N209SW

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAP) · airframe 29,987 hrs · 36,775 cycles

FLAP DISAGREEMENT AFTER TAKEOFF AND ON THE GROUND ON TAXI IN. REMOVED AND REPLACED RIGHT NACELLE FLAP ACTUATOR IAW AMM 27-50-08. REPLACED ROLLERS ON RIGHT OUTBOARD FLAP. OPS AND LEAK CHECKS GOOD. P/N: 343100-1001, S/N ON: 6024, S/N OFF: 0127.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 30,026 hrs · 36,818 cycles

FLAP DISAGREEMENT WHEN RETRACTING FLAPS AFTER TAKEOFF. REMOVED AND REPLACED FLAP CONTROL UNIT IAW 27-50-06. ALSO REMOVED AND REPLACED RIGHT NACELLE FLAP ACTUATOR IAW AMM 27-50-08 AND RII CARD 27-307. REPLACED ROLLERS ON RIGHT OUTBOARD FLAP. OPS CHECKS GOOD.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 29,721 hrs · 36,457 cycles

F/O AUTOPILOT CONTINUES TO MAKE UNCOMMANDED SMALL FORE AND AFT PITCH CHANGES. REMOVED AND REPLACED NR 2 AUTOPILOT COMPUTER WITH A SERVICEABLE COMPUTER. OPS CHECK GOOD IAW 22-10-00.

Part: WIRE — DAMAGED (CABIN) · airframe 28,804 hrs · 35,372 cycles

EMERGENCY LIGHT OVERHEAD BIN DOOR ROW 9 B & C INOP. REPAIRED WIRE TO EMERGENCY LIGHT AT 9BC. OPS CHECK GOOD.

Part: UPLOCK SENSOR — MALFUNCTIONED (MLG) · airframe 28,591 hrs · 35,124 cycles

UPON DEPARTURE, LANDING GEAR WOULD NOT RETRACT. SYSTEM A & B SHOWED DISAGREEMENT, WITH THE EXCEPTION OF SYSTEM A, LEFT MAIN GEAR. RAN QRH, NO RESULTS, CYCLED GEAR, NO RESULTS, PULLED & RESET LANDING GEAR CB, GEAR RETRACTED.REMOVED AND REPLACED ''A'' UPLOCK PROX SENSOR ON LEFT MAIN GEAR IAW MM 32-61-01. OPERATIONAL CHECK OF GEAR SWING, GOOD.

Part: WIRE HARNESS — DAMAGED (MLG) · airframe 28,228 hrs · 34,670 cycles

AFTER TAKEOFF AND GEAR RETRACTION, RECEIVED GEAR INDICATIONS, LOUD NOISE AND VIBRATION FROM THE NOSE THAT INCREASED WITH AIRSPEED. RETURNED TO LAX. PERFORMED GEAR RETRACTION. FOUND THAT GEAR DOORS WOULD NOT CLOSE DUE TO A FAULTY NOSE GEAR A-HARNESS. REMOVED AND REPLACED LT MLG DOWNLOCK B-HARNESS AND NLG A & B HARNESS. PERFORMED NUMEROUS GEAR RETRACTION AND EXTENSION CYCLES. OPS CHECKED GOOD.

Part: INDICATOR — MALFUNCTIONED (AIR SPEED) · airframe 28,128 hrs · 34,550 cycles

HIGH SPEED AURAL WARNING ON TAKEOFF ROLL AT 70 KNOTS. ABORTED TAKEOFF. REMOVED AND REPLACED CO-PILOTS AIRSPEED INDICATOR. OPS CHECKS GOOD. LEAK CHECK GOOD.

Part: SUPPORT — CRACKED (COCKPIT) · airframe 27,802 hrs · 34,166 cycles

COCKPIT LEFT SIDE LOWER SUPPORT FOR SIDE VIEW WINDOW, NEAR SIDE POST, IS CRACKED. FOUND DURING C-CHECK INSPECTION. REMOVED AND REPLACED LEFT SIDE LOWER SUPPORT IAW SRM 51-40-02 & 51-00-00. P/N: 120-34535-005.

Part: SKIN — CRACKED (LT NACELLE) · airframe 27,802 hrs · 34,166 cycles

LEFT NACELLE OUTBOARD SIDE JUST AFT OF FRAME 3 FORWARD HOOK FOR FORWARD COWL DOOR LATCH NACELLE IS CRACKED WHERE AFT PART OF THE LATCH HOOK GOES INTO THE NACELLE. FOUND DURING C-CHECK INSPECTION. FABRICATED AND INSTALLED REINFORCEMENT PLATE IAW EMB120 SRM 51-40-02.

Part: BRACKET — CRACKED (HYD BAY) · airframe 27,802 hrs · 34,166 cycles

CRACKED ALUMINUM BRACKET IN THE RIGHT SIDE OF THE HYDRAULIC BAY (AGAINST THE FIRE WALL, NEAREST TO THE INBOARD SIDE). FOUND DURING C-CHECK INSPECTION. FABRICATED AND INSTALLED REPAIR ANGLE IAW EMB SRM 51-70-06 & 51-40-02.

Part: BOLT — CORRODED (ELE BELLCRANK) · airframe 27,802 hrs · 34,166 cycles

THE BOLTS THAT HOLD THE ELEVATOR BELLCRANK MOUNT TO THE VERTICAL STABILIZER HAVE CORROSION ON THEM. FOUND DURING C-CHECK INSPECTION. REPLACED 8 BOLTS ON ELEVATOR BELLCRANK MOUNT WITH NEW ONES IAW 55-30-01.

Part: BRACKET — CRACKED (LT HYD RESERVOIR) · airframe 27,802 hrs · 34,166 cycles

LEFT HYDRAULIC RESERVOIR INBOARD VERTICAL BRACKET MOUNTING HAS 3 INCH + VERTICAL CRACK INSIDE THE BRACKET. FOUND DURING C-CHECK INSPECTION. REMOVED VERTICAL MOUNTING BRACKET AND INSTALLED NEW HYDRAULIC RESERVOIR MOUNTING BRACKET IN ITS PLACE IAW EMB SRM 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,802 hrs · 34,166 cycles

COCKPIT LEFT SIDE CRACK IN INTERCOSTAL BETWEEN FRAME 12A AND 13 (2 CRACKED RIVETS NEAR CRACK). FOUND DURING C-CHECK INSPECTION. STOP-DRILLED CRACK AND FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 51-40-02 AND 51-00-00.

Part: BUSHING — CORRODED (LT ELEVATOR) · airframe 27,802 hrs · 34,166 cycles

LT ELEVATOR ATTACHMENT BRACKET INBOARD BUSHINGS ARE CORRODED (HAT AND FLOAT BUSHINGS). FOUND DURING C-CHECK INSPECTION. REMOVED AND REPLACED BOTH HAT AND FLOAT BUSHINGS ON LEFT INBOARD ELEVATOR ATTACH BRACKET IAW 20-40-03.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,802 hrs · 34,166 cycles

FRAME 13 RT AND LT SIDE INBOARD AND OUTBOARD, PREVIOUS REPAIRS CRACKED OUTBOARD SIDE. CRACK GOES BEYOND DOUBLER ON THE RIGHT SIDE. FOUND DURING C-CHECK INSPECTION. FABRICATED AND INSTALLED DOUBLERS TO CRACKED AREAS IAW EMB SRM 51-00-00 AND 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 27,802 hrs · 34,166 cycles

FORWARD AND AFT, RIGHT AND LEFT SIDES, FLOOR SEAT TRACKS ARE CORRODED. FOUND DURING C-CHECK INSPECTION. INSTALLED NEW SEAT TRACKS IAW MM 53-01-05.

Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 27,596 hrs · 33,941 cycles

FRAME 13A DAMAGED AT DOOR ACTUATOR MOUNT. EXTENSIVE DAMAGE TO SHEAR CLIP 120-29047-001 AND SEVERAL OTHER TIPPED AND DAMAGED RIVETS OUTBOARD OF SHEAR CLIP. AT FRAME 13A, REMOVED AND REPLACED THE DAMAGED SHEAR CLIPS AND DAMAGED RIVETS IAW EMB SRM 51-00-00, 51-40-02, 53-00-03 AND 53-00-04, RII 53-301.

Part: ACTUATOR — FAILED (RUDDER) · airframe 27,574 hrs · 33,912 cycles

RUDDER PEDALS FROZE JUST AFTER TAKEOFF, NO WARNINGS OR AURAL INDICATIONS. RIGHT SIDE COULD ONLY MOVE AN 1 INCH OR SO, LEFT PEDAL HAD SLIGHTLY MORE TRAVEL. RUDDER PEDAL TRAVEL WAS NORMAL ON THE GROUND. REMOVED AND REPLACED GREEN AND BLUE SYSTEM RUDDER ACTUATORS IAW EMB MM 27-22-02. OPS AND LEAK CHECK GOOD IAW 27-20-00 & 27-22-00.

Part: BOOT — FAILED (LT WING) · airframe 27,393 hrs · 33,679 cycles

LEADING EDGE MIDDLE, RIGHT & LEFT WING BOOTS FAILED. RETURNED TO SLC. REMOVED AND REPLACED LEFT MIDDLE DEICE BOOT IAW 30-10-00. OPS & LEAK CHECK GOOD.

Part: FLAP — MALFUNCTIONED (WING) · airframe 26,712 hrs · 32,882 cycles

ON DEPARTURE RECEIVED A FLAP DISAGREEMENT ON THE OUTBOARD PAIR. WHILE ON THE RAMP WITHOUT ANY HYD POWER HAD A NACELLE DISAGREEMENT. LEFT NACELLE FLAP WAS HANGING DOWN A FEW DEGREES ALONG WITH ONE LIGHT BAR ILLUMINATED ON THE FLAP ANNUNCIATOR PANEL. REMOVED AND REPLACED ALL ROLLERS, BOTH FLAPS, AND FIXED INBOARD TRACK ON RIGHT OUTBOARD FLAP. CYCLED FLAPS WITH HYDRAULIC POWER. OPS CHECK GOOD.

Part: BALLAST — MALFUNCTIONED (LAVATORY) · airframe 26,651 hrs · 32,808 cycles

SMOKE COMING FROM LAV OVERHEAD LIGHTS. CIRCUIT BREAKER 30A POPPED. REPLACED LAV LIGHT BALLAST. OPS CHECKS GOOD.

Part: PRESSURE SWITCH — FAULTY (NR 1 ENGINE) · airframe 25,739 hrs · 31,724 cycles

ABORTED TAKEOFF DUE TO OIL WARNING (AURAL) AND NR 1 OIL LIGHT BLINKING ON. OIL LEVELS WERE SATISFACTORY DURING PREFLIGHT. ABORT INITIATED AT APPROXIMATELY 80 KTS. REPLACED NR 1 ENGINE LOW OIL PRESSURE SWITCH. OPS CHECK AND LEAK CHECK GOOD ON GROUND RUNUP. P/N 1153P0013-01, S/N OFF 1165.

Part: PROPELLER — FAULTY (LT ENGINE) · airframe 25,739 hrs · 31,724 cycles

ON ROLLING TAKEOFF, TORQUE ON LEFT ENGINE SHOT UP TO 134 PERCENT TQ. TAKEOFF AURAL WARNING AUTO FEATHER SOUNDED WITH SWITCH ON. ABORTED TAKEOFF. WHEN POWER LEVERS PULLED BACK TO GROUND IDLE, RT ENGINE READ 75 PERCENT TQ AND 53 PERCENT NH. WHEN AUTO FEATHER SWITCH TURNED OFF, RT ENGINE LIMITS/SPEEDS NORMAL. COMPLIED WITH OVER TORQUE INSPECTION ON LEFT ENGINE AND REPLACED LEFT PROPELLER ASSEMBLY.

Part: WIRE — OUT OF POSITION (CABIN) · airframe 25,739 hrs · 31,724 cycles

ROW SIX OVERHEAD RECESSED EMERGENCY LIGHTS ARE TOO DIM. BATTERY PACKS NEED TO BE REPLACED ON THAT CIRCUIT, NOT CHARGING. POSITIONED WIRES ON RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT TO CORRECT POSITION. OPS CHECK GOOD.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 25,739 hrs · 31,724 cycles

DESCENDING THROUGH 16,000 LOST CAPTAIN'S EHSI. NOTICED STRONG BURNING ODOR, SMOKE, WHICH CLEARED ALMOST IMMEDIATELY. NO CIRCUIT BREAKERS POPPED. REMOVED AND REPLACED CAPTAIN'S ELECTRONIC FLIGHT DISPLAY IAW EMB MM 34-22-03. OPS CHECK GOOD.

Part: WIRE — BURNED (ELECTRICAL SYS) · airframe 25,669 hrs · 31,654 cycles

WIRE W110-2230-16N IS BURNED AT CANNON PLUG P0952 PIN 43 TO GROUND. INSPECTED SURROUNDING WIRING AND REPLACED BURNED WIRE IAW WM 20-00-00.`

Part: DOOR SEAL — OUT OF POSITION (CARGO DOOR) · airframe 25,240 hrs · 31,140 cycles

RAPID DEPRESSURIZATION AT FL 260. MASKS DEPLOYED.REINSTALLED CARGO DOOR SEAL IAW MM 52-30-01 AND STOWED O2 MASKS IAW MM 35-20-01.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 24,908 hrs · 30,730 cycles

ON APPROACH, LEFT ENGINE EXPERIENCED A SEVERE POWER LOSS. TRIPLE CHIME ''ENGINE CONTROL'' AND WHITE ''MANUAL'' LIGHT ILLUMINATED. INITIATED A GO-AROUND TO AVOID TERRAIN CONTACT. ON GO-AROUND, REGAINED SOME POWER ON LEFT ENGINE. BROUGHT POWER BACK TO LEVEL OFF AND LEFT ENGINE AUTO-FEATHERED. POSSIBLE OVER-TORQUE OF LEFT ENGINE. BROUGHT LEFT POWER LEVER TO FLT-IDLE. ENGINE APPEARED HEALTHY. RESET AUTO-FEATHER; LANDED NORMALLY. DOWNLOADED FDAU. RIGHT ENGINE RECORDED EXCEEDANCE. RIGHT TORQUE MAX 112 PERCENT EXCEEDANCE (AVERAGE 111.5 PERCENT) FOR 007 SECONDS. MAX T6 TEMP 769 DEGREES. RAN BOTH ENGINES ON GROUND PER EMB MM 71-00-00. ALL PROCEDURES REF. MM 61-00-00. RIGHT ENGINE EXCEEDANCES WITHIN LIMITS

Part: FAN — SMOKE (AIR DIST) · airframe 4,157 hrs · 4,908 cycles

IMMEDIATELY AFTER ENGINE START WHEN PACKS WERE SWITCHED ON, SMOKE BECAME VISIBLE IN CABIN.REMOVED AND REPLACED LEFT GROUND COOLING FAN WITH A SERVICEABLE UNIT IAW MM 21-51-03.

Part: SWITCH — OUT OF ADJ (FUEL DOOR) · airframe 24,558 hrs · 30,292 cycles

SERVICE DOOR LIGHT CAME ON JUST AFTER ROTATION. RETURNED TO FIELD. ADJUSTED OUTBOARD FUEL PANEL MICRO SWITCH IAW 52-73-03. OPS CHECK GOOD.

Part: CABLE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 4,063 hrs · 4,788 cycles

BOTH TOP, OUTBOARD CABLES ON CARGO DOOR CORRODED. FOUND DURING C-CHECK. REMOVED AND REPLACED BOTH OUTBOARD CABLES IAW MM 52-31-00. P/N 120-32772-003, P/N 120-32772-007.

Part: FLAP TRACK — DIRTY (T/E FLAPS) · airframe 24,468 hrs · 30,189 cycles

FLAP DISAGREEMENT OUTBOARD PAIR WHEN SELECTING FLAPS UP AFTER TAKEOFF, 2 BARS STILL LIGHTED ON PANEL. WOULD NOT RECYCLE PER QRH. WOULD NOT EXCEED 15 DEGREES UPON LANDING. CLEANED AND LUBRICATED TRACKS AND ROLLERS. OPS CHECK NORMAL.

Part: STALL WARNING — MALFUNCTIONED (COCKPIT) · airframe 24,434 hrs · 30,152 cycles

SYSTEM 1 STALL WARNING CAME ON DURING TAKEOFF. REPLACED LAMP IN STALL WARNING PANEL. RERACKED NR 1 STALL COMPUTER. STALL WARNING OPS CHECK GOOD.

Part: REGULATOR — FAILED (CABIN PRESSURE) · airframe 24,272 hrs · 29,959 cycles

A/C WOULD NOT PRESSURIZE. TRIED MANUAL CONTROLLER. STILL WOULD NOT PRESSURIZE. LEFT PACK PRESSURE REGULATOR SHUT OFF VALVE LOW PRESSURE. REPLACED PRESSURE REGULATOR AND SHUT OFF VALVE IAW 21-50-01. P/N: 3214414-3, S/N ON: 693, S/N OFF: 949. PERFORMED FUNCTIONAL CHECK OF PRESSURIZATION SYSTEM IN AUTO/MAN IAW 21-30-00-501, PARAGRAPHS A-E. FUNCTION CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,160 hrs · 29,829 cycles

FORWARD EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVE AND REPLACE THE FORWARD EMERGENCY LIGHTS BATTERY PACK. P/N D366-04-001, S/N ON 7720, OFF 891. OPS CHECK GOOD.

Part: ENGINE — MALFUNCTIONED (LT ENGINE) · airframe 23,969 hrs · 29,595 cycles

LEFT ENGINE DID NOT SPOOL UP WITHIN NORMAL PARAMETERS AS DID THE RIGHT ENGINE ON TAKEOFF ROLL. AS A RESULT ABORTED TAKEOFF. RAN BOTH ENGINES TO TAKEOFF POWER SEVERAL TIMES. BOTH ENGINES ACCELERATED NORMAL. ALL CHECKS GOOD.

Part: ENGINE — OUT OF ADJ (LT ENGINE) · airframe 23,854 hrs · 29,460 cycles

LEFT ENGINE SPOOLED UP TO 30 PERCENT ON TAKEOFF THEN HUNG AT 30 PERCENT. ABORTED TAKEOFF. DEFERRED EEC. FOUND LEFT ENGINE OUT OF TRIM. TRIMMED ENGINE IAW MM 71-00-00. OPS CHECK GOOD.

Part: ENGINE — MALFUNCTIONED (LT ENGINE) · airframe 23,779 hrs · 29,372 cycles

ON INITIAL POWER APPLICATION LEFT TORQUE ONLY CAME UP TO APPROXIMATELY 25 PERCENT, RIGHT CAME UP NORMALLY. ABORTED TAKEOFF. RAN AIRCRAFT, ADVANCED BOTH ENGINES TO TAKEOFF POWER 6 TIMES. CHECKS NORMAL. VERIFIED EEC MANUAL REVERSION FOR OPERATION AND ADJUSTMENT. BOTH ENGINES CHECK OK. REMOVED RIGGING DOOR, OPEN LEFT COWL (OUTBOARD), INSPECTED LEFT ENGINE POWER LEVER LINKAGES AND ATTACHMENTS FOR CONDITION AND SECURITY. CHECKS GOOD. RIG DOOR REINSTALLED. COWL SECURED. UNABLE TO DUPLICATE SQUAWK.

Part: UPLOCK SENSOR — FAILED (MLG) · airframe 23,340 hrs · 28,823 cycles

FELT AND HEARD A STRONG VIBRATION AFTER GEAR RETRACTION. HAD A LEFT GEAR RED LIGHT (A SYSTEM). CYCLED GEAR, VIBRATION STOPPED. HAD 3 GREEN LIGHTS WHEN GEAR CAME UP THE VIBRATION STARTED AGAIN AND CONTINUED UNTIL GEAR WAS DOWN AND LOCKED. RED GEAR LIGHT WAS ILLUMINATED UNTIL GEAR WAS DOWN AND LOCKED AND HAD 3 GREEN. REPLACED LEFT MAIN LANDING GEAR A SYSTEM UPLOCK PROXIMITY SENSOR IAW MM 32-61-01. LANDING GEAR INDICATION AND OPERATION CHECKS GOOD. ABLE TO DUPLICATE GEAR DOOR WOULD NOT CLOSE CAUSING VIBRATION. DOOR OPS GOOD WITH NEW PROXIMITYSENSOR.

Part: CONNECTOR — INOPERATIVE (AIR INLET SWITCH) · airframe 22,567 hrs · 27,928 cycles

LEFT ENGINE AIR INLET INOP (WHEN SWITCH IS ON AND OFF) FL 240, TEMP -14 DEGREES. IT BEGAN OPERATING AGAIN ON DESCENT (TEMP +5 DEGREES). RETURNED TO SLC. FOUND FRONT BELLOWS LOOSE AND CANNON PLUG ON DEICE PRESSURE SWITCH FULL OF WATER. CLEANED WATER FROM SWITCH AND CANNON PLUG. OPS CHECK WARNING SYSTEM AND BOOT GOOD. RESECURED BELLOWS AND CLEANED AREAS AS REQUIRED.

Part: PCU — FAILED (RT ENGINE) · airframe 22,354 hrs · 27,680 cycles

TORQUE AND NP FLUCTUATE INFLIGHT. TORQUE PLUS OR MINUS 10 - 15 PERCENT, NP FLUCTUATES 5 - 7 PERCENT. NO FUEL FLOW FLUCTUATIONS NOTED. RIGHT ENGINE TAKEN TO FEATHER. NORMAL LANDING. REMOVED AND REPLACED RIGHT ENGINE PCU. OPS CHECK AND LEAK CHECKS GOOD. P/N ON: 782490-46, SN: 911041, S/N OFF: 860536.

Part: PROBE — FAILED (RT ENGINE) · airframe 22,275 hrs · 27,589 cycles

RIGHT EEC FAILED WHEN APPLYING TAKEOFF POWER. ABORTED TAKEOFF. REMOVED AND REPLACED NH PICKUP PROBE WITH SERVICEABLE UNIT IAW MM 77-12-00, OPS CHECKS GOOD. P/N ON: 3039242, S/N ON: CH17129, S/N OFF: CH13519.

Part: HARNESS — CONTAMINATED (MLG UPLOCK)

DEPARTING SLC, LANDING GEAR WOULD NOT RETRACT. RETURNED TO THE FIELD. DRAINED WATER FROM RIGHT MLG A UPLOCK HARNESS ON AIRFRAME. OPERATED GEAR SEVERAL TIMES, OPS CHECK GOOD MM 323000.

Part: SOLENOID VALVE — FAILED (MLG)

LANDING GEAR WOULD NOT RETRACT, RED TRANSIT LIGHTS CAME ON, BUT GEAR WOULD NOT MOVE. RETURNED TO SLC. REPLACED LANDING GEAR SOLENOID VALVE IAW 323203 AND LEFT MAIN LANDING GEAR OUTBOARD DOOR SEQUENCE VALVE IAW 323204. LEAK CHECK GOOD, PN ON: 12032943001SN: 458 SN OFF: 1855PN ON: 18190003, SN: 175 SN OFF: 710.

Part: RETRACT SYSTEM — CONTAMINATED (LT MLG)

LEFT MAIN GEAR WOULD NOT RETRACT. RETURNED TO FIELD. JACKED AIRCRAFT AND CYCLED GEAR WITH GROUND POWER AND GREEN SYSTEM ONLY. FAULT FREE CYCLES. SUSPECT SNOW AND SLUSH CONDITION TO BE THE FAULT. GEAR OPERATION TESTED OK IAW MM 32.

Part: FILTER — CONTAMINATED (HYDRAULIC SYST)

HYDRAULIC FILTER LIGHT ILLUMINATED ALONG WITH HYD LIGHT ON MAP. RETURNED TO SLC. FOUND HYDRAULIC PRESSURE FILTER BYPASS POPPED. REMOVED AND REPLACED PRESSURE RETURN FILTER. OPS CHECK AND LEAK CHECKED GOOD.

Part: DEICE BOOT — TORN (RT WING)

ALL INBOARD BOOTS FAILED STAB AND WING. RETURNED TO SLC. INSTALLED PATCH ON SMALL TEAR IN LEFT INBOARD WING BOOT. SET FOR 20 MINUTES. RUN UP OPS CHECKS GOOD.

Part: VALVE — MALFUNCTIONED (LEFT)

AFTER DEPARTURE WITH APU ASSIST TAKEOFF WHEN SWITCHING TO ENGINE BLEED, DUCT LEAK ILLUMINATED. LIGHT EXTINGUISHED AT 3 MINUTES. RETURNED TO SLC. REMOVED AND REPLACED LEFT SIDE PRESSURE VALVE WITH SERVICEABLE UNIT, IAW MM 30-10-06. OPS CHECKS GOOD.

Part: TEE SECTION — CORRODED (FRAME 16)

RIGHT T-SECTION BETWEEN CENTER AND RIGHT BUTT STRAPS AT FRAME 16 HAS CORROSION. REMOVED AND REPLACED RIGHT T-SECTION AT FRAME 16 IAW SRM 51-40-02.

Part: STRAP — CORRODED (LAVATORY)

RIGHT FORWARD BUTT STRAP UNDER LAVATORY AREA HAS CORROSION. REMOVED AND REPLACED RIGHT FORWARD BUTT STRAP UNDER LAVATORY AREA IAW SRM 51-40-02.

Part: CROSS BEAM — CORRODED (CABIN)

LEFT FLOOR CROSSBEAM AT FRAME 16 HAS CORROSION. REMOVED AND REPLACED LEFT FLOOR CROSS BEAM AT FRAME 16 IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (CABIN)

FORWARD LONG SECTION OF CABIN SEAT TRACK, RIGHT SIDE FLOOR LEVEL HAS NUMEROUS AREAS OF CORROSION. REPLACED RIGHT SIDE FLOOR LEVEL SEAT TRACK WITH NEW SEAT TRACK IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (CABIN)

LEFT FLOOR SEAT TRACK LONG SECTION UNDER GALLEY AREA HAS CORROSION. REMOVED AND REPLACED LEFT SEAT TRACK WITH A NEW SEAT TRACK IAW SRM 51-40-02.

Part: HARNESS — FAILED (LT MLG)

AT CRUISE, THE LEFT MAIN A GREEN INDICATION CAME ON, TRIED TO PUT TO GEAR DOWN NOTHING HAPPENED. USED THE ELECTRICAL OVERRIDE CHECK LIST AND GEAR CAME DOWN. REMOVED AND REPLACED THE LEFT MLG DOWNLOCK A HARNESS IAW MM 32-61-01, OPS CHECKS GOOD. PERFORMED GEAR SWING, OPS AND INDICATION CHECKS GOOD IAW MM 32-30-00.

Part: SEALS — FAILED (CARGO DOOR)

AT FL 280 AIRCRAFT DEPRESSURIZED. DESCENDED TO 12,000 FEET AND OXYGEN MASKS DEPLOYED. TRIED UNSUCCESSFULLY TO PRESSURIZE IN MANUAL MODE. MEL 21-31-1C.REPAIRED CARGO DOOR SEAL AND DEFERRED AIRCRAFT PRESSURIZATION. RESTOWED O2 MASKS. LAX REPLACED CARGO DOOR SEAL AND PRESSURIZED AIRCRAFT. OPS CHECKS GOOD.

Part: SEAL — FAILED (CARGO DOOR)

CABIN BROKE AT 21,000 FEET IN AUTO MODE. TRIED MANUAL AND FOUND UNSUCCESSFUL. DESCENDED TO 11,000 FEET AND WAS THROUGH 14,000 FEET BEFORE THE PASSENGER OXYGEN MASKS DROPPED, MEL 21-30-1C. OUTFLOW VALVES LOCKED OPEN. LAX SECURED LOOSE SECTION OF CARGO DOOR SEAL AT LOWER CORNER AND RESTORED OUTFLOW FLOW VALVES TO NORMAL CONFIGURATION, OPS CHECKS GOOD.

Part: HYD FILTER — DIRTY (RT HYD SYST)

AFTER TAKEOFF, RT HYDRAULIC FILTER LIGHT ILLUMINATED. FOUND RETURN HYDRAULIC FILTER BYPASS BUTTOM POPPED. REPLACED RETURN HYD FILTER, RESET BYPASS BUTTON, RAN RT HYD SYSTEM AND INSPECTED FOR LEAKS. NO LEAKS NOTED AND OPS CK GOOD.

Part: STALL WARN PNL — MALFUNCTIONED (E/E COMPT)

ON TAKEOFF ROLL, THE STALL SYSTEM ACTIVATED. ABORTED TAKEOFF. RT SYSTEM FAILS TO TEST PROPERLY. DEFERRED PER MEL 27-36-2. REMOVED STALL WARNING PANEL AND REPLACED IT WITH A SERVICEABLE ONE, IAW MM 27-34-08, OPS CKS GOOD, SEE F/L 75803.