N954UW

Part: PNEUMATIC SYSTEM — LEAKING (SERVICE DOOR) · airframe 26,056 hrs · 21,682 cycles

AIRCRAFT IN BASE MAINTENANCE - AFT SERVICE DOOR, UPON SERVICING ATTEMPT OF DOOR PNEUMATIC ASSEMBLY, FOUND IT TO BE LEAKING AND UNABLE TO HOLD A PRE-CHARGE. REMOVED AND REPLACED AFT SERVICE DOOR PNEUMATIC ASSEMBLY PER E190 AMM 52-42-51. ADJUSTMENT CHECK GOOD, PRESSURE AND LEAK CHECK GOOD.

Part: STOP FITTING — WORN (FUSELAGE) · airframe 26,056 hrs · 21,682 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT SERVICE DOOR CUTOUT HAS 5 DOOR FITTING STOP PADS (1, 3, , 4, 5 AND 8) WORN. REPLACED 5 DOOR FITTING STOP PADS PER AMM 53-23-25.

Part: SERVICE DOOR — OUT OF ADJUST (ZONE 800) · airframe 26,056 hrs · 21,682 cycles

AIRCRAFT IN BASE MAINTENANCE - AFT SERVICE DOOR FAIL TO OPEN DURING SLIDE DEPLOYMENT, FORWARD DOORSTOPS HITTING SEAL DEPRESSOR. FOUND AFT SERVICE DOOR OUT OF RIG, ADJUSTED DOOR PER E190 AMM 52-42-00. ADJUSTMENT CHECKS GOOD.

Part: WINDOW — DAMAGED (COCKPIT) · airframe 26,056 hrs · 21,682 cycles

AIRCRAFT IN BASE MAINTENANCE: CO-PILOTS DIRECT-VISION (SLIDING) WINDOW HAS CRAZING, SCRATCHES,AND DELAMINATION THROUGHOUT WINDOW. REPLACED WINDOW PER AMM 56-12-00.

Part: STOP FITTING — WORN (FUSELAGE) · airframe 26,056 hrs · 21,682 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT PASSENGER DOOR CUTOUT HAS 4 AFT LOWER STOP PADS WORN. REPLACED 4 DOOR STOP PADS PER AMM 53-73-21.

Part: ATTACH BOLT — LOOSE (GIRT BAR) · airframe 26,056 hrs · 21,682 cycles

AIRCRAFT IN BASE MAINTENANCE - AFT SERVICE DOOR, GIRT BAR AFT BOLT AND LOCKNUT LOOSE. MARKED RJ-051. INSTALLED PROPERLY AND TORQUED AFT SERVICE DOOR GIRT BAR AFT HOLD AND LOCKNUT PER E190 AMM 52-42-41-400-801-A.

Part: SLAT TRACK — WORN (LE SLAT) · airframe 26,056 hrs · 21,682 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT WING LEADING EDGE SLAT TRACK #6 WORN / WIDTH REDUCTION ON THE INBOARD AND OUTBOARD SIDE. REPLACED SLAT TRACK PER AMM 57-47-00.

Part: FITTING — WORN (FUSELAGE) · airframe 26,056 hrs · 21,682 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CARGO DOOR CUT OUT #4 LATCH FITTING FATIGUE PIN IS WORN. REPLACED LATCH FITTING PER AMM 53-23-29.

Part: FITTING — WORN (FUSELAGE) · airframe 26,056 hrs · 21,682 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CARGO DOOR CUT OUT #1 LATCH FITTING FATIGUE PIN IS WORN. REPLACED LATCH FITTING PER AMM 53-23-29.

Part: GAUGE — CONTAMINATED (PAX DOOR) · airframe 26,056 hrs · 21,682 cycles

AIRCRAFT IN BASE MAINTENANCE - FORWARD PASSENGER DOOR PNEUMATIC ASSEMBLY PRESSURE GAUGE SHOWS NO FLUID IN THE GAUGE PR032. REMOVED AND REPLACED PRESSURE GAUGE AT FWD PASSENGER DOOR PNEUMATIC ASSEMBLY PER CMM 52-11-51, CHARGE AND LEAK CHECK GOOD, AREA FREE OF FOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 26,056 hrs · 21,682 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON MAIN CABIN FLOOR SILL BETWEEN FR 17 AND FR 18 AT RBL 42. REPLACED FLOOR SILL PER AARD 53-00-00-3 REPAIR 3.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 26,056 hrs · 21,682 cycles

AIRCRAFT WAS GROUNDED: CORROSION ON AFT MAIN CABIN SUPPORT BRACKET AT FR 86 AND Y= +710. REPLACED SUPPORT BRACKET PER SRM 51-75-16.

Part: FASTENER — RUSTED (SERVICE DOOR) · airframe 26,056 hrs · 21,682 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT SERVICE DOOR EMERGENCY EVACUATION SLIDE CLEVIS BRACKET HARDWARE RUSTED. REPLACED CLEVIS BRACKET HARDWARE PER AMM 20-10-01.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · airframe 26,056 hrs · 21,682 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT MAIN CABIN RIGHT SHEAR PANEL BETWEEN FR 87 AND FR 88 AT Y=+610. REPLACED SHEAR PANEL PER AARD 53-00-00-3 AND SRM 51-40-02.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 26,056 hrs · 21,682 cycles

AIRCRAFT IN BASE VISIT: R2 DOOR EMERGENCY PNEUMATIC ASSY, PRESSURE BELOW MINIMUM. PERFORMED R-2 DOOR EMERGENCY PNEUMATIC ASSY SERVICING IAW E190 AMM 52-42-51-614-801-A.

Part: SENSOR — UNSERVICEABLE (LT WING) · airframe 24,516 hrs · 20,280 cycles

AFTER TAKEOFF, SLAT FAIL EICAS MESSAGE WAS INDICATED FOLLOWED BY SHAKER ANTICIPATED AND AOA LIMIT FAIL. REPLACED LT SLAT 2/3 SKEW SENSOR DUE TO LOW INSULATION RESISTANCE, LESS THAN .01 MILLIOHMS TO GND, IAW AMM 27-83-01-401. THE AIRCRAFT WAS GROUNDED.

Part: SENSOR — MALFUNCTIONED (LT WING) · airframe 24,516 hrs · 20,280 cycles

AFTER TAKEOFF, SLAT FAIL EICAS MESSAGE WAS INDICATED FOLLOWED BY SHAKER ANTICIPATED AND AOA LIMIT FAIL. REPLACED LT SLAT 2/3 SKEW SENSOR DUE TO LOW INSULATION RESISTANCE, LESS THAN .01 MILLIOHMS TO GND, IAW AMM 27-83-01-401. THE AIRCRAFT WAS GROUNDED.

Part: DAMPENER — LOW PRESSURE (R1 DOOR) · airframe 24,501 hrs · 20,268 cycles

AIRCRAFT WAS NOT GROUNDED: R1 ENTRY DOOR EMERGENCY ACTUATOR/DAMPENER PRESSURE WAS BELOW LIMITS. MAINTENANCE SERVICED PNEUMATIC ASSEMBLY TO PROPER PRESSURE PER AMM 52-41-51 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: SENSOR — FAULTED (LT WING SLAT) · airframe 24,474 hrs · 20,249 cycles

SLAT FAIL INDICATION. EMERGENCY DECLARED AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED THE LT SLAT 2/3, AND 3/4 SKEW SENSORS DUE TO LOW INSULATION RESISTANCE IAW AMM 27-83-01-401. ALSO REPLACED THE LT SLAT 2/3 SLAT HARNESS IAW AMM 27-83-07-401. OPS TESTED OK IAW AMM 27-80-00-501.

Part: MODULE — FAULTED · airframe 23,619 hrs · 19,568 cycles

DURING DECENT, THE FLIGHT CREW DECLARED AN EMERGENCY DUE TO SPDA FAILURE AND BRAKE CONTROL FAULT MESSAGES INFLIGHT. FLIGHT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED SPDA 2 POWER MODULE FROM SLOT 5 PER AMM 24-61-13.

Part: LINKAGE — LACK OF LUBE (L2 DOOR) · airframe 21,508 hrs · 17,949 cycles

L2 DOOR STUCK IN ARMED POSITION. LUBRICATED DOOR LOCKING LINKAGE.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 21,210 hrs · 17,698 cycles

ADVISORY MESSAGE EMERGENCY BATTERY FAULT, SHOWS ON EICAS. RESET EMERGENCY LIGHT POWER UNIT. AIRCRAFT WAS GROUNDED.

Part: SKIN — CHAFED (RT WING) · airframe 21,205 hrs · 17,696 cycles

CHAFED RIGHT WING SPAR NR 1, FIXED LEADING EDGE EXTERNAL SKIN BETWEEN SLATS NR 3 AND 4. REPAIRED SKIN IAW EA 272504.

Part: SKIN — CHAFED (RT WING) · airframe 21,205 hrs · 17,696 cycles

CHAFED RIGHT WING SPAR NR 1, FIXED LEADING EDGE EXTERNAL SKIN BETWEEN SLATS NR 3 AND 4. REPAIRED THE SKIN IAW EA 272504.

Part: RIB — CRACKED (RT WING) · airframe 21,205 hrs · 17,696 cycles

CRACK ON RIGHT WING SPAR NR 1 LEADING EDGE RIB 17. REPLACED THE RIB IAW DRAWING 190-31005-409.

Part: LENS — CRACKED (CABIN) · airframe 21,205 hrs · 17,696 cycles

AIRCRAFT WAS GROUNDED. MAIN CABIN R2 DOOR SURROUND PANEL 252HRW EXIT SIGN IS CRACKED. REPLACED EMERGENCY EXIT IDENTIFIER SIGN.

Part: FLAP TRACK — WORN (LT WING) · airframe 21,205 hrs · 17,696 cycles

THICKNESS AND WIDTH REDUCTION ON LEFT WING INBORAD FLAP TRACK RAIL 2A AT -Y3025.80. REPLACED FLAP TRACK IAW AMM 27-51-08 SUB TASK 420-035-A.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 21,205 hrs · 17,969 cycles

MAIN CABIN FORWARD LEFT CLOSET EXIT LIGHT LENS COVER IS CRACKED. REPLACED THE LENS. AIRCRAFT WAS GROUNDED.

Part: SEAT TRACK — ELONGATED (FRAMES 62-63) · airframe 21,205 hrs · 17,696 cycles

ELONGATED HOLE ON MAIN CABIN LEFT INBD SEAT TRACK -Y276, BETWEEN FRAMES 62 AND 63. REPAIRED THE SEAT TRACK IAW SRM 53-00-10, REPAIR 51, FIGURE 205.

Part: FINGER DOUBLER — CORRODED (FRAMES 24-27) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON FORWARD CARGO FINGER DOUBLER AT STRINGER 26R, BETWEEN FRAMES 24 AND 27. REPLACED THE FINGER DOUBLER IAW SRM 51-40-02.

Part: SUPPORT FITTING — CORRODED (FRAME 84) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON AFT MAIN CABIN DIVIDER SUPPORT FITTING AT -Y335 AND FRAME 84. REPLACED SUPPORT FITTING IAW DRAWING 170-65600-441.

Part: FLOOR SUPPORT — DAMAGED (FRAME 62) · airframe 21,205 hrs · 17,696 cycles

ELONGATED HOLE ON MAIN CABIN FLOOR SUPPORT AT -Y1200 AND FRAME 62. REPLACED THE FLOOR SUPPORT IAW DRAWING 190-25000-433.

Part: SEAT TRACK — CORRODED (FRAME 84) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON LEFT AFT MAIN CABIN SEAT TRACK AT -Y280 AND FRAME 84. REPAIRED THE SEAT TRACK IAW SRM 53-00-10, REPAIR 51, FIGURE 205.

Part: SEAT TRACK — CORRODED (FRAME 84) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON RIGHT SIDE AFT MAIN CABIN SEAT TRACK AT Y300 AND FRAME 84. REPAIRED THE SEAT TRACK IAW SRM 53-00-10, REPAIR 51, AND DRAWING 170-65600-443.

Part: SEAT TRACK — CORRODED (FRAMES 58-74) · airframe 21,205 hrs · 17,696 cycles

CORROSION ON RIGHT LATERAL SEAT TRACK AT Y1300, BETWEEN FRAMES 58 AND 74. REPLACED THE SEAT TRACK IAW DRAWING 190-25000-437.

Part: DOUBLER — CORRODED (FRAMES 15-16) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR DOUBLER AT -Y320, BETWEEN FRAMES 15 AND 16. REPLACED THE DOUBLER IAW 53-00-00-3, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-13) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT BETWEEN FRAMES 12 AND 13, -Y330 AND -Y480. REPLACED FLOOR SUPPORT IAW DRAWING 170-00822-5031.

Part: SEAT TRACK — CORRODED (FRAMES 14-20) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON FORWARD MAIN CABIN LEFT SEAT TRACK AT -Y270, BETWEEN FRAMES 14 TO 20. REPLACED THE SEAT TRACK IAW 53-00-00-3, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-16) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON FORWARD FUSELAGE LEFT FLOOR SUPPORT AT -Y1220, BETWEEN FRAMES 12 AND 16. REPLACED THE FLOOR SUPPORT IAW 53-00-00-3, REPAIR 3.

Part: DOUBLER — CORRODED (FRAMES 19-20) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON FORWARD FUSELAGE MAIN CABIN LEFT FLOOR DOUBLER BETWEEN -Y320 AND -Y640, BETWEEN FRAMES 19 AND 20. REPLACED THE FLOOR DOUBLER IAW SRM 51-41-02, AND 51-43-04.

Part: BEAM — CORRODED (FRAMES 17-18) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON FORWARD MAIN CABIN SILL BEAM AT L1 DOOR CUTOUT AT -Y1330, BETWEEN FRAMES 17 TO 18. REPLACED SILL BEAM IAW DRAWING 170-03719-005 AND 170-01330-507.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-18) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON FORWARD MAIN CABIN RIGHT FLOOR SUPPORT AT Y330, BETWEEN FRAMES 17 AND 18. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-00822-413.

Part: SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON AFT MAIN CABIN FLOOR SUPPORT AT FRAME 84, BETWEEN Y340 AND Y1160. REPLACED FLOOR SUPPORT AIW DRAWING 190-65140-801.

Part: SEAT TRACK — CORRODED (FRAMES 16-17) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON FORWARD MAIN CABIN RIGHT SEAT TRACK AT Y270, BETWEEN FRAMES 16 AND 17. REPLACED THE SEAT TRACK IAW 53-00-00-3, SRM 51-41-01, 51-41-02, 51-43-03, AND 51-43-04.

Part: FLOOR SUPPORT — CORRODED (FRAME 89) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON AFT MAIN CABIN FLOOR SUPPORT AT FRAME 89 AND Y279. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-66000-463.

Part: FLOOR SUPPORT — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON AFT MAIN CABIN FLOOR SUPPORT SPLICE AT -Y1016, BETWEEN FRAMES 87 AND 88. REPLACED THE FLOOR SUPPORT SPLICE IAW DRAWING 190-66000-455, AND 53-00-00-3, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON AFT MAIN CABIN LEFT FLOOR SUPPORT AT -Y980 AND FRAME 84. REPLACED THE FLOOR SUPPORT DRAWING 170-65600-441.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON FORWARD MAIN CABIN LEFT FLOOR SUPPORT AT -Y1150 AND FRAME 16. REPLACED FLOOR SUPPORT IAW DRAWING 170-21768-407 AND SRM 51-43-03.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-20) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT BETWEEN FRAMES 17 AND 20, BETWEEN Y1060 AND Y1130. REPLACED THE FLOOR SUPPORT IAW 53-00-00-3, REPAIR 3.

Part: SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON AFT MAIN CABIN LEFT SUPPORT AT -Y1184 AND FRAME 84. REPLACED THE SUPPORT IAW DRAWING 170-66000-441.

Part: BEAM — CORRODED (FRAME 87) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON AFT MAIN CABIN LEFT SIDE LONGITUDNAL BEAM AT FRAME 87 AND -Y279. REPAIRED THE LONGITUDINAL BEAM IAW SRM 53-23-10, REPAIR 51.

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON AFT MAIN CABIN FLOOR STRUCTURE LEFT SHEAR PANEL AT -Y920, BETWEEN FRAMES 87 AND 88. REPLACED THE SHEAR PANEL IAW 53-00-00-3, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON FORWARD MAIN CABIN RIGHT FLOOR SUPPORT AT Y980, BETWEEN FRAMES 12 AND 14. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-00822-503.

Part: FLOOR SUPPORT — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON AFT MAIN CABIN FLOOR SUPPORT RIGHT SPLICE AT Y1016 BETWEEN FRAMES 87 AND 88. REPLACED FLOOR SUPPORT SPLICE IAW 53-00-00-3, REPAIR 3.

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON AFT MAIN CABIN RIGHT SHEAR PANEL BETWEEN FRAMES 87 AND 88, BETWEEN Y610 - Y940. REPLACED THE SHEAR PANEL IAW53-00-00-3, REPAIR 3.

Part: FLOORBEAM — CORRODED (FRAME 14) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON RIGHT HAND FORWARD MAIN CABIN FLOORBEAM ANGLE AT FRAME 14 AND Y720. REPLACED FLOORBEAM ANGLE IAW DWG 170-00822-503.

Part: FLOOR SUPPORT — CORRODED (FRAME 89) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON AFT MAIN CABIN FLOOR SUPPORT AT FRAME 89 AND Y914. REPLACEDTHE FLOOR SUPPORT IAW 53-00-00-3 REPAIR 3.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 21,205 hrs · 17,696 cycles

CORROSION ON AFT MAIN CABIN FLOOR STRUCTURE RIGHT GUSSET AT FRAME 90 AND Y610. REPLACED THE GUSSET IAW DRAWING 170-60001-823.

Part: IDG — LEAKING (NR 1) · airframe 20,342 hrs · 17,076 cycles

ABORTED TAKEOFF AT 70 KNOTS DUE TO NR 1 IDG OIL FAULT INDICATION. BRAKE TEMPS NORMAL. NO ASSOCIATED MESSAGES. MAINTENANCE FOUND THE NR 1 ENGINE IDG OUT OF OIL AND REPLACED IT. AIRCRAFT WAS GROUNDED.

Part: SIGHT GLASS — LEAKING (IDG) · airframe 20,283 hrs · 17,030 cycles

DURING TAXI OUT, AN ODOR FROM AIRCRAFT LIKE DIRTY SOCKS, VERY STRONG. TURNED THE PACKS AND BLEEDS OFF AND THE ODOR WENT AWAY. AIRCRAFT WAS GROUNDED. MAINTENANCE PERFORMED JOB CARD 43L00021001 AND FOUND THE NR 1 ENGINE IDG OIL SIGHT GLASS LEAKING. TIGHTENED FASTENERS, CLEANED AREA, AND RAN ENGINE. ACCOMPLISHED SATISFACTORY LEAK AND OPS CHECK.

Part: FIRE DETECTOR — FALSE INDICATION (NR 2 NACELLE)

ENG 2 FIRE INDICATION AT FL 300, SHUTDOWN ENG 2 AND FIRED BOTH BOTTLES. WITH ENG 2 FIRE STILL INDICATING, DECLARED AN EMERGENCY AND DIVERTED TO GSO. ENG 2 FIRE CONTINUED TO INDICATE EVEN AFTER LANDING. AFTER STOPPING ON RUNWAY, ARFF INSPECTED AIRCRAFT AND FOUND NO FIRE. SINGLE ENGINE TIME WAS 20 MINUTES. PER FIM TASK 26-11-0028UT1. REMOVED & REPLACED ENGINE 2 RT FWD FIRE DET/LOOP PER AMM 26-11-01/400. PER MOC R&R UPPER & LOWER CORE DETECTORS LOOPS PER AMM 26-11-01/400. RAN ENGINE FOR 10 MINUTES. NO FAULTS NOTED. THE AIRCRAFT WAS GROUNDED.

Part: ACM — SMOKE (RIGHT) · airframe 19,279 hrs · 16,225 cycles

AFTER NR 2 ENGINE START A SULFUR ODOR AND SMOKE IN CABIN WAS REPORTED. ACCOMPANIED BY GRINDING NOISE. AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE RIGHT AIR CYCLE MACHINE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 21-51-05-000-801-A.

Part: LENS — DETACHED (EXIT SIGN) · airframe 18,525 hrs · 15,536 cycles

AIRCRAFT WAS NOT GNDED. EXIT SIGN LENS MID CABIN DETACHED. REPLACED EXIT SIGN IAW AMM 33-50-19 400.

Part: UNKNOWN — ODOR · airframe 18,349 hrs · 15,394 cycles

RETURNED TO PHL, ACFT WAS GNDED. DURING TAKEOFF A STRONG ODOR OF OIL, MUSTY DIRTY SOCKS BEGAN, IT CONTINUED FOR SEVERAL MINUTES. THEN SUBSIDED. ODOR WAS STRONGER TOWARD THE FRONT OF THE ACFT. THE FLIGHT CREW DECLARED AN EMER & RETURNED WHERE THE ACFT LANDED SAFELY. AFTER LANDING THE FLIGHT ATTENDANT REPORTED THE ODOR AGAIN. ACCOMPLISHED AIR QUALITY TROUBLESHOOTING TASK CARDS, JC 43L000722001, 43L00021001, & 43L00036002. GND RAN BOTH ENGS & APU TO HIGH POWER & ALL CHECKS WERE NORMAL. IT WAS NOTED THAT DURING THE PREVIOUS RON, BOTH ENGS HAD A COMPRESSOR WAS ACCOMPLISHED.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

MAIN CABIN AFT LEFT FLIGHT ATTENDANT SEAT FLASHLIGHT BATTERY IS LOW. R & R MAIN CABIN AFT LEFT FLIGHT ATTENDANT SEAT FLASHLIGHT BATTERY IAW AMM 33-51-01.

Part: DAMPER — CORRODED (FWD SERVICE DOOR)

CORRODED FWD SERVICE DOOR STEEL DAMPER. R & R THE DOOR DAMPER IAW AMM 52-41-27-020-002-A & AMM 52-41-27-420-003-A. OPS CHECKED GOOD IAW AMM 52-41-27-710-801-A.

Part: ROD — CHAFED (L2 DOOR)

L2 DOOR ARMING LEVER ROD CHAFED DOT NR 33-5. R & R L2 DOOR ARMING LEVER ROD IAW AMM 52-12-40-020-002-A & AMM 52-12-40-420-005-A. NO ADJUSTMENT DISTURBED.

Part: PANEL — CORRODED (FUSELAGE) · airframe 16,810 hrs · 14,050 cycles

C3 CHECK, CORROSION ON SHEAR PANEL BETWEEN FRAME 86 & FRAME 87, +Y304.8 & +Y1041.4. REPLACED SHEAR PANEL IAW SRM 51-42-01.

Part: PANEL — CORRODED (FUSELAGE) · airframe 16,810 hrs · 14,050 cycles

C3 CHECK, CORROSION ON CENTER SHEAR PANEL BETWEEN FRAME 86 & FRAME 87, +Y222.3 & -Y222.3. REPLACED SHEAR PANEL IAW SRM 51-42-01.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 16,810 hrs · 14,050 cycles

C3 CHECK, CORROSION ON GUSSET AT FRAME 90 BETWEEN +Y457.2 & +Y698.5. REPLACED GUSSET IAW SRM 51-41-02.

Part: SLIDE — DAMAGED (L2 DOOR) · airframe 16,810 hrs · 14,050 cycles

C3 CHECK, L2 DOOR EMER EVACUATION SLIDE SAFETY THREAD IS BROKEN & JUNCTION LOOP IS FRAYED NEXT TO RELEASE PIN. REPLACED L2 DOOR EMER EVACUATION SLIDE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 16,371 hrs · 13,681 cycles

FLIGHT 9010 EN-ROUTE, DURING APPROACH, BLUE BRK LT OR RT FAULT ILLUMINATED WHILE LOWERING THE LG. THE GEAR WAS RETRACTED & THE APPROACH WAS ABANDONED. THE FLIGHT DECLARED AN EMER & DIVERTED FOR A LONGER RUNWAY. WHILE LANDING, THE GEAR WAS AGAIN LOWERED & MSG EXTINGUISHED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MX WAS UNABLE TO DUPLICATE THE FAULT. AS A PRECAUTION, REPLACED THE BCM 1.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 16,048 hrs · 13,388 cycles

WINDOW IS MISSING SEAL IN THREE PLACES, SEAL EROSION. GLASS HAS TWELVE CRACKS UPPER WINDSHIELD AREA. REPLACED WINDSHIELD IAW AMM 56-11-11-0401-001-A.

Part: UNKNOWN — ODOR (CABIN) · airframe 15,586 hrs · 13,034 cycles

LEAD FLIGHT ATTENDANT NOTIFIED CAPTAIN ON INITIAL CLIMB OUT OF A, STRONG ODOR, MID CABIN TO AFT FLIGHT ATTENDANT GALLEY AREA. NO ABNORMAL INDICATIONS NOTED. WE DIVERTED & FLIGHT ATTENDANT HAD BURNING SENSATION. TROUBLESHOOTING CABIN AIR QUALITY, UNABLE TO DUPLICATE REMARKS, NO CABIN ODOR NOTED AT THIS TIME. RUN BOTH ENGS & APU. PERFORMED OPERATIONAL CHECK OF LT & RT PACK AT HOT & COLD TEMP SETTINGS. NO ODOR NOTED.

Part: CHAIN — OUT OF ADJUST (PAX DOOR) · airframe 14,608 hrs · 12,048 cycles

FORWARD DOOR WILL NOT CLOSE PROPERLY. ACCOMPLISHED FWD PAX DOOR ARM ASSEMBLY INSPECTION. FOUND LOWER ARM MECHANISM ASSEMBLY CHAIN ADJUSTER LOOSE. ADJUSTED LOWER ARM MECHANISM CHAIN. FWD PAX DOOR NOW OPERATES NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 14,499 hrs · 11,928 cycles

EMERGENCY CEILING LIGHT ROW 2 INOPERATIVE. R & R LT FWD EMER LIGHT POWER.

Part: HEAT EXCHANGER — CRACKED (AC BAY) · airframe 14,482 hrs · 11,914 cycles

FLIGHT 2044, ATL TO PHL DIVERTED TO CLT DUE TO PRESS PROBLEM. CAPTAIN STATED THEY HAD BLEED 1 LEAK WITH PACK 2 ON MEL FOLLOWED BY CABIN ALT WARNING. THE FLIGHT DECLARED AN EMERGENCY & LANDED UNEVENTFULLY.

Part: BOTTLE — LOW PRESSURE (DOOR)

PHL R1 & R2 DOOR ASSIST BOTTLES REQUIRES SERVICE. SERVICED DOOR ASSIST BOTTLES ON R1 & R2 DOORS.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 13,692 hrs · 11,295 cycles

R2 DOOR ASSIST BOTTLE LOW PRESS. SERVICED R2 DOOR ASSIST BOTTLE.

Part: SENSOR — DEFECTIVE (LE SLAT) · airframe 13,615 hrs · 11,249 cycles

FLIGHT SENT ACARS THEY HAD SLAT FAILURE DURING CLIMB & WERE RETURNING TO PHL. THE FLIGHT LANDED WITHOUT INCIDENT, NO EMERGENCY DECLARED. REPLACED THE LT 3/4 SLAT SKEW SENSOR.

Part: SENSOR — DEFECTIVE (LE SLAT) · airframe 13,612 hrs · 11,247 cycles

SLAT FAIL CAUTION DURING SLAT RETRACTION. LT OTBD 2/3 SKEW SENSOR & HARNESS BAD. REPLACED SKEW SENSOR & THE SENSOR HARNESS. OPERATION CHECKED GOOD, NO FURTHER FAULTS NOTED.

Part: ENGINE — VIBRATION (NR 2) · airframe 11,594 hrs · 9,817 cycles

FLT 1607 EN ROUTE. NR 2 ENGINE VIBRATION HIGH, AT TIMES MOMENTARILY EXCEEDING LIMITS (AMBER INDICATION). HIGHEST READING 4.1. STILL NOTICED VIBRATION AT GROUND IDLE. MX R & R NR 2 ENGINE.

Part: GLOWSTRIP — DEFECTIVE (CABIN) · airframe 11,502 hrs · 9,763 cycles

FLOOR LIGHTING BY SEAT 5C IS NOT WORKING PROPERLY. MAINTENANCE REPLACED SECTION OF THE PHOTO LUMINESENT STRIP NEAR SEAT 5C. OKAY FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 11,015 hrs · 9,421 cycles

C2 CHECK - CABIN CEILING PANEL 243GLC EMERGENCY LIGHT IS INOP. REPLACED EMERGENCY POWER SUPPLY BATTERY ON CEILING PANEL 243GLC IAW EMBRAER E190 AMM 33-50-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - NR 1 EMERGENCY POWER SUPPLY BATTERY DOES NOT HOLD 15 MINUTE CHARGE. FAILS TEST. REPLACED NR 1 EMERGENCY POWER SUPPLY BATTERY IAW EMBRAER E190 AMM 33-50-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - NR 6 EMERGENCY POWER SUPPLY BATTERY DOES NOT HOLD 15 MINUTE CHARGE. FAILS TEST. REPLACED NR 6 EMERGENCY POWER SUPPLY BATTERY IAW EMBRAER E190 AMM 33-50-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BEAM BETWEEN FR85 TO FR86, WL-490, RBL 11. REPLACED SEAT TRACK BEAM BETWEEN FR85 TO FR86, WL-490, RBL 11 IAW EMRAER E190 SRM 51-40-00.

Part: LIGHT — BROKEN (CABIN) · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - EMERGENCY LIGHT FRAME BROKEN ON PANEL 252KRW. REPLACED EMERGENCY LIGHT IAW EMBRAER E-190 AMM 20-10-07.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FORWARD CARGO FINGER DOUBLER BETWEEN FR24 TO FR25 & BETWEEN S25R TO S26R. REPLACED FORWARD CARGO FINGER DOUBLER BETWEEN FR24 TO FR25 & BETWEEN S25R TO S26R IAW EMRAER E190 SRM II 51-41-02, 51-43-02 & 51-23-04.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR17 TO FR19, WL-490, LBL 11. REPAIRED FLOORBEAM BETWEEN FR17 TO FR19, WL-490, LBL 11 IAW EA 504553.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON RIGHT FORWARD STILL RIGHT PANEL BETWEEN FR12 TO FR14, WL-490, RBL 36. REPLACED RIGHT FORWARD STILL RIGHT PANEL BETWEEN FR12 TO FR14, WL-490, RBL 36 IAW EMRAER E190 SRM II 51-40-02 & 51-48-04.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON GUSSET AT FR90, WL-490, RBL 22. REPLACED GUSSET AT FR90, WL-490, RBL 22 IAW E-190 SRM 51-41-02.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR87 TO FR88, WL-490, RBL 15. REPLACED SHEAR PLATE BETWEEN FR87 TO FR88, WL-490, RBL 15 IAW E-190 SRM 51-42-02.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON GUSSET AT FR90, WL-490, RBL 14. REPLACED GUSSET AT FR90, WL-490, RBL 14 IAW E-190 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR12 TO FR17, WL-490, RBL 11. REPLACED FLOORBEAM BETWEEN FR12 TO FR17, WL-490, RBL 11 IAW E-190 SRM 51-41-01, 51-41-02, 51-41-03 & 51-41-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR85 TO FR86, WL-490, LBL11. REPLACED SEAT TRACK BETWEEN FR85 TO FR86, WL-490, LBL11IAW E-190 SRM II 51-40-00.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR CLIP BETWEEN FR84 TO FR85, WL-490, RBL 40. REPLACED SHEAR CLIP BETWEEN FR84 TO FR85, WL-490, RBL 40 IAW E-190 SRM II 51-42-02 & 51-21-02.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PANEL BETWEEN FR87 TO FR88, WL-490, LBL 22. REPLACED SHEAR PANEL BETWEEN FR87 TO FR88, WL-490, LBL 22 IAW E-190 SRM 51-42-01, 51-43-03 & 51-42-02.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PANEL BETWEEN FR87 TO FR88, WL-490, RBL 23. REPLACED SHEAR PANEL BETWEEN FR87 TO FR88, WL-490, RBL 23 IAW EMBRAER E190 SRM 51-42-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BEAM BETWEEN FR88 TO FR89, WL-490, RBL 12. REPLACED SEAT TRACK BEAM BETWEEN FR88 TO FR89, WL-490, RBL 12 IAW E-190 SRM II 51-41-01.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR87 TO FR88, WL-490, LBL 40. REPLACED SHEAR PLATE BETWEEN FR87 TO FR88, WL-490, LBL 40 IAW E-190 SRM 51-42-02.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON GUSSET AT FR90, LBL 14. REPLACED GUSSET AT FR90, LBL 14 IAW E-190 SRM II 51-40-02 & 51-41-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FITTING BETWEEN FR24 TO FR27, S26R. REPLACED FITTING BETWEEN FR24 TO FR27, S26R IAW E-190 SRM II 51-41-01.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PANEL BETWEEN FR87 TO FR88, WL-490 & BETWEEN LBL 4 TO LBL 9. REPLACED SHEAR PANEL BETWEEN FR87 TO FR88, WL-490 & BETWEEN LBL 4 TO LBL 9 IAW E-190 SRM 51-42-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BEAM AT FR84, WL-490, RBL 11. REPAIRED SEAT TRACK BEAM AT FR84, WL-490, RBL 11 IAW E-190 SRM 53-00-01, REPAIR 51, 51-31-00 & EA 504562.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON GUSSET AT FR90, WL-490, RBL 14. REPLACED GUSSET AT AT FR90, WL-490, RBL 14 IAW E190 SRM II 51-40-02.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 11,013 hrs · 9,420 cycles

C2 CHECK - CORROSION AT GUSSET AT FRAME 90 AND LBL 22. REPLACED GUSSET AT FRAME 90 AND LBL22 IAW E190 SRM 51-40-02.

Part: BOTTLE — LOW PRESSURE (RT DOOR) · airframe 10,106 hrs · 8,607 cycles

AFT RIGHT DOOR ASSIST BOTTLE PRESSURE LOW. MAINTENANCE SERVICED DOOR ASSIST BOTTLE.

Part: DOOR — LACK OF LUBE (L1) · airframe 9,313 hrs · 7,883 cycles

FORWARD 1L DOOR VERY DIFFICULT TO OPEN AND CLOSE. MAINTENANCE LUBED 1L DOOR. OPERATIONAL CHECKS OKAY, DOOR OPENS AND CLOSES NORMALLY, OKAY FOR SERVICE.

Part: CABLE — BROKEN (R2 DOOR) · airframe 9,193 hrs · 7,790 cycles

PHL - R2 DOOR GIRT BAR IS STILL ENGAGED WHEN INDICATING DISARMED. MAINTENANCE FOUND SLIDE ARMING CABLE/FLEX BROKEN. REPLACED CABLE/FLEX ASSY PER AMM 52-42-40-400-801A. ADJ/TEST OF ARMING SYSTEM PER AMM 52-42-40-820-801A GOOD. RE-INSTALLED SAME SERVICEABLE SLIDE ASSY PER AMM 25-65-01-000-801A.

Part: TRANSDUCER — FAULTY (BRAKE SYSTEM) · airframe 9,129 hrs · 7,735 cycles

FLIGHT 2141, BOS - LGA - PILOT REPORTS: DURING TAKEOFF ROLL, RECEIVED BRK RT AND BRK LT FAULT LIGHTS. AIRCRAFT WEAVED LEFT AND RIGHT WITH NO PILOT INPUT. RTO CLICKED OFF. PERFORMED ABORTED TAKEOFF. TAXIING IN GOT LG NO DISPATCH EICAS. MAINTENANCE REMOVED AND REPLACED L SYS 1 BRAKE PRESSURE TRANSDUCER PER AMM 32-41-05. OPS NORMALLY, NO FAULTS NOTED.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 7,991 hrs · 6,791 cycles

BOS - R2 & L2 DOOR ASSIST BOTTLE PRESSURES BELOW LIMITS PER WEEKLY CHECK. MAINTENANCE SERVICED R2 & L2 DOOR ASSIST BOTTLES PER AMM 52-41-51.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 7,991 hrs · 6,791 cycles

BOS - R2 & L2 DOOR ASSIST BOTTLE PRESSURES BELOW LIMITS PER WEEKLY CHECK. MAINTENANCE SERVICED R2 & L2 DOOR ASSIST BOTTLES PER AMM 52-41-51.

Part: HOOK — OUT OF ADJUST (DOOR)

BOS - THE FORWARD DOOR OPEN HOOK WAS INOPERATIVE. MAINTENANCE ADJUSTED THE FORWARD DOOR OPEN HOOK. OPERATIONALLY CHECKS GOOD.

Part: BATTERY — FAULTED (CABIN)

BOS - MAINTENANCE REPORTED AN EMERGENCY LIGHT BATTERY FAULT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MID EMERGENCY BATTERY PER AMM CHAPTER 33-50-01. CHECKS OK.

Part: BOTTLE — LOW PRESSURE (PAX DOOR)

BOS - THE RIGHT AFT PASSENGER DOOR ASSIST BOTTLE REQUIRES SERVICING. MAINTENANCE SERVICED THE RIGHT AFT DOOR ASSIST BOTTLE PER 52-10-00.

Part: BATTERY — DISCHARGED (CABIN)

PHL - EMERGENCY LIGHT BATTERY FAULT EICAS MESSAGE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY NICAD BATTERY, MID RIGHT POSITION. OPERATIONAL CHECK IS SATISFACTORY.

Part: ACCUMULATOR — LOW (R1 DOOR)

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

Part: BATTERY — ACTIVATED (CABIN)

PHL - THE EMERGENCY LIGHTS ARE INOPERATIVE IN AFT SIGN AND PATH LIGHTS, FORWARD OF AFT OVERHEAD EMERGENCY EXIT SIGN. MAINTENANCE REPLACED THE AFT TOP BATTERY.

Part: BATTERY PACK — DISCHARGED (CABIN)

PHL - THE RIGHT WING EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK NR 4.

Part: BATTERY — DISCHARGED (CABIN)

EMERGENCY LIGHT INOP. MAINTENANCE INSTALLED SERVICEABLE BATTERY.

Part: CONTROL MODULE — MALFUNCTIONED (BRAKE SYSTEM)

PHL ORD-PHL FLT 856. DURING DESCENT TO PHL THE CAPTAIN DECLARED AN EMERGENCY WITH ATC, RECEIVED A FAULT MESSAGE ON EICAS THAT THE OUTBOARD BRAKES ARE COLD AND THE INBOARD BRAKES ARE AMBER. THE FLIGHT DID A GO-AROUND AND THE CAPTAIN AND FIRST OFFICER RAN THROUGH THE PROCEDURES IN THE HANDBOOK. THE FLIGHT THEN MADE THE APPROACH AND LANDED WITHOUT INCIDENT. THE BRAKES FUNCTIONED PROPERLY. MAINTENANCE REPLACED BRAKE CONTROL MODULE NR 2. CHECKS OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

CLT - EMERGENCY LIGHT MID CABIN, OVERWING CEILING PANEL EXIT SIGN, FORWARD SIDE AND CEILING EMERGENCY LIGHT AT PANEL FIVE ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY NICAD BATTERY PACK.