N593UA

Part: POUCH — BROKEN (CABIN) · airframe 51,942 hrs · 19,293 cycles

CABIN SVC REPORTS: 14DE LIFE VEST POUCH BROKEN. SECURED LIFE VEST POUCH.

Part: BLADE — NICKED (NR 2 ENGINE) · airframe 51,866 hrs · 19,265 cycles

NR 2 ENGINE BLADE NR 5 HAS NICK IN AREA 5 ABOUT .375 X.250. NR 2 ENGINE WILL NEED EDDY CURRENT INSPECTION DUE TO FAN BLADE BLEND REPAIR. INSPECTED BLADE PER MM, NO CRACKS FOUND.

Part: ACTUATOR — LEAKING (MLG) · airframe 50,647 hrs · 18,847 cycles

ON CLIMBOUT, FL260 AT 310 KTS, GEAR HANDLE TO OFF CAUSED GEAR DOORS LIGHT TO ILLUMINATE. SLOWED, ACFT YAWD RT & SLIGHT VIBRATION. SLOWED TO 270KTS. RETRYED GEAR HANDLE TO UP, YAW & VIBRATION STOPPED GEAR LIGHT OUT. ONCE SPEED WAS 270, PLACED GEAR LEVER TO OFF, ALL INDICATION NORMAL. RETURNED TO NORMAL SPEED. ALL NORMAL. TROUBLESHOT PER FIM 32-30 -00. FOUND LEFT TILT ACTUATOR LEAKING OUT OF THE RETURN PORT REF BOX 21 PG 130 OF FIM. REPLACED ACTUATOR REF MM 32-32-15. CYCLED GEAR SEVERAL TIMES REF MM 32-32-00 AND ALTERNATE SYSTEM REF 32-35-00. OPS CHECKED NORMAL.

Part: OIL SYSTEM — LEAKING (NR 1 ENGINE) · airframe 50,122 hrs · 18,708 cycles

OIL LEAK COMING OUT OF 2.5 BLEED AND DIRTY SOCK ODOR IN COCKPIT. REPLACE NR 1 ENGINE PER MM.

Part: PIN — UNSECURE (STANDBY POWER) · airframe 49,548 hrs · 18,519 cycles

IN REFERENCE TO DF958, FOUND POWER FROM (115V AC STANDBY BUS) FLUCTUATES BETWEEN 114V AND 120V WHEN POWERED FROM LEFT BUS. WHEN POWER TURNED OFF AND USING POWER SUPPLIED FROM STATIC INVERTER, POWER IS CONSTANT. CHECKED POWER AT P6 PANEL BREAKER K16 (AC STBY BUS PWR) AND VOLTAGE IS CONSTANT. HUNG IN AC STBY PWR RELAY K105, NO HELP. NEED FURTHER TROUBLESHOOTING TO FIND WHAT IS CAUSING VOLTAGE FLUCTUATIONS. SEE SEQ# 5482013 FOR FIX STANDBY PWR SWITCH . INSERTED PIN AND GRD CHECKED OKAY. THERE WAS NO CONTINUITY FROM D3508 PIN 20 THROUGH 22.

Part: FEEDER CABLE — BURNED (NR 1 IDG) · airframe 49,181 hrs · 18,372 cycles

NR 1 ENGINE IDG PHASE C, FEEDER CABLE AND THRU LEAD FOUND BURNED DURING PRELIMINARY INSPECTION. REMOVED & REPLACED IDG. REPLACED NR 1 IDG POWER FEEDER CABLE PHASE C TERMINAL LUG & HEAT SLEEVE. OPS CHECKED IAW AMM.

Part: PAN — GOUGED (L4 DOOR HANDLE) · airframe 49,181 hrs · 18,372 cycles

DOOR 4 LEFT HANDLE PAN IS GOUGED BELOW EXTERIOR DOOR HANDLE. FOUND IT OUT OF LIMITS. REMOVED & REPLACED HANDLE PAN ASSEMBLY.

Part: PAN — GOUGED (L1 DOOR HANDLE) · airframe 49,181 hrs · 18,372 cycles

DOOR 1 LEFT HANDLE PAN IS GOUGED BELOW EXTERIOR DOOR HANDLE. FOUND IT OUT OF LIMITS OF SRM. REMOVED & REPLACED HANDLE PAN ASSEMBLY.

Part: PAN — GOUGED (L2 DOOR) · airframe 49,181 hrs · 18,372 cycles

DOOR 2 LEFT HANDLE PAN IS GOUGED BELOW THE EXTERIOR HANDLE. FOUND GOUGE TO BE OUT OF LIMITS PER B757 SRM 52-10-01. INSTALLED NEW HANDLE PAN IAW B767 SRM.

Part: LIGHT — CORRODED (INDICATOR) · airframe 49,175 hrs · 18,369 cycles

EXTERNAL POWER AC CONNECTED LIGHT ASSY CORRODED. REPLACED LIGHT ASSY.

Part: BRACKET — CRACKED (FWD CARGO DOOR) · airframe 49,171 hrs · 18,366 cycles

FWD CARGO DOOR, AFT EDGE, INSIDE STRUCTURE, 3RD SUPPORT WEB UP FROM BOTTOM HAS A TEAR APPROX ONE INCH LONG. REMOVED AND REPLACED BRACKET.

Part: GASKET — MISSING (CHECK VALVE) · airframe 48,585 hrs · 18,142 cycles

ASBESTOS GASKET PARTIALLY MISSING ON TOPSIDE OF LT NIPPLE CHECK VALVE ASSY (GROUND CONNECTION FOR AIR START). LARGE AMOUNT OF HOT AIR ESCAPING AND BLOWING UP ONTO FUEL TANK. REPLACED GASKET PER MM, NO LEAKS NOTED.

Part: DOOR — BINDS (R3) · airframe 48,261 hrs · 18,014 cycles

DOOR 3R HARD TO CLOSE.

Part: SEAT — MALFUNCTIONED (COCKPIT) · airframe 48,232 hrs · 18,003 cycles

CAPTAINS SEAT DOES NOT LOCK IN UP POSITION. FALLS TO LOWER LEVEL RAPIDLY. REPLACED CAPT'S SEAT.

Part: CABLE — TWISTED (NLG) · airframe 47,944 hrs · 17,895 cycles

TILLER STEERING - STEERING FORCES ARE HIGH. CREW COMMENTS: NOSE STEERING TILLER HAS GRINDING-BAD BEARINGS FEEL. SLUGGISH RETURN TO CENTER. RUDDERS OKAY. FOUND NOSE GEAR STEERING CABLES TWISTED AFTER THE RUN THROUGH THE GUIDE. REMOVED CASTELLATED NUT AND CABLES RETURNED TO NORMAL. CLEANED ALL PARTS AND REINSTALLED AND CABLES STILL BOUND UP. NEEDS NEW SEALING RING AND SEAL ASSY. CASTELLATED NUT AND LOCK ARE STILL REMOVED AND WAITING FOR NEW PARTS. REPLACED SEAL RING AND SEAL ASSY. RIGGED CABLES. STEERING FEELS OK, CABLES NOT BINDING, REQUESTING TAXI CHECK. LUBED STEERING COLLAR, CK'D TIRE PRESSURE, FOUND NORMAL. STEERING OPS CKS NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 47,636 hrs · 17,779 cycles

GROUND CREW REPORTS SCRAPE ON FUSELAGE UNDER AFT CARGO PIT DOOR. SAMC TEXT: DENT MEASURES .25 BY .25 AND IS .03125 DEEP. THE DENT IS 6.5 INCHES FROM THE DOOR CUT OUT AND 1.750 INCHES FROM A SKIN LAP. AREA LOWER OF FWD CARGO DOOR. BLENDED AREA SKIN REF SRM. WITININ LIMITS PG 101, AREA A. AREA WAS A GOUGE NOT A DENT. 2 INCHES LENGTH DEPTH .010. PRIMERED AREA WILL NEED PAINT.

Part: INLET — DELAMINATED (NR 1 NACELLE) · airframe 47,565 hrs · 17,753 cycles

NR 1 ENG INBOARD FAN COWL HAS A LARGE AREA OF DELAMINATION LOWER FWD CORNER. FOUND ONE LAYER OF DELAMINATED FIBERGLASS INSTALLED OVER ALUMINUM FOIL REPAIR. ALUMINUM FOIL DELAMINATED FROM COWL APPROX 27" X 18". DELAM BEYOND LIMITS. WILL REQUIRE REPAIR PER SAME SRM PARA 15. REPLACED LEFT INBOARD FAN COWL. NR 1 ENG INBD FAN COWL LOWER HEAT BLANKET DAMAGED. ALUMINIZED COVER IS MISSING. REPLACED N0 1 ENG INBOARD FAN COWL.

Part: FAN — NOISY (CABIN) · airframe 47,247 hrs · 17,644 cycles

RT RECIRC FAN TOO LOUD. PLZ WORK WITH CH1637. ACP COCKPIT GROUND NOISE LEVEL CHECK IAW AMM. VERIFIED BOTH PACKS IN LOW FLOW WITH MCDU. RT RECIRC FAN ON: 108DB. RT RECIRC FAN OFF: 107DB. NOTE - THIS IS ONE OF THE QUIETER 757(S) IN UA FLEET ON GROUND. CLEANED DUCTS REF MM. DECIBELS ARE 73 WITH RIGHT RECIRC ON AND 72 OFF VELOCITY IS 3150 AND FLOW RATE IS 345.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,237 hrs · 17,642 cycles

FLOOR EMERGENCY LIGHTS INOP, ALL FIRST CLASS. REPLACED SHORTED EMERGENCY LIGHT AT MID CABIN FLOOR, OPS CHECKED OKAY.

Part: FASTENER — LOOSE (LT WING) · airframe 47,167 hrs · 17,618 cycles

LT WING, INBOARD MOST, LOWER, FUEL TANK ACCESS PANEL LEAKING FUEL. RETORQUED FASTENERS. REFUELED CTR FUEL TANK, LEAK CHECKED FOR AN EXTENDED TIME. LEAK CHECKED OKAY. REBALANCED FUEL LOAD.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 46,876 hrs · 17,508 cycles

WINDOW R2 HAS DELAMINATION. REPLACED WINDOW REF MM 56- 11-94 AND 56-11-02.

Part: LIGHT — INOPERATIVE (SEAT 25C) · airframe 46,788 hrs · 17,476 cycles

EMERGENCY LIGHT AT 25C INOPERATIVE. REPLACED SECTION. OPS NORMAL.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 46,524 hrs · 17,375 cycles

PLASTIC STRIP OVER EMERGENCY EXIT FLOOR LTS IS LOOSE AT SEATS 9ABC. REPLACED PLASTIC LIGHT COVER.

Part: O-RING — LEAKING (LT ENGINE) · airframe 46,388 hrs · 17,326 cycles

LT ENG OIL QTY EICAS, FLIGHT DIVERTED. RAN ENG JRH AND FOUND LEAK AT THE NR 3 BEARING THERMOCOUPLE. REPLACED THE O-RING AND REINSTALLED THERMOCOUPLE. CLEANED AFFECTED AREAS AND RAN ENG IAW JRH, ALL PARAMETERS NORMAL AND NO LEAKS NOTED.

Part: BOTTLE — READS LOW (L3 DOOR SLIDE) · airframe 45,435 hrs · 16,988 cycles

SLIDE RAFT DOOR 3L SHOWS RED. REPLACED DOOR SLIDE. OP TESTS GOOD. PINS REMOVED.

Part: BOTTLE — READS LOW (L4 DOOR SLIDE) · airframe 45,435 hrs · 16,988 cycles

ESCAPE SLIDE DOOR 4L PRESSURE IS IN THE RE D BAND (LOW PRESSURE).

Part: LEVER — FAULTY (SPEED BRAKE) · airframe 45,368 hrs · 16,962 cycles

SPEED BRAKE HANDLE FORCES OUT OF LIMITS. SPEED BRAKE LEVER STIFF TO OPERATE. NEED TO TROUBLESHOOT THE SPEED BRAKE. FOUND THE PULL FORCE ON THE SPEED BRAKE HANDLE AT 16LBS. MAXIMUM PULL FORCE IS 6LBS. THIS IS OUT OF LIMITS. CHECKED SPEED BRAKE LINKAGE AND FOUND NO BRAKE CLUTCH IS DRAGGING. R & R SPEEDBRAKE, NO BACK CLUTCH IAW MM AND R &R LT BLACK SPEEDBRAKE LVDT. PERFORMED LVDT ADJMNT TEST, AUTOSPEED BRAKE TST, SPDBRK MECHB TEST & SPD BRK LEVER FORCE TST. ALL OPS TEST CHECKED GOOD.

Part: COVER — CRACKED (EMERGENCY EXIT) · airframe 44,193 hrs · 16,532 cycles

CREW REPORTED OF FWD LT PAX WINDOW FRAME FELL OFF. FOUND COVER OVER LT OVERWING EXIT DOOR HANDLE SECURED ONLY BY LANYARD. COVER FOUND CRACKED NOT ALLOWING COVER TO SNAP SECURELY IN PLACE. PERFORMED INTERIM REPAIR OF CRACK ON INSIDE OF COVER WITH TAPE, COVER NOW SECURE. OPS OF COVER TO ACCESS HANDLE IN EGRESS SITUATION IS NOT AFFECTED. PART APPEARS TO BE COVER-HANDLE.

Part: GCU — FAILED (RIGHT) · airframe 44,147 hrs · 16,512 cycles

RIGHT GEN DRIVE ISSUE, ABORTED TO. REPLACED RT GCU, OPS CHECKED NORMAL. RAN ENG AND RT IDG, OPS OK.

Part: FEEDER CABLE — LOOSE (EMERGENCY LIGHT) · airframe 44,087 hrs · 16,487 cycles

EMERGENCY LIGHT LAMP NEXT TO FIRST CLASS CLOSET INOP. SECURED POWER FEEDER CABLE TO LAMP. EMERGENCY LIGHT OP CHECK OKAY.

Part: DOOR FRAME — CRACKED (ENTRY DOOR) · airframe 43,769 hrs · 16,367 cycles

NR 2 RT ENTRY DOOR ASSY, FWD FRAME IS CRACKED AT PREVIOUS REPAIR DOUBLER LOCATION. ACP REPAIR PER PEMCO ENGINEERING DOC PD57-52-0002 WITHOUT DEVIATION. THE REPAIR IS MAJOR AND RECEIVED FAA STG ONE APPROVAL VIA FAA FORM 8100-9 ON 02MAR10. COMPLIANCE FINDING TO 14 CFR25.571 AND 26.43 HAS NOT BEEN EVALUATED. A NEW FAA FORM 8100-9 MUST BE ISSUED PRIOR 01MAR11, DTA 10-017 HAS BEEN CREATED TO 094972TRACK THIS CONDITION. OK TO CF PER EVA-73494.

Part: SHROUD — OUT OF ADJUST (L2 DOOR) · airframe 41,401 hrs · 15,467 cycles

DOOR 2L WILL NOT ARM. ARMING INDICATOR STICKING, ADJUSTED SHROUD.

Part: FEEDER CABLE — BURNED (APU GEN) · airframe 41,132 hrs · 15,353 cycles

APU GENERATOR FEEDER CABLE SEVERELY BURNED. REPLACED TERMINAL END ON APU GEN FEEDER. OPS CHK'D GOOD.

Part: POWER CABLE — DEFECTIVE (CABIN) · airframe 40,789 hrs · 15,204 cycles

EMERGENCY PATH LIGHTING INOP FROM ROW 9-13. FOUND BAD POWER CABLE FROM INVERTER TO EEL STRIP, REPLACED POWER CABLE, ALL CHECKS NORMAL.

Part: SLIDE — LOW PRESSURE (DOOR)

PRESSURE LOW. UNKNOWN. GAUGE READS WITHIN LIMITS. NO ACTION TAKEN.

Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 40,117 hrs · 14,930 cycles

EEL STRIP COVER FROM ROW 25 TO BACK OF ACFT CHEWED UP AND BROKEN. REPLACED COVER STRIP.

Part: CABLE — FAULTY (CABIN) · airframe 39,414 hrs · 14,652 cycles

EEL STRIP LIGHTING FROM ROW 9 THRU 15 BLINK INTERMITTANTLY. REPLACED CABLE RIBBON FROM SEAT 12 THRU 15. OPS CHECKS GOOD.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 38,889 hrs · 14,455 cycles

LEAK IN CAPT'S OXYGEN MASK. HEAD STRAP HAS LEAK. LEAKING HEAD STRAP ON O2 MASK. REPLACED CAPT O2 MASK ASSY, OPS CHECKED NORMAL.

Part: SLIDE — READS LOW (L3 DOOR) · airframe 38,845 hrs · 14,439 cycles

SLIDE AT DOOR 3L PRESSURE LOW. *S/D* CYLINDER FITTING LEAK INSIDE SLIDE ASSY. REPLACED DOOR SLIDE AT 3L.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,741 hrs · 14,404 cycles

DENT IN EXTERNAL SKIN AT BS 424, 2 INCHES BELOW STR 19L. ACCOMPLISHED A MAJOR REPAIR AT GS0- CUT-OUT DAMAGED AREA AND FABRICATED A -1 DOUBLER AND INSTALLED PER TIMCO REO G1 2367, REV. B AND UAL EVA 71691 ON NON ROUTINE 21326 BY MECH DELG ADO-111486 AND INSP KPAKPO-5189. 85625PER UAL EVA 71691, THIS EXTERNAL DOUBLER REQUIRES SUPPLEMENTAL INSPECTIONS TO BEGIN WHEN THE AIRCRAFT REACHES A TOTAL OF 34,000 C WITH REPEAT INSPECTIONS EVERY 3000C THEREAFTER.

Part: STRUCTURE — GOUGED (LT WING TE FLAP) · airframe 38,741 hrs · 14,404 cycles

LT WING INBOARD FLAP UPPER SURFACE OUTBOARD EDGE GOUGED. PREVIOUS REPAIR DAMAGED. REMOVED PREVIOUS REPAIR AND INSTALLED BONDED REPAIR.

Part: SKIN — DENTED (BS 429-434) · airframe 38,741 hrs · 14,404 cycles

DENT IN EXTERNAL SKIN STA 429 - 434, 6 INCHES BELOW STR 17L. ACCOMPLISHED MAJOR REPAIR AT GSO. EVALUATED DENT AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-01, DETAIL III - OIL CANNED. CUT OUT DAMAGED AREA AND FABRICATED DOUBLER AND FILLER, INSTALLED PER TIMCO REO-G12367, REV B AND EVA 71697 ON NON ROUTINE 21325. INSP KPAKPO-5189. THIS REPAIR IS AN INTERNAL DOUBLER AND PER EVA 71697, THIS REPAIR HAS RECEIVED ONLY FIRST STAGE APPROVAL FOR STATIC STRENGTH, 85625 PENDING DATA ANALYSIS BY BACO PRIOR TO 19JUN09. THE AIRCRAFT WILL BECOME UNAIRWORTHY UNLESS A NEW 8100-9 IS ISSUED PRIOR TO 19J UN09, REF 14 CFR 25.571.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 38,741 hrs · 14,404 cycles

FWD PIT STA 540 STR 24L-25L HAS 1 EA DENT. ACCOMPLISHED MAJOR REPAIR AT GSO. REPAIRED IAW REO G12368 AN D EVA 71698 AND SRM 51-00-06. THIS IS A CAT B REPAIR AND REQUIRES SUPPLEMENTAL INSPECTIONS TO BEGIN AT 50000C AND 12000C THEREAFTER. THIS CONSISTS OF BOTH DETAILED VISUAL INSP AND NDT PER EVA 71698 CURRENT PTC IS 14404.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,741 hrs · 14,404 cycles

AFT PIT FRAME AT FS 1460 STR 26L HAS DENT. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR IAW 53-00-07 REPAIR 5 THIS IS A CAT B REPAIR IN ZONE 1 AND REQUIRES S UPPLEMENTAL INSPECTIONS STARTING AT 50000FC AND 12000FC THERE AF TER. INSPS CONSISTS OF BOTH DETAILED VISUAL AND NDT PER SRM 53-0 0-07 RPR 5 TABLE II. CURRENT PTC IS 14404C.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 38,741 hrs · 14,404 cycles

FUSELAGE STA 540 HAS DENT BETWEEN STR 24 AND 25. REMOVED DAMAGE, FABRICATED RPR DOUBLER AND FILLER AND INSTALLED IAW SRM 53-00-01

Part: STRUCTURE — DAMAGED (L2 DOOR) · airframe 38,741 hrs · 14,404 cycles

DOOR 2L NEEDS REPAIR DOUBLER AT UPPER HINGE CUTOUT. ACCOMPLISHED MAJOR REPAIR AT GSO. ACP HFEC NO DEFECT FOUND. INSTALLED REPAIR DOUBLER IAW MM 52-11-87.

Part: STRUCTURE — CRACKED (R2 DOOR) · airframe 38,741 hrs · 14,404 cycles

DOOR 2R NEEDS REPAIR DOUBLER AT UPPER HINGE CUTOUT. ACCOMPLISHED MAJOR REPAIR AT GSO. ACP HFEC FOUND CRACK IN LW RT INBOARD CORNER REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW MM.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,741 hrs · 14,404 cycles

FWD CARGO PIT STA 620 STR 24L FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,741 hrs · 14,404 cycles

AFT PIT FRAME AT FS 1360 STR 26L HAS 1EA DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,741 hrs · 14,404 cycles

AFT PIT FRAME AT BS 1320 BETWEEN STR 25R-26R INBOARD FLANGE IS DENTED. ACCOMPLISHED MAJOR REPAIR AT GSO. REPAIRED IAW SRM 53-00-07 RPR 5. THIS IS A CAT B REPAIR IN ZONE 1 AND REQUIRES SUPPLEMENTAL INSP STARTING AT 50,000 TOTAL FLT CYCLES PER SRM 53-00-07 REPAIR 5 TBL II AND 12,000 FC THEREAFTER. INSP CONSIST OF BOTH VISUAL AND NDT. CURRENT PTC IS 14404.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,741 hrs · 14,404 cycles

AFT PIT FS 1520 STR 26L HAS DENT IN FRAME. ACCOMPLISHED MAJOR REPAIR AT GSO. REPAIRED IAW SRM 53-00-07 REPAIR 5. THIS IS A CAT B REPAIR IN ZONE 1 AND REQUIRES SUPPLEMENTAL INSP STARTING AT 50,000 TOTAL FLT CYCLES PER SRM 53-00-07 RPR 5 TBL II AND 12,000FC THEREAFTER. INSP CONSIST OF BOTH VISUAL AND NDT. CURRENT PTC IS 144 04.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,741 hrs · 14,404 cycles

AFT PIT FRAME STA 1480 STR 26L HAD DENT. ACCOMPLISHED MAJOR REPAIR AT GSO. REPAIRED IAW SRM 53-00-07 REPAIR 5. THIS IS A CAT B REPAIR IN ZONE 1 AND REQUIRES SUPPLEMENTAL INSP STARTING AT 50,000 TOTAL FLT CYCLES PER SRM 53-00-07 REPAIR 5 TBL II AND 12,000FC THEREAFTER. INSP CONSIST OF BOTH VISUAL AND NDT. CURRENT PTC IS 144 04.

Part: MOUNT — OBSTRUCTED (BARRIER BAR) · airframe 38,343 hrs · 14,256 cycles

SECONDARY BARRIER DOES NOT LOCK. FOUND DEBRIS IN FLOOR MOUNT HOLE WHERE SLIDE BAR SITS IN. CLEANED HOLE OF DEBRIS, LUBED BAR AND LATCHES, INSTALLED BARRIER, OPS CHECKED GOOD.

Part: SWITCH — UNKNOWN (SLIDE LIGHT) · airframe 37,203 hrs · 13,859 cycles

SLIDE LIGHT AT DOOR 1R INOP. REARMED TARGET SWITCH AND SYSTEM OPERATES/TESTS NORMALLY.

Part: MASK — DEFECTIVE (COCKPIT) · airframe 35,700 hrs · 13,326 cycles

OXYGEN MASK DEFECTIVE AT (1=CAPT, 2=1ST OFF, 3=1ST OBS), CREW COMMENTS, TEST BUTTON STICKS IN WHEN PUSHED. [08-07-07] REPLACED MASK.

Part: TRANSDUCER — FAULTY (CREW O2) · airframe 34,251 hrs · 12,815 cycles

O2 PANEL INDICATOR READS 1550 WHEN O2 BOTTLE IS FULL, ALSO COCKPIT GAUGE READS 1550. SERVICED CREW BOTTLE TO FULL MID-RANGE RED ON BOTTLE, AND O2 QTY ON CREW SERVICE PANEL OR EICAS WILL NOT READ OVER 1700PSI. QTY READING ABOUT 200PSI LOW. REMOVED AND REPLACED CREW O2 PRESSURE TRANSDUCER WHICH FAILED.

Part: WARNING MESSAGE — ACTIVATED (COCKPIT) · airframe 33,322 hrs · 12,479 cycles

EICAS MESSAGE 'POWER XFER UNIT' IS DISPLAYED. STATUS MSG CAME ON AT CRUISE. OPERATED PTU MANUALLY, COMPLETED VISUAL INSPECTION OF PTU CONTROL AND INDICATION WIRING IN LH & RH WW, COMPLETED TEST PROCEDURE FOR THIS MESSAGE WITH BOTH ENGINES AS PER PROCEDURE - AND NO PROBLEMS NOTED IN ANY OF THESE TESTS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,048 hrs · 12,378 cycles

THE FOLLOWING EMERGENCY LIGHTS ARE INOP: SLIDE LIGHT 4L, EXIT SIGN OVER DOOR 4L, EXIT MARKERS DOORS 4L & 4R. AFT GALLEY OVERHEAD EXIT SIGN, AISLE LIGHTS AT ROWS 29 & 32. THE CAUSE OF EMERGENCY LIGHT INOP CONDITION IS ATTRIBUTED TO A FAILED BATTERY CHARGER. REPLACED BATTERY CHARGER.

Part: IDG — FAILED (RIGHT) · airframe 32,808 hrs · 12,294 cycles

FLIGHT DIVERTED UNDER AMBER ALERT AFTER THE LOSS OF THE RIGHT GENERATOR AND THE INABILITY TO START THE APU. RT IDG FAULT DISPLAYED, IDG DISCONNECTED. REPLACED IDG.

Part: SKIN — DENTED (FUSELAGE) · airframe 24,385 hrs · 9,214 cycles

THERE ARE TWO SMOOTH DENTS FWD OF DOOR 2L ON AN EXISTING PATCH. EACH DENT IS APPROX 2 INCHES WIDE BY .125 INCHES DEEP. MAJOR REPAIR ACCOMPLISHED. REPLACED EXISTING DOUBLER WITH DOUBLER-TRIPLER.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 22,310 hrs · 8,416 cycles

NR 2 ENGINE COMPRESSION STALL ON TAKEOFF

Part: SKIN — DENTED · airframe 20,185 hrs · 7,629 cycles

FUSELAGE DENTED AT STATION 1690-1706, BELOW STRINGER 17R-RADIUS. MAJOR REPAIR ACCOMPLISHED. DOUBLER AND TRIPLER INSTALLED.

Part: SKIN — DENTED (FUSELAGE) · airframe 20,185 hrs · 7,629 cycles

STATION 220 STRINGER 17L WL 208 FUSELAGE SKIN DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED · airframe 20,185 hrs · 7,629 cycles

AFT PIT AT STATION 1440 ABOVE STRINGER 26 LEFT, TOP OF FRAME FLANGE DENTED. MAJOR REPAIR ACCOMPLISHED. FRAME DOUBLER INSTALLED.

Part: FRAME — DENTED · airframe 20,185 hrs · 7,629 cycles

AFT PIT LH SIDE STATION 1400 ABOVE STRINGER 26L TOP OF FRAME DENTED. MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW DOUBLER, STRAP AND CAP INSTALLED.

Part: CARBON SEAL — WORN (ENGINE) · airframe 18,888 hrs · 7,147 cycles

SMOKE FILLED AIRCRAFT IMMEDIATELY AFTER TAKEOFF. UPON DISASSEMBLY AT THE TURBINE SHOP, THE NR 2/3 CARBON SEAL WAS FOUND WORN.

Part: CARBON SEAL — WORN (ENGINE) · airframe 18,888 hrs · 7,148 cycles

SMOKE FILLED AIRCRAFT IMMEDIATELY AFTER TAKEOFF. UPON DISASSEMBLY AT THE TURBINE SHOP, THE NR 3 BEARING AFT CARBON SEAL WAS FOUND WORN.

Part: WEB — DENTED · airframe 18,816 hrs · 7,119 cycles

FOUND DAMAGED WEB IN AREA OF FUSELAGE DENT. BELOW DOOR 1 LEFT STATION 220 AT FLOOR LINE. MAJOR REPAIR ACCOMPLISHED. INSTALLED OF NEW SHEAR TIE.

Part: SMOKE — DETECTED (COCKPIT) · airframe 17,773 hrs · 6,719 cycles

SMOKE IN FLIGHT DECK AND MAIN CABIN. *S/D* UNABLE TO DUPLICATE PROBLEM. ALL SYSTEMS OPERATE NORMALLY. ACCOMPLISHED PACK BURNOUT.

Part: CONNECTOR — BROKEN (CIRCUIT BREAKER) · airframe 15,988 hrs · 6,080 cycles

120 KTS STBY BUS OFF LIGHT ILLUMINATED. SELECTED STBY POWER SELECTOR TO BATTERY, OFF LIGHT WENT OUT AND DISCHARGE LIGHT ILLUMINATED. SUPPLEMENTAL DATA UPDATE REPLACED BROKEN CONNECTOR AT DC STANDBY BUSS OFF CIRCUIT BREAKER 6A3. (BOEING SPEC BACC45FT18-8P7)

Part: LIGHTS — MALFUNCTIONED (CABIN)

AFTER PLACING THE EMERGENCY LIGHTS SWITCH TO OFF POSITION, ALL EMERGENCY LIGHTS CAME ON.

Part: INVERTER — FAILED (CABIN)

EMERGENCY EGRESS LIGHTING ROWS 23 THROUGH 28 INOP. REPLACED INVERTER FOR EMERGENCY EGRESS LIGHTING, OPERATION CHECKS NORMAL.