N525UA

Part: SWITCH — FAULTY (LT MLG DOOR) · airframe 75,581 hrs · 22,790 cycles

LEFT MAIN LANDING GEAR DOOR UNSAFE LIGHT STAYS ON WITH DOOR CLOSED. REPLACED LEFT GEAR DOOR CLOSED SWITCH S10371 REF WDM-32-12-12 AND AMM. DOOR NOW OPERATES NORMAL.

Part: SKIN — CORRODED (RT WING) · airframe 74,972 hrs · 22,673 cycles

ON RIGHT WING PERFORM STEP 1. REMOVE EXISTING FASTENERS LOCATED IN THE CORRODED AREAS. REF AVO ESC120524-5325-1. REMOVED 6EA FASTENERS LOCATED IN CORRODED AREA TOP RIGHT WING. REAMED 6 EA FASTENERS TO 1ST OVER, .324". REAMED 6EA FASTENER HOLES TO 2ND OVER REF AVO. HFEC INSP ACCOMPLISHED. 6EA FASTENERS INSTALLED AND NUTS CAP SEALED REF AVO.

Part: SKIN — DAMAGED (RT WING) · airframe 74,972 hrs · 22,673 cycles

MEASURE THE REMAINING SKIN THICKNESS IN THE BLEND OUT AREAS AND RECORD IT ON THE WING SURFACE. REF AVO ESC120524-5325-1. RIGHT WING REWORKED AREAS: 4 EACH, SKIN THICKNESS MEASURMENTS IN THOUSANDS OF AN INCH: BY LOCATION, WBL 90 & 90 INCHES FROM TRAILING EDGE, ORIG THICKNESS .170" REMOVED .002", WBL 87 & 6" FROM T/E, ORG THICKNESS .230" REMOVED .006", WBL 121-129, 13" FROM T/E .263 ORG THICKNESS REMOVED .010". 4 EACH, SKIN THICKNESS MEASURMENTS IN THOUSANDS OF AN INCH. LOCATION, WBL 90& 90INCHES FROM TRAILING EDGE, ORIG THICKNESS . 170" REMOVED.002", WBL 87& 6"FROM TE,ORG THKNESS .230" REMOVED .006", WBL121-129,13" FROM TE .263 ORG THICKNESS REMOVED .010" SKIN THICKNESS MEASURMENTS, RT WING SURFACE, LAST REWORK AREA: WBL 126-131, 2" FROM TE, .385 ORIG, REMOVED .010", USING 757NDT PART 4 51 00 10 & AVOESC 120524-5325-1.

Part: STRUCTURE — CORRODED (RT WING) · airframe 74,972 hrs · 22,673 cycles

ACP INSPECTION OF RIGHT WING CORROSION REWORK ROTO PEEN, PEENING SATISFACTORY USING SOPM 20 10 03 AND AVO ESC 120524-5325-1. ACCOMPLISH RII INSPECTION OF AMIS ITEM 9722017 :ACCOMPLISHED ROTO PEEN .REF SOPM 20-10-03.

Part: STRUCTURE — CORRODED (LT WING) · corrosion level 2 · airframe 74,972 hrs · 22,673 cycles

LEFT UPPER WING, REMOVED CORROSION AT 57\ O/B OF BBL 70.5 AND 8\ FWD OF REAR SPAR. REMOVED APPROX .010\ MAT AND TREATED AREA WITH ALODINE. CORR DID NOT GO INTO FASTENER AND FASTENER OKAY REF AVO ENC120524-5325-1. INSPECTED AREA WBL 139.0 USING 757 NDT PART 4 51 00 00 AND MEASURED .007 INCH, REMOVED FOR CORROSION, ORIG THICKNESS .330 INCH NO LAMINAR CORROSION FOUND, USING AVO ENC120524-5325-1 ITEMS 4 & 5.

Part: STRUCTURE — DAMAGED (LT WING) · airframe 74,972 hrs · 22,673 cycles

ON LEFT WING PERFORM ITEM 2. BLEND SMOOTH PER 757 SRM 57-20-01, ALLOWABLE DAMAGE 1, FIGURE 101, DETAIL 1. REF AVO ESC120524-5325-1. REMOVED CORR AND SMOOTH OUT AREA, WITHIN LIMITS REF SRM 57-20-01M AND AVO ESC120524-5325.

Part: STRUCTURE — CORRODED (RT WING) · airframe 74,972 hrs · 22,673 cycles

ON RIGHT WING PERFORM STEP 8. FLAP PEEN THE BLEND AREA PER SOPM 0-10-03 WITH FADE-OUT 1 INCH BEYOND THE REWORKED AREA. REF VO ESC120524-5325-1. ACCOMPLISHED ROTO PEEN REF SOPM 20-10-03. ACP INSP OF RT WING CORROSION REWORK ROTO PEEN, PEENING SATISFACTORY USING SOPM 20 10 03 AND AVO ESC 120524-5325-1.

Part: SKIN — DAMAGED (LT WING) · airframe 74,972 hrs · 22,673 cycles

ON LEFT WING PERFORM STEP 5. MEASURE REMAINING SKIN THICKNESS IN THE BLEND OUT AREAS AND RECORD IT ON THE WING SURFACE. REF AVO ESC120524-5325-1. BY- 92992 AT REWORK AREAS: WBL 150.5 NORMAL THICKNESS .424 INCH, .016 INCH REMOVED FOR CORROSION. IN REWORK AREA WBL 139.0 NORMAL THICKNESS .330 INCH, .007 INCH REMOVED FOR CORROSION.

Part: STRUCTURE — CORRODED (LT WING) · corrosion level 2 · airframe 74,972 hrs · 22,673 cycles

LEFT UPPER WING, REMOVED CORROSION AT REAR SPAR, 69.5\ O/B OF BBL 70.5. REMOVED APROX .020\ MAT AND ALODINE AREA. CORR DID NOT GO INTO FASTENER. FASTENER OKAY. INSPECTED REWORK AREA WBL 150.5, .016 INCH MATERAL REMOVED FOR CORROSION FROM .424 INCH ORIG THICKNESS, FASTENER NOT AFFECTED, NO LAMINAR CORROSION FOUND, USING 757 NDT PART 4 51 00 00 AND AVO ESC120524-5325-1.

Part: STRUCTURE — CORRODED (LT WING) · corrosion level 2 · airframe 74,972 hrs · 22,673 cycles

ON LEFT WING PERFORM ITEM 1 - REMOVE EXISTING FASTENERS IN THE CORRODED AREAS REF AVO NUMBER ESC120524-5325-1. FASTENERS NOT AFFECTED BY REWORK PROCESS USING AVO ESC120524-5325-1. ACCOMPLISHED ROTO PEEN AS PER ABOVE. ROTO PEEN SATISFACTORY USING SOPM 20 10 03 AND AVOESC120524-5325-1.

Part: STRAP — UNSECURE (R4 DOOR) · airframe 73,993 hrs · 22,470 cycles

DOOR 4R SLIDE PACK COVER LATCH STRAP IS ROUTED INCORRECTLY THRU LOWER SLIDE PACK HARNESS LATCH. STATIC LINE LOOP NOT ON GIRT BAR. SECURED STRAP PER MM 25-6 6-01-401 AND MM 52-11-25-501. SECURED PER MM 25-66-01-4 01 AND MM 52-11-25-501.

Part: WIRE HARNESS — DAMAGED (EGT) · airframe 73,026 hrs · 22,285 cycles

FOUND DAMAGE TO EGT HARNESS WIRE AND BROKEN GROUND WIRE EVALUATING REPAIRS. HARNESS 585-4989 AND 564-1252 ON AOG. REPLACED WIRING HARNESS & WIRE BUNDLE.

Part: PANEL — CRACKED (NR 2 SLAT) · airframe 71,333 hrs · 21,958 cycles

FOUND A CRACK ON THE NR 2 LEADING EDGE SLAT COVE PANEL, CRACK IS LOCATED ON THE OUTBD COVE PANEL INBD SIDE IN THE MIDDLE AND THRU A FASTENER, CRACK MEASURES 1 AND 1-4TH OF AN INCH. FOUND NR 2 SLAT WITH A 1.5 INCH CRACK ON THE O/B COVE SKIN PANEL. REMOVED NR 2 LEADING EDGE SLAT. REPAIRED NR 2 LEADING EDGE SLAT. OPS CHECKED GOOD.

Part: TERMINAL BLOCK — LOOSE (WINDSHIELD HEAT) · airframe 70,193 hrs · 21,737 cycles

WITH NO OTHER INDICATIONS NOTED SMELLED AN ACRID ODOR TWO TIMES WITHIN 10 MINUTES. THERE WAS NO REPEAT, NO SMOKE OR OTHER INDICATIONS ANYWHERE IN THE COCKPIT OR CABIN. CALLED DD AND MM. REPORTED ODOR WAS COMING FROM GLARESHIELD AREA. MM ACCOMPLISHED VISUAL OF FLT DECK OVERHEAD CB PANELS, E&E COMPT, WINDSHLD HEAT WIRING, ALL FLT DECK LIGHTING. DURING TROUBLESHOOTING OF COCKPIT ODOR, FOUND CAPT WINDSHIELD POWER TERMINAL BLOCK ON TOP LEFT CORNER LOOSE. REPLACED CAPTAIN'S WINDSHIELD. ALL OTHER WIRING WAS FOUND OKAY. PRECAUTIONARY REMOVED HIGH STAGE DUCT FROM NR 1 ENG TO EXAM FOR POSSIBLE OIL. FOUND DUCT CLEAN AND DRY.

Part: DOOR — DAMAGED (R4) · airframe 70,179 hrs · 21,734 cycles

DOOR 4R APPEARS TO HAVE DAMAGE ON LOWER CORNER. REMOVED LEVELING COMPOUND, REMOVED LOWER LATCHING TORQUE TUBE AND FASTENERS COMMON TO REPAIR AREA, CUT OUT DAMAGE WILL REQUIRE EDDY CURRENT INSP REF SRM 52-10-01 REPAIR 7. EDDY CURRENT ACP, RPR DOUBLER MANUFACTURED & INSTALLED, CATEGORY B RPR WILL REQUIRE INTERVAL INSPECTION EVERY 3000 FLIGHT CYCLES REF SRM 52-10-01 REPAIR 7 PG 210 ** MF7627 CREATED TO MONITOR ***

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,928 hrs · 21,686 cycles

DURING C-6 VISIT, SKIN DOUBLER RPR INSTALL AT UPPER ANTI-COLLISION LIGHT, STA 569-598 PER REO-G13640, STR 2L-2R. THIS RPR HAS RECEIVED 1ST STAGE APPROVAL ONLY. MUST RECEIVE NEW DTA BEFOR 09-MAY-2013. IF NEW 8100-9 IS NOT ISSUED IN 24 MONTHS, A-C IS NO LONGER AIRWORTHY.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 69,928 hrs · 21,686 cycles

LIGHTNING STRIKE AT BS 575, STR 1L, DAMAGE BLEND OUT EXCEEDS SRM LIMITS AND REQUIRES A REPAIR. INSTALLED DOUBLER RPR PER REO G13640 AND EVA 80839.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,928 hrs · 21,686 cycles

UPPER FUSELAGE LIGHTNING STRIKE AT BS 480, STR 1L AND REQUIRES REPAIR DUE TO PREVIOUSLY INSTALLED BLIND FASTENERS NOT OUT OF TOLERANCE. INSTALLED DOUBLER RPR PER TIMCO REO-G13640 AND EVA 80839.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,928 hrs · 21,686 cycles

SKIN DOUBLER RPR INSTALLED ON CROWN STA 473-490, STR 2L -2R PER REO G13640. THIS RPR HAS RECEIVED 1ST STAGE APPROVAL ONLY. ACCOMP DURING C-6 VISIT.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 69,928 hrs · 21,686 cycles

LIGHTNING STRIKES FOUND ON CROWN. MAJOR REPAIRS ACCOMPLISHED: 460 & 575 CROWN DBLR RPRS DONE, SKIN DOUBLER RPR INSTALL AT UPR ANTI-COLLISION LITE, STA 569-598 PER REO-G13640, STR 2L-2R. SKIN DOUBLER RPR INSTALLED ON CROWN STA 473-490, STR 2L -2R PER REO G13640. UPPER FUSELAGE LIGHTNING STRIKE AT BS 480, STR 1L AND REQUIRES REPAIR DUE TO PREVIOUSLY INSTALLED BLIND FASTENERS NOT IAW THE SRM. INSTALLED DOUBLER RPR PER REO-G13640 AND UAL EVA 80839. LIGHTNING STRIKE AT BS 575, STR 1L, DAMAGE BLEND OUT EXCEEDS SRM LIMITS AND REQUIRES A REPAIR. INSTALLED DOUBLER RPR PER REO G13640 AND UAL VA 80839.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 69,928 hrs · 21,686 cycles

EMERGENCY LIGHT STRIP AT G1B INOP. RECONNECTED EMERGENCY LIGHT STRIP AT G1B, OPS CHECKS GOOD.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 69,928 hrs · 21,686 cycles

EMERGENCY LIGHT STRIP AT G4B INOP. RECONNECTED EMERGENCY LIGHT STRIP AT G4B. LIGHT CHECKS GOOD.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 69,928 hrs · 21,686 cycles

FWD LAV SMOKE DETECTOR INOPERATIVE. REMOVED AND REPLACED FWD LAV SMOKE DETECTOR PER MM AND OPS CHECKED GOOD.

Part: LIGHT — MISSING (SEAT 19C) · airframe 67,889 hrs · 21,289 cycles

EMERGENCY LIGHT MISSING AT SEAT 19C. REPLACED EMERGENCY LIGHT, OPS CK OK.

Part: FLOORBOARD — FAULTY (CABIN) · airframe 65,009 hrs · 20,734 cycles

FLOORBOARD IN MIDDLE OF AISLE BETWEEN ROW 7 & 8 SPONGY. INSTALLED TEMP SHEETMETAL REPAIR. REPLACED FLOOR PANEL.

Part: BALLAST — ODOR (EMERGENCY LIGHTS) · airframe 63,790 hrs · 20,496 cycles

ELECTRICAL ODOR IN MID GALLEY, FLT DIVERTED. IN MID GALLEY RT OVERHEAD FOUND BALLAST M9033 CAUSING ELECTRICAL ODOR. INOP'D BALLAST TWO EA EMERGENCY LIGHTS IN GALLEY INOP. REPLACED M9033 BALLAST. LIGHT AND BALLAST CHECK OKAY.

Part: LIGHT — MISSING (CABIN) · airframe 63,635 hrs · 20,464 cycles

EEL LIGHT STRIP MISSING AT ROW 16 ABC. REPLACED LIGHT ASSY, OP CHECK OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,680 hrs · 20,273 cycles

CABIN SEAT 20 ABC, AISLE END BAY EEL LIGHTS ARE INOP. NEEDS LIGHT ASSY. REPAIRED LIGHT ASSY, SYSTEM RETURNED TO SERVICE.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 60,707 hrs · 19,903 cycles

REPAIR DOUBLER AT BS 610 IS DENTED BETWEEN STR 16L AND STR 17L. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED AREA, FABRICATED REPAIR, AND INSTALLED. REPAIR MADE IAW MM 53-30-92 PG 801.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 60,702 hrs · 19,902 cycles

FUSELAGE DAMAGE BY CABIN SERVICE TRUCK LEFT OF OUTFLOW VALVE. MAJOR REPAIR ACCOMPLISHED. SHEAR TIES BEING MFG IN SFO. RECEIVED STRINGER, DRILLING. CONT TO MFG DOUBLER & TRIPLER. ACCOMPLISHED REPAIR AT FRAME 1600 AND 1620 AND BETWEEN STRINGER 27L AND 28L. PERFORMED PERMANENT REPAIR.

Part: FITTING — DIRTY (GIRT BAR) · airframe 60,492 hrs · 19,862 cycles

DOOR 4R ESCAPE SLIDE GIRT BAR STILL ENGAGE NOTICED BY CATERING DURING DOOR OPENING. DIRT AND DEBRIS ACCUMULATION UNDER GIRT BAR. CLEANED AND LUBRICATED GIRT BAR FITTINGS. DOOR ARMS/DISARMS NORMALLY.

Part: LIGHT — MISSING (SEAT 26C) · airframe 60,298 hrs · 19,825 cycles

LIGHT ASSY AT 26C IS MISSING. LIGHT ASSY MISSING. INSTALLED NEW LIGHT ASSEMBLY. OPERATIONS CHECKED GOOD.

Part: LIGHT — MISSING (SEAT 3B) · airframe 59,881 hrs · 19,744 cycles

EMERGENCY EXIT LIGHT ASSEMBLY MISSING SIDE OF SEAT 3B.

Part: LIGHT — BROKEN (SEAT 15C) · airframe 59,881 hrs · 19,744 cycles

EMERGENCY EXIT LIGHT ASSEMBLY BROKEN AT SIDE OF SEAT 15C. *S/D* REPLACED EEL ASSY ON SEAT 15C. OPS CHECK OKAY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,605 hrs · 19,691 cycles

EMERGENCY LIGHT STRIP INOP ON LEFT SIDE OF A-C ROW 9. *S/D* LIGHT BATTERY PACK FAULTY, ALSO SUSPECT CHARGER IS WEAK. REPLACED EMERGENCY LIGHT BATTERY PACK CHARGER ASSY AND INVERTER, OP CHECKS OK.

Part: CYLINDER — CORRODED (LT MLG) · airframe 59,304 hrs · 19,633 cycles

GLAND NUT AND CARRIER CORRODED, REMOVED INNER CYL FOUND. EXTENSIVE CORROSION ON INNER SURFACE OF OUTER CYL. REPLACED LT MAIN LANDING GEAR, GEAR SENT TO SHOP FOR OVERHAUL.

Part: SENSOR — DIRTY (R4 DOOR) · airframe 59,123 hrs · 19,599 cycles

SLIDE ARMED INDICATOR LIGHT DOOR 3R BULB NOT LIT AFTER ARMING. DOOR SENSOR/SLIDER TARGET DIRTY. CLEANED DOOR SLIDER TARGET SENSOR, OPS CHECKED OK.

Part: KNOB — MISSING (COCKPIT) · airframe 58,216 hrs · 19,430 cycles

EMERGENCY EVACUATION PANEL HAS MISSING HORN SHUTOFF KNOB MISSING IN FLIGHT DECK COMPARTMENT. REPLACED EES PANEL, OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (EVAC SLIDE) · airframe 58,147 hrs · 19,417 cycles

SLIDE WILL NOT ARM LEFT AFT DOOR. LAMPS BURNT OUT. RELAMPED 2 EACH LIGHT BULBS IN SLIDE INDICATOR. OPS NORMAL.

Part: PROXIMITY SWITCH — DIRTY (R1 DOOR) · airframe 58,111 hrs · 19,409 cycles

DOOR 1R SLIDE LT DOES NOT ILLUMINATE W/ DOOR CLOSED. FOUND DIRT AND DEBRIS CAUSING JAMMING, PROX SWITCH ALSO DIRTY. CLEANED AREA AND PROX SWITCHES, SYSTEM OPS NORMAL.

Part: LIGHT — LOOSE (EXTERIOR) · airframe 55,862 hrs · 20,464 cycles

EMERGENCY LIGHT AT DOOR 4 RT INOP (EXT). LIGHT BULB VIBRATED LOOSE. SECURED LIGHT BULB AND OPS CHECKED GOOD.

Part: SKIN — DAMAGED (VERTICAL STAB) · airframe 57,498 hrs · 19,292 cycles

VERTICAL FIN DAMAGED ON CONTACT WITH HANGAR DOOR. PERFORMED A MAJOR REPAIR.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,354 hrs · 19,264 cycles

SKIN DENT AT STA 334, BETWEEN STR 24 AND 25R. MAJOR REPAIR ACCOMPLISHED.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 57,354 hrs · 19,264 cycles

AFT PIT AT BS 1440 BETWEEN STR 27R AND STR 28R, ANGLE DOUBLER IS CORRODED UNDER TRANSITION PANEL. MAJOR REPAIR ACCOMPLISHED: REMOVED SPLICE, FABRICATED & INSTALLED A NEW SPLICE REPAIR.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 57,354 hrs · 19,264 cycles

CABIN AT BS 1020, RBL 69, CUSP WEB CORRODED. MAJOR REPAIR ACCOMPLISHED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 57,354 hrs · 19,264 cycles

MAIN CABIN INTERCOSTAL APPEARS TO BE CRACKED 1.5 INCH AT BS 680 STRINGER 12L. MAJOR REPAIR ACCOMPLISHED: REPLACED INTERCOSTAL.

Part: GATE — CORRODED (DOOR 4L UPPER) · airframe 57,354 hrs · 19,264 cycles

L4 DOOR UPPER GATE CORRODED. REMOVED & REPLACED GATE.

Part: FRAME — DENTED (BS 1460 S25-26L) · airframe 57,354 hrs · 19,264 cycles

AFT PIT STA 1460 BETWEEN STR 25L AND 26L FRAME DENTED. REMOVED DAMAGED AREA, FABRICATED REPAIR, AND INSTALLED A NEW DOUBLER.

Part: SKIN — CRACKED (L2 DOOR) · airframe 57,354 hrs · 19,264 cycles

L2 DOOR UPPER HINGE CUTOUT REQUIRES DOUBLER (NOT CRACKED). PRECAUTIONARY MAJOR REPAIR ACCOMPLISHED. PERFORMED HFEC PER NDT MANUAL. NO DEFECT NOTED. INSTALLED DOUBLER IN THE AREA.

Part: SKIN — CRACKED (R2 DOOR) · airframe 57,354 hrs · 19,264 cycles

R2 DOOR UPPER HINGE CUTOUT REQUIRES DOUBLER CRACKED. PERFORMED HFEC PER NDT MANUAL. FOUND 1 EA CRACK. REMOVED DAMAGED AREA AND INSTALLED DOUBLER IN THE AREA.

Part: SKIN — DENTED (BS 1480 S25L) · airframe 57,354 hrs · 19,264 cycles

AFT PIT STA 1480 STR 25L DENTED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED AREA, FABRICATED REPAIR, AND INSTALLED A NEW DOUBLER.

Part: SKIN — DENTED (BS 610 S16-17L) · airframe 57,354 hrs · 19,264 cycles

REPAIR DOUBLER AT BS 610 IS DENTED BETWEEN STR 16L-STR 17L. REMOVED DAMAGED AREA, FABRICATED REPAIR, AND INSTALLED A NEW DOUBLER.

Part: INTERCOSTAL — GOUGED (R1 DOOR) · airframe 57,354 hrs · 19,264 cycles

R1 DOOR WEB GOUGED BY UPPER HINGE ARM CUTOUT INTERCOSTAL STRUCTURE OF DOOR. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (BS 1520 S26L) · airframe 57,354 hrs · 19,264 cycles

AFT PIT FRAME STA 1520 STR 26L DENTED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED & INSTALLED REPAIR ANGLE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,555 hrs · 18,916 cycles

EEL LIGHTS INOP AT ROWS 5-8 & EXIT LIGHTS OVERWING DOORS. [06-22-07] REPLACED THE BATTERY ON BATTERY EMERG BATTERY CHARGER M10567 & OPS CHECK OK.

Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 54,132 hrs · 18,643 cycles

DOOR 4R AND 4L DOOR SIDEWALL EEL LIGHTS INOP. FOUND SHORT IN WIRING BETWEEN PINS A&B. FOUND FLOOR EEL LIGHT ON GALLEY WALL SATURATED WITH WINE CAUSING CONTAMINATION OF POWER FEEDER CABLE RESULTING SYSTEM TO BE INOPERATIVE. CLEANED CONTAMINATION. DID NOT REPLACE ANY MAJOR PART/COMPONENT.

Part: ASPIRATOR — LEAKING (ESCAPE SLIDE) · airframe 50,233 hrs · 17,884 cycles

ASPIRATOR FLAPPER VALVES LEAKING. ASPIRATOR WAS OBSERVED LEAKING DURING AIR RETENTION TEST. LEAK WAS DUE TO WORN ASPIRATOR FLAPPER VALVE. ASPIRATOR WAS REPLACED.

Part: SKIN — BIRD STRIKE (RT WING LE) · airframe 49,439 hrs · 17,731 cycles

BIRD STRIKE TO RIGHT OUTBOARD WING L/E. REPAIRED NR 10 LE SLAT NOSE SKIN PER SRM 57-43-01.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 44,860 hrs · 16,531 cycles

EEL STRIP IN FRONT OF LAV 108 INOP. SECURED LOOSE CONNECTOR.

Part: WEDGE — DELAMINATED (NR 6 SLAT)

LEADING EDGE DELAMINATED NR 6 SLAT WEDGE. MAJOR REPAIR. REPLACED WEDGE.

Part: WIRE — BURNED (WINDOW HEAT) · airframe 46,818 hrs · 17,255 cycles

WINDOW HEAT RT 1 INOP, FOUND WIRES ON TB5070 TERMINALS 4, 5 & 6 SEVERELY BURNED. ELECTRICAL POWER PANEL WIRES AT P-37 OVERHEATED AND BECAME LOOSE AT TERMINALS 4, 5, AND 6. REPLACED TERMINAL STRIP. REPAIRED AND RE-TERMINATED WIRES.

Part: INDICATOR — FAILED (AIRSPEED) · airframe 40,569 hrs · 14,975 cycles

CAPTAINS AIRSPEED INDICATOR FLAGGED. CAPTAIN'S MACH/AIRSPEED INDICATOR FAILED AND WAS REPLACED.

Part: BLADE — FAILED (STAGE 2 TURBINE) · airframe 40,441 hrs · 14,930 cycles

RT ENGINE EICAS MSG FOR FUEL FILTER. SUPPLEMENTAL DATA UPDATE AT ENGINE TEARDOWN, A STAGE 2 TURBINE BLADE FAILURE WAS FOUND TO BE THE CAUSE.

Part: HYDRAULIC SYSTEM — FAILED (LEFT) · airframe 39,127 hrs · 14,428 cycles

LOSS OF LEFT SYSTEM HYDRAULICS.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 37,930 hrs · 13,972 cycles

FUSELAGE STATION 297 STRINGER 2L HAS DEEP GOUGE ON STRINGER. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER.

Part: SKIN — DENTED · airframe 37,930 hrs · 13,972 cycles

FUSE SKIN AT BODY STATION 760, BELOW STRINGER 16L, DENTED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.SKIN DOUBLER INSTALLED.

Part: WEB — CORRODED · airframe 37,930 hrs · 13,972 cycles

LEFT HAND CABIN WEB STATION 1640 JUST BELOW STRINGER 7L CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR.

Part: FRAME — DAMAGED · airframe 37,930 hrs · 13,972 cycles

STATION 1520 BETWEEN STRINGER 23R AND STRINGER 25R, EDGE OF FRAME DAMAGED AT RBL 36.5, 39.25, 41.5 AND 49 RESPECTIVELY. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR.

Part: STRINGER — GOUGED · airframe 37,930 hrs · 13,972 cycles

STATION 1280 ABOVE STRINGER 26R GOUGED AND HAS EXCESS MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR.

Part: WEB — DAMAGED · airframe 37,930 hrs · 13,972 cycles

RIGHT HAND AFT CABIN STATION 1640 FLOOR BEAM WEB DAMAGED AT RBL 56, ALSO FLOOR BEAM CAP CORRODED AROUND FASTENER HOLES BETWEEN RBL49-52. MAJOR REPAIR ACCOMPLISHED.INSTALLED ANGLE DOUBLER ON CAP AND WEB DOUBLERS ON INTERCOSTAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,930 hrs · 13,972 cycles

STATION 1681 CABIN FLOORBEAM TOP CAP LOWER SURFACE CORRODED AT LBL 24 - LBL 32. MAJOR REPAIR ACCOMPLISHED. INSTALLED CAP STRAP REPAIR.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 37,930 hrs · 13,972 cycles

BODY STATION 640 BL 0 RBL 22 FLOORBEAM TOP SURFACE GOUGED. MAJOR REPAIR ACCOMPLISHED. CUT AWAY DAMAGED AREA AND INSTALLED T-CAP REPAIR.

Part: FRAME — DAMAGED · airframe 37,930 hrs · 13,972 cycles

FORWARD E & E ACCESS HOLE STATION 223.5 RBL 29" FRAME IS DAMAGED FROM FASTENER GOING THRU STAND-OFF ALSO HOLE CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER.

Part: SKIN · airframe 37,930 hrs · 13,972 cycles

FUSELAGE BLIND FASTENER STATION 310 JUST BELOW STRINGER 2L REQUIRES PERMANENT REPAIR. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPLACED FASTENER.

Part: SKIN — DAMAGED · airframe 37,930 hrs · 13,972 cycles

EXTERNAL FUSELAGE SKIN STATION 359, STRINGER 3R, REQUIRED PERMANENT REPAIR. STRINGER 3R DAMAGED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REPAIRED FUSELAGE SKIN AND STRINGER 3R WITH DOUBLERS.

Part: INTERCOSTAL — CORRODED · airframe 37,930 hrs · 13,972 cycles

CABIN FLOOR INTERCOSTAL AT STATION 332 RBL 25" TO 39" STRINGER 1 7R CORRODED ON UPPER SURFACE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW INTERCOSTAL U-CHANNEL.

Part: SKIN · airframe 37,930 hrs · 13,972 cycles

FUSELAGE SKIN BLIND FASTENER INSTALLED STA. 333, STRINGER 2L. MAJOR REPAIR ACCOMPLISHED. INSTALLED SOLID FASTENER.

Part: INTERCOSTAL — CORRODED · airframe 37,930 hrs · 13,972 cycles

CABIN FLOOR INTERCOSTAL AT STATION 332 RBL 4" TO 22" CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW U-CHANNEL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,930 hrs · 13,972 cycles

CABIN FLOOR SUPPORT BEAM FOR FWD GALLEY CORRODED UNDER GALLEY MOUNT AT BODY STATION 300 RBL 41 WL 208. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOORBEAM.

Part: BEAM — CORRODED · airframe 37,930 hrs · 13,972 cycles

CABIN FLOOR STRUCTURE, INNER CREASE BEAM CHORD STATION 666 TO 755 HAD SEVERE CORROSION, ALSO INTERCOSTAL BELOW DOORWAY 2L DRAIN GUTTER STATION 680 TO 700 LBL 62" AT STRINGER 17L (CREASE BEAM WAS ALSO AT 62" LBL AT STRINGER 17L) HAD SEVERE CORROSION. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REMOVED INNER CREASE BEAM CHORD INSTALLED NEW PART AND INSTALLED REPLACEMENT INTERCOSTAL.

Part: INTERCOSTAL — GOUGED · airframe 37,930 hrs · 13,972 cycles

CABIN FLOOR INTERCOSTAL AT STATION 395 TO 418 RBL 56" STRINGER 17R HAD DEEP GOUGES. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW INTERCOSTAL AND UPPER SURFACE JOGGLE FILLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,930 hrs · 13,972 cycles

CABIN FLOORBEAM HAS CORROSION STATION 310 RBL 39 TO 41 UPPER T-CAP. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM WITH ANGLE INSTALLED ON AFT FLANGE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,930 hrs · 13,972 cycles

CABIN FLOORBEAM HAS CORROSION AT STATION 324 RBL 41-68. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM BY SPLICING IN T-CAP.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 37,930 hrs · 13,972 cycles

CABIN RIGHT HAND CREASE BEAM WEB BETWEEN STATION 996-1006 CORRODED. MAJOR REPAIR ACCOMPLISHED. CREASE BEAM WEB REPLACED.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 37,930 hrs · 13,972 cycles

STATION 1680 PRESSURE DECK UPPER SURFACE AT FORWARD EDGE HAS CORROSION BEYOND LIMIT 0 TO 24 LBL AT STRINGER 17 LT. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE. INSTALLED DOUBLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,930 hrs · 13,972 cycles

CABIN FLOORBEAM STATION 365 RBL 39 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE AND TOP STRAP ON FLOORBEAM.

Part: BULB — FAILED (DOOR 2R)

DOOR 2R ARM LIGHT INOP. RELAMPED AND ARM FUNCTION CHECKED OK.

Part: OVERHEAT WARN — ACTIVATED (E/E COMPT)

EICAS EQUIPMENT OVERHEAT AND STATUS MESSAGES, SUPPLY FAN AND OVERBOARD EXHAUST VALVE DISPLAYED IN NORMAL. ALTERNATE EQUIPMENT COOLING DOES NOT CLEAR MESSAGES PER CREW. A/C DIVERTED TO ORD UNDER AMBER ALERT.

Part: CHARGER — INOPERATIVE (CABIN)

FOUND INOPERATIVE EMERGENCY LIGHTS UNDER STOW BINS AT ROWS 24 RIGHT, 22 LEFT AND 20 RIGHT. *S/D* REPLACED BATTERY CHARGER AND BATTERY PACK.