N336AG

Part: CONTROL PANEL — INOPERATIVE · airframe 39,570 hrs · 44,394 cycles

FLIGHT: 124 STI/SJU GEAR HANDLE LIGHT DOES NOT COME ON DURING OPERATION. CORRECTIVE ACTION: REPLACED LANDING GEAR CONTROL PANEL WITH SERVICABLE LANDING GEAR CONTROL PANEL OPERATIONAL CHECK GOOD.

Part: LIGHT — UNSECURE (CABIN) · airframe 38,422 hrs · 42,923 cycles

FLIGHT# 0053 MCO/FLL REPORT: ESCAPE PATH LIGHTING IS COMING OFF BETWEEN ROWS 5 TO 7. CORRECTIVE ACTION: SECURED ESCAPE PATH LIGHTING BETWEEN ROWS 5 TO 7, OPERATIONAL TEST GOOD IAW SAAB 340 AMM 33-50-20-04.

Part: SMOKE DETECTOR — FAILED (E/E BAY) · airframe 38,398 hrs · 42,904 cycles

SUPPLEMENTAL FLIGHT# 0142 FLL/FPO REPORT:AVIONICS SMOKE LIGHT ILLUMINATED IN CRUISE ( WITH ODOR)@7000'. RAN QRC/QRH 11-2, LIGHT WENT OUT DURING THE QRH POSSIBLY ONCE AVIONICS L&R WERE TURNED OFF. LIGHT REMAINED OFF UNTIL WE LANDED AND ROLL. THE LIGHT CAME BACK ON, AND WE STILL DIDN"T EXPERIENCE SMOKE OR ODOR AND OFF LOADED PAX. WE DECLARED AN EMERGENCY, AND CHOSE THE DESTINATION TO LAND IMMEDIATELY AT FPO. CORRECTIVE ACTION: PERFORMED FUALT ISOLATION IAW AMM 26-13-00-01, FOUND AVI SMOKE DETECTOR TEST FAILED , R&R AVI SMOKE DETECTOR IAW SAAB 340 AMM 26-13-05-04, OPS CHECK GOOD RAN SYSTEM FOR 4HR NO DEFECTS

Part: BUTTON — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 38,320 hrs · 42,825 cycles

FLIGHT 0067, EMERGENCY LIGHT WILL NOT TURN OFF FROM FA PANEL. EXERCISED FA PANEL PUSH BUTTON SWITCH, OPS CHECKED NORMAL IAW MM 33-50-00-00-2.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 38,006 hrs · 42,538 cycles

FLIGHT# 0092 TPA/FLL REPORT: AIRCRAFT DAMAGE TO BOTTOM TAIL AREA. CORRECTIVE ACTION: PERFORMED REPAIR IAW SDS 047813 AND SRM CHAPTERS 51-40-60 SRM 53-80010-202 TOPCOATED IAW SF340 SRM 51-20-43.

Part: CONNECTOR — LOOSE (CABIN) · airframe 37,646 hrs · 42,206 cycles

FLIGHT 0054 PNS/MCO REPORT: MAIN EXIT DOOR EMERGENCY LIGHT INOP. CORRECTIVE ACTION: FOUND CONNECTOR 463 VP P1 LOOSE AT FWD. LT. GALLEY, RESECURED CONNECTOR IAW AMM 33-50-50, OP'S CHECK GOOD.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 37,160 hrs · 41,746 cycles

FLIGHT 0091 JAX/TPA REPORT: BACK LIGHT ABOVE RT FORWARD EMERGENCY EXIT SIGN INOP. CORRECTIVE ACTION: R/R 21LN EMERGENCY POWER SUPPLY IAW AMM 33-50-10-04-1. EMERGENCY LIGHTS OPS CHECK GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 37,112 hrs · 41,691 cycles

FLIGHT# 0118 HSV/MCO REPORT: EMERGENCY EXIT FORWARD CABIN LIGHT INOP. CORRECTIVE ACTION: RESECURED CONNECTOR ON RH FWD EMERGENCY EXIT SIGN IAW SAAB 340 WM 20-20-10, OPS CHECK GOOD IAW SAAB 340 AMM 33-50-00-05-1

Part: SIGN — DETACHED (CABIN) · airframe 37,050 hrs · 41,367 cycles

FLIGHT 0067 FLL/MCO REPORT: EMERGENCY EXIT SIGN ON FORWARD STARBOARD DOOR DETACHED. RE-ATTACHED EMERGENCY EXIT SIGN IAW AMM 51-30-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,954 hrs · 41,530 cycles

F/A REPORTED THE EMERGENCY LIGHT, BULB NOT WORKING. R & R THE BULB IAW AMM 33-20-00

Part: WIRE — UNSECURE (EMERGENCY LIGHTS) · airframe 36,922 hrs · 41,495 cycles

EMERGENCY LIGHTS ON THE CABIN FLOOR WERE INOPERATIVE, AFT PART OF CABIN. SECURED A WIRE AT 46LN IAW AMM 33-50-20-04. EMERGENCY LIGHTS OPS CHECKED NORMAL IAW AMM 33-50-00-05-1.

Part: SIGN — UNSECURE (CABIN) · airframe 36,903 hrs · 41,473 cycles

FLT 0068 MHH/FLL, EMERGENCY EXIT SIGN HANGING 2D. SECURED EXIT SIGN IAW AMM 33-50-50-04 OPS CHECK GOOD.

Part: PANEL — FAILED (EMERGENCY LIGHT) · airframe 36,891 hrs · 41,459 cycles

FLIGHT 0051 MHH/FLL REPORT: EMERGENCY LIGHT RIGHT FRONT EMERGENCY EXIT DOOR NOT WORKING. REMOVED AND REPLACE EMERGENCY EXIT LIGHT PANEL OPS CHECK OK IAW 33-50-45-04 AMM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 36,865 hrs · 41,431 cycles

FLIGHT 0081 TPA/PBI REPORT: LUMININESCENT EXIT SIGN OVER 2F EXIT INOP. FOUND LOOSE CONNECTOR, RESCEURED CONNECTOR IAW AMM 33-50-40-04. OPS CHECKED SEVERAL TIMES GOOD.

Part: CONTROL UNIT — FAILED (DE-ICE SYSTEM) · airframe 36,828 hrs · 41,387 cycles

FLIGHT 0090 PBI/TPA REPORT: TIMER LIGHT ILLUMINATED IN FLIGHT NO STAB ILLUMINATED IN CONTINUES MAN ON ONE CYCLE CAPT DECLARED EMERGENCY FOR EXPECTED FLAPS 0 LANDING FOR TIMER LIGHT TOGETHER WITH A STAB BOOT LT NOT ILLUM. IAW QRH. CORRECTIVE ACTION: R&R TIMER LIGHT CONTROL BOX IAW AMM 30-10-25, PERFORMED OPERATIONAL TEST OF AIRFOIL DE-ICE SYSTEM, CHECKS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,284 hrs · 40,838 cycles

FLIGHT 0117 FLL/FPO REPORT. GATE RETURN DUE TO EMERGENCY LIGHTS INOP ON ROW 3 4 5 6 AND OVERHEAD LIGHTS ON ROW 7. RECHARGHED BATTERY FOR 20 MINUTES IAW AMM 33-50-00 AND PERFORMED AN OPERATIONAL CHECK OF EMERGENCY LIGHTS IAW AMM 33-50-0-05-1, SYSTEM OPERATES NORMAL

Part: CONNECTOR — LOOSE (CABIN) · airframe 36,236 hrs · 40,786 cycles

FLIGHT 0123 EYW/MCO REPORT: EMERGENCY SIGN ON TOP OF BRIEDER STOPPED LIGHTING UP. FOUND CONNECTOR LOOSE ON LT GALLEY SECURED PLU TO GALLEY IAW CMM 25-33-82, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,236 hrs · 40,786 cycles

FLIGHT 0123 EYW/MCO REPORT: NO LIGHTS COMES ON, ON THE FIA PANEL FOR THE EMERGENCY LIGHTS WHEN THEY ARE ARMED. R&R LIGHT BULB ON F/A EMERGENCY LIGHT SWITCH IAW AMM 20-10-00-00, OPS CHECK GOOD

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 34,063 hrs · 38,454 cycles

EMERGENCY POWER LIGHT ILLUMINATED ON OVERHEAD PANEL, FOLLOWED QRH. LOST CAPTAIN EADI AND EHSI ON CAPTAIN SIDE. RESET EMERGENCY POWER SUPPLY CIRCUIT BREAKER, K-4, PERFORMED OPS CHECK OF EMERGENCY BUS AND FOUND NORMAL AT THIS TIME IAW AMM 24-35-00.

Part: BRAKE ASSY — WEAK (MLG) · airframe 33,750 hrs · 38,121 cycles

CAPTAIN BRAKES MUSHY. MINIMAL BRAKING. F/O BRAKES MUCH MORE RESPONSIVE. BLED THE BRAKE SYSTEM IAW AMM 32-42-00-02. OPS CHECK GOOD.

Part: BRAKE SYS — WEAK (MLG) · airframe 33,423 hrs · 37,783 cycles

BRAKES SPONGY. CHECKED HYD QTY, ACCUMULATOR PRESSURE, BRAKES FOR WEAR. BLED BRAKES IAW AMM CHAPTER 32-42-00-02 LOW SPEED MAINTENANCE TAXI GOOD, HIGH SPEED CREW TAXI CHECK GOOD.

Part: BRAKE SYS — MALFUNCTIONED · airframe 33,383 hrs · 37,742 cycles

NO BRAKES ON PARKING WITH ANTI-SKID SWITCH OFF ABLE TO STOP AIRCRAFT. INSPECTED AND TROUBLESHOT ANTI-SKID IAW TI NR: 340B-3243-2013-002, WM 32-43-00, AND AMM 32-34-00. OPS CHECK GOOD UNABLE TO DUPLICATE DISCREPANCY ON TAXI WITH ANTI-SKID SWITCH OFF.

Part: TRANSDUCER — FAULTY (ANTI SKID SYS) · airframe 33,373 hrs · 37,732 cycles

LOSS OF BRAKING DURING TAXI. ANTI-SKID SWITCH TURNED OFF AND REGAINED BRAKING ON AIRCRAFT. R & R WHEEL SPEED TRANSDUCER IAW MM 32-43-15-01. OPS CHECK OK.

Part: BRAKE SYS — WEAK (MLG) · airframe 33,369 hrs · 37,727 cycles

DURING TAXI, AFTER LANDING, BRAKES FELT MUSHEY AND LATE TO RESPOND TO PEDAL PRESSURE. BLED THE BRAKE SYS IAW AMM 32-42-00-05, LEAK CHECK AND OPS CHECK NORMAL.

Part: BRAKE SYS — WEAK (MLG) · airframe 33,369 hrs · 37,727 cycles

WHILE PARKING, BRAKES FELT SOFT. PERFORMED PROCEDURE TO BLEED THE WHEEL BRAKE SYSTEM IAW AMM 32-42-00-02, LEAK CHECK GOOD.

Part: CONTROL BOX — FAULTY (BRAKES) · airframe 33,331 hrs · 37,689 cycles

EXPERIERENCE LOSS OF BRAKING. AFTER TURNING OFF ANTI-SKID, AIRPLANE WAS BRAKING NORMALLY. INSPECTED AND FOUND ANTI-SKID CONTROL BOX AT FAULT ALSO BLEED BRAKE SYS. OPS CHECK GOOD AT THIS TIME IAW AMM 32-43-05 & 32-42-00.

Part: PANEL — LOOSE (PAX DOOR) · airframe 33,327 hrs · 37,684 cycles

F/A REPORTED HAVING TROUBLE CLOSING THE MAIN DOOR FROM INSIDE. IT CAN ONLY BE CLOSED FROM OUTSIDE. SECURED UPPER PANEL INBD CABIN MAIN DOOR, OPS TEST GOOD IAW AMM 52-10-00-05.

Part: PANEL — UNSECURE (PAX DOOR) · airframe 33,327 hrs · 37,684 cycles

F/A REPORTED HAVING TROUBLE CLOSING THE MAIN DOOR FROM INSIDE. IT CAN ONLY BE CLOSED FROM OUTSIDE. SECURED UPPER PANEL INBD CABIN MAIN DOOR, OPS TEST GOOD IAW AMM 52-10-00-05.

Part: WIRE — UNSECURE (EMERGENCY LIGHTS) · airframe 33,054 hrs · 37,296 cycles

EMERGENCY LIGHTING SYSTEM INOPERATIVE IN ROWS 8 AND 9. FOUND LOOSE WIRE CONNECTION ON ROW 8, SECURED AND OPS CHECK GOOD IAW AMM 33-50-20. R & R ROW 9 EMERGENCY LIGHT STRIP IAW AMM 33-50-20-04. OPS CHECK GOOD.

Part: BRAKE SYS — FAILED · airframe 32,808 hrs · 36,933 cycles

DURING THE TAXI INTO THE GATE BOTH CAPTAIN AND F/O LOST FULL BRAKING AUTHORITY.

Part: TRANSDUCER — INOPERATIVE (ANTI-SKID SYS) · airframe 32,808 hrs · 36,933 cycles

SUP: DURING THE TAXI INTO THE GATE, BOTH CAPTAIN AND F/O LOST FULL BRAKING AUTHORITY. INSPECTED FOUND NR 1 ANTI-SKID TRANSDUCER INOPERATIVE. ALSO, FOUND EXCESSIVE AIR IN BRAKE SYSTEM. R & R NR 1 ANTI-SKID TRANSDUCER IAW 32-43-15-04 MM. ALSO, BLED THE BRAKE SYSTEM IAW 32-42-00 -02, MM, OPS CHECK OK IAW 32-42-00 MM.

Part: BRAKE SYS — INOPERATIVE (MLG) · airframe 32,802 hrs · 36,926 cycles

BRAKES NOT WORKING PROPERLY DURING TAXI. BLED ALL 4 MAIN BRAKES. OPS CHECK GOOD IAW AMM 32-42-40.

Part: VALVE — MALFUNCTIONED (BRAKE SYS) · airframe 3,283 hrs · 36,926 cycles

FLIGHT 100, BRAKES WORK INTERMITTENTLY. BRAKES MUSHY AT TIMES. AT TIMES THERE IS ZERO BRAKING ACTION. R & R BRAKE VALVE. OPS CHECK/ LEAK CHECK GOOD.

Part: BRAKE SYS — MALFUNCTIONED · airframe 32,802 hrs · 36,926 cycles

FLIGHT 9002: BRAKE AUTHORITY IS INTERMITTENT. PERFORMED OPS CHECK OF THE ACFT BRAKE SYSTEM IAW AMM 32-42-40-05. CHECK GOOD.

Part: CONTROL BOX — MALFUNCTIONED (BRAKE SYS) · airframe 32,799 hrs · 36,923 cycles

FLIGHT 81: ON TAXI USING BRAKES, PLANE IS VERY HARD TO STOP. HAVING TO PRESS FULL BRAKES AND REVERSE TO STOP ACFT. R & R ANTI-SKID CONTROL BOX IAW AMM 32-43-05-04. PERFORMED OPS CHECK, OPS CHECK IS SATISFACTORY.

Part: FLAP SYSTEM — OUT OF RIG · airframe 32,791 hrs · 36,914 cycles

FLIGHT 108: AT T/O NOSE TRYING TO LIFT OFF WELL BEFORE ROTATION SPEED. THEN NOTICED TRIM WAS .5 TO .7500 NOSE DOWN ON THE TRIM INDICATOR IN LEVEL FLIGHT, TO HOLD A NORMAL APPROACH/LANDING CONFIGURATION, TRIM INDICATED .7500 TO 1 UNIT NOSE DOWN BELOW GREEN ARC, FLIGHT CHARACTERISTICS NORMAL, JUST TRIM ABORMALLY NOSE DOWN INDICATIONS. FLAPS APPEAR SLIGHTLY DEPLOYED IN THE UP POSITION. INSPECTED & FOUND LT & RT FLAPS TO NEED MECHANICAL RIGGING. PERFORMED MECHANICAL RIGGING OF THE FLAPS IAW AMM 27-51-00-05 PROCEDURE D, OPS CHECK GOOD. FLAP RIGGING COMPLETED. ACFT REQUIRES ELEVATOR TRIM LT. CHECKED ELEVATOR TRIM RIGGING AND LT ELEVATOR TRIM NEED ADJUSMENT. RE-RIGGED LT ELEVATOR TRIM IAW AMM 27-32-00-02 AND 27-32-00-05. FLAP AND ELEVATOR TRIM SYSTEM, OPS CHECKED NORMAL IAW AMM 27-51-00 AND 27-32-00.