N270AT

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 34,281 hrs · 40,019 cycles

EMERGENCY EXIT LIGHT IN AFT SERVICE DOOR INOPERATIVE. REMOVED EMERGENCY GROUND ILLUMINATION FLOOD LIGHT 70WL IAW JIC 33-51-24.

Part: CONTROL VALVE — FAILED (MLG) · airframe 34,278 hrs · 40,015 cycles

WHEN LANDING GEAR LEVER SELECTED UP, THE RT MAIN GEAR DID NOT RETRACT. WE HAD RED UNLK AND THE GREEN ARROW ON BOTH UPPER AND LOWER PANELS. R & R LG SELECTOR CONTROL VALVE. OPS AND LEAK CHECK GOOD IAW ATR JIC VAR32-31-51 RAI 10000 002 AND PERFORMED SEVERAL EXT AND RETRACTION OPS CKS IAW ATR JIC 32-31-00 OPT 10000 OPS CHECK WAS GOOD EACH TIME.

Part: ACTUATOR — LEAKING (RT MLG) · airframe 34,239 hrs · 39,964 cycles

RIGHT MLG DID RETRACT WITH GEAR LEVER UP. HAD GREEN AND RED ON RT MLG BOTH UPPER & LOWER PANELS. FOUND RT MLG UNLOCKING ACTUATOR LEAKING. R & R RT MLG UNLOCKING ACTUATOR IAW JIC 32-11-53. OPS & LEAK CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,239 hrs · 39,964 cycles

FLOOR PROXIMITY EMERGENCY LIGHT ON FWD 2ND ROW HAS ONE LIGHT INOPERATIVE. ITEM DEFERRED IAW MEL 33-29 AUTH 080188D-C. ENTERED ONTO MIC SHEET.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 34,184 hrs · 39,891 cycles

ABORTED TAKEOFF DUE TO NR 2 ENGINE NOT MAKING THE CORRECT TORQUE. IDLE REVERSE AND MINIMAL BRAKING BUT LT MAIN TIRES WENT FLAT. PERFORMED LT/RT ENGINE GROUND OPS CHECK AND FOUND TORQUE VALUES WITHIN RANGE IAW ATR MM 72-00-00 ERU10040. LT ENGINE TQ: 83.5 PERCENT RT ENG TQ: 83.5 PERCENT.

Part: UNKNOWN — ODOR (CABIN)

THE CREW NOTICED A STRONG ODOR OF SMOKE IN THE COCKPIT, THE NR2 ENGINE ITT ROSE TO 715 DEGREES C, THE DUCT TEMPERATURE ON THE CABIN WENT TO 100 DEGREES C .THE F/A ADVISED SMOKE IN THE CABIN. THE CREW DECLARED AN EMERGENCY. THE ACFT WAS REMOVED FROM SERVICE. (OPEN)

Part: CONTROLLER — INOPERATIVE (AUTO TEMP)

CREW NOTICED A STRONG ODOR OF SMOKE IN THE COCKPIT. THE NR 2 ENGINE ITT ROSE TO 715 DEGREES C. THE DUCT TEMP ON THE CABIN WENT TO 100 DEGREES C. THE F/A ADVISED OF SMOKE IN THE CABIN. GROUND RAN ACFT DURING T/S FOUND RT AUTO TEMP CONTROL INOPERATIVE. MANUAL OK. NORMAL INDICATION, NO ODOR IN ACFT.

Part: CONTROLLER — FAILED (AUTO TEMP) · airframe 341,493 hrs · 39,842 cycles

THE CREW REPORTED AN ODOR THEN NOTICED SMOKE IN THE CABIN. THE CREW RECEIVED OVERHEAT INDICATIONS ON THE TEMPERATURE CONTROLLER. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. GROUND RAN AIRCRAFT DURING T/S FOUND RIGHT AUTO TEMP CONTROL INOPERATIVE, MANUAL OK. NORMAL INDICATION NO ODOR IN AIRCRAFT MEL 21-24 AUTH 070238D-C CAT C. REMOVED AND REPLACED CABIN SKIN TEMP SENSOR AS PER JIC 21-61-13, OPS CHECKED GOOD

Part: VALVE — LEAKING (ENGINE)

ON APPROACH, THE CAPTAIN REPORTED A SMOKE ODOR IN COCKPIT & QUICKLY AFTER THAT NR 1 F/A REPORTED SMOKE IN CABIN. THE COCKPIT CREW COMPLETED THE EMERGENCY PRODCURES CHECK LIST. F/A CALLED COCKPIT BACK TO REPORT THE SMOKE HAD BECOME THICKER AND AN EMERGENCY EVACUATION WOULD BE NEEDED UPON LANDING. CAPTAIN DECLARED AN EMERGENCY LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. FOUND CROSSFEED VALVE LEAKING AND R & R IAW JIC 36-11-21. OPS CHECKED GOOD. ALSO FOUND NR 2 RECIRC FAN INOP, REF ITEM NR 2 FOR C/A. NO OTHER DEFECTS NOTED AT THIS TIME. REF ITEM NR 4 FOR FCF.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 34,100 hrs · 39,777 cycles

THE CREW REPORTED UPON LANDING, THE ACFT VEERED SHARPLY TO THE RIGHT. FULL RUDDER DEFLECTION DID NOT KEEP DIRECTIONAL CONTROL. NOSE WHEEL STEERING WAS USED TO KEEP AIRPLANE ON THE RUNWAY. THE ACFT WAS ALSO BANKED TO THE LEFT 20' WHILE TAXING. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. CHECKED TIRE PRESSURES ALL OK, VISUALLY CHECKED FLIGHT CONTROLS NO DEFECT NOTED JIC 32-41-00. NO PARTS R & R. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,094 hrs · 39,768 cycles

DURING PREFLIGHT CHECK, FOUND THE EMERGENCY BATTERY CHARGER FAULT LIGHT ILLUMINATED DURING TAXI OUT. THE ACFT WAS REMOVED FROM SERVICE. R & R THE EMERGENCY BATTERY IAW EX-243185-RAI-10020-002. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 33,821 hrs · 39,400 cycles

AFT RT EXTERIOR EMERGENCY LIGHT INOP. R & R POWER SUPPLY FIN 73WL IAW JIC 33-51-21. OPT FOUND GOOD IAW W/C EX-335000-10000-001.

Part: ACM — ODOR (NR 1) · airframe 32,962 hrs · 38,287 cycles

DURING CLIMBOUT NR 1 PACK EMITTED ODOR, THEN DUCT TEMP WENT TO 45. R & R NR1 PACK ACM OPS CHECKS GOOD IAW JIC 21-51-52 MEL RESTORED.

Part: BRAKE SYS — FAILED (MLG) · airframe 32,423 hrs · 37,581 cycles

LOST BRAKES PARKING. C/A AWAITING AML PAGE FOR FURTHER DETAILS.

Part: BRAKE ASSY — UNKNOWN (MLG) · airframe 32,423 hrs · 37,581 cycles

LOST BRAKES PARKING. PROBLEM RELATED TO LOSS OF POWER SEE LGPG 347364 PERFORMED BREAKING TEST IAW JIC 32-42-00, OPS TEST OK.

Part: UNKNOWN — SMOKE (CABIN) · airframe 32,307 hrs · 37,427 cycles

SMELL OF ELECTRICAL SMOKE IN CABIN AND FLIGHT DECK, SMOKE COMING FROM AREA OF 90VU. AWAITING AML PAGE FOR FURTHER DETAILS.

Part: STATIC INVERTER — HOT (ZONE 100) · airframe 32,307 hrs · 37,428 cycles

R & R NR2 STATIC INVERTER IAW JIC 24-21-81 RAI 10000-001.

Part: FIRE WARNING — FALSE ACTIVATION (NR 1 NACELLE) · airframe 32,264 hrs · 37,376 cycles

DURING TAXI FOR TAKEOFF NR 1 ENG FIRE WARNING ACTIVATED, WHEN THE ENGINE WAS SHUTDOWN, THE INDICATION WENT OUT. PERFORMED DVI OF THE FIRE DETECTION SYS IAW JIC 26-12-61 DVI 10000 - PERFORMED IDLE RUN. ALL SYS NORMAL AT THIS TIME. NO DEFECTS FOUND. (THE CAPT DID NOT DECLARED AND EMERGENCY WITH ATC BUT CRASH FIRE CAME TO THE ACFT, EVERYTHING IS SAFE).

Part: FIRE WARNING — ILLUMINATED (NR 1 NACELLE) · airframe 32,264 hrs · 37,376 cycles

DURING TAXI FOR TAKOFF, NR 1 ENG FIRE WARNING ACTIVATED, WHEN ENG WAS SHUTDOWN, THE INDICATION WENT OUT. EMERGENCY DECLARED. PERFORMED DVI OF ENGINE FIRE DETECTION SYS IAW JIC 26-12-61 DVI10000 - PERFORMED IDLE RUN. ALL SYS NORMAL AT THIS TIME. NO DEFECTS FOUND.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 31,035 hrs · 35,632 cycles

F/O FRONT WINDSHIELD CRACKED IN FLIGHT. REMOVED AND REPLACED F/O FRONT WINDSHIELD. OPS CHECK GOOD. NO LEAKS NOTED.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 31,035 hrs · 35,632 cycles

F/O WINDSHIELD CRACKED IN CRUISE. AWAITING AML PAGE FOR FURTHER DETAILS.

Part: DAU — FAILED (ENGINE) · airframe 30,497 hrs · 35,028 cycles

ELECTRICAL ODOR IN COCKPIT UPON ENGINE SHUTDOWN. REMOVED AND INSTALLED FDAU IAW JIC NR 31-31-81-RAI-10000-003.

Part: LIGHT — FAILED (CABIN) · airframe 30,234 hrs · 34,701 cycles

FOUND EMERGENCY LIGHT AT BOTTOM SERVICE DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AND PERFORMED OPERATIONAL CHECK IAW AMM NR 33-50-00.

Part: BRAKE SYS — MALFUNCTIONED · airframe 29,210 hrs · 33,348 cycles

CAPT REPORTED BRAKE PROBLEMS. CAPT RT BRAKE AND F/O LT BRAKE INOP. AWAITING AML PAGE FOR DETAILS.

Part: BRAKE ASSY — INOPERATIVE (MLG) · airframe 29,210 hrs · 33,348 cycles

CAPT REPORTED BRAKE PROBLEMS. CAPT RT BRAKE AND F/O LT BRAKE INOP. AWAITING AML PAGE FOR DETAILS.

Part: BRAKE — WEAK (MLG) · airframe 29,206 hrs · 33,347 cycles

NO PEDAL BRAKE UPON LANDING EITHER SIDE. AWAITING AML PAGE FOR DETAILS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,196 hrs · 33,344 cycles

FLOORBEAM AT FR 36 CORRODED. CORROSION ON FLOORBEAM FR 36 REPAIRED IAW SRM 53-00-00 FIG 435.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,196 hrs · 33,344 cycles

CORROSION FOUND ON LT O/B SEAT TRACK BTW FR 29-35. REPLACED LT O/B SEAT TRACK BTW FR 29-35 IAW SRM 51-25-04.

Part: PLATE — CORRODED (FUSELAGE) · airframe 29,196 hrs · 33,344 cycles

CORROSION FOUND UNDER THE PLATE BTW FR 42-43, BL O. PLATE AT FR 42-43 BL O REPAIRED IAW SRI-DO/TS-1616/08-10077 AND EO NR E2-53MR-195.

Part: SKIN — CORRODED (FUSELAGE) · airframe 29,196 hrs · 33,344 cycles

ON INTERNAL TAIL BUMPER LOWER SURFACE AT FR 39, BTW STGR 21L TO 21R, CORRODED AROUND THE FASTENERS. SKIN REPLACED ON INTERNAL TAIL BUMPER, LWR SURFACE AT FR 39 BTW STRG 21L TO 21R IAW SRM 51-25-04.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 29,196 hrs · 33,344 cycles

RT FWD CARGO CREASE BEAM LOWER CHORD CORRODED ON BTW FR 13-17. REPLACED RT FWD CARGO CREASE BEAM LOWER CHORD IAW SRM 51-25-01, 51-25-03 AND 51-24-04.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · airframe 29,196 hrs · 33,344 cycles

RT 2 FLOOR CORRODED. RT ZEE FLOOR REPLACED IAW SRM 51-25-03.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 29,128 hrs · 33,282 cycles

SEVERAL FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY 43WL IAW AMM JIC 33-51-21. OPS CHECKED OK IAW MM 33-50-00.

Part: PRESSURE SWITCH — FAILED (LANDING GEAR) · airframe 29,129 hrs · 33,283 cycles

RT MAIN GEAR FAILED TO RETRACT AFTER TAKEOFF. UPON TROUBLE SHOOTING FOUND GREEN LOW PRESSURE INDICATION, RAI SWITCH 12GNA, LEAK CHECKED. PERFORMED LG EXTENSION RETRACTION IAW JIC 32-31-00. NO FAULTS NOTED AT THIS TIME.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 28,615 hrs · 32,691 cycles

EMERGENCY LIGHTS FROM CABIN STAY ON ALL THE TIME (HALF OF THEM). REPLACED AND TESTED EMERGENCY BATTERY POWER SUPPLY 73WL AS PER MM 33-51-21 AND FOUND WORKING PROPERLY.

Part: CONTROL SWITCH — INOPERATIVE (TE FLAPS)

WHILE IN TAXIING, FLAPS DID NOT EXTEND TO 15 DEGREES POSITION FOR TAKEOFF. AIRCRAFT RETURNED TO GATE. REPLACED FLAP CONTROL SWITCH IAW JIC 27-51-12. PERFORMED OP TEST, SYSTEM WORKING PROPERLY. (M)

Part: INDICATION SYS — MALFUNCTIONED (RT ENGINE)

RIGHT ENGINE TORQUE FLUCTUATED BETWEEN 10-60 PERCENT. NO ELECTRONIC ENGINE CONTROL (EEC) FAULT. PROP RPM DROPPED TO ABOUT 71 PERCENT MOMENTARILY. AIRCRAFT RETURNED TO MIAMI AND DECLARED EMERGENCY LANDING. GENERAL INSPECTION OF TORQUE SENSORS CONDUCTED AND NO DISCREPANCY FOUND. ALSO, INSPECTED TORQUE SENSOR WIRING AND FOUND SATISFACTORY. AIRCRAFT RELEASED FOR A FUNCTIONAL CHECK FLIGHT AND PASSED WITHOUT FURTHER PROBLEM. (M)

Part: SHOCK ABSORBER — CRACKED (NLG) · airframe 22,672 hrs · 25,817 cycles

DURING PARKING, THE AIRCRAFT A LOUD NOISE CAME FROM THE NOSE GEAR. INSPECTION REVEALED THAT THE NOSE GEAR AXLE WAS CRACKED. REMOVED AND REPLACED NOSE LANDING GEAR SHOCK ABSORBER.

Part: BATTERY PACK — DISCHARGED (CABIN)

SJU - FLT 3956 - CREW REPORTED THE FORWARD AND AFT EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD BATTERY PACK AND RECONNECTED THE BATTERY PACK IN THE AFT POWER SUPPLY UNIT. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BALLAST — SHORTED (CABIN)

SDQ - FLT 3979 - CREW REPORTED THE OVERHEAD COMPARTMENT BALLAST LIGHT SHORTING AT THE TERMINAL END AT SEAT POSITIONS 13/14 A/B WITH VISIBLE SMOKE. LIGHT WAS PUT ON MEL. (M)

Part: BATTERY — DISCHARGED (CABIN)

DFW - FLT 3574 - CREW REPORTED SOME FLOOR PROXIMITY EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY IN EMERGENCY POWER SUPPLY UNIT 67WL. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING MBV-1 INSPECTION MAINTENANCE REPORTED RIGHT AFT INBOARD AND LEFT AFT INBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200114403. (M)

Part: SILL — CORRODED (FUSELAGE)

DURING MBV-1 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR SILL PLATE AND DRAIN TRACK CORRODED BETWEEN FRAMES 36 AND 39. MAINTENANCE REMOVED AND REPLACED THE DRAIN TRACK IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: TRACK — CORRODED (FUSELAGE)

DURING MBV-1 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR SILL PLATE AND DRAIN TRACK CORRODED BETWEEN FRAMES 36 AND 39. MAINTENANCE REMOVED AND REPLACED THE DRAIN TRACK IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200114402. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING MBV-1 INSPECTION MAINTENANCE REPORTED RIGHT AFT INBOARD AND LEFT AFT INBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE LEFT FLOOR SUPPORT BETWEEN FRAMES 38 AND 39 CORRODED, AND LEFT FLOOR SUPPORT BETWEEN FRAMES 39 AND 40 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORTS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20011435. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

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

Part: FLOORBEAM — CRACKED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAM 38 AND 40 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE RIGHT FLOOR SUPPORT BETWEEN FRAMES 36 AND 38 CORRODED, AND RIGHT FLOOR SUPPORT BETWEEN FRAMES 38 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORTS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20011434. (M)

Part: FITTING — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE FOUND THE LEFT AFT ZEE MEMBER BETWEEN FRAMES 39 AND 40 CORRODED, AND THE RIGHT AFT ZEE MEMBER BETWEEN FRAMES 39 AND 41 CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH ZEE MEMBERS IAW SRM 53-25-04. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED FLOORBEAM 38 AND 40 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAMS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20011433. (M)

Part: FITTING — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE FOUND THE LEFT AFT ZEE MEMBER BETWEEN FRAMES 39 AND 40 CORRODED, AND THE RIGHT AFT ZEE MEMBER BETWEEN FRAMES 39 AND 41 CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH ZEE MEMBERS IAW SRM 53-25-04. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20011436. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION MAINTENANCE REPORTED THE LEFT FLOOR SUPPORT BETWEEN FRAMES 38 AND 39 CORRODED, AND LEFT FLOOR SUPPORT BETWEEN FRAMES 39 AND 40 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORTS IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: GUIDE — CORRODED (T/E FLAP)

SAW - DURING MBV-1 INSPECTION MAINTENANCE FOUND THE LEFT OUTBOARD FLAP NR 5 CAM GUIDE CORRODED, AND THE LEFT INBOARD FLAP NR 3 CAM GUIDE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CAM GUIDES IAW CMM 57-53-11. AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20011432. (M)

Part: GUIDE — CORRODED (T/E FLAP)

DURING MBV-1 INSPECTION, MAINTENANCE REPORTED THE LEFT OUTBOARD FLAP NR 5 CAM GUIDE CORRODED, AND THE LEFT INBOARD FLAP NR 3 CAM GUIDE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CAM GUIDES IAW CMM 57-53-11. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — DENTED (FUSELAGE)

SAW - DURING MBV-1 INSPECTION MAINTENANCE REPORTED A DENT IN THE LEFT SIDE OF THE FUSELAGE BETWEEN FRAMES 31 AND 32 AND STRINGERS 12 AND 13. MAINTENANCE REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 405. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — LOOSE (CABIN)

DFW - FLT 3826 - EMERGENCY FLOOR LIGHT IN AFT GALLEY IS LOOSE FROM FLOORBOARD. MAINTENANCE RESECURED LIGHT ASSEMBLY TO FLOORBOARD. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - FLT 3858 - CREW REPORTED FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT 8B AND 10B ARE INOPERATIVE. PUT ON MEL AT THIS TIME. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - FLT 3858 - CREW REPORTED FLOOR PROXIMITY EMERGENCY LIGHTS AT SEAT 8B AND 10B ARE INOPERATIVE. REMOVED AND REPLACED LAMPS IN EMERGENCY FLOOR LIGHTING. OPS CHECK GOOD. (M)

Part: GEARBOX — INOPERATIVE (COCKPIT)

DFW - DURING PHASE 3 INSPECTION, MAINTENANCE FOUND THE FREE FALL HANDLE COULD NOT BE PULLED FOR THE FUNCTIONAL TEST OF LANDING GEAR FREE FALL SYSTEM. MAINTENANCE REMOVED AND REPLACED HANDLE AND GEARBOX ASSEMBLY IAW ATR MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA3349. (M)

Part: HANDLE — INOPERATIVE (COCKPIT)

DFW - DURING PHASE 3 INSPECTION, MAINTENANCE FOUND THE FREE FALL HANDLE COULD NOT BE PULLED FOR THE FUNCTIONAL TEST OF LANDING GEAR FREE FALL SYSTEM. MAINTENANCE REMOVED AND REPLACED HANDLE AND GEARBOX ASSEMBLY IAW ATR MM. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: COVER — LOOSE (CABIN) · airframe 17,931 hrs · 20,680 cycles

DFW - FLT 3398 - EMERGENCY LIGHT ROW 5 OBSTRUCTED. RESECURED PLASTIC COVER STRIP AT ROW 5. (X).

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - FLT 3832 - EMERGENCY FLOOR PROX LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK IN POWER SUPPLY 63WL. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - FLT 3832 - SECOND OVERHEAD EMERGENCY EXIT ILGHT FROM LEFT REAR IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK IN POWER SUPPLY 73WL. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: VALVE — FAILED (NR 2 PACK) · airframe 17,437 hrs · 20,245 cycles

LT - FLT 3667 - AFTER ADJUSTING TEMPERATURE ON RT TEMP SELECT, DUCT TEMP WENT TO 100 DEGREES CELSIUS. OVERHEAT CAUTION CAME ON AND F/A REPORTED SMOKE IN THE CABIN COMING FROM AIR DUCTS. PERFORMED QRH PROCEDURES. TURNED OFF NR 2 PACK AND SMOKE STARTED TO CLEAR. SMOKE DID CLEAR COMPLETELY WITH NR 2 PACK OFF. CONTINUED TO DESTINATION LIT. THERE WERE NO RECIRC FAN FAULTS. SUBMITTER SUSPECTED NR 2 PACK/ACM FAILURE. MEL 21-23. REMOVED AND REPLACED AIR TRIM VALVE. OPS CHECK GOOD. MEL 21-23 RESTORED. (X)

Part: BULB — FAILED (CABIN)

DFW - FLT 3495 - AFT FLOOR PROXIMITY LIGHT INOPERATIVE AND 3RD FORWARD INOPERATIVE LIGHT PUT ON MEL. C/A 9-6-00 MAINTENANCE REMOVED AND REPLACED BULB. OPS CHECK GOOD. (X)

Part: FRAME — CRACKED (CARGO DOOR)

SAW - DURING MAINTENANCE INSPECTION, FOUND CRACK IN FORWARD CARGO DOOR FRAME. REPAIRED FRAME IAW SRM 52-31-00. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FRAME — CRACKED (CARGO DOOR)

SAW - DURING MAINTENANCE INSPECTION, FOUND CRACK IN FORWARD CARGO DOOR FRAME. REPAIRED FRAME IAW SRM 52-31-00. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

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

Part: SEAT TRACK — CORRODED (FUSELAGE)

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

Part: SEAT TRACK — CORRODED (FUSELAGE)

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

Part: SEAT TRACK — CORRODED (FUSELAGE)

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

Part: SEAT TRACK — CORRODED (FUSELAGE)

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

Part: SEAT TRACK — CORRODED (FUSELAGE)

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

Part: LIGHT — INOPERATIVE (CABIN)

MIA - FLT 5672 - ONE FLOOR PROXIMITY LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)

Part: BRAKE — INOPERATIVE (MLG)

MIA - FLT 5799 - FIRST OFFICERS BRAKES INOPERATIVE. BLED BRAKE SYSTEM. FUNCTIONAL CHECK GOOD. (M)

Part: FLOORBEAM — CORRODED (CABIN)

SAW - DURING MBV-1 INSPECTION, FOUND FLOORBEAMS 36, 38, AND 39 CORRODED. REMOVED AND REPLACED THE FLOORBEAMS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA982082 AND 98ZZZX3287.

Part: FLOORBEAM — CORRODED (CABIN)

SAW - DURING MBV-1 INSPECTION, FOUND FLOORBEAMS 36, 38, AND 39 CORRODED. REMOVED AND REPLACED THE FLOORBEAMS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR 98ZZZX3287 AND 98ZZZX3288. (X)

Part: FLOORBEAM — CORRODED (CABIN)

SAW - DURING MBV-1 INSPECTION, FOUND FLOORBEAMS 36, 38, AND 39 CORRODED. REMOVED AND REPLACED THE FLOORBEAMS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA982082 AND 98ZZZX3288.

Part: SEAT TRACKS — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, FOUND THE LT AND RT FLIGHT ATTENDANT, LT FORWARD INBD AND OTBD, LT MIDDLE AND AFT OTBD, LT AFT INBD, RT AFT CARGO, RT MIDDLE AND AFT OTBD, AND THE RT MIDDLE INBD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR 98ZZZX3289 THROUGH NR 98ZZZX3298. (X)

Part: SEAT TRACKS — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, FOUND THE LT AND RT FLIGHT ATTENDANT, LT FORWARD INBD AND OTBD, LT MIDDLE AND AFT OTBD, LT AFT INBD, RT AFT CARGO, RT MIDDLE AND AFT OTBD, AND THE RT MIDDLE INBD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98206-2, AND, NR 98ZZZX3289 THROUGH NR 98ZZZX3298.

Part: SEAT TRACKS — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, FOUND THE LT AND RT FLIGHT ATTENDANT, LT FORWARD INBD AND OTBD, LT MIDDLE AND AFT OTBD, LT AFT INBD, RT AFT CARGO, RT MIDDLE AND AFT OTBD, AND THE RT MIDDLE INBD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98206-2, AND, NR 98ZZZX3289 THROUGH NR 98ZZZX3298.

Part: PANEL — CORRODED (RT WING)

DURING CPCP-4 INSPECTION, FOUND THE RT WING FEEDER TANK AND CENTER WING TANK ACCESS PANELS CORRODED. REMOVED AND REPLACED BOTH PANELS. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL NR SIMA982061.

Part: PANEL — CORRODED (RT WING)

DURING CPCP-4 INSPECTION, FOUND THE RT WING FEEDER TANK AND CENTER WING TANK ACCESS PANELS CORRODED. REMOVED AND REPLACED BOTH PANELS. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL NR 98ZZZX3299. (X)

Part: SEAT TRACKS — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, FOUND THE LT AND RT FLIGHT ATTENDANT, LT FORWARD INBD AND OTBD, LT MIDDLE AND AFT OTBD, LT AFT INBD, RT AFT CARGO, RT MIDDLE AND AFT OTBD, AND THE RT MIDDLE INBD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98206-2, AND, NR 98ZZZX3289 THROUGH NR 98ZZZX3298.

Part: SEAT TRACKS — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, FOUND THE LT AND RT FLIGHT ATTENDANT, LT FORWARD INBD AND OTBD, LT MIDDLE AND AFT OTBD, LT AFT INBD, RT AFT CARGO, RT MIDDLE AND AFT OTBD, AND THE RT MIDDLE INBD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98206-2, AND, NR 98ZZZX3289 THROUGH NR 98ZZZX3298.

Part: SEAT TRACKS — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, FOUND THE LT AND RT FLIGHT ATTENDANT, LT FORWARD INBD AND OTBD, LT MIDDLE AND AFT OTBD, LT AFT INBD, RT AFT CARGO, RT MIDDLE AND AFT OTBD, AND THE RT MIDDLE INBD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98206-2, AND, NR 98ZZZX3289 AND 98ZZZX3298.

Part: SEAT TRACKS — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, FOUND THE LT AND RT FLIGHT ATTENDANT, LT FORWARD INBD AND OTBD, LT MIDDLE AND AFT OTBD, LT AFT INBD, RT AFT CARGO, RT MIDDLE AND AFT OTBD, AND THE RT MIDDLE INBD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98206-2, AND, NR 98ZZZX3289 THROUGH NR 98ZZZX3297.

Part: SEAT TRACKS — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, FOUND THE LT AND RT FLIGHT ATTENDANT, LT FORWARD INBD AND OTBD, LT MIDDLE AND AFT OTBD, LT AFT INBD, RT AFT CARGO, RT MIDDLE AND AFT OTBD, AND THE RT MIDDLE INBD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98206-2, AND, NR 98ZZZX3289 THROUGH NR 98ZZZX3298.

Part: SEAT TRACKS — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, FOUND THE LT AND RT FLIGHT ATTENDANT, LT FORWARD INBD AND OTBD, LT MIDDLE AND AFT OTBD, LT AFT INBD, RT AFT CARGO, RT MIDDLE AND AFT OTBD, AND THE RT MIDDLE INBD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98206-2, AND, 98ZZZX3290 AND NR 98ZZZX3298.

Part: SEAT TRACKS — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, FOUND THE LT AND RT FLIGHT ATTENDANT, LT FORWARD INBD AND OTBD, LT MIDDLE AND AFT OTBD, LT AFT INBD, RT AFT CARGO, RT MIDDLE AND AFT OTBD, AND THE RT MIDDLE INBD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98206-2, AND, NR 98ZZZX3289 THROUGH NR 98ZZZX3298.

Part: SEAT TRACKS — CORRODED (CABIN)

SAW - DURING CPCP-4 INSPECTION, FOUND THE LT AND RT FLIGHT ATTENDANT, LT FORWARD INBD AND OTBD, LT MIDDLE AND AFT OTBD, LT AFT INBD, RT AFT CARGO, RT MIDDLE AND AFT OTBD, AND THE RT MIDDLE INBD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98206-2, AND, NR 98ZZZX3289 THROUGH NR 98ZZZX3298.

Part: ZEE MEMBER — CORRODED (BS 39-40)

SAW DURING MBV-1 INSPECTION, FOUND THE LT AND RT AFT ZEE MEMBERS AND LT WEB BETWEEN FRAMES 39 AND 40 CORRODED. REMOVED AND REPLACED BOTH ZEE MEMBERS AND WEB. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR 98ZZZX3300 AND NR 98ZZZX3301. (X)

Part: ZEE MEMBER — CORRODED (BS 39-40)

SAW DURING MBV-1 INSPECTION, FOUND THE LT AND RT AFT ZEE MEMBERS AND LT WEB BETWEEN FRAMES 39 AND 40 CORRODED. REMOVED AND REPLACED BOTH ZEE MEMBERS AND WEB. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98205-1 AND NR 98ZZZX3300.

Part: ZEE MEMBER — CORRODED (BS 39-40)

SAW DURING MBV-1 INSPECTION, FOUND THE LT AND RT AFT ZEE MEMBERS AND LT WEB BETWEEN FRAMES 39 AND 40 CORRODED. REMOVED AND REPLACED BOTH ZEE MEMBERS AND WEB. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98205-1 AND NR 98ZZZX3301.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - UPON ENTERING A/C FOUND EMERGENCY LIGHTS SW ARMED ND FORWARD LIGHT TO BE INTERMITTENT. ALSO, EMERGENCY LIGHT AT SEAT 4AB WAS ALSO INOP. RAI'D EMERGENCY LIGHT BATTERY PACK AT 43WL. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: HANDLE — STUCK (LANDING GEAR)

ORD - FLT 4045 - AFTER TAKEOFF WHEN CREW WENT TO LIFT LANDING GEAR HANDLE, HANDLE WOULD NOT GO UP. THEREFORE, GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO ORD AND NO FURTHER INCIDENT WAS REPORTED. REPLACED LANDING GEAR HANDLE, PERFORMED GEAR SWING. OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (X)

Part: WIRE — BROKEN (CABIN)

ORD - FLT 4151 - EMERGENCY LIGHT OUT IN GALLEY AREA. LIGHT FOUND INTERMITTENT. DEFERRED PER MEL 33-22. AIRCRAFT RETURNED TO SERVICE. REPAIRED WIRE. PERFORMED OPS CHECK, SATISFACTORY. RETURNED AIRCRAFT TO SERVICE. (X)

Part: LIGHT — INOPERATIVE (CABIN)

ORD - FLT 4152 - STAIR EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY AIRSTAIR LIGHT ASSEMBLY IAW ATR 72 JIC 33-51-24-RAI-10000-002. EMERGENCY LIGHTS OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: WIRE — LOOSE (CABIN)

ICT - FLT 3806 - PASSENGER DOOR CANNON PLUG WIRES PULLED OUT OF CANNON PLUG MAKES DOOR WARNING SYSTEM AND EMERGENCY LIGHT INOP. STOWED WIRES FOR MX. FERRY FLT TO DFW FOR REPAIRS INSTALLED NEWS PINS ON WIRES FOR PASSENGER ENTRANCE CANNON PLUG IAW ATR AMM. EMERGENCY LIGHTS AND DOOR WARNING OPS CHECK GOOD. (M) AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHTS — INOPERATIVE (PAX DOOR)

GRR - EMERGENCY EXIT LIGHT ON PASSENGER DOOR INOP. REPAIRED WIRING AND RAI'D PINS ON CANNON PLUG AT PASSENGER DOOR. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: WIRE — BROKEN (CABIN)

ICT - PERIODIC SERVICE INSPECTION REVEALED EMERGENCY LIGHT ON PASSENGER DOOR INOPERATIVE. FOUND BROKEN WIRE, NR 33512216. REPAIRED WIRE, OPS CHECK SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. (X)

Part: CONNECTOR — DIRTY (NR 1 ENG)

HOU - FLT NR 3618 - AFTER TAKEOFF LEFT ENGINE TORQUE INDICATIONS DROPPED TO 60 PERCENT CREW ELECTED TO RETURN TO HOU. CLEANED ELECTRICAL CONNECTOR ON LEFT ENGINE T 1.8 SENSOR. GROUND PERFORMANCE RUNS WERE SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

OKC - EMERGENCY FLOOR PATH LIGHTING PORTIONS REMAIN ILUMINATED WHEN SYSTEM IS DISARMED. REPLACED EMERGENCY BATTERY PACK 73WL IAW MM 33-50-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: FAN — FAILED (NR 1)

DFW - FLT NR 3816 - INBOUND INTO DFW, CREW SMELLED SMOKE IN THE COCKPIT, COMPLIED WITH EMERGENCY PROCEDURES AND NOTIFIED CFT. LANDED WITHOUT FURTHER INCIDENT. RAN ALL SYSTEMS AND FOUND FAULT ON THE NR 1 RECIRC FAN. REMOVED AND REPLACED NR 1 RECIRC FAN. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: PROBE — BROKEN (NR 1 ENGINE)

ORD - FLT NR 4043 - NR 1 ENGINE TQ SURGED FROM APPROXIMATELY 40-110 PERCENT, SURGE STOPPED WHEN NP WAS SET TO 100 PERCENT. REPLACED NR 1 ENGINE NH SENSOR, IAW PWA MM, CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M0

Part: SELECTOR VALVE — FAILED (LT MLG WW)

DFW - FLT 3810 - LANDING GEAR FAILED TO EXTEND WHEN SELECTED. EMERGENCY EXTENSION WAS SELECTED AND THE GEAR EXTENDED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REMOVED AND INSPECTED GEAR SELECTOR VALVE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: EEL ASSY — INOP (GALLEY)

DFW - FLT 3812 - EMERGENCY EXIT LIGHT OUT ON AIRSTAIR DOOR. MAINTENANCE REMOVED AND REPLACED LIGHT ASSY. SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)