N351AG

Part: CONTROL PANEL — FAILED (CTOT) · airframe 38,300 hrs · 43,674 cycles

FLIGHT# 7006 STT/STX REPORT: ON VECTOR FOR ILS 10 STX APPARENT LEFT ENGINE FAILURE. CONT. W/VECTOR DECLARED EMERGENCY INTERCEPTED ILS AND LANDED, UPON SHUTDOWN IT WAS OBVIOUS LEFT ENGINE WAS ALREADY FEATHERED IE NO SOUND OR CHANGE IN ENGINE "FEEL" WHEN MOVING LEFT CONDITION LEVER TO FEATHER. INSPECTED ENGINE INLET/EXHAUST AND BOTH CHIP DETECTORS PER GE MM 72-00-00. NO FAULTS FOUND. CHANGED CTOT PANEL PER AMM 76-10-50-04, OPS CHECKED PER AMM 71-00-00, OPS CHECKED, RAN ENGINES PER GE MM 72-00-00, CHECKS GOOD.

Part: NOT REPORTED — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 37,811 hrs · 43,022 cycles

FLIGHT 0061 FLL/MCO REPORT, WHEN AIRCRAFT IS POWERED OFF, WITH EMERGENCY LIGHTS SWITCH IN THE OFF POSITION, EMERGENCY LIGHT TURNS ON AND REMAIN ON. RESET C/B APPLY GROUND POWER EMERGENCY LIGHT CHECKS GOOD IAW 33-50-00.

Part: PIN — BENT (EMERGENCY LIGHT) · airframe 37,809 hrs · 43,020 cycles

FLIGHT 0135 RSW/EYW REPORT, CIRCUIT BREAKER L-8 POPPED MORE THAN ONE TIME. REMOVED AND REPLACED LT EXTERIOR EMERGENCY LIGHT IAW AMM 33-50-25-02. OPS CHECKS GOOD IAW AMM 33-50-25-02. INSTALLED 2 PINS IAW WM 20-20-00.

Part: BULB — INOPERATIVE · airframe 37,510 hrs · 42,704 cycles

ARM LIGHT ON FLIGHT ATTENDENT LIGHT PANEL EMERGENCY LIGHT SWITCH INOPERATIVE. R & R THE ARM LIGHT BULB, OPS CHECK GOOD IAW AMM 33-50-00.

Part: DOWNLOCK SWITCH — FAILED (LT MLG) · airframe 37,239 hrs · 42,419 cycles

LEFT MLG DOWN AND LOCKED LIGHT DOES NOT GO OUT WITH GEAR UP. R & R THE LT MLG DOWN LOCK SWITCH IAW AMM 32-61-05-02 OPS CHECKED GOOD.

Part: LIGHT — DEBONDED (CABIN) · airframe 36,363 hrs · 41,517 cycles

2A EMERGENCY LIGHT STRIP ON FLOORBOARD IS DISBONDED. R & R THE EMERGENCY LIGHT, OPS CHECKED GOOD IAW AMM 33-50-20-04.

Part: ACM — FAILED (RIGHT) · airframe 36,272 hrs · 41,418 cycles

DURING CLIMBING OUT, SMELLED AN ODOR LIKE EPOXY COMING FROM THE COCKPIT VENTS. THE ODOR WENT AWAY AND THEN THE AIR BECAME HOT IN BOTH MANUAL AND AUTO MODES. NEVER GOT COLD IN THE COCKPIT. THE AIR IN THE CABIN STAYED COOL. SO ONLY THE FLIGHT DECK AIR WAS CONSTANTLY HOT. R & R THE RT ACM IAW TC 21-51-81, OPS CHECKED GOOD.

Part: CONTROL VALVE — FAILED (BRAKE SYSTEM) · airframe 36,065 hrs · 41,192 cycles

EXCESSIVE BRAKE PRESSURE REQUIRED TO SLOW THE AIRCRAFT DOWN ON LANDING ROLL, PEDALS ARE ALMOST DOWN TO THE FLOOR. R & R THE BRAKE VALVE IAW AMM 32-42-10. OPS AND LEAK CHECKED IAW AMM 32-42-40.

Part: RELAY — UNKNOWN (ESS BUSS) · airframe 35,642 hrs · 40,742 cycles

FOUND RIGHT ESS LIGHT ILLUMINATED, ALL THREE LANDING GEAR INDICATIONS ARE OUT AND NOT TESTING. FOUND THE RT PDU AND RT ESS BUSS RELAY STICKING. R & R THE RT PDU IAW AMM 24-31-20 AND R & R RT ESS BUSS RELAY IAW 20-10-00. OPS CHECKED BOTH SYS NORMAL.

Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 35,249 hrs · 40,352 cycles

FLIGHT 0075, LOST HYDRAULIC PRESSURE FOR STEERING AND BREAKING DURING TAXI. OVERIDE INOPERATIVE. R & R HYDRAULIC DRIVEN MOTOR PUMP IAW AMM 29-10-10. OPS AND LEAK CHECKED GOOD.

Part: SKIN — GOUGED (BS 718-730) · airframe 34,856 hrs · 39,911 cycles

FLIGHT 0067, GOUGE AFT OF CARGO DOOR. PERFORMED SHEET METAL REPAIR TO LOWER AFT CARGO DOOR IAW TO 340B-5330-2016-001.

Part: BRAKE SYS — WEAK (MLG) · airframe 34,543 hrs · 39,563 cycles

STIFF AND WEAK BRAKES. BLED BRAKES IAW AMM 32-42-00-02. OPS CHECK GOOD.

Part: BRAKE SYS — MALFUNCTIONED (MLG) · airframe 34,353 hrs · 39,354 cycles

CAPTAIN BRAKE PEDALS WENT ALMOST ALL THE WAY TO THE FLOOR FOR BRAKE EFFECTIVENESS. ALL HYD PRESSURES WERE IN THE GREEN. PERFORMED BLEEDING OF THE BRAKES IAW AMM 32-42-00-02, PERFORMED OPS CHECKS, OPS CHECK IS SATISFACTORY.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 33,970 hrs · 38,948 cycles

EMERGENCY LIGHT STRIP, LEFT SIDE DOES NOT ILLUMINATE. CABIN EMERGENCY LIGHT ON THE AISLE. GS4104, RESECURED LOOSE CONNECTION ON FIRST EMERGENCY PATH LIGHTING. IAW AMM 33-50-20-04. OPS CHECKS GOOD.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 33,482 hrs · 38,286 cycles

DURING TAXI OUT HYD PUMP FAILED. ENGINE NR 1 SHUTDOWN WITH T-HANDLE. R & R HYDRAULIC PUMP REF AMM 29-10-10-04. OPS CHECK GOOD. NO LEAKS, FOUND AND SAFETY WIRE REPLACED ON T-HANDLE.

Part: CONNECTOR — CONTAMINATED (MLG) · airframe 32,726 hrs · 36,995 cycles

AFTER DEPARTURE CONFIGURATION WARNING ACTIVATED IN FLIGHT ANY TIME CONDITION LEVERS AND POWER LEVERS POSITION CHANGE IT WILL TRIGGER CONFIGURATION WARNING HORN. FOUND SLUGE AND OIL LEAKS ON CONNECTOR PLUGS ON RT LANDING GEAR AREA CLEANED ALL CONNECTOR PLUG, PERFORMED GEAR SWING NO FAULT NOTED, COMPLIED WITH FUNCTIONAL CHECK FLIGHT, NO DEFECTS NOTED.

Part: LANDING GEAR — ICED (LEFT) · airframe 32,620 hrs · 36,817 cycles

AFTER TAKEOFF WHEN GEAR RETRACTED, ALL 3 GREEN EXTINGUISHED, INTRANSIT LIGHT CAME ON AND HYDRAULIC PUMP TURNED ON. GEAR DID NOT LOCK UP QRH COMPLETED, GEAR RECYCLED, RETRACTED AS NORMAL. AIR RETURN TO DEPARTURE. FOUND SIGNIFICANT ICE ACCUMULATION ON RT LANDING GEAR. EVIDENCE THAT A LARGE CHUNK OF ICE RECENTLY BROKE AWAY AT RT UPSTOP PAD ON SHOCK STRUT, EXPLAINING WHY A SECOND RETRACT ATTEMPT WAS SUCCESSFUL. GEAR RETRACT CHECKS GOOD.

Part: LANDING GEAR — MALFUNCTIONED · airframe 32,558 hrs · 36,717 cycles

GEAR WILL NOT SHOW UP AND LOCKED. SERVICED ALL 3 GEARS PERFORMED GEAR SWING, OPS CHECK GOOD.

Part: ANNUNCIATOR — FALSE INDICATION (MLG) · airframe 32,534 hrs · 36,674 cycles

CREW DID NOT GET THE THREE GREEN LIGHTS WHEN THE LANDING GEAR WAS LOWERED, PROCEDURES FROM QRH WERE FOLLOWED. INSPECTED AND OPERATION OF LT MAIN LANDING GEAR ANNUNCIATOR, OPS CHECK GOOD.

Part: CIRCUIT BREAKER — TRIPPED · airframe 32,324 hrs · 36,329 cycles

FLIGHT IDLE STOP, FAILED ON LANDING AND NOSE WHEEL STEERING FAILED ON ROLL OUT AFTER LANDING. RESET F1 BUTTON, COULD NOT DUPLICATE FAILURE, RESET CIRCUIT BREAKER F 5 FOR NOSE WHEEL STEERING OPS CHECK GOOD.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 31,379 hrs · 35,173 cycles

PASSENGER DOOR WILL NOT CLOSE FROM THE OUTSIDE. REMOVED PASSENGER DOOR COVER LUBE DOOR MECHANISM OPS CHECK OK.

Part: ELECTRONIC UNIT — LOOSE (WARNING SYSTEM) · airframe 31,118 hrs · 34,869 cycles

RIGHT MAIN BUSS AND RT ESSENTIAL BUSS LIGHT ILLUMINATED AND ASSOCIATED CIRCUIT BREAKERS TRIPPED. F/A REPORTED ELECTRICAL ODOR IN AFT CABIN. RERACKED WARNING ELECTRONIC UNIT PERFORMED FULL ELECTRICAL LOAD, OPS CHECKED GOOD.

Part: ACM — FAULTY (AC BAY) · airframe 29,940 hrs · 33,393 cycles

FLIGHT: 4010 GGT/FLL PILOT REPORTED SMELLED OF BURN SMELL AND THEN HOT AIR BLOWING OUT OF VENTS. REPLACED AIR CYCLE MACHINE, OPERATIONAL CHECKS GOOD.

Part: SPRING — DEFECTIVE (DOOR) · airframe 29,221 hrs · 32,635 cycles

FLIGHT:3603 ATL/GNV DOOR STAIRS JAMMING DURING EXTENSION AND RETRACTION. REPLACED LOWER HANDLE GAS SPRING, OPERATIONAL CHECK NORMAL.

Part: AIRSTAIR — LACK OF LUBE (PAX DOOR) · airframe 29,221 hrs · 32,635 cycles

FLIGHT: 4046 MGW/IAD DOOR STAIRS JAMMING DURING EXTENSION AND RETRACTION. LUBED PASSENGER STAIRS, OPERATIONAL CHECK GOOD.