N514UA

Part: LENS — LOOSE (R4 DOOR) · airframe 75,282 hrs · 28,130 cycles

DOOR 4R SLIDE LIGHT INOPERATIVE. TROUBLE SHOT IAW FIM25-66 00, FOUND LIGHT LENS ASSEMBLY LOOSE. REPLACED LIGHT LENS ASSEMBLY IAW WDM25-66-11, OPERATIONS CHECKED GOOD.

Part: KIT — MISSING (CABIN) · airframe 75,246 hrs · 28,120 cycles

FLIGHT ATTENDANT CANNOT LOCATE ONBOARD SECURITY KIT. SECURITY KIT MISSING DF2520 FT. REPLACED SECURITY KIT.

Part: UNKNOWN — MALFUNCTIONED (FIRE TEST) · airframe 75,226 hrs · 28,113 cycles

APU FIRE TEST FAILED.

Part: THRUST REVERSER — OUT OF RIG (NR 1 ENGINE) · airframe 75,104 hrs · 28,073 cycles

WHILE TESTING NR 1 ENG REVERSER FOUND OTBD HALF OF REVERSER TO OPEN & CLOSE SIX SECONDS AFTER IT WAS STOWED. PUT REVERSER BACK IN SERVICE. RIGGED OTBD REVERSER HALF IAW AMM. CHECKED SYNK LOCK IAW AMM, REVERSER OPERATIONS CHECKED GOOD.

Part: STRUCTURE — DAMAGED (CARGO BAY) · airframe 75,095 hrs · 28,070 cycles

AFT CARGO PIT FLOOR HAS DAMAGE AT APPROXIMATELY 18 INCHES INBD & APPROXIMATELY 8 INCHES AFT OF DOOR SILL. MEASURES APPROXIMATELY 1.0 X 1.75 INCHES. SECOND DAMAGE NOTED AT APPROXIMATELY 36 INCHES FROM DOOR SEAL MEASURES APPROXIMATELY .75 INCHES. INSTALLED TEMPORARY REPAIRS IAW GNMM 1-0-1-102.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 75,074 hrs · 28,064 cycles

EMERGENCY EXIT LIGHTS INOPERATIVE AT ABOVE MED 1R & FIRST CLASS CABIN AT CURTAIN FWD SIDE. SECURED BATTERY & POWER SUPPLY CONNECTOR IAW WDG 33-51-12. EMERGENCY EXIT LIGHT SYSTEM OPERATION CHECKED OK.

Part: LIGHT — INOPERATIVE (R4 DOOR) · airframe 75,015 hrs · 28,042 cycles

DOOR 4R WILL NOT ARM. DOOR ARMED OK, ARM LIGHT RELAMPED & KNEE KNOCKER POP OUT WAS STICKING. ADJUSTED KNEE KNOCKER. DOOR ARMS NORMALLY.

Part: ACTUATOR — LEAKING (RT SPOILER) · airframe 75,004 hrs · 28,040 cycles

HYD LEAK RT ENG PYLON. REPLACED NR 10 SPOILER PCA.

Part: INDICATOR — LACK OF LUBE (R4 DOOR) · airframe 74,875 hrs · 28,002 cycles

DOOR 4R ARMED INDICATOR BEHIND HANDLE IS STICKING. LUBED INDICATOR ON DOOR 4R, OPERATIONS CHECKED GOOD

Part: LEVER — OUT OF ADJUST (L4 DOOR) · airframe 74,817 hrs · 27,979 cycles

DOOR 4L ARMING HANDLE DOES NOT GO ALL THE WAY TO ARMED POSITION. ADJUSTED ARM LEVER POSITION, OPERATIONS CHECKED OK IAW MM.

Part: VSI — MALFUNCTIONED (COCKPIT) · airframe 74,808 hrs · 27,976 cycles

CAPTS VSI OFF FLAG & ERRATIC INDICATOR RTFL. REPLACED CAPTS VSI IAW B757 AMM 34-22-06. PERFORMED LT IRU OPERATIONS CHECKED IAW 34-21-00 & LT AIR DATA COMPUTER TESTED NORMAL.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 74,805 hrs · 27,974 cycles

FRETTING CORROSION ON METAL FLOOR & ATTACHED FITTING BETWEEN BS1681 & BS 1720, RBL48 & RBL57. REMOVED CORROSION AT AFT DECK PLATE BS 1681 TO 1720 RBL48-57 IAW SRM 51-10-02. FOUND 3 ARE AS OUT OF LIMITS AT STATION 1692.2 RBL 50.2, STATION 1696.8 RBL 50.2, STATION 170 4.5 RBL 50.3 IAW SRM 53-60-51. FABRICATED & INSTALLED REPAIR DOUBLERS & FILLERS IAW ECRA 5330-04259. R & R AFT GALLEY FORWARD FITTING STATION 686 RBL56 IAW SRM 51-40-02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 74,805 hrs · 27,974 cycles

FUSELAGE SKIN REPAIR AT BS685-694 BETWEEN STRINGER 22L & 24L IS CAT 'B' REPAIR. ACCOMPLISHED EXTERNAL FUSELAGE SKIN REPAIR BS685-694 BETWEEN STRINGER 22L & 24L IAW ECRA5330- 04729.

Part: SKIN — DENTED (FUSELAGE) · airframe 74,805 hrs · 27,974 cycles

LOWER FUSELAGE SKIN BETWEEN BS680-694 BETWEEN STRINGER 22L & 24L HAS DENT FROM THE INSIDE OUT. REPAIRED LOWER FUSELAGE SKIN BS685-694 BETWEEN STRINGER 23L & 24L IAW ECRA5330-04729.

Part: SKIN — CRACKED (R4 DOOR) · airframe 74,805 hrs · 27,974 cycles

2 INCH CRACK ON R4 DOOR INNER SKIN 10 INCHES FROM FWD EDGE & 31 INCHES FROM TOP EDGE. CUTOUT DAMAGE AREA ON R4 DOOR INNER SKIN 10 INCHES FROM FWD EDGE & 31" FROM TOP EDGE. FABRICATED DOUBLER & SHIM, INSTALLED IAW SRM 20-41-02 & 51-70-13 FIG 1.

Part: SKIN — CANNING (R2 DOOR) · airframe 74,805 hrs · 27,974 cycles

FOUND THE R 2 DOOR SKIN OIL CANNED 10" FROM AFT EDGE ABOVE STRINGER 21R. REPAIRED IAW 52-10-01 REPAIR NR 1. REMOVED DAMAGED AREA & REPAIRED IAW B757 SRM 52-10-01 RPR-1.

Part: SKIN — DENTED (BS 1885.2) · airframe 74,805 hrs · 27,974 cycles

AFT UPPER FUSELAGE EXTERNAL SKIN DENTED BS 1885.20 L3L. FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-00-01 RPR 3.

Part: STRAP — CORRODED (BS 1681) · corrosion level 2 · airframe 74,805 hrs · 27,974 cycles

FRETTING CORROSION ON METAL WEB ON TOP OF FRAME FLANGE AROUND BS 1681 AT BL 0 & LBL 58. R & R STRAP.

Part: SKIN — BULGED (FUSELAGE) · airframe 74,805 hrs · 27,974 cycles

THERE IS A SHARP SMALL BULGE ON THE FUSELAGE SKIN AT STATION 677.8 BETWEEN S25R & S26R, THAT WAS FOUND TO BE OUT OF LIMITS. REPAIRED IAW 53-00-01 REPAIR 3 & IS IN ZONE A.

Part: GIRT BAR — DIRTY (R4 DOOR) · airframe 74,368 hrs · 27,843 cycles

R4 DOOR WILL NOT ARM, LIGHT DOES NOT COME ON. CLEAN DEBRIS FROM GIRT BAR AREA. GIRT BAR ARMS NORMALLY AND ARMED LIGHT OPERATES.

Part: FAIRING — DAMAGED (TE FLAP) · airframe 74,015 hrs · 27,735 cycles

DURING WALK AROUND FOUND DAMAGE ON THE RT WING CANOE FAIRING JUST OTBD NR 2 ENG. SMALL HOLE MEASURED .500 X .500 THRU OUTER SKINS PLYS. PLACED ON CF 934 AW WITH SRM 57-53-70. AD1, FIG 101.

Part: SEAL — DAMAGED (COCKPIT WINDOW) · airframe 73,806 hrs · 27,674 cycles

CAPTAIN`S L2 WINDOW HAS LOUD WHISTLE IN CRUISE, 8.5 DIFFERENTAL PRESSURE, FL 370 AUTO 1. REPLACED CAPTAIN`S NR 2 WINDOW PRESSURE SEAL IAW MM.

Part: SMOKE DETECTOR — INOPERATIVE (AFT LAVATORY) · airframe 73,542 hrs · 27,595 cycles

AFT LAVATORY SMOKE DETECTOR INOPERATIVE. REPLACED AFT SMOKE DETECTOR, OP CHECKED GOOD.

Part: CAP — MISSING (EMERGENCY LIGHTS) · airframe 73,388 hrs · 27,540 cycles

EMERGENCY LIGHT STRIP ON FLOOR MISSING ALL END CAPS. REPLACED ALL END CAPS.

Part: INLET — DENTED (NR 1 ENGINE) · airframe 73,254 hrs · 27,496 cycles

RAMP REPORT DENT ON NR 1 ENGINE INLET COWL SKIN. PERFORMED INTERIM REPAIR PER ECRA 5411-01066 PART 1 INTERIM STEPS 1-4. INITIATED CF TO INSPECT PER PART 2 AT INTERVALS NOT TO EXCEED 3 DAYS AND PERFORM PERMANENT REPAIR PER PART 3 WITHIN 15 DAYS. CW PART 2 OF ECRA 5411-01 066 NO CRACK NOTED.

Part: BEARING — LACK OF LUBE (L4 DOOR) · airframe 73,043 hrs · 27,418 cycles

INBOUND FLT ATT REPORTED THAT DOOR 4L SLIDE HARD TO ARM-DISARM. REMOVED SLIDE PACK 4L AND LUBED BEARINGS AND ROD ENDS. RE-INSTALLED SLIDE PACK ARM DISARM FUNCTION CHECKS NORMAL.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 72,589 hrs · 27,274 cycles

CARGO PIT FLOOR PANEL CRACKED. DAMAGED AREA NOT ABLE TO RPR. NEED NEW FLOOR PANEL 170-3422. INSTALLED PANEL PER AMM.

Part: BLOCK — FAULTY (FIRE INDICATION) · airframe 72,458 hrs · 27,227 cycles

AFT CARGO FIRE IND LIGHT ON CTR CONSOLE BULB IS BLOWN. REPLACED DIODE BLOCK IN SWITCH, OP OKAY.

Part: PROXIMITY SENSOR — DEFECTIVE (R1 DOOR) · airframe 72,383 hrs · 27,202 cycles

DOOR 1R ESCAPE SLIDE; UPON ARMING "SLIDE" LIGHT ILLUMINATED BRIGHT, DIMMED AND OUT. LIGHT IS VERY DIM IN ARMED POSITION. REPLACED PROXIMITY SENSOR S10217, OPS CHECKED GOOD.

Part: TERMINAL BLOCK — CRACKED (ELECTRICAL) · airframe 72,239 hrs · 27,156 cycles

TB190 BLOCK 5-6 IS CRACKED AND UNUSABLE.

Part: WINDOW — CRACKED (COCKPIT) · airframe 71,777 hrs · 26,997 cycles

BIG CRACK ON WINDSHIELD F/O SIDE. REPLACED NR 1 RIGHT WINDOW.

Part: SNUBBER — WORN (L4 DOOR) · airframe 71,649 hrs · 26,951 cycles

MAIN CABIN L-4 DOOR BODY TORQUE TUBE SNUBBER WEAR INDICATOR SHOWS WORN BEYOND SERVICEABLE LIMITS. REMOVED & REPLACED SNUBBER WITH SERVICEABLE UNIT IAW 757 AMM. REMOVED AND RE-INSTALLED GUIDE ARM AND DOOR IAW 757 AMM.

Part: SNUBBER — WORN (L2 DOOR) · airframe 71,649 hrs · 26,951 cycles

MAIN CABIN L-2 DOOR BODY TORQUE TUBE SNUBBER WEAR INDICATOR SHOWS WORN BEYOND SERVICEABLE LIMITS. REMOVED AND REPLACED L-2 DOOR BODY TORQUE TUBE ROTARY SNUBBER IAW 757 AMM. DOOR OPS CHECKED GOOD IAW 757 AMM.

Part: SNUBBER — WORN (R4 DOOR) · airframe 71,649 hrs · 26,951 cycles

MAIN CABIN R-4 DOOR BODY TORQUE TUBE SNUBBER WEAR INDICATOR SHOWS WORN BEYOND SERVICEABLE LIMITS. REMOVED DOOR & GUIDE ARM & RE-INSTALLED DOOR & GUIDE ARM IAW 757 AMM. REMOVED AND REPLACED SNUBBER IAW 757 AMM.

Part: SNUBBER — WORN (L1 DOOR) · airframe 71,649 hrs · 26,951 cycles

MAIN CABIN L-1 DOOR BODY TORQUE TUBE SNUBBER WEAR INDICATOR SHOWS WORN BEYOND SERVICEABLE LIMITS. REMOVED AND REPLACED MAIN CABIN L4 DOOR ROTARY SNUBBER IAW 757 AMM & OPS CHECKED DOOR GOOD IAW MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,649 hrs · 26,951 cycles

MAIN CABIN STA 324 FLOORBEAM UPPER T-CAP CORRODED FROM RBL 20 TO RBL 65. REMOVED BOTH LT AND RT T-CAPS FROM LBL 8-LBL 60 AND LBL 8 TO RBL 60, FABRICATED NEW SECTIONS OF T-CAP, SPLICE ANGLES AND STRAPS AND INSTALLED PER SRM 53-10-08, REPAIR 2. PER SRM, THIS IS A CAT B REPAIR, AND PER TABLE 202, FUTURE INSPECTIONS REQUIRED AT INITIAL THRESHOLD OF 37,500 TOTAL AIRFRAME CYCLES.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 71,649 hrs · 26,951 cycles

BS 1640 FLOORBEAM TEE CORRODED FROM LBL 3 TO RBL 10. REMOVED DAMAGED TEE BETWEEN LBL3 TO RBL 60. FABRICATED A NEW TEE, REPAIR STRAPS, AND ANGLES, AND INSTALLED PER SRM 53-00-51, REPAIR 3. CATEGORY -A- REPAIR.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 71,649 hrs · 26,951 cycles

MAIN CABIN BS 365 FLOORBEAM UPPER TEE ANGLE IS CORRODED FROM RBL 20 TO 65. REMOVED DAMAGED TEE ANGLE, FABRICATED A NEW TEE ANGLE, SPLICE ANGLES, STRAPS AND INSTALLED PER SRM 53-00-51, REPAIR 3. CATEGORY A REPAIR.

Part: FITTING — GOUGED (L1 DOOR) · airframe 71,649 hrs · 26,951 cycles

MAIN L1 DOOR FRAME UPPER ROLLER GUIDE GOUGED. REPLACED UPPER ROLLER LATCH CAM FITTING. ADJUST AND OPS CHECKED DOOR PER AMM.

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 71,649 hrs · 26,951 cycles

CABIN FLOORBEAM TEE CAP FROM LBL 3 TO RBL 10 HAS SURFACE CORROSION. BLENDED CORROSION, FOUND REMAINING MATERIAL THICKNESS TO BE OUT OF SRM LIMITS. FABRICATED TEE CAP AND TWO REPAIR ANGLES PER SRM.

Part: MOUNT — CORRODED (GALLEY) · corrosion level 2 · airframe 71,649 hrs · 26,951 cycles

MAIN CABIN FLOOR STA 380 BL42R GALLEY FITTING CORRODED. REPLACED CORRODED GALLEY MOUNT FITTING WITH NEW PART.

Part: MODULE — FAULTY (SPOILERS) · airframe 70,683 hrs · 26,625 cycles

EICAS MESSAGE 'SPOILERS' - CONFIGURATION LIGHT ILLUMINATED. ACFT ON GROUND WITH SPOILERS DOWN. RT YAW DAMPER EICAS ILLUMINATED AS WELL. RT FLT CONTROL ELEC, MESSAGE AND FAULT BALL DISPLAYED. REPLACED NR 1R CSEU POWER SUPPLY (M538), OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,229 hrs · 26,472 cycles

NR 4 DOOR EVAC LIGHT IS INOP. RELAMPED NR 4R EVAC LIGHT, OP CHECKS GOOD.

Part: GIRT BAR — DIRTY (L1 DOOR SLIDE) · airframe 69,841 hrs · 26,326 cycles

L1 DOOR WOULD NOT DISARM. FOUND DEBRIS IN GIRTBAR PAWL AREA. REMOVED, CLEANED, AND ADJUSTED SLIDE PACK STRAPS, OPS OKAY.

Part: PLACARD — OUT OF POSITION (CABIN) · airframe 69,453 hrs · 26,199 cycles

F/A REPORTED, UNABLE TO ARM L2 DOOR. FOUND GIRT BAR ARMING HANDLE RUBBING ON ARMING PLACARD. ADJUSTED PLACARD ASSY CHECKS OKAY PER CREW.

Part: AUDIO PANEL — FAILED (COCKPIT) · airframe 69,104 hrs · 26,052 cycles

CAPTAIN'S MICROPHONE FROM O2 MASK NOT COMING THRU SPEAKER. REPLACED AUDIO CONTROL PANEL, OPS OKAY.

Part: MICROPHONE — INOPERATIVE (OXYGEN MASK) · airframe 68,938 hrs · 25,987 cycles

F/O O2 MIC INOPERATIVE. SWAPPED OUT TO THE FIRST OBSERVER BEHIND THE CAPTAIN SEAT. THIS AIRCRAFT HAS 2 OBSERVER SEATS. MIC INOP ONLY O2 OK. SEAT IS INOP. REPLACED O2 MASK. OPS CHECKED NORMAL.

Part: FILTER — DIRTY (CABIN) · airframe 67,224 hrs · 25,367 cycles

ODOR LIKE ACETONE VERY STRONG AROUND ROWS 11 &12 AND THROUGHOUT CABIN. REPLACED LEFT AND RIGHT RECIRCULATION HEPA FILTERS PER MM.

Part: GIRT BAR — OUT OF POSITION (L1 DOOR) · airframe 67,188 hrs · 25,352 cycles

CREW REPORTS AFTER DOOR 1L OPENED. MATERIAL IS HANGING FROM BOTTOM OF DOOR. NEED MECHANIC TO INVESTIGATE & CONTACT SAMC. DOOR 1L SLIDE DEACTIVATED FOR MAINTENANCE. REMOVED SLIDE COVER AND INSPECTED GIRT BAR ASSY, FOUND RT GIRT BAR SLIDER ASSY DISCONNECTED FROM GIRT BAR. REPORTED FINDING TO SAMC CONTROLLER. SECURED GIRT BAR PER MM, NO DEFECTS NOTED. REACTIVATED SLIDE.

Part: SWITCH — BROKEN (L2 DOOR) · airframe 67,174 hrs · 25,347 cycles

SPRING BROKEN ON GUARD FOR SLIDE PRESSURE TEST BUTTON AT 2L. REPLACED SWITCH ASSY AT DOOR 2 LEFT. SYSTEM CHECKS NORMAL WHILE AT THE GATE.

Part: PLATE — CRACKED (FUSELAGE) · airframe 66,177 hrs · 24,959 cycles

LOWER AFT CORNER OF SCUFF PLATE HAS A CRACK IN IT. TWO FASTENERS ARE ALSO SHEARED OFF, ONE ON THE AFT CUFF PLATE AND ONE ON THE CENTER SCUFF PLATE. REPAIRED BY WELD REF MM AND GNMM.

Part: END PLUG — MISSING (EMERGENCY LIGHTS) · airframe 65,997 hrs · 24,882 cycles

EMERGENCY ESCAPE LIGHT STRIP END CAPS MISSING 9C & 34C. REPLACED END CAPS.

Part: END PLUG — MISSING (EMERGENCY LIGHTS) · airframe 65,936 hrs · 24,860 cycles

EMERGENCY ESCAPE FLOOR LIGHTING STRIP END CAP MISSING 9C AND 34C. REPLACED MISSING END CAPS.

Part: SKIN — DELAMINATED (THRUST REVERSER) · airframe 64,880 hrs · 24,450 cycles

NR 2 ENG OUTBOARD THRUST REVERSER UPPER BIFURCATION PANEL INNER SKIN AND OUTER SKIN BOTH 90 PERCENT DELAMINATED. DELAM EXCEEDS 600 SQUARE IN AND IS BEYOND LIMITS TO TEMP REPAIR. REQUIRES FERRY FLIGHT TO REPAIR. REPLACED NR 2 ENG OUTBOARD THRUST REVERSER.

Part: SKIN — DAMAGED (LT MLG DOOR) · airframe 64,448 hrs · 24,294 cycles

LT MAIN GEAR STRUT DOOR HAS DAMAGE ON L/E AT MID POINT WITH SKIN MISSING AND OPEN TO CORE FOAM. OPEN AREA IS 4 BY 1-2 WITH L SHAPED CRACK 2 INCH BY 1 INCH AT LWR EDGE OF DAMAGE CONT OF AMIS ITEM 4482001. ACP INTERIM REPAIR PER EVA -73721, TAPE RECHECK REQUIRED PRIOR TO EACH DEPARTURE, PERMANENT REPAIR IN 150 HRS. ACCMP'D REPAIRED IAW SRM.

Part: FUSE — FAULTY (CABIN) · airframe 64,448 hrs · 24,294 cycles

AFT CARGO DOOR EXTERIOR EMERGENCY EVACUATION LIGHT INOP. REPLACED LAMP, NO HELP. REPLACED FUSE P/N FU305 IN M10699, CHECKS OKAY.

Part: LIGHT — INOPERATIVE (LT MLG WW) · airframe 64,448 hrs · 24,294 cycles

LEFT WHEEL WELL UNSAFE LIGHT INOPERATIVE. REPLACED LAMP, OPS GOOD.

Part: SLIDE — FAULTY (R3 DOOR) · airframe 63,317 hrs · 23,845 cycles

DOOR 3R SLIDE PACK LOW PRESSURE. REPLACED DOOR SLIDE AT 3R. INSPECTED SLIDE FOUND SECURED ON DOOR, REMOVED AND STOWED SLIDE PIN, REMOVED AND STOWED DOOR ASSY BOTTLE PIN.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,598 hrs · 23,568 cycles

MAIN CABIN EMERGENCY LIGHT AT ROW 13L INOP. TROUBLESHOT AND FOUND EMERGENCY LIGHT BATTERY PACK BAD. REPLACED BATTERY PACK AND OPS CHECKS GOOD.

Part: MOUNT — LOOSE (CABIN) · airframe 61,619 hrs · 23,194 cycles

SEAT ASSYS LOOSE IN SEAT TRACK. REPLACED LEFT FRONT SEAT MOUNT, SECURED REMAINING MOUNT POINTS.

Part: WINDOW — OPEN (COCKPIT) · airframe 60,969 hrs · 22,958 cycles

CREW HEARD LOUD NOISE FROM F/O SLIDING WINDOW. RTFL. FOUND WINDOW PARTIALLY OPENED ON THE AFT SIDE. HANDLE STILL LOCKED AND INDICATOR STILL READING CLOSED. NO HISTORY. BELIEVE WINDOW CLOSED BUT LINKAGE NOT FULLY OVER CENTER, ALLOWING WINDOW TO COME OPEN PARTIALLY ON TAKEOFF. OPERATED WINDOW NUMEROUS TIMES, OPERATED OK AND LOCKED PROPERLY. CREW STATED ON ARRIVAL AT ACFT - WINDOW WAS OPEN APPROX 2 INCHES. CREW MEMBER STATED THAT THEY CLOSED AND LATCHED WINDOW, BUT ADMITTED THAT THEY MAY NOT HAVE CRANKED WINDOW TO THE FULLY CLOSED POSITION PRIOR TO LATCHING IT AND AGREED THAT MOST LIKELY THIS WAS OPERATOR ERROR.

Part: JAM-NUT — LOOSE (R1 DOOR) · airframe 60,002 hrs · 22,579 cycles

NR 1 RT PASSENGER DOOR - COCKING PUSHROD ROD END JAM NUT LOOSE - REQUIRES ADJUSTMENT. RED DANGER TAG ATTACHED FROM PREVIOUS VISIT WARNING TO ADJUST AND SAFETY. ROD END LOCATED FWD OF INTERNAL DOOR HANDLE MECHANISM.

Part: SPRING — BROKEN (R2 DOOR) · airframe 58,707 hrs · 22,108 cycles

DOOR 2R EVAC SLIDE ARM-DISARM LEVER COVER DOOR HAS BROKEN RETURN SPRING. REPLACED ARM DISARM DOOR COVER.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,707 hrs · 22,108 cycles

LEFT AFT OVERWING EXIT EMERGENCY LIGHT FWD AND ABOVE HATCH INOP WHEN LIGHTS SELECTED ON. RELAMPED BULB, OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,119 hrs · 21,901 cycles

EXTERIOR EMERGENCY LIGHTS HAS 2 INOP LIGHTS, ONE AT THE DPP R R2 AND ONE AT THE LEFT WING. FOUND BULBS OUT/INOP. RELAMPED BULBS, ALL OPS CHECKS OK.

Part: FEEDER CABLE — LOOSE (EMERGENCY LIGHTS) · airframe 58,119 hrs · 21,901 cycles

A ZONE EEL INOP. FOUND POWER FEEDER WAS LOOSE. RECONNECTED POWER FEEDER AND OPS CHECKED OK.

Part: SKIN — TORN (THRUST REVERSER) · airframe 57,891 hrs · 21,803 cycles

NR 1 ENG LEFT REVERSER HALF HAS A 10 INCH TEAR IN SKIN AT AFT COWL LATCH PANEL ACCESS DOOR. REPLACED NR 1 ENGINE THRUST REVERSER HALF.

Part: SQUIB — MALFUNCTIONED (RT ENGINE) · airframe 57,053 hrs · 21,498 cycles

THE R ENG SQUIB TEST 1 FAILED. SWAPPED SQUIBS, RESET C/B OPS CHECKED NORMALLY, NO KNOWN CAUSE. NO REPEATS SINCE ORIGINAL.

Part: A/C PACK — ODOR (LEFT) · airframe 56,933 hrs · 21,452 cycles

ACRID ODOR FROM AIR CONDITIONING SYS ON DEPARTURE. CREW ISOLATED LT PACK OFF AND ODOR DISSIPATED. CREW STATED IT SMELLED LIKE HYD FLUID. LT PACK INOP. ENGINE HISTORY SHOWS THAT ENGINE WAS REMOVED DUE TO OIL PUDDLE AT NR 3 BEARING AREA, ACCOMPLISHED BORESCOPE OF THE ENGINE NR 1, LOOKING FOR EVIDENCE OF OIL IN THE NR 3 BEARING COMPARTMENT. NO OIL FOUND BUT STREAKING PRESENT COMING FROM HOLES ON HUB & ON IGV'S AND HPC BLADES. REPLACED NR 1 ENGINE.

Part: CHARGER — UNKNOWN (MAIN BATTERY) · airframe 56,127 hrs · 21,158 cycles

MAIN BATTERY CHARGER STATUS MESSAGE DISPLAYED. [08-08-07] REPLACED AC MAIN BATTERY AND CHARGER.

Part: PROXIMITY SENSOR — OBSTRUCTED (BIRT BAR) · airframe 56,089 hrs · 21,145 cycles

DOOR 2R GIRT BAR ENGAGEMENT LIGHT WILL NOT COME ON WHEN ARMING DOOR. *S/D* REMOVED DEBRIS FROM PROX SENSOR AREA. REPLACED FWD GIRT BAR PROX SENSOR & ADJUSTED.

Part: RIVET — MELTED (FUSELAGE) · airframe 55,770 hrs · 21,022 cycles

SECTION 41, STATION 399.5 HAS 6 MELTED RIVETS. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE & INSTALLED DOUBLER REPAIR.

Part: STRAP — CRACKED (FUSELAGE) · airframe 55,765 hrs · 21,020 cycles

CRACKED FLOORBEAM STABILIZING STRAP AT BS 375, LBL 25. MAJOR REPAIR ACCOMPLISHED: REPAIRED & INSTALLED STRAP.

Part: SLIDE — FAULTY (L1 DOOR) · airframe 55,765 hrs · 21,020 cycles

L-1 DOOR HARD TO ARM AND DISARM. [06-20-07] REMOVED AND REPLACED SLIDE DUE TO SKIRTING MATERIAL INTERFERING WITH GIRT BAR,

Part: STRUCTURE — DENTED (CARGO DOOR) · airframe 55,765 hrs · 21,020 cycles

FWD CARGO DOOR DENTED ON AFT EDGE OF FWD CARGO DOOR APPROX DAMAGE TO MEASURE QUARTER INCH IN DEPTH AND HALF INCH IN LENGTH. MAJOR REPAIR ACCOMPLISHED: INSTALLED EXTERNAL DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 55,763 hrs · 21,019 cycles

AFT PIT, LEFT STA 1580, STR 25L AREA, MAIN FRAME DENTED. MAJOR REPAIR ACCOMPLISHED: REMOVED DENT DAMAGE ON FRAME INBOARD FLANGE BETWEEN STR 23L - 24L & BETWEEN 26L-27L. REMOVED EXISTING PRODUCTION SPLICE. FABRICATED & INSTALLED A NEW PRODUCTION SPLICE ANGLE. FABRICATED & INSTALLED 3EA -20 STRINGER CLIPS & 1EA -1 STRINGER CLIP.

Part: FRAME — DENTED (FUSELAGE) · airframe 55,763 hrs · 21,019 cycles

AFT PIT, LEFT SIDE STA 1420 BETWEEN STR 24- 25L, MAIN FRAME DENTED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE & EXISTING PRODUCTION SPLICE. FABRICATED & INSTALLED A NEW PRODUCTION SPLICE ANGLE. FABRICATED & INSTALLED 2 EA -15 STRINGER CLIPS.

Part: FRAME — BENT (FUSELAGE) · airframe 55,763 hrs · 21,019 cycles

FWD PIT LEFT SIDE, STA 580, STR 24L - 25L MAIN FRAME BENT (RIB). MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE AND EXISTING PRODUCTION SPLICE AND FABRICATED A REPAIR ANGLE AND INSTALLED. ALSO FABRICATED & INSTALLED 1 EA -80 STRINGER CLIP.

Part: FRAME — DENTED (FUSELAGE) · airframe 55,763 hrs · 21,019 cycles

FWD PIT, LEFT SIDE, STA 680, BETWEEN STR 23 - 24L, MAIN FRAME HAS DENT (RIB). MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE AND FABRICATED A J-REPAIR ANGLE AND INSTALLED TO NEST INSIDE THE FRAME INBOARD FLANGE.

Part: FRAME — CRUSHED (FUSELAGE) · airframe 55,763 hrs · 21,019 cycles

FWD PIT- LEFT SIDE, STA 600 BETWEEN STR 22- 25L MAIN FRAME CRUSHED (RIB). MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED & INSTALLED A J-ANGLE REPAIR NESTED INSIDE THE FRAME INBOARD FLANGE. FABRICATED & INSTALLED 2 EA -80 STRINGER CLIPS. FABRICATED & INSTALLED ONE -6 SHEAR TIE.

Part: FRAME — DENTED (FUSELAGE) · airframe 55,763 hrs · 21,019 cycles

AFT PIT, RIGHT SIDE, STA 1580 AT STR 25R AREA, MAIN FRAME DENTED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE AND FABRICATED A J-ANGLE REPAIR PIECE AND INSTALLED NESTED INSIDE FRAME INBOARD FLANGE.

Part: FRAME — DENTED (FUSELAGE) · airframe 55,763 hrs · 21,019 cycles

FWD PIT, LEFT SIDE, STA 660, BETWEEN STR 24 -25L, MAIN FRAME DENTED (RIB). MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE AND EXISTING PRODUCTION SPLICE. FABRICATED A NEW PRODUCTION SPLICE AND 1 EA -30 STRINGER CLIP.

Part: FRAME — DENTED (FUSELAGE) · airframe 55,763 hrs · 21,019 cycles

AFT PIT RIGHT SIDE, STA 1560 AT STR 25R, MAIN FRAME DENTED (RIB). MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE AND FABRICATED A J-ANGLE REPAIR PIECE AND INSTALLED NESTED INSIDE FRAME INBOARD FLANGE.

Part: FITTING — DAMAGED (NR 1 PYLON) · airframe 55,763 hrs · 21,019 cycles

NR 1 PYLON AT NAC STA 201, INBOARD MID SPAR FITTING, LOWER TANG, FASTENER HOLE ELONGATED. MAJOR REPAIR ACCOMPLISHED: CLEANED UP DAMAGE. FABRICATED & INSTALLED A FREEZE PLUG.

Part: FRAME — DENTED (FUSELAGE) · airframe 55,763 hrs · 21,019 cycles

AFT PIT, LEFT SIDE, STA 1480 BETWEEN STR 24 - 25L, MAIN FRAME HAS 2 EA DENTS. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE AND FABRICATED A J-REPAIR ANGLE AND INSTALLED NESTED INSIDE THE FRAME INBOARD FLANGE.

Part: FITTING — DAMAGED (RT WING) · airframe 55,763 hrs · 21,019 cycles

INBOARD SIDE LOAD FITTING, INBOARD FWD HOLE DAMAGED RIGHT WING. MAJOR REPAIR ACCOMPLISHED: REAMED HOLE OVERSIZED. COLD WORKED HOLE & FINAL REAMED FOR OVERSIZED FASTENER INSTALLATION.

Part: FRAME — DENTED (FUSELAGE) · airframe 55,763 hrs · 21,019 cycles

AFT PIT, LEFT SIDE STA 1440, STR 25L AREA, MAIN FRAME DENTED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE ON FRAME INBOARD FLANGE BETWEEN STR 23L - 23L & 25L, REMOVED EXISTING PRODUCTION SPLICE. FABRICATED & INSTALLED A NEW PRODUCTION SPLICE ANGLE. FABRICATED & INSTALLED 3EA -15 STRINGER CLIPS.

Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 55,763 hrs · 21,019 cycles

R-2 DOOR, FORWARD FRAME AT UPPER HINGE CUTOUT IS CRACKED. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED A CRES DOUBLER.

Part: FRAME — DENTED (FUSELAGE) · airframe 55,763 hrs · 21,019 cycles

AFT PIT, LEFT SIDE, STA 1400, STR 25L AREA, MAIN FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: REMOVED EXISTING REPAIR FROM FRAME INBOARD FLANGE AT STR 27L. FABRICATED & INSTALLED A NESTED J-ANGLE REPAIR WHICH IS NESTED INSIDE THE EXISTING CHORD BETWEEN STR 25L AND 27L.

Part: SWITCH — BROKEN (CABIN) · airframe 55,763 hrs · 21,019 cycles

DOOR 1L EMERGENCY LIGHT TEST SWITCH BROKEN. REPLACED SWITCH.

Part: PIN — PULLED (EVAC SLIDE) · airframe 55,763 hrs · 21,019 cycles

DOOR L2 SLIDE, PIN IS PULLED OUT OF STITCHING. [06-20-07] REPLACED A FAILED SLIDE.

Part: CREASE BEAM — CORRODED (BS 1022 S17R) · airframe 55,763 hrs · 21,019 cycles

STR 17R CREASE BEAM WEB AT BS 1022 HAS SURFACE CORROSION ON UPPER SURFACE. [SUP 06-01-07] MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION. REMOVED WEB. FABRICATED & INSTALLED NEW WEB.

Part: BEARING — BROKEN (NR 8 SLAT) · airframe 55,763 hrs · 21,019 cycles

NR 8 SLAT I/B AUX TRACK BEARING & ATTACH BOLT FOUND BROKEN. LAYING IN WING L/E CAVITY 2 MORE BROKEN BOLTS & BEARINGS FOUND IN SAME CAVITY. [06-20-07] INSTALLED NR 8 IB AUX TRACK BOLT AND BEARING. CHECKED AND ADJUSTED SLAT. ATTRIBUTED FAILURE TO A FAILED BEARING.

Part: PULLEY — CRACKED (ELEVATOR CONTROL) · airframe 55,763 hrs · 21,019 cycles

CRACKED PULLEY, ELEV CONTROL CABLE ROUTING AT STA 343, FWD CABIN, LEFT UPPER. [06-20-07] INSTALLED NEW PULLEY.

Part: WIRE HARNESS — FRAYED (L4 DOOR SLIDE) · airframe 55,763 hrs · 21,019 cycles

DOOR 4L ESCAPE SLIDE LATCH HARNESS FRAYED INTO STITCHING. [06-20-07] REPLACED DOOR 4L SLIDE LATCH HARNESS.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 55,763 hrs · 21,019 cycles

AFT GALLEY AREA STA 1640, BL 0 TO RBL 54 AREA, FLOORBEAM TEE CAP UPPER SURFACE HAS SURFACE CORROSION AT FASTENER HOLES. [SUP 06-01-07] MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION. REMOVED DAMAGED SECTION OF T-CAP. FABRICATED & INSTALLED NEW TEE CAP SECTION.

Part: SMOKE — DETECTED (CABIN) · airframe 50,899 hrs · 19,275 cycles

DURING TEST FLIGHT CREW EXPERIENCED SMOKE OUT IN CABIN. REPLACED LOWER RECIRC FAN, OPS CHECK OK.

Part: SKIN — DENTED (STA 618 TO 620 S) · airframe 50,539 hrs · 19,142 cycles

LT FUSELAGE APPROX STA 618 TO 620, S-15 TO S-16 HAS A DENT. REMOVED DAMAGED ACP NDT INSP, NO CRACKS NOTED. FABRICATED REPAIR AND INSTALLED IAW SRM 53-00-01.

Part: LIGHT — INOPERATIVE (SLIDE) · airframe 50,539 hrs · 19,142 cycles

EXTERIOR EMERGENCY SLIDE LIGHT L41 AT DOOR 2RT IS INOPERATIVE. RE-SECURED TERMINAL LUGS.

Part: SKIN — DAMAGED (6 O'CLOCK POSITI) · airframe 50,539 hrs · 19,142 cycles

FOUND DENT AT 6 O'CLOCK POSITION STA 1600. FOUND DENT WITHIN LIMITS IAW SRM 53-00-01. BURNISHED AND SMOOTHED OUT DENT.

Part: SKIN — DAMAGED (NR2 ENG PYLON IB) · airframe 50,375 hrs · 18,881 cycles

NR 2 ENGINE PYLON IB SIDE FWD ACCESS HOLE, DAMAGED. MAJOR REPAIR ACP ON NR 2 ENGINE PYLON INBD SIDE FWD ACCESS HOLE REF DOCK W.U.G2788H.

Part: WARNING LIGHT — ILLUMINATED (GENERATOR/APU) · airframe 50,499 hrs · 19,125 cycles

LANDED UNDER AMBER ALERT DUE TO INOP GENERATOR & APU OIL QTY STATUS MESSAGE. APU REMOVED. DIAGNOSTIC TEST FOUND NO HOC/ OIL LEAKS. APU DISSASSEMBLED FOR LIFE LIMITED PART. APU OIL QTY MESSAGE DISPLAYED ON EICAS. - NO HOC IN AMIS (ENGOIL) EXCEPT ONE AMBER HIT, & DECLINING! MECH NAME THAT DID WRITE UP IS: FESTA, M F/N118437 SFOMM SEQ 5002004 ON 10/17/05. DIAG TEST GOOD. NO OIL CONSUMPTION, NO HIDING OIL. SECOND STAGE TURBINE DISK CLOSE TO CYCLE LIMITED LIFE EXPIRATION (412 CYCLES REMAIN). REPLACED. REMOVED TURBINE PARTS SHOW NO SIGNS OF DISTRESS OR REASON FOR A NO START OR HOC CONDITION. NO CAUSE FOUND FOR APU REMOVAL AND REPORTED AS MAINTENANCE ERROR.

Part: ENGINE — FLAMED OUT (NR 2) · airframe 50,059 hrs · 18,958 cycles

ENGINE FLAMEOUT DURING NR 2 ENGINE START.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,114 hrs · 18,219 cycles

EXTERNAL FUSELAGE SKIN DAMAGED STA 1618 AT STR 19L. INSTALLED SKIN AND STRINGER REPAIRS.

Part: LIGHT — WILL NOT TEST (CABIN) · airframe 47,145 hrs · 17,850 cycles

EEL LIGHTS INOP FROM ROW 31 TO AFT LAV. REPLACED POWER STRIP.

Part: O-RING — LEAKING (HYD PUMP) · airframe 46,286 hrs · 17,543 cycles

HYDRAULIC QUANTITY DROPPED TO .47. TURNED OFF BOTH LEFT HYDRAULIC PUMPS TILL DESCENT AND LANDING. *S/D* CASE DRAIN MODULE O-RING FAILED. REPLACED O-RING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,241 hrs · 16,096 cycles

EEL STRIP INOPERATIVE, IN FRONT OF AFT LAV. REPLACED EEL STRIP.

Part: ISOLATOR — WORN (NR 1 ENGINE) · airframe 41,291 hrs · 15,758 cycles

NR 1 ENGINE FWD MOUNT ISOLATOR JOURNAL ON MOUNT BEAM IS WORN AND DISCOLORED. MAJOR REPAIR ACCOMPLISHED. REPLACED ENGINE MOUNT BEAM.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 37,538 hrs · 14,317 cycles

CENTER EICAS "C HYD LOW QTY" RSVR LIGHT ON OVERHEAD. TURNED OFF CENTER HYD PUMPS, LOW PRESSURE LIGHTS CAME ON AT THAT TIME. LOWER EICAS STATUS CENTER QUANTITY ZERO

Part: PLUG — LOOSE · airframe 37,474 hrs · 14,294 cycles

LEFT EMERGENCY ESCAPE SQUIB DID NOT TEST IN TEST 1. ALL TEST IN TEST 2. FOUND CANNON PLUG ON SQUIB LOOSE, REINSTALLED CANNON PLUG, AND PERFORMED SQUIB TEST. TESTED NORMAL IN BOTH LEFT AND RIGHT IN TEST 1 AND 2.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 37,430 hrs · 14,275 cycles

FWD EDGE OF AFT PRESSURE DECK CORRODED STA 1681 LBL 3.5 TO LBL 14.5 AREA IS APPROX 2.55 INCH X 10.7 INCH WL 208.1. *S/D* MAJOR REPAIR ACCOMPLISHED. DOUBLER INSTALLED.

Part: INDICATOR — TRIPPED (TE FLAP) · airframe 32,619 hrs · 12,520 cycles

LANDED UNDER AMBER ALERT DUE TO A FLAP DISAGREEMENT. *S/D* T/E FLAP SYSTEM LOCKED OUT. FOUND FLAP TRANSMISSION OVERLOAD INDICATORS TRIPPED. RESET TRANSMISSIONS AND OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER PROBLEMS.

Part: HANDLE — BROKEN (FIRE EXT)

LEAD SEAL BROKEN ON WATER FIRE EXTINGUISHER. *S/D* CHARGE HANDLE WAS FOUND FROZEN OPEN WITH CORROSION. REPLACED BOTTLE.

Part: ENGINE — HUNG START (NR 1)

NUMBER ONE ENGINE HAD HUNG START AND DID NOT ACCELERATE. *S/D* FOUND NO PROBLEMS AND ENGINE WAS RESTARTED USING MAXIMUM MOTOR PROCEDURE.

Part: STRIP — INOPERATIVE (CABIN)

EMERGENCY ESCAPE LIGHT STRIP INOP ROW 35. REPLACED LIGHT STRIP AND CHECKS OK.

Part: BATTERY — DISCHARGED (CABIN)

FORWARD CABIN EMERGENCY ESCAPE PATH LIGHTS INOP. REPLACED BATTERY PACK, CHECKS OK.