N576UA

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,776 hrs · 24,923 cycles

FORWARD LUMINESCENT EXIT LIGHTS DOOR 1L & 1 RIGHT AS WELL AS FWD MOST FLOOR EEL INOPERATIVE. REPLACED FWD MOST EEL CABIN ENTRANCE IAW MM33-51-96. ALL LUMINESCENT LIGHTS OPERATIONS CHECKED GOOD.

Part: CONTROL VALVE — FAULTY (HYDRAULIC SYS) · airframe 69,486 hrs · 24,494 cycles

POWER XFER STATUS. AIRPLANE FAILS MEL MX PROCEDURE 3161B. REPLACED K10051 RELAY & M10145 TIME DELAY AS SUGGESTED BY MEL 3161B A 9 A, NO HELP. REPLACED PTU CONTROL VLV IAW AMM 29-22-03.

Part: HYDRAULIC SYSTEM — MALFUNCTIONED (C SYSTEM) · airframe 69,379 hrs · 24,465 cycles

C HYD SYS PRESSURE MESSAGE ON EICAS. PERFORMED QRH PROCEDURE. YAW DAMPER KICKED OFF & NOTICED DIFFERENCE IN FLIGHT CONTROL PERFORMANCE. PRESSURE WENT TO ZERO ON BOTH CENTER ELECTRIC PUMPS. RECEIVED CTR HYD EICAS MESSAGE & IAW QRH SHUT OFF CTR PUMPS. DURING TROUBLESHOOTING, FOUND C HYD SYS LOW MESSAGE ON HYD PAGE OF EICAS. REPLACED RESERVOIR DEPRESSURE VALVE, RESERVOIR PRESSURE RELIEF VALVE, C HYD SYS PRESSURE TRANSMITTER IAW AMM 29-11-25, 29-11-24 & 29-31-01.

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY) · airframe 69,127 hrs · 24,395 cycles

BURNING SMELL WHEN BREWING COFFEE AT M41. REPLACED COFFEE MAKER AT M41 IAW MM25-32-96-201. OPERATIONS CHECKED NORMAL, NO ODOR PRESENT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 68,464 hrs · 24,202 cycles

DOOR EMERGENCY EXIT MARKERS AT DOOR 1 RT & LT & FLOOR STRIP BY FWD CLOSET INOPERATIVE. REPLACED BATTERY PACK IAW MM 33-51-07, OPERATIONS CHECKED OK.

Part: HOUSING — MISSING (R4 DOOR LIGHT) · airframe 67,891 hrs · 24,037 cycles

DURING PUSH BACK R4 ARMED LIGHT FELL OUT. SLIDE LIGHT CAP IS MISSING. VERIFIED DOOR 4R GIRT BAR ENGAGED. REPLACED DOOR 4R LIGHT HOUSING ASSEMBLY. OPS CHECKED SEVERAL TIMES ARE GOOD.

Part: PCA — OUT OF ADJUST (AILERON) · airframe 67,460 hrs · 23,891 cycles

280K DESCENT REQUIRED 6 UNITS LT TRIM. 250 DESCENT REQUIRED 4.5 UNITS LT. AT CRUISE RUDDER 1.5 UNITS LT, WITH CONTROL WHEEL CTR THE CREW NOTICED RT AIL WAS UP A BIT LT AIL WAS LEVEL ON EICAS. THERE WAS NO AIL TRIM INPUT. THE RUDDER TRIM AT 6 UNITS 280K GOT BETTER WITH FLAPS BEING LOWERED. ADJUSTED LT & RT AIL PCA.

Part: UNKNOWN — MALFUNCTIONED (AC BAY) · airframe 67,246 hrs · 23,819 cycles

REPEAT GRIP LT PACK UNCONTROLLABLE ALL MODES TEMPERATURE IN COCKPIT 98 DEGREES. COMPLIED WITH ZONE TEMPERATURE TOO HOT AMM 21-61-00, PACK TEMPERATURE CONTROL BITE 21-51-00 FIG 104, ZONE TEMPERATURE CONTROL BITE TEST 21-60-00 & OPERATIONS CHECKED 21-51-00. NO FAULTS NOTED, ALL SYSTEMS TESTED NORMAL.

Part: STRUCTURE — DAMAGED (WINDOW TRIM) · airframe 66,797 hrs · 23,665 cycles

L3 COCKPIT WINDOW TRIM STRIP PULLED AWAY SCREWS STRIPPED IAW ECRA2515-01020, INTERIM REPAIR MADE, REBONDED L3 WINDOW COVER TRIM.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 66,347 hrs · 23,519 cycles

RIGHT FUSELAGE SKIN PANEL HAS NUMEROUS ELONGATED HOLES AT WBD FAIRING DOMENUT ATTACHMENT BETWEEN BS 1210 AND BS 1310 & STR 16R AND 20R. REPAIRED ELONGATED HOLES AT RT FUSELAGE SKIN PANEL AT WBD FAIRING DOME NUT ATTACHMENT BETWEEN BS 1210 AND BS 1310 AND STR 16R AND STR 20R IAW UNITED ECRA 5330 -04626 AND REO-M0691, REV 1R. HFEC INSPECTED HOLES COMMON TO SKIN REPAIR. NO DEFECTS NOTED.

Part: SKIN — DAMAGED (BS 1240-1320) · airframe 66,347 hrs · 23,519 cycles

DAMAGE ON RT AFT WING TO BODY FAIRING AREA FUSELAGE SKIN BS 1240 - 1320. REPAIRED FUSELAGE SKIN AT BS1264-1303, S17-20R IAW ECRA 5300-01687. ACCOMPLISHED HFEC NTM PART6 51-00-16 NO DEFECT NOTED. MAJOR REPAIR.

Part: SKIN — DENTED (BS 1620 S29R) · airframe 66,347 hrs · 23,519 cycles

DENT ON FUSELAGE SKIN AT BS 1620 S29R. REPAIRED EXTERIOR FUSELAGE SKIN BETWEEN BS 1612 - 1624 S28R-29L IAW ECRA 5300-01685. ACCOMPLISHED HFEC IAW NTM PART 651-00-19. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 1600 S19L) · airframe 66,347 hrs · 23,519 cycles

LARGE GAPS BETWEEN REPAIR DOUBLER AND EXTERNAL FUSELAGE SKIN AT BS 1600, S19L. R & R EXTERNAL FUSELAGE SKIN REPAIR DOUBLER BS 1582-1612 BETWEEN S17-21L IAW ECRA 5361-01061. ACCOMPLISHED HFEC IAW NTM 51-00-19,51-00-16 NO DEFECTS NOTED. MAJOR REPAIR.

Part: SPLICE — DAMAGED (BS 1620) · airframe 66,347 hrs · 23,519 cycles

BUTT SPLICE AT BS 1620 S29-30R HAS DAMAGE. REPAIRED BUTT SPLICE IAW ECRA 5300-01685.

Part: SKIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 66,347 hrs · 23,519 cycles

CORROSION ON FWD CARGO DOOR LOWER SKIN APPROX 9 INCHES ABOVE LOWER EDGE AND 17 INCHES AFT OF FWD EDGE AND IN PREVIOUS BLENDED AREA. REPAIRED FWD CARGO DOOR IAW SRM 52-30-01. REPAIR 4, FIG 201.

Part: SKIN — DENTED (BS 430) · airframe 66,347 hrs · 23,519 cycles

EXTERNAL SKIN HAS A DENT AT BS 430, S15-16L. EVALUATED DENTS AND FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-00-01, REPAIR 2, FIG 201. PERFORMED NDT INSP HOLE AND CUTOUT REF NTM 51- 00-19 AND 51-00-16. NO DEFECTS NOTED.

Part: SKIN — DAMAGED (BS 430) · airframe 66,347 hrs · 23,519 cycles

SKIN DAMAGED BS 430, S15-16L. REPAIRED IAW SRM 53-00-01, TABLE 5. MAJOR REPAIR.

Part: VALVE — FAILED (FUEL CELL) · airframe 66,285 hrs · 23,501 cycles

RIGHT TANK FUEL SLOWLY TRANSFERS INTO CENTER TANK. REPLACED CENTER FUEL TANK RIGHT FILL VALVE DUE TO FAILURE AND THE RIGHT DEFUEL VALVE AND ACTUATOR DUE TO FOUND FUEL MIGRATING THRU VALVE. SYSTEM CHECKED NORMAL.

Part: FLOOR PANEL — DAMAGED (FWD LAVATORY) · airframe 65,842 hrs · 23,362 cycles

SOFT SPOT ON FWD LAVATORY FLOOR. INSTALLED STAINLESS DOUBLER UNDER FORWARD LAV FLOOR MAT.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 65,342 hrs · 23,192 cycles

FLOOR EMERGENCY LIGHTS INOPERATIVE AT 11,12, 26, 27. REPLACED CABLE AT ROW 27. ALL EMERGENCY LIGHTS IN CABIN, OP CHECK OKAY. LIGHT'S CHECKED OKAY.

Part: OXYGEN MASK — BROKEN (COCKPIT) · airframe 65,332 hrs · 23,189 cycles

OBSERVER O2 MASK BROKEN DOES NOT INFLATE. REPLACED OBSERVER O2 MASK. OP CHECKED OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,238 hrs · 23,156 cycles

FOUND ON 2SV EMERGENCY LIGHT CHECK EEL PATH LIGHTS BETWEEN ROW 26-27 NOT WORKING. REF MM 33-51-96, SECURED EEL LIGHT STRIP. CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,238 hrs · 23,156 cycles

FOUND ON 2SV EMERGENCY LIGHT CHECK ROW 4AB OVERHEAD EMERGENCY LIGHT BURNT OUT REF MM 33-51-05. RELAMPED, TESTED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,238 hrs · 23,156 cycles

FOUND ON 2SV EMERGENCY LIGHT CHECK, ROW 2EF OVERHEAD EMERGENCY LIGHT BURNT OUT. REF MM33-51-05, RELAMPED.

Part: MOTOR — FAULTY (WINDSHIELD WIPER) · airframe 65,088 hrs · 23,105 cycles

FIRST OFFICER WINDSHIELD WIPER ONLY MOVES ALONG TOP HALF OF TRAVEL. REPLACED MOTOR PER MM AND WIPER ARM, OPS CHECKED NORMAL.

Part: PLATE — LOOSE (WIPER MOTOR) · airframe 65,093 hrs · 23,107 cycles

UNBEARABLE OCARINA-LIKE HOWLING NOISE IN VICINITY OF F/O'S FWD INSTRUMENT PANEL & ABV 2.6 FOUND WIPER MOTOR ACCESS PLATE LOOSE. SECURED SCREWS ON PLATE REF AMM. SEALANT CHECKS OK. PRESSURED AC, NO NOISE OR LEAKS NOTED AFTER TIGHTENING PLATE.

Part: WINDOW — DAMAGED (COCKPIT) · airframe 64,432 hrs · 22,866 cycles

CAPTAIN'S FIXED SIDE AFT WINDOW'S VISIBILITY IS AFFECTED BY DEFECTS, REPLACE FIRST AVAILABLE. CREW COMMENTS: IN SUN SCRATCHES AFFECT VISIBILITY FOUND WINDOW EXTREMELY GRIMY ON THE OUTSIDE. GAVE WINDOW GOOD CLEANING AND VISIBILITY IS NOW BACK TO NORMAL.

Part: COVER — LOOSE (CABIN) · airframe 64,369 hrs · 22,841 cycles

FLOOR EMERGENCY ESCAPE LIGHTING HAS COME LOOSE AT LAST PAX ROW. MAINT TEXT: EEL STRIP COVER IS LOOSE, LAST ROW LEFT SIDE. SEC COVER LIGHTS OP CHECK OK.

Part: VALVE — LEAKING (FUEL SYSTEM) · airframe 64,085 hrs · 22,749 cycles

FUEL LEAKING INTO CTR FUEL TANK FROM FUELING MANIFOLD LT DRAIN VALVE BOTH STATIC AND WITH LT BOOST PUMPS RUNNING. LEFT FUEL TANK LEAKING STATIC FROM REFUELING SHUTOFF VALVE AND WITH LT FUEL PUMPS RUNNING FUEL LEAKING FROM LEFT DEFUEL VALVE. REPLACED LT REFUELING VALVE IAW AMM 28-21-02-401 AND ACTUATOR IAW AMM 28-21-12. REPLACED LT DEFUELING VALVE REF AMM 28-26-01-401 94405 AND LT DEFUEL ACTUATOR REF AMM28-26-02-401. ACCOMPLISHED OP AND LEAK CHECKS REF FIM 28-21 FAULT TREE 813. NO LEAKS FROM FUELING MANIFOLD DRAINS OR UNCOMMANDED TRANSFER NOTED.

Part: DENSITOMETER — DEFECTIVE (FUEL SYSTEM) · airframe 63,861 hrs · 22,670 cycles

FUEL IMBALANCE OF 1100 LBS AT END OF 3.5 HR FLT. ACP'D CHECK OF DEFUEL, CROSSFEED, & FUEL FILL VALVES, HAD NO FUEL TRANSFER. VERIFIED FUEL BOOST PUMP PRESSURES, AND ACP'D TEST OF THE FUEL SCAVENGE SYSTEM, OPERATES NORMAL. REF 28-22-00 CONT OF AMIS ITEM 8612003. ACCOMPLISHED FQIS PROCESSER CHECK. NO FAULTS, HISTORY, OR ERRONEOUS READINGS NOTED. REF AMM28-41-08. CONT OF AMIS ITEM 8612004. ACCOMPLISHED CH3050; ENG FUEL-FEED MANIFOLD LEAK CHECK AND CHECKED OK. SUSPECT RIGHT MAIN QTY READING LOW DUE TO BAD DENSITOMETER. REPLACED RIGHT DENSITOMETER REF AMM28-41-03-401 CONFIG 2. ACCOMPLISHED FUEL QTY SYS BITE AND CHECKED OK.

Part: BONDING STRAP — CHAFED (FUEL TANK) · airframe 63,837 hrs · 22,662 cycles

FOUND BONDING WIRE ARCING AT GAMA-CUPPING ON LEFT CENTER FUEL PUMP, INSIDE OF CENTER FUEL TANK. REPLACED BONDING WIRE. WIRE WAS CHAFING NOT ARCING.

Part: BONDING STRAP — CHAFED (FUEL TANK) · airframe 63,837 hrs · 22,662 cycles

FOUND BONDING WIRE ARCING AT GAMA-CUPPING ON RT CENTER FUEL PUMP INSIDE OF CENTER FUEL TANK. INSPECTED AND FOUND BONDING WIRE CHAFING, REPLACED BONDING WIRE.

Part: SKIN — DENTED (NR 2 NACELLE) · airframe 63,164 hrs · 22,440 cycles

NR 2 ENG NOSE COWL HAS OUT OF LIMIT DENT AT 12 O'CLOCK POSITION. REPLACED NOSE COWL ASSY.

Part: LINE — OUT OF POSITION (R1 DOOR) · airframe 63,011 hrs · 22,375 cycles

UNABLE TO ARM DOOR 1R. RE-STOWED ESCAPE SLIDE STATIC LINE REF MM.

Part: MODULE — FAULTY (LANDING GEAR) · airframe 62,964 hrs · 22,362 cycles

LANDING GEAR LEVER LOCK HANDLE IS DEFECTIVE. REMOVED AND INSTALLED LANDING GEAR CONTROL LEVER MODULE PER MM.

Part: EXCITER — FAULTY (LT ENGINE) · airframe 62,893 hrs · 22,338 cycles

CREW REPORT: NO ENG START LEFT ENGINE IGNITOR ON ONE NORMAL START IN BOTH. REPLACED LT ENGINE NR 1 SYS IGNITOR PLUG AND LT ENGINE NR 1 SYSTEM IGNITION EXCITER. PERFORMED A SUCCESSFUL OPERATIONAL TEST OF THE LT ENG NR 1 SYSTEM IGN SYSTEM AND ENG RUN PER AMM 74-00-00.

Part: SKIN — DENTED (FUSELAGE) · airframe 61,367 hrs · 21,772 cycles

FOUND DENT ON EXTERNAL FUSELAGE APPROX STA BS 640, STR 25R. MAJOR REPAIR ACCOMPLISHED. DENT FROM BS 636-645 AT STRINGERS 24R - 26R WAS REPAIRED PER THE INSTRUCTIONS ON PD 57-53-181 AND EVA 81242 WITHOUT DEVIATION.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 61,367 hrs · 21,772 cycles

CORROSION ON RT CREASE BEAM STA 324. MAJOR REPAIR ACCOMPLISHED. REPAIRED STA 324 CREASE BEAM PER THE INSTRUCTIONS ON PD 57-53-174 AND EVA 81240 WITHOUT DEVIATION.

Part: SKIN — DENTED (FUSELAGE) · airframe 61,367 hrs · 21,772 cycles

FOUND DENT ON EXTERNAL FUSELAGE APPROX BS 660, STR 25R. MAJOR REPAIR ACCOMPLISHED TO THE FUSELAGE SKIN AT BS 654-661 AND STRINGERS 24R - 26R PER THE INSTRUCTIONS ON PEMCO PD 57-53-182 AND EVA 81243 WAS ACCOMPLISHED WITHOUT DEVIATION.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 61,367 hrs · 21,772 cycles

CORROSION ON AFT CARGO DOOR SILL ANGLE FROM STA 1400 - 1420. A PERMANENT MINOR REPAIR WAS ACCOMPLISHED PER DIRECTIONS ON PD 57-53-175 WITHOUT DEVIATION.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,367 hrs · 21,772 cycles

CORROSION ON FRAME STA 1680, STR 28R AND 29R. MAJOR REPAIR ACCOMPLISHED. REPAIRED BS 1681.8 BETWEEN STR 28R - 29L PER THE INSTRUCTIONS IN PD 57-53-176 AND EVA 81247 WITHOUT DEVIATION.

Part: SKIN — DENTED (FUSELAGE) · airframe 61,367 hrs · 21,772 cycles

FOUND DENT ON EXTERNAL FUSELAGE APPROX BS 520, STR 25R. ACCOMPLISHED REPAIR AT BS 540 STR 25R- 26R IAW PD 57-53-178 AND EVA 81248 WITHOUT DEVIATION DTA ON CF9069.

Part: SKIN — DENTED (FUSELAGE) · airframe 61,367 hrs · 21,772 cycles

SKIN DENT AT STA 760 STR 15 LT AFT OF DOOR 2L. MAJOR REPAIR ACCOMPLISHED. DENT IS 3.5 IN ABOVE STR 15L AND .625 IN AFT OF STA 760L. SHOULD READ 3.5 IN ABOVE STR 16L. OK PER EVA 73942 WILL BE REPAIRED AT NEXT HO3 VISIT. MF6132 CREATED PER OPBLM FOR RECHECK AT EACH AK. **OPBLM WILLS**^10JUL OPB INF- REQUIRES RECHECK AT EVERY A CHECK PER EVA 73942. SKIN DENT AT STATION 760 STRINGERS 14L - 17L WAS REPAIRED PER THE INSTRUCTIONS ON PD 57-53-172 AND EVA 81244 WITHOUT DEVIATION.

Part: FRAME — CORRODED (FUSELAGE) · airframe 61,367 hrs · 21,772 cycles

CORROSION ON FRAME STA 1160, STR 17. REPAIRED PER THE INSTRUCTIONS ON PD 57-53-177 AND EVA 81239 WITHOUT DEVIATION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,367 hrs · 21,772 cycles

CORROSION ON TOP OF FLOORBEAM STA 324 AT RBL 41 TO RBL 63. MAJOR REPAIR ACCOMPLISHED. REMOVED CORRODED FLOORBEAM & REPLACED IT PER THE INSTRUCTIONS ON EA PD 57-53-171 AND EVA 81235 WITHOUT DEVIATION. CF9062 CREATED FOR DTA TRACKING.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,367 hrs · 21,772 cycles

CORROSION ON FLOOR SUPPORT STA 297 RBL -38 TO RBL -50. MAJOR REPAIR ACCOMPLISHED. FOUND TO BE OUT OF LIMITS, REMOVED P-6 & P-61 PNLS, REPLACED FLOORBEAM AT STA 297 FROM BL 0 - RBL 60. REINSTALLED P-6 AND P-61 PNLS. (OPS CKS ACP ON PEMCO NR 3026N0701), ON PEMCO NR 3026N00260.

Part: PRESSURE DECK — CORRODED (FUSELAGE) · airframe 61,367 hrs · 21,772 cycles

CORROSION ON PRESSURE DECK FROM 1681 TO 1685 RBL 10 - RBL 55. MAJOR REPAIR ACCOMPLISHED: PRESSURE DECK AT STATION 1681-1685 RBL 10 - RBL 55 PER THE INSTRUCTIONS ON PEMCO PD57-53-173 WITHOUT DEVIATION. A FAA FORM 8100-9 DATED AUG 18TH 2011 WAS RECEIVED AND THIS REPAIR IS CONSIDERED PERMANENT WITH NO FURTHER ACTION REQUIRED.

Part: PAN — GOUGED (L1 DOOR) · airframe 61,367 hrs · 21,772 cycles

DOOR 1L HANDLE PAN GOUGED. REMOVED & REPLACED DOOR 1L HANDLE PAN.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,367 hrs · 21,772 cycles

CORROSION ON FLOORBEAM STA 1640 RBL 58-31. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION & FOUND MATERIAL LOSS OUT OF LIMITS OF SRM. REMOVED UPPER 'T' CHORD SECTION FROM LBL 10 RBL 60. FABRICATED & INSTALLED NEW 'T' CHORD & NESTED REPAIR ANGLES & REPAIR STRAPS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 61,367 hrs · 21,772 cycles

CORROSION ON FLOORBEAM AT STATION 1660 BL 0 - LBL 58. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION & FOUND MATERIAL LOSS TO BE OUT OF LIMITS OF SRM. REMOVED UPPER 'T' CHORD SECTION FROM BS 1660 FROM BL 0 TO LBL 58. FABRICATED & INSTALLED UPPER 'T' CHORD, REPAIR ANGLE & REPAIR STRAPS.

Part: INTERCOSTAL — CORRODED (BS 1000 - 1020) · airframe 61,367 hrs · 21,772 cycles

RIGHT OVERWING HATCH RT INTERNAL LOWER INTERCOSTAL WEB BS 1000 TO 1020 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION IAW 51-21-03 AND FOUND TO BE OUT OF LIMITS. REMOVED INTERCOSTAL & FABRICATED A REPLACEMENT AND HEAT TREATED TO T6 IAW SRM. ALODINED AND PRIMED IAW MM. INSTALLED IAW SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 61,367 hrs · 21,772 cycles

STRINGER SPLICE CORRODED AT STA 440 STR 14L. MAJOR REPAIR ACCOMPLISHED. AFTER CORROSION RMVL ON STRINGER SPLICE IAW SRM AND WAS BEYOND LIMITS. FABRICATED NEW STRINGER SPLICE FROM .032" 7075-T6 LOCATED AND DRILLED IAW SRM. TREATED, PRIMED AND INSTALLED IAW AMM.

Part: STOP FITTING — DAMAGED (CARGO DOOR FRAME) · airframe 61,365 hrs · 21,771 cycles

AFT CARGO DOOR FRAME TOP FWD DOOR STOP IS BROKEN. TOP FWD CARGO DOOR STOP FITTING BEARING PLATE SHEARED OFF. REMOVED DAMAGED STOP FITTING. REPLACEMENT PART OSTF H5142. REPLACED STOP FITTING.

Part: BEARING — DEFECTIVE (L2 DOOR HANDLE) · airframe 61,310 hrs · 21,747 cycles

CREW REPORTED DOOR 2L INTERIOR HANDLE WILL NOT GO TO FULLY CLOSED POSITION WHEN DOOR IS CLOSED FROM THE OUTSIDE. FOUND DOOR 2L EXTERIOR HANDLE CAM FOLLOWER BEARING DEFECTIVE. MOUNT ASSY ON AOG B1522. RPLC'D CAM FOLLOWER, NO HELP. OBSERVED SLOP BETWEEN INNER & OUTER HANDLES. REMOVED HANDLE MECHANISM. INSTALLED DOOR HANDLE MECHANISM. OPERATED NORMAL. DOOR LATCHES WITH EXTERNAL HANDLE.

Part: LANYARD — UNSECURE (R1 DOOR SLIDE) · airframe 60,993 hrs · 21,636 cycles

DOOR 1R SLIDE LANYARD HANGING BELOW BUSTLE. SECURED LOOSE LANYARD.

Part: BEARING — FAILED (TRACK TRACK) · airframe 60,789 hrs · 21,564 cycles

NR 5 MAIN TRACK- RT INBOARD FLAP INBOARD TRACK, FORWARD ATTACH POINT BEARING FAILED AND IS LOOSE FROM TRACK ASSY, TRACK HAS SHIFTED INBOARD AND IS AGAINST SUPPORT BRACKET WITH FLAPS DOWN. TRACK IS CAPTURED BY SUPPORT BRACKET WITH AND CAN NOT MOVE FURTHER. REMOVED WORN BUSHING, REAMED BORE FWD END FLAP AND INSTALLED RPR SLEEVE. REINSTALLED FLAPS AND FLAPS OPS CHECK GOOD.

Part: CYLINDER — OUT OF ALIGNMENT (R2 DOOR) · airframe 60,789 hrs · 21,564 cycles

MAIN CABIN R-2 DOOR RED BAND ON EMERGENCY POWER SPRING CYLINDER NOT ALIGNED. ADJUSTED MAIN CABIN DOOR 2R EMERGENCY POWER SPRING CYLINDER. DOOR OPS NORMAL.

Part: FITTING — BINDING (R2 DOOR) · airframe 60,789 hrs · 21,564 cycles

DOOR 2R ARM-DISARM LEVER BINDING SEVERELY, DOOR WILL NOT ARM. ADJUSTED DOOR 2R FLOOR FITTINGS REF MM, OPS CHECKED GOOD.

Part: MECHANISM — OUT OF ADJUST (R1 DOOR) · airframe 60,789 hrs · 21,564 cycles

DOOR 1R FAILED MIDWAY CHECK. ADJUSTED DOOR 1R MODE SELECT LOCKOUT MECHANISM. MIDWAY CHECKS GOOD REF MM.

Part: SKIN — DAMAGED (BS 683 S2-3L) · airframe 60,789 hrs · 21,564 cycles

UPPER EXTERNAL FUSELAGE HAS LIGHTNING STRIKES AT BS 683, STR 2L TO STR 3L. THE DAMAGE CUT-OUT IS TOO CLOSE TO A STRINGER AND THE SRM DOES NOT PROVIDE REPAIR INSTRUCTIONS. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER DOUBLER RPR PER EVA80896 AND REO-G13681.

Part: MECHANISM — OUT OF ADJUST (R4 DOOR) · airframe 60,789 hrs · 21,564 cycles

DOOR 4R FAILS MIDWAY CHECK. ADJUSTED MAIN CABIN R-4 DOOR MODE SELECT LOCKOUT MECHANISM PER MM. OPS CHECK GOOD ON NON ROUTINE 29062.

Part: SHAFT — OUT OF TOLERANCE (R4 DOOR) · airframe 29,985 hrs · 13,213 cycles

DOOR 4R EXTERNAL HANDLE DOES NOT RETRACT OR STOW. REMOVED R-4 DOOR EXTERNAL HANDLE AND REPLACED CENTER SHAFT, YOKE, BEARING, CLUTCH COLLAR AND REGREASED PER MM. OPS CHECK GOOD ON NON ROUTINE 29063.

Part: PISTON — OUT OF ADJUST (L4 DOOR) · airframe 60,789 hrs · 21,564 cycles

MAIN CABIN L-4 DOOR RED BAND ON POWER SPRING CYLINDER PISTON NOT VISIBLE. ADJUSTED L-4 DOOR SPRING CYLINDER PISTON PER MM ON NON ROUTINE 29335.

Part: HINGE — WORN (R1 DOOR) · airframe 60,789 hrs · 21,564 cycles

R-1 DOOR CUTOUT UPPER HINGE BEARING WORN OUT. REMOVED UPPER HINGE LINK AND REPLACED HINGE LINK BEARING WITH NEW AND RE-INSTALLED HINGE LINK PER MM AND GN-MM 1-0-1-097.

Part: REGULATOR — OUT OF ADJUST (L2 DOOR SLIDE) · airframe 60,789 hrs · 21,564 cycles

DOOR 2L SLIDE RAFT SAFETY PIN WILL NOT GO ALL THE WAY IN. ADJUSTED MAIN CABIN L-2 DOOR SLIDE REGULATOR ASSY PER MM ON NON ROUTINE 29039 .

Part: BOTTLE — UNSERVICEABLE (R4 DOOR) · airframe 60,789 hrs · 21,564 cycles

MAIN CABIN, R-4 DOOR EMERGENCY POWER BOTTLE DATE OF MANUFACTURE NOT VISIBLE, HYDROSTATIC TEST DATE EXPIRED AS NOTED ON ROUTINE JIC 5R52I8050. REPLACED R-4 DOOR EMERGENCY POWER RESERVOIR BOTTLE PER MM ON NON ROUTINE 29382.

Part: VALVE — OUT OF ADJUST (R4 DOOR SLIDE) · airframe 60,789 hrs · 21,564 cycles

DOOR 4R EMERGENCY ESCAPE SLIDE SAFETY PIN CANNOT BE INSERTED INTO THE INFLATION CYLINDER VALVE. ADJUSTED MAIN CABIN DOOR R -4 ESCAPE SLIDE VALVE ASSY PER MM ON NON ROUTINE 29134.

Part: DOOR — OUT OF ADJUST (R2) · airframe 60,789 hrs · 21,564 cycles

DOOR 2R FAILS MIDWAY CHECK. ADJUSTED MAIN CABIN R-2 DOOR MODE SELECT LOCKOUT MECHANISM PER MM AND DOOR OPS CHECKED GOOD ON NON-ROUTINE 29061.

Part: CIRCUIT CARD — FAULTY (FIRE WARNING) · airframe 60,488 hrs · 21,457 cycles

NO SOUND ON FIRE WARNING TEST. REPLACED AURAL WARN PWR SUPPLY B, NO HELP. NO CLAXON WITH FIRE TEST. RPL'D CARD M10224. SYS OPS CKS OKAY.

Part: CIRCUIT CARD — FAULTY (FIRE DETECTION) · airframe 60,440 hrs · 21,439 cycles

FIRE BELL AURAL WARNING WILL NOT EXTINGUISH. REPLACED M1000 BELL-CHIME AURAL WARNING CARD ASSY PER MM. CHECKS OKAY. ALSO REPLACED WARNING ELECTRONICS POWER SUPPLY MODULE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,345 hrs · 21,399 cycles

DOOR NR 2 LT OUTBD EMERGENCY EXIT LIGHT INOP. RELAMPED, OPERATES NORMAL.

Part: MODULE — FAULTY (FIRE WARNING) · airframe 60,105 hrs · 21,319 cycles

FIRE BELL FAILED TO RING DURING FIRE OVERHEAT TEST. SUPPLEMENTAL DATA UPDATE OTHER FIRE INDICATIONS NORMAL. REPLACE THE BELL-CHIME AURAL WARNING MODULE M1000. REPAIRED PUSH BACK PIN ON P51 M10 00 REF WDM31-51-21 PIN 10 AND 50 WERE SECURED IN D113. REPLACED M1000 CARD AND PWR SUPPLY MOD M616 PER MM. PERFORMED ALL TEST EICAS SYS, TO WARN , MC WARN, AURAL WARN AND LDG CONFIG CHKS. ALL TEST PASS.

Part: BEARING — WORN (L1 DOOR) · airframe 62,443 hrs · 22,168 cycles

L1 DOOR UPPER HINGE AND BODY TORQUE TUBE BEARINGS ARE WORN MAKING DOOR HARD TO CLOSE. DOOR WILL STILL OPEN AND CLOSE MORE THAN NORMAL FORCE NEEDED TO BE USED. DOOR UPPER LATCHING CAM PLATES AND ROLLERS DAMAGED. REPLACED LATCH CAM AND UPPER FWD ROLLER BEARING PER IPC AND RIGGED. DOOR UPPER LATCH AND ROLLER'S GALLED. FOUND BODY TORQUE TUBE UPPER HINGE LINK ASSEMBLY AND BEARINGS WORN AND UPPER DOOR HINGE ARM TO HINGE LINK WORN. CAUSING UPPER SECTION OF DOOR TO HANG INBOARD PREVENTING UPPER LATCH ROLLERS FROM ENGAGING PROPERLY. UPPER ROLLER AND UPPER LATCH WAS REPLACED AND RIGGED.

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 58,871 hrs · 20,866 cycles

NR 6 SPOILER HAS RUNNING HYD LEAK WITH PRESSURE ON AND SPOILERS STOWED. LEAK IS RUNNING FROM CAP 550 AND O-RING 555. REPLACED NR 6 SPOILER PCA IAW MM.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,970 hrs · 20,544 cycles

SKIN DENT AT STA 760 STR 15 LT AFT OF DOOR 2L. DENT IS 3.5 INCHES ABOVE STR 15L AND .625 INCH AFT OF STA 760L. OK IAW EVA 73942 WILL BE REPAIRED AT NEXT HO3 VISIT.

Part: STATIC LINE — DEFECTIVE (R4 DOOR) · airframe 57,607 hrs · 20,407 cycles

F/A OPENED AFT RT DOOR AND SLIDE DID NOT DEPLOY BUT CAME OUT OF HSG. SAMC TEXT: SLIDE PARTIALLY DEPLOYED AND MUST BE REPLACED. DOOR 4R SLIDE DID NOT COME OUT OF ASSY AND WAS FOUND TO BE SECURE. FOUND STATIC LINE EXCESS LENGTH CATCHING ON GIRT BAR MECHANISM. PERFORMED SERVICE TIP AND GIRT BAR MECHANISM TEST. SLIDE ARMING OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,680 hrs · 20,056 cycles

EXTERIOR EVAC LT INOP AT DR 2 LT. RELAMPED.

Part: GATE — CRACKED (MAIN ENTRY) · airframe 56,230 hrs · 19,906 cycles

MED 1 RT UPPER GATE HAS 2 CRACKS ON AFT SIDE OF GATE, CLOSE TO HINGE. REMOVED UPPER GATE FROM DOOR, DRILLED UP NEW GATE READY TO BE INSTALLED. REPLACED NR1 RT MED UPPER GATE ASSY.

Part: O-RING — LEAKING (EVAC SLIDE) · airframe 55,463 hrs · 19,584 cycles

LOW BOTTLE. LEAKING FROM GAUGE LOCK NUT. IMPROPER GAUGE SPACING. REMOVED GAUGE AND REPLACED O-RING AND BACK UP O-RINGS AND RE-INSTALLED GAUGE.

Part: OXYGEN MASK — NO TEST (COCKPIT) · airframe 55,585 hrs · 19,639 cycles

CAPTAIN'S O2 MASK DOES NOT TEST. SWAPPED CAPTAIN'S O2 BOX AND MASK WITH 1ST OBSERVER. FIRST OBSERVER'S SEAT AND ASSOCIATED EQUIPMENT INOP. REPLACED 1ST OBSERVER O2 MASK, TESTS NORMAL.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 55,463 hrs · 19,584 cycles

PASSENGER ENTRY-SERVICE DOORS R AFT ESCAPE SLIDE PRESSURE BELOW GREEN BAND. REPLACED DOOR 2R PASSENGER DOOR SLIDE ASSY. INSPECTED OF DOOR 2R ESCAPE SLIDE INSTALLATION.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 54,700 hrs · 19,293 cycles

FLASHLIGHT AT 1L INOPERATIVE. REPLACED FLASHLIGHT AND BATTERY OPERATED NORMALLY.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 50,340 hrs · 17,657 cycles

DAMAGE FOUND 4 FT AFT AND ONE FOOT ABOVE DOOR SILL AT DOOR 4R. ACCOMPLISHED MAJOR REPAIR AT SFO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 50,340 hrs · 17,657 cycles

CREW REPORTS FUSELAGE HAS A DENT AND SCRATCH BELOW AND FORWARD OF DOOR 2LH. BURNISHED AREA AND CHECKED FOR CRACKS, NONE FOUND. ACCOMPLISHED HFEC, NO CRACKS NOTED. ALODINE AND PAINT, PERMANENT REPAIR TO BE PERFORMED BY NEXT "C" CHK.

Part: GIRT BAR — DIRTY (L3 DOOR) · airframe 49,918 hrs · 17,502 cycles

CREW REPORT: DOOR 3L WILL NOT DISARM. FOUND DIRT ACCUMULATION UNDER GIRT BAR. CLEANED AREA UNDER GIRT BAR, OPS NORMALLY.

Part: COMPUTER — MALFUNCTIONED (ELEVATOR FEEL) · airframe 48,904 hrs · 17,159 cycles

CREW REPORTS ON APPROACH AT APPROX 20 FT EXCESSIVE FORCE REQUIRED TO FLAIR ELEVATOR. REQUIRED THREE TIMES THE FORCE THAN NORMAL. ACCOMPLISHED ELEVATOR FEEL SYSTEM FORCE TEST AND FOUND FEEL COMPUTER LEAKING AND FORCES NOTICEABLY DIFFERENT WITH LEFT AND RIGHT SYSTEM PRESSURIZED. REMOVED AND REPLACED THE ELEVATOR FEEL COMPUTER.

Part: INDICATOR — SPLIT (COCKPIT) · airframe 48,672 hrs · 17,084 cycles

FLAP INDICATORS ARE SPLIT. SPLIT IN MOTION AND AT 1-5-15. RT FLAP INDICATION NEEDLE LAG BEHIND ONE NEEDLE WIDTH. REPLACED FLAP POSITION INDICATOR / TRANSMITTER.

Part: TRANSCEIVER — FAILED (WX SYSTEM) · airframe 48,250 hrs · 16,928 cycles

RTFL DUE TO WEATHER RADAR FAILURE. [08-07-07] REPLACED WX RADAR TRANSCEIVER.

Part: GIRT BAR — STIFF (3R DOOR) · airframe 47,852 hrs · 16,781 cycles

DOOR 3R DOOR ARM DISARM SWITCH VERY STIFF AND DIFFICULT TO USE. [SUP 06-06-07] REMOVED SLIDE LUBED MECHANISM TO ALLEVIATE THE STIFFNESS CONDITION.

Part: LANYARD — UNSECURE (R4 DOOR) · airframe 47,673 hrs · 16,714 cycles

DOOR 4R WILL NOT ARM. [06-14-07] SECURED SLIDE LANYARD: OPS CHK GOOD.AND ARMS NORMAL

Part: BOTTLE — READS LOW (DOOR 1L) · airframe 47,342 hrs · 16,599 cycles

SLIDE AT DOOR 1L BOTTLE PRESSURE LOW. [SUP 05-08-07] WATER VALVE TESTED FOR LEAKS. FOUND THE SEAL WAS BROKEN INSIDE THE GAUGE AND BECAME NON-SERVICEABLE. REMOVED AND REPLACED GAUGE.

Part: FEEDER CABLE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,268 hrs · 16,572 cycles

FOUND EEL LIGHTS INOP IN FWD CABIN FROM ROW 1-6. REPLACED EEL CABLE.

Part: O-RING — LEAKING (SLIDE BOTTLE) · airframe 46,364 hrs · 16,223 cycles

LOW BOTTLE PRESSURE. *S/D* LEAKAGE FOUND THROUGH GAUGE BACKUP O-RING AND THE SECOND O-RING. REPLACED BACKUP O-RING & SECOND O-RING.

Part: SLIDE — READS LOW (DOOR 2L) · airframe 46,364 hrs · 16,223 cycles

DOOR 2L SLIDE PRESSURE LOW. DOOR 2L SLIDE PRESS LOW. REPLACED NR 2L SLIDE RAFT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,678 hrs · 15,974 cycles

LT MAIN TANK TRANSFERRED INTO CENTER TANK. FLT CREW BURNED CENTER TANK DOWN TO 800...ONE HR LATER IN CRUISE CENTER TANK SHOWS 1500# INDICATING FUEL TRANSFER. ACCOMPLISHED SUCCESSFUL TEST 4 OF THE FUEL SCAVENGE SYSTEM. CAUSE OF DISCREPANCY WAS NOT ESTABLISHED.

Part: WARNING MESSAGE — ILLUMINATED (SPOILERS) · airframe 44,980 hrs · 15,724 cycles

SPOILER EICAS CAUTION ILLUMINATED AT CRUISE. NO YAW OR ROLL . FOUND INTERMITTENT, IN CRUISE PCA 12 FAULT ..... M317... ON SCM 1 LEFT...M530... SECOND HIT IN 9 TRIPS. REPLACED SPOILER CONTROL MODULE 1 LEFT.

Part: LIGHT — INOPERATIVE (LAVATORY) · airframe 43,902 hrs · 15,311 cycles

EEL STRIP INOP AT AFT LAV.

Part: O-RING — LEAKING (INFLATION VALVE)

LOW SLIDE PRESSURE. PRESSURE LOSS WAS DUE TO LEAKAGE AT RESERVOIR TO VALVE O-RING. O-RING WAS REPLACED.

Part: WARNING LIGHT — ILLUMINATED (DOOR WARNING) · airframe 39,855 hrs · 13,822 cycles

ABORTED TAKEOFF AT 110 KTS DUE TO A DOOR EICAS INDICATION.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,644 hrs · 13,749 cycles

AFT PIT FUSELAGE FRAME INBOARD FLANGE DENTED AT BS 1420 STR 25L TO STR 26L. INSTALLED J-ANGLE REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,644 hrs · 13,749 cycles

FUSELAGE SKIN AND STRINGER BELOW THE AFT ENTRY DOOR IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIRED SKIN DOUBLER , TRIPLER, & FILLER. SPLICED IN NEW STRINGER SECTION.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,644 hrs · 13,749 cycles

STA 1460 FRAME HAS DENT IN THE UPPER FLANGE AT STR 26L. DAMAGE WAS CUTOUT AND A FRAME "J" ANGLE REPAIR ACCOMPLISHED.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,644 hrs · 13,749 cycles

DENT ON INNER FRAME CHORD AT STA 660 NEAR STR-24L. CAUSED BY TYPICAL CARGO LOADING. "J" ANGLE REPAIR WAS ACCOMPLISHED.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 39,644 hrs · 13,749 cycles

CABIN CREASE BEAM ANGLE CORRODED AT FS 1410 LBL 68. DAMAGED CAUSED BY TYPICAL CABIN CORROSION. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR ANGLE AND FILLER.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 39,644 hrs · 13,749 cycles

EXTERNAL FUSELAGE SKIN CREASED AT BS 1705 BETWEEN STR 15L & 16L. INSTALLED FILLER, DOUBLER & TRIPLER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,644 hrs · 13,749 cycles

MAIN CABIN STA 330 BETWEEN STR 10R & STR 11R, FRAME INBD FLANGE CRACKED. FABRICATED & INSTALLED NEW SECTION OF FRAME.

Part: FRAME — DAMAGED (FUSLEAGE) · airframe 39,644 hrs · 13,749 cycles

AFT PIT FRAME UPPER FLANGE HAS ELONGATED HOLE AT BS 1620 BETWEEN STR 29L & STR 30L. INSTALLED REPAIR DOUBLER & FILLER.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,644 hrs · 13,749 cycles

AFT PIT FRAME UPPER FLANGE DENTED AT BS 1400 STR 25L & STR 26L. INSTALLED J ANGLE REPAIR.

Part: FRAME — DENTED (FUSELAGE) · airframe 39,644 hrs · 13,749 cycles

AFT PIT FRAME INNER FLANGE IS DENTED AT BS 1440 STR 26L. INSTALLED J ANGLE REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,644 hrs · 13,749 cycles

FLOORBEAM AT STA 365 BL0 TO RBL15 CORRODED. REMOVED CORROSION AND INSTALLED FLOOR BEAM REPAIR.

Part: PDU — FAILED (SLATS) · airframe 37,093 hrs · 12,914 cycles

FLIGHT RETURNED TO FIELD WITH A LEADING EDGE SLAT DISAGREEMENT MESSAGE. LEFT PDU TORQUE LIMITER TRIPPED. REPLACED LEFT LEADING EDGE POWER DRIVE UNIT.

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 37,050 hrs · 12,900 cycles

ON FLAP RETRACTION THE L/E FLAP DISAGREE EICAS MESSAGE ILLUMINATED. EXCESSIVE TORQUE FORCES IN THE LE SLAT DRIVE SYSTEM INITIATED A LE SLAT DISAGREE FAULT WHICH WAS DETECTED BY THE FLAP/SLAT ELECTRONIC UNIT (FSEU) LE SLAT MOVEMENT IS AUTOMATICALLY INHIBITED BY HYDRAULIC BYPASS TO PREVENT DAMAGE TO ASSOCIATED LE SLAT DRIVE COMPONENTS. THE NR 6 AND 15 LE SLAT DRIVE ROTARY ACTUATORS WERE FOUND TO HAVE TRIPPED TORQUE OVERLOAD INDICATORS. THE NR 6 AND 15 LE SLAT DRIVE ACTUATORS WERE REPLACED. THE DRIVE TRANSMITTER IN THE LE SLAT POWER DRIVE UNIT (PDU) WAS ALSO REPLACED.

Part: STRINGER — DENTED (FUSELAGE) · airframe 36,026 hrs · 12,546 cycles

FUSELAGE STRINGER S-20L DENTED AT BS 1690 LAP. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,026 hrs · 12,546 cycles

FUSELAGE SKIN DENTED AND CRACKED AT STA 1600 AND STR 19L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: STRINGER — DENTED (FUSELAGE) · airframe 36,026 hrs · 12,546 cycles

STRINGER DENTED AT STATION 1600, STRINGER 19L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,026 hrs · 12,546 cycles

FUSELAGE SKIN DENTED AT BS 1690 AND STRINGER S-20L LAP. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: SKIN — DENTED · airframe 33,541 hrs · 11,653 cycles

LEFT HAND FUSELAGE STATION 613 AND 617 BELOW STRINGER 16 SKIN DENTED BELOW PREVIOUS INSTALLED REPAIR DOUBLER. MAJOR REPAIR ACCOMPLISHED.SKIN DOUBLER REPAIR INSTALLED.

Part: CDU — FAILED (COCKPIT) · airframe 26,374 hrs · 9,048 cycles

FIRST OFFICER CONTROL DISPLAY UNIT CDU FAILED PRIOR TO CLASS II AIRSPACE. *S/D* REPLACED FIRST OFFICERS CDU PER AMM, CHECKS OK.

Part: SENSOR — DIRTY (WING SLIDE)

RETURNED TO EWR DUE TO EICAS WING SLIDE MESSAGE. LEFT OFF-WING SLIDE COMPARTMENT DOOR FOUND CLOSED. DOOR SENSOR S283T006-10 WAS FOUND TO BE DIRTY. SENSOR WAS CLEANED, AND TESTED GOOD.

Part: FUEL CONTROL — MALFUNCTIONED (RT ENGINE)

ON TAKEOFF, MAX POWER OF 1.42 EPR SET, LEFT ENGINE WAS 1.42. RIGHT ENGINE 1.38 TO 1.39 EPR. RIGHT ENGINE FUEL FLOW SEVERAL HUNDRED POUNDS LESS THAN LEFT ENGINE. LEFT ENGINE HAD THROTTLE REMAINING. RIGHT ENGINE THROTTLE AGAINST THE FIREWALL.

Part: TUBE — LEAKING (SLIDE RAFT)

DURING SHOP OVERHAUL OF SLIDE/RAFT, FOUND THAT LOWER TUBE RELIEF VALVE HAD WORN A HOLE IN THE LOWER TUBE DOG LEG AND THROUGH TO THE UPPER TUBE REPAIRED HOLE IN DOG LEG WITH A PATCH ON THE OUTSIDE. REPAIRED HOLE BETWEEN LOWER AND UPPER TUBES WITH A PATCH ON THE INSIDE OF THE LOWER TUBE.

Part: COMPRESSOR BLADE — BROKEN (LT ENGINE)

LEFT ENGINE HAD 2 COMPRESSOR STALLS AT ALTITUDE. FLIGHT DIVERTED TO ICT. *S/D* BROKEN 9TH STAGE COMPRESSOR BLADE. SCRAPPED ALL 6TH THROUGH 17TH STAGE BLADES AND REPLACED WITH NEW.

Part: LIGHT — INOPERATIVE (CABIN)

LEFTSIDE, FORWARD OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED INOP OVERWING EMERGENCY EXIT LIGHT, OPERATION CHECKS NORMAL.

Part: TOP TUBE — LEAKING (SLIDE/RAFT)

SLIDE RAFT REMOVED FOR FIRST TIME. CONTROLLED OVERHAUL AND FAILED AIR RETENTION TEST. SLIDE RAFT HAD POROSITY AT ALL SEAMS AND A SEAM LEAK AT THE TOP TUBE. RETURNED FAULTY SLIDE RAFT TO ORGINAL EQUIPMENT MANUFACTURER FOR WARRANTY REPAIR.

Part: TURBINE BLADE — FAILED (LT ENGINE)

DURING CLIMBOUT, LEFT ENGINE HAD A COMPRESSOR STALL WITH RISING EGT, MAXIMUM 657C. POWER WAS REDUCED TO IDLE AND EGT STABLIZED AT 550C, RETURNED TO DEN. INSPECTED ON GROUND, FOUND METAL IN THE TAILPIPE. ENGINE DISASSEMBLY FOUND A FAILED T-1 HIGH PRESSURE TURBINE BLADE.

Part: COMPRESSOR — STALLED (LT ENGINE)

ON CLIMBOUT, LEFT ENGINE HAD COMPRESSOR STALL WITH RISING EGT, MAX REACHED 657C. POWER REDUCED TO IDLE EGT STABLIZED AT 550C, LANDED OVERWEIGHT.

Part: COMPRESSOR — STALLED (LT ENGINE)

LEFT ENGINE COMPRESSOR STALL ON TAKEOFF OUT OF EWR AT 1,000 FT, HEARD ONE BANG. ENGINE INDICATIONS DID NOT CHANGE. DURING REMAINDER OF FLIGHT, ALL ENG OPERATIONS NORMAL. ENGINE WAS BORESCOPED AND FOUND WITHIN LIMITS, ACCOMPLISHED HIGH POWER RUN, ACCELERATION AND DECELERATION CHECKS AND ALL PARAMETERS WITHIN LIMITS. CHECKED ENGINE INLET, EXHAUST AND CHIP DETECTOR, NO DISCREPENCIES FOUND.