA 1610 STR 19R PER INSTRUCTIONS PROVIDED ON EVA 80750 AND PEM EA.

Part: FITTING — CORRODED (FUSELAGE) · airframe 61,366 hrs · 22,757 cycles

STA 1720 RT CUSP TO BULKHEAD T-FITTING CORRODED AT PRESSURE DECK. MAJOR REPAIR ACCOMPLISHED: RT T-FITTING AT STA 1720 REPLACED PER SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 61,366 hrs · 22,757 cycles

FLOOR SUPPORT CORRODED STA 322, RBL 42. MAJOR REPAIR ACCOMPLISHED: FLOOR SUPPORT FROM STA 310.5 TO 322, RBL 42 REPLACED PER SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 61,366 hrs · 22,757 cycles

INTERCOSTAL CORRODED AT R1 DOOR BS 324 TO 367. MAJOR REPAIR ACCOMPLISHED: REPLACED INTERCOSTAL AT DOOR R1 STA 324 TO STA 367 PER SRM.

Part: BEAM — CORRODED (FUSELAGE) · airframe 61,366 hrs · 22,757 cycles

CORROSION ON SUB BEAM AT STA 1713, RBL 40 TO RBL 60. MAJOR REPAIR ACCOMPLISHED: REPLACED SUB BEAM AT STA 1713, RBL 40 TO RBL 60, PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,366 hrs · 22,757 cycles

FWD CARGO FRAME HAS CRACK AT BS 600 AT STR 24L. MAJOR REPAIR ACCOMPLISHED: CUT OUT AND REMOVED DAMAGE FRAME, ACCOMPLISHED NDT OF AREA & FOUND NO CRACKS PER REF NDT. FABRICATED REPLACEMENT FRAME ASSEMBLY FROM 7075 T6 ,063 AND HEAT TREATED ON TRAVLER 2486N00415. INSTALLED FRAME AT STATION 600 PER B757-200 SRM.

Part: FRAME — DENTED (FUSELAGE) · airframe 61,366 hrs · 22,757 cycles

FWD CARGO FRAME HAS DENTS IN TWO LOCATIONS AT BS 580 BETWEEN S-25L AND S-24L. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED FRAME. NDT INSPECTED AREA AND FOUND NO CRACKS PER NDT. FABRICATED FRAME OUT OF 7075 T-6 .063. HEAT TREATED PER PEMCO TRAVLER 2486N00414. INSTALLED REPAIR AT STATION N580 PER B757 SRM.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 61,366 hrs · 22,757 cycles

FLOORBEAM HAS EVIDENCE OF CORROSION AT STA 1640 FROM BL 64 TO BL 0. MAJOR REPAIR ACCOMPLISHED: AFTER CORROSION REMOVAL AREA OF FLOORBEAM WAS OUT OF LIMITS PER SRM. REMOVED DAMAGE UPPER CHORD AT STA 1640 LBL 10 - RBL 65. PERFORMED NDT OF CUT OUT AND FOUND NO CRACKS. FABRICATED NEW TEE CHORD IAW SRM AND STRAPS PER SRM AND INSTALLED. PRIMED AND TOP COATED PER SRM. PERM REPAIR NO DTA.

Part: FITTING — CORRODED (FUSELAGE) · airframe 61,071 hrs · 22,648 cycles

FOUND EXFOLIATING CORROSION ON FUSELAGE AT DUMP FITTING MOUNTING FLANGE AREA. CORROSION WAS ISOLATED TO MID LAV DUMP VALVE ATTACH DOUBLER REF DWG 143N3412. REMOVED CORRODED DOUBLER AND FABRICATED REPLACEMENT DOUBLER USING .063 2024 T3 PART IS IN SHEET METAL SHOP CURING PRIMER. CLEANED PAN AREA WHERE DUMP VALVE ATTACHED AND PRIMED.

Part: SKIN — DENTED (BS 1630 S19R) · airframe 61,025 hrs · 22,632 cycles

DENT REPORTED FWD OF DOOR 3R AT STA 1630, STR 19R, DENT 1"LONG .1562" DEEP SHARP, .7500" WIDE. INSPECTED AND REPAIRED DENT IAW UA-EVA-80517 AND SRM. HFEC ACP SEE PTT SEQ 2522006 PERMANENT REPAIR TO BE ACP WITHIN 50 FLT HRS.

Part: UNKNOWN — ODOR (CABIN) · airframe 60,979 hrs · 22,612 cycles

CREW REPORTED STRONG FUEL ODOR THROUGHOUT ACFT. SEEMS THE STRONGEST AT OVERWING AREA. RAN BOTH ENGINES AT POWER, NO ODORS NOTED. ALSO INSPECTED APU COMPARTMENT FOR LEAKS, NONE FOUND. INSPECTED AC BAYS, NO ODORS NOTED. RAN APU BLEED, NO ODOR OF FUEL NOTED. INSPECTED WHEEL WELLS FOR LEAKS AROUND PUMPS AND DUCTING NO LEAKS OR ODORS FOUND.

Part: WINDOW — OVERHEATED (COCKPIT) · airframe 60,856 hrs · 22,563 cycles

FIRST OFFICER'S SLIDING WINDOW IS HOT TO THE TOUCH ON LOWER RIGHT AND ENTIRE LEFT SIDE. SAMC TEXT: DISCOLORATION IS APPARENT ON RIGHT SIDE OF THE SLIDING WINDOW. REPLACED NR 2 RT MOVEABLE WINDOW PER MM.

Part: SIGN — UNSECURE (EMERGENCY LIGHT) · airframe 59,194 hrs · 21,943 cycles

EMERGENCY EXIT SIGN, OVERWING EXIT ROW DEF HAS FALLEN OFF. SECURED LOOSE SIGN.

Part: SKIN — DENTED (FUSELAGE) · airframe 59,178 hrs · 21,938 cycles

EXTERNAL FUSELAGE SKIN WAS DENTED AT LWR SIDE OF FWD CARGO DOOR CUT OUT ABOUT 17 TO 21 INCHES FROM FWD END. REPAIR DENT IAW EA PD57-53-039 AND EVA 73889. TRIMED OFF DAMAGE AND INSTALLED FILLER, DOUBLER AND TRIPLERS. THE REPAIR IS A PERMANENT REPAIR AND HAS RECEIVED BAC 8100-9 SIGNED, DATED 15JUN10. THE REPAIR RESULTED IN A WEIGHT AND BALANCE CHANGE OF 13.64LB. OPS, ENGINEER MUST BE NOTIFIED VIA FORM SFR 4655.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 59,178 hrs · 21,938 cycles

AFT CARGO DOOR CUT OUT LWR EDGE, SKIN IS DENTED ABOUT 12 TO 15 INCHES FROM AFT EDGE. REPAIR IAW EA PD57-5 3-040. AND UA EVA 73868. TRIMMED DAMAGE AND INSTALLED FILLER, DOUBLER, AND TRIPLER. THE REPAIR IS A PERMANENT REPAIR APPROVED AND SIGNED BY BAC VIA 8100-9, DATED 15JUN10. THE REPAIR RESULTED A WEIGHT CHANGE OF 13.96LB. OPS ENGINEERING MUST BE NOTIFIED WITH THE WEIGHT AND BALANCE DATA VIA FORM SFR4655.

Part: TRANSMITTER — FAULTY (OIL PRESSURE) · airframe 59,173 hrs · 21,936 cycles

LT LOW OIL PRESS ON TAKEOFF ROLL. DUE TO RTO CAUSED BY LOW OIL PRES WARNING FOR NO 1 ENG, ACP OIL PRESS TROUBLE SHOOTING. OP TRANSMITTR REMOVAL AND INSTALLATION. OPS TRANSMITTER ADJUST-TEST. COMPLETED INSTALLATION OF LT ENG TRANSMITTER. OPS NORMAL. DUE TO RTO CAUSED BY LOW OIL PRESS WARNING ON UPPER ECAM, R & R NR 4 SCAVENGE PUMP IAW MM. REMOVED NR1 ENGINE MAIN OIL FILTER. OIL FILTER COMPLETE WITH NEW SCAV PUMP. NO ACTION REQUIRED. FURTHER INFORMATION FROM THE CREW, THEY ARE NOT SURE WHICH ENGINE WAS THE SOURCE OF THE LOW OIL PRESSURE WARNING. ACP TROUBLESHOOTING FOR LOW OIL PRESSURE ON BOTH THE NR 2 AND 1 ENGINES. RAN BOTH ENGS TO POWER, NO LOW PRESSURE LIGHT. AS REQUESTED, REPLACED PRES XTMR AND SCAV PUMP ON NR1 ENG, REVIEWED WITH SMC, REPLACEMENT IAW MAINT REQUEST. BASIC TS , OPS NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 58,394 hrs · 21,631 cycles

EXTERIOR FUSE EMERGENCY EXIT LIGHT INOP 1L. REPLACED LAMP P/N 767, OPS GOOD.

Part: OXYGEN MASK — FAULTY (COCKPIT) · airframe 57,107 hrs · 21,114 cycles

F/O OXYGEN MASK WILL NOT TRANSMIT VOICE. F/O OXYGEN MASK BOX ASSY, OPS GOOD.

Part: ACTUATOR — FAULTY (LT ENGINE) · airframe 55,105 hrs · 20,335 cycles

LT ENG THROTTLE WILL NOT ADVANCE FULLY FWD. FOUND L REV INTERLOCK ACTUATOR PREVENTING FULL TRAVEL. REPLACED L ENG REV INTERLOCK ACT, CHECKS OK.

Part: O-RING — LEAKING (ESCAPE SLIDE)

LOW BOTTLE. LEAKING AT BALL SHAFT O-RING. REMOVED AND REPLACED O-RING.

Part: O-RING — LEAKING (ESCAPE SLIDE)

LOW BOTTLE. LEAKING AT BALL SHAFT O-RING. REMOVED AND REPLACED O-RING.

Part: O-RING — LEAKING (EVAC SLIDE)

LOW SLIDE PRESSURE. CAUSE: LEAKING AT GAUGE O-RING. REMOVED & REPLACED O-RING.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,435 hrs · 19,682 cycles

DOOR 1L EXTERIOR EMERGENCY LIGHT IS INOP. RELAMPED EXTERIOR EMERGENCY LIGHT AT DOOR 1L. OPS CHECK GOOD.

Part: OXYGEN SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 53,005 hrs · 19,518 cycles

CAPTAIN'S OXYGEN MASK YELLOW FLOWBAR INOP BUT O2 FLOWING TO MASK & HARNESS. CAPTAIN`S O2 MASK BOX (UNKNOWN ISSUE). REPLACED CAPTAIN`S O2 MASK BOX, ALL OPS TESTS ARE GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 51,969 hrs · 19,151 cycles

EXTERIOR EMERGENCY LIGHT AT DOOR 1L INOP. LAMP IS OUT. RELAMPED DOOR 1L, OPS CHECKED OK. FOUND LAMP OUT. RELAMPED DOOR 1L, OPS CHECKED OK.

Part: FUEL CELL — CONTAMINATED (FUEL SYSTEM) · airframe 51,609 hrs · 19,022 cycles

RTFL DUE TO L ENGINE FUEL FILTER MSG. FOUND POSSIBLE MICROBIAL CONTAMINATION ON FILTER. ACCOMPLISHED FUEL CONTAMINATION TEST PER MM28-10-00 ON LT AND RT FUEL TANKS. RT TANK TESTED NEGATIVE -- LT TANK TESTED LOW POSITIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,496 hrs · 18,246 cycles

EEL LIGHT IN FRONT OF MID LAV INOPERATIVE. REPLACED EEL STRIP.

Part: BOTTLE — LOW (EVAC SLIDE) · airframe 49,193 hrs · 18,136 cycles

LOW BOTTLE PRESSURE. REPLACED SLIDE.

Part: LAMP — INOPERATIVE (L3 DOOR) · airframe 49,243 hrs · 18,155 cycles

CREW REPORT: DOOR 3L SLIDE LIGHT WON`T ILLUM WITH DOOR ARMED. [06-20-07] SLIDE LIGHT RELAMPED.

Part: OIL SYSTEM — LOW (NR 1 ENGINE) · airframe 48,104 hrs · 17,728 cycles

FLIGHT DIVERTED DUE TO LOSS OF OIL PRESSURE AND OIL QUANTITY IN NR 1 ENGINE. ENGINE WIND-MILLED FOR 15 TO 20 MINUTES, NOTED THAT N2 WAS TURNING (ABOUT 17%) DURING WIND MILL. FOUND OIL IN TAIL PIPE. REPLACED NR 1 ENG. NO FAULTS ON ENGINE RUN.

Part: CONTACTOR — CORRODED (EXT SLIDE LIGHT) · airframe 48,063 hrs · 17,709 cycles

EMERGENCY EXIT LIGHT INOP, EXTERIOR SLIDE LIGHT ON AFT CARGO DOOR INOP. CLEANED CORRODED AREAS AT CONTACT POINTS FOR BULB.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 48,063 hrs · 17,709 cycles

EMERGENCY EXIT LIGHT INOP, FLOOR LIGHT INBOARD OF 'S' LAV INOP. PLUGGED IN LOOSE CONNECTOR TO POWER FEEDER STRIP.

Part: OXYGEN SYSTEM — LEAKING (SUPPLEMENTAL O2) · airframe 47,861 hrs · 17,624 cycles

FLIGHT DIVERTED TO ORD DUE TO A SUPPLEMENTAL OXYGEN LEAK. CREW REPORTS LOSS OF ALL O2, STATUS PAGE INDICATES LESS THAN 100PSI, CREW MASKS ARE NOT INFLATING. SUPPLEMENTAL DATA UPDATE FOUND CO PILOTS O2 STOWAGE BOX AND MASK LEAKING REPLACED O2 STOWAGE AND HOSE. ALSO FOUND O2 BOTTLES PARTIALLY EMPTY. SERVICED O2 TO NORMAL LEVEL.

Part: ODOR — UNKNOWN · airframe 46,182 hrs · 17,015 cycles

STRONG ODOR THROUGH A/C VENTS DURING DESCENT.

Part: SKIN — DENTED (FUSELAGE) · airframe 42,603 hrs · 15,703 cycles

EXTERNAL FUSELAGE SKIN DENTED 1 INCH BELOW FLOOR LEVEL AND 10 INCHES FORWARD OF 2 LT MED. MAJOR REPAIR WAS ACCOMPLISHED PER UA-EVA-50430.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE)

ESCAPE SLIDE HAS A LOW BOTTLE. CYLINDER ASSEMBLY GAUGE ADAPTER FITTING O-RING LEAKING. REPLACED O-RING.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,512 hrs · 14,548 cycles

FRAME INNER FLANGE DENTED AT BS 1420, STR 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED NESTED J-ANGLE REPAIR.

Part: CREASE BEAM — CORRODED (STA) · airframe 39,512 hrs · 14,548 cycles

MAIN CABIN STA 760-770, CREASE BEAM AT LBL60 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED AN EXTRUDED SECTION REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,512 hrs · 14,548 cycles

LT FWD CROWN AT STA 440 IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND FILLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,512 hrs · 14,548 cycles

FRAME FLANGE DENTED AT BS 1400, STR 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED NESTED J-ANGLE REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 39,512 hrs · 14,548 cycles

DOOR 4R FLOOR SUPPORT INNER CHORD BROKEN OUT AND CORRODED AT BS 1681. MAJOR REPAIR ACCOMPLISHED. FLOOR SUPPORT REPAIR SPLICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,512 hrs · 14,548 cycles

FLOORBEAM CAP AT BS 1681 RBL 45-60 CORRODED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED A REPAIR ANGLE SPLICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,512 hrs · 14,548 cycles

CABIN FLOORBEAM CORRODED BEYOND LIMITS AT BS 1640, RBL 12R-14R. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM WITH ANGLE AND STRAP.

Part: SKIN — DENTED (FUSELAGE) · airframe 35,009 hrs · 12,901 cycles

DENT AND GOUGE 34 INCHES AFT OF DOOR 2L, STA 760, STR 16L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,382 hrs · 12,302 cycles

DENT AND GOUGES FOUND IN AND AROUND PREVIOUS REPAIR APPROX 80 INCHES FWD OF DOOR 2L AND 24 INCHES BELOW WINDOW LOWER CUTOUT. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED.

Part: LVDT — FAILED (RT ENGINE)

ON CLIMBOUT LOUD NOISE HEARD AND EGT WENT TO 705. RIGHT ENGINE WAS SHUTDOWN. *S/D* ENGINE EXPERIENCED A COMPRESSOR STALL DUE TO AN INOP STATOR VANE ACTUATOR (SVA) FEEDBACK CHANNEL. THIS SITUATION CAUSED THE SVA TO GO TO FAIL-SAFE POSITION (FULL OPEN). WHEN THE THROTTLE WAS REDUCED FROM TAKEOFF POWER, A STALL OCCURRED SINCE THE STATOR VANES COULD NOT CLOSE. THE INOPERATIVE CHANNEL WAS CAUSED BY A DEFECTIVE LINEAR VARIABLE DUAL TRANSDUCER (LVDT), WHICH HAD A BREAK IN ITS COIL WINDINGS. LVDTS WITH GREATER THAN 7000 HRS TIS AT SHOP VISIT WILL BE REPLACED.

Part: DUCT — BROKEN (NR 1 ENGINE)

NR 1 ENGINE, REPORT SLOW ACCELERATION TO IDLE. AFTER INSPECTION OF APU AREA, BROKEN DUCT WAS IDENTIFIED. APU INOP. *S/D* REPLACED BROKEN DUCT. APU OPS CHECKED NORMAL, AND BOTH ENGINES START AND OPERATE WITHIN NORMAL PARAMETERS.

Part: BULB — FAILED (CABIN)

LEFT OVERHEAD OVERWING SLIDE EMERGENCY LIGHT INOP. RELAMPED LEFT OVERWING SLIDE EMERGENCY LIGHT, OPERATION CHECKS NORMAL.

Part: LIGHT STRIP — INOPERATIVE (CABIN)

EMERGENCY ESCAPE LIGHT STRIP INOPERATIVE AT ROW 13 ABC. RESECURED EMERGENCY LIGHT STRIP AT ROW 13 ABC. OP CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

RIGHT SIDE EXTERNAL EMERGENCY LIGHT INOP FORWARD OF DOOR 4. RELAMPED.