N565SW

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 31,945 hrs · 43,715 cycles

PAX DOOR SUPPORT PROFILE CRACKED AT BAY NR 2. C-CHECK NEW SUPPORT PROFILE INSTALLED ON PAX DOOR AT BAY NR 2 IAW SRM.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 31,945 hrs · 43,715 cycles

PAX DOOR BAY NR 5 HAS A CRACKED UNDERNEATH WEBBING SUPPORT PROFILE. C-CHECK NEW SUPPORT PROFILE INSTALLED ON PAX DOOR AT BAY NR 5 IAW SRM.

Part: ROD — CORRODED (PAX DOOR) · airframe 31,945 hrs · 43,715 cycles

PAX DOOR STEP RODS HAVE CORROSION. C-CHECK REPLACED PAX DOOR NR 2 & NR 3 STEP RODS IAW AMM.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 31,945 hrs · 43,715 cycles

PAX DOOR AFT FRAME UNDER MID STEP STRUCTURE CRACKED. C-CHECK NEW FRAME INSTALLED ON AFT PAX DOOR BELOW MID STEP IAW SRM.

Part: DOOR FRAME — CORRODED (PAX DOOR) · airframe 31,945 hrs · 43,715 cycles

PAX DOOR LOWER FWD BAY 2 FRAME HAS SEVERE CORROSION. C-CHECK NEW FRAME INSTALLED ON PAX DOOR LOWER BAY 2 IAW SRM.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 31,945 hrs · 43,715 cycles

PAX DOOR ENTRANCE LOWER FLOOR BOARD ATTACH ANGLES NEED REPLACED, CORRODED. C-CHECK REPLACED PAX DOOR ENTRANCE LOWER FLOOR BOARD ATTACH ANGLES REPLACEMENT IAW EMB 120 SRM.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 31,945 hrs · 43,715 cycles

CARGO DOOR COUNTER WEIGHT FWD MOUNT SUPPORT STRUCTURE CRACKED AS MARKED. C-CHECK REPLACED CARGO DOOR COUNTER WEIGHT FWD MOUNT SUPPORT ASSEMBLY PN 120-20235-605 IAW EMB120 SRM.

Part: SUPPORT — FAILED (LT WING) · airframe 31,945 hrs · 43,715 cycles

LT WING INBD SIDE OF THE FUEL PANEL NR 5 HAS A BROKEN SKIN CLEAT ON UPPER SKIN. C-CHECK REPLACED SKIN SUPPORT CLEAT PN 120-17063-609 IAW 120 SRM.

Part: CLEAT — CRACKED (RT WING) · airframe 31,945 hrs · 43,715 cycles

RT WING TOP SKIN CLEAT INBD OF NR 5 ACCESS PANEL CRACKED. C-CHECK REPLACED 1 UPPER SKIN CLEAT IN RT WING INBD OF NR 5 FUEL ACCESS PANEL PN 120-17062-613 IAW EMB120 SRM.

Part: SUPPORT — CRACKED (RT WING) · airframe 31,945 hrs · 43,715 cycles

RT WING TOP SKIN CLEAT INBD OF NR 6 ACCESS PANEL CRACKED AT TOP. C-CHECK REPLACED SKIN SUPPORT AT RT WING NR 6 FUEL ACCESS PANEL UPPER CLEAT INBD SIDE PN 120-17064-009 IAW SRM.

Part: SUPPORT — CRACKED (RT WING) · airframe 31,945 hrs · 43,715 cycles

RT WING AT TOP AT NR 4 ACCESS PANEL HAS THREE CRACKED SKIN CLEATS. C-CHECK REPLACED THREE CRACKED SKIN SUPPORTS IN RT WING FUEL ACCESS PANEL, 1 INBD UPPER OF FUEL PANEL PN 120-61345-609 & 2 UPPER OTBD OF FUEL PANEL PN 120-17060-607,120-17063-009 IAW SRM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,945 hrs · 43,715 cycles

ROW 6A EMERGENCY LIGHTS DO NOT ILLUMINATE. FLT 5504 REPLACED ELBP. PN D366-04-001 SN ON 176 SN OFF 489

Part: UNKNOWN — SMOKE (CABIN) · airframe 31,008 hrs · 42,567 cycles

WITH LEFT BLEED AND PACK IN AUTO, LOW - OBSERVED FAINT SMOKE WITH STRONG BURNING SMELL. (FLT 5625) RAN RT PACK ON LT ENGINE AT VARIOUS ENGINE POWER SETTINGS AND COULD NOT DUPLICATE SMOKE OR BURNING SMELL. OPS CHECK GOOD.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 30,755 hrs · 42,259 cycles

RAPID HARD PRESSURE BUMPS WITH AUTO PRESSURIZATION, SWITCHED TO MANUAL MODE, CABIN KEPT WANTING TO DUMP. MASKS DEPLOYED IN CABIN. (FLT 7407) REPLACED THE ELECTRONIC CONTROLLER IAW AMM, RESTOWED MASKS. P/N 22201T011400 S/N ON 434 S/N OFF 488.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,686 hrs · 42,178 cycles

FLOOR EMERGENCY LIGHT DOES NOT ILLUMINATE. (FLT 6339) REPLACED FLOOR EMERGENCY LIGHT LAMP.

Part: ROLLER — OUT OF ADJUST (CABIN DOOR) · airframe 30,416 hrs · 41,808 cycles

MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN AND CLOSE. (FLT 5615) ADJUSTED PASSENGER FORWARD AND AFT ROLLERS.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 30,332 hrs · 41,696 cycles

ON DESCENT WITH BOTH PACKS AND BLEED SOURCES IN AUTO AND LOW, THE COCKPIT FILLED WITH SMOKE. LEFT SIDE TEMPERATURE CONTROLLER WAS IN AUTO AND FELT COLD. (FLT 5356) OPERATED LEFT PACK WITH APU AND THEN ENGINE BLEEDS FOR 30 MINS. NO ABNORMALITIES NOTED.

Part: ENGINE — FAULTY (RIGHT) · airframe 29,882 hrs · 41,176 cycles

WITH LOW POWER SETTINGS AND BLEED PACKS IN AUTO/LOW, CABIN FILLS WITH SMOKE. (FLT 7802) REPLACED RIGHT ENGINE ASSEMBLY. P/N OFF: PW11813, S/N OFF: AP0019.

Part: UNKNOWN — ODOR · airframe 29,862 hrs · 41,151 cycles

WHEN REDUCING POWER LEVERS TO DESCEND, HAD AN ODOR OF OVERHEATING FROM RIGHT AIR CONDITIONING PACK. (FLT 7759) RAN RIGHT AIR CONDITIONING PACK IN ALL MODES WITH APU AND RIGHT ENG RUNNING, NO DISCREPANCIES NOTED.

Part: COOLING FAN — MALFUNCTIONED (CABIN) · airframe 29,327 hrs · 40,524 cycles

RIGHT PACK OVERHEATED AND BLEW SMOKE INTO CABIN. (FLT 5633) REPLACED RIGHT GROUND COOLING FAN IN REFERENCE TO MM. P/N: AE1711AA0 S/N OFF: 127

Part: FIXTURE — FAILED (CABIN) · airframe 29,051 hrs · 40,153 cycles

EMERGENCY EXIT ROW SIGN AT 9C IS INOPERATIVE. (FLT 7777) REPLACED EMERGENCY LIGHT FIXTURE. PN: 10-1110-5, SN OFF: NSN

Part: SWITCH — FAILED (CABIN DOOR) · airframe 28,800 hrs · 39,864 cycles

MAIN CABIN DOOR DOES NOT OPEN USING HYDRAULICS. (FLT 6220) REPLACED FORWARD DOOR CONTROL MICROSWITCH.

Part: ACTUATOR — OUT OF RIG (MLG) · airframe 28,707 hrs · 39,745 cycles

FLT 7755, A & B RED DISAGREE ON LEFT MAIN GEAR. INSPECTED LEFT MLG ACTUATING CYLINDERS FOR RIG AND FOUND NO GAP ON HOOK, ROLLER AND UPLOCK. RIGGED MAIN LANDING GEAR ACTUATOR CYLINDER. CYCLED LANDING GEAR AND PERFORMED EMERGENCY EXTENSION WITH THREE CYCLES AFTERWARD. SYSTEM CHECKS GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 28,707 hrs · 39,745 cycles

FLT 5432, NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,331 hrs · 39,293 cycles

CEILING EMERGENCY LIGHT AT ROW 7 INOPERATIVE. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: SUPPORT BRACKET — CRACKED (LT NACELLE) · airframe 28,339 hrs · 39,305 cycles

LEFT ENGINE NACELLE AFT EXHAUST INBOARD AND OUTBOARD MOUNT SUPPORT BRACKETS ARE CRACKED. (SERVICE) REPLACED NEW RIBS ON LEFT INBOARD AND OUTBOARD EXHAUST MOUNTING AREAS.

Part: DOOR FRAME — WORN (FUSELAGE) · airframe 28,910 hrs · 39,991 cycles

THE LEFT OVERWING EXIT FRAME HAS WEAR MARKS. (C-CHECK) REPLACED AFT PROFILE L IN REFERENCE TO EMB-120 SRM.

Part: DOOR FRAME — WORN (FUSELAGE) · airframe 28,910 hrs · 39,991 cycles

THE RIGHT OVERWING EXIT FRAME HAS WEAR MARKS. (C-CHECK) REPLACED THE L PROFILE FRAME ON RIGHT OVERWING EXIT IN REFERENCE TO SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,889 hrs · 38,763 cycles

RIGHT SIDE EMERGENCY LIGHT AT ROW 6 IS OUT. (FLT 6297) RELAMPED EMERGENCY LIGHT.

Part: CONTROL ROD — OUT OF ADJUST (WINDOW) · airframe 27,824 hrs · 38,691 cycles

CAPTAIN'S DV WINDOW HARD TO OPEN AND CLOSE. (FLT 7793) ADJUSTED CAPTAINS DV WINDOW CONTROL ROD.

Part: ROLLER — WORN (MCD) · airframe 26,839 hrs · 37,437 cycles

MCD DIFFICULT TO OPEN. (FLT 6286) REPLACED PAX DOOR ROLLERS AND LUBED DOOR LOCKING MECHANISM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,637 hrs · 37,196 cycles

AFT EXTERIOR EMERGENCY LIGHT NOT ILLUMINATING ON RIGHT SIDE OF AIRCRAFT. (FLT 7756) RELAMPED EMERGENCY LIGHT.

Part: SEAL — LACK OF LUBE (CABIN DOOR) · airframe 26,209 hrs · 36,696 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6200) LUBED MAIN CABIN DOOR SEAL.

Part: STRINGER — CRACKED (RT WING) · airframe 25,635 hrs · 36,043 cycles

RIGHT WING STRINGER CRACKED. (C-CHECK) REPAIRED PER SRM.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 25,635 hrs · 36,043 cycles

FS 14 SUPPORT BEAM CORRODED. (C-CHECK) REPLACED PER SRM.

Part: FLAP — CRACKED (RT WING) · airframe 25,635 hrs · 36,043 cycles

RIGHT NACELLE FLAP IS CHAFED AND CRACKED. (C-CHECK) REPAIRED PER SRM.

Part: WIRE — BROKEN (CABIN) · airframe 24,550 hrs · 34,749 cycles

TWO FLOOR EMERGENCY LIGHTS INOP AT ROW 10. (FLT 6817) REPAIRED BROKEN WIRE.

Part: LIGHT — LOOSE (CABIN) · airframe 24,550 hrs · 34,749 cycles

TWO EMERGENCY FLOOR LIGHTS INOP. (FLT 6576) RESEATED BULB AT ROW 2 AND REPLACED CONNECTOR AT ROW 9.

Part: WIRE — LOOSE (CABIN) · airframe 24,156 hrs · 34,214 cycles

AFT SECTION OF EMERGENCY TRACK LIGHTING INOP. (FLT 7781) RESEATED WIRING.

Part: LIGHT — LOOSE (CABIN) · airframe 23,860 hrs · 33,856 cycles

EMERGENCY FLOOR LIGHT AT ROW 3 INOP. (FLT 7802) RESEATED LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,740 hrs · 33,714 cycles

FLOOR EMERGENCY LIGHTS AT ROW 3 INOP. (FLT 6295) RELAMPED EMERGENCY LIGHT.

Part: LANDING GEAR — MALFUNCTIONED · airframe 23,639 hrs · 33,585 cycles

FLT 6652 ON LANDING ROLL OUT REVERSE, NOSE WHEEL STEERING, AND BRAKES INOP. REMOVED & REPLACED THE RIGHT MLG STRUT WITH A SERVICEABLE UNIT IAW MM 32-11-00.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 23,382 hrs · 33,225 cycles

FLT 6329 - ONE FLOOR EMERGENCY WHITE LIGHT MISSING. RESECURED CONNECTOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,315 hrs · 33,146 cycles

FLT 6320 - ONE RED FLOOR PROXIMITY LIGHT INOP. REPOSITIONED LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 23,032 hrs · 32,771 cycles

FLT 7814 - SECOND BULB IN FORWARD FLOOR EMERGENCY LIGHTING SYSTEM INOP. RELAMPED.

Part: ACTUATOR — FAILED (RT MLG) · airframe 22,500 hrs · 32,051 cycles

FLT 5791 - RIGHT MAIN GEAR WOULD NOT FULLY RETRACT. REPLACED RIGHT MAIN GEAR ACTUATOR PER AMM, PN 19595-000-07, SN ON 91, SN OFF B161.

Part: DETECTION SYS — MALFUNCTIONED · airframe 22,226 hrs · 31,695 cycles

FLT 5752 - FIRE BELL INTERMITTENTLY RINGS IN FLIGHT, NO LIGHT ASSOCIATED WITH IT. RESET FIRE SYSTEM, CHECKS NORMAL.

Part: STRIP — CORRODED (FUSELAGE) · airframe 22,052 hrs · 31,482 cycles

PASSENGER DOOR CUTOUT HAS CORROSION AT BOTTOM. (C-CHECK) REPLACED BOTTOM STRIP AT DOOR CUTOUT.

Part: STRINGER — CRACKED (RT WING) · airframe 22,052 hrs · 31,482 cycles

RIGHT WING STRINGER AFT OF SECOND OUTBOARD FUEL ACCESS PANEL CRACKED. (C-CHECK) REPAIRED PER SRM 57-20-03.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 21,921 hrs · 31,329 cycles

CAPTAINS WINDSHIELD CRACKED. (FLIGHT NR 3620) REPLACED LT WINDSHIELD IAW AMM 56-10-01. OPS AND LEAK CHECK GOOD. P/N: NP-151311-1 S/N OFF: 97204H1888

Part: CONNECTOR — LOOSE (SMOKE DETECTOR) · airframe 21,843 hrs · 31,223 cycles

TEST NR2 ON BAGGAGE SMOKE AND FIRE SYSTEM DOES NOT WORK. (FLIGHT NR 5566) RESECURED CONNECTOR PLUG ON AFT CARGO SMOKE DETECTOR. OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (SMOKE DETECTOR) · airframe 21,728 hrs · 31,072 cycles

FLT 3594 - NR 2 BAGGAGE SMOKE DETECTOR WILL NOT TEST. SECURED CONNECTOR ON SMOKE DETECTOR 2. ALL OPS CHECKS NORMAL.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 21,106 hrs · 30,323 cycles

FOUND MISSING RIVET AND CORROSION AT STRINGER 20R BETWEEN FRAMES 22 AND 23. REPAIRED AND TREATED CORRODED STRINGER IAW 120 CPM 51-14-00 AND 51-14-02 ALONG WITH SRM 51-40-02.

Part: FAN — SMOKE (RECIRCULATION) · airframe 21,065 hrs · 30,277 cycles

SMELL OF SMOKE WHILE IN FLIGHT AT LOW POWER SETTINGS, FLIGHT NR 5499. REPLACED THE LEFT RECIRCULATION FAN WITH A SERVICEABLE UNIT IAW EMB 120 MM 21-24-03. OPS CHECK GOOD AT THIS TIME.

Part: HEATER — INOPERATIVE (WINDSHIELD) · airframe 20,946 hrs · 30,110 cycles

RIGHT WINDSHIELD HEAT IS INOP, FLIGHT NR 5477. REPLACED RIGHT WINDSHIELD IAW AMM 56-10-01, P/N NP-151311-2, S/N OFF 98111H3490.

Part: CONNECTOR — ODOR (TEMP SENSOR) · airframe 20,872 hrs · 30,004 cycles

FLIGHT ATTENDANT NOTICED A BURNING ODOR COMING FROM THE VENTS AFTER TAKEOFF, FLIGHT NR5745. INSPECTED BOTH PACKS AND CLEANED CONNECTORS FOR RIGHT PACK DUCT TEMPERATURE SENSOR. OPS CHECKS GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED · airframe 19,629 hrs · 28,412 cycles

FIREBELL, ACCOMPANIED WITH INTERMITTENT MAP LIGHTS. REPLACED AURAL WARNING UNIT IAW MM 31-53-02, OPS CK GOOD.

Part: SEQUENCE VALVE — MALFUNCTIONED (MLG) · airframe 18,974 hrs · 27,614 cycles

LEFT MAIN GEAR DID NOT RETRACT PROPERLY WITH RED AND GREEN A&B REMAINING LIT. RETURNED TO FIELD. REPLACED BOTH LEFT GEAR DOOR SEQUENCE VALVES. OPERATIONAL CHECKS GOOD IAW 32-32-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,670 hrs · 27,237 cycles

LEFT FLOOR SEAT TRACK CORRODED AT BEGINNING TO ABOUT 4 FEET, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT FLOOR SEAT TRACK FROM SEAT 2A TO SEAT 4A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,670 hrs · 27,237 cycles

LEFT FLOOR SEAT TRACK CORRODED AT END TO ABOUT 4" FEET BY GALLEY. INSTALLED LEFT FLOOR SEAT TRACK AFT SECTION FROM SEAT 9A TO GALLEY.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 18,670 hrs · 27,237 cycles

CABIN CENTER AFT FLOORBEAM CAP CORRODED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CABIN AFT CENTER FLOORBEAM CAP.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 18,448 hrs · 26,896 cycles

FORWARD FLOOR EMERGENCY LIGHTS, MAP AS WELL AS FORWARD EXIT SIGN INOP. REMOVED AND REPLACED FORWARD ELBP. OPERATIONAL CHECKS GOOD.

Part: RIB — CRACKED (NACELLE FLAP) · airframe 18,332 hrs · 26,750 cycles

LT NACELLE FLAP HAS A CRACKED RIB, DISCOVERED DURING C-CHECK INSPECTION. REPLACED LT NACELLE FLAP IAW RII 27-900-1006. OPERATIONAL CHECKS GOOD, PN ON 120-40327-001.

Part: CONNECTOR — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 18,125 hrs · 26,456 cycles

EMERGENCY FLOOR LIGHTS INOP. SECURED LOOSE CONNECTOR. OPERATIONAL CHECKS GOOD.

Part: CONNECTOR — OUT OF ADJUST (CABIN) · airframe 17,974 hrs · 26,239 cycles

FLIGHT ATTENDANT REPORTED 4 EMERGENCY LIGHTS IN A ROW OUT OR INOP. ADJUSTED EMERGENCY LIGHT CONNECTOR BY ROW 6. OPERATIONAL CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 17,187 hrs · 25,168 cycles

AFT EMERGENCY LIGHT STRIP FAILS TO ILLUMINATE. REPLACED AFT ELBP. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (FLAPS) · airframe 16,760 hrs · 24,593 cycles

WHEN LOWERING FLAPS, CONTROL FAULT ON FLAP PANEL. REPLACED THE FLAP CONTROL UNIT IAW MM 27-50-06. OPERATIONAL CHECK GOOD.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 16,564 hrs · 24,367 cycles

ONE WHITE EMERG FLOOR LIGHT INOP ON FLOOR STRIP. RESECURED WIRING ON FLOOR STRIP. OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 16,454 hrs · 24,220 cycles

LAST THREE EMERGENCY LIGHTS OUT. REPAIRED BROKEN WIRE UNDER FLOORBOARD AT SEAT 9A, OPERATIONAL CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (E/E BAY) · airframe 16,072 hrs · 23,741 cycles

AUTOPILOT PITCH IS JERKY AND NOT SMOOTH IN ALL MODES OF FLIGHT. REPLACED PITCH SERVO AND NR 1 AHRS IAW MM 34-21-01. OPERATIONAL TEST GOOD IAW MM 22-10-00. P/N: 622-5734-002, S/N: OFF 3767.

Part: SIGN — MISSING (EMERGENCY LIGHT) · airframe 15,853 hrs · 23,485 cycles

EMERGENCY EXIT SIGN MISSING FORWARD DOOR. INSTALLED NEW EMERGENCY LIGHT FIXTURE, OPERATIONAL CHECK GOOD.

Part: RELAY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 15,416 hrs · 22,866 cycles

EMERGENCY LIGHTS WILL NOT TURN OFF. INSTALLED NEW K0201 RELAY. OPERATIONAL CHECK GOOD.

Part: LIGHT — BURNED OUT (9 BC) · airframe 14,932 hrs · 22,208 cycles

RED EMERGENCY TRACK LIGHTING OUT AT 9B. RELAMPED RED LIGHT TRACK LIGHTING AT 9BC.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 14,882 hrs · 22,123 cycles

AFTER DEPARTURE, RECEIVED DISAGREEMENT FOR FLAPS (INBOARD PAIR). REPLACED LEFT INBOARD FLAP ACTUATOR, OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,882 hrs · 22,123 cycles

WHITE EMERGENCY LIGHT INOPERATIVE BY 4A. REPAIRED WHITE FLOOR STRIP EMERGENCY LIGHT BY SEAT 4A. OPERATIONAL CHECK GOOD.

Part: SERVO — STUCK (RUDDER) · airframe 14,213 hrs · 21,192 cycles

DISENGAGED AP WITH BALL CENTERED DURING A DESCENT AND RUDDER WAS JAMMED. SHORTLY AFTER SOMETHING LET LOOSE AND PROBLEM WAS CORRECTED. REPLACED RUDDER SERVO IAW AMM 27-11-00. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (TE FLAP) · airframe 14,058 hrs · 20,984 cycles

AFTER ENGINE START, RECEIVED A FLAP ASYMMETRY WITH THE IB PAIR. REPLACED LT IB FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 13,664 hrs · 20,503 cycles

UPON FLAP RETRACTION AFTER LANDING, THE IB PAIR REPEATEDLY STUCK AT TEN DEGREES. REMOVED AND REPLACED RT IB FLAP ACTUATOR IAW MM 27-50-00. OPERATIONAL CHECK GOOD.

Part: SELECTOR — MALFUNCTIONED (TE FLAPS) · airframe 13,462 hrs · 20,228 cycles

CREW REPORTED WHILE SELECTING FLAPS 45 DEGREES, FLAPS DID NOT MOVE, NO FAULTS SHOWN AND COMMAND BAR AT 45 DEGREES. REMOVED FLAP SELECTOR HANDLE AND INSTALLED SERVICEABLE HANDLE, OPERATIONAL CHECK GOOD.

Part: TRANSDUCER — MALFUNCTIONED (AOA) · airframe 13,279 hrs · 19,955 cycles

LEFT AOA C/B POPS. REPLACED LEFT AOA TRANSDUCER WITH SERVICEABLE UNIT. OPS CHECK GOOD. P/N C-81817-1, S/N ON 733, S/N OFF 898.

Part: CIRCUIT BREAKER — TRIPPED (TRIM WARNING) · airframe 13,182 hrs · 19,807 cycles

ON TAKEOFF ROLL AURAL TRIM SOUNDED WITH TRIM WITHIN GREEN. ABORTED TAKEOFF. RESET AURAL WARN CB (H8). OPS CHECK GOOD ON GROUND.

Part: CLIP — CRACKED (FUSELAGE) · airframe 12,106 hrs · 18,156 cycles

SKIN CLIP CRACKED AT FRAME 9, BELOW RIGHT DV WINDOW. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED RIGHT FRAME 9 IAW SB 120-53-0073.

Part: CLIP — CRACKED (RT WING) · airframe 12,106 hrs · 18,156 cycles

FOUR CRACKED SKIN SUPPORT CLIPS ON RT WING, RIB 15 LOWER SURFACE. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED FOUR SKIN SUPPORT CLIPS ON RIGHT WING, RIB 15 LOWER SURFACE PER SRM 51-40-02 AND RII 57-301.

Part: CLIP — CRACKED (FUSELAGE) · airframe 12,106 hrs · 18,156 cycles

SKIN CLIP CRACKED AT FRAME 9, BELOW LEFT DV WINDOW. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED LEFT FRAME 9 IAW SB 120-53-0073.

Part: BRACKET — CRACKED (LT WINDOW) · airframe 12,106 hrs · 18,156 cycles

BRACKET CRACKED AFT OF LEFT DV WINDOW. REMOVED AND REPLACED SUPPORT BRACKET AFT MIDDLE OF DV WINDOW REF SRM 51-10-02 & 51-40-00 EMB SRM.

Part: BALLAST — BURNED OUT (LAVATORY) · airframe 11,083 hrs · 16,583 cycles

THERE WAS AN ODOR OF SMOKE IN THE CARGO AREA AND IN THE AFT CABIN. THE SMOKE DETECTOR IN THE LAVATORY WENT OFF WHILE BOARDING PASSENGERS. INVESTIGATED AFT CABIN, FOUND LIGHT IN LAVATORY BALLAST BURNED OUT AND RELEASED SMOKE INTO AFT CABIN AND LAV. REPLACED BALLAST OF LAV LIGHT, OPS CHECK GOOD.

Part: BRACKET — CRACKED (RIGHT TE FLAP) · airframe 10,938 hrs · 16,375 cycles

FOUND CRACK IN INBOARD RIGHT FLAP ROLLER BRACKET. INSTALLED NEW BRACKET AND ROLLER ASSEMBLY IAW 54-20-00. ALL CHECKS OK.

Part: CONTROL HEAD — MALFUNCTIONED (TRANSPONDER) · airframe 9,880 hrs · 14,772 cycles

AFTER TAKEOFF, ATC REPORTS NO TRANSPONDER REPORTING. TRIED BOTH ONE AND TWO TRANSPONDERS, NEITHER WORKED. RETURNED TO LAX. REPLACED TRANSPONDER CONTROL HEAD. TESTED WITH TEST BOX. OPS CHECKS GOOD.

Part: ODOR — DETECTED (COCKPIT) · airframe 9,340 hrs · 13,905 cycles

DURING CRUISE A STRONG ELECTRICAL ODOR IN THE COCKPIT LASTED 1 MINUTE. NO ABNORMAL INDICATIONS ON GAUGES OR ELECTRICAL PANEL. LOWERED AND INSPECTED OVERHEAD AND CIRCUIT BREAKER PANELS. REMOVED PILOT AND COPILOT SIDE CONSOLE PANELS, INSPECTED FOR SIGN OF OVERHEATED AND BURNED WIRES AND ELECTRICAL COMPONENTS. NO DISCREPANCIES NOTED.

Part: CONNECTOR — BURNED (GALLEY) · airframe 8,568 hrs · 12,709 cycles

UPON DESCENT F/A'S GALLEY ELECTRICAL PANEL LOST LIGHTING, FUNCTIONING AND WAS HOT TO THE TOUCH. ALL 3 CREW MEMBERS SMELLED SMOKE, BUT NO VISUAL. FOUND CANNON PLUG ON COFFEE POT BURNED. REPLACED COFFEE POT, OPS CHECK GOOD.

Part: CONTROL CABLE — WORN (AILERON TAB) · airframe 8,171 hrs · 12,107 cycles

UPPER AND LOWER AILERON TRIM CABLES WORN ON RIGHT SIDE. REPLACED RIGHT UPPER AND LOWER AILERON TRIM CABLES IAW EMB120 MM 27-00-01.

Part: CONTROL CABLE — WORN (RUDDER) · airframe 8,171 hrs · 12,107 cycles

LEFT OUTBOARD RUDDER CABLE IN AFT RIGGING BAY IS WORN NEAR LIMITS. REPLACED LEFT OUTBOARD RUDDER AFT CABLE IAW EMB120 MM 27-00-01.

Part: CONTROL CABLE — WORN (RUDDER) · airframe 8,190 hrs · 12,137 cycles

RIGHT RUDDER AFT OUTBOARD CABLE WORN. REPLACED RIGHT AFT OUTBOARD RUDDER CABLE IAW EMB120 MM 27-00-01.

Part: CONTROL CABLE — WORN (AILERON) · airframe 8,171 hrs · 12,107 cycles

LEFT AILERON UPPER AND LOWER CABLES WORN ON WING. REPLACED LEFT UPPER AND LOWER AILERON CABLES IAW EMB120 MM 27-00-01.

Part: CONTROL CABLE — WORN (RUDDER) · airframe 8,171 hrs · 12,107 cycles

RIGHT RUDDER INBOARD AND OUTBOARD CABLES FORWARD OF THE WING BOX IS WORN NEAR LIMITS. REPLACED RIGHT RUDDER INBOARD AND OUTBOARD CABLES FORWARD OF WING BOX IAW EMB120 MM 27-00-01.

Part: CONTROL CABLE — WORN (RUDDER) · airframe 8,190 hrs · 12,137 cycles

RIGHT INBOARD RUDDER CABLE IN AFT RIGGING BAY IS WORN NEAR LIMITS. REPLACED RIGHT INBOARD AFT RUDDER CABLE IAW EMB120 MM 27-00-0.

Part: CONTROL CABLE — WORN (AILERON) · airframe 8,171 hrs · 12,107 cycles

UPPER AND LOWER AILERON CABLES WORN AT INBOARD NACELLE FAIRLEADS, RIGHT SIDE. REPLACED RIGHT UPPER AND LOWER AILERON CABLES IAW EMB120 MM 27-00-01.

Part: CONTROL CABLE — WORN (ELEVATOR) · airframe 8,190 hrs · 12,137 cycles

RIGHT INBOARD AND OUTBOARD ELEVATOR CABLES IN AFT RIG BAY ARE WORN NEAR LIMITS. REPLACED RIGHT INBOARD AND OUTBOARD AFT ELEVATOR CABLES IAW EMB120 MM 27-00-01.

Part: WIRE — DAMAGED (LT WING) · airframe 8,165 hrs · 12,099 cycles

VENT VALVE WIRING LINE INSIDE FUEL TANK NEAR LEFT WING TIP HAS DAMAGE. REPLACED LEFT VENT VALVE WIRING LINE ASSY.

Part: CONTROL CABLE — WORN (ELEVATOR) · airframe 8,190 hrs · 12,137 cycles

LEFT INBOARD AND OUTBOARD ELEVATOR CABLES IN AFT RIG BAY ARE WORN NEAR LIMITS. REPLACED LEFT INBOARD AND OUTBOARD AFT ELEVATOR CABLES IAW EMB120 MM 27-00-01. P/N: 120-27655-017.

Part: BLEED VALVE — MALFUNCTIONED (LT ENGINE) · airframe 3,875 hrs · 5,558 cycles

SMELLED SMOKE ON TAKEOFF. RETURNED TO LAX. REPLACED LEFT ENGINE HIGH PRESSURE BLEED VALVE. RAN ENGINE. OPS CHECK GOOD. P/N: 979626-4-1, S/N ON: 2461, S/N OFF: 2020.

Part: ANNUNCIATOR — FAULTY (COCKPIT) · airframe 6,977 hrs · 10,360 cycles

FLAP DISAGREEMENT LIGHT ILLUMINATES AFTER FLAP RETRACTION. RETURNED FLAP HANDLE TO 15 DEGREES SETTING AND THEN SELECTED FLAPS UP. AGAIN DISAGREEMENT LIGHT REMAINED ILLUMINATED. FLAP POSITION INDICATOR DISPLAYS APPROX 2 DEGREES. REPLACED FLAP ANNUNCIATOR UNIT. OPS CHECK GOOD. P/N 347100-1001, S/N ON 0157, OFF 0078.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 6,936 hrs · 10,298 cycles

FIRST THREE ROWS OF EMERGENCY LIGHTS DO NOT ILLUMINATE. ALSO FORWARD EXIT SIGNS DO NOT ILLUMINATE. REPLACED FORWARD (NR 1) EMERGENCY LIGHT BATTERY PACK. GROUND CHECK NORMAL. P/N D366-04-001, S/N ON 883, S/N OFF 397.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 6,628 hrs · 9,833 cycles

LIGHT INSPECTION LEFT SIDE DOES NOT ILLUMINATE. ICING CONDITIONS EXIST AT DESTINATION. RETURNED TO LAX. REPLACED LEFT DEICE INSPECTION LIGHT BULB. OPS CHECK GOOD.

Part: TRANSPONDER — INOPERATIVE (ATC SYSTEM) · airframe 4,305 hrs · 6,495 cycles

NUMBER ONE AND NUMBER TWO TRANSPONDER INOP. RETURNED TO LAX. PERFORMED OPERATIONAL CHECK ON ATC TRANSPONDER ONE AND TWO, FOUND NO PROBLEMS OR CODES. OPS CHECKS GOOD.

Part: FUEL FILTER — CLOGGED (FUEL SYSTEM) · airframe 4,264 hrs · 6,444 cycles

LEFT FUEL FILTER ILLUMINATED. RETURNED TO SFO. REPLACED HIGH AND LOW FUEL FILTER, OPS AND LEAK CHECK GOOD.

Part: ANNUNCIATOR — MALFUNCTIONED (TE FLAP)

AT CRUISE, FLAP AND ADVANCED SWS MAP LIGHT ILLUMINATED WITH CONTROL FAULT LIGHT ON FLAP PANEL. UNABLE TO RESET. RETURNED TO LAX. REPLACED FLAP ANNUNICATOR, OPS CHECKS GOOD.