N959UW

Part: FAN — BURNED OUT (ZONE 100 - FUSE) · airframe 27,474 hrs · 20,501 cycles

AIRCRAFT WAS GROUNDED: FAN 1 EBAY MID C/B OUT AND WON'T RESET. FAN SMELLS BURNT AND WILL NEED REPLACEMENT. REPLACED FAN-1 EBAY MID. IAW AMM 21-26-04. OPS CK GOOD. REPLACED K8 RELAY IAW AMM 21-26-00.

Part: ACM — FAILED (NR 1) · airframe 27,154 hrs · 20,249 cycles

AIRCRAFT WAS GROUNDED: FLIGHT CREW DECLARED AN EMERGENCY INTO LGA ON ACCOUNT OF ODOR IN THE CABIN AND COCKPIT. ODOR DISSIPATED AFTER PACK #1 WAS TURNED OFF. SMELLED LIKE GUN POWDER. MAINTENANCE ACCOMPLISHED JOB CARD 43L00021001- SMOKE ODOR FUMES. FOUND PACK 1 ACM TO GRIND AND EMIT "GUN POWDER " ODOR . REPLACED PACK 1 ACM IAW AMM 21-51-05. OPS CHECK NORMAL.

Part: PIN — DETACHED (L2 DOOR SLIDE) · airframe 25,779 hrs · 18,981 cycles

AIRCRAFT WAS NOT GROUNDED: PIN WAS LOOSE AND DANGLING FROM SLIDE AT 2L DOOR. MAINTENANCE FOUND 2L DOOR BUSTLE LATCH PIN OUT AND INSTALLED PIN PER AMM 25-23-07.

Part: RIB — CRACKED (RT WING) · airframe 25,410 hrs · 18,697 cycles

RIGHT WING LEADING EDGE RIB 17 WAS CRACKED. REPLACED THE RIB IAW SRM 51-43-04, AND 51-41-02.

Part: FLAP TRACK — WORN (LT WING) · airframe 25,410 hrs · 18,697 cycles

LEFT WING FLAP TRACK NR 1, OUTBOARD EDGE WIDTH REDUCED AND WORN. REPLACED THE FLAP TRACK IAW AMM 57-54-21-400-801-B.

Part: STOP FITTING — WORN (AFT DOOR FRAME) · airframe 25,410 hrs · 18,697 cycles

AFT PASSENGER DOOR FRAME HAD THREE WORN DOOR STOPS. REPLACED THE DOOR STOPS IAW AMM 53-23-21.

Part: FLOOR SUPPORT — CORRODED (FRAMES 90-91) · airframe 25,410 hrs · 18,697 cycles

CORROSION FOUND ON THE AFT CABIN FLOOR SUPPORT BETWEEN FRAMES 90 AND 91, -Y279. REPLACED THE FLOOR SUPPORT IAW EA 288607, SRM 51-41-01, AND SRM 51-41-02.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 25,410 hrs · 18,697 cycles

LEFT WING INBD AFT FLAP OTBD UPPER SURFACE SKIN DELAMINATED. REPAIRED THE FLAP SKIN IAW SRM 51-73-00.

Part: FLOOR SUPPORT — CORRODED (FRAME 90) · airframe 25,410 hrs · 18,697 cycles

CORROSION FOUND ON THE AFT CABIN WET AREA FLOOR SUPPORT, FRAME 90, -Y279. REPLACED THE FLOOR SUPPORT IAW SRM 51-10-03, AND SRM 51-12-01.

Part: SEAT TRACK — CORRODED (FRAME 84) · airframe 25,410 hrs · 18,697 cycles

CORROSION FOUND ON THE SEAT TRACK, FRAME 84, +Y330. REPAIRED THE SEAT TRACK IAW SRM 53-00-10, REPAIR 51.

Part: FLOORBEAM — CORRODED (FRAME 84) · airframe 25,410 hrs · 18,697 cycles

CORROSION FOUND ON THE AFT CABIN WET AREA FLOORBEAM ANGLE, AT FRAME 84, Y330. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-75-16, 51-10-03, 51-41-02, AND 51-53-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 86-87) · airframe 25,410 hrs · 18,697 cycles

CORROSION ON THE FLOOR SUPPORT BETWEEN FRAMES 86 AND 87, RBL 260. REPLACED THE FLOOR SUPPORT IAW RD 53-00-00-3, REPAIR 3.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 25,410 hrs · 18,697 cycles

LEFT WING INBOARD TRAILING EDGE FLAP, LOWER FORWARD SKIN HAS EXPOSED COMPOSITE MESH. REPAIRED THE FLAP SKIN IAW SRM 51-71-08.

Part: SUPPORT FITTING — WORN (FRAME 84) · airframe 25,410 hrs · 18,697 cycles

AFT PASSENGER DOOR CUTOUT SUPPORT FITTING HOLE ELONGATED AT FRAME 84 BETWEEN STRINGERS 5 AND STRINGER 6. REPLACED SUPPORT FITTING IAW SRM 51-43-01.

Part: FLOOR SUPPORT — CORRODED (FRAMES) · airframe 25,410 hrs · 18,697 cycles

CORROSION FOUND ON THE AFT WET AREA FLOOR SUPPORT BETWEEN FRAMES 90 AND 91, RBL 254. REPLACED THE FLOOR SUPPORT IAW SRM 51-10-03.

Part: FLOORBEAM — CORRODED (FRAME 90) · airframe 25,410 hrs · 18,697 cycles

CORROSION ON AFT CABIN WET AREA FLOORBEAM AT FRAME 90 AND -Y320. REPLACED THE FLOORBEAM ANGLE IAW RD 53-00-00-3, REPAIR 3.

Part: FLOORBEAM — CORRODED (FRAMES 86-89) · airframe 25,410 hrs · 18,697 cycles

CORROSION ON AFT CABIN WET AREA FLOOR SUPPORT BETWEEN FRAMES 86 AND 89, LBL 279. REPLACED THE FLOOR SUPPORT IAW RD 53-00-00-3, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAME 84) · airframe 25,410 hrs · 18,697 cycles

CORROSION FOUND ON THE AFT CABIN FLOOR SUPPORT, FRAME 84, +Y330. REPLACED THE FLOOR SUPPORT IAW SRM 51-75-16, 51-10-03, 51-41-02, AND 51-43-02.

Part: WEB — CORRODED (FRAME 85-86) · airframe 25,410 hrs · 18,697 cycles

CORROSION ON THE AFT CABIN WET AREA UPPER SHEET BETWEEN FRAMES 85 AND 86 AT -Y279. REPLACED THE UPPER SHEET IAW AARD 53-00-00-3 REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (ZONE 100 - FUSE) · airframe 25,410 hrs · 18,697 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SUPPORT BETWEEN FR 88 AND FR 90 AT RBL 889. REPLACED FLOOR SUPPORT PER AARD 53-00-00-3 REPAIR 3.

Part: WEB — CORRODED (FRAMES 85-86) · airframe 25,410 hrs · 18,697 cycles

CORROSION FOUND ON THE AFT CABIN FLOOR UPPER SHEET, BETWEEN FRAMES 85 AND 86, +Y279. REPLACED THE UPPER SHHET IAW SRM 51-40-08, AND RD 53-00-00-3, REPAIR 3.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · airframe 25,410 hrs · 18,697 cycles

CORROSION FOUND ON THE AFT CABIN SHEAR PANEL BETWEEN FRAMES 87 AND 88, RBL 508. REPLACED THE SHEAR PANEL IAW RD 53-00-00-3, REPAIR 3.

Part: GUSSET — CORRODED (FRAME 90) · airframe 25,410 hrs · 18,697 cycles

CORROSION ON THE GUSSET AT FRAME 90, RBL 58.4. REPLACED THE GUSSET IAW SRM 51-40-03.

Part: GCU — FAILED (NR 2) · airframe 25,289 hrs · 18,581 cycles

FLT 1869 EN-ROUTE MCI - PHL. THE AIRCRAFT WAS GROUNDED. IDG 2 OFF BUS CAUTION MSG OCCURRED IN FLIGHT COMPLIED WITH QRH MESSAGE REMAINED ON. THE FLIGHT DECLARED AN EMERGENCY AND DIVERTED TO IND WITHOUT FURTHER INCIDENT. MAINTENANCE INSTALLED SERVICEABLE NR 2 MAIN GENERATOR CONTROL UNIT IAW AMM2 24-21-19-000-801-A. OPERATIONAL CHECK IS GOOD AT THIS TIME. AIRCRAFT OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 23,702 hrs · 17,292 cycles

AFTER TAKEOFF LANDING GEAR HANDLE WOULD NOT ALLOW UP SELECTION, LANDING GEAR WOW SYSTEM FAIL MESSAGE APPEARED. EMERGENCY DECLARED AND RETURNED TO DEPARTURE. FLIGHT LANDED WITHOUT INCIDENT. MESSAGE CLEARED AFTER SEVERAL MINUTES. ACCOMPLISHED JOB CARD 43L71132002 AND PERFORMED SUCCESSFUL GEAR EXTENSION AND RETRACTION IAW AMM 32-33-00. THE AIRCRAFT WAS GROUNDED.

Part: CONNECTOR — LOOSE (MLG) · airframe 23,699 hrs · 17,288 cycles

NOSE LANDING GEAR SENSOR FAULTED. EMERGENCY WAS DELCARED, AIRCRAFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. FLIGHT CHANGED EQUIPMENT, PLANNED REDEPARTURE. FOUND P27 OF CONNECTOR J2352 LOOSE IN THE RIGHT GEAR WELL, SECURED. MESSAGES CLEARED IAW AWM 32-62-50. ACCOMPLISHED SATISFACTORY GEAR SWING IAW AMM 32-33-00-710-801-A. NO FAULTS NOTED. AIRCRAFT WAS GROUNDED.

Part: ACCUMULATOR — LOW PRESSURE (ZONE 800) · airframe 22,345 hrs · 16,241 cycles

AIRCRAFT WAS NOT GROUNDED. SYSTEM 1 EMERGENCY ACCUMULATOR, LOW PRESSURE. SERVICED SYSTEM 1 EMERGENCY ACCUMULATOR PER AMM 12-15-05. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: APU — FIRE · airframe 21,917 hrs · 15,902 cycles

DURING TAXI IN, THE APU FAIL EICAS MESSAGE. GROUND PERSONEL REPORTED FIRE FROM APU. REPLACED APU ASSEMBLY. AIRCRAFT WAS GROUNDED.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 21,840 hrs · 15,826 cycles

FLASHLIGHT FOR AFT FLIGHT ATTENDANT IS NOT WORKING. REPLACED BATTERY IN AFT EMERGENCY FLASHLIGHT.

Part: COVER — MISALIGNED (L2 DOOR SLIDE) · airframe 21,435 hrs · 15,513 cycles

COVER ON L2 DOOR SLIDE APPEARS MISALIGNED. MAINTENANCE REPLACED L2 DOOR LINER COVER IAW AMM 25-23-05.

Part: BOTTLE — LOW PRESSURE (L2 DOOR ASSIST) · airframe 21,357 hrs · 15,449 cycles

THE L2 DOOR ASSIST BOTTLE HAS LOW PRESSURE. SERVICED THE L2 DOOR BOTTLE IAW AMM 52-42-00.

Part: BATTERY PACK — INOPERATIVE (ZONE 200 - FUSE)

LEFT FWD OVERWING EMERGENCY LIGHT AND RT MID OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK NR 4 IAW MM 33-50-01 OPS CHECKED GOOD.

Part: WINDOW — SCRATCHED (COCKPIT) · airframe 20,101 hrs · 14,448 cycles

PILOT'S DIRECT VIEW WINDOW HAS EXCESSIVE SCRATCHES. REPLACED PILOT'S DIRECT VIEW WINDOW IAW AMM 56-12-00.

Part: WINDOW — SCRATCHED (COCKPIT) · airframe 20,101 hrs · 14,448 cycles

AIRCRAFT IN BASE MAINTENANCE: CO-PILOT'S DIRECT VIEW WINDOW HAS EXCESSIVE SCRATCHES. REPLACED CO-PILOT'S DIRECT VIEW WINDOW PER AMM 56-12-00.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 20,101 hrs · 14,448 cycles

THE R2 LOWER EMERGENCY EXIT SIGN IS DAMAGED. REPLACED THE SIGN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-00.

Part: SIGN — CRACKED (EMERGENCY LIGHTS) · airframe 20,101 hrs · 14,448 cycles

THE R1 DOOR LOWER EMERGENCY EXIT SIGN IS CRACKED. REPLACED THE SIGN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-00.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 20,101 hrs · 14,448 cycles

FORWARD LAVATORY LOWER EMERGENCY EXIT SIGN IS DAMAGED. INSTALLED THE SIGN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-15-000-801-A AND 33-50-15-400-801-A.

Part: WINDOW — CRAZED (PAX CABIN) · airframe 20,101 hrs · 14,448 cycles

PASSENGER CABIN WINDOW NR 1 LEFT OUTER PANE OUTER SURFACE CRAZED. REPLACED WINDOW OUTER PANE IAW AMM 56-20-00.

Part: HINGE FITTING — WORN (LT AILERON) · airframe 20,101 hrs · 14,448 cycles

LEFT AILERON, LEFT HAND INBOARD HINGE FITTING BETWEEN RIB 24 AND 25 HAS EXCESSIVE PLAY FOUND DURING THE AILERON BLACKLASH CHECK. REPLACED HINGE FITTING IAW AMM 57-61-01.

Part: HINGE FITTING — WORN (LT AILERON) · airframe 20,101 hrs · 14,448 cycles

LEFT AILERON, RIGHT HAND MID HINGE FITTING BETWEEN RIB 24 AND 25 HAS EXCESSIVE PLAY FOUND DURING THE AILERON BLACKLASH CHECK. REPLACED HINGE FITTING IAW AMM 57-61-01.

Part: HINGE FITTING — WORN (LT AILERON) · airframe 20,101 hrs · 14,448 cycles

LEFT AILERON LEFT HAND OUTBOARD INBOARD HINGE FITTING BETWEEN RIB 25 AND 26 HAS EXCESSIVE PLAY FOUND DURING THE AILERON BLACKLASH CHECK. REPLACED HINGE FITTING PER AMM 57-61-01.

Part: HINGE FITTING — WORN (LT AILERON) · airframe 20,101 hrs · 14,448 cycles

LEFT AILERON, RIGHT HAND INBOARD HINGE FITTING BETWEEN RIB 23-23 HAS EXCESSIVE PLAY FOUND DURING THE AIRLIERON BACKLASH CHECK. REPLACED HINGE FITTING IAW AMM 57-51-01.

Part: DOUBLER — CORRODED (FRAME 8 FLOOR) · airframe 20,101 hrs · 14,448 cycles

CORROSION ON COCKPIT LEFT FLOOR DOUBLER AT FRAME 8 AND -Y762. REPAIRED THE DOUBLER IAW EA 261761.

Part: SKIN — WORN (R2 DOOR) · airframe 20,101 hrs · 14,448 cycles

R2 DOOR INNER SKIN WORN BETWEEN BEAM 3 AND 4, JUST BELOW THE AFT LOWER GUSSET. REPLACED DOOR INNER SKIN PER DRAWING 170-69500-411, SRM 51-41-01 & 51-42-03.

Part: BEAM — CORRODED (FRAMES 16-19) · corrosion level 2 · airframe 20,101 hrs · 14,448 cycles

CORROSION ON L1 DOOR CUT OUT LOWER BEAM BETWEEN FRAMES 16 AND 19 AT STRINGER 17 LEFT. REPLACED THE BEAM IAW DRAWING 170-01330-507, SRM 51-43-02,51-43-01,51-41-01 & 51-23-04.

Part: DOUBLER — CORRODED (FRAMES 19-20) · airframe 20,101 hrs · 14,448 cycles

CORROSION ON LOWER FORWARD FUSELAGE INTERNAL ANTENNA DOUBLER BETWEEN FRAMES 19 AND 20 AND BETWEEN STRINGERS 26 - 27R. REPLACED ANTENNA DOUBLER IAW SRM 51-41-02, 51-23-06, AND DRAWING 170-05292-503.

Part: BEAM — CORRODED (FRAMES 16-19) · corrosion level 2 · airframe 20,101 hrs · 14,448 cycles

CORROSION ON R1 DOOR CUT OUT LOWER BEAM BETWEEN FRAMES 16 AND 19, +Y1250. REPLACED THE BEAM IAW SRM 51-40-02, 51-43-03/-04, & DRAWING 170-65480-445.

Part: SEAT TRACK — CORRODED (FRAMES 74-84) · corrosion level 2 · airframe 20,101 hrs · 14,448 cycles

CORROSION AND GOUGES ON LEFT SEAT TRACK CROWN BETWEEN FRAMES 74 AND 84 AT -Y260. REPAIRED THE SEAT TRACK IAW SRM 53-00-10 REPAIR 51 FIGURE 205.

Part: SEAL REST — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 20,101 hrs · 14,448 cycles

CORROSION ON L2 DOOR CUT OUT LOWER CENTER SEAL REST BETWEEN FRAMES 85 AND 86 AT -Y1240. REPLACED SEAL REST IAW SRM 51-40-02 51-41-01 & DRAWING 170-65480-445.

Part: SHEAR TIE — CORRODED (FRAME 72) · airframe 20,101 hrs · 14,448 cycles

CORROSION ON AFT CARGO COMPARTMENT BILGE SHEAR TIE AT FRAME 72 BETWEEN STRINGERS 29 LEFT AND 29 RIGHT. REPLACED THE SHEAR TIE IAW SRM 51-41-02, 51-41-01 & DRAWING 190-25014-417.

Part: SEAT TRACK — CORRODED (FRAMES 12-20) · corrosion level 2 · airframe 20,101 hrs · 14,448 cycles

CORROSION FOUND ON MAIN CABIN RIGHT SEAT TRACK BETWEEN FRAMES 12 AND 20, +Y276. REPLACED THE SEAT TRACK IAW AARD 53-00-00-3 REPAIR 3, SRM 51-40-02, 51-41-01, & 51-41-02.

Part: SEAT TRACK — CORRODED (FRAMES 74-84) · corrosion level 2 · airframe 20,101 hrs · 14,448 cycles

CORROSION AND GOUGES ON RIGHT SEAT TRACK BETWEEN FRAMES 74 AND 84 AT +Y273. REPLACED SEAT TRACK IAW SRM 51-43-01, 51-43-02 & DRAWING 170-65600-407.

Part: SEAL REST — CORRODED (FRAME 27) · airframe 20,101 hrs · 14,448 cycles

CORROSION ON FORWARD CARGO COMPARTMENT DOOR CUT OUT LOWER AFT SEAL REST AT FRAME 27 AND STRINGER 25R. REPLACED THE SEAL REST IAW AMM 20-10-01, SRM 51-23-04 & 51-23-05.

Part: FLOORBEAM — CORRODED (FRAME 14) · corrosion level 2 · airframe 20,101 hrs · 14,448 cycles

DURING MAINTENANCE, CORROSION FOUND ON THE CABIN FLOORBEAM UPPER FLANGE AT FRAME 14, +Y762. REPAIRED THE FLOORBEAM IAW EA 261622.

Part: FITTING — ELONGATED (FRAME 84) · airframe 20,101 hrs · 14,448 cycles

ELONGATED HOLE ON FITTING AT AFT PAX DOOR SURROUND STRUCTURE AT FRAME 84 BETWEEN STRINGERS 5 - 6L. REMOVED AND REPLACED THE FITTING IAW SRM 51-43-03.

Part: FLAP TRACK — WORN (RT WING) · airframe 20,101 hrs · 14,448 cycles

RIGHT WING, NR 1A FLAP TRACK HAS THICKNESS REDUCTION DAMAGE. REPLACED RIGHT WING, FLAP TRACK IAW AMM 57-54-25.

Part: ROLLER — FROZEN (EMERGENCY EXIT) · airframe 20,101 hrs · 14,448 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT EMERGENCY EXIT HATCH FRAME, THE FORWARD DOOR ROLLER IS FROZEN. REPLACED ROLLER IAW AMM 20-10-08.

Part: SEAT TRACK — CORRODED (FRAMES 23-35) · airframe 20,101 hrs · 14,448 cycles

DURING MAINTENANCE, CORROSION AND GOUGES FOUND ON THE SEAT TRACK BETWEEN FRAMES 23 AND 35, +Y1150. REPLACED THE SEAT TRACK IAW SRM 51-43-03 AND DRAWING 170-67030-439.

Part: ROLLER — FROZEN (EMERGENCY EXIT) · airframe 20,101 hrs · 14,448 cycles

AIRCRAFT IN BASE MAINTENANCE: RT EMERGENCY EXIT HATCH FRAME, THE AFT DOOR ROLLER IS FROZEN. REPLACED ROLLER IAW AMM 20-10-08.

Part: FLOORBEAM — CORRODED (FRAME 86) · corrosion level 2 · airframe 20,101 hrs · 14,448 cycles

CORROSION ON FLOORBEAM AT FRAME 86 AND +Y273. REPLACED THE FLOORBEAM IAW AARD 53-00-00-3 REPAIR 3, SRM 51-41-01, SRM 51-43-03, 51-42-03, & 51-12-01.

Part: GUSSET — ELONGATED (FRAME 90) · airframe 20,101 hrs · 14,448 cycles

ELONGATED FASTENER HOLES ON RIGHT HAND INBOARD GUSSET AT FRAME 90 AND Y=-273. REPLACED GUSSET IAW SRM 51-41-02.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 20,101 hrs · 14,448 cycles

AIRCRAFT IN BASE MAINTENANCE, CORROSION ON AFT CABIN RT FLOOR SUPPORT PANEL BETWEEN FRAME 88 AND FRAME 90 AND BETWEEN +Y914 AND +Y1016. REPLACED FLOOR SUPPORT PANEL IAW AARD 53-00-00-3, REPAIR 3 & SRM 51-40-02, 51-42-03, 51-43-03.

Part: UPPER SHEET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,101 hrs · 14,448 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CABIN RT UPPER SHEET BETWEEN FRAME 85 AND FRAME 86 AT +Y273. REPLACED SHEET IAW AARD 53-00-00-3. REPAIR 3 & SRM 51-43-01 & 51-41-01.

Part: GIRT BAR — OBSTRUCTED (ZONE 800) · airframe 20,001 hrs · 14,381 cycles

AIRCRAFT WAS NOT GNDED. AFT RT DOOR DISARM GREEN INDICATION NOT FULLY DISPLAYED. CLEANED DEBRIS FROM GIRT BAR AT THE AFT RT DOOR, GREEN DISARM INDICATION OPERATIONAL CHECKS GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 18,664 hrs · 13,172 cycles

FIRST OFFICERS FIXED WINDSHIELD HAS MULTIPLE CRACKS, 3 TO 9 INCHES IN LENGTH, ALONG THE UPPER EDGE. REPLACED THE WINDSHIELD IAW AMM 56-11-00. ACCOMPLISHED A SATISFACTORY LEAK CHECK.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 18,598 hrs · 13,084 cycles

FLIGHT 2121, FLIGHT ATTENDANTS IN FLIGHT, REPORTED FLOOR LOOSE IN THE CABIN, SINKING AROUND ROWS 9 - 13, COMBINED WITH SQUEAKY NOISES. R & R CABIN AISLE FLOORBOARD 241CLF IAW AMM 53-01-39.

Part: GUIDE — CRACKED (TE FLAP) · airframe 18,459 hrs · 12,898 cycles

LEFT INBD TE FLAP, INBD GUIDE RAIL IS CRACKED. REPLACED GUIDE RAIL IAW AMM 57-54-25.

Part: FAIRING — PUNCTURED (TE FLAP) · airframe 18,459 hrs · 12,898 cycles

LEFT WING INBD FLAP NR 2 FAIRING HAS PUNCTURE ON BOTTOM & THREE GOUGES ON TOP. ACCOMPLISHED A PERMANENT REPAIR IAW EA 253831.

Part: WEDGE — DAMAGED (LT WING TE FLAP) · airframe 18,459 hrs · 12,898 cycles

LEFT WING INNER FLAP DAMAGED AT INBD AFT FLAP OTBD TE WEDGE AREA. ACCOMPLISHED A PERMANENT REPAIR IAW EA 253829.

Part: PUSHROD — DAMAGED (TE FLAP) · airframe 18,459 hrs · 12,898 cycles

LEFT WING INBD TE FLAP PUSH PULL RODS DAMAGED. REPLACED LT WING INBD TE FLAP PUSH PULL RODS.

Part: UNKNOWN — MALFUNCTIONED (BRAKE SYSTEM) · airframe 18,249 hrs · 12,687 cycles

FLIGHT 2123 EN-ROUTE, AFTER TOUCHDOWN, BRAKE LT & RT FAULT ILLUMINATED. BRAKING EFFECTIVENESS REDUCED & OTBD BRAKES ON BOTH SIDES DID NOT WARM UP WHILE INBD HEATED UP, 200 DIFF. ACCOMPLISHED FIM TASK 32-41-00-810-847A TEST PASSED, NO HISTORY PAST 30 DAYS, NO FAULTS FOUND. SYS OK FOR SERVICE.

Part: WINDSHIELD — LEAKING (COCKPIT) · airframe 17,528 hrs · 12,077 cycles

FLIGHT 2157, CAPTAIN DECLARED AN EMERGENCY & DIVERTED DUE TO COMPLETE ELEC FAILURE. FLIGHT WAS AT 12000FT & DESCENDED TO 10,000 CROSSING WHEN LOSS OF ELEC HAPPENED. RAT DEPLOYED. MAINTENANCE FOUND THE PILOT WINDSHIELD LEAKING WATER. WATER HAD INGRESSED ONTO TRAY TABLE THAT HOLDS SPDA MODULES CAUSING FAILURE.

Part: PNEUMATIC SYSTEM — DEPLETED (L2 DOOR) · airframe 17,199 hrs · 11,824 cycles

L2 DOOR BOTTLE READING ZERO PRESS. REPLACED PNEUMATIC ASSEMBLY DIAPHRAGM & SEALS IAW AMM 52-12-52-000 400-801A & 52-12-51-614-801-A.

Part: SHEAR PIN — LOOSE (LT PYLON) · airframe 15,988 hrs · 10,718 cycles

RON, DURING ACCOMPLISHMENT OF EO 5414P124 THE LT PYLON OTBD LOWER LINK FITTING ASSEMBLY WAS FOUND LOOSE. RE-TORQUED & SAFETIED THE LOWER LINK FITTING ASSEMBLY IAW EO 5414P124.

Part: SEAT TRACK — DIRTY (COCKPIT) · airframe 15,932 hrs · 10,676 cycles

WHEN IN FULL AFT POSITION, CAPTAIN'S SEAT DOES NOT LOCK INTO FULL RT OR FULL LT POSITION. WHEN FULL FWD & UNOCCUPIED, SEAT IS VERY DIFFICULT TO MOVE AFT. CLEANED & LUBRICATED CAPTAIN'S SEAT TRACK.

Part: TRIM SWITCH — MISINSTALLED (COCKPIT) · airframe 15,915 hrs · 10,659 cycles

CAPTAIN LEG AP DISCONNETED PITCH WENT FULL DOWN PEDESTAL TRIM WENT INOPERATIVE. THE CAPTAIN HAD TO HOLD BOTH ARMS AROUND YOKE TO MAINTAIN ALTITUDE. ONCE ON THE GND AT THE GATE CAPTAIN TRIM WAS BACKWARDS. FIRST OFFICER NORMAL PEDESTAL NORMAL. FOUND THE CAPTAIN PITCH TRIM SWITCH INSTALLED INCORRECT & WIRE CHAFED, R & R BOTH. THE HS ACE COMPUTER WAS ALSO R & R.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 15,676 hrs · 10,425 cycles

C3 CHECK .2812 INCH LONG CRACK IN RT ELEVATOR UPPER LE SKIN APPROX 31.75 INCHES FROM INBD END & 5.5 INCHES FROM SERVO ACTUATOR CUT OUT YH= -1571.31 +3 INCHES, ER 3. REPAIRED RT ELEVATOR UPPER LE SKIN IAW EA 507484.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 15,676 hrs · 10,425 cycles

C3 CHECK CRACK ON VERTICAL STABILIZER AT RIB 9, ZY-4269.0. REPLACED VERTICAL STABILIZER AT RIB 9, ZY-4269.0 IAW EA 507492.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,676 hrs · 10,425 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FRAME 85 TO FRAME 87, Z-497.8, Y 270. REPAIRED FLOORBEAM AT FRAME 85 TO FRAME 87, Z-497.8, Y 270 IAW SRM 53-23-10.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,676 hrs · 10,425 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON SHEAR PANEL BETWEEN FRAME 87 TO FRAME 88, Z-490 BETWEEN Y300 TO Y1050. REPLACED SHEAR PANEL BETWEEN FRAME 87 TO FRAME 88, Z-490 BETWEEN Y300 TO Y1050 IAW SRM 51-40-02, 51-43-01 & 51-42-01.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,676 hrs · 10,425 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR SHEAR PANEL BETWEEN FRAME 87 TO FRAME 88, Z-490 & BETWEEN -Y270 & Y270. REPLACED CABIN FLOOR SHEAR PANEL BETWEEN FRAME 87 TO FRAME 88, Z-490 & BETWEEN -Y270 & Y270 IAW SRM 51-40-02, 51-42-01, 51-42-01 & 53-23-10.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,676 hrs · 10,425 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON SHEAR PANEL BETWEEN FRAME 84 TO FRAME 85, Z-490, Y1168 4. REPLACED SHEAR PANEL BETWEEN FRAME 84 TO FRAME 85, Z-490, Y1168.4 IAW SRM 51-40-02 & 51-43-02.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,676 hrs · 10,425 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR SHEAR PANEL SPLICE BETWEEN FRAME 87 TO FRAME 88, Z-490, Y1050. REPLACED CABIN FLOOR SHEAR PANEL SPLICE BETWEEN FRAME 87 TO FRAME 88, Z-490, Y1050 IAW SRM 51-40-02 & 51-42-02.

Part: BATTERY — WEAK (CABIN) · airframe 15,676 hrs · 10,425 cycles

C3 CHECK 2 FWD CEILING EMERGENCY LIGHTS FAILED DISCHARGE TEST, STAYED ON LESS THAN 15 MINUTES. REPLACED EMERGENCY BATTERY IN FWD CABIN IAW AMM 33-50-01.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,676 hrs · 10,425 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON SHEAR PANEL AT FRAME 87, Z-490 BETWEEN -Y300 TO -Y1050. REPLACED SHEAR PANEL AT FRAME 87, Z-490 BETWEEN -Y300 TO -Y1050 IAW SRM 51-42-01.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,676 hrs · 10,425 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON FWD RT DOOR SILL AT FRAME 12, STRINGER 17R, Z-490, -Y1250. REPLACED FWD RT DOOR SILL AT FRAME 12, STRINGER 17R, Z-490, -Y1250 IAW SRM 51-41-02, 51-43-04, 51-40-02 & 51-43-03.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,676 hrs · 10,425 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR CROSSBEAM ATTACHED SUPPORT BRACKET AT FRAME 87, Y27.0. REPLACED CABIN FLOOR CROSSBEAM ATTACHED SUPPORT BRACKET IAW SRM 51-43-02 & 51-43-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,676 hrs · 10,425 cycles

C3 CHECK, LEVEL 2 GALVANIC CORROSION ON FLOOR TRACK FLOOR SPLICE AT FRAME 19, Z-19.6, Y10. REPLACED FLOOR TRACK FLOOR SPLICE AT FRAME 19, Z-19.6, Y10 IAW SRM 53-10-10 & 51-41-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,676 hrs · 10,425 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON PAX DOOR CUT OUT LOWER FITTING BETWEEN FRAME 16 TO FRAME 19, Z-490, Y1375. REPLACED PAX DOOR CUT OUT LOWER FITTING IAW SRM 53-40-00 & AMM 20-10-01.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,676 hrs · 10,425 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR DOUBLER AT FRAME 20, Z-490, Y32. REPLACED CABIN FLOOR DOUBLER AT FRAME 20, Z-490, Y32 IAW SRM 51-43-04.

Part: UPPER SHEET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,676 hrs · 10,425 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN FLOORBEAM UPPER SHEET BETWEEN FRAME 85 TO FRAME 86, Y 250. REPLACED CABIN FLOORBEAM UPPER SHEET BETWEEN FRAME 85 TO FRAME 86, Y 250 IAW SRM 51-43-01 & 51-41-01.

Part: RIB — CRACKED (LT WING) · airframe 15,676 hrs · 10,425 cycles

C3 CHECK LT WING RIB NR 9 CRACKED AT Z-29.6, Y193.6. REPLACED LT WING RIB 9 AT Z-29.6, Y193.6 IAW SRM 51-43-02 & 51-41-01, STEP 4 & 5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,676 hrs · 10,425 cycles

C3 CHECK, LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FRAME 12 TO FRAME 20, Z-940, Y304.8. REPLACED SEAT TRACK BETWEEN FRAME 12 TO FRAME 20, Z-940, Y304.8 IAW SRM 51-41-01, 51-43-03, 51-43-04 & 51-45-00.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 15,676 hrs · 10,425 cycles

C3 CHECK CRACK ON COCKPIT FLOOR CONSOLE SUPPORT ANGLE AT FRAME 12, Z-490, LBL 35. REPLACED COCKPIT FLOOR CONSOLE SUPPORT ANGLE AT FRAME 12, Z-490, LBL 35 IAW SRM 51-41-01, P1-2.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,676 hrs · 10,425 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR STRUCTURE GUSSET AT FRAME 90, Z-490, Y100. REPLACED GUSSET AT FRAME 90, Z-490, Y100 IAW SRM 51-43-03 & 51-43-01.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 15,676 hrs · 10,425 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR SKIN PANEL AT FRAME 84, Z-490 BETWEEN Y=0 TO Y46. REPLACED CABIN FLOOR SKIN PANEL AT FRAME 84, Z-490 BETWEEN Y=0 TO Y46 IAW SRM 51-40-03, 51-41-02 & 51-43-02.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,676 hrs · 10,425 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR SUPPORT GUSSET AT FRAME 20, Z-490, Y500. REPLACED CABIN FLOOR SUPPORT GUSSET AT FRAME 20, Z-490, Y500 IAW SRM 51-41-02 P 1.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,676 hrs · 10,425 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR SILL AT FRAME 12, STRINGER 17L, Z-490, Y1450. REPLACED CABIN FLOOR SILL AT FRAME 12, STRINGER 17L, Z-490, Y1450 IAW SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,676 hrs · 10,425 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON CABIN FLOOR ANGLE AT FRAME 19, Z-490, Y250. REPLACED CABIN FLOOR ANGLE AT FRAME 19, Z-490, Y250 IAW SRM 51-40-02 STEP 4, FIG 1.

Part: DOUBLER — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 15,676 hrs · 10,425 cycles

C3 CHECK LEVEL 2 GALVANIC CORROSION ON FWD CARGO DOOR DOUBLER BETWEEN FRAME 24 TO FRAME 25 & BETWEEN STRINGER 25R TO STRINGER 26R, Z-1559, -Y300. REPLACED FWD CARGO DOOR DOUBLER IAW SRM 51-40-03.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,676 hrs · 10,425 cycles

C3 CHECK, LEVEL 2 GALVANIC CORROSION ON FWD CARGO LOWER SURROUND BAG DOUBLER BETWEEN FRAME 26 TO FRAME 27, Z-1515, -Y300. REPLACED FWD CARGO LOWER SURROUND BAG DOUBLER BETWEEN FRAME 26 TO FRAME 27, Z-1515, -Y300 IAW SRM 51-40-02 & 51-43-05.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 15,676 hrs · 10,425 cycles

C3 CHECK LEVEL 2 INTERGRANULAR CORROSION ON FWD CARGO DOOR SILL BETWEEN FRAME 24 TO FRAME 27, STRINGER 26R, Z-1559, Y450. REPLACED FWD CARGO DOOR FWD CARGO DOOR SILL BETWEEN FRAME 24 TO FRAME 27, STRINGER 26R, Z-1559, Y450 IAW SRM 51-40-03P2 & 51-41-01.

Part: LIGHT — MISSING (CABIN) · airframe 14,333 hrs · 9,444 cycles

SECTION OF EMERGENCY LIGHT MISSING. REPLACED MISSING SECTIONS OF EMERGENCY LIGHTS.

Part: SENSOR — FAILED (SLAT FLAPS) · airframe 14,147 hrs · 9,320 cycles

ON APPROACH, THE SLATS WOULD NOT WORK AND THE FLAPS ONLY DEPLOYED TO 2 DEGREES. THE FLIGHT CREW HAD MULTIPLE ALERT MESSAGES SO THEY DECLARED AN EMERGENCY. DUE TO THE SLAT/FLAP FAIL THE CREW LANDED IAW QRH PROCEDURES. THE LANDING WAS UNEVENTFUL AND TAXIED TO GATE WITH NO ISSUES.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 14,129 hrs · 9,310 cycles

FORWARD F/A FLASHLIGHT INOPERATIVE. MX REPLACED BATTERY.

Part: WARNING MESSAGE — FALSE INDICATION (SLAT FLAPS) · airframe 14,068 hrs · 9,276 cycles

THE CAPTAIN REPORTED A FLAP POSITION PROBLEM, SLAT FAILED IN UP POSITITON DID NOT EXTEND. EMERGENCY EQUIPMENT REQUESTED TO RESPOND ON LANDING, THE FLIGHT LANDED WITHOUT INCIDENT. MX PERFORMED FIM TASK AND NO FAULTS NOTED AT THIS TIME. FUNCTIONAL CHECK OF SLAT/FLAP ON GROUND OPS CHECK NORMAL.

Part: HEAT EXCHANGER — CONTAMINATED (ZONE 100) · airframe 13,581 hrs · 8,939 cycles

MUSTY DOOR DETECTED DURING POWER ADVANCES. MX TROUBLSHOT CABIN AIR QUALITY AS REQUIRED. RAN ENGINES (APU) PACKS AT IDLE AND 80 PERCENT N2. NO AIR QUALITY DEGRADATION NOTED. ACCOMPLISHED DUAL HEAT EXCHANGERS CLEAN-OUT DUE TO RT PACK COFFEE SATURATION. OPS TEST AND AIR QUALITY CHECK GOOD. NO PREVIOUS HISTORY. ACFT OK FOR CONTINUED SERVICE.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 13,260 hrs · 8,701 cycles

LUMINESCENT STRIP MISSING ON FLOOR BETWEEN ROWS 1 & 2 (RIGHT). MAINTENANCE INSTALLED NEW GLOW STRIP AS REQUIRED.

Part: BOTTLE — LOW PRESSURE (R2 DOOR)

ATL - THE R2 DOOR ASSIST BOTTLE IS LOW. MAINTENANCE SERVICED THE R2 DOOR ASSIST BOTTLE PRESSURE PER AMM 52-12-51.

Part: ACCUMULATOR — LOW PRESSURE (R1 DOOR)

ATL - THE R1 DOOR EMERGENCY ACCUMULATOR IS LOW. MAINTENANCE SERVICED THE R1 DOOR EMERGENCY ACCUMULATOR PER MM 52-12-51-614-801A.

Part: SENSOR — OPEN (LE SLAT)

FLIGHT 1944, ON APPROACH TO CLT THE FLAPS FAILED TO EXTEND WHEN COMMANDED. THE CAPTAIN DECLARED AN EMERGENCY, THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RIGHT OUTBOARD SLAT SKEW SENSOR S0162 OPEN. MAINTENANCE REMOVED AND REPLACED THE SKEW SENSOR.

Part: SENSOR — FAULTY (LE SLAT)

SLAT FAIL ON FLAP EXTENSION, FAILED TO RESET WHEN CYCLED TO 0 THEN BACK TO 1. CREW DECLARED AN EMERGENCY LANDING. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED WIRING FROM BOTH RIGHT OUTBOARD SKEW SENSOR TO SF-ACE 1. REPLACED RT OUTBOARD SKEW SENSOR 3/4 AS PRECAUTIONARY. NO FAULTS NOTED.

Part: WIRE HARNESS — SHORTED (ZONE 600)

FLIGHT 1615, EWR-CLT - THE CREW RECEIVED A "SLAT FAIL" EICAS MESSAGE ON APPROACH TO CLT. THE CREW DECLARED AN EMERGENCY AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A SHORT IN THE HARNESS WIRE, REMOVED AND REPLACED THE HARNESS.

Part: BOLT — MISSING (ZONE 100)

FLIGHT 1171, BWI-CLT - THE FLIGHT REPORTED A PRESSURIZATION PROBLEM AFTER TAKEOFF FROM BWI. THE CREW ADVISED, HAD A CABIN ALT HIGH LIGHT. MAINTENANCE PERFORMED A SATISFACTORY CHECK OF THE PRESSURE CONTROL SYSTEM AND THE AIRCRAFT RETURNED TO SERVICE. AFTER TAKEOFF A SECOND TIME BOTH PACKS WERE LOST MOMENTARILY AND RETURNED TO NORMAL OPERATION. THE CREW RETURNED TO BWI A SECOND TIME. MAINTENANCE FOUND BOLT MISSING FROM RIGHT RAM DUCT SUPPORT BRACKET. ALSO REPLACED THE AIR CONDITION CHECK VALVE AND RECIRCULATION FILTERS.

Part: CYLINDER — LOW PRESSURE (L2 DOR)

ATL - L-2 DOOR CYLINDER/ACCUMULATOR LOW. MAINTENANCE SERVICED THE L-2 DOOR CYLINDER.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

PHL - THE FORWARD FLIGHT ATTENDANT FLASHLIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN THE FLASHLIGHT.