N941UW

Part: CONTROL BOX — ODOR (ENTERTAIN SYS) · airframe 71,987 hrs · 26,143 cycles

FLIGHT ATTENDANT REPORTED ODOR OF HOT, POSSIBLE ELECTRICAL FOR THE IN-FLIGHT ENTERTAINMENT. INDICATED THE ODOR DISSIPATED AROUND ROW 8-10. FA TURNED OFF THE IN-FLIGHT ENTERTAINMENT AND ODOR COMPLETELY DISSIPATED. WHILE ON APPROACH HOT ELECTRICAL ODOR RETURNED IN SAME GENERAL AREA ROWS 8-10. REPLACED SEAT ENTERTAINMENT BOX AT ROW 7 IAW AMM 23-34-06.

Part: ANGLE — CHAFED (RT PYLON) · airframe 71,491 hrs · 25,990 cycles

AIRCRAFT IN BASE MAINTENANCE. CHAFED RIGHT HAND ENGINE OUTBOARD PYLON ON LOWER METAL PLATE ZEE ANGLES, SEAL MATING SURFACE. REPAIRED ZEE ANGLES WITH REPAIR STRAP PER EA-264290 AND SRM 51-40-02.

Part: ANGLE — CHAFED (LT PYLON) · airframe 71,491 hrs · 25,990 cycles

AIRCRAFT IN BASE MAINTENANCE. CHAFED LEFT HAND ENGINE INBOARD PYLON ON LOWER METAL PLATE ZEE ANGLES, SEAL MATING SURFACE. REPAIRED ZEE ANGLES WITH REPAIR STRAP PER EA-264304 AND SRM 51-40-02.

Part: ANGLE — CHAFED (LT PYLON) · airframe 71,491 hrs · 25,990 cycles

AIRCRAFT IN BASE MAINTENANCE. CHAFED LEFT HAND ENGINE INBOARD PYLON ON LOWER METAL PLATE ZEE ANGLES, SEAL MATING SURFACE. REPAIRED ZEE ANGLES WITH REPAIR STRAP PER EA-264304 AND SRM 51-40-02.

Part: ANGLE — CHAFED (RT PYLON) · airframe 71,491 hrs · 25,990 cycles

AIRCRAFT IN BASE MAINTENANCE. CHAFED RIGHT HAND ENGINE OUTBOARD PYLON ON LOWER METAL PLATE ZEE ANGLES, SEAL MATING SURFACE. REPAIRED ZEE ANGLES WITH REPAIR STRAP PER EA-264290 AND SRM 51-40-02.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 71,107 hrs · 25,898 cycles

EMERGENCY EXIT SIGN BETWEEN L2 AND R2 DOOR INOPERABLE. REPLACED BATTERY CHARGER ASSEMBLY ABOVE DOOR R2 PER AMM 33-51-07-022-020 AND AMM 33-51-07-862-054.

Part: SKIN — DEBONDED (LE SLAT) · airframe 71,491 hrs · 25,990 cycles

AIRCRAFT IN BASE MAINTENANCE: NR 6 SLAT WEDGE HAS DISBOND COMMON TO REPAIR ON INNER SKIN INBOARD END. DISBOND ON OUTER SKIN CLOSE TO REPAIR ON INNER SKIN. BOTH DISBONDS GREATER THAN 1.5 INCHES. OUTER DISBOND LESS THAN 1 INCH FROM EDGE. REPLACED SLAT PER TASK CARD 19C61227001.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 71,491 hrs · 25,990 cycles

AIRCRAFT IN BASE MAINTENANCE. EXIT LIGHTS WILL NOT TEST IN FOUR PLACES: L3 INTERIOR DOOR; L3 EXTERIOR DOOR; R3 DOOR SIDE EXIT LIGHT; AND EMERGENCY LIGHT AT ROW 21L. REPLACED EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-07-902-001.

Part: WEBBING — WORN (EVAC SLIDE) · airframe 71,491 hrs · 25,990 cycles

AIRCRAFT IN BASE MAINTENANCE. L-1 SLIDE "Y" HARNESS WEBBING IS WORN. INSTALLED NEW L-1 SLIDE "Y" HARNESS PER WORK CARD 19C3125004.

Part: ATTACH BOLT — LOOSE (L3 DOOR) · airframe 71,491 hrs · 25,990 cycles

AIRCRAFT IN BASE MAINTENANCE. LOOSE PASSENGER CABIN L3 DOOR EVACUATION SLIDE FORWARD TOP ATTACHMENT BOLT. RETORQUED ATTACHMENT BOLT PER AMM 20-11-00.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 71,491 hrs · 25,990 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON MAIN CABIN FLOOR SUPPORT ANGLE AT BL 0 BETWEEN FUSELAGE STATIONS 1320 AND 1340. REPLACED ANGLE PER SRM 51-40-02.

Part: BUSHING — EXCESS PLAY (GIRT BAR) · airframe 71,491 hrs · 25,990 cycles

AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON L2 DOOR GIRT BAR MECHANISM, FWD AND AFT CRANKS. REPLACED GIRT BAR BUSHING PER SOPM 20-50-03 AND AMM 52-11-00-5.

Part: BUSHING — EXCESS PLAY (GIRT BAR) · airframe 71,491 hrs · 25,990 cycles

AIRCRAFT IN BASE MAINTENANCE. EXCESSIVE PLAY ON R2 DOOR GIRT BAR MECHANISM, FORWARD AND AFT CRANKS. REPLACED GIRT BAR BUSHING PER SOPM 20-50-03 AND AMM 52-11-00-5.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 71,339 hrs · 25,959 cycles

DURING INITIAL CLIMB AT 1,500 FT, CLIMB POWER WAS SET AND RIGHT ENGINE WAS SLOW TO RESPOND. AUTO-THROTTLE DISCONNECTED AND ENGINE POWER REDUCED TO 1.5 EPR AND APPEARED NORMAL. DECISION MADE TO RETURN TO DEPARTURE. THE AIRCRAFT WAS GROUNDED. MAINTENANCE R & R THE NR 2 ENGINE IAW JC 19L40071001.

Part: CIRCUIT CARD — MALFUNCTIONED (RT ENGINE) · airframe 71,042 hrs · 25,886 cycles

FLIGHT CREW REPORTED THAT DURING CLIMB OUT EICAS CAUTION RIGHT CENTER FUEL PUMP OCCURRED. AT 045 DEGREES WITH RT ENGINE N3 BEGAN TO FLUCTUATE ERRATICALLY BETWEEN 73-81%. NO VIBRATION OR SURGE NOTED. AIRCRAFT GROUNDED. MAINTENANCE REPLACED THE RT ENGINE SPEED CARD IAW AMM 77-12-03-0401. ACCOMPLISHED SATISFACTORY SPEED CARD TEST. VERIFIED STABILITY OF RT ENGINE N3 IAW AMM 77-12-00. SATISFACTORY OPS CHECKED THE AIR SUPPLY DISTRUBUTUION SYSTEM IAW AMM 36-11-00-710-801, AND THE RT CENTER FUEL PUMP IAW AMM 28-22-00-101 ACCOMPLISHED.

Part: PROXIMITY SWITCH — DEFECTIVE (R2 DOOR) · airframe 70,187 hrs · 25,679 cycles

AIRCRAFT WAS NOT GNDED. R2 DOOR WHEN DISARMED, LIGHT ABOVE DOOR INDICATES ARMED. REPLACED GIRT BAR FWD PROXIMITY SWITCH & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 25-66-11.

Part: GIRT BAR — OBSTRUCTED (R2 DOOR) · airframe 70,088 hrs · 25,657 cycles

AIRCRAFT WAS NOT GNDED. R2 DOOR SLIDE ARM LIGHT STAYS ON WITH SLIDE DISARMED. CLEANED DEBRIS FROM GIRT BAR & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: SWITCH — STICKING (R2 DOOR) · airframe 70,042 hrs · 25,646 cycles

AIRCRAFT WAS NOT GNDED. R2 DOOR SLIDE ARMED LIGHT ILLUMINATES WITH THE LOWER DOOR LEVER IN THE DISARM POSITION. EXERCISED DOOR SWITCH. OPERATIONAL CHECKED GOOD.

Part: PCU — DEFECTIVE (CABIN) · airframe 69,341 hrs · 25,451 cycles

AIRCRAFT WAS GNDED. BURNING & ACRID ELEC NEAR ROWS 21 - 23, BOTH SIDES OF CABIN. ACCOMPLISHED JC 757 TROUBLESHOOTING CABIN AIR QUALITY IAW JC 19L00021001 & FOUND PCU'S BROKEN AT 15F, 16B, 20F, 21D, 23AB, & 24AB WHICH WERE CORRECTED BY REPLACING THE DEFECTIVE PCU'S IAW AMM 25-25-00.

Part: LATCH — DEFECTIVE (L1 DOOR) · airframe 69,255 hrs · 25,424 cycles

AIRCRAFT WAS GNDED. CABIN DOOR 1L DIFFICULT TO CLOSE. REPLACED THE UPPER & LOWER AFT LATCH ROLLERS & FITTINGS & THE UPPER FWD FITTING IAW AMM 52-11-00-825-001. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED. SEE AALA201602189006, AALA201602189007 & AALA201602189008 FOR ADDITIONAL PART INFORMATION.

Part: LATCH — DEFECTIVE (L1 DOOR) · airframe 69,255 hrs · 25,424 cycles

AIRCRAFT WAS GNDED. CABIN DOOR 1L DIFFICULT TO CLOSE. REPLACED THE UPPER & LOWER AFT LATCH ROLLERS & FITTINGS & THE UPPER FWD FITTING IAW AMM 52-11-00-825-001. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED. SEE AALA201602179008, AALA201602189006 & AALA201602189008 FOR ADDITIONAL PART INFORMATION.

Part: LATCH — DEFECTIVE (L1 DOOR) · airframe 69,255 hrs · 25,424 cycles

AIRCRAFT WAS GNDED. CABIN DOOR 1L DIFFICULT TO CLOSE. REPLACED THE UPPER & LOWER AFT LATCH ROLLERS & FITTINGS & THE UPPER FWD FITTING IAW AMM 52-11-00-825-001. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED. SEE AALA201602179008, AALA201602189007 & AALA201602189008 FOR ADDITIONAL PART INFORMATION.

Part: ROLLER — DEFECTIVE (L1 DOOR) · airframe 69,255 hrs · 25,424 cycles

AIRCRAFT WAS GNDED. CABIN DOOR 1L DIFFICULT TO CLOSE. REPLACED THE UPPER & LOWER AFT LATCH ROLLERS & FITTINGS & THE UPPER FWD FITTING IAW AMM 52-11-00-825-001. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED. SEE AALA201602179008, AALA201602189006 & AALA201602189007 FOR ADDITIONAL PART INFORMATION.

Part: LENS — DETACHED (CABIN) · airframe 68,215 hrs · 25,128 cycles

2L DOOR EXIT LIGHT LENS FELL OFF. SECURED 2L DOOR EXIT LIGHT LENS.

Part: PUMP — DEFECTIVE (NR 2 ENGINE) · airframe 67,868 hrs · 25,052 cycles

FLIGHT CREW REPORTED THAT DURING CRUISE UP THE NE COAST, THE RT ENG UNSPOOLED. THE CREW SEEMED TO THINK IT MAY HAVE BEEN A COMPRESSOR STALL. THE CREW ELECTED TO DIVERT & DECLARED AN EMER. IT WAS REPORTED INITIALLY THAT THERE MAY HAVE BEEN SOME FUMES IN THE CABIN, BUT PAXS DID NOT COMPLAIN OF ANY FUMES. UPON DESCENDING, THE ENG ROLLED BACK & THE ENG PARAMETERS RETURNED TO NORMAL. REPLACED NR 2 ENG HP FUEL PUMP IAW AMM 73-11-03-004-001 & 73-11-03-404-016. SEE INITIAL SDR AALA201509129014 FOR ADDITIONAL PART INFORMATION.

Part: PUMP — DEFECTIVE (RT ENGINE) · airframe 67,868 hrs · 25,052 cycles

FLIGHT CREW REPORTED THAT DURING CRUISE UP THE NE COAST, THE RT ENG UNSPOOLED. THE CREW SEEMED TO THINK IT MAY HAVE BEEN A COMPRESSOR STALL. THE CREW ELECTED TO DIVERT & DECLARED AN EMER. IT WAS REPORTED INITIALLY THAT THERE MAY HAVE BEEN SOME FUMES IN THE CABIN, BUT PAXS DID NOT COMPLAIN OF ANY FUMES. UPON DESCENDING, THE ENG ROLLED BACK & THE ENG PARAMETERS RETURNED TO NORMAL. REPLACED NR 2 ENG HP FUEL PUMP IAW AMM 73-11-03-004-001 & 73-11-03-404-016.

Part: CABLE — BROKEN (L4 DOOR)

L4 DOOR EMER MECHANISM EXTERNAL HANDLE CABLE BROKEN. REPLACED THE L4 DOOR EXTERNAL HANDLE DISARM CABLE.

Part: GATE — CORRODED (L1 DOOR) · corrosion level 2 · airframe 66,964 hrs · 24,837 cycles

C1 CHECK. CORROSION ON L1 DOOR LOWER DOOR GATE. REPLACED L1 DOOR LOWER GATE IAW SRM 51-40-02.

Part: GATE — CORRODED (R1 DOOR) · corrosion level 2 · airframe 66,964 hrs · 24,837 cycles

C1 CHECK. CORROSION ON R1 DOOR, LOWER GATE. REPLACED R1 DOOR LOWER GATE IAW AMM 52-11-38.

Part: LIGHT — DAMAGED (CABIN) · airframe 64,913 hrs · 24,220 cycles

FLOOR EMER LIGHTS BY SEAT 12ABC & 12DEF. REPAIRED LUMINESCENT FLOOR STRIP POSITION 12ABC.

Part: COVER — DETACHED (CABIN) · airframe 64,913 hrs · 24,220 cycles

EMERGENCY EXIT LIGHT COVER AT DOOR 2L HAS FALLEN OFF. REFITTED LIGHT COVER.

Part: ATTACH FITTING — OUT OF ADJUST (EXIT SIGN) · airframe 64,881 hrs · 24,210 cycles

EMERGENCY EXIT SIGN OVER 2L FALLS OFF REPEATEDLY. ADJUSTED END HOLDING CLIPS. OPERATIONS CHECKED GOOD. OK FOR SERVICE.

Part: SIGN — UNSECURE (CABIN) · airframe 64,881 hrs · 24,210 cycles

EXIT SIGN ABOVE 2L DOOR FELL OFF, RE-SECURED.

Part: COMPUTER — MALFUNCTIONED (EICAS) · airframe 64,271 hrs · 24,061 cycles

EN-ROUTE, AT ROTATION, LT ENG OVERHEATED. CLIMBING OUT HAD TO REDUCE POWER TO STAY OUT OF RED, 744 DEGREES MOMENTARY. LT ENG STAYED AT IDLE POSITION. DECLARED AN EMER, THE FLIGHT RETURNED TO FIELD & LANDED WITHOUT FURTHER INCIDENT. RETRIEVED EXCEEDANCE ON EXCEEDANCE PAGE. ACFT TRIGGERED A START LIMIT EGT ON TAKEOFF. MAX EGT ON TAKEOFF WAS 744 DEGREES, FOR 27 SECONDS. FOR EGT LIMIT WITH N3 ABOVE 50% IS 850 DEGREES BEFORE ENTERING INTO ZONE A. CONTACTED, & SENT DATA TO ENGINEERING. OCCURRENCE WAS DUE TO A SOFTWARE ISSUE IN EICAS COMPUTER. ALL PARAMETERS WERE IN LIMITS.

Part: SKIN — DEBONDED (LE SLAT) · airframe 63,346 hrs · 23,866 cycles

RON VISIT, RT WING NR 3 LE SLAT DISBONDED ON LOWER SURFACE OF TE WEDGE BETWEEN WS 423 TO WS 425. ACCOMPLISHED TEMPORARY REPAIR ON RT WING NR 3 LE SLAT IAW SRM 51-70-10-2R, PROCEDURE 5.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 62,464 hrs · 23,576 cycles

PHL FOUND EMERGENCY MEGA PHONE INOPERATIVE, AFT CABIN. R & R MEGA PHONE, OPERATIONS CHECKED GOOD.

Part: PUMP — LEAKING (NR 1 ENGINE) · airframe 62,156 hrs · 23,474 cycles

FLIGHT 1793, CLT TO PHX, EICAS LT HYD QTY APPEARED, RAN QRM PROCEDURE. EICAS LT HYD ENG PUMP, RAN QRH PROCEDURE, LT HYD SYS PRESS RAN QRM PROCEDURE, PTU MAINTAINED NORMAL SYS PRESS UNTIL GEAR EXTENSION. EXTENDED GEAR & FLAPS VIA ALTERNATE PROCEDURES SUCCESSFULLY. R & R NR 1 ENG DRIVEN HYD PUMP. OPERATIONAL & LEAK CHECKED GOOD. FOUND DIFFERENTIAL INDICATOR AT NR 1 ENG HYD FILTER MODULE LEAKING. R & R O RING, LEAK CHECKED GOOD. R & R FILTERS AS PRECAUTION, NO CONTAMINATES FOUND. ACFT OK FOR SERVICE.

Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 61,973 hrs · 23,395 cycles

LEFT AFT MEGAPHONE INOPERATIVE. REPLACED LT AFT MEGAPHONE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 61,777 hrs · 23,328 cycles

FOUND EMERGENCY LIGHT TEST SWITCH ABOVE DOORS L2 AND L3 IS NOT WORKING. R & R EMERGENCY LIGHT BATTERIES. OPS CHECKED GOOD.

Part: INDICATOR — FAILED (HYD RESERVOIR) · airframe 61,727 hrs · 23,313 cycles

ENROUTE, CREW RECEIVED "C HYD QTY" EICAS C MESSAGE, WITH PRESSURE C SYS NORMAL DURING CRUISE. INSTRUCTED TO RETURN TO DEPARTURE. AN EMERGENCY DECLARED. LANDED WITHOUT FURTHER INCIDENT. R & R HYD RESERVOIR FILL INDICATOR. UNIT FAILED INCOMING TEST. METER POINTER STICKING & FRICTION HIGH IN METER. WINDOW GLASS LEAKING, OVERHAULED UNIT. REPLACED WINDOW & BEZEL. REPLACED METER ASSEMBLY & RECALIBRATED THE UNIT. UNIT PASSED FINAL TEST.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 61,697 hrs · 23,305 cycles

C4 CHECK -OUTSIDE EMERGENCY LIGHT AT L-1 INOPERATIVE. REPAIRED GROUND GD479-ST SYS TESTED NORMAL IAW WD 33-51-12WD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,697 hrs · 23,305 cycles

C4 CHECK, INSIDE EMERGENCY LIGHTS INOPERATIVE AT 26D, 19D AND 3C. REPAIRED GROUND SYSTEM, TESTED NORMAL IAW WDM 33-51-12, REPLACED LAMP, OPS CHECKED NORMAL IAW AMM 33-51-05 3C. TESTED NORMAL AFTER GROUND REPAIR.

Part: DOUBLER — CORRODED (ZONE 100) · airframe 61,696 hrs · 23,304 cycles

C4 CHECK, CORROSION ON DOUBLER BETWEEN BS 1661 TO 1681 & BETWEEN S24-25R. REPLACED DOUBLER IAW SRM 51-10-02, 53-00-53-1A, 51-30-01 & 51-40-02.

Part: LIGHT — BROKEN (CABIN) · airframe 61,697 hrs · 23,305 cycles

C4 CHECK, EMERGENCY SLIDE LIGHT ASSY OVER L1 DOOR BROKEN. REPLACED EMERGENCY LIGHT ASSY IAW WDM 25-66-11 & PERFORMED TEST AMM 25-66-11-822-011. TEST NORMAL IAW SPWM 20-84-18.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 61,697 hrs · 23,305 cycles

C4 CHECK, POWER SUPPLY AT BS 1324 BEHIND LT MID LAV FAILED. REPLACED POWER SUPPLY BATTERY CHARGER ASSY . BATTERY CHARGE TESTED OK IAW WDM 33-51-14.

Part: CHARGER — FAILED (EMERGENCY LIGHT) · airframe 61,697 hrs · 23,305 cycles

C4 CHECK, POWER SUPPLY AT BS 1324 BEHIND RT MID LAV FAILED. REPLACED POWER SUPPLY BATTERY CHARGER ASSY. TESTED OK IAW WDM 33-51-14.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 61,697 hrs · 23,305 cycles

C4 CHECK, EXIT SIGN LENS DAMAGED AT L-2 DOOR. REPLACED EXIT SIGN LENS.

Part: STRINGER — CRACKED (ZONE 100) · airframe 61,696 hrs · 23,304 cycles

2S CHECK, CRACK ON STRINGER AT BS 1675, S24R. REPAIRED STRINGER24R IAW SRM 53-00-03-2R-1, FIG. 201, DETAIL II, SHEET 8.

Part: GATE — CORRODED (R4 DOOR) · airframe 61,696 hrs · 23,304 cycles

C4 CHECK, CORROSION FOUND ON R4 DOOR LOWER GATE AT BS 1660, RBL 66. REPLACED R4 DOOR LOWER GATE IAW AMM 52-11-38.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,696 hrs · 23,304 cycles

C4 CHECK, CORROSION ON FLOORBEAM AT BS 1681, LBL 12-47. REPAIRED FLOORBEAM IAW SRM 51-10-02, 53-00-51-1A & 53-60-51-2R, PROC 3, FIG 201.

Part: DOUBLER — CHAFED (R4 DOOR SKIN) · airframe 61,696 hrs · 23,304 cycles

C4 CHECK, CHAFED AREA ON R4 DOOR INNER SURFACE SKIN DOUBLER AT BS 1660, RB L66. REPLACED DOOR SKIN DOUBLER IAW SRM 51-10-02, 51-10-01-1A-1, 51-40-02 & DWG 146N6215.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,696 hrs · 23,304 cycles

C4 CHECK, CORROSION FOUND ON FLOORBEAM AT BS 1681, RBL 25. REPAIRED FLOORBEAM IAW SRM 51-10-02, 53-00-51-1A & 53-60-51-2R, PROC.3, FIG 201.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 61,696 hrs · 23,304 cycles

C4 CHECK, CRACK FOUND IN INTERCOSTALWEB, BETWEEN BS 1620 TO 1640, BL 0. REPLACED INTERCOSTAL IAW SRM 51-40-02.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,696 hrs · 23,304 cycles

C4 CHECK, CORROSION FOUND ON ANGLE BETWEEN BS 1640 TO 1680, RBL 60. REPLACED ANGLE IAW SRM 51-10-02, 53-00-51-1A & 51-40-02.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,696 hrs · 23,304 cycles

C4 CHECK, CORROSION FOUND ON HAT CHANNEL SUPPORT BRACKET AT BS 1675, LBL 65. REPLACED HAT CHANNEL SUPPORT BRACKET IAW SRM 51-10-02, 53-00-51-1A & DWG 146N8016.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,696 hrs · 23,304 cycles

C4 CHECK, CORROSION FOUND ON FLOOR SUPPORT BETWEEN BS 1661 TO 1681, LBL 62. REPLACED FLOOR SUPPORT IAW SRM 51-10-02, 53-00-04-1A & 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,696 hrs · 23,304 cycles

C4 CHECK, CORROSION ON FLOOR SUPPORT AT BS 1670, LBL 52. REPLACED FLOOR SUPPORT IAW SRM 51-10-02, 53-00-04-1A & 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,696 hrs · 23,304 cycles

C4 CHECK, CORROSION FOUND ON FLOOR SUPPORT BETWEEN BS 1640 TO 1661, LBL 62. REPLACED FLOOR SUPPORT IAW SRM 51-10-02, 53-00-04-1A & 51-40-02.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,696 hrs · 23,304 cycles

C4 CHECK, CORROSION ON INTERCOSTAL AT BS 329 BETWEEN RBL 5 TO 25. REPAIRED INTERCOSTAL IAW SRM 51-10-02, 53-00-04-1A & 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 324-345) · corrosion level 2 · airframe 61,696 hrs · 23,304 cycles

C4 CHECK, CORROSION ON FLOOR SUPPORT TEE BETWEEN BS 324 TO 345, RBL 25. REPAIRED FLOOR SUPPORT IAW SRM 51-10-02, 53-00-04-1A, 51-40-02 & DWG 141N5150.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,696 hrs · 23,304 cycles

C4 CHECK, CORROSION ON INTERCOSTAL BETWEEN BS 324 TO 345, RBL 63. REPAIRED INTERCOSTAL IAW SRM 51-10-02-0G, 53-00-51-1A, 51-40-02-0G & DWG 141N5170.

Part: FLOORBEAM — CORRODED (BS 324) · corrosion level 2 · airframe 61,696 hrs · 23,304 cycles

C4 CHECK - CORROSION ON FLOORBEAM AT BS 324 BETWEEN RBL 45 TO 65. REPAIRED FLOORBEAM IAW SRM 53-10-08-1A, 53-10-08-2R-1, FIG 201.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,696 hrs · 23,304 cycles

C4 CHECK, CORROSION ON INTERCOSTAL BETWEEN BS 377.7 TO 395, RBL 61. REPAIRED INTERCOSTAL IAW SRM 51-10-02-0G, 53-00-51-1A, 51-40-02-0G & DWG 141N5166.

Part: GATE — CORRODED (L4 DOOR) · corrosion level 2 · airframe 61,696 hrs · 23,304 cycles

C4 CHECK, CORROSION FOUND ON L4 DOOR LOWER GATE AT BS 1661, LBL 66. REPLACED GATE IAW SRM 52-10-02-1A-1 & CMM 52-11-25.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,696 hrs · 23,304 cycles

C4 CHECK, CORROSION ON FLOORBEAM AT BS 1640 AT RBL 60. REPAIRED FLOORBEAM IAW SRM 51-10-02, 53-00-51-1A & 53-00-51-2R-9.

Part: SLAT — DEBONDED (NR 1 SLAT) · airframe 61,696 hrs · 23,304 cycles

C4 CHECK, DEBONDING ON NR 1 SLAT WEDGE AT WS 775.5. REPAIRED NR 1 SLAT WEDGE IAW SRM 51-70-10-2R, REPAIR NR 4, FIG 201.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,696 hrs · 23,304 cycles

C4 CHECK, CORROSION ON FLOORBEAM AT BS 377, LBL3. REPAIRED FLOORBEAM IAW SRM 51-10-02, 53-00-51-1A & 53-00-51-02R-5.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,696 hrs · 23,304 cycles

C4 CHECK, CORROSION ON FLOOR SUPPORT FITTING BETWEEN BS 324 - 333, RBL 3. REPLACED FLOOR SUPPORT FITTING IAW SRM 51-10-02, 53-00-04-1A & 51-20-01.

Part: WEDGE — DEBONDED (NR 3 SLAT) · airframe 61,696 hrs · 23,304 cycles

C4 CHECK, DEBONDING ON NR 3 SLAT WEDGE AT WS 481.5. REPAIRED NR 3 SLAT WEDGE IAW SRM 51-70-10-2R, REPAIR 34, FIG 201.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 61,696 hrs · 23,304 cycles

C4 CHECK, CORROSION ON FLOORBEAM AT BS 1640 BETWEEN BL 0 TO LBL 60. REPAIRED FLOORBEAM IAW SRM 51-10-02, 53-00-51-1A & 53-00-51-02R-9.

Part: UNKNOWN — ODOR (CABIN) · airframe 61,320 hrs · 23,203 cycles

ENROUTE, F/A REPORTED 3 F/A`S IN REAR ILL FROM ODOR IN REAR GALLEY. CREW DECLARED AN EMERGENCY, RAN SMOKE & FUMES QRH PROCEDURE AND RETURNED TO FIELD. ODOR SMELLED LIKE BODY ODOR, CAUSING ILLNESS. DETECTED IN REAR GALLEY RUN 16. ON GEAR EXTENSION, FRONT & FWD F/A SMELLED IN FRONT GALLEY & COCKPIT. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MX TROUBLESHOT THE ACFT. NO OBNOXIOUS FUMES OR ODORS DETECTED.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,989 hrs · 23,114 cycles

CORROSION ON FUSELAGE SKIN AT BS1380, S28R. REPAIRED FUSELAGE SKIN AT BS1380, S28R IAW EA NR 104872.

Part: HANDLE — LACK OF LUBE (R4 DOOR) · airframe 60,779 hrs · 23,072 cycles

R4 DOOR EXTERIOR HANDLES DO NOT STOW WHEN DOOR IS OPENED, PREVENTING DOOR FROM OPENING FULLY ONTO LOCK AND GOUGING FUSELAGE SKIN. FOUND R4 DOOR EXT HANDLES STIFF. LUBRICATED HANDLE. OPS CHECKED OK.

Part: LIGHT — BROKEN (CABIN) · airframe 60,779 hrs · 23,072 cycles

EMERGENCY LIGHT BROKEN. R & R EMERGENCY LIGHT.

Part: LENS — LOOSE (CABIN)

PHX - 2R EMERGENCY EXIT LIGHT COVER IS LOOSE. REPLACED 2R DOOR EMERGENCY EXIT LIGHT LENS - OPS NORMAL.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 58,920 hrs · 22,431 cycles

CLT - CREW FLASHLIGHT LEFT SIDE ROW 24 FAILS LED CHECK. REPLACED BATTERY. CHECKS NORMAL.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 56,166 hrs · 21,564 cycles

C3 CHECK - CRACK ON FLOORBEAM AT BS 1661, RBL 25. REPLACED FLOORBEAM AT BS 1661, RBL 25 IAW TYPICAL REPAIR 757-5335-11-0334.

Part: PANEL — CRACKED (LE SLAT) · airframe 56,166 hrs · 21,564 cycles

C3 CHECK - CRACK ON NR 1 LEFT WING SLAT COVE PANEL AT INBOARD MAIN TRACK. REPLACED NR 1 LEFT WING SLAT COVE PANEL AT INBOARD MAIN TRACK IAW BOEING DRAWINGS 114N4075 AND 114N4002.

Part: PANEL — DELAMINATED (VERTICAL STAB) · airframe 56,166 hrs · 21,564 cycles

C3 CHECK - DELAMINATION ON RIGHT LOWER VERTICAL STABILIZER TORQUE BOX PANEL BETWEEN FSS119.467 TO FSS270. REPLACED RIGHT LOWER VERTICAL STABILIZER TORQUE BOX PANEL BETWEEN FSS199.467 TO FSS270 IAW B757 SRM 51-40-02 AND BOEING DRAWING 175N2001.

Part: PANEL — CRACKED (LE SLAT) · airframe 56,166 hrs · 21,564 cycles

C3 CHECK - CRACK ON NR 9 SLAT COVE PANEL 11 INCHES FROM TRAILING EDGE UPPER SURFACE AND 1 INCH FROM INBOARD END. REPLACED COVE PANEL 11 INCHES FROM TRAILING EDGE UPPER SURFACE AND 1 INCH FROM INBOARD END ON NR 9 SLAT IAW BOEING DRAWING 14N4003.

Part: PANEL — CRACKED (LE SLAT) · airframe 56,166 hrs · 21,564 cycles

C3 CHECK - CRACK ON NR 9 SLAT COVE PANEL 11.5 INCHES FROM TRAILING EDGE UPPER SURFACE AND 32 INCHES FROM INBOARD END. REPLACED COVE PANEL 11.5 INCHES FROM TRAILING EDGE UPPER SURFACE AND 32 INCHES FROM INBOARD END ON NR 9 SLAT IAW BOEING DRAWING 14N4003.

Part: FLAP — DELAMINATED (RT WING) · airframe 56,166 hrs · 21,564 cycles

C3 CHECK - DELAMINATION ON RIGHT WING OUTBOARD TRAILING EDGE FLAP APPROX 51 INCHES INBOARD FROM OUTBOARD END AT NR 3 FLAP TRACK. REPLACED RIGHT WING OUTBOARD TRAILING EDGE FLAP.

Part: LIGHT — BROKEN (CABIN)

PHL - EMERGENCY LIGHT SWITCH PANEL HAS A BROKEN LIGHT ASSY. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH PANEL. OPS CHECK GOOD AT THIS TIME.

Part: DOOR — OUT OF ADJUST (CABIN)

PHL - AIRCRAFT AFT LEFT SERVICE DOOR HANDLES ON OUTSIDE OF A/C NOT FLUSH. MAINTENANCE FOUND DOOR OUT OF SEQUENCE. WORKED DOOR. NO FAULTS.

Part: UNKNOWN — ODOR (CABIN)

DUB FLT 724 CLT TO DUB. FLIGHT ATTENDANTS REPORTED DIRTY SOCKS SMELL IN AFT CABIN UPON DESCENT. MAINTENANCE CHECKED GALLEY OVENS AND CLEANED. OPERATED LT AND RT PACKS FOR ONE HOUR. COULD NOT REPRODUCE SMELL. CHECK HYDRAULIC QUANTITY AND ENGINE NO UPLIFT: LT HYD 97%, CTR 93%, R/H 97%. ENG NR 1 20, ENG NR 2 20. VERIFIED NOTHING COMING FROM THE AFT GALLEY AREA WITH BOTH PACKS ON FOR ONE HOUR.

Part: CHARGER — FAULTY (CABIN)

PHL - MAINTENANCE FOUND THE EXTERIOR EMERGENCY LIGHT AT THE R2 DOOR INOPERATIVE. REPLACED THE CHARGER ASSEMBLY.

Part: CHARGER — INOPERATIVE (CABIN)

PHX - THE AIRCRAFT LEFT EMERGENCY LIGHT ON L3 DOOR IS NOT WORKING. REPLACED THE L3 DOOR SLIDE LIGHT ASSEMBLY, AND THE EMERGENCY LIGHT BATTERY PACK CHARGER.

Part: LIGHT — INOPERATIVE (CABIN)

PHX - THE AIRCRAFT LEFT EMERGENCY LIGHT ON L3 DOOR IS NOT WORKING. REPLACED THE L3 DOOR SLIDE LIGHT ASSEMBLY, AND THE EMERGENCY LIGHT BATTERY PACK CHARGER.

Part: COUPLER — INOPERATIVE (HF COMM)

PHX FLT 807 EN-ROUTE PHX TO HNL. THE CREW COULD NOT GET THE AIRCRAFT HF RADIOS TO TRANSMIT OR RECEIVE, REPORTING: "TRANSMISSION AND RECEPTION ON R HF AT 5547, 8843 KHZ INOP (OCCASIONAL XMISSIONS ON 5547, WEAK)" AND "TRANSMISSION AND RECEPTION ON L HJF AT 5547, 8843 KHZ INOP". MAINTENANCE AND DISPATCH WERE CONSULTED. A CIRCUIT BREAKER RESET ONLY BROUGHT BACK HF RADIO RECEIVING CAPABILITY. THE FLIGHT COULD NOT CONTINUE ETOPS OPERATION, SO IT RETURNED TO PHX. A DECISION WAS MADE TO LAND OVERWEIGHT DUE TO TURBULENCE IN THE AREA. AN EMERGENCY WAS REPORTED TO HAVE BEEN DECLARED. TUNING AND RECEIVE FAULTS. REPLACED REAR CONTACT TO FIX UNIT.

Part: TRANSCEIVER — INOPERATIVE (HF COMM)

FLT 807 EN-ROUTE. THE CREW COULD NOT GET THE AIRCRAFT HF RADIOS TO TRANSMIT OR RECEIVE, REPORTING: "TRANSMISSION AND RECEPTION ON R HF AT 5547, 8843 KHZ INOP (OCCASIONAL XMISSIONS ON 5547, WEAK)" AND "TRANSMISSION AND RECEPTION ON L HJF AT 5547, 8843 KHZ INOP". MAINTENANCE AND DISPATCH WERE CONSULTED. A CIRCUIT BREAKER RESET ONLY BROUGHT BACK HF RADIO RECEIVING CAPABILITY. THE FLIGHT COULD NOT CONTINUE ETOPS OPERATION, SO IT RETURNED TO PHX. A DECISION WAS MADE TO LAND OVERWEIGHT DUE TO TURBULENCE IN THE AREA. AN EMERGENCY WAS REPORTED TO HAVE BEEN DECLARED. VENDER FOUND NO FAULTS.

Part: COUPLER — INOPERATIVE (HF COMM)

PHX FLT 807 EN-ROUTE PHX TO HNL. THE CREW COULD NOT GET THE AIRCRAFT HF RADIOS TO TRANSMIT OR RECEIVE, REPORTING: "TRANSMISSION AND RECEPTION ON R HF AT 5547, 8843 KHZ INOP (OCCASIONAL XMISSIONS ON 5547, WEAK)" AND "TRANSMISSION AND RECEPTION ON L HJF AT 5547, 8843 KHZ INOP". MAINTENANCE AND DISPATCH WERE CONSULTED. A CIRCUIT BREAKER RESET ONLY BROUGHT BACK HF RADIO RECEIVING CAPABILITY. THE FLIGHT COULD NOT CONTINUE ETOPS OPERATION, SO IT RETURNED TO PHX. A DECISION WAS MADE TO LAND OVERWEIGHT DUE TO TURBULENCE IN THE AREA. AN EMERGENCY WAS REPORTED TO HAVE BEEN DECLARED. NO FAULTS FOUND.

Part: TRANSCEIVER — INOPERATIVE (HF COMM)

FLT 807. CREW COULD NOT GET THE ACFT HF RADIOS TO TRANSMIT OR RECEIVE, REPORTING: "TRANSMISSION AND RECEPTION ON RT HF AT 5547, 8843 KHZ INOP (OCCASIONAL XMISSIONS ON 5547, WEAK)" AND "TRANSMISSION AND RECEPTION ON LT HJF AT 5547, 8843 KHZ INOP". MAINTENANCE AND DISPATCH WERE CONSULTED. A CIRCUIT BREAKER RESET ONLY BROUGHT BACK HF RADIO RECEIVING CAPABILITY. THE FLIGHT COULD NOT CONTINUE ETOPS OPERATION, SO IT RETURNED TO PHX. A DECISION WAS MADE TO LAND OVERWEIGHT DUE TO TURBULENCE IN THE AREA. AN EMERGENCY WAS REPORTED TO HAVE BEEN DECLARED. NO FAULTS FOUND.

Part: LINE — LOW PRESSURE (L1 DOOR SLIDE)

FLL - THE L1 DOOR EMERGENCY POWER RESERVOIR PRESSURE WAS FOUND BELOW LIMITS. REMOVED AND REPLACED THE EMERGENCY POWER RESERVOIR AT L1 DOOR. FOUND BOURDON TUBE IN PRESSURE GAUGE LEAKING. REPLACED PRESSURE GAUGE AND SERVICED THE UNIT.

Part: PANEL — DEBONDED (VERTICAL STAB) · airframe 51,421 hrs · 20,269 cycles

CLT - C2 - MAJOR REPAIR - NR 19-9755-8-0020 & 5003005 - DISBONDING ON RIGHT VERTICAL TORQUE BOX PANEL. REPAIRED RIGHT VERTICAL TORQUE BOX PANEL IAW B757 SRM 51-70-10 & US AIRWAYS EA 101928.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 51,421 hrs · 20,269 cycles

CLT - C2 - MAJOR REPAIR - CORROSION ON LEFT CREASE BEAM INNER CHORD BETWEEN BS 670 & BS 686, S17L. REPLACED LEFT CREASE BEAM INNER CHORD BETWEEN BS 670 & BS 755, S17L IAW B757 SRM 51-10-02 & BOEING DRAWING 143N8322.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

MCO - F/A EMERGENCY FLASHLIGHT AT POSITION 3R DOOR HAS A LOW BATTERY. MAINTENANCE REPLACED FLASHLIGHT.

Part: GIRT BAR — DEFECTIVE (R1 DOOR)

PHL - THE SLIDE ARMED LIGHT AT DOOR R1 IS INOPERATIVE. REPLACED R1 GIRT BAR.

Part: CHARGER — FAULTY (EMERGENCY LIGHTS)

BRU - DURING DAILY CHECK FOUND EMERGENCY LIGHTING AT ROW 21 A, B, C AND AT DOOR 3 L & R EXIT SIGNS & OVERHEAD EXIT SIGN AT ROW 24 NOT WORKING. MAINTENANCE REPLACED BATTERY CHARGER ASSEMBLY.

Part: FAN — DEFECTIVE (RIGHT)

PHL PILOT REPORTED THE RIGHT RECIRC FAN INOP LIGHT ILLUMINATED WITH ELECTRICAL BURNING ODOR IN COCKPIT AND CABIN. WHEN SWITCH WAS TURNED OFF, ODOR WENT AWAY. WHEN SWITCH WAS RESET AND TURNED ON, ODOR RETURNED. MAINTENANCE REMOVED AND REPLACED THE RIGHT RECIRC FAN IN ASSOCIATION WITH AMM 21-25-01. OPERATIONAL CHECK GOOD PER AMM 21-25-00.

Part: LIGHT — INOPERATIVE (EVAC SLIDE)

DUB - THE R4 DOOR SLIDE ENGAGEMENT LIGHT REQUIRED A RELAMP. MAINTENANCE RELAMPED THE R4 DOOR SLIDE ENGAGEMENT LIGHT.

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 46,822 hrs · 19,185 cycles

EMERGENCY LIGHT BATTERY PACK ABOVE LEFT EMERGENCY DOOR NR 3 DOES NOT CHARGE. REPLACED EMERGENCY LIGHT BATTERY PACK ABOVE LEFT EMERGENCY DOOR NR 3 IAW B757 AMM 33 33-51-07.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 46,822 hrs · 19,185 cycles

SAL - C1 - MAJOR REPAIR - CORROSION ON FLOORBEAM AT BS 740, WL 208, BETWEEN RBL 49 TO RBL 61. REPAIRED FLOORBEAM AT BS 740, WL 208, BETWEEN RBL 49 TO RBL 61 IAW SRM 53-00-51.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 46,822 hrs · 19,185 cycles

MCN - C1 - MAJOR REPAIR - CORROSION ON FLOORBEAM AREA GUTTER SUPPORT AT R2 DOOR BETWEEN BS 720 TO BS 740, RBL 65. REPLACED GUTTER SUPPORT AT R2 DOOR BETWEEN BS 720 TO BS 740, RBL 65 IAW B757 SRM 51-40-02.

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 46,822 hrs · 19,185 cycles

MCN - C1 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON WEB BETWEEN BS 648 TO BS 651, LBL 8. REPLACED WEB BETWEEN BS 648 TO BS 651, LBL 8 IAW B757 SRM 51-40-02.

Part: FLAP — DEBONDED (TE FLAP) · airframe 46,822 hrs · 19,185 cycles

MCN - C1 - MAJOR REPAIR - RIGHT INBOARD FLAP DISBONDED AT WS 233 TO WS 235. REPAIRED RIGHT INBOARD FLAP AT WS 233 TO WS 235 IAW B757 SRM 51-70-10.

Part: POWER SUPPLY — NO TEST (CABIN)

CLT - THE EMERGENCY LIGHT POWER SUPPLY OVER L3 DOOR WILL NOT TEST. MAINTENANCE REPLACED THE POWER SUPPLY UNIT FOR THE L3 DOOR. OPERATIONALLY CHECKS OK.

Part: FLOOR SUPPORT — CORRODED (FUSLEAGE) · corrosion level 1 · airframe 41,217 hrs · 41,217 cycles

AROUND NUT PLATE HOLES (90 PERCENT) CTR FLOOR SUPPORT BL 0 STA 1640-1681.8 HAS CORROSION. REPLACED CHANNELS PER SRM 51-40-02; CORR TASK JL-58-53516; LEVEL 1, DEFECT SIZE: 1 INCH.

Part: MOUNT — CORRODED (AFT GALLEY) · corrosion level 1 · airframe 41,217 hrs · 41,217 cycles

AFT GALLEY RIGHT OUTBOARD MOUNTS 2 EA AROUND BARREL NUT HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER BOEING DWG 415N40C2; CORR LEVEL 1; TASK JL-58-5316, DEFECT SIZE: 1 INCH.

Part: ATTACH ANGLE — CORRODED (APU DOOR) · airframe 41,217 hrs · 41,217 cycles

TOP, LWR & FWD SIDES OF APU INTAKE DOOR ON 3 ATTACH ANGLES HAS CORROSION. MFG ANGLES PER BOEING DWG 148N3152 & SRM 53-00-07, DEFECT SIZE: 10 SQ INCHES.

Part: MOUNT — CORRODED (AFT GALLEY) · corrosion level 1 · airframe 41,217 hrs · 41,217 cycles

AFT GALLEY LEFT OUTBOARD MOUNTS 2 EA AROUND BARREL NUT HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENT PART PER BOEING DWG 415N40C2; CORR LEVEL 1; TASK JL-58-53516, DEFECT SIZE: 1 INCH.

Part: GALLEY TRACK — CORRODED (FUSELAGE) · corrosion level 1 · airframe 41,217 hrs · 41,217 cycles

AFT GALLEY RT OUTBOARD MOUNTS 2 EA HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER BOEING DWG 415N40C2; CORR LEVEL 1; TASK JL-58-5316, DEFECT SIZE: 1 INCH.