N573UA

Part: MOUNT BRACKET — BROKEN (FIRE BOTTLE) · airframe 68,028 hrs · 24,842 cycles

PORTABLE WATER FIRE EXTINGUISHER MOUNT BRACKET FOUND BROKEN ON ARRIVAL AFT OF SEAT ROW 40ABC. REPLACED BRACKET & INSTALLED EXTINGUISHER.

Part: O-RING — DAMAGED (LT SPOILER) · airframe 67,814 hrs · 24,777 cycles

LT OTBD FLAP LEAKING FLUID FROM FOUR DRAIN HOLES UNDER WING. REPLACED LEAKING O-RING MOST OTBD SPOILER ACTUATOR LT WING, LEAKS CHECKED GOOD.

Part: SEAL — MISSING (FLAP TRACK) · airframe 67,687 hrs · 24,733 cycles

NR 1 FLAP TRACK CANOE IS MISSING INBD & OTBD BLADE SEALS, MEL COMPLIED WITH. INSTALLED NEW BLADE SEALS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,111 hrs · 23,890 cycles

EEL AT AFT LAV IS IN-OP. REPLACED EEL STRIP.

Part: RUDDER PEDAL — JAMMED (COCKPIT) · airframe 65,006 hrs · 23,855 cycles

CAPT'S RUDDER PEDALS JAMMED FULL FORWARD.

Part: SEAL — DEFECTIVE (RT DEOILER) · airframe 64,537 hrs · 23,686 cycles

RIGHTT ENGINE HAS OIL DRIPPING EVERY FEW SECONDS, FROM BOTTOM OF ENGINE COWL. LCL AMT REPORTS OIL WETNESS AT DEOILER BREATHER OUTLET AREA, NO OTHER LEAKS NOTED, PER AMM 79- 00-95 PARA 6.E CLEANED AREA, PER PARA 6.F A SMALL AMOUNT OF OIL WILL EXIT OUT OF DEOILER BREATHER OUTLET, TO PREVENT IRREG OPS, REPLACE THE DEOILER SEAL ASSY WITHIN 25 HRS, AND CHECK OIL TANK PRIOR TO EACH DEPARTURE, REPLACED DE-OILER SEAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 64,245 hrs · 23,580 cycles

EXTERIOR EMERGENCY LIGHT AT DOOR 1R IS INOP. INOP LIGHT NEEDS EVAC LIGHT ASSY. ACCOMPLISHED OPERATIONAL CHECK ON DOOR 1R EMERGENCY EXTERIOR LIGHT. LIGHT CHECKED OKAY.

Part: UNKNOWN — ODOR (CABIN) · airframe 63,795 hrs · 23,425 cycles

BURNT ACRID ODOR NOTICED IN COCKPIT AND CABIN DURING TO ROTATION. DISSIPATED AFTER FEW MINS. RAN APU WITH BOTH PACKS ON, CHECKED ALL CABIN, LAV, GALLEY, E/E AND CARGO PITS FOR SMELLS, NONE NOTED. CHECKED ALL LIGHTS AND BREAKERS PER MM, ALL CHECKS NORMAL. RAN BOTH ENGINES WITH PACKS ISOLATED WITH NO ODORS THRU-OUT CABIN, ALL AREAS CHECKED NORMAL.

Part: WINDOW — OUT OF ADJUST (COCKPIT) · airframe 63,509 hrs · 23,331 cycles

REPEAT WRITE UP. AFTER FLT CAPTS WINDOW BINDS AND WON'T UNLOCK. ADJUSTED NR 2 WINDOW CAPTS SIDE PER MM. PRESSURIZED CABIN TO 4 LBS & RECHECKED AFTER DEPRESSURIZATION WINDOW LATCH LOCK OPS GOOD.

Part: WIRE — MISROUTED · airframe 63,202 hrs · 23,227 cycles

FOUND WIRING ROUTING FOR LOWER CLAMP INCORRECT PER FIGURE 3. ADDITIONAL WIRE LOOPING LOCATED IN WRONG POSITION, FOUND UPPER E CLIP LOOSE. FOUND WIRING CLAMP 12 INCHES ABOVE LOWER CLAMP NOT FASTENED TO STRUCTURE. FOUND WIRING ROUTING FOR LOWER CLAMP INCORRECT. ROUTED WIRE CORRECTLY. INSTALLED LOWER CLAMP AS REQUIRED. REF LM 3707 FCD 2125-01080 REV "F", FOUND ADDITIONAL WIRE LOOPING LOCATED IN WRONG POSITION. INSTALLED WIRE HARNESS CORRECTLY. FOUND UPPER ECLIP LOOSE. INSTALLED NEW ECLIP AND INSULATION AS NEEDED PER FCD2125-01080 REV F. SECURED. FOUND WIRING CLAMP 12 INCHES ABOVE LOWER CLAMP NOT FASTENED TO STRUCTURE, REPAIR AS REQR'D. INSTALLED STRINGER CLAMP AND WIRE CLAMP IN CORRECT LOCATION. SECURED AND ROUTED WIRE.

Part: ACTUATOR — FAULTED (SPEED BRAKES) · airframe 62,858 hrs · 23,095 cycles

SPEED BRAKE ISSUE. AC ROLLING LEFT WHEN SPEED BRAKES ARE EXTENDED. ACCOMPLISHED STEPS 1 THRU 2C STEP (6) REF MM 27-61-00. NEED TO FINISH SPEED BRAKE ADJUSTMENT AND TEST DUE TO LOG 1. AIRCRAFT ROLLS TO LEFT DURING SPEED BRAKE DEPLOYMENT. NEED TO FINISH SPEED BRAKE ADJUSTMENT AND TEST DUE TO LOG 1. AIRCRAFT ROLLS TO LEFT DURING SPEED BRAKE DEPLOYMENT. ACCOMPLISHED SPEED BRAKE ADJUSTMENT AND TEST PER MM. NR 11 SPOILER WAS OUT OF LIMITS. REMOVED AND REPLACED NR 11 SPOILER PER MM AND ADJUSTED PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,854 hrs · 23,094 cycles

DOOR 1L, 4L AND BEHIND FAIRING OF FUSELAGE TO WING EMERGENCY EVAC LIGHTS INOPERATIVE. RELAMPED ALL, OPS CHECKED GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 62,365 hrs · 22,910 cycles

AFT LAV EEL LIGHT INOPERATIVE. REPAIRED BROKEN EEL LIGHT, OPS CHECK OKAY.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 62,365 hrs · 22,910 cycles

ECONOMY PLUS EEL LIGHT INOPERATIVE. FOUND CONNECTOR UNPLUGGED. RECONNECTED, OPS OKAY.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 62,235 hrs · 22,857 cycles

CAPTAIN'S FIXED SIDE-FORWARD WINDOW'S VISIBILITY IS AFFECTED BY DEFECTS, REPLACE FIRST AVAILABLE. CREW COMMENTS: DELAMINATING NEAR BOTTOM LEFT CORNER. MAINT TEXT: PER FLT CREW FOUND CAPT'S NR 2 SLIDING WINDOW WITH DEFORMED OUTER SURFACE IN LWR AFT CORNER. SHOWS NO SERVICE LIMITS FOR DAMAGE FOUND. STARTED REMOVING WINDOW LINING. RPL'D NR 2 LAMINATE PER AMM.

Part: FIRE BOTTLE — LOW PRESSURE (CABIN) · airframe 62,206 hrs · 22,848 cycles

MID & AFT H2O FIRE EXTINGUISHER HAVE LOW PRESSURE. MID HALON FIRE EXTINGUISHER PRESSURE WITHIN LIMITS PER AMM. AFT HALON EXTINGUISHER GAGE READING LOW. REPLACED AFT HALON FIRE EXTINGUISHER PER AMM.

Part: SWITCH — FAULTY (L3 DOOR) · airframe 61,473 hrs · 22,578 cycles

SLIDE ARM ON WITH SLIDE DISARMED AT 3L. *SUPPLEMENTAL DATA UPDATE* CYCLED DOOR FOUND PROX SWITCHES CLEAN, BUT LIGHT STAYS ON. REPLACED SWITCH S10223 AND TESTED OKAY.

Part: ACTUATOR — MALFUNCTIONED (RUDDER) · airframe 61,302 hrs · 22,513 cycles

SLIGHT YAW OSCILLATIONS AT 250 KTS IN SMOOTH AIR, AUTOPILOT ON OR OFF. OK TO CONTINUE PER MM, THIS IS A KNOWN CONDITION AND IS ACCEPTABLE FOR DISPATCH WITHOUT CORRECTIVE ACTION. THE OUTBOUND FLIGHT CREW DETERMINED THAT NOT ENOUGH WORK WAS ACCOMPLISHED TO CORRECT THE DITHER IN THE RUDDER SYSTEM AND REFUSED TO FLY THE AIRCRAFT. ACCOMPLISHED SERVICE TIP MM, NO OSCILLATION FOUND AND NO UNWANTED MOVEMENT OF THE RUDDER CHANGER MECHANISM, ALSO ACP THE RUDDER RATIO ACTUATOR DITHER TEST AND THE YAW DAMP, ALL NORMAL.

Part: LIGHT — INOPERATIVE (R4 DOOR) · airframe 61,285 hrs · 22,505 cycles

DOOR 4R ARM LIGHT WILL NOT COME WHEN ARMED. RIGHT AFT DOOR SLIDE LIGHT FLICKERING. INTERNAL CONTACT ON SWITCH IS STICKING ON DOOR ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT ON DOOR 4R. CLEANED & LUBED DOOR 4R GIRT BAR MECHANISM, LIGHT WORKS NORMAL. STILL INOPERATIVE. REPLACED LIGHT ASSY, OP CHECKED GOOD.

Part: SEAL — UNSECURE (L4 DOOR) · airframe 61,238 hrs · 22,486 cycles

F/A REPORTS AIR LEAK AT DOOR 4L DURING CLIMBOUT AND DESCENT. FOUND LWR FWD AREA OF DOOR SEAL UNEVEN. REPAIRED REF SERVICE TIP 52-09-01. ALSO FOUND DOOR SEAL OUT OF IT'S RETAINER IN SAME AREA. SECURED DOOR SEAL.

Part: FLOOR SKIN — CORRODED (FUSELAGE) · airframe 61,230 hrs · 22,482 cycles

MAIN CABIN FLOOR SKIN CORRODED BS 1681, LBL 17 TO RBL 57. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION & MATERIAL REMAINING WAS OUT OF LIMITS PER SRM. FABRICATED A REPAIR DOUBLER AND FILLERS PER TIMCO REO G14002, RECV. D ON NON ROUTINE 24359. THIS IS A CATEGORY A PERMANENT REPAIR.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,230 hrs · 22,482 cycles

AFT CARGO STA 1620 FRAME AT BL 0 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED CORRODED SECTION OF FRAME BETWEEN STR 29R TO STR 30. FABRICATED A REPAIR DOUBLER AND STRINGER CLIPS, PER BAC DWG 140N2005, AND REPLACED 2 SHEAR TIES PER TIMCO REO G14040, REV A ON NON ROUTINE 23803. THIS REPAIR HAS RECEIVED FIRST STAGE APPROVAL FOR STATIC STRENGTH ONLY. A NEW FAA FORM 8100 -9 085625 MUST BE ISSUED ON OR BEFORE 13SEP2013. THE AIRCRAFT WILL BECOME UNAIRWORTHY UNLESS A NEW 8100-9 IS ISSUED BEFORE 13SEP2013.

Part: SKIN — DENTED (FUSELAGE) · airframe 61,230 hrs · 22,482 cycles

REPAIR FUSELAGE SKIN DENT JUST FWD OF AFT CARGO DOOR. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SKIN AND FABRICATED A REPAIR DOUBLER AND FILLER PER REO G14013, REV B ON NON ROUTINE 23688.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,230 hrs · 22,482 cycles

MAIN CABIN BS 322 FLOORBEAM CORRODED OUT OF LIMITS BETWEEN BS 320 TO BS 324 AND RBL 40 TO RBL 44. MAJOR REPAIR ACCOMPLISHED. RMV'D T-CAP SECTION FROM RBL 68 TO LBL 7. FABRICATED A NEW T-CAP SECTION PER BGACO DWG 141N2937, FABRICATED REPAIR STRAPS AND INSTALLED PER REO G1 4007, REV B ON NON ROUTINE 24348. THE FLOORBEAM UPPER CHORD REPAIR AT BS 234, BETWEEN RBL 30 TO RBL 50 HAS RECEIVED FIRST 85625 STAGE APPROVAL FOR STATIC STRENGTH ONLY. A NEW FAA FORM 8100-9 MUST BE ISSUED BEFORE 07SEP2013 FOR THIS REPAIR TO REMAIN VALID. THE AIRCRAFT WILL BECOME UNAIRWORTHY IS A NEW 8100-9 IS NOT RECEIVED PRIOR TO 07SEP2013. DOCUMENTED ON NON ROUTINE 24348.

Part: FRAME — DENTED (FUSELAGE) · airframe 61,230 hrs · 22,482 cycles

AFT CARGO COMPARTMENT BS 1620 BETWEEN STR 26L AND STR 25L FRAME IS DENTED. MAJOR REPAIR ACCOMPLISHED. TRIMMED OUT DAMAGE ON FRAME FLANGE AND FABRICATED A REPAIR DOUBLER PER SRM, REPAIR 5, DETAIL III, AND INSTALLED PER SRM ON NON ROUTINE 24207.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,230 hrs · 22,482 cycles

CABIN FLOOR SEAT TRACK SUPPORT CORRODED BS 365, RBL 30. MAJOR REPAIR ACCOMPLISHED. REMOVED CORRODED DOUBLER & FILLER AND FABRICATED A NEW FILLER AND DOUBLER AND INSTALLED PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,230 hrs · 22,482 cycles

MAIN CABIN BS 365, FLOORBEAM CORRODED OUT OF LIMITS BETWEEN BS 362 - BS 366 AND RBL 18 TO RBL 60. MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING FLOORBEAM PREVIOUS CORRODED REPAIR AND FABRICATED A NEW CHORD, ANGLES AND STRAPS PER SRM, REPAIR 3 AND INSTALLED PER SRM ON NON ROUTINE 24352.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,230 hrs · 22,482 cycles

AFT CARGO BS 1620 FRAME SHEAR TIE IS CORRODED BETWEEN STR 29L TO STR 30. REMOVED & REPLACED SHEAR TIE WITH NEW P/N 140N2002-307 SHEAR TIE AND INSTALLED PER SRM.

Part: SWITCH — INTERMITTENT (CABIN) · airframe 61,230 hrs · 22,482 cycles

L-2 EMERGENCY LIGHTS TEST BUTTON INTERMITTENT. REMOVED & REPLACED L2 EMERGENCY LIGHTS TEST SWITCH PER MM. OPS CHECK GOOD PER MM ON NON ROUTINE 24562.

Part: FRAME — DENTED (FUSELAGE) · airframe 61,230 hrs · 22,482 cycles

AFT CARGO COMPARTMENT, BS 1540, STR 26R FRAME IS DENTED ON INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. TRIMMED OUT DAMAGE ON FRAME INBOARD FLANGE AND FABRICATED A NEW REPAIR DOUBLER ANGLE AND INSTALLED PER SRM, REPAIR 5 AND SRM ON NON ROUTINE 24195.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 61,230 hrs · 22,482 cycles

AFT CARGO COMPARTMENT, BS 1500 AND STR 26L, FRAME DOUBLER IS DENTED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED FRAME DOUBLER AND FABRICATED A NEW REPAIR DOUBLER PER SRM, REPAIR 5, AND INSTALLED PER SRM ON NON ROUTINE 24194.

Part: FRAME — DENTED (FUSELAGE) · airframe 61,230 hrs · 22,482 cycles

AFT CARGO COMPARTMENT FRAME DENTED AT BS 1600, STR 25L TO STR 26L. MAJOR REPAIR ACCOMPLISHED. REMOVED DENTED FRAME SPLICE & FABRICATED A NEW REPAIR DOUBLER PER SRM, REPAIR 5 AND INSTALLED PER SRM ON NON ROUTINE 24336.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,230 hrs · 22,482 cycles

AFT CARGO STA 1620 FRAME SHEAR TIE IS CORRODED FROM STR 29R TO STR 30. MAJOR REPAIR ACCOMPLISHED. REMOVED SHEAR TIE AND REPLACED WITH NEW P/N 140N2002-252 SHEAR TIE AND INSTALLED PER SRM ON NON ROUTINE 23804.

Part: COLLAR — WORN (R1 DOOR) · airframe 61,230 hrs · 22,482 cycles

R1 PAX DOOR HOLD OPEN LOCK COLLAR WORN. REMOVED AND REPLACED R-1 PASSENGER DOOR HOLD OPEN LOCK COLLAR ASSY PER MM 52-11-08 ON NON ROUTINE 24488.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 61,230 hrs · 22,482 cycles

AFT CARGO BS 1580 SHEAR TIE BETWEEN STR 27L-28L IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED CORRODED SHEAR TIE WITH 100 PERCENT MATERIAL LOSS, FABRICATED A NEW SHEAR TIE PER BAC DWG 140N2002-566 AND INSTALLED PER SRM 51-40-2 ON NON ROUTINE 24535.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,230 hrs · 22,482 cycles

MAIN CABIN FLOORBEAM AT BL 0 TO RBL 66 HAS SURFACE CORROSION AT BS 1640. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF T-CAP DUE MATERIAL REMAINING OUT OF LIMITS AFTER CORROSION REMOVAL, AND FABRICATED A NEW SECTION OF T-CAP, SPLICES AND STRAPS PER SRM AND INSTALLED PER SRM ON NON ROUTINE 24413.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 61,230 hrs · 22,482 cycles

AFT CARGO COMPARTMENT STRINGER HAT CHANNEL CORRODED BS 1460 TO BS 1480, STR 29L. MAJOR REPAIR ACCOMPLISHED. REMOVED STRINGER SPLICE SECTION AND FABRICATED A NEW SPLICE CHANNEL PER BAC DWG 146N3820- 23 AND INSTALLED PER SRM 51-40-2 ON NON ROUTINE 24111.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,230 hrs · 22,482 cycles

CABIN FLOOR SEAT TRACK SUPPORT CORRODED AT BS 365 AND RBL 52. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SEAT TRACK & REPLACED WITH NEW TRACK P/N 654N0243-8 AND 2 EACH SUPPORT CHANNELS AND INSTALLED PER SRM ON NON ROUTINE 24406.

Part: COLLAR — WORN (L4 DOOR) · airframe 61,230 hrs · 22,482 cycles

L4 PAX DOOR HOLD OPEN LOCK COLLAR WORN. REPLACED HOLD OPEN SPLIT LOCK COLLAR PER MM AND OPS CHECK GOOD ON NON ROUTINE 24490.

Part: COLLAR — WORN (R4 DOOR) · airframe 61,230 hrs · 22,482 cycles

R4 PAX DOOR HOLD OPEN LOCK COLLAR WORN. REPLACED HOLD OPEN SPLIT LOCK COLLAR PER MM. OPS CHECK GOOD ON NON ROUTINE 24491.

Part: GATE — DAMAGED (R2 DOOR) · airframe 61,230 hrs · 22,482 cycles

R-2 DOOR LOWER GATE, RUBSTRIP ATTACH HOLES ARE ELONGATED. WELDED HOLES PER SM, PREHEATED & STRESS RELIEVED PER SM, PERFORMED FPI INSPECTION PER GN-MM, PROCESS 32, NO CRACKS NOTED. REPLACED LEVELING COMPOUND PER SM AND INSTALLED RUB STRIP ON NON ROUTINE 24731.

Part: HINGE — CORRODED (R2 DOOR) · airframe 61,230 hrs · 22,482 cycles

R-2 DOOR, HINGE ARM ASSY PIVOT SURFACE CORRODED. REPLACED HINGE, P/N 140N26 51-50 AND TRANSFERRED HARDWARE FROM OLD HINGE TO NEW HINGE PER SM-50-52-11-07-JD, HINGE ARM ASSY INSTALLED ON TIMCO OPS 6013.

Part: GATE — CORRODED (R4 DOOR) · airframe 61,230 hrs · 22,482 cycles

R-4 DOOR, LOWER GATE LOWER EDGE CORRODED. REMOVED & REPLACED LOWER GATE PER CMM AND SM ON NON ROUTINE 24256.

Part: COLLAR — WORN (L2 DOOR) · airframe 61,230 hrs · 22,482 cycles

L2 PAX DOOR HOLD-OPEN LOCK COLLAR WORN. REMOVED & REPLACED L-2 PASS DOOR HOLD OPEN LOCK COLLAR ASSY PER MM ON NON ROUTINE 24486.

Part: GATE — CORRODED (R2 DOOR) · airframe 61,230 hrs · 22,482 cycles

R-2 DOOR LOWER GATE LOWER EDGE CORRODED. REMOVED LOWER GATE & REMOVED CORROSION PER CMM SM, AND MATERIAL REMAINING IS WITHIN LIMITS. FILLED AND SMOOTHED AREA AND REINSTALLED GATE ON DOOR PER SM ON NON ROUTINE 24230.

Part: COLLAR — WORN (R2 DOOR) · airframe 61,230 hrs · 22,482 cycles

R2 PAX DOOR HOLD OPEN LOCK COLLAR WORN. REMOVED & REPLACED R-2 DOOR HOLD OPEN COLLAR LOCK ASSY PER MM ON NON ROUTINE 24487.

Part: COLLAR — WORN (L1 DOOR) · airframe 61,230 hrs · 22,482 cycles

L1 PAX DOOR HOLD OPEN LOCK COLLAR WORN. REMOVED AND REPLACED L-1 PASSENGER DOOR HOLD OPEN LOCK COLLAR ASSY PER MM ON NON ROUTINE 24489.

Part: LINK — WORN (R2 DOOR) · airframe 61,230 hrs · 22,482 cycles

R-2 DOOR HINGE LINK ASSY IS WORN. REMOVED AND REPLACED R-2 DOOR UPPER HINGE LINK ASSY PER MM ON NON ROUTINE 24485

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 61,230 hrs · 22,482 cycles

MAIN CABIN RIGHT SIDE CUSP CREASE BEAM WEB CORRODED BETWEEN BS 1400 TO BS 1420. MAJOR REPAIR ACCOMPLISHED. REMOVED WEB DUE OUT OF LIMITS PER SRM. FABRICATED AND INSTALLED A NEW WEB PER BAC DWG 146N5590 AND INSTALLED PER SRM ON NON ROUTINE 23953.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 61,230 hrs · 22,482 cycles

MAIN CABIN SECTION 46 RT SIDE CUSP CORRODED BS 1420-1440. MAJOR REPAIR ACCOMPLISHED. REMOVED WEB AS FOUND OUT OF LIMITS PER SRM. FABRICATED A NEW WEB AND INSTALLED PER BACO DWG 146N5590, REV E AND SRM ON NON ROUTINE 23954.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 60,899 hrs · 22,360 cycles

LT INBD AFT FLAP - 1.5" X 1.5" LOWER SURFACE PUNCTURE. PUNCTURE IS 2 INCHES FROM THE EDGE OF AFT FLAP. 6" FROM THE INBD EDGE OF DAMAGED AFT FLAP. -ACP'D INTERIM RPR PER SRM. APPLIED ALUMINUM FOIL TAPE (SPEED TAPE). INSPECT EVERY AIRPLANE "A" CHECK. REPLACE THE ALUM FOIL TAPE IF ANY PEELING OR DETERIORATION EVIDENT. REPAIR NO LATER THAN NEXT AIRPLANE "C" CHECK. ** MF7784 CREATED TO MONITOR **. FLAP NEEDS TO BE REMOVED SEND TO SHOP FOR REPAIRS, WILL NEED MORE THAN 2 SHIFTS. SHIFT SLOT REQUESTED. REMOVED DAMAGED LOWER SKIN, CLEANED AND PREPPED FOR PRE-PREG LAYUP PER SRM. ACCOMPLISHED REPAIR ON NON ROUTINE 23664.

Part: STRUCTURE — DAMAGED (NACELLE) · airframe 60,899 hrs · 22,360 cycles

AS REPORTED ON STATUS NR 1 ENG HAS BIRD STRIKE DAMAGE. REPLACED NR 1 ENG INLET COWL PER MM.

Part: SKIN — DAMAGED (BS 249 S16-17L) · airframe 60,585 hrs · 22,266 cycles

FUSELAGE SKIN HAS LIGHTNING STRIKES AT BS 249, STR 16-17L. MAJOR REPAIR ACCOMPLISHED: BLENDED AREA AND FOUND TO BE OUT OF LIMITS PER SRM. REMOVED DAMAGE AND FABRICATED A REPAIR FILLER & DOUBLER AND INSTALLED PER REO G13718, REV C ON NON ROUTINE 40068. PER EVA 80916.

Part: PUSHROD — OUT OF ADJUST (L4 DOOR) · airframe 60,585 hrs · 22,266 cycles

MAIN CABIN L-4 DOOR MODE SELECTOR LEVER FAILS MIDWAY CHECK. ADJUSTED MAIN CABIN DOOR L -4 MODE SELECTOR LEVER GIRT BAR CRANK PUSH RODS PER MM. DOOR MIDWAY CHECK IS GOOD PER MM ON NON ROUTINE 39871.

Part: CAM — FAULTY (R4 DOOR) · airframe 60,585 hrs · 22,266 cycles

MAIN CABIN R-4 DOOR MODE SELECTOR LEVER FAILS MIDWAY CHECK. REMOVED AND REPLACED R-4 DOOR LOCKOUT CAM AND ADJUSTED LOCK OUT CAM MECHANISM PER MM AND OPS CHECK GOOD. ADJUSTED R-4 DOOR CRANK PUSH RODS PER MM ON NON ROUTINE 39872.

Part: SHAFT — FAILED (L1 DOOR HANDLE) · airframe 60,585 hrs · 22,266 cycles

MAIN CABIN L-1 DOOR EXTERNAL HANDLE WILL NOT STOW. REMOVED AND REPLACED MAIN CABIN L-1 DOOR EXTERIOR HANDLE CENTER SHAFT, YOKE ASSY, INNER SHAFT AND CLUTCH COLLAR PER CMM. L-1 DOOR EXT HANDLE OPS CKS GOOD PER CMM ON NON ROUTINE 39921.

Part: SLAT TRACK — DAMAGED (RT WING) · airframe 60,585 hrs · 22,266 cycles

RIGHT WING NR 8 SLAT OB AUXILIARY TRACK HARDWARE MISSING. WU 40267. REPLACED NR 8 SLAT OUTBOARD AUX TRACK HARDWARE PER MM.

Part: SPACER — MISSING (R4 DOOR) · airframe 60,585 hrs · 22,266 cycles

R-4 MAIN ENTRY DOOR ROTARY SNUBBER GUIDE ARM MISSING TWO SPACERS. INSTALLED 2 SPACERS ON GUIDE ARM PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,585 hrs · 22,266 cycles

EMERGENCY EXIT LIGHT INOP ROW 26 & 14 ABC. RELAMPED AND OPS CHECK EMERGENCY AISLE LIGHTS AT ROWS 26 AND 14 ABC IAW MM.

Part: BEARING — SPLIT (R1 DOOR) · airframe 60,511 hrs · 22,237 cycles

MAIN ENTRY DOOR 1 RT BODY TORQUE TUBE BEARING, LOWER HINGE BRG SPLIT IN TWO IN CAM PLATE. INSTALLED NEW BRG IN CAM PLATE AND INSTALLED LWR TORQUE TUBE ASSY.

Part: UNKNOWN — MALFUNCTIONED (AUTOPILOT SYS) · airframe 60,195 hrs · 22,121 cycles

AUTOPILOT DISCREPANCY, RTFL.

Part: WIRE — FRAYED (COCKPIT) · airframe 59,781 hrs · 21,968 cycles

CAPTAIN O2 MIC INOPERATIVE. FOUND WIRE FRAYED AT O2 BOX. REPLACED BOX IAW MM, OP CKS OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,727 hrs · 21,576 cycles

AFT LAV EMERGENCY FLOOR LIGHT STRIP INOP. REPLACED AFT LAV EMERGENCY LIGHT STRIP, OPS CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,039 hrs · 20,216 cycles

DOOR 4R EXTERIOR EMERGENCY LIGHT INOP. RELAMPED DOOR 4R EXT EMERGENCY LIGHT, OPS CHECKS GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (AFT LAV) · airframe 55,026 hrs · 20,208 cycles

FOUND AFT LAV SMOKE DETECTORS GOING OFF WHILE PRESSURIZED AND REPLACED. REPLACED BOTH AFT AND FWD AFT LAV SMOKE DETECTORS. REPLACED BOTH AFT AFT AND FWD AFT LAV SMOKE DETECTORS.

Part: SKIN — DENTED (FUSELAGE) · airframe 54,839 hrs · 20,141 cycles

EXT FUSE LT SIDE STA 580 SKIN LAP HAS DENT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR STR 19L STA 580.

Part: POWER SUPPLY — DISCHARGED (FUSELAGE) · airframe 54,177 hrs · 19,898 cycles

FWD GALLEY EMERGENCY LIGHTS WILL NOT COME ON. REPLACED M731 EMER LIGHTS POWER SUPPLY. EMERGENCY LIGHTS CHECKS OKAY.

Part: O-RING — DEFECTIVE (EVAC SLLIDE)

BOTTLE LOW, BELOW GREEN BAND. BOTTLE LEAKS AROUND BALL STEM O-RING. REMOVED & REPLACED O-RINGS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 53,921 hrs · 19,796 cycles

AIRCRAFT DAMAGED BY BELT LOADER ON FUSELAGE FWD OF AFT CARGO DOOR NEAR BOTTOM OF DOOR CUTOUT. DAMAGED AREA IS APPROX A LONG GOUGE 5\ LEADING UP TO A SERIES OF SMALL GOUGES. CENTER OF DAMAGED AREA ONE EIGHT INCH DEEP AND GOUGE ACROSS ONE RIVET. COMPLIED WITH EVA UA72507 BLENDED ALL DAMAGED AREA AND INSPECTED INSIDE STRINGER SURROUNDING, NO DAMAGED NOTED.

Part: LIGHT — LOOSE (CABIN) · airframe 53,419 hrs · 19,593 cycles

EXIT PATH LIGHTING LOOSE AT 1L. SECURED EMERGENCY AISLE LIGHTING STRIP.

Part: LIGHT — UNSECURE (CABIN) · airframe 53,419 hrs · 19,593 cycles

EXIT PATH LIGHTING LOOSE AT 1L. SECURED EMERGENCY AISLE LIGHTING STRIP.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 53,236 hrs · 19,520 cycles

EXTERIOR EVAC LIGHTS INOP AT DOORS 1RT, 2LT, 4RT AND 4LT. REPLACED LAMPS, CHECKS OKAY.

Part: PROXIMITY SWITCH — INOPERATIVE (R3 DOOR) · airframe 52,631 hrs · 19,288 cycles

DOOR 3R SLIDE LIGHT IS OUT. REPLACED DOOR 3R AFT GIRT BAR PROXIMITY SWITCH. OPS CHECKS OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,854 hrs · 19,001 cycles

EMERGENCY LIGHT ON LT SIDE OF AC BY PRESSURE RELIEF VALVES INOP. FOUND LIGHT INOP. REPLACED LAMP. OP CHECKS GOOD.

Part: CHIP DETECTOR — LEAKING (NR 1 ENGINE G/B) · airframe 50,721 hrs · 18,569 cycles

DIVERTED UNDER AMBER ALERT DUE TO NR 1 ENGINE SHUTDOWN. FOUND MAIN GEARBOX CHIP DETECTOR BAYONET PINS NOT LOCKED & PARTIAL INSTALLED & UNSEATING CHIP DETECTOR ASSY POPPET. CLEANED ENGINE, REINSTALLED CHIP DETECTOR. ADDED 16QTS OF MAINTENANCE OIL. ACCOMPLISHED IDLE ENGINE RUN PER JRH2-5-63 PG2 ITEM 3.A.(2) . AFTER 5 MIN ENG RUN RECHECKED CHIPS ALL NORMAL NO OIL LEAKS

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,516 hrs · 17,779 cycles

THE FOLLOWING EMERGENCY LIGHTS ARE INOP: SLIDE LIGHT DOOR 4L, EXIT MARKERS DOORS 4L & 4R, EXIT SIGN OVER DOOR 4L, AFT GALLEY EXIT SIGN, AISLE LIGHT ROW 32. REPLACED BATTERY PACK & CHARGER ASSEMBLY.

Part: UNKNOWN — WARNING MESSAGE (UNKNOWN) · airframe 48,237 hrs · 17,667 cycles

STATUS MESSAGE NOSE A-G DISAGREE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 48,029 hrs · 17,586 cycles

OUTSIDE EMERGENCY LIGHTS INOP DOORS 2L, 3L, 3R, 1R. RELAMPED LIGHTS. OPS CHECKED OK.

Part: PROXIMITY SWITCH — INOPERATIVE (DOOR 2R SLIDE) · airframe 47,206 hrs · 17,293 cycles

DOOR SLIDE LIGHT DOOR 2R DOES NOT ILLUM WHEN ARMED. [06-14-07] CHANGED LIGHT UNIT - NO HELP. REPLACED LIGHT BASE OPS CHECK NORMAL. REPLACED PROX SWITCH S10220 FOR ULTIMATE FIX.

Part: GATE — DAMAGED (L2 DOOR) · airframe 46,096 hrs · 16,882 cycles

FOUND DAMAGE AT DOOR 2L LOWER GATE AREA OF THE DOOR GOING FORWARD.

Part: CARRIAGE — DAMAGED (L2 DOOR GATE) · airframe 46,096 hrs · 16,882 cycles

FOUND DAMAGE AT DOOR 2L LOWER GATE AREA OF THE DOOR GOING FORWARD. ITEM ROLLED FORWARD. *S/D* MAJOR REPAIR ACCOMPLISHED. LEFT FUSELAGE BELOW DOOR 2L DAMAGED, 4' OF MAJOR DAMAGE EFFECTING A PRODUCTION SPLICE AND RUNS ALONG A STRINGER. MFG SM REPAIR PIECES, ACCOMPLISHED DOUBLER-TRIPLER & FILLER REPAIR.

Part: SKIN — DAMAGED (BS 1605) · airframe 45,178 hrs · 16,539 cycles

FUSELAGE SKIN WAS DAMAGED AT STA 1605, JUST BELOW STR 18L FROM CONTACT WITH GROUND EQUIPMENT. MAJOR REPAIR ACCOMPLISHED. REPAIRED DAMAGED AREA PER ENGINEERING AUTHORIZATION.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 45,178 hrs · 16,539 cycles

ACFT FUSELAGE PUNCTURE DAMAGE APPROX 5 INCHES IN LENGTH INTO PRESSURIZED SKIN JUST FWD AND LOWER SIDE OF DOOR 3L. REPAIR ACCOMPLISHED DAMAGED AREA HAS BEEN CUT OUT. REMOVED DUCTINGS FOR ACCESS THEN PERFORMED NDT. REPAIRED DAMAGED AREA.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 40,444 hrs · 14,833 cycles

CREW ABORTED TAKEOFF AT APPROXIMATELY 105 KNOTS NECESSARY TO LOCK OUT LEFT HIGH STAGE VALVE. PRIMARY CAUSE OF FAILURE WAS PRESSURE REGULATOR. REPLACED HIGH STAGE PILOT.

Part: SHEAR TIE — DAMAGED (FUSELAGE) · airframe 39,664 hrs · 14,525 cycles

AFT CARGO PIT, SHEAR TIE CORRODED BETWEEN STR 29R AND 28R.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,664 hrs · 14,525 cycles

CABIN FLOORBEAM CAP AT BS 311 CORRODED AT RBL 41.

Part: SKIN — CORRODED (FUSELAGE) · airframe 39,664 hrs · 14,525 cycles

FWD PIT LT TUNNEL, LAV SERVICE AREA, SKIN CORRODED AT BS 705-715, STR 21L-22L.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,664 hrs · 14,525 cycles

CABIN FLOORBEAM UPPER CAP CORRODED STA 1639 TO 1641, RBL 48 TO RBL 56.

Part: FLOORBEAM — BULGED (FUSELAGE) · airframe 39,664 hrs · 14,525 cycles

STATION 1681 RT AFT DECK PLATE (FLOORBEAM) BULGED AROUND FASTENER HOLE RBL 39.5 TO RBL 40.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,664 hrs · 14,525 cycles

CABIN FLOORBEAM T-CAP AT BS 365 CORRODED FROM BL 0 TO RBL 62, NUMEROUS AREAS.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 39,664 hrs · 14,525 cycles

CREASE BEAM WEB UPPER SURFACE CORRODED FROM STA 1422 TO 1434, RBL 69-71.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 39,664 hrs · 14,525 cycles

CREASE BEAM WEB CORRODED UPPER SURFACE STA 1385 TO 1397, RBL 68-71.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 39,664 hrs · 14,525 cycles

CREASE BEAM WEB CORRODED STA 1406-1411, RBL 69-70 UPPER SURFACE.

Part: CREASE BEAM — CORRODED (BS680 TO BS740) · airframe 39,664 hrs · 14,525 cycles

CABIN FLOOR, RT CREASE BEAM I/B CHORD ANGLE CORRODED AT BS 680 TO BS 740 BL 66R. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION FOUND OUT OF LIMITS. REMOVED CREASE BEAM I/B CHORD ANGLE AND REINSTALLED WITH NEW PART.

Part: SKIN — CORRODED (FUSELAGE) · airframe 39,664 hrs · 14,525 cycles

FUSELAGE EXTERNAL SKIN HAS CORROSION AROUND FASTENER HOLES TO RIGHT FWD UPPER WING TO BODY FAIRING ATTACH PT.

Part: SKIN — CORRODED (FUSELAGE) · airframe 39,664 hrs · 14,525 cycles

FUSELAGE EXTERNAL SKIN HAS CORROSION AROUND FASTENER HOLES TO FWD LEFT UPPER WING TO BODY FAIRING ATTACH PTS.

Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 39,605 hrs · 14,500 cycles

DOOR 1R DIFFICULT TO ARM. GALLEY DEBRIS IN GIRT AREA. GIRT BAR ATTACHMENT SYSTEM WAS CLEANED AND LUBED.

Part: STATIC INVERTER — OVERHEATED (FWD E/E BAY) · airframe 37,463 hrs · 13,723 cycles

STATIC INVERTER OVER-TEMPED IN FORWARD LOWER NOSE COMPARTMENT. STATIC INVERTER WAS REMOVED AND REPLACED. REMOVED UNIT SHIPPED TO MANUFACTURER TO DETERMINE ROOT CAUSE OF FAILURE.

Part: CONNECTOR — DAMAGED (BOOST PUMP) · airframe 37,463 hrs · 13,723 cycles

IN CRUISE AT FL 370 WITH 7.8 IN CENTER TANK RIGHT CENTER BOOST PUMP LOW PRESS EICAS CAME ON. THE CTR PMP LOW PRESS INDICATION OCCURED DUE TO LOSS OF PUMP POWER AS A RESULT OF A TRIPPED RT FUEL OVRD CIRCUIT BREAKER (C370). THE CAUSE OF THE TRIPPED BREAKER WAS TRACED TO AN ELECTRICAL SHORT OF CONNECTOR D40358J. FURTHER ANALYSIS OF THE CONNECTOR INDICATES THAT THE SHORT CIRCUIT CONDITION WAS A RESULT OF A DAMAGED CONTACT LOCKING MECHANISM WHICH CUT INTO THE CONNECTOR INSULATION & CONTACTED THE ADJACENT WIRE. REPLACED THE CONNECTOR AND SPLICED IN NEW WIRES PER STANDARD PRACTICES.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,664 hrs · 14,525 cycles

AFT CARGO PIT STA 1480 BETWEEN STR 25L AND 27L FRAME DENTED.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,664 hrs · 14,525 cycles

AFT CARGO PIT FRAME UPPER FLANGE DENTED AT BS 1420 STR 27L.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,664 hrs · 14,525 cycles

AFT PIT FRAME UPPER FLANGE DENTED AT BS 1460 STR 25L.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,664 hrs · 14,525 cycles

AFT PIT FRAME UPPER FLANGE DENTED AT BS 1400 STR 26L.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,664 hrs · 14,525 cycles

CABIN FLOORBEAM CAP AT STA 324 CORRODED FROM RBL 30 TO RBL 63.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,664 hrs · 14,525 cycles

FRAME AT STA 1520 AND STR 26L AND 25L IS DENTED.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,664 hrs · 14,525 cycles

FRAME AT STA 1500 AND STR 26L-25L IS DENTED.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 39,664 hrs · 14,525 cycles

AFT PIT STA 1560 STR 25L FRAME IS DAMAGED.

Part: SKIN — DENTED · airframe 34,061 hrs · 12,506 cycles

SCRAPE ON BOTTOM SURFACE OF RIGHT WING, 3 FEET INBD FROM TIP. FOUND DENT 3 BY 6 INCHES WITH DELAM. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED QUADRUPLER REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,073 hrs · 10,693 cycles

FUSELAGE DAMAGED STA 580 - 600, STR 16L-17L. MAJOR REPAIR ACCOMPLISHED. SPLICED STRINGER, INSTALLED NEW SHEAR TIE AND INSTALLED SKIN DOUBLER.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 28,115 hrs · 10,336 cycles

RIGHT WINDSHIELD OUTER PANE CRACKED. RIGHT WINDOW HEAT EICAS MESSAGE. *S/D* WINDOW FINDINGS: 1) SLIGHT MOISTURE INGRESSION ON UPPER BUS BAR BY SENSOR WIRES. 2) BUS BARS IN GOOD CONDITION, SLIGHT DISCOLORATION. 3) HUMP SEAL REPAIR HISTORY, MINIMAL EROSION, BUT IN GOOD CONDITION. 4) INTERLAYER LEAKAGE THROUGH CRACKS DUE TO WINDOW HEAT LEFT ON AFTER WINDOW FAILURE. CAUSE OF FAILURE WAS DETERMINED TO BE FOD. FOD WAS NOTED 2.5 INCHES FROM LOWER BUS BAR, 14 INCHES FROM FWD EDGE. BREAKAGE PATTERN FANNED OUT FROM FOD ORIGIN.

Part: APU — CONTAMINATED (AFT) · airframe 25,331 hrs · 9,326 cycles

RETURNED TO DEN UNDER AMBER ALERT DUE TO SMOKE IN THE CABIN AND COCKPIT. *S/D* APU HAD MASSIVE COOLING FAN FAILURE, METAL IN THE SYSTEM. OIL WAS SUCKED INTO THE APU INLET PLENUM THROUGH THE COOLING FAN DUCT CAUSING THE SMOKE IN THE CABIN. THE APU WILL BE DISASSEMBLED FOR OVERHAUL.

Part: APU — CONTAMINATED (AFT) · airframe 25,330 hrs · 9,325 cycles

AFT LAV SMOKE DETECTOR WENT OFF CLIMBING OUT OF DEN. SMOKE HAZE IN CABIN, RETURNED TO DENVER. *S/D* APU HAD MASSIVE COOLING FAN FAILURE, METAL IN THE SYSTEM. OIL WAS SUCKED INTO THE APU INLET PLENUM THROUGH THE COOLING FAN DUCT CAUSING THE SMOKE IN THE CABIN. THE APU WILL BE DISASSEMBLED FOR OVERHAUL.

Part: PUMP — LEAKING (LT HYD SYS)

LANDED AT PDX UNDER AN AMBER ALERT DUE TO LEFT HYDRAULIC SYSTEM LOSING FLUID. FOUND LEFT ACMP LEAKING. REPLACED PUMP.

Part: IDG — FAILED (LT ENGINE)

LEFT GENERATOR DRIVE OFF LIGHT ON DURING DEPARTURE. RETURNED TO FIELD. *S/D* THE INTEGRATED DRIVE GENERATOR HAD INTERNAL PISTON FAILURE. REPLACED LEFT (NR 1) INTEGRATED DRIVE GENERATOR.