N308SW

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 37,021 hrs · 47,665 cycles

ONE FUSELAGE SKIN SUPPORT CLIP AT FRAME 18A & BETWEEN STRINGERS 20R & 21R IS WORN, CORRODED BEYOND LIMITS. C-CHECK REPLACED SKIN SUPPORT CLIP AT FRAME 18A & BETWEEN STRINGERS 20R & 21R.

Part: SKIN — CRACKED (RT NACELLE) · airframe 37,021 hrs · 47,665 cycles

RT NACELLE LOWER AFT OTBD CORNER SKIN IS CRACKED. C-CHECK STOP DRILLED CRACK & INSTALLED REPAIR DOUBLER IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,021 hrs · 47,665 cycles

CORROSION SPOTS ON FLOOR T SUPPORT TO THE LT BUTT STRAP AT FRAME. C-CHECK REPLACED SHORT FLOOR T SUPPORT TO THE LT BUTT STRAP AT FRAME 15 & INSTALLED FASTENERS IAW SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 37,021 hrs · 47,665 cycles

CTR BRACKET BEHIND CAPT`S DV WINDOW CUTOUT IS CRACKED AT FRAME 12. C-CHECK REPLACED CTR SUPPORT BRACKET AT FRAME 12 BEHIND CAPT`S DV WINDOW CUTOUT IAW SRM.

Part: CHANNEL — CRACKED (RT MLG DOOR) · airframe 37,021 hrs · 47,665 cycles

RT MLG FWD OTBD DOOR Z CHANNEL IS CRACKED. C-CHECK REPAIRED RT MLG FWD OTBD DOOR Z CHANNEL IAW SST.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,021 hrs · 47,665 cycles

THERE ARE TWO PIN HOLES MOST LIKELY CAUSED BY CORROSION ON LT FWD OMEGA BEAM BETWEEN FRAME 15 & 16. C-CHECK CLEANED OUT CORROSION HOLES, INSTALLED PLUG RIVETS & APPLIED SURFACE FINISH ON TWO PIN HOLES IN LT FWD OMEGA BEAM BETWEEN FRAME 15 & 16 IAW ETD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 37,021 hrs · 47,665 cycles

CORROSION SPOTS ON SHORT FLOOR T SUPPORT TO THE LEFT BUTT STRAP AT FRAME 16. C-CHECK REPLACED CABIN FLOOR T SUPPORT LT BUTT STRAP AT FRAME 16.

Part: BRACKET — CRACKED (COCKPIT) · airframe 37,021 hrs · 47,665 cycles

PILOTS SIDE AFT INBD FLOOR PROP CRACKED UNDER JUMP SEAT FLOOR. C-CHECK REPLACED PILOTS SIDE AFT INBD FLOOR PROP L BRACKET UNDER JUMP SEAT FLOOR.

Part: BRACKET — CRACKED (COCKPIT) · airframe 37,021 hrs · 47,665 cycles

COPILOTS SIDE AFT INBD FLOOR PROP CRACKED UNDER JUMP SEAT FLOOR. C-CHECK REPLACED COPILOTS SIDE AFT INBD FLOOR PROP L BRACKET UNDER COCKPIT STEP.

Part: STRUCTURE — CRACKED (COCKPIT) · airframe 37,021 hrs · 47,665 cycles

COPILOT AFT INBD FLOOR PROP CRACKED. C-CHECK REPAIRED COPILOTS INBD AFT FLOOR PROP IAW ETD.

Part: ANGLE — CRACKED (RT WING) · airframe 37,021 hrs · 47,665 cycles

RT INBD WING RIB NR 8 FWD OF PANEL, LOWER ANGLE CLIP CRACKED. C-CHECK REPLACED LOWER ANGLE CLIP ON RT INBD WING RIB NR 8 FWD OF PANEL IAW SRM.

Part: ANGLE — CRACKED (RT WING) · airframe 37,021 hrs · 47,665 cycles

RT INBD WING RIB NR 5 FWD LOWER ANGLE CLIP CRACKED. C-CHECK REPLACED RT INBD WING RIB NR 5 FWD LOWER ANGLE CLIP IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 37,021 hrs · 47,665 cycles

BETWEEN ROWS 2 & 3 OF THE BELLY, HAS QUITE A LOT OF SURFACE CORROSION ON RIBS & SKIN. C-CHECK REMOVED, BLENDED OUT & APPLIED CONVERSION COATING TO TRACES OF CORROSION AREAS IN FUSELAGE INTERNAL SKIN BETWEEN FRAME 17 TO 19, ROWS 2 & 3 & STRINGER 20L TO 20R IAW SRM.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 37,021 hrs · 47,665 cycles

MAIN CABIN DOOR CUTOUT THRESHOLD NUTPLATE BRACKETS & FLOOR BEAMS AROUND ENTRY AREA HAVE SURFACE CORROSION. C-CHECK REPLACED MAIN CABIN DOOR CUTOUT THRESHOLD FWD & AFT NUTPLATE BRACKETS & MOST FWD LT BUTT STRAP & INSTALLED FASTENERS IAW SRM.

Part: PROBE — CHAFED (LT WING) · airframe 37,021 hrs · 47,665 cycles

LT OTBD WING 2ND PROBE OTBD OF NACELLE CHAFING ON LOWER STRINGER. C-CHECK BLENDED OUT CHAFE MARK IN LT OTBD WING 2ND PROBE OTBD OF NACELLE ON LOWER STRINGER IAW ETD.

Part: RIVET — CRACKED (RT NACELLE) · airframe 37,021 hrs · 47,665 cycles

RT NACELLE TO INBD UPPER WING FILLET HAS 1 CRACKED RIVET. C-CHECK REPLACED CRACKED LOCK FASTENER ON RT NACELLE TO INBD UPPER WING FILLET IAW SRM.

Part: CRADLE — CHAFED (RT NACELLE) · airframe 37,021 hrs · 47,665 cycles

RT NACELLE EXHAUST CRADLE AFT UPPER CORNER PREVIOUS REPAIR CHAFED. C-CHECK COMPLIED WITH PERMANENT REPAIR IAW ETD.

Part: HYDRAULIC SYSTEM — LOW (GREEN SYSTEM) · airframe 36,922 hrs · 47,541 cycles

GEAR DISAGREE ON TAKEOFF, RT MAIN GEAR DID NOT SHOW UP & LOCKED UNTIL SECOND ATTEMPT. GREEN SYSTEM QUANTITY LIGHT ILLUMINATED. FLT5291 SERVICED GREEN SYSTEM & PERFORMED MULTIPLE GEAR SWINGS, OPERATIONS CHECKED GOOD.

Part: CAM — OUT OF ADJUST (CABIN DOOR) · airframe 36,572 hrs · 47,125 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN & CLOSE. FLT#7413 ADJUSTED FWD LOCK CAM IAW AMM.

Part: BLEED VALVE — FAULTY (BLEED AIR SYS) · airframe 35,916 hrs · 46,348 cycles

SMOKE IN CABIN DURING DESCENT. SMOKE DETECTOR WENT OFF IN LAV. WHEN BLEEDS AND PACKS WERE SWITCHED TO LOW SMOKE APPEARED. (FLT 7388) REMOVED AND REPLACED THE RT HIGH STAGE BLEED VALVE IAW AMM. P/N: 979626-6 S/N ON: 892 S/N OFF: 2654

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 35,886 hrs · 46,313 cycles

ON DEPARTURE FROM SFO AIRCRAFT WOULD NOT PRESSURIZE IN MANUAL MODE. (FLT 5451) PERFORMED PRESSURIZATION OF AIRCRAFT IN MANUAL MODE WITH NO FAULTS. COULD NOT DUPLICATE. OPS CHECK GOOD.

Part: ACM — FAILED (AC BAY) · airframe 35,886 hrs · 46,313 cycles

SMOKE IN CABIN, SET OFF SMOKE ALARM IN LAV WHILE ON DESCENT OUT OF FL200. SMOKE IN COCKPIT AS WELL. (FLT 5303) REPLACED RIGHT PACK ACM. P/N: 2204540-4 S/N ON: N/A569SW S/N OFF: 77-298

Part: SMOKE DETECTOR — DETACHED (LAVATORY) · airframe 35,844 hrs · 46,253 cycles

LAV SMOKE DETECTOR CAME UNATTACHED FROM CEILING. (FLT 5625) RE-INSTALLED LAV SMOKE DETECTOR TO ITS MOUNTING BRACKET.

Part: COOLING FAN — MALFUNCTIONED (CABIN) · airframe 35,707 hrs · 46,066 cycles

LEFT PACK FAIL, SMOKE IN COCKPIT. (FLT 6282) REPLACED LEFT GROUND COOLING FAN. OPS CHECK GOOD AT THIS TIME. P/N ON: EVAC2322C2 S/N ON: 507 P/N OFF: AE1711AA0 S/N OFF: 127

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 35,676 hrs · 46,025 cycles

LEFT PACK BLOWING SMOKE INTO COCKPIT ON MANUAL AND AUTO. (FLT 5359) RAN LEFT PACK WITH ENGINE BLEEDS ON AND OFF ON GROUND FOR 15 MINS WITH NO DEFECTS NOTED COULD NOT DUPLICATE AT THIS TIME. OPS CHECK GOOD.

Part: WIRE HARNESS — FAULTY (RT ENGINE) · airframe 35,676 hrs · 46,025 cycles

RIGHT ENGINE TORQUE RAN AWAY TO 120% AFTER SETTING TAKEOFF POWER. (FLT 5309) REPLACED UPPER ENGINE WIRING HARNESS AND T1.8 SENSOR. P/N 1: 3037603 S/N ON: NSN S/N OFF: NSN P/N 2: 315911-01 S/N ON: NS N S/N OFF: NSN

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,514 hrs · 45,806 cycles

FORWARD FLOOR LEVEL EMERGENCY LIGHT NEAR MAIN CABIN DOOR DOES NOT ILLUMINATE. (FLT 5334) REPLACED FORWARD FLOOR LEVEL EMERGENCY LIGHT FIXTURE NEAR MAIN CABIN DOOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,505 hrs · 45,797 cycles

OVERHEAD AFT EMERGENCY OVERHEAD LIGHT DOES NOT ILLUMINATE. (FLT 7413) RELAMPED EMERGENCY LIGHT.

Part: CONTROL PANEL — MALFUNCTIONED (AUTOPILOT SYS) · airframe 35,315 hrs · 45,554 cycles

DURING APPROACH DISCONNECTED AUTO PILOT ON CENTER CONSOLE. AILERONS FELT TIGHT. RAN QRH FOR JAMMED AILERON. (FLT 7782) RECONNECTED AILERON DISCONNECT SYSTEM, REMOVED AND REPLACED AP PANEL.

Part: UNKNOWN — ODOR · airframe 35,015 hrs · 45,215 cycles

WITH BLEED SOURCE SELECTED TO APU THERE IS A HOT SMELL COMING FROM THE LEFT PACK. (FLT 7782) COULD NOT DUPLICATE. RAN LEFT PACK OFF APU BLEEDS FOR 20 MINUTES WITH NO ODOR.

Part: COOLING FAN — DEFECTIVE (LEFT) · airframe 33,769 hrs · 43,733 cycles

STRONG BURNING WIRE SMELL. (FLT 7756) REPLACED THE LEFT GROUND COOLING FAN. PN: AE1711AA0, SN OFF: 175

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,318 hrs · 43,183 cycles

EMERGENCY LIGHT BELOW F/A JUMPSEAT IS OUT. (FLT 6267) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,630 hrs · 41,140 cycles

ALL EMERGENCY LIGHTS AT ROW 6 INOPERATIVE. (FLT 6383) REPLACED NR 3 ELBP.

Part: CONTROL VALVE — INOPERATIVE (BRAKE SYSTEM) · airframe 30,778 hrs · 40,131 cycles

TAXIING INTO POSITION WITH ANTI-SKID ON, ATTEMPTING TO STOP ON RUNWAY, BRAKES WOULD NOT ENGAGE. (FLT 7775) REMOVED AND REPLACED RT BRAKE METERING CONTROL VALVE.

Part: RIB — CRACKED (NACELLE) · airframe 30,545 hrs · 39,847 cycles

RIB UNDER LEFT EXHAUST AFT INBOARD MOUNT CRACKED. (C CHECK) REPAIRED PER EMB APPROVED REPAIR AND SRM.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 30,545 hrs · 39,847 cycles

BUTT STRAP UNDER SEAT TRACK AT FRAMES 36 TO 39 CORRODED. (C CHECK) REPLACED PER SRM.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 30,545 hrs · 39,847 cycles

CORROSION ON LAVATORY AREA BUTT STRAPS BETWEEN FRAMES 38 AND 40. (C CHECK) REPLACED PER SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 30,545 hrs · 39,847 cycles

SECOND FROM AFT T-STRAP CORRODED AT PASSENGER ENTRY. (C CHECK) REPLACED PER SRM.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 30,545 hrs · 39,847 cycles

BUTT STRAP AFT AND OUTBOARD OF PASSENGER ENTRY CORRODED. (C CHECK) REPLACED BUTT STRAP PER SRM.

Part: RIB — CRACKED (RT WING) · airframe 30,545 hrs · 39,847 cycles

RIGHT WING INBOARD LEADING EDGE NOSE RIB CRACKED. (C CHECK) REPLACED PER SRM.

Part: TORQUE TUBE — WORN (CABIN DOOR) · airframe 29,996 hrs · 39,152 cycles

MAIN CABIN DOOR HANDLE VERY HARD TO OPERATE. (FLT 6266) REPLACED INTERNAL HANDLE ACTUATING TORQUE TUBE AND BEARINGS.

Part: LINKAGE — LACK OF LUBE (CARGO DOOR) · airframe 29,858 hrs · 38,991 cycles

MCD DIFFICULT TO OPEN AND CLOSE. (FLT 7772) LUBRICATED DOOR HANDLE LINKAGE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,661 hrs · 38,770 cycles

RED FORWARD EMERGENCY LIGHT INOP. (FLT 7772)RELAMPED.

Part: WIRE — BROKEN (CABIN) · airframe 29,552 hrs · 38,636 cycles

FIRST RED EMERGENCY LIGHT ON FLOOR INOP. (FLT 7770) REPAIRED BROKEN WIRE.

Part: SPLICE — DAMAGED (CABIN) · airframe 29,442 hrs · 38,485 cycles

FLOOR EMERGENCY LIGHTS AT 3A INOP. (FLT 7763) REPLACED SPLICES.

Part: SPLICE — DAMAGED (EMERGENCY LIGHT) · airframe 29,442 hrs · 38,485 cycles

RED EMERGENCY TRACK LIGHT AT FORWARD MOST STATION INOP. (FLT 7759) REPAIRED SPLICE.

Part: LIGHT — NOT SEATED (CABIN) · airframe 28,870 hrs · 37,788 cycles

FORWARD MOST CEILING EMERGENCY LIGHT INOP. (FLT 6318) RESEATED LIGHT BULB.

Part: TRIM PANEL — OUT OF POSITION (CABIN DOOR) · airframe 28,738 hrs · 37,608 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. (FLT 6287) REPOSITIONED LOWER TRIM, OPERATED MAIN CABIN DOOR NUMEROUS TIMES, OPS CHECK GOOD.

Part: HANDLE — FAILED (MLG) · airframe 28,663 hrs · 37,505 cycles

FLT 6841 - GEAR DISAGREE MESSAGE DISPLAYED. REPLACED GEAR HANDLE ASSEMBLY.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 28,554 hrs · 37,352 cycles

MAIN CABIN DOOR STICKS WHEN OPENING. (FLT 7765) LUBED DOOR ROLLERS AND HOOKS.

Part: HMU — POWER LOSS (ENGINE) · airframe 28,516 hrs · 37,306 cycles

FLT 7785 - LEFT ENGINE POWER LOSS ON CLIMB. REPLACED HMU.

Part: DOOR — STIFF (MAIN PAX) · airframe 28,413 hrs · 37,182 cycles

FLT 6494 - MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. REPOSITIONED FLIGHT ATTENDANT SEAT.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 28,322 hrs · 37,079 cycles

FLT 6102 - EMERGENCY "EXIT" SIGN ROW 9 BROKEN. RESECURED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,783 hrs · 36,351 cycles

FLT 5491 - EMERGENCY LIGHT ROW 1 INOP. RELAMPED.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LT MLG) · airframe 27,693 hrs · 36,231 cycles

FLT 5706 - LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. ADJUSTED LEFT MLG DOWNLOCK PROX SENSOR. REPLACED GEAR HANDLE ASSEMBLY, P/N 120-38594-401 S/N ON, 120346, S/N OFF: 120350.

Part: ACTUATOR — BINDING (PAX DOOR) · airframe 27,662 hrs · 36,193 cycles

FLT 5441 - FA REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. CLEANED AND LUBED DOOR HANDLE ACTUATOR AND BEARING COMPONENTS.

Part: GUIDE — BINDING (PAX DOOR) · airframe 26,846 hrs · 35,110 cycles

MAIN CABIN DOOR WILL NOT OPEN. FLIGHT 5473. ADJUSTED GUIDE RETAINING HARDWARE AND OPS CHECKED DOOR PER AMM 52-10-00.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 26,792 hrs · 35,045 cycles

FIRST TWO FLOOR EMERGENCY LIGHTS ARE INOP. (FLIGHT NR 5438) REPAIRED WIRING TO EMERGENCY LIGHTS. OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 26,463 hrs · 34,576 cycles

ON DESCENT, THE CABIN PRESSURE BEGAN TO INCREASE FOLLOWED BY A "CABIN PRESS WARNING" MESSAGE. FLIGHT 3616 - PRESSURIZED AIRCRAFT SEVERAL TIMES. COULD NOT DUPLICATE. OPS CHECK GOOD AT THIS TIME.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 26,256 hrs · 34,307 cycles

FLT 5590 - ROW 1 EMERGENCY LIGHT IS INOP. REPAIRED WIRING AT EMERGENCY LIGHT. OPS CHECK GOOD.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 26,187 hrs · 34,212 cycles

FLT 3695 - AUTO PRESSURIZATION FAILED ON CLIMB-OUT. REPLACED ELECTRONIC ALTITUDE CONTROLLER AND ELECTROPNEUMATIC OUTFLOW VALVE IAW AMM 21-30-03. OPS CHECK GOOD, PN 2091G010800, SN/OFF 205, PN 22201T011400, SN/OFF 527.

Part: BRACKET — CRACKED (LT TE FLAP) · airframe 25,541 hrs · 33,382 cycles

FLT 5490 - LEFT OUTBOARD FLAP, INBOARD ROLLER BRACKET IS CRACKED. REPLACED LEFT OUTBOARD FLAP, INBOARD ROLLER ASSEMBLY AS NEEDED IAW 51-40-02.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 25,319 hrs · 33,093 cycles

FLT 5561 - RED EMERGENCY LIGHTS ON FLOOR ARE INOP. REPAIRED WIRES AT RED EMERGENCY LIGHT FIXTURE.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,276 hrs · 33,029 cycles

FLT 5589 - MULTIPLE FLOOR LEVEL EMERGENCY LIGHTS ARE INOPERATIVE. REPAIRED WIRING ON FLOOR EMERGENCY LIGHTS.

Part: COFFEEMAKER — OVERHEATED (GALLEY) · airframe 24,561 hrs · 32,101 cycles

F/A REPORTS COFFEE POT OVERHEATED WITH A BURNING ODOR. REPLACED COFFEE POT WITH SERVICEABLE UNIT. OPS CHECKS GOOD.

Part: CONTROL VALVE — SMOKE (LT A/C PACK) · airframe 23,791 hrs · 30,977 cycles

SELECTED PACKS TO NORMAL AND LEFT PACK FAILED WITH AIR CONDITION SMOKE. REPLACED LEFT PACK TEMPERATURE CONTROL VALVE IAW 21-60-01. OPERATIONAL CHECKS GOOD.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 23,476 hrs · 30,548 cycles

RIGHT FLOORBEAM AT FRAME 13 ANGLE, INBOARD SIDE, CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED SUPPORT ANGLE AT FRAME 13A FLOOR PROP, INBOARD SIDE OF RIGHT FLOOR PROP PER EMB 120 SRM 51-40-02.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 23,476 hrs · 30,548 cycles

NR 10 STRINGER CRACKED BETWEEN RIBS NR 8 AND NR 9 AT RIGHT INBOARD WING, DISCOVERED DURING C-CHECK INSPECTION. REPAIRED NR 10 STRINGER BETWEEN RIBS NR 8, NR 9 INSIDE RIGHT WING IAW SRM 57-20-03 AND RII CARD 57-900-1000.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 23,476 hrs · 30,548 cycles

LEFT FLOORBEAM AT FRAME 13 CRACKED BOTH SIDES, DISCOVERED DURING C-CHECK INSPECTION. SPLICED IN REPLACEMENT SECTION PER EMB 120 SRM 53-10-10. SEE RII 53-800-1000.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 23,476 hrs · 30,548 cycles

LEFT FORWARD BULKHEAD IN FRONT OF 1ST SEAT LOWER ATTACH TRACK CORRODED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LOWER ATTACH TRACK FOR LEFT FORWARD BULKHEAD WITH A SERVICEABLE UNIT.

Part: RIB — CRACKED (LT WING) · airframe 23,476 hrs · 30,548 cycles

LEFT INBOARD WING RIB NR 8 LOWER CLIP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP ON LEFT INBOARD WING RIB NR 8 LOWER. SEE RII 28-900-1000 IAW SRM 51-40-02.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,451 hrs · 29,283 cycles

EMERGENCY LIGHTS CENTER SECTION AND ROW 6 INOP. REPLACED EMERGENCY LIGHTS BATTERY PACK. OPERATIONAL CHECKS GOOD, SN OFF 1193/0396.

Part: CONTROL VALVE — LEAKING (BRAKE SYSTEM) · airframe 22,416 hrs · 29,242 cycles

SHORTLY AFTER TAKEOFF, GREEN SYSTEM "LOW LEVEL" LIGHT ILLUMINATED AND STAYED ON AND THE BLUE SYSTEM WAS FLUCTUATING ERRATICALLY FROM ZERO TO FULL. REPLACED BLUE SYSTEM BRAKE CONTROL VALVE REF MM 32-41-02.

Part: STOP — OUT OF ADJUST (PAX DOOR) · airframe 21,986 hrs · 28,629 cycles

MAIN CABIN DOOR VERY HARD TO OPEN/CLOSE. ADJUSTED MAIN CABIN DOOR BACKSTOPS IAW MM 52-11-00, PG 501. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,144 hrs · 26,266 cycles

FIRST 4 FLOOR LEVEL EMERGENCY LIGHTS NOT WORKING. REPLACED LIGHT ASSY WITH SERVICEABLE UNIT. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 19,907 hrs · 25,899 cycles

ONE OF THE FLOOR EMERGENCY LIGHTING STRIPS AND THE 2 OVERWING EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED CENTER AND AFT ELBP. OPS CHECKED GOOD, PN D366-04-001 SN/OFF 551 PN D366-04-001 SN/OFF 1219.

Part: STICK SHAKER — INOPERATIVE (STALL WARNING) · airframe 19,566 hrs · 25,468 cycles

F/O STICK SHAKER INOPERATIVE. REPLACED STICK SHAKER IAW EMB MM 27-34-04, OPERATIONAL CHECK GOOD. P/N C-81802-2, S/N OFF 843.

Part: STICK SHAKER — INOPERATIVE (STALL WARNING) · airframe 18,571 hrs · 24,210 cycles

FOS STICK SHAKER INOPERATIVE. REMOVED AND REPLACED FOS STICK SHAKER IAW MM 27-34-04. OPERATIONAL CHECK SATISFACTORY. P/N: C-81802-2 S/N OFF: 641

Part: FITTING — LEAKING (HYD SYSTEM) · airframe 14,706 hrs · 19,342 cycles

WHILE INFLIGHT RECEIVED A LOW RESERVOIR PRESSURE LIGHT. WHEN EXTENDING GEAR THE MAIN PUMP LOW PRESSURE LIGHT ILLUMINATED. TURNED ELECTRIC PUMP TO ON. IMMEDIATELY LOW LEVEL LIGHT ILLUMINATED AND GAUGE WENT TO 0. PRESSURE FLUCTUATED BUT FLAPS CAME DOWN. PRESS DROPPED WHEN ELECTRIC PUMP OFF. TIGHTENED LOOSE HYDRAULIC LINE FITTING AT RIGHT ENGINE FIREWALL AND REPLACED ENGINE DRIVEN HYDRAULIC PUMP. RAN RIGHT ENGINE 30 MINUTES. NO LEAKS.

Part: RELAY — ARCED (COCKPIT) · airframe 14,549 hrs · 19,149 cycles

RELAYS FO SIDE PANEL HOT. SMOKE ODOR IN COCKPIT. REPLACED APU FEEDER PROTECTION RELAY K0152 AND BUS BARS W1264, W163 DUE TO ARCING. OPERATED AIRCRAFT ELECTRICAL UNDER HEAVY LOADS ON APU GENERATOR WITHOUT CONTACTOR OR BUS BAR AREA SHOWING ANY SIGNS OF ABNORMAL HEATING.

Part: SWITCH — DEFECTIVE (LT ENGINE) · airframe 12,124 hrs · 16,168 cycles

FUEL LOW TEMPERATURE LIGHT CAME ON DURING TAXI. INSTALLED SERVICEABLE FUEL TEMPERATURE SWITCH ON LEFT ENGINE. CHECKS OK.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 12,124 hrs · 16,168 cycles

CABIN PRESSURE PEGGED AT 2000 FPM, SWITCHED TO MANUAL; THAT HAD NO EFFECT ON PRESSURE. RETURNED TO SLC. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER IAW 21-30-00. OPS CHECK GOOD.

Part: TRANSDUCER — MALFUNCTIONED (ANTI-SKID SYS) · airframe 11,987 hrs · 15,996 cycles

ABORTED TAKEOFF DUE TO ANTI-SKID LIGHT ON OVERHEAD. ANTI-SKID DISENGAGES (ON RIGHT SIDE) THROUGH 60 KTS ON TAKEOFF ROLL UNTIL AIRBORNE, THEN NORMAL IN AIR. UPON LANDING DISENGAGES UPON TOUCHDOWN THROUGH 20KTS, THEN NORMAL AT LOW SPEEDS.REMOVED AND REPLACED LEFT INBOARD WHEEL SPEED TRANSDUCER. OPS CHECK GOOD, REF. 32-42-04. P/N: 140-043 S/N OFF: 81982

Part: PROBE — INOPERATIVE (RIGHT ENGINE) · airframe 11,951 hrs · 15,957 cycles

ABORTED TAKEOFF IN COD DUE TO ERRATIC NP GAUGE. TAXIED BACK TO GATE AND OBTAINED SPECIAL FLIGHT PERMIT. FERRIED AIRCRAFT TO SLC.INSTALLED SERVICEABLE NP PROBE ON RIGHT ENGINE. P/N: 01R3033515 S/N OFF: CH17235.

Part: ROD END — WORN (RIGHT PCU) · airframe 11,809 hrs · 15,795 cycles

ABORTED TAKEOFF DUE TO RIGHT ENGINE TORQUE FLUCTUATIONS. DEFERRED PER MEL 73-21-1. TROUBLESHOT SYSTEM. FOUND A WORN ROD END ON THE RIGHT ENGINE PCU. REPLACED THE ROD END AND PERFORMED AN OPS CHECK OF ENGINE. ALL CHECKS GOOD.

Part: RELAY — FAILED (FUEL CONTROL) · airframe 11,708 hrs · 15,672 cycles

RIGHT ENGINE TORQUE LOSS AT 14,000 FEET. PERFORMED OPS CHECK OF EEC 14,000 FT SWITCH PER MM 73-23-01. NO DEFECTS NOTED. REMOVED AND REPLACED REVERSION RELAY. PERFORMED OPS CHECK GOOD IAW MM 73-23-00. P/N: M83536/6-022

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 4,116 hrs · 4,854 cycles

MIDDLE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED MIDDLE ELBP IAW 33-50-02. OPS CHECK GOOD.

Part: FUSE — BLOWN (CABIN) · airframe 4,116 hrs · 4,854 cycles

EMERGENCY LIGHT STRIP IN AISLE INOP. REMOVED AND REPLACED FUSE. OPS CHECK GOOD.

Part: PRESSURE SWITCH — FAULTY (RT FUEL PUMP) · airframe 11,096 hrs · 14,944 cycles

DURING EN ROUTE CLIMB THE RIGHT REAR ELECTRIC FUEL PUMP COULD NOT SUPPLY ENOUGH PRESSURE. THE RIGHT FORWARD PUMP WOULD CYCLE ON AND OFF. WITH THE FORWARD PUMP IN THE ON POSITION THE LOW PRESSURE LIGHT WENT OUT. REMOVED AND REPLACED RIGHT ENGINE LOW PRESSURE SWITCH IAW EMB MM 73-32-01. RAN ENGINE. OPS CHECK OK.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 10,768 hrs · 14,547 cycles

PRESSURIZATION SYSTEM UNABLE TO MAINTAIN THE CABIN ALTITUDE SELECTED. OPERATED AUTO PRESSURIZATION WITH TEST BOX, OPERATION NORMAL. NO LEAKS FOUND AT EXITS OR BOTH ECS PACKS ENTERING CABIN. COULD NOT DUPLICATE.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 10,179 hrs · 13,848 cycles

AUTOPILOT AND TRIM ON THE MAP PANEL. FD COMMANDED PITCH DOWN. COMPUTER FLAG ON FOS SIDE. DC AFCS CIRCUIT BREAKER POPPED. ELECTRONIC ALARM IN THE HEAD SET. RETURNED TO SLC. RESET DC AFCS CIRCUIT BREAKER. PERFORMED OPS CHECK OF AUTOPILOT SYSTEM IAW MM 22-22-10. AUTOPILOT OPS CHECK GOOD AT THIS TIME.

Part: CIRCUIT BREAKER — FAILED (PITOT HEAT) · airframe 9,700 hrs · 13,293 cycles

NUMBER TWO PITOT HEAT CIRCUIT BREAKER POPPED INFLIGHT. RETURNED TO SLC. REMOVED AND REPLACED CIRCUIT BREAKER FOR NUMBER TWO PITOT HEAT. OPS CHECKS GOOD.

Part: WIRE — MISINSTALLED (PITOT HEAT) · airframe 9,687 hrs · 13,279 cycles

NUMBER TWO PITOT STATIC HEATER CB POPPED. RESET ONCE AND POPPED AGAIN. RETURNED TO FIELD. FOUND THE WIRES FOR NUMBER TWO AND AUX PITOT HEAT TO BE REVERSED. INSTALLED WIRES TO CORRECT PITOT HEAD IAW MM 30-32-00 AND 30-33-00. INSTALLED A SERVICEABLE AUX PITOT HEAD IAW 34-11-01, OPS AND LEAK CHECKS GOOD. P/N ON: 866NB2, S/N: 185393, S/N OFF: 1738315.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 9,314 hrs · 12,860 cycles

OUTBOARD FLAP DISAGREEMENT. COULD NOT FIX PER QRH. RETURNED TO SLC. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR IAW MM 27-50-09. OPS CHECKS AND LEAK CHECKS GOOD. RII 27-307. P/N ON: 343000-1003, S/N: 0330, S/N OFF: 0554.

Part: FUEL FILTER — MALFUNCTIONED (LT ENGINE)

ON CLIMBOUT FROM SLC, LEFT FUEL FILTER LIGHT CAME ON. RETURNED TO FIELD. REPLACED LEFT ENGINE LOW AND HIGH PRESSURE FUEL FILTERS, RUN UP OPS CHECKS OK, AND LEAK CHECK OK.

Part: DEICE LIGHT — ILLUMINATED (LT WING)

MIDDLE LEFT WING DEICE LIGHT ILLUMINATED FOLLOWED BY SEVERAL OTHER DEICE LIGHTS. RETURNED TO BFL. REPLACED AIR ON RIGHT ENGINE. PERFORMED OPS CHECK OF DEICE SYSTEM AND OPS CHECK GOOD AT THIS TIME.

Part: DEICE BOOT — FAILED (LT HORIZ STAB)

ON CLIMB, LEFT OUTBOARD STABLIZER DEICE BOOT FAILED, BOTH TIMERS. RETURNED TO FIELD. RAN BOTH ENGINES BUT COULD NOT DUPLICATE ON GROUND ON ALL SETTINGS. OPS CHECKS GOOD.

Part: ANNUNICATOR — MALFUNCTIONED (TE FLAPS)

DISAGREEMENT INDICATION WITH FLAPS UP FROM 15 DEGREES. RETURNED TO FIELD. REPLACED ANNUNICATOR UNIT IAW MM 27-50-05, OPS CHECKS GOOD.

Part: STRAP — CORRODED (CARGO COMPT)

BUTT STRAP UNDER FLOOR BOARD PANELS IN CARGO COMPARTMENT CORRODED. REMOVED AND REPLACED AFT CENTER BUTT STRAP IN CARGO COMPARTMENT IAW MM 51-40-02.

Part: RELAY BOX — INOPERATIVE (LANDING GEAR)

AFTER DEPARTURE, RED INTRANSIT LIGHT A-SYSTEM DISAGREED WITH B-SYSTEM. CYCLED GEAR DOWN 3 TIMES, GREEN OK BUT WITH GEAR UP SAME RED INTRANSIT LIGHT REMAINED ON. RETURNED TO FIELD. CHECKED RIGHT MAIN A-SYSTEM PROXIMITY SENSORS. REMOVED LANDING GEAR SELECTOR HANDLE ASSEMBLY, PROBLEM STILL EXISTS. REPLACED LANDING GEAR RELAY BOX WITH A SERVICEABLE ONE, OPS CHECKS GOOD.

Part: SWITCH — OUT OF ADJUST (AVIONICS DOOR)

SERVICE DOOR LIGHT ILLUMINATED AFTER TAKEOFF. RETURNED FOR LANDING. ALL DOORS SECURE. ADJUSTED NOSE AVIONICS BAY DOOR MICRO SWITCH, OPS CHECKS GOOD.