N440AM

Part: WARNING LIGHT — ILLUMINATED (BATTERY CHARGER) · airframe 28,846 hrs · 32,935 cycles

EMERGENCY BATTERY CHARGER FAULTED. REPLACED EMERGENCY BATTERY CONTACTOR 42PA IAW AMM 24-31-11. OPS CHECKED IAW W/C EX 343100-OPT 10020-002. FOUND SYS WORKING PROPERLY.

Part: SWITCH — OUT OF POSITION (EMERGENCY LIGHT) · airframe 28,535 hrs · 32,496 cycles

TOP FRONT AND BACK EMERGENCY LIGHT IN CABIN STAY ON. REPOSITIONED SWITCH OF EMERGENCY LIGHT 9LE. PERFORMED OPT WORKING PROPERLY IAW JIC 33-20-00.

Part: SIGN — ILLUMINATED (CABIN) · airframe 28,490 hrs · 342,432 cycles

EMERGENCY SIGN LOCATED FWD AND AFT IN THE TOP STILL ILLUMINATED ALL THE TIME. PERFORMED OPS CHECK TO EMERGENCY LIGHTS IAW EX-335000-OPT-10000-001.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 26,623 hrs · 30,190 cycles

CORROSION FOUND ON LT WING T/E ON LWR SURFACE AT RIB 4. COMPLIED WITH SRI DO/TS 308/10-13617. REF NDT REPORT AMS 100603-27 FOR HFEC, ROTO & UI INSP NO DEFECTS FOUND ACCOMPLISHED EO E2-57-MR-397 COMPLIED WITH SRM DO/TS-3081/10-5841. SUPP TASK INSP VI FOR CRACKS AROUND FASTENERS IN BLENDED AREA EVERY 1000 FC.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,623 hrs · 30,190 cycles

6 CONTACT POINTS ON FWD BULKHEAD HAS SURFACE CORROSION. COMPLIED WITH SRI DO/TS-3031 /10 -13625 REF NDT REPORT AMS 100603-24 FOR HFEC & VT RESULTS. NO DEFECTS NOTED AT THIS TIME ACCOMPLISHED EO E2-53MR-254 C/W SRAS DO/TS-3031/10-5830 DVI OF BLENDED AREA EVERY 2 YEARS FOR NEW CORROSION. FURTHER CLEANED LIGHT SURFACE CORROSION ON 3EA CONTACT POINTS IAW SRM 51-21-42 NO MAT'L LOSS NOTED. NO FURTHER ACTION REQ.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 26,623 hrs · 30,190 cycles

CORROSION FOUND ON LT WING T/E ON LWR SURFACE BTW RIBS 7-8. COMPLIED WITH SRI DO/TS-3114/10 136SG. REF NDT REPORT AMS 100603-26 FOR HFEC & UT INSP NO DEFECTS NOTED ACCOMPLISHED EO E2-57MR-398 COMPLIED WITH SRM. SUPPLEMENTARY INSP TASK US INSP FOR CRACKS AROUND FASTENERS IN BLENDED AREA EVERY 1000 FC.

Part: WINDOW — DEPARTED (COCKPIT) · airframe 25,028 hrs · 28,281 cycles

CAPT FWD SIDE WINDOW BLOW OUT. AWAITING AML/NRWC PAGE FOR FURTHER DETAILS.

Part: WINDOW — DEPARTED (COCKPIT) · airframe 25,028 hrs · 28,280 cycles

DURING CABIN PRESS CHECK ON F/O WINDOW, CAPT SIDE WINDOW BLEW OFF FROM FRAME. REMOVED AND REPLACED CAPT SIDE WINDOW IAW JIC NR 56-12-00-RAI-10000. AWAITING AML FOR PARTS INFO.

Part: WINDSHIELD — DEPARTED (COCKPIT) · airframe 25,028 hrs · 28,280 cycles

DURING CABIN PRESS CHECK ON F/O WINDOW, CAPT FWD SIDE WINDOW BLEW OFF FROM FRAME. REMOVED AND REPLACED CAPT FWD SIDE WINDOW IAW JIC NR56-12-00-RAI-10000.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 22,736 hrs · 25,531 cycles

EMERGENCY LIGHTS STAYS STAY ON WHEN THE SWITCH IS ON THE ARM POSITION. REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY AT 73WL, THE EMERGENCY BATTERY LIGHT PACK AT 62WL, OPS CHECK NORMAL IAW MM 33-51-00. OPS CHECKS NORMAL AS PER MM 25-60-00.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 22,308 hrs · 25,030 cycles

DEVELOPED CRACK IN F/O'S WINDSHIELD DURING DEPARTURE CLIMBING (FROM SXM) THROUGH 4,000 FT FOR 10,000 FT. REMOVED AND REPLACED F/O WINDSHIELD AS PER JIC NR 56-11-00.

Part: BATTERY PACK — INOPERATIVE

DURING PREFLIGHT, THE CREW NOTED THE PAX DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT PACK ASSEMBLY. (K)

Part: ODOR — DETECTED (CABIN)

WHILE TAXIING, BURNING ODOR NOTICED BY THE FLIGHT CREW. VISUALLY INSPECTED ALL OVERHEAD BINS WIRING BUNDLES AND FOUND NO EVIDENCE OF BURNING. OPERATIONAL CHECK OF ALL SYSTEMS PERFORMED AND FOUND SATISFACTORY. (K)

Part: WINDOW — CRACKED (COCKPIT)

DURING CRUISING, THE CAPTAIN WINDSHIELD CRACKED. REPLACED CAPTAIN WINDSHIELD ASEMBLY. (M)

Part: WINDOW — CRACKED (COCKPIT)

DURING CRUISING, THE CAPTAIN WINDSHIELD CRACKED. REPLACED CAPTAIN WINDSHIELD ASSEMBLY. (M)

Part: SENSOR — MALFUNCTIONED (RT ENGINE)

DURING APPROACH, RIGHT ENGINE TORQUE FLUCTUATED BETWEEN 20 PERCENT AND UP TO 80 PERCENT UNABLE TO CONTROL ENGINE WAS SHUTDOWN. REPLACED TORQUE SENSOR. (M)

Part: HMU — FAULTY (NR 2 ENGINE)

DURING CLIMB-OUT, THE NR 2 ENGINE TQ FLUCTUATED UP TO 117 PERCENT. ALL OTHER PARAMETERS FOLLOWED THE TQ. THE CREW COULD NOT CONTROL THE TQ SO ENGINE WAS SHUT DOWN IN FLIGHT. EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO AIRPORT SAFELY WITH NO OTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE EEC, HMU, AND THE FUEL PUMP IAW ATR MM. OPERATIONAL AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

CRP - DURING PREFLIGHT, AFTER TESTING EMERGENCY LIGHTS, THE FORWARD HALF WOULD NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY UNIT BATTERY PACK AT 43WL. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE THE LEFT INTERCOSTALS BETWEEN FRAMES 38 AND 40 CORRODED, AND THE RIGHT INTERCOSTALS BETWEEN FRAMES 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTALS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20011177. (M)

Part: TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR AND PAX DOOR DRAIN TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE DRAIN TRACKS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE THE LEFT INTERCOSTALS BETWEEN FRAMES 38 AND 40 CORRODED, AND THE RIGHT INTERCOSTALS BETWEEN FRAMES 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTALS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURNIG CPCP-2 INSPECTION MAINTENANCE REPORTED THE RIGHT FLIGHT ATTENDANT AND LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURNIG CPCP-2 INSPECTION MAINTENANCE REPORTED THE RIGHT FLIGHT ATTENDANT AND LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE THE LEFT INTERCOSTALS BETWEEN FRAMES 38 AND 40 CORRODED, AND THE RIGHT INTERCOSTALS BETWEEN FRAMES 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTALS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20011177. (M)

Part: SILL — CORRODED (FUSELAGE)

DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR SILL PLATE WEB CORRODED BETWEEN FRAMES 36 AND 39. MAINTENANCE REMOVED AND REPLACED THE WEB IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: INTERCOSTAL — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE THE LEFT INTERCOSTALS BETWEEN FRAMES 38 AND 40 CORRODED, AND THE RIGHT INTERCOSTALS BETWEEN FRAMES 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTALS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20011177. (M)

Part: GUSSET — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT GUSSET BETWEEN FRAMES 40 AND 41 CORRODED. MAINTENANCE REMOVED AND REPLACED THE GUSSET IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36, 38, 39 AND 40 CORRODED. MAINTENANCE REMOVED AND REPLACED FLOORBEAMS 36, 38, AND 39 IAW SRM 51-25-02. MAINTENANCE REPAIRED FLOORBEAM 40 IAW SRM 53-00-00 FIGURE 436. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20011175. (M)

Part: SILL — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR WEB BETWEEN FRAMES 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE WEB IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR AND PAX DOOR DRAIN TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE DRAIN TRACKS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20011174. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36, 38, 39 AND 40 CORRODED. MAINTENANCE REMOVED AND REPLACED FLOORBEAMS 36, 38, AND 39 IAW SRM 51-25-02. MAINTENANCE REPAIRED FLOORBEAM 40 IAW SRM 53-00-00 FIGURE 436. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20011175. (M)

Part: ANGLE — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE RIGHT ZEE MEMBER BETWEEN FRAMES 39 AND 44 CORRODED. MAINTENANCE REMOVED AND REPLACED THE ZEE MEMBER IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36, 38, 39 AND 40 CORRODED. MAINTENANCE REMOVED AND REPLACED FLOORBEAMS 36, 38, AND 39 IAW SRM 51-25-02. MAINTENANCE REPAIRED FLOORBEAM 40 IAW SRM 53-00-00 FIGURE 436. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAMS 36, 38, 39 AND 40 CORRODED. MAINTENANCE REMOVED AND REPLACED FLOORBEAMS 36, 38, AND 39 IAW SRM 51-25-02. MAINTENANCE REPAIRED FLOORBEAM 40 IAW SRM 53-00-00 FIGURE 436. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20011175. (M)

Part: SOCKET — BURNED (CABIN)

MCO - FLT 5262 - CREW REPORTED AN ELECTRICAL BURNING SMELL IN FLIGHT. AIRCRAFT RETURN TO MCO. MAINTENANCE FOUND AN OVERHEAD FLUORESCENT TUBE SOCKET DAMAGED. SOCKET WAS REMOVED AND REPLACED IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT — LOOSE (CABIN)

FLL - FLT 5400 - FOUND SEAT AT 14CD CAME OUT OF SEAT TRACKS. MAINTENANCE INSPECTED SEAT ASSEMBLY AND SEAT TRACKS AND FOUND NO DISCREPANCY. SEAT WAS REINSTALLED IAW ATR MM AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: PSU — FAILED (ROW 5A)

MIA - FLT 5386 - PASSENGER SERVICE UNIT ABOVE SEAT 5A EXCESSIVELY HOT WITH ASSOCIATED SMOKE AND ODOR. TURNED OFF MAIN SWITCH FOR ALL PASSENGER READING LIGHTS, HEAT, SMOKE AND ODOR DISSIPATED. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED PASSENGER SERVICE UNIT ABOVE SEAT 5A. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT MIDDLE INBOARD AND OUTBOARD, THE LEFT AFT INBOARD AND OUTBOARD, AND THE RIGHT MIDDLE INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT MIDDLE INBOARD AND OUTBOARD, THE LEFT AFT INBOARD AND OUTBOARD, AND THE RIGHT MIDDLE INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT MIDDLE INBOARD AND OUTBOARD, THE LEFT AFT INBOARD AND OUTBOARD, AND THE RIGHT MIDDLE INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ZEE — CORRODED (FRAME 39-40)

SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT AFT ZEE MEMBER BETWEEN FRAMES 39 AND 40 CORRODED. REMOVED AND REPLACED THE ZEE MEMBER IAW 51-25-03. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (PAX DOOR)

SAW - DURING CPCP-8 INSPECTION, FOUND THE PASSENGER DOOR SILL PLATE AND DRAIN TRACK CORRODED. REMOVED AND REPLACED THE PASSENGER DOOR SILL PLATE AND DRAIN TRACK IAW SRM 51-25-01 AND 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-8 INSPECTION, FOUND FLOORBEAM 36 HAD AN EXTRA HOLE DRILLED INTO IT. REPAIRED THE FLOORBEAM IAW SRM 53-00-00 FIGURE 435. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT MIDDLE INBOARD AND OUTBOARD, THE LEFT AFT INBOARD AND OUTBOARD, AND THE RIGHT MIDDLE INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SUPPORT — CORRODED (FRAME 38-39)

SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT FLOOR SUPPORT CHANNEL BETWEEN FRAMES 38 AND 39 CORRODED. REMOVED AND REPLACED THE CHANNEL IAW SRM 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: DRAIN TRACK — CORRODED (PAX DOOR)

SAW - DURING CPCP-8 INSPECTION, FOUND THE PASSENGER DOOR SILL PLATE AND DRAIN TRACK CORRODED. REMOVED AND REPLACED THE PASSENGER DOOR SILL PLATE AND DRAIN TRACK IAW SRM 51-25-01 AND 51-25-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: VALVE — FAILED (LT ENGINE)

CRP - FLT 3674 - SMOKE IN THE COCKPIT. TURNED OFF NR 1 BLEED AD SMOKE CLEARED. DIVERTED TO CRP. FERRIED AIRCRAFT TO DFW FOR REPAIR. REMOVED AND REPLACED NR 1 P2.5 AND P3 AIR SWITCHING VALVE. GROUND RUN CHECKS GOOD. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (E/E COMPT)

FLT 9724 - CRP - ELECTRICAL SMOKE INDICATION ON CWP ILLUMINATED. FERRIED AIRCRAFT TO DFW FOR REPAIR. REMOVED AND REPLACED AVIONICS EXTRACTION FAN AND SMOKE DETECTOR. PERFORMED OPERATIONAL TESTS AND TEST FLIGHT WITH NO FURTHER SMOKE INDICATIONS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (E/E BAY)

CRP - FLT 3739 - ELECTRICAL SMOKE INDICATION ON CWP ILLUMINATED. REMOVED AND REPLACED FORWARD ELECTRONICS RACK SMOKE DETECTOR. OPERATIONAL TESTS NORMAL. NO FURTHER SMOKE INDICATIONS NOTED. (M)

Part: FAN — FAILED (E/E COMPT)

FLT 9724 - CRP - ELECTRICAL SMOKE INDICATION ON CWP ILLUMINATED. FERRIED AIRCRAFT TO DFW FOR REPAIR. REMOVED AND REPLACED AVIONICS EXTRACTION FAN AND SMOKE DETECTOR. PERFORMED OPERATIONAL TESTS AND TEST FLIGHT WITH NO FURTHER SMOKE INDICATIONS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (BS 39)

SAW - DURING CPCP-4 INSPECTION, FOUND FLOORBEAM 39 CORRODED AROUND THE NUT PLATE ATTACH POINT ON THE RIGHT SIDE. REPAIRED FLOORBEAM. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (SERVICE DOOR)

SAW - DURING CPCP-4 INSPECTION, FOUND THE SERVICE DOOR SILL PLATE CORRODED. REMOVED AND REPLACED SILL PLATE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, FOUND THE LEFT AFT INBOARD AND THE FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED BOTH SEATS TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, FOUND THE LEFT AFT INBOARD AND THE FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED BOTH SEATS TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ORD - FLT 4342 - EMERGENCY EXIT LIGHT PAX ENTRANCE INOP. REPAIRED BROKEN WIRE AND REPLACED ASSY IAW STANDARD MX PRACTICE. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

DFW - FLT 3506 - WITH BATTERY MASTER SWITCH OFF AND EMERGENCY LIGHTS SELECTED ON AT FLIGHT ATTENDANT PANEL, SEVERAL FLOOR EMERGENCY LIGHTS ARE OUT AND AFT EXIT SIGN ABOVE FLIGHT ATTENDANT PANEL IS INOPERABLE. WITH BATTERY MASTER ON, ALL LIGHTS ARE NORMAL. INSTALLED BATTERY EMERGENCY LIGHT AT 73 WL. AIRCRAFT RETURNED TO SERVICE. (X)

Part: T1.8 SENSOR — SHORTED (NR 1 ENGINE)

DFW - FLT 3599 - DURING TAKEOFF, NR 1 ENGINE TORQUE INDICATION SURGED. AIRCRAFT RETURNED TO DFW. REMOVED AND INSPECTED T1.8 SENSOR. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 391.0. (X)

Part: EEL — DEFECTIVE (PAX DOOR)

ORD - FLT NR 4021 - CREW REPORTS PASSENGERS EMERGENCY EXIT DOOR LIGHT INOP. MAINTENANCE REPLACED LIGHT ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. (M)