N369AT

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 34,746 hrs · 33,253 cycles

ON FLIGHT 4823, CREW REPORTED EMERGENCY PATH LIGHT PLASTIC COVER BROKEN. THE ACFT REMOVED FROM SERVICE. R & R EMERGENCY FLOOD LIGHT ASSY IAW JIC 33-51-24. THE OPS CHECKED SATISFACTORY. THE ACFT RETURNED TO SERVICE.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 34,436 hrs · 32,931 cycles

SERV DOOR EMERGENCY SIGN BROKEN. R & R SERVICE DOOR EMERGENCY SIGN COVER IAW CMM 33-51-27.

Part: SOCKET — BURNED (CABIN LIGHTS) · airframe 34,273 hrs · 32,767 cycles

BURNING ODOR COMING FROM THE AIR CONDITIONING VENTS. R & R BURNED SOCKETS 294 LGB & 231 LGA. OPS CHECKED OK IAW JIC 33-21-23. NO BURNING ODOR NOTICE AT THIS TIME.

Part: BATTERY — INOPERATIVE (MASTER)

AFTER ENG START, MAIN BATTERY CHARGER LIGHT CAME ON. MAIN BATT SHOR 25.5 VOLT. REPLACED MAIN BATTERY IAW WC EX-243182-RAI-10010-006.

Part: BATTERY — DISCHARGED (MAIN) · airframe 34,145 hrs · 32,654 cycles

THE CREW REPORTED THAT AFTER ENGINE START THE MAIN BATTERY CHARGE LIGHT ON (MAIN BATT SHOW 25.5 VOLT). THE ACFT WAS REMOVED FROM SERVICE. REPLACED MAIN BATTERY IAW WORK CARD EX-243185-RAI-10010-006. THE ACFT WS RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (EMERGENCY BATT) · airframe 34,104 hrs · 32,614 cycles

THE CREW REPORTED THEY RECEIVED AN EMERGENCY BATTERY CHARGE FAULT. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY BATTERIES WITH APU AND ENGINE RUNNING AND CHECK WAS OK IAW MM 24-23-00 AND 72-00-00. NO PARTS R & R. THE ACFT WAS RETURNED TO SERVICE.

Part: BRAKE SYS — MALFUNCTIONED

EXCESSIVE BRAKE PRESSURE REQUIRED FOR BRAKES TO WORK ON CAPT'S SIDE. PERFORMED NORMAL BRAKING, OPS TEST IAW MM 32-42-00. FOUND ALL BRAKES WORKING PROPERLY.

Part: LIGHT — BROKEN (CABIN) · airframe 33,957 hrs · 32,460 cycles

F/A REPORTED PROXIMITY LIGHT BROKEN NEXT TO THE GALLEY. THE ACFT WAS REMOVED FROM SERVICE. R & R EMERGENCY LIGHT AT GALLEY AREA JIC 33-51-24 . THE OPS CHECK WAS OK. THE ACFT WAS RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 33,910 hrs · 32,402 cycles

FOR FLIGHT 4845, DURING THE PREFLIGHT INSP FOUND THE AISLE PATH EVACUATION LIGHT BURNED OUT (AROUND ROW NR 3). THE ACFT WAS REMOVED FROM SERVICE. REPLACED FLOOR EMERGENCY LIGHT ON ROW NR 3 IAW MM 33-50-00. PERFORMED OPS CHECK AND FOUND WORKING PROPERLY. THE ACFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 33,868 hrs · 32,366 cycles

DURING THE PREFLIGHT INSP, FOUND THE EXIT SIGN LOCATED AT 2 C/D SEAT INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. INSTALLED EXIT SIGN LOCATED AT SEAT 2 C/D IAW JIC 33-50-00. THE ACFT WAS RETURNED TO SERVICE.

Part: SOCKET — BURNED (CABIN LIGHTS) · airframe 32,956 hrs · 31,323 cycles

ELECTRICAL SMOKE ODOR IN CABIN. AT THIS TIME OPENED MIDDLE TO AFT OVERHEAD BINS, FOUND BURNED LIGHTSOCKET AT OVERHEAD 12AB. REMOVED LIGHT SOCKET AND DEFERRED ON MEL 33-02 AUTH NR 120088-C FIN NR303LGA. CLOSED BINS IAW MM 25-24-21. R & R CEILING LIGHT 12AB BULB SOCKET IAW JIC 33-21-23. THIS ACTION CLEARS MEL 33-02.

Part: NONE — NONE (CABIN PRESSURE) · airframe 32,617 hrs · 30,953 cycles

LIGHTENING STRUCK THE ACFT IN FLIGHT, AS A RESULT THE PRESSURIZATION CABIN ALTITUDE RATE STARTED CLIMBING. (EMERGENCY DECLARED) PERFORMED DETAILED VISUAL INSP AFTER LIGHTENING STRIKE IAW WORK CARD EX-055113-DVI-10000-003 AND PLACED THE AUTO PRESSURIZATION SYS ON MEL, AWAITING COMPLETION OF MEL 21-08 AUTH 100051M-C FOR FURTHER DETAILS. OP'S CHECK AUTO PRESS SYS AND FOUND WORKING PROPERLY IAW AMM JIC 23-31-00 AND ETN NR E2-21-00, MEL CLEARED.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 31,852 hrs · 30,084 cycles

THE EMERGENCY EXIT LIGHT ON THE PASSENGER CABIN ENTRY DOOR IS INOPERATIVE. REMOVED AND REPLACED BROKEN WIRE IAW MM STD PRACTICE 20-42-10 OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,852 hrs · 30,084 cycles

THE EMERGENCY EXIT LIGHT ON THE PASSENGER CABIN ENTRY DOOR IS INOPERATIVE. AWAITING AML PAGE FOR FURTHER DETAILS.

Part: WING — CORRODED (RT WING) · corrosion level 2 · airframe 31,615 hrs · 29,789 cycles

RT WING HAS CORROSION AT RIB 8 BETWEEN STIFFENERS 8-9 UNDER FLAP HINGE FAIRING. COMPLIED WITH SRI DO/TS-0623/10-12890 REF NDT REPORT AMS100121-32 FOR UT AND HFEC RESULTS. NO DEFECTS NOTED AT THIS TIME. COMPLIED WITH EO E2-57MR-365. RT WING LOWER SKIN PNL AT RIB 8 BTW STIFF 8-9 CORROSION BLEND-OUT REPAIR.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 31,615 hrs · 29,789 cycles

CORROSION AROUND RT WING FUEL PUMP CUT-OUT. COMPLIED WITH SRI-DO/TS-OS67/10-12887. RT WING FUEL PUMP CUT-OUT. NO DEFECTS NOTED. COMPLIED WITH SRAS DO/TS-127/08..4458 TO BE INSPECTED IN 2YR INTERVALS. TASK 571402/DVI 10000. OK FOR SERVICE. COMPLIED WITH EO E2-57 MR-364. RT WING LWR SKIN, CORROSION BLEND-OUT REPAIR AT FUEL PUMP CUT-OUT.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 31,615 hrs · 29,789 cycles

CORROSION AROUND LT WING FUEL PUMP CUT-OUT. COMPLIED WITH SRI-DO/TS-0618/10-12888 REF NDT REPORT AMS100121-33 FOR UT & HFEC RESULTS. NO DEFECTS NOTED AT THIS TIME. LT WING SRAS DO/TS-128/08, 4450. AROUND LT WING FUEL PUMP CUTOUT. COMPLIED WITH. OK FOR SERVICE. TO BE INSPECTED IN 2YR INTERVALS TASK571402-DVI-10000. COMPLIED WITH EO E2-57MR-362 LT WING LOWER SKIN CORROSION BLEND OUT AT FUEL PUMP CUT OUT.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 31,615 hrs · 29,789 cycles

LT WING HAS CORROSION AROUND JACK POINT AT RIB 10. COMPLIED WITH SRI-DO/TS-0634/10-1288. REF AMS100121-19. FOR UT VALUES & HFEC RESULTS, NO CRACKS NOTED AT THIS TIME. COMPLIED WITH ATR-SRAS DO/TS-129/08.4451. COMPLIED WITH AE-EO E2-57MR-363 TDMI OPENED FOR 2 YR INTERVAL INSP FOR NEW CORROSION AND HFEC INSP AT 10000 FC, DUE AT 36161 FC.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,615 hrs · 29,789 cycles

AREAS OF CORROSION AT FRAME 17 BETWEEN LT OTBD SEAT TRACKS ( 7 AREAS MARKED IN RED) ON THE FLOORBEAM. R & R FRAME SEGMENT IAW SRM 53-00-00, FIG 435.

Part: NONE — NONE (NONE) · airframe 31,053 hrs · 29,131 cycles

CAPT REPORTED EMERGENCY LIGHTS WILL ARM.

Part: POWER SUPPLY — FAILED (EMEGENCY LIGHTS) · airframe 31,053 hrs · 29,131 cycles

EMERGENCY EXIT LIGHTS IN THE COCKPIT REMAINS ILLUMINATED. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY FIN 73WL IAW JIC 33-51-21. OPERATIONAL CHECK PERFORMED AND FOUND SATISFACTORY AT THIS TIME IAW JIC 33-50-00.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 30,093 hrs · 28,020 cycles

LANDING GEAR WILL NOT RETRACT AND GIVING LOW PRESSURE WARNING. RETURN BACK TO STATION (SJU). ITEM DEFERRED ON MEL NR 29-01 AUTH NR 030060-C. ON 03-16-09 AT SJU (TAT: 30151.44 TAC: 28084), REMOVED AND REPLACED ACW DRIVEN HYD PUMP AS PER JIC NR 29-10-00. THIS ACTION CLEARS MEL NR 29-01 AUTH NR 030060-C.

Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 30,093 hrs · 28,020 cycles

LANDING GEAR WILL NOT RETRACT AND GIVING LOW PRESSURE WARNING. RETURN BACK TO STATION (SJU). GREEN HYDRAULIC SYSTEM ACW DRIVEN PUMP DEFERRED ON MEL NR 29-01 AUTH NR030060-C.

Part: HYDRAULIC LINE — FAILED (HYHDRAULIC SYS) · airframe 28,500 hrs · 26,368 cycles

GREEN SYSTEM LOW LEVEL LOST GREEN SYSTEM PRESSURE. REMOVED AND REPLACED HYDRAULIC HOSE, OPS CHECK GOOD IAW JIC 29-00-00.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 28,413 hrs · 26,303 cycles

SEVERAL FLOOR PATH EMERGENCY LIGHTS STAYS ON WHILE SWITCH TURNED OFF. REMOVED AND REPLACED EMERGENCY POWER SUPPLY FIN NR 43WL IAW JIC NR 33-51-21. OPS CK OK.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 28,241 hrs · 26,161 cycles

R/T INTERCOSTAL BETWEEN FRAME 36-38 CORRODED. RT INTERCOSTAL REPLACED AS PER SRM 51-25-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,241 hrs · 26,161 cycles

FOUND FLOORBEAM 39 CORRODED. FLOORBEAM 39 REPAIRED IAW SRM 53-00-00 FIG 436.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,241 hrs · 26,161 cycles

FOUND FLOORBEAM 39 CORRODED. FLOORBEAM 39 REPAIRED IAW SRM 53-00-00 FIG 436.

Part: FRAME — CORRODED (FUSELAGE) · airframe 28,241 hrs · 26,161 cycles

FRAME 39 BETWEEN STRINGER 21L-21R CORRODED. FRAME 39, BETWEEN STRINGER 21L-21R REPAIRED IAW SRM 53-61-40 FIG 415.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 28,241 hrs · 26,161 cycles

RT INTERCOSTAL BETWEEN FRAME 36-38 CORRODED. RT INTERCOSTAL REPLACED AS PER SRM 51-25-01.

Part: LAMP — FAILED (EMERGENCY LIGHTS) · airframe 28,207 hrs · 26,132 cycles

PASSENGER STAIR EMERGENCY FLOOD LIGHT IS INOP. REMOVED AND INSTALLED ENTRANCE DOOR EMERGENCY LIGHT AS PER MM 33-51-00.

Part: LAMP — BROKEN (EMERGENCY LIGHT) · airframe 27,515 hrs · 25,495 cycles

LOWER EMERGENCY EXIT SIGN ON SERVICE DOOR BROKEN. REMOVED AND REPLACED LIGHT BULBS AND EMERGENCY EXIT SIGN COVER IAW JIC NR 33-51-24. PERFORMED OPT CK IAW JIC NR 33-50-00 AND FOUND WORKING PROPERLY.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 27,426 hrs · 25,418 cycles

EMERGENCY FLOOR LIGHT AT PASSENGER SEAT 8B HAS BEEN PULLED OUT FROM ITS PROTECTIVE PLASTIC STRIP GUARD COVER. MAINTENANCE PERSONNEL REPOSITIONED PROTECTIVE PLASTIC STRIP GUARD COVER ON EMERGENCY LIGHT BULB AT ROW 8B AS PER STANDARD PRACTICE. PERFORMED OPERATIONAL CHECK AS PER ATR 72-AMM 33-51-00.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 27,275 hrs · 25,254 cycles

EMERGENCY LIGHTS CAME ON DURING TAXI. WILL NOT RESET. UNABLE TO EXTINGUISH LIGHTS. REMOVED AND REPLACED BATTERY PACK AT PWR SUPPLY FIN NR 61WL IAW JIC NR 33-51-21. OP CK OK.

Part: WINDSHIELD — CRACKED (COCKPIT)

WHILE IN CRUISE AT 11,000 FTS RT WINDSHIELD STARTED CRACKING. RETURNED TO POS FOR CHECK. REPLACED F/O WINDSHIELD IAW JIC 56-11-00, FOUND WORKING PROPERLY WITH NO LEAK. (K)

Part: BLEED VALVE — MALFUNCTIONED (LT ENGINE)

LT ENGINE EXCEEDS TQ AND ITT DURING TAKE-OFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED NR 1 ENGINE INTERCOMPRESSOR BLEED VALVE IAW JIC 72-01-30, PERFORMED OPT FOUND SYSTEM WORKING PROPERLY. (K)

Part: CONNECTOR — DIRTY (PRESSURE XMITTER)

WHILE IN CLIMB, ENGINE OIL WARNING LIGHT IN FLIGHT. ENGINE INDICATION KEPT COMING BACK WHILE REDUCING POWER. SHUTDOWN ENGINE AS PRECAUTIONARY MEASURE. RETURNED TO THE SJU AIRPORT. CLEANED RIGHT ENGINE OIL PRESSURE TRANSMITTER AND OIL LOW PRESSURE SWITCH CONNECTOR PLUGS. PERFORMED OPS CHECK AS PER ATR 72 JIC 79-34-00 AND FOUND SATISFACTORY. (M)

Part: HARNESS — DEFECTIVE (RT MLG)

ON TAKEOFF, LANDING GEAR HANDLE STUCK ON DOWN POSITION. UNABLE TO RETRACT THE GEARS. AIRCRAFT RETURNED TO THE AIRPORT. REPLACED MLG HARNESS IAW MM. OPS CHECK FOUND GEAR RETRACTING PROPERLY. (K)

Part: COMPUTER — MALFUNCTIONED (TE FLAPS)

DURING APPROACH, CREW REPORTED A FLAP UNLOCK INDICATION. EMERGENCY DECLARED. AIRCRAFT LANDED SAFELY. VISUAL INSPECTION AND OPERATIONAL CHECK PERFORMED AND FOUND NO DISCREPANCIES. MULTIFUNCTION COMPUTER RERACKED. FUNCTIONAL CHECK FLIGHT CONDUCTED AND FOUND SATISFACTORY. (K)

Part: MFC — FAILED (NR 1)

WHILE IN CRUISE, ALL THREE GEARS UNSAFE LIGHT ILLUMINATED ON THE LOWER PANEL, ALONG WITH A LOW PRESSURE INDICATION ON THE HYDRAULIC GREEN SYSTEM. UPPER PANEL HAD NO UNSAFE INDICATION. UNABLE TO DUPLICATE DISCREPANCY. AS A PRECAUTIONARY PROCEDURE, THE MULTIFUNCTION COMPUTER NR 1 WAS REPLACED. (M)

Part: PANEL — CORRODED (LT WING)

LEFT FEEDER TANK ACCESS PANEL NR 622CT HAS CORROSION ON IT TRANSFERRED FROM CRIC NR 7858. BLENDED CORROSION IAW ATR SRM 53-14-12. INSTALLED NEW LEFT FEEDER TANK PANEL IAW ATR72 AMM/JIC 57-00-00 OAC. (M)

Part: FLOORBEAM — CORRODED (FRAME 39)

RIGHT AFT CARGO Z-MEMBER BY FLOORBEAM 39 CORRODED AROUND PLATE NUTS. BLENDED CORROSION AND FOUND TO BE BEYOND LIMITS IAW SRM 53-00-00. REMOVED AND INSTALLED SEAT TRACK IAW ATR72 51-25-01. (M)

Part: SEAT TRACK — CORRODED (FRAME 29)

LEFT AFT INBOARD SEAT TRACK CORRODED. BLENDED OUT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND INSTALLED SEAT TRACK IAW EO NR E9 5300-013 R4. (M)

Part: SEAT TRACK — CORRODED (FRAME 29)

RIGHT AFT INBOARD SEAT TRACK CORRODED. BLENDED OUT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND INSTALLED SEAT TRACK IAW EO NR E9 5300-013 R4. (M)

Part: SEAT TRACK — CORRODED (FRAME 36)

RIGHT F/A SEAT TRACK CORRODED. BLENDED CORROSION AND FOUND TO BE BEYOND LIMITS IAW SRM 53-00-00. REMOVED AND INSTALLED SEAT TRACK IAW EO NR E9-5300-013. (M)

Part: SEAT TRACK — CORRODED (FRAME 29)

RIGHT AFT INBOARD SEAT TRACK CORRODED. BLENDED OUT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND INSTALLED SEAT TRACK IAW EO NR E9 5300-013 R4. (M)

Part: PANEL — CORRODED (RT WING)

RIGHT FEEDER TANK PANEL NR 622CT HAS CORROSION ON IT TRANSFERED FROM CRIC NR 7873. BLENDED CORROSION IAW ATR SRM 53-14-12. INSTALLED NEW RIGHT FEEDER TANK PANEL IAW ATR72 AMM/JIC 57-00-00 OAC. (M)

Part: SEAT TRACK — CORRODED (FRAME 36)

RIGHT F/A SEAT TRACK CORRODED. BLENDED CORROSION AND FOUND TO BE BEYOND LIMITS IAW SRM 53-00-00. REMOVED AND INSTALLED SEAT TRACK IAW EO NR E9-5300-013. (M)

Part: FUEL PROBE — CORRODED (LT WING)

TOP OF LEFT WING, HIGH LEVEL SENSOR HAS FLOORING PAINT AND CORROSION. BLENDED CORROSION IAW ATR SRM 53-14-12. REMOVED AND REPLACED LEFT MAIN OUTBOARD TANK PROBE PER JIC 28-42-72 RA/10000-001. (M)

Part: FLOORBEAM — CORRODED (FRAME 36)

FLOORBEAM, FRAME 36, DAMAGED. REMOVED DAMAGED FLOORBEAM. REPLACED SECTION IAW SRM 53-00-00 FIG 435. (M)

Part: FLOORBEAM — CORRODED (FRAME 38)

FRAME 38, CORRODED AROUND NTU PLATED. BLENDED CORROSION AND FOUND TO BE BEYOND LIMITS IAW SRM 53-00-00. REMOVED AND INSTALLED FLOORBEAM SECTION AND PERFORMED SPLICE IAW SRM 53-00-00 FIG 435. (M)

Part: SEAT TRACK — CORRODED (FRAME 36)

LEFT F/A SEAT TRACK CORRODED. BLENDED OUT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND INSTALLED SEAT TRACK IAW EO NR E9 5300-013 R4. (M)

Part: SEAT TRACK — CORRODED (FRAME 29)

LEFT AFT SEAT TRACK CORRODED. BLENDED OUT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND INSTALLED SEAT TRACK IAW EO NR E9 5300-013 R4. (M)

Part: PANEL — CORRODED (WING BOX)

CENTER WING DRY BAY PAREL NR 52105 HAS CORROSION, UNIT TRANSFERED FROM CRIC NR 7860. BLENDED CORROSION IAW ATR SRM 53-14-12. INSTALLED NEW CENTER WING DRY BAY PANEL IAW ATR 72 AMM/JIC 57-00-00 OAC. (M)

Part: PANEL — CORRODED (LT WING)

LEFT OVERWING REFUELING PANEL HAS CORROSION. INSTALLED NEW PANEL IAW ATR72 AMM/JIC 57-00-00 OAC. (M)

Part: CHANNEL — CORRODED (FRAME 36-38)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR CHANNEL BETWEEN FRAME 36 AND 38 CORRODED AND THE FLOOR CHANNEL BETWEEN FRAME 38 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH FLOOR CHANNELS IAW SRM 51-25-02. A/C WAS RETURNED TO SERVICE. (M)

Part: CHANNEL — CORRODED (FRAME 38-39)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR CHANNEL BETWEEN FRAME 36 AND 38 CORRODED AND THE FLOOR CHANNEL BETWEEN FRAME 38 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH FLOOR CHANNELS IAW SRM 51-25-02. A/C WAS RETURNED TO SERVICE. (M)

Part: SKIN — DENTED (FRAME 5/6)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE NOTED DENT IN FUSELAGE. LEFT SIDE 36 INCHES BELOW STATIC PORT BETWEEN FRAME 5 AND 6. MAINTENANCE INSTALLED A PATCH IAW SRM 53-00-00 PAGE 410. A/C WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THAT THE FLOORBEAM 38 WAS CORRODED OUT OF LIMITS. MAINTENANCE REPAIRED FLOORBEAM 38 IAW SRM 53-00-00 PAGE 498. A/C WAS RETURNED TO SERVICE. (M)

Part: SKIN — DENTED (FRAME)

SAW - DURING CPCP-1 INSPECTION, MAINTENANCE NOTED DENT IN FUSELAGE. LEFT SIDE AT FRAME 2 AND STRINGER 11. MAINTENANCE REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 422. A/C WAS RETURNED TO SERVICE. (M)

Part: DRAIN TRACK — CORRODED (SERVICE DOOR)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR DRAIN TRACK AND THE SERVICE DOOR DRAIN TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH DRAIN TRACK IAW SRM 51-25-03. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: DRAIN TRACK — CORRODED (PAX DOOR)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR DRAIN TRACK AND THE SERVICE DOOR DRAIN TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH DRAIN TRACK IAW SRM 51-25-03. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (CARGO DOOR)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR SILL PLATE AND THE CARGO DOOR SILL PLATE WERE CORRODED OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED BOTH SILL PLATES IAW SRM 51-25-03. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (CARGO DOOR)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR SILL PLATE AND THE CARGO DOOR SILL PLATE WERE CORRODED OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED BOTH SILL PLATES IAW SRM 51-25-03. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SWITCH — FAILED (NLG)

HOU - FLT 3547 - INBOUND TO HOU FOR LANDING, WHEN GEAR WAS SELECTED DOWN FOR LANDING THE NOSE GEAR GREEN LIGHT FLASHED INTERMITTENT ON THE LOWER INDICATOR PANEL. THE UPPER INDICATION PANEL INDICATED ALL GEAR DOWN AND LOCKED. PILOT CONTINUED TO HOU AND LANDED SAFELY. MEL ITEM WAS ISSUED AGAINST THE LANDING GEAR FOR RETURN FLIGHT FOR DFW. DFW MAINTENANCE REPLACED THE NOSE LANDING GEAR UPLOCK BOX SWITCH AND PERFORMED GEAR RETRACTION TEST SATISFACTORILY. A/C WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - FLT 3626 - EMERGENCY LIGHTS WILL NOT EXTINGUISH. RAI BATTERY PACK AT 61 WL PER JIC, PERFORMED OPERATIONAL CHECK SATISFACTORILY. A/C RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

GRR - FLT 4051 - FORWARD EMERGENCY LIGHT INOP. REPLACED BATTERY PACK AND OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BULB — FAILED (CABIN)

DFW - FLT 3724 - EMERGENCY LIGHT AT ROW 5 BURNED OUT. DEFERRED AS PER MEL 33-22 AUTH NR 060023. RAI'D BULB AT ROW 5. PERFORMED OPS CHECK IAW JIC 33-50-00, CLEARED MEL. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN EEL)

DFW - FLT 3605 - EMERGENCY FLOOR LIGHTING SYSTEM INOP. REMOVED AND INSTALLED EMERGENCY BATTERY PACK 73WL. OPS CHECK PERFORMED SATISFACTORILY. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: TRANSMITTER — FAILED (NR 2 ENGINE)

CRP - FLT 3739 - NR 2 ENGINE OIL PRESSURE WENT TO ZERO, LOW OIL PRESSURE LIGHT ON, NO ASSOCIATED MASTER WARNING. SHUT DOWN NR 2 AND RESTARTED PER CREW EMERGENCY PROCEDURE. COULD NOT DUPLICATE REPLACED TRANSMITTER. OPS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. (X)

Part: EEL WIRE — BROKEN (PASSENGER DOOR)

ORD - FLT 4187 - CREW REPORTED PASSENGER STAIRS EMERGENCY LIGHT INOP. MAINTENANCE REPAIRED BROKEN WIRES UNDER TOP STEP. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: EEL WIRE — BROKEN (PASSENGER DOOR)

ORD - FLT 4187 - CREW REPORTED PASSENGER STAIRS EMERGENCY LIGHT INOP. MAINTENANCE REPAIRED BROKEN WIRES UNDER TOP STEP. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SCREWS — BROKEN (ANTI-SKID VALVE)

CRP - FLT NR 3857 - BLUE AND GREEN HYDRAULIC SYSTEM LOW LEVEL LIGHT ON INFLIGHT, LANDING GEAR EXTENDED MANUALLY, ZERO FLAPS LANDING. CFR CALLED OUT. (M)

Part: EEL CONNECTOR — BROKEN (PAX DOOR)

DFW - CABIN DOOR, TOP STEP CONNECTOR HAS ALL WIRES PULL OUT WITH ASSOCIATED EMERGENCY LIGHT INOPERATIVE. INSTALLED NEW CONNECTOR. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ADC — FAILED (NR 1 ENG)

DFW - FLT 3807 - AFTER TAKEOFF, LT ENGINE TORQUE SURGED 15 PERCENT. PILOTS RETURNED TO DFW AND LANDED WITHOUT INCIDENT. RAI LT DAT SENSOR AND NR 1 ADC. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 3,520. (X)

Part: PROP CONTL UNIT — MALFUNCTIONED (NR 2 ENGINE)

DFW - FLT 3835 - NR 2 ENGINE ONLY ACHIEVED 70 PERCENT TORQUE ON TAKEOFF ROLL. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. CHANGED FEATHERING CONTROL UNIT. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: EEL — MALFUNCTIONED (NR 1 ENGINE)

DFW - FLT 3831 - NR 1 ENGINE LOST TORQUE ON TAKEOFF ROLL DOWN TO 50 PERCENT. REMOVED AND REPLACED NR 1 EEC, PERFORMED GROUND RUNS. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: NH SENSOR — MALFUNCTIONED (LT ENG)

GRR - FLT 4194 - NR 1 ENGINE TQ SURGED 30 TO 35 PERCENT AFTER TAKEOFF. AIRCRAFT CONTINUED TO DESTINATION WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND INSPECTED SENSOR, SYSTEM OPS CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. (M)