N288SW

Part: REGULATOR VALVE — FAILED (DE-ICE SYSTEM) · airframe 33,219 hrs · 48,364 cycles

RIGHT ENGINE DUCT LEAK WARNING. FOLLOWED QRH WHICH LED TO RIGHT ENGINE SHUT DOWN. (FLT 1300) REPLACED RIGHT DEICE PRESSURE REGULATOR VALVE. P/N 38E96, S/N OFF RF-1805.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,943 hrs · 47,979 cycles

THE 1ST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6493) REPLACED FUSE IN OVERHEAD PANEL BY ROW 1.

Part: CAM — OUT OF ADJUST (CABIN DOOR) · airframe 32,625 hrs · 47,562 cycles

MAIN CABIN DOOR IS DIFFICULT TO OPEN. (FLT 6527) LUBRICATED DOOR HANDLES (IN & OUT) AND ADJUSTED AFT LOCK CAM.

Part: SPAR — CRACKED (RT WING) · airframe 32,826 hrs · 47,814 cycles

RIGHT WING INBOARD INTERNAL DRY BAY CLOSEST TO NACELLE, SPAR IS CRACKED. (C-CHECK) REPAIRED RIGHT WING AUXILIARY SPAR INBOARD OF NACELLE PER ETD AND SRM.

Part: SKIN — CORRODED (PAX DOOR) · airframe 32,671 hrs · 47,616 cycles

PASSENGER DOOR SKIN IS CORRODED. (C-CHECK) REPLACED PAX DOOR SKIN PER SRM.

Part: SPAR CAP — CRACKED (LT WING) · airframe 32,826 hrs · 47,814 cycles

LEFT WING INBOARD INTERNAL DRY BAY CLOSEST TO NACELLE HAS CRACKED SPAR CAP. (C-CHECK) REPAIRED LEFT WING AUXILIARY UPPER SPAR CAPPER ETD AND SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,599 hrs · 46,095 cycles

FLOOR LEVEL EMERGENCY LIGHTS INOP. (FLT 6650) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,468 hrs · 45,895 cycles

EMERGENCY LIGHTS ON THE 1ST OVERHEAD CEILING INOP. (FLT 6938) RELAMPED EMERGENCY LIGHTS.

Part: FLAP — CRACKED (RT WING) · airframe 31,100 hrs · 45,362 cycles

RIGHT WING NACELLE FLAP CRACKED ON OUTBOARD SIDE. (C CHECK) REPAIRED PER SRM.

Part: TERMINAL — BROKEN (EMERGENCY LIGHT) · airframe 31,047 hrs · 45,291 cycles

EMERGENCY OVERHEAD LIGHT AT 6A INOP. (FLT 6820) REPLACED WIRE TERMINAL.

Part: FLAP — CRACKED (NACELLE) · airframe 30,058 hrs · 43,880 cycles

NACELLE FLAP CRACKED. (C-CHECK) REPLACED FLAP PER AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 29,245 hrs · 42,651 cycles

FLT 6263, CEILING EMERGENCY LIGHT INOP, ROW 7. RELAMPED.

Part: LIGHT — LOOSE (CABIN) · airframe 29,068 hrs · 42,389 cycles

WHITE FLOOR EMERGENCY LIGHT AT ROW 11 INOP. (FLT 6129) RESECURED BULB.

Part: LIGHT — BROKEN (CABIN) · airframe 28,955 hrs · 42,213 cycles

FLT 6006 - LOWER EXIT LIGHT ROW 6A BROKEN. REPLACED LIGHT ASSEMBLY.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 28,871 hrs · 42,087 cycles

FLT 6177 - FLOOR LEVEL FORWARD EMERGENCY LIGHT INOP. RELAMPED.

Part: STRINGER — CRACKED (RT WING) · airframe 29,147 hrs · 42,502 cycles

C-CHECK, RIGHT INBOARD WING STRINGER CRACKED. REPAIRED PER SRM.

Part: UNKNOWN — ODOR (CABIN) · airframe 27,494 hrs · 40,208 cycles

RIGHT BLEED OVERHEAT WARNING LIGHTS CAME ON ALONG WITH A BURNING ODOR AND VISUAL SMOKE IN THE MAIN CABIN. PERFORM OPS CHECK OF RT ENG BLEED, COULDN'T DUPLICATE AT THIS TIME.

Part: RELAY — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 27,192 hrs · 39,772 cycles

WITH EMERGENCY LIGHTS IN THE ARM POSITION, LIGHTS STAY ILLUMINATED. (FLIGHT NR 5728) REPLACED RELAY K0201. OPS CHECK GOOD.

Part: STRUCTURE — CRACKED (NACELLE FLAP) · airframe 26,709 hrs · 39,106 cycles

LEFT NACELLE FLAP IS CRACKED. REPLACED LEFT NACELLE FLAP IAW EMB MM CH 27-50-03.

Part: WIRE — DAMAGED (FUSELAGE) · airframe 26,375 hrs · 38,655 cycles

FLT 5561 - RED EMERGENCY LIGHTS ARE NOT WORKING. REPAIRED WIRING AT ENVIRONMENTAL SPLICE. OPS CHECK GOOD.

Part: FLAP TRACK — CRACKED (T/E FLAP) · airframe 25,632 hrs · 37,646 cycles

RIGHT INBOARD FLAP TRACK IS CRACKED. REPLACED FLAP TRACK WITH A SERVICEABLE UNIT IAW 57-53-02.

Part: SIGN — DAMAGED (EMERGENCY LIGHT) · airframe 25,211 hrs · 37,078 cycles

FLT 5720 - EXIT ROW EMERGENCY LIGHT ASSEMBLY IS BROKEN. REPLACED EXIT SIGN ASSEMBLY, P/N 10-1301-15.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 23,898 hrs · 35,276 cycles

EMERGENCY FLOOR LIGHT AT ROW 11A IS NOT WORKING. REPLACE LIGHT BULB ON FLOOR EMERGENCY LIGHT AT SEAT 11A. OPERATIONAL CHECKS GOOD.

Part: SMOKE DETECTOR — FALSE INDICATION (LAVATORY) · airframe 22,086 hrs · 32,610 cycles

SMOKE DET IN LAVATORY SOUNDS INTERMITTENTLY. REPLACED DETECTOR AND BATTERY. OPERATIONAL CHECK GOOD.

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 22,086 hrs · 32,610 cycles

FLOOR LEVEL EXIT SIGN AT 6C IS MISSING. INSTALLED SERVICEABLE EMER EXIT PANEL AT SEAT 6C. OPERATIONAL CHECK GOOD.

Part: SERVO — MALFUNCTIONED (AUTOPILOT) · airframe 21,688 hrs · 31,986 cycles

WHILE IN A DESCENT, AC PITCHED UP AND STARTED CLIMBING. BOTH FLIGHT DIRECTORS PITCHED UP AND DESC BUTTON WOULD NOT STAY ILLUM. REPLACED ELEVATOR AUTOPILOT SERVO IAW MM 22-10-05. OPERATIONAL CHECK GOOD.

Part: CONTROL PANEL — INOPERATIVE (STALL WARNING) · airframe 21,017 hrs · 30,981 cycles

STALL WARNING SYSTEM 2 INOP. REPLACED STALL WARNING TEST PANEL. OPERATIONAL CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,789 hrs · 30,631 cycles

LAST EMERGENCY LIGHT IN BACK OF CABIN IS OUT. INSTALLED BULB INTO SOCKET OF EMERGENCY LIGHT IN THE BACK OF THE CABIN. OPS CHECKS GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 20,621 hrs · 30,369 cycles

ROW 10 FLOOR LEVEL EXIT ROW WHITE LIGHT OUT. REPLACED BULBS AT ROW 10 EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD.

Part: SERVO — INOPERATIVE (STICK SHAKER) · airframe 20,037 hrs · 29,435 cycles

WHEN CAPTAIN'S STALL WARNING SYSTEM IS TESTED THE SHAKER DOES NOT ACTIVATE. REPLACED NR 1 STICK SHAKER SERVO. OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 19,751 hrs · 29,009 cycles

EMERGENCY LIGHTS BETWEEN ROW 2 & 5 INOPERATIVE. REPLACED BLOWN FUSE AND REPAIRED WIRES. OPERATIONAL CHECK GOOD.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 19,535 hrs · 28,675 cycles

EMERGENCY EXIT SIGN IN SEAT 6A BROKEN. REPAIRED EMERGENCY EXIT SIGN AT 6A. OPERATIONAL CHECK GOOD.

Part: SERVO — INOPERATIVE (STICK SHAKER) · airframe 18,952 hrs · 27,836 cycles

RIGHT STALL SHAKER INOPERATIVE. INSTALLED SERVICEABLE SERVO STICK SHAKER ON NR 2 SIDE. OPERATIONAL CHECK GOOD. P/N C-81802-2, S/N ON 408, S/N OFF 298.

Part: SEAL — DAMAGED (CARGO DOOR) · airframe 18,551 hrs · 27,218 cycles

LEVELING AT 22,000 CABIN PRESSURIZATION DUMPED. REPLACED CARGO DOOR SEAL AT 3 LOWER SEAL RETAINERS IAW EMB MM 52-30-01. LEAK CHECK GOOD.

Part: SERVO — WORN (RT RUDDER PEDAL) · airframe 18,514 hrs · 27,156 cycles

RIGHT RUDDER PEDAL RUBBING AND GRINDING AND CATCHING ON SOMETHING DURING FLIGHT CONTROL CHECK. REMOVED AND REPLACED RUDDER AUTOPILOT SERVO AND SERVO CLUTCH IAW MM 22-10-05 AND 27-00-03. OPERATIONAL CHECK GOOD. P/N 622-5734-004, S/N OFF 7268.

Part: FRAME — CRACKED (RT NACELLE) · airframe 18,380 hrs · 26,952 cycles

RIGHT OUTBOARD NACELLE INTERNAL FRAME CRACKED. DISCOVERED AT C-CHECK INSPECTION. INSTALLED DOUBLER AT AFFECTED AREA IAW 120 SRM 51-10-02 P2 SEC 2B.

Part: FRAME — CRACKED (RT NACELLE) · airframe 18,380 hrs · 26,952 cycles

RIGHT ENGINE FRAME NR 1 IS CRACKED ON OUTBOARD SIDE. DISCOVERED AT C-CHECK. INSTALLED NEW RIGHT ENGINE FRAME NR 1 IAW SB 120-54-0036 AND RII CARD RII54-301.

Part: FRAME — CRACKED (RT NACELLE) · airframe 18,380 hrs · 26,952 cycles

RIGHT INBOARD NACELLE INTERNAL FRAME CRACKED. DISCOVERED AT C-CHECK INSPECTION. APPLIED DOUBLER TO RIGHT INBOARD NACELLE FRAME IAW SRM 120 51-10-02 PG 2 SEC 2B.

Part: CHANNEL — CRACKED (RT NACELLE) · airframe 18,380 hrs · 26,952 cycles

RIGHT HYDRAULIC RESERVOIR LOWER SUPPORT CHANNEL CRACKED. DISCOVERED AT C-CHECK. REPLACED RIGHT HYDRAULIC RESERVOIR LOW SUPPORT CHANNEL IAW SRM 120 51-10-02 PG 3 SEC 3A.

Part: FRAME — CRACKED (LT NACELLE) · airframe 18,380 hrs · 26,952 cycles

LEFT OUTBOARD NACELLE INTERNAL FRAME CRACKED. DISCOVERED AT C-CHECK INSPECTION. APPLIED DOUBLER TO LEFT OUTBOARD NACELLE FRAME IAW SRM 120 51-10-02 PG 2 SEC 2B.

Part: FRAME — CRACKED (LT NACELLE) · airframe 18,380 hrs · 26,952 cycles

LEFT INBOARD NACELLE INTERNAL FRAME CRACKED. DISCOVERED AT C-CHECK INSPECTION. INSTALLED DOUBLER AT AFFECTED AREA IAW EMB120 SRM 51-10-02 PG 2 SEC 2B.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 17,286 hrs · 25,340 cycles

CA'S AP DOES NOT HOLD ALTITUDE. REMOVED AND REPLACED NR 1 APC-65B. OPS CHECK GOOD IAW MM 22-11-00. P/N: 622-8317-402, S/N OFF: 4147.

Part: ACTUATOR — MALFUNCTIONED (LT NACELLE FLAP) · airframe 17,176 hrs · 25,161 cycles

AFTER LANDING, BOTH NACELLE FLAPS WERE SLOW TO RETRACT, CAUSING DISAGREEMENT. NACELLE FLAPS EVENTUALLY RETRACTED ON THEIR OWN. REMOVED AND REPLACED LT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-00. OPS CHECKS GOOD. PN: 343100-1001, SN ON: 0228, SN OFF: 0175

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 17,050 hrs · 24,967 cycles

CAPTAIN'S AUTOPILOT AND TRIM FAIL. REPLACED CAPTAIN'S AUTO PILOT COMPUTER. OPS CHECK GOOD.

Part: SERVO — MALFUNCTIONED (STICK SHAKER) · airframe 16,985 hrs · 24,868 cycles

NR 2 STALL SHAKER INOPERATIVE. REPLACED NR 2 STALL SHAKER. SYSTEM TESTS NORMALLY IAW MM 27-34-00.

Part: COMPUTER — MALFUNCTIONED (AUTO PILOT) · airframe 16,921 hrs · 24,775 cycles

ALTITUDE HOLD ON CAPT SIDE WILL DRIFT 150' DOWN. REPLACED AUTO PILOT COMPUTER APC-65B. OPS CHECK GOOD IAW MM 22-10-00.

Part: FAN — MALFUNCTIONED (RT PACK) · airframe 16,438 hrs · 24,014 cycles

SMOKE IN CABIN AND ASSOCIATED RIGHT PACK FAIL. REPLACED RIGHT PACK GROUND COOLING FAN. OPS CHECKED NORMAL.

Part: ACTUATOR — LEAKING (T/E FLAP) · airframe 15,517 hrs · 22,597 cycles

ON TAXI OUT, AFTER SELECTING FLAPS 15 DEGREES, THE HYDRAULIC QUANTITY ON THE BLUE SIDE WENT TO ZERO WITH ASSOCIATED LIGHTS. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR IAW RII 27-307 AND 27-50-08. LEAK CHECKS GOOD. NO LEAKS NOTED AT THIS TIME.

Part: COOLING FAN — FAULTY (CABIN) · airframe 15,179 hrs · 22,064 cycles

RIGHT GROUND COOLING FAN STOPS INTERMITTENTLY AND CAUSES SMOKE IN CABIN. REPLACED RIGHT GROUND COOLING FAN. OPS CHECK GOOD.

Part: A/C PACK — CONTAMINATED (A/C BAY) · airframe 15,046 hrs · 21,833 cycles

F/A SMELLED SMOKE IN CABIN AFTER PAX DEPLANED IN MFR. CABIN HAD FILLED WITH SMOKE. LAV SMOKE DETECTOR ACTIVATED. CALLED FIRE DEPT. INVESTIGATED CABIN FOR SMOKE. RAN APU ON BOTH PACKS AT SEPARATE TIMES. INSPECTED EXTERIOR OF PACK UNITS. OIL NOTED ON RT PACK. RAN RT ENGINE WITH RT PACK. DETERMINED POSSIBLE CAUSE TO BE OIL IN RT BLEED & RT PACK. INSPECTED RT ENGINE BLEED DUCT AFT OF FIRE SEAL FOR OIL ON INSIDE. NONE NOTED. RAN RT PACK WITH RT ENGINE BLEED FOR 15-20 MINUTES. NO SMOKE NOTED. DID NOTICE RT PACK MODE SELECT IN MANUAL, SWITCHED TO AUTO. OPS CHECKED GOOD, NO DISCREPANCIES NOTED.

Part: ENGINE — LEAKING (RIGHT) · airframe 14,961 hrs · 21,715 cycles

RIGHT ENGINE SMOKES ON SHUTDOWN. FOUND ENGINE BLOWING OIL OUT FROM FRONT COMPRESSOR. REMOVED AND REPLACED RT ENGINE AS REQUIRED IAW 71-00-00. OPS CHECK GOOD. PACKS NO LONGER SMOKING.

Part: PIN — BACKED OUT (AUTOPILOT SYS) · airframe 14,939 hrs · 21,682 cycles

CAPTAINS AUTOPILOT DOES NOT CAPTURE GS WITH APPR MODE. CAPTAIN'S AUTOPILOT FAILED WITH AILERON SERVO FAILURE. REPLACED PUSHED OUT PIN 44 ON J3 OF PILOT'S AUTOPILOT COMPUTER RACK. CAPTAIN`S AUTOPILOT OPS CHECK GOOD IAW MM 22-10-00. TESTED AILERON SERVO WITH BOTH CAPT'S AND F/O'S AUTOPILOT. COULD NOT DUPLICATE DISCREPANCY. BOTH AUTOPILOTS AND AILERON SERVO OPS CHECKS GOOD IAW MM 22-10-00.

Part: CONNECTOR — LOOSE (COCKPIT) · airframe 14,016 hrs · 20,183 cycles

EXIT SIGN ON FIRST OFFICER'S SIDE BULKHEAD DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE TESTED. FOUND LOOSE CONNECTION. SECURED CONNECTION. OPS CHECK GOOD.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 13,647 hrs · 19,624 cycles

AFTER DEPARTURE, BOTH THE EHSI AND THE NAVIGATION SCREENS WENT BLANK ON THE FIRST OFFICER'S SIDE. REMOVED AND REPLACED CTL32 (NR 2). OPS CHECKS GOOD ON GROUND.

Part: COMPUTER — OUT OF TOLERANCE (E/E BAY) · airframe 12,172 hrs · 17,382 cycles

FIRST OFFICERS HDG FLAG AND NR 1 RMI FLAG ON IN CRUISE. RETURNED TO THE FIELD. RE-ORIENTATED BOTH NR 1 AND 2 AHRS SYSTEMS IAW 34-00-00. GROUND OPS CHECK GOOD AT THIS TIME.

Part: BELLCRANK — OBSTRUCTED (LT AILERON) · airframe 12,053 hrs · 17,202 cycles

ON DOWNWIND THE AILERONS FROZE FOR 12 SECONDS, WE WERE UNABLE TO MOVE YOKE. ON BASE TURN THE AILERONS FROZE FOR 5 SECONDS AND ON FINAL THE AILERONS FROZE FROM APPROX 200 FT AGL UNTIL 20 SECONDS AFTER ROLLOUT. AUTOPILOT WAS CONFIRMED DISCONNECTED BY BOTH PILOTS. WHEN AILERONS WERE FROZEN THE YOKE WAS NEUTRAL AND UNMOVEABLE BY BOTH PILOTS. REMOVED UPPER AND LOWER ACCESS PANELS TO LEFT AND RIGHT AILERONS. INSPECTED YOKE CHAIN DRIVE. NO DEFECTS NOTED. FOUND PANEL MISSING 2 SCREWS ON LT AILERON JUST FWD OF THE TRIM TAB. LEADING EDGE WAS BENT FORWARD AND IMPEDING TRAVEL ON LEFT AILERON BELLCRANK. RE-SECURED PANEL. SCREW HOLES ARE NOT ELONGATED. CLOSED ALL PANELS. CONTROL DISCONNECT LIGHTS OUT ON MAP.

Part: ACTUATOR — MALFUNCTIONED (ELEVATOR TRIM) · airframe 11,698 hrs · 16,687 cycles

ELEVATOR TRIM FROZE IN FLIGHT AND BROKE LOOSE SUDDENLY, CAUSING VIOLENT PITCH DOWN. REMOVED AND REPLACED RIGHT AND LEFT ELEVATOR TRIM TAB LINEAR ACTUATORS IAW EMB 120 MM 27-32-02 AND 27-00-01. LEFT TRIM ACTUATOR S/N OFF: 735, S/N ON: UNKNOWN. RIGHT TRIM ACTUATOR S/N OFF: 736, S/N ON: 426.

Part: SENSOR — FAILED (A/C PACK) · airframe 11,337 hrs · 16,168 cycles

NOTICED HOT AIRCRAFT BEFORE TAKEOFF. AFTER TAKEOFF FA SMELLED SMOKE AND SMOKE DETECTOR IN LAV WENT OFF. RETURNED TO LAX. INSTALLED NEW LEFT PAC DUCT TEMP SENSOR. CHECKS GOOD.

Part: VALVE — LEAKING (RT ENGINE) · airframe 10,660 hrs · 15,209 cycles

RIGHT ENGINE DUCT LEAK LIGHT ILLUMINATED ONE MINUTE AFTER TAKEOFF. RIGHT ENGINE WAS SHUT DOWN PER QRH PROCEDURE. RETURNED TO PSP AIRPORT. REPLACED RIGHT DEICE LINE PRESSURE REGULATOR VALVE. RAN RIGHT ENGINE FOR SEVERAL MINUTES AT TAKEOFF SETTINGS. OPS CHECKS GOOD. P/N ON: 38E96-6A, S/N: RF-2273, S/N OFF: B-2266.

Part: SEAL — LOOSE (CARGO DOOR) · airframe 10,608 hrs · 15,135 cycles

AIRCRAFT LOST PRESSURIZATION AT 17,000 FEET. SLOW LOSS OF PRESSURIZATION, DESCENDED PER QRH. RETURNED TO LAX. INSPECTED AND FOUND SMALL SECTION OF CARGO DOOR SEAL LOOSE FROM RETAINER. REINSTALLED AND SECURED CARGO DOOR SEAL. PRESSURIZED AIRCRAFT TO 5+ PSID. NO LEAKS NOTED. PRESSURIZATION OPS CHECKS GOOD.

Part: WIRE — BROKEN (DOOR WARNING)

PASSENGER DOOR LIGHT CAME ON AFTER TAKEOFF. RETURNED TO SEA. REPAIRED BROKEN WIRE AT DOOR HINGE, OPS CHECK GOOD IAW 52.

Part: CONTROLLER — MALFUNCTIONED (CABIN)

CABIN ALTITUDE CLIMBS IN AUTO, OK IN MANUAL. RETURNED TO SFO. REPLACED AUTO CONTROLLER. OPS CHECKS GOOD.

Part: PACK — FAILED (LEFT)

DIVERTED TO BUR WHEN THE LEFT PACK FAILED AND FILLED CABIN WITH SMOKE. OPERATIONAL CHECKED LEFT PACK, LEFT ENGINE HIGH STAGE BLEED SWITCHING SYSTEM, RAM AIR SYSTEM AND PACK FAIL SWITCH WIRING. NO DISCREPANCIES NOTED ANY WHERE. ALL SYSTEMS OPERATE NORMALLY.

Part: DUCT LIGHT — ILLUMINATED (RT ENGINE)

RIGHT DUCT LEAK LIGHT CAME ON AFTER TAKEOFF DURING CLIMB-OUT. WENT THROUGH PROCEDURE BUT THE LIGHT WOULD NOT EXTINGUISH UNTIL ENGINE SHUTDOWN. RETURNED TO SLC. INSPECTED ENTIRE RIGHT SIDE BLEED ON DUCT SYSTEM AND FOUND NO DISCREPANCIES. RAN AIRCRAFT ON GROUND FOR 1/2 HR AND COULD NOT DUPLICATE.

Part: BEAM — CORRODED (CABIN)

CORRODED CENTER OMEGA BEAM AFT CABIN ADJACENT TO LAVATORY. REMOVED CENTER OMEGA BEAM AFT CABIN ADJACENT TO LAVATORY AND REPLACED WITH A NEW OMEGA BEAM IAW SRM 51-40-02.

Part: BEAM — CORRODED (CABIN)

RIGHT CENTER FLOOR BOARD CROSS BEAM TOP PLATE CORRODED, ADJACENT TO LAVATORY. REMOVED AND REPLACED RIGHT CENTER FLOOR BOARD CROSS BEAM TOP T-SECTION ADJACENT TO LAVATORY IAW SRM 51-40-02.

Part: STRAP — CORRODED (CENTER)

AFT CENTER BUTT STRAP CORRODED. REMOVED AFT CENTER BUTT STRAP AND REPLACED WITH A NEW BUTT STRAP IAW SRM 51-40-02.

Part: STRAP — CORRODED (RIGHT)

RT AFT BUTT STRAP CORRODED. REMOVED AND REPLACED RT AFT BUTT STRAP WITH A NEW BUTT STRAP IAW MM SRM 51-40-02.

Part: STRAP — CORRODED (CENTER)

CORRODED BUTT STRAP JUST FORWARD OF AFT CENTER BUTT STRAP. REMOVED CENTER BUTT STRAP SECOND FROM AFT OF PLANE AND REPLACED WITH A NEW BUTT STRAP IAW SRM 51-40-02.

Part: HYDRAULIC LINE — FAILED (RT ENGINE)

IN-FLIGHT FAILURE OF THE BLUE HYDRAULIC SYSTEM WITH LOSS OF FLUID. FOUND NR 6 HYDRAULIC LINE CHAFING ON ENGINE OIL COOLER AIR INLET. REPLACED NR 6 LINE AND RIGHT ENGINE DRIVEN HYDRAULIC PUMP. RAN RIGHT ENGINE, OPS CHECK AND LEAK CHECK GOOD.