N299SW

Part: PROXIMITY SENSOR — FAILED (LANDING GEAR) · airframe 35,728 hrs · 49,988 cycles

LG WOULD NOT COME UP UNTIL DOWN LOCK RELEASE SWITCH WAS PRESSED. THE GEAR EXTENDED NORMALLY FOR LANDING. FLT 5335 REPLACED THE NLG PROXIMITY SENSOR & PERFORMED NUMEROUS GEAR SWINGS, LANDING GEAR SYSTEM OPERATES NORMALLY. OPERATIONS CHECKED, PN ZS-00417-02.

Part: FITTING — CRACKED (LT WING) · airframe 35,590 hrs · 49,799 cycles

LT WING CRACKED CLIP UPPER IN PANEL MARKED NR 6 ABOVE WIRE HARNESS. C-CHECK REPLACED LT UPPER WING SKIN CLIP IN PANEL MARKED NR 6 IAW SRM.

Part: FITTING — CRACKED (LT WING) · airframe 35,590 hrs · 49,799 cycles

LT OTBD WING UPPER CLIP IS CRACKED AT RIB 20 AREA. C-CHECK REPLACED LT UPPER WING SKIN CLIP AT RIB 20 IAW SRM & AMM.

Part: FRAME — CRACKED (RT NACELLE) · airframe 35,590 hrs · 49,799 cycles

RT NACELLE CRACKED FRAME AT FWD COWL FWD BAYONET LATCH RECEPTACLE. C-CHECK REPLACED RT NACELLE FRAME AT FWD COWL FWD BAYONET LATCH.

Part: STRUCTURE — CRACKED (RT NACELLE) · airframe 35,590 hrs · 49,799 cycles

RT ENG OIL COOLER EXHAUST CRACKED AT OTBD CORNER. C-CHECK COMPLIED WITH PERMANENT REPAIR IAW ETD.

Part: ACM — DAMAGED (AC BAY) · airframe 34,984 hrs · 49,018 cycles

ON LANDING, PACKS WENT TO FULL HOT & STARTED TO SMELL. FLT#5406 GROUND COOLING FANS OPERATE NORMALLY, RAN LT & RT PACKS ON BOTH APU & ENGINE BLEED AIR SOURCES. NEVER WENT FULL HOT OR SMELLED. FOUND MINOR BLADE DAMAGE & VIBRATION ON RT TURNINE IMPELLER. REPLACED RT ACM IAW AMM. PN ON: 2204540-2, PN OFF: 2204540-4SER1, SN ON: 81-567R SN OFF: 6/9INGL0244

Part: COVER — MISSING (EXIT SIGN) · airframe 34,930 hrs · 48,939 cycles

EXIT SIGN COVER MISSING AT ROW 6A. FLT#5324 REPLACED MISSING EMERGENCY EXIT SIGN.

Part: FUSE — FAILED (CABIN) · airframe 34,348 hrs · 48,234 cycles

FIRST FEW FLOOR EMERGENCY LIGHTS DO NOT ILLUMINATE. (FLT 7388) REPLACED FUSE BY NR 1 ELBP.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 34,322 hrs · 48,205 cycles

FORWARD SECTION OF EMERGENCY LIGHTS FAIL TO ILLUMINATE. (FLT 5320) REPLACED NR 1 ELBP FUSE.

Part: PROXIMITY SENSOR — OUT OF ADJUST (TRIM SYSTEM) · airframe 34,112 hrs · 47,960 cycles

TRIM SET IN THE GREEN. TAKEOFF WARNING OF - TRIM - ON TAKEOFF ROLL, ABORTED TAKEOFF. (FLT 5479) ADJUSTED THE LEFT TRIM PROX SENSOR IAW AMM.

Part: FUSE — BLOWN (CABIN) · airframe 33,875 hrs · 47,628 cycles

EMERGENCY FLOOR LIGHTING INOP. (FLT 7761) REPLACED FUSE.

Part: FUSE — FAILED (EMERGENCY LIGHT) · airframe 33,644 hrs · 47,357 cycles

FLOOR EMERGENCY STRIP IS INOPERATIVE. (FLT 5447) REPLACED EMERGENCY LIGHTING SYSTEM FUSE BY FORWARD ELBP IN REFERENCE TO AMM.

Part: WIRE — DAMAGED (CABIN) · airframe 33,377 hrs · 47,026 cycles

EMERGENCY LIGHTS FLICKERED ON AND OFF. (FLT 7799) REPAIRED DAMAGED WIRE AND REPLACED CONTACTOR K0519.

Part: CONTACTOR — FAILED (EMERGENCY LIGHTS) · airframe 33,353 hrs · 46,998 cycles

EMERGENCY LIGHTS CYCLES ON AND OFF INTERMITTENTLY IN FLIGHT. (FLT 7771) REPLACED EMERGENCY BUS CONTACTOR K0028 IN REFERENCE TO MM. P/N: 11KC01AY1, S/N OFF: 15355

Part: RELAY — FAILED (EMERGENCY LIGHTS) · airframe 33,353 hrs · 46,998 cycles

EMERGENCY LIGHTS ILLUMINATED RANDOMLY, THEN THE FORWARD 1/2 OF THE LIGHTS WENT OFF. (FLT 5574) REPLACED RELAY K0221 AND CONTACTOR K0028.

Part: RADIO ALTIMETER — FAILED (COCKPIT) · airframe 33,353 hrs · 46,998 cycles

LANDING GEAR AURAL WARNING DURING SHORT FINAL. LANDING GEAR LEVER WAS IN THE DOWN POSITION WITH GREEN INDICATION. (FLT 5481) REPLACED THE RADIO ALTIMETER TRANSCEIVER. P/N: 622-2855-011, S/N OFF: 4FOC

Part: STRINGER — CRACKED (LT WING) · airframe 33,260 hrs · 46,885 cycles

LEFT LOWER WING STRINGER AFT OF NR 2 FUEL PANEL IS CRACKED. (SERVICE) REPAIRED IN REFERENCE TO EMB 120 SRM.

Part: PIN — BACKED OUT (EMERGENCY LIGHTS) · airframe 32,584 hrs · 46,008 cycles

FIRST FOUR FLOOR EMERGENCY LIGHTS ARE INOPERATIVE. (FLT 6359) FOUND FORWARD FLOOR EMERGENCY LIGHT CONNECTOR PIN OUT. PUSHED PIN IN PLACE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,508 hrs · 45,917 cycles

OVERHEAD EMERGENCY LIGHTS ABOVE ROW 9 B AND C ARE OUT. (FLT 7797) RELAMPED EMERGENCY LIGHTS.

Part: SEAT BELT — STUCK (COCKPIT) · airframe 32,230 hrs · 45,550 cycles

F/O'S SEATBELT WILL NOT RELEASE EASILY. (FLT 7776) REPLACED F/O'S SEATBELT ASSEMBLY.

Part: WIRE — BROKEN (CABIN) · airframe 32,074 hrs · 45,364 cycles

WHITE FLOOR EMERGENCY LIGHT NEAR SEAT 3A IS OUT. (FLT 5503) REPAIRED WIRING AT 3A FLOOR EMERGENCY LIGHTS.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 32,052 hrs · 45,339 cycles

CARGO COMPARTMENT LEFT FLOOR BUTT STRAPS SHOW SIGNS OF CORROSION. (C-CHECK) REPLACED CARGO COMPARTMENT LEFT FLOOR BUTTSTRAPS PER SRM.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 32,052 hrs · 45,339 cycles

CABIN FORWARD BUTTSTRAPS NEAR PAX DOOR ARE CORRODED. (C-CHECK) REPLACED BUTTSTRAPS AT FORWARD CABIN NEAR PAX DOOR PER SRM.

Part: HUB — GROOVED (LT PROPELLER) · airframe 32,644 hrs · 46,080 cycles

LEFT PROP HUB BORES HAVE HEAVY GROOVING. (C-CHECK) REPLACED LEFT PROP HUB.

Part: STRINGER — CRACKED (LT WING) · airframe 32,052 hrs · 45,339 cycles

CRACKED STRINGER INSIDE LEFT WING NR 2 FUEL PANEL. (C-CHECK) REPAIRED SPLICE STRINGER SECTION AT LEFT NR 2 FUEL PANEL 10 STRINGER PER SRM.

Part: FRAME — CRACKED (NACELLE) · airframe 32,644 hrs · 46,080 cycles

LEFT HYDRAULIC BAY AROUND DOOR STRUCTURE CRACKED. (C-CHECK) REPLACED DAMAGED SECTION OF LEFT HYDRAULIC FRAME OPENING IN REFERENCE TO EMB-120 SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 32,644 hrs · 46,080 cycles

STRINGER 19L BETWEEN FRAME 15 AND 15A HAS CORROSION. (C-CHECK) REPAIRED STRINGER 19L WITH SPLICE IN REFERENCE TO EMB 120.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 32,052 hrs · 45,339 cycles

CENTER FORWARD FLOOR BUTTSTRAP HAS SURFACE CORROSION. (C-CHECK) REPLACED CENTER FLOOR BUTTSTRAP PER SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 32,052 hrs · 45,339 cycles

CARGO COMPARTMENT ENTRANCE FLOOR T-SECTION FRAME IS CORRODED. (C-CHECK) REPLACED CARGO COMPARTMENT ENTRANCE FLOOR T-SECTION FRAME PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,992 hrs · 45,265 cycles

FORWARD FLOOR RED EMERGENCY LIGHT AT ROW 2 IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,940 hrs · 45,195 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 9 AND FLOOR LEVEL EMERGENCY LIGHT AT 8A ARE OUT. (6371) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,029 hrs · 44,128 cycles

FLOOR LEVEL EMERGENCY LIGHT NEAR ROW 4 IS OUT. (FLT 6815) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — UNSECURE (CABIN) · airframe 30,964 hrs · 44,038 cycles

ONE WHITE FLOOR LEVEL EMERGENCY LIGHT AT ROW 9 IS OUT. (FLT 6264) RE-SECURED BULB.

Part: CARBON SEAL — LEAKING (ACCESSORY G/B) · airframe 30,566 hrs · 43,498 cycles

LOW OIL PRESSURE WARNING ON LEFT ENGINE IN FLIGHT, CREW SHUT ENGINE DOWN PER QRH. (FLT 6264) REPLACED LEFT ENGINE ACCESSORY GEARBOX CARBON SEAL AND STARTER GARLOCK SEAL.

Part: WIRE — DAMAGED (CABIN) · airframe 30,496 hrs · 43,411 cycles

FORWARD FLOOR EMERGENCY LIGHT OUT. (FLT 7761) REPAIRED 2 WIRES FOR FORWARD EMERGENCY FLOOR LIGHT.

Part: BLOCKER DOOR — OUT OF ADJUST (AC PACK) · airframe 30,053 hrs · 42,906 cycles

SMOKE IN CABIN AND COCKPIT. (FLT 6183) ADJUSTED AND LUBRICATED LEFT PACK BLOCKER DOOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,612 hrs · 42,389 cycles

WHITE FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHT INOP. (FLT 7806) REPLACED LIGHT FIXTURE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,274 hrs · 42,011 cycles

FLOOR LEVEL EMERGENCY LIGHT ON LEFT SIDE INOP. (FLT 6181) RELAMPED EMERGENCY LIGHT.

Part: EEC — DEFECTIVE (RT ENGINE) · airframe 29,125 hrs · 41,826 cycles

NR 2 ENGINE SHUT DOWN IN FLIGHT, AIRCRAFT WAS SURGING WITH TQ AND NP FLUCTUATIONS. (FLT 1099) REPLACED RIGHT EEC. P/N 3039187, S/N OFF C95090004.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 29,156 hrs · 41,861 cycles

RIGHT SIDE FRAME 36 FLOORBOARD BUTT STRAP BEAM CORRODED BETWEEN FLOOR STRINGERS 151 AND 181. (C CHECK)REPLACED FLOORBOARD BUTT STRAP BEAM.

Part: FRAME — CRACKED (RT NACELLE) · airframe 28,452 hrs · 40,962 cycles

RIGHT NACELLE INBOARD FRAME 10 CRACKED. (C CHECK)REPAIRED PER SRM.

Part: BUSHING — LACK OF LUBE (MAIN DOOR) · airframe 28,354 hrs · 40,849 cycles

THE MAIN CABIN DOOR HARD TO OPEN. (FLT 7769) LUBED SHAFT BUSHINGS.

Part: BUSHING — DAMAGED (PAX DOOR) · airframe 28,145 hrs · 40,579 cycles

F/A REPORT MCD IS VERY DIFFICULT TO OPEN. (FLT 7767) REMOVED PAX DOOR FWD AND AFT LOWER HINGES AS NEEDED. REPLACED ALL BUSHINGS AND BOLTS IN HINGE ARMS AND AIRFRAME FITTING. RE-INSTALLED BOTH HINGES ARMS IAW 52-10-00. REPLACED PAX DOOR SEAL ON DOOR AC PRESSURIZED LEAK CHECK GOOD.

Part: BRAKE — LOOSE (MLG) · airframe 27,464 hrs · 39,697 cycles

FLT 7782 - NO BRAKES AT SLOW SPEED WITH ANTI-SKID ON. SECURED LOOSE HARDWARE ON ALL (4) WHEEL SPEED TRANSDUCER DRIVE TABS.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,061 hrs · 39,183 cycles

FLT 5748 - FIRST RED LIGHT OF THE FLOOR EMERGENCY PATH LIGHTING SYSTEM INOP. RELAMPED.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 26,779 hrs · 38,805 cycles

FLT 7790 - FIRST TWO EMERGENCY FLOOR LIGHTS INOP. REPAIRED BROKEN WIRE.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 26,779 hrs · 38,805 cycles

FLT 7754 - FIRST FOUR EMERGENCY FLOOR LIGHTS INOP. SECURED LOOSE WIRE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 26,674 hrs · 38,686 cycles

FLT 7811 - WHEN RIGHT BLEED SET TO AUTO-NORM CABIN FILLED WITH SMOKE. RAN RIGHT PACK WITH APU BLEED AND RIGHT ENGINE BLEED, BOTH AUTO AND LOW BLEED SELECTED. UNABLE TO DUPLICATE.

Part: FRAME — CRACKED (RT NACELLE) · airframe 26,103 hrs · 37,934 cycles

C-CHECK, RIGHT INBOARD NACELLE FRAME CRACKED. REPLACED FRAME.

Part: FRAME — CRACKED (FUSELAGE) · airframe 26,103 hrs · 37,934 cycles

C-CHECK, CRACK IN FRAME IN FRONT OF LEFT HEAT EXCHANGER. INSTALLED DOUBLER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 26,103 hrs · 37,934 cycles

C-CHECK, CRACK IN FRAME IN FRONT OF RIGHT HEAT EXCHANGER. INSTALLED DOUBLER REPAIR ON FRAME.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 26,103 hrs · 37,934 cycles

FLT 3563 - EMERGENCY EXIT LIGHT AT 6 A INOP. CONNECTED LOOSE WIRE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,602 hrs · 37,304 cycles

ROW 6 EMERGENCY LIGHTS ARE INOP. (FLT 5785) REPLACED EMERGENCY LIGHT BATTERY. OPS CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 25,439 hrs · 37,078 cycles

FLT 5717 - FIRST OFFICERS DV WINDOW IS CRACKED. REPLACED COPILOT'S WINDOW IAW MM 56-11-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,396 hrs · 37,022 cycles

FLT 5464 - EMERGENCY EXIT SIGNS WILL NOT ILLUMINATE WHILE TESTING. REPLACED ELBP ABOVE ROW 6. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,582 hrs · 35,978 cycles

FLT 3722 - AFT EMERGENCY LIGHT AT ROW 9 IS INOP. INSTALLED SERVICEABLE ELBP IAW AMM 33-50-02. OPS CHECK GOOD.

Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 23,009 hrs · 33,912 cycles

ENTRY WAY EXIT PLACARD IS MISSING. REMOVED REMAINING EXIT SIGN HOUSING AT AND INSTALLED NEW LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD, P/N 10-1301-15.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 22,942 hrs · 33,838 cycles

FIRST SECTION OF EMERGENCY FLOOR LIGHTING DOES NOT ILLUMINATE. REPLACED FORWARD EMERGENCY LIGHTING BATTERY PACK. OPERATIONAL CHECKS GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 22,711 hrs · 33,515 cycles

CAPTAIN'S WINDSHIELD PANE AND FO'S WINDSHIELD PANE SHATTERED ON LANDING ROLLOUT. REPLACED CAPTAIN'S WINDSHIELD IAW EMB120 AMM REF NR 56-10-01, P/N NP-151311-1 S/N OFF 04149146184. REPLACED FIRST OFFICER'S WINDSHIELD IAW EMB120 MM 56-10-01 AND RII 56-200-1000, P/N NP-151311-2, S/N OFF 1526H3005. OPERATIONAL CHECKS GOOD.

Part: NACELLE — CONTAMINATED (LEFT) · airframe 22,616 hrs · 33,407 cycles

UPON AIRCRAFT POWER DOWN CREW NOTICED SMOKE COMING FROM THE LEFT ENGINE NACELLE. INSPECTED ENGINE COMPARTMENT AND NOTED EXCESS GLYCOL. NO OTHER DISCREPANCIES NOTED.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 22,541 hrs · 33,309 cycles

PAX ENTRANCE LOWER THRESHOLD ANGLE IS CORRODED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED PAX ENTRANCE LOWER THRESHOLD ANGLE AND CLEANED AND TREATED ALL OTHER AREAS BELOW ANGLE IAW CPM 51-14-00.

Part: SKIN — CRACKED (FUSELAGE) · airframe 22,541 hrs · 33,309 cycles

FUSELAGE SKIN CLEAT CRACKED JUST FORWARD AND ABOVE FORWARD CARGO DOOR TRACK, DISCOVERED DURING C-CHECK INSPECTION. REPLACED SKIN CLEAT IAW RII 53-800-1000 AND IAW RM 57-40-02 AND 51-10-02, PG 3, SEC 3A.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAPS) · airframe 20,171 hrs · 29,982 cycles

FLAP LIGHT AND ADVANCE STALL WARN LIGHT ON MAP ASYMMETRY, CONTROL FAULT AND DISAGREEMENT LIGHTS CAME ON IN CRUISE. REPLACED FLAP ANNUNCIATOR ASSY AND RIGHT NACELLE FLAP ACTUATOR IAW EMB MM 27-50-05 AND 27-50-03. OPERATIONAL CHECK GOOD, PN OFF 306900-10176; SN OFF 0076 PN 343100-1001; SN OFF 0167.

Part: BUTTON — STUCK (STALL WARNING) · airframe 19,594 hrs · 29,085 cycles

STALL WARNING BUTTON STICKS IN DOWN POSITION. REMOVED AND REPLACED STALL WARNING PANEL. OPERATIONAL CHECKS GOOD IAW 27-00-00.

Part: GASPER FAN — INOPERATIVE (CABIN) · airframe 19,024 hrs · 28,216 cycles

SMELLED SMOKE IN THE CABIN RIGHT BEFORE LANDING. REPLACED GASPER FAN. OPERATIONAL CHECK GOOD.

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · airframe 19,056 hrs · 28,264 cycles

CENTER BUTT STRAP BELOW CABIN FLOOR AFT OF ROW 10 CORRODED, ITEM FOUND AT C-CHECK INSPECTION. NEW BUTT STRAP INSTALLED IAW SRM 120 51-10-02 PG 3 SEC 3.A.

Part: ACTUATOR — MALFUNCTIONED (ELEVATOR TRIM) · airframe 18,296 hrs · 27,144 cycles

ON DESCENT FROM FLIGHT LEVEL 270 A/P FAILED FOUND ELEVATOR TRIM FROZEN. REPLACED BOTH LEFT AND RIGHT ELEVATOR TRIM TAB LINEAR ACTUATORS IAW EMB 120 MM 27-32-02 AND ACCOMPLISHED CABLE TENSION IAW EMB 120 MM 27-00-01 PAGE 209 FIG 201. OPERATIONAL CHECK GOOD. P/N 5299-1, S/N OFF 735, 742.

Part: ACTUATOR — CONTAMINATED (ELEVATOR) · airframe 18,247 hrs · 27,083 cycles

UPON LEVEL OFF AT 270 ELEVATOR TRIM WHEEL SPRANG FORWARD ABOUT 1/2 TURN AND AUTOPILOT KICKED OFF. INSPECTED TRIM ACTUATORS FOR BOTH ELEVATOR AND AILERON TRIM AND FOUND MOISTURE ON ALL ACTUATOR SHAFTS. CLEANED RESIDUAL MOISTURE FROM ALL ACTUATORS AND LUBRICATED AS NECESSARY. ALL CHECKS GOOD, ALL WORK PERFORMED IAW EMB MM CH 27.

Part: SENSOR — FAULTY (STALL WARNING) · airframe 18,247 hrs · 27,083 cycles

STALL WARNING SYSTEM ALARM ON F/O SIDE ILLUMINATES WITH ASSOCIATED AURAL WARNING. REMOVED AND REPLACED SIDE SLIP SENSOR. OPERATIONAL CHECK GOOD.

Part: RCCB — FAULTY (COCKPIT) · airframe 18,239 hrs · 27,071 cycles

DURING INITIAL POWER UP, AN ELECTRICAL ODOR AND SMOKE DEVELOPED IN THE COCKPIT. REPLACED RCCB FOR GREEN HYDRAULIC AUX PUMP. OPERATIONAL CHECK GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 17,919 hrs · 26,584 cycles

BOTH FORWARD EXIT FLOOR LIGHTS (RED) INOPERATIVE. REPAIRED WIRES TO FLOOR TRACK LIGHTS (2 RED FWD). OPERATIONAL CHECK GOOD.

Part: FAN — SMOKE (RT PACK) · airframe 17,872 hrs · 26,513 cycles

ON GROUND RIGHT PACK FILLED CABIN WITH SMOKE. REPLACED RIGHT GROUND COOLING FAN. OPERATIONAL CHECKED GOOD.

Part: HEAT EXCHANGER — SMOKE (RT A/C PACK) · airframe 17,846 hrs · 26,479 cycles

RIGHT PACK PUTS SMOKE IN THE CABIN WHEN IT IS RUN ON THE APU BLEED. REMOVED AND REPLACED RIGHT HEAT EXCHANGER IAW EMB 120 MM 21-50-03. OPERATIONAL CHECK GOOD. P/N 194546-3, S/N OFF 10-576.

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT CARGO) · airframe 16,445 hrs · 24,339 cycles

SMOKE AURAL WARNING FOR CARGO SOUNDED. REPLACED AFT CARGO SMOKE DETECTOR. OPS CHECK GOOD.

Part: ROD END — OUT OF ADJUST (RT MLG DOOR) · airframe 15,852 hrs · 23,406 cycles

RIGHT GEAR DOOR REMAINS OPEN AFTER GEAR SELECTOR UP. VISUALLY VERIFIED THAT GEAR WAS UP WITH DOORS OPEN. RED INTRANSIT LIGHT IS REMAINING ON. ADJUSTED ACTUATOR ROD END (LENGTHENED 1 TURN) PER32-32-10 AND ADJUSTED UPLOCK TARGET PER MM 32-61-01. OPS CHECKS GOOD.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 15,825 hrs · 23,368 cycles

OBS SEAT FRAME, BELOW FLOOR, AFT SIDES CRACKED AS MARKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED FRAME BELOW FLOOR IAW SRM 120 51-10-02 PG 2 SEC 2B.

Part: LIGHT — WILL NOT TEST (CABIN) · airframe 15,231 hrs · 22,436 cycles

EMERGENCY LIGHTS DO NOT TEST PROPERLY. CENTER SECTION LIGHTS GO INOP AFTER COUPLE SECONDS. INSTALLED NEW K201 RELAY AND OPS CHECK GOOD.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 15,186 hrs · 22,360 cycles

FIRST THREE (FORWARD) EMERGENCY EXIT FLOOR LIGHTS, AS WELL AS FIRST (FORWARD) OVERHEAD POD LIGHT INTERMITTENT OPERATION. REPLACED FORWARD EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD.

Part: INVERTER — FAILED (AUTOPILOT) · airframe 15,131 hrs · 22,277 cycles

F/O'S AUTO PILOT FAILED ON THE APPROACH MODE. RED AP LIGHT ON MAP AND FCP. REMOVED AND REPLACED NR 1 INVERTER WITH SERVICEABLE UNIT IAW MM 24-22-00. OPS CHECK GOOD. P/N OFF: AL-251-1G, S/N OFF: 6074.

Part: EJECTOR VALVE — FAILED (DEICE SYSTEM) · airframe 14,242 hrs · 20,936 cycles

DURING CLIMB IN MODERATE ICING CONDITIONS, THE LEFT AND RIGHT MIDDLE WING DEICE BOOTS FAILED REPEATEDLY ON BOTH TIMERS. RETURNED TO FAT. REPLACED EJECTOR VALVE FOR LEFT AND RIGHT MIDDLE DEICE BOOTS WITH SERVICEABLE UNITS IAW MM 30-10-04. OPS CHECK GOOD.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 13,774 hrs · 20,170 cycles

APU BULKHEAD CRACKED BY BIG CANNON PLUG. DISCOVERED DURING A-CHECK INSPECTION. INSTALLED SERVICEABLE DOUBLER AT APU BULKHEAD IAW SRM. NO OTHER DEFECTS NOTED.

Part: BATTERY — DISCHARGED (E/E BAY) · airframe 13,379 hrs · 19,541 cycles

T/O BRAKES AURAL WARNING ON T/O ROLL WITH BRAKES RELEASED. ABORTED T/O. REMOVED AND REPLACED EMERGENCY BATTERY, OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (E/E BAY) · airframe 13,261 hrs · 19,343 cycles

ABORTED TAKEOFF FOR ATTITUDE DISPLAY MESSAGE. REPLACED NR 1 AHRS COMPUTER WITH SERVICEABLE UNIT AND REINITIALIZED AS REQUIRED. OPS CHECKS GOOD.

Part: CONNECTOR — CORRODED (COMM ANTENNA) · airframe 11,998 hrs · 17,390 cycles

CORROSION FOUND INSIDE CO-AX CONNECTOR OF COMM NR 2 ANTENNA. ANTENNA REQUIRES REPLACEMENT. REPLACED NR 2 COMM ANTENNA WITH NEW SERVICEABLE ANTENNA. ALL WORK CONFORMS TO MM REMOVAL AND REPLACEMENT INSTRUCTIONS CHAPTER 34-55-01. P/N OFF: 16-21B MOD 1 S/N OFF: 10443.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 11,998 hrs · 17,390 cycles

BRACKET AT FRAME 13 AFT OF DIRECT VISION WINDOW ON LEFT SIDE OF COCKPIT CRACKED. REPLACED BRACKET AT FRAME 13 AFT OF DV WINDOW ON LEFT SIDE OF COCKPIT IAW MM 53-00-00.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 12,011 hrs · 17,408 cycles

UPPER BRACKET FORWARD OF FRAME 9 IS CRACKED ON LEFT AND RIGHT SIDES OF COCKPIT. ELIMINATED SHEAR CLIPS AND CUT END OF LEFT AND RIGHT FRAME 9 CHANNEL PER SB 120-53-0073.

Part: CONTROL CABLE — WORN (AILERON) · airframe 11,998 hrs · 17,390 cycles

AILERON CABLES WORN. REPLACED AILERON CABLES WITH TIN CARBON STEEL CABLE PER EMB120 MM 27-00-01.

Part: DOOR — DAMAGED (FUEL DOOR) · airframe 10,196 hrs · 14,808 cycles

DURING TAKEOFF ROLL PRIOR TO V1 RECEIVED RED DOOR LIGHT ON MAP AND RED FLASHING WARNS LIGHT. ABORTED TAKEOFF. FOUND OUTBOARD REFUEL DOOR FWD FASTENER BAD AND POPPED OUT. REPLACED FASTENER AND RESECURED FORWARD DOOR. OPS CHECKS GOOD.

Part: UPLOCK — OUT OF ADJ (LT & RT MLG) · airframe 10,196 hrs · 14,808 cycles

UPON ATTEMPTING TO RAISE LANDING GEAR, RECEIVED A RED-A LIGHT AND A RED-B LIGHT. VISUALLY NOTICED THAT GEAR DOORS FOR LEFT AND RIGHT GEAR DO NOT CLOSE. DIVERTED TO FAT. ADJUSTED LEFT AND RIGHT UPLOCK HOOK PLUNGERS IAW 32-11-01. SWUNG GEAR SEVERAL TIMES IAW 32-00-00. OPS CHECK GOOD.

Part: UNKNOWN

FLAP DISAGREEMENT AFTER TAKEOFF. RETURNED TO PSP REPLACED FLAP SELECTOR HANDLE. OPS CHECKS GOOD.

Part: AHRS — MALFUNCTIONED (LT COCKPIT)

CAPTAIN'S AHRS FAILED AFTER TAKEOFF, WOULD NOT RESET (GYRO FLAG AND RED HEADING). RETURNED TO ACV. PERFORMED REORIENTATION OF AHRS (PILOTS). CHECKED OK.

Part: FCU — LOOSE (TE FLAPS)

NACELLE FLAP ASYMMETRY INDICATION, NO ADVERSE ROLL TENDENCY NOTED. THIS OCCURED ON APPROACH TO IMPERIAL, RETURNED TO PSP. FOUND FCU LOOSE IN MOUNT, CYCLED FLAPS NUMEROUS TIMES, OPS CHECKS GOOD.

Part: VENTURI TUBE — FAILED (LT ACM)

LEFT DUCT LEAK LIGHT ILLUMINATED IN FLIGHT. RETURNED TO FAT. INSTALLED SERVICEABLE VENTURI TUBE ON LEFT ACM.

Part: FUEL FILTER — DIRTY (LT ENGINE)

LEFT FUEL FILTER LIGHT ILLUMINATED IN FLIGHT. DIVERTED FROM FAT TO ACV. REPLACED LEFT ENGINE FUEL FILTER WITH SERVICEABLE UNIT. OPS CHECKS GOOD WITH NO LEAKS NOTED.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS)

AT V1 GOT A FLAP ASYMMETRY AND CONTROL FAULT. CONSULTED QRH AND HIT RESET. EVERYTHING NORMAL BUT RETURNED TO LAX FOR LONG RUNWAY. CYCLED FLAPS SEVERAL TIMES AND COULD NOT DUPLICATE DISCREPANCY. RERACKED FLAPS COMPUTER AND CYCLED FLAPS 10 TIMES ON GROUND. OPS CHECKS GOOD AT THIS TIME.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR)

CARGO DOOR LIGHT CAME ON RIGHT AFTER TAKEOFF AND DID NOT EXTINGUISH UNTIL LANDING. RETURNED TO FIELD. MEL 52-70-1. RE-ADJUSTED CARGO DOOR MICROSWITCH IAW MM 52-22-00. OPS CHECKS GOOD.