N208WQ

Part: BATTERY PACK — INOPERATIVE (MEGAPHONE) · airframe 9,355 hrs · 9,069 cycles

CREW REPORTED THAT THE MEGAPHONE WAS INOPERATIVE. R & R MEGAPHONE BATTERIES IAW AMM AND OPS CHECKED GOOD.

Part: ANTENNA — CORRODED (NR 1 VHF) · corrosion level 2 · airframe 8,977 hrs · 8,693 cycles

DURING HEAVY CHECK, NR 1 VHF ANTENNA SHOWS EVIDENCE OF CORROSION AT BASE. MX R & R NR 1 VHF COMM ANTENNA IAW AMM 23-11-26.

Part: DOOR — CORRODED (LAV SERVICE) · corrosion level 2 · airframe 8,977 hrs · 8,693 cycles

DURING HEAVY CHECK. LAVATORY SERVICE DOOR HAS EVIDENCE OF CORROSION. FABRICATED NEW SERVICE DOOR DOUBLER AND SERVICE DOOR IAW DWG 85307797 AND SRM 51-42-05.

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 8,977 hrs · 8,693 cycles

DURING HEAVY CHECK, CORROSION WAS FOUND ON THE LAV SERVICE DOOR FUSELAGE DOUBLER UNDER BONDING WIRE ATTACH POINT. MX PERFORMED A REPAIR WITH A FABRICATED REPAIR PACKER DOUBLER AND FILLER IAW SRM 52-42-10 AND 51-25-10.

Part: SKIN — DAMAGED (ZONE 600) · airframe 8,977 hrs · 8,693 cycles

WHILE IN FOR HEAVY CHECK FOUND BOLT HOLE UNDER PANEL 622AT HAS MINOR DAMAGE ON 1 SIDE. MX PERFORMED PERMANENT REPAIR FOR DAMAGE TO FASTENER HOLE ON RT WING UPPER SKIN ASSY. RETURNED TO SERVICE. MAJOR

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 8,977 hrs · 8,693 cycles

DURING HEAVY CHECK, RT OTBD SEAT TRACK FROM BS 32.4 - 71.2. FOUND CORRODED AND PITTED IN NUMEROUS AREAS. MX R & R NEW SEAT TRACK IAW SRM 51-42-05.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 8,977 hrs · 8,693 cycles

DURING HEAVY CHECK. CORROSION FOUND ON INBD RT SIDE SEAT TRACK, AT BS 570 TO 612. MX R & R SEAT TRACK IAW SRM 51-40-07, 51-42-05 AND 51-40-15.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 8,977 hrs · 8,693 cycles

DURING HEAVY CHECK. RT OTBD SEAT TRACK FROM BS 229.5 - 571.5 CORRODED. MX R & R SEAT TRACK IAW SRM 51-42-05 AND SRM 51-40-15.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 8,977 hrs · 8,693 cycles

DURING HEAVY CHECK. RT OTBD SEAT TRACK FROM BS 571.5 - 670 FOUND CORRODED. MX R & R SEAT TRACK IAW SRM 51-42-05 AND 51-40-15.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 8,977 hrs · 8,693 cycles

DURING HEAVY CHECK. CORROSION WAS FOUND ON THE RT INBD SEAT TRACK BETWEEN STATIONS 612 - 670. MX R & R SEAT TRACK IAW SRM 51-42-05 AND 51-41-05.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 8,977 hrs · 8,693 cycles

DURING HEAVY CHECK, FOUND RT INBD SEAT TRACK FROM BS 228.5 - 570 CORRODED. MX R & R SEAT TRACK IAW SRM 53-20-49.

Part: SEAT TRACK — CORRODED (BS 570-670) · corrosion level 2 · airframe 8,977 hrs · 8,693 cycles

DURING HEAVY CHECK, LT INBD SEAT TRACK CORRODED FROM BS 570 TO 670. REMOVED AND REPLACED IAW SRM 51-42-05 AND 51-40-15.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 8,977 hrs · 8,693 cycles

DURING HEAVY CHECK, LT INBD SEAT TRACK FROM BS 228.5 - 570 FOUND CORRODED. MX R & R SEAT TRACK IAW SRM 51-42-05 AND 51-40-15.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 8,977 hrs · 8,693 cycles

DURING HEAVY CHECK. RT INBD SEAT TRACK FROM BS -39.00 TO 10.50 CORRODED. MX REMOVED AND INSTALLED NEW SEAT TRACK IAW SRM 51-42-05 AND 51-42-15.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 8,977 hrs · 8,693 cycles

DURING HEAVY CHECK, FOUND LT INBD SEAT TRACK BS 102.5 - 228.5 CORRODED. MX R & R SEAT TRACK IAW SRM 53-20-49.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 8,977 hrs · 8,693 cycles

DURING HEAVY CHECK. LT OTBD SEAT TRACK FOUND CORRODED. MX R & R SEAT TRACK FROM STA 229.5 TO 571.5 IAW SRM 51-42-05.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 8,977 hrs · 8,693 cycles

DURING HEAVY CHECK. MAINTENANCE FOUND CORROSION ON LT OUTBD SEAT TRACK FROM BS 32.4 TO 229.5. MX R & R SEAT TRACK IAW SRM 51-42-05 AND 51-42-45.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 8,977 hrs · 8,693 cycles

DURING HEAVY CHECK. MX FOUND CORROSION ON RT INBD SEAT TRACK FROM 102.5 TO 228.5. MX R & R SEAT TRACK IAW SRM 51-40-15 AND 51-42-05.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 8,977 hrs · 8,693 cycles

DURING HEAVY CHECK. LT OTBD SEAT TRACK FROM BS 571.5 - 568 HAD CORROSION AND PITTING THROUGHOUT ENTIRE LENGTH. MX R & R SEAT TRACK IAW SRM 51-42-05 AND 51-40-15.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 8,977 hrs · 8,693 cycles

DURING HEAVY CHECK. MX FOUND RT INBD SEAT TRACK FROM BS 10.50 TO 102.5 CORRODED. MX R & R SEAT TRACK IAW SRM 51-42-05 AND 51-40-15.

Part: SKIN — DENTED (ZONE 100)

DURING HEAVY CHECK. MX FOUND A DENT AND SMALL GOUGE IN LT AFT FUSELAGE SKIN APPROX 9 INCHES FORWARD OF FS 866.303 AND APROX .5 INCHES BELOW STRINGER 13P. MX PERFORMED MAJOR REPAIR IN SKIN IAW RD8/4-55-884.

Part: SKIN — DENTED (ZONE 200) · airframe 8,977 hrs · 8,693 cycles

DURING HEAVY CHECK. MX FOUND DENT AT AFT LOWER RT FUSELAGE SKIN FWD OF FS 866.303 BETWEEN STRINGERS 30 - 31S. MX REPAIRED DAMAGE IAW RD8/4-55-883.

Part: CABIN PRESSURE — FAILED · airframe 8,606 hrs · 8,326 cycles

AT 10000FT, CABIN PRESSURE MASTER WARNING LIGHT ILLUMINATED. AIRCRAFT LOST CABIN PRESSURE. CREW RAN THE CHECKLIST AND CONTINUED TO DESTINATION WITHOUT FURTHER INCIDENT.

Part: WARNING SYSTEM — FALSE ACTIVATION (HYDRAULIC SYS) · airframe 8,461 hrs · 8,167 cycles

DURING TAXI CREW REPORTED THE NR 3 HYDRAULIC CAUTION LIGHT ILLUMINATED. FLIGHT RETURNED TO THE GATE FOR MX. CONTRACT MX CHECKED THE NR 3 ACCUMULATORS AND THE RESERVOIR BOTH ARE SHOWING IN THE GREEN. RECYCLED DCMP C/B AND DRAINED RESIDUAL PRESSURE FROM NR 3 SYSTEM. CREW RAN NR 3 SYSTEM AND CYCLED ELEVATORS, ALL OP'S CHECKED GOOD.

Part: CABIN PRESSURE — FAILED · airframe 8,355 hrs · 8,068 cycles

AT 11,000FT ACFT LOST CABIN PRESSURE DURING DESCENT. CREW RAN CHECKLIST AND CONTINUED TO DESTINATION. ACFT LANDED WITHOUT FURTHER INCIDENT.

Part: WARNING LIGHT — ILLUMINATED (CABIN PRESSURE) · airframe 8,117 hrs · 7,837 cycles

FLIGHT 4931, ABORTED TAKEOFF DUE TO A PRESSURIZATION FAULT LIGHT. ABORTED TAKEOFF AT 60 KNOTS. AIRCRAFT RETURNED TO THE GATE FOR MAINTENANCE INSPECTION.

Part: RIB — CRACKED (RT WING) · airframe 7,764 hrs · 7,476 cycles

RIGHT I/B LEADING EDGE CLOSURE RIBS CRACKED. REPAIRED IAW TD340-57-11-17 CONTROL= 4208-32.

Part: WARNING SYSTEM — ACTIVATED (HYDRAULIC SYS) · airframe 7,375 hrs · 7,094 cycles

UPON INITIATING DESCENT CREW SAW THE HYDRAULIC VALVE LIGHT FLICKER ON AND OFF. AFTER A MINUTE IT CAME BACK ON AND STAYED CONSTANT. NOTICED THAT NR 2 HYDRAULIC QTY HAD DROPPED TO 0 AND THE NR 2 HYD PRESSURE WAS DROPPING. CREW RAN THE QRH WHICH CALLED FOR ALTERNATE GEAR EXTENSION. CREW DECLARED AN EMERGENCY AND RECEIVED DELAY VECTORS FROM MAF TOWER. ALTERNATE GEAR SHOWED ALL GEAR LOCK. LANDED SAFELY AND STOPPED ON THE RUNWAY. A/C WAS SHUTDOWN ON RUNWAY AND TOWED TO GATE.

Part: WARNING SYSTEM — FALSE ACTIVATION (HYDRAULIC SYS) · airframe 7,298 hrs · 7,019 cycles

FLIGHT 4872 IAH-BTR A/C 208WQ AIR RETURN DUE TO HYDRAULIC NR 1 CAUTION LIGHT. PERFORMED OPS CHECK OF THE NR 1 ENGINE HYDRAULIC PUMP CAUTION LIGHT PER FIM. OPS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 6,956 hrs · 6,688 cycles

AIRCRAFT DEPARTED IAH AND RECEIVED FORWARD CARGO DOOR LIGHT DURING CLIMBOUT. RETURNED TO IAH. CARGO DOOR SYSTEM OPS CHECKED GOOD.

Part: SELECTOR PANEL — FAILED (COCKPIT) · airframe 6,680 hrs · 6,429 cycles

TWENTY MINUTES NORTH OF IAH CREW REPORTED LT GEAR GREEN LIGHT STAYING ILLUM AFTER PULLING THE GEAR UP DURING CLIMB. F/A REPORTED THAT GEAR WAS UP BY LOOKING OUTSIDE. THE CREW REFERENCED THE QRH AND RETURNED TO IAH. AN EMERGENCY WAS DECLARED, THE CABIN WAS PREPAIRED FOR AN EMERGENCY AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. A/C TOWED TO THE GATE. MX CHANGED LANDING GEAR SELECTOR PANEL, AND PERFORMED GEAR SWINGS. OPS CHECKED GOOD.

Part: ADAPTER — MALFUNCTIONED (ENGINE) · airframe 6,099 hrs · 5,903 cycles

WHILE WAITING IN LINE FOR DEPARTURE THE CREW SMELLED A BURNING SMELL, NO SMOKE, AND RECEIVED AN ENGINE ADAPT HEAT LIGHT. RETURNED TO GATE. REPLACED ENGINE INTAKE ADAPTER, OPS CHECKED GOOD.

Part: SELECTOR VALVE — MALFUNCTIONED (LANDING GEAR) · airframe 5,846 hrs · 5,667 cycles

LANDING GEAR DID NOT EXTEND. CREW PERFORMED ALTERNATE GEAR EXTENSION PROCEDURE. LANDED WITHOUT INCIDENT. WAITED ON TAXIWAY TO PIN GEAR THEN TAXIED TO THE GATE ON ITS OWN POWER. REPLACED SELECTOR VALVE. WAITING ON WX TO CLEAR TO FERRY TO ALB FOR GEAR SWINGS OR MOVE EQUIPMENT TO EWR TO DO SWINGS THERE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 5,632 hrs · 5,462 cycles

PERFORM PERMANENT REPAIR OF BURN DAMAGE AT 9-OFF LOCATIONS IAW TD 400-53-10-67.

Part: SPOILER — MALFUNCTIONED (RT WING) · airframe 5,430 hrs · 5,282 cycles

RIGHT O/B SPOILER STAYS UP IN FLIGHT APPROX 20 SEC. THEN WENT DOWN ON UNCOMMANDED ROLL. CHANGED THE FOLLOWING PARTS: BOTH SPOILER LIFT DUMP VALVES, THE SOLENOID UNLOAD VALVE, AND THE SPOILER PCU. THE REASON FOR CHANGING ALL OF THESE WAS TO SUPPORT THE INVESTIGATION WITH PARKER AND BBD INTO THE UNCOMMANDED SPOILER DEPLOYMENT, WHICH I THEN LEARNED HAD HAPPENED ONCE BEFORE ON A POST AD CONFIGURED AIRCRAFT. AFTER THESE 4 PARTS WERE REPLACED THERE WAS NO FURTHER ISSUES REPORTED WITH THE SYSTEM.

Part: STRUCTURE — DAMAGED (ELEVATOR) · airframe 5,011 hrs · 4,910 cycles

PERFORMED PREM REPAIR FOR ELEVATOR LIGHTNING STRIKE DAMAGE IAW TD 400-55-10-08.

Part: PROXIMITY SENSOR — OUT OF RIG (MLG) · airframe 4,449 hrs · 4,380 cycles

MAIN LANDING GEAR DOOR OPEN IN FLIGHT AT ABOUT 210KTS WITH LANDING GEAR SELECTED IN UP POSITION (2 AMBER/2 RED IN TRANSIT LIGHT WERE ILLUMINATED - GEAR STARTED TO COME DOWN. CREW FOLLOWED CHECKLIST AND PROCEEDED TO THE DESTINATION WITHOUT FURTHER INCIDENT. FERRIED TO ALB - RIGGED PROX SENSOR AND PERFORMED GEAR SWINGS.

Part: FILTER — DIRTY (NR 1) · airframe 4,329 hrs · 4,262 cycles

ABORTED TAKEOFF NR 1 BLEED HOT LIGHT ILLUMINATED. CLEANED FILTER AND OPS CHECK GOOD.

Part: WARNING LIGHT — ILLUMINATED (SERVICE DOOR) · airframe 3,600 hrs · 3,554 cycles

ON ROTATION, SERVICE DOOR WARNING LIGHT ILLUMINATED. INITIALLY AIRCRAFT DID NOT PRESSURIZE. AFTER 15 MIN, AIRCRAFT STARTED TO PRESSURIZE. F/A SAID THERE WAS LOUD BANGING AND AIR COMING THROUGH THE DOOR. UPON ARRIVAL, MAINTENANCE INSPECTED THE AIRCRAFT, CABIN DOOR SEALS AND PRESSURIZED DOORS WITH NO DEFECTS NOTED.