N565UA

Part: LENS — CRACKED (EVAC SLIDE) · airframe 68,313 hrs · 25,182 cycles

RT OW BOTTLE GAUGLE LENS CRACKED. R & R RT OW SLIDE BOTTLE ASSEMBLY.

Part: SHUTOFF VALVE — INOPERATIVE (FUEL SYSTEM) · airframe 68,126 hrs · 25,124 cycles

RT FUEL SHUTOFF VALVE INOPERATIVE.

Part: CONDENSER — CRACKED (AC PACK) · airframe 68,015 hrs · 25,088 cycles

FOUND LT PACK AIR CONDITION COOLING PACK CONDENSER CRACKED 3.5 IN. LENGTH. REPLACED LT PACK CONDENSER IAW MM, OPERATIONS CHECKED GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (CABIN) · airframe 67,709 hrs · 24,988 cycles

SMOKE DECTECTOR CONTINUALLY SOUNDING. R & R SMOKE DETECTOR. CHECKED GOOD.

Part: CONTROL PANEL — INOPERATIVE (RUDDER TRIM) · airframe 67,612 hrs · 24,962 cycles

RUDDER TRIM FAILED TO TRIM IN RIGHT DIRECTION. UNABLE TO MOVE RUDDER TRIM TO THE NOSE RIGHT POSITION. REPLACED RUDDER TRIM ACTUATOR, STILL FAILS, DRIVES NOSE LT. RECHECKED WIRING FOUND POWER BAD ON RT TRIM COMMAND. REPLACED P8 CONTROL PANEL.

Part: CONNECTOR — SHORTED (EMERGENCY LIGHT) · airframe 67,405 hrs · 24,902 cycles

RIGHT FWD OVERWING EMERGENCY LIGHT INOPERATIVE. NO POWER TO TERMINALS AT LIGHT ASSY. FOUND CONNECTOR MISSING GROUND, CONNECTOR SHORTED TO GROUND. SECURED GROUND WIRE, OPS CHECKED OK IAW WDM 33-51-13.

Part: BLADE — DENTED (NR 2 ENGINE) · airframe 67,332 hrs · 24,879 cycles

NR 2 ENGINE, NR 12 BLADE DENTED. DRESSED DENT REF MM 72-31-02. DAMAGE WAS APPROX 3" FROM BLADE TIP.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 67,175 hrs · 24,832 cycles

EMERGENCY LIGHT CAP MISSING FROM END. REPLACED EMERGENCY LIGHT END CAP.

Part: CREASE BEAM — DAMAGED (BS 560) · airframe 66,551 hrs · 24,635 cycles

DURING EXT FUSELAGE REPAIR FROM BS 550- 630 FROM STR 13-20L. CREASE BEAM OTBD ANGEL AFT OF BS 560,STR 17L FOUND DAMAGED. ACCOMPLISHED SPLICE REPAIR ON CREASE BEAM PER ECRA 5330-04490 REV A. MAJOR REPAIR.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 66,551 hrs · 24,635 cycles

DENT FOUND ON DOUBLER BS 640 BELOW STR 18L WITH 2 SCRATCHES BELOW THE DENT. DENT WITHIN SRM LIMITS IAW MM. SCRATCHES BLENDED OUT, TREATED AND PRIMED REF 53-00-01. ACCOMPLISHED HFEC, AREA IS CRACK FREE AND WITHIN SRM 53-00-01, PG 103 LIMITS.

Part: SKIN — DENTED (BS 618 S18L) · airframe 66,551 hrs · 24,635 cycles

EXT FUSELAGE SKIN DENT ON PREVIOUS REPAIR DOUBLER AT BS 618 BELOW STR 18L. REPAIRED IAW ECRA5330-04490 REV A.

Part: SKIN — DAMAGED (BS 570) · airframe 66,551 hrs · 24,635 cycles

DAMAGE FOUND AT FASTENER HOLES OF BS 570 BETWEEN STR 18-19L, FABRICATED & INSTALLED REPAIR DOUBLER FROM BS 558-592, S18-21L IAW ECRA 5330-04490 REV A.

Part: STRINGER — DAMAGED (BS 560-580) · airframe 66,551 hrs · 24,635 cycles

STRINGER 18L UPPER FLANGE BETWEEN FRAMES 560L - 580L HAS HOLE. DAMAGE WAS REMOVED AND REPAIRED IAW SRM 53-00-03 REPAIR 3.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 66,551 hrs · 24,635 cycles

AFT CABIN BS 1640, LBL 2 - RBL 10 TOP OF FLOORBEAM HAS CORROSION. FABRICATED AND INSTALLED NEW FLOORBEAM UPPER TEE IAW EC-RA 5310-05536.

Part: CUSP WEB — CORRODED (BS 1020-1027) · corrosion level 2 · airframe 66,551 hrs · 24,635 cycles

MAIN CABIN, RT CUSP WEB CORRODED BS 1020 - 1027, RBL 65 - 69. FABRICATED NEW WEB IAW DWG 144N5140. INSTALLED WEB IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 324 RBL 50) · corrosion level 2 · airframe 66,551 hrs · 24,635 cycles

BS 324 FLOORBEAM TEE CAP CORRODED AT RBL 50. FABRICATED AND INSTALLED NEW TEE CAP AND SPLICE IAW SRM 53-10-08, REPAIR 1.

Part: FAN — NOISY (LEFT) · airframe 66,495 hrs · 24,616 cycles

LOUD NOISE FROM FRONT OF COCKPIT. INSTALLED RECIRC FAN PER MM. LEFT RECIRC, SOUNDS AND OPS CHECKED NORMAL

Part: SCUFF PLATE — CRACKED (R1 DOORWAY) · airframe 66,490 hrs · 24,614 cycles

R1 DOOR HAS A PRESSURE SQUEAL LOWER LEFT SIDE. FOUND R1 AFT LWR CORNER SCUFF PLATE CRACKED. WELD REPAIRED. SANDED AND BLENDED AREA PERFORMED LEAK CHECK NO LEAKS OR NOISE.

Part: WINDSHIELD — CRAZED (COCKPIT) · airframe 65,196 hrs · 24,163 cycles

CAPTAIN'S FIXED SIDE-AFT WINDOW'S VISIBILITY IS AFFECTED BY DEFECTS, REPLACE FIRST AVAILABLE. CREW COMMENTS: WINDOW 3L HAS MANY SCUFFS FROM JETWAYS CRAZING IN DIRECT SUN. NEEDS POLISHING OR REPLACEMENT. WINDOW CLEANED PER ECRA 5611-01100. WINDOW ASSY REPLACED PER MM.

Part: DRAIN LINE — CLOGGED (GALLEY) · airframe 65,142 hrs · 24,146 cycles

FIRST CLASS GALLEY DRAIN CLOGGED. CLEANED LINE - OPS OKAY.

Part: LATCH — DEFECTIVE (COCKPIT DOOR) · airframe 64,864 hrs · 24,057 cycles

COCKPIT DOOR TAKES EXCESSIVE FORCE TO CLOSE-LATCH AND STRIKE MECHANISM NOT RETRACTNG PROPERLY. REPLACED DOOR LATCH ASSY, OPS CHECKED OK.

Part: FLOAT VALVE — FAILED (FUEL TANK) · airframe 64,663 hrs · 23,985 cycles

CREW REPORTED A FUEL IMBALANCE BETWEEN LT AND RT MAINS. TROUBLESHOTING PER 3287 FIM. CENTER TANK LT VENT MANIFOLD DRAIN LEAKING. SEALED AS REQUIRED ALSO REPLACED THE LT MAIN FLOAT VALVE.

Part: IDG — FAILED (RT GENERATOR) · airframe 64,619 hrs · 23,968 cycles

CREW REPORTS RT ENG GENERATOR DRIVE LIGHT CAME ON IN FLT. CREW DISCONNECTED RT GENERATOR. REPLACED IDG PER MM.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 64,419 hrs · 23,893 cycles

RIGHT PACK TEMP CONTROLLER FAULTING RIGHT FLOW CONTROL VALVE. (PLACED IN COCKPIT) ATTEMPTED TO ACP HEALTH CHECK AMM 21-00-99, 601 BUT WAS UNABLE TO CLEAR MESSAGE. SWAPPED LEFT AND RIGHT TEMP CONTROLLERS AND MESSAGE SWAPPED. RETURNED CONTROLLERS TO ORIGINAL POSITIONS. WILL NEED NEW CONTROLLER MR 21656. REPLACED FLOW CONTROL VALVE PER MM. OPS CHECKS GOOD NO LEAKS NOTED. PACK FAULT MESSAGE CLEARED.

Part: CONTROLLER — FAULTY (AC BAY) · airframe 64,419 hrs · 23,893 cycles

RIGHT PACK ISSUE, FLIGHT DIVERTED. NOTICED RIGHT RAM AIR INLET DOOR CLOSED AND IRRATIC BEHAVIOR IN COCKPIT. BITE CHECK FAULTED PACK TEMP VALVE & PACK CONTROLLER. REPLACED PACK TEMP CONTROLLER REF MM 7 REPLACED PACK TEMP CONTROL VALVE. ALSO REPLACED RAM AIR INLET ACTUATOR.

Part: GATE — CRACKED (R1 DOOR) · airframe 63,411 hrs · 23,553 cycles

DOOR 1 RT UPPER GATE CRACKED TO FASTNER HOLE. DOOR REMOVED AND IN OUR SHOP. REMOVING GATE. DOOR SEAL WILL NEED REPLACEMENT ALSO. REPLACED GATE ASSY.

Part: ACTUATOR — MALFUNCTIONED (FUEL TRANSFER) · airframe 62,753 hrs · 23,318 cycles

UNWANTED FUEL TRANSFER FROM THE LT WING TO CTR TANK. WITH APU RUNNING AND APU FUEL PUMP ON, FUEL TRANSFERS FROM LT TO CENTER, WITH APU OFF, NO UNWANTED FUEL TRANSFER. UNABLE TO DUPLICATE. RAN APU, NO TRANSFER NOTED WITH OR WITHOUT APU RUNNING. UNWANTED FUEL TRANSFER INTO CTR TANK AT THE RATE OF 1K LBS PER MINUTE WITH ALL 3 FUELING SHUTOFF VALVES CLOSED AND FUELING MANIFOLD PRESSURIZED USING CENTER BOOST PUMPS AND TRANSFER VALVES OPEN. ACCOMPLISHED INTERNAL FUEL TANK STATIC CHECK, NO LEAKS FOUND, PRESSURE CHECKED FUELING MANIFOLD, OP'S CHECK FOUND LEAKAGE RATE 1,000 LBS PER MINUTE BOTH BY TANK TRANSFER AND TANKER TRUCK. FOUND BOTH LEFT AND RIGHT CENTER FUEL TANK FUELING SHUTOFF VALVE ACTUATORS SAFTEY WIRES CUT AND FUEL ENTER CENTER TANK WITH FUEL VALVES CLOSE 1,000 LBS PER MINUTE. RESAFETIED BOTH LT AND RT CENTER FUEL TANK SHUTOFF VALVE ACTUATORS.

Part: SWITCH — LOOSE (CABIN) · airframe 61,943 hrs · 22,997 cycles

EMER LIGHT SWITCH IS LOOSE. TIGHTENED LOCKING NUT ON EMER LIGHT SWITCH.

Part: FAN — FAILED (NR 1) · airframe 61,293 hrs · 22,769 cycles

FL340 FLT CREW NOTICED A STRONG ACRID SULPHURIC TYPE SMELL. FLT ATTDS CONTACTED AND THEY STATED SAME TYPE ODOR IN AFT CABIN AREA NOTICED BY FA'S AND PAX. NO MESSAGES DISPLAYED, NO SMOKE DETECTOR ALERTS. ONCE ON GROUND, PACK TURNED OFF, ODOR DISSIPATED. PACKS THEN TURNED BACK ON AND ODOR STARTED TO RETURN. EXTERIOR INSPECTED NO DAMAGE FOUND. FLT UNABLE TO CONTACT SAM. FOUND NR 1 EQPT COOLING FAN BLADES BINDING ON FAN CASE. REPLACED FAN & FWD COOLING FILTER & BOTH AIR DISTRIBUTION AIR CIRCULATION FILTERS ACCOMPLISHED PACK BURNOUT WITH ENGINES AT HIGH POWER IAW JRH REF MM. F/A REPORTED NO OVENS OPERATING AT THE TIME OF ODOR. NO VISIBLE SMOKE IN COCKPIT OR MAIN CABIN REPORTED. BLEED CONFIG WAS LT AND RT BLEEDS ISOLATED WITH LT AND RT PACKS ON IN AUTO AT TIME OF ODOR. NO LIGHTS FLICKERING REPORTED BY F/A. CREW UNABLE TO CONTACT SAM DUE TO PHONE & COMPUTER OUTAGE. REPLACED NR 1 FWD EQUIPMENT COOLING AIR FAN AND FAN FILTER, & RECIRC FILTERS.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,011 hrs · 22,666 cycles

CORROSION ON FRAME AT STA 1460 BETWEEN STR 16R AND 17R. MAJOR REPAIR ACCOMPLISHED: REPAIRED PER INSTRUCTIONS ON EA57-53-122 AND UA EVA 80836 WITHOUT DEVIATION. CF9044 CREATED FOR 24 MONTH DTA REQUIREMENT.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,011 hrs · 22,666 cycles

CORROSION ON AIRCRAFT SKIN JUST AFT OF BS 1620 BTWN STR 29 AND 30R. REPAIRED IAW EA PD57 -53-124 AND UA EVA 80852 WITHOUT DEVIATION.

Part: SKIN — CORRODED (FUSELAGE) · airframe 61,011 hrs · 22,666 cycles

AFT CABIN DECK SKIN UPPER SURFACE CORRODED STA 1690 TO 1710, RBL 50. MAJOR REPAIR ACCOMPLISHED: AFTER BLEND OUT FOUND SEVERAL AREAS OUT OF LIMITS PER SRM. A SRM DOUBLER RPR WAS INSTALLED PER INSTRUCTIONS ON EA PD57-53-120 WITHOUT DEVIATION. BOEING APPROVED THIS AS A PERMANENT REPAIR AND A FAA 8100-9 WAS RECEIVED DATED APR 27TH 2011.

Part: STRAP — CORRODED (FUSELAGE) · airframe 61,011 hrs · 22,666 cycles

DURING HMV VISIT CORROSION WAS FOUND AND REPAIRED AT BUTT SPLICE STRAP AT BS 1621 BETWEEN STR 29R AND STR 29L. THE FIRST STAGE FAA APPROVAL FOR THE REPAIR WAS RECEIVED. THIS REPAIR MUST RECEIVE A NEW FAA FORM 8100-9 SHOWING COMPLIANCE TO 14 CFR 25.571 AND 26.43(D) AND DTA INCORPORATED IN THE AIRCRAFT MAINT PROGRAM WITHIN 24 MONTHS FROM MAY 11TH 2011 TO REMAIN VALID AND AIRCRAFT TO REMAIN AIRWORTHY.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,011 hrs · 22,666 cycles

MAIN CABIN FLOOR BEAM CORRODED STA 324 RBL 37 TO RBL 60. MAJOR REPAIR PER INSTRUCTIONS ON EA PD 57-53-117 AND UA EVA 80825 WITHOUT DEVIATION.

Part: FLOORBEAM — CORRODED (BS 310) · airframe 61,011 hrs · 22,666 cycles

MAIN CABIN FLOORBEAM CORRODED STA 310, RBL 37 TO RBL 41. AFTER CORROSION REMOVAL FOUND T-CHORD TO BE OUT OF LIMITS PER SRM. A PERMANENT REPAIR WAS EXECUTED PER INSTRUCTIONS ON PEMCO PD57-53-121 WITHOUT DEVIATION AND APPROVED BY FAA 8100-9 DATED MAY 6 2011.

Part: FAILSAFE — DAMAGED (FUSELAGE) · airframe 61,011 hrs · 22,666 cycles

MAJOR REPAIR TO THE FAIL SAFE CHORD AT BS 1460 BETWEEN STR 16R AND STR 17R WAS ACCOMPLISHED DURING HMV AND RECEIVED FIRST STAGE APPROVAL FOR THE REPAIR WITHOUT DEVIATION. THE FAIL SAFE CHORD REPAIR MUST RECEIVE A NEW FAA FORM 8100-9 SHOWING COMPLIANCE TO 14 CFR 25.571 AND 26.43(D) AND DTA INCORPORATED IN THE AIRCRAFT MAINT PROGRAM WITHIN 24 MONTHS FROM MAY 5TH 2011 TO REMAIN VALID AND AIRCRAFT TO REMAIN AIRWORTHY.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 61,011 hrs · 22,666 cycles

CORROSION ON STRINGER SPLICE AT STR 29L, AFT OF STA 1460. MAJOR REPAIR ACCOMPLISHED: CLEANED AND PREPPED 2 AREAS ON HONEYCOMB TAIL CONE PANEL. BLIND FASTENERS ARE NOT AN APPROVED REPAIR FOR THIS AREA. FABRICATED AND BONDED 2 EA DOUBLERS AND BONDED IAW SRM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,011 hrs · 22,666 cycles

STATIC DISCHARGE IN SKIN. ACCOMPLISH INSPECTION OR RE-CHECK AS REQUIRED IN CF9040 STATIC DISCHARGE IN SKIN AT STA 490 BETWEEN STR 27L AND 28L. REMOVED SKIN DAMAGE BY DRILLING SKIN, ACP INSPECTION OF SKIN AND INSTALLED BLIND FASTENER. BLIND FASTENER NEEDS TO BE INSPECTED EVERY 2500 CYCLES AND REPLACED WITH A SOLID FASTENER BEFORE 12,000 C. REMOVED CHERRY MAC RIVET AT STA 490, BETWEEN STR'S 27R AND 28R PER SRM. ACCOMPLISHED NDT NO CRACKS DETECTED, INSTALLED SOLID FASTENER PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,011 hrs · 22,666 cycles

MAIN CABIN FLOORBEAM CORRODED STA 365.25 RBL 4 TO RBL 63. MAJOR REPAIR ACCOMPLISHED: FABRICATED AND INSTALLED FLOORBEAM T-CHORD PER SRM.

Part: NUT PLATE — DEFECTIVE (ADF ANTENNA) · airframe 61,011 hrs · 22,666 cycles

ADF ANTENNA REMOVED AND TWO BAD NUT PLATES REMOVED FROM AIRCRAFT STRUCTURE. ACCOMPLISHED CF9050 METER TWO BAD NUT PLATES REMOVED AND REPLACED IAW B757 SRM. RE-INSTALLED ADF ANTENNA IAW B757AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 60,708 hrs · 22,557 cycles

LEFT AFT OVERWING EMERGENCY LIGHT INOP. RELAMPED, OPERATIONAL CHECKED IS GOOD.

Part: WIRE — SHORTED (LANDING GEAR) · airframe 60,708 hrs · 22,557 cycles

C/B MLG ALT-EXT CONT. F5 POPPING. AFTER REPAIR ABOVE CB OKAY. DOOR OPENS FROM ALT EXTEND FROM COCKPIT BUT NOT FROM P72 ELEC SERVICE PANEL. SUSPECT BAD ARM SWITCH S10191 AT P72 PANEL. SECURED WIRE BUNDLE ABOVE AND OPS CHECKED COCKPIT ALT SWITCH AND ALL DOORS OPEN. NO PWR S10190 PIN 2 SAME AT S10370 SPLICES. S10370 IS OK. NO PWR D4037P PIN 25 WDM. FOUND NO DC VOLTS AT PINS 21 AND 25 ON CONNECTOR D40370J & NO DC VOLTS AT PIN 2 ON CONN D4360. FOUND 28 VDC ON PIN 28 CONN D40370J. TRACED PROBLEM TO CONNECTOR D42012P BEHIND E3-4 RACK 26230 REF WDM32-12-12. SECURED D42012P CONNECTOR & OPS CHECKED ALL MLG DOORS THRU 3 OPS OF OPENING & CLOSING, NO FAULTS NOTED.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 60,493 hrs · 22,481 cycles

FIRST OBS O2 MASK INOP. SUCCESSFULLY REPLACED THE LEAKING MASK. OPS NORMAL.

Part: FLOORBEAM — DAMAGED (BS 1681) · airframe 60,415 hrs · 22,455 cycles

FLOORBEAM, STA 1681 AT RBL 32 HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED REPAIRED IAW EVA UA-EVA-80549B.

Part: BEARING — WORN (R1 DOOR HANDLE) · airframe 60,415 hrs · 22,455 cycles

DOOR 1R EXT HANDLE HAD OVERTRAVEL, INTERNAL HANDLE NOT IN LOCK POSITION. REPLACED WORN STUB SHAFT (SLOTS WORN OUT), REPLACED BEARINGS AND ADJUSTED DOOR ON ROUTINE JIC 5R52I020, OPS CHECK GOOD.

Part: FLOORBEAM — CORRODED (BS 1640 BL 0) · airframe 60,415 hrs · 22,455 cycles

CABIN FLOORBEAM AT STA 1640 BL 0 UPPER FLANGE CORRODED. MAJOR REPAIR ACCOMPLISHED: REPAIRED PER SRM 53-00-51, REPAIR 3, AFTER CORROSION REMOVAL ON WU J1215S ITEMS 1,2,3,4.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 60,091 hrs · 22,338 cycles

CABIN COULDN'T KEEP UP ON DESCENT THRU CABIN ALT ABOUT 3000AGL AT GATE IT READS 100. REPLACED NR 2 CPC AND PRESSURIZATION & INDICATION WARNING MODULE. ACP CPC BITE FIM21-30-00. PRESSURIZED ACFT CABIN PRESS INDICATIONS NORMAL AND BITE CHECKED OK.

Part: SKIN — DELAMINATED (NR 6 SLAT) · airframe 59,647 hrs · 22,172 cycles

NR 6 L/E SLAT HAS UPPER SKIN & LOWER SKIN WITH DELAM AT PREVIOUSLY INSTALLED RIVET REPAIR AT APROX CTR OF SLAT DELAM IS 16 INCHES LONG ACROSS T/E AND EXTENDS 8 INCHES FWD FROM T/E. DELAM IS 3 INCHES FROM EDGE OF PREVIOUS BONDED REPAIR DELAM IAW SIDE APROX 120 INCH OUT OF LIMITS IAW SRM. MAX ALLOWED 1.5 INCH AND LOCATION IS NOT ALLOWED AS WELL. SLAT NR 6 INSTALLED IS PN 114N3002-120A, SN IS A2-575.

Part: SHUTOFF VALVE — INOPERATIVE (ENGINE) · airframe 58,783 hrs · 21,858 cycles

RT BLEED VALVE INOP, FLIGHT DIVERTED. FOUND THE PRSOV & REGULATOR TO BE DEFECTIVE. REPLACED NR 2 ENG PRSOV, PRSOV REGULATOR AND OVER TEMP LIMITING SENSOR. ACCOMPLISHED RUN OF ENGINES, BLEED SHIFT NORMAL. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (AFT LAV) · airframe 57,804 hrs · 21,487 cycles

AFT LAV EMERGENCY LIGHT STRIP INOP. REPLACED EMERGENCY LIGHT ASSY AND CKD OK.

Part: PANEL — CORRODED (CARGO BAY) · airframe 55,688 hrs · 20,672 cycles

AFT CARGO PIT FLOOR PANEL DAMAGED AND CORROSION ON UNDERLYING STRUCTURE. MAJOR REPAIR ACCOMPLISHED. FLOOR PANEL REMOVAL. CORROSION WAS NOTED AT THE SILL PLATE HAT CHANNEL EXTENDING THE WIDTH OF THE CARGO PIT ENTRY WAY. REMOVED AFT PIT UPPER SCUFF PLATE. ORDERED AND RECEIVED NEW SILL PLATE HAT CHANNEL (TRANSITION PANEL). INSTALLED PANEL AND UPPER SCUFF PLATE. WORKED ON W-U 30802. MANUFACTURING INTERCOSTAL, WORKING FLOORBOARD STR REPLACEMENT. LIGHT CORROSION ON 2ND INTERCOSTAL. EVALUATED SKIN, GOOD.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 55,066 hrs · 20,410 cycles

EICAS MSG CABIN ALT WARN AND CABIN AUTO INOP LITE ON. SELECTOR IN AUTO 2 SWITCHED TO AUTO 1 NO HELP OPERATING IN MAN OPBLM HANN SAMC TEXT: INFO FL250 CABIN PRESS DIFF 5.1 CAB ALT 8500 BOTH PACKS ON AUTO OUT FLOW VALVE CLSD DUCT PRESS 31 LT AND RT 40. REPLACED BOTH PRESSURE CONTROLLERS AND ACCOMPLISHED POST INSTALLATION TEST; PASSED. REPLACED OUTFLOW VALVE. ACCOMPLISHED POST INSTALLATION TEST, VALVE PASSED.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 55,066 hrs · 20,410 cycles

PRESSURIZATION PROBLEMS. FLIGHT DIVERTED. REPLACED BOTH CABIN PRESSURE CONTROLLERS. ACCOMPLISHED POST INSTALLATION TEST, PASSED.

Part: BATTERY — DISCHARGED (APU) · airframe 53,324 hrs · 19,741 cycles

APU WON`T START TRIED TWO TIMES. APU BATTERY ZERO VOLTS. REPLACED SHIP'S APU BATTERY. ALL START-RUN-CHARGE FUNCTIONS OKAY.

Part: BRACKET — OBSTRUCTED (R1 DOOR) · airframe 53,200 hrs · 19,695 cycles

DOOR 1R WILL NOT ARM OR DISARM PROPERLY. CLEANED DEBRIS FROM GIRT BAR BRACKETS. ARMED AND DISARMED NORMAL.

Part: BOTTLE — LOW PRESSURE (EVAC SLIDE) · airframe 50,147 hrs · 18,553 cycles

NR 2 RT MED SLIDE BOTTLE PRESSURE READING AT LOW PRESSURE EDGE OF GREEN BAND AFTER CONSTANT FOR MORE THAN 2 HRS.

Part: CABLE — DISCONNECTED (ESCAPE SLIDE) · airframe 49,685 hrs · 18,380 cycles

RIGHT OVERWING EVACUATION SLIDE RELEASE CABLE FOUND DISCONNECTED FROM QUICK RELEASE PIN.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,478 hrs · 18,310 cycles

EXTERIOR EMERGENCY LIGHT INOP AT DOORS 1L & 4R. RELAMPED EXTERIOR EMERGENCY LIGHT AT DOOR 1L & 4R.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,179 hrs · 18,206 cycles

MOST FWD EEL LIGHT IN 1ST CLASS CABIN IS INOPERATIVE. REPLACED LIGHT SEGMENT.

Part: SWITCH — FAULTY (FIRE WARNING SYS) · airframe 49,163 hrs · 18,199 cycles

CARGO FIRE SYSTEM FAIL LIGHT ON PED SEEMS INCORRECT. [08-08-07] REPLACED KORRY SWITCH IN FIRE TEST PANEL, AND OPS CHECKED NORMAL.

Part: PROXIMITY SWITCH — FAULTY (L1 DOOR) · airframe 49,031 hrs · 18,155 cycles

DOOR 1R "SLIDE" LIGHT REMAINS DIMLY ILLUMINATED AT ALL TIMES. [08-08-07] REPLACED BOTH GIRT BAR PROXIMITY SWITCHES.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,997 hrs · 18,147 cycles

R-4 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. *S/D* REPLACED LAMP. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,997 hrs · 18,147 cycles

EMERGENCY LIGHT INOP IN OVERHEAD PANEL SEAT 6AB. *S/D* REPLACED EMERGENCY LIGHT IN OVERHEAD PANEL AT SEAT 6AB PER MM 33-51-01, PERFORMED OPS CHECK, CHECK OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,997 hrs · 18,147 cycles

EMERGENCY LIGHT ON AFT CARGO DOOR INOPERATIVE. *S/D* REPLACED LAMP, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 48,997 hrs · 18,147 cycles

LEFT OVERWING EXTERNAL AFT EMERGENCY LIGHT INOP. [06-22-07] REPLACED LAMP. OPS CK GOOD.

Part: ACTUATOR — MALFUNCTIONED (RUDDER TRIM) · airframe 48,623 hrs · 18,004 cycles

RUDDER TRIM FAILED TO TRIM IN LEFT DIRECTION. [SUP 06-06-07] DURING DESCENT STARTED TO WORK ERRATICALLY IN ONE DIRECTION. BY THE TIME IT ARRIVED AT GATE, IT OPERATED NORMALLY. REPLACED RUDDER TRIM ACTUATOR. ACCOMPLISHED INSPECTION OF RUDDER TRIM ACTUATOR INSTALLATION.

Part: TRIM SYSTEM — MALFUNCTIONED (RUDDER) · airframe 47,400 hrs

RUDDER TRIM INOP NEAR TOP OF CLIMB, THEN WORKED OK. REPLACED RUDDER TRIM FEEL CENTERING TRIM ACTUATOR.

Part: WARNING MESSAGE — ILLUMINATED · airframe 47,291 hrs · 17,499 cycles

DUE TO MASTER WARNING ABORTED TAKEOFF AT 100 KNOTS. LEFT ENGINE GENERATOR DROPPED OFF LINE ON REJECTED TAKE-OFF. REPLACED IDG,

Part: APU — FAILED (APU BAY) · airframe 45,965 hrs · 16,996 cycles

FLIGHT DIVERTED - APU OIL QTY STATUS MESSAGE. APU FAILED.

Part: FLUID — LEAKING (APU) · airframe 45,965 hrs · 16,996 cycles

FOUND LOSS OF APU OIL QTY AND AN INOPERATIVE GENERATOR.

Part: ENGINE — SMOKE (NR 1) · airframe 42,789 hrs · 15,852 cycles

OBSERVED SMOKE FROM BOTTOM OF NR 1 ENGINE COWLING ON TAXI INTO ORD. LINE MAINTENANCE DETERMINED THAT HYDRAULIC FLUID WAS LEAKING FROM A LOOSE B-NUT. B-NUT WAS TIGHTENED AND SYSTEM WAS CHECKED. NO OTHER LEAKS NOTED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,716 hrs · 14,667 cycles

SKIN, BS 580 S-15L TO S-18L IS DAMAGED. ACCOMPLISHED PARTIAL SKIN REPLACEMENT WITH SKIN DOUBLER SPLICES AND TRIPLER SPLICES. ACCOMPLISHED STRINGER REPAIR USING STRINGER SPLICES.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,716 hrs · 14,667 cycles

FUSELAGE SKIN DENTED AT BS 780 AND STR 17L. DOUBLER-TRIPLER REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,716 hrs · 14,667 cycles

EXTERNAL FUSELAGE SKIN EXPERIENCED DAMAGE FROM JETWAY OPERATION CAUSING DENTS AT STA 600-620 BETWEEN STR 15 LT AND 17 LT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER - TRIPLER REPAIR.

Part: SKIN — DAMAGED (PYLON) · airframe 39,716 hrs · 14,667 cycles

NR 2 PYLON EXISTING FASTENER HOLES IN THE RT AND LT FWD PYLON SKINS ARE LARGER THAN ALLOWABLE LIMITS. *S/D* REPAIRED OVERSIZED HOLES WITH FREEZE PLUG REPAIRS.

Part: SKIN — DENTED (FUSELAGE) · airframe 39,716 hrs · 14,667 cycles

EXTERIOR FUSELAGE AT BS 760, STR 16L, SKIN DENTED OUT OF LIMITS 2 PLACES. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER - TRIPLER REPAIR.

Part: SKIN — DAMAGED (PYLON) · airframe 39,716 hrs · 14,667 cycles

EXISTING FASTENER HOLES IN THE NR 1 RT AND LT FWD PYLON SIDE SKINS ARE LARGER THAN ALLOWABLE LIMITS. REPAIRED OVERSIZED HOLES WITH FREEZE PLUG REPAIRS.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 39,716 hrs · 14,667 cycles

FUSELAGE STRINGER REPAIR SPLICE AT BS 570, STR 16L REQUIRES REPLACEMENT AND REPOSITIONING DUE TO SKIN SPLICE REPAIR AND SHARING OF COMMON FASTENERS. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW STRINGER SPLICE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,716 hrs · 14,667 cycles

FRAME IS DENTED AT BS 1560, LBL 8, UNDER THE CARGO FLOOR, ON THE UPPER FLANGE. MAJOR REPAIR ACCOMPLISHED. FRAME REPAIRED WITH NESTED J-ANGLE.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,716 hrs · 14,667 cycles

AFT PIT FRAME DENTED BS 1420 AT STR 26L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME UPPER FLANGE WITH NESTED J-ANGLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,716 hrs · 14,667 cycles

STATION 1640 FLOORBEAM CORRODED, RBL 54, AFT OF GALLEY MOUNT. MAJOR REPAIR ACCOMPLISHED. FLOORBEAM WAS REPAIRED WITH U-CHANNEL ANGLE SPLICE REPAIR AND MODIFIED INTERCOSTAL.

Part: SILL — CRACKED (FUSELAGE) · airframe 39,716 hrs · 14,667 cycles

AFT CABIN AT BS 1681, RBL 55, THE R4 DOOR LOWER SILL WAS FOUND CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED DOOR SILL AT R-4 DOOR WITH A DOUBLER.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,716 hrs · 14,667 cycles

AFT PIT FRAME DENTED, BS 1440 IS DENTED 2 PLACES BETWEEN STR 25L AND STR 26L ON INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME WITH NESTED J-ANGLE.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,716 hrs · 14,667 cycles

AFT PIT FRAME DENTED AT BS 1460 BETWEEN STR 25L TO STR 26L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME WITH NESTED J-ANGLE REPAIR.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 39,716 hrs · 14,667 cycles

BS 620 STRINGER 16L HAS OVERSIZED HOLES. MAJOR REPAIR ACCOMPLISHED. REPAIRED STRINGER WITH NEW STRINGER SPLICE SECTION AND REINSTALLED 3 EACH SHEAR TIES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,716 hrs · 14,667 cycles

CABIN FLOORBEAM UPPER CHORD CORRODED AT STA 1640 RBL 52. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR CHORD.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 39,716 hrs · 14,667 cycles

LEFT HAND CREASE BEAM HAS A LARGE AREA OF CORROSION AT BS 686, JUST FORWARD OF THE L2 CABIN DOOR. MAJOR REPAIR ACCOMPLISHED. REPLACED CHORD ANGLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,716 hrs · 14,667 cycles

CABIN FLOORBEAM UPPER CHORD SURFACE CORRODED AT BS 1660 RBL 54. MAJOR REPAIR ACCOMPLISHED. INSTALLED REINFORCING ANGLE REPAIR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 39,716 hrs · 14,667 cycles

CREASE BEAM WEB CORRODED ON UPPER SURFACE STA 1406 TO 1413. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM WEB.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,502 hrs · 13,892 cycles

CABIN FLOORBEAM 365 AT RBL 10 TO RBL 45.5 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. CORROSION WAS REMOVED AND FLOORBEAM WAS REPAIRED.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,502 hrs · 13,892 cycles

BODY STATION 588 TO 624 STR 15L TO 17L HAS A DOUBLER INSTALLED WITH DENTS NEXT TO IT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: SKIN — CRACKED · airframe 33,650 hrs · 12,398 cycles

2 CRACKS AT FWD SIDE OF LH FUSELAGE BETWEEN WINDOWS 10 AND 11. FIRST CRACK IS ABOVE ORANGE PAINT STRIPE ABOUT 10 INCHES AND IS ABOUT ONE TO ONE-AND-A-HALF INCHES LONG. THE AFT CRACK IS AT THE TOP PORTION OF THE ORANGE PAINT STRIPE JUST AFT OF PATCH LOWER AFT CORNER ABOUT ONE INCH LONG. MAJOR REPAIR ACCOMPLISHED. SKIN DOUBLERS INSTALLED.

Part: INDICATOR — FAILED (HYD PUMP) · airframe 33,599 hrs · 12,379 cycles

RIGHT HYDRAULIC SYSTEM SHOWED EMPTY. DIFFERENTIAL PRESSURE INDICATOR (DPI) ON RT ENGINE DRIVEN PUMP HYDRAULIC PRESSURE MODULE FAILED. REPLACED DPI, EDP AND FILTER MODULE.

Part: CONTROL UNIT — MALFUNCTIONED (RUDDER) · airframe 31,210 hrs · 11,478 cycles

RUDDER REQUIRES 6 UNITS OF LEFT TRIM. ACCOMPLISHED TROUBLESHOOTING OF RUDDER TRIM AND RUDDER RATIO SYSTEMS AND EXAMINED RATIO CHANGER SHEAR PINS. NO DISCREPANCIES FOUND, AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER GRIPES ABOUT EXCESSIVE TRIM REQUIRED.

Part: CONTROLLER — DEFECTIVE (BLEED AIR) · airframe 29,067 hrs · 10,710 cycles

RIGHT DUCT PRESSURE FLUCTUATING BETWEEN 25 PSI AND 40 PSI. EPR FLUCTUATES BETWEEN 1.16 AND 1.28 FL410. *S/D* REPLACED THE RT PRSOV AND PRSOV CONTROLLER. PROBLEM WAS MOST LIKELY CAUSED BY THE PRSOV CONTROLLER.

Part: BEARING — FAILED (LT ENGINE) · airframe 28,299 hrs · 10,438 cycles

LEFT OIL FILTER EICAS MESSAGE. SHUTDOWN LEFT ENGINE. *S/D* FOUND FAILED BUMPER BEARING DUE TO ONE ROLLER ROTATING 90 DEG IN THE CAGE. THIS CAUSED THE ROLLER TO SKID AND THE BEARING TO FAIL.

Part: SWITCH — FAILED (CARGO DOOR)

UPON ARRIVAL AT GATE, UNCOMMANDED FWD CARGO DOOR OPENING WHEN GROUND POWER BUS ENERGIZED. *S/D* FWD CARGO DOOR CONTROL SWITCH WAS FOUND STUCK IN OPEN POSITION. SWITCH WAS REPLACED.

Part: LIGHT STRIP — INOPERATIVE (CABIN)

EMERGENCY ESCAPE LIGHT FORWARD OF MID LAVATORY INOP. REPLACED EMERGENCY ESCAPE LIGHT STRIP, OPERATION CHECKS NORMAL.

Part: PMA SHAFT — FAILED (NR 2 ALTERNATOR)

NR TWO ENGINE SHUT DOWN IN FLIGHT WITH NO INDICATION OF IMPENDING FAILURE. SUPPLEMENTAL DATA UPDATE. THE IN-FLIGHT SHUT DOWN DUE TO THE FAILURE OF THE PERMANENT MAGNET ALTERNATOR DRIVESHAFT. PRELIMINARY INVESTIGATION OF THE SHAFT FAILURE INDICATED THE SHAFT FRACTURED TRANSVERSELY THROUGH THE .031 INCH DIAMETER STUD SECTION. FURTHER INVESTIGATION BY PRATT & WHITNEY AND FIAT INDICATE THE FRACTURE WAS THE RESULT OF HIGH CYCLE FATIGUE (HCF). THE EXACT CAUSE OF THE ORGIN OF HCF IS STILL UNDER INVESTIGATION. PART TOTAL CYCLES, 6,178.

Part: EEL — INOPERATIVE (CABIN)

RIGHT FORWARD EMERGENCY OVERWING LIGHT INOP. RELAMPED, OPS CHECKS OK.