N451AT

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 31,219 hrs · 30,876 cycles

DURING INSPECTION, FOUND THE EMERGENCY FLOOR LIGHT STRIP MISSING END CAP AT GALLEY AREA, AT SEAT 3B AND 6B. THE ACFT WAS REMOVED FROM SERVICE. INSTALLED EMERGENCY FLOOR LIGHT STRIP END CAP AT GALLEY AREA, AT SEAT 3B AND 6B IAW 33-51-24 RAI 10000. THE ACFT WAS RETURNED TO SERVICE.

Part: BRAKE — WEAK · airframe 30,951 hrs · 30,557 cycles

F/O LT BRAKE VERY SOFT. LT BRAKE BLED IAW JIC 32-42-00, BLD 10010, OPS CHECK GOOD.

Part: BRAKE — WEAK (MLG)

ON FLIGHT 9830, ON TAXI, THE CREW REPORTED THE F/O LT BRAKE WAS VERY SOFT. THE ACFT WAS REMOVED FROM SERVICE. LT BRAKE BLED IAW JIC 32-42-00, BLD 10010. THE OPS CK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY) · airframe 30,929 hrs · 30,541 cycles

EMERGENCY BATTERY FULLY DISCHARGED. RAI EMERGENCY BATTERY IAW W/C EX-243185-RAI-10020-002.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,925 hrs · 30,537 cycles

EMERGENCY EVACUATION PATH LIGHT STRIP AT 4B IS INOP. RELAMPED EMERGENCY EVACUATION PATH LIGHT STRIP AT 4B IAW JIC 33-20-00.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 30,859 hrs · 30,467 cycles

F/A ADVISES EVACUATION PATH EMERGENCY LIGHTING HAS BURNED OUT BULB AT ROW 4. RELAMPED FLOOR EMERGENCY LIGHT. OPS CHECKED GOOD IAW JIC 33-50-00-OPT-10000.

Part: MASTER CYLINDER — INOPERATIVE (MLG) · airframe 30,534 hrs · 30,123 cycles

THE F/O REPORTED THE LT BRAKE FELT SPONGY DURING LANDING. THE ACFT WAS REMOVED FROM SERVICE. R & R THE F/O MASTER CYLINDER IAW JIC 32-42-13. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,451 hrs · 30,028 cycles

DURING THE PREFLIGHT INSP, FOUND THE FLOOR LIGHTING IS OUT AT ROW 4. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED OPS CHECK ON THE EMERGENCY LIGHT STRIP IAW EX-335000-OPT-10000-001. THE LIGHTS CHECK WAS GOOD. NO PARTS R & R. THE ACFT WAS RETURNED TO SERVICE.

Part: BRAKE SYS — INOPERATIVE (LEFT) · airframe 30,412 hrs · 29,991 cycles

ON FLIGHT 4901, THE CREW REPORTED THE F/O LT BRAKE WAS INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED BRAKE LOW PRESSURE BLEEDING IAW JIC 32-42-00. THE OPS CHECK FOUND IT WORKING PROPERLY. NO PARTS REMOVED OR REPLACED. THE ACFT WAS RETURNED TO SERVICE.

Part: SOCKET — BURNED (CABIN LIGHTS) · airframe 30,130 hrs · 29,671 cycles

BETWEEN ROWS 9 & 12 RT SIDE SMELLS LIKE SOMETHING IS BURNING. REPLACED SOCKET FIN NR 311LGB ON PASSENGER CEILING FLOURESCENT LIGHT IAW SPM 20-43-12.

Part: SMOKE DETECTOR — FAILED (E/E BAY) · airframe 30,089 hrs · 29,626 cycles

10 MINS AFTER POWER UP, MASTER WARNING ON CAP. ELECTRICAL SMOKE. R & R AVIONIC SMOKE DETECTOR IAW JIC 26-15-21, OPS CK GOOD.

Part: WARNING LIGHT — ILLUMINATED (MLG) · airframe 29,399 hrs · 28,837 cycles

UNSAFE LANDING GEAR ON THE LT MAIN GEAR ON BOTH PANEL. FOLLOW THE AOE MANUAL CHECK LIST AND RETURNED TO DEPARTURE. (DECLARED EMERGENCY) REMOVED WATER AND CLEANED LT MLG PROXIMITY SWITCHES (WOW) AND PERFORMED NORMAL EXTENSION AND RETRACTION FUNCTIONAL TEST IAW JIC 32-31-00, SYSTEM WORKING PROPERLY.

Part: ENGINE — ODOR (NR 1) · airframe 29,210 hrs · 28,617 cycles

AFTER PARKING THE ACFT AND SHUTTING DOWN THE NR 1 ENGINE A VERY STRONG PLASTIC BURNING ODOR ENTERED THE COCKPIT AND CABIN. INSPECTED CABIN & COCKPIT FOR PLASTIC ODOR, RUN ENGINE NR 1 FOR 30 MIN NO DISCREPANCIES NOTED IAW JIC 72-00-00, ERU 10040.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 27,626 hrs · 26,697 cycles

FIRST 6 LIGHTS ON THE FLOOR EMERGENCY LIGHTS STAYS ON IN FLIGHT. PERFORMED OPS CHECK OF EMERGENCY LIGHTING SYS AND CANNOT DUPLICATE DISCREPANCY AT THIS TIME IAW JIC NR 33-50-00-OPT-10000.

Part: FLANGE — UNKNOWN (FUSELAGE) · airframe 26,912 hrs · 25,860 cycles

LAVATORY SERVICE DOOR CUT OUT AT FUSELAGE LINE 0451. REMOVED AND REPLACED DOUBLER FLANGE IAW SRM NR 51-25-01.

Part: SKIN — CORRODED (RT WING) · airframe 26,912 hrs · 25,860 cycles

RT FUEL PUMP HAS CORROSION AROUND PUMP AREA. COMPLIED WITH EO NR E2-57MR-305 RT WING LWR SKIN PANEL EXTERNAL CORROSION AT FUEL PUMP CUT-OUT BETWEEN RIBS 4 - 5.

Part: MOUNT — CORRODED (LT ENGINE) · airframe 26,912 hrs · 25,860 cycles

FOUND CORROSION ON LT WING AT NR 1 ENG UPPER AFT INBD ENGINE MOUNT. ACCOMPLISHED EO NR E2-57MR-308 LT WING FWD SPAR LWR SLAT EXTERNAL CORROSION REPAIR AT RIB 10.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 26,815 hrs · 25,739 cycles

EMERGENCY LIGHTING ILLUMINATES IN ARMED POSITION. TURNING THEM OFF THEN ARMING RESETS THE LIGHTS TEMPORARILY. PERFORMED AN OPERATIONAL TEST OF THE EMERGENCY LIGHTING SYSTEM. OPERATED SEVERAL TIMES IAW AMM NR 33-50-00-OPT-10000.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 26,813 hrs · 25,737 cycles

FORWARD "HALF" OF THE EMERGENCY LIGHTS ARE ILLUMINATED WHILE THE SWITCH IS IN THE ARM POSITION. REMOVED AND INSTALLED ALL EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW JIC NR 33-51-21-RAI-10010-004.

Part: UNKNOWN — UNKNOWN (EMERGENCY LIGHT) · airframe 26,804 hrs · 25,727 cycles

EMERGENCY LIGHTS STAY ON. PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTS AND FOUND ALL WORKING NORMALLY IAW JIC NR 33-50-00-OPT-10000.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,793 hrs · 25,709 cycles

FORWARD LEFT UPPER EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BURNED BULB IAW MM NR 33-50-00. OPERATIONAL CHECK OK.

Part: PSU — FAILED (CABIN LIGHTS) · airframe 25,385 hrs · 24,289 cycles

SMOKE FROM PASSENGER READING LIGHT AT 5AB. FLIGHT DIVERTED TO MIA FROM FLL. REMOVED AND REPLACED PSU (PASSENGER SERVICE UNIT) AT SEAT 5AB. PERFORMED OPT CK IAW JIC NR 25-23-22 RAI 10000.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,048 hrs · 23,972 cycles

ON POST FLIGHT, FOUND EMERGENCY LIGHT AT MAIN CABIN DOOR STEP INOPERATIVE. REMOVED AND REPLACED MAIN CABIN DOOR EMERGENCY LIGHT ASSEMBLY IAW JIC NR 33-51-24. OP CK GOOD IAW JIC NR 33-51-10.

Part: SKIN — CORRODED (LT WING)

DURING INSPECTION FOUND LT WING LOWER EXTERNAL SKIN WITH CORROSION AT THE T/E (UNDERWING BOX ANGLE END). REMOVED CORROSION AND TREATED IAW SRM. DEFERRED IAW SRAS. AREA BLENDED AS INSTRUCTED.

Part: COMPRESSOR — FOD (ENGINE)

( REF NR: SDR2005065 ) DURING TAKEOFF ROLL, SPARKS WERE COMING OUT THE RT ENGINE. TAKEOFF ABORTED. FOUND FOD DAMAGE IN THE COMPRESSOR BLADES. ENGINE REPLACED. (K)

Part: WIRE HARNESS — BROKEN (RT MLG)

WHILE IN CLIMB, LANDING GEAR DID NOT RETRACT WHEN SELECTED TO THE UP POSITION. AIRCRAFT RETURNED. REPLACED RT MLG INTERNAL UPPER HARNESS. (M)

Part: CONTROL CABLE — DAMAGED (RUDDER)

DURING ACCOMPLISHMENT OF A FLEET CAMPAIGN DIRECTIVE FCD, IT WAS FOUND THAT THE CAPTAINS RUDDER CABLE LOCATED AT FK 12 COMING APART. REMOVED AND REPLACED RUDDER CABLE UNDER THE CAPTAIN SEAT AS PER MM 27-21-00. DURING ACCOMPLISHMENT OF A FCD, FOUND PRESENCE OF FOD EMBEDDED IN THE CAPTAIN RUDDER CABLE PULLEY LOCATED AT THE FRONT CABIN AREA. (M)

Part: SPACER — CRACKED (LT MLG)

DURING PERFORMANCE OF FCD E2-32-004, FOUND CRACK ON FRONT FACE OF LEFT LANDING GEAR SWINGING LEVER SPACER. (M)

Part: SEAT TRACK — CORRODED (FRAME 29-36)

LEFT OUTBOARD AFT SEAT TRACK, CORRODED BETWEEN FRAMES 32 AND 33, OVER 29, 30, 33, 34 AND 35. BLENDED OUT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED TRACK IAW EO NR E9-5300-013 R4 PART B. (M)

Part: SUPPORT — CORRODED (FRAME 36-38)

FLOOR SUPPORT CORRODED OUT BETWEEN FRAMES 36 AND 38. BLENDED AND FOUND TO BE BEYOND LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-25-01. (M)

Part: SEAT TRACK — CORRODED (FRAME 27-33)

LEFT OUTBOARD AFT MID SEAT TRACK, CORRODED BETWEEN FRAMES 28B AND 28C. BLENDED OUT OAN FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 304SHEET 2. BETWEEN F/A SEAT TRACKS IN TWO PLACES. BLENDED OUT AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WITH NEW TRACK BETWEEN FRAMES 27 AND 33, IAW SRM 51-25-03. (M)

Part: SEAT TRACK — CORRODED (FRAME 29 - 36)

LEFT INBOARD AFT SEAT TRACK, CORRODED BETWEEN FRAMES 19, 30, 31, 32 AND 33. BLENDED OUT AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED TRACK BETWEEN FRAMES IAW EO E9-5300-013 R4 PART B. (M)

Part: SEAT TRACK — CORRODED (FRAME 29-36)

LEFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 32 AND 33OVER 33, 34, 29 AND 30. BLENDED OUT IAW SRM 53-00-00 AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK BETWEEN FRAMES IAW EO NR E9-5300-013-020, PART B. (M)

Part: FLOORBEAM — CORRODED (FRAME 36)

FLOORBEAM 36 IS CORRODED BETWEEN F/A SEAT TRACKS IN TWO PLACES. BLENDED OUT AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-58. REMOVED AND REPLACED IAW SRM 51-25-01. (M)

Part: BRACKET — CORRODED (FRAME 25)

AIR CONDITIONER LINE ATTACHMENT BRACKET ON STRINGER 21L ATFRAME 25 IS CORRODED. FABRICATED ATTACHMENT BRACKET IAW SRM 53-51-26, FIG 102. INSTALLED BRACKET IAW SRM 51-25-02. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-8 INSPECTION, MAINTENANCE REPORTED THE LEFT MIDDLE INBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, RIGHT MIDDLE INBOARD, RIGHT MIDDLE OUTBOARD AND RIGHT AFT INBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW SRM 51-25-04. A/C WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-8 INSPECTION, MAINTENANCE REPORTED THE LEFT MIDDLE INBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, RIGHT MIDDLE INBOARD, RIGHT MIDDLE OUTBOARD AND RIGHT AFT INBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW SRM 51-25-04. A/C WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-8 INSPECTION, MAINTENANCE REPORTED THE LEFT MIDDLE INBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, RIGHT MIDDLE INBOARD, RIGHT MIDDLE OUTBOARD AND RIGHT AFT INBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW SRM 51-25-04. A/C WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-8 INSPECTION, MAINTENANCE REPORTED THE LEFT MIDDLE INBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, RIGHT MIDDLE INBOARD, RIGHT MIDDLE OUTBOARD AND RIGHT AFT INBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW SRM 51-25-04. A/C WAS RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

ORD - FLT 4132 - FORWARD EXIT LIGHT STAYS ON ALONG WITH HALF THE FLOOR STRIP LIGHTING. RAI'D EMERGENCY POWER SUPPLY UNITS AND POWER SUPPLY BATTERIES AT ROW 4AB. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - FLT 3610 - RAI'D POWER SUPPLY AND BATTERY PACK AT 61WL IAW JIC 33-51 AND OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. REFERENCE SIMA963031.

Part: POWER SUPPLY — FAILED (CABIN)

DFW - FLT 3610 - RAI'D POWER SUPPLY AND BATTERY PACK AT 61WL IAW JIC 33-51 AND OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: HANDLE — FAILED (LANDING GEAR)

LBB - FLT 3810 - AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO LBB AND LANDED SAFELY. AIRCRAFT RELOCATED TO DFW PER MEL 32-3 AUTHORITY. MAINTENANCE REPLACED LANDING GEAR SELECTOR HANDLE. PERFORMED LANDING GEAR RETRACTION/EXTENSION. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — FAILED (CABIN)

ORD - FLT 4058 - EMERGENCY AIRSTAIR LIGHT INOP. REPLACED EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: OIL PSI TRANSM — INTERMITTENT (NR 2 ENG)

LBB - FLT NR 3826 - DURING TAKEOFF FROM LBB, NR 2 ENGINE OIL PRESSURE INDICATION DROPPED TO ZERO, NO LOW OIL PRESSURE WARNINGS GIVEN. CREW SHUT DOWN NR 2 ENGINE AND RETURNED TO LBB. DFW - MAINTENANCE SENT TO LBB WHERE THEY GROUND RAN AIRCRAFT SATISFACTORY, BUT REPLACED THE OIL PRESSURE TRANSMITTER AS PRECAUTION. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)