N521UA

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 75,120 hrs · 27,859 cycles

VERY STRONG ODOR IN COCKPIT & CABIN AFTER TAKEOFF. OIL CHEMICAL ODOR DISSIPATED AFTER 5 MINS. RAN ENG'S & PACKS, NO SMELL OR ODOR.

Part: UNKNOWN — ODOR (GALLEY) · airframe 75,120 hrs · 27,859 cycles

FLT ATTENDANTS SAY THEY CAN DETECT AN ODOR IN THE AFT GALLEY, ODOR OF JET FUEL ONE HOUR INTO. DEFERRING AFT GALLEY FWD SECTION CHILLER DUE TO SMELL WHEN CARTS PLUGGED IN, WHEN CARTS REMOVED THERE IS NO SMELL UNLESS YOU OPEN CHILLER PORTS WITH UNIT RUNNING. PARTS 581-2053 & MR23371 P5057/DEN/06DEC LOB N.

Part: UNKNOWN — MALFUNCTIONED (FLIGHT CONTROL) · airframe 74,813 hrs · 27,757 cycles

DUE TO REPORT OF UNCOMMANDED NOSE PITCH DOWN PERFORM THE FOLLOWING: AUTO FLIGHT FAULTS BITE FIM MM22-00-02-101, PAY PARTICULAR ATTENTION TO ANY FCC & STAB TRIM RELATED FAULTS. BITE OF BOTH SAM MODULES IAW MM27-09-00-150 FIG.106 & TEST SAMS IAW MM27-09-00 P210. PERFORM A DVI & GVI OF THE STAB BALL SCREW ASSEMBLY IAW MM 27-41-10 PGS.607-613. ELEVATOR OPERATIONAL CHECK IAW MM27-31-00-501. STAB TRIM OPERATIONAL CHECK IAW MM 27-41-00-501. BITE BOTH ADCS IAW MM34-12-00 FIG109 PG112. INSPECT PITOT PROBES IAW MM34-11-01-601. CORRECT ALL DISCREPANCIES FOUND. ACP STEPS 2 TO 7 ALL OPERATIONS CHECKED & VISUAL INSP WERE GOOD. STEP 1 WAS ACP IAW PTT SEQ 8132003.

Part: MODULE — FAULTY (ELEVATOR) · airframe 74,813 hrs · 27,757 cycles

STABILIZER TRIM FAULTS DUE TO AN UNSCHEDULED STAB TRIM MOVEMENT & NO DEFINITIVE FINDINGS DURING TESTING IAW AM1568 & PTT 8132005. ACCOMPLISHED A MACH TRIM & SPEED STABILITY TEST IAW MM22-24-00 P501. REPLACED THE STAB TRIM ELEVATOR ASYM MODULES LT & RT & RECORDED NO FAULTS IAW AMM27-09-00.

Part: MINITEL — DEFECTIVE (COCKPIT) · airframe 74,690 hrs · 27,711 cycles

NR 1 PILOT'S HEADSET IS DEFECTIVE. SPARE MINITEL USED, REPLACED MINITEL.

Part: B-NUT — LOOSE (HYDRAULIC SYS) · airframe 74,666 hrs · 27,699 cycles

HYDRAULIC LEAK EVIDENCE UNDER RT WING RT AILERON. ACCOMPLISHED OPERATIONAL CHECK OF RT AILERON SYSTEM. TIGHTENED AILERON B-NUT UNIONS, NO LEAKS NOTED IAW AMM-29-00-99.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 74,489 hrs · 27,631 cycles

AISLE SOFT AT ROW 26 & 27. REMOVED & INSTALLED FLOOR BOARD AT ROWS 26 & 27 IAW AMM 53-01-01.

Part: MODULE — FAULTY (SPOILER SYS) · airframe 74,489 hrs · 27,631 cycles

EICAS MESSAGE 'SPOILERS' DISPLAYED WITH FLAPS SET AT 25 OR 30. CREW REPORTS "SPOILERS" EICAS MESSAGE DISPLAYED ON TAXI OUT AFTER SECOND ENGINE START, FLAPS AT 5, AT ARRIVAL. UNABLE TO CLEAR EICAS MESSAGE & OVERHEAD LIGHT. CYCLED CIRCUIT BREAKERS & DEPOWERED ACFT, NO HELP. ALL SCMS BITE CHECKED GOOD BUT UNABLE TO DETERMINE CAUSE. WIGGLED ALL SCMS & NOTED 1L MODULAR WOULD CAUSE FAULTS AS DESCRIBED. REPLACED IAW MM & ALL CHECKED GOOD. MESSAGE CLEARED & OPERATIONS OK.

Part: STRUCTURE — DAMAGED (NR 2 PYLON) · airframe 74,489 hrs · 27,631 cycles

NR 2 PYLON STRUCTURE HAS DAMAGE.

Part: LINE — LOOSE (FUEL SYSTEM) · airframe 74,489 hrs · 27,631 cycles

NR 2 ENGINE PYLON MAIN FUEL LINE AT BULKHEAD IS LOOSE. REMOVED FUEL LINE & BULKHEAD FITTING. FOUND CRACK IN PYLON WHERE FITTING IS ATTACHED. ACCOMPLISHED REPAIR ON CRACKED NR 2 PYLON STRUCTURE.

Part: TRANSCEIVER — MALFUNCTIONED (WX RADAR SYS) · airframe 74,164 hrs · 27,529 cycles

WEATHER RADAR VERY WEAK, RETURNS ON OBSERVED PRECIPITATION WITHIN 80 NM. NO RETURNS EXCEPT GROUND ABOVE 80. R & R WEATHER RADAR TRANSCEIVER.

Part: MECHANISM — DIRTY (ELEVATOR FEEL) · airframe 74,092 hrs · 27,507 cycles

MORE THAN NORMAL FORE-AFT PLAY IN BOTH YOKES IN BOTH MANUAL AND AUTOPILOT FLT. APPROX 1 INCH. IAW MM27-31-00, VERIFIED ELEVATOR CONTROL IS ADJUSTED CORRECTLY PG 529. WHILE TROUBLESHOOTING ELEVATOR FEEL UNIT, FOUND DIRT AND GREASE BUILD UP ON CAM DETENT ROLLER OF ELEVATOR FEEL MECHANISM. CLEANED MECHANISM AND PERFORMED ELEVATOR FEEL CHECK IAW 27- 31-17, PG 219, PARA 9. OPS NORMAL AFTER REMOVING RIG PINSE-ST7 AND E-ST6.

Part: THRESHOLD — DAMAGED (L2 DOORWAY) · airframe 73,506 hrs · 27,328 cycles

L2 DOOR HAD A LOUD SQUEAL DURING DESCENT, BEGINNING AT 20,000 FT. REMOVED AND REPLACED LOWER AFT THRESHOLD.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,414 hrs · 27,303 cycles

EMERGENCY EXIT SIGN INOPERATIVE AT L4 DOOR. REPLACED FUSE IN BATTERY CHARGER. LIGHT OPS NORMAL IAW AMM 33-51-07, WDM 33-51-15.

Part: LENS — MISSING (CABIN) · airframe 73,265 hrs · 27,256 cycles

DOOR 2L THRESHOLD LIGHT IS MISSING THE LENS COVER. LAMP REMOVED REF IPC 33-20-51-002 NEED ITEM 238. P/N 25-1116-1. COMPLIED WITH MEL. INF- :170-4384 IS THE BEZEL ASSY. REPAIR- :INSTALLED LAMP AND BEZEL ASSY, OPS CHECKED NORMAL.

Part: CAP — MISSING (CABIN) · airframe 73,253 hrs · 27,253 cycles

EEL TRACK END CAPS MISSING, 8C AND 40C. REPLACED END CAPS 8C AND 40C.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 73,179 hrs · 27,229 cycles

EMERGENCY LIGHT END CAP MISSING NEAR SEAT 8C. REPLACED EMERGENCY LIGHT END CAP.

Part: SMOKE DETECTOR — MISWIRED (FWD LAV) · airframe 73,088 hrs · 27,201 cycles

FOUND CB N8 AT P11 POPPED WHEN FIRST CLASS LAV DOOR LATCH SWITCH LOCKED. CONNECTOR D42 CHECKED NO DAMAGE FOUND. FOUND SMOKE DETECTOR WIRES IN FWD LAVATORY INSTALLED INCORRECTLY. INSTALLED AND SECURED WIRES REF WDM 26-14-11, OPS CHECKED GOOD.

Part: CIRCUIT BREAKER — TRIPPED · airframe 73,088 hrs · 27,201 cycles

DOOR GIRT BAR ENTRY DIM CIRCUIT BREAKER R34 TRIPPED. CYCLED SYSTEM POWER. OPS CHECKED ARM DISARM LEVER OF ALL MED DOORS FEW TIME, CIRCUIT BREAKER R34 NOT POPPED.

Part: SKIN — DENTED (BS 607, STR 16L) · airframe 73,083 hrs · 27,199 cycles

SKIN DENTED BS 607, BELOW STRINGER 16L. INSTALLED SKIN DOUBLER REPAIR PER ECRA 5330-04460, AND EA 130227 REV IR.

Part: SKIN — DENTED (BS 820 S17L) · airframe 73,083 hrs · 27,199 cycles

SKIN DENTED BS 820, ABOVE STRINGER 17L. INSTALLED DOUBLER REPAIR PER EA 130246, ECRA 5330-04465.

Part: DOOR FRAME — CORRODED (R1 DOORWAY) · corrosion level 2 · airframe 73,083 hrs · 27,199 cycles

R1 DOOR AFT CUTOUT FRAME HAS CORROSION AT WL 207. REMOVED DAMAGED SECTION OF FRAME AND INSTALLED SLICE DOUBLER RPR SRM 53-10-15 AND EA 130272.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 73,083 hrs · 27,199 cycles

FLOORBEAM UPPER AND LOWER SURFACE AT FLOORBOARD ATTACH HOLES CORRODED STA 365, RBL 10- RBL 50. TRIMMED UPPER SECTION OF DAMAGED TEE CAP AND INSTALLED ANGLE STRAP REPAIR PER ECRA 5310-05536.

Part: FLOORBEAM — CORRODED (BS 1661) · corrosion level 2 · airframe 73,083 hrs · 27,199 cycles

CABIN FLOORBEAM TEE CAP HAS CORROSION BS 1661, BL 0 TO LBL 25. INSTALLED TEE CAP SECTION FILLER ANGLE REPAIR PER ECRA 5310-05536 AND SRM 53-00-51.

Part: STRINGER — DAMAGED (BS 607 S16L) · airframe 73,083 hrs · 27,199 cycles

STRINGER 16L IS DAMAGED AT BS 607. INSTALLED STRINGER SPLICE REPAIR PER EA 130227 REV IR AND ECRA 5330- 04460.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 73,083 hrs · 27,199 cycles

RIGHT WING INBOARD AFT FLAP UNDERSIDE SKIN OUT OF CONTOUR. REMOVED AND REPLACED RT INBOARD AFT FLAP.

Part: FRAME — DAMAGED (BS 365.25 S17R) · airframe 73,083 hrs · 27,199 cycles

FRAME WEB IS PARTIALLY CUT ON FWD SIDE BS 365.25 S17R. REMOVED DAMAGED FRAME BS 365.25 FABRICATED SPLICE AT RT WL190. ACCOMPLISHED REPAIR IAW EA 130272 AND ECRA 5310- 05704.

Part: FLOORBEAM — GOUGED (BS 1600) · airframe 73,083 hrs · 27,199 cycles

PASSENGER CABIN AFT WET AREA BS 1600 LBL 15 RBL 22 FLOORBEAM TEE GOUGED. REMOVED DAMAGE OUT OF LIMITS. REPAIRED AREA. IAW EA130218 & ECRA 5360-01266.

Part: FLOORBEAM — CORRODED (BS 377) · corrosion level 2 · airframe 73,083 hrs · 27,199 cycles

BS 377 RBL 49 FLOORBEAM UPPER TEE HAS SMALL AREA OF CORROSION. REPAIRED FLOORBEAM IAW EA 130222 & ECRA5310-05698.

Part: SKIN — DAMAGED (BS 1385-1401) · airframe 73,083 hrs · 27,199 cycles

MAJOR REPAIR REF TASK CARD 59745401C ACCOMPLISH DOUBLER REPAIR AT LOWER FUSELAGE STA 1393 PER ITEM 2A. SKIN REPAIR BS 1385-1401 BETWEEN STR 28 LT-STR 29 RT AS STAGE 2 PER FAA FORM 8100-9. MAJOR REPAIR ACCOMPLISHED. INSTALLED EXTERNAL DOUBLER REPAIR AT STA 1393 STR 28L-24R IAW ECRA5360-01265. THRESHOLD TO BEGIN SUPPLEMENTAL INSPECTION 58,600 PTC.N EW8100-9 MUST BE RECVD PRIOR TO AIRCRAFT REACHING 58,600 PTC WITH METHOD OF INSPECTION & INTERVAL STAGE 3. IF NEW 8100-9 NOT RECVD PRIOR 58.600. AIRCRAFT UNSERVICEABLE.

Part: CHANNEL — CORRODED (BS 345-365) · corrosion level 2 · airframe 73,083 hrs · 27,199 cycles

BS 345-365 RBL 60 HAT CHANNEL UPPER AND LOWER SURFACE CORRODED. HAT CHANNEL WAS FOUND WITH 100% MATERIAL LOSS. REMOVED AND REPLACED HAT CHANNEL IAW SRM 51-40-02 & DWG 141N5160. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 1433) · airframe 73,083 hrs · 27,199 cycles

TASK CARD 59745401C ACCOMPLISH DOUBLER REPAIR ON LOWER FUSELAGE AT STA 1433 PER ITEM 2A OF TASK CARD. FABRICATED DOUBLER PER SRM 53-00-01 TABLE 1 REPAIR 3 & REPEAT INSPECTION 37,500 PTC PER SRM 53-00-01 REPAIR 3 TABLE V FLAG J. REMOVED EXISTING DOUBLER REPAIR, NDT CUT-OUT EXISTING HOLES, FABRICATED LOCATED DRILLED & INSTALLED NEW DOUBLER REPAIR STA 1433 PER SRM 53-00-01.

Part: CREASE BEAM — CORRODED (BS 1661-1681) · corrosion level 2 · airframe 73,083 hrs · 27,199 cycles

BS 1661 - 1681 RBL 55, CREASE BEAM HAS CORROSION. INSTALLED NEW CREASE BEAM REF DWG 146N5230, SRM 51-40-02, AND SRM 53-00-04. MAJOR REPAIR.

Part: SHEAR TIE — CRACKED (BS 600) · airframe 73,083 hrs · 27,199 cycles

SHEAR TIE CRACKED AT BS 600, S16-17L. INSTALLED NEW SHEAR TIE. FABRICATED IAW DWG 140N2002-53, SRM 51-40-02, & SRM 51-40-05. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 73,083 hrs · 27,199 cycles

CABIN FLOORBEAM BS 1640, LBL 17 TO RIGHT CREASE BEAM TEE HAS CORROSION. REMOVED DAMAGED TEE SECTION AND SPLICED IN REPAIR PER ECRA 5310-05536. MAJOR REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,083 hrs · 27,199 cycles

FLOORBEAM CORRODED AT STA 1661 RBL 58 WL 208 CREASE FLOORBEAM AS MARKED. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION AT FLOORBEAM STA 1661 RBL 58 WL 208 BELOW CREASE BEAM IAW SRM 53-00-51 ORIG T .125 MAT LOSS .042 FOUND OUT OF LIMITS. ACCOMPLISHED ECRA 531 0-05536 CMPLD NDT INSP IAW NDTM 51-00-19 AND 51-00-16.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,083 hrs · 27,199 cycles

STA 1681.8 BL 0 52R GALLEY FLOOR DECK PLATE HAS CORROSION. REMOVED CORROSION FOUND TO BE 100% MATERIAL LOSS BL 0 REMOVED FASTENERS FOR ACCESS FROM FROM STA 1681 BL 0-52R. PERFORMED UT ORIG T .071 REMAINING T .064 LOSS OF .007 FOUND TO BE WITHIN LIMITS REPAIRED BS1681 BL 0 IAW ECRA5330-04259.

Part: SKIN — GOUGED (BS 760-747) · airframe 73,083 hrs · 27,199 cycles

SKIN DOUBLER GOUGED BS 760-747, S15 - 16L. REMOVED DOUBLER REPAIR, INSTALLED NEW DOUBLER REPAIR PER SRM 53-00-01, REPAIR 3, FIG 201. THIS A CAT B REPAIR IN ZONE A. PER SRM 53-00-01 REPAIR 3, TABLE V.

Part: SKIN — GOUGED (FUSELAGE) · airframe 73,083 hrs · 27,199 cycles

SKIN IS GOUGED STA 1360, STR 30. MAINT TEXT: CUT OUT SKIN DAMAGE AND INSTALLED DOUBLER REPAIR. THIS IS A CAT B REPAIR. PER SRM 53-00-01 REPAIR 2, ZONE A, MUST REINSP START 37,500C FROM REPAIR INSTALL. CURRENT PTC 27199C. REQUIRES HFEC INSP, AND EVERY 6000C THEREAFTER. INSTALLED DOUBLER REPAIR PER SRM 53- 00-01 REPAIR 2. N-R 1701082.

Part: SIGN — INOPERATIVE (CABIN) · airframe 72,915 hrs · 27,141 cycles

SEAT 21F LIGHT ASSY INOPERATIVE ABOVE EMERGENCY EXIT. REPLACED LIGHT ASSY. OPS CHECK NORMAL.

Part: CABLE — FAILED (EMERGENCY LIGHT) · airframe 72,795 hrs · 27,106 cycles

EMERGENCY LIGHTING AT FIRST CLASS COAT CLOSET IS INOPERATIVE. REPLACED LEAD CABLE OPS CHECKED GOOD.

Part: PLATE — OUT OF ADJUST (CABIN) · airframe 72,408 hrs · 26,981 cycles

AIR FLOW FROM DOOR 2R TO OVERWING IS VERY NOISY. FOUND RESTRICTOR PLATE AT ROW 9 HAD AIR GAP. ADJUSTED AND SECURED.

Part: HOSE — DEFECTIVE (OXYGEN MASK) · airframe 71,296 hrs · 26,599 cycles

OXYGEN MASK HOSE DEFECTIVE AT2 (1=CAPT, 2=1ST OF, 3= 1ST OBS). FIRST OFFICER OXYGEN HOSE AROUND HEAD POPPED WHEN DONNED AND DOESN'T HOLD AIR. REPLACED MASK ASSY.

Part: BATTERY — FAULTY (MAIN) · airframe 71,290 hrs · 26,597 cycles

EICAS MESSAGE, MAIN BATTERY CHARGER DISPLAYED AND BATTERY DISCHARGE LIGHT EXTINGUISHED. REPLACED MAIN AIRCRAFT BATTERY, OPS CHECKED GOOD.

Part: HINGE — BROKEN (SLIDE COVER) · airframe 71,260 hrs · 26,584 cycles

SMALL OVERWING SLIDE ACCESS PANEL ON RT SIDE, TOP PART PROTRUDES APPROX 1-4 INCH. REPLACED BROKEN HINGE ASSY ON OFF WING SLIDE HANDLE COVER.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,957 hrs · 26,483 cycles

WHILE TROUBLESHOOTING DF792 FOUND EEL FLOOR LIGHTING INOP AT ROW 21 ABC THROUGH 24 ABC. ALSO INOP FROM ROW 34 ABC TO 40 ABC. PERFORMED OPS CHECK PER A MM 33-51-00 PG 501 ALLOWED BATTERY PACKS TO CHARGE, OPS CHECK GOOD.

Part: WINDSHIELD — CHIPPED (COCKPIT) · airframe 69,749 hrs · 26,057 cycles

F/O AFT WINDOW R3 OVAL CHIP ON INSIDE PANE. PEEL CHIP LOCATED APPROX CENTER OF WINDOW.

Part: DUCT — DETERIORATED (CABIN) · airframe 68,783 hrs · 25,692 cycles

CEILING AIR VENTS VERY LOUD. REMOVED CEILING PANELS, HAVE DETERIORATED DUCT AT RISER SECTION ROW 10-12, WILL REQUIRE REPLACEMENT. MULTIPLE REPAIRS REQUIRED AT ROWS 6, 32-34.

Part: GUST LOCK — FAULTY (R1 DOOR) · airframe 68,781 hrs · 25,691 cycles

UNABLE TO OPEN DOOR 1R. REPLACED DOOR GUST LOCK. ADJUSTED GUIDE ARM.

Part: WINDOW — LEAKING (EMERGENCY EXIT) · airframe 68,737 hrs · 25,677 cycles

PRESSURE LEAK WHINE AT SEAT 20A WINDOW. ACCOMPLISHED INSPECTION OF OVERWING EMERGENCY EXIT HATCH. FOUND NO NOTABLE PROBLEMS CLEANED AREA AND SPRAYED ICE RELEASE ON SEAL AND FRAME PER MM. REINSTALL EXIT ESCAPE HATCH AND RE-ARMED DOOR SLIDE.

Part: MODULE — FAULTY (TE FLAP) · airframe 68,000 hrs · 25,406 cycles

SLAT LOCKOUT, RTFL. ACCOMPLISHED BITE TEST OF FSEU 1 HAS GROUND FAULT OF FLAP-SLAT DEPRESSURATION MODULE V10060. SUSPECT VALVE IS BAD. REPLACED FLAP SLAT DEPRESSURIZATION MODULE.

Part: SKIN — DAMAGED (BS 627 S14L) · airframe 67,437 hrs · 25,199 cycles

LOW FREQUENCY EDDY CURRENT HAS INDICATION AT REPAIR DOUBLER ABOVE STRINGER 14L, STA 627, (ABOVE FWD FASTENER IN TOP ROW). REMOVED THE SPLICE STRAP TRIPLER, ACCOMPLISHED HFEC AND LFEC PER NDT 6-51-00-19 AND NO DEFECTS NOTED. FABRICATED AND INSTALLED A NEW TRIPLER PER REO G13629, REV. D ON NON ROUTINE 27617. PER EVA 80805.

Part: SHAFT — DEFECTIVE (L2 DOOR) · airframe 67,437 hrs · 25,199 cycles

MAIN CABIN DOOR 2L EXTERNAL HANDLE DOES NOT RETRACT. INSTALLED NEW CENTER SHAFT, CLEANED INTERNAL CNTR SHAFT, CLUTCH COLLAR AND INNER SHAFT. OPS CHECKED NORMAL.

Part: GUARD — LOOSE (COCKPIT) · airframe 67,437 hrs · 25,199 cycles

EMERGENCY LIGHT SWITCH COVER ON OVERHEAD PANEL LOOSE. REPLACED GUARD ON EMERGENCY LIGHT SWITCH ON COCKPIT OVERHEAD PANEL IAW MM.

Part: FITTING — OUT OF ADJUST (GIRT BAR) · airframe 67,437 hrs · 25,199 cycles

MAIN CABIN DOOR 2R ARM AND DISARM LEVER BINDS. ADJUSTED GIRT BAR FLOOR FITTINGS. OPS CHECKED NORMAL.

Part: GIRT BAR — DAMAGED (L4 DOOR) · airframe 67,437 hrs · 25,199 cycles

L-4 ENTRY DOOR EMERGENCY ESCAPE SLIDE GIRT BAR FITTING END, LEAF SPRING HOLES ELONGATED. REMOVED AND REPLACED L-4 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR PER MM ON NON ROUTINE.

Part: SPACER — MISSING (R2 DOOR) · airframe 67,437 hrs · 25,199 cycles

MAIN CABIN, DOOR 2R DOOR EMERGENCY POWER BOTTLE LINKS ATTACH BOLT TO SPRING CYLINDER SHANKED OUT. *SUPPLEMENTAL DATA UPDATE* GAP BETWEEN LINK AND SPRING CYLINDER. INSTALLED SPACER BETWEEN LOWER LINKAGE AND SPRING CYLINDER AT MAIN CABIN R-2 DOOR EMERGENCY POWER BOTTLE RESERVOIR PER MM ON NON ROUTINE.

Part: PLATE — MISALIGNED (R1 DOOR) · airframe 67,437 hrs · 25,199 cycles

MAIN CABIN, DOOR R1 DOOR EMERGENCY POWER BOTTLE SERRATED PLATE NOT ALIGNED WITH CABLE TERMINAL SERRATIONS. ALIGNED MAIN CABIN DOOR R-1 EMERGENCY POWER BOTTLE SERRATED PLATE WITH CABLE TERMINAL SERRATIONS PER MM ON NON ROUTINE.

Part: SPACER — MISSING (R4 DOOR) · airframe 67,437 hrs · 25,199 cycles

MAIN CABIN, DOOR 4R DOOR EMERGENCY POWER BOTTLE LINKS HAVE INSUFFICIENT CLEARANCE WITH TRIGGER LEVER ATTACH RIVET, SPACERS MISSING. INSTALLED SPACERS AT UPPER AND LOWER LINKS ON MAIN CABIN, R-4 DOOR EMERGENCY POWER BOTTLE RESERVOIR PER MM ON NON ROUTINE.

Part: CHARGER — MALFUNCTIONED (MASTER BATTERY) · airframe 64,522 hrs · 24,080 cycles

EICAS STATUS MSG MAIN BATTERY CHARGER. REPLACED MAIN BATTERY CHARGER AND MAIN BATTERY IAW MM. STATUS MSG MAIN BATTERY CHARGER STILL DISPLAYED.

Part: COVER — CRACKED (GALLEY LIGHT) · airframe 62,075 hrs · 23,140 cycles

EMERGENCY EXIT FLOOR LIGHTING IN AFT EXIT-GALLEY AREA IS COMING LOOSE. AN INTERIM REPAIR HAS BEEN ACP, THE LAST TWO FEET OF THE EEL COVER HAVE HAD THE EDGES ONLY TAPED TO KEEP THE EEL STRIP DOWN. CLEAR COVER IS CRACKED AND WILL NOT STAY DOWN. LIGHT STRIP HAS NOT BEEN TAPED OVER. OTHERWISE SYSTEM CHECKS OKAY. REPLACED DAMAGED COVER.

Part: OXYGEN MASK — FAULTY (COCKPIT) · airframe 61,664 hrs · 22,982 cycles

CAPTAIN'S OXYGEN MASK DEFECTIVE. CREW COMMENTS: ELASTIC ANCHOR BAND IS STRETCHED AND LOOSE. SWAPPED CAPTS AND OBSERVERS SEAT O2 MASK AND THEN INOP OBSERVERS SEAT. REPLACED OBS MASK ASSY.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,512 hrs · 22,917 cycles

STA 640 STR 15L FUSE SKIN CRACKED UNDER REPAIR DOUBLER VERIFIED WITH HFEC. MAJOR REPAIR ACCOMPLISHED. REPAIR PER UA-EVA 72686 ON WU K6112B.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,512 hrs · 22,917 cycles

FUSELAGE SKIN DAMAGED BS 600 - BS 620, BETWEEN STR 15L & STR 17L. REPAIRED; REPAIR IS TIME LIMITED FOR 12 MONTHS FROM 06-15-09. THE AIRPLANE BECOMES UNAIRWORTHY ON 06-15-2010 UNLESS A NEW FAA 8100-9 APPROVAL IN COMPLIANCE WITH FAR 25.571 IS ISSUED PRIOR TO THAT TIME. MAJOR REPAIR: ACP REPAIR PER UA-EVA 72686 AND ON WU K6112B. REPAIR IS TIME LIMITED FOR 12 MONTHS FROM 06-15-09. CREATED CF9064 TO MONITOR THE NEW DOUBLER APPROVAL.

Part: LEAD — DISCONNECTED (CABIN) · airframe 61,512 hrs · 22,917 cycles

LEAD TO EEL STRIP BY S\ LAV. FOUND LEAD WAS NOT CONNECTED. REPLACED ON SMB W-U K1702F. OP CHECK GOOD.

Part: SKIN — DELAMINATED (THRUST REVERSER) · airframe 57,933 hrs · 21,540 cycles

NR 2 ENG OB REV UPPER BIFURCATION PANEL INNER SKIN DELAMINATED. REPLACED REVERSER HALF.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,647 hrs · 21,062 cycles

DOOR R2 FWD UPPER HINGE CUTOUT CRACKED.

Part: STRUCTURE — CRACKED (L2 DOOR) · airframe 56,647 hrs · 21,062 cycles

L2 DOOR HANDLE BOX CRACKED.

Part: DOOR — MALFUNCTIONED (PAX O2 SYSTEM) · airframe 56,647 hrs · 21,062 cycles

DURING AUTO DEPLOYMENT OF PASS O2 SYSTEM THE FOLLOWING DOORS DID NOT OPEN 14ABC, 14DEF, AND 16 DEF.

Part: STRUCTURE — DAMAGED (L2 DOOR) · airframe 56,647 hrs · 21,062 cycles

L2 DOOR UPPER HINGE CUT OUT ROUTED BEYOND LIMITS. NDT CONFIRMED CRACK.

Part: FRAME — DENTED (BS 1500 S26-27L) · airframe 56,647 hrs · 21,062 cycles

AFT PIT DENT IN FRAME AT STA 1500 BETWEEN STR 26L AND STR 27L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. ACP'D HFEC, NO CRACK FOUND. FABRICATED & INSTALLED REPAIR ANGLE.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 56,647 hrs · 21,062 cycles

CORROSION FOUND AT STA 1380 TO STA 1400 AT STR 17R,CREASE BEAM IN MAIN CABIN.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 56,647 hrs · 21,062 cycles

CORROSION FOUND AT STA 1420 TO STA 1440 AT CREASE BEAM IN MAIN CABIN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,523 hrs · 21,018 cycles

NR 1 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT OPS CHK GOOD,

Part: GIRT BAR — OUT OF POSITION (4R DOOR) · airframe 56,505 hrs · 21,011 cycles

FOUND DOOR 4R GIRT BAR ENGAGEMENT ARM LIGHT IS INOP.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 55,162 hrs · 20,524 cycles

ACRID SMOKEY SMELL IN CABIN AND RIGHT RECIRC FAN WENT INOP AS WELL. RIGHT RECIRC TURNED OFF AND SMELL DISSIPATED.

Part: GIRT BAR — MALFUNCTIONED (DOOR 4R) · airframe 54,533 hrs · 20,305 cycles

UNABLE TO DISARM SLIDE PACK WITH SAFETY PIN DOOR 4R. [SUP 05-18-07] FOUND DOOR 4R GIRT BAR AFT FOOT MISSING AND SLIDE NOT SERVICEABLE WHILE WORKING INBOUND GRIPE. REPLACED SLIDE AND GIRT BAR FOOT. GIRT BAR IS MOVING WHEN TRYING TO ARM. UNABLE TO DISARM SLIDE PACK WITH SAFETY PIN DOOR 4R. REPLACED SLIDE AS PRECAUTION DUE TO GIRT BAR MALFUNCTION. ADJUSTED GIRT BAR.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHT) · airframe 54,076 hrs · 20,151 cycles

EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY POWER SUPPLY AND CHARGER ASSEMBLY, AND BATTERY PACK.

Part: O-RING — UNSERVICEABLE (BOTTLE VALVE) · airframe 52,597 hrs · 19,589 cycles

LOW BOTTLE PRESSURE. THE FAILURE IS ATTRIBUTED TO A DAMAGED FILL VALVE O-RING. THE O-RING WAS FOUND PINCHED AND HAD A NOTCH OUT OF IT. REPLACED O-RING.

Part: SEAM — DENTED (FUSELAGE) · airframe 52,296 hrs · 19,476 cycles

DENT 42 INCHES FWD OF DOOR 4R AT LAP SEAM DENT IS 4 X 2 X .050 INCH.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 50,218 hrs · 18,722 cycles

EXTERIOR EEL LIGHT LT OVERWING AFT IS INOP. RELAMPED

Part: WARNING SYSTEM — ACTIVATED (FUEL FLOW) · airframe 49,410 hrs · 18,422 cycles

RETURNED TO FIELD DUE TO FUEL FLOW INDICATION. DURING TROUBLESHOOTING FOUND DAMAGE TP WIRE INSULATION AT CONNECTOR D5004 FUEL FILTER DIFFERENTIAL PRESSURE SWITCH APPROXIMATELY A HALF INCH FROOM THE BACKSHELL. REPAIRED WIRING PER MM 71-51-00 PAGES 820/821.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 44,449 hrs · 16,619 cycles

FOUND PUNCTURE ON FUSELAGE FWD OF THE APU, APPROX STA 1860 NEAR STRINGER 22. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED DOUBLER REPAIR.

Part: APU — FAILED (APU BAY) · airframe 44,347 hrs · 16,583 cycles

DIVERTED DUE TO APU FAILURE WITH RT GENERATOR DRIVE LIGHT INOP. FOD ON LOAD COMPRESSOR. AT ENGINE DISSASSEMBLY FOUND LOAD COMPRESSOR LABRYNTH SEAL ABRADIBLE WITH HIGH WEAR CAUSING POOR PRESSURE BALANCE RESULTING IN HOC WEAR DUE TO VIBRATION FROM FOD.

Part: CONTROL UNIT · airframe 38,971 hrs · 14,617 cycles

FUEL CONFIGURATION LIGHT ILLUMINATED. SUPPLEMENTAL DATA UPDATE THE CAUSE WAS A COMBINATION OF A LEAK IN THE RIGHT ENGINE DRY BAY AND A DEFECTIVE RIGHT MAIN TANK FUEL FILL VALVE CONTROL UNIT. THE PRIMARY CAUSE OF IMBALANCE CAN BE ATTRIBUTED TO THE FUEL FILL VALVE CONTROL UNIT WHICH WAS STUCK IN THE OPEN POSITION. AN OPEN FUEL FILL VALVE CONTROL UNIT TOGETHER WITH A FULL LOAD OF FUEL IN A CLIMB WOULD TRANSFER FUEL BACK INTO THE FUELING MANIFOLD WHERE IT WOULD DRAIN INTO THE CENTER TANK.

Part: SKIN — PUNCTURED · airframe 37,736 hrs · 14,160 cycles

EXT. FUSELAGE STATION 1760 STRINGER 19R SKIN PUNCTURED. MAJOR REPAIR ACCOMPLISHED. DOUBLER AND FLLER INSTALLED.

Part: STRINGER — DENTED · airframe 37,736 hrs · 14,160 cycles

LEFT HAND FUSELAGE AT BODY STATION 1587 AND STRINGER 20 LH HAS DENT IN SKIN. MAJOR REPAIR ACCOMPLISHED. DAMAGE WAS REMOVED AND SKIN LAP DOUBLER INSTALLED.

Part: FRAME — DENTED (FUSELAGE) · airframe 37,736 hrs · 14,160 cycles

AFT CARGO COMPT BODY STATION 1480 INNER CHORD ON CIRCUMFERENTIAL FRAME IS DENTED ABOVE STRINGER 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,736 hrs · 14,160 cycles

FWD CABIN FLOORBEAM T-CAP BODY STATION 310 RBL 40 HAS SURFACE CORROSION AND ADJACENT WEB DAMAGED DURING INTERCOSTAL REMOVAL. MAJOR REPAIR ACCOMPLISHED. STRAP AND ANGLE REPAIR INSTALLED.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 37,736 hrs · 14,160 cycles

AFT CARGO COMPARTMENT BODY STATION 1400 CIRCUMFERENTIAL FRAME INNER CHORD IS DAMAGED ABOVE STRINGER 26L. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 37,736 hrs · 14,160 cycles

LEFT EXT FUSE SKIN DOUBLER DENTED AT STATION 612 STRINGER 16L. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.

Part: SKIN — DENTED · airframe 37,736 hrs · 14,160 cycles

EXTERNAL FUSELAGE SKIN BODY STATION 640 STRINGER 18L HAS TWO EACH DENTS. MAJOR REPAIR ACCOMPLISHED. INSTALLED 16"X10" SKIN DOUBLER.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 37,736 hrs · 14,160 cycles

AFT PIT LT SIDEWALL STATION 1420 FRAME IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. DAMAGE REMOVED, INSTALLED DOUBLER.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 37,736 hrs · 14,160 cycles

CABIN FLOOR CHANNEL STATION 329 AND RBL 40 CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED CABIN FLOOR CHANNEL.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,736 hrs · 14,160 cycles

CABIN LT OUTBOARD FLOOR SUPPORT CORRODED AT STATION 758 AND LBL 60. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.

Part: FLANGE — DENTED · airframe 37,736 hrs · 14,160 cycles

AFT PIT FRAME STATION 1460 UPPER FLANGE DENTED BETWEEN STRINGER 25L AND 26L. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR SPLICE CHANNEL.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 37,736 hrs · 14,160 cycles

MID CABIN CREASE BEAM INNER CHORD BODY STATION 745 TO 756 CORRODED AT LBL 60. MAJOR REPAIR ACCOMPLISHED. REPLACED CREASE BEAM INNER CHORD.

Part: CREASE BEAM — CORRODED · airframe 37,736 hrs · 14,160 cycles

MID CABIN CREASE BEAM BODY STATION 1000 TO BODY STATION 1020 AT STRINGER 17R HAS CORROSION ON UPPER SURFACE OF WEB. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. WEB REPLACED.

Part: SKIN — CRACKED (NR2 PYLON) · airframe 37,736 hrs · 14,160 cycles

NR 2 PYLON FORWARD OUTBOARD ACCESS PANEL CUTOUT PYLON SKIN IS CRACKED AT THE 1 O'CLOCK AND 2 O'CLOCK POSITION. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLERS ON PYLON SKIN.

Part: CREASE BEAM — CORRODED · airframe 37,736 hrs · 14,160 cycles

MID CABIN CREASE BEAM BODY STATION 1020 TO BODY STATION 1040 AT STRINGER 17R HAS CORROSION ON UPPER SURFACE WEB. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.WEB REPLACED.

Part: CREASE BEAM — DAMAGED · airframe 37,736 hrs · 14,160 cycles

MID CABIN CREASE BEAM BODY STATION 960 TO BODY STATION 980 STRINGER 17L HAS TOOLING DAMAGE ON WEB. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED.WEB REPLACED.

Part: FRAME — DENTED · airframe 37,736 hrs · 14,160 cycles

AFT PIT LEFT HAND SIDE AT STATION 1440 FRAME IS DENTED BETWEEN STRINGER 25L AND 26L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 37,736 hrs · 14,160 cycles

NR 2 PYLON FORWARD OUTBOARD ACCESS PANEL CUTOUT PYLON SKIN IS CRACKED AT THE 2 O'CLOCK POSITION. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER ON PYLON SKIN CUTOUT.

Part: SKIN — CRACKED · airframe 37,736 hrs · 14,160 cycles

#2 PYLON FWD INBD SKIN PANEL CUTOUT, SKIN CRACKED AT AFT UPPER CORNER OF CUTOUT AS SEEN FROM INSIDE, CRACK APPROXIMATELY .250" LONG. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. APPLIED DOUBLER, TRIPLER,QUADRUPLER REPAIR TO SKIN.

Part: SWITCH · airframe 36,998 hrs · 13,878 cycles

DURING FLAP RETRACTION ON TAKEOFF LEADING EDGE CAUTION LIGHT AND LEADING EDGE ASSYM EICAS MSG ILLUMINATED. FLIGHT CONTROL NOT AFFECTED SUPPLEMENTAL DATA UPDATE LEADING EDGE SLAT LOSS SENSOR SWITCH FAILED.REPLACED RIGHT INBOARD LEADING EDGE LOSS SENSOR SWITCH S10338.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,767 hrs · 13,800 cycles

FUSELAGE SKIN DENTED AT FUSELAGE STA 446 BETWEEN STR 24L AND 25L. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER.

Part: OVEN — CONTAMINATED (GALLEY) · airframe 35,657 hrs · 13,416 cycles

CABIN CREW REPORT FLAMES IN FORWARD GALLEY. SUPPLEMENTAL DATA UPDATE FLAMES IN GALLEY OVEN CAUSED BY PAPER STUCK IN VENT. REPLACED OVEN. NO DAMAGE TO AIRCRAFT.

Part: CONTROLLER — SURGES (NR 1) · airframe 33,641 hrs · 12,683 cycles

NUMBER 1 ENGINE SURGED FROM 1.10 TO 1.22 ENGINE PRESSURE RATIO. *S/D* REPLACED HIGH STAGE CONTROLLER.

Part: VALVE — MALFUNCTIONED (POTABLE WATER)

DIVERTED TO MCI DUE TO VIBRATION IN AFT GALLEY AREA. *S/D* POTABLE WATER FILL/SHUTOFF VALVE WAS FOUND OPEN, CAUSING PRESSURE TO VENT AND MAKE WATER LINE VIBRATE. VALVE WAS MOVED TO CLOSED POSITION AND VIBRATION WENT AWAY.

Part: HYDRAULIC LINE — RUPTURED (LT MLG)

RETURNED TO ORD DUE TO LEFT SYSTEM HYDRAULIC FAILURE. *S/D* LINE TO THE LEFT SIDE STRUT DOWNLOCK ACTUATOR WAS LEAKING. REPLACED LINE.

Part: SEAL — FAILED (RUDDER ACTUATOR)

FLIGHT DIVERTED TO LAX AND LANDED UNDER AMBER ALERT DUE TO LOSS OF LEFT HYDRAULIC SYSTEM. *S/D* RUDDER RATIO CHANGE ACTUATOR ROD SEAL FAILED. REPLACED RRCA AND SERVICED LEFT SYSTEM.

Part: LIGHT — LOOSE (CABIN)

EMERGENCY EXIT LIGHTS DAMAGED/PULLED UP AT ROW 13. RESECURED EEL LIGHTING TRACK TO FLOOR, OPERATIONAL CHECK OK.

Part: PRSOV — MALFUNCTIONED (RT ENGINE)

DURING FLIGHT, THE RIGHT ENGINE COMPRESSOR STALLED AND RECOVERED WITHOUT EXCEEDING LIMITS. THIRTY MINUTES LATER COMPRESSOR STALL REOCCURRED, EGT STARTED TO RISE AND THROTTLE WAS PULLED TO IDLE. ENGINE STABILIZED AND POWER WAS RESTORED. ENGINE INSPECTED AND BORESCOPED AT MCO, NOTHING FOUND. SUSPECT 14TH STAGE STABILITY BLEED VALVE MALFUNCTION. REPLACED 14TH STAGE BLEED CONVERTER VALVE, REVERSE FLOW AIR VALVE, HIGH STAGE PILOT CONTROL, HIGH STAGE VALVE, PRSOV AND PRSOV REGULATOR. NO REOCCURANCES OF PROBLEM.

Part: SWITCH — FAILED (TE FLAPS)

ON FINAL, WHEN FLAPS SELECTED FROM 20-25 DEGREES, TRAILING EDGE FLAP DISAGREE LIGHT CAME ON. FLAPS STOPPED AT 20 DEGREES AND WOULD NOT MOVE. LANDED WITH FLAPS 20 DEGREES. REPLACED TRAILING EDGE ALTERNATE FLAP SWITCH ASSEMBLY AND CIRCUIT CARD. FLAPS WERE CYCLED SEVERAL TIMES. CHECKS O.K.