N595UA

Part: DOOR SILL — CORRODED (BS 1397-1420) · airframe 74,310 hrs · 19,463 cycles

CORROSION FOUND ON THE AFT CARGO DOOR SILL AROUND SEVERAL FASTENERS FROM BS 1397 TO 1420. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-A2-F101. EMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02, PG 6-7, DWG 146N8522 , AND EC/RA 5310-07401.

Part: FRAME — DENTED (BS 1420) · airframe 74,310 hrs · 19,463 cycles

FOUND THE FRAME UPPER FLANGE DENTED BS 1420, STRINGER 25L TO 26L, FOUND OUT OF LIMITS IAW SRM 53-00-07-A1-F. CUTOUT AREA, FABRICATED, AND INSTALLED A REPAIR IAW SRM 53-00-07-R5-F 201.

Part: CHANNEL — CORRODED (RT OVERWING) · airframe 74,310 hrs · 19,463 cycles

RIGHT FWD OVERWING ESCAPE HATCH, LOWER NUTPLATE CHANNEL HAS CORROSION. REMOVED AND REPLACED THE LOWER NUTPLATE CHANNEL IAW DRAWING 414N1003, AND SRM 51-40-02, PAR 4, 5, AND 7. FOUND OUT OF LIMITS IAW SRM 52-00-0 2-A1

Part: FRAME — DENTED (BS 1400) · airframe 74,310 hrs · 19,463 cycles

FOUND FRAME UPPER FLANGE DENTED IN THE AFT CARGO AT BS 1400 STRINGER 26L, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-A1, FIG 101. CUT OUT THE DAMAGE, FABRICATED AND INSTALLED A REPAIR IAW SRM 53-00-07, REPAIR 5.

Part: CHANNEL — CORRODED (RT OVERWING) · airframe 74,310 hrs · 19,463 cycles

RIGHT AFT OVERWING ESCAPE HATCH, LOWER NUTPLATE CHANNEL HAS CORROSION, FOUND TO BE OUT OF L IMITS IAW SRM 52-00-02-A1. REMOVED AND REPLACED THE CHANNEL IAW SRM 51-40-05, PG 1-5, AND DWG 144N6302.

Part: DOOR SILL — CORRODED (CABIN) · airframe 74,310 hrs · 19,463 cycles

B757-53-3-6494 OFF AIRCRAFT PART. CORROSION FOUND AFTER REMOVAL OF PART FOR F.O.M. AFT CARGO DOOR SILL (UPPER CHORD) CORROSION A T NUMEROUS LOCATIONS, TO INCLUDE UNDER NUTPLATES 5995-918 AFT CARGO DOOR SILL UPPER CHORD AT STA 1345-1465 RBL 22-5 CORROS ION REMOVAL FOUND OUT OF LIMITS IAW B757-200 SRM 53-60-15 FIG 10 1 L=.5, W=.5, D=.035. LOCATED NEW CHORD P/N 146N8522-57, PO SAG1 890693 IAW B757-200 SRM 51-40-05. SEE CARD 0019657 FOR REMOVAL A ND INSTALL.

Part: LIGHT — FALSE ACTIVATION (R2 DOOR SLIDE) · airframe 73,472 hrs · 19,301 cycles

R2 DOOR IS DISARMED, BUT THE SLIDE INDICATOR LIGHT REMAIN ILLUMINATED, SLIDE PACK LIGHT SHOULD EXTINGUISH. PERFORMED A FUNCTIONAL CHECK OF THE R2 DOOR, SLIDE ARMS AND DISARMS NORMALLY. ALL INDICATION NORMAL. ACFT OK TO CONTINUE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,926 hrs · 19,196 cycles

GREEN EMERGENCY LIGHT INOPERATIVE AT 21F. FOUND INVERTER FAILED (M10950). REPLACED THE INVERTER AND OPS CHECKED GOOD.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 72,926 hrs · 19,196 cycles

GREEN EMERGENCY EXIT INDICATOR LIGHT INOPERATIVE AT 20A, FOUND THE INVERTER FAILED (M10950). REPLACED THE INVERTER AND OPS CHECKED GOOD.

Part: LATCH — BROKEN (COCKPIT) · airframe 72,811 hrs · 19,174 cycles

EMERGENCY EQUIPMENT F/O - ESCAPE STRAP/COVER DEFECTIVE FO ESCAPE ROPE COVER UNABLE TO BE SECURED SHUT. FOUND ESCAPE ROPE UPPER LATCH ASSY BROKEN, REPLACED LATCH. OPS C HECK OK.

Part: SIGN — DETACHED (CABIN) · airframe 72,811 hrs · 19,174 cycles

AISLE OVERHEAD EMER EXIT SIGN NEEDS REATTACHING. REPLACED OVERWING EXIT SIGN AND CHECK OK

Part: SIGN — LOOSE (ROW 20) · airframe 72,785 hrs · 19,169 cycles

EXIT SIGN, LEFT SIDE BY ROW 20 WILL NOT STAY UP. ADJUSTED THE EXIT SIGN BACK IN PLACE.

Part: SIGN — DETACHED (SEATS 20ABC) · airframe 72,785 hrs · 19,169 cycles

SEAT 20ABC EMERGENCY EXIT SIGN DETACHED. SECURED THE SIGN.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 72,544 hrs · 19,123 cycles

EMERGENCY EXIT LIGHT LENS OVER THE L3 DOOR MISSING. REPLACED THE LENS.

Part: CONTROL SWITCH — BURNED (APU) · airframe 71,958 hrs · 19,011 cycles

STRONG ELECTRICAL ACRID ODOR THROUGHOUT CABIN. REPLACED A BURNED APU CONTROL SWITCH IAW WDM 24-27-41. OPS CHECKED GOOD.

Part: SENSOR — FAULTY (L1 DOOR) · airframe 71,380 hrs · 18,900 cycles

1L SLIDE LIGHT ON WITH DOOR DISARMED REPLACED FWD GIRT BAR PROXIMITY SENSOR IAW MM 25-66-11, OP-CHECKS GOOD.

Part: LANYARD — OUT OF POSITION (L2 DOOR) · airframe 71,280 hrs · 18,881 cycles

2L WONT DISARM, REPOSITIONED DOOR 2L SLIDE BUSTLE. SURVIVAL ATTACH LANYARD INTERFERING WITH GIRT BAR ARMING PAWL. ALL OPS OK AFTER REPOSITIONING. PER AMM 25-66-00 NO ADJ NEEDED.

Part: SIGN — DETACHED (EMERGENCY LIGHT) · airframe 71,108 hrs · 18,848 cycles

EMERGENCY EXIT SIGN OVER THE L2 DOOR FELL OFF. ATTACHED THE SIGN.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,790 hrs · 18,787 cycles

EMERGENCY LIGHT INOPERATIVE AT STOW BIN 2FE. REPLACED THE LAMP, CHECKED OK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,817 hrs · 18,205 cycles

MAIN CABIN FLOORBEAM UPPER CHORD CORRODED AT BS 1640 BETWEEN BL0 AND RBL 24.75. REMOVED CORROSION AND FOUND BLEND OUT EXCEED SRM LIMITS. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED NEW UPPER CHORD SPLICE. REPAIR CHORD FROM RBL63-LBL 24.75 REF ECRA 5310-05536 AND SRM 53-00-51, REPAIR NR 10.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,817 hrs · 18,205 cycles

LOWER LOBE AT BS 1642, STR S-22R WAS FOUND CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED STR SECTION FROM BS1620-1652. ACP HFEC INSPECTION OF OPEN FASTENER HOLES. NO CRACKS FOUND. FABRICATED AND INSTALLED STR SPLICE REPAIR REF SRM 53-00-03, REPAIR 1.

Part: SKIN — PUNCTURED (R4 DOOR) · airframe 67,817 hrs · 18,205 cycles

R-4 DOOR INNER SKIN WAS FOUND PUNCTURED NEAR UPPER HINGE. FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIR REF ECRA 5210-02732.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,817 hrs · 18,205 cycles

SUPPORT TASK, MAIN CABIN FLOOR CENTER SECTION FROM STA 900 TO STA 1020 AND RBL 63 FLOOR SUPPORT ANGLE HAS EVIDENCE OF SURFACE CORROSION. R & R NEW FLOOR SUPPORT ANGLE, PN BAC1515-551, PO 1402636, STA 900-1020, RBL 63, IAW SRM 51-40-02.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,817 hrs · 18,205 cycles

WING CTR FUEL TANK SECTION. UPPER SKIN HAS EVIDENCE OF CORROSION UNDER INTERCOSTAL FITTING BS 930, RBL 61. REPAIR AT CTR FUEL TANK UPPER SKIN PANEL, STATION 980, RBL 61 APPROX IAW RES 2010587-23.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 67,158 hrs · 18,070 cycles

LEADING EDGE SLAT DISAGREE. EMER DECLARED WITH ATC IAW FIM. OPERATED SLATS SEVERAL CYCLES WITH NORMAL HYD OPERATIONS & ALTERNATE ELEC LE SLAT MOVE FREELY & NO ECAS MSG NOTED. CHECKED PDU FOR LEAKS, NO LEAKS NOTED. PERFORMED FSEU BITE PROCEDURE IAW FIM, NO FAULTS.

Part: SKIN — WORN (TE FLAP) · airframe 62,484 hrs · 17,164 cycles

RIGHT WING INBD MAIN FLAP UPPER OTBD EDGE WORN IAW ECRA 5753-01414. THE RT INBD FLAP UPPER SKIN REPAIR RECEIVED FIRST STAGE APPROVAL. A NEW FAA 8100-9 APPROVAL SHOWING COMPLIANCE WITH 14 CFR 26.43 D & 25.571 IS REQUIRED ON OR BEFORE 20 OCT 2014 FOR THE ACFT TO REMAIN AIRWORTHY. VIA ECRA 5753- 01414 REV A REPAIR IS NOW A PERMANENT REPAIR ON RT INBD MAIN FLAP UPPER INBD SKIN PANEL.

Part: SKIN — GOUGED (R2 DOOR) · airframe 62,484 hrs · 17,164 cycles

DENT GOUGE IN R2 DOOR OUTER SKIN JUST AFT 13 STATION 720. REPAIRED R2 DOOR OUTER SKIN BETWEEN DOOR BEAMS NR 4 & NR 5 AT BS 720 IAW ECRA 5210-02511. THE R2 DOOR SKIN RECEIVED 1ST & 2ND STAGE APPROVAL. THE INSPECTION THRESH HOLD FOR THIS REPAIR IS 30000 PTC. A NEW FAA APPROVAL FINDING COMPLIANCE WITH 14CFR26.43 D & 25.571 IS REQUIRED BEFORE THE ACFT REACHES 30000 PTC FOR THE ACFT TO REMAIN AIRWORTHY AFTER THAT TIME. CONTACT ENGINEERING AFTER THE ACFT COMPLETES 28000 BUT BEFORE 29000 PTC FOR DISPOSITION IAW ECRA 5210-02511.

Part: CONTROL VALVE — FAULTY (RT ENGINE) · airframe 62,304 hrs · 17,128 cycles

RIGHT ENG STARTER EICAS & START VLV LIGHT DURING RT ENG START. NORMAL START INDICATIONS. ACCOMPLISHED MANUAL START ON GATE, START VLV LIGHT OPERATIONS NORMAL. REPLACED RT ENG STARTER CONTROL VLV IAW MM80-11-02 & RELAYS K10251 & K10221. RAN RT ENG, VLV LIGHT OPERATIONS CHECK NORMAL.

Part: START VALVE — FAULTY (RT ENGINE) · airframe 61,586 hrs · 16,992 cycles

RIGHT ENG NO START. DURING A NORMAL START, START VLV LIGHT STAYED ON DURING THE WHOLE CYCLE EXTINGUISHED AFTER CUT OUT. REPLACED RT ENG START VLV & CHECKED OK IAW AMM 80-11-02.

Part: WIRE — PINCHED (CABIN) · airframe 61,242 hrs · 16,928 cycles

DOOR 2RT EMERGENCY SLIDE LIGHT IS INOPERATIVE. RELAMPED & CLEANED LAMP SOCKET, NO HELP. REPLACED EMERGENCY LIGHT POWER SUPPLY ASSEMBLY M732 ABOVE DOOR 2 RT, NO HELP. RANG WIRE FROM POWER SUPPLY CONN D70 POS 9 TO LAMP ASSEMBLY CHECKED OK. LIGHT ASSEMBLY GND IS GOOD. POWER SUPPLY ASSEMBLY M732 IS BLOWING THE FUSE TO THE SLIDE LT. CHECKED FOR SHORTS FROM D70 POS 9 WITH LAMP OUT, NO SHORT FOUND. FOUND WIRE W3632-0110-18 PINCHED IN STOW BIN SUPPORT ROD AT STATION 790, REPAIRED IAW SWP 20-10-13, IAW WD 33-51-13, OPERATIONS CHECKED NORMAL.

Part: SOCKET — DIRTY (OVERHEAT SYS) · airframe 60,691 hrs · 16,821 cycles

LT ENG OVERHEAT LIGHT FAILS TO ILLUMINATE WHEN DOING FIRE TEST, ADD LIGHT TEST. CLEANED LIGHT SOCKET, TESTED OK.

Part: GCU — FAULTY (LEFT) · airframe 60,241 hrs · 16,734 cycles

AFTER RT ENG START GEN DID NOT COME ON LINE, SELECTED GEN OFF-ON, NO HELP. BIT BPCU HAD FAULT LT GCU REPLACED, WOULD NOT RESET. RESET BREAKER STILL WOULD NOT CLEAR. REPLACED LT GCU IAW MM 24-22-02. TESTED ALL GCU NO FAULTS. RAN ENGS ALL CONFIGS ASSOCIATED GEN PICKED UP LOAD, AFTER RUNS BPCU CLEAN, NO FAULTS.

Part: IDG — FAULTED (RT ENGINE) · airframe 60,189 hrs · 16,724 cycles

RT IDG FAULT. RTFL.

Part: GENERATOR — FAULTY (RT ENGINE) · airframe 60,169 hrs · 16,719 cycles

RT GENERATOR FAULTS LEVEL 1. IF OIL QTY IS LOW, PLEASE EXAMINE OIL COOLING SYSTEM FOR ANY EXTERNAL LEAKS. IF NONE FOUND SUGGEST REPLACING THE FUEL OIL COOLER PCN 645-9029 IAW AMM 79-21-01 PB. 401. AS PRECAUTION AS THIS COULD HAVE AN INTERNAL LEAK WHERE OIL LOSS IS OCCURRING. ALSO ACCOMPLISH SERVICE TIP 24-20-00-100A TO CHECK IDG ELEC CONNECTOR FOR WEAR OR DAMAGE. LEVEL 1 CHRONIC

Part: PUMP — FAILED (NR 2 HYD SYSTEM) · airframe 60,071 hrs · 16,700 cycles

RT ENGINE HYD PUMP EICAS MESSAGE. TURNED OFF & VERIFIED NO RT SYSTEM PRESSURE. REPLACED RT ENGINE DRIVEN PUMP. RAN ENG IAW JRH 2-5-8, OPS CHECKED NORMAL.

Part: IDG — FAULTY (RT ENGINE) · airframe 59,984 hrs · 16,683 cycles

RT GEN TRIPPED OFF ON TAKEOFF ROLL, ABORTED AT 60-70 KTS. RESET GEN ATTEMPTED ANOTHER TAKE OFF, GEN TRIPPED AGAIN DURING 2ND TAKE OFF ATTEMPT. FOUND NR 2 IDG OIL QTY LOW. REPLACED NR 2 IDG IAW MM, OPERATIONS CHECKED GOOD.

Part: MINITEL — BROKEN (COCKPIT) · airframe 59,978 hrs · 16,682 cycles

CAPT MINITEL BOOM MIKE BROKE. REPLACED WITH FLIGHT DECK SPARE. REPLACED BROKEN MINTEL & INSTALLED IN SPARE MINITEL BAG.

Part: STRIKER — DEFECTIVE (COCKPIT DOOR) · airframe 59,936 hrs · 16,674 cycles

COCKPIT DOOR WILL NOT STAY SECURELY CLOSED. DEF IAW MEL. REPLACED COCKPIT DOOR STRIKER IAW MM, OPERATIONS CHECKED OKAY.

Part: UNKNOWN — MALFUNCTIONED (AUTOPILOT SYS) · airframe 59,843 hrs · 16,656 cycles

AIRPLANE HAS PITCH OSCILLATION, PORPOISES, WITH ANY A-P CHANNEL IN CMD & V-S, ALT HOLD, FLCH, VNAV MODE SELECTED. WORSE IN VNAV PATH AT CRZ. +- 60 FEET AT ALTITUDE. ACP MCDP TEST 30 & 40 NO FAULTS FOUND. CHECKED ELEV PCA'S. ELEV OPERATIONS FOUND TO BE NORMAL IAW MM.

Part: IDG — FAULTY (NR 3 ENGINE) · airframe 59,586 hrs · 16,606 cycles

RT GEN CONT LT ILLUMINATED IN CRUISE, WENT AWAY. REAPPEARED ON DESCENT. OPS NORMAL BUT BROKE DRIVE SAFETY WIRE. IDG DRIVE WAS NEVER DISCONNECTED, ONLY SAFETY WIRE BROKEN. ECS PAGE SHOWS " R IDG OIL L EVEL" MAINT STATUS MSG. COMPLIED WITH MEL. GEN DISC AND GEN CONT PUSH BUTTON SWITCHES COVERED WITH TAPE PER MEL ** DL1614 CREATED TO MONITOR ** REPLACED R ENG IDG PER MM AND ACCOMPLISHED TEST AND CHECK PER JRH 2-5-1. OPS CK OKAY.

Part: FASTENER — MISSING (RT NACELLE) · airframe 59,406 hrs · 16,570 cycles

RIVET MISSING ON RT SIDE OF RT PYLON AFT REGION. REPLACED FASTENER.

Part: IDG — FAILED (RT ENGINE) · airframe 59,335 hrs · 16,556 cycles

RT GENERATOR DRIVE EICAS ON, DISCONNECTED GENERATOR DRIVE. IDG HAD LOW OIL. R & R NR 2 IDG IAW MM.

Part: SEAL — LEAKING (NR 2 IDG) · airframe 59,335 hrs · 16,556 cycles

FOUND NR 2 ENGINE IDG DRIVE SEAL LEAKING. R & R NR 2 ENG IDG DRIVE SEAL IAW MM, NO LEAKS ON IDLE RUN.

Part: GROUND STUD — FAILED (EMERGENCY LIGHTS) · airframe 59,330 hrs · 16,554 cycles

EMERGENCY LIGHT UNDER INTERIOR STOW BIN BETWEEN SEAT ROW 3FE AND 4FE DOES NOT ILLUMINATE. FOUND BAD GROUND TO LUG, REPAIRED GROUND, OPS CHECKED NORMAL.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 58,874 hrs · 16,464 cycles

R2 DOOR EXIT SIGN LENS FELL OFF. REPLACED LENS ASSY.

Part: SIGN — MISSING (CABIN) · airframe 58,827 hrs · 16,455 cycles

EXIT SIGN AT 2R IS LOOSE, SECURED SIGN.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 58,776 hrs · 16,445 cycles

EMERGENCY LIGHTS SYS TEST AMM 33-51-00-735-013 FAILED OPS TEST FOR THE FOLLOWING: LIGHT R1 DOOR EXIT SIGN, R1 DOOR ESCAPER SLIDE, ROW 7 CEILING EXIT SIGN, AISLE LIGHT BETWEEN ROW 7BC AND ROW 20EC. RT EMERGENCY EXIT SIGN ABOVE DOORS, FWD RT EMERGENCY EXIT IDENTIFIER LT AFT EMERGENCY EXIT. PERFORMED TROUBLESHOOTING OF EMERGENCY LIGHT SYS IAW AND 33-51-21 AND FOUND CONNECTOR D5472 AND D7722 DISCONNECTED. RECONNECTED CONNECTORS AND PERFORMED OPS CHECK IAW AMM 33-51-00, OPS CHECK NORMAL. SN 1798547, 895948.

Part: WIRE — REVERSED (CABIN) · airframe 58,776 hrs · 16,445 cycles

PASSENGER LOADING LIGHTS, OPS CHECK FAILED DUE TO BREAKER GIRT BAR FWD DIM R33 TRIPPING WHEN L1 DOOR SLIDE IS ARMED. ON T/S FOUND WIRES SWAPPED ON LIGHT ASSY L403 LT GIRT BAR REPOSITION WIRES TO CORRECT TERMINAL ON L403 IAW WD 25 66 11. PERFORMED PASSENGER LOADING LIGHTS TEST, CHECKED NORMAL IAW AMM 33-22-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,770 hrs · 16,443 cycles

EEL EXIT SIGN MARKERS INOP 1L 1R, 1A BULL NOSE. REPLACED M731 CHARGER RELAMPED 1A AND DOOR 1 LEFT ALL LIGHT BULBS FOR EXIT SIGN AND RELAMPED 2A, OPS CHECK OK. VERIFIED PER IDT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,770 hrs · 16,443 cycles

EMERGENCY EXIT SIGNS INOPERATIVE 1L 1R, 1A BULL NOSE. EMERGENCY LIGHT AT 2C ALSO INOPERATIVE. SYMPTOMS CHANGE WITH DIFFERENT CHARGERS REPLACED. REPLACED M731 CHARGER RELAMPED 1A AND L1 DOOR ALL LIGHT BULBS FOR EXITING AND REPLACED LAMPS 2A, OPS CHECKED OK.

Part: CONTROL UNIT — FAILED (ELEVATOR) · airframe 58,766 hrs · 16,442 cycles

LEFT ELEV PCU EICAS WON'T CLEAR. HARD FAULT ELEVATOR PCU. FOUND OUTBOARD PCA AT FAULT. REMOVED AND REPLACED LT OB ELEVATOR.

Part: CONTROLLER — FAULTY (NR 1) · airframe 58,666 hrs · 16,414 cycles

ENGINE DUCT PRESSURES SPLIT DURING CRUISE WITH ISOL VLV CLOSED & BLEED SWITCH SELECTED ON. RECORD DUCT PRESSURES. REPLACED 14TH STG CONTROLLER. REVERSED MEL RAN PER JRH, OPS CHECK GOOD.

Part: FAN — NOISY (COCKPIT) · airframe 56,661 hrs · 15,844 cycles

RECIRC FAN NOISE VERY LOUD ON FLT DECK. RIGHT RECIRC CAUSING EXCESSIVE NOISE INFLIGHT. RPL- :REMOVED AND REPLACED RECIRC FAN.

Part: COVER — LOOSE (CABIN) · airframe 58,661 hrs · 16,411 cycles

AFT CABIN EMERGENCY LIGHT CLEAR COVER LOOSE. CLEANED TRACK RE-INSTALLED PLASTIC COVER AND OPS CHECKED EMERGENCY LIGHTS GOOD.

Part: STABILIZER — DAMAGED (RIGHT) · airframe 58,641 hrs · 16,404 cycles

RIGHT STAB HAS A CREASE 10 FT INBD OF OTBD EDGE 1 FT LONG .5 DEEP,STARTS AT LEADING EDGE AND GOES AFT. ACP'D HFEC OF CREASED AREA IAW NDTM 51-10-08 PART 6. NO CRACKS INDICATED.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 58,641 hrs · 16,404 cycles

HOLE IN AFT PIT FLOOR CENTER FLOOR JUST AFT OF DOOR. APPROX 1 INCH DIA. TEMP REPAIR MADE PER GNMM. DAMAGE IS 3" X 2" AREA, WILL NEED EITHER DOUBLER REPAIR OR CARGO FLOOR REPLACED. REPAIRED DECK PANEL IAW SRM.

Part: COUPLER — FAILED (HF SYSTEM) · airframe 58,631 hrs · 16,402 cycles

LEFT HF RADIO FAILED TO TUNE OR TRANSMIT IN FLIGHT. GROUND TESTED LEFT HF RADIO, OP CHECKED OK. RANG-OUT COAX CABLE FROM M241 AT COUPLER TO LEFT HF TRANSCEIVER M152 READ 1.23 OHMS. JUMPED BETWEEN CENTER CONDUCTOR AND SHIELD. REPLACED LEFT HF COUPLER PER AMM, OP CHECKED GOOD.

Part: TRANSCEIVER — FAULTED (LT HF SYS) · airframe 58,547 hrs · 16,373 cycles

LEFT HF NOT TUNING, NOT RECEIVING, TRANSMITS INTERMITTENTLY. REPLACED LEFT HF TRANSCEIVER, GROUND CHECKED GOOD IAW 23-11-00 & 23-11-03.

Part: CONTROL PANEL — MALFUNCTIONED (AUDIO CONTROL) · airframe 58,355 hrs · 16,317 cycles

NR 2 AUDIO SELECTOR PANEL HAS BLEED THREW. LOUD 400 HZ TONE IN FIRST OFFICER`S HEADSET ANYTIME AISLE STAND BACKLIGHTING IN ON AT ANY LEVEL. REPLACED F/O AUDIO CONTROL PANEL IAW AMM, OPS CHECKED GOOD.

Part: LIGHT — UNSECURE (AFT CABIN) · airframe 58,338 hrs · 16,311 cycles

EMERGENCY LIGHT LOOSE IN AFT CABIN. SECURED LIGHT, OPS GOOD.

Part: LIGHT — UNSECURE (CABIN) · airframe 58,323 hrs · 16,308 cycles

EMERGENCY EXIT LIGHT COVER DETACHED NEAR ROW 12. SECURED LIGHT.

Part: DISPLAY — FAILED (COCKPIT) · airframe 58,181 hrs · 16,261 cycles

LEFT CDU FAILURE, RTFL.

Part: IDG — FAULTY (LT GENERATOR) · airframe 57,827 hrs · 16,161 cycles

"DRIVE" ILLUMINATED ON LEFT GEN DRIVE DISC SWITCH. CREW REPORTED RIGHT ENGINE DRIVE LIGHT IS NOT ILLUMINATED WHEN ENGINE IS SHUTDOWN. REPLACED RIGHT ENGINE IDG IAW MM 24-11-01, OPERATIONAL CHECK OK AND NO LEAKS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,727 hrs · 16,161 cycles

EMERGENCY EXIT FLOOR LIGHT OUT BY SEAT 40. REPLACED LIGHT STRIP. EMERGENCY LIGHTS OP CHECKED GOOD.

Part: EEC — FAULTY (NR 2 ENGINE) · airframe 57,821 hrs · 16,158 cycles

MAINT REPORTED THAT WITH AUTO THROTTLE DISCONNECT FOUND EEC R PRI MESSAGE ON MULTIPLE LEGS REPLACED EEC AND TESTED REF AMM.

Part: WIRE — BROKEN (HANDSET JACK) · airframe 57,789 hrs · 16,149 cycles

FWD JUMPSEAT INTERPHONE HAS STATIC, PA IS OKAY. REPAIRED BROKEN WIRE ON HANDSET JACK PER WDM.

Part: DOOR SEAL — OBSTRUCTED (L1 DOOR) · airframe 57,702 hrs · 16,128 cycles

DOOR 1L HAS SILICONE AND TRIM ENCROACHING INTO DOOR SEAL AREA AT FORWARD FRAME. REMOVED MATERIAL AND CLEANED SEAL AREA.

Part: DOOR SEAL — OBSTRUCTED (R1 DOOR) · airframe 57,702 hrs · 16,128 cycles

DOOR 1R HAS SEALANT ENCROACHING INTO SEAL MATING SERVICE. CLEANED SEALING SERVICE.

Part: DOOR SEAL — OBSTRUCTED (L4 DOOR) · airframe 57,702 hrs · 16,128 cycles

DOOR 4L HAS SEALANT ENCROACHING INTO SEAL MATING AREA AT FWD FRAME. REMOVED AND CLEANED SEAL AREA.

Part: DOOR SEAL — OBSTRUCTED (R4 DOOR) · airframe 57,702 hrs · 16,128 cycles

DOOR 4R HAS SEALANT ENCROACHING INTO SEAL MATING AREA AT FWD FRAME. REMOVED MATERIAL AND CLEANED SEAL BEARING AREA.

Part: DOOR SEAL — OBSTRUCTED (R2 DOOR) · airframe 57,702 hrs · 16,128 cycles

DOOR 2R HAS SEALANT ENCROACHING INTO SEALING AREA AT FWD FRAME. REMOVED AND CLEANED SEAL BEARING AREA.

Part: DOOR SEAL — OBSTRUCTED (L2 DOOR) · airframe 57,702 hrs · 16,128 cycles

DOOR 2L HAS SEALANT ENCROACHING INTO SEAL MATING AREA AT FWD FRAME. REMOVED SEALANT AND MATERIAL FROM SEAL AREA.

Part: ACM — FAULTY (AC BAY) · airframe 57,669 hrs · 16,119 cycles

WHILE GATE ON APU PNEUMATICS, CCKPI TEMP RAN WAY HOT. UNABLE TO COOL CCKPT W- ENGINE ON PACK. REPLACED LEFT ACM PER MM, OPS CHECKS GOOD.

Part: SWITCH — STICKS (AUDIO PANEL) · airframe 57,569 hrs · 16,095 cycles

SWAPPED L ASP WITH 1ST OBSERVERS ASP DUE TO CAPT PTT SWITCH STICKING. REPLACED 1ST OBSERVERS ASP, OPS CHECK GOOD.

Part: SEAL — KINKED (L1 DOOR) · airframe 57,490 hrs · 16,075 cycles

DOOR 1L HAS LOUD SQUEAL BELOW FL180 POSSOBLE SEAL LEAK. FWD EDGE DOOR SEAL KINKED BY LOWER GATE AREA, LOWER DOOR HINGE LEAKING, ALSO DUE TO EXCESSIVE SEALANT. ADJUSTED LOWER FWD SEAL TO REMOVE KINK, PRESSURIZED AC TO 4 PSI.

Part: FIRE DETECTOR — NO TEST (MLG WW) · airframe 57,314 hrs · 16,031 cycles

WHEEL WELL FIRE DET WILL NOT TEST. BRAKES ARE COOL TO TOUCH. OK TO DEFER. OK FOR SERVICE PER MM.

Part: ACTUATOR — LEAKING (LT MLG) · airframe 57,234 hrs · 16,009 cycles

OIL LEAKING FROM LEFT MAIN GEAR. REF AMM 29-00-99 PG 603 4 DROPS PER MIN PRESSURIZED LEFT GEAR TILT ACTUATOR ROD END SEAL 0 DROPS PER MIN UNPRESSURIZED. PARTS: 643-9106 MR32338 ACTUATOR *SPA* LOB:N. REPLACED LEFT MLG TILT ACTUATOR REF MM. TESTED WORKS OK, NO LEAKS.

Part: SKIN — WORN (RT WING TE FLAP) · airframe 57,116 hrs · 15,979 cycles

RIGHT WING MAIN FLAP EDGE WORN. FLAP SKIN REPAIRED PER ECRA 5753-01414.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 57,116 hrs · 15,979 cycles

ACP INTERIM REPAIR TO FUSELAGE SKIN FROM BS 1420-BS 1480 BET STR 18L-22L IAW ECRA 5331-01654.

Part: SKIN — DENTED (BS 570-660 S14L) · airframe 57,116 hrs · 15,979 cycles

DENT IN FUSELAGE 5 FRAMES FWD OF DOOR 2L, 2 STRINGERS BELOW SKIN LAP. DENT APPROX 8 IN LONG, 4 IN WIDE, 3-8 IN DEEP AND EXTENDS INTO EXISTING DOUBLER. SUPPLEMENTAL DATA UPDATE, INSTALLED NEW REPAIR PER ECRA 5331-01652 AND TIMCO REO G15485 STA 570-660, STR 14L-19L, THIS REPAIR WILL NEED A NEW 8100-9 APPROVAL SHOWING COMPLIANCE WITH 14 CFR 26.43(D) AND 25.571 ON OR BEFORE 10-26-14 OR ACFT BECOMES UNAIRWORTHY. CF-9027 REPAIRED

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 57,116 hrs · 15,979 cycles

STR 20L AT APPROX STA 1455 HAS DAMAGED HOLE. REPAIRED IAW SRM 53-00-03 RPR 1.

Part: SKIN — DAMAGED (BS 1480 S21L) · airframe 57,116 hrs · 15,979 cycles

AFT FUSELAGE, MISDRILLED HOLE IN SKIN AND STRINGER AT STA 1480, STR 21L. SUPPLEMENTAL DATA UPDATE, REPAIRED STR 21L IAW SRM 53-00-03, RPR 1.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 57,116 hrs · 15,979 cycles

LEFT AFT FUSELAGE EXTERNAL SKIN WRINKLED IN AREA OF STATIC PORT AT BS 1360-1440 BETWEEN STR 20L-24L. MAJOR REPAIR ACCOMPLISHED: EVALUATED DAMAGED AREAS & FOUND OUT OF LIMITS OF SRM 51-10-01 FIG 7 DETAIL 7. REMOVED ADJACENT EXISTING FLUSH REPAIR & CUT-OUT DAMAGED AREAS REF REO-G15546 & ECRA-5361-01027. ACP NDT OF CUT-OUTS & FASTENERS COMMON TO THE REPAIR AREA. NO DEFECTS. FABRICATED & INSTALLED EXTERNAL DOUBLER, FILLER & TAPERED FILLER REPAIR REF 094632 REO-G15546 & ECRA 5361-01027.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 57,116 hrs · 15,979 cycles

FUSELAGE STRINGER 16L AT BS 615 WAS FOUND DAMAGED FROM PREVIOUS REPAIR INSTALLATION. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SECTION OF STRINGER FROM BS 590-650. ACP NDT OF FASTENER HOLES FOR CRACKS NONE FOUND. FABRICATED & INSTALLED STRINGER SPLICE REPAIR REF SRM 53-00-03 REPAIR NR 1 ZONE 1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,116 hrs · 15,979 cycles

BS 324 FLOORBEAM UPPER CHORD "T" CAP FOUND CORRODED NEAR EXISTING REPAIR. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION & FOUND MATERIAL LOSS OUT OF SRM LIMITS. REMOVED EXISTING REPAIR & ACP NDT OF HOLES COMMON TO REPAIR. NO CRACKS. FABRICATED & INSTALLED UPPER "T" CHORD REPAIR REF SRM 53-10-08 REPAIR NR 1 ITEM 4C.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 57,116 hrs · 15,979 cycles

DAMAGE FOUND TO EXISTING FUSELAGE EXTERNAL DOUBLER REPAIR (CF0395) AT BS 640-660 BETWEEN STR 21L-22L. MAJOR REPAIR ACCOMPLISHED: REMOVED EXISTING REPAIR DOUBLER & FOUND DAMAGED FASTENER HOLES. TRIMMED OUT DAMAGE & ACP NDT OF CUTOUT & FASTENER HOLES COMMON TO REPAIR. NO DEFECTS. FABRICATED & INSTALLED EXTERNAL DOUBLER & FILLER REPAIR REF ECRA 5330-04352 & REO-G15496 REV D.

Part: CIRCUIT BREAKER — INTERMITTENT (CABIN OXYGEN) · airframe 57,116 hrs · 15,979 cycles

PASSENGER CABIN RIGHT SIDE OXYGEN SYSTEM DROP CHECK FAILED DURING ACCOMPLISHMENT OF TASKCARD 5R35I1138. TROUBLESHOT OXYGEN SYS REF B757 WDM 35-21-11. FOUND PASSENGER OXYGEN R CIRCUIT BREAKER P-N 2TC47-5 TO BE INTERMITTENT. REMOVED, REPLACED & OPS CHECKED CB REF AMM35-21-00 & AMM20-60-05. OPS CHECKED GOOD.

Part: HANDLE — DIRTY (R2 DOOR) · airframe 57,116 hrs · 15,979 cycles

R-2 DOOR FAILED BUTTERFLY CHECK. HANDLE WAS REMOVED CLEANED AND RE-INSTALLED IAW MM.

Part: MECHANISM — OUT OF ADJUST (L4 DOOR) · airframe 57,116 hrs · 15,979 cycles

MAIN CABIN L-4 DOOR FAILED MIDWAY CHECK - GIRT BAR BECAME DETACHED. ADJUSTED L4 PASSENGER DOOR EMERGENCY MECHANISM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,116 hrs · 15,979 cycles

MAIN CABIN INTERCOSTAL UPPER SURFACE OF T- CAP CORRODED BS 324 -BS 365, RBL 0. REMOVED & REPLACED T-CAP AND SUPPORT ANGLE IAW SRM.

Part: BEARING — CHAFED (L2 DOOR) · airframe 57,116 hrs · 15,979 cycles

L-2 DOOR UPPER LATCH BEARINGS, (BOTH FORWARD AND AFT) ARE CHAFING AGAINST THEIR RESPECTIVE FITTINGS WHILE CLOSING. REMOVED & REPLACED UPPER LATCH BEARING ON BOTH FWD & AFT L2 DOOR. CHECKED ALL CLEARANCES & DIMENSIONS.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 57,116 hrs · 15,979 cycles

MAIN CABIN L-2 DOOR FAILED UNLATCH MINIMUM CHECK. ADJUSTED L2 DOOR UNLATCH TORQUE TO GREATER THAN 200 LBS.

Part: BOLT — GALLED (L1 DOOR) · airframe 57,116 hrs · 15,979 cycles

L-1 DOOR INTERNAL FWD EDGE STOP BOLTS NR 1 THROUGH NR 7 HAVE GALLING. REMOVED & REPLACED, RIGGED AND SAFETIED L1 DOOR FWD STOP PINS, NR 1 THRU NR 7 IAW MM 52-11-00, PARA.4.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 57,116 hrs · 15,979 cycles

MAIN CABIN R-4 DOOR FAILED UNLATCH TORQUE CHECK. ADJUSTED R4 DOOR UNLATCH TORQUE IAW MM.

Part: MECHANISM — OUT OF ADJUST (R4 DOOR) · airframe 57,116 hrs · 15,979 cycles

MAIN CABIN R-4 DOOR FAILED MIDWAY CHECK. ADJUSTED R4 DOOR MODE SELECTOR LOCKOUT CAM MECHANISM IAW AMM, SEC 3. FUNCTION GOOD IAW AMM 52-11-20, SECTION 3.

Part: STRAP — DAMAGED (FUSELAGE) · airframe 57,116 hrs · 15,979 cycles

SPLICE STRAP P/N 143N3700-22 AT STA 660 DRILLED THROUGH AND DRILL STARTS AT APPROX 2.5" ABOVE STR 21L AND APPROX 2.5" AND BELOW 22L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AT SPLICE STRAP, FAB NEW STRAP REF BOEING DWG 143N3700. INSTALLED REF SRM 51-40-05, 51-20-01, & 51-40-02. N-R 49036.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,116 hrs · 15,979 cycles

MAIN CABIN FLOOR FRAME BS 365 UPPER SURFACE OF T-CAP CORRODED RBL 0 TO RBL 64. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF 'T' CHORD, FABRICATED AND INSTALLED NEW 'T' CHORD, SPLICE ANGLES AND STRAPS.

Part: FLOORBEAM — CORRODED (BS 1661) · corrosion level 2 · airframe 57,116 hrs · 15,979 cycles

AFT CABIN FLOOR WET AREA, BS 1661 FLOORBEAM UPPER TEE HAS AREAS OF CORROSION, CENTERLINE TO RBL56. REMOVED DAMAGED SECTION OF TEE AND FABRICATED A NEW TEE, SPLICE ANGLES AND STRAPS AND INSTALLED PER SRM 53-00-51, REPAIR 3. MAJOR REPAIR.

Part: HANDLE — FAULTY (R1 DOOR) · airframe 57,116 hrs · 15,979 cycles

MAIN CABIN R1 DOOR EXTERNAL HANDLES DO NOT RETRACT CORRECTLY. REMOVED EXTERIOR HANDLES AND SHAFTS. REPLACED NEW OUTER SHAFT TO EXTERIOR HANDLE PER MM AND REINSTALLED HANDLE ASSY PER MM AND FUNCTIONAL CHECKED GOOD.

Part: MECHANISM — OUT OF ADJUST (R2 DOOR) · airframe 57,116 hrs · 15,979 cycles

R2 DOOR FAILED MIDWAY CHECK. ADJUSTED MODE SELECTOR LOCKOUT MECHANISM PER MM AND OPS TESTED GOOD.

Part: LATCH — OUT OF ADJUST (R2 DOOR) · airframe 57,116 hrs · 15,979 cycles

R2 DOOR UNLATCH TORQUE MINIMUM FAILED CHECK. ADJUSTED R2 DOOR UNLATCH TORQUE PER MM, UNLATCHING FORCE IS GREATER THAN 200 INCH-POUNDS WITH SLIDE AND LINERS REMOVED.

Part: HANDLE — OUT OF ADJUST (L4 DOOR) · airframe 57,116 hrs · 15,979 cycles

L4 DOOR FAILED UNLATCH TORQUE CHECK. ADJUSTED L4 DOOR HANDLE UNLATCHING TORQUE PER MM 52-11-00 AND TORQUE CHECKED GOOD.

Part: SHAFT — DEFECTIVE (L4 DOOR) · airframe 57,116 hrs · 15,979 cycles

L-4 DOOR FAILED BUTTERFLY CHECK. REMOVED & REPLACED CENTER SHAFT, INNER SHAFT, THRUST COLLAR AND YOKE. OPS CHECKS GOOD IAW MM 52-11-13.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,116 hrs · 15,979 cycles

AFT CABIN FLOOR WET AREA, NUMEROUS SMALL AREAS OF BARE METAL & LIGHT CORROSION ON WEB AND ATTACHING BRACKETS, STA1680 - STA.1720, C-L TO RBL 57. MAJOR REPAIR ACCOMPLISHED: REMOVED CORRODED DOUBLER AT STA 1680-1686, RBL 28-RBL 39 IAW SRM 51-40-02. FABRICATED AND INSTALLED NEW DOUBLER & FILLER IAW EC-RA 5330-04259, REPAIR 1, FIG 210.

Part: ROLLER — OUT OF RIG (R2 DOOR) · airframe 57,116 hrs · 15,979 cycles

MAIN CABIN R-2 DOOR LATCH ROLLERS OUT OF RIG. ADJUSTED LATCH ROLLERS R2 DOOR PER AMM 52-11-00, RIG CHECK GOOD PER AMM 52-11-00.

Part: HANDLE — FAULTY (R4 DOOR) · airframe 57,116 hrs · 15,979 cycles

R-4 DOOR MAKES UNUSUAL SOUND DURING OPENING AND CLOSING. REMOVED AND INSTALLED R4 DOOR HANDLE ASSY IAW AMM 52-11-13. OPS CHECKS GOOD.

Part: RIVET — LOOSE (FUSELAGE) · airframe 57,091 hrs · 15,973 cycles

REF ECRA 5331-01634 FOUND 1 EA LOOSE RIVET AT STA 616 ON STRINGER 16L. REPLACED LOOSE RIVET. ACP HFEC INSP OF HOLE, NO CRACKS FOUND REF NDT51-00-16 PART 6 RIVET IS SECURE.

Part: SNUBBER — BINDING (COCKPIT WINDOW) · airframe 57,074 hrs · 15,964 cycles

REPEAT WRITE UP. CAPTS WINDOW BINDING. WILL NOT UNLOCK AFTER PRESSURE CYCLE. REPLACED SNUBBER AND ADJUSTED WINDOW, REF AMM 56-11-02.

Part: TUBE — DAMAGED (NR 1 ENGINE) · airframe 57,074 hrs · 15,964 cycles

NR 1 ENGINE BLEED TUBE ASSY ON REAR OF FUEL OIL HEAT EXCHANGER IS DAMAGED ON LOWER END. REMOVED TUBE ASSY, REPLACED TUBE ASSY.

Part: IDG — FAULTY (RIGHT) · airframe 57,054 hrs · 15,956 cycles

RIGHT GEN DRIVE LIGHT EXTINGUISHED ON THE GROUND. RAN ENGINE DISCONNECTED IDG, RECEIVED MESSAGE. CLOSED ENGINE COWL. REPLACED IDG PER MM.

Part: SKIN — DAMAGED (BS 654-661) · airframe 56,727 hrs · 15,863 cycles

PUNCTURE AT BS 654 AND GOUGES BETWEEN BS 656 TO 661 BETWEEN STR 21 AND STR 22. CUT OUT DAMAGE IAW AVO 1385. ACCOMPLISHED HFEC OF AREA REF NDT 51-00-19 PART 6, NO CRACKS FOUND. ACCOMPLISHED REPAIR REF AVO 1385.

Part: BLOWOUT PANEL — MISINSTALLED (AFT CARGO BAY) · airframe 56,475 hrs · 15,789 cycles

FOUND BLOWOUT PANEL INSTALLED IMPROPERLY AND WITHOUT CAP STRIPS. INSTALLED BLOWOUT PANEL AND CAP STRIPS PER AMM.

Part: SPEAKER — INOPERATIVE (COCKPIT) · airframe 56,380 hrs · 15,761 cycles

CAPTS O2 MASK MIC INOPERATIVE WHEN TRANSMITTING CANNOT BE HEARD OVER CAPTAIN`S SIDE SPEAKER. REPLACED CAPT'S SPEAKER AND CAPT'S HAND MIC DUE TO STICKY PTT SWITCH AND SPEAKER LOADING SYSTEM DOWN.

Part: PUMP — FAULTY (RT FUEL BOOS) · airframe 56,374 hrs · 15,758 cycles

RIGHT FORWARD FUEL BOOST PUMP LIGHT ILLUMINATED WITH ASSOCIATED EICAS MESSAGE. CIRCUIT BREAKER TRIPPED. CIRCUIT BREAKER RESETS OK WITH CONNECT OR REMOVED FROM RIGHT FORWARD BOOST PUMP. REPLACED RT FWD FUEL BOOST PUMP PER AMM. CIRCUIT BREAKERS REMAINS SET AND PUMP OPS NORMAL.

Part: CONTROL PANEL — MALFUNCTIONED (AUDIO) · airframe 55,998 hrs · 15,656 cycles

1ST OBSERVER S O2 MASK MICROPHONE INOPERATIVE. SWAPPED CAPTAIN`S AND 1ST OBSV AUDIO SELECT PANEL, O2 MASK MICROPHONE OPS NORMAL. REPLACED 1ST OBSV AUDIO SELECT PANEL, O2 MASK MICROPHONE SYS NORMAL.

Part: SMOKE GOGGLES — CRACKED (COCKPIT) · airframe 55,702 hrs · 15,569 cycles

FLIGHT DECK OBSERVERS SMOKE GOGGLES IS CRACKED.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 55,483 hrs · 15,505 cycles

APPROXIMATELY 1 INCH BY 1 INCH PUNCTURE AT STA 1350 BETWEEN STR 20 AND 21 FROM CONTACT WITH LIFT. SHOULD ALSO READ LEFT SIDE OF ACFT. STOP DRILLED CRACKS PER SRM. OK FOR NON REVENUE FLT TO REPAIR STATION WITH MAX CABIN DIFFERENTIAL PRESSURE LIMITED TO 6.0 PSIG. SHOULD READ, SRM 53-00 -01 PAGE 102 ALLOWABLE DAMAGE 2. ACCOMPLISHED STRINGER 22L REPAIR PER B757-200 SRM. ACCOMPLISHED SKIN REPAIR PER B757-200 SRM. PERFORMED RII INSP OF SKIN AND STRINGER REPAIR REF SRM 53-00-01, FIG 201 AND SRM 53-00-0 3, FIG 201. SEE MX WORKSHEET SHEET 1-3 FOR PARTIAL WORK ACCOMPLISHED.

Part: DOOR — DAMAGED (LAVATORY) · airframe 55,488 hrs · 15,506 cycles

LAVATORY OCCUPIED LIGHT INOPERATIVE. LIGHT DID NOT ILLUMINATE BECAUSE OF DOOR MALFUNCTION. CORRECTED DOOR PROBLEM, OCCUPIED LIGHT CHECKED GOOD.

Part: GENERATOR — FAULTY · airframe 55,268 hrs · 15,448 cycles

HMG FAILED TEST. STARTS TO SPIN THEN STOPS. DOES NOT REACH OPERATING SPEED. REF DF330 REMOVED 3EA HYD LINES TO HMG MOTOR TO FACILITATE HMG MOTOR REMOVAL. REINSTALLED AND SEC'S 3 EACH HYDRAULIC LINES.

Part: MODULE — INOPERATIVE (CABIN) · airframe 55,266 hrs · 15,447 cycles

EEL EXIT LIGHT JUST FWD OF DOOR 2R AND 2L INOP. RPL INVERTER MODULE M1094 9. REF WDM 33-51-21.

Part: COVER — MISSING (CABIN) · airframe 55,266 hrs · 15,447 cycles

DOORWAY AT DOOR 2L JUST FWD OF DOORS' LWR FWD CORNER VENT IS MISSING. REPLACED 1R DOOR MISSING AIR VENT COVER.

Part: DUCT — CRACKED (NR 1 ENGINE) · airframe 54,813 hrs · 15,323 cycles

NR 1 ENG ANTI-ICE DUCT CRACKED AT FLANGE WHERE ANTI-ICE DUCT IS CONNECTED TO NOSE COWL.

Part: CIRCUIT CARD — FAULTY (E&E BAY) · airframe 54,745 hrs · 15,303 cycles

LANDING GEAR LEVER WOULD NOT MOVE TO UP POSITION IN FLIGHT WAS FREE TO MOVE UP POSITION WHEN LOCK OVRD WAS PUSHED. REPLACED PSEU CIRCUIT CARD A6 PER MM. ACP'D TEST OF PSEU TASK. TEST OKAY. ACP'D OPERATION TEST WITH LANDING GEAR SWING, TESTED OKAY.

Part: CONTACT — DIRTY (CARGO BAY) · airframe 54,667 hrs · 15,284 cycles

AFT CARGO SQUIB BULB OUT. CLEANED CONTACT IN LAMP ASSY AFT CARGO SQUIB TEST GOOD.

Part: CONNECTOR — LOOSE (STAB TRIM) · airframe 54,614 hrs · 15,271 cycles

ALTN STAB TRIM CB B19 POPS WHEN ELEC PEDESTAL TRIM SWITCHES ARE MOVED. FOUND STCM CONN D01847 LOOSE BY 1 TURN. REMOVED & INSPECTED LOCK MECH. CLEANED & SECURED. CHECKED ALL REMAINING CONNECTORS OKAY. OPERATED ALT SYS MANY TIMES OK.

Part: CAP — MISSING (R1 WINDOW) · airframe 54,526 hrs · 15,245 cycles

WINDOW R1 LOWER RT CORNER WINDOW HT WIRE CAP MISSING. INSTALLED CAP.

Part: LANYARD — OUT OF POSITION (L4 DOOR) · airframe 54,444 hrs · 15,225 cycles

L4 DOOR WILL NOT ARM. MOVED LANYARD OUT OF WAY OF DOOR. DOOR ARMS NORMALLY.

Part: UNKNOWN — NOISY (COCKPIT) · airframe 53,964 hrs · 15,084 cycles

VERY HIGH COCKPIT NOISE LEVELS FROM PACK-RECIRC FAN. ACP'D CHECK OF RECIC FANS AND FILTERS. FANS AND FILTERS ARE CLEAN. ACP'D FLIGHT DECK GROUND NOISE LEVEL CHECK. FLIGHT DECK NOISE WAS BELOW LIMITS OF 70.5 DB.

Part: BULB — MISSING (COCKPIT) · airframe 53,948 hrs · 15,081 cycles

MISSING TWO 1864 BULBS FROM SPARE BULB KIT. NO TIME. REPLACED BULBS.

Part: D-RING — MISSING (SLIDE RAFT) · airframe 53,884 hrs · 15,061 cycles

THE 'D' RING AT STRAP MISSING FROM DOOR 1L SLIDE RAFT. REPLACED MISSING STRAP, CHECKS OKAY.

Part: CONTROL UNIT — FAULTY (GALLEY) · airframe 53,859 hrs · 15,054 cycles

NO POWER AFT GALLEY. FOUND CB S3 ON P11 PNL G4 B GALLEY PWR TRIPPED, NO RESET. REPLACED M227 L AFT GALLEY PWR ELCU MM. OPS CHECK OK. NEW ELCU BORROWED FROM AMERICAN AIRLINES P/N 3B39-1-C, SN 077C-6539. SHIPPING CONTAINER IN FWD PIT ON S/N SHOULD READ 078C-6887.

Part: NUT — LOOSE (COCKPIT) · airframe 53,856 hrs · 15,053 cycles

CAPT'S SLIDING WINDOW IS BINDING AT AFT LOWER LATCH CAM, PRYING AT WINDOW INBOARD AT THIS LOCATION FREES UP WINDOW LATCH, REQUIRES RE-RIG TO BRING AFT LATCH CAM INBOARD. ATTEMPTED TO RIG WINDOW PER ADJUSTMENT MM AND COULD NOT ADJUST. FRAME LOWER AFT CORNER MOVES OTBD TOO FAR AT PRESSURE AND IS NOT CENTERED ON LATCH CAM. REPLACED LINK ARM, NO HELP. SUSPECT WINDOW SEAL. CAPTAINS WINDOW STUCK AFTER FLIGHT. FOUND LOWER LINK ARM SPRING CYLINDER RETAINER NUT LOOSE. SECURED RETAINER NUT. VERIFIED WINDOW OPERATES NORMALLY.

Part: UNKNOWN — ODOR (CABIN) · airframe 53,648 hrs · 14,985 cycles

STRONG ELECTRICAL SMELL AROUND ROW 12 ON APPROACH. ACP'D OPENED UP CEILING PANELS, PCU PANELS, FROM ROWS 10 THRU 20. NO EVIDENCE OF ANYTHING RAN BOTH ENGS, CYCLED PACKS AND RECIRC FANS. NO EVIDENCE OF ELECTRICAL ODOR. ACFT POWERED UP FOR SEVERAL HOURS, NO ODOR. CONFERRED WITH SAMC.

Part: RADIO ALTIMETER — MALFUNCTIONED (COCKPIT) · airframe 53,638 hrs · 14,983 cycles

CREW REPORT: CAPTS RADAR ALTIMETER CONSTANTLY FLASHING ERRONEOUS VALUES. SAMC TEXT: FLT CREW REPORTED 'GEAR NOT DOWN' WARNING ON THROTTLE RETARDING. ALTIMETER ERRONEOUS CONSTANT THROUGHOUT FLIGHT. REPEAT WRITE-UP. COMPLIED WITH MEL 3433E. -INF- :CB F5, LEFT RADIO ALT PULLED AND COLLARED.

Part: IGNITER — FAULTY (APU) · airframe 53,620 hrs · 14,974 cycles

APU FAULT LIGHT STAYS ON WHEN ATTEMPTING START. NO TIME TO WORK. -INF- :RESET FAULTS ON ECB. RESTART ATTEMPT FAILED. ECU FAULTS "NO FLAME". PARTS: 265-0040 305766-1 (IGNITER). 671-0049 53109-3 (LEAD). 671-0050 MR49410 (EXCITER).

Part: ROLLER — OUT OF RIG (L1 DOOR) · airframe 53,333 hrs · 14,872 cycles

PASSENGER ENTRY-SERVICE DOORS-L FWD NOISE FROM AIR LEAK. MAINT TEXT: DOOR CLOSURE DIFFICULT, APPEARS TO TRANSITION TO FAR FWD WHEN CLOSING. FOUND DOOR 1L OUT OF RIG ALL FOUR CAM ROLLERS HITTING ON THE FOLLOWERS. NEED NEW ROLLERS AND FOLLOWERS AOG'S (E4430, E5179, B5180, G2090&F3763), THEN RIG THE DOOR. RMV'D CENTER & FWD SCUFF PLATE DOOR 1L. REINSTALLED CENTER AND FWD SCUFF PLATES PER MM. WILL NEED TO LET BMS 5-95 DRY. SCUFF PLATE INSTALLED AT 0930 AM ON 9-13 AND DRIED. NEED TO REPRESSURIZE AND CHECK FOR LEAKS. PRESSURIZED AIRCRAFT AFTER SEALANT DRIED. NO LEAKS OR INTERIOR NOISE.

Part: CONTROL PANEL — FAULTY (VHF COMM) · airframe 53,325 hrs · 14,870 cycles

VHF-L ON CAPTS SIDE BOTH LIGHT BULBS BURNED OUT. REPLACED VHF L CHANNEL SELECT FREQ PANEL.

Part: TRANSCEIVER — FAULTY (RADIO ALTIMETER) · airframe 53,233 hrs · 14,840 cycles

F/O RAD ALT STILL INOP AFTER CB RESETS PREFLIGHT. NO TIME TO T-S. ACFT REMOVED FROM CATIII PER MEL 3433J. PLACARDS INSTALLED NEXT TO ASA'S. REPLACED F/O'S RADIO ALTIMETER RECEIVER AND CHECKED OKAY.

Part: PANEL — FAULTY (ATC) · airframe 53,228 hrs · 14,839 cycles

ATC XMISSION FROM NR 2 XPNDR IS WEAK, INTERMIT, ETC.(1=L XPNDR, 2=R XPNDR, 3=BOTH XPNDR). CREW COMMENTS: ATC FAIL LIGHT ON INTERMITTENTLY. ATC REPORTS SQUAWK SHOWS 0000 WITH 7226 SELECTED. REPLACED DUAL ATC PANEL PER AMM.

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 53,221 hrs · 14,837 cycles

LEFT ENGINE START. LT SPAR LIGHT ON PED AND LT ENGINE VALVE LIGHT ON EICAS. P6 PANEL F1 CIRCUIT BREAKER POPPED. REPLACED THE SPAR VALVE ACTUATOR AND ELECTRICAL CONNECTOR DUE TO THE BACK SHELL BEING LOOSE. OPS CHECKED NORMAL. ALSO ACCOMPLISHED ELECTRICAL CONNECTOR REPLACEMENT.

Part: ACCESSORY UNIT — FAULTY (PA SYSTEM) · airframe 53,197 hrs · 14,832 cycles

F/O CANNOT MAKE ANY PA ANNOUNCEMENT FROM ANY MIC SWITCH (BOOM, YOKE, HAND OR CONSOLE PTT). GROUND CHECK OK. BUT COULD BE INTERMITTENT. REPLACED AUDIO ACCESSORY UNIT, OP TEST OKAY.

Part: SELECTOR PANEL — FAULTY (COCKPIT) · airframe 53,175 hrs · 14,827 cycles

FIRST OBSERVERS AUDIO SELECT PANEL INOP. AUDIO SELECT PANEL INOP. REPLACED AUDIO SELECT PANEL PER MM. OP CHECKS GOOD.

Part: AUDIO PANEL — FAULTY (HF COMM) · airframe 53,170 hrs · 14,826 cycles

FIRST OFFICER SIDE TONE INOP ON NR 1 HF RADIO ONLY. *SUPPLEMENTAL DATA UPDATE* REPLACED AUDIO SELECT PANEL PER AMM.

Part: SELECTOR PANEL — FAULTY (CABIN) · airframe 53,165 hrs · 14,825 cycles

WHEN F/O'S PA IS USED, ALL RECEPTION ON VHF IS BLOCKED ON HEADSETS & SPEAKERS. COULD NOT DUPLICATE THE PROBLEM. REPLACED F/O'S AUDIO SELECT PANEL PER MM, PRECAUTIONARY OP CHECK GOOD.

Part: OIL SYSTEM — LOW PRESSURE (NR 2 ENGINE) · airframe 52,995 hrs · 14,782 cycles

NR 2 ENG ALL OIL PRESSURE INDICATION LOST. AFTER 'A' CHECK ENG RUN SHUT DOWN NR 1 ENG LOST NR 2 OIL PRESSURE, SCAVENGE AND DIFFERENTIAL PRESSURE INDICATIONS. RAN BOTH ENGINES NR 2 ENG INDICATIONS NEVER RETURNED. FOUND CB C878 TRIPPED, RESET OPS NORMAL.

Part: GIRT BAR — DIRTY (L4 DOOR) · airframe 52,982 hrs · 14,776 cycles

DOOR 4L SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED DEBRIS FROM GIRT BAR AREA, GRD CHECKED GOOD.

Part: IDG — FAILED (LEFT) · airframe 52,558 hrs · 14,659 cycles

LEFT GEN DRIVE OFF WITH ENG SHUT DOWN. REPLACED LEFT GCU, NO HELP. REPLACED LT IDG. LT GEN DRIVE "DRIVE" LIGHT INOPERATIVE. REPLACED LT IDG. FOR TROUBLESHOOTING, SWAPPED LEFT AND RIGHT ENG GCU'S.

Part: VALVE — FAULTY (CABIN HEAT) · airframe 52,481 hrs · 14,636 cycles

COCKPIT TEMP UNCONTROLLABLE & UNACCEPTABLE ON CLIMB & DESCENT WITH TRIM AIR ON OR OFF. FLT DECK TEMP STILL ERRATIC, W-TEMP CTL OFF TEMP STILL WANDERS IN STBY STEADY BUT CONT. FOUND LT PACK TEMP CONTROL VALVE SEIZED. REPLACED IAW AMM.

Part: SCREEN — CLOGGED (TEMP SENSOR) · airframe 52,284 hrs · 14,583 cycles

COCKPIT AIR COND DUCT TEMP EXCEEDED 100 DEGREES SEVERAL TIMES DURING THE FLIGHT. FOUND FLIGHT DECK TEMP SENSOR SCREEN CLOGGED, CLEANED SCREEN. PERFORMED BITE TEST, NO FAULTS NOTED ON TEMP CONTROLLER.

Part: CHECK VALVE — FAULTY (BRAKE SYSTEM) · airframe 52,284 hrs · 14,583 cycles

BRAKE PRESSURE DECAY. CONDUCTED PARKING BRAKE SYS ADJUSTMENT TEST. ACCUMULATOR BRAKE PRESSURE AFTER 10 MIN DOWN 900 LBS. CHECKED ACCUMULATOR PRESSURE NORMAL. BRAKE PRESSURE DECAY EXCESSIVE. REPLACED ACCUMULATOR AND PARK BRAKE VALVE, NO HELP. REPLACED ACCUMULATOR ISOLATION VALVE PCN 641-1159, NO HELP. REPLACED BRAKE SYS ACCUMULATOR CHECK VALVE. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,037 hrs · 14,498 cycles

FLOOR EEL LIGHT INOP ROW 2 AFT LT SIDE ONLY. REPLACED BATTERY PACK M732 AND FOUND GROUND STUD LOOSE (GD3288-DC). SECURED AND OPS TEST OKAY.

Part: BLEED VALVE — FAULTY (NR 2 ENGINE) · airframe 51,913 hrs · 14,461 cycles

NR 2 ENG PWR FLUX. REPLACED HIGH STAGE PILOT AND HIGH PRESSURE SHUTOFF VALVE.

Part: SLIDING WINDOW — SCRATCHED (COCKPIT) · airframe 51,863 hrs · 14,442 cycles

F/O SLIDING WINDOW IS HEAVILY SCRATCHED IMPAIRING VISION. REPLACED F/O OPENABLE WINDOW PER MM.

Part: GUIDE ARM — LOOSE (PAX DOOR) · airframe 51,656 hrs · 14,380 cycles

DOOR 3L VERY DIFFICULT TO OPEN AND CLOSE. FOUND GUIDE ARM ATTACH BOLTS TO DOOR LOOSE AND GUIDE ARM ROD ARM BEARING WORN AND SERPENTINE GUIDE PIN WORN. REPLACED GUIDE ARM AND RIGGED. DOOR STILL VERY HARD TO OPERATE. FOUND HANDLE MECHANISM VERY STIFF. WILL REQUIRE FURTHER TROUBLESHOOTING. GUIDE ARM REPLACED PER AMM. NEED TO CONFIRM DOOR 3L CLOSED PROPERLY AND FLUSH WITH FUSELAGE SKIN WITH NO GAPS AND ALL OPEN RII ITEMS RELATED TO THE DOOR HAVE BEEN CLOSED. CONFIRMED DOOR 3L CLOSED PROPERLY

Part: GUIDE ARM — DEFECTIVE (L3 DOOR) · airframe 51,656 hrs · 14,380 cycles

DOOR 3R (AFT PAX DOOR) VERY DIFFICULT TO OPEN AND CLOSED. FOUND GUIDE ARM ATTACH BOLTS TO DOOR LOOSE AND GUIDE ARM ROD ARM BEARING WORN AND SERPENTINE GUIDE PIN WORN. REPLACED GUIDE ARM AND RIGGED. DOOR STILL VERY HARD TO OPERATE. FOUND HANDLE MECHANISM VERY STIFF. WILL REQUIRE FURTHER TROUBLESHOOTING. REPLACED GUIDE ARM.

Part: SKIN — DAMAGED (TE FLAP) · airframe 51,606 hrs · 14,363 cycles

LT INBOARD AFT FLAP INBOARD END POTTING SPLIT OPEN BOTH UPPER AND LOWER SKIN. MAJOR REPAIR ACCOMPLISHED: AREA FROM FWD SPAR T/E AFT 13 INCH ON UPPER SKIN AND 12 INCH ON LOWER SKIN AND OUTBOARD FROM INBD END OTBD 8 INCHES BOTH SIDES HAS DELAMINATION & FROZEN WATER IN CORE. DELAM IS CONSIDERED A HOLE. MAX LIMIT ON REPAIRS IS 1 INCH PER NOTE. REPLACED LT TRAILING EDGE FLAP.

Part: LIGHT — UNSECURE (CABIN) · airframe 51,451 hrs · 14,321 cycles

EMERGENCY EXIT FLOOR PATH LIGHT STRIP NEEDS TO BE SECURED TO THE FLOOR AT ROW 12. RE-SECURED LIGHT STRIP.

Part: VALVE — LEAKING (ENGINE OIL) · airframe 51,417 hrs · 14,314 cycles

RT ENG DRIPPING OIL EVERY 2 SECONDS. NR 3 DRAIN LEAKING FUEL. NR 3 DRAIN DRIPPING 14 DROPS PER MINUTE. REPLACED HEAT EXCHANGER VALVE PER MM.

Part: OIL SYSTEM — LEAKING (NR 2 ENGINE) · airframe 51,316 hrs · 14,286 cycles

NR 2 OIL QTY LOSS, RTFL UPON ARRIVAL DRAINED MAIN GEAR BOX, APPROX 1 QT. CLEANED ENGINE AS BEST AS POSSIBLE WITH AVAILABLE RESOURCES. UNABLE TO DETERMINE REASON FOR HIGH OIL CONSUMPTION. ENGINE TO BE REPLACED PER LM CALLOUT 7847.

Part: MANIFOLD — LEAKING (BREATHER) · airframe 51,314 hrs · 14,285 cycles

RT ENG OIL PRESS EICAS. NR 2 ENG ESN 726613, DUE TO LOSS OF OIL QTY AND DECREASING OIL PRESSURE THAT RESULTED IN A IN-FLT SHUTDOWN. NO OIL FOUND IN TAILCONE AREA. FOUND BREATHER MANIFOLD CRACKED. REPLACED FRACTURED OIL BREATHER MANIFOLD LINE. IDLE RUN LEAK CHECK. RAN ENG PER REQUEST. ALL INDICATIONS NORMAL. ACCOMPLISHED WINDMILLING INSPECTION PER MM. NO CHIPS FOUND ON CHIP DETECTORS OR IN MAIN OIL FILTER. NO LEAKS NOTED. CORRECTIVE ACTION HAS BEEN ACCOMPLISHED, FIX WAS CONFIRMED BY ENGINE RUN ON THE GROUND (80 PERCENT PWR FOR 10 MIN NO LEAK.)

Part: GCU — INOPERATIVE (NR 1 GENERATOR) · airframe 51,189 hrs · 14,242 cycles

HYDRAULIC MOTOR GEN DOES NOT TEST. VALVE OPENS, GEN DOES NOT OPERATE. POS CONTROL UNIT OR GEN. COMPLIED WITH MEL. REPLACED HYD MOTOR GENERATOR CONTROL UNIT. OPS NORMAL.

Part: LIGHT — UNSECURE (ROW 12C) · airframe 51,198 hrs · 14,245 cycles

EMERGENCY EXIT PATH LIGHT STRIP IS RAISED AT 12C. RESECURED EMERGENCY LIGHT TRACK, CARPET AND TRACK COVER. OPS CHECK OF LIGHT OK.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,182 hrs · 14,240 cycles

FLOOR EMERGENCY LIGHTING INOP ROW 1-6. REPLACED M732 CHARGER, OPS CHECK OF EMERGENLCY LIGHTING WORKS GOOD.

Part: LIGHT — FAULTY (SELECTOR PANEL) · airframe 51,178 hrs · 14,239 cycles

RADIO HEAD NR 1 BACKLIGHT INOPERATIVE. REPLACED FREQUENCY SELECTOR PANEL IAW MM, OPS NORMAL.

Part: SELECTOR SWITCH — BROKEN (VHF) · airframe 51,160 hrs · 14,234 cycles

1 VHF COMM CONTROL PANEL HAS MECHANICAL DEFECT. BROKEN, MISSING OR LOOSE PARTS. (01=L VHF, 02=R VHF) COPILOTS L-VHF SELECTOR SWITCH BROKEN. WILL NOT STAY IN WHEN PUSHED. WON'T DESELECT OTHER SWITCHES. SWAPPED WITH F/O WITH 1ST OBSERVER. NEED TO REPLACE 1ST OBSERVER'S AUDIO SELECT PANEL MR23524. REPLACED NR3 AUDIO CONTROL PANEL IAW MM, TEST OK.

Part: WIRE — BROKEN (APU FUEL ACT) · airframe 51,150 hrs · 14,232 cycles

APU FUEL SHUTOFF VALVE IS INOPERATIVE AND THE APU IS CONSIDERED INOPERATIVE. APU IS INOP ON ACCOUNT OF FUEL SPAR VALVE IS INOP. REPLACED APU FUEL SHUTOFF ACTUATOR, NO HELP. APU STARTS OK, HOWEVER AT SHUTDOWN RECEIVED APU FUEL VALVE MSG UPPER SCREEN ALONG WITH APU FAULT LIGHT ON P11 PANEL. MR28227-52 ON AND MR28227-67156413 SN OFF. RDF-T : REF WD 28-25-21 PG1, FOUND WIRE W2658-003-18 RINGS OPEN FROM D2382 PIN-5 TO D41770 PIN-3. POWER OK (28V) UP TO D41770J PIN-3. REPAIRED BROKEN WIRE. CHECKED OK.

Part: GENERATOR — FAULTY (APU) · airframe 51,150 hrs · 14,232 cycles

APU GENERATOR WILL NOT COME ON LINE. REPLACED APU GENERATOR, OPS CHECKED GOOD.

Part: O-RING — LEAKING (ENGINE OIL SYS) · airframe 51,042 hrs · 14,195 cycles

FOUND EXCESSIVE OIL BAKED ON TO EXHAUST NOZZLE OF NR 2 ENGINE DURING ETOPS INSP. FURTHER INSPECTION REVEALED OIL MAYBE COMING FROM NR 5 BEARING SCAVENGE LINE. REPLACED O-RING AT NR 5 BEARING SCAVENGE LINE COUPLING TO NR 5 BEARING COMPARTMENT. RAN ENGINE FOR LEAK CHECK.

Part: IDG — FAULTY (LEFT) · airframe 51,038 hrs · 14,193 cycles

LT GEN DRIVE LIGHT NOT ON WITH ENG SHUTDOWN. SERVICED APU TO FULL IAW MEL, HMG OPS NORMAL IAW MEL. TAPED OVER LIGHTS REF MEL. DISCONNECTED IDG. DL8173 CREATED TO MONITOR. REPLACED NR 1 ENGINE IDG IAW MM AND DRIVE SEALS IAW MM. OPS AND LEAK CHECKED GOOD. DRIVE LIGHT ON AFTER SHUTDOWN.

Part: LEVER — FAULTY (R4 GIRT BAR) · airframe 51,019 hrs · 14,187 cycles

4R DOOR SLIDE GIRT BAR ENGAGEMENT LIGHT, ALWAYS ON. QUICK TURN, REPORTED BY INBD CREW. CYCLED ARMING LEVER AND SLIDE LIGHT WORKS NORMAL.

Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 51,019 hrs · 14,187 cycles

EMERGENCY FLOOR LIGHT COVER COMING OFF AT 12C. SECURED LIGHT COVER.

Part: LIGHT — UNSECURE (CABIN) · airframe 50,979 hrs · 14,178 cycles

EMERGENCY EXIT LIGHT PANEL STICKING UP ROWS 12 AND 13. SECURED EMERGENCY LIGHT TRACK TO FLOOR CHECKS OK.

Part: CAP — MISSING (CABIN) · airframe 50,857 hrs · 14,147 cycles

AT 34C EMERGENCY EXIT LIGHT STRIP MISSING END CAP. END CAP REPLACED. OPS NORMAL.

Part: LIFE VEST — MISSING (SEAT 18D) · airframe 50,809 hrs · 14,131 cycles

SEAT 18D AND 19A MISSING LIFE VEST UNDER SEATS. REPLACED MISSING LIFE VESTS.

Part: LIGHT — UNSECURE (ROWS 12-13) · airframe 50,747 hrs · 14,108 cycles

EMERGENCY ESCAPE PATH LIGHTING NOT SECURE BETWEEN ROWS 12 AND 13. SECURED EMERGENCY LIGHT. OPS CHECKED NORMAL.

Part: SHUTOFF VALVE — FAULTY (LT ENGINE) · airframe 50,747 hrs · 14,108 cycles

LEFT ENG PRSOV IS FAULTY. CHECKED PRSOV WITH HEALTH CHECK KIT, AND VERIFIED VALVE POSITION SWITCH WAS DEFECTIVE. REPLACED NR 1 ENG PRSOV PER MM. VERIFIED NEW VALVE WAS GOOD FROM STOCK WITH HEALTH CHECK. LEAK CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,747 hrs · 14,108 cycles

DURING OPS CHECK OF EMERGENCY LIGHTS, FOUND CENTER SECTION INOP. REPLACED EMERGENCY LIGHT BATTERY OUTBOARD OF SEAT 17 A, B, C. OPS CHECKED NORMAL.

Part: CONTROL SYSTEM — FAILED (CABIN TEMP) · airframe 50,631 hrs · 14,073 cycles

COCKPIT TEMP FAULT, FLIGHT DIVERTED. REPLACED THE LT PACK TEMP SENSOR AND LT PACK TEMP CONTROLLER VALVE. LT AIR CONDITIONER CHECKED GOOD.

Part: SERVO — FAULTY (LEFT) · airframe 50,355 hrs · 14,001 cycles

NO LAND 3 MESSAGE DISPLAYED INFLT. EFI NO LUCK. CAPT INST SOURCE SEL C CLEARED MESSAGE. LAST FLT FAULT RUDDER SERVO FCC L CODE 111481. REPLACED LT AUTOPILOT ROLLOUT GUIDANCE SERVO ACTUATOR. OP CHECKED GOOD. LEAK CHECKED GOOD.

Part: STRUCTURE — CORRODED (R4 DOOR) · airframe 50,223 hrs · 13,958 cycles

R4 DOOR HANDLE BOX CORRODED. REPLACED THE 4R DOOR HANDLE BOX ASSEMBLY.

Part: LINK — WORN (L1 DOOR) · airframe 50,223 hrs · 13,958 cycles

NR 1 LEFT PASSENGER DOOR UPPER DOOR HINGE LINK ASSY WORN. REPLACED THE UPPER DOOR HINGE ASSEMBLY. ACCOMPLISHED ON TASK CARD 5R52I1810.

Part: GUIDE — BENT (R4 DOOR) · airframe 50,223 hrs · 13,958 cycles

R4 DOOR TRIGGER ASSY., GUIDE STOP BENT. REPLACED THE R4 DOOR TRIGGER ASSEMBLY AND GUIDE STOP PER CMM.

Part: LIFTER — WORN (L4 GIRT BAR) · airframe 50,223 hrs · 13,958 cycles

DOOR 4L GIRT BAR LIFTER WORN FWD AND AFT. REPLACED 2 EACH LIFTER ASSEMBLIES FWD AND AFT AT DOOR 4L PER MM.

Part: STRUCTURE — CRACKED (L1 DOOR) · airframe 50,223 hrs · 13,958 cycles

NR 1 LT DOOR HANDLE BOX FOUND CRACKED BY NDT INSPECTION. REPLACED THE 1L DOOR HANDLE BOX.

Part: LIFTER — WORN (R4 GIRT BAR) · airframe 50,223 hrs · 13,958 cycles

R4 DOOR GIRT BAR MECHANISM LIFTERS ARE WORN, FWD AND AFT. REMOVED AND REPLACED BOTH FWD AND AFT LIFTER ASSYS.

Part: LINK — WORN (L2 DOOR) · airframe 50,223 hrs · 13,958 cycles

#2 LEFT PASSENGER DOOR UPPER DOOR HINGE LINK ASSY WORN. REPLACED L-2 DOOR UPPER HINGE LINK ASSY.

Part: GATE — CORRODED (R2 DOOR) · airframe 50,223 hrs · 13,958 cycles

NR 2 RT DOOR LOWER GATE HAS CORROSION. REPAIRED R2 DOOR LOWER GATE.

Part: GATE — CORRODED (R4 DOOR) · airframe 50,223 hrs · 13,958 cycles

NR 4 RT DOOR LOWER GATE CORRODED. REMOVED CORROSION AND ACCOMPLISHED REPAIR.

Part: PRESSURE PANEL — CORRODED (BS 1680) · airframe 50,223 hrs · 13,958 cycles

CORROSION ALONG TOP OF AFT PRESSURE DECK PLATE AT STA 1 680, RIGHT SIDE AT FUSELAGE AND INBD OF WATER TANK-FLOOR PANEL TO FLOORBEAM. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA AND FABRICATED AND INSTALLED A REPAIR DOUBLER AND FILLER.

Part: FLOORBEAM — CORRODED (BS 324) · airframe 50,223 hrs · 13,958 cycles

BS 324 FLOORBEAM HAS CORROSION ON TEE AT RBL 58. MATERIAL REMAINING AFTER BLENDOUT EXCEEDS LIMITS OF SRM. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED TEE AND FABRICATED A REPLACEMENT T-CHORD AND INSTALLED PER PEMCO EA PD 57-53-052 AND UAL EVA 80278 ON NON ROUTINE 2297N00243. PER UAL EVA 80278.

Part: FLOORBEAM — CORRODED (BS 1660) · airframe 50,223 hrs · 13,958 cycles

CORROSION ON FLOORBEAM AT STA 1660, RBL 0 -15, AND MATERIAL REMAINING AFTER CORROSION BLEND OUT EXCEEDS LIMITS OF SRM. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA AT UPPER FLANGE AND FABRICATED AND INSTALLED ANGLE DOUBLERS AND STRAPS.

Part: SKIN — GOUGED (R2 DOOR) · airframe 50,223 hrs · 13,958 cycles

R2 DOOR EXTERIOR SKIN GOUGED BELOW EXTERNAL HANDLE. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM, REPAIR 7 ON NON ROUTINE 2297N00591.

Part: LINK — WORN (L4 DOOR) · airframe 50,223 hrs · 13,958 cycles

NR 4 LT PASSENGER DOOR UPPER DOOR HINGE LINK ASSY WORN. REPLACED NR 4 UPPER LT DOOR HINGE LINK ON ROUTINE TASK CARD.

Part: LINK — WORN (R4 DOOR) · airframe 50,223 hrs · 13,958 cycles

NR 4 RT PASSENGER DOOR UPPER DOOR HINGE LINK ASSY WORN. REPLACED DOOR 4 RT UPPER LINK ASSY.

Part: MOUNT — CORRODED (FWD GALLEY) · airframe 50,223 hrs · 13,958 cycles

CORROSION IN FWD GALLEY FLOOR AREA IN GALLEY MOUNT AT STA 366, REMOVED CORROSION AND FOUND THAT BLENDED ARE WAS BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED: R & R FLOOR SUPPORT MOUNT IAW SRM AND FABRICATED NEW SUPPORT CHANNEL IAW SRM.

Part: FLOORBEAM — CORRODED (STA 330) · airframe 50,223 hrs · 13,958 cycles

CORROSION IN FLOOR CHANNEL IN FWD GALLEY AREA AT STATION 330 FROM RBL 0 TO 40. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION FROM AREA AND FOUND TO BE BEYOND LIMITS IAW THE SRM AFTER BLENDING. REMOVED FLOOR CHANNEL AND INTERCOSTALS AND FABRICATED & INSTALLED REPLACEMENTS IAW SRM.

Part: FLOORBEAM — DAMAGED (BS 366.25) · airframe 50,223 hrs · 13,958 cycles

FWD GALLEY FLOOR AREA, FLOORBEAM STRUCTURE AT STA 366.25 RBL 0 TO 65 HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED: MATERIAL REMAINING AFTER BLENDOUT EXCEEDS LIMITS OF SRM. REMOVED 34" DAMAGED AREA AND REPLACED WITH FABRICATED NEW FLOORBEAM IAW SRMS.

Part: FLOORBEAM — CORRODED (BS 1681) · airframe 50,223 hrs · 13,958 cycles

FLOORBEAM CORRODED ON UNDERSIDE, APPROX STA 1681, RBL 32. MAJOR REPAIR ACCOMPLISHED: MATERIAL REMAINING AFTER BLENDOUT EXCEEDS LIMITS OF SRM. TRIMMED OUT DAMAGED SECTION OF T-CAP AT BS 1681 FLOORBEAM FROM RBL 32 TO CUSP, FABRICATED 2 REPLACEMENT STRAPS AND ONE CLIP AND INSTALLED IAW SRM.

Part: SHEAR TIE — GOUGED (BS 440 S17L) · airframe 50,223 hrs · 13,958 cycles

FWD CABIN LT SIDE & FWD OF STA 440, JUST BELOW S-17L, SHEAR TIE GOUGED. MAJOR REPAIR ACCOMPLISHED: BLENDED GOUGE, AND MATERIAL REMAINING EXCEEDS LIMITS OF SRM. R & R SECTION OF FLOOR SUPPORT SPLICE WITH NEWLY MFG SUPPORT ANGLE AND SPLICE.

Part: FLOORBEAM — CORRODED (STA 1640, RBL 64) · airframe 50,223 hrs · 13,958 cycles

MAIN CABIN, FLOORBEAM T-CAP HAS CORROSION ON TOP AND BOTTOM SIDES AT STA 1640, RBL 64 TO LBL 64. MAJOR REPAIR ACCOMPLISHED: MATERIAL REMAINING AFTER BLEND OUT EXCEEDS LIMITS OF SRM. TRIMMED OUT DAMAGED SECTION OF T-CAP AT BS 1641 FLOOR BEAM FROM LBL 8 TO RT CUSP, FABRICATED REPLACEMENT UPPER CHORD AND SPLICE ANGLES AND INSTALLED IAW SRM, REPAIR 3.

Part: SLIDE — FAULTY (OVERWING) · airframe 50,223 hrs · 13,958 cycles

LEFT OFFWING SLIDE, UNLACED, NEEDS TO BE REPLACED. R & R LT OFFWING SLIDE IAW MM.

Part: SKIN — DENTED (FUSELAGE) · airframe 50,078 hrs · 13,911 cycles

DENT IN FUSE 5, FRAMES FWD OF DOOR 2L, 2 STRINGERS BELOW SKIN LAP. DENT APPROX 8 IN LONG, 4 IN WIDE, 3-8 IN DEEP AND EXTENDS INTO EXISTING DOUBLER. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR DOUBLER, STRUCTURAL FILLER AND TRIPLER.

Part: GCU — FAULTY (NR 2) · airframe 49,570 hrs · 13,761 cycles

ON APPLICATION OF T/O POWER RT ENG TRIPPED OFF LINE WITH EICAS MSG. SAMC TEXT: CREW REPORTS THAT RT IDG FREQ FLUCTUATES BETWEEN 419 TO 420 HZ AND THEN GOES BLANK AT IDLE. REPLACED RT GEN CONTROL UNIT IAW MM. ALSO ADJ IDG FREQUENCY 5 TURNS CW EQUAL TO 15 HZ, OP UT NOW READS 398 HZ IAW MM. ALL OPS NORMAL.

Part: STOWAGE BOX — LEAKING (COCKPIT) · airframe 49,541 hrs · 13,753 cycles

THE O2 SYS NOT HOLDING PRESSURE. FOUND CAPTAINS O2 MASK STOWAGE BOX LEAKING AT B-NUT CONNECTION. REPLACED STOWAGE BOX PER MM. SERVICED O2 TO FULL.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 49,011 hrs · 13,609 cycles

CTR HYD SYS QUANTITY READS .57RF ON LANDING. FOUND PIN HOLE LEAK AT STAB HYD MOTOR RETURN LINE AT AFT COMPT. IN PROCESS OF REMOVING LINE TO MFG IAW SAMPLE. REMOVED LINE AND SHOP REPAIRED REF R & R TAG R42781, REINSTALLED LINE AND LEAK CHECKS GOOD.

Part: LIGHT — OBSTRUCTED (CABIN) · airframe 49,004 hrs · 13,607 cycles

MID LAV EMERGENCY LIGHT STRIP COVERED BY CARPET. TRIMMED CARPET TO EXPOSE EMERGENCY LIGHT, OPS CHECKED NORMAL.

Part: SWITCH — FAULTY (SQUIB TEST PANEL) · airframe 49,004 hrs · 13,607 cycles

SQUIB TEST PANEL TEST SWITCH 2 DIFFICULT TO OPERATE. R&R TEST PANEL. REMOVED AND REPLACED TEST PANEL. REPLACED NR 2 TEST SWITCH. TESTS OKAY.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,004 hrs · 13,607 cycles

1 RH MED EMER EXIT LIGHT SIGN, OVER DOOR IS INOP. REPLACED BATTERY CHARGER AND BATTERY FOR EMER. LIGHT ASSY, OPS CHECKED NORMAL.

Part: STOWAGE BOX — DEFECTIVE (O2 SYSTEM) · airframe 48,984 hrs · 13,600 cycles

CAPT O2 MASK STORAGE BOX TEST SW STIFF TO OPERATE. REPLACED OXYGEN STORAGE BOX. LEAK CHECKED FITTING. NO LEAKS NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,525 hrs · 13,480 cycles

DOOR 1R OUTSIDE EMERGENCY LIGHT INOPERATIVE. RELAMPED, CHECKS OK.

Part: B-NUT — LEAKING (HYD SYSTEM) · airframe 48,116 hrs · 13,365 cycles

FOUND HYD LEAK AT RT WING OTBD AILERON. SECURED LOOSE B-NUT AND NEXT TO ACTUATOR, OPS CHECK OK. NO LEAKS FOUND.

Part: WINGLET — UNKNOWN (WING) · airframe 48,070 hrs · 13,347 cycles

BLENDED WINGLET RETROFIT. ACP COA 506741 ON TASKCARD 5C0674248.

Part: LIGHT — DETERIORATED (CABIN) · airframe 48,070 hrs · 13,347 cycles

EXIT PATH LIGHTING SECTION DETERIORATED. ACP SMC003 ON TASK CARD NR 1 990N00309. OPS OKAY.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 48,070 hrs · 13,347 cycles

EMERGENCY LIGHT BATTERY PACK FOR R-1 DOOR IS DEAD. ACCOMPLISHED SMC004 ON NON ROUTINE TASK CARD 1990N00312.

Part: VALVE — LEAKING (FUEL SYSTEM) · airframe 47,293 hrs · 13,139 cycles

FUEL LEAK DOWN LEFT MLG DOOR. FOUND LT WING FUELING VALVE CONTROL LEAKING. REPLACED WITH A SERVICEABLE UNIT. LEAKED CHECKED OKAY. ALL WORK ACCOMPLISHED.

Part: DRAIN — FAULTY (IDG) · airframe 47,155 hrs · 13,097 cycles

NR 2 ENGINE IDG DRAIN BOSS IS STRIPPED OUT. REPLACED NR 2 ENGINE IDG DRAIN BOSS. LEAK CHECKED GOOD.

Part: PUMP — LEAKING (NR 2 ENGINE) · airframe 46,909 hrs · 13,034 cycles

NR 2 ENG FUEL LEAKING FROM FUEL PUMP PARTING SURFACE AT 20 DROPS PER MIN. REMOVED FUEL PUMP AND CONTROL TOGETHER AS A UNIT. INSTALLED SERVICEABLE FUEL PUMP AND RE-INSTALLED FUEL CONTROL.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 46,909 hrs · 13,034 cycles

NR 2 ENG DRIVEN HYD PUMP LEAKING 20 DPM AT A PUMP SEAM. REPLACED NR 2 ENG DRIVEN HYD PUMP. NO LEAKS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,751 hrs · 12,993 cycles

EMERGENCY LIGHT AT STOW BIN 25B INOPERATIVE. REPLACED LAMP. OPS CHECKED OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,751 hrs · 12,993 cycles

EEL LIGHT STRIP INOP AT SEAT 9C. REPLACED EEL LIGHT STRIP AND OPS CHECKED OKAY.

Part: D-RING — STUCK (EVAC RAFT) · airframe 46,178 hrs · 12,823 cycles

DOOR 2L RAFT D-RING IS STUCK INSIDE SLIDE HOUSING. FOUND D-RING ATTACHED TO RIGHT DOOR INSTALLATION SIDE HOOK. REMOVED D-RING, INSTALLED ON LEFT DOOR INSTALLATION SIDE.

Part: STARTER — DEFECTIVE (RT ENGINE) · airframe 46,078 hrs · 12,788 cycles

NO ROTATION ON RT MOTOR WHEN START VALVE ENGAGED. REPLACED RT ENGINE STARTER. OPS CHECK GOOD.

Part: PUSHROD — LACK OF LUBE (L3 DOOR) · airframe 46,069 hrs · 12,784 cycles

THE 3L DOOR WILL NOT ARM. REMOVED SLIDE AND LUBED DISARM PUSHRODS AND RE-INSTALLED SAME SLIDE AT 3L.

Part: GCU — FAILED (LT ENGINE) · airframe 45,940 hrs · 12,739 cycles

LEFT ENGINE GEN CONT FAILURE, RESET OKAY. BPCU FAULTS LT GCU. REPLACED GCU. ALSO RAN ENGINE TO MAKE SURE GEN 1 OKAY.

Part: LIGHT — DAMAGED (SEAT 34A) · airframe 45,828 hrs · 12,705 cycles

EMERGENCY LIGHT AT SEAT 34A DAMAGED. REPAIRED EMERGENCY LIGHT SYSTEM AT SEAT 34A. EMERGENCY LIGHT SYSTEM CHECK OKAY.

Part: START VALVE — FAULTY (RT ENGINE) · airframe 44,482 hrs · 12,324 cycles

NO ENG STARTER EICAS MESSAGE. RETURNING TO GATE. RIGHT ENG, LEFT ENGINE START NORMAL. REPLACED START VALVE. OPS GOOD.

Part: CIRCUIT CARD — FAILED (RT ENGINE) · airframe 44,243 hrs · 12,263 cycles

R ENG NO START. GOOD ENGAGE. REACHES 12 PERCENT N2 THEN DISENGAGES, 2ND ATTEMPT SAME. MANUAL START WAS OK. REPLACED STARTER VALVE AND RT ENGINE SPEED CARD. GROUND CHECKED GOOD.

Part: IDG — DEFECTIVE (NR 1 ENGINE) · airframe 43,670 hrs · 12,099 cycles

DURING 3SV SERVICE NR 1 IDG TOOK 50 STROKES TO FULL SERVICE. CK'D IDG NO EXTERNAL LEAKS. VERIFIED IDG SERVICED FROM A SERVICEABLE SERVICE CART. REPLACED NR 1 ENG IDG PRECAUTIONARY FOR TAKING 50 STROKES. OP CHECKED GOOD ON ENG RUN, NO LEAKS, NO FAULTS.

Part: IDG — FAULTY (RT ENGINE) · airframe 43,334 hrs · 12,014 cycles

AFTER RT ENG SHUTDOWN, HAD COMPLETE ELEC FAILURE. LT BUS ISLN LIGHT ON+LT GEN DROPPED OFF. REPLACED NR1 ENGINE IDG. OPS CHECK OKAY.

Part: GENERATOR — DAMAGED (APU) · airframe 43,173 hrs · 11,971 cycles

AFTER APU START UP, OIL RUNNING FROM UNDERNEATH OF GEN TERMINAL BLOCK. CTR 2 FIELD STUDS APPEAR TO BE BROKEN. REPLACED APU GENERATOR AND FEEDER CABLES. NO LEAKS DURING APU OPS CHECK.

Part: BLEED VALVE — FAULTY (LT ENGINE) · airframe 43,107 hrs · 11,951 cycles

THE L ENG BLEED WON'T CLOSE WITH SWITCH OFF. CYCLE LEFT END START SW AND APU BLEED OPENED. ALL INDICATIONS NORMAL. REPLACED RELAY K10282 LT AIR SUPPLY ENGINE START RELAY. REPLACED AIR GROUND SYS 2 RELAY K10201. OP CHECKS GOOD ON ENGINE RUN.

Part: BATTERY — DISCHARGED (CABIN) · airframe 42,854 hrs · 11,885 cycles

EEL LIGHTS INOP AT FWD COACH CABIN ALONG WITH 1 EA STOW BIN LIGHT AND HATCH LIGHTS. REPLACED BATTERY FOR POWER SUPPLY M10567. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,656 hrs · 11,830 cycles

EEL STRIP INOP AT SEAT ROW 14ABC. REPLACED EEL SEGMENT, OPS GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 42,618 hrs · 11,822 cycles

THE 34C EXIT STRIP MISSING. REPLACED EEL STRIP AT SEAT 34C.

Part: STATUS MESSAGE — ACTIVATED (FIRE WARNING) · airframe 42,525 hrs · 11,800 cycles

L ENG FIRE LOOP 1 STATUS MSG.

Part: INDICATOR — NO TEST (COCKPIT) · airframe 42,476 hrs · 11,787 cycles

STANDBY ENGINE INDICATOR (SEI) WILL NOT BITE TEST. REPLACED SEI. OP CHECKS NORMAL.

Part: INVERTER — FAILED (CABIN) · airframe 42,006 hrs · 11,670 cycles

CENTER SECTION BY FWD CTR EMERGENCY EXIT WILL NOT ILLUMINATE DURING TEST, FOUND INVERTER FOR ASSOCIATED AREA COLD. SUSPECT INVERTER FAILURE. REPLACED INVERTER. OPS CHECK GOOD.

Part: GENERATOR — LEAKING (HYD SYSTEM) · airframe 42,006 hrs · 11,670 cycles

HMG TEST FAILED WITH ONLY PARTIAL VOLTAGE SHOWING ON EICAS. REPLACED HMG PER MM 24-25- 01. PERFORMED OPERATIONAL TEST AND LEAK CHECK. FOUND HYDRAULIC FLUID LEAKING FROM MAIN BODY PARTING SURFACES. RE-INSTALLED ORIGINAL HMG, OPS CHECK GOOD.

Part: IDG — FAULTY (RIGHT) · airframe 41,806 hrs · 11,620 cycles

RIGHT GENERATOR OFF LIGHT ILLUMINATED, THEN A SHORT TIME LATER RIGHT GENERATOR DRIVE LIGHT ILLUMINATED. FOUND FAULTY IDG. REPLACED NR 1 IDG. RAN, OP CHECKED & LEAKED CHECKED. OK FOR SERVICE.

Part: SHUTOFF VALVE — FAULTY (LT ENGINE) · airframe 41,712 hrs · 11,594 cycles

LT ENGINE PRSOV NOT FULLY CLOSING AFTER ENGINE SHUTDOWN. REPLACED PRSOV, CHECKS GOOD. LT PRSOV & APU BLEED LIGHT WORK NORMALLY.

Part: ANTI-ICE VALVE — LOCKED (NR 1 ENGINE) · airframe 40,849 hrs · 11,352 cycles

LEFT ENG ANTI-ICE EICAS, LEFT ENG ANTI-ICE SWITCH OFF WITH VALVE LIGHT. NR 1 ENG ANTI ICE VALVE LOCKED IN THE OPEN POSITION. REPLACED NR 1 ENG AI VALVE, OPS OK.

Part: FITTING — LOOSE (HYDRAULIC SYS) · airframe 40,762 hrs · 11,327 cycles

HYDRAULIC QUANTITY DECREASED TO 47. QUANTITY STABLE WITH PUMPS OFF, CENTER SYSTEM. CREW COMMENTS, C HYD QTY .38 WITH PUMPS ON. SUPPLEMENTAL DATA UPDATE, FOUND C2 PRESS INLET UNION TO FILTER MODULE SPRAYING HYDRAULIC FLUID. SECURED UNION FITTING AND SERVICED HYD, NO LEAKS NOTED.

Part: SHUTOFF VALVE — FAILED (RIGHT) · airframe 40,762 hrs · 11,327 cycles

FUEL CONFIG LIGHT ON. IMBALANCE OF 3000 POUNDS BETWEEN LEFT AND RIGHT TANKS WITH BOTH CROSSFEED. SUPPLEMENTAL DATA UPDATE, RT FUELING SHUTOFF VALVE INOP. REPLACED RT FUELING SHUTOFF VALVE, OPS CHECKED NORMAL.

Part: TANK — LEAKING (FUEL CELL) · airframe 40,756 hrs · 11,320 cycles

FUEL ODOR IN COCKPIT FOR 5 SECONDS AFTER TAKEOFF. FOUND FUEL LEAK IN CENTER TANK CAUSING ODOR TO ENTER LT PACK. TANKS RESEALED, PACK BURN OUT PERFORMED.

Part: CARBON SEAL — FAILED (NR 1 ENGINE) · airframe 40,690 hrs · 11,296 cycles

FLIGHT DIVERTED WITH A FUEL ODOR ON THE FLIGHT DECK. FOUND CARBON SEAL FAILED AT NR 3 BEARING, OIL WETTING OF AREA. REPLACED NR 1 ENG, PERFORMED PACK BURN OUT.

Part: ACTUATOR — WEAK (RT MLG DOOR) · airframe 40,516 hrs · 11,250 cycles

GEAR SELECTED DOWN "DOORS" LIGHT AND "GEAR DOORS" EICAS. DURING TAXI IN TO GATE RT MLG DOOR WAS NOT CLOSED, DOOR WAS HANGING OPEN. FOUND ACTUATOR (DOOR) WEAK- POSSIBLE WATER CONTAMINATION. REPLACED RIGHT MLG DOOR ACT, PERFORMED SEVERAL DOOR/GEAR SWINGS, ALL SATISFACTORY.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 40,490 hrs · 11,244 cycles

ON APPROACH FLT EXPERIENCED A YELLOW GEAR DOOR WHEN LANDING GEAR WAS LOWERED. WHEELS SHOWED 3 GREEN. ALSO, A YELLOW AUTO SPEEDBRAKE LIGHT WHEN ATTEMPTED TO ARM. FLT EXECUTED A GO AROUND AND CONTACTED DISPATCH. ACCOMPLISHED BITE OF PSEU NO FAULTS NOTED. OPERATED DOORS MANUALLY AND PINNED GEAR AND OPERATED LANDING GEAR HANDLE ALL DOOR AND GEAR INDICATIONS NORMAL PER MM 32-00-15-201 OPERATED GEAR AND DOOR THROUGH SEVERAL CYCLES ALL INDICATIONS AND DOORS CHECK NORMAL, NO REPEATS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,117 hrs · 11,140 cycles

SEAT 16A EMERGENCY EXIT LIGHT BURNT OUT. LAMP BURNT OUT. RELAMPED EMERGENCY LIGHT, OPS CHECK GOOD.

Part: SWITCH — FAULTY (T/E FLAP) · airframe 39,891 hrs · 11,078 cycles

STATUS MESSAGE: FLAP ISLN VAL. PTU PRESSURE SWITCH FAULTY. REPLACED PTU PRESSURE SWITCH, OPS AND LEAK CHECKED OK.

Part: CONTROLLER — MALFUNCTIONED (NR 1 ENGINE) · airframe 39,413 hrs · 10,948 cycles

FOUND THIN PIECES OF METAL IN HI-STAGE VALVE NR 1 ENGINE. REPLACED HIGH STAGE VALVE AND HIGH STAGE CONTROLLER, ALSO ACCOMPLISHED A BOROSCOPE WITH NO DAMAGE NOTED TO INTERNAL AREAS. NO FURTHER DAMAGE WAS FOUND.

Part: STARTER — FAILED (APU) · airframe 39,319 hrs · 10,921 cycles

APU AUTO SHUTDOWN WILL NOT RESTART. REPLACED APU STARTER. ALL OPS CHECKED OK. ECU SHOWED NO FAULT FOR AUTO-SHUTDOWN.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 38,849 hrs · 10,795 cycles

FA REPORTS HOT SPOT AT SEAT 15A SIDEWALL.

Part: IDG — MALFUNCTIONED (LT ENGINE) · airframe 38,804 hrs · 10,782 cycles

AT CRUISE, LEFT IDG DRIVE LT AND DRIVE MESSAGE, CREW ACCOMPLISHED LEFT IDG DISCONNECT PER AFM.

Part: APU — OIL CONSUMPTION · airframe 37,803 hrs · 10,492 cycles

APU OIL CONSUMPTION ABOVE LIMIT. REPLACED GEARBOX SHUTOFF VALVE.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 37,605 hrs · 10,442 cycles

EMERGENCY FLOOR LIGHTS INOP (EEL) FROM DOOR 2 LEFT TO ROW 15. *S/D* SECURED BATTERY CONNECTOR, OPS CHECK OK.

Part: PBE — TORN (CABIN) · airframe 37,568 hrs · 10,433 cycles

PBE ON FWD WALL ON LEFT AFT CABIN LAV STORAGE BAG IS TORN. 09-07-07 FOUND A FAULTY PERSONAL BREATHING EQUIPMENT. REPLACED PBE.

Part: SPRING — BROKEN (R1 DOOR LEVER) · airframe 37,568 hrs · 10,433 cycles

CABIN DOOR 1R ARM-DISARM LEVER COVER SPRINGS BROKEN. 09-07-07 AFTER DIAGNOSING THE PROBLEM, DISARMED LEVER AT DOOR. REPLACED COVER FOR ARM.

Part: WIRE — CHAFED (WS 300) · airframe 35,491 hrs · 9,822 cycles

LEFT WING AFT SPAR BAY, WS 300, WIRING BUNDLE CHAFING HARD AGAINST HYD B-NUT, OUTER SHIELD ON BUNDLE IS TORN. REROUTED WIRE BUNDLE TO ENSURE ADEQUATE SEPARATION AND REPLACED OUTER SHIELD FOR BETTER PROTECTION.

Part: INDICATOR — MALFUNCTIONED (SLIDE PRESSURE) · airframe 33,413 hrs · 9,236 cycles

NR 4 RT SLIDE RAFT PRESSURE GAUGE READS LOW 1 NEEDLE FROM LOWER EDGE OF GREEN BAND. REPLACED NR 4 RT SLIDE RAFT.

Part: CONNECTOR — LOOSE (EEC) · airframe 33,203 hrs · 9,181 cycles

RETURNED TO THE FIELD DUE TO LEFT ENGINE PARAMETER FLUCTUATIONS. NR 1 ENGINE EEC CONNECTOR LOCKING RING WAS DAMAGED AND REPLACED EEC. THIS EEC WAS INSTALLED ON JUNE 25, 2006.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 33,145 hrs · 9,166 cycles

RETURNED TO FIELD DUE TO A NR 1 ENGINE COMPRESSOR STALL DURING CLIMB AT FL 240. SUPPLEMENTAL DATA UPDATE NO EXCEEDANCES NOTED WHEN POWER REDUCED TO IDLE, BUT FELT A SLIGHT VIBRATION. ACCOMPLISHED FIM 71-05-00, THRU BLOCK 37. INLET, EXHAUST OK. OIL FILTER AND 6 CHIP DETECTORS OK. EPCS HAD NO FAULTS OR MESSAGES AND NO AUTO EVENT. ALSO BORO FRONT AND REAR N2 COMP, AP2 AND AP8. REPLACED 14 STAGE CONVERTER VALVE AND ACCOMPLISHED 14TH STAGE CONVERTER VLV TEST. ALSO REPLACED EEC AND DAMAGED CONNECTOR.

Part: ENGINE — CONTAMINATED · airframe 29,363 hrs · 8,048 cycles

RETURNED TO FIELD UNDER AMBER ALERT DUE TO FUMES IN THE COCKPIT. ODOR DISSAPATED DURING RETURN TO GATE. THE DETERGENT WASH OF THE ENGINES IS THE SORCE OF THE ODOR. PER MM 72-05-99 PAGE 701, ENGINE NEEDS HIGH POWER RUN AFTER WASH TO REMOVE ANY DETERGENT RESIDUAL FROM PNUEMATIC SYSTEM.

Part: O-RING — LEAKING (SLIDE BOTTLE)

ESCAPE SLIDE BOTTLE HAS LOW PRESSURE. FILLER VALVE O-RING WAS LEAKING. FILLER VALVE O-RING WAS REPLACED.

Part: LIGHT — INOPERATIVE (L1 DOOR SLIDE) · airframe 24,755 hrs

DOOR 1L SLIDE ARM LIGHT INOP. RELAMPED LIGHT, OPS CHECKED OK.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 23,731 hrs · 6,461 cycles

FUSELAGE SKIN IS DAMAGED AT BS 1440 AND SKIN LAP 20L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 23,731 hrs · 6,461 cycles

SKIN DENTS STA 600-640, AND STRINGER 14L-19L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER TRIPLER REPAIR.

Part: SEAL SEAT — DETECTED (NR 3 SEAL) · airframe 22,601 hrs · 6,149 cycles

FLT DIVERTED DUE TO SMOKE IN CABIN. ENGINE REMOVED AND NR 1, 2&3, NR 3 FORWARD & NR 3 AFT CARBON SEALS ALL REMOVED AND CHECKED. ALL CARBON SEALS CHECKED GOOD, MATING SURFACES OF SEAL SEATS OF NR 3 FWD & NR 3 AFT WERE FOUND TO HAVE HEAT CRACKS. MICROCRACKS ARE TYPICAL OF SEAL SEATS & ALTHOUGH THEY PRESSURE TESTED GOOD, STILL HAVE CONTRIBUTED TO SLIGHT LEAKAGE. IN ADDITION, SEAL SEATS ALSO FOUND TO BE SLIGHTLY OUT OF SPEC FOR FLATNESS. COMBINATION OF INCONTIGUOUS FLATNESS & MICROCRACKS IS BELIEVED TO HAVE CAUSED THE INTERMITTANT SEAPAGE OF OIL INTO GAS PATH.

Part: LINE — CRACKED (NR 2 ENG OIL) · airframe 22,561 hrs · 6,138 cycles

NR 2 ENGINE OIL QUANTITY DROPPED STEADILY IN FLIGHT. REPLACED CRACKED & LEAKING FUEL/OIL HEAT EXCHANGER RETURN LINE. LINE CRACKED DUE TO LIBERATED TUBE CLAMP.

Part: SKIN — DENTED (FUSELAGE) · airframe 15,474 hrs · 4,220 cycles

FUSELAGE SKIN DENTED AT STATION 1440 JUST BELOW S20L. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER.

Part: VANE — FRACTURED (NR 1 ENGINE) · airframe 15,196 hrs · 4,156 cycles

NUMBER 1 ENGINE FAILED. UPON DISASSEMBLY THE ROOT CAUSE FOR THE FAILURE WAS LOW PRESSURE TURBINE (LPT) 4TH VANE SULFIDATION FRACTURE. WHEN THESE VANES FAILED, IT RESULTED IN HEAVY DAMAGE TO THE 5TH, 6TH, & 7TH STAGES OF THE LPT.

Part: SKIN — DAMAGED (BS 1692)

FUSELAGE SKIN AT BS 1692, STR 20L RECEIVED DAMAGE FROM A SERVICE TRUCK. THE RESULTING DAMAGE IS ELEVEN INCHES LONG INCLUDING A 2.75 INCH TEAR IN THE SKIN. THERE WAS NO DAMAGE TO THE UNDERLYING STRUCTURE. *S/D* DAMAGE CAUSED BY CONTACT FROM SERVICE TRUCK. DAMAGED AREA WAS CUT OUT AND AN EXTERNAL REPAIR DOUBLER WAS INSTALLED BASED ON 757 SRM.

Part: PRESSURIZATION — MALFUNCTIONED (CABIN)

CABIN ALTITUDE AUTO 1 AND 2 STATUS MESSAGES, AND AUTO INOP LIGHT ON OVERHEAD ILLUMINATED. UNSCHEDULED LANDING WAS MADE INTO DEN.