N532UA

Part: INDICATOR — UNRELIABLE (COCKPIT) · airframe 74,903 hrs · 22,417 cycles

CAPT'S AIRSPEED UNRELIABLE, RTFL. ALTN AIR DATA, NO HELP. REPLACED CAPT'S AIR SPEED INDICATOR. CREW COMMENTS, CAPT'S SPEED IND UNRELIABLE IN BOTH NORM AND ALT MODE. CAPT'S ATTITUDE AND STBY INDICATORS ALL SAME READING WITH FIRST OFFICERS.

Part: PTU — VIBRATION (HYDRAULIC SYS) · airframe 74,195 hrs · 22,281 cycles

F/A'S NOTICED VIBRATION IN AISLE ABOVE WING BAY. REPLACED HYDRAULIC, POWER TRANSFER UNIT, PTU AS PER MM TESTED. OP'S CHECKS NORMAL.

Part: SERVICE PANEL — FAULTY (CABIN) · airframe 73,292 hrs · 22,106 cycles

ABNORMAL NOISE, VIBRATION IN CENTER MAIN CABIN FLOOR. NOTICEABLE VIBRATION FELT ON CLIMB. PASSENGER IN 9C NOTED A LOUD THUMPING AND VIBRATION BELOW FLOOR. ACCOMPLISHED THE REPLACEMENT OF THE RT OVERWING SERVICE PNL. REPLACED OVERWING SERVICE PNL HINGE PER MM.

Part: WIRE HARNESS — DEFECTIVE (NR 2 ENGINE) · airframe 72,731 hrs · 21,998 cycles

NR 2 ENG OVERTEMP, RTFL. PERFORMED BOROSCOPE INSP AS PER MM 72-00-97. CHECKED COMPESSOR BLADES, NO DEFECTS, TURBINE BLADES, COMBUSTER BORE. REPLACED NR 2 ENGINE 14 STAGE CONVERTER VALVE PER MM. ACCOMPLISHED IDT INSPECTION OF NR 2 ENGINE 14 STAGE CONVERTER VALVE. REPLACED EEC PER AMM. CLEANED WATER TRAPS PER AMM. ACCOMPLISHED RII INSPECTION OF NR 2 ENGINE EEC. FOUND THAT THE EEC PRIMARY ACCESS CB WILL NOT RESET TRIPS. REPLACED HARNESS BETWEEN CONNECTOR D1088P AND CONNECTOR D42242P REF WIRING DIAGRAM 73-21-33, TEST OK.

Part: WIRE — SHORTED (CABIN) · airframe 71,083 hrs · 21,682 cycles

DOOR 1L & 1R - EXIT IDENTIFIER SIGNS DO NOT ILLUMINATE DURING TEST OF INTERIOR EMERGENCY LIGHTS. BY- 054816 :TRIED NEW POWER SUPPLY M731 AND INVERTER M10822 NO HELP. SEAT 1AB AND GALLEY AISLE LIGHT ALSO INOP. REF WDM 33-51-21 PG 5A SH1. CONT OF AMIS ITEM 0832018 :FOUND 6VDC AT INPUT OF INVERTER AND GROUND AT CONNECTOR D6608 PIN 5. NO OUTPUT FROM INVERTER. TRIED NEW INVERTERS, NO HELP. CONT OF AMIS ITEM 0832025. FOUND SHORTED WIRE AT LIGHT CONNECTOR OF SEAT 1A, REPAIRED WIRE, SYSTEM CHECKS GOOD.

Part: CONNECTOR — OUT OF POSITION (CABIN) · airframe 71,083 hrs · 21,682 cycles

EMERGENCY EQUIPMENT LIGHTS AT LT AISLE SEATS 1AB, 5AB, 6AB, AND 7AB DO NOT ILLUMINATE DURING TEST OF INTERIOR EMERGENCY LIGHTS. SEAT 1AB IS COVERED BY SMC 8. RESET CONNECTOR AT M732, SEATS 5, 6, AND 7 NOW OK.

Part: TAPE — MISSING (CABIN) · airframe 70,798 hrs · 21,628 cycles

BOARDING MUSIC BOX HOT AND NOISY. PROG TEXT: - ITEM ROLLED FORWARD. PULLED AND COLLARED 3 AMP. TAPE RPDRS. C-B IN P-37 PANEL PER WD. REPLACED MISSING AUDIO CASSETTE, OPS CHECK OKAY.

Part: BLADES — NICKED (LT ENGINE FAN) · airframe 70,642 hrs · 21,598 cycles

LEFT ENGINE FOUND NICKS ON SEVERAL FAN BLADES. CHECKED AND FOUND 3 BLADES ON LEADING OF BLADE ON NR 2 INDEX AREA. BLENDED BLADES LEFT ENGINE.

Part: BLADE — NICKED (LT ENGINE) · airframe 70,626 hrs · 21,595 cycles

LEFT ENGINE FOUND NICKS ON SEVERAL FAN BLADES. REF MM 72-31-02 PAGE 612. BLENDED BLADES LEFT ENGINE REF MM.

Part: BLADES — NICKED (LT ENGINE FAN) · airframe 70,626 hrs · 21,595 cycles

ON LEFT ENGINE FAN, FOUND NICKS ON SEVERAL BLADES. CHECKED FOUND 3 BLADES ON LEADING OF BLADE ON NUMBER TWO INDEX AREA. ACCOMPLISHED EDDY CURRENT INSPECTION OF BLENDED FAN BLADES ON NR 1 ENG PER MM. NO CRACKS FOUND. ACCOMPLISHED FINAL BLEND OF BLADES.

Part: SLIDING WINDOW — CRAZED (COCKPIT) · airframe 70,372 hrs · 21,546 cycles

CAPTAIN'S L2 SOME CRAZING ON WINDOW -MORE VISIBLE WITH SUNLIGHT LOW ON HORIZON - AFFECTS VIS. REPLACED NR 2L SLIDING WINDOW PER MM.

Part: BOTTLE — EMPTY (R4 DOOR ASSIST) · airframe 69,974 hrs · 21,470 cycles

DOOR 4R ASSIST BOTTLE EMPTY. REPLACED EMERGENCY POWER RESERVOIR DOOR 4R IAW AMM.

Part: METERING VALVE — LEAKING (RT BRAKE) · airframe 69,963 hrs · 21,468 cycles

HYDRAULIC QUANTITY READS RF - RIGHT SYSTEM. CREW COMMENTS: RIGHT 0.55 CENTER 1.02 LEFT 1.22. ACCOMPLISH CHRONIC REVIEW. MAINT TEXT: NEED MINIMUM 2 SHIFTS FOR T-S AND RPR FOR FLUID TRANSFER BETWEEN SYSTEMS. RT BRAKE METERING VLV DOES NOT FULLY CLOSE WHEN MANUALY OPERATED AND WHEN OPENED VLV YOU CAN HEAR VLV BYPASSING, LT DOESN'T AND CK'D ANOTHER ACFT, NO BYPASS. REMOVED VLV PER MM. INSTALLED RT BRAKE METERING VALVE. TAXIED AIRCRAFT FOR APPROX 30 MIN. NO LEAKS NOTED. NO FLUID TRANSFER NOTED, NO HYDRAULIC QTY LOSS NOTED.

Part: SLIDE — MISINSTALLED (R2 DOOR) · airframe 69,360 hrs · 21,351 cycles

MAIN CABIN DOOR 2R EMERGENCY SLIDE NOT IN MOUNTS PROPERLY. REMOVED AND RE-INSTALLED R-2 DOOR SLIDE CORRECTLY PER MM ON NON ROUTINE 47013.

Part: CAM — OUT OF ADJUST (L1 DOOR) · airframe 69,360 hrs · 21,351 cycles

L-1 DOOR, MUST PUSH ARM LEVER VERY HARD TO GET DOOR SLIDE LIGHT TO COME ON. ADJUSTED L-1 DOOR LIFTER CAM BRACKETS PER MM AND DOOR OPS CHECK GOOD ON NON ROUTINE 47544.

Part: STRAP — CHAFED (EVAC SLIDE) · airframe 69,360 hrs · 21,351 cycles

MAIN CABIN L-2 DOOR SLIDE, GIRT BAR RELEASE STRAP CHAFED. RMV'D & RPL'D MAIN CABIN L-2 DOOR SLIDE ASSY PER MM.

Part: LEVER — OUT OF ADJUST (L2 DOOR) · airframe 69,360 hrs · 21,351 cycles

L-2 DOOR ARM AND DISARM LEVER IS BINDING. ADJUSTED L-2 DOOR ARM AND DISARM LEVER PER MM AND OPS CHECK GOOD ON NON ROUTINE.

Part: SLIDE — MISINSTALLED (L1 DOOR) · airframe 69,360 hrs · 21,351 cycles

MAIN CABIN DOOR 1L DOOR SLIDE NOT IN MOUNTS PROPERLY. REINSTALLED SLIDE CORRECTLY PER MM.

Part: ROD END — LACK OF LUBE (CABIN DOOR) · airframe 69,360 hrs · 21,351 cycles

MAIN CABIN DOOR 45R SLIDE ARM HANDLE STIFF TO OPERATE. LUBED DOOR ROD ENDS AND BEARING PER MM.

Part: MECHANISM — OUT OF ADJUST (R4 DOOR) · airframe 69,360 hrs · 21,351 cycles

R-4 ENTRY DOOR FAILED MIDWAY CHECK. ADJUSTED LOCKOUT CAM MECHANISM PER MM AND OPS CHECK GOOD ON NON ROUTINE.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR) · airframe 69,360 hrs · 21,351 cycles

MAIN CABIN L-1 DOOR MODE SELECTOR LEVER FAILS MIDWAY CHECK. ADJUSTED L-1 DOOR GIRT BAR MECHANISM PER MM AND DOOR OPS CHECK GOOD PER MM ON NON ROUTINE 47096.

Part: STOP — OUT OF ADJUST (R1 DOOR) · airframe 69,360 hrs · 21,351 cycles

MAIN CABIN 1R DOOR HANDLE CLOSING FORCE IS EXCESSIVE. CLEANED AND LUBED DOOR PER MM. ADJUSTED DOOR STOP PINS PER MM AND DOOR OPS CHECK IS GOOD PER MM ON NON ROUTINE 47023.

Part: LOCK — DAMAGED (L1 HOLD OPEN) · airframe 69,360 hrs · 21,351 cycles

MAIN CABIN L-1 DOOR HOLD OPEN LOCKING COLLAR BROKEN. REMOVED AND REPLACED THE L -1 DOOR HOLD OPEN LOCKING COLLAR PER MM AND DOOR OPS CHECK GOOD PER MM ON NON ROUTINE 47030.

Part: SPRING — BROKEN (L2 DOOR) · airframe 69,360 hrs · 21,351 cycles

MAIN CABIN DOOR 2L DOOR SLIDE ARM HANDLE DISARM FLAG SPRING BROKEN. REMOVED AND REPLACED L-2 DOOR ARM-DISARM FLAG SPRING PER GN-MM 01-0-08-025 AND DOOR OPS CHECK GOOD ON NON ROUTINE.

Part: ATTACH BOLT — LOOSE (L1 DOOR) · airframe 69,360 hrs · 21,351 cycles

MAIN CABIN L-1 DOOR LOWER CONTROL ARM DOOR ATTACH BOLTS LOOSE. SECURED MAIN CABIN L-1 DOOR LOWER CONTROL ARM DOOR ATTACH BOLTS PER SRM AND OPS CHECK GOOD.

Part: DUCT — DAMAGED (CABIN) · airframe 69,118 hrs · 21,304 cycles

CENTER CABIN AIR DISTRIBUTION DUCT HAS NUMEROUS HOLES AT ROW 5. REPLACED PORTION OF DUCT ASSY BY ROW 5. LEAK CHECKS GOOD. AIRCRAFT INSPECTED AND IS IN A COND FOR SAFE FLIGHT. MAIN DISTRIBUTION DUCT IN CEILING ABOVE ROW 5 APPEARS TO HAVE HOLE OR CRACK ON TOP OF DUCT. RMVD CEILING PNLS FROM ROW 5->8 FOR ACCESS TO OVERHEAD DISTRB DUCT, RMVD CTR VENT CHNL FOR DUCT ACCESS, NEED TO CONTINUE DISASSEMBLY. INSTALLED CTR VENT CHNL. REMOVED ABOUT 44 INCHES OFF THE FWD END OF THE DAMAGED RISER DUCT. DUCT ON ORDER OSTF Z6835 AND DAMAGED SECTION ROUTED TO SHOP R40563. FOUND NEW DUCT SECTION. CUT TO FIT SEALED EDGES. NEED TO INSTALL ISOLATERS ON BRACKET AND INSTALL DUCT. INSTALLED NEW OVHD DUCT SECTION STA.790 TO STA.835. SECURED ISOLATORS, LOWER JOINT BRACKETS AND APPLIED JOINT TAPE AND EPOXY. NEEDS NOZZLE DIFFUSERS. RPR'D DUCT ASSY AND INSTALLED. DUCT LEAK CHECK GOOD.

Part: OXYGEN BOTTLE — READS LOW (SEAT 3AB) · airframe 68,385 hrs · 21,164 cycles

O2 BOTTLE LOW AT SEAT 3AB. R & R O2 BOTTLE AT SEAT 3AB.

Part: LANYARD — DISLODGED (GIRT BAR) · airframe 65,843 hrs · 20,668 cycles

DOOR 3L HAS ESCAPE ROPE HANGING OUT NEEDS TO BE RESECURED. REINSTALLED GIRT BAR LANYARD & BUSTLE. ACCMP'D RII ON 4 LT LANYARD REPOSITIONING.

Part: ACCESS PANEL — LEAKING (RT WING) · airframe 65,659 hrs · 20,632 cycles

RT WING FUEL ACCESS PLATE 641EB LEAKING FUEL. REMOVED RT WING PLATE 641EB. INSPECTED SEAL AND GASKET AND FOUND GOOD. CLEARED AND CLOSED. NEEDS TO STATIC LEAK CHECK. STATIC LEAK CHECKED GOOD.

Part: A/C PACK — ODOR · airframe 64,429 hrs · 20,400 cycles

PACKS PUT OUT STRONG MUSTY ODOR WHEN FLYING IN MOISTURE. SEE HISTORY. ACCOMPLISHED ENG RUN OIL LEAKAGE EXTERNAL FROM REV COWL OPEN ACT REF LM3422 AND CREATED SMC08. SECOND RUN NEEDS TO BE ACCOMPLISHED REF SMC08.

Part: FAN — OVERHEATED (NR 2) · airframe 64,280 hrs · 20,372 cycles

CARGO DET AIR STATUS MSG COMPLETED SMOKE DET BITE, NO HELP WITH RESET OR ERASE IAW MM FIG 107 STEP '5' WAS A NEGATIVE FOR THE MESSAGE, THEREFORE AFT PIT SMOKE DET SYS INOP. REPLACED AFT DET PRESS SWITCH, NO HELP. MAINT PAGE MESSAGE 'FWD DETECT FAN' AND EICAS MESSAGE 'CARGO DET AIR'. REPLACED NR 1 DETECTOR TO CLEAR FWD DET MAINT MESSAGE. REPLACED NR 1 FWD DETECTOR FAN NO HELP. SUSPECT BAD FWD PRESS SWITCH. NR 2 DET FAN RUNS EXTREMELY HOT. RECOMMEND CHANGING ALSO PN 563-0126. 563-3898. REINSTATED CARGO COMPT FIRE DET SYST, SYS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (SEAT 21ABC) · airframe 64,095 hrs · 20,337 cycles

CABIN AISLE EMERGENCY EXIT STRIP LIGHTING ON SEAT 21ABC INOPERATIVE. REPLACED SEAT EMERGENCY LIGHT STRIP.

Part: ENGINE — FIRE (NR 1) · airframe 63,215 hrs · 20,167 cycles

NR 1 ENG SHUT DOWN DUE TO FLAME IN TAILPIPE. NR 1 ENGINE HAD FLAMES ON START UP, IDG LIGHT & DISCONNECT BY CREW AS WELL AS BLANK INDICATION ON N-1 THEN ALL INDICATIONS. ENGINE STOPPED WITHOUT STARTER SWITCH TURNED TO OFF. REPLACED NR1 ENGINE.

Part: CONTROL VALVE — ODOR (LT A/C PACK) · airframe 63,128 hrs · 20,146 cycles

EXCESSIVE NOISE & ODOR IN CABIN, FLT DIVERTED. FOUND DISTRIBUTION DUCT AIR LEAK AT FWD END. REPAIRED DUCT. SUSPECT STRANGE ODOR FROM LT PACK DUE TO ICING. REPLACED TEMP CONTROL VALVE. OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,290 hrs · 19,985 cycles

EMERGENCY EXIT FLOOD LIGHT MOUNTED ON STOW BIN ABOVE SEAT 7C IS INOP. RELAMPED EMERGENCY LIGHT, OPS CHECKS GOOD.

Part: PUSHROD — OUT OF ADJUST (DOOR 4L) · airframe 62,290 hrs · 19,985 cycles

MAIN CABIN DOOR 4L SLIDE ARM-DISARM HANDLE STIFF. CHECKED DOOR, ADJUSTED PUSHROD-D. OPS CHECKS GOOD.

Part: ATTACH FITTING — DIRTY (GIRT BAR) · airframe 62,155 hrs · 19,959 cycles

DOOR 3L HARD TO DISARM. CLEANED AND LUBED GIRT BAR ATTACH FITTINGS. DOOR ARMS AND DISARMS OKAY.

Part: ENGINE — SURGES (LEFT) · airframe 60,672 hrs · 19,681 cycles

LEFT ENGINE SURGED 3 TIMES IN 20 MINUTES. *S/D* FOUND NO EPCS MESSAGES OR EVENT RECORDINGS ON ARRIVAL. CONTACTED ENGINE DESK WHICH REPORTED NO ABNORMAL PARAMETERS. PERFORMED VISUAL AND CHIP DETECTOR CHECKS, ALL FINDINGS NORMAL. PERFORMED POWER ASSURANCE CHECK. ALL INDICATIONS NORMAL.

Part: ENGINE — SURGES (LEFT) · airframe 60,672 hrs · 19,681 cycles

LEFT ENGINE SURGED 3 TIMES IN 20 MINUTES. FOUND NO EPCS MESSAGES OR EVENT RECORDINGS ON ARRIVAL. CONTACTED ENGINE DESK WHICH REPORTED NO ABNORMAL PARAMETERS. PERFORMED VISUAL AND CHIP DETECTOR CHECKS, ALL FINDINGS NORMAL. PERFORMED POWER ASSURANCE CHECK. ALL INDICATIONS NORMAL.

Part: REGULATOR — LEAKING (OXYGEN SYSTEM) · airframe 59,178 hrs · 19,398 cycles

CREW O2 BELOW LIMITS - RTFL. FOUND LEAK AT REGULATOR AND INDICATION ISSUE. REPLACED PRESSURE TRANSDUCER AND REPLACED PRESSURE REGULATOR OPS OK, NO REPEATS.

Part: GIRT BAR — CLOGGED (L3 DOOR) · airframe 58,559 hrs · 19,279 cycles

DOOR 3L WILL NOT ARM PROPERLY. *S/D* FOUND DEBRIS STUCK UNDER GIRT BAR. REMOVED DEBRIS, DOOR ARMS/DISARMS NORMALLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,185 hrs · 19,208 cycles

EMERGENCY EXIT LIGHT ROW 15 TO ROW 20 INOP. LOOSE CONNECTOR. SECURED LOOSE CONNECTOR AT SEAT 20, ALL OPS OK.

Part: LIGHT — BROKEN (L2 DOOR) · airframe 56,434 hrs · 18,877 cycles

L2 DOOR SLIDE LIGHT ASSY IS BROKEN. REMOVED AND REPLACED SLIDE LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,434 hrs · 18,877 cycles

EEL LIGHT AT G4A GALLEY INOP. REPLACED EMERGENCY LIGHT ASSY, OPS CHECK NORMAL.

Part: SWITCH — INOPERATIVE (L1 DOOR) · airframe 56,434 hrs · 1,887 cycles

EMERGENCY LIGHT SWITCH INOPERATIVE AT L1 DOOR. FOUND DOOR 1L LIGHT SWITCH FAILED. REPLACED DOOR 1L EMERGENCY LIGHT SWITCH. OPS CHECK NORMAL.

Part: CONNECTOR — BROKEN (EXIT SIGN) · airframe 56,434 hrs · 18,877 cycles

L2 DOOR EXIT SIGN FWD OF DOOR HAS A BROKEN CONNECTOR. REPLACED CONNECTOR.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 56,434 hrs · 18,877 cycles

FRAME AT STA 1280, STR 27L IS DAMAGED. A TIME LIMITED REPAIR AT FRAME STA 1280 AND STR 27L WAS REMOVED PER UAL EVA IMC-30128 FOR REPLACEMENT WITH A PERMANENT REPAIR. THE EXISTING REPAIR DID NOT PASS DTA ANALSYS. REMOVED EXISTING REPAIR AND TRIMMED OUT THE BS 1280 FRAME FLANGE TO REMOVE ALL DAMAGE AND FABRICATED A NEW REPAIR ANGLE AND FILLER AND INSTALLED BETWEEN STR 26L -28L. THIS REPAIR IS TIME LI MITED FOR 12 MONTHS FROM 02JAN08

Part: DOOR FRAME — DAMAGED (R2 DOOR) · airframe 56,434 hrs · 18,877 cycles

DOOR 2R UPPER HINGE ARM CUTOUT ON FRAME REQUIRES DOUBLER INSTALLATION. ACCOMPLISHED MAJOR REPAIR.

Part: BRACE — CRACKED (NR 2 PYLON) · airframe 56,434 hrs · 18,877 cycles

NR 2 PYLON UPPER BRACE FUSE PIN SHOWS CRACK INDICATION IN SIDE INNER BORE. PERFORMED MAJOR REPAIR.

Part: FRAME — DAMAGED (L2 DOOR) · airframe 56,434 hrs · 18,877 cycles

DOOR 2L UPPER HINGE ARM CUTOUT ON FRAME IS DAMAGED.

Part: FITTING — DAMAGED (NR 2 PYLON) · airframe 56,434 hrs · 18,877 cycles

NR 2 PYLON STRUT FITTING (DELTA FITTING) NEEDS TO BE FABRICATED.

Part: FITTING — CORRODED (FUSELAGE) · airframe 56,434 hrs · 18,877 cycles

AFT PRESSURE BULKHEAD BS 1720 AND STR 17R, FITTING IS CORRODED THROUGH. ACCOMPLISHED MAJOR REPAIR.

Part: STRUCTURE — CRACKED (L4 DOOR) · airframe 56,434 hrs · 18,877 cycles

L4 DOOR HANDLE BOX CRACKED. REMOVED & REPLACED DOOR 4L HANDLE BOX.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,434 hrs · 18,877 cycles

MAIN CABIN FLOORBEAM STA 324 UPPER SURFACE HAS CORROSION. ACCOMPLISHED MAJOR REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 51,330 hrs · 17,907 cycles

FOUND DENT 1" BELOW STRINGER 16L AT STA 600 MEASURING 2.875 LONG BY .875 WIDE WITH .10 DEPTH. CUT OUT DAMAGED AREA IN A RECT. SHAPE PARLLEL TO STR WITH A 0.50 CORNER RAD. RETURNED ALL INDENTED AND PROJECTING SKIN TO CONTOUR. REMOVED ALL BURRS, NICKS, SCRATCHES. FABRICATED A DOUBLER REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 51,330 hrs · 17,907 cycles

FOUND 2 DENTS ABOVE STRINGER 16L MEASURING .375 WITH .05 DEPTH. CUT OUT DAMAGED AREA IN A RECT. SHAPE PARLLEL TO STR WITH A 0.50 CORNER RAD. RETURNED ALL INDENTED AND PROJECTING SKIN TO CONTOUR. REMOVED ALL BURRS, NICKS, SCRATCHES. FABRICATED A DOUBLER REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 51,330 hrs · 17,907 cycles

EXTERNAL FUSELAGE SKIN IS DENTED BEYOND LIMITS IN TWO AREAS FWD OF 2LT MED IN AREA OF PREVIOUS REPAIR AT STA 600. CUT OUT DAMAGED AREA IN A RECT. SHAPE PARLLEL TO STR WITH A 0.50 CORNER RAD. RETURNED ALL INDENTED AND PROJECTING SKIN TO CONTOUR. REMOVED ALL BURRS, NICKS, SCRATCHES. FABRICATED A DOUBLER REPAIR.

Part: INVERTER — INOPERATIVE (OVERWING EXIT) · airframe 44,275 hrs · 16,237 cycles

EMERGENCY EXIT PATH LIGHT INOPERATIVE NEAR OVERWING EXIT. REPLACED INVERTER.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE)

ZERO BOTTLE PRESSURE. PRESSURE RELEASE VALVE ON GAUGE INOP. PRESSURE GAUGE WAS REPLACED WHICH INCLUDED REPLACEMENT OF PRESSURE RELIEF VALVE.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 37,550 hrs · 13,787 cycles

AFT PIT STATION 1638, LT CREASE BEAM, OUTER CHORD ANGLE CORRODED. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,550 hrs · 13,787 cycles

CABIN FLOORBEAM UPPER CAP HAD CORROSION ON UNDER SIDE AT STATION 365 AT APPROX RBL 36 STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. REMOVED PORTION OF UPPER T-CAP AND USED SPLICE REPAIR IN INSTALLING NEW UPPER T-CAP.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,550 hrs · 13,787 cycles

CABIN FLOORBEAM STATION 1640 DAMAGED AND CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED T-CAP.

Part: PLATE — CORRODED (FUSELAGE) · airframe 37,550 hrs · 13,787 cycles

AFT CABIN DECKPLATE CORRODED STATION 1690 TO 1694 RBL 50. MAJOR REPAIR ACCOMPLISHED. REPAIRED DOUBLER INSTALLED.

Part: FRAME — GOUGED (FUSELAGE) · airframe 37,550 hrs · 13,787 cycles

AFT CARGO PIT FRAME STATION 1280 LBL 23 IS GOUGED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE AND INSTALLED TWO REPAIR STRAPS.

Part: PACKING · airframe 36,719 hrs · 13,486 cycles

LEFT ENGINE OIL QUANTITY DECREASED TO 3 QUARTS IN CRUISE. OIL PRESSURE AND TEMPERATURE NORMAL. SUPPLEMENTAL DATA UPDATE OIL FILTER WAS REPLACED AT DEPARTING STATION DUE TO A FILTER BYPASS MESSAGE. AT MSP OIL WAS FOUND LEAKING AT THE OIL FILTER HOUSING COVER. IT WAS REPORTED THAT THE O-RING WAS DETERMINED TO BE TOO SMALL AND WAS THROWN AWAY. ANOTHER O-RING WAS INSTALLED AND THE ENGINE CHECKED OK.

Part: ENGINE — FAILED (NR 2) · airframe 35,649 hrs · 13,082 cycles

NR 2 ENGINE INFLIGHT SHUTDOWN. ENG IND SHOWED LOW OIL PRESS AND NO N1 OR N2 ROTATION. IFSD OCCURRED IN CRUISE FLT.

Part: AXLE — FRACTURED · airframe 35,602 hrs · 13,062 cycles

RIGHT REAR TIRE RIGHT TRUCK AXLE FAILED PRIOR TO TAKEOFF. RIGHT REAR AXLE SHEARED OFF. SUPPLEMENTAL DATA UPDATE A CHROME GRINDING DEFECT ON THE 4.5 INCH OUTER DIAMETER CAUSED CIRCUMFERENTIAL CRACKING AND THE EVENTUAL FAILURE OF THIS AXLE. THE GRINDING DEFECT HAS CHARACTERISTICS CONSISTENT WITH A GRINDING WHEEL PLUNGE MANEUVER. THIS DEFECT WAS IN THE MAXIMUM BENDING STRESS LOCATION FOR THIS AXLE, A MOST CRITICAL AND WORST PLACE FOR ANY DEFECT ON THIS PART. REPLACED AXLE.

Part: IDG — FAILED (ENGINE)

RIGHT GENERATOR DRIVE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO FIELD. *S/D* RIGHT INTEGRATED DRIVE GENERATOR WAS REMOVED AND SENT TO SHOP. INTEGRATED DRIVE GENERATOR HAD BROKEN PISTON SLIPPERS. NEW INTEGRATED DRIVE INSTALLED, OPERATION CHECKS NORMAL.

Part: IDG — FAILED (LT ENGINE)

NR 1 GENERATOR WENT OFF LINE, DIVERTED TO BDL. RESET OK BUT LEFT GENERATOR DRIVE DISCONNECT LIGHT FLASHES INTERMITTENTLY. PROCEEDED EWR WITH APU OPERATING. *S/D* FOUND THE INTEGRATED DRIVE GENERATOR FAILED. REPLACED INTEGRATED DRIVE GENERATOR, CHECKS OK.

Part: IDG — FAILED (LT ENGINE)

PER CREW, FELT SUDDEN BUMP IN FLIGHT AND NR 1 GENERATOR DRIVE LIGHT ILLUMINATED AND BREAKER OFF. NUMEROUS EICAS MESSAGES. DIVERTED TO SLC. *S/D* FOUND INTEGRATED DRIVE GENERATOR FAILED. REPLACED GENERATOR, CHECKS OK.

Part: EEL LEAD — FAILED (CABIN)

EEL STRIP INOP SEAT 9C TO 16C. REPLACED EEL LEAD.