N348AE

Part: IGNITER — FAILED (NR 1 ENGINE) · airframe 33,415 hrs · 379,395 cycles

WHILE WAITING TO BE PARKED AT GATE, NR 1ENGINE SHUTDOWN WITH 450 LBS FUEL. HAD FUEL TRUCK FILL TANK AND NR 1 ENGINE WOULD NOT START. R & R BOTH IGNITERS FOR NR 1 ENGINE. OPS CHECKED NORMAL. MADE SEVERAL STARTS AND TOOK ENGINE TO POWER, WORKED NORMAL IAW MM 72-01-20.

Part: SOCKET — BURNED (CABIN LIGHTS) · airframe 32,966 hrs · 36,780 cycles

ELECTRICAL BURNING ODOR AROUND MID-CABIN SECTION. FOUND UPPER PAX LIGHT AT SEAT 9AB SOCKET BURNED AND ARCHING , R & R SOCKET IAW AWM 20-43-13, OPS CHECK GOOD IAW JIC 33-20-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,740 hrs · 36,475 cycles

DURING THE PREFLIGHT INSP FOUND THE RT FWD EMERGENCY EXTRIOR FLOOD LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. CLEANED AND REPOSITIONED THE RT FWD EMERGENCY FLOOD LIGHT BULB AND ASSY. THE OPS CHECK IAW EX-335000 OPT-10000-001 WAS GOOD. NO PARTS R & R. THE ACFT WAS RETURNED TO SERVICE.

Part: FDAU — BURNED (E/E BAY) · airframe 32,485 hrs · 36,127 cycles

STRONG ELECTRICAL ODOR AND SMOKE FELT DURING CLIMB AT 7,000 FT. DIVERTED AND EMERGENCY WAS DECLARED. DURING INSPECTION OF LT AVIONICS RACK FOUND FDAU ON SHELF 81VU BURNED. REMOVED AND REPLACED FDAU IAW ATR 72 JIC 31-31-81. PERFORMED FDAU OPS CHECK IAW ATR JIC 31-31-00-OPT-10000. ALSO REMOVED AND REPLACED THE THREE AXIS ACCELEROMETER IAW ATR 72 JIC 31-31-21 AS PRECAUTIONARY MEASURE. AWAITING AML FROM DFW FOR PARTS REPLACEMENT INFOMATION.

Part: CONTROLLER — FAILED (NR 2 PROPELLER) · airframe 32,116 hrs · 35,657 cycles

(EMERGENCY DECLARED) DURING CRUISE FLIGHT, NR 2 ENGINE PROPELLER FEATHERED AND GOT EEC NR 2 FAULT, IAW CREW DEBRIF, CREW SHUTDOWN NR 2 ENGINE PRECAUTIONARY IAW MFG PROCEDURES. NR 2 ENG PCU REPLACED IAW MM 61-22-00, OPT CHECK AND LEAK CHECK GOOD, ALSO REFERENCE NRWC 348-DFW-00062 AND NRWC 348-DFW-00075. REF. NRWC 348-DFW-00081: FOUND LOWER RT OIL TRANSFER TUBE BORE OVERSIZED OUT OF LIMITS. ENGINE REQUIRES REPLACEMENT. REMOVED AND REPLACED NR 2 ENGINE IAW ATR WORKCARD EX-ATR-72-RAI-002 OPS CHECK LEAK CHECK NORMAL.

Part: SKIN — CORRODED (LT WING) · airframe 31,148 hrs · 34,403 cycles

AN AREA OF CORROSION WAS FOUND AT LT WING LOWER SURFACE AT T/E BETWEEN RIBS 11-12. AWAITING COMPLETION OF EO E2-57MR-390 AND AML PAGE FOR FURTHER DETAILS.

Part: SKIN — DAMAGED (LT WING) · corrosion level 2 · airframe 31,148 hrs · 34,403 cycles

LT WING LOWER SKIN PANEL AT T/E AT RIB 9. TEMPORARY CORROSION BLEND OUT REPAIR IAW AE-E0 NR E2-57MR-388, REF AMS-NDT-REPORT 8130-3 NR 100505-78.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 31,148 hrs · 34,403 cycles

ACCOMPLISHED TDMI 3485102C8 RT WING AT RIB 13 LWR SURFACE FWD HAS CORROSION TEMPORARY REPAIR AT NEXT C-CHECK PENDING FINAL REPAIR EMBODIMENT OR REPAIR LIFE LIMIT 5 MONTHS IAW AE EO E2-57MR-389. REF AMS-NDT-REPORT 8130-3 NR 100505-73. THIS ACTION CLOSES.

Part: SPAR — DAMAGED (LT WING) · corrosion level 2 · airframe 31,148 hrs · 34,403 cycles

INSTALLED REPAIR DOUBLER AT RT WING LWR REAR SPAR IAW AE EO E2-57MR-395. REF ART W/O 11951 NRWC 334519, ART FORM L -004-2R1 AND AMS NDT REPORT 100514-13. THIS ACTION CLOSES TDMI 348570218.

Part: STRUCTURE — DAMAGED (LT WING) · corrosion level 2 · airframe 31,148 hrs · 34,403 cycles

REPAIRED RT WING ELECTRO FUEL PUMP SURROUNDING AREA IAW EO E2 57-MR-385 REF AMS NDT REPORT 8/30 3H100505-70.

Part: SKIN — DAMAGED (FLT WING) · corrosion level 2 · airframe 31,148 hrs · 34,403 cycles

LT WING LOWER SKIN PANEL JACK PAINT AT RIB 10 TEMPORARY CORROSION BLEND OUT REPAIR IAW EO E2-57MR-387 REF AMS NDT REPORT 8130-3 NR 100505-72. THIS ACTION CLOSES TDMI.

Part: SKIN — CORRODED (LT WING) · airframe 31,148 hrs · 34,403 cycles

AN AREA OF CORROSION WAS FOUND AT LT WING LOWER SKIN AT T/E AT RIB 9. AWAITING COMPLETION OF EO E2-57MR-388 AND AML PAGE FOR FURTHER DETAILS.

Part: SKIN — UNKNOWN (LT WING) · airframe 31,148 hrs · 34,403 cycles

LT WING SKIN AROUND RIB 10 JACK PAD. AWAITING COMPLETION OF EO E2-57MR-387 AMD AML PAGE FOR FURTHER DETAILS.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 31,148 hrs · 34,403 cycles

ACCOMPLISHED TDMI 348570288 LT WING LWR SKIN PANEL AT TE BTW RIBS 11-12 TEMPORARY CORROSION BLEND OUT REPAIR. EO E2-57MR-390, REF AMS-NDT-REPORT 8130-3 NR 100505-75.

Part: PRESSURE BLKHD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,148 hrs · 34,403 cycles

FWD PRESSURE BULKHEAD APPEARS TO HAVE CORROSION AT CONTACT POINTS 5 AND 8. C/W SRI ATR DO/TS 2482/10-13438 AND AE EO E2-53MR-252. REF AMS NDT- REPORT 8130-3 NR 100505-71.

Part: SKIN — CORRODED (RT WING) · airframe 31,148 hrs · 34,403 cycles

AN AREA OF CORROSION WAS FOUND AT RT WING LOWER SKIN AT L/E BETWEEN RIBS 12-13. AWAITING COMPLETION OF EO E2-57MR-389 AND AML PAGE FOR FURTHER DETAILS.

Part: SKIN — CORRODED (RT WING) · airframe 31,148 hrs · 34,403 cycles

RT WING LOWER SKIN REAR SPAR AT RIB 12 CORROSION TITANIUM DOUBLER PERMANENT REPAIR. AWAITING COMPLETION OF EO E2-57MR-395 AND AML PAGE FOR FURTHER DETAILS.

Part: STRUCTURE — CORRODED (RT WING) · airframe 31,148 hrs · 34,403 cycles

DISCREP: REF AML 434552/4 - RT WING ELECTRO FUEL PUMP SURROUNDING AREA HAS CORROSION. AWAITING COMPLETION OF EO E2-57MR-385 AND AML PAGE.

Part: BRAKE — WEAK (LEFT) · airframe 31,007 hrs · 34,217 cycles

SIDE LT BRAKE PEDAL IS TOO LOW BEFORE BRAKING ACTION. PERFORMED OPS TEST TO BRAKING SYS FOUND OK IAW JIC 32-42-00. NORMAL BRAKING.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 30,658 hrs · 33,736 cycles

RT WING AT RIB 13 LOWER SURFACE FWD SKIN HAS CORROSION. TEMPORARY REPAIR, REMOVED CORROSION AND BLENDED OUT OF SKIN IAW SRM 51-21-58. PERFORMED A PERMANENT REPAIR AREA UNDER THIS EO E2-57 MR-360 AT NEXT SCHEDULED C-CK. PENDING FINAL REPAIR EMBODIMENT OR REPAIR LIFE LIMITS MONTH TACT. 33736. TDMI 3485702CB.

Part: SKIN — CORRODED (RT WING) · airframe 30,658 hrs · 33,736 cycles

RT WING AT RIB 13 LOWER SURFACE FWD SKIN HAS CORROSION. AWAITING NRWC FOR DETAILS.

Part: SKIN — CORRODED (RT AILERON) · airframe 30,658 hrs · 33,736 cycles

CORROSION FOUND ON RT AILERON SKIN. AWAITING NRWC FOR DETAILS.

Part: SKIN — CORRODED (RT WING AILERON) · corrosion level 2 · airframe 30,658 hrs · 33,736 cycles

CORROSION FOUND BY DQC ON RT AILERON SKIN. NRWC NR 282327 FOR MORE INFORMATION. PERFORMED CORROSION CUT-OUT REPAIR IAW STRUCTURAL REPAIR INSTRUCTION DO/TS-164/10-12805.

Part: FUEL TANK — CONTAMINATED (WING) · airframe 30,613 hrs · 33,667 cycles

NR 2 ENG FAILED WHILE CRUISING. EMERGENCY DECLARED AND LANDED. DURING TROUBLESHOOTING FOUND NR 2 ENG, WING TANK AND FEEDER TANK JET PUMP WITH DEBRIS. ACCOMPLISHED INSP OF FEEDER TANK AND ENG JET PUMPS IAW EO NR E9-2800-001R1. ALSO REMOVED AND REPLACED NR 2 ENG FUEL HEATER FILTER IAW MM NR 72-01-40. NO LEAKS NOTED.

Part: FUEL CELL — CONTAMINATED (WING) · airframe 30,613 hrs · 33,667 cycles

NR 2 ENG FAILED WHILE CRUISING, EMERGENCY DECLARED AND LANDED. DURING TROUBLESHOOTING FOUND NR 2 ENG, WING TANK AND FEEDER TANK JET PUMP WITH DEBRIS. ACCOMPLISHED INSP OF FEEDER TANK AND ENG JET PUMPS IAW EO NR E9-2800-001R1. ALSO REMOVED AND REPLACED NR 2 ENG FUEL HEATER FILTER IAW MM NR 72-01-40. NO LEAKS NOTED.

Part: SOCKET — BURNED (CABIN LIGHT) · airframe 30,398 hrs · 33,374 cycles

STRONG ELECTRICAL BURNING SCENT AT MID-CABIN ABEAM THE OVERHEADS. ITEM DEFERRED IAW MEL NR33-2 AUTH NR 110039-C. REMOVED OVERHEAD LIGHT AT 10CD DO TO BAD SOCKET ENTER IN MIC SHEET. MEL CLEARED AT MIA ON 11-12-09: REMOVED AND REPLACED SOCKET AT CEILING LIGHT 10CD IAW AWM NR 33-21-01. OPS CHK GOOD.

Part: SOCKET — FAILED (CABIN LIGHTS) · airframe 30,398 hrs · 33,374 cycles

STRONG ELECTRICAL BURNING ODOR AT MID-CABIN A BEAM THE OVERHEADS. ITEM DEFERRED IAW MEL NR33-2 AUTH. NR110039-C. REMOVED OVERHEAD LIGHT AT 10CD DO TO BAD SOCKET. ENTER IN MIC SHEET.

Part: LAMP — FAILED (EMERGENCY LIGHTS) · airframe 30,398 hrs · 33,374 cycles

EMERGENCY EXIT LIGHT ON MAIN CABIN ENTRY DOOR (STEP-LIGHT) IS INOPERATIVE. REMOVED AND INSTALLED EMERGENCY GROUND ILLUMINATION FLOOD LIGHT ON MAIN CABIN DOOR IAW JIC NR 33-51-24.

Part: PACKING — FAILED (FUEL NOZZLE) · airframe 30,270 hrs · 33,221 cycles

UPON LANDING STRONG FUEL ODOR IN COCKPIT AND CABIN. AFTER PARKING FUEL WAS POURING OUT OF THE BOTTOM OF LEFT NR 1 ENGINE. REMOVED AND REPLACED NR 9 FUEL NOZZLE TRANSFER TUBES PACKINGS IAW JIC NR 73-13-61-RAI-10000-004 AND P&W MM 72-01-40. LEAK CHECK GOOD.

Part: ENGINE — FAILED · airframe 28,941 hrs · 31,599 cycles

OIL PRESSURE FLUCTUATING, LOUD BANG AND ENGINE SHUTDOWN. ENGINE REMOVAL IN PROGRESS, AWAITING AML PAGE FOR FURTHER DETAILS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,854 hrs · 30,194 cycles

LT INBD SEAT TRACK CORRODED BTW FR 29-36. REPLACED SEAT TRACK BTW FR 29-36 AS PER SRM 51-25-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,854 hrs · 30,194 cycles

LT SEAT TRACK BTW FR 36-39 CORRODED. REPLACED SEAT TRACK BTW FRAME 36-39 IAW SRM 51-25-04.

Part: HINGE FITTING — CORRODED (AILERON TAB) · airframe 27,854 hrs · 30,194 cycles

HINGE FITTINGS OF RT AILERON TRIM TAB ARE CORRODED. RT AILERON TRIM TAB HINGE FITTINGS NR 1-3-4 REPLACED IAW SRM 51-25-03.

Part: STIFFENER — CORRODED (FUSELAGE) · airframe 27,854 hrs · 30,194 cycles

LT UPPER BONDING SPOT BTW STIFFENER ON BL 187.5 AND BL 350 FIND CORRORED. LT UPPER BONDING SPOT BTW STIFFENER ON BL 187.5 AND BL 350 CORROSION REPAIRED IAW SRM 53-11-10 FIG 403.

Part: RETAINER — CORRODED (RT WING TE FLAP) · airframe 27,854 hrs · 30,194 cycles

RT OUTB FLAP RIB 19 BRUSH RETAINER IS CORRODED. RT OUTB FLAP RIB 19 BRUSH RETAINER REPLACED IAW SRM 51-25-03.

Part: HINGE — CORRODED (AILERON) · airframe 27,854 hrs · 30,194 cycles

(4) HINGE FITTINGS OF LT AILERON TRIM TAB ARE CORRODED. LT AILERON TRIM TAB HINGE FITTING REPLACED NR 2 AND 33 IAW SRM 51-25-03.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 27,211 hrs · 29,411 cycles

NR 1 ENGINE OIL PRESSURE FLUCTUATING BETWEEN 50 AND 40 PSI. PRECAUTIONARY ENGINE SHUT DOWN PERFORMED. EMERGENCY DECLARED AND AIRCRAFT LANDED UNEVENTFULLY AT RSW. REMOVED AND REPLACED HYDRAULIC PUMP AND OVERSPEED GOVERNOR IAW MM NR 61-12-63 AND NR 61-23-61. PERFORMED OPS RUN CHECK. OPS CHECK GOOD.

Part: FAN — ODOR · airframe 26,996 hrs · 29,160 cycles

BURN ODOR IN CABIN, EARLY IN GROUND EXTRACT FAN WAS REPORTED MAKING LOUD NOISE. ITEM DEFERRED ON MEL 21-06 AUTH 090137D-C. REMOVED AND REPLACED AIR EXTRACTION FAN IAW JIC 21-23-21. THIS ACTION CLEARS MEL 21-06. PERFORMED FLIGHT COMPARTMENT AND CABIN AIR DISTRIBUTION OPERATIONAL CHECK. NO BURN ODOR NOTICED IAW 21-22-00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 26,684 hrs · 28,744 cycles

INTERIOR EMERGENCY EXIT LIGHT (UNDER LT EMERGENCY EXIT WINDOW) BURNED OUT. REMOVED AND REPLACED LAMPS AS PER MM NR 33-51-00 AND FOUND WORKING PROPERLY AT THIS TIME.

Part: LIGHT — FAILED (CABIN) · airframe 26,404 hrs · 28,414 cycles

MAIN PAX DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AS PER JIC #33-51-24. OPERATIONAL CHECK GOOD.

Part: FUSE — BLOWN (BATTERY PACK)

CREW NOTICED LOWER EXIT LIGHT AT SERVICE DOOR INOPERATIVE. REPLACED FUSE AT POWER SUPPLY FIN 62WL AND BULB AT LOWER ASSY FOR EMERGENCY LIGHT AT SERVICE DOOR IAW JIC 33-50-00, OPS CHECKS GOOD. (K)

Part: WINDSHIELD — CRACKED (COCKPIT)

WHILE IN CRUISE, CAPT SIDE WINDSHIELD CRACKED. AC DIVERTED. EMERGENCY DECLARED. AC LANDED SAFELY. REMOVED AND REPLACED CAPT WINDSHIELD AND PERFORMED PRESSURIZATION LEAK OK AND NO LEAK NOTED IAW MM. (K)

Part: WINDSHIELD — CRACKED (COCKPIT)

WHILE IN CLIMB, THE FO WINDSHIELD CRACKED. AIRCRAFT RETURNED TO AIRPORT. REPLACED FO WINDSHIELD ASSY. (K)

Part: TORQUE SENSOR — INOPERATIVE (LT ENGINE)

DURING TAKEOFF, LEFT ENGINE TORQUE INDICATOR NOT INCREASING. ABORTED TAKEOFF. REPLACED ENGINE TORQUE SENSOR. (M)

Part: INDICATOR — FAILED (TE FLAPS)

ON APPROACH WHEN SELECTED 30 DEGREES OF FLAPS IT STAYED IN THE UP POSITION. REPLACED FLAP INDICATOR. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

MIA - MAINTENANCE REPORTED SEVERAL FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY UNIT 61WL. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: WIRE — LOOSE (CABIN)

DFW - FLT 3624 - MAINTENANCE SAFETY TEAM FOUND ONE FLOOR PROXIMITY EMERGENCY LIGHT BETWEEN ROWS 7 AND 8 TO BE INOPERATIVE. MAINTENANCE FOUND A LOOSE WIRE FOR THE FLOOR LIGHT. WIRE WAS RECONNECTED, AN OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

MAINTENANCE REPORTED AN EMERGENCY LIGHT BY THE FORWARD CABIN DOOR TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNIT 62WL. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: PAN — CORRODED (COCKPIT)

SAW - DURING MBV-1 INSPECTION, MAINTENANCE REPORTED THE FIRST OFFICERS SEAT FLOOR PAN CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR PAN IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: DAMPENER — MALFUNCTIONED (TAIL)

MIA - FLT 5385 - AFTER TAKEOFF AND YAW DAMPNER ENGAGED Y/D DISCONNECTED BY ITSELF TWICE, THEN CREW NOTICED RUDDER WOULD STICK IN CENTER POSITION. REMOVED AND REPLACED RUDDER DAMPNER IAW JIC 27-71-41. OPS CHECK GOOD. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

NAS - FLT 5320 - ON CLIMB-OUT, FLIGHT ATTENDANT REPORTED AN ELECTRICAL BURN SMELL IN THE CABIN. THE BURN SMELL WAS REPORTED AS COMING FROM READING LIGHT 16B. AFTER TURNING OFF THE READING LIGHTS ODOR DISSIPATED. TRANSFORMER WAS FOUND BURNED, POWER SOURCE WAS DISCONNECTED. REMOVED AND REPLACED POWER SUPPLY IAW CMM 33-25-21. (M)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,319 hrs · 16,851 cycles

MIA - FLT 5353 - DISCOVERED FLOOR PROXIMITY LIGHT AT ROW 8 INOPERATIVE. LIGHT WAS PUT ON MEL. MAINTENANCE C/W OPERATIONAL CHECK IAW ATR MM 33-50-00 AND COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT WAS RETURNED TO SERVICE. (X)

Part: FIRE WARNING — FALSE INDICATION (NR 1 ENGINE)

DFW - FLT 3646 - WHLE ON TAXI, FIRE INDICATION ON NR 1 ENGINE, ENGINE SHUT DOWN, FIRE HANDLE PULLED. AIRCRAFT RETURNED TO BLOCKS. PERFORMED INSPECTION OF NR 1 ENGINE AND AREA, NO INDICATION OF FIRE. REPLACED FIRE BOTTLE, OPS CHECK GOOD. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT FORWARD INBOARD, LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD, LEFT AFT CARGO, RIGHT AFT INBOARD, RIGHT AFT OUTBOARD, RIGHT FLIGHT ATTENDANT, RIGHT MIDDLE OUTBOARD, RIGHT MIDDLE INBOARD, RIGHT FORWARD INBOARD, AND RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW ENGINEERING ORDER E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: RELAY — FAILED (CABIN)

HOU - FLT 3618 - SEVERAL EMERGENCY LIGHTS WOULD NOT EXTINGUISH. REMOVED AND REPLACED EMERGENCY LIGHT RELAY 12LF AND OPERATIONAL CHECKED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ZEE — CORRODED (FUSELAGE)

DURING MBV-2 INSPECTION, FOUND RIGHT AFT ZEE MEMBER BETWEEN FRAMES 39 AND 42 CORRODED. MAINTENANCE REMOVED AND REPLACED THE ZEE MEMBER IAW SRM 51-25-03. AIRCRAFT RETURNED TO SERVICE. (M)

Part: TRANSFORMER — FAILED (SEAT 6CD)

DFW - FLT 3625 - AIRCRAFT RETURNED TO DFW DUE TO ODOR OF SMOKE IN THE CABIN. EMEGENCY WAS DECLARED. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED SHORTED OUT TRANSFORMER AT SEAT 6CD PSU PANEL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: HYD PUMP — FAILED (GREEN HYD SYSTEM)

DFW - FLT 3737 - AFTER TAKEOFF, NOSE GEAR FAILED TO RETRACT TO THE UP AND LOCKED POSITION. FLIGHT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED GREEN SYSTEM HYDRAULIC PUMP. EXTENSION AND RETRACTION CHECKS WERE SATISFACTORY COMPLETED. A/C RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING ROUTINE CHECK, FOUND RIGHT FORWARD EXTERIOR EMERGENCY LIGHT INOP. RAI'D LIGHT ASSEMBLY, PERFORMED OPS CHECKS. RETURNED AIRCRAFT TO SERVICE. (M)

Part: POWER SUPPLY — FAILED (CABIN)

CRP - FLT 3858 - EMERGENCY LIGHTS IN REAR PORTION OF AIRCRAFT WOULD NOT EXTINGUISH. REPLACED EMERGENCY POWER SUPPLY AND BATTERY PACK AT 73WL. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPERATOR CONTROL NR 97ZZZX2008. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

CRP - FLT 3858 - EMERGENCY LIGHTS IN REAR PORTION OF AIRCRAFT WOULD NOT EXTINGUISH. REPLACED EMERGENCY POWER SUPPLY AND BATTERY PACK AT 73WL. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPERATOR CONTROL NR SIMA9701092.

Part: PUMP — FAILED (BLUE HYD SYST)

DFW - FLT 3750 - EN ROUTE TO DFW, PILOT REPORTED THE BLUE SYSTEM HYDRAULIC LOW LEVEL INDICATOR ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT AFTER DECLARING EMERGENCY. MAINTENANCE INSPECTED SYSTEM AND FOUND PUMP TO HAVE INTERNAL DAMAGE AND WAS LEAKING OVERBOARD. PUMP REPLACED IAW THE J.I.C. AND OPS CHECK AND LEAK CHECK WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X)

Part: SENSOR — FAILED (NR 2 ENGINE)

TUL - FLT 3734 - RIGHT ENGINE TORQUE FLUCTUATION OF 23 PERCENT IN CRUISE, IN-FLIGHT SHUT DOWN BY CREW. REPLACED 1.8 SENSOR, GROUND RUN GOOD. AIRCRAFT RETURNED TO SERVICE. (X)