N577UA

Part: CONNECTOR — CORRODED (NR 1 VHF) · airframe 63,992 hrs · 22,594 cycles

NR 1 VHF HAS INTERMITTENT SHORT BURSTS OF STATIC. SOME JUST SECONDS APART. REMOVED ANTENNA CONNECTOR WAS VERY CORRODED BUT ANTENNA CABLE AND CONNECTOR CLEANED OK WITH NO CORROSION. TESTED CHF COMM L-C & R PER MM. THEN TESTED ACARS PER MM. C VHF ANTENNA REPLACED BECAUSE STATIC PROBABLY WAS COMING FROM ACARS TRANSMISSION FROM C VHF.

Part: INLET — GOUGED (NR 1 NACELLE) · airframe 63,347 hrs · 22,377 cycles

NR 1 ENGINE NACELLE HAS A DENT IN THE INLET COWL LOCATED AT THE 12:00 POSITION, DENT IS IN THE LIP, SKIN PORTION OF THE INLET COWL. DENT DIMENSIONS REPORTED TO BE 3.5 INCHES (LENGTH) BY 0.875 INCHES (WIDTH) BY .0625 INCHES DEEP DOES NOT MEET THE A OVER Y CRITERIA OF SRM 54-11-01. REPLACED INLET COWL IAW MM 71-11-01 AND PL314N3080 REV N.

Part: RUDDER CONTROL — MALFUNCTIONED · airframe 63,068 hrs · 22,286 cycles

EICAS MESSAGE 'RUDDER RATIO' DISPLAYED, RUDDER RATIO LIGHT ILLUMINATED ON GROUND. RUDDER RATIO LIGHT ON TAKEOFF ROLL AND IN FLIGHT CROSS WIND LIMITED TO 15 KNOTS. REPLACED RUDDER RATIO CHANGER.

Part: SWITCH — FAULTY (WINDOW HEAT) · airframe 62,353 hrs · 22,031 cycles

LEFT SIDE WINDOW HEAT INOPERATIVE. DF AS PER 3141J, SUSPECT SWITCH. REPLACED SWITCH, OPS NORMAL AND TEST OKAY.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 62,275 hrs · 22,005 cycles

A/C NOISE VERY LOUD EVEN WITH RT RECIRC FAN OFF WITH ALL VENTS OPEN. CHK'D FLIGHT DECK NOISE LEVEL PER SVC TIP 21-22-00 & FOUND DB LEVEL TO MEASURE AT 79, 70.5 IS LIMIT. CONFIRMED PACKS ARE NOT STUCK IN HI FLOW PER REF'D SVC TIP METHOD 2. REPLACED LT PACK FLOW CONTROL & SHUTOFF VALVE IAW MM. CHECKS GOOD IAW SERVICE TIP MM.

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 61,959 hrs · 21,885 cycles

RT ENG COMPRESSOR STALL, RTFL. RIGHT ENGINE HAD COMPRESSOR STALL DURING T-O CLIMB AND LANDING (REVERSE) SAMC TEXT: ESN 726514. CHECK PER FIM. SEAMM REPORTS DURING HPC BORESCOPE EXTENSIVE DAMAGE TO HPC-6 (1EA. HALF THE BLADE MISSING AND DAMAGE TO SUBSEQUENT STAGES ALL THE WAY TO HPC-17 HAVE INPACT DAMAGE). RPL'D ENG 726514 WITH ENG 717981. NR 2 ENG NOSE COWL AFT MATING SURFACE AT THE 6 O'CLOCK POS HAS HONEYCOMB DAMAGE. IT IS CRACKED IN SEVERAL PLACES AND PARTS ARE BROKEN FREE. RPL'D PER MM.

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 61,959 hrs · 21,885 cycles

AIR RETURN DUE TO RIGHT ENGINE COMPRESSOR STALL DURING TAKE OFF, CLIMB AND LANDING. CHECKED PER MM. REPLACED ENGINE.

Part: POWER CABLE — BURNED (CABIN) · airframe 61,676 hrs · 21,780 cycles

PC POWER CABLE FROM SIDEWALL TO SEAT 1CD BURNT AT SEAT CONNECTION, BREAKERS POPPED AT P37 PNL. WALL TO SEAT CABLE AND JUNCTION BOX DAMAGED. NIS SEA. INOPED PER MEL. NOTE: SEATS DO NOT HAVE PC JACKS INSTALLED THIS AC. BREAKERS PULLED AND CAPPED. REPLACED JUCTION BOX, NEEDS CABLE ASSY. REPLACED CABLE, 021-1162. REVERSED MEL. APPLIED POWER AND NO CIRCUIT BREAKER POPPED.

Part: LIFE VEST — MISSING (CABIN) · airframe 61,381 hrs · 21,669 cycles

OBSERVER LIFE VEST IS MISSING. SEAT TO BE RENDERED INOP UNTIL LIFE VEST REPLACED. DEFERRED PER SAMC. REPLACED OBSERVER LIFE VEST.

Part: SEAL — DAMAGED (R1 DOOR) · airframe 61,086 hrs · 21,560 cycles

CREW REPORT: VERY LOAD SQUEAL FROM DOOR 1R ON CLIMB BETWEEN 15K & FL30K. NOISE ON LOWER RT SIDE. REPAIRING REN ON LOWER RT CORNER, NEED TO SMOOTH OUT REN AND CHECK. REMOVED EXCESSIVE SEALANT, CONTOURED REN APPLICATION, LEAK SLOWED BUT STILL PRESENT. TRIMMED REN ON LOWER CORNER, NO HELP. PRESSURIZED TWICE AND FOUND CENTER OF LOWER FLAPSEAL WITH A HOLE IN IT. SEALED FLAPSEAL

Part: PBE — OUT OF TOLERANCE (COCKPIT) · airframe 60,830 hrs · 21,473 cycles

FLIGHT DECK PBE POUCH IS SOFT. REPLACED PBE.

Part: PSEU — UNKNOWN (MLG) · airframe 60,714 hrs · 21,431 cycles

LANDING GEAR STATUS MSG ON LANDING. NO FAULTS FOUND, REPLACED PSEU PER MM. BITE NORMAL.

Part: AILERON — OUT OF ADJUST (WING) · airframe 60,701 hrs · 21,425 cycles

LATERAL TRIM OUT OF LIMITS AT 350 F0 1.8R, 250 F0 1.0R 180 F5 0.5R, 160 F20 0, 140 F25 0.2R, 130 F30 0. ADJUSTED THE FLAP SHIMS AND SPOILER GAPS PER MM. CREW REPORTS LATERAL TRIM AT FLAPS 20 AND 25 IS OUT OF LIMITS. WITH RUDDER SET AT ZERO THE REQUIRED LATERAL TRIM IS .5 RWD 350, 0.3 RWD AT 250, 0.2 LWD AT 180 - FLAPS 5, 0.8 LWD 140 FLAPS 25 GEAR DOWN AND ZERO 130 - FLAPS 30 GEAR DOWN. ADJUSTED LATERAL TRIM IAW B757-200 AMM. DURING TEST FLIGHT FOUND OUT OF LIMITS. 130 F30 .8L, 140 F25 1.4L, 160 F20 1.1L, 180 F5 .9L, 250 F0 .6L 350 F0 .3L ALL POINTS BALANCED FUEL AND RUDDER TRIM 0. ADJUSTED LATERAL TRIM AND ADJUSTED LT AILERON PER MM. ADDED .097 SHIMS TO THE LT INBD & OTBD POSITIONS PER MM AND ADJUSTED LT AILERON PCA PER MM.

Part: SKIN — DENTED (BS 458 S17L) · airframe 60,697 hrs · 21,421 cycles

DENT AT BS 458 AT S-17L. MAJOR REPAIR. REPAIRED DENT IAW EA PD57-53-147 AND EVA 81000.

Part: CREASE BEAM — CORRODED (BS 1120-1140) · airframe 60,697 hrs · 21,421 cycles

CORROSION ON CREASE BEAM WEB AT STA 1120 - 1140. MAJOR REPAIR ACCOMLISHED: REMOVED WEB AND FABRICATED A REPLACEMENT. TREATED, PRIMED AND TOPCOATED AND INSTALLED NEW WEB IAW SRM.

Part: CREASE BEAM — CORRODED (BS 1580-1600 LBL) · airframe 60,697 hrs · 21,421 cycles

CORROSION CREASEBEAM INNER CHORD BETWEEN BS 1580-1600 AT LBL 60. MAJOR REPAIR ACCOMPLISHED: REPAIRED CREASE BEAM INNER CHORD BETWEEN PER EA PD 57-53-149. MINOR REPAIR

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,697 hrs · 21,421 cycles

CORROSION ON FLOORBEAM AT BS 324 RBL 35-58 IN MAIN CABIN (N-R 2775N00263). MAJOR REPAIR ACCOMPLISHED: REPAIRED PER INSTRUCTIONS PROVIDED IN EA PD57-53-146 AND EVA 81001 WITHOUT DEVIATIONS.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 60,697 hrs · 21,421 cycles

CORROSION ON PRODUCTION SPLICE AT BS 1460 S-28L. (N-R 2775N00421). MAJOR REPAIR ACCOMPLISHED: FABBED AND INSTALLED STR SPLICE AND ATTACH CLIP AT STA 1460, S28L PER SRM ON PEMCO NR 2775N00421.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 60,697 hrs · 21,421 cycles

CORROSION ON DOUBLER ON AFT PRESSURE DECK BS 1681 RBL 5-40 MAIN CABIN (N-R 2775N00390). MAJOR REPAIR ACCOMPLISHED: REPLACED DOUBLER SAME SIZE AND SHAPE PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,697 hrs · 21,421 cycles

CORROSION ON FLOORBEAM AT BS 365.25 RBL 0 - RBL 58 MAIN CABIN (N-R 2775N00239). MAJOR REPAIR ACCOMPLISHED: FABBED T-CHORD, STRAPS, ANGLES, SHIMS AND INTERCOSTALS. INSTALLED T-CHORD, ANGLES AND STRAPS STA 365, RBL 0 - RBL 58. INSTALLED INTERCOSTALS STA 345 - 365, RBL 24 AND RBL 55 PER SRM ON NR 2775N00239.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,697 hrs · 21,421 cycles

CORROSION ON FLOORBEAM AT BS 1640 FROM LBL 5 -RBL 58. (N-R 775N00395) MAJOR REPAIR ACCOMPLISHED: REMOVED OLD REPAIR, FABBED AND INSTALLED T-CHORD AT STA 1640, LBL 5 - RBL 58 PER SRM ON PEMCO NR 2775N00395.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 60,697 hrs · 21,421 cycles

FLOORBEAM AT BS 660 HAS TOOLING MARK AT RBL 37-41.5 (N-R 2775N00559). MAJOR REPAIR ACCOMPLISHED: FABBED AND INSTALLED SUPPORT BEAM, ANGLES AND STRAPS AT STA 660, RBL 35 - 51 PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,697 hrs · 21,421 cycles

CORROSION ON LOWER PART FLOORBEAM AT BS 345 RBL 58 RBL 12 (N-R 2775N00237). MAJOR REPAIR ACCOMPLISHED: REMOVED AND REPLACED STA 345 FLOORBEAM RBL 8 - RBL 60 USING BAC 1505-100880 7075-T6 IAW B757 SRM. REPAIR ANGLES FROM PO 1061690. INSTALLED REPAIR PER B757 SRM.

Part: SKIN — CORRODED (BS 1681-1691) · airframe 60,697 hrs · 21,421 cycles

CORROSION AT BS 1681-1691 AT RBL. FABRICATED DOUBLER IAW SRM AND PWIT1422. TREATED AND PRIMED DOUBLER PER SRM AND RESTORED FINISH IAW AMM.

Part: SKIN — DENTED (BS 430 S17L) · airframe 60,697 hrs · 21,421 cycles

SKIN DENT AT BS 430 AT S-17L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED AREA AND INSTALLED A .063 INCH DOUBLER IAW SRM. IDENTIFIED REPAIR IAW GNMM.

Part: SKIN — DENTED (CARGO DOOR) · airframe 60,697 hrs · 21,421 cycles

FWD CARGO DOOR DENT AFT EDGE OF DOOR, APPROX 4\ FWD OF AFT EDGE, CTR OF DOOR. DENT IS 1.25 X 1.25 X .046 DEPTH. FOUND IT OUT OF LIMITS PER SRM. DENT LESS THAN 10" FROM NEAREST CUTOUT. REMOVED DAMAGE. FABRICATED & INSTALLED FLUSH DOUBLER REPAIR.

Part: INDICATOR — FAULTY (RUDDER TRIM) · airframe 60,309 hrs · 21,276 cycles

EXCESSIVE RUDDER TRIM. ACCOMPLISHED UP TO BLOCK 7 RUDDER RIG HIGH AND LOW SPEED GOOD. NEED TO CONTINUE BLOCK 8 PG 116 CHECK THERMAL COMPENSATION. BOTTOM CLEARANCE .080 TOP CLEARANCE .100. WILL NEED TO BE ADJUSTED TO PROPER CLEARANCES. THERMAL COMP LINKAGE PER AMM. OPERATION NORMAL. REPLACED RUDDER TRIM INDICATOR PER MM. CONFERRED WITH OPBLM. NO TEST FLIGHT REQUIRED.

Part: CONTROL VALVE — DEFECTIVE (CABIN TEMP) · airframe 60,079 hrs · 21,189 cycles

COCKPIT AIR NOISE EXCESSIVE. DUCT CLEAN UP IS DONE, PREP TO ACP ENG RUN TO CHECK DUCT PRESS AND DECIBLE READINGS. COMPLETED NOISE CHECK WITH METER WITH ENGINE RUNNING. DUCT PRESSURE WAS AT 12 PSI. 76 DECIBELS WITH RIGHT RECIRCULATION FAN OFF, 79 DECIBELS WITH FAN ON. RESTRICTOR PLATE IS INSTALLED, AIRFLOW IS DIMINSHED IN THE BACK HALF OF ECONOMY AREA IAW CH1625. CLEANED DUCTS DECIBEL READINGS 73 RT FAN ON 71 RT FAN OFF WITH BOTH ENGINES RUNNING WITHIN LIMITS. FWD CABIN TEMP CONTROL VLV BAD. REPLACED FWD CABIN TEMP CONTROL VALVE PER MM, OPS CHECK GOOD, NO LEAKS NOTED.

Part: RADIO ALTIMETER — FAULTY (LEFT) · airframe 60,004 hrs · 21,167 cycles

WHEN THRUST IDLE IN DESCENT EICAS GEAR NOT DOWN CAME ON L RA YELLOW BOX FLASHING ON AND OFF. REPLACED LEFT RADIO ALTIMETER IAW MM. LANDING CONFIG SYS TEST CHECKED OKAY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 58,950 hrs · 20,799 cycles

EMERGENCY EXIT EXTERIOR LIGHT INOP AT 2 LT MED, 4 RT MED AND AFT LT OVERWING. REPLACED LAMP, OPS GOOD.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 58,950 hrs · 20,799 cycles

F/O O2 MASK HARNESS LEAKS. REPLACED FIRST OFFICERS OXYGEN MASK ASSEMBLY. OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,997 hrs · 20,436 cycles

L2 DOOR EMERGENCY LIGHT INOPERATIVE (EXTERNAL). RELAMPED, OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,997 hrs · 20,436 cycles

L3 DOOR (EXTERIOR) EMERGENCY LIGHT INOPERATIVE. RELAMPED, OPS CHECKED GOOD.

Part: CONTROLLER — FAULTY (COCKPIT TEMP) · airframe 57,912 hrs · 20,405 cycles

COCKPIT TEMP STILL UNCONTROLLABLE OVER 91 DEGREES IN AUTO. SUPPLEMENTAL DATA UPDATE WORKING WITH LM5719, REPLACED RT PACK TEMP CONTROLLER. DURING BITE TEST OF USING THE AIR COND ZONE TEMP WE GOT A FLT DECK SELECTOR MSG. CHANGED THAT. NOW WE NOTICE THAT WE HAD THE FLT DECK AND FWD CABIN SEL INOP LITES ON IN THE OVERHEAD COCKPIT. WE NOTICED AS WELL THE TRIM VALVES WERE NOT MOVING ON THE ECS PAGE. THEN WE NOTICED WE ALSO HAD THE LT PACK BITE MSG ON THE LOWER EICAS. WE STOPPED THERE. REPLACED RT PACK TEMP CONTROLLER. REPLACED LT PACK RAM AIR INLET DOOR ACTUATOR. REPLACED FLIGHT DECK OVERHEAD TEMP SELECTOR, WIRING CHECKS SHOWED NO FAULTS, RAM AIR TEST SHOWED NO FAULTS, TEMP CONTROL SYS OPS CK OK WITH ENGINES AS SOURCE AND WITH APU. TRIM AIR VALVE SYS TESTS OK.

Part: LATCH — FAILED (LIFE RAFT) · airframe 57,323 hrs · 20,186 cycles

AFT LIFE RAFT IN OVERHEAD AISLE, DOOR LATCH NOT HOLDING. REMOVED RAFT. INSTALLED NEW BASE ASSEMBLY ON RIGHT SIDE. REPLACED SPRING ACTUATORS CMPT. OPS CK OKAY. INSTALLED RAFT.

Part: FRAME — DELAMINATED (LT WING AILERON) · airframe 56,751 hrs · 19,980 cycles

LEFT WING AILERON, OTBD MOST, LOWER TRAILING EDGE, HAS SKIN DELAMINATING. CONDUCTIVE FRAME IS DELAMINATING FROM LOWER SURFACE OF AILERON, REMOVED ENTIRE CONDUCTIVE FRAME. MFG NEW FRAME REF UA-EVA. ACCOMPLISHED ITEM 2 AND 3 IAW EVA 73687. REPLACED FRAME AT HMV NR 3.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,062 hrs · 19,731 cycles

FOUND EMERGENCY EGRESS LIGHTING OUT AT FWD MID LAV DOOR. REPLACED EMERGENCY EGRESS LIGHTING STRIP IN FRONT OF MID LAV DOOR.

Part: OVEN — ODOR (GALLEY) · airframe 55,885 hrs · 19,675 cycles

CREW REPORTED OVEN NR 010 FIRST CLASS GALLEY. ELECTRICAL ODOR. REMOVED POWER & ODOR DISSIPATED. OPERATED OVEN HALF AN HOUR, NO PARTICULAR ODOR NOTED. INSIDE IS CLEAN. REPLACED OVEN, TEST GOOD. NO ODOR.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 55,643 hrs · 19,587 cycles

F-O 02 MASK HARNESS LEAKS. FOUND HEAD HARNESS INFLATION COMPLETELY INOP DUE TO DISCONTINUITY OF BLADDER IN HARNESS. REPLACED MASK ASSY.

Part: GIRT BAR — UNSECURE (R1 DOOR SLIDE) · airframe 55,162 hrs · 19,401 cycles

DOOR 1R WILL NOT TURN ON SLIDE LIGHT GIRT BAR APPEARS TO BE OUT OF POSITION. SECURED GIRT BAR FWD BAR LOCK ON DOOR 1R. OPS CHECK NORMAL.

Part: UNKNOWN — ODOR (CABIN) · airframe 55,050 hrs · 19,358 cycles

CREW REPORT: THREE MINUTES PRIOR TO LANDING F/A REPORTED ACRID SMELL IN LAST THREE ROWS, GONE ON LANDING. SAMC TEXT: FA'S REPORTED ACRID RUBBER TYPE SMELL IN LAST 3 ROWS OF COACH, NO SMELL IN AFT GALLEY NOTED. FLT CREW CHECKED AREA AFTER LANDING, NO DEFECTS NOTED, NO SMELL NOTED. EXTERIOR WALKAROUND DETECTED NO DEFECTS. NO SMELL NOTED IN COCKPIT AT TIME OF OCCURRENCE. INBOUND CAPT CHECKED AFT CABIN AFTER ARRIVAL, NO UNUSUAL ODOR PRESENT. CHECKED ALL SEAT SEB'S AND PCU'S, ALL AFT GALLEY COMPONENTS, ALL CABIN LIGHTING IN THE AREA, NO DEFECTS NOTED. ALSO DROPPED CEILING PANELS AND CHECKED OVERHEAD, NO DEFECTS NOTED. RAN PACKS AND NO UNUSUAL ODORS PRESENT.

Part: DUCT — DAMAGED (CABIN) · airframe 54,814 hrs · 19,259 cycles

CEILING & PANEL UNSECURE, RTFL. INSPECTED AREA AROUND OVERWING EXITS AND FOUND DAMAGE ON TOP OF OVAL MAIN DISTRIBUTION DUCT BETWEEN ROWS 17 AND 18. REMOVED PLENUM NOZZLE ASSY UNDER DISTRIBUTION DUCT SECTION FROM ROW 17 TO 19. REMOVED DAMAGED DUCTS BETWEEN ROWS 15 TO 19. BEGAN INSTALLING 2 EA NEW DUCT ASSY'S AT ROWS 15 THRU 19, DUCT HARDWARE IS INSTALLED AND SECURE. HOSES INSTALLED BUT NOT YET SECURE. NEED SPLICES INSTALLED. INSTALLED END CAPS FOR UNUSED HOSE CONNECTION. FINISHED INSTALLATION OF DUCTS. ACFT DETERMINED OK FOR REV SVC.

Part: LANYARD — FRAYED (R2 DOOR SLIDE) · airframe 54,778 hrs · 19,247 cycles

THE 2R MED EVAC SLIDE GIRT BAR LANYARD FRAYED. ACP ON WU K6903D, REPLACED SLIDE.

Part: LANYARD — UNSECURE (R1 DOOR SLIDE) · airframe 54,225 hrs · 19,040 cycles

DOOR 1R SLIDE PACK RETAINER RING HANGING OUT OF COVER MAKING DOOR HARD TO CLOSE AND ARM. SECURED LANYARD AND DOOR CHECKS OKAY.

Part: COVER — BROKEN (CABIN) · airframe 54,126 hrs · 19,003 cycles

ONE (1) FT OF EEL COVER BROKEN AT SEAT 34C. REPLACED SECTION OF COVER.

Part: BLADE — DENTED (LT ENGINE) · airframe 54,121 hrs · 19,002 cycles

CREW REPORT: ON PREFLIGHT FOUND DIME SIZED DENT ON LEADING EDGE OF LEFT ENGINE NR 26 1ST STAGE BLADE. BLENDED SMALL DING ON NR 1 ENGINE, BLADE NR 26 LEADING EDGE, MARKED.

Part: SWITCH — STUCK (CABIN) · airframe 52,924 hrs · 18,544 cycles

FLOOR EMERGENCY EXIT EEL LIGHTS FROM ROW 28 TO REAR OF ACFT, AFT MOST CTR LINE EMERGENCY EXIT SIGN AND EMERGENCY EXIT SIGN ABOVE AFT LT EXIT DOOR ARE ILLUMINATED ALL THE TIME. FOUND TEST SWITCH OVER LT AFT DOOR TO BE STUCK IN, REPAIRED, SYS CHECKS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 52,924 hrs · 18,544 cycles

COVE EMERGENCY LIGHTING INOP FROM ROW 27 RT SIDE TO REAR AND EMERGENCY EXIT SIGN ABOVE AFT RT EXIT DOOR. REPLACED BATTERY, SYS CHECKS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 52,924 hrs · 18,544 cycles

FLOOR EEL LIGHTS INOP FROM ROW 23 TO REAR OF ACFT. REPLACED EEL BATTERY, SYS CHECKS GOOD.

Part: SLIDE — LOW (R1 DOOR) · airframe 51,400 hrs · 17,988 cycles

NR 1 RT MED SLIDE PRESSURE INDICATOR IS AT LOW EDGE OF GREEN BAND. *S/D* UNKNOWN PRESSURE LEAK. REPLACED SLIDE ASSY, OPS CHECKED NORMAL.

Part: COVER — FAILED (NR 5 BEARING)

NR 2 ENGINE OIL PRESSURE READING 0 ON THE QUANTITY OIL TEMP READING NORMAL. PSI BETWEEN 100-140. FLIGHT DIVERTED. *S/D* FOUND COVER SEAL DEFECTIVE AND BLOWN OUT OF GROOVE OF NR 5 BEARING COVER. CLEANED EXCESS OIL AND REPLACED SEAL AND SERVICED OIL. ACCOMPLISHED HIGH POWER RUNS AND NO LEAKS NOTED.

Part: LIGHT — UNSECURE (ROW 1) · airframe 51,296 hrs · 17,950 cycles

CABIN EMER LT STRIP COMING UP NEAR ROW 13. SECURED STRIP, OPS CHECKED OK.

Part: SIGN — SHORTED (EMERGENCY EXIT) · airframe 50,200 hrs · 17,572 cycles

LAST EXIT SIGN IN FIRST CLASS INOP. FOUND SHORT IN SIGN. REPLACED EMER EXIT SIGN, OPS CHECKED NORMALLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,200 hrs · 17,572 cycles

EXTERIOR EMERGENCY LIGHT AT DOOR 2L INOP. REPLAMPED ASSY, OPS CHECKED NORMALLY. FOUND LAMP INOPERATIVE. REPLAMPED ASSY, OPS CHECKED NORMALLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,200 hrs · 17,572 cycles

EXTERIOR EMERGENCY LIGHT AT DOOR 4R INOP. RELAMPED ASSY, OPS CHECKED NORMAL. FOUND AMP INOPERATIVE. RELAMPED ASSY, OPS CHECKED NORMAL.

Part: SLIDE — LOW (L1 DOOR) · airframe 50,200 hrs · 17,572 cycles

DOOR 1L MOUNTED ESCAPE SLIDE BOTTLE PRESSURE AT THE LOW END OF THE GREEN BAND AFTER 2 HOURS. FOUND SLOW LEAK ON SLIDE BOTTLE. REPLACED ESCAPE SLIDE ASSY.

Part: LIFTER — WORN (DOOR 4R) · airframe 50,081 hrs · 17,524 cycles

DOOR 4R IS HARD TO ARM. FOUND AFT LIFTER ASSY WORN. FOUND METAL BURRS ON SLIDER. FILED OFF BURRS AND CLEANED SLIDERS, DOOR ARMS AND DISARMS NORMALLY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,275 hrs · 17,247 cycles

EEL LIGHT STRIP SEGMENT AFT OF SEAT 6B INOPERATIVE. FOUND LAMP ASSY BURNED OUT. REPLACED LIGHT ASSY (RELAMPED).

Part: SPRING — BROKEN (R4 DOOR) · airframe 49,275 hrs · 17,247 cycles

DOOR 4R MODE SELECTOR GUARD FOR SLIDE HAS BROKEN SPRING. REPLACED SELECTOR GUARD.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 49,275 hrs · 17,247 cycles

EMERGENCY LIGHT AT OVERHEAD BIN SEAT 5C. FOUND BURNED OUT BULB. REPLACED BULB ASSY FOR OVERHEAD BIN 5C.

Part: GUARD — OUT OF ADJUST (L4 DOOR) · airframe 49,275 hrs · 17,247 cycles

DOOR 4L MODE SELECTOR GUARD DOES NOT PREVENT SLIDE HANDLE FROM BEING MOVED. FOUND SELECTOR GUARD OUT OF ADJUSTMENT. ADJUSTED SELECTOR GUARD, OPS CHECKED NORMAL.

Part: SLAT — DAMAGED (NR 3) · airframe 49,166 hrs · 17,207 cycles

NR 3 OUTBOARD L/E SLAT HAS DAMAGE. NR 3 SLAT WAS DAMAGED AND REMOVED AND SENT TO SHOP FOR REPAIR.

Part: GIRT BAR — OUT OF ADJUST (R3 DOOR) · airframe 49,138 hrs · 17,196 cycles

FOUND DOOR 3R DIFFICULT TO ARM.

Part: BOTTLE — READS LOW (ESCAPE SLIDE) · airframe 47,322 hrs · 16,545 cycles

EMERGENCY ESCAPE LIGHT REMAINED EXTINGUISHED DURING SLIDE SQUIB TEST 2 ON SIDE 5 (05=L, 06=R). [SUP 06-06-07] FOUND LEFT OVERWING EVAC SLIDE BOTTLE PRESS LOW. ACCOMPLISHED A ONE TIME RECHARGE. SQUIB TEST OK. CYLINDER REPLACED AT FIRST MAINT STATION WHERE PARTS WERE AVAILABLE.

Part: CONNECTOR — FAILED (BATTERY CHARGER) · airframe 45,949 hrs · 16,045 cycles

EICAS MESSAGE MAIN BATTERY CHARGER DISPLAYED AND BATTERY DISCHARGE LIGHT EXTINGUISHED. ACCOMPLISHED CHRONIC REVIEW. FOUND DEFECTIVE PIN ON BATTERY CHARGER. REPLACED CHARGER, MSG ERASED AND BATTERY CHARGING OK. ALSO REPLACED THE MAIN BATTERY.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 45,681 hrs · 15,934 cycles

OXYGEN MASK DEFECTIVE AT 1 (1=CAPT,2=1ST OFF,3=1ST OBS) CAPT O2 MASK LEAKS AIR WHEN RED HANDLES ARE SQUEEZED AND HEADSTRAP INFLATED. REPLACED DEFECTIVE COCKPIT CREW OXYGEN MASK.

Part: O-RING — DAMAGED (SLIDE) · airframe 44,448 hrs · 15,511 cycles

FOUND LOW BOTTLE PRESSURE FILLER VALVE O-RING FOUND DAMAGED AND LEAKING. REPLACED FILLER VALVE O-RING.

Part: FRAME — DENTED (BS 1500) · airframe 39,432 hrs · 13,623 cycles

AFT PIT FRAME STA 1500, STR 25L AND 26L HAS DENT UPPER FLANGE. CUTOUT DAMAGE AND REPAIRED PER REO G10197 AND EVA-50005.

Part: FRAME — DENTED (BS 1580) · airframe 39,432 hrs · 13,623 cycles

AFT PIT STA 1580 FRAME HAS A DENT BETWEEN STR 25L AND 26L ON UPPER FLANGE. TRIMMED DAMAGE, INSURANCE CUT, INSTALLED ANGLE DOUBLER PER REO G-10195 AND EVA-50003.

Part: FRAME — DAMAGED (BS 1600) · airframe 39,432 hrs · 13,623 cycles

AFT PIT STA 1600 FRAME HAS A DENT BETWEEN STR 25L AND 26L ON UPPER FLANGE. CUT OUT DAMAGE, INSURANCE CUT, INSTALLED DOUBLER REPAIR PER RE0-G10199, AND EVA-50007.

Part: FRAME — DAMAGED (BS 1520) · airframe 39,432 hrs · 13,623 cycles

AFT PIT STA 1520 FRAME HAS A DENT BETWEEN STR 25L AND 26L ON UPPER FLANGE. TRIMMED OUT DAMAGE TO FRAME, INSURANCE CUT, INSTALLED ANGLE REPAIR PER REO G10198 AND EVA 50006.

Part: SLIDE — DISLODGED (DOOR 1L) · airframe 42,300 hrs · 14,708 cycles

DOOR 1L SLIDE PACK OFF OF DOOR. PER AMIS HISTORY, DURING THE PERIOD OF 1OCT&14NOV 2005, THERE WAS NO REPORTED PREVIOUS ACTIVITY RELATED TO THE 1L DOOR SLIDE THAT COULD HELP IN PINPOINTING A PROBABLE CAUSE WHY THE SLIDE WAS OFF THE DOOR. A PROBABLE CAUSE THAT COULD PERHAPS HAVE ATTRIBUTED TO THIS, COULD BE THAT THE SLIDE WAS SUBJECTED TO SOME IN-SERVICE IMPACT.CORRECTIVE ACTION: SLIDE WAS REINSTALLED PER THE AMM.

Part: LIGHT — BURNED (GALLEY) · airframe 41,893 hrs · 14,557 cycles

SMOKE COMING FROM LIGHT FIXTURE IN FORWARD GALLEY. ACCOMPLISHED VISUAL INSPECTION. FOUND NO BURNT WIRES NO CHAFFING, BALLASTS OK , NO ARCING, 0-2 GEN OK. OP CHECK LIGHTS FOR 20 MINUTES NO SMELL OR SMOKE. NO FURTHER INCIDENTS SINCE.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,432 hrs · 13,623 cycles

AFT PIT STA 1600 FRAME HAS A DENT BETWEEN STR 25L AND 26L ON UPPER FLANGE. INSTALLED DOUBLER REPAIR.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,432 hrs · 13,623 cycles

AFT PIT SHEAR TIE CORRODED, BS 1420 STR 28L-29L. FABRICATED AND INSTALLED NEW SHEAR-TIE.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,432 hrs · 13,623 cycles

AFT PIT STA 1520 FRAME HAS A DENT BETWEEN STR 25L AND 26L ON UPPER FLANGE. INSTALLED ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,432 hrs · 13,623 cycles

AFT PIT STA 1580 FRAME HAS A DENT BETWEEN STR 25L AND 26L ON UPPER FLANGE. INSTALLED ANGLE DOUBLER.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,432 hrs · 13,623 cycles

AFT CARGO PIT FRAME UPPER FLANGE DENTED AT BS 1480 STR 25LTO 26L. INSTALLED J ANGLE REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,432 hrs · 13,623 cycles

FUSELAGE SKIN IS DAMAGED AT BS 1712 STR 14R. INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,432 hrs · 13,623 cycles

AFT CARGO PIT FRAME UPPER FLANGE DENTED, BS 1340 STR 25L-26L. INSTALLED J ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,432 hrs · 13,623 cycles

AFT CARGO PIT FRAME UPPER FLANGE DENTED AT BS 1380 STR 25L TO 26L. INSTALLED J ANGLE REPAIR.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,432 hrs · 13,623 cycles

AFT PIT SHEAR TIE CORRODED, BS 1440 STR 29L-30L. FABRICATED AND INSTALLED NEW SHEAR-TIE.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,432 hrs · 13,623 cycles

AFT PIT FRAME STA 1500, STR 25L AND 26L HAS DENT UPPER FLANGE. INSTALLED DOUBLER REPAIR.

Part: SKIN — BIRD STRIKE (SLAT)

OUTBOARD END L/E SKIN DAMAGED BY BIRD STRIKE. REPLACED SECTION OF L/E SKIN.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 39,432 hrs · 13,623 cycles

ATTACH ANGLE FOR BS 940 FRAME BELOW LEFT FWD OVERWING DOOR CUTOUT CORRODED BETWEEN STR 16L.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 39,432 hrs · 13,623 cycles

CABIN AFT FLOOR SHEAR WEB HAS UPPER SURFACE CORROSION IN AREAS FROM BS 1680-1720 FROM LBL 62 TO RBL 56.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,432 hrs · 13,623 cycles

FLOORBEAM HAS AREAS OF CORROSION FROM BL 0 TO RBL 60 AT BS 365.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,432 hrs · 13,623 cycles

CABIN FLOORBEAM T-CAP CORRODED ON PREVIOUS REPAIR DOUBLER AT BS 1640, RBL 48-56.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,432 hrs · 13,623 cycles

CABIN FLOORBEAM AT STA 324 RBL 40 IS CORRODED BEYOND LIMITS.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,432 hrs · 13,623 cycles

FWD PIT FUSELAGE FRAME PRODUCTION SPLICE HAS A DENT ON INNER FLANGE AT STA 580 ABOVE STR 26L.

Part: INFLATION TUBE — CHAFED (SLIDE)

DURING TIME CONTROLLED OVERHAUL, SLIDE UNIT INFLATABLE SHOWS CHAFE DAMAGE CAUSED BY THE PRESSURE RELIEF VALVE SCREWS. HOLES ARE WORN THROUGH THE CHAFE COVER (2) AND THROUGH THE TOP INFLATION TUBE (5 HOLES). EACH HOLE IS .25 INCH IN DIAMETER. PATCH PER MANUFACTURERS MANUAL. REPLACED CHAFE COVER WITH NEW COVER, OPERATION CHECKS NORMAL.

Part: BATTERY PACK — FAILED (CABIN)

EMERGENCY ESCAPE FLOOR LIGHTING INOPERATIVE. FINAL 10 FEET IN AFT SECTION. REPLACE EMERGENCY ESCAPE LIGHTING BATTERY PACK. OPERATION CHECKS NORMAL.

Part: EEL LAMP — FAILED (CABIN)

SLIDE EMERGENCY LIGHT INOP AT DOOR ONE LEFT. RELAMPED, CHECKS OK.