N528UA

Part: SOCKET — DAMAGED (EXTERIOR LIGHT) · airframe 77,113 hrs · 28,280 cycles

NUMBER 2 R-H DOOR EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED, NO HELP. SLAVED IN NEW POWER SUPPLY M732, NO HELP. REPAIRED LIGHT SOCKET ASSEMBLY IAW IPC 33-51-06-051. OPERATIONS CHECKED GOOD.

Part: FRAME — DENTED (FUSELAGE) · airframe 75,974 hrs · 27,902 cycles

DENT ON AFT CARGO COMPARTMENT MAIN FRAME UPPER SURFACE AT BS 1500 JUST BETWEEN & ABOVE STRINGER 26L & 27L. TRIMMED OUT DAMAGE AREA OF FRAME FLANGE AT AFT CARGO BS 1500 FRAME. FABRICATED, LOCATED, DRILLED & INSTALLED J SECTION REPAIR DOUBLER IAW SRM 53-00-07 FIG 201 REPAIR 5. THIS A CAT B REPAIR ZONE 1 WITH SUPPLEMENTAL INSPECTIONS GIVEN IN SRM 53-00-07 REPAIR 5 TABLE II. INSPECTION THRESHOLD IS 50000 PTC REPEAT INSPECTIONS INTERVAL 12000 FLIGHT CYCLES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 75,974 hrs · 27,902 cycles

CORROSION ON FLOORBEAM IN MAIN CABIN BS 1640 BETWEEN LBL 4 & RBL 10. REMOVED DAMAGE. HFEC. FABRICATED & INSTALLED REPAIR PARTS IAW ECRA 5310-05536.

Part: FRAME — DENTED (FUSELAGE) · airframe 75,974 hrs · 27,902 cycles

DENT ON AFT CARGO FRAME UPPER SFC AT BS 1580 JUST ABOVE STRINGER 26L. REMOVED DAMAGE. HFEC. FABRICATED & INSTALLED REPAIR PARTS IAW SRM 53-00-07 REPAIR 5.

Part: FRAME — DENTED (FUSELAGE) · airframe 75,974 hrs · 27,902 cycles

AFT CARGO PIT STATION 1560 JUST ABOVE STRINGER 16R. DENT IN STRUCTURE MAIN FRAME UPPER SURFACE. REMOVED DAMAGE. HFEC FABRICATED & INSTALLED REPAIR PARTS IAW SRM 53-00-07T.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 74,538 hrs · 27,477 cycles

TE FLAP DISAGREE EICAS ILLUMINATED WHEN FLAP LEVER MOVED FROM 20 TO 25 FLAPS. TROUBLE SHOT IAW FIM 27-51 PG 135 & FOUND A RT FLAP TRANSMITTER WIRE FAULT ON THE 2 FSCU. SWAPPED THE 2 & 3 FSCU. PERFORMED BITE TEST & HAVE NO MORE FAULTS. DID CHECK THE CP ON THE RT FLAP TRANSMITTER & FOUND NO FAULTS.

Part: FILTER — CLOGGED (GALLEY) · airframe 74,168 hrs · 27,353 cycles

WATER LEAKING IN AFT GALLEY. FLIGHT ATTENDANTS STATED THAT THERE WAS VISIBLE SMOKE & ACRID SMELL COMING FROM BETWEEN THE GALLEY CARTS & THE GALLEY COUNTER. COULD FIND NO EVIDENCE OF ANY COMPONENT CAUSING ODOR OR SMOKE, OPERATED ALL GALLEY COMPONENTS & LIGHTING, ALL OPERATIONS NORMAL. BOTH COFFEEMAKER DRAIN FILTERS CLOGGED CAUSING OVERFLOW ONTO REAR OF COUNTER & WAS SOURCE OF WATER ON GALLEY FLOOR AREA. DUE TO WATER GATHERING IN COFFEEMAKER TRAYS, BOTH COFFEEMAKERS REPLACED PRECAUTIONARY. WARMERS, CHILLER, LIGHTS, ALL OPERATIONS NORMAL. REMOVED & REINSTALLED GALLEY ELECT PANELS TO CHECK FOR ANY EVIDENCE OF ARCING OR OVERHEATING, FOUND NONE IAW 25-32-95.

Part: TRIM PANEL — BROKEN (CABIN) · airframe 73,468 hrs · 27,132 cycles

WINDOW TRIM BROKE OFF AT 20F. SECURED AS NECESSARY. WINDOW SHADE OPERATES NORMALLY. THIS IS THE EMERGENCY EXIT WINDOW (PCN 192-1455) IS NOT THE RIGHT PART.

Part: CIRCUIT CARD — FAULTY (FIRE WARNING) · airframe 73,350 hrs · 27,093 cycles

RT ENG FIRE WARNING, RTFL FOUND BAD DETECTOR 2 FOR SYS 1 ON RT ENGINE. REPLACED DETECTOR 2, REF MM 26-11-01. CLEARED FAULT, MSG NO LONGER DISPLAYED, SYSTEM CHECKED OK. ALSO REPLACED CONNECTOR.

Part: BRACKET — BROKEN (CABIN) · airframe 72,824 hrs · 26,934 cycles

CREW REPORTED FIRE EXTINGUISHER BEHIND 6B MISSING. FOUND BRACKET BROKEN.

Part: FASTENER — MISSING (FAIRING) · airframe 72,759 hrs · 26,914 cycles

CREW REPORT: RIGHT L/E COWL BETWEEN WING AND FUSELAGE MISSING FASTENER. REPLACED MISSING FASTENER.

Part: WIRE — FRAYED (O2 MASK COMMS) · airframe 72,713 hrs · 26,895 cycles

OXYGEN MASK HOSE DEFECTIVE AT2. F/O MASK COMM CORD FRAYED. REPLACED F/O OXYGEN MASK, OPS CHECKED GOOD.

Part: TERMINAL — OPEN (WINDOW HEAT) · airframe 72,600 hrs · 26,860 cycles

LEFT SIDE WINDOW HEAT INOPERATIVE. TROUBLESHOT IAW AMM 30-41-00 AND FIM 30-41-00. FOUND RESISTANCE FOR TERMINAL J8 OPEN. CONFIRMED L2 WINDOW REPLACEMENT REQUIRED. VERIFIED CONTROLLER OPS NORMAL. REPLACED NR 2L WINDOW LAMINATE REF AMM. WINDOW HEAT TEST NORMAL.

Part: CARPET — DEFECTIVE (CABIN) · airframe 72,293 hrs · 26,771 cycles

MID LAV EEL LIGHT HAS CARPET OBSTRUCTING EEL LIGHT. TRIMMED CARPET SO EEL LIGHT IS FULLY VISIBLE. OP CHECKED GOOD.

Part: DOOR FRAME — DAMAGED (R4 DOORWAY) · airframe 72,203 hrs · 26,745 cycles

R4 DOOR AFT FRAME WEB HAS DAMAGE BS 1681.8, WL 208, RBL 55-66 BS 1681.8, RBL 55-RBL 60, WL 208. REPAIRED DOOR FRAME IAW ECRA5362-01023. MAJOR REPAIR.

Part: STRAP — CRACKED (BS1340 FLOORBEAM) · airframe 72,203 hrs · 26,745 cycles

STABILIZER STRAPS ON FLOORBEAM AT BS 1340 WL 199 RBL 25 AND LBL 25 IN AFT CARGO COMPARTMENT ARE CRACKED. REPAIRED STABILIZER STRAPS IAW ECRA 5360-01276. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1681) · corrosion level 2 · airframe 72,203 hrs · 26,745 cycles

CORROSION ON TOP OF FLOORBEAM BS 1681 RBL 41. REMOVED DAMAGE SECTION OF FLOORBEAM UPPER TEE AND MANUFACTURED NEW AND INSTALLED PER ECRA 5365-01074. MAJOR REPAIR.

Part: SKIN — CORRODED (BS 1672 S26R) · corrosion level 2 · airframe 72,203 hrs · 26,745 cycles

CORROSION ON INNER SURFACE OF SKIN BS 1672 S26R. CORROSION FOUND TO BE ON DRAIN MAST INNER DOUBLER. REMOVED, FABRICATED, AND INSTALLED NEW -85 DOUBLER IAW SRM 51-30-01 PARA 8 FIG 7 AND DWG 146N3700 SHEET 84. MAJOR REPAIR.

Part: SKIN — DENTED (BS 1709 S13L) · airframe 72,203 hrs · 26,745 cycles

FUSELAGE SKIN DENTED BS 1709 BELOW S13L, AFT OF L4 DOOR IS OUT LIMITS. REPAIRED IAW ECRA5361-01050.

Part: SKIN — DENTED (BS 1375 S25-26R) · airframe 72,203 hrs · 26,745 cycles

DENT IN FUSELAGE SKIN BS 1375 BETWEEN S25-26R. SKIN REPAIRED AT BS 1365-1392 BETWEEN STR 24R-28R.

Part: LONGERON — CORRODED (BS 365-345) · corrosion level 2 · airframe 72,203 hrs · 26,745 cycles

CORROSION ON LONGERON BS 365-345. REMOVED & INSTALLED LONGERON PER SRM. MAJOR REPAIR

Part: SUPPORT — CORRODED (G4 GALLEY) · corrosion level 2 · airframe 72,203 hrs · 26,745 cycles

G4 GALLEY SUPPORT AT BS 1620 TO BS 1640 RBL 52 WL 208.1 CORRODED ON PREVIOUS REPAIR. REMOVED, FABRICATED AND REPLACED G4 GALLEY SUPPORT AT BS 1620 TO 1640 RBL 52 WL 208.1 IAW SRM 51-40-02 FIG 12 AND DWG 146N5233. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (BS 365) · corrosion level 2 · airframe 72,203 hrs · 26,745 cycles

CORROSION ON MAIN CABIN FLOOR SUPPORT SPLICE BS 365 BL RBL 27. REMOVED, FABRICATED AND INSTALLED NEW MAIN CABIN FLOOR SUPPORT SPLICE DOUBLER IAW ECRA 5315-01064.

Part: INTERCOSTAL — CORRODED (BS1379 S26-27R) · corrosion level 2 · airframe 72,203 hrs · 26,745 cycles

CORROSION AFT CARGO DOOR SURROUND INTERCOSTAL BETWEEN STR 26-27R BS 1379. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02 FIG 8, 12 AND 51-40-05 FIG 4.

Part: SUPPORT CHANNEL — CORRODED (BS 1620-1640) · corrosion level 2 · airframe 72,203 hrs · 26,745 cycles

GALLEY MOUNT SUPPORT CHANNEL FROM BS 1620 - 1640 RBL 12 WL 208.1 HAS CORROSION ON AFT END. REMOVED, FABRICATED AND INSTALLED GALLEY MOUNT SUPPORT IAW SRM 51-40-02 PAR 7 FIG 12 AND DWG 146N5233. MAJOR REPAIR

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 72,203 hrs · 26,745 cycles

SOFT SPOT IN AISLE FLOOR PANEL AT ROWS 39-40. SOFT SPOT IS 9 X 12 INCHES IN SIZE. DELAMINATION REPAIRED. FABRICATED FLOOR PANE IAW UNITED DWG 15FS5866.

Part: GUSSET — CORRODED (BS 1681 RBL38) · corrosion level 2 · airframe 72,203 hrs · 26,745 cycles

CORROSION ON GUSSET BS 1681 RBL 38. REMOVED AND FABRICATED & INSTALLED GUSSET IAW SRM 51-40-05 PARAGRAPH 4 AND DRAWING 146N5216 AND SRM 51-40-02 PAR 7D FIG 12. MAJOR REPAIR.

Part: DECK PLATE — CORRODED (BS 1681.8) · corrosion level 2 · airframe 72,203 hrs · 26,745 cycles

CORROSION AT BS 1681.8 RBL 46, 48, 52 WL 208.1 ON AFT CABIN DECK PLATE. REPAIRED AFT DECK PLATE IAW ECRA 5330-04259. MAJOR REPAIR

Part: GUSSET — CORRODED (BS 1681 RBL 31) · corrosion level 2 · airframe 72,203 hrs · 26,745 cycles

CORROSION ON GUSSET BS 1681 RBL 31. REMOVED, FABRICATED & INSTALLED GUSSET IAW DRAWING 146N5216 & SRM 51-40-01 PAR 7D FIG 12. MAJOR REPAIR.

Part: SKIN — DELAMINATED (NR 7 SLAT WEDGE) · airframe 72,203 hrs · 26,745 cycles

NR 7 SLAT DISBONDED LOWER SURFACE T/E WEDGE 40 INCHES FROM I/B END. REPAIRED NR 7 SLAT IAW SRM 51-70-10 REPAIR 2 FIG 203.

Part: SKIN — DEBONDED (NR 1 SLAT) · airframe 72,203 hrs · 26,745 cycles

A 1.5 X 1.5 INCH ON LOWER SURFACE OF NR 1 SLAT T/E WEDGE 19 INCHES FROM O/B EDGE AND 8 INCHES FROM T/E DEDBONDED. REPAIRED NR 1 SLAT IAW SRM 51-70-10 REPAIR 2 FIG 203.

Part: SKIN — DEBONDED (NR 1 SLAT) · airframe 72,203 hrs · 26,745 cycles

NR 1 SLAT T/E WEDGE BOTTOM SURFACE 9 INCHES FROM O/B END DEBONDED. REPAIRED NR 1 SLAT T/E WEDGE IAW SRM 51-70-10 REPAIR 2 FIG 203.

Part: SKIN — DELAMINATED (NR 4 SLAT) · airframe 72,203 hrs · 26,745 cycles

SKIN DEBONDED ON LOWER SURFACE I/B EDGE OF NR 4 SLAT T/E. REPAIRED NR 4 SLAT IAW SRM 51-70-10 REPAIR 2 FIG 203.

Part: SKIN — DEBONDED (NR 9 SLAT) · airframe 72,203 hrs · 26,745 cycles

NR 9 SLAT LOWER SURFACE HAS DEDBONDED AT OSS 584 TWO PLACES 1.5" APART. REPAIRED NR 9 SLAT IAW SRM 51-70-10 REPAIR 4 FIG 202.

Part: SKIN — DEBONDED (NR 9 SLAT) · airframe 72,203 hrs · 26,745 cycles

NR 9 SLAT UPPER T/E WEDGE DEBONDED 11 INCHES FROM I/B END. REPAIRED NR 9 SLAT IAW SRM 51-70-10 REPAIR 4 FIG 202.

Part: SKIN — DENTED (FUSELAGE) · airframe 72,203 hrs · 26,745 cycles

EXTERNAL SKIN DENT WITH GOUGE ON AFT PIT LWR AFT CORNER. REPAIRED SKIN IAW SRM 52-30-01 FIG 201 REPAIR 4.

Part: SUPPORT FITTING — CORRODED (BS 365-377.5) · corrosion level 2 · airframe 72,203 hrs · 26,745 cycles

CORROSION ON MAIN CABIN GALLEY SUPPORT BS 365-377.7 RBL 12. REMOVED AND CORROSION FROM GALLEY SUPPORT FITTING, FOUND OUT OF SRM LIMITS. REMOVED AND REPLACED GALLEY SUPPORT IAW SRM 53-00-04 FIG 101, 51-40-02 PG 4-7 FIG 1 2, 51-00-53 PG 201-234 DWG 141N5161.

Part: SUPPORT FITTING — CORRODED (BS 365-377) · corrosion level 2 · airframe 72,203 hrs · 26,745 cycles

CORROSION ON MAIN CABIN GALLEY SUPPORT BS 365-377 RBL 57. REMOVED CORROSION FROM GALLEY SUPPORT BS 365-377 RBL57, OUT OF SRM LIMITS. REPLACED GALLEY SUPPORT IAW SRM 53-00-04 FIG 101, 51-40-02 FIG 12, AMM 51-00-53 PG 201-234, DWG 141N5161.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 72,203 hrs · 26,745 cycles

CORROSION ON MAIN CABIN FLOORBEAM BS 365, BL 0-RBL 65. REMOVED AND REPLACED FLOORBEAM TEE.

Part: WIRE — SHORTED (COCKPIT) · airframe 72,020 hrs · 26,680 cycles

STRONG BURNING ODOR IN COCKPIT AND FIRST CLASS. FOUND LEFT RUNWAY TURNOFF SW SHORTED AND WIRE TERMINAL BURNED OFF. WIRE SPLICED AT PIN 3 OF S1 P5 PANEL LIGHTING CONTROL, WIRE LOCATED BETWEEN CONNECTOR D3 501 TO SWITCH S1. REPLACED LEFT RUNWAY TURN OFF SW ON P5 LIGHTING PANEL. WIRE SPLICED AT PIN 3 OF S1 P5 PANEL LIGHTING CONTROL, WIRE LOCATED BETWEEN CONNECTOR D3 501 TO SWITCH S1 PER WD 33-42-21 PAGE 1.

Part: COMPUTER — MALFUNCTIONED (AUTOTHROTTLE) · airframe 71,822 hrs · 26,616 cycles

REJECTED TAKEOFF FOR AUTOTHROTTLE DISENGAGEMENT AND SPEED FLAG ON EADI. REJECTED TAKEOFF AT 100 KNOTS, PER CREW. INSPECTED AC PER AMM 05-51-14. NO DEFECTS FOUND, NORMAL BRAKING AFTER RTO. ACP TEST 30 PER AMM 22-03-00 FIG 117, NO FAULTS NOTED FOUND. REPLACED THE TMC, SYSTEM CHECKED OK PER MM 22-10-00, SYSTEM OK, AIRCRAFT IS AUTOLAND CAPABLE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,552 hrs · 26,514 cycles

FWD AFT LAV EEL LIGHT INOP. ACCOMPLISH NON-RII INSPECTION OF AMIS ITEM 5522012 :RELAMPED EEL LIGHT AT FWD AFT LAV (PCN 560-3325), OPS CHECK GOOD. INSPECTION COMPLETED. OPS CHECKED GOOD.

Part: OXYGEN MASK — UNKNOWN (CABIN) · airframe 71,475 hrs · 26,486 cycles

FWD CABIN SMALL O2 BOTTLE MASK NEEDS TO BE REPLACED. REPLACED O2 MASK AS REQUIRED.

Part: SWITCH — STUCK (COCKPIT) · airframe 71,005 hrs · 26,324 cycles

CAPTAIN`S YOKE PUSH TO TALK SWITCH STUCK OPEN. AT DEPARTURE. DEFERRED PER MEL. REPLACED CAPTAIN'S PUSH TO TALK SWITCH IAW 23-51-03-401.

Part: TURBINE BLADES — DAMAGED (NR 2 ENGINE) · airframe 70,879 hrs · 26,279 cycles

NR 2 ENGINE HPT STG 1 BLADES 2 EACH HAVE BURN THRU HOLES IN LEADING EDGE AREA "C" WHICH IS OUT OF LIMITS PER MM. REPLACE ENGINE WITHIN 4 CYCLES. ENGINE REPLACED.

Part: ENGINE — FAULTY (NR 1) · airframe 70,746 hrs · 26,228 cycles

TOP OF DESCENT FLIGHT DECK HAD A FAINT SMOKY SMELL FOR 3-4 MINS. DUE TO HISTORY OF OIL SMELL, REVIEW TROUBLESHOOTING ACP'D (CHP 21, 36, 49, 71, 72, 79), IF OIL SMELL IS REPORTED AGAIN, TO PREVENT IRREG OPS, REPLACE LEFT ENGINE PER AMM71-00-02 (401). LABEL REMOVAL REASON AS "CHRONIC OIL SMELL" OPBLM TOMC- 31OCT12. REPLACED ESN 727142 WITH ESN 726522 IN POS 01 PER TOD AMM 71-00-02 CONFIG 2 PB400. REF AMIS SEQ 7462017 #1 ENG WAS REPLACED. ACP'D AMM 21-00-01 PB100 AND FOUND NO RESIDUAL ODOR AFTER ENGINE CHANGE.

Part: HEAT EXCHANGER — FAULTY (AC BAY) · airframe 70,696 hrs · 26,212 cycles

REF LOG 5: DUE TO HISTORY OF OIL SMELL IN COCKPIT, REPLACE LEFT PACK PRIMARY AND SECONDARY HEAT EXCHANGERS PER TOMC. REPLACED BOTH PRIMARY & SECONDARY HEAT EXCHANGERS IN LEFT PACK IAW MM. NEED TO ACP LEFT PACK BURNOUT. REPLACED RT AND LT RECIRCULATION AIR FILTERS PER MM. PERFORMED ENGINE BURNOUT ON THE LEFT ENGINE NO SMELLS NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 70,322 hrs · 26,087 cycles

EMERGENCY LIGHT STRIP STICKING UP AT 12C. ONE EMERGENCY LIGHT INOPERATIVE AND SECURED WITH TAPE. SECURED AS REQUIRED. RELAMPED AND OPS NORMAL.

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 69,750 hrs · 25,899 cycles

NR 2 ENGINE BLADE NR 1 IS DAMAGED AT THE BLADE TIP. BLENDED BLADE.

Part: SKIN — DAMAGED (BS 450 S25R) · airframe 69,373 hrs · 25,761 cycles

LIGHTNING STRIKES AT 10K FT, TEN MINS BEFORE LANDING. LIGHTNING STRIKE FUSELAGE SKIN BS 450 S25R. DRILLED OUT DAMAGE AND INSTALLED RIVET.

Part: LIGHT — UNSECURE (ROW 12ABC) · airframe 69,352 hrs · 25,755 cycles

EXIT ROW 12ABC EXIT LIGHT BULGED UP. RESECURED, OPS CHECKED GOOD.

Part: SPOILER — MALFUNCTIONED (LT WING) · airframe 69,225 hrs · 25,712 cycles

ON LEFT WING FLOATING SPOILER; SECOND FROM FUSELAGE AS OBSERVED BY CAPTAIN IN THE CABIN. NO ABNORMAL FEEL BY PILOT FLYING REGARDING THE FLOATING SPOILER.

Part: SLAT — DENTED (NR 5) · airframe 68,901 hrs · 25,585 cycles

NR 5 LEADING EDGE SLAT IS DENTED FWD OF THE NOSE BEAM LOCATION. DENT MEASURES 4" X 4" WITH A DEPTH OF .1875". DENT IS OUT OF LIMITS PER 757 SRM WITH MINOR AXIS BEING 4" & DEPTH AT .1875 A-Y = 22.6. REMOVED NR 5 L/E SLAT PER MM. INSTALLED NR 5 SLAT. WILL NEED TO CONTINUE FROM "B " TO END. FLAPS HAVE BEEN LOWERED TO THE TWENTY UNIT POSITION. SLATS HAVE BEEN MANUALLY EXTENDED PAST PARTIAL EXTEND MANUALLY. MANUALLY RETRACT TO REFERENCED TORQUE TUBE POSITION BEFORE FLAP RETRACTION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,793 hrs · 25,544 cycles

EMERGENCY EXIT LIGHT IN STOWBIN LIP AT SEAT 26ABC IS INOPERATIVE. RELAMPED, OPS CHECKED OKAY.

Part: CONTROL MODULE — FAULTY (RUDDER TRIM) · airframe 68,262 hrs · 25,356 cycles

RUDDER TRIM COMPLETELY INOP. INDICATOR AND RUDDER DO NOT MOVE. MAINT TEXT: DUE HISTORY, RECOMMEND REPLACEMENT OF RUDDER TRIM ACTUATOR REF SVC TIP. PCN 563-9038 AVAIL SFO. REPLACED AILERON AND RUDDER TRIM CONTROL MODULE PER MM, OPS CHECKED GOOD.

Part: OXYGEN MASK — DEFECTIVE (O2 SYSTEM) · airframe 68,260 hrs · 25,354 cycles

CREW REPORT: O2 DEPLETES APPROX 10 PSI-SEC WHEN CAPTS MASK IS TESTED. REPLACED CAPTAIN'S OXYGEN MASK, OPS CHECKS GOOD.

Part: STRUCTURE — WORN (NR 1 PYLON) · airframe 67,835 hrs · 25,191 cycles

NR 1 ENG PYLON HYD PRESSURE LINE FITTING STRUCTURE WORN BEYOND LIMITS. HOLE ELONGATION EXCEEDS 1.60 LIMIT. REPAIRED STRUCTURE REF SRM ON OV WU B4752X.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,359 hrs · 25,036 cycles

TWO RT MED EXTERIOR FUSE EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED.

Part: CAP — DISLODGED (EMERGENCY LIGHT) · airframe 66,867 hrs · 24,868 cycles

END CAP CAME OFF EMERGENCY EXIT PATH LIGHTS BY FWD CLOSET. REPLACED END CAP, FLOOR LIGHTS CHECKED NORMAL.

Part: FLOORBEAM — CRACKED (BS 700) · airframe 66,825 hrs · 24,854 cycles

STA 700 FLOORBEAM LBL 25-45 CRACKED. MAJOR REPAIR ACCOMPLISHED: EVA 80894A.

Part: SKIN — DEBONDED (RT WING TE FLAP) · airframe 66,045 hrs · 24,563 cycles

RIGHT INBD MID FLAP LOWER SURFACE HAS BONDED DOUBLER REPAIR MISSING. APPROX 4 FT OTBD FROM INBD EDGE. REPAIRED FLAP. UPON COMPLETION OF RT FLAP REPAIR, REMOVED BAGGING MATERIAL AND INSPECTED REPAIR PRIOR TO PRIME AND PAINT. REPAIR IS OK. APPLIED FIBERGLASS LAYER. APPLIED CONDUCTIVE COATING. APPLIED PRIMER AND PAINTED.

Part: GIRT BAR — OUT OF POSITION (R3 DOOR) · airframe 65,268 hrs · 24,263 cycles

3R ARMED LIGHT INOPERATIVE. FOUND GIRT BAR KNOCKED OFF CARRIER. NO DAMAGE NOTED. REATTACHED GIRT BAR PER MM. OPS CKS OKAY. ARMED LIGHT FUNCTIONS NORMAL NOW.

Part: PANEL — DAMAGED (THRUST REVERSER) · airframe 65,064 hrs · 24,183 cycles

NR 2 ENGINE INBOARD REVERSER UPPER BIFURCATION PANEL HAS DELAMINATION. INNER SKIN DELAM IS 30 INCH LONG BY 9 INCH WIDE OUTER SKIN IS 35 INCH LONG BY 9 INCHES WIDE DELAMINATION TOTALS 585 SQ INCH BEYOND 330 MAX LIMIT. REMOVED NR 2 ENG INBD REVERSER. INSTALLED REVERSER ASSY.

Part: ENGINE — FAILED (RIGHT) · airframe 64,175 hrs · 23,855 cycles

RIGHT OIL FILTER EICAS -LIGHT STAYED ON AT IDLE -ENGINE SHUTDOWN. IAW CAPT NO OIL PRESSURE LOSS, NO PARAMETER CHANGES, CREW BROUGHT ENG BACK TO IDLE FOR 2 MIN. MSG STILL PRESENT, CREW SHUTDOWN NR 2 ENG IAW FLIGHT MANUAL. REPLACED NR2 ENGINE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,142 hrs · 23,843 cycles

EMERGENCY EXIT LIGHT AT DOOR 2R IS INOP. RELAMPED AND CHECKED OKAY.

Part: FAN — MALFUNCTIONED (E&E BAY) · airframe 62,341 hrs · 23,155 cycles

CREW REPORT: ELEC BURNING SMELL 13000 & 20000 ALT. *S/D* FOUND EICAS MESSAGE AFT EQ EXH FAN 1, REPLACED FAN. ACP HIGH POWER RUN AND CHECKED ECS SYSTEM FOR ODOR, FOUND NO ODOR FROM PACKS. COULD NOT DUPLICATE ANY TYPE OF BURNING SMELL THROUGHOUT THE AIRCRAFT. INBOUND CREW REPORTED NO EICAS MESSAGES RELATED TO EQUIPMENT COOLING OR FAN STATUS MESSAGES. ACCOMPLISHED TEST FLIGHT OF ACFT. TEST FLOWN 1.5 HRS FOR BURNING ODOR. NO ODOR DETECTED. OPS NORMAL.

Part: PANEL — DELAMINATED (TRHUST REVERSER) · airframe 61,290 hrs · 22,735 cycles

NR 2 ENGINE RT REV COWL UPPER BIFURCATION PANEL DELAMINATED BEYOND LIMITS. REMOVED NR 2 ENGINE RT REVERSER. NEW REVERSER STILL IN THE SHOP FOR PAINT & STENCILED. REPLACED NR 2 OUTBOARD REVERSER COWL.

Part: FSEU — MALFUNCTIONED (NR 2) · airframe 61,128 hrs · 22,675 cycles

LEADING EDGE SLAT DISAGREE MSG. RTFL. ON FLAP RETRACTION LEADING EDGE SLAT DISAGREE MSG. VISUALLY VERIFIED FLAPS AND SLATS RETRACTED. SELECTED ALT SLATS AND FLAPS MSG CLEARED. USED ALT FLAPS TO RETURN TO DEN. CHECKED FSEUS, NO FAULTS, NO HISTORY. CHECKED OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,975 hrs · 22,243 cycles

SLIDE LIGHT AT 2 RT INOP. RELAMPED SLIDE LIGHT.

Part: ACTUATOR — LEAKING (RUDDER) · airframe 59,921 hrs · 22,225 cycles

EICAS L HYD QTY SHOWS .42. FLIGHT DIVERTED. FOUND RUDDER RATIO CHANGER ACTUATOR PISTON LEAKING. REPLACED ACTUATOR. SERVICED LEFT HYD QTY TO FULL.

Part: WARNING SYSTEM — ACTIVATED (NR 2 ENGINE) · airframe 59,818 hrs · 22,180 cycles

NR 2 ENGINE OIL TEMP EICAS. RTFL. AFTER DRAINING 4 GALLONS FROM GEAR BOX, CHECKED ALL CHIPS AND FOUND OK. OPERATED ENG AT 1,27 EPR,DIFF OIL PRESS 100, SCAV OIL PRESSURE 92, OIL TEMP 140 AFTER 15 MIN RUN. NOTE: ENGINE WAS SHUTDOWN AFTER LANDING ROLLOUT AND WAS NOT AN IFSD.

Part: FEEDER CABLE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 59,514 hrs · 22,051 cycles

EMERGENCY EXIT LIGHT POWER STRIP DISCONNECTED AT 6B. POWER LEAD DAMAGED, REQUIRES REPLACEMENT. NO EXPOSED WIRING. REPLACED EMERGENCY LIGHT STRIPS.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 59,514 hrs · 22,051 cycles

EMERG EXIT LT PWR STRIP DISCONNECTED AT 6B. POWER LEAD DAMAGED, REQUIRES REPLACEMENT. NO EXPOSED WIRING. REPLACED EMERGENCY LIGHT STRIPS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,972 hrs · 21,832 cycles

FLIGHT ATTENDANT REPORTED EEL TRACK COVER BROKE. FOUND EEL LIGHT OUT BETWEEN ROW 14ABC TO 20ABC. REPLACED MISSING EEL SEGMENT AND SECURED LOOSE CONNECTORS. REPLACED BROKEN COVER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,972 hrs · 21,832 cycles

FLIGHT ATTENDANT REPORT EEL TRACK COVER BROKE. FOUND EEL LIGHT OUT BETWEEN ROW 14ABC TO 20ABC. REPLACED MISSING EEL SEGMENT AND SECURED LOOSE CONNECTORS. REPLACED BROKEN COVER.

Part: LIGHT — DAMAGED (CABIN) · airframe 58,817 hrs · 21,768 cycles

EEL LIGHT FLOOR STRIP AT 13ABC DAMAGED. REINSTALLED LOOSE EEL STRIP AND SECURED EEL COVER, OPS CHECKED OKAY.

Part: LIGHT — LOOSE (CABIN) · airframe 58,761 hrs · 21,741 cycles

EMERGENCY EXIT PATH LIGHTING LOOSE NEAR ROW 14. SECURED EEL STRIP AND COVER. CHECKS OK.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 58,750 hrs · 21,736 cycles

DOOR 2L SLIDE PRESSURE IS LOW. UNKNOWN PRESSURE LEAK. REPLACED SLIDE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,588 hrs · 21,681 cycles

EEL FLOOR STRIP INOP AT FRONT OF COACH. EEL DAMAGE. REINSTALLED LIGHT STRIP. CHECKS OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,588 hrs · 21,681 cycles

EEL FLOOR STRIP INOP AT FWD AFT LAV. SHORT IN EEL WIRING. REPLACED EEL STRIP. CHECK OK.

Part: CONNECTOR — CONTAMINATED (FIRE LOOP) · airframe 58,216 hrs · 21,548 cycles

EICAS MSG - R ENG FIRE LP 1. CREW COMMENTS: R ENG FIRE LOOP 1. FOUND CONNECTORS ON LOOP 1 VERY CONTAMINATED. CLEANED BOTH CONNECTORS, RESISTANCE CHECKS WITHIN LIMITS. MESSAGE CLEARED. SYSTEM TESTS NORMAL.

Part: PANEL — SHORTED (COCKPIT) · airframe 56,335 hrs · 20,870 cycles

EVACUATION COMMAND - SIGNAL IN COCKPIT OVERHEAD PNL HAS DARK AREAS. ELECTRICAL SHORTING ON PANEL ITSELF. REPLACED COCKPIT EVAC PANEL, NORMAL OPERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,335 hrs · 20,870 cycles

EMERGENCY LIGHT AT SEAT 29 ABC ON BULLNOSE BIN PNL IS INOP. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,335 hrs · 20,870 cycles

LEFT FWD EXT EMERGENCY SLIDE LIGHT INOP. RELAMPED EMERGENCY LIGHT.

Part: SKIN — DENTED (L2 DOOR) · airframe 56,335 hrs · 20,870 cycles

L2 DOOR EXTERNAL SKIN HAS 2 DENTS ABOVE LOWER GATE. ACCOMPLISHED MAJOR REPAIR.

Part: SKIN — DENTED (R1 DOOR) · airframe 56,335 hrs · 20,870 cycles

R1 DOOR EXTERNAL SKIN HAS A DENT BY LOWER HINGE ARM CUTOUT. ACCOMPLISHED MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,335 hrs · 20,870 cycles

FLOORBEAM UPPER CAP CORRODED AT BS 1640 BL 8L TO 57R WL 208. PERFORMED MAJOR REPAIR.

Part: DOOR FRAME — DAMAGED (L2 DOOR) · airframe 56,335 hrs · 20,870 cycles

L-2 DOOR UPPER HINGE ARM CUTOUT REQUIRES DOUBLER INSTALLATION, FRAME DAMAGE PREVIOUSLY ROUTED OUT. MAJOR REPAIR ACCOMPLISHED.

Part: DOOR FRAME — DAMAGED (R2 DOOR) · airframe 56,335 hrs · 20,870 cycles

R-2 DOOR UPPER HINGE ARM CUTOUT REQUIRES A REPAIR DOUBLER, FRAME DAMAGE PREVIOUSLY ROUTED OUT. MAJOR REPAIR ACCOMPLISHED.

Part: LIGHT — DAMAGED (CABIN) · airframe 56,181 hrs · 20,819 cycles

EEL LIGHT INOP AT MID LAV THRESHOLD. FOUND EEL LIGHT ASSY DAMAGED. REPLACED EEL LIGHT ASSY AT MID LAV THRESHOLD. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,181 hrs · 20,819 cycles

EMERGENCY EXIT LIGHT INOP AT AFT RT BULLNOSE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,181 hrs · 20,819 cycles

EMERGENCY EXIT FLOODLIGHT INOP AT FWD LT OVERWING HATCH.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 55,342 hrs · 20,509 cycles

NR 2 FORWARD CARGO COMPARTMENT SMOKE DETECTOR INOPERATIVE.

Part: WARNING MESSAGE — ILLUMINATED (NR 1 ENG T/R) · airframe 50,766 hrs · 18,820 cycles

NR 1 ENG REV UNLOCK LIGHT ON EICAS DISPLAYED ON TAKE OFF ROLL. THE INITAL PROBLEM WAS AN ACTUATOR LEAK. PDX RPL THE ACTUATOR. THE DEPLOY PROXIMITY SENSOR NEEDS TO BE REMOVED FROM THE OFF ACTUATOR AND REINSTALLED TO THE NEW ACTUATOR BECAUSE ITS HARDWIRED TO THE REVERSER. DURING THIS REINSTALLATION THE MECHANIC MUST OF MIS RIGGED IT OR LEFT THE SENSOR LOOSE BECAUSE THE VERY NEXT FLIGHT WAS THIS INCIDENCE OF THE UNLOCK LIGHT AND THE SENSOR WAS FOUND OUT OF RIG.

Part: LIGHT — DAMAGED (ROW 1) · airframe 46,585 hrs · 17,263 cycles

EMERGENCY EQUIPMENT LIGHT DAMAGED ROW 1. REPLACED STRIP

Part: RELAY — FAILED (RT A/C PACK) · airframe 45,228 hrs · 16,729 cycles

CABIN TEMPERATURE STUCK IN FULL HOT. RT PACK TEMP VLV WOULDN'T DRIVE COLD--RPL K56, REF WDM21-51-23 . VALVE WILL NOW DRIVE COLD.

Part: BLADE — FAILED (RT ENGINE) · airframe 42,069 hrs · 15,548 cycles

RIGHT ENGINE COMPRESSOR STALL, EGT OVERTEMP. OIL PRESSURE DROPPED TO ZERO. ENGINE TEARDOWN VERIFIED THAT THE HPT T1 BLADE FAILED. PRATT & WHITNEY HAS BEEN INVESTIGATING THIS FAILURE FOR ROOT CAUSE AND DETERMINED THAT THE SYMPTOMS AND PART CONDITION ARE UNIQUE IN THIS EVENT. THE HPT T1 BLADE FAILED FROM A STRESS CORROSION CRACK ABOVE THE PLATFORM. AS AN ADDED NOTE, THIS TURBINE BLADE DID NOT HAVE PWA 545 PROTECTIVE COATING IN THE DAMPER POCKET.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,829 hrs · 13,961 cycles

CABIN FLOORBEAM AT STATION 324, RBL 41.60 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 37,830 hrs · 13,961 cycles

HAT CHANNEL AT STATION 324 RBL 344 CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED HAT CHANNEL.

Part: FRAME — DENTED (FUSELAGE) · airframe 37,830 hrs

AFT PIT STA 1540 ABOVE STRINGER 25L FRAME DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR ON FRAME.

Part: FRAME — CORRODED · airframe 37,830 hrs · 13,961 cycles

STATION 1681 STRINGER 17R FRAME CORRODED AT FLOOR Z ANGLE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR ON FRAME.

Part: CLIP — CORRODED · airframe 37,830 hrs · 13,961 cycles

AFT PIT FRAME CLIP CORRODED STATION 1500 RBL17. MAJOR REPAIR ACCOMPLISHED. CLIP REMOVED AND CORROSION REMOVED FROM CLIP AND AFT LIP OF FRAME THEN CLIP REINSTALLED.

Part: FRAME — DENTED · airframe 37,830 hrs · 13,961 cycles

AFT PIT, STATION 1420, ABOVE STRINGER 25L, FRAME DENTED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FRAME DOUBLER REPAIR ACCOMPLISHED.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 37,830 hrs · 13,961 cycles

CABIN CREASE BEAM BODY STATION 758 RBL 65 HAS EXCESSIVE MATERIAL LOSS AT FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: CREASE BEAM — CORRODED · airframe 37,829 hrs · 13,961 cycles

CREASE BEAM BODY STATION 740 RBL 65 CORRODED. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER REPAIR

Part: DOOR — DAMAGED · airframe 37,830 hrs · 13,961 cycles

LEFT HAND APU DOOR HAS DAMAGE 38" FROM AFT END 3" FROM LOWER END RIVET IS PUSHING METAL AWAY FROM BUCKTAIL. MAJOR REPAIR ACCOMPLISHED. FLUSH REPAIR INSTALLED.

Part: PANEL — CORRODED (FUSELAGE) · airframe 37,829 hrs

CABIN FLOOR DECK PLATE CORRODED STA 1681, RBL 12-24 WL 208. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,830 hrs · 13,961 cycles

CABIN FLOORBEAM AT STATION 1640 RBL 51.5 AFT SIDE OF CAP CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 37,830 hrs · 13,961 cycles

AFT CAB, FLOORBEAM AT STATION 1640 BL 0, HAD EXCESSIVE MATERIAL REMOVED. MAJOR REPAIR ACCOMPLISHED. DOUBLE FLANGE REDUCED FASTENER REPAIR INSTALLED.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 37,830 hrs · 13,961 cycles

AFT CABIN FLOORBEAM CAP AT BODY STATION 1540, LBL 3, RBL 12, EXCESSIVE MATERIAL LOSS AFTER BLEND. MAJOR REPAIR ACCOMPLISHED. STRAP REPAIR INSTALLED.

Part: BRACKET — FAILED (NR 1 ENGINE) · airframe 36,711 hrs · 13,518 cycles

NR 1 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. *S/D* LOSS OF OIL QUANTITY AND PRESSURE DUE TO A HOLE WORN IN THE LINE. REPLACED OIL OUT LINE FROM FOX TO AOX AND SUPPORT BRACKET ON NR 1 ENG.

Part: CONTROL BOX — FAILED (SPOILER) · airframe 33,551 hrs

SPOILER EICAS MESSAGE AND LIGHT ON OVERHEAD PANEL ILLUMINATED. *S/D* REPLACED ELECTRICAL CONNECTOR AT NR 2 LEFT SPOILER AND REPLACED NR 1 RIGHT SPOILER CONTROL MODULE SYSTEM. CKS NORMAL.

Part: ACTUATOR — FAILED (LE SLAT)

RETURNED TO ORD DUE TO A LEADING EDGE FLAP PROBLEM. *S/D* POSITION NUMBER 15 LEADING EDGE SLAT ACTUATOR WAS FOUND WITH AN INTERMITTENT PROBLEM CAUSING THE EICAS MESSAGE AND LOCKOUT OF THE LEADING EDGE SLATS. REPLACED NUMBER 15 LEADING EDGE SLAT ACTUATOR AND RETURNED AIRCRAFT TO SERVICE WITH NO FURTHER PROBLEMS.

Part: BLEED VALVE — OPEN (NR 2 ENGINE)

ENGINE PRESSURE RATIO FLUCTUATED AT LEAST 0.41 (FROM 1.40 TO 0.99) TWICE AS AIRCRAFT LEVELED OFF FROM CLIMB. ENGINE PRESSURE RATIO, FUEL FLOW AND RPM MOVE TOGETHER. AFTER REDUCING ALTITUDE AND CLOSING NUMBER 2 ENGINE BLEED, FLUCTUATION STOPPED AND REST OF FLIGHT UNEVENTFUL.

Part: SIDE PANEL — CORRODED (BS 1420)

DISCOVERED CORRODED AFT CARGO FLOOR SIDE PANEL MEMBER, JUST INBOARD FO CARGO DOOR SILL, SRM 53-60-53 PG 8 NR 4. REMOVED CORROSION AND REPAIRED PER SRM GUIDELINES, OPERATION CHECKS NORMAL.

Part: FAN BLADE — BENT (RT ENGINE)

ON TAKEOFF FROM SMF, INGESTED ONE BIRD IN THE RIGHT ENGINE. DAMAGE DONE TO AT LEAST TWO BLADES. ODOR IN CABIN. INITIAL VIB 22. VIBRATION NOTED AT ALL POWER SETTINGS. PEEK VIBRATION EPR 1.05. BIRD INGESTION REQUIRED REPLACEMENT OF TWO FAN BLADE PAIRS.