N508UA

Part: SLIDING WINDOW — FAULTY (COCKPIT) · airframe 77,286 hrs · 23,447 cycles

WINDOW EICAS MSG DISPLAYED POSITION 4. (1=L FWD, 2=L SIDE, 3=R FWD, 4=R SIDE) INOP LIGHT ILLUM. FOUND FO'S SLIDING WINDOW R2 HEATER RESISTANCE READING 200 OHMS. WINDOW CONTROL SENSORS CK'D OK. NEED WINDOW PANE & WINDOW THICKNESS GAUGE. INSTALLED NEW LAMINATE. WINDOW WOULD NOT LOCK. REINSTALLED OLD LAMINATE. WINDOW LOCKED.

Part: LIGHT — UNSECURE (CABIN) · airframe 76,818 hrs · 23,358 cycles

FIRE LIGHT ON FWD PANEL NEEDS TO BE RELAMPED. SECURED LIGHT ASSY, LIGHT TEST GOOD.

Part: COVER — OUT OF POSITION (EEL SWITCH) · airframe 75,374 hrs · 23,080 cycles

WITH OVERHEAD PANEL SWITCH IN ARMED POSITION, UNARMED LIGHT ILLUM AND MSG DISPLAYED. RE-INSTALLED EMERGENCY LIGHT SWITCH COVER IN PROPER CONFIG. EMERGENCY LIGHTS CHECK OK.

Part: SLIDE — DISLODGED (L4 DOOR) · airframe 75,343 hrs · 23,074 cycles

SLIDE PACK FELL OUT AT 4L. INSPECTED AND REINSTALLED SLIDE PACK.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 75,146 hrs · 23,036 cycles

20C HAS WIRES HANGING FROM SEAT. WIRES ARE FOR EMERGENCY EXIT LIGHTS, 20ABC THRU 25ABC EMERGENCY LIGHTS INOPERATIVE DUE TO DAMAGED HARNESS.

Part: UNKNOWN — ODOR (CABIN) · airframe 74,889 hrs · 22,988 cycles

ODOR LIKE OVERHEATED PACK FOR 2 MINUTES AFTER TAKEOFF. PACK OPERATIONS WAS NORMAL ON BOTH GROUND AND AFTER TAKEOFF. PER ECS PAGE, ALL ZONE TEMPS NORMAL EXCEPT AFT CABIN WHICH WAS 80 ON THE GROUND AND THEN COOLED TO 71 AFTER TAKEOFF. RAN PACKS, NO OVERHEAT FOUND ALL NORMAL.

Part: GIRT BAR — UNSECURE (R3 DOOR) · airframe 74,664 hrs · 22,946 cycles

GIRT BAR CAME LOOSE AT DOOR 3R, WHEN CATERING OPENED DOOR. SECURED GIRT BAR PER AMM.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 74,623 hrs · 22,938 cycles

DENT NOTICED ON LDG EDGE OF LEFT HORIZONTAL STAB. DENT SIZE 5 INCHES BY 3 INCHES BY .125 DEPTH, ACCOMPLISHED INTERIM REPAIR PER EC-RA 5517-01001.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 74,606 hrs · 22,935 cycles

DENT ON LEADING EDGE OF LEFT HORIZONTAL STAB. DENT SIZE 5 BY 3 INCHES BY .125 DEPTH, ACCOMPLISHED INTERIM REPAIR PER EC-RA 5517-01001.

Part: SKIN — DENTED (BS 1618 S18-19R) · airframe 74,597 hrs · 22,932 cycles

LOWER FUSELAGE SKIN BS 1618 S18R AND S19R DENTED. ACCOMPLISHED INTERIM REPAIR PER ECRA 5330-04224. MAJOR REPAIR

Part: SKIN — DAMAGED (FUSELAGE) · airframe 74,597 hrs · 22,932 cycles

SKIN DAMAGED, REPAIRED AT DOOR 1R AT LWR DOOR CUTOUT PER ECRA 5330-04221.

Part: SKIN — DAMAGED (BS 1620 S18-19R) · airframe 74,597 hrs · 22,932 cycles

SKIN DAMAGED. REPAIRED AT BS 1620 S18-19R PER ECRA 5330-04224.

Part: SKIN — CORRODED (BS 1714-1719) · airframe 74,597 hrs · 22,932 cycles

LOWER FUSELAGE SKIN BULGING AT BS 1714 TO 1719 LBL-16. INSTALLED REPLACEMENT SKIN PANEL BS 1621-1720 S-26L TO S-26R. ALL WORK PERFORMED PER ECRA 5330-04223 AND SRM 51-40-02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 74,597 hrs · 22,932 cycles

FUSELAGE SKIN AND STRINGER DAMAGED STA 1720-1740 AT S-15AL REF SCAL LP 9963950, 9964047. MAJOR REPAIR ACCOMPLISHED: INSTALLED FUSELAGE SKIN AND STRINGER REPAIRS IN REF TO SCAL ECRA 5300-01411 SEE SCAL LP 9963950, 9964047 FOR ALL REPAIR WORK PERFORMED.

Part: STRINGER — BENT (FUSELAGE) · airframe 74,597 hrs · 22,932 cycles

STR S-14L BENT STA 630 REF SCAL LP 9664075. REPAIR ACCOMPLISHED ON SCAL NON ROUTINE 9664075. ALSO SEE PTT 5972065 FOR ADDITIONAL INFORMATION.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 74,597 hrs · 22,932 cycles

STRINGER S-14L DAMAGED STA 600-630 REF SCAL LP 9964075,9965403,9965693. MAJOR REPAIR ACCOMPLISHED: INSTALLED STRINGER REPAIRS STA 580-640.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 74,590 hrs · 22,929 cycles

FOUND CRACK IN LONGITUDINAL FLOORBOARD SUPPORT ANGLE BETWEEN STA 460-480 AT BL 0. REPLACED FLOOR SUPPORT.

Part: CONTROL CABLE — OUT OF RIG (AILERONS) · airframe 74,590 hrs · 22,929 cycles

AT CRUISE ACFT WOULD START TO ROLL LEFT AND HAD TO INPUT RUDDER TRIM TO LEVEL OFF. ACCOMPLISHED REVIEW OF AMIS HSI, AND AILERONS. ACCOMPLISHED RIG CHECK OF AILERON AND AILERON TRIM CONT SYS REF MM 27-11-00-501. ACCOMPLISHED STEP 3H, FOUND NO DISCREPANCIES, ACCOMPLISHED STEP I, AND FOUND RIG PIN A1 OK, FOUND RIG PIN A2 OUT OF RIG, ADJUSTED CABLE RUNS A2A & A2B. PIN A2 NOW RIGGED. ACCOMPLISHED STEP J AND K, AND ADJUSTED WING CABLE RUNS A1A AND A1B FOR LEFT WING AND RUNS A2A AND A2B FOR RIGHT WING. BOTH RIG PINS A3 AND A4 FIT FREELY. SAFETIED TURNBUCKLES FOR BODY CABLES IN FWD PIT ON RIGHT SIDE FOR RUNS A2A AND A2B. SAFETIED TURNBUCKLES IN RT AND LT WHEEL WELL FOR WING CABLE RUNS A1A AND A1B, A2A AND A2B. TOTAL OF 6EA TURNBUCKLES DISTURBED. ADJUSTED LEFT AND RIGHT AILERON PCA'S PER STEP L". ACCOMPLISHED DIRECTIONAL OPERATIONAL CHECK, ALL INDICATIONS ON EICAS GOOD.

Part: ACTUATOR — FAULTY (SPOILER) · airframe 74,433 hrs · 22,898 cycles

FIRST OFFICER'S CONTROL WHEEL LOOSE. REPLACED ACTUATORS AT POSITIONS 1,4,5&6. INBOUND CREW DEFECT REPORT WAS FOR EXCESSIVE RUDDER TRIM IN CRUISE FOLLOWED LATER IN FLIGHT WITH SIGNIFICANT RIGHT AILERON UPWARD DEFLECTION. TEST FLIGHT PERFORMED AS REQUIRED WITH NO ABNORMALITIES OF THE FLIGHT CONTROLS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,330 hrs · 22,874 cycles

EEL LIGHTS ON SEAT NR 1 AND SEAT NR 20 IS INOP. RELAMPED AFT EEL STRIP AT 1AB PER MM AND SECURED EEL STRIP CONNECTOR AT 20ABC. BOTH STRIPS OP OK.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 73,531 hrs · 22,717 cycles

FLUID LEAK FROM LEFT ENGINE PYLON DRAIN TUBE. LOCATED ON LOWER AFT CORNER OF ENGINE PYLON. MAINT TEXT: FOUND LARGE HYD LINE DRIPPING INSIDE AFT SIDE OF PYLON. UNION AND 'B' NUT VISIBLY DRIPPING. IT APPEARS THAT AFT PYL ON TRAILING EDGE PANEL NEEDS TO BE REMOVED SO THAT 2 EA MECHS CAN RETORQUE AND HOLD LINE AS NEEDED FROM EACH END OF LEAK. EST MIN 2 HRS. IF IT STILL LEAKS AFTER RETORQUE, POSSIBLE CRACK EXISTS. REPLACE HYD LINE IN NR 1 PYLON. OPS CHECK GOOD.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 73,531 hrs · 22,717 cycles

DIRTY SOCK SMELL AFTER TAKEOFF. REPEAT WRITEUP. ACP'D NR 1 ENGINE CHARGE. FLUID LEAK FROM LEFT ENGINE PYLON DRAIN TUBE. LOCATED ON LOWER AFT CORNER OF ENGINE PYLON. FOUND LARGE HYD LINE DRIPPING INSIDE AFT SIDE OF PYLON. UNION AND B-NUT VISIBLY DRIPPING. REPLACED HYD LINE IN NR 1 PYLON, OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 73,416 hrs · 22,695 cycles

OVERHEAD EMERGENCY LIGHTS INOP ABOVE SEATS 8AB AND 10AB. REPLACED BATTERY PACK AT SEAT 10A, LIGHTS NOT OP NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,416 hrs · 22,695 cycles

EMERGENCY LIGHT INOPERATIVE AT SEATS 9AB, 10AB, 11AB AND 12AB. REPLACED BATTERY PACK , OPS CHECKED NORMAL.

Part: SENSOR — INOPERATIVE (R2 GIRT BAR) · airframe 73,234 hrs · 22,660 cycles

THE R2 DOOR ARMED LIGHT INOPERATIVE. REPLACED R2 DOOR GIRT BAR PROXIMITY SENSORS A (S10220) AND B (S102211). R2 DOOR ARM LIGHT CHECKED OKAY.

Part: SEQUENCE VALVE — FAULTY (NLG) · airframe 73,047 hrs · 22,624 cycles

USED ALT GEAR TO EXTEND ON LANDING AFTER NO NOSE GEAR GREEN LIGHT. AS PER FAULT ISOLATION PROCEDURE 32-30-00 FIG 104, FOUND THE DOOR OPERATED SEQUENCE VALVE AT FAULT. REPLACED NOSE GEAR DOOR OPERATED SEQUENCE VALVE.

Part: FAN — FAULTY (EQUIPEMENT BAY) · airframe 72,807 hrs · 22,573 cycles

CREW SELECTED ALTERNATE AND LIGHT REMAINED ILLUMINATED. 'AFT EQ EXH FAN 1' AND 'AFT EQ EXH FAN 2' MSG DISPLAYED. REPLACED AFT EQUIPMENT FANS 1 AND 2, OPS CHECKED OKAY.

Part: TRANSCEIVER — FAULTY (WEATHER RADAR) · airframe 72,640 hrs · 22,539 cycles

AFTER TURNING ON WX RADAR GOT WXR FAIL MESSAGE SAMC TEXT: CREW REPORT CB F2 ON P11 FOR WXR RT POPPED. REPLACED WXR SCANNER ANTENNA AND WXR TRANSCEIVER. OPERATIONAL TEST OK WITH NO ABNORMALITIES NOTED. ALSO REPLACED WXR CONTROL PANEL (P/N 2041223-0427 - S/N 45). CIRCUIT BREAKER DID NOT POP DURING OPS CHECK.

Part: ACTUATOR — FAULTY (NLG) · airframe 72,633 hrs · 22,537 cycles

L/G DISAGREE MSG, RTFL. PER CREW, HAD LG DISAGREE MSG WITH ASC LIGHT. HEARD THUMP NOISE WHEN GEAR HANDLE SELECTED OFF AND WHEN SELECTED BACK UP. MAINT TEXT: PSEU SHOWS FAULTS 65 AND 78 FAULTING THE NOSE GEAR LOCK SENSORS. PER SAMC REQUESTED, RPL'D NOSE GEAR LOCK ACTUATOR PER MM & GEAR SWING PERFORMED OK.

Part: ACTUATOR — FAILED (RUDDER) · airframe 69,692 hrs · 21,972 cycles

RUDDER RATIO EICAS, FLIGHT DIVERTED. FOUND PCA FAULT BALL AND TEST FAIL FAULT BALL ON LT RUDDER RATIO CHANGER MODULE. INSTALLED NEW RRCM IN LT SIDE AND TESTED, BOTH RRCM'S SHOW FAIL AFTER 14 SECONDS. REINSTALLED ORIGINAL RRCM IN LT SIDE. NEW RRCM ON AOG R0994. OSCILLATION CHECK WAS OK. REPLACED THE RRCA IAW MM. WHILE ATTEMPTING TO RIG RUDDER RATIO CHANGER LVDT, FOUND PRIMARY CONTROL ROD HAS NO JAM NUTS ON EITHER ROD END AND APPEARS TO HAVE ROTATED WITH VISIBLE DAMAGE TO LOWER ROD END THREADS. REMOVED PRIMARY CONTROL ROD. SHIM, CUPPED WASHER, & NEW SHEAR PIN ATTACHED TO REPLACEMENT ROD ON WORK TABLE. REPLACED PRIMARY CONTOL ROD & INSTALLED A NEW SHEAR PIN.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 69,247 hrs · 21,884 cycles

ROW 18-26 ABC STOWBIN EMERGENCY LIGHTS DO NOT COME ON WHEN TESTED. REPLACED BATTERY POWER SUPPLY, M10818 AND BATTERY IAW MM. TESTS OK.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 69,247 hrs · 21,884 cycles

AISLE EMERGENCY LIGHTS AT 15 THROUGH 20 ABC DO NOT ILLUMINATE. SWAPPED INVERTER NO HELP, BATT ON ORDER. INSTALLED NEW PWR SUPPLY- NO HELP. SHORT IN SYS DUE TO SEAT-TO-SEAT CABLE BEING BOLTED DOWN UNDER ROW 19'S SEAT TRACK. SEATS AT ROW 19 NEED TO BE REMOVED SO CABLE CAN BE FIXED OR REPLACED. REMOVED SEAT ROW 19 ABC. EMERGENCY LIGHT CONNECTORS DISCONNECTED FROM SEATS FROM ROW 15 THRU 20 FOR TS. REMOVED BROKEN WIRE, REINSTALLED ROW. WIRE HARNESS SHOP REPAIRED BROKEN WIRE IN HARNESS. REPAIRED HARNESS, REINSTALLED, CHECKS GOOD. RECONNECTED CONNECTORS, CHECKS GOOD. FLOOR PANEL HAD BEEN REMOVED AT ROW 20 FOR TS. SECURED FLOOR PANEL.

Part: BOTTLE — READS LOW (L4 DOOR SLIDE) · airframe 69,237 hrs · 21,882 cycles

SLIDE 3L BOTTLE PRESS INDICATOR IN THE RED. SLIDE READS LOW. REPLACED SLIDE ASSY.

Part: SKIN — DAMAGED (EMERGENCY EXIT) · airframe 68,724 hrs · 21,781 cycles

LT AFT OVERWING EXIT DOOR HAS A HOLE IN OUTER SKIN. MAJOR REPAIR ACCOMPLISH: REPAIRED HOLE IN OVERWING EXIT DOOR, FABRICATED A REPAIR DOUBLER, FILLER AND SHIM.

Part: RESERVOIR — READS LOW (DOOR 1R) · airframe 68,724 hrs · 21,781 cycles

R1 DOOR EMERGENCY POWER RESERVOIR READS NO PRESSURE. REMOVED AND REPLACED R1 DOOR EMERGENCY POWER RESERVOIR.

Part: O-RING — DAMAGED (HYD SYSTEM) · airframe 67,280 hrs · 21,505 cycles

HYDRAULIC QTY LOW , FLT DIVERTED SHUTDOWN BOTH RT SYS PUMPS AT 49 PERCENT INDICATED. SYSTEM QTY DECLINED SOME MORE-NOW DOWN TO 47 PERCENT. RT, AC HYD. PUMP PRESSURE LINE UNION O-RING.

Part: MECHANISM — DAMAGED (ELEVATOR) · airframe 66,647 hrs · 21,381 cycles

HEAVY ELEVATOR FORCES. WORSE AT SLOWER SPEEDS, ALSO WITH RT HYD SYS OFF FORCES IMPROVE. ACP ELEV FEEL FORCE TEST. FOUND 3 LB ABOVE MAX ALLOWED. REPLACED ELEVATOR NEUTRAL SHIFT MECHANISM. ACP ELEV RIG AND FORCE CHECK. GROUND OPS CHK OKAY.

Part: ACTUATOR — FAULTY (AILERON TRIM) · airframe 66,289 hrs · 21,309 cycles

RIGHT AILERON TRIM PROBLEM, RTFL. REPLACED LATERAL TRIM ACTUATOR. OP CHECK OKAY. MOTOR SPEED NORMAL. CHK'D FOR ELEVATOR PCU HYD BYPASSING, NO BYPASSING NOTED. PERFORMED ELEVATOR FEEL CHK, WITHIN LIMITS. PERFORMED ELEVATOR SERVO TEST, CHK'D FOR ELEVATOR PCU FOR BYPASSING AND DID TEST OF THE ELEVATOR FEEL. NO FAULTS NOTED. ALL SYSTEMS WITHIN LIMITS.

Part: FEEDER CABLE — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,111 hrs · 21,079 cycles

EMERGENCY LIGHT INOP ON SEAT 19A. REPLACED SEAT CABLE. CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,523 hrs · 20,967 cycles

EEL AT 16C INOP - EMERGENCY ESCAPE PATH LIGHT AT SEAT 16C IS INOP (BROKEN WIRE). REPLACED LIGHT STRIP. OPS CHECKED OKAY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,523 hrs · 20,967 cycles

EMERGENCY LIGHT AT 19C INOP, EMERGENCY ESCAPE PATH LIGHT AT SEAT 19C IS INOP. REPLACED LIGHT STRIP. OPS CHECKED OK.

Part: LIGHT — MISSING (CABIN) · airframe 63,794 hrs · 20,831 cycles

THE 20C LIGHT STRIP ON SEAT MISSING.

Part: LIGHT — BROKEN (CABIN) · airframe 63,196 hrs · 20,719 cycles

SEAT 10B EMERGENCY LIGHT BROKEN. NEW EMERGENCY LIGHT INSTALLED.

Part: LIGHT — MISSING (CABIN) · airframe 63,196 hrs · 20,719 cycles

SEAT 16C EMERGENCY LIGHT MISSING. REPLACED EMERGENCY LIGHT STRIP. OPS CHECKED OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,943 hrs · 20,484 cycles

DOOR 2L SLIDE ARMING LIGHT INOP. FOUND SLIDE LIGHT INOP. DOOR VERIFIED TO BE ARMED. RELAMPED ARMING LIGHT, CHECKS OKAY.

Part: RADAR — INTERMITTENT (WX SYSTEM) · airframe 61,527 hrs · 20,401 cycles

WEATHER RADAR FAILURE. FLIGHT DIVERTED. *S/D* WX RADAR AUTO TILT INOP MANUAL TILT OK. CHRONIC PROBLEM, NEED NEW SCANNER. REPLACED SCANNER, OPS CHECKED NORMAL.

Part: SWITCH — FAULTY (OXYGEN MASK) · airframe 59,656 hrs · 20,048 cycles

1ST OBSV O2 MASK EMERGENGY BUTTON STUCK ON. REPLACED SWITCH, OPS NORMAL.

Part: ELEVATOR — OUT OF ADJUST (RIGHT) · airframe 59,544 hrs · 20,027 cycles

AIRCRAFT REQUIRES 4 UNITS OF RUDDER TRIM IN LEVEL FLT. CHECKED RUDDER AND RUDDER TRIM SYSTEM OK. FOUND RT ELEVATOR NOT WITHIN LIMITS ON INDEX PLATE AND E-ST9 RIG PIN HOLE NOT LINING UP. ADJUSTED, ALL CHECKS NORMAL.

Part: STRUCTURE — DAMAGED (LWR RUDDER) · airframe 59,365 hrs · 19,991 cycles

LOWER RUDDER DAMAGED. MAJOR REPAIR ACCOMPLISHED ON A/C.

Part: CONTROL PANEL — INOPERATIVE (FIRE CONTROL) · airframe 59,232 hrs · 19,966 cycles

DURING SQUIB TEST FWD AND AFT CARGO LIGHT SMOKING AND INOP. FOUND INTERNAL SHORT IN CONTROL PANEL FOR SQUIB TEST. REPLACED SQUIB TEST CONTROL PANEL.

Part: WARNING LIGHT — ILLUMINATED (ELECTRICAL SYS) · airframe 59,211 hrs · 19,962 cycles

RTFL DUE TO GENERATOR DRIVE LIGHT ILLUM.

Part: IDG — FAULTY (LEFT) · airframe 59,211 hrs · 19,962 cycles

RTFL DUE TO GENERATOR DRIVE LIGHT ILLUM. *S/D* IDG FAILURE. NO SHOP FINDINGS OTHER THAN NOISY DISCONNECT TEST. UNKNOWN FAILURE ON AIRCRAFT. REPLACED IDG.

Part: UNKNOWN — SMOKE (CABIN) · airframe 58,270 hrs · 19,783 cycles

SMOKE IN CABIN ON TAKEOFF ROLL.

Part: UNKNOWN — SMOKE (CABIN) · airframe 58,265 hrs · 19,783 cycles

SMOKE IN CABIN ON TAKEOFF ROLL.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,954 hrs · 19,722 cycles

EMERGENCY EXIT LIGHTS INOP AT ROWS 9-11, 16 & 19. 10-05-07 REPLACED INVERTER AT ROW 9 AND OPERATIONS NORMAL FOR ROWS 9-11. REPLACED SEAT LIGHTS AT ROWS 16 AND 19 AND OPERATIONS CK GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 57,451 hrs · 19,625 cycles

GEAR DISAGREE LIGHT ON WITH GEAR HANDLE UP-GONE AFTER CYCLING HANDLE TO OFF THEN UP. PERFORMED BITE TEST ON PROXIMITY SENSE ELECTRONIC UNIT (PSEU), WHICH SHOWED BOTH NOSE LANDING GEAR LOCK SENSORS 065 AND 078 ON MEMORY.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,272 hrs · 19,588 cycles

MED 2R UPPER EMERGENCY EXIT SIGN INOP ALONG WITH EEL LIGHTING AT SEATS 2AB, 3AB, 9AB, 10AB & 11AB. [07-27-07] REPLACED POWER SUPPLY. CHECKS GOOD.

Part: SWITCH — SHORTED (LAVATORY) · airframe 56,533 hrs · 19,449 cycles

DIVERTED TO DEN UNDER AMBER ALERT DUE ELECTRICAL ODOR IN FORWARD LAVATORY. [06-20-07] FOUND LAV DOOR LOCK-LIGHTING SWITCH SHORTED & BURNED. LAV POWER CIRCUIT BREAKER POPPED. REPLACED DOOR SWITCH. ALL FUNCTIONS AND SMELLS NORMAL.

Part: LIGHT — MISSING (CABIN) · airframe 56,493 hrs · 19,441 cycles

EEL LIGHT MISSING SEAT 16C. [SUP 06-06-07] REPLACED LIGHT.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 56,493 hrs · 19,441 cycles

SEAT EEL LIGHTS OUT FROM 9AB - 11AB. [SUP 06-06-07] RESEATED CONNECTOR FROM INVERTER TO SEAT LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,028 hrs · 19,352 cycles

EMERGENCY LIGHTS - THE FOLLOWING ARE INOP: EXIT DOOR 2R, SEAT ROWS 2 AND 3 AND STOW BIN LIGHT AFT OF 3AB. REMOVED AND REPLACED LAMPS, OPS CHECK GOOD.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 56,028 hrs · 19,352 cycles

DURING REWORK OF TAIL STRIKE REPAIR AT BS 1742, DAMAGE WAS INCURRED TO STR'S 29L, 29R AND REPAIRED PER EVA IMC-00680A. [06-14-07] MAJOR REPAIR ACCOMPLISHED. REPAIRED PER UA SPEC AFTER DTA RESULTS, IT HAS BEEN DETERMINED THAT THESE REPAIR'S ARE CONSIDERED TO BE CAT 'C' TIME LIMITED. RE-INSPECTED STR 29R & 29L REPAIRS AT BS 1742 AT EACH 'C' CHK FOR CORROSION OR DAMAGE PER REVISED INSTRUCTIONS.

Part: LIGHT — INOPERATIVE (R1 DOOR) · airframe 56,028 hrs · 19,352 cycles

DOOR R1 SLIDE ARMED LIGHT ABOVE DOOR INOPERATIVE. [06-14-07] REPLACED PROXIMITY SWITCH S10217.

Part: SPRING — BROKEN (EVAC SLIDE) · airframe 56,028 hrs · 19,352 cycles

DOOR 4R SLIDE SPRING FOR CLIPS BROKEN. [06-14-07] REPLACED SLIDE.

Part: ANNUNCIATOR — INOPERATIVE (L2 DOOR) · airframe 56,028 hrs · 19,352 cycles

DOOR 2L SLIDE ARMED LIGHT INOPERATIVE. [06-14-07] REPLACED L405 GIRT BAR ANNUNCIATOR.

Part: FRAME — DENTED (BS 1440 S26L) · airframe 56,028 hrs · 19,352 cycles

AFT PIT STA 1440 AT STR 26L FRAME DENTED. *S/D* MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT DAMAGED INBOARD FLANGE. INSTALLED A NESTED J-ANGLE DOUBLER.

Part: WEB — CORRODED (BS 1681) · airframe 56,028 hrs · 19,352 cycles

MAIN CABIN SHEAR WEB CORRODED STA 1681, RBL 16 TO RBL 50. *S/D* MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA. INSTALLED DOUBLER-TRIPLER FILLER REPAIR.

Part: WIRE HARNESS — DAMAGED (BS 590 RBL 30) · airframe 56,028 hrs · 19,352 cycles

AISLE LIGHT AT STA 590, RBL 30 AND AISLE LIGHT AT STA 1430, LBL 30, WIRE HARNESS DAMAGED. [SUP 4-17-07] REPAIRED EEL LIGHT AT STA 590, RBL 30 WIRE HARNESS PER BSWPM 20-30-12. REPLACED WIRE HARNESS TO AISLE EEL LIGHT AT STA 1430.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,028 hrs · 19,352 cycles

L-1 DOOR AND R-3 DOOR EXTERIOR EMERGENCY LIGHTS INOP. [SUP 4-17-07] RELAMPED L1 DOOR AND R3 DOOR EXTERNAL EEL LIGHTS. OPS CHECK GOOD.

Part: FLOORBEAM — CORRODED (BS 1681) · airframe 56,028 hrs · 19,352 cycles

MAIN CABIN FLOORBEAM CORRODED STA 1681, BL 0 (AFT SHEAR WEB DECK PLATE). *S/D* MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA. INSTALLED DOUBLER-TRIPLER FILLER REPAIR.

Part: FLOORBEAM — CORRODED (BS 960) · airframe 56,028 hrs · 19,352 cycles

MAIN DECK FLOORBEAM AREA, WEB IS CORRODED AT BS 960, RBL 67. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED FLOORBEAM WEB.

Part: SKIN — PUNCTURED (BS 700 S26L) · airframe 56,028 hrs · 19,352 cycles

FUSELAGE SKIN HAS PUNCTURE AT BS 700, STR 26L. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SKIN. FABRICATED & INSTALLED DOUBLER REPAIR.

Part: FRAME — CRACKED (BS 480-500) · airframe 56,028 hrs · 19,352 cycles

WEB FRAME BETWEEN FRAMES 500-480, RBL 12, TOP OF WEB IS CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED WEB & TOP OF WEB. FABRICATED & INSTALLED ANGLE REPAIR.

Part: FRAME — INADEQUATE (R2 DOOR) · airframe 56,028 hrs · 19,352 cycles

DOOR 2R FWD FRAME IS INADEQUATE. MAJOR REPAIR ACCOMPLISHED: INSTALLED FWD FRAME STEEL DOUBLER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 56,028 hrs · 19,352 cycles

AFT PIT STA 1360 BETWEEN STR 29R-28R SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED NEW TIE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,028 hrs · 19,352 cycles

FWD CARGO LEFT SIDE WALL LAV SERVICE PORT UPPER SKIN CORRODED AROUND DUCT AT STA 705-711, STR 19L-21. MAJOR REPAIR ACCOMPLISHED. REPLACED DOUBLER.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 56,028 hrs · 19,352 cycles

MAIN CABIN FLOORBEAM T-CAP CORROSION, STA 1640 RBL 56-59. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION. INSTALLED NEW T-CAP SECTION.

Part: FLOORBEAM — CORRODED (BS 365) · airframe 56,028 hrs · 19,352 cycles

RIGHT FWD MAIN CABIN FLOOR STRUCTURE, FLOORBEAM UPPER CHORD ON UPPER AND LOWER SURFACES CORRODED AROUND FASTENER HOLES IN MULTIPLE PLACES, BS 365.25, RBL 0 TO RBL 64. MAJOR REPAIR ACCOMPLISHED: RMV'D CORROSION. FABRICATED & INSTALLED REPAIR ANGLE & STRAP.

Part: TORQUE TUBE — DAMAGED (L1 GIRT BAR) · airframe 56,028 hrs · 19,352 cycles

L-1 DOOR LOWER GIRT BAR LINKAGE TORQUE TUBE IS GOUGED AND CORRODED. [SUP 05-22-07] L-1 DOOR LOWER GIRT BAR LINKAGE TORQUE TUBE IS GOUGED AND CORRODED. REPLACED TORQUE TUBE DURING DOOR OVERHAULS.

Part: RAM AIR TURB — UNWANTED EXTEND · airframe 55,851 hrs · 19,318 cycles

DURING WALK AROUND NOTICED RAT IN THE FULLY EXTENDED POSITION. STILL WIRED SHUT IN COCKPIT. REPLACED RAM AIR TURBINE AIRSPEED SWITCH, SYSTEM 1 AIR GRND RELAY, AND RAT TIME DELAY MODULE, TRANSFERRED APU TO EXTERNAL PWR, COULD NOT DUPLICATE FAULT, VERIFIED NO VOLTAGE AT RAT CNTRL VALVE WITH MANUAL SWITCH OFF, CYCLED SWITCH AND POWER CHECKS OK. ACCOMPISHED INPECTION AND STOWING OF RAM AIR TURBINE.

Part: STRUCTURE — CRACKED (R2 DOOR)

MAIN ENTRY DOOR 2R IS CRACKED AT RIGHT MEDIUM TOP CUTOUT. REPLACED WITH ANOTHER MAIN ENTRY CABIN DOOR. REMOVED DOOR SENT TO SHOP FOR EVALUATION. ROOT CAUSE OF CRACK IS STILL UNDER INVESTIGATION.

Part: O-RING — FAILED (SLIDE BOTTLE)

LOW BOTTLE PRESSURE. BOTTLE TO VALVE O-RING WAS DETERIORATED. REPLACED CYLINDER ASSY. OSV, WINSLOW, HAS ADDED ULTRASONIC LEAK DETECTION TO BOTTLE INSPECTION PROCESS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 44,387 hrs · 16,606 cycles

LEFT EXTERNAL FUSELAGE SKIN, BS 600 ABOVE STR 18L IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. REPAIRED PER EVA MOC1-8454.

Part: MODULE — LEAKING (LT HYD SYSTEM) · airframe 44,197 hrs · 16,537 cycles

LT HYDRAULIC SYSTEM QUANTITY DECREASE. THE CAUSE OF THIS EVENT WAS AN INCORRECT UNION/SEAL COMBINATION ON THE LT SLAT/FLAP DEPRESSURIZATION MODULE. THE SEAL/RETAINER WAS REPLACED WITH THE CORRECT PACKING.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,955 hrs · 14,611 cycles

FUSELAGE DENTED AFT OF THE NR 2 MAIN DOOR. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER.

Part: STRUCTURE — DAMAGED (TAIL) · airframe 34,545 hrs · 13,014 cycles

OVER ROTATION ON LANDING CAUSED TAIL STRIKE. *S/D* AIRCRAFT HAD A PREVIOUS TAIL STRIKE PRIOR TO THIS EVENT. THE EXISTING REPAIR WAS ABRADED AWAY BY CONTACT WITH RUNWAY. NO FURTHER DAMAGE WAS DONE TO AIRCRAFT STRUCTURE. REMOVED EXISTING REPAIR, AND RESTORED REPAIR USING SRM AND OEM REPAIR INFORMATION. REPAIR RECORDED ON MRA 115.

Part: BEARING — WORN (DOOR 2L)

UPON ARRIVAL, AGENT COULD NOT FULLY OPEN DOOR 2L. DOOR ONLY SWINGS TO THREE QUARTERS OF FULL TRAVEL. *S/D* REPLACED DOOR 2L ROTARY SNUBBER AND UPPER AND LOWER HINGE LINK BEARINGS, OPS CHECKED NORMAL.

Part: AIR DISTR — ODOR (CABIN)

RUBBER ODOR IN COCKPIT AND CABIN AFTER ANTI-ICE ACTIVATED. APPROXIMATELY FIVE MINUTES AFTER ANTI-ICE ACTIVATION ODOR BEGINS.

Part: EEL LAMP — INOPERATIVE (CABIN)

LEFT HAND OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED LAMP, CHECKS OK.