N515UA

Part: WIRE — FAULTY (TRIM SYSTEM) · airframe 75,896 hrs · 28,195 cycles

EICAS MESSAGE, MACH SPD TRIM, DISPLAYED & MACH SPD LIGHT ILLUMINATED. FOR AIRCRAFT N501UA-N522UA DO 27-09-00 FIG106C AIRCRAFT N523UA-N594UA DO 27-09-00 FIG 106. CREW COMMENTS ILLUMINATED AFTER USE OF ALTERNATE STAB TRIM LEVERS, ITEM ROLLED FWD. WHEN ACTIVATING ALTERNATE STAB TRIM LEVERS EICAS MESSAGE, UNSCHEDULED STAB TRIM, APPEARS ALONG WITH AURAL WARNING. WIRE AT STAB TRIM STANDBY SWITCH S538. OPERATIONS OK, NO MESSAGES OR LIGHTS.

Part: BLADE — NICKED (NR 2 ENGINE) · airframe 75,679 hrs · 28,126 cycles

NR 2 ENG FAN BLADE AT 6 O`CLOCK POSITION HAS SMALL NICK ON EDGE BLENDED BLADE. HFEC NR 2 ENG FAN BLADE, NO CRACK NOTED, REPAIRED BLADE.

Part: ACTUATOR — FAULTY (ELEVATOR) · airframe 75,658 hrs · 28,120 cycles

ELEVATOR ASYMMETRY STATUS MESSAGE. R & R NEW ASYMMETRY LIMITER ACTUATOR IAW MM.

Part: CONTROL MODULE — FAULTY (SPOILER) · airframe 75,629 hrs · 28,110 cycles

DURING TROUBLESHOOTING FOUND TWO SPOILER CONTROL MODULES M534 & M535 FAULTED. REPLACED SPOILER CONTROL MODULES M534 & M535. GND TEST CHECKED GOOD.

Part: NUT PLATE — MISSING (RT WING) · airframe 75,608 hrs · 28,104 cycles

MISSING FASTENER RIGHT WING INBD OF ENG. REMOVED PANEL, REPLACED MISSING NUTPLATE & ALL PANEL FASTENERS AS REQUIRED. THIS IS THE INBD HINGED PANEL 611FB. TOMC WOULD NOT ALLOW FASTENER SUBSTITUTION.

Part: AUDIO PANEL — INTERMITTENT (COCKPIT) · airframe 75,432 hrs · 28,056 cycles

CAPT`S AUDIO PANEL INTERMITTENT. REPLACED CAPT'S AUDIO SELECT PANEL, GROUND TESTED OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,222 hrs · 27,983 cycles

EMERGENCY PATH LIGHTING INOPERATIVE FROM SEAT 37 TO AFT OF LAVATORY STATION 1500 TO 1640. TROUBLESHOT IAW WDM 33-51-22 FOUND LEAD ASSEMBLY PN 5879-1 & LIGHT GALLERY PN 6024-3 IAW IPC 33-52-00 ITEMS 113 & 115 DAMAGED. REPLACED BOTH, OPERATIONS CHECKED GOOD IAW AMM 33-51-11.

Part: VALVE — OPEN (POTABLE WATER) · airframe 75,151 hrs · 27,957 cycles

POTABLE WATER ISSUE, FLIGHT DIVERTED. FOUND REFILL VALVE OPEN A LITTLE, RESEATED REFILL VALVE. SERVICED WATER OPERATIONS CHECKED OKAY.

Part: LANYARD — OUT OF POSITION (L2 DOOR) · airframe 74,895 hrs · 27,879 cycles

DOOR 2L WOULD NOT ARM. FOUND SURVIVAL KIT CORD BLOCKING LANYARD. STOWED CORD, ARMED DOOR SEVERAL TIMES, OPERATIONS CHECKED GOOD.

Part: SENSOR — CLOGGED (CABIN TEMP) · airframe 74,762 hrs · 27,829 cycles

UNABLE TO MAINTAIN COCKPIT TEMP IN ANY MODE. TEMP VARIES FROM 61-85. FOUND SENSOR CLOGGED, CLEANED SENSOR AND OPERATES NORMALLY NOW.

Part: UNKNOWN — ODOR (CABIN) · airframe 74,548 hrs · 27,762 cycles

CREW REPORTED AN ELECTRICAL ODOR AROUND ROW 4. SELECTED UTILITY BUSSES OFF, LT RECIRCULATION FAN OFF AND CABIN CEILING LIGHTS OFF. ODOR DISSIPATED AFTER A FEW MINUTES. REPLACED LT, AND RT CEILING LIGHT BALLASTS. OPS CHECKED CABIN LIGHTS, AUDIO, VIDEO SYS, PC POWER SYS, LT RECIRCIRCULATION FAN, AND ALL GALLEYS LIGHTS ON. ALSO ODOR CHECKED UNDER SEAT ROWS 3,4,5 LT AND RT SIDE, NO ODOR NOTICE. AFTER 4 HOURS OPS CHECKED, NO ELECTRICAL ODOR. (BOTH REMOVED BALLASTS NO ODOR). OPENED SIX PSU PANELS AT SEAT ROW 3,4,5 LT, AND 3,4,5 RT CHECKED FOR ELECTRICAL ODOR. NO DISCREPANCY NOTICED.

Part: DETECTOR — FAULTY (OVERHEAT) · airframe 74,391 hrs · 27,716 cycles

RT ENGINE OVERHEAD LP 2 STATUS MESSAGE, TROUBLESHOT IAW FIM 26-11-00, FOUND OVERHEAT DETECTOR DAMAGED. REPLACED DETECTOR IAW AMM, OPS TESTED OK, NO FAULTS SHOWING.

Part: DUCT — TORN (OIL COOLER) · airframe 74,391 hrs · 27,716 cycles

FLEX DUCT BETWEEN OIL COOLER (TEMP. REGULATOR) AND OVERBOARD EXHAUST DUCT TORN. APU IS UNABLE TO BE USED AND REQUIRES GROUND START TRUCK. DUCT REQUIRED TO REPAIR IS IPC 49-11-01-001, ITEM 20, PCN 181-0477.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 74,063 hrs · 27,610 cycles

EMERGENCY LIGHT END CAP IS MISSING AT MID LAV. REPLACED END CAP IAW AMM.

Part: SLIDING WINDOW — DELAMINATED (R2) · airframe 73,770 hrs · 27,523 cycles

F/O FWD SIDE WINDOW DELAMINATED TOP AND SIDE. REPLACED F/O SLIDING WINDOW.

Part: FILTER — MISSING (EMERGENCY LIGHT) · airframe 73,745 hrs · 27,517 cycles

OVERWING EXIT EEL NOT RED OR ORANGE. INSTALLED EEL ORANGE FILTER LAMINATE AMM.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 73,723 hrs · 27,511 cycles

PSU MASKS ROW 20 DEPLOYED. ACCOMPLISHED REPACK AND STOW OF O2 MASKS AT SEAT 20 ABC PER AMM, OPS CHECKS OK.

Part: LEVER — MISSING (LAVATORY) · airframe 73,325 hrs · 27,378 cycles

AFT FWD LAV LOCKING LEVER MISSING. REPLACED MISSING AFT FWD LAV LOCKING LEVER. OPS CHECK GOOD.

Part: DRAIN — LEAKING (WASTE WATER) · airframe 73,018 hrs · 27,274 cycles

BLUE WATER LEAKING FROM LOWER FUSELAGE AFT DRAIN HOLES. WATER COMING FROM AFT FWD LAV TANK. DISCONNECTED APU AIR DUCT AND EQUIP COOLING DUCT IN RIGHT AFT AREA OF AFT CARGO PIT TO FACILITATE REMOVAL OF WASTE TUBE ELBOW. REPLACED ELBOW DRAIN HOLES.

Part: FITTING — OUT OF ADJUST (L1 DOOR) · airframe 72,795 hrs · 27,196 cycles

DOOR 1L HARD TO ARM-DISARM WEDGE DOES NOT POP OUT ADJUSTED AFT GIRT BAR FITTING, WEDGE AND ARM-DISARM OPS CHECKED NORMAL. WITNESSED SLIDE BOTTLE PIN REMOVAL AND STORAGE. WITNESSED DOOR ASSIST BOTTLE PIN REMOVAL. REF AMM 52-11-25 AND RII LST CHAPTER 25 GROUP 7.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 72,764 hrs · 27,184 cycles

THE FUSE SKIN REPAIR INSTALLED PER ECRA 5361-01031 BETWEEN BS 1384 - 1401, AND STR 28L -29R RECEIVED FIRST AND SECOND STAGE APPROVAL. MAJOR REPAIR ACCOMPLISHED: DOUBLER INSTALLED OVER EXISTING HOLE AT STA 1393, STR 30.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,764 hrs · 27,184 cycles

EEL LIGHT STRIP AT FWD COAT CLOSET INOP. PERFORM TS ON EEL LIGHT STRIP AT FWD COAT CLOSET OPEN. REPLACE EEL LIGHT STRIP IAW B757 A MM 33-51-11. PERFORM OPS CHECK OF EEL LIGHT STRIP AT FWD COAT CLOSET, OPS CHECK FOUND NORMAL IAW AMM B757 33-51-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,764 hrs · 27,184 cycles

AFT CABIN STA 1640 FLOORBEAM UPPER CAP CORRODED RBL 58 .22 TO BL 0. UPPER CHORD REPAIR ACCOMPLISHED PER ECRA 5310-05634.

Part: SKIN — DENTED (BS 1732 S29-30L) · airframe 72,764 hrs · 27,184 cycles

FUSELAGE SKIN FOUND DENTED AT BS 1732 S29 - 30L. FOUND OUT OF SRM LIMITS. CUT OUT DAMAGE AND ACCOMPLISHED NDT OF CUT-OUT AND HOLES COMMON TO REPAIR. FABRICATED AND INSTALLED EXTERNAL DOUBLER REF SRM 53-00-01 FIG 201 DETAIL 1. MAJOR REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 72,764 hrs · 27,184 cycles

SKIN DENTED STA 729, STR 32R TO 33R, 3 PLACES. MAJOR REPAIR ACCOMPLISHED: DAMAGE IS AT STA 729, BETWEEN STR 24R AND 25R. DOUBLER REPAIR INSTALLED PER SRM 53-00-01, REPAIR 3 FIGURE 201.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 72,764 hrs · 27,184 cycles

FUSELAGE SKIN CREASED AT STA 615 BETWEEN STR 28L AND 28R (SEE CF9043). MAJOR REPAIR ACCOMPLISHED: DOUBLER REPAIR INSTALLED PER SRM 53-00-01 REPAIR 3 FIGURE 201.

Part: SKIN — DENTED (FUSELAGE) · corrosion level 2 · airframe 41,800 hrs · 15,655 cycles

FUSELAGE CREASE APPROX 1 FT AFT OF DOOR 3R AT MID LEVEL. MAJOR REPAIR ACCOMPLISHED. FUSELAGE SKIN DENT IS SMOOTH, CRACK FREE & WITHIN LIMITS PER SRM 53-00-01PG101. NO ACTION REQUIRED. DAMAGE WAS AT STA 1707, BETWEEN STR 15R & 16R. FOUND TO BE OUT OF LIMITS. DOUBLER REPAIR INSTALLED PER SRM 53-00-01 REPAIR 3 FIGURE 201.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 72,764 hrs · 27,184 cycles

CLASS 'B' FUSELAGE SKIN DOUBLER REPAIR INSTALLED AT STA 610, STR 16L, PER SRM 53-00-01 REPAIR 2, FIG 201, (REF PTT# 7646050). INSTALLED DOUBLER REPAIR PER SRM 53-00-01 REPAIR 2, FIGURE 201. REPAIR WAS ACP ON NR1468535. REFER TO SRM 53-00-01 REPAIR 2 FIG 201, TABLE 4.

Part: SKIN — DENTED (FUSELAGE) · airframe 72,764 hrs · 27,184 cycles

SKIN DENTED BETWEEN STR 17 AND 16L, AT STA 590. -1.2 X .015 = 80. HFEC INSP PER NDT PT. 6, 51-00-19, NO CRACKS NOTED. PER SRM 53-00-01, NO ACTION REQUIRED. OK TO ARCHIVE. ACTUAL DAMAGE WAS AT STA 610 STR 16L. INSTALLED DOUBLER REPAIR PER SRM 53-00-01 REPAIR 2 FIGURE 201.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 72,764 hrs · 27,184 cycles

CLASS B DOUBLER REPAIR INSTALLED AT ST 1707 BETWEEN STR 15R AND 16R, PER SRM 53-00-01 REPAIR 3 FIG 201 (REF PTT# 7646052). REFER TO SRM 53-00-01, REPAIR 3, FIG 201, TABLE 5.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,764 hrs · 27,184 cycles

STA 1681.8 UPPER FLOORBEAM CAPPED CORRODED BETWEEN BL 0 AND RBL 58. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE & RE-INSTALLED REPAIR PER SRM 52-40-02 AND SRM 53-60-51, REPAIR 3 DETAIL 2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,764 hrs · 27,184 cycles

FWD CABIN FLOORBEAM STA 324 UPPER CAP CORRODED FROM RBL 40 TO RBL 60. REPLACED FLOORBEAM UPPER CAP FROM LBL 6 TO RBL 70 PER SRM. WORK ACP ON AAR NR 14 68626.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,764 hrs · 27,184 cycles

AFT CABIN FLOOR SUPPORT CORRODED STA 1640 TO 1681.8, RBL 60. MAJOR REPAIR ACCOMPLISHED: FLOOR SUPPORT (2 SECTIONS). REPLACED ON PER SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,764 hrs · 27,184 cycles

CABIN FLOOR SUPPORT CHANNELS CORRODED - STA 1640 TO 1660 AND 1660 TO 1681.8. MAJOR REPAIR ACCOMPLISHED: CORRODED FLOOR CHANNELS REPLACED PER SRM 51-40-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,764 hrs · 27,184 cycles

CABIN FLOOR SUPPORT CORRODED STA 345 TO 365, RBL 45.5. MAJOR REPAIR ACCOMPLISHED: CORRODED FLOOR SUPPORT REPLACED PER SRM 51-40--02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,764 hrs · 27,184 cycles

CABIN FLOOR SUPPORT CORRODED STA 324 TO 418, BL 0. MAJOR REPAIR ACCOMPLISHED: CORRODED FLOOR SUPPORT REPLACED PER SRM.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,764 hrs · 27,184 cycles

AFT CABIN FLOOR SUPPORT BRACKET CORRODED AT STA 365, RBL 60. MAJOR REPAIR ACCOMPLISHED: CORRODED BRACKET REPLACED PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,764 hrs · 27,184 cycles

CABIN FLOORBEAM UPPER CAP CORRODED BS 365 RBL 3 TO RBL 6. MAJOR REPAIR ACCOMPLISHED: INSTALLED FABRICATED RPR IAW ECRA 5310-05536.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,764 hrs · 27,184 cycles

CABIN FLOOR SUPPORT CORRODED STA 333 TO STA 365, RBL 61. FLOOR SUPPORT REPLACED PER SRM 51-40-02. ACP ON AAR NR 1468627.

Part: STRINGER — BENT (FUSELAGE) · airframe 72,764 hrs · 27,184 cycles

STRINGER 16L BENT AT STA 610 (WORKED WITH DOUBLER REPAIR PTTSEQ # 7646050) MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND ACP STRINGER REPAIR PER SRM 53-00-03 REPAIR 1, FIGURE 201.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,764 hrs · 27,184 cycles

CABIN FLOOR SUPPORT CORRODED FROM AT STA 333, FROM RBL 25 TO RBL 38. MAJOR REPAIR ACCOMPLISHED: CORRODED FLOOR SUPPORT REPLACED PER SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,764 hrs · 27,184 cycles

CABIN FLOOR SUPPORT CORRODED - STA 345 TO 365, RBL 55. MAJOR REPAIR ACCOMPLISHED: CORRODED FLOOR SUPPORT REPLACED PER SRM 51-40-02, ON AAR NR 1468662.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,764 hrs · 27,184 cycles

CABIN FLOORBEAM UPPER CAP CORRODED BS 365 RBL 3 TO RBL 6. MAJOR REPAIR ACCOMPLISHED: INSTALLED FABRICATED REPAIR.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,764 hrs · 27,184 cycles

CABIN FLOOR SUPPORT CORRODED STA 345 TO 365, RBL 25. MAJOR REPAIR ACCOMPLISHED: CORRODED SUPPORT REPLACED PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,644 hrs · 27,142 cycles

STAR CHECKLIST, ITEM 10 EMERGENCY ESCAPE LIGHTS, FLOOR EEL NEXT TO MID LAV INOP. REPLACED EEL STRIP AT MID LAV. PIN AT CONNECTOR MISSING. REPLACED PER AMM, OPS CHECKED GOOD. P/N 6024-3.

Part: LIGHT — INOPERATIVE (REFUEL PANEL) · airframe 72,641 hrs · 27,140 cycles

SINGLE POINT REFUELING PANEL LIGHTS INOPERATIVE. OPS CHECK IAW FIM. FOUND BOTH LIGHTS BURNT OUT. REPLACED TWO FUELING PANEL LIGHTS. OPS CHECK GOOD. AC OK FOR SERVICE.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 72,537 hrs · 27,101 cycles

CAPTAINS NR 1 WINDOW DELAMINATED. REMOVED WINDOW. NEED TO START INSTALLATION FROM STEP 3 PAGE 403 AFTER COMPLETION OF COA 507401. MR 56601-441 OFF WINDOW.

Part: SCUFF PLATE — BENT (CARGO DOORWAY) · airframe 71,810 hrs · 26,862 cycles

FWD CARGO DOOR SCUFF PLATE DAMAGED. ON ARRIVAL RAMP NOTIFIED MAINTENANCE THAT THERE WAS SHEET METAL BENT ON LOWER PORTION OF FWD CARGO DOOR. BENT SECTION IS THE LOWER THRESHOLD SILL AFT CORNER.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,750 hrs · 26,842 cycles

EMERGENCY EXIT INDICATOR LIGHTS AT 950L AND 990R INOPERATIVE. REPLACED M10828 INVERTER. OPS TESTED OKAY.

Part: BONDING WIRE — UNSECURE (FUSELAGE) · airframe 71,640 hrs · 26,803 cycles

BONDING WIRE HANGING FROM THE AFT GAP BETWEEN THE RIGHT MLG DOOR AND LOWER BODY FAIRING. SECURED BONDING WIRE.

Part: RADOME — DAMAGED · airframe 71,275 hrs · 26,685 cycles

STATIC DISCHARGE NEAR RIGHT SIDE OF RADOME. INSPECTED RADOME FOR PINHOLES, PUNCTURES, ETC AND WXR ANTENNA AND WAVE GUIDE FOR DAMAGE. NO DAMAGE FOUND EXCEPT FOR DIVERTER STRIPS. REFERENCE CF 314 FOR DIVETER REPLACEMENT. OK FOR SERVICE PER MM 05-51-19.

Part: WINDOW — SCRATCHED (L2 DOOR) · airframe 70,473 hrs · 26,409 cycles

DOOR 2L WINDOW HAS MANY DEEP SCRATCHES. REPLACED DOOR MOUNTED WINDOW IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,390 hrs · 26,382 cycles

FOUND MID LAV EGRESS LIGHTING NOT WORKING, IN FRONT OF LAV DOOR. REPLACED EMERGENCY LIGHT.

Part: COMPUTER — FAULTY (ELEVATOR FEEL) · airframe 70,379 hrs · 26,377 cycles

TROUBLESHOOTING FOUND THAT THE CENTER AND RIGHT HYDRAULIC SYSTEM HAVE THE HEAVY FEEL WHILE LEFT SYSTEM IS NORMAL. REPLACED ELEVATOR FEEL COMPUTER PER MM. PERFORMED TESTS FOR AUX PITOT SYSTEMS, EICAS MESSAGE TEST FORCES FOR ELEVATOR FEEL SYSTEM AND MCDP GROUND TEST. OPS AND LEAK CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,145 hrs · 26,288 cycles

ONE GREEN EEL STRIP LIGHT SEAT ROW 11 INOPERATIVE. FOUND PINS BROKEN ON LIGHT STRIP. REPLACED PART #36262-4 PCN 560-0806 LIGHT STRIP AND CHECKED OPERATION.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 69,324 hrs · 25,993 cycles

RECEIVED A TRAILING EDGE FLAP DISAGREE EICAS MESSAGE. MESSAGE CAME ON BETWEEN FLAPS 20 & 25. BITE CHECKED FSEU NR1 SHOWED INTERMITTENT FLAP FAULT. CLEARED FAULT, OPERATED FLAPS SEVERAL TIMES ALL CHECKED NORMAL.

Part: HANDSET — FAULTY (CABIN) · airframe 68,135 hrs · 25,545 cycles

CABIN INPH (DESCRIBE PROBLEM: NOISY, INOP, ETC WHEN USING 5 (04=FWD, L, 05=MID L, 06=AFT L) HANDSET. CREW COMMENTS: MID CAN'T TALK TO THE AFT CABIN. REPLACED MID CREW HANDSET, OP CHECK OKAY.

Part: LENS — UNSECURE (CABIN) · airframe 68,119 hrs · 25,539 cycles

EMERGENCY EXIT SIGN HANGING LOOSE MID CABIN RT SIDE FWD. FLOURESCENT LIGHT IS LOOSE AT 15DEF, MADE INTERM REPAIR WITH CLEAR TAPE. LIGHT OPERATION & USEABILITY IS NOT AFFECTED. ADJUSTED LATCH BRACKET AND SECURED EMERGENCY LIGHT LENS.

Part: SKIN — WORN (RT WING TE FLAP) · airframe 67,215 hrs · 25,182 cycles

RIGHT WING INBD FLAP UPPER SURFACE IS WORN AT OTBD END. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE AND BONDED NEW DOUBLER AND INSTALLED IAW SRM AND APPLIED TEFLON PAINT.

Part: COVER — LOOSE (RT OVRWING SLIDE) · airframe 67,215 hrs · 25,182 cycles

RIGHT OVERWING SLIDE COVER IS LOOSE, SLIDE COVER IS UNLACED. R & R THE RT OVERWING SLIDE IAW MM.

Part: SPLICE — DEFECTIVE (CABIN) · airframe 67,215 hrs · 25,182 cycles

OVERHEAD EMERGENCY EXIT SIGN ABOVE SEAT 6B INOP. (LOOKING AFT) SUPPLEMENTAL DATA UPDATE, REMOVED AND REPLACED SPLICE IAW BSWPM. OPS CHECKS NORMAL IAW MM, WORKED ON W-U 34414.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 67,212 hrs · 25,180 cycles

EMERGENCY EXIT LIGHTING END CAP MISSING NEAR 1B AND 34C. REPLACED END CAPS.

Part: DUCT — MISSING (NR 1 ENGINE) · airframe 67,198 hrs · 25,175 cycles

NR 1 ENG ESN 726631 TRANSITION DUCT SECTION BETWEEN HPT-LPT HAS BROKEN LOOSE AND CONTACTED THE LPT 3. DUCT SECTION MISSING AT 6:OO POS. REPLACED ESN 726631 WITH ESN 717942 IN POS 01 PER TOD.

Part: LIGHT — INOPERATIVE (MID LAV) · airframe 66,749 hrs · 25,020 cycles

MID LAV EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT.

Part: FIRE LOOP — FAULTY (LT NACELLE) · airframe 66,230 hrs · 24,821 cycles

EICAS MSG - FIRE OVHT SYS- FIRE OVHT TEST PANEL SYS FAIL LIGHT ON: EICAS MSG - L ENG FIRE LP 2. STATUS MESSAGE ENGINE FIRE LOOP 2. LT ENGINE LOOP 2 INOP. FOUND RT FAN OVERHEAT LOOP CHAFED AT 3 O'CLOCK POSITION, REPLACED LOOP AND ACCOMPLISHED ADJUST AND TEST. OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,375 hrs · 24,486 cycles

EXTERIOR EVACUATION LIGHT INOPERATIVE AT R1 DOOR. RELAMPED.

Part: INDICATOR — FAULTY (TE FLAPS) · airframe 65,285 hrs · 24,450 cycles

SPLIT FLAPS IND, RTFL. REPLACED FLAP INDICATOR. INDICATION CHECKS WITHIN TOLERANCE BANDS AT ALL STOPS UP AND DOWN. VISUAL CHECK OF LEFT TRANSMITTER AND LINKAGE LOOKS OK. VISUAL OF FLAPS AND SLATS DURING MOVEMENT CHECKS GOOD.

Part: SMOKE GOGGLES — FAULTY (COCKPIT) · airframe 63,996 hrs · 23,955 cycles

CAPT AND OBSERVER'S SMOKE GOGGLE BANDS HAVE NO ELASTICITY. GOGGLES FOUND FAULTY. REPLACED BOTH GOGGLES.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,492 hrs · 23,766 cycles

EEL BETWEEN ROWS 17 AND 23 INOPERATIVE. REPLACED BATTERY P/N 2013-1 AND POWER SUPPLY 2012-1 M10770.

Part: LIGHT — MISSING (CABIN) · airframe 63,343 hrs · 23,708 cycles

EEL STRIP MISSING IN FRONT OF CLOSET BY DOOR 1L. CONNECTOR CONTACTS EXPOSED. REPLACED MISSING SECTION OF EEL LIGHTING. ACCOMPLISHED OPERATIONAL TEST. FOUND OPERATIONS NORMAL.

Part: COVER — DAMAGED (CABIN) · airframe 63,123 hrs · 23,616 cycles

EXIT FLOOR LIGHTING IN AFT OF AIRCRAFT IS COMING UP. REPLACED DAMAGED COVER SECTION. EMERGENCY LIGHTS TEST GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,112 hrs · 23,611 cycles

EXTERIOR EVAC LIGHT INOP AT DOOR 4LT. RELAMPED EXTERIOR EVAC LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 62,693 hrs · 23,447 cycles

NR 4 LT DOOR EMERGENCY EXIT LIGHT INOP (EXT). RELAMPED, OPERATES NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,269 hrs · 23,277 cycles

AFT CARGO DOOR EXTERIOR EMERGENCY ESCAPE PATH LIGHT INOP. REPLACED LAMP, OPS GOOD.

Part: SLIDE — UNDERSERVICED (R2 DOOR) · airframe 61,806 hrs · 23,101 cycles

MED 2 RIGHT EMER SLIDE MISSING MR NUMBER ON VALISE. REF LM 1045. REPLACED 2 RIGHT MED SLIDE.

Part: BEARING — CORRODED (R4 DOOR) · airframe 61,330 hrs · 22,911 cycles

R-4 DOOR WILL NOT ARM-DISARM. FOUND LOWER ARM-DISARM TORQUE TUBE INBOARD BEARING RUSTED AND FROZEN. REPLACED BEARING.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 60,950 hrs · 22,753 cycles

UNABLE TO MAINTAIN CABIN PRESSURE. FLIGHT DIVERTED.

Part: CLAMP — DETACHED (CABIN PRESSURE) · airframe 60,950 hrs · 22,753 cycles

UNABLE TO MAINTAIN CABIN PRESSURE. FLIGHT DIVERTED. FOUND LT PACK SUPPLY CK VALVE CLAMP OFF. REINSTALLED CLAMP. RT PACK PERRY SEAL IS LEAKING AT ACM OUTLET. REPLACED PERRY SEALS. RT PACK OVERHEAT SWITCH BOSS SEPARATED FROM DUCT. REPAIRED ATTACHING BOSS AND INSTALLED DUCT.

Part: BEARING — MISSING (TE FLAP) · airframe 60,445 hrs · 22,546 cycles

RT WING T/E FLAP AFT FLAP INBOARD SUPPORT TRACK LOWER AFT BEARINGS ATTACHED ON T/E FLAP REAR SPAR ARE MISSING AND THRU BOLT IS SHEARED OFF. REPLACED ROLLER SUPPORT ASSY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 60,165 hrs · 22,438 cycles

EEL LIGHTS INOP ROWS 1-6. REPLACED EMERGENCY BATTERY M732, OPS OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,165 hrs · 22,438 cycles

EMERGENCY EXIT LIGHTS INOP ROWS 9 AND 13. REPLACED EMERGENCY BATTERY M732, OPS OK.

Part: MICROPHONE — FAULTY (OXYGEN MASK) · airframe 59,593 hrs · 22,217 cycles

FIRST SEAT O2 MASK MIC INOP. *S/D* REPLACED O2 MASK.

Part: LIGHT — DAMAGED (CABIN) · airframe 59,009 hrs · 22,024 cycles

ESCAPE LIGHTING ON FLOOR BETWEEN ROWS 12 & 13 IS NEEDING REPAIR. REPAIRED LENS STRIP.

Part: UNKNOWN — ODOR (CABIN) · airframe 58,816 hrs · 21,951 cycles

FLIGHT ATTENDANT REPORTS A "HOT PACK DUCTING" SMELL NEAR HER JUMP SEAT AT DOOR 2L. CHECK ELECTRICAL EQUIPMENT AROUND DOOR 2L FOR ANY BURNT AND ELECTRICAL SMELL. REMOVED AND INSPECTED AREA ABOVE DOOR 2L. NO ABNORMALITY FOUND AND NO BAD SMELL. CHECKED WITH PACKS RUNNING AND NOTICED NO HOT AIR SMELL.

Part: VALVE — OPEN (POTABLE WATER) · airframe 58,715 hrs · 21,916 cycles

POTABLE WATER INDICATION CAUSED FLIGHT DIVERSION. SUPPLEMENTAL DATA UPDATE CAUSE, LAV DRAIN VALVE IN LAV 2L WAS OPEN. CLOSED DRAIN VALVE IN LAV 2L, SERVICED LAVS, NO LEAKS NOTED.

Part: GIRT BAR — DIRTY (DOOR 1R) · airframe 58,508 hrs · 21,833 cycles

DOOR 1R WILL CLOSE BUT NOT ARM. FOUND DEBRIS UNDER GIRT BAR. CLEANED DEBRIS, DOOR ARMS/DISARMS NORMALLY.

Part: LAMP — INOPERATIVE (SLIDE ARM) · airframe 58,227 hrs · 21,738 cycles

DOOR 2L ARM LIGHT NOT ILLUMINATED WITH DOOR ARMED. CYCLED ARMING LEVER, NO HELP. FOUND LAMP IS OUT IN INDICATOR. RELAMPED DOOR ARM SWITCH AT DOOR 2L AND RESET GIRT BAR, OVERHEAD CB OPS CHECKED NORMAL.

Part: LIGHT — LOOSE (CABIN) · airframe 57,683 hrs · 21,550 cycles

EMERGENCY FLOOR LIGHTING LOOSE NEAR 12C. RESECURED LIGHTING.

Part: FITTING — OUT OF ADJUST (DOOR 1R GIRT BAR) · airframe 56,435 hrs · 21,102 cycles

DOOR 1R DOES NOT HAVE ARM LIGHT WHEN DOOR IS ARMED AND CREW STATES THAT DOOR DOES NOT FEEL NORMAL WHEN ARM SELECTED.

Part: PUSHROD — FAULTY (R1 DOOR GIRT BAR) · airframe 56,163 hrs · 21,003 cycles

DOOR 1R: DIFFICULT TO ARM, TOOK NUMEROUS ATTEMPTS BEFORE IT ARMED. SAMC TEXT: ARM LT INTERMITTENT IN FLT. ADJUSTED GIRT BAR PUSH ROD

Part: SKIN — DAMAGED (L2 DOOR) · airframe 56,134 hrs · 20,988 cycles

L-2 DOOR IS DAMAGED AT UPPER HINGE CUTOUT. FABRICATED AND INSTALLED A FORMED ANGLE DOUBLER.

Part: SKIN — DAMAGED (R2 DOOR) · airframe 56,134 hrs · 20,988 cycles

R-2 DOOR IS DAMAGED AT UPPER HINGE CUTOUT. FABRICATED AND INSTALLED A FORMED ANGLE DOUBLER.

Part: SKIN — MISREPAIRED (BS 600) · airframe 56,134 hrs · 20,988 cycles

EXTERNAL FUSELAGE EXTERNAL DOUBLER AT STA 600 LT SIDE HAS NO MINIMUM DISTANCE FROM EXISTING FLUSH REPAIR. MAJOR REPAIR ACCOMPLISHED. PERFORMED A FUSELAGE EXTERNAL DOUBLER REPAIR AT STA 600 LH SIDE WITHOUT A MINIMUM DISTANCE FROM EXISTING FLUSH REPAIR. THIS IS AN INTERM REPAIR REQUIRING SUPPLEMENTAL INSPECTIONS STARTING AT 50000FC. THEN INSPECT UPPER AND LOWER SKIN PANEL LAP SPLICE EVERY 3000FC. A DETAILED VISUAL INSPECTION IS THEN REQUIRED EVERY 12000FC.

Part: GATE — DAMAGED (L2 DOOR LWR) · airframe 56,134 hrs · 20,988 cycles

L-2 DOOR LWR GATE HAS CORROSION AND FOUND MISDRILLED HOLES AT RUB STRIP AND EDGES. REPLACED LOWER DOOR GATE

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,134 hrs · 20,988 cycles

MAIN CABIN FLOORBEAM STA 365 RBL 20 TO RBL 50 HAS SURFACE CORROSION. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED T-CAP, RBL 20 TO CUSP. FABRICATED T-CAP. INSTALLED ANGLE DOUBLER & STRAP.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,134 hrs · 20,988 cycles

AT BS 680 STRINGER 14L FWD OF L2 DOOR THERE IS A STRESS CRACK AT THE INTERCOSTAL STRUCTURE. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED INTERCOSTAL & STRINGER.

Part: FRAME — DENTED (FUSELAGE) · airframe 56,134 hrs · 20,988 cycles

DENTED FRAME STA 1580 BETWEEN STR 25-26L IN AFT PIT. [08-17-07] MAJOR REPAIR ACCOMPLISHED. REPAIRED PER UA ENGINEERING SPECIFICATIONS.

Part: SCREW — CORRODED (GIRT BAR) · airframe 56,134 hrs · 20,988 cycles

R-1 DOOR SLIDE, CENTER GIRT BAR SUPPORT, 2 EACH SCREWS CORRODED. [08-17-07] REPLACED SUPPORT PLATE.

Part: FRAME — DENTED (FUSELAGE) · airframe 56,134 hrs · 20,988 cycles

DENTED FRAME STA 1500, STR 25L IN AFT PIT. [08-17-07] MAJOR REPAIR ACCOMPLISHED. REPAIRED PER UA ENGINEERING SPECIFICATIONS.

Part: SUPPORT — CORRODED (GIRT BAR) · airframe 56,134 hrs · 20,988 cycles

R-4 DOOR SLIDE, CENTER GIRT BAR SUPPORT IS CORRODED. [08-17-07] REMOVED AND REPLACED SUPPORT PLATE.

Part: SUPPORT — CORRODED (GIRT BAR) · airframe 56,134 hrs · 20,988 cycles

L-2 DOOR SLIDE, CENTER GIRT BAR ATTACH SUPPORT, ON SLIDE ASSY, IS CORRODED. [08-17-07] REPLACED SUPPORT PLATE.

Part: PRESSURE PANEL — DAMAGED (BS 1681-1697) · airframe 56,134 hrs · 20,988 cycles

DURING HMV CORROSION DAMAGE REPAIRS WERE ACP AT AFT PRESS DECK BS 1681 BETWEEN RBL 8.75 - 10.25 & BS 1697 RBL 50.25.

Part: TARGET — DIRTY (PROX SENSOR) · airframe 55,749 hrs · 20,850 cycles

LEFT AFT ENTRY DOOR EICAS ON GROUND TAXIING IN. INDICATIONS NORMAL AT GATE. *S/D* CLEANED DEBRIS FROM PROXIMITY TARGET PLATE AND GROUND PROX SENSOR. NO COMPONENTS REPLACED.

Part: FRAME — MISREPAIRED (BS 223) · airframe 55,331 hrs · 20,693 cycles

STA 223 FRAME IS DAMAGED ON UPPER RADIUS, 6 O'CLOCK POSITION, JUST FWD OF NOSE COMPARTMENT DOOR CUTOUT. [SUP 05-16-07] MAJOR REPAIR ACCOMPLISHED. STA 223 FRAME IS DRILLED WITH A .375 INCH HOLE ON UPR RADIUS, DUE TO PREVIOUS IMPROPER REPAIR, HFEC INSPECTED ROUTED OUT HOLE AND VERIFIED NO CRACKS OR ADDITIONAL DAMAGE EXISTS. INSTALLED REPAIR DOUBLER.

Part: SKIN — DAMAGED · airframe 38,345 hrs · 14,386 cycles

FUSELAGE SKIN DAMAGED STATION 1697 AT STRINGER 20LT AND STRINGER 21LT. MAJOR REPAIR ACCOMPLISHED.STRINGER 20LT AND 21LT REPAIRED. FILER AND DOUBLER INSTALLED.

Part: IDG · airframe 37,564 hrs · 14,101 cycles

L GEN OFF AND L GEN DRIVE EICAS MSG'S DISPLAYED. SUPPLEMENTAL DATA UPDATE IDG CHECK VALVE FITTING LEAKING.REPLACED IDG.

Part: INTERCOSTAL — CORRODED · airframe 37,496 hrs · 14,081 cycles

CABIN FLOOR INTERCOSTAL CORRODED. STA 365 TO 377, RBL 10. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW INTERCOSTAL AND GALLEY SUPPORT CHANNEL.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 37,496 hrs · 14,081 cycles

CABIN FLOOR INNER CREASE BEAM CORRODED. STA 740-780, RBL 60. MAJOR REPAIR ACCOMPLISHED.INSTALLED J-ANGLE REPAIR.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 37,496 hrs · 14,081 cycles

CABIN FLOOR INNER CREASE BEAM CORRODED. STA 900-1040 RBL 70-75. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW CREASE BEAM AND WEB.

Part: CREASE BEAM — CORRODED · airframe 37,496 hrs · 14,081 cycles

CABIN FLOOR INBOARD CREASE BEAM CORRODED. STA 720-740, LBL 59. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW CREASE BEAM AND Z-ANGLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,496 hrs · 14,081 cycles

CABIN FLOOR BEAM CORRODED. STA 365, RBL1-RBL 27. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 37,496 hrs · 14,081 cycles

CABIN FLOOR PRESSURE DECK CORRODED. STA 1680, RBL 9.5. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 37,496 hrs · 14,081 cycles

CABIN FLOOR PRESSURE DECK CORRODED. STA 1965, RBL 52. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.

Part: CHANNEL — CORRODED · airframe 37,496 hrs · 14,081 cycles

CABIN FLOOR SUPPORT STRUCTURE CORRODED. STA 1660-1680, RBL 65. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW J-CHANNEL.

Part: CARBON SEAL — FAILED (LP COMPRESSOR) · airframe 34,053 hrs · 12,837 cycles

BURNING OIL SMELL IN COCKPIT AND CABIN. UPON ENGINE DISASSEMBLY, FOUND ENGINE OIL IN THE LOW PRESSURE COMPRESSOR SHAFT. PRESSURE CHECK OF THE NR 1 MAINLINE BEARING CARBON SEAL CONFIRMED THAT THE CARBON SEAL HAD FAILED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 32,738 hrs · 12,343 cycles

FUSELAGE DAMAGE. *S/D* IMPACTED BY SERVICE TRUCK DURING TRUCK POSITIONING. DAMAGE REPAIRED WITH EXTERNAL DOUBLER .063 INCH THICK FROM APPROX BS 1596 TO 1618, EXTENDING JUST ABOVE S-18L AND DOWN OVER LAP JOINT AT S-20L WITH REPAIR TRIPLER .056 INCH THICK BELOW LAP JOINT. STRINGER S-19L REPAIRED WITH ADAPTATION OF SRM 53-00-03 REPAIR. RESULTED IN MAJOR REPAIR MRA NR 109.

Part: VALVE — NOT CLOSED (WATER SYS)

DIVERTED TO DEN DUE TO ABNORMAL NOISE UNDER AFT GALLEY. *S/D* THIS IS THE FIRST HIT FOR THIS TYPE OF PROBLEM ON THIS AIRCRAFT. MAINTENANCE FOUND THAT THE POTABLE WATER FILL VALVE WAS PARTIALLY OPEN, VENTING AIR PRESSURE OVERBOARD. NO OTHER DESCREPANCIES WERE FOUND. THE PROBLEM HAS NOT OCCURRED SINCE.

Part: FAN — FAILED (COCKPIT)

ELECTRIC SMOKE ODOR DETECTED IN COCKPIT. LATER, EQUIPMENT COOLING OVERHEAT LIGHT CAME ON, AND FWD EQUIPMENT COOLING SUPPLY FAN 1 CB POPPED. SMOKE ODOR DISSIPATED WHEN ALTERNATE FAN WAS SELECTED. *S/D* ELECTRICAL SMOKE ODOR WAS CAUSED BY A FAULTY EQUIPMENT COOLING FAN. THE FAN WAS REPLACED.

Part: RESERVOIR — BLOWN (DOOR 2L)

DOOR 2L HARD TO OPEN ON ARRIVAL AT GATE. *S/D* FOUND 2L DOOR OUT OF SEQUENCE AFTER DOOR OPENED PARTIALLY FROM OUTSIDE WHILE STILL ARMED. FOUND EMERGENCY POWER RESERVOIR BLOWN. REPLACED RESERVOIR AND RESEQUENCED DOOR, OPS CHECKS NORMAL.

Part: SLIDE — OUT OF ADJUST (DOOR 1R)

DOOR ARM CONTROL ROD INTERFERING WITH FABRIC THAT WRAPS AROUND THE GIRT BAR AT CENTER AND BOTTOM OF DOOR. ADJUSTED DOOR ARM CONTROL ROD AND FABRIC THAT WRAPS AROUND THE GIRT BAR AT CENTER OF DOOR AT THE BOTTOM TO ELIMINATE INTERFERENCE.

Part: HYD PANEL — SHORTED (FLIGHT DECK)

STRONG ELECTRICAL BURNING SMELL IN FLIGHT DECK. *S/D* LEFT ELECTRICAL PUMP SWITCH ON PILOTS OVERHEAD P5 PANEL SHORTED. REPLACED HYDRAULIC CONTROL PANEL, OPERATIONS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHT INOP AT ROW 26. REPLACED BATTERY PACK, CHECKS OK.