N295SW

Part: RELAY — FAILED (ELECTRICAL SYS) · airframe 37,459 hrs · 54,217 cycles

ELECTRICAL SMELL & SMOKE ORIGINATING FROM RELAY PANEL. FLT#5432 REPLACED K0152, R0005, & BUSS BAR W1263 IAW AMM.

Part: SKIN — CRACKED (LT WING) · airframe 37,114 hrs · 53,712 cycles

LT WING INBD OF FUEL ACCESS PANEL CUT OUT NR 6 HAS ONE UPPER SKIN CLEAT CRACKED. C-CHECK REPLACED UPPER SKIN CLEAT AT FWD SECTION OF LT WING RIB 23 IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 37,114 hrs · 53,712 cycles

LT WING OTBD OF FUEL ACCESS PANEL CUT OUT NR 3 HAS ONE UPPER SKIN CLEAT CRACKED. C-CHECK R&R ONE UPPER SKIN CLEAT ON LT WING OTBD ABOVE NR 3 FUEL ACCESS PANEL IAW SRM.

Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 37,114 hrs · 53,712 cycles

PAX DOOR ENTRANCE LOWER FRAME CRACKED AT THRESHOLD. C-CHECK REPLACED PAX DOOR ENTRANCE LOWER THRESHOLD IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 37,114 hrs · 53,712 cycles

LT WING INBD OF FUEL ACCESS PANEL CUT OUT NR 5 HAS TWO UPPER SKIN CLEATS CRACKED. C-CHECK REPLACED TWO UPPER FORWARD SKIN CLEATS AT LT WING, RIB 20 IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 37,114 hrs · 53,712 cycles

LT WING OTBD OF FUEL ACCESS PANEL CUT OUT NR 4 HAS TWO UPPER SKIN CLEATS CRACKED. C-CHECKED R&R TWO UPPER SKIN CLEAT ON LT WING OTBD ABOVE NR 4 FUEL ACCESS PANEL IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 37,114 hrs · 53,712 cycles

RT WING NR 1 FUEL ACCESS PANEL AREA HAS CRACKED SKIN CLEAT. C-CHECK REPLACED SKIN CLEAT AT RT WING NR 1 FUEL ACCESS PANEL AREA IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 37,114 hrs · 53,712 cycles

RT WING NR 2 FUEL ACCESS PANEL AREA HAS CRACKED SKIN CLEAT. C-CHECK REPLACED SKIN CLEAT AT RT WING NR 2 FUEL ACCESS PANEL AREA IAW SRM.

Part: SIGNAL COND UNIT — FAILED (LT ENGINE) · airframe 36,741 hrs · 53,165 cycles

TAKEOFF AUTO FEATHER AURAL WARNING. AUTO FEATHER SWITCH WAS IN THE ON POSITION. (FLT 5473) REPLACED LEFT ENGINE TORQUE SIGNAL CONDITIONER. P/N: 3005-0000-57 S/N ON: MM4765 S/N OFF: MM4917

Part: CONTROL UNIT — FAILED (ANTI-SKID SYS) · airframe 36,680 hrs · 53,093 cycles

NO BRAKE AUTHORITY SLOWING BELOW 5 KTS WITH ANTI-SKID ON. BRAKES WORK WITH ANTI-SKID OFF. (FLT 5401) REPLACED THE ANTI-SKID ELECTRONIC CONTROL UNIT IAW AMM. OPS CHECK GOOD ON THE GROUND. P/N: 42-687-1 S/N ON: 508 S/N OFF: 451

Part: RELAY — DEFECTIVE (COCKPIT) · airframe 36,551 hrs · 52,904 cycles

WEIRD SMELL FROM LEFT SIDE OF FLIGHT DECK. (FLT 6476) REPLACED APU HEATER PROTECTION RELAY.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 36,499 hrs · 52,817 cycles

FLT 5308, LAVATORY SMOKE DETECTOR ACTIVATED. INSPECTED LT AND RT HIGH PRESSURE VALVES. PERFORMED LT AND RT ENGINE RUNS WITH PACKS ON, NO SMOKE DETECTED, NO LAVATORY ALARM, FOUND RESIDUAL OIL IN RT ACM. COULD NOT DUPLICATE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,051 hrs · 52,182 cycles

EMERGENCY LIGHT BY 5A IS BURNED OUT. (FLT 5427) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,051 hrs · 52,182 cycles

ROW 9 EMERGENCY LIGHT BURNED OUT. (FLT 6293) RELAMPED EMERGENCY LIGHT.

Part: CONTROL MODULE — FAILED (LANDING GEAR) · airframe 36,051 hrs · 52,182 cycles

RIGHT MAIN LANDING GEAR WOULD NOT RETRACT. ATTEMPTED 3 TIMES TO CYCLE GEAR, BUT WOULD NOT RETRACT. LEFT GEAR DOWN, AND RETURNED TO FIELD. (FLT 5636) REPLACED LANDING GEAR CONTROL MODULE. P/N: 120-38594-001 S/N ON: 120127 S/N OFF: 120335

Part: CONTROL MODULE — FAILED (COCKPIT) · airframe 35,880 hrs · 51,916 cycles

RIGHT GEAR FAILED TO COME UP ON FIRST TRY. (FLT 5339) REPLACED LANDING GEAR CONTROL HANDLE/MODULE. P/N: 120-38594-501 S/N OFF: 293329-314.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,897 hrs · 51,940 cycles

NR 1 RED FLOOR PATH NOT WORKING. (FLT 5440) REPLACED THE NR 1 RED FLOOR EMERGENCY LIGHT ASSY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,802 hrs · 51,795 cycles

EMERGENCY OVERHEAD LIGHT SEAT 6C BURNED OUT. (FLT 5365) RELAMPED EMERGENCY LIGHT.

Part: WIRE — BROKEN (CABIN) · airframe 35,582 hrs · 51,510 cycles

ONE RED FLOOR LEVEL EMERGENCY LIGHT AT 2A FAILS TO ILLUMINATE. (FLT 6320) FOUND BROKEN WIRE ON FORWARD RED EMERGENCY FLOOR LIGHT AND REPAIRED WIRE IN REFERENCE TO EMB 120 WDM.

Part: PCU — MALFUNCTIONED (RT ENGINE) · airframe 35,318 hrs · 51,129 cycles

LEVELING OFF AT 7000 FT, RIGHT NP SURGED TO 103 PERCENT THREE TIMES. (FLT 5469) REPLACED RIGHT ENGINE PCU IN REFERENCE TO AMM. P/N:782490-46 S/N OFF: 880836

Part: SELECTOR — FAILED (COCKPIT) · airframe 34,346 hrs · 49,738 cycles

GEAR WOULD NOT EXTEND. GEAR CAME DOWN USING ELECTRIC OVERRIDE PROCEDURE. (FLT 5304) REPLACED GEAR SELECTOR HANDLE. P/N 120-38594-001 S/N OFF 120148

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,842 hrs · 48,994 cycles

EMERGENCY LIGHTS WILL NOT REMAIN ILLUMINATED. (FLT 5398) REPLACED AFT AND MIDDLE EMERGENCY LIGHT BATTERIES. P/N:D366-04-001 S/N OFF:1183401-96 P/N:D366-04-001 S/N OFF:1282110-96

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,433 hrs · 48,404 cycles

FORWARD FLOOR EMERGENCY LIGHT IS OUT. (FLT 6320) RELAMPED EMERGENCY LIGHT.

Part: SIGN — MISSING (CABIN) · airframe 30,984 hrs · 45,026 cycles

FORWARD LOWER EMERGENCY EXIT SIGN, NEXT TO F/A JUMPSEAT, WAS FOUND TO BE MISSING. (FLT 6678) REPLACED EMERGENCY EXIT SIGN ASSEMBLY.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 30,781 hrs · 44,741 cycles

AFT PORTION OF EMERGENCY LIGHTS IN CABIN EXTREMELY DIM. (FLT 6232) REPLACED LIGHT ASSEMBLY.

Part: SHAFT — CRACKED (LT ENGINE) · airframe 29,915 hrs · 43,485 cycles

(FLT 5941) LEFT ENGINE FLAMEOUT DURING DESCENT. TOWER SHAFT FAILED DUE TO FATIGUE CRACKING. REPLACED ENGINE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 30,003 hrs · 43,614 cycles

MAIN CABIN DOOR LOWER THRESHOLD ANGLE CORRODED. (C CHECK) REPLACED LOWER THRESHOLD ANGLE.

Part: SPAR CAP — CRACKED (RT NACELLE) · airframe 30,003 hrs · 43,614 cycles

RIGHT NACELLE FORWARD SPAR CAP UPPER CORNER CRACKED. (C CHECK) INSTALLED DOUBLER REPAIR PER ETD.

Part: FRAME — CRACKED (LT NACELLE) · airframe 30,003 hrs · 43,614 cycles

LEFT NACELLE FRAME NR 1 CRACKED. (C CHECK) REPLACED FRAME PER EMB SB 120-54-0036.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 30,003 hrs · 43,614 cycles

CORROSION ON BUTT STRAP UNDER LAVATORY. (C CHECK) REPLACED BUTT STRAP PER SRM.

Part: PIVOT — LACK OF LUBE (CABIN DOOR) · airframe 29,813 hrs · 43,343 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6237) LUBED OUTSIDE HANDLE AT SHAFT PIVOT POINT.

Part: DOOR — LACK OF LUBE (CABIN DOOR) · airframe 29,813 hrs · 43,343 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. (FLT 6840) LUBED MAIN CABIN DOOR.

Part: SIGN — BROKEN (CABIN) · airframe 29,587 hrs · 43,034 cycles

EMERGENCY EXIT SIGN AT ROW 6 BROKEN. (FLT 6444)REPLACED SIGN ASSEMBLY.

Part: PULLEY — WORN (AILERON) · airframe 29,290 hrs · 42,603 cycles

CONTROL FOR AILERON INPUT IS VERY STIFF AND DIFFICULT TO CONTROL. (FLT 6262) REPLACED LEFT AND RIGHT OUTBOARD PULLEYS PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,712 hrs · 41,773 cycles

RED EMERGENCY LIGHT AT ROW 1 INOP. (FLT 6236)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,651 hrs · 41,698 cycles

FORWARD MOST RED LIGHT ON FLOOR EXIT STRIP INOP. (FLT 6535) RELAMPED LIGHT ON FLOOR EXIT STRIP.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,579 hrs · 41,593 cycles

FLT 6237 - FORWARD RED EMERGENCY LIGHT INOP. RELAMPED.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 28,359 hrs · 41,309 cycles

FLT 6290 - FRONT EXIT EMERGENCY FLOOR SIGN COVER MISSING. REPLACED SIGN.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 28,252 hrs · 41,173 cycles

FLT 6182 - EMERGENCY FLOOR LIGHTS AT 7A INOP. RESEATED CONNECTOR.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 28,232 hrs · 41,148 cycles

FLT 6422 - EXIT PATH FLOOR LIGHTS ROWS 6 - 8 INOP. RESEATED CONNECTOR.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 28,207 hrs · 41,111 cycles

FLT 5982 - FLOOR EMERGENCY LIGHTS AT 2A AND 4A INOP. REPAIRED WIRE ON FLOOR LIGHT STRIP.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 28,088 hrs · 40,954 cycles

FLT 5434 - RED FLOOR EMERGENCY LIGHT INOP. RELAMPED.

Part: ACTUATOR — JAMMED (RUDDER TRIM) · airframe 27,477 hrs · 40,143 cycles

FLT 5522 - RUDDER TRIM JAMMED. REPLACED RUDDER TRIM ACTUATOR PER MM, P/N: 5-5298, S/N ON: 40, SN OFF: 399.

Part: BATTERY — DISCHARGED (SMOKE DETECTOR) · airframe 26,094 hrs · 38,281 cycles

FLT 5718 - SMOKE DETECTOR IS INOP. REPLACED BATTERY IN SMOKE DETECTOR. OPS CHECK GOOD.

Part: TERMINAL — DEFECTIVE (EMERGENCY LIGHT) · airframe 25,975 hrs · 38,111 cycles

LEFT OVERWING EMERGENCY LIGHT IS INOP. REPLACED TERMINALS ON EMERGENCY LIGHT ASSEMBLY.

Part: DOOR — BINDING (MAIN PAX) · airframe 25,805 hrs · 37,875 cycles

FLT 5744 - CABIN DOOR IS VERY DIFFICULT TO CLOSE. LUBRICATED DOOR AS REQUIRED. OPS CHECK GOOD.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 25,403 hrs · 37,369 cycles

FLT 5727 - FORWARD LEFT BULKHEAD "EXIT" SIGN IS BROKEN. REPLACED "EXIT" SIGN ASSEMBLY PER MM 33-51-02.

Part: LIGHT — BROKEN (CABIN) · airframe 24,367 hrs · 35,936 cycles

FLT 5547 - FRONT LEFT FLOOR EMERGENCY LIGHT IS BROKEN. INSTALLED NEW LENS ASSEMBLY.

Part: BELLCRANK — WORN (AILERON CONTROL) · airframe 24,249 hrs · 35,769 cycles

FLT 5788 - THE YOKE FEELS AS THOUGH IT FALLS INTO A DETENT IN THE CENTER POSITION. REPLACED LEFT AILERON BELLCRANK AND AILERON SPIGOT BEARING IAW EMB 120 MM 27-11-05.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 23,273 hrs · 34,373 cycles

FOUND EXIT ROW 6 RIGHT SIDE LIGHT INOP. RELAMPED EXIT ROW 6 EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 23,182 hrs · 34,236 cycles

EMERGENCY LIGHT OVER MCD IS INOP. REPLACED BULB OVER MCD. OPERATIONAL CHECKS GOOD.

Part: RIB — CRACKED (LT WING) · airframe 22,422 hrs · 33,104 cycles

LEFT OUTBOARD WING LOWER CENTER SKIN CLIP CRACKED AT RIB NR 16. REPLACED LEFT OUTBOARD WING LOWER CENTER SKIN CLIP AT RIB NR 16 IAW EMB 120 SRM 51-40-02 AND RII 28-900-1000.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 22,422 hrs · 33,104 cycles

CRACK IN PAX DOOR FRAME SUPPORT 2ND STOP FROM BOTTOM, DISCOVERED DURING C-CHECK INSPECTION. REPAIRED PAX DOOR FRAME SUPPORT 2ND STOP FROM BOTTOM IAW SRM 52-10-02 AND RII 52-800-1000.

Part: RIB — CRACKED (RT WING) · airframe 22,422 hrs · 33,104 cycles

CLIP CRACKED AT TOP OF RIB STA 6 RIGHT WING, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SERVICEABLE CLIP AT TOP OF RIB NR 6 IAW EMB 120 SRM 51-40-02 AND RII 28-900-1000.

Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 22,422 hrs · 33,104 cycles

RIGHT WING OUTBOARD TWO CLIPS CRACKED AT STA 15 ON LOWER PART OF RIB, DISCOVERED DURING C-CHECK INSPECTION. REPLACED TWO LOWER SKIN SUPPORT CLIPS ON RIB NR 15 IN RIGHT WING PER SRM 51-40-02 AND RII 28-900-1000.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,422 hrs · 33,104 cycles

2ND FROM RIGHT LATERAL FLOORBEAM CORRODED AT FRAME NR 38, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SERVICEABLE 2ND FROM RIGHT LATERAL FLOOR SUPPORT AT FRAME NR 38 IAW SRM 51-40-02.

Part: STRINGER SPLICE — CRACKED (NR 2 NACELLE) · airframe 22,422 hrs · 33,104 cycles

NR 2 NACELLE INBOARD STRINGER NR 1 SPLICE CRACKED AT FRAME NR 10, DISCOVERED DURING C-CHECK INSPECTION. REPLACED NR 1 SPLICE FOR NR 2 NACELLE INBOARD STRINGER AT FRAME NR 10 PER SRM 51-40-02 AND RII 54-900-1000.

Part: FLOOR SUPPORT — CORRODED (FUSLEAGE) · airframe 22,422 hrs · 33,104 cycles

SEVERAL AREAS OF CORROSION UNDER GALLEY FLOORBOARDS, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CENTER BUTT STRAP (FLOOR SUPPORT) BETWEEN FRAMES 39 THRU 44 PER SRM 51-40-02.

Part: RIB — CRACKED (RT WING) · airframe 22,422 hrs · 33,104 cycles

STATION 18 RIGHT WING CRACKED CLIPS FOR RIB, TWO ARE CRACKED FOR LOWER PART OF RIB, DISCOVERED DURING C-CHECK INSPECTION. REPLACED TWO LOWER WING SUPPORT CLIPS (AFT AND 2ND FROM AFT) AT RIB 18 OF RIGHT WING PER SRM 51-40-02 AND RII 28-900-1000.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,637 hrs · 31,927 cycles

ON EMERGENCY RED LIGHT AT FRONT PAX ENTRY BURNED OUT. RELAMPED. OPERATIONAL CHECK GOOD.

Part: SELECTOR — MALFUNCTIONED (TE FLAPS) · airframe 21,608 hrs · 31,881 cycles

ON FINAL, WHEN SELECTING FLAPS 25, FLAP MSG. REPLACED FLAP CONTROL HANDLE. OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (TE FLAPS) · airframe 21,562 hrs · 31,821 cycles

ON FLAP EXTENSION RECEIVED CONTROL FAULT FOR FLAPS 15 DEG AND 25 DEG. REPAIRED BROKEN WIRE AT AFT FLAP O/B ACTUATOR CONNECTOR. OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 21,236 hrs · 31,333 cycles

FORWARD BULKHEAD EXIT SIGN INOPERATIVE. REPAIRED WIRE TO FORWARD BULKHEAD EMERGENCY EXIT SIGN. OPERATIONAL CHECK GOOD.

Part: ANNUNCIATOR — MALFUNCTIONED (TE FLAPS) · airframe 20,999 hrs · 30,984 cycles

AFTER SELECTING FLAPS 15 DEGREES, GOT CONTROL FAULT ON OVERHEAD PANEL. REPLACED FLAP ANNUNCIATOR PANEL IAW MM 27-50-00. OPERATIONAL CHECK GOOD, P/N: 347100-1001 S/N OFF: 0066.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAPS) · airframe 20,747 hrs · 30,610 cycles

MULTIPLE CONTROL FAULTS ON APPROACH TO SEA. REPLACED RT NACELLE FLAP ACTUATOR IAW MM 27-50-08. OPERATIONAL CHECK GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (STALL WARNING) · airframe 20,338 hrs · 30,019 cycles

STALL WARNING LIGHT ON MAP STAYS ILLUMINATED. REPLACED STALL WARNING PANEL, OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (TE FLAP HANDLE) · airframe 20,025 hrs · 29,557 cycles

AFTER DEPARTURE AND MOVING FLAP HANDLE TO 0 RECIEVED A FLAP CONTROL FAULT. REPAIRED BROKEN WIRE AT LEFT OUTBOARD FLAP ACTUATOR. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAP) · airframe 19,930 hrs · 29,417 cycles

CONTROL FAULT FLAPS EXTEND TO 7 DEGREES. REPLACED FLAP COMPUTER IAW 27-50-06. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 19,912 hrs · 29,394 cycles

LT OUTBOARD FLAP FAILED ON TAXI TO GATE. REPLACED LT OUTBOARD FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECK SATISFACTORY.

Part: SELECTOR — MALFUNCTIONED (TE FLAP) · airframe 19,277 hrs · 28,405 cycles

ON FINAL, SELECTED FLAPS 15; GOT CONTROL FAULT. REPLACED FLAP SELECTOR LEVER ASSY. OPERATIONAL CHECK GOOD.

Part: SELECTOR — MALFUNCTIONED (TE FLAPS) · airframe 19,180 hrs · 28,248 cycles

FLAP CONTROL FAULT WHEN SELECTING FLAPS DOWN. REPLACED FLAP SELECTOR LEVER ASSY WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,508 hrs · 27,271 cycles

FORWARD SECTION OF EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD BATTERY PACK. OPERATIONAL CHECK GOOD IAW MM 33-50-00.

Part: CONTROL UNIT — CONTAMINATED (TE FLAPS) · airframe 18,440 hrs · 27,170 cycles

FLAP CONTROL FAULT ON TAXI OUT. RERACKED FLAP CONTROL UNIT IAW AMM 27-50-06 PAGE 401. CLEANED MOISTURE FROM LEFT AND RIGHT FLAP ACUTATOR CANNON PLUG. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAP) · airframe 18,232 hrs · 26,838 cycles

RECEIVED A CONTROL FAULT WARNING DURING LANDING ROLL. REPLACED FLAP CONTROL UNIT WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.

Part: SEAL — DAMAGED (CARGO DOOR) · airframe 17,866 hrs · 26,282 cycles

LOST PRESSURIZATION IN AUTO AND MANUAL MODES. REINSTALLED CARGO DOOR SEAL AS REQUIRED. OPERATIONAL CHECK GOOD.

Part: SERVO — MALFUNCTIONED (STICK SHAKER) · airframe 16,557 hrs · 24,285 cycles

F/O SIDE CLACKER IS INOP. REPLACED F/O'S SIDE STICK SHAKER. OPS CHECKS GOOD.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 16,284 hrs · 23,856 cycles

VARIOUS EMERGENCY LIGHTS INOPERATIVE. REPLACED CENTER ELBP IAW MM 33-50-00. OPS CHECK GOOD.

Part: LIGHT — FAILED (GALLEY) · airframe 16,284 hrs · 23,856 cycles

LIGHT TO LEFT OF PHONE IN GALLEY BURNED OUT IN FLIGHT. AFTER, WE NOTICED AN ACRID SMELL IN COCKPIT AND CABIN. AFTER ABOUT 10 MINUTES, SMELL CAME BACK AND LIGHTS ON GALLEY PANEL FLICKERED.REPLACED AFT GALLEY LIGHT BALLAST. OPS CHECKS OKAY.

Part: SERVO — MALFUNCTIONED (AUTOPILOT) · airframe 16,166 hrs · 23,689 cycles

CAPTAIN SIDE AUTOPILOT INOP - WILL NOT MAINTAIN ALT OR PITCH IN CLIMB. REPLACED ELEVATOR AUTOPILOT SERVO. OPERATES NORMALLY PER MM 22-11-00.

Part: FLAP TRACK — LACK OF LUBE (T/E FLAP) · airframe 16,131 hrs · 23,642 cycles

FLAP DISAGREEMENT ON CLIMBOUT FROM GEG. FLAPS STUCK BETWEEN 0-15 DEGREES. FLAPS CAME DOWN TO 25 DEGREES OK, BUT WOULD NOT GO UP UNTIL ON THE GROUND. CLEANED AND LUBED TRACKS AND ROLLERS, CYCLED FLAPS SEVERAL TIMES. NO FAULTS NOTED, FLAPS OPS CHECK NORMAL.

Part: SERVO — MALFUNCTIONED (AUTOPILOT SYS) · airframe 16,131 hrs · 23,642 cycles

ENGAGING EITHER YAW DAMPER CAUSES UNCOMMANDED RUDDER DEFLECTION. REMOVED AND REPLACED RUDDER SERVO MOTOR WITH NEW SERVO MOTOR IAW 22-10-09. OPS CHECK GOOD AT THIS TIME.

Part: CONTROLLER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 16,083 hrs · 23,571 cycles

AFTER AUTOPILOT IS ENGAGED, ALL PARTS OF AUTOPILOT SYSTEM WORK PROPERLY EXCEPT THE AUTOPILOT WILL NOT CHANGE THE PITCH OF THE AIRPLANE. REPLACED TRANSFER BOX IAW 22-10-1. OPS CHECKS GOOD.

Part: SOCKET — CRACKED (EMERGENCY LIGHT) · airframe 15,909 hrs · 23,316 cycles

EMERGENCY EXIT LIGHTED SIGN BY FLIGHT ATTENDANT SEAT LOWER FIXTURE BROKEN. INSTALLED NEW LIGHT FIXTURE. OPS CHECK GOOD.

Part: CLIP — CRACKED (FUSELAGE) · airframe 15,597 hrs · 22,823 cycles

LEFT AND RIGHT FRAME 9 CLIPS CRACKED IN COCKPIT. FOUND DURING C-CHECK INSPECTION. COMPLIED WITH SB 120-53-0073.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,597 hrs · 22,823 cycles

CORROSION ON FLOORBEAM IN LAVATORY AREA. FOUND DURING C-CHECK INSPECTION. REMOVED AND REPLACED BUTT STRAP WITH SERVICEABLE UNIT, LAV TO CARGO, RIGHT SIDE.

Part: BRACKET — CRACKED (HYD POWERPACK) · airframe 15,597 hrs · 22,823 cycles

BLUE HYDRAULIC SYSTEM PACK LOWER BRACKET CRACKED FOUND DURING C-CHECK INSPECTION. INSTALLED NEW LOWER SUPPORT BRACKET FOR BLUE SYSTEM HYDRAULIC PACK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 15,597 hrs · 22,823 cycles

CRACK ON SKIN SUPPORT LEFT SIDE OF COCKPIT BEHIND DV WINDOW. FOUND DURING C-CHECK INSPECTION. REPLACED SKIN SUPPORT LEFT SIDE OF COCKPIT AFT OF DV WINDOW PER MM 53-00-00 AND 51-00-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,597 hrs · 22,823 cycles

CORROSION ON LEFT INBOARD FLOORBEAM AND SEAT TRACK AT FORWARD END OF SEAT TRACK. FOUND DURING C-CHECK INSPECTION. REPAIRED CORROSION ON LEFT INBOARD FLOORBEAM AND SEAT TRACK AT FORWARD END OF SEAT TRACK. REPAIRED FLOORBEAM IAW SRM 53-00-03 AND REPAIRED SEAT TRACK IAW EMB EST 186/96. NO DEFECTS NOTED.

Part: DIODE — FAILED (EMERGENCY LIGHTS) · airframe 15,070 hrs · 22,036 cycles

TWO RED FLOOR PROXIMITY EMERGENCY LIGHTS OUT AT MAIN CABIN DOOR EXIT. SOLDERED IN NEW DIODE AT ROW 6. OPS CHECK GOOD AT THIS TIME.

Part: STARTER GEN — SHORTED (APU) · airframe 15,070 hrs · 22,036 cycles

SMELLED SOMETHING BURNING. APU GEN DROPPED OFF LINE. APU SHUT ITSELF DOWN. REPLACED APU CURRENT SENSOR RELAY (FOUND MELTED). FOUND WIRES AT APU STARTER GENERATOR TERMINAL BOARD MELTED. REPLACED APU STARTER GEN WITH SERVICEABLE STARTER GENERATOR. REMOVED DAMAGED TERMINALS AND TRIMMED OFF DAMAGED WIRE ENDS. SWEDGED ON NEW TERMINALS AS REQUIRED. PERFORMED OPS CHECK OF APU STARTER/GEN. OPS CHECK GOOD.

Part: BULB — BURNED OUT (MLG INDICATOR) · airframe 14,817 hrs · 21,612 cycles

ON APPROACH INTO SFO, THE RT MLG SHOWED ALL LIGHTS OUT WITH GEAR DOWN. INSTALLED NEW BULBS. OPS CHECK GOOD.

Part: ANNUNCIATOR — MALFUNCTIONED (TE FLAPS) · airframe 14,817 hrs · 21,612 cycles

UPON SELECTING FLAPS 15 DEGREES ON TAXI OUT, WE HAD A ''CONTROL FAULT'' AFFECTING THE OUTBOARD PAIR OF FLAPS. REPLACED FLAP ANNUNCIATOR UNIT. OPS CHECKS GOOD.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 13,562 hrs · 19,648 cycles

NR 1 ENGINE NH GAUGE (ANALOG & DIGITAL), INOP DURING FLIGHT. NL WAS OK. RETURNED TO PDX. LEFT ANALOG AND DIGITAL PORTION OF NH GAUGE READ EITHER -0- OR ERRATIC. NL WORKS FINE. REPLACED WIRE HARNESS 3115911-01 ON LEFT ENGINE. RAN ENGINES FOR OPS CHECK. OPS CHECK GOOD PER MM 77-00-00. REMOVED AND REPLACED LEFT NH/NL INDICATOR IAW M/M 77-00-00. RAN ENGINES AT HIGH POWER SETTINGS FOR 15 MINUTES. OPS CHECK GOOD.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 13,395 hrs · 19,413 cycles

DURING TAKEOFF ROLL GOT A HIGH SPEED AURAL WARNING. ABORTED TAKEOFF. REPLACED CAPTAIN'S AIRSPEED INDICATOR. CHECKED PITOT STATIC SYSTEM PER FAR 91-411 & PART 43 APPENDIX E. OPS CHECK GOOD.

Part: SERVO — DAMAGED (AUTOPILOT SYS) · airframe 13,336 hrs · 19,315 cycles

ON PREFLIGHT, RUDDER HAS A BINDING FEEL WHEN LEFT RUDDER IS DEPRESSED. FOUND RUDDER TRIM SERVO DAMAGED. REPLACED RUDDER TRIM SERVO WITH SERVICEABLE UNIT IAW MM 22-10-05. OPS CHECKS GOOD.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 12,268 hrs · 17,710 cycles

''TRIM FAIL'' LIGHT ON MAP ILLUMINATED ON TAKEOFF ROLL. MEL 22-10-1A, MC 021OPERATED TRIM SEVERAL TIMES FULL RANGE. OPS CHECK GOOD ON GROUND.

Part: ACCESS PANEL — OPEN (FUSELAGE) · airframe 4,146 hrs · 5,683 cycles

DOOR CONTROL ACCESS PANEL OPENED DURING TAKEOFF ROLL. RETURNED TO LAX. INSPECTED DOOR. NO DEFECT FOUND. RELATCHED DOOR. OPS CHECK GOOD.

Part: CONNECTOR — DIRTY (TE FLAPS) · airframe 11,949 hrs · 17,212 cycles

WHILE RETRACTING FLAPS AFTER TAKEOFF THE INBOARD FLAPS STOP RETRACTING AT APPROXIMATELY 12 DEGREES, WHILE THE OUTBOARD AND NACELLE FLAPS STOP AT APPROXIMATELY 6 DEGREES. PERFORMED QRH PROCEDURE FOR A FLAP DISAGREEMENT. THE PROBLEM DID NOT CORRECT ITSELF. RETURNED TO LAX FOR LANDING. ENABLED MX MODE OF ANN PNL. ALL HISTORIES REPORTED NO FAILURES. CLEANED ALL CANNON PLUGS. RESTORED A/C TO NORMAL. CYCLED FLAPS 50+ TIMES. NO DISCREPANCIES NOTED.

Part: FUEL CONTROL — MALFUNCTIONED (RT ENGINE) · airframe 11,607 hrs · 16,725 cycles

RIGHT ENGINE HAD TORQUE FLUCTUATIONS ON TAKEOFF ROLL. OPERATED RT ENGINE AND LT ENGINE. TRIMMED RT ENGINE AS NECESSARY. NO FURTHER DEFECTS NOTED. OPS CHECK GOOD.

Part: INTERPHONE — INOPERATIVE (CABIN) · airframe 11,466 hrs · 16,521 cycles

FLIGHT ATTENDANT HANDSET SMOKING AND INOPERATIVE. REMOVE AND REPLACE FLIGHT ATTENDANT HANDSET. OPS CHECK GOOD IAW 23-30-1. P/N: 5096-1-2, S/N ON: 669.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 10,959 hrs · 15,875 cycles

TRIM FAIL ILLUMINATED ON MAP. NO AURAL WARNING WHILE ON TAKEOFF ROLL. ABORTED TAKEOFF. MEL 22-10-1B, ELECT TRIM, MC 122. RE-RACKED NUMBER ONE AND NUMBER TWO APC-65S. OPERATED AND TESTED TRIM SYSTEM. NO DEFECTS NOTED, COULD NOT DUPLICATE.

Part: WARNING SYSTEM — MALFUNCTIONED (TRIM SYS) · airframe 10,257 hrs · 14,916 cycles

TRIM FAIL LIGHT ON MAP WITH 3 CHIME WHILE USING MANUAL TRIM. TRIM FEELS LIKE ENGAGED WITH AUTO PILOT WHEN AUTO PILOT DISENGAGED. REMOVED AND REPLACED ELEVATOR TRIM SERVO WITH SERVICEABLE UNIT IAW MM 22-10-05. OPS CHECKS NORMAL.

Part: WARNING SYSTEM — MALFUNCTIONED (TRIM SYSTEM) · airframe 10,257 hrs · 14,916 cycles

TRIM FAIL LIGHT ILLUMINATES ON MAP WITH 3 CHIME MASTER WARNING WHILE USING THE MANUAL TRIM WHEEL DURING FLIGHT. INSPECTED TRIM ACTUATORS AND CABLES. FOUND WELL GREASED AND NO SIGNS OF MOISTURE. ACTUATED SYSTEM SEVERAL TIMES. GROUND OPS CHECKS GOOD.

Part: CONNECTOR — DIRTY (INDICATOR) · airframe 9,608 hrs · 13,989 cycles

LEFT NH INTERMITTENT 50 - 93 PERCENT WITH NO FLUCTUATION IN NL OR NP. RETURNED TO SEA. REMOVED AND REPLACED LEFT NH/NL INDICATOR IAW MM 77-00-00 AND CLEANED CANNON PLUG AT NL SENSOR. ENGINE RUN UP AND OPS CHECKS GOOD. P/N ON: SEDL-0C29M, S/N: 197, S/N OFF: B339.

Part: REU — FAILED (E&E COMPT)

RADIO FAILURE, LOSS OF ABILITY TO TRANSMIT OR RECEIVE. RETURNED TO FAT. REPLACED REU. OPS CHECKS GOOD.

Part: PRESSURIZATION — MALFUNCTIONED (CABIN)

ERRATIC PRESSURIZATION ON CLIMBOUT AND AT 5,000 FEET THE CABIN WAS CLIMBING AT 2,000 FEET PER MINUTE. TRIED TO CONTROL BY AUTO-NORM BUT NOT ABLE TO. MOVED AUTO/MANUAL SWITCH TO CHECK SWITCH AND MASKS DROPPED. THE CABIN WAS AT 10,000 AT THIS TIME. RETURNED TO SAN. PRESSURIZED AIRCRAFT TWICE IN AUTO AND TESTED IN MANUAL. COULD NOT DUPLICATE. GOOD CONTROL IN AUTO AND MANUAL. RESTORED ALL CABIN MASKS. OPS CHECKS GOOD AT THIS TIME.

Part: PRESS SYST — MALFUNCTIONED (CABIN)

AIRCRAFT WOULD NOT PRESSURIZE IN AUTO OR MANUAL MODE. DIVERTED TO LAX. CHECKED OUT FLOW VALVES AND CARGO DOOR SEAL. RAN RIGHT PACK AND PRESSURIZED AIRCRAFT IN AUTO AND MANUAL MODES, OPS CHECKS GOOD.

Part: RETRACT MECH — MALFUNCTIONED (LANDING GEAR)

LEFT MAIN LANDING GEAR WILL NOT RETRACT, 2 RED INTRANSIT LIGHTS REMAIN ILLUMINATED. HYD PUMP RUNS AND THERE WAS NOISE FROM THE LEFT GEAR. RETURNED TO FIELD. INSPECTED LEFT MAIN GEAR IAW MM 32-32-00 AND ACCOMPLISHED GEAR RETRACTION TEST IAW MM 32-30-00, OPS NORMALLY AT THIS TIME.