N944UW

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 27,323 hrs · 22,597 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY LIGHT POWER UNIT INOPERATIVE AT DOOR 2R. MAINTENANCE REPLACED EMERGENCY LIGHT POWER UNIT BATTERY PER AMM 33-55-01.

Part: PRECOOLER — LEAKING (LT ENGINE) · airframe 27,323 hrs · 22,597 cycles

ATL-PHL, DIVERTED TO CLT ACCOUNT BLEED ISSUE. EMERGENCY DECLARED. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AIRCRAFT FROM SERVICE. REPLACED LEFT ENG PRECOOLER AND PRECOOLER EXHAUST DUCT SEAL IAW AMM 36-11-08. PERFORMED SATISFACTORY OPERATIONAL TEST OF ENGINE PNEUMATIC BLEED SYSTEM PER AMM 36-11-00-710-801-A.

Part: BATTERY — NO TEST (FLY BY WIRE) · airframe 26,321 hrs · 21,683 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS FLY-BY-WIRE BACK-UP BATTERY FAILS FUNCTIONAL TEST. REMOVED AND REPLACED FLY-BY-WIRE BACK-UP BATTERY IAW AMM 27-03-05. OPS CHECK GOOD.

Part: WINDOW — LEAKING (COCKPIT) · airframe 25,324 hrs · 20,847 cycles

HISSING AND WHISTLING SOUND FROM CAPTAIN`S SIDE COCKPIT WINDOW AT 36,000 FT AND AGAIN AT 29,000 FT. THE AIRCRAFT WAS GROUNDED. DURING PRESSURIZATION CHECK, FOUND DIRECT VIEW WINDOW LEAKING BETWEEN GLASS AND SEAL. REPLACED THE WINDOW IAW AMM 56-12-00. NO LEAKS NOTED DURING PRESSURIZATION FUNCTIONAL CHECK. OK FOR SERVICE.

Part: INTERCOSTAL — CORRODED (FRAMES 86-87) · airframe 25,152 hrs · 20,705 cycles

CORROSION FOUND ON THE AFT CARGO BAY FORWARD INTERCOSTAL BETWEEN FRAMES 86 AND 87, STRINGERS 27R AND 28R. REPLACED THE INTERCOSTAL.

Part: INTERCOSTAL — CORRODED (FRAMES 86-87) · airframe 25,152 hrs · 20,705 cycles

CORROSION ON THE AFT CARGO BAY AFT INTERCOSTAL BETWEEN FRAME 86 AND 87 AND BETWEEN STINGERS 27R AND S28R. REPLACED THE INTERCOSTAL.

Part: LIGHT — WORN (CABIN) · airframe 25,152 hrs · 20,705 cycles

MAIN CABIN LT EMERGENCY LIGHT STRIP WAS IN POOR CONDITION. REPLACED THE EMERGENCY LIGHT STRIP IAW AMM 33-50-21.

Part: LIGHT — WORN (CABIN) · airframe 25,152 hrs · 20,705 cycles

MAIN CABIN RT EMERGENCY LIGHT STRIP WAS IN POOR CONDITION. REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-21.

Part: SHEAR TIE — CORRODED (FRAME 83) · airframe 25,152 hrs · 20,705 cycles

CORROSION FOUND ON THE AFT CARGO BAY SHEAR TIE AT FRAME 83 BETWEEN STRINGERS 27R AND 28R. REPLACED THE SHEAR TIE IAW SRM 51-41-01.

Part: SHEAR TIE — CORRODED (FRAME 82) · airframe 25,152 hrs · 20,705 cycles

CORROSION FOUND ON THE AFT CARGO SHEAR TIE AT FRAME 82, BETWEEN STRINGERS 27 - 28R. REPLACED THE SHEAR TIE IAW DRAWING 170-66674-001.

Part: SHEAR TIE — CORRODED (FRAME 84) · airframe 25,152 hrs · 20,705 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. CORROSION FOUND ON AFT CARGO SHEAR TIE AT FRAME 84, BETWEEN STRINGERS 27-28R. REPLACED SHEAR TIE IAW DRAWING 170-66868-001.

Part: SHEAR TIE — CORRODED (FRAME 85) · airframe 25,152 hrs · 20,705 cycles

CORROSION FOUND ON THE SHEAR TIE, FRAME 85, STRINGERS 27R - 28R. REPLACED THE SHEAR TIE IAW DWG 170-66065-001.

Part: SKIN — CRACKED (LT WING) · airframe 25,152 hrs · 20,705 cycles

LEFT WING LOWER SURFACE SKIN WAS CRACKED, FORWARD OF SPAR 2, AND OUTBOARD OF RIB 10. REPAIRED THE SKIN IAW EA 286670.

Part: SHEAR TIE — CORRODED (FRAME 81) · airframe 25,152 hrs · 20,705 cycles

AFT CARGO SHEAR TIE HAD CORROSION AT FRAME 81, STRINGERS 27R - 28R. REPLACED THE SHEAR TIE IAW DWG 170-66885-001.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 25,152 hrs · 20,705 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON AFT CARGO COMPARTMENT SHEAR TIE AT FR 87 BETWEEN STR 27R - STR 28R. REPLACED SHEAR TIE PER SRM 51-41-02 & DWG 170-66043-001 REV 1.

Part: PAD — WORN (DOOR STOP) · airframe 25,152 hrs · 20,705 cycles

FORWARD SERVICE DOOR FRAME UPPER AFT DOOR STOP PAD HAD WEAR. REPLACED THE DOOR STOP PAD IAW AMM 52-10-25.

Part: SEAT TRACK — CORRODED (FRAME 84) · corrosion level 2 · airframe 25,152 hrs · 20,705 cycles

CORROSION FOUND ON THE SEAT TRACK, FRAME 84, Y276. ACCOMPLISHED A SPLICE REPAIR IAW SRM 53-00-10, REPAIR 51.

Part: FLOOR SUPPORT — CORRODED (FRAME 89) · airframe 25,152 hrs · 20,705 cycles

CORROSION FOUND ON THE AFT MAIN CABIN, RIGHT FLOOR SUPPORT AT FRAME 89, Y+960. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: WINDOW SHADE — CRACKED (CABIN) · airframe 25,152 hrs · 20,705 cycles

AIRCRAFT IN BASE MAINTENANCE: MAIN CABIN RIGHTHAND OVER WING EXIT WINDOW SHADE ASSEMBLY CRACKED. REPLACED WINDOW SHADE ASSEMBLY AT CABIN RIGHTHAND OVER WING EXIT PER AMM 25-23-15.

Part: SHEAR TIE — CORRODED (FRAME 88) · airframe 25,152 hrs · 20,705 cycles

CORROSION FOUND ON SHEAR TIE ON FRAME 88, BETWEEN STRINGERS 27 - 28R. REPAIRED SHEAR TIE IAW SRM 51-40-08.

Part: ROLLER — LACK OF LUBE (EMERGENCY EXIT) · airframe 25,152 hrs · 20,705 cycles

RIGHT OVERWING ESCAPE HATCH FORWARD ROLLER WAS FROZEN. LUBRICATED THE ROLLER. INSPECTION CHECKED GOOD IAW AMM 53-22-11-212-801-A.

Part: ROLLER — FROZEN (EMERGENCY EXIT) · airframe 25,152 hrs · 20,705 cycles

THE AIRCRAFT IS IN BASE MAINTENANCE. OVER WING ESCAPE HATCH AFT ROLLER IS FROZEN. LUBRICATED LEFT HAND OVERWING ESCAPE HATCH AFT ROLLER. INSPECTION CHECK GOOD PER AMM 53-22-11-212-801-A.

Part: FLOOR SUPPORT — CORRODED (FRAME 89) · airframe 25,152 hrs · 20,705 cycles

CORROSION FOUND ON THE RIGHT, AFT MAIN CABIN FLOOR SUPPORT, FRAME 89, Y960. REPLACED THE FLOOR SUPPORT IAW DWG 170-66000-455.

Part: SEAT — OUT OF ADJUST (COCKPIT) · airframe 24,935 hrs · 20,530 cycles

CAPTAIN`S SEAT WON'T STAY IN LOCKED POSITION ALONG FWD & BACK RAIL POSITION. IF YOU LOCK THE SEAT, AND SIMPLY LIFT UP ON THE SEAT, IT FORCES IT OUT OF TRACK. THIS HAPPENS OCCASIONALLY WITHOUT ADDITIONAL ACTION DURING FLIGHT. ADJUSTED THE CAPTAIN`S SEAT CABLE AND LUBRICATED THE SEAT CABLE, TRACK AND RAIL ASSEMBLY. OPS CHECKED GOOD. OK FOR CONTINUED SERVICE.

Part: CONNECTOR — DIRTY (BLEED AIR SYS) · airframe 24,847 hrs · 20,466 cycles

AIRCRAFT WAS GROUNDED. ON DESCENT RECEIVED "BLEED APU LEAK" ON EICAS ASSOCIATED WITH A STRONG BURNING SMELL. TROUBLESHOOT PER FIM 36-22-00-810-822-A AND REPAIR PER APPLICABLE AMM. ACCOMPLISHED J/C 43L00021001 RAN BOTH ENGINES INDIVIDUALLY AT IDLE AND BOTH PACKS INDIVIDUALLY FROM EACH ENGINE BLEED SOURCE (FULL HOT, FULL COLD). NO ODOR NOTED. FOUND OPEN WIRING FAULT ON BOTH LOOP 1 AND LOOP 2. CLEANED CONNECTIONS ON LOOP 1 AT LOCATION 46 AND LOOP 2 AT LOCATION 74 PER TSM 36-22-00-810-813. OPERATIONS CHECK GOOD.

Part: SLIDING WINDOW — DAMAGED (COCKPIT) · airframe 23,914 hrs · 19,716 cycles

CAPTAIN`S SIDEVIEW WINDOW DIFFICULT TO CLEARLY SEE THROUGH AT NIGHT DUE TO MULTIPLE SCRATCHES AND BLEMISHES ON EXTERIOR GLASS. REPLACED THE CAPTAIN`S SLIDING WINDOW ASSY IAW AMM 56-12-00. LEAK CHECK OK.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 23,108 hrs · 19,081 cycles

L2 DOOR FLASHLIGHT WAS INOPERATIVE. REPLACED THE BATTERY. MAINTENANCE PERFORMED SUCCESSFUL OPS CHECK.

Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 22,458 hrs · 18,553 cycles

OVERHEAD EXIT SIGN CAME OFF IN FLIGHT. MID CABIN LOCATION. REINSTALLED AND SECURED COVER.

Part: GIRT BAR — DISLODGED (L1 DOOR SLIDE) · airframe 21,265 hrs · 17,633 cycles

L1 DOOR IS JAMMED IN THE ARMED POSITION. FOUND THE GIRT BAR DISLODGED. AIRCRAFT WAS GROUNDED. ADJUSTED THE GIRT BAR IAW AMM 26-65-01.

Part: STRUT — UNDERSERVICED (NLG) · airframe 21,107 hrs · 17,538 cycles

LANDING GEAR LEVER WOULD NOT MOVE UP AFTER TAKE OFF, LANDING GEAR WOW SYSTEM FAIL EICAS MESSAGE SHORTLY AFTER. MAINTENANCE ACCOMPLISHED FIM 32-33-00 AND FOUND NOSE LANDING GEAR WOW 1 AND 2 SENSOR DISAGREE, SERVICED NOSE LANDING GEAR STRUT FLUID CORRECTLY AND PERFORMED SATISFACTORY LANDING GEAR EXTENTION AND RETRACTION SYSTEM TESTS PER E190 AMM 32-33-00 AND 32-34-00.

Part: LENS — CRACKED (EXTERIOR LIGHT) · airframe 20,050 hrs · 16,602 cycles

AIRCRAFT IN BASE MAINTENANCE: RT MOST AFT EXTERIOR FUSELAGE EMERGENCY LIGHT HAS A CRACKED LENS. REPLACED EMERGENCY LIGHT AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 33-50-25-000-802-A AND 33-50-25-710-801-A.

Part: PIN — MISSING (EVAC SLIDE) · airframe 20,047 hrs · 16,601 cycles

AIRCRAFT IN BASE MAINTENANCE: L1 DOOR EMERGENCY SLIDE IS MISSING A SAFETY PIN. INSTALLED MISSING SAFETY PIN ON THE L1 DOOR EMERGENCY SLIDE PER AMM 52-00-23-910-003-A.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 20,047 hrs · 16,601 cycles

ACFT IN BASE MAINTENANCE: AFT LT F/A SEAT FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT IAW TC 43C20025028.

Part: LINE — GOUGED (SERVICE DOOR) · airframe 20,047 hrs · 16,601 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT SERVICE DOOR NITROGEN CYLINDER LINE IS GOUGED ON SUPPORT ARM. R & R NEW AFT SERVICE DOOR NITROGEN CYLINDER LINE IAW AMM 52-42-51-000-801-A & 52-42-51-400-801-A.

Part: LENS — DIRTY (EXTERIOR LIGHT) · airframe 20,047 hrs · 16,601 cycles

AIRCRAFT IN BASE MAINTENANCE: LT AFT WING TO BODY FAIRING PANEL 199EL, LOWER AFT LIGHT LENS IS DIRTY/CLOUDED. REPLACED LT AFT WING TO BODY FAIRING PANEL, 199EL, LOWER AFT LIGHT LENS IAW AMM 33-50-25.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 20,047 hrs · 16,601 cycles

AIRCRAFT IN BASE MAINTENANCE: WHILE PERFORMING AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTS THE LEFT AFT WING TO BODY EMERGENCY LIGHT DID NOT COME ON. MAINTENANCE FOUND CONNECTOR J2556 DISCONNECTED, RECONNECTED IT AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 33-50-25, FIM 33-50-00-810-816-A AND W19 33-50-50.

Part: LENS — CRACKED (EXTERIOR) · airframe 20,047 hrs · 16,601 cycles

AIRCRAFT IN BASE MAINTENANCE: LT AFT WING TO BODY FAIRING PANEL 199LL AFT UPPER WING LIGHT EMERGENCY ESCAPE PATH LENS IS YELLOWED, CRACKED. REPLACED EMERGENCY ESCAP PATH LIGHT ASSY AND OPS CHECKED IAW AMM 33-50-25.

Part: LENS — CRACKED (EXTERIOR) · airframe 20,047 hrs · 16,601 cycles

ACFT IN BASE MAINTENANCE: RT AFT WING TO BODY FAIRING PANEL 198MR, AFT UPPER WING EMERGENCY ESCAPE PATH LIGHT LENS IS YELLOW/CRACKED. REPLACED EMERGENCY ESCAPE PATH LIGHT ASSY AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 33-50-25.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,047 hrs · 16,601 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO DOOR CUTOUT LOWER THRESHOLD PLATE LOWER BEAM BETWEEN FRAME 24 AND FRAME 27 AT +Y398. REPLACED BEAM IAW SRM 51-43-04 AND DWG 170-67080-431.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,047 hrs · 16,601 cycles

CORROSION ON FORWARD MAIN CABIN LT FLOOR SEAT TRACK BETWEEN FRAME 19 AND FRAME 20 AT -Y276. REPLACED FLOOR SEAT TRACK IAW AARD 53-00-00-3, REPAIR 3.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,047 hrs · 16,601 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD PASSENGER DOOR CUTOUT LOWER BEAM BETWEEN FRAME 16 AND FRAME 19 AT +Y1240. REPLACED LOWER BEAM IAW DWG 170-01330-507 AND SRM'S 51-43-03, -04 & 51-41-03.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 20,047 hrs · 16,601 cycles

AIRCRAFT IN BASE MANITENANCE: COCKPIT FLOOR STRUCTURE SUPPORT ANGLE CRACKED AT FR 12 AND -Y520. REPLACED SUPPORT ANGLE IAW SRM 51-40-01, 51-23-04, 51-23-05 AND 51-23-06.

Part: SEAL REST — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,047 hrs · 16,601 cycles

CORROSION ON FORWARD CARGO DOOR CUTOUT CENTER SEAL REST. REPLACED SEAL REST IAW AARP 53-00-00-3, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,047 hrs · 16,601 cycles

CORROSION ON FLOOR SUPPORT BETWEEN FRAME 88 AND FRAME 90 AT -Y0000. REPLACED FLOOR SUPPORT IAW DWG 170-65780-443, SRM 51-41-01, 51-42-02, 51-43-03, 51-23-04, 51-23-05 AND 51-23-06.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,047 hrs · 16,601 cycles

CORROSION ON FLOOR SUPPORT BETWEEN FRAME 88 AND FRAME 90 AT +Y1000. REPLACED FLOOR SUPPORT IAW AARD 53-00-00-3, REPAIR 3 AND SRM 51-41-02.

Part: FLOORBEAM — CORRODED (FRAME 16) · corrosion level 2 · airframe 20,047 hrs · 16,601 cycles

CORROSION ON FWD CABIN LT FLOORBEAM AT FRAME 16 & -Y1143. REPLACED FLOORBEAM IAW SRM 51-40-02 & 51-43-03.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,047 hrs · 16,601 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON CABIN FLOOR PANEL SUPPORT AT FRAME 19 AND -Y1092. REPLACED CABIN FLOOR PANEL SUPPORT IAW SRM 51-43-03.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 20,047 hrs · 16,601 cycles

AIRCRAFT IN BASE MX. CORROSION ON CABIN FLOOR STRUCTURE SPLICE AT CROSSBEAM AT FRAME 90 & BL 0. REPLACED SPLICE IAW SRM 51-40-02 & 51-43-03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,047 hrs · 16,601 cycles

CORROSION ON FLOOR SEAT TRACK AROUND CROWN AREA AT FRAME 33 AND -Y260. ACCOMPLISHED A FLOOR SEAT TRACK TYPICAL SPLICE DEVICE REPAIR IAW SRM 53-00-10, REPAIR 52.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,047 hrs · 16,601 cycles

CORROSION ON FORWARD MAIN CABIN, FORWARD RT FLOOR SILL BETWEEN FRAME 12 AND FRAME 14 AND +Y939 AND +Y122. REPLACED FLOOR SILL IAW SRM 51-43-01 & 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,047 hrs · 16,601 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT BETWEEN FRAME 17 AND FRAME 18 AT +Y330. REPLACED FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 170-00822-503.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,047 hrs · 16,601 cycles

CORROSION ON FORWARD MAIN CABIN RT AFT FLOOR SILL BETWEEN FRAME 17 AND FRAME 18 AT +Y1092. REPLACED FLOOR SILL IAW SRM 51-40-02 AND 51-43-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,047 hrs · 16,601 cycles

CORROSION ON FORWARD CABIN, LT FORWARD FLOOR SILL BETWEEN FRAME 12 AND FRAME 13 AT -Y1168. REPLACED FLOOR SILL IAW SRM 51-23-04, 51-23-05, 51-41-02 AND DWG 170-00822-413.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,047 hrs · 16,601 cycles

CORROSION ON LT FORWARD FLOOR DOUBLER AT FRAME 16 AND -Y330. REPLACED FLOOR DOUBLER IAW AARD 53-00-00-3, REPAIR 3 AND SRM 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,047 hrs · 16,601 cycles

CORROSION ON FORWARD MAIN CABIN RT FLOOR SEAT TRACK BETWEEN FRAME 12 AND FRAME 20 AT +Y276. REPLACED FLOOR SEAT TRACK IAW SRM 51-40-02 AND DWG 170-00822-413.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,047 hrs · 16,601 cycles

CORROSION ON LT FLOOR SEAT TRACK AT FRAME 84 AND -Y275. REPAIRED SEAT TRACK IAW SRM 53-00-10, REP 51, FIG 205, SHEET 2.

Part: WINDOW — CRAZED (CABIN) · airframe 20,047 hrs · 16,601 cycles

AIRCRAFT IN BASE MAINTENANCE: LT SIDE NR 1 PASSENGER CABIN WINDOW OUTER PANE IS CLOUDY, CRAZED. REPLACED WINDOW IAW AMM 56-20-00.

Part: ACM — DEFECTIVE (AC BAY) · airframe 19,338 hrs · 16,031 cycles

AIRCRAFT WAS NOT GNDED. CABIN CREW & PAXS REPORT UNKNOWN SMOKE IN THE CABIN. ACCOMPLISHED TROUBLESHOOTING OF CABIN AIR QUALITY IAW JC 43L00021001. FOUND SOURCE OF THE CABIN ODOR TO BE THE ACM & REPLACED IT IAW AMM 21-51-05. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 19,262 hrs · 15,966 cycles

AIRCRAFT WAS NOT GNDED. ACFT LEFT AFT FLASHLIGHT IS NOT BLINKING. REPLACED AFT LT EMER FLASHLIGHT BATTERY. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-01-000-802 & 400-802.

Part: BATTERY — DISCHARGED (CABIN) · airframe 19,012 hrs · 15,755 cycles

FORWARD GALLEY MONUMENT EMER LIGHT INOPERATIVE. REPLACED EMER LIGHT POWER UNIT NR 2 BATTERY & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-50-01.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 16,402 hrs · 13,676 cycles

CABIN PRESSURIZATION WAS -600 AT 16,000 FT A6.9. FUNNY ODOR FROM ECS WENT AWAY WITH PACK 2 TO OFF. R & R NR 2 EDP.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 16,169 hrs · 13,449 cycles

C3 CHECK LT AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED LT AFT FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW AMM 33-51-01. OPERATIONS CHECKED GOOD.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 16,169 hrs · 13,449 cycles

C3 CHECK MAIN CABIN RT FLOOR PANEL 242ARF IS DELAMINATED. REPLACED IAW AMM 25-24-01 & 53-01-39.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,167 hrs · 13,448 cycles

LEVEL 2 GALVANIC CORROSION ON SEAL REST BETWEEN FRAME 77 TO 80, Z-1559, Y457.2. REPLACED SEAL REST IAW SRM 51-12-01, 53-23-11, 51-41-01 & AMM 53-23-29.

Part: PANEL — CORRODED (FUSELAGE) · airframe 16,167 hrs · 13,448 cycles

C3 CHECK CORROSION ON UPPER SURFACE OF SHEAR PANEL BETWEEN FRAME 87 TO 88, Z-490MM & BETWEEN -Y275MM TO Y275MM. REPLACED SHEAR PANEL IAW SRMS 51-10-03, 53-23-01, 53-23-10, 51-42-02 & 51-43-01.

Part: PANEL — CORRODED (FUSELAGE) · airframe 16,167 hrs · 13,448 cycles

C3 CHECK CORROSION ON UPPER SURFACE OF SHEAR PANEL BETWEEN FRAME 87 TO 88, Z-490MM & BETWEEN -Y275MM TO -Y1050MM. REPLACED SHEAR PANEL IAW SRMS 51-10-03, 53-23-10, 53-23-10, 51-42-02 & 51-42-01.

Part: PANEL — CORRODED (FUSELAGE) · airframe 16,167 hrs · 13,448 cycles

C3 CHECK CORROSION ON UPPER SURFACE OF SHEAR PANEL BETWEEN FRAME 87 TO 88, Z-490MM & BETWEEN Y275MM TO Y1050MM. REPLACE SHEAR PANEL IAW SRMS 51-10-03, 53-23-10, 51-42-02 & 51-43-01.

Part: LOCK NUT — LOOSE (RT PYLON)

THE RT PYLON LOWER LINK OTBD FITTING SHEAR PIN LOCKNUT WAS FOUND LOOSE WITH A MIGRATED BUSHING. ACCOMPLISHED A RE-TORQUE OF THE LOCKNUT & INSTALLED THE PROPER SAFETIES.

Part: DIAPHRAGM — PUNCTURED (L1 DOOR)

PHL FOUND L1 DOOR ACCUMULATOR DIAPHRAGM PUNCTURED DURING SERVICING OF DOOR ACCUMULATOR. REPLACED L1 DOOR PNEUMATIC ASSEMBLY.

Part: FITTING — DEFECTIVE (L1 DOOR) · airframe 15,086 hrs · 12,523 cycles

THE FLIGHT ATTENDANT COULD NOT DISARM DOOR L1 WHEN WE ARRIVED AT THE GATE. MX REPLACED FWD PAX L1 DOOR EVACUATION SLIDE FWD FITTING. PRESSURIZED CABIN TO 5.8 PSI, L1 DOOR ARMS & DISARMS NORMALLY.

Part: SPRING — OUT OF TOLERANCE (GIRT BAR) · airframe 15,080 hrs · 12,519 cycles

1L DOOR WOULD NOT DISARM AFTER FLIGHT AT GATE. MX FOUND FWD GIRT BAR SPRING DOUBLER OPENING OUT OF LIMITS. R & R FWD GIRT BAR SPRING DOUBLER. OPERATIONAL TEST IS GOOD, OK FOR SERVICE.

Part: HANDLE — MISALIGNED (L1 DOOR SLIDE) · airframe 15,076 hrs · 12,517 cycles

UNABLE TO DISARM 1L DOOR. ARM - DISARM HANDLE & GIRT BAR OUT OF SYNC. REMOVED SLIDE & SYNCED HANDLES & GIRT BAR.

Part: DUCT SEAL — LEAKING (PRECOOLER EXHAUS) · airframe 14,452 hrs · 12,091 cycles

BLEED NR 1 LEAK ANNUCIATED CLIMBING THROUGH FL 230. FLIGHT DESCENDED AND DIVERTED. MAINTENANCE R & R THE NR 1 ENGINE PRECOOLER EXHAUST DUCT SEALS. MAINTENANCE ALSO REPLACED AMS SOFTWARE, CONTROLLER NACELLE VALVE, BLEED PRESSURE VALVE, AND CROSS BLEED VALVE.

Part: LINE — LEAKING (NR 1 BLEED) · airframe 14,452 hrs · 12,090 cycles

FLIGHT 1914, BLEED 1 LEAK CLIMBING THROUGH 12,000 FT. RESET BLEED 1 AND 2, OFF MESSAGE, COULD NOT RESET. ACFT UNPRESSURIZED AND DIVERTED. FLIGHT LANDED UNEVENTFULLY. MAINTENANCE R & R TORQUE MOTOR CONTROLLER SERVO LINE BETWEEN HPRSOV TO TORQUE MOTOR CONTROLLER FILTER.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 13,995 hrs · 11,755 cycles

EMERGENCY LIGHTS ARE INOPERATIVE CENTER AND AFT. MX REPLACED EMERGENCY BATTERIES AFT AND MID CABIN.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 13,995 hrs · 11,755 cycles

EMERGENCY LIGHTS ARE INOPERATIVE CENTER & AFT. MX REPLACED EMERGENCY BATTERIES AFT & MID CABIN.

Part: SIGN — DELAMINATED (CABIN) · airframe 13,196 hrs · 11,169 cycles

FWD GALLEY - ZONE 225 (NEAR L1 DOOR) - EMERGENCY EXIT IDENTIFIER SIGN REQUIRES REPLACEMENT. MAINTENANCE REPLACED EXIT IDENTIFIER SIGN.

Part: MODULE — INOPERATIVE (MLG) · airframe 10,654 hrs · 9,030 cycles

BRAKE RIGHT AND LEFT FAULT MESSAGES ANNUNCIATED SHORTLY AFTER GEAR RETRACTION, LIGHT STAYED ON FOR DURATION OF FLIGHT. FOLLOWED QRH AND DECLARED AN EMERGENCY WITH ATC. FLIGHT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE MAIN BRAKE CONTROL MODULE ONE.

Part: CONTROL QUADRANT — ERRATIC (THROTTLE SYS) · airframe 11,895 hrs · 10,163 cycles

FLIGHT 970, PHL-BOS - ON TAKEOFF ROLL, ENGINE NR 2 WENT TO RSV POWER. AFTER TOGA POWER WAS ENGAGED THE NR 2 N1 SHOT PAST THE SELECTED POWER SETTING, NR 1 N1 LAGGED BEHIND QUITE A BIT, WHEN BOTH N1 GAUGES FINALLY MET AT POWER SETTING, IT THEN WENT INTO TO-2 RSV POWER THEN WE REJECTED TAKEOFF. MAINTENANCE PERFORMED PNEUMATIC TASK, PERFORMED AUTO THROTTLE FUNCTIONAL PER 22-31-00. REPLACED THRUST QUADRANT CONTROL. OPERATIONAL CHECK IS GOOD AT THIS TIME.

Part: STRIP — MISSING (CABIN) · airframe 11,868 hrs · 10,136 cycles

FLOOR EMERGENCY LIGHTING STRIP FORWARD 4 INCH PIECE MISSING. MAINTENANCE INSTALLED MISSING SEGMENT OF STRIP.

Part: STRIP — UNSECURE (CABIN) · airframe 11,628 hrs · 9,909 cycles

STRIP OF EMERGENCY FLOOR LIGHTING HAS LIFTED. MAINTENANCE RE-SECURED EMERGENCY FLOOR LIGHTNING STRIP AS REQUIRED.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 11,052 hrs · 9,363 cycles

LEFT EMERGENCY ESCAPE HATCH EXIT MARKER INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY ABOVE ROW 13. NO FURTHER DEFECTS NOTED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 10,263 hrs · 8,749 cycles

C2 CHECK - EMERGENCY LIGHT IN CEILING AFT OF OVERWING EXIT DOORS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY IAW E190 AMM 33-50-01.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON DOOR SILL FRAME FITTINGS BETWEEN FR24 TO FR27, S26R. REPLACED DOOR SILL FRAME FITTINGS BETWEEN FR24 TO FR27, S26R IAW ERJ-190 SRM 53-21-11.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - LEVEL 2 CORROSION ON GUSSET AT FR90, Z-490 BETWEEN -Y26. REPLACED GUSSET AT FR90, Z-490 BETWEEN -Y26 IAW ERJ 190 SRM 51-40-02, 51-23-00 & EMBRAER DRAWING 170-60001-825.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR85 TO FR86, Z-490, Y26. REPLACED FLOORBEAM BETWEEN FR85 TO FR86, Z-490, Y26 IAW ERJ190 TYPICAL REPAIR TR190-5300-11-0563.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR85 TO FR86, Z-490, Y26. REPLACED SHEAR PLATE BETWEEN FR85 TO FR86, Z-490, Y26 IAW ERJ190 TYPICAL REPAIR TR190-5300-11-0563.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON GUSSET AT FR90, Z-490 & BETWEEN Y26 TO Y50. REPLACED GUSSET AT FR90, Z-490 & BETWEEN Y26 TO Y50 IAW ERJ-190 SRM PART 2, 51-40-02.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON GUSSET AT FR90, Z-490 & BETWEEN Y26 TO Y50. REPLACED GUSSET AT FR90, Z-490 & BETWEEN Y26 TO Y50 IAW ERJ-190 SRM PART 2, 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK AT FR84, Z-490, Y272. REPLACED SEAT TRACK AT FR84, Z-490, Y272 IAW EMBRAER DRAWING 170-65600-435 & EA 201448.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON UPPER BEAM SHEET BETWEEN FR85 TO FR86, Z-490, -Y26. REPLACED UPPER BEAM SHEET BETWEEN FR85 TO FR86, Z-490, -Y26 IAW TYPICAL REPAIR TR190-5300-11-0563 & EA201448.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN FR87 TO FR88, Z-490 & BETWEEN -Y26 TO Y26. REPLACED FLOOR SUPPORT BETWEEN FR87 TO FR88, Z-490 & BETWEEN -Y26 TO Y26 IAW TYPICAL REPAIR TR190-5300-11-0563.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT AT FR87, Z-490 & BETWEEN -Y26 TO -Y1150. REPLACED FLOOR SUPPORT AT FR87, Z-490 & BETWEEN -Y26 TO -Y1150 IAW TYPICAL REPAIR TR190-5300-11-0563 & EA 201448.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FITTINGS BETWEEN FR24 TO FR27, S26R. REPLACED 3 EACH FITTINGS BETWEEN FR24 TO FR27, S26R IAW ERJ-190 SRM 51-41-01.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FORWARD CARGO DOOR SILL FRAME BETWEEN FR24 TO FR26, S26R. REPLACED FORWARD CARGO DOOR SILL FRAME BETWEEN FR24 TO FR26, S26R IAW ERJ-190 SRM 53-21-11.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FORWARD CARGO DOOR SILL FRAME BETWEEN FR24 TO FR26, S26R. REPLACED FORWARD CARGO DOOR SILL FRAME BETWEEN FR24 TO FR26, S26R IAW ERJ-190 SRM 53-21-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT AT FR16, Z-490 BETWEEN -Y350 TO -Y780. REPLACED FLOOR SUPPORT AT FR16, Z-490 BETWEEN -Y350 TO -Y780 IAW TYPICAL REPAIR TR190-5300-11-0563 & ERJ 190 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBOARD SUPPORT WEB AT FR16, Z-490 BETWEEN -Y350 TO -Y780. REPLACED FLOOR SUPPORT AT FR16, Z-490 BETWEEN -Y350 TO -Y780 IAW TYPICAL REPAIR TR190-5300-11-0563 & ERJ 190 SRM 51-41-02.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR WEB AT FR16, Z-490 & BETWEEN -Y1280 TO -Y1380. REPLACED FLOOR WEB AT FR16, Z-490 & BETWEEN -Y1280 TO -Y1380 IAW TYPICAL REPAIR TR190-5300-11-0563.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON CLIP AT FR18, Z-490, -Y750. REPLACED CLIP AT FR18, Z-490, -Y750 IAW ERJ 190 SRM CHAPTER 51 & EMBRAER DRAWING 170-00822-413.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR16 TO FR19, BETWEEN -Y250 TO -Y300. REPLACED FLOORBEAM BETWEEN FR16 TO FR19, BETWEEN -Y250 TO -Y300 IAW E190 SRM PART II, 51-43-01, 51-43-02 AND TYPICAL REPAIR 190-5300-11-0563.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBOARD SUPPORT WEB BETWEEN FR17 TO FR18, WLZ-500, Y1080. REPLACED FLOOR BOARD SUPPORT WEB BETWEEN FR17 TO FR18, WLZ-500, Y1080 IAW TYPICAL REPAIR TR190-5300-11-0563 & ERJ 190 SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - CORROSION ON FLOOR SUPPORT WEB BETWEEN FR 19 AND FR 20, BETWEEN Y-300 AND Y-900 AT Z-490. REPLACED FLOOR SUPPORT WEB BETWEEN FR 19 AND FR 20, BETWEEN Y-300 AND Y-900 AT Z-490 IAW E190 SRM 51-41-02, TR190-5300-11-0563 AND EA 201488.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK AT FR14, Z-490, Y273. REPLACED SEAT TRACK AT FR14, Z-490, Y273 IAW ERJ 190 TYPICAL REPAIR TR 190-5300-11-0563.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR STRUCTURE REINFORCEMENT AT FR84, BETWEEN Y30 TO Y1150. REPLACED FLOOR STRUCTURE REINFORCEMENT AT FR84, BETWEEN Y30 TO Y1150 IAW E190 SRM PART II, 53-23-10, EMBRAER DRAWING 190-65140-801 AND EA201448.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,259 hrs · 8,745 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN FR87 TO FR88, Z-490 & BETWEEN -Y26 TO Y26. REPLACED FLOOR SUPPORT BETWEEN FR87 TO FR88, Z-490 & BETWEEN -Y26 TO Y26 IAW TYPICAL REPAIR TR190-5300-11-0563 & EA 201448.

Part: DUCT CLAMP — LOOSE (BLEED AIR SYS) · airframe 10,089 hrs · 8,604 cycles

FLIGHT 1824, IAH - PHL - NR 1 BLEED LEAK MESSAGE ON EICAS AS WE CLIMBED THRU FL 200. THE AIRCRAFT ALSO HAD THE NR 2 PACK AND APU ON MEL. THIS REQUIRED A NORMAL DESCENT TO 10,000FT. THE CABIN OXYGEN MASK WERE NOT DEPLOYED. FLIGHT DIVERTED TO DFW AND LANDED WITHOUT INCIDENT. EMS ALSO MET THE AIRCRAFT UPON ARRIVAL DUE TO PASSENGER COMPLANITS OF BEING UNCOMFORTABLY WARM. MAINTENANCE FOUND DUCT CLAMP LOOSE IN NR 1 PYLON, TIGHTENED CLAMP. LEAK CHECK GOOD RUN ENGS & PACKS FOR 10 MINS NO FAULTS NOTED. OK FOR SERVICE.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 9,782 hrs · 8,372 cycles

BOS - R2 DOOR REQUIRES SERVICING. MAINTENANCE SERVICED DOOR PER AMM 52-12-51-03.

Part: TAB — BROKEN (NLG DOOR) · airframe 9,419 hrs · 8,035 cycles

FLIGHT 1465, PHL-ATL - LANDING NOSE DOOR OPEN EICAS. MAINTENANCE FOUND LEFT AFT NOSE GEAR DOOR LINKAGE LOCK TABS BROKEN & ROD ENDS BACKED OFF. REPLACED LOCK TABS 7 ADJUSTED AFT NOSE DOOR PER 32-22-03 ALSO NLG POSITION SENSOR ADJ/TEST PER 32-61-13. ALL OPS NORMAL.

Part: VENT — DIRTY (LAVATORY)

BOS - STRONG "BLUE WATER" ODOR IN COCKPIT FROM FRONT LAVATORY. IRRITATING TO EYES. MAINTENANCE REMOVED DUST AND DEBRIS FROM FORWARD LAVATORY AIR EXTRACT VENT. FOUND PLUGGED SOLID.

Part: WARNING SYSTEM — FALSE INDICATION (SPOILER SYS)

FLIGHT 1980, PHL-PVD - PASSING THRU 10,000 FEET THE CREW RECEIVED A SPOILER FAULT EICAS MESSAGE. THE CREW PERFORMED AN UNSUCCESSFUL RESET AND RETURNED TO PHL. THE PHL ATC DECLARED AN EMERGENCY, THE LANDING WAS UNEVENTFUL AND THE AIRCRAFT TAXIED TO THE GATE. MAINTENANCE PERFORMED FIM TASK 27-00-00-810-802A, ALL INDICATIONS ARE GOOD, NO FAULTS WERE NOTED. PERFORMED A RETURN TO SERVICE TASK OF THE FLIGHT CONTROL SYSTEM PER AMM 27-00-00-00-801-A/200, SYSTEM CHECKS GOOD. NO HISTORY FOR PAST 30 DAYS, AIRCRAFT RETURNED TO SERVICE.

Part: PIN — LOOSE (CONNECTOR)

BOS - THE LOWER OVERWING EMERGENCY EXIT DOOR LIGHTS ARE INOPERATIVE. MAINTENANCE REPAIRED A LOOSE PIN CONNECTION AT THE LEFT EMERGENCY OVERWING DOOR AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: UNKNOWN — ODOR (CABIN)

FLIGHT 2132, LGA-BOS - REPORTED AN ACRID ODOR IN THE CABIN AND COCKPIT CAUSING THE CREW AND FLIGHT ATTENDANT'S EYES TO BURN. MAINTENANCE TROUBLESHOOT SYSTEM PER FIM TASK 21-20-00-810-801-A, ISOLATED DOWN TO THE APU BLEED. INSPECTED THE APU COMPARTMENT AND PACK BAYS. RAN THE AIRCRAFT FOR SEVERAL HOURS AND TRIED TO ISOLATE THE ODOR. NO ODOR PRESENT OR BURNING OF EYES. ALL OPERATIONAL CHECKS ARE SATISFACTORY AT THIS TIME, AIRCRAFT RELEASED FOR SERVICE.

Part: SEAT — MALFUNCTIONED (COCKPIT)

CLT - THE FIRST OFFICER'S SEAT WILL NOT STAY IN THE BACK POSITION, IT SLOWLY DRIFTS FORWARD. MAINTENANCE COULD NOT DUPLICATE, THE SEAT RECLINE OPERATES NORMAL.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

PHL - THE FORWARD FLIGHT ATTENDANT FLASHLIGHT BATTERY IS DEAD. MAINTENANCE REPLACED THE BATTERY PER AMM 33-50.

Part: SLIDE — UNSERVICEABLE (PAX DOOR) · airframe 5,170 hrs · 4,237 cycles

PIT - EES - C1 CHECK - AFT PASSENGER DOOR SLIDE ASSEMBLY PACK OPENING PIN CLOSURE STRING BROKEN. REPLACED SLIDE.

Part: BLEED AIR SYS — LEAKING (NR 1 ENGINE) · airframe 339 hrs · 362 cycles

FLIGHT 1212, DFW-PHL: DURING CLIMB, RECEIVED ENGINE 1 FIRE WARNING. SHUT DOWN NUMBER 1 ENGINE AND RETURNED TO FIELD. NO EVIDENCE OF FIRE NOTED. HEAT DAMAGE FROM BLEED LEAK TO ENGINE HARNESSES WAS NOTED. MAINTENANCE FERRIED TO PHL. REPLACED THE NUMBER ONE ENGINE.