N522UA

Part: ATTACH BOLT — LOOSE (TE FLAP) · airframe 74,743 hrs · 27,817 cycles

FOUND FWD ATTACH BOLT LEAKING. NR 7 FLAP TRACK CLEANED & RESEALED ALL FOUR FWD ATTACH BOLTS AT NR 7 FLAP TRACK.

Part: SLIDE — LOW PRESSURE (L4 DOOR) · airframe 74,542 hrs · 27,754 cycles

SLIDE PACK GAUGE IN RED 4L. REPLACED L4 DOOR SLIDE, OK TO CONTINUE.

Part: BLADE — BENT (LT ENGINE) · airframe 74,321 hrs · 27,689 cycles

LT ENG HAS BENT BLADE. IAW MM 72-31-02 FOR ALLOWABLE LIMITS. BLENDED LE AT AREA 1 IAW AMM 72-31-02, DAMAGE REMOVAL IS WITHIN LIMITS.

Part: LIGHT — BURNED (CABIN) · airframe 74,235 hrs · 27,662 cycles

POSSIBLE ELECTRICAL SMOKE SMELL, SOURCE NOT IDENTIFIED. SMELL DISSIPATED NO OBVIOUS IRREGULARITIES NOTED. DID FIND NO SMOKING FASTEN SEAT SIGN LIGHT BULBS BURNT AT ROW 25 DEF. RELAMPED, OPERATIONS CHECKED GOOD. FOUND BURNT PAINT IN READING LIGHTS 26 DEF.

Part: FUEL LINE — LEAKING (LT WING) · airframe 74,131 hrs · 27,627 cycles

LT WING HAS EVIDENCE OF FUEL LEAKING OUT OF TWO DRY BAY DRAIN HOLES.. REPLACED MAIN ENG FUEL LINE THRU DRY BAY, LEAK CHECKED OK.

Part: LIGHT — LOOSE (CABIN) · airframe 73,964 hrs · 27,572 cycles

EMERGENCY EXIT LIGHT STRIP LOOSE 32 ROW. REPLACED 3' SECTION OF EMERGENCY EXIT LIGHT COVER & ONE PIECE OF MISSING EMERGENCY EXIT LIGHT STRIP. CHECKED EMERGENCY EXIT LIGHT OPERATION, OPERATIONS CHECKED GOOD.

Part: LAMP — INOPERATIVE (ARM LIGHT) · airframe 73,374 hrs · 27,382 cycles

LAMPS INSIDE ARM LIGHT BURNED OUT. REPLACED LAMP, OP CHECKED NORMAL. SLIDE ARMS NORMALLY.

Part: PANEL — DAMAGED (INTAKE) · airframe 73,234 hrs · 27,335 cycles

ON 2 SRV WALK AROUND FOUND THREE GOUGES ON INLET COWL ACOUSTIC PANELS AT 7, 5 AND 10 O'CLOCK POSITIONS.

Part: WIRE — BROKEN (MASTER BATTERY) · airframe 73,180 hrs · 27,318 cycles

NO MAIN BATTERY VOLTS DISPLAYED ON EICAS ELEC PAGE. BROKEN WIRE FROM D40246P TO D40904P, REF WD 24-34-11. ACCOMPLISHED WIRING INTERIM REPAIR IAW ECRA 2434-01044. BATTERY VOLTAGE DISPLAYS CORRECTLY ON EICAS.

Part: OXYGEN SYSTEM — MALFUNCTIONED (CREW) · airframe 73,077 hrs · 27,289 cycles

CREW OXYGEN AT 0 THEN 1670 PSI. VISUALLY INSPECTED CREW OXYGEN BOTTLE AND OTHER OXYGEN COMPONENTS. NO DISCREPANCIES NOTED. R & R OXYGEN TRANSDUCER. LEAK AND OPS TESTED NORMAL.

Part: CONTROLLER — INOPERATIVE (WINDOW HEAT) · airframe 72,929 hrs · 27,243 cycles

LEFT WINDOW HEAT IS INOPERATIVE. LEFT CONTROLLER WILL NOT SELF TEST, REPLACED CONTROLLER IAW AMM. TESTED GOOD. NOW SHOWING LT SIDE WINDOW NR 3 FAILURE.

Part: NUT — CRACKED (WHEEL) · airframe 72,660 hrs · 27,159 cycles

WHEEL TIE BOLT NUT CRACKED 4 COUNTERCLOCKWISE FROM VALVE STEM MARKED. REPLACED WHEEL & TIRE ASSEMBLY IAW MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 72,475 hrs · 27,099 cycles

EMERGENCY LIGHT ASSY IN FRONT OF LAVATORY INOPERATIVE. FOUND LIGHT ASSY LEADS DAMAGED. LIGHT ASSY 30 INCH LONG. REPLACED LIGHT ASSY, GROUND CHECKED NORMAL.

Part: STRAP — CRACKED (BS 1380) · airframe 72,166 hrs · 27,004 cycles

AFT CARGO COMPARTMENT AT BS 1380 WL 199 RBL 46 STABILIZER STRAP IS CRACKED & BROKEN. INSTALLED STABILIZER STRAP REPAIR IAW ECRA 5315-01063.

Part: PANEL — CRACKED (BS 1780 S17R) · airframe 72,166 hrs · 27,004 cycles

RIGHT HORIZONTAL STABILIZER FORWARD LOWER SLIDING PANEL CRACKED BS 1780, STR 17R. REPAIRED RIGHT HORIZONTAL STABILIZER FORWARD LOWER SLIDING PANEL IAW ECRA 5387-01000.

Part: STRUCTURE — CORRODED (BS1398) · corrosion level 2 · airframe 72,166 hrs · 27,004 cycles

CORROSION ON AFT CARGO BAY DOOR CUT THRESHOLD UPPER STRUCTURE BS 1398, RBL 21, WL 146. BLENDED MEASUREMENT ON AFT CARGO BAY DOOR CUT THRESHOLD UPPER STRUCTURE BS 1398 RBL 21 WL 146. MATERIAL REMOVED .023, MATERIAL REMAINING .107 AND IS OUT OF LIMITS IAW SRM 53-60-15, FIG 101, DETAIL VIII. REMOVED AND REPLACED UPPER STRUCTURE IAW SRM 51-40-02.

Part: SKIN — MISREPAIRED (BS1657 S29R-29L) · airframe 72,166 hrs · 27,004 cycles

SKIN MISREPAIRED BS 1657 BETWEEN STR 29R AND 29L. REPAIRED IAW REO-M0611 AND ECRA NR 5361-01045.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,166 hrs · 27,004 cycles

CORROSION AT RIGHT NR 4 DOOR SILL SUPPORT BS 1640 TO BS 1680. REMOVED AND REPLACED DOOR SILL SUPPORT AT RIGHT NR 4 DOOR IAW B757-200 SRM 51-40-02 PAR 7D FIG 12. CORROSION OUT OF LIMITS IAW B757-200 SRM 53-60-15 DETAIL VIII.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,166 hrs · 27,004 cycles

CORROSION ON REPAIR DOUBLER ON FLOORBEAM BS 366 RBL 26. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED REPAIR DOUBLER ON FLOORBEAM AT STA 366 RBL 26 IAW TIMCO REO M0615 AND ECRA 5315-01062 B.

Part: ATTACH BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,166 hrs · 27,004 cycles

CORROSION ON AFT CARGO COMPARTMENT DOOR CENTER AFT THRESHOLD ATTACH BRACKET BS 1420. REMOVED AND REPLACED AFT CARGO DOOR CENTER AFT THRESHOLD ATTACH BRACKET BS 1420 IAW B757-200 SRM 51-40-02 PAR 9 AND SRM 51-40-04 FIG 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,166 hrs · 27,004 cycles

CORROSION ON LONGERON BETWEEN BS 350-365 RBL 61 4 EACH. MAJOR REPAIR ACCOMPLISHED. REMOVED & REPLACED LONGERON BETWEEN BS 350 AND BS 365 RBL 61 IAW B757-200 SRM 51-40-02 PAR 4B AND 7D FIG 3 AND 12 (FLOORBOARD SUPPORT).

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,166 hrs · 27,004 cycles

CORROSION ON AFT CARGO BAY WEB AT BS 1449 RBL 22 WL 147. REMOVED AND REPLACED WEB IN AFT CARGO BAY AT BS 1449 RBL 22 WL 147 IAW B757-200 SRM 51-40-02 PAR 4 AND 7 FIG 8 AND FIG 12.

Part: PLATE — DENTED (FUSELAGE) · airframe 72,166 hrs · 27,004 cycles

RAMP REPORTS SMALL DENT ON FWD CARGO COMPMENT SCUFF PLATE MEASURES APPROX 1.25 LONG. DEPTH IS APPROX 3-16TH INCH. NO CRACKS NOTED. DENT IS ON FWD CARGO THRESHOLD, NOT SCUFF PLATE. REF MM 53-30-98 ACP INTERIM REPAIR WITH TAPE PG 804 ITEM G. DAMAGE ALSO WITHIN LIMITS OF 53-00-53 DETAIL VI PERMANENT REPAIR TO BE ACP NEXT CK. DENT ON F-CARGO COMPT THRESHOLD PLT OUT OF LIMITS IAW SRM 53-00-53 FIG 101. REPLACED T-HOLD PLATE IAW SRM 51-40-05 FIG 2.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,166 hrs · 27,004 cycles

CORROSION ON AFT CARGO BAY WEB AT BS 1449 RBL 22 WL 147. REMOVED AND REPLACED WEB IN AFT CARGO BAY AT BS 1449 RBL 22 WL 147 IAW B757-200 SRM 51-40-02 PAR 4 AND 7 FIG 8 AND FIG 12.

Part: SKIN — DEBONDED (NR 10 SLAT) · airframe 72,166 hrs · 27,004 cycles

A 1.5 INCH DIA AREA OF DISBOND ON LOWER SURFACE T/E WEDGE OF NR 10 SLAT 8 INCHES FROM T/E AND 5 INCHES FROM OUTBD EDGE. REPAIR ON NON ROUTINE 24007 DISBONDED AREA ON LOWER SURFACE T/E WEDGE OF NR 10 SLAT 8 INCHES FROM T/E AND 5 INCHES FROM O/B EDGE.

Part: SKIN — DEBONDED (NR 10 SLAT) · airframe 72,166 hrs · 27,004 cycles

TWO INCH DIA AREA OF DISBOND ON LWR SURFACE OF NR 10 SLAT T/E WEDGE 8 INCHES FROM T/E AND 20 INCHES FROM O/B EDGE. REPAIR DISBONDED AREA ON LOWER SURFACE OF NR 10 SLAT T/E WEDGE 8 INCHES FROM T/E AND 20 INCHES FROM O/B EDGE.

Part: WEDGE — DAMAGED (LE SLAT) · airframe 72,166 hrs · 27,004 cycles

MULTIPLE DRILL HOLES ON UPPER AND LWR AFT SURFACE OF NR 10 SLAT WS 738. REPAIR UPPER AND LOWER AFT SURFACE OF NR 10 SLAT T/E WEDGE AT WS 738.

Part: WEB — CRACKED (FUSELAGE) · airframe 72,166 hrs · 27,004 cycles

MAIN CABIN WEB CRACKED BELOW FLOOR LEVEL AT FWD LIGHTNING HOLE BETWEEN STA 324 AND STA 345 BL 0. MAJOR REPAIR ACCOMPLISHED. ACP REMOVED AND REPLACED MAIN CABIN WEB BS 324 TO 345 BL 0 IAW B757-200 SRM 51-40-02 PAR 7 FIG 12.

Part: SKIN — GOUGED (FUSELAGE) · airframe 72,166 hrs · 27,004 cycles

BS 1525-1530 HAS GOUGE HEAVY DENT BETWEEN STRINGER 23 AND 24 RIGHT. REPAIRED DAMAGE ON FUSELAGE SKIN BETWEEN BS 1525-1530 STR 23R AND 24R IAW B757-200 SRM 53-00-01 FIG 201 REPAIR 3. REPAIR ACCOMPLISHED IAW B757-200 SRM 53-00-01 FIG 201 REPAIR 3.

Part: ACTUATOR — LEAKING (RUDDER) · airframe 72,166 hrs · 27,004 cycles

RRCM P/N 3800022-108 S/N 0521 LEAKING. REMOVED AND REPLACED RUDDER RATIO CHANGER ACTUATOR IAW B757 27-21-13-002-001 AND 27-21-13-402-032. LEAK AND OPS CHECK GOOD IAW B757 AMM 27-21-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,166 hrs · 27,004 cycles

CORROSION IN SEVERAL PLACES BS 1661 RBL 60 TO BL 0 FLOORBEAM. REMOVED CORROSION FOUND ALL AREAS TO BE IN LIMITS IAW B757-200 SRM 53-00-51 FIG 101 DETAI L III EXCEPT DISCREPANT AREA ON UPPER CAP BS 1661 RBL 35 TO RBL 39 WHICH WAS FOUND TO BE OUT OF LIMITS IAW B757-200 SRM 53-00-51 FIG 101 892477 DETAIL III. REPAIRED DISCREPANT AREA UPPER CAP BS 166 RBL 35 TO RBL 39.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,166 hrs · 27,004 cycles

CORROSION IN BOLT HOLES, BS 1640, BL 0 TO RBL 64 WL 208. REMOVED CORROSION AT BOLT HOLES FLOORBEAM BS 1640 RBL 64 WL 208 IAW B757-200 SRM 51-10-02-0G PAR 14 FIG 1. ORG MAT THICKNESS IS .125.MAT REMAINING IS .094. MAT REMOVED IS .031 AND IS OUT OF LIMITS IAW B757-200 SRM 53-00-51 DETAIL VI. REPAIRED BS 1640 RBL 64 WL 208 IAW ECRA 5310-05536.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,166 hrs · 27,004 cycles

CORROSION ON FLOORBEAM BS 365 BL 0-RBL 63 15EA. FLOORBEAM BS 365 BL 0 - RBL 63 IAW ECRA 5310-05536 REPAIR 3 FIG 203.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,166 hrs · 27,004 cycles

CORROSION ON FLOORBOARD DIVIDER BS 367 RBL 61. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED FLOORBOARD DIVIDER BS 367 RBL 61 IAW B757-200 SRM 51-40-02 PAR 7D FIG 12.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,166 hrs · 27,004 cycles

CORROSION IN SEVERAL PLACES, BS 1640 LBL 65 BL 0 WL 208 FLOORBEAM. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION AT BS 1640 LBL 14, 31 AND 56 IAW B757-200 SRM 51-10-02. ORG MAT THICKNESS IS .125 MAX REMOVED IS .011 AND IS WITHIN LIMITS IAW B757-200 SRM 53-00-51 FIG 101. REMOVED CORROSION AT BS 1640 LBL 9 IAW B757-200 SRM 51-10-02 PAR 15 FIG 1 ORG THICKNESS IS .125 MATERIAL REMOVED IS .015 AND IS OUT OF LIMITS IAW B757-200 SRM 53-00-51 FIG 101. REPAIRED FLOORBEAM BS 1640 LBL 9 IAW EC-RA 5310-05536 TREATED AND APPLIED 2 COATS PRIMER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,166 hrs · 27,004 cycles

CORROSION IN SEVERAL PLACES, BS 1640 LBL 65 BL 0 WL 208 FLOORBEAM. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION AT BS 1640 LBL 14, 31, AND 56 IAW B757-200 SRM 51-10-02 ORG MAT THICKNESS IS .125 MAX REMOVED IS .011 AND IS WITHIN LIMITS IAW B757-200 SRM 53-00-51 FIG 101. REMOVED CORROSION AT BS 1640 LBL 9 IAW B757 -200 892477.

Part: FLOORBEAM — CORRODED (BS 1042) · corrosion level 2 · airframe 72,166 hrs · 27,004 cycles

CORROSION ON FLOORBEAM WEB UPPER SURFACE BS 1042 LBL 72. REMOVED AND REPLACED FLOORBEAM WEB IAW SRM 51-40-02 FIG 12. FABRICATED NEW FLOORBEAM WEB IAW SRM 51-30-01 FIG 7 AND DRAWING 144N5140. MAJOR REPAIR.

Part: STRUCTURE — CORRODED (BS 369) · corrosion level 2 · airframe 72,166 hrs · 27,004 cycles

CORROSION ON LONGERON BETWEEN RBL 65-72. BLENDED CORROSION ON LONGERON BS 369 IAW SRM 51-10-02 PAR 15 FIGS 1&5. REMOVED AND REPLACED LONGERON IAW SRM 51-40-02 PAR 7D. MAJOR REPAIR

Part: FLOORBEAM — CORRODED (BS 1680) · corrosion level 2 · airframe 72,166 hrs · 27,004 cycles

CORROSION ON AFT CABIN FLOORBEAM REPAIR ANGLE LOWER SURFACE BS 1680 RBL 47 WL 208. REMOVED LWR REPAIR ANGLES. LOCATED, DRILLED AND INSTALLED REPAIR ANGLE IAW SRM 53-60-51 REPAIR 3 FIG 201. MAJOR REPAIR.

Part: PRESSURE DECK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,166 hrs · 27,004 cycles

CORROSION RBL 48, BS 1681 TO BS 1710 PRESSURE DECK. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION AT RBL 48, BS 1681 TO BS 1710 PRESSURE DECK IAW B757-200 SRM 51-10-02 PAR 15, FIG 1. ORIGINAL MATERIAL THICKNESS IS.071, MATERIAL REMOVED AT DEEPEST LOCATION IS .023, MATERIAL REMAINING IS .048 AND IS OUT OF LIMITS IAW B757-200 SRM 53-60-51, PAR 4, FIG 101. REPAIRED BLENDED AREA IAW ECRA 5330-04259.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,817 hrs · 26,880 cycles

RIGHT OVERWING ESCAPE HATCH, AFT HATCH EEL'S INOP. RELAMPED BOTH HATCH EEL RIGHT OVERWING HATCH. P-N 1317.

Part: BEARING — WORN (R4 DOOR) · airframe 71,136 hrs · 26,634 cycles

DOOR 4R SLIDE LIGHT INOP. WHILE WORKING CH4018 FOR DOOR 4R SLIDE LIGHT, FOUND A WORN ROLLER BEARING. 761-0431 BEARING NIS SYSTEM. NEED SHAFT AND BELL CRANK. STILL NEED BELL CRANK. ACP 4R ARM-DISARM LEVER CHECK. FOUND ROLLER IN GIRT BAR MECHANISM WORN. PLAY OR WEAR IS CAUSING INTERMITTENT LIGHT. ROLLER IS ITEM 370 IPC REF 52-11-20-032. REPLACED ROLLER AND LINK ASSY, ITEM #370 & #395.

Part: THRU BOLT — FAILED (NR 6 WHEEL) · airframe 70,898 hrs · 26,549 cycles

NR 6 MAIN GEAR HAS FAILED THROUGH BOLT. REMOVED AND REPLACED NR 6 TIRE AND WHEEL ASSY, GROUND CHECKED OKAY.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 70,799 hrs · 26,516 cycles

SMOKE IN CABIN, RTFL. REPLACED NR 2 ENGINE. REMOVED ENGINE S/N 727109 AND INSTALLED ENGINE S/N 717996 REF MM 71-00-02.

Part: SWITCH — OUT OF ADJUST (EMERGENCY LIGHTS) · airframe 70,732 hrs · 26,492 cycles

EMERGENCY LIGHTING AT ROW 13 IS LOOSE. ADJUSTED SWITCH, CHECKED OK.

Part: RECEIVER — MALFUNCTIONED (ILS) · airframe 70,697 hrs · 26,482 cycles

NO LAND 3 LIGHT WITH ACRID ODOR IN COCKPIT AND THROUGHOUT CABIN STRONGER IN 1ST CLASS. FOUND CTR ILS RECEIVER SMOKED.

Part: LIGHT — BROKEN (CABIN) · airframe 70,592 hrs · 26,446 cycles

EMERGENCY LIGHTS INOPERATIVE FROM ROW 3 TO DOOR 2L. REPAIRED BROKEN EMERGENCY LIGHT AT DOOR 2L TO ROW 3. OPS CHECKED NORMAL.

Part: LIGHT — LOOSE (SEATS 11C & 12C) · airframe 70,592 hrs · 26,446 cycles

EMERGENCY LIGHT LOOSE SEATS 11C AND 12C. SECURED LOOSE LIGHT.

Part: GIRT BAR — LACK OF LUBE (R3 DOOR SLIDE) · airframe 69,500 hrs · 26,082 cycles

R3 DOOR WILL NOT ARM. LUBED SLIDE ARMING LINKAGE AND GIRT BAR LINKAGE.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 67,585 hrs · 25,378 cycles

CREW COMMENTS: DOOR 2L PRESSURE GAUGE OUT OF GREEN BAND. REPLACED DOOR 2L ASSIST BOTTLE ASSY.

Part: THRESHOLD — DENTED (FUSELAGE) · airframe 67,558 hrs · 25,368 cycles

DENT ON FWD CARGO THRESHOLD, MEASURES APPROX 1.25 LONG. DEPTH IS APPROX 3-16TH INCH. NO CRACKS NOTED. ACCOMPLISHED INTERIM REPAIR WITH TAPE PG 804 ITEM G. DAMAGE ALSO WITHIN LIMITS OF 53-00-53 DETAIL VI.

Part: ACTUATOR — FROZEN (RUDDER TRIM) · airframe 67,479 hrs · 25,338 cycles

RUDDER TRIM WAS FROZEN FOR SEVERAL MINUTES BEFORE IT RELEASED. REPLACED RUDDER TRIM ACTUATOR PER MM, OPS CHECK OK.

Part: RUDDER — CONTAMINATED (TAIL) · airframe 67,423 hrs · 25,319 cycles

WHILE OPERATING RUDDER OBSERVED HYD FLUID DRIPS FROM BASE OF RUDDER. OPENED VERTICAL STAB ACCESS PANEL AND CHECKED ALL THREE RUDDER ACTUATORS. FOUND SOME EVIDENCE OF SEEPAGE BUT NO ACTIVE LEAKS. CLEANED ACTUATOR COMPARTMENT AND AREA BELOW RUDDER OF SKYDROL. CLOSED AND SECURED STAB ACCESS PANEL AND NOTICED A RE-ACCUMULATION OF FLUID BENEATH RUDDER. REMOVED ACCESS PANEL FOR YAW DAMP ACTUATORS. CYCLED YAW DAMP SYSTEM - FOUND NO ACTIVE LEAKS. NEEDS MORE TROUBLESHOOTING.

Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 66,734 hrs · 25,062 cycles

DOOR 1R SLIDE LIGHT DOES NOT ILLUMINATE. SAMC TEXT: GIRT BAR UNATTACHED AND DROPPED AND DAMAGED WHEN DOOR CLOSED. REPLACED SLIDE.

Part: SLIDE — MALFUNCTIONED (R1 DOOR) · airframe 66,734 hrs · 25,062 cycles

DOOR 1R SLIDE LIGHT DOES NOT ILLUMINATE. GIRT BAR UNATTACHED AND DROPPED AND DAMAGED WHEN DOOR CLOSED. REPLACED SLIDE PER MM.

Part: HANDLE — DEFECTIVE (R1 DOOR) · airframe 66,565 hrs · 24,998 cycles

DOOR 1R WILL NOT ARM. FOUND ARMING HANDLE NOT FULLY DISARMED. MOVED HANDLE TO DISARMED POSITION. CHECKED GIRT BAR TO MAKE SURE IT IS DISARMED. OPENED DOOR, FOUND NOTHING THAT WOULD CAUSE ARMING LEVER TO HANG UP. CLOSED DOOR. OPERATED SEVERAL TIMES, NO ISSUES NOTED.

Part: FLOORBEAM — CRACKED (BS 700) · airframe 66,546 hrs · 24,992 cycles

STA 700 FLOORBEAM CRACKED AT LBL 25 AND LBL 45. MAJOR REPAIR ACCOMPLISHED: REPAIRED PER SRM AND EVA 80794 ON SMB W-U X0425H.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 66,534 hrs · 24,987 cycles

CREW REPORT: CAPTS OXYGEN MASK HAS NO OXYGEN FLOW. SWAPPED WITH OBSERVERS MASK. OBVS SEAT INOP. RPLCD OBVS. MASK AND OP CHECK ON SMB W-U X0407H.

Part: WIRE — BROKEN (COCKPIT) · airframe 66,370 hrs · 24,928 cycles

DURING NR 2 ENGINE START, LOST COCKPIT ELEC POWER. T-R MSG DISPLAYED ON LOWER EICAS. REPLACED LEFT TRU, NO HELP. LEFT ENG DID NOT TRANSFER PWR. SWAPPED LEFT AND RIGHT GCU, NO HELP. SWAPPED BACK. REPLACED LEFT GEN CNTL BREAKER C901 AND LEFT BUS TIE CNTL BREAKER C902, NO HELP. FOUND WIRE BROKEN AT LEFT GEN CONTROL SWITCH OVERHEAD PANEL. REPAIRED PER GNMM. CHECK OK, ENGINES RUN AND CHECKS OKAY.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 66,361 hrs · 24,926 cycles

CREW REPORTED 1R GIRT BAR HARD TO DISARM. FOUND ICE AROUND GIRT. REMOVED ICE AND EXERCISED ARMING LEVER. OPS NORMAL.

Part: LAMP — INOPERATIVE (CABIN) · airframe 66,261 hrs · 24,894 cycles

FLOOR PATH WAY LIGHTING AT AFT CABIN SECTION WILL NOT LIGHT. CHECKED PATH LIGHTING AND DEFERRED REF MEL 3351C. TRACED POWER PROBLEM BACK TO SIDE WALL POWER SOURCE AT ROW 33ABC. REPLACED INVERTER, NO HELP. RE-INSTALLED OLD PART. REF TO WD33-51-22 NO PWR COMING FROM CONN D6630 BAD PWR SUPPLY, PART ON AOG P1421. ACCESS FOR PWR PACK. ACCESS FOR POWER SUPPLY IS TO LOWER AFT GALLEY OVERHEAD LIGHT. REPLACED BATTERY PACK AND ALL LIGHTS ARE OK EXCEPT EEL LIGHT BY LAST ROW OF SEATS. DF IS NOW WITHIN MEL LIMITS. REPLACED LAMP AT ROW 34.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 65,846 hrs · 24,739 cycles

OVERWING EXIT LEFT SIDE SIGN COVER LOOSE. REPLACED LT OVERWING EXIT SIGN LENS COVER.

Part: WINDSHIELD — DAMAGED (COCKPIT) · airframe 64,111 hrs · 24,049 cycles

CAPTAINS WINDSHIELD HAS SEVERAL BURN SPOTS ON LOWER EDGE. CAPTAIN'S WINDSHIELD HAS SEVERAL BURN SPOTS ON LOWER EDGE. REMOVED CAPTAINS WINDSHIELD AND HAVE NEW WINDSHIELD IN PLACE WITH INITIAL TORQUE ACP'D AT 1900 HRS. NEED TO COMPLETE WINDSHIELD INSTALLATION. CAPTS WINDSHIELD TERMINAL POST J4 CAP WILL NOT STAY IN PLACE. NEW TERMINAL POST IN COCKPIT, IF NEEDED. SECURED CAP.

Part: VALVE — FAILED (CABIN PRESSURE) · airframe 63,018 hrs · 23,632 cycles

ENCOUNTERED A DECOMPRESSION AT 28,000'. FOUND HPSOV CONTROL PRESSURE PORT ELBOW & HARD LINE CONNECTION LOOSE & DAMAGED THREADS. REPLACED NR 1 ENG HPSOV CONTROL PRESSURE PORT ELBOW & LINE. WHILE PERFORMING HEALTH CHECK ON NR 1 ENG FOUND HPSOV FAILING PRESSURE TEST. REPLACED NR 1 ENG HPSOV. PRSOV FAILED CONTINUITY CHECK. REPLACED NR 2 ENG PRSOV, PRSOV OK, BUT NO HIGH STAGE AIR. REPLACED NR 2 ENG PRE-COOLER TEMP SENSOR & OVER TEMP SWITCH, NO HELP. REPLACED NR 2 ENG PRSOV-REG, OP CHECKED GOOD. REPLACED LT ENG FAMV & FATS, 2ND ENG RUN BOTH JUST BELOW BLEED SHIFT, LT PRECOOLER TEMP 332 DEG, RT 328, LT 40 PSI, R-39 PSI. BOTH ENG SHIFT NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,291 hrs · 22,984 cycles

DOOR 4 LT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP P/N 767, OPS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,824 hrs · 22,810 cycles

FOUND SMALL EEL STRIP FWD OF AFT LAV DOOR NOT WORKING. REPLACED SMALL EEL LIGHT STRIP. OPS CHECK GOOD.

Part: FIRE BOTTLE — FAULTY (NR 2 ENGINE) · airframe 60,726 hrs · 22,774 cycles

EICAS MSG "ENG BTL 2". ENG BTL DISCH LIGHT ON. DISCHARGE SWITCH NOT USED. REPLACED NR 2 ENGINE FIRE BOTTLE.

Part: LIGHT — FAULTY (COCKPIT & CABIN) · airframe 58,999 hrs · 22,084 cycles

CREW REPORT: EMERGENCY LIGHTS ON WHEN ALL SWITCHES IN COCKPIT AND CABIN ARE OFF. NOW LIGHTS ARE INOP FROM ROWS 9-15. RESET SYSTEM AND RE-TESTED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,987 hrs · 21,718 cycles

EMERGENCY EXIT IDENTIFIER LIGHTS AT 15F AND 16A INOP. LIGHT ASSY HAS A SHORT INTERNAL. REPLACED 16A EMERGENCY EXIT IDENTIFIER LIGHT ASSY & CLEANED 15F CONNECTOR. OPS CHECK OK.

Part: LIGHT — LOOSE (SEAT 21ABC) · airframe 57,552 hrs · 21,554 cycles

EMERGENCY LIGHT STRIP AT SEAT 21ABC LOOSE. SECURED LIGHT STRIP 21 ABC. OPS CHECKED GOOD.

Part: LIGHT — MISWIRED (DOOR 4R SLIDE) · airframe 56,130 hrs · 21,056 cycles

DOOR 4R, "SLIDE" SIGN ABOVE DOOR INOP. ARMING DOOR POPS C-B.

Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 56,127 hrs · 21,055 cycles

DOOR 2R FRAME IS CRACKED AT UPPER HINGE CUTOUT.

Part: STRUCTURE — DAMAGED (L2 DOOR) · airframe 56,127 hrs · 21,055 cycles

DOOR 2L NEEDS PREP DOUBLER AT UPPER HINGE CUT OUT.

Part: STRUCTURE — CRACKED (4R DOOR) · airframe 56,127 hrs · 21,055 cycles

DOOR 4R HANDLE BOX CRACKED AT CAM BASKET MOUNT HOLES. REPLACED HANDLE BOX.

Part: FRAME — DENTED (BS 1400 S21L) · airframe 56,127 hrs · 21,055 cycles

AFT PIT STA 1400 STR 21L FRAME DENTED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE, FABRICATED & INSTALLED FRAME.

Part: FLOORBEAM — CORRODED (BS 324) · airframe 56,127 hrs · 21,055 cycles

MAIN CABIN FLOORBEAM CORRODED AT STA 324 RBL 40 TO RBL 60.

Part: FRAME — DENTED (BS 580 S22-23L) · airframe 56,127 hrs · 21,055 cycles

FWD CARGO PIT FUSELAGE FRAME, DENTED AT UPPER FLANGE, BS 580 AND STR 22L-23L.

Part: GATE — CRACKED (DOOR 1R UPPER) · airframe 56,127 hrs · 21,055 cycles

R-1 DOOR UPPER GATE CRACKED. REPLACED GATE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 56,127 hrs · 25,055 cycles

MAIN CABIN FLOOR SUPPORT CORRODED STA 324 TO 377, RBL 6 0. MAJOR REPAIR ACCOMPLISHED: REPLACED FLOOR SUPPORT.

Part: SKIN — DAMAGED (BS 218 S18L) · airframe 56,127 hrs · 21,055 cycles

EXTERIOR FUSELAGE STA 218, STR 18L SKIN DENTED.

Part: LAMP — LOOSE (EMERGENCY LIGHTS) · airframe 56,076 hrs · 21,036 cycles

EMERGENCY FLOOR LIGHTING STRIP BY DOOR 2L IS LOOSE. 11-01-07 INSTALLED EEL LAMP AND COVER.

Part: UNKNOWN — ODOR (AFT CARGO BAY) · airframe 55,742 hrs · 20,905 cycles

ELECTRICAL ODOR IN DOORWAY AREA OF AFT CARGO PIT.

Part: WEDGE — DELAMINATED (L/E SLAT) · airframe 55,722 hrs · 20,898 cycles

RIGHT WING, 10 SLAT T/E WEDGE IS DELAM ALONG TRAILING EDGE FOR APPROX 20 INCHES.

Part: SKIN — DELAMINATED (THRUST REVERSER) · airframe 55,146 hrs · 20,689 cycles

NR 2 ENG REVERSER MAKING HEAVY POPPING AND CRACKLING SOUNDS. AFTER INVESTIGATION FOUND UPPER SIDEWALL (UPPER BI-FURCATION PANEL) OF REVERSER 90 PERCENT DELAMINATION ON INNER SKIN. DELAMINATION WAS CAUSED BY THE FAILURE OF BOND LINE BETWEEN OUTER SKIN AND HONECOMB SECTION. BOND LINE FAILURE IS DUE TO HIGH HEAT IN THIS AREA IN COMBINATION WITH UPPER REVERSER COMPRESSION RODS HAVING A GAP LARGER THAN 0.050 IN. THIS ALLOWS FLEXING OF PANEL BY THE PRESSURE IN C-DUCT DURING THRUST. COULD BE REQUIRING PERIODIC REVERSER FIT CHECKS, WHICH ENGINEERING IS CONSIDERING ADDING TO MAINT PROG AT HMV.

Part: GIRT BAR — DAMAGED (L1 DOOR) · airframe 53,007 hrs · 19,889 cycles

DOOR 1L SLIDE GIRT BAR HUNG UP ON DOOR FRAME AND CAME APART ON ARRIVAL. REPLACE DOOR 1L FWD GIRT BAR LIFTER ACCT FOUND BROKEN AT ARRIVAL. REMOVED AND REPLACED FWD GIRT BAR LIFTER AND TESTED NORMAL

Part: WARNING LIGHT — FALSE ACTIVATION (HYD SYSTEM) · airframe 52,252 hrs · 19,603 cycles

LEFT HYD RSVR PRESS LOW EICAS MSG CAME ON DURING TAXI WITH ASSOC OVERHEAD LIGHT. WOULD NOT GO AWAY WITH BLEED AIR ON. THIS IS ATTRIBUTED TO A FAULTY PRESSURE SWITCH IN THE HYDRAULIC RESERVOIR. REPLACED PRESSURE SWITCH.

Part: CIRCUIT CARD — MALFUNCTIONED (ENGINE) · airframe 52,132 hrs · 19,560 cycles

ABORTED TAKEOFF AT 100 KNOTS DUE TO NR 1 ENGINE EGT INDICATION. PROBLEM ATTRIBUTED TO NR 1 ENGINE SPEED CARD. REPLACED NR 1 ENGINE SPEED CARD PER 77-12-01. ALSO REPLACED NR 1 ENGINE PDIU PRECAUTIONARY.

Part: CLAMP — LOOSE (CABIN PRESSURE) · airframe 49,418 hrs · 18,593 cycles

EMERGENCY DESCENT DUE TO LOSS OF CABIN PRESSURE CONTROL. FOUND CLAMPS TO LEFT AND RIGHT CABIN AIR SUPPLY CHECK VALVES LOOSE. SECURED CLAMPS. LEAK AND OPS CHECKED OK PER MM21-31-00. RETURNED AIRCRAFT TO SERVICE.

Part: LINE — CRACKED (WATER SEPARATOR) · airframe 49,419 hrs · 18,594 cycles

FLIGHT DIVERTED DUE TO CABIN ALTITUDE WARNING AND INABILITY TO MAINTAIN CABIN PRESSURE. ORD FOUND RIGHT AIR CONDITIONING PACK WATER SEPARATOR DRAIN LINES CRACKED. REPLACED PART NUMBERS 213N1001-16 AND 213N1001-15. RETURNED AIRCRAFT TO SERVICE. NOTE: THIS SAME PROBLEM OCCURRED ON 10/16/2005 (NEXT DAY) AND DETAILS ARE ON SDR 2005UALA01150.

Part: WIRE — DAMAGED (MLG) · airframe 48,467 hrs · 18,236 cycles

RETURNED TO FIELD DUE TO AIR/GROUND SENSOR FAILURE, MANUAL GEAR RETRACTION. FOUND TRIPPED SYS 2 AIR GROUND CB AND CHAFED WIRE IN P37 PANEL (W1270-5852-22).REPLACED CIRCUIT BREAKER AND ACCOMPLISHED REPAIR OF DAMAGED WIRE.

Part: SLIDE — FAILED (CABIN)

SLIDE FAILS AIR RETENTION TEST. MULTIPLE SEAM DEGRADATION CAUSED SLIDE TO FAIL AIR RETENTION TEST.

Part: CONTROLLER — FAILED · airframe 41,491 hrs · 15,693 cycles

RT ENGINE HIGH STAGE LIGHT ON DURING TAKE OFF ROLL. SUPPLEMENTAL DATA UPDATE ROOT CAUSE: HIGH STAGE CONTROLLER OVER PRESSURE SENSOR & ANTI-ICE SWITCHER CALIBRATION WAS OUT. REPLACED CONTROLLER.

Part: STRINGER — MISDRILLED · airframe 38,007 hrs · 14,396 cycles

AFT PIT FRAME STATION 1220 ABOVE STRINGER 27L IS MISDRILLED. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 38,007 hrs · 14,396 cycles

DAMAGE TO FRAME BUILD UP AT STATION 740 BETWEEN STRINGER 13R-14R, EXCESS MATERIAL REMOVED ON CLEAN UP TO SHEAR TIE PART. MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW SHEAR TIE AND INSTALLED.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,007 hrs · 14,396 cycles

AFT PIT FRAME STATION 1320, RBL 13 -16 STRINGER 28R, UPPER CAP HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. PARTIAL FRAME CUTOUT REMOVED FROM UPPER CAP. PLUG INSTALLED.

Part: FRAME — DENTED · airframe 38,007 hrs · 14,396 cycles

AFT PIT FRAME FLANGE FROM INBOARD OF STRINGER 25L TO JUST INBOARD OF STRINGER 26L 3 EA DENTS STATION 1400. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED A FORMED FRAME REPAIR.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,007 hrs · 14,396 cycles

AFT FUSE FRAME AT STATION 1640 BETWEEN STRINGER 7L AND 8L HAS EXCESSIVE MATERIAL REMOVED FROM WEAR BLEND OUT. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AREA AND INSTALLED DOUBLE STRAP.

Part: FRAME — GOUGED · airframe 38,007 hrs · 14,396 cycles

FRAME AT STATION 365 WAS GOUGED BETWEEN STRINGERS 16R AND 17R. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED 'L' ANGLE DOUBLER.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 38,007 hrs · 14,396 cycles

CABIN FLOOR CREASE BEAM WEB ATTACH ANGLE BRACKET HAD EXCESSIVE CORROSION, STATION 981 RBL 68 STRINGER 17R. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED REPLACEMENT ATTACH BRACKET.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 38,007 hrs · 14,396 cycles

CORROSION ON THE LT CREASE BEAM INNER CHORD P/N 143N5520-27 AT BODY STATION 758 LBL 64 STRINGER 17L. MAJOR REPAIR ACCOMPLISHED. REMOVED COMPLETE SECTION OF CREASE BEAM INNER CHORD AND INSTALLED NEW SECTION.

Part: RETAINER — GOUGED (CARGO DOOR) · airframe 38,007 hrs · 14,396 cycles

FORWARD CARGO PIT DOOR LOWER AFT CORNER AND LOWER CENTER SECTION OF SEAL DEPRESSERS HAD DEEP GOUGES. MAJOR REPAIR ACCOMPLISHED. REMOVED LOWER CENTER AND AFT CORNER SEAL DEPRESSOR AND INSTALLED NEW PARTS.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 38,007 hrs · 14,396 cycles

STA 1681, PRESS DECK, RBL 47, HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.

Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 38,007 hrs · 14,396 cycles

CABIN FLOORBEAM UPPER SURFACE OF UPPER CAP HAD GOUGE AT STATION 640 STRINGER 17R AT 12 RBL TO 20 RBL. MAJOR REPAIR ACCOMPLISHED. BLENDED OUT GOUGE AND AFT. INSTALLED TWO TAPERED STRAPS BELOW FWD AND AFT.

Part: FLOORBEAM — CORRODED (FUSLEAGE) · airframe 38,007 hrs · 14,396 cycles

STATION 1681, RBL 47 RBL 48, FLOORBEAM UPPER CAP HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLERS AND FILLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,007 hrs · 14,396 cycles

CABIN FLOORBEAM UPPER T-CAP CORRODED AT STATION 324 FROM 6 LBL OUT TO RBL AT STRINGER 17L-R. MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW T-CAP BEAM.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 38,007 hrs · 14,396 cycles

CABIN FLOOR HAT CHANNEL AT STATION 334 RBL 23 TO 38 CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW HAT CHANNEL.

Part: INTERCOSTAL — CORRODED · airframe 38,007 hrs · 14,396 cycles

CABIN FLOOR STRUCTURE INTERCOSTAL AT STATION 324 TO 345 RBL 64" CORRODED ON UPPER SURFACE. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW U-SHAPED CHANNEL.

Part: FRAME — DENTED · airframe 38,007 hrs · 14,396 cycles

FRAME AT STA.1420 HAS DENTS ON INNER UPPER FLANGE BETWEEN STRINGER 23L AND 26L. MAJOR REPAIR ACCOMPLISHED.FABRICATED AND INSTALLED J-ANGLE REPAIR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,007 hrs · 14,396 cycles

FRAME CRACKED STATION 1862, RBL 5. REPAIR ACCOMPLISHED, INSTALLED ANGLE DOUBLERS.

Part: FRAME — DENTED (FUSELAGE) · airframe 38,007 hrs · 14,396 cycles

AFT PIT FRAME UPPER FLANGE HAS DENT AT STATION 1440 STRINGER 25L. MAJOR REPAIR ACCOMPLISHED, FRAME REPAIRED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,007 hrs · 14,396 cycles

STATION 1640 BBL 63 FLOORBEAM CAP CORRODED. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 38,007 hrs · 14,396 cycles

STA 1681 PRESSURE DECK EXCESSIVE MATERIAL LOSS AT LBL 3 & 12 MAJOR REPAIR ACCOMPLISHED, DOUBLER INSTALLED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,007 hrs · 14,396 cycles

CABIN FLOORBEAM AT STA 1681 LBL12 HAS CORROSION AROUND NUTPLATE HOLE. MAJOR REPAIR ACCOMPLISHED. FLOORBEAM STRAP & ANGLE DOUBLER INSTALLED. VERIFIED NO CRACKS AFTER DAMAGE REMOVED.

Part: CONTROL UNIT — FAILED (ANTI SKID SYS)

DIVERTED TO JFK DUE TO ANTISKID EICAS MESSAGE. *S/D* PERFORMED BITE TEST AND FOUND CARD 2-6 DISPLAYED. REPLACED ANTISKID AUTOBRAKE CONTROL UNIT.