N301YV

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,646 hrs · 51,701 cycles

EMERGENCY LIGHT NEXT TO COURTESY LIGHT DOES NOT ILLUMINATE. FLT 7391 REPLACED THE EMERGENCY LAMP AT THE MAIN CABIN DOOR. OPERATIONS CHECKED GOOD PN 209.

Part: PIN — BROKEN (MLG DOOR LATCH) · airframe 36,943 hrs · 50,772 cycles

FLT 5427, ON RAISING LANDING GEAR LEVER, RECEIVED DISAGREEMENT LIGHTS A & B FOR THE RT MAIN GEAR. RAN THE QRH & CYCLED THE GEAR LEVER. AFTER RAISING LEVER AGAIN, RECEIVED BOTH GREEN & RED A & B LIGHTS FOR THE RT MAIN GEAR. REPLACED BROKEN RT INBD GEAR DOOR LATCH PIN IAW AMM.

Part: CONNECTOR — CORRODED (RT MLG) · airframe 36,763 hrs · 50,521 cycles

DURING TAXI OUT TO RUNWAY AIRCRAFT WOULD NOT STOP WITH NORMAL BRAKING. PLANE FINALLY STOPPED WHEN ANTI-SKID WAS TURNED OFF. (FLT 5459) CLEANED HEAVY CORROSION FROM RIGHT MAIN GEAR ANTI-SKID HARNESS CONNECTOR ABOVE RIGHT MAIN GEAR STRUT. COMPLIED WITH TAXI CHECK AND OPERATION OF BRAKES WITH ANTI-SKID SELECTED ON. BRAKE OPERATION NORMAL.

Part: BRAKE SYS — CONTAMINATED (MLG) · airframe 36,763 hrs · 50,521 cycles

UPON LANDING IN LAX, BRAKES FAILED. PARKING BRAKE STOPPED A/C. BRAKING WAS STICKY AND ABRUPT WITH ANTI-SKID OFF. (FLT 6452) PERFORMED BLEEDING OF ALL BRAKES AND HIGH SPEED TAXI WITH ANTI-SKID SELECTED ON. BRAKING ACTION NORMAL. BRAKES OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,620 hrs · 50,327 cycles

EMERGENCY LIGHT SWITCH ON, EMERGENCY LIGHTS WOULD NOT TEST PROPERLY. (FLT 5927) REPLACED FORWARD AND MIDDLE EMERGENCY LIGHT BATTERIES. P/N: D366-04-001 S/N ON: 972 S/N OFF: 265 P/N D366-04-001 S/N ON:1320 S/N OFF: 340

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 36,312 hrs · 49,917 cycles

SELECTED GEAR DOWN, DOORS OPENED BUT LANDING GEAR DID NOT EXTEND. CYCLED GEAR HANDLE AND LANDING GEAR CAME DOWN NORMALLY NO FURTHER PROBLEMS. (FLT 6233) PERFORMED 10 GEAR SWINGS AND COULD NOT DUPLICATE DISCREPANCY. CLEANED ALL GEAR SEQUENCE VALVES AND REPLACED LDG CONTROL HANDLE MODULE IAW AMM. P/N-120-38594-001 S/N ON-120153 P/N OFF-120-38594-501 S/N OFF-120343

Part: SHAFT — LACK OF LUBE (DOOR) · airframe 36,273 hrs · 49,866 cycles

FLIGHT ATTENDANT REPORTS THE FORWARD DOOR HANDLE IS STIFF AND HARD TO ACTUATE. (FLT 5335) LUBRICATED FWD DOOR HANDLE SHAFT, OPS CHECK GOOD.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 36,220 hrs · 49,787 cycles

MAIN CABIN DOOR VERY HARD TO OPEN AND CLOSE. (FLT 6295) LUBED UPPER FUSELAGE ROLLERS AND MAIN HANDLE PIVOT POINT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,143 hrs · 49,672 cycles

ONE RED EMERGENCY LIGHT AT ROW SIX DOES NOT ILLUMINATE. (FLT 7391) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,120 hrs · 49,643 cycles

EMERGENCY RED LIGHT AT ROW SIX IS OUT. (FLT 6295) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,061 hrs · 49,574 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. (FLT 5385) RELAMPED EMERGENCY LIGHT.

Part: CONTROL UNIT — FAILED (ANTI-SKID SYS) · airframe 36,008 hrs · 49,499 cycles

NO WHEEL BRAKES WITH ANTI-SKID ON AND PEDALS PUSHED. (FLT 6445) REPLACED THE ANTI-SKID CONTROL UNIT IAW AMM 32-42-03. P/N: 42-687-1 S/N ON: 101 S/N OFF: 422.

Part: SOLENOID VALVE — FAILED (LANDING GEAR) · airframe 35,879 hrs · 49,335 cycles

LANDING GEAR WOULD NOT EXTEND WHEN THE GEAR HANDLE WAS SELECTED DOWN. THE GEAR EXTENDED NORMALLY ON THE SECOND APPROACH. (FLT 7783) REPLACED LANDING GEAR SOLENOID VALVE IN REFERENCE TO AMM. P/N: 18190-003 S/N OFF: 767

Part: STRUCTURE — CRACKED (WINDSHIELD) · airframe 35,727 hrs · 49,148 cycles

LOUD RUSHING AIR NOISE COMING FROM BOTTOM OF PILLAR BETWEEN CAPTAIN'S WINDSHIELD AND DV WINDOW. (FLT 6408) FOUND CRACK ON LEFT WINDSHIELD PILLAR. REMOVED PILLAR AND INSTALLED SERVICEABLE PILLAR.

Part: STRINGER — CRACKED (LT WING) · airframe 35,627 hrs · 49,020 cycles

LEFT WING AT FUEL PANEL NR 2 AFT STRINGER 8 IS CRACKED. (SERVICE) REPAIRED STRINGER NR 8 AT LEFT AFT NR 2 FUEL PANEL AREA IN REFERENCE TO SRM.

Part: SCREW — MISSING (EMERGENCY LIGHT) · airframe 34,958 hrs · 48,175 cycles

ENTRY COURTESY LIGHT NOT WORKING IN THE EMERGENCY MODE. (FLT 7800) FOUND EMERGENCY DOME LIGHT TO BE INOPERATIVE DUE TO A MISSING SCREW FOR TERMINAL. INSTALLED NEW SCREW.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,821 hrs · 48,024 cycles

ENTRY WAY OVERHEAD EMERGENCY COURTESY LIGHTS ARE OUT. (FLT 6327) RELAMPED EMERGENCY LIGHTS.

Part: CONNECTOR — LOOSE (CABIN) · airframe 34,307 hrs · 47,394 cycles

RED EMERGENCY ON LOWER PASSENGER ENTRANCE LIGHT ON WALL CONTROL IS OUT. (FLT 7811) TIGHTENED LOOSE ELECTRICAL CONNECTOR ON LOWER PASSENGER ENTRANCE LIGHT.

Part: TRACK — BROKEN (CABIN) · airframe 34,229 hrs · 47,306 cycles

TRACK BELOW RIGHT FLIGHT ATTENDANT SEAT SIDE IS BROKEN. (SERVICE) REPLACED TRACK.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 33,494 hrs · 46,430 cycles

BRINGING TORQUE BACK TO 20 PERCENT, CABIN AND FLIGHT DECK FILLED WITH SMOKE. (FLT 5626) REPLACED LEFT ENGINE. NO FURTHER SMOKE NOTED IN CABIN. P/N OFF PW188B S/N OFF AP0011.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 33,347 hrs · 46,249 cycles

SMOKE IN THE COCKPIT DURING DESCENT. (FLT 5552) LEFT ENGINE REQUIRES REPLACEMENT. COULD NOT DUPLICATE SMOKE. LEFT ENGINE BLEED OPERATIONAL CHECKS ARE GOOD. NO SMOKE NOTED.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 33,302 hrs · 46,183 cycles

SMOKE IN COCKPIT WITH PACKS AUTO/NORM AND AUTO/LOW. (FLT 7777) REPLACED LEFT PACK ACM, LEFT PACK TEMP CONTROL VALVE AND TIC VALVE. P/N 2204540-5 (ACM) S/N OFF 76-840.

Part: EXTRACTOR — MALFUNCTIONED (AC BAY) · airframe 33,271 hrs · 46,147 cycles

REDUCED POWER TO 50 PERCENT TORQUE AND IMMEDIATELY GOT SMOKE IN COCKPIT FROM PACKS. (FLT 7795) REPLACED WATER EXTRACTOR UNIT AND CLEANED 2.5/3.0 BLEED VALVE. P/N 2340830-1-1, S/N ON 75-354, S/N OFF 73-295.

Part: LIGHT — BROKEN (CABIN) · airframe 33,065 hrs · 45,888 cycles

LEFT EMERGENCY LIGHT AT ROW 6 IS BROKEN. (FLT 6695) REPLACED LEFT EMERGENCY LIGHT ASSEMBLY AT ROW 6.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,146 hrs · 44,693 cycles

EMERGENCY LIGHT ON CABIN FORWARD BULKHEAD INOPERATIVE. (FLT 6515) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — BROKEN (CABIN) · airframe 31,996 hrs · 44,521 cycles

EMERGENCY FLOOR LIGHT NOT WORKING AT ROW 4. (FLT 6822) REPLACED FLOOR EMERGENCY LIGHT FIXTURE AT ROW 4.

Part: STRINGER — CRACKED (RT WING) · airframe 31,946 hrs · 44,469 cycles

RIGHT LOWER WING STRINGER, AFT OF NR 2 FUEL PANEL IS CRACKED. (C-CHECK) PERFORMED STRINGER SPLICE TO RT WING STRINGER 8 AT NR 2 FUEL CELL ACCESS PANEL PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,664 hrs · 44,102 cycles

FORWARD RIGHT EXTERNAL EMERGENCY LIGHT INOPERATIVE. (MAINTENANCE)RELAMPED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,392 hrs · 43,769 cycles

EMERGENCY LIGHTS MIDDLE OF CABIN INOP. (FLT 7799) REPLACED AFT EMERGENCY LIGHT BATTERY PACK.

Part: SWITCH — MALFUNCTIONED (AUTOFEATHER SYS) · airframe 30,732 hrs · 42,999 cycles

THE LEFT AUTO FEATHER TEST SWITCH STUCK IN THE TEST POSITION ON TAKEOFF RESULTING IN OVER TORQUE. (FLT 7759) REPLACED SWITCH, RIGHT PROP HUB AND BLADES.

Part: SEAL — CRACKED (RUDDER) · airframe 30,462 hrs · 42,679 cycles

RIGHT INBOARD RUDDER CABLE PRESSURE SEAL FLANGE CRACKED AT AFT SIDE OF WING BOX. (C CHECK) REPLACED SEAL FLANGE PER AMM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 30,448 hrs · 42,665 cycles

FUSELAGE SKIN AT FRAME 21 CORRODED. (C CHECK) REPAIRED PER ETD2009-120/10021.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,448 hrs · 42,665 cycles

LEFT FORWARD FLOOR SEAT TRACK CORRODED. (C CHECK) REPLACED SEAT TRACK PER AMM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 30,448 hrs · 42,665 cycles

STRINGERS 18 AND 19 BETWEEN RIBS 15 AND 16 CORRODED. (C CHECK) REPAIRED PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 30,066 hrs · 42,185 cycles

EXIT SIGN ON 6C IS BROKEN. (FLT 7769) REPLACED EMERGENCY EXIT SIGN AT 6C IAW MM 20-21-00.

Part: STRINGER — CRACKED (RT WING) · airframe 29,788 hrs · 41,836 cycles

RIGHT WING FUEL TANK STRINGER 10 IS CRACKED. (C CHECK) REPAIRED PER SRM.

Part: SENSOR — DIRTY (RT MLG) · airframe 29,776 hrs · 41,815 cycles

GEAR WOULD NOT RETRACT. (FLT 7760) CLEANED RIGHT MLG WOW SENSOR CONNECTOR.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 29,624 hrs · 41,625 cycles

FRONT ROW OF EMERGENCY LIGHTS INOP. (FLT 7769) REPLACED ELBP.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 28,443 hrs · 40,136 cycles

FLT 5442 - BURNING ODOR IN COCKPIT AND CABIN ACCOMPANIED WITH SMOKE. CLEANED AIR CONDITIONING HEAT EXCHANGERS, RAN BOTH PACKS OFF ENGINE BLEEDS AND APU BLEED FOR OVER AN HOUR, NO DISCREPANCIES NOTED. INSPECTED WIRING AND CONTACTORS NO DISCREPANCIES NOTED.

Part: WIRE — DAMAGED (DC RELAY BOX) · airframe 27,748 hrs · 39,207 cycles

DAMAGED WIRE W206-0051019 FOUND IN LT DC 1 RELAY BOX. (FOUND AT C-CHECK) REPLACED THE WIRE IAW EMB 120, WDM 21-51-00 AND THE RCCB IAW MM 24-52-05. OPS CHECKS GOOD.

Part: ROD END — CORRODED (RUDDER) · airframe 27,748 hrs · 39,207 cycles

RUDDER II ROD ENDS HAVE SURFACE CORROSION. (FOUND AT C-CHECK) REPLACED UPPER AND LOWER RUDDER II CONTROL ROD ENDS IAW AMM 27-21-02

Part: FRAME — CRACKED (PAX DOOR) · airframe 27,748 hrs · 39,207 cycles

PAX DOOR FWD AND AFT MID CORNERS ARE CRACKED. (FOUND AT C-CHECK) REPLACED FRAME AND INSTALLED DOUBLERS IAW SRM 120 52-10-02.

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · airframe 27,748 hrs · 39,207 cycles

BUTT STRAP IN FRONT OF LAV IS CORRODED. (FOUND AT C-CHECK) REPLACED BUTT STRAP IN FRONT OF LAV IAW SRM 51-10-02 AND SECURED IAW 51-40-07.

Part: ACM — MALFUNCTIONED (LEFT) · airframe 27,185 hrs · 38,455 cycles

LEFT PACK PRODUCES SMOKE. REPLACED LEFT AIR CYCLE MACHINE IAW MM 21-50-05.

Part: RETAINER — LOOSE (CARGO DOOR) · airframe 25,918 hrs · 36,796 cycles

THE O2 MASKS DROPPED AFTER TAKEOFF FLIGHT NR 5774. RESECURED CARGO DOOR SEAL AND RETAINER. PRESSURIZATION CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 25,931 hrs · 36,819 cycles

LEFT WINDSHIELD CRACKED, FLIGHT NR 5778. REPLACED WINDSHIELD IAW MM 56-00-00, OPS CHK GOOD.

Part: SIGN — BROKEN (EMERGENCY EXIT) · airframe 25,839 hrs · 36,681 cycles

EXIT ROW "EXIT" SIGN BROKEN AT ROW 6, FLIGHT NR 5471. REPLACED EXIT SIGN WITH A SERVICEABLE UNIT. OPS TEST GOOD, P/N: 10-1262-1.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 24,531 hrs · 34,962 cycles

FOUND EMERGENCY LIGHTS IN ROW 6 ARE INOP. REPLACED MIDDLE EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD IAW 33-50-02, PN: D366-04-001,SN ON: 1003/05-91, SN OFF: 720-03/90.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 24,078 hrs · 34,319 cycles

NUMEROUS EMERGENCY LIGHTS IN THE CABIN INOP. REPLACED FORWARD ELBP. OPERATIONAL CHECKS GOOD.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 23,637 hrs · 33,766 cycles

VERTICAL ANGLES LEFT AND RIGHT CRACKED BELOW COCKPIT ENTRY STEP, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT AND RIGHT VERTICAL ANGLES IAW SRM 51-10-02, PG 3, SEC 3A AND 51-40-02.

Part: SUPPORT ANGLE — CRACKED (COCKPIT) · airframe 23,637 hrs · 33,766 cycles

INSTRUMENT PANEL SUPPORT ANGLE CRACKED CAPTAIN'S SIDE AT BASE OF WINDSCREEN SIDE POST. REPLACED INSTRUMENT PANEL SUPPORT ANGLE EMB 120 SRM 51-40-02 AND 51-10-02, PG 3, SECT 3A, P/N: 120-42010-001.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 23,637 hrs · 33,766 cycles

RIGHT SIDE FORWARD OUTBOARD FLOOR/SIDEWALL ATTACH STRIP (LAVATORY AREA) HAS CORROSION, DISCOVERED DURING C-CHECK INSPECTION. REPLACED ATTACH STRIP IAW SRM 51-10-02, PG 3, SEC 3A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 23,637 hrs · 33,766 cycles

SEAT TRACK ON FLOOR BELOW GALLEY (FORWARD) CORRODED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED SEAT TRACK ON FLOOR BELOW GALLEY (FORWARD).

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 23,637 hrs · 33,766 cycles

FLOORBEAMS UNDER LAVATORY FLOORBOARD HAVE CORROSION, DISCOVERED DURING C-CHECK INSPECTION. REPLACED BUTT STRAP AT FORWARD FUSELAGE FLOOR IAW SRM 120 51-10-02, PG 3, SEC 3A AND RII 53-800-1000.

Part: FIREWALL — CRACKED (LT MLG WW) · airframe 23,637 hrs · 33,766 cycles

LEFT UPPER AFT WHEEL WELL, CRACK ON FIREWALL ACCESS 434 F2, DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CRACKED FIREWALL IAW EMB 120 SRM 51-10-02 AND 51-40-02.

Part: LEVER — MALFUNCTIONED (FLAP SELECTOR) · airframe 22,806 hrs · 32,539 cycles

FLAPS WILL NOT GO INTO 45 DEGREE POSITION. REPLACED FLAP CONTROL LEVER. OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,577 hrs · 32,169 cycles

ONE RED LIGHT ON FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM INOPERATIVE AT MAIN CABIN DOOR. REPLACED FWD FLOOR RED PROXIMITY EMERGENCY LIGHT. OPERATIONAL CHECK GOOD IAW AMM 33-51-00.

Part: SWITCH — BROKEN (PAX DOOR) · airframe 21,064 hrs · 29,929 cycles

PAX DOOR WILL NOT CLOSE. REPLACED PAX DOOR AFT HINGE FORWARD MICROSWITCH IAW 32-00-00. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,649 hrs · 29,327 cycles

ONE EMERGENCY FLOOR LIGHT IN GALLEY WILL NOT ILLUMINATE. RELAMPED EMERGENCY FLOOR LIGHT, OPERATIONAL CHECK GOOD.

Part: DOOR — BLOCKED (O2 MASK) · airframe 20,474 hrs · 29,068 cycles

PAX O2 MASKS DROPPED DURING DEPRESSURIZATION. MASKS IN ROW 3 DID NOT DROP. CREW MASKS WERE DEPLOYED. CLEANED THE USED MASKS AND RE-PACKED AND STOWED. ROW 3 PAX O3 MASK DOOR INTERFERES WITH ADJACENT ACCESS PANEL. TRIMMED EDGE OF ACCESS PANEL AS NEEDED TO PROVIDE CLEARANCE FOR O2 MASK DOOR. OPERATIONAL CHECK GOOD.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 20,474 hrs · 29,068 cycles

RAPID DEPRESSURIZATION IN FLIGHT CABIN ALT LIGHT ILLUMINATED AND PAX O2 MASKS DEPLOYED. REMOVED AND REPLACED ELECTRO PNEUMATIC OUTFLOW VALVE IAW 21-30-03. OPERATIONAL CHECK GOOD.

Part: PROXIMITY SENSOR — MALFUNCTIONED (RT ELEVATOR) · airframe 18,496 hrs · 26,081 cycles

ON TAKEOFF, RECEIVED TAKEOFF TRIM AURAL WARNING WITH TRIM SET AT 25 PERCENT. ABORTED TAKEOFF. REPLACED RIGHT ELEVATOR TRIM PROX SENSOR IAW 120 MM 27-32-05. OPS CHECK GOOD.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 18,373 hrs · 25,899 cycles

NACELLE FLAP DISAGREEMENT. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR WITH A SERVICEABLE UNIT IAW 27-50-08. OPS CHECKS GOOD.

Part: CONTROL HANDLE — FAULTY (COCKPIT) · airframe 17,726 hrs · 24,898 cycles

ON TAXI OUT, FLAPS CONTROL FAULT 3 TIMES. COULD NOT GET FLAPS TO GO TO 15 DEGREES. REMOVED AND REPLACED FLAP HANDLE WITH A SERVICEABLE UNIT. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,588 hrs · 24,668 cycles

FLOOR LEVEL EMERGENCY LIGHT BURNED OUT. INSTALLED BULB. OPS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 17,212 hrs · 24,064 cycles

CONTROL FAULT RECEIVED ON OUTBOARD FLAPS. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR WITH A SERVICEABLE UNIT IAW 27-50-09.

Part: ENGINE — OVERSPEED (RIGHT) · airframe 16,773 hrs · 23,391 cycles

AFTER LANDING ROLLOUT AND DURING DECELERATION, HEARD A TRIPLE CHIME WARNING AND THE AURAL WARNING ENGINE CONTROL WHICH STARTED AT ABOUT 90 KTS. AT ABOUT 70 KTS, THE RIGHT ENGINE SURGED SEVERAL TIMES RESULTING IN MODERATE INCREASING YAWING TENDENCIES. POSITIVE AIRCRAFT CONTROL WAS UNCERTAIN AND RIGHT ENGINE WAS SHUT DOWN. FDR DOWNLOAD INDICATES THE RIGHT ENGINE NP REACHED 130 PERCENT NP. REMOVED AND REPLACED RIGHT ENGINE ASSEMBLY IAW EMB120 MM 71-00-00.

Part: ACTUATOR — FROZEN (ELEVATOR TRIM) · airframe 16,474 hrs · 22,938 cycles

TRIM ACTUATOR FROZE UP DURING CRUISE AT 22,000 FT. RETURNED TO SFO. REPLACED BOTH ELEVATOR TRIM TAB ACTUATORS IAW EMB 120 MM. OPS CHECKED GOOD.

Part: PRESSURE SWITCH — MALFUNCTIONED (HYD SYSTEM) · airframe 16,342 hrs · 22,727 cycles

LT HYDRAULIC RESERVOIR LOW PRESSURE LIGHT ILLUMINATED DURING TAKEOFF. ABORTED THE TAKEOFF. REMOVED & REPLACED LT HYDRAULIC RESERVOIR LOW PRESSURE SWITCH. OPS CHECK GOOD. NO LEAKS NOTED. PN OFF 120-48659-001 SN OFF 0134.

Part: WIRE — BROKEN (NR 1 TRIM SWITCH) · airframe 16,265 hrs · 22,605 cycles

WITH AUTO PILOT SELECTED TO CAPTAIN'S SIDE, RECEIVED RED ''TRIM FAIL'' ON MAP, WITH TRIPLE CHIME AND AURAL WARNING AFTER ROTATION AND DURING LANDING ROLLOUT. REPAIRED WIRING TO NR 1 TRIM SWITCH AS REQUIRED. SYSTEM OPS CHECKS GOOD IAW 22-10-00.

Part: INDICATOR — MALFUNCTIONED (RT TORQUE) · airframe 16,265 hrs · 22,605 cycles

RIGHT TORQUE GAUGE, DIGITAL PORTION ONLY, FAILED ON TAKEOFF ROLL. ABORTED TAKEOFF. REPLACED RIGHT TORQUE GAUGE. OPS CHECK GOOD ON ENGINE RUN.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 16,016 hrs · 22,243 cycles

SUPPORT AFT OF CAPTAIN'S DV WINDOW CRACKED. FOUND DURING C CHECK INSPECTION. REPLACED SUPPORT AFT OF CAPTAIN'S DV WINDOW WITH SERVICEABLE UNIT PER EMB SRM 51-40-02, 51-22-00, AND 51-40-01.

Part: SUPPORT — CRACKED (RT COWLING) · airframe 16,016 hrs · 22,243 cycles

RIGHT ENGINE FRAME 1 COWLING SUPPORT CRACKED, TOP INBOARD SIDE. FOUND DURING C CHECK INSPECTION. REMOVED AND REPLACED RIGHT ENGINE FRAME 1 COWLING SUPPORT BRACKET ON TOP INBOARD SIDE.

Part: CAP — OUT OF POSITION (LT ENGINE) · airframe 15,898 hrs · 22,057 cycles

ON TAXI OUT TO RUNWAY, OIL PRESSURE WARNING LIGHT ILLUMINATED FOLLOWED BY OIL AURAL WARNING ON LEFT ENGINE. SHUT DOWN LEFT ENGINE IMMEDIATELY. OIL PRESSURE FELL BELOW 40 PSI D FOR LESS THAN 5 SECONDS. REASON FOR LOW OIL PRESSURE ON LEFT ENGINE WAS OIL CAP INADVERTENTLY LEFT OFF AFTER OIL SERVICE.

Part: GOVERNOR — LEAKING (NR 2 ENGINE) · airframe 15,679 hrs · 21,701 cycles

DURING CRUISE, GOT A TRIPLE CHIME OIL WARNING WITH CORRESPONDING OIL PRESSURE BETWEEN 40-55 PSI ON ENGINE NR 2. COMPLIED WITH QRH AND FEATHERED ENGINE NR 2. OIL PRESSURE THEN FELL TO APPROXIMATELY 20-30 PSI AND ENGINE NR 2 WAS SHUTDOWN PER QRH. ALL OTHER ENGINE INDICATIONS WERE NORMAL. FOUND OIL LEAK COMING FROM OVERSPEED GOVERNOR SWITCH ON NR 2 ENGINE. REPLACED OVERSPEED GOVERNOR PER MEL 61-22-01. ALSO REPLACED BAD BREATHER SEAL PER MM 72-20-00. ALL RUNS AND LEAK CHECK GOOD. OIL LEVEL GOOD AFTER ENGINE RUNS.

Part: DOOR — OUT OF ADJUST (LT MLG) · airframe 15,285 hrs · 21,103 cycles

ON GEAR RETRACTION, LEFT INDICATION REMAINED RED IN EXCESS OF 12 SECONDS WITH SLIGHT VIBRATION. RETURNED TO PDX. ADJUSTED GEAR DOOR IAW MM 32-32-09 & 32-32-10 AND ADJUSTED TARGET IAW MM 32-61-01. SWUNG GEAR SEVERAL TIMES. OPS CHECK GOOD.

Part: RELAY — FAILED (RT ENGINE) · airframe 15,208 hrs · 20,999 cycles

RIGHT EEC FAILED. ABORTED TAKEOFF. REPLACED RIGHT ENGINE REVERSION RELAY. ALL OPS CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 14,228 hrs · 19,540 cycles

BACKUP BATTERY/EMERGENCY LIGHTS FAILED WHEN TESTED. REPLACED FORWARD, MIDDLE EMERGENCY LIGHTING BATTERY PACKS. OPS CHECK GOOD.

Part: FUSE — BLOWN (CABIN) · airframe 14,228 hrs · 19,540 cycles

EMERGENCY EXIT SIGNS AT 2A AND ON EITHER SIDE OF JUMPSEAT FAIL TO ILLUMINATE. REPLACED CENTER EMERGENCY LIGHTING BATTERY PACK FUSE. OPS CHECK GOOD.

Part: FCU — OUT OF ADJ (RT ENGINE) · airframe 14,200 hrs · 19,498 cycles

RIGHT TORQUE FLUCTUATED 5 - 8 PERCENT AFTER TAKEOFF. RETURNED TO FAT. PERFORMED ENGINE RUNS IAW EMB 120 MM 71-00-00. OPS CHECKS GOOD. NO DEFECTS NOTED AT THIS TIME. UPDATE 10/12/2001: PREVIOUS OPS CHECK DONE WITH EECS OFF. RAN AND ADJUSTED TRIM ON RIGHT ENGINE. RAN RIGHT ENGINE AT DIFFERENT PARAMETERS WITH EEC ON. COULD NOT DUPLICATE. OPS CHECK GOOD AT THIS TIME.

Part: SENSOR — READS HIGH (RT ENGINE) · airframe 14,127 hrs · 19,395 cycles

RIGHT EEC FAILED ON TAKEOFF. MANUAL AND RED EEC LIGHT ILLUMINATED. PERFORMED ENGINE RUNS FOR 20 MINUTES IN TAKEOFF AND CRUISE CONFIGURATIONS, NO DEFECTS NOTED. CLEANED AND OHMED ALL EEC CANNON PLUGS. FOUND NP SENSOR HIGH. REMOVED AND REPLACED RT ENGINE NP SENSOR AS NEEDED. OPS CHECK GOOD ON RIGHT ENGINE NP SENSOR. EEC OPS CHECK GOOD IAW 71-00-00 120MM.

Part: DOOR — UNLATCHED (SERVICE DOOR) · airframe 13,186 hrs · 18,026 cycles

SERVICE DOOR AND MAP DOORS LIGHT ILLUMINATED SHORTLY AFTER DEPARTURE. RETURNED TO THE FIELD. INBOARD FUEL SERVICE DOOR FORWARD FASTENER CAME UNLATCHED. LATCHED DOORS. OPS CHECK GOOD FOR SECURITY.

Part: HANDLE — STUCK (PAX DOOR) · airframe 12,523 hrs · 17,088 cycles

FORWARD DOOR WOULD NOT OPEN FULLY WHEN OPENED FOR PASSENGER DE-PLANNING, HANDLE IS STUCK IN HALF-TRAVEL POSITION. REMOVED BROKEN LOCKING CAM ROD PUSH END FORWARD AND REPLACED WITH ROD END IAW EMB 120 MM 52-11-00. OPS CHECK GOOD. OPERATES NORMALLY.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 12,320 hrs · 16,766 cycles

LATERAL FLOOR SUPPORT JUST AFT OF TOILET HAS CORROSION BEYOND LIMITS.(DISCREPANCY DISCOVERED DURING FIRE SUPPRESSION MODIFICATION) DRILLED AND INSTALLED NEW FLOOR SUPPORT PER 51-70-00, COMPLETED RII CARD 53-301. PN 120-04149-002

Part: BOOT — INOPERATIVE (RT WING) · airframe 11,863 hrs · 16,144 cycles

RIGHT OUTBOARD STABILIZER BOOT INDICATES INOP. RETURNED TO SEA. INSTALLED SERVICEABLE OUTBOARD STABILIZER EJECTOR VALVE AND RIGHT DEICE PRESS REGULATOR. FUNCTIONAL TEST GOOD. 30-10-00 S/N: N0190 S/N OFF: N218 EJECTOR VALVE, S/N: RF2220, S/N OFF: RF1576 PRESS REGULATOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,141 hrs · 15,139 cycles

EMERGENCY EXIT ROW LIGHTS AT ROW 6 DO NOT ILLUMINATE WHEN TESTED. REPLACED EMERGENCY EXIT ELBP, OPS CHECKS GOOD. (P/N D36604001) ON, (S/N 265) ON, (S/N 226) OFF.

Part: FLAPS — MALFUNCTIONED (WINGS)

AFTER TAKEOFF, INBOARD FLAP DISAGREEMENT. CYCLED FLAPS BUT THEY WOULD NOT RETRACT. RETURNED FOR LANDING USING FLAPS 25. FLAPS RETRACTED NORMALLY ON GROUND. REPLACED FLAP ANNUNCIATOR PANEL, OPS CHECKS GOOD.

Part: TQ PROB — FAILED (LT ENGINE)

LEFT TORQUE GAUGE INOP TO INTERMITTENT AT 13,000 MSL ON CLIMB-OUT. RETURNED TO SFO. REMOVED AND REPLACED LEFT TORQUE PROBE SENSOR. RAN LEFT ENGINE THROUGH PARAMETERS. NO INTERMITTENT FLUCTUATION OR FAILURE. OPS CHECKS GOOD.

Part: CONTROL BOX — FAILED (LANDING GEAR)

LANDING GEAR WOULD NOT RETRACT ON DEPARTURE. RETURNED TO SAN. REMOVED AND REPLACED LANDING GEAR CONTROL BOX. OPERATED LANDING GEAR SEVERAL TIMES WITH NO DISCREPANCIES. OPS CHECKS GOOD.

Part: EEC — FAILED (RIGHT)

ON CLIMB AT 1000 FT, RIGHT ENGINE TORQUE ROSE UNCOMMANDED TO APPROXIMATELY 124 PERCENT. PROP NP WAS APPROXIMATELY 100 PERCENT, T6 BELOW 800 FT. ALL OTHER PARAMETERS NORMAL AND EEC WARNING ENSUED. CHECK LIST CALLED FOR EEC SWITCH TO MANUAL AT WHICH TIME CONTROL OVER ENGINE WAS RETAINED TO POWER LEVER, TORQUE REMAINED 124 PERCENT FOR 10-15 SECONDS. RETURNED TO SFO. RIGHT ENGINE TORQUE IS WITHIN LIMITS AS PER PRATT AND WHITNEY ENGINE MM 05-10-00, PAGE 8 FIGURE 2. PERFORMED ENGINE RUN. FOUND RIGHT EEC FAILED, WON'T RESET. DEFERRED RIGHT EEC AS PER MEL 73-21-1.

Part: ROLLERS — WORN (LT TE FLAP)

AFTER TAKEOFF, FLAPS WERE RETRACTED AND GOT FLAP DISAGREEMENT. APPLIED QRH PROCEDURE TWICE WITH NO SUCCESS. RETURNED TO FAT. FLAPS RETRACTED NORMALLY ON THE GROUND. REMOVED AND REPLACED LEFT INBOARD FLAP ROLLERS IAW MM 27-50-12. NO OTHER DISCREPANCIES NOTED. OPS CHECKS GOOD.

Part: COMPUTER — MALFUNCTIONED (E/E COMPT)

RDD - STALL WARNING ON LEFT SIDE ILLUMINATED ON MAP ON TAKEOFF ROLL. TAKEOFF ABORTED. MAINTENANCE DEFERRED LEFT STALL WARNING PER MEL 27-36-2. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY RERACKING STALL WARNING COMPUTER. OPERATIONAL CHECK SATISFACTORY. (M)

Part: FIRE EXTINGUISH — INOPERATIVE (LT ENGINE)

PSP - LEFT ENGINE FIRE INOP LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED LEFT ENGINE FIRE EXTINGUISHER. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SWITCH — OUT OF ADJUST (CARGO DOOR)

FAT - CARGO DOOR LIGHT ILLUMINATED ON TAKEOFF. TAKEOFF ABORTED DEFERRED CARGO DOOR WARNIGN PER MEL 52-70-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY ADJUSTING CARGO DOOR MICROSWITCHES. OPERATIONAL CHECK SATISFACTORY. (M)

Part: GEAR SELECTOR — MALFUNCTIONED (COCKPIT)

SFO - NOSE A SYSTEM INTRANSIT LIGHT REPORTED INTERMITTENT WITH GEAR RETRACTED. B SYSTEM INDICATION NORMAL. MAINTENANCE REPLACED LANDING GEAR SELECTOR HANDLE. LANDING GEAR POSITION INDICATION NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FUEL DOOR — NOT SECURED (WING)

SBA - DOOR WARNING ON TAKEOFF REPORTED. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE RESECURED FUEL SERVICE DOOR. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ENGINE — BIRD STRIKE (LEFT)

SFO - BIRD STRIKE AT LEFT ENGINE NACELLE REPORTED ON TAKEOFF FROM SMF. AIRCRAFT CONTINUED TO STATION WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION OF AIRCRAFT, ENGINE AND PROPELLER PER APPLICABLE MANUFACTURES MM. DAMAGE REPORTED AT LEFT ENGINE INLET COWL DE-ICE BOOT AND ON ONE BLADE OF LEFT PROPELLER. EVIDENCE OF BIRD MATERIAL IN INERTIAL SEPARATOR. DETERMINED NO ENGINE INGESTION OCCURRED. REPLACED INLET COWL. PROP BLADE DETERMINED OK FOR CONTINUED SERVICE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FUEL DOOR — NOT SECURED (RT WING)

SFO - TAKEOFF ABORTED WITHOUT INCIDENT. MOMENTARY DOR LIGHT ILLUMINATION ON MAP WITH NO OTHER ASSOCIATED AURAL OR VISUAL INDICATIONS DURING TAKEOFF ROLL. MAINTENANCE INSPECTED SERVICE DOORS. FOUND FRONT CAMLOCK FASTENERS ON RT WING INBOARD FUEL ACCESS DOOR NOT FULLY ENGAGED. RESECURED CAMLOCK. DOOR WARNING SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURN TO SERVICE. (M)

Part: SELECTOR — FAILED (COCKPIT)

LAX - FLAP CONTROL FAULT REPORTED. FLAP STUCK AT ZERO. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED FLAP SELECTOR. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X)

Part: CONNECTOR — DIRTY (COCKPIT)

FAT - TAKEOFF WARNING CAME ON AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE CLEANED CONNECTION ON LANDING GEAR RELAY BOX, P/N 120011R. PERFORMED MULTIPLE LANDING GEAR SWINGS. SYSTEMS OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X)