N512UA

Part: COVER — OUT OF ADJUST (R2 DOOR SLIDE) · airframe 94,135 hrs · 26,850 cycles

R2 DOOR ARMED INDICATOR WON`T ARM CORRECTLY. ADJUSTED THE DOOR SLIDE COVER, OPS NORMAL.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 92,834 hrs · 26,598 cycles

LOSS OF CABIN CONTROL AT FL360. CABIN ALT AUTO 1 STATUS MESSAGE . EMERGENCY DECLARED . REPLACED CABIN AUTO CONTROLLER IAW AMM 21-31-02-404-005. SYSTEM OPS CHECKED GOOD.

Part: PANEL — OUT OF ADJUST (R2 DOOR) · airframe 92,438 hrs · 26,521 cycles

DOOR 2R SLIDE ARMED PLACARD STICKS IN INTERMITTANTLY WHEN DOOR IS ARMED. ADJUSTED DOOR 2R PANEL OPS CHECK GOOD.

Part: SUPPORT BEAM — GOUGED (NR 1 COWLING) · airframe 91,121 hrs · 26,264 cycles

NR 1 ENG I/B FAN COWL SUPPORT BEAM WEB HAS DEEP GOUGES. ACCOMPLISHED NR 1 ENGINE I/B FAN COWL SUPPORT BEAM WEB REPAIR IAW EC/RA 5410-01844 PER 75-7100- 1-2907.

Part: BATTERY — DISCHARGED (CABIN) · airframe 87,096 hrs · 25,483 cycles

EXIT SIGN ABOVE SEAT 20A INOPERATIVE. REPLACED BATTERY FOR EXIT SIGN AT SEAT 20A.

Part: ANGLE — CRACKED (L2 DOOR) · airframe 84,690 hrs · 25,016 cycles

DOOR 2L LT FWD FRAME, EXISTING REPAIR ANGLE WAS FOUND CRACKED. REPAIRED ANGLE. FABRICATED & INSTALLED IAW SRM 52-10-02 FIG 201 REPAIR 1.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,690 hrs · 25,016 cycles

AFT PIT STRINGER 28R SPLICE CORRODED AT STATION 1458. SPLICE REPLACED IAW DWG 146N3820 & SRM 51-40-02.

Part: ILS SYSTEM — INOPERATIVE (COCKPIT) · airframe 80,305 hrs · 24,176 cycles

UNABLE TO CLEAR NO LAND 3 ON ASA, LT ILS INOPERATIVE.

Part: DRAIN — CLOGGED (GALLEY) · airframe 79,472 hrs · 24,018 cycles

WATER DRAINING OUT OF THE BELLY DRAIN HOLE. CHECKED AFT GLY DRAINAGE OPERATION IAW AMM & APPEARS OPERATION IS NORMAL. DOOR DRAINS & AFT FLOOR DRAIN COME OUT OF BELLY WEEP HOLE BY THE AFT DRAIN MAST & LAVATORY SVC PANEL. GALLEY SINK COMING OUT OF DRAIN MAST. COFFEEMAKERS DO NOT APPEAR TO HAVE ANY DRAINAGE & SPILL ON COUNTER THEN TO FLOOR, NEED MORE TROUBLESHOOTING. REMOVED CM & FOUND BOTH DRAINS COMPLETELY CLOGGED. CLEANED DRAINS, GALLEY DRAIN FILTER, OPERATIONS CHECKED CM & NO LEAKS. CHECKED WATER & DRAIN LINES BEHIND SHUT OFF VLV & NO LEAKS NOTICED.

Part: ANTENNA — FAULTY (RADAR ALTIMETER) · airframe 79,043 hrs · 23,928 cycles

DURING CLIMBS, FIRST OFFICER'S RADAR ALTITUDE INTERMIT SHOWS RADAR ALTITUDE FROM 540 TO 700. OPERATIONS OK AT CRUISE. REPLACED M254 RIGHT XMTR RAD ALTM ANTENNA IAW AMM.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 78,932 hrs · 23,905 cycles

CORROSION ON WEB BS1027 LBL70 JUST AFT OVERWING EXIT DOOR CUTOUTS BS1027, BL70L. REPAIRED CREASE BEAM SHEAR WEB FROM BS1020 TO BS1040 AT STR17L LBL70 BY FABRICATION OF WEB P/N 144N5140 & DOUBLER IAW ECRA 5311-01621 REV A. REPAIR PART MARKED "REO-M0703001" IAW ECRA 5311-01621 REV A.

Part: WEB — CORRODED (BS 1022) · corrosion level 2 · airframe 78,932 hrs · 23,905 cycles

CORROSION ON WEB, BS 1022, STR 17L, RBL 70, JUST BELOW RT AFT OVERWING EXIT AT FLOOR LEVEL. R & R WEB IAW ECRA 5311-01619 AND REO-M0705, REV 1R.

Part: WEB — CORRODED (BS 1022) · corrosion level 2 · airframe 78,932 hrs · 23,905 cycles

CORROSION ON WEB BS 1022, STR 17L, RBL 70 JUST BELOW RT AFT OVERWING EXIT AT FLOOR LEVEL. R & R WEB IAW ECRA 5311-01619 AND REO-M0705, REV 1R. MAJOR REPAIR.

Part: WEB — CORRODED (BS 979 RBL 70) · corrosion level 2 · airframe 78,932 hrs · 23,905 cycles

CORROSION ON WEB BS 979 RBL 70 UNDER RT OVERWING EXIT AT FLOOR LEVEL. MAJOR REPAIR ACCOMPLISHED. REMOVED & REPLACED WEB BS 964 TO BS 984 IAW UAL ECRA 5311-01616.

Part: INTERCOSTAL — CRACKED (BS 680) · airframe 78,932 hrs · 23,905 cycles

INTERCOSTAL CRACKED AT BS 680, S12R JUST FWD OF R2 DOOR. R & R INTERCOSTAL IAW SRM 51-40-02, 3 FIG, TABLE 1. MAJOR REPAIR.

Part: INTERCOSTAL — CORRODED (BS 1442) · corrosion level 2 · airframe 78,932 hrs · 23,905 cycles

CORROSION ON INTERCOSTAL BS 1442 AND 3 INCHES BELOW S26R IN AFT CARGO BAY. REMOVED CORROSION ON INTERCOSTAL IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-04. REMOVED AND FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 51-30-01 FIG 7, 51-40-05, FIG 2, 51-20-01, 51-40-02, PARA 7, FIG14 AND DWG 146, N5215. MAJOR REPAIR.

Part: CABLE — BROKEN (ESCAPE SLIDE) · airframe 78,932 hrs · 23,905 cycles

SAFETY STRING ON SLIDE DEPLOYMENT CABLE BROKE ON AFT SIDE OF L1 DOOR SLIDE. REMOVED L1 DOOR SLIDE & REPLACED WITH NEW SLIDE IAW AMM 25-66-01.

Part: INTERCOSTAL — CORRODED (BS 1418) · corrosion level 2 · airframe 78,932 hrs · 23,905 cycles

CORROSION ON AFT CARGO COMPARTMENT INTERCOSTAL BS 1418, LBL 3. R & R INTERCOSTAL IAW SRM 51-40-02, PAR 4 AND 7 AND FIG 6 AND 12. MAJOR REPAIR.

Part: CHANNEL — CRACKED (BS 700) · airframe 78,932 hrs · 23,905 cycles

U-CHANNEL CRACKED, CABIN FLOOR LEVEL BS 700, BL LBL 24. R & R U-CHANNEL IAW SRM 51-40-01, PARA 7, FIG 12 AND DWG 143N5120.

Part: CHANNEL — CRACKED (BS 700, LBL 45) · airframe 78,932 hrs · 23,905 cycles

U-CHANNEL CRACKED CABIN FLOOR LEVEL BS 700, BL LBL 45. R & R U-CHANNEL IAW SRM 51-40-02, PARA 7, FIG 12 AND DWG 143N5130. MAJOR REPAIR.

Part: ANGLE — CORRODED (BS 690-730) · corrosion level 2 · airframe 78,932 hrs · 23,905 cycles

CORROSION ON MAIN CABIN L2 DOOR THRESHOLD INNER ANGLE SEVERAL AREAS BETWEEN BS 690 TO 730, LBL 67, WL 208. R & R L2 DOOR THRESHOLD INNER CHORD IAW SRM 51-40-02, PAR 7, FIG 12. MAJOR REPAIR.

Part: FLOOR SUPPORT — CRACKED (BS 1520-1540) · airframe 78,932 hrs · 23,905 cycles

MAIN CABIN FLOOR SUPPORT CRACKED AROUND FASTENER HOLES BS 1520 TO 1540 BL 0. LOCATED AND FABBED NEW UPPER ATTACH ANGLE AND SHIM FOR MAIN CABIN FLOOR SUPPORT IAW DWG 140N2505 AND SRM 53-00-51, REPAIR 4, FIG 201. MAJOR REPAIR.

Part: LUG — CORRODED (POTABLE WATER) · airframe 78,714 hrs · 23,864 cycles

POTABLE WATER INOP IN AFT LAVS AFTER 4 HRS OF FLT. SUSPECT WATER LINE HEATER TAPE THERMOSTAT, B10105. NEED PCN 563-0015. SHUTOFF WATER ONLY. LOCATE WATER LINE HEATERS TO AFT LAVS IN REF TO IPC 38-13-01-001,VERIFY IF POWER PRESENT AND REPLACE INOP HTR TAPES IN REF TO WDM 30-71-21 PG.71. FOUND CORROSION ON GROUND LUG. REMOVED, CLEANED & SECURED. OPS CHECK GOOD IAW AMM.

Part: LIGHT — INOPERATIVE (SEAT 19ABC) · airframe 78,522 hrs · 23,827 cycles

EMERGENCY LIGHT AT SEAT 19ABC INOPERATIVE. REPLACED EMERGENCY LIGHT ASSY, OPS CHECKED OKAY.

Part: SEAL — OBSTRUCTED (L3 DOOR) · airframe 78,502 hrs · 23,823 cycles

L3 DOOR HAS LOUD PRESSURE SQUEAL. CLEANED RESIDUAL DEBRIS FROM SEAL AND DOOR FRAME. PRESSURIZED PER AMM, NO LEAKS NOTED.

Part: PACKING — LEAKING (SPOILER PCA) · airframe 78,367 hrs · 23,797 cycles

EVIDENCE OF HYDRAULIC LEAK AT THE RIGHT WING FLAP WELL AREA. FOUND NR 10 SPOILER PCU LEAK COMING FROM SMALL PLUG. FOUND LEAKING HYD PORT CAP, REPLACED PACKING.

Part: CONTROLLER — FAILED (WINDOW HEAT) · airframe 78,163 hrs · 23,759 cycles

LEFT FWD WINDOW EICAS WOULD NOT RESET. REPLACED LEFT WINDOW CONTROLLER, OPS OKAY. SECURED LOOSE FWD WINDOW SENSOR MOUNTING SCREWS.

Part: LIGHT — BROKEN (CABIN) · airframe 77,995 hrs · 23,727 cycles

SEAT EEL LT AT SEAT 15C BROKEN OFF. REPLACED SEAT EEL LT AT 15C, CHECKS GOOD.

Part: LIGHT — UNSECURE (CABIN) · airframe 77,832 hrs · 23,697 cycles

EMERGENCY STRIP LIGHTS NEAR 16C NOT SECURE. SECURED EMERGENCY LIGHT STRIP. SEAT 16CB EMERGENCY LIGHT REQUIRES INSPECTION. INSPECTED PER IDT SEAT 16C EMERGENCY LIGHT PER GMM 09-10-05.

Part: UNKNOWN — LEAKING (WATER WASTE SYS) · airframe 77,089 hrs · 23,557 cycles

BLUE WATER LEAKING FROM WEEP HOLE UNDER AFT PIT. AFT PIT PANELS WAS OPENED BY PREVIOUS SHIFT, DID NOT FIND ANY SOLID EVIDENCE OF BLUE WATER LEAK (WITH THE DUMP VALVES OPENED, HAD LAV SERVICE PERSON CYCLE THRU 30-40 GALS THRU FILL LINE. NO LEAKAGE NOTED. LAV TANKS RESERVICED FOR DISPATCH).

Part: STRIP — MISSING (AC SYSTEM) · airframe 76,844 hrs · 23,511 cycles

EXCESSIVE CABIN AIRFLOW AND NOISE AT ROW 3. OPEN CEILING PANELS AND INSPECTED DUCT WORK, NO LEAKS, RIGHT RECIRC FAN OFF TO REDUCE AIR VOLUME. INF- :NEED INFO FROM EG ON COA' S 506931 AND 506932. WORK RECENTLY ACP IN IAH FOR DUCT REPLACEMENT. FOUND NO CRACKS OR LOOSE HOSES. REF 5551 SAME PROBLEM AFTER COA ACP, INSTALLED MISSING PHENOLIC STRIP BETWEEN DIFFUSER AND DUCT AT ROW 3 REF IPC 21-22-03 SEALED AND LEAK CHECKED OK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,778 hrs · 23,498 cycles

CORROSION AT CABIN FLOOR BEAM STATION 324 LP 9986885. DURING CHORD REPLACEMENT NUMEROUS ELONGATED DAMAGED HOLES WERE FOUND COMMON TO THE UPPER CHORD & VERTICAL FLOOR BEAM WEB. TRIMMED OUT DAMAGED AREA, FABRICATED & INSTALLED ALL REPAIR PARTS IAW ECRA 5310-05604 ON LP 9986885.

Part: GATE — CORRODED (R1 DOOR) · airframe 76,778 hrs · 23,498 cycles

R-1 PASSENGER DOOR HAS DEEP CORROSION ON THE LOWER GATE. REMOVED AND REPLACED DOOR LOWER GATE.

Part: GATE — CRACKED (R1 DOOR) · airframe 76,778 hrs · 23,498 cycles

R-1 PASSENGER DOOR HAS A LARGE CRACK ON THE UPPER GATE. REMOVED AND REPLACED DOOR UPPER GATE PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 76,778 hrs · 23,498 cycles

CORROSION AT CABIN FLOORBEAM STA 324 LP 9986885. DURING CHORD REPLACEMENT NUMEROUS ELONGATED-DAMAGED HOLES WERE FOUND COMMON TO THE UPPER CHORD AND VERTICAL FLOORBEAM WEB. TRIMMED OUT DAMAGED AREA, FABRICATED AND INSTALLED ALL REPAIR PARTS PER ECRA 5310-05604 ON LP 9986885. ACCMP'D RII FOR FLOOR BEAM REPAIR REF:ECRA5310-05604.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,778 hrs · 23,498 cycles

CABIN FLOORBEAM STA 1640 HAS CORROSION AT LBL 33 TO RBL 52. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA OF FLOORBEAM, FABRICATED AND INSTALLED REPAIR PARTS PER ECRA 5310-05605.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 76,778 hrs · 23,498 cycles

CORROSION AT CABIN FLOORBEAM STA 365. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF FLOORBEAM, FABRICATED AND INSTALLED REPAIR PARTS PER ECRA 5310-05536. ACCOMPLISHED RII ON FLOORBEAM REPAIR.

Part: PAN — GOUGED (L1 DOOR) · airframe 76,778 hrs · 23,498 cycles

DOOR L-1 HAS GOUGED PAN FROM RUBBING DOOR HANDLE. REMOVED AND REPLACED DOOR PAN PER ECRA 5200-01155.

Part: CREASE BEAM — GOUGED (FUSELAGE) · airframe 76,778 hrs · 23,498 cycles

DEEP GOUGES AT RIGHTT INBOARD CREASE BEAM, STA 1630. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR PARTS PER ECRA 5300-01416

Part: SKIN — DENTED (FUSELAGE) · airframe 76,778 hrs · 23,498 cycles

SHARP SKIN DENT AT STA 549 AND STR 28L MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT SKIN, FABRICATED AND INSTALLED REPAIR PARTS PER ECRA 5330-04347.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 76,778 hrs · 23,498 cycles

CABIN FLOORBEAM STA 1640 HAS DEEP CORROSION. REMOVED DAMAGED SECTION, INSTALLED REPAIR PARTS PER ECRA 5300-01416.

Part: GATE — CORRODED (L2 DOOR) · corrosion level 2 · airframe 76,778 hrs · 23,498 cycles

L2 DOOR LOWER GATE IS CORRODED. REMOVED AND INSTALLED L2 LOWER GATE. ADJUSTMENT TO BE COMPLIED WITH ON NR 9987521.

Part: HOSE — OBSTRUCTED (GALLEY DRAIN) · airframe 73,699 hrs · 22,905 cycles

GALLEY DRAIN PLUGGED AT DOOR-1R FWD-CABIN FWD GALLEY. CLOG IN SAME AREA HOSE UPSTREAM OF PREVIOUS REPAIR ALSO DAMAGED. NO LEAKS NOTED IN EITHER LOCATIONS. CLEARED LINES AND REPLACED DAMAGED HOSES.

Part: POWER SUPPLY — INTERMITTENT (CABIN) · airframe 73,278 hrs · 22,824 cycles

THE 24C STOWBIN MOUNTED EMERGENCY LIGHT IS INTERMITTENT HAD TO BE TAPPED TO COME ON. REPLACED PWR SUPPLY, OPS CHECKS GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 73,278 hrs · 22,824 cycles

THE 23C AISLE EMERGENCY LIGHT IS INOPERATIVE. SECURED CONNECTOR. CHECKED GOOD.

Part: STRUCTURE — CRACKED (GALLEY) · airframe 73,278 hrs · 22,824 cycles

CABIN, GLY G1B, COUNTER TOP MOD BOX CUTOUTS FOR 109 &110, VERTICLE 'I-BEAM' DIVIDER CRACKED AT BOTH UPPER & LWR RADII. (FOUND DURING REMOVAL OF JAMMED MOD BOX). REMOVED UPPER & LOWER 'T' ANGLES FROM VERTICLE SHEAR WEB. CUT 2 PIECES OF 7075-T6, .050 HAVING 1.5" FLANGES. INSTALLED RIVETS & PAINTED. PICKED UP CSK HOLES INSTALLED REPLACEMENT "I" BEAM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,278 hrs · 22,824 cycles

EMERGENCY LIGHTS AT SEATS 2A AND 3A ARE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECKED NORMAL.

Part: CAP — BROKEN (SEAT) · airframe 73,076 hrs · 22,785 cycles

ARM CAPS BROKEN AT SEATS 16C, 17C, 18C. REPLACED ARM CAPS.

Part: UNKNOWN — ODOR (CABIN) · airframe 72,845 hrs · 22,740 cycles

STRONG SMOKE SMELL IN FORWARD GALLEY. ODOR CLEARED WITH VENTILATION BUT COULD NOT REPRODUCE CONDITION. LOWERED GALLEY OVERHEAD PANELS, CHECKED ALL LIGHT BALLASTS, COFFEEMAKERS, & CHILLER UNITS FOR HEAT OR DISCREPANT CONDITIONS, NONE FOUND. OVENS COLD, NOT A FACTOR. DID FIND TWO EA COFFEE WARMERS TURNED ON WITH EMPTY POTS IN PLACE, BUT ODOR NOT REGENERATED. NO FAULTS FOUND.

Part: WIRE HARNESS — FAULTY (WINDSHIELD) · airframe 71,121 hrs · 22,400 cycles

THE INSULATION ON WIRE BUNDLE LEADING TO F/O WINDOW IS DETERIORATED. OUTER PROTECTIVE INSULATION SPIRAL CABLE DETERIORATED FOR THE FO NR 2 WINDOW HEAT. WIRE INSULATION & CLEAR INSULATION STILL GOOD. CABLE NEEDS TO BE REPLACED. C-B PULLED & COLLARED PER MEL. -INF- :REF IPC 56-11-02-002 ITEM 940 CABLE PCN 561-2049 -INF- :REF IPC 56-11-02-001 ITEM 880 PCN IS CORRECT. JUST EFFECTIVITY WAS DIFFERENT. REPLACED WINDOW 2R, B39 ELECTRICAL CABLE ASSY AND CONN D41576P PER WD. WINDOW HEAT OPERATIONAL CHECK GOOD.

Part: LAMP — INTERMITTENT (EMERGENCY LIGHT) · airframe 70,962 hrs · 22,370 cycles

DOOR NR 4 SLIDE LEFT EXTERIOR EMERGENCY LIGHT INTERMITTENT. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,484 hrs · 22,280 cycles

SEAT 23ABC EEL INOP. REPLACED EEL STRIP, OPS CHECK OKAY.

Part: FLOORBEAM — CORRODED (BS 1680) · airframe 69,847 hrs · 22,159 cycles

AFT PIT STA 1680 BETWEEN RBL 39 AND RBL 42 BELOW GALLEY FLOORBEAM HAS CORROSION. ACP REPAIR IAW MM(S) ON W/O 235N6N00221.

Part: CABLE — FAILED (R4 DOOR) · airframe 69,847 hrs · 22,159 cycles

R4 DOOR FAILED EXTERNAL DISARM CHECK. REPLACED ARM DISARM CABLE, OP CHECK OK ON WO 2356N00319.

Part: SHUTOFF VALVE — FAILED (APU FUEL) · airframe 68,996 hrs · 21,997 cycles

FUEL LEAKING FROM CTR TANK REAR SPAR AT APU SHUTOFF ACTUATOR. REMOVED COUPLINGS TO APU FUEL SHUTOFF INSIDE FUEL TANK. REMOVED ACTUATOR ON THE OUTSIDE AND SHUTOFF VALVE AND SEAL FROM INSIDE TANK. REPLACED APU SHUTOFF VALVE AND REINSTALLED APU SHUTOFF VALVE ACTUATOR. OPS CK GOOD.

Part: GROUND WIRE — DAMAGED (GALLEY) · airframe 66,695 hrs · 21,553 cycles

FOUND G2B GALLEY COUNTER NOT GROUNDED. HOT PLATE INOP UNTIL GROUNDS FIXED. SUPPLEMENTAL DATA UPDATE PULLED AND COLLARED HOT PLATE CB. ALSO PULLED AND COLLARED G2B GALLEY CB ON P70 PANEL. NEEDS GD9095 & GD9074 CONNECTED TO GROUND. FOUND OPEN ON GROUND TO AIRFRAME. WILL NEED TO REMOVE GALLEY FOR ACCESS. REPAIRED GROUND YSEGD9092, CK GOOD.

Part: SEAL — DAMAGED (COCKPIT WINDOW) · airframe 66,505 hrs · 21,517 cycles

HIGH PITCH SQUEAL FROM F/O SLIDING WINDOW, RTFL. SUSPECTED AREA OF SQUEAL IS FWD UPPER CORNER OF WINDOW. PUSHING ON WINDOW FRAME NO HELP IN ATTEMPT TO QUIET OR ALTER SQUEAL PITCH. REPLACED F-O'S SLIDING WINDOW PRESSURE SEAL. PRESSURIZED ACFT TO 4.5 DPSI, NO LEAKS NOTED, NO NOISE NOTED.

Part: LENS — OUT OF POSITION (CABIN) · airframe 66,100 hrs · 21,434 cycles

CREW COMMENTS: EMERGENCY EXIT LIGHT LENS FROM DOOR 1L-R AREA IS OUT OF POSITION. SECURED LIGHT LENS. CHECKS OKAY.

Part: PROXIMITY SENSOR — FAULTY (LANDING GEAR) · airframe 64,005 hrs · 21,034 cycles

GEAR DISAGREE MESSAGE, RTFL. REPLACED S10069 AND S10239 PROX SENSORS AND WD 32-61-11. PSEU BITE AND TARGET TESTS OK.

Part: LIGHT — MISSING (CABIN) · airframe 63,180 hrs · 20,876 cycles

EEL LIGHTS AT SEATS 7B AND 9B ARE MISSING. REPLACED EEL LIGHTS. OPS CHECKED OKAY.

Part: LIGHT — MISSING (CABIN) · airframe 63,180 hrs · 20,876 cycles

EMERGENCY LIGHTS AT SEATS 7B AND 9B ARE MISSING. REPLACED EMERGENCY LIGHTS. OPS CHECKED OKAY.

Part: LIGHT — MISSING (CABIN) · airframe 63,180 hrs · 20,876 cycles

EEL LIGHTS AT SEATS 7B AND 9B ARE MISSING. REPLACED EEL LIGHTS. OPS CHECKED OKAY.

Part: MECHANISM — OUT OF ADJUST (L2 DOOR) · airframe 62,977 hrs · 20,838 cycles

DOOR 2L FAILS MIDWAY CHECK, DISARM LEVER GOES TO ARM POSITION WHEN DOOR IS UNLATCHED. RE-ADJUSTED MODE SELECT LOCKOUT MECHANISM AND OPS CHECK GOOD.

Part: MECHANISM — OUT OF ADJUST (L2 DOOR) · airframe 62,977 hrs · 20,838 cycles

DOOR 2L FAILS MIDWAY CHECK, DISARM LEVER GOES TO ARM POSITION WHEN DOOR IS UNLATCHED. SUPPLEMENTAL DATA UPDATE READJUSTED MODE SELECT LOCKOUT MECHANISM AND OPS CHECK GOOD.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 62,977 hrs · 20,838 cycles

FLOORBEAM UPPER CHORD CRACKED. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM UPPER CHORD WITH REPAIR ANGLE AND SPLICE STRAPS.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 62,977 hrs · 20,838 cycles

SEAT ROW 20ABC EMERGENCY LIGHTS INOP IN SEAT. RESECURED CONNECTOR AT SEAT ROW 20 ABC AS REQUIRED. OPS CHECKED GOOD.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 62,977 hrs · 20,838 cycles

SEVERAL EMERGENCY LIGHTS ON SIDE OF ECONOMY SEATS INOP. RESECURED CONNECTOR AT SEAT ROW 20ABC AND PERFORMED OPS CHECK OF ECONOMY CLASS EMERGENCY LIGHTING, AND OPS CHECK GOOD.

Part: WIRE — FAULTY (CABIN) · airframe 62,977 hrs · 20,838 cycles

EMERGENCY LIGHTS TEST SWITCH ABOVE L-4 DOOR WILL NOT TEST. RE-TERMINATED WIRING. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,977 hrs · 20,838 cycles

SEAT ROW 17ABC EMERGENCY LIGHT IS INOP IN SEAT. REMOVED AND REPLACED SEAT ROW 17ABC EMERGENCY LIGHT STRIP, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,977 hrs · 20,838 cycles

SEAT ROW 23 ABC EMERGENCY LIGHT INOP IN SEAT. REMOVED AND REPLACED BROKEN LIGHT BAR FOR SEAT 23ABC AND OPS CHECK GOOD.

Part: JAM-NUT — LOOSE (GIRT BAR) · airframe 62,977 hrs · 20,838 cycles

L-1 DOOR LOWER GATE FWD GIRT BAR MECHANISM, FASTENER CHECK NUT LOOSE. RESECURED JAM NUT.

Part: PANEL — DAMAGED (LE SLAT) · airframe 62,133 hrs · 20,680 cycles

NR 1 AND NR 2 LEADING EDGE SLAT AND UNDER WING PANEL 521MB DAMAGE BY AIRSTAIR.

Part: SLAT — DAMAGED (WING) · airframe 62,133 hrs · 20,680 cycles

NR 1 AND NR 2 LEADING EDGE SLAT DAMAGE.

Part: SLAT — DAMAGED (NR 1 AND 2) · airframe 62,133 hrs · 20,680 cycles

NR 1 AND NR 2 LEADING EDGE SLAT AND UNDER WING PANEL 521MB DAMAGED BY AIR STAIR. SLATS REPLACED.

Part: BEARING — DAMAGED (R4 DOOR) · airframe 62,067 hrs · 20,667 cycles

DOOR 3R HARD TO ARM-DISARM. DOOR 4R UPPER ARMING MECHANISM CROSSTUBE BEARINGS COMING APART, SEIZED AND CORRODED. REPLACED ARMING LEVER CROSS TUBE FORWARD BEARING. DOOR OPS NORMALLY.

Part: BALLAST — OVERHEATED (CABIN) · airframe 61,931 hrs · 20,641 cycles

STRONG ELECTRICAL SMELL IN FIRST CLASS AND FWD GALLEY. REPLACED BALLAST. CHECKS OKAY.

Part: ARM — OBSTRUCTED (R3 DOOR) · airframe 61,121 hrs · 20,483 cycles

UNABLE TO ARM DOOR 3R. *S/D* DEBRIS UNDER DOOR LEDGE. REMOVED DEBRIS FROM UNDER DOOR LEDGE. DOOR ARMS/DISARMS NORMALLY.

Part: BEARING — FAILED (NR 1 ENGINE) · airframe 60,741 hrs · 20,411 cycles

STINK ODOR IN FLIGHT DECK AT TAKEOFF AND LANDING. NR 1 ENG BEARING FAILURE CAUSING OIL LEAK/COKING ODOR COMING IN THROUGH ENG BLEED AIR. REPLACED NR 1 ENG.

Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 60,610 hrs · 20,386 cycles

DOOR 1R HARD TO DISARM. DEBRIS UNDER GIRT BAR. REMOVED BOTTLE CAP FROM UNDER GIRT BAR. DOOR ARMING SYS OPS CHECKS OK.

Part: LANYARD — LOOSE (EVAC SLIDE) · airframe 60,447 hrs · 20,355 cycles

CREW REPORTED LANYARD LOOSE AT DOOR 1R. SECURED LANYARD.

Part: BUTTON — MISSING (COCKPIT) · airframe 59,714 hrs · 20,218 cycles

OVERHEAD PANEL EVAC HORN SHUTOFF BUTTON MISSING. REPLACED EMER EVAC PANEL.

Part: BRACKET — DIRTY (GIRT BAR) · airframe 58,534 hrs · 19,993 cycles

CANNOT ARM DOOR 1R. FOUND BRACKET DIRTY. CLEANED AREA AROUND GIRT BAR BRACKETS, DOOR OPS CHECKED NORMALLY.

Part: UNKNOWN — UNKNOWN (STAB TRIM) · airframe 56,792 hrs · 19,660 cycles

STAB TRIM WILL NOT TRIM IN NOSE DOWN DIRECTION WITH CENTER STAB TRIM CUTOUT SWITCH IN NORMAL AND RIGHT STAB TRIM SWITCH IN CUTOUT POSITION. TRIMS NORMALLY WITH TRIM LEVERS. [08-08-07] STABILIZER NOSE DOWN OPERATION STARTED WORKING OKAY AFTER CYCLING STABILIZER WITH ALTERNATE LEVERS. IN THE ALTERNATE ELECTRIC STAB TRIM MODE, THE UP LIMIT IS RESTRICTED TO APPROX.+3.85 DEGREES. PASSED MCDP TEST 65. REPLACED STAB TRAVEL LIMIT AND POSITION TRANSMITTER MODULE.

Part: IDG — MALFUNCTIONED (NR 1) · airframe 56,756 hrs · 19,653 cycles

EICAS MESSAGE LEFT GENERATOR DRIVE DISPLAYED. [08-08-07] ON CLIMB OUT CREW GOT LEFT GENERATOR DRIVE INDICATION. CREW DISCONNECTED LEFT GENERATOR DRIVE AND STARTED APU. RAN FUEL BURN FOR APU ENROUTE. REPLACED NR 1 IDG AND ENG FUEL-OIL EXCHANGER.

Part: OXYGEN SYSTEM — LOW (CREW) · airframe 56,633 hrs · 19,627 cycles

CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. [08-08-07] FOUND 02 SYSTEM AT 1150 PSI, SERVICED 02 TO 1800 PSI. RECORD PRESSURE PRIOR TO SERVICING.

Part: FRAME — DENTED (BS 1560 S26R) · airframe 56,545 hrs · 19,608 cycles

MAIN FRAME, STA 1560 AT STR 26R, FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED -J- ANGLE REPAIR.

Part: FRAME — DENTED (BS 1340 S25L) · airframe 56,545 hrs · 19,608 cycles

MAIN FRAME, STA 1340 LEFT SIDE BETWEEN STR 25L, FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED -J- ANGLE REPAIR AND NEW SPLICE REPAIR.

Part: FRAME — DENTED (BS 1520 S26L) · airframe 56,545 hrs · 19,608 cycles

MAIN FRAME, STA 1520 AT STR 26L FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED -J- ANGLE REPAIR.

Part: FRAME — DENTED (BS 1540 S25-26L) · airframe 56,545 hrs · 19,608 cycles

MAIN FRAME, STA 1540 BETWEEN STR 25L-26L, FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR SPLICE AND NEW SPLICE REPAIR.

Part: FRAME — DENTED (BS 1400 S25-27L) · airframe 56,545 hrs · 19,608 cycles

MAIN FRAME, STA 1400 BETWEEN STR 25L-27L, FRAME HAS 2 EACH DENTS. MAJOR REPAIR ACCOMPLISHED: INSTALLED -J- ANGLE AND NEW PRODUCTION SPLICE REPAIR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,545 hrs · 19,608 cycles

DOOR R2 AT UPPER HINGE CUTOUT IS UNDERSERVICED. MAJOR REPAIR ACCOMPLISHED: ACCOMPLISHED INSURANCE CUT AND INSTALLED DOUBLER REPAIR.

Part: FRAME — DENTED (BS 1460 S25-26L) · airframe 56,545 hrs · 19,608 cycles

MAIN FRAME, STA 1460 BETWEEN STR 25L-26L, FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED -J- ANGLE REPAIR.

Part: FRAME — DENTED (BS 1340, S26R) · airframe 56,545 hrs · 19,608 cycles

MAIN FRAME, STA 1340, STR 26R, FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED -J- ANGLE REPAIR.

Part: FRAME — DENTED (BS 1480 S25-26L) · airframe 56,545 hrs · 19,608 cycles

MAIN FRAME, STA 1480 BETWEEN STR 25L-26L, FRAME HAS 2 EACH DENTS. MAJOR REPAIR ACCOMPLISHED: INSTALLED -J- ANGLE REPAIR.

Part: FRAME — DENTED (BS 1540 S26R) · airframe 56,545 hrs · 19,608 cycles

MAIN FRAME, STA 1540 AT STR 26R, FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED ANGLE REPAIR.

Part: FRAME — DENTED (BS 1440 S25-26L) · airframe 56,545 hrs · 19,608 cycles

MAIN FRAME, STA 1440 BETWEEN STR 25L-26L, FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED -J- ANGLE REPAIR.

Part: FRAME — DENTED (BS 1500 S25-26L) · airframe 56,545 hrs · 19,608 cycles

MAIN FRAME, STA 1500 BETWEEN STR 25L-26L, FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED ANGLE REPAIR AND NEW SPLICE REPAIR.

Part: FRAME — DENTED (BS 1580 S23R) · airframe 56,545 hrs · 19,608 cycles

MAIN FRAME, STA 1580 AT STR 23R, FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED -J- ANGLE REPAIR.

Part: FRAME — DENTED (BS 1420 S25-26L) · airframe 56,545 hrs · 19,608 cycles

MAIN FRAME, STA 1420 BETWEEN STR 25L-26L, FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,545 hrs · 19,608 cycles

EXIT LOCATOR SIGN ABOVE SEAT ROW 7AB INOP. *S/D* TROUBLESHOT SYSTEM AND FOUND BATTERY PACK WITH LOW VOLTAGE. REPLACED BATTERY PACK.

Part: PUSHROD — OUT OF ADJUST (DOOR 2L) · airframe 56,545 hrs · 19,608 cycles

DOOR 2L DOES NOT FULLY DISARM WHEN HANDLE IS HALFWAY ENGAGED. [08-07-07] CHECKED PAX DOOR 2L EMERGENCY MECHANISM RIG PIN PD5, AND FOUND ITS SETTING OUT OF LIMITS. ADJUSTED PUSH ROD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,545 hrs · 19,608 cycles

EXTERIOR EMERGENCY LIGHT AT DOOR 2R INOP. *S/D* RELAMPED, OPS CHECKS NORMAL.

Part: LEVER — OUT OF ADJUST (R1 DOOR) · airframe 56,545 hrs · 19,608 cycles

R-1 MED MODE SELECTOR NEEDS ADJUSTMENT.

Part: PANEL — WARPED (NR 8 SPOILER) · airframe 56,545 hrs · 19,608 cycles

RT WING, NR 8 SPOILER PANEL HAS EXCESSIVE WARP ON TRAILING EDGE. [08-07-07] REPLACED TRAILING EDGE SPOILER PANEL. ADJUSTED NR 8 SPOILER GAP AND ADJUSTMENT CHECKED NR 8 PCA RVDT. CHECKED BONDING JUMPER RESISTANCE.

Part: STRUCTURE — UNDERSERVICED (L2 DOOR) · airframe 56,545 hrs · 19,608 cycles

DOOR L2 UPPER HINGE CUTOUT IS UNDERSERVICED. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED DOUBLER REPAIR.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,545 hrs · 19,608 cycles

AFT PIT LOWER SKIN ANTENNA CUTOUT CORRODED AT STA 1430 LBL 2. MAJOR REPAIR ACCOMPLISHED: REMOVED ANTENNA DOUBLER TO FACILITATE CORROSION REMOVAL. FABRICATED & INSTALLED A NEW -31 DOUBLER.

Part: HARNESS — TORN (ESCAPE SLIDE) · airframe 56,545 hrs · 19,608 cycles

DOOR L2 ESCAPE SLIDE HARNESS AT LATCH YOKE IS TORN, PEELING. [08-07-07] INSTALLED NEW HARNESS.

Part: FEEDER CABLE — DAMAGED (CABIN) · airframe 56,545 hrs · 19,608 cycles

AFT C-ZONE & FWD A-ZONE EEL FEEDERS ARE DAMAGED. REPAIRED EEL FEEDER.

Part: RIVET — DAMAGED (FUSELAGE) · airframe 56,545 hrs · 18,069 cycles

TWO RIVETS DAMAGED BY LIGHTNING STRIKE STA 630 WL 160 ON LEFT SIDE OF FUSELAGE. REMOVED 2 EA BLIND FASTENERS, STEPPED UP HOLES AS REQUIRED. HFEC REVEALED NO CRACKS. INSTALLED 2EA SOLIDS.

Part: RIVET — DAMAGED (FUSELAGE) · airframe 56,545 hrs · 18,069 cycles

RIVET DAMAGED BY LIGHTNING STRIKE STA 720 WL 160 ON LEFT SIDE OF FUSELAGE. REMOVED 1EA BLIND FASTENER, STEPPED UP HOLES AS REQUIRED, HFEC REVEALED NO CRACKS. INSTALLED SOLID FASTENER.

Part: RIVET — DAMAGED (FUSELAGE) · airframe 48,533 hrs · 18,069 cycles

RIVET DAMAGED BY LIGHTNING STRIKE STA 590 WL 160 ON LEFT SIDE OF FUSELAGE. REMOVED BLIND RIVET. HFEC REVEALED NO CRACKS. INSTALLED SOLID.

Part: RIVET — DAMAGED (FUSELAGE) · airframe 48,533 hrs · 18,069 cycles

RIVET DAMAGED BY LIGHTNING STRIKE STA 610 WL 160 ON LEFT SIDE OF FUSELAGE. REMOVED BLIND FASTENER, STEPPED UP HOLE AS REQUIRED. NO CRACKS FOUND, INSTALLED SOLID FASTENER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,484 hrs · 19,406 cycles

DOOR 4R EMERGENCY LIGHT INOPERATIVE. RELAMPED R-4 DOOR EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,484 hrs · 19,406 cycles

SEATS 5, 6 AND 7 LEFT EMERGENCY LIGHTS INOPERATIVE. RESEATED SEAT 5L CONNECTOR AND OPS CHECK GOOD.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 55,484 hrs · 19,406 cycles

NR 2 NACELLE STRUT SIDE SKIN OUTBOARD FORWARD ACCESS DOOR CUT-OUT HAS A CRACK INDICATION, INSIDE OF CUT-OUT, CRACK ENDS MARKED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED & INSTALLED 3 EACH DOUBLERS.

Part: SKIN — CORRODED (FUSELAGE) · airframe 55,484 hrs · 19,406 cycles

SIGNS OF CORROSION (WHITE POWDER) AT DME (RIGHT) ANTENNA MOUNTING AT BS 668.5 BETWEEN STR 28L TO 29L. REMOVED ANTENNA FOR EVALUATION OF LEVEL 1 SKIN CORROSION. REPLACED ANTENNA MOUNT AND ANTENNA.

Part: GIRT BAR — OUT OF ADJUST (L4 DOOR) · airframe 55,484 hrs · 19,406 cycles

MAIN CABIN L-4 DOOR GIRT BAR IS OUT OF ADJUSTMENT. ADJUSTED L-4 GIRT BAR FOR PROPER ENGAGEMENT OF GIRT BAR SLIDERS. DOOR L-4 ARM-DISARM OPERATIONAL TEST WAS ACCOMPLISHED FOR ASSURING PROPER FUNCTIONALITY. NO COMPONENTS REPLACED.

Part: HYDRAULIC SYSTEM — UNKNOWN (LEFT) · airframe 54,686 hrs · 19,253 cycles

LOSS OF THE LEFT HYDRAULIC SYSTEM. FOUND FLAP SLAT DEPRESSURIZATION MODULE IN LEFT WHEEL WELL WITH ONE UNION BROKEN. REPLACED FLAP-SLAT DEPRESSURIZATION VALVE. ALSO REPLACED L EDP CASE DRAIN FILTERS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,475 hrs · 18,828 cycles

EEL LIGHTS ON SEATS 8, 19, AND 25 ABC OUT.

Part: SKIN — WORN (LT WING FOREFLAP) · airframe 50,100 hrs · 18,374 cycles

LT WING INBD FOREFLAP HAS WORN AREA AT UPPER OTBD END. SUPPLEMENTAL DATA UPDATE REMOVED EXISTING DOUBLER, NDT FOR DELAM, INSTALLED BOND REPAIR PER REO-G10990-B AND APPROVED PER 8100-9 DATED 9-23-05.

Part: LIGHT — CUT (GALLEY G2B) · airframe 50,100 hrs · 18,374 cycles

EEL INOP AT GALLEY G2A AND G2B. SUPPLEMENTAL DATA UPDATE, G2B EEL FOUND CUT, REPLACED EEL LIGHT.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 47,443 hrs · 17,857 cycles

DIVERTED DUE TO A CRACK IN THE CAPT SIDE WINDSHIELD, LEFT TO RIGHT EDGE WITH WINDOW HEAT ARCING. WINDOW HEAT FAILURE. REPLACED WINDOW, AND WINDOW HEAT CONTROL.

Part: SKIN — DELAMINATED (NR 5 SLAT)

T/E WEDGE DELAMINATED, SLAT NR 5. REPLACED TRAILING EDGE WEDGE.

Part: WEDGE — DELAMINATED (NR 6 SLAT)

DELAMINATION AND INFLIGHT SEPARATION OF NR 6 SLAT T/E WEDGE. MAJOR REPAIR ACCOMPLISHED. REPLACED SLAT T/E WEDGE.

Part: LIGHT — BURNED OUT (EMERGENCY EXIT) · airframe 42,183 hrs · 15,958 cycles

RIGHT AFT EMERGENCY HATCH HANDLE LIGHT IS INOP RELAMPED.

Part: TURBINE — DAMAGED (NR 1 ENGINE) · airframe 37,458 hrs · 14,184 cycles

NUMBER 1 ENGINE LPT 3RD STAGE FAILED BORESCOPE INSPECTION.

Part: SUPPORT — CORRODED · airframe 37,013 hrs · 14,036 cycles

FLOOR SUPPORT CORRODED. MAJOR REPAIR ACCOMPLISHED.INSTALLED NEW J-ANGLE AND STRAP.

Part: SKIN — DENTED (FUSELAGE) · airframe 37,013 hrs · 14,036 cycles

FUSELAGE SKIN DENTED STA 602 - 622 STR 16L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLERS ON SKIN AND REPAIR U-CHANNELS ON STRINGER.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 37,013 hrs · 14,036 cycles

CABIN FLOOR STRUCTURE CORRODED STA 1640 TO 1681, LBL 57. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW J-ANGLES.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,013 hrs · 14,036 cycles

CABIN FLOOR SUPPORT CORRODED. STA 297, RBL 40-42. MAJOR REPAIR ACCOMPLISHED. REPLACED L-ANGLE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,013 hrs · 14,036 cycles

CABIN FLOORBEAM UPPER SURFACE CORRODED. STA 324, RBL 58 MAJOR REPAIR ACCOMPLISHED. INSTALLED FREEZE PLUB AND INSTALLED T-ANGLE REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,013 hrs · 14,036 cycles

CABIN FLOORBEAM CORRODED STA 345 - 365, BL 0. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOORBEAM SUPPORT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,013 hrs · 14,036 cycles

CABIN FLOOR SUPPORT STRUCTURE CORRODED STA 324 - 344, RBL 60. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR STRAPS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,013 hrs · 14,036 cycles

CABIN FLOORBEAM UPPER FLANGES CORRODED STA 310.5, RBL 40. *S/D* RECONNECTED POWER CONNECTOR IN INSIDE OF SIDE WALL. OP CHECKS OK.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 37,013 hrs · 14,036 cycles

CABIN FLOORBEAM VERTICAL L-ANGLE CRACKED STA 324, RBL 60. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW Z-CHANNEL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,013 hrs · 14,036 cycles

AFT CABIN FLOORBEAM LOWER SURFACE CORRODED STA 1681, RBL 4, RBL 30, LBL 12. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE AND STRAP REPAIR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,013 hrs · 14,036 cycles

FLOORBEAM CORRODED STA 1640, LBL 53. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR.

Part: BULB — FAILED (CABIN)

EMERGENCY EXIT LIGHT INOP ROW 33 ABC. RELAMPED EMERGENCY EXIT LIGHT. OPERATION CHECKS NORMAL.

Part: VALVE — LEAKING (ENGINE)

FUEL LEAK ON NR 2 ENGINE COMING FROM CORE ACCESSORY DRAIN DURING ENGINE OPERATION. NO FUEL LEAK AFTER SHUTDOWN. *S/D* REPLACED THE LPT CASE COOLING VALVE AND THE HPT CASE COOLING VALVE, CHECKS OK.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY ESCAPE PATH LIGHTING INOP AT ROWS 16 AND 17. EMERGENCY EXIT LIGHT INOP AT ROW 13. REPLACED BATTERY PACK, CHECKS OK.