N283AS

Part: CONTROL LEVER — INTERMITTENT (MLG) · airframe 34,557 hrs · 34,547 cycles

AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. REPLACED LANDING GEAR CONTROL LEVER ASSEMBLY.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 34,544 hrs · 34,531 cycles

FLIGHT: 9273, PILOT REPORTED MAIN CABIN DOOR WILL NOT OPEN FROM THE OUTSIDE. LUBRICATED MAIN CABIN DOOR.

Part: CONTROL LEVER — INOPERATIVE (MLG) · airframe 34,548 hrs · 34,537 cycles

AFTER TAKEOFF, LT MAIN AND NOSE LANDING GEAR RED (A) LIGHTS ILLUMINATED. REPLACED LANDING GEAR CONTROL LEVER ASSEMBLY.

Part: PROXIMITY SENSOR — DIRTY (LT MLG) · airframe 34,537 hrs · 34,523 cycles

DURING FLIGHT LANDING GEAR DISAGREEMENT LIGHTS (A) RED ON LT MAIN GEAR AND (A) RED ON NOSE GEAR ILLUMINATED. CLEANED LT MAIN LANDING GEAR AND NOSE LANDING GEAR UPLOCK AND DOWNLOCK PROXIMITY SENSORS.

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 34,532 hrs · 34,517 cycles

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED MAIN CABIN DOOR WILL NOT OPEN FROM THE OUTSIDE AND WILL CLOSE FROM THE INSIDE OR OUTSIDE. ADJUSTED MAIN CABIN DOOR LOCKING CAMS.

Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 34,415 hrs · 34,386 cycles

DURING PREFLIGHT DISCOVERED RT FWD OVERWING EMERGENCY LIGHT INOPERATIVE. SECURED BULB AT RT FWD OVERWING EMERGENCY LIGHT SOCKET.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LT MLG) · airframe 33,197 hrs · 32,977 cycles

AFTER TAKEOFF LT LANDING GEAR (A) AND (B) DISAGREEMENT LIGHTS WOULD NOT EXTINGUISH UPON RETRACTION, A GRINDING SOUND COULD BE HEARD IN THE FLIGHT DECK. RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. ADJUSTED THE LT MAIN LANDING GEAR UPLOCK PROXIMITY SENSORS OPERATIONAL CHECK NORMAL.

Part: CONTROL BOX — MALFUNCTIONED (MLG) · airframe 33,010 hrs · 32,749 cycles

FLIGHT: 9180 TCB/FLL DURING FLIGHT LEFT MAIN LANDING GEAR "B" LOOP RED ANNUNCIATOR ILLUMINATED INTERMITTENTLY. CONTINUED TO FLL LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR CONTROL BOX OPERATIONAL CHECK NORMAL.

Part: WIRE HARNESS — DAMAGED (UPLOCK) · airframe 32,992 hrs · 32,728 cycles

FLIGHT:9258 FPO/FLL DURING FLIGHT, THE LEFT MAIN LANDING GEAR "B" LOOP RED ANNUNCIATOR ILLUMINATES INTERMITTENTLY. CONTINUED TO FLL LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN LANDING GEAR "B" LOOP UPLOCK PROXIMITY SENSOR AND HARNESS.

Part: DOWNLOCK SWITCH — OUT OF ADJUST (LT MLG) · airframe 32,969 hrs · 32,705 cycles

FLIGHT: 9131 TPA/MIA - DURING FLIGHT, THE LEFT MAIN LANDING GEAR "B" LOOP RED ANNUNCIATOR ILLUMINATES INTERMITTENTLY. CONTINUED TO MIA LANDED WITHOUT INCIDENT. ADJUSTED THE LEFT "B" SYSTEM DOWNLOCK PROXIMITY SENSOR.

Part: CONNECTOR — DIRTY (MLG) · airframe 32,950 hrs · 32,683 cycles

FLIGHT: 9258 FPO/FLL DURING FLIGHT LT MAIN LANDING GEAR (B) LOOP LIGHT ILLUMINATES INTERMITTENTLY. CONTINUED TO FLL LANDED WITHOUT INCIDENT.CLEANED AND RESECURED CONNECTORS 151548 AND 151549 OPERATIONAL CHECK NORMAL.

Part: LAMP — NO TEST (EMERGENCY LIGHTS) · airframe 32,821 hrs · 32,525 cycles

FLIGHT:9227 NAS/FLL RIGHT EMERGENCY EXTERIOR LIGHT WILL NOT TEST. REPLACED RT EMERGENCY AFT LIGHT LAMP.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 32,788 hrs · 32,488 cycles

FLIGHT: 9263 RT EXTERIOR EMERGENCY LIGHT INOPERATIVE. RESECURED EMERGENCY LIGHT LOOSE WIRING OPERATIONAL CHECK NORMAL.

Part: FIRE DETECTOR — MALFUNCTIONED (APU BAY)

FLIGHT: 9154 MCO/MIA DURING FLIGHT APU FIRE DETECTION INOPERATIVE LIGHT ILLUMINATED AND STAYED ON. REPLACED FIRE DETECTOR, OPERATIONAL CHECK GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (APU FIRE LOOP)

FLIGHT: 9254 ELH/FLL DURING FLIGHT THE APU FIRE EXTINGUISHER LIGHT ILLUMINATED. TROUBLESHOT APU FIRE EXTINGUISHER SYSTEM, UNABLE TO DUPLICATE PROBLEM.

Part: FIRE DETECTOR — MALFUNCTIONED (APU BAY)

FLIGHT: 9154 MCO/MIA DURING FLIGHT APU FIRE DETECTION INOPERATIVE LIGHT ILLUMINATED AND STAYED ON. REPLACED FIRE DETECTOR, OPERATIONAL CHECK GOOD.

Part: TIRE — DELAMINATED (NLG)

FLIGHT:9170 FLL/TCB ON ROTATION TIRE APPEARED TO BLOW. RETURNED TO FLL. FOUND LT NOSE TIRE CAP DELAMINATED REPLACED LT AND RT NOSE WHEEL TIRES.

Part: DISPLAY — SHORTED (FWD INSTR PANEL)

DURING FLIGHT, A MOMENTARY SMELL OF ELECTRICAL SMOKE. MULTI-FUNCTION DISPLAY BLANKED OUT, FLIGHT CONTINUED. REPLACED MULTI-FUNCTION DISPLAY. (K)

Part: SKIN — CRACKED (FUSELAGE)

DURING A HANGAR INSPECTION IN TXK, THE FIRST OFFICER'S WINDOW POST SKIN WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CRACKED SKIN IAW ASA EO 120-53-0119A. (M)

Part: WIRE — BROKEN (CABIN)

FLT 4056 - DURING GROUND INSPECTION IN ATL, THE EXTEROR RIGHT AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FUSE ABOVE ROWS 7 AND 8, AND ALSO REPAIRED THE BROKEN GROUND WIRE (P/N M22759-20-9) ON THE EXTERIOR RIGHT AFT EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE RIGHT FORWARD SEAT TRACK BETWEEN FRAMES 15 AND 32. MAINTENANCE REMOVED THE CORRODED SEAT TRACK IAW SRM 51-40-02. A NEW SEAT TRACK WAS FABRICATED AND INSTALLED THE NEW SEAT TRACK IAW AMM 53-01-05. (M)

Part: BUTTSTRAP — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE LEFT BUTT STRAP BETWEEN FRAMES 25 AND 30. MAINTENANCE REMOVED THE CORRODED BUTT STRAP IAW SRM 51-40-02. A NEW BUTT STRAP WAS LOCATED AND DRILLED IAW SRM 51-25-05. MAINTENANCE INSTALLED THE NEW BUTT STRAP IAW WITH SRM 51-40-02. (M)

Part: SILL — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE LEFT SILL PLATE BETWEEN FRAMES 15A AND STATION 6653.1. MAINTENANCE REMOVED THE LEFT BUTT SILL PLATE. MAINTENANCE LOCATED, DRILLED, ALODINED, AND PRIMED HOLED ON NEW SILL PLATE IAW SRM 51-25-05 AND 51-25-06. THE NUT PLATES AND THE NEW SILL PLATE WERE INSTALLED IAW SRM 51-40-02. (M)

Part: STRINGER — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON STRINGER 21 LEFT BETWEEN FRAMES 9 AND 15. MAINTENANCE REMOVED THE CORRODED STRINGER AND INSTALLED THE NEW STRINGER IAW SRM 51-40-02. (M)

Part: CROSSBEAM — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION IN BNA, THE 3 RIGHT, MOST OUTBOARD CROSS FRAMES HAD CORROSION AT FRAME 20. MAINTENANCE REMOVED THE 3 CORRODED, RIGHT, OUTBOARD MOST CROSS FRAMES IAW SRM 51-40-02. MAINTENANCE INSTALLED THE NEW CROSSBEAMS IAW SRM 51-21-02. (M)

Part: BUTTSTRAP — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION IN BNA, THE RIGHT SIDE BUTT STRAP WAS CORRODED BETWEEN STATION 6653.1 AND FRAME 25. MAINTENANCE REMOVED THE CORRODED BUTT STRAP AND INSTALLED THE NEW BUTT STRAP IAW SRM 51-40-02. (M)

Part: BUTTSTRAP — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE RIGHT BUTT STRAP BETWEEN FRAME 13 AND STATION 6653.1. MAINTENANCE REMOVED THE CORRODED BUTT STRAP AND REPLACED IT WITH A NEW ONE IAW SRM 51-21-02. (M)

Part: STRINGER — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION IN BNA, STRINGER 21 RIGHT WAS FOUND TO BE CORRODED BETWEEN FRAMES 9 AND 13. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM 51-40-02. (M)

Part: BUTTSTRAP — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP WAS CORRODED BETWEEN FRAMES 30 AND 34. MAINTENANCE REMOVED THE CORRODED LEFT BUTT STRAP AND INSTALLED THE NEW BUTT STRAP IAW SRM 51-40-02. (M)

Part: CROSSBEAM — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION IN BNA, ALL FOUR FLOOR CROSS FRAMES WERE CORRODED AT FRAME 16. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOOR CROSS FRAMES IAW SRM 51-40-02. (M)

Part: BUTTSTRAP — CORRODED (FUSELAGE)

DURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 14 AND STATION 6653.1. MAINTENANCE REMOVED THE CORRODED BUTT STRAP IAW SRM 51-40-02. A NEW BUTT STRAP WAS LOCATED AND DRILLED IAW SRM 51-25-05. MAINTENANCE INSTALLED THE NEW BUTT STRAP IAW SRM 51-40-02. (M)

Part: FRAME — CORRODED (FUSELAGE)

FLT 4815 - DURING INSPECTION, MAINTENANCE FOUND CORROSION AT FRAME 21. MAINTENANCE REPAIRED CORROSION FOLLOWING EO 120-53-0149 WHICH OUTLINES PROCEDURES FOR FRAME 21 CORROSION REPAIR. (M)

Part: RIVET — MISSING (WING)

FLT 4815 - DURING FLIGHT TUL-DFW - PASSENGER NOTICED FUEL SPILLING OUT OF THE TOP PORTION OF THE LEFT WING. CAPTAIN CONFIRMED FUEL LEAKAGE AND DECLARED AN EMERGENCY. FLIGHT DIVERTED TO OKC AND LANDED SAFELY. MAINTENANCE INSPECTED SKIN TO RIB ATTACHMENT BRACKET FOR DAMAGE. NO DAMAGE WAS NOTED. MAINTENANCE INSTALLED RIVET FOLLOWING EMB 120 SRM. MAINTENANCE THEN REINSTALLED LEFT WING FUEL PANEL JUST OUTBOARD OF NACELLE IAW EO 120-51-0005. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

FLT 4049 - DURING INSPECTION, CREW NOTICED EMERGENCY EXIT LIGHT OVER FLIGHT ATTANDANT SEAT WOULD NOT COME ON. MAINTENANCE REMOVED AND REPLACED THE NR 2 AND NR 3 EMERGENCY BATTERY PACKS. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: WIRE — CHAFED (CABIN)

MAINTENANCE WAS ADVISED THAT THE FLIGHT ATTENDANT EMERGENCY LIGHTS TESTS SWITCH POPS THE EMERGENCY LIGHTS C/B. ATL, MAINTENANCE FOUND A CHAFED WIRE AT CANNON PLUG P0389 (AT NR 2 BATTERY PACK) AND REPAIRED WIRE AS NEEDED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M)

Part: ACTUATOR — FAILED (LT TE FLAP)

INBOUND ILE-DFW - EXPERIENCED FLAP CONTROL FAULT ON THE INBOARD PAIR. DUE TO WEATHER CONDITIONS, CREW DECLARED AND EMERGENCY AND PERFORMED A ZERO FLAP LANDING AT DFW WITHOUT FURTHER INCIDENT. DFW MAINTENANCE MEGOHMED ALL FLAP WIRING HARNESSES AND DETERMINED THAT THE LEFT INBOARD FLAP ACTUATOR WAS BAD. REMOVED AND REPLACED FLAP ACTUATOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED AND FURTHER SERVICE. (M)

Part: CONNECTOR — DIRTY (TE FLAPS)

INBOUND DFW-ICT, EXPERIENCED FLAP CONTROL FAULT. RAN CHECKLIST WITHOUT SUCCESS. AFTER CONSULTING WITH FLT CONTROL, AGREED TO CONTINUE TO ICT. CREW DECLARED AN EMERGENCY AND PERFORMED A ZERO-FLAP LANDING WITHOUT FURTHER INCIDENT. DFW MECHANIC WAS DISPATCHED AND CLEANED THE INBOARD FLAP CONNECTORS AND OPERATED THE FLAPS SEVERAL TIMES WITH NO DISCREPANCIES NOTED. THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M)