N566SW

Part: BLADE — CRACKED (PROPELLER)

DURING MAJOR INSPECTION, FOUND FPI CRACK INDICATION IN FILLET RADIUS OF BLADE SHANK.

Part: SOCKET — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,106 hrs · 48,048 cycles

RED EMERGENCY LIGHTS ARE INOPERATIVE NEAR THE CABIN MAIN ENTRY DOOR. R & R THE LIGHT SOCKET ASSY AND REPAIRED WIRING, OPS CHECKED GOOD, IAW AMM AND WDM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,548 hrs · 47,312 cycles

NR 4 FLOOR WHITE EMERGENCY LIGHT STRIP INOPERATIVE. REPLACED THE LAMP IN NR 4 FLOOR WHITE EMERGENCY LIGHT STRIP IAW AMM.

Part: SKIN — GOUGED (FUSELAGE) · airframe 33,383 hrs · 47,095 cycles

GOUGE APPROXIMATELY 3.5 INCHES LONG, .2500 INCHES WIDE, .0625 INCHES DEEP ON AFT FUSELAGE AT CARGO DOOR, WITHIN .2500 INCHES OF RIVETS BETWEEN SKIN EDGE AND RIVET ROW. OUT OF LIMITS IAW SRM. REMOVED DAMAGE SECTION AND INSTALLED DOUBLER ON EXTERNAL SKIN AFT OF CARGO DOOR CUT OUT SURROUNDING IAW ETD.

Part: PROPELLER — OVERSPEED (RIGHT) · airframe 33,364 hrs · 47,075 cycles

RIGHT PROPELLER SPEED WENT TO 103.7 PERCENT RPM. CHANGED PCU AND TRANSFER TUBE. OPS CHECK GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY · airframe 32,944 hrs · 46,499 cycles

OXYGEN MASK DEPLOYED DURING FLIGHT. RESTOWED.

Part: SUPPORT — CRACKED (LT NACELLE) · airframe 31,919 hrs · 45,062 cycles

LT NACELLE FLAP INBD INTERIOR VERTICAL SUPPORT CRACKED. C-CHECK REPLACED LT NACELLE FLAP INTERIOR VERTICAL SUPPORT IAW SRM.

Part: FITTING — CRACKED (RT WING) · airframe 31,919 hrs · 45,062 cycles

RT WING LOWER SMALL CLIP CRACKED AT RIB 15 2ND FROM FWD. C-CHECK REPLACED RT WING LOWER SMALL CLIP AT RIB 15, 2ND FROM FWD IAW SRM.

Part: FITTING — CRACKED (RT WING) · airframe 31,919 hrs · 45,062 cycles

RT WING UPPER CLIP CRACKED 2ND FROM FWD AT RIB 20. C-CHECK REPLACED UPPER WING CLIP AT RT WING 2ND FROM FWD AT RIB 20, IAW SRM.

Part: SUPPORT FITTING — CRACKED (LT WING) · airframe 31,919 hrs · 45,062 cycles

LT OTBD WING HAS ONE CRACKED UPPER SKIN SUPPORT CLIP AT STATION 20A. C-CHECK REPLACED LT OTBD WING ONE CRACKED UPPER SKIN SUPPORT CLIP AT WING STATION 20A IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,919 hrs · 45,062 cycles

EMERGENCY LIGHT AT PASSENGER ENTRYWAY IS BURNED OUT. FLT#6338 RELAMPED.

Part: CAP — LOOSE (CABIN) · airframe 31,919 hrs · 45,062 cycles

FLOOR EMERGENCY LIGHTS FAILED. FLT#6023 REINSTALLED LOOSE FUSE CAP.

Part: PCU — FAILED (RUDDER) · airframe 31,636 hrs · 44,690 cycles

ON TAXI OUT AIRCRAFT PERFORMED AN UNCOMMANDED RT TURN. DURING TAKEOFF ROLL WARNING LIGHT ON MAP FLASHED A COUPLE OF TIMES & THE AIRCRAFT JERKED TO THE RT TWO TIMES, AFTER TAKEOFF AIRCRAFT JERKED TO THE RT TWICE AGAIN. FLT#6264 REPLACED RUDDER PCU & ADJUSTED ALL GCU`S IAW AMM. PN: 321100-1003 SN ON: 0010A SN OFF: 0336

Part: SOCKET — FAILED (CABIN) · airframe 31,597 hrs · 44,635 cycles

EMERGENCY FLOOR LEVEL LIGHTING SYSTEM HAS FIVE LIGHTS NOT WORKING. REPLACED 1 MOLEX SOCKET AT MID STRIP PLUG & REPLACED SOCKET AT MID STRIP.

Part: SIGN — MISSING (CABIN) · airframe 31,093 hrs · 43,915 cycles

LOWER LEFT SIDE OF THE EMERGENCY EXIT SIGN ON ROW 6 IS MISSING. (FLT 6327) REPLACED LOWER LEFT SIDE OF EMERGENCY EXIT SIGN AT ROW 6A.

Part: SIGN — DETACHED (CABIN) · airframe 30,976 hrs · 43,751 cycles

EMERGENCY EXIT SIGN AT ROW 6 FELL. (FLT 5488) REPLACED 6C LOWER EMERGENCY EXIT SIGN LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,761 hrs · 43,437 cycles

CABIN FLOOR EMERGENCY LIGHT BURNED OUT NEAR ROW 3. (FLT 6268) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,606 hrs · 43,221 cycles

FLOOD LIGHT OVER SEAT 6A DOES NOT ILLUMINATE. (SERVICE) RELAMPED FLOOD LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,606 hrs · 43,221 cycles

ONE WHITE EMERGENCY TRACK LIGHT DOES NOT ILLUMINATE. (FLT 5401) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,456 hrs · 43,020 cycles

EMERGENCY FLOOR LEVEL LIGHT ROW 8A IS BURNED OUT. (FLT 5647) RELAMPED EMERGENCY LIGHT.

Part: WIRE — BROKEN (CABIN) · airframe 30,393 hrs · 42,938 cycles

AFT FOUR FLOOR EMERGENCY LIGHTS INOPERATIVE. (FLT 5632) REPAIRED BROKEN WIRE ON AFT RED FLOOR LEVEL LIGHT AND REPLACED FUSE.

Part: LIGHT — DETACHED (CABIN) · airframe 30,151 hrs · 42,609 cycles

ROW 5 FLOOR EMERGENCY WHITE LIGHT FOUND DETACHED AN UNCOVERED FROM SOCKETS. (FLT 5816) RE-ATTACHED FLOOR EMERGENCY WHITE LIGHT IAW AMM.

Part: HANDLE — LACK OF LUBE (CABIN DOOR) · airframe 30,102 hrs · 42,539 cycles

MAIN CABIN DOOR HARD TO OPEN AND CLOSE. (FLT 5405) LUBRICATED HANDLE ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,102 hrs · 42,539 cycles

EMERGENCY FLOOR LIGHT AT ROW 5 IS OUT. (FLT 5339) RELAMPED EMERGENCY LIGHT.

Part: WIRE — DAMAGED (CABIN) · airframe 30,102 hrs · 42,539 cycles

TWO RED FLOOR EMERGENCY LIGHTS AT ROW 9 FAIL TO ILLUMINATE. (FLT 5538) REPAIRED WIRE FOR FLOOR EMERGENCY EXIT IN REFERENCE TO EMB 120-WDM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,820 hrs · 42,140 cycles

FLOOR EMERGENCY LIGHT AT 5A IS INOPERATIVE. (SERVICE) REPLACED LIGHT FIXTURE FOR EMERGENCY LIGHT AT ROW 5 IN REFERENCE TO EMB 120 MM.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 29,365 hrs · 41,504 cycles

FLOOR EMERGENCY STRIP AT ROW 5 HAS ONE WHITE LIGHT OUT. (SERVICE) SPLICED BROKEN WIRE AT ROW 5 FLOOR STRIP EMERGENCY LIGHTS.

Part: SOCKET — BROKEN (CABIN) · airframe 29,365 hrs · 41,504 cycles

EMERGENCY LIGHT ON FLOOR AT 11A IS BROKEN. (FLT 6332) REPLACED AFT FLOOR STRIP EMERGENCY LIGHTING SOCKET ASSEMBLY IN REFERENCE TO M/M.

Part: LINKAGE — LACK OF LUBE (CABIN DOOR) · airframe 29,313 hrs · 41,432 cycles

CABIN DOOR DIFFICULT TO PUSH OPEN. (FLT 5614) LUBRICATED LINKAGES THROUGHOUT CABIN DOOR OPENING AND LOCKING MECHANISMS.

Part: SHOULDER BELT — FRAYED (COCKPIT) · airframe 29,313 hrs · 41,432 cycles

F/A'S SHOULDER HARNESS IS FRAYED AND IS DIFFICULT TO TAKE ON AND OFF. (FLT 5614) REPLACED F/A'S SEAT BELT HARNESS IN REFERENCE TO AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,313 hrs · 41,432 cycles

FLOOR LEVEL EMERGENCY LIGHTS AT 8A ARE INOPERATIVE. (FLT 5473) RELAMPED EMERGENCY LIGHTS.

Part: WIRE — BROKEN (CABIN) · airframe 29,127 hrs · 41,167 cycles

ONE FLOOR EMERGENCY LIGHT AT 3A IS OUT. (FLT 6282) REPAIRED BROKEN WIRE AT FLOOR ESCAPE EMERGENCY LIGHT AT 3A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,001 hrs · 40,973 cycles

FLOOR EMERGENCY LIGHT AT 3A IS OUT. (FLT 5529) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,910 hrs · 40,848 cycles

FLOOR EMERGENCY LIGHT AT ROW 10 IS OUT. (FLT 6232) RELAMPED EMERGENCY LIGHT.

Part: WIRE — DAMAGED (CABIN) · airframe 28,555 hrs · 40,361 cycles

FLOOR EMERGENCY LIGHT AT 7A IS OUT. (FLT 5403) REPAIRED FLOOR EMERGENCY LIGHT WIRE AT 7A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,442 hrs · 40,225 cycles

THE 7A FLOOR EMERGENCY LIGHT IS OUT. (FLT 6379) RELAMPED EMERGENCY LIGHT.

Part: WIRE — BROKEN (CABIN) · airframe 28,381 hrs · 40,142 cycles

A WHITE FLOOR LEVEL EMERGENCY LIGHT AT 3A IS OUT. (FLT 5610) REPAIRED FLOOR LEVEL EMERGENCY LIGHT WIRING.

Part: CONTROL VALVE — MALFUNCTIONED (BRAKE SYSTEM) · airframe 28,378 hrs · 40,137 cycles

LEFT BRAKE LOCKED UP DURING TAXI. (FLT 6352) REPLACE INBOARD BRAKE CONTROL VALVE. P/N: 39-651-2 S/N OFF: 506

Part: PIVOT — LACK OF LUBE (PAX DOOR) · airframe 28,042 hrs · 39,654 cycles

PAX DOOR DIFFICULT TO OPEN. (FLT 5326) LUBRICATED MCD HANDLE PIVOT POINT AND DOOR ROLLERS.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 27,981 hrs · 39,554 cycles

MAIN CABIN DOOR IS HARD TO OPEN. (FLT 6327) LUBED PAX DOOR LOCK ROLLERS ON FUSELAGE AT LOCK MECHANISM IN DOOR.

Part: FUSE — BLOWN (CABIN) · airframe 27,906 hrs · 39,452 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5343) REPLACED NR 1 EMERGENCY LIGHT FUSE.

Part: COMPUTER — FAILED (AHRS) · airframe 27,530 hrs · 38,923 cycles

AUTO PILOT DISCONNECTED WITH RED MSG ON AP CONTROL PANEL. DISPLAY MSG ON MAP AND PITCH AND ROLL FLAGS ON EFIS DISPLAY ON BOTH SIDES. CAPT AND FO EFIS SCREENS NOT WORKING CORRECTLY. (FLT 5409) REPLACED NR 1 AND NR 2 AHRS COMPUTERS AND NR 2 DPU / (LT) P/N 622-6190-204 S/N OFF 2643 / (RT) P/N 622-6190-204 S/N OFF 2620 / P/N 622-7711-003 S/N OFF 7002.

Part: SHIM — OUT OF ADJUST (CABIN DOOR) · airframe 27,267 hrs · 38,570 cycles

MAIN CABIN DOOR HARD TO OPEN. (FLT 6310) ADJUSTED FORWARD UPPER SHIM STACK ON MAIN CABIN DOOR.

Part: WIRE — BROKEN (CABIN) · airframe 27,092 hrs · 38,328 cycles

FLOOR LEVEL EMERGENCY LIGHT AT ROW 4 IS OUT. (FLT 6263) REPAIRED BROKEN WIRE AT FLOOR LEVEL EMERGENCY LIGHT NEAR ROW 4.

Part: LIGHT — UNSECURE (CABIN) · airframe 27,092 hrs · 38,328 cycles

FLOOR LEVEL EMERGENCY LIGHT AT ROW 6 IS OUT. (FLT 6263) RE-SECURED EMERGENCY LIGHT.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 26,919 hrs · 38,083 cycles

MAIN CABIN DOOR IS HARD TO OPEN. (FLT 6358) LUBED MAIN CABIN DOOR ROLLERS.

Part: WIRE — BROKEN (CABIN) · airframe 26,862 hrs · 37,995 cycles

FLOOR EMERGENCY LIGHT NEAR ROW 4 IS OUT. (FLT 6307) REPAIRED BROKEN WIRE AT FLOOR EMERGENCY LIGHT NEAR ROW 4.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,588 hrs · 37,603 cycles

RED EMERGENCY FLOOR LIGHT AT ROW 6 IS OUT. (FLT 6711) RELAMPED EMERGENCY LIGHT.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 26,082 hrs · 36,890 cycles

F/A COULD NOT OPEN CABIN DOOR. HAD TO RELIEVE PRESSURE TO GET DOOR OPEN. (FLT 6677) REPLACED ELECTRONIC ALTITUDE CONTROLLER.

Part: HINGE — OUT OF RIG (PAX DOOR) · airframe 25,806 hrs · 36,520 cycles

MAIN CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. (FLT 6305) ADJUSTED PAX DOOR RIGGING AT AFT HINGE ARM AND LUBRICATED MECHANISM.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 25,490 hrs · 36,069 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6269) LUBRICATED MAIN CABIN DOOR.

Part: STRINGER — CRACKED (LT WING) · airframe 25,631 hrs · 36,271 cycles

LEFT INBOARD WING STRINGER NR 10 CRACKED BETWEEN RIB 5 AND 5B, MARKED. (C-CHECK) REPAIRED LEFT INBOARD WING STRINGER 10 AT RIB 5 PER SRM.

Part: STRINGER — CRACKED (RT WING) · airframe 25,631 hrs · 36,271 cycles

RIGHT INBOARD WING STRINGER 10 CRACKED AT 1ST ACCESS PANEL INBOARD OF NACELLE. (C-CHECK) REPAIRED STRINGER PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,884 hrs · 35,174 cycles

EMERGENCY RED FLOOR LIGHT INOP AT ROW 6. (FLT 6139) RE-INSTALLED RED LIGHT COVER.

Part: TRIM PANEL — OUT OF POSITION (CABIN) · airframe 24,810 hrs · 35,062 cycles

ONE RED EMERGENCY LIGHT ON THE FLOOR AT 6A INOP. (FLT 6279) REPOSITIONED TRIM IN FLOOR TRACK LIGHTING.

Part: LIGHT — NOT SEATED (CABIN) · airframe 24,727 hrs · 34,930 cycles

RED LIGHT ON FLOOR EMERGENCY STRIP AT ROW 6 INOP. (FLT 6149) RESEATED LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,578 hrs · 34,718 cycles

ONE FLOOR LEVEL RED EMERGENCY LIGHT INOP AT MAIN CABIN DOOR AND ROW 6. (FLT 6281) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,396 hrs · 34,459 cycles

WHITE FLOOR LEVEL EMERGENCY LIGHT NEAR ROW 5 INOP. (FLT 6199) REPLACED LIGHT FIXTURE.

Part: LENS — OUT OF POSITION (CABIN) · airframe 23,421 hrs · 33,041 cycles

EXIT ROW 6 EMERGENCY LIGHT LENS FELL OFF. (FLT 6246) REPLACED LIGHT ASSEMBLY.

Part: TIRE — BLOWN (NR 2) · airframe 23,133 hrs · 32,633 cycles

NR 2 TIRE BLEW ON LANDING. (FLT 7809) REPLACED TIRES.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 21,940 hrs · 31,085 cycles

C-CHECK, LEFT FRAME WEB CRACKED, AFT OF CENTER DV WINDOW FRAME. REPAIRED PER SRM.

Part: AILERON — MALFUNCTIONED · airframe 20,904 hrs · 29,742 cycles

FLT 5721 - THERE IS A SLIGHT BIND WHEN THE AILERONS ARE MOVED LEFT TO RIGHT. INSPECTED AILERON CABLES, FITTINGS AND PULLEYS IAW MM 27-11-00. COULD NOT DUPLICATE THE DISCREPENCY. AILERONS CHECK GOOD.

Part: BRAKE ASSY — MALFUNCTIONED (MLG) · airframe 20,742 hrs · 29,529 cycles

FLT 5751 - POWER LEVERS WOULD NOT GO INTO REVERSE ALONG WITH A MOMENTARY LOSS OF BRAKING FORCE. SERVICED RIGHT STRUT AND INSPECTED AND CLEANED MAIN LANDING GEAR PROX SWITCH AND HARNESS. BLED BRAKE SYSTEM. ALL OPS CHECKS GOOD.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 20,563 hrs · 29,287 cycles

FLT 3738 - LAV SMOKE DETECTOR INOP. REPLACED LAV SMOKE DETECTOR ASSEMBLY. OPS CHECKS GOOD AT THIS TIME, PN FAV751A-4, SN/OFF 041532.

Part: DOOR — BINDING (MAIN PAX) · airframe 19,259 hrs · 27,576 cycles

MAIN CABIN DOOR IS DIFFICULT TO OPEN, FLIGHT NR 5553. CLEANED AND LUBED MAIN CABIN DOOR. OPS CHECK GOOD.

Part: LIGHT — BROKEN (EMERGENCY EXIT) · airframe 19,064 hrs · 27,317 cycles

EMERGENCY EXIT LIGHT AT ROW 6 IS BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. OPS CHECK GOOD.

Part: RIB — CRACKED (LT NACELLE) · airframe 18,307 hrs · 26,281 cycles

LEFT MLG MID COWL FIRST RIB AFT OF DOOR FRAME CRACKED AT STRINGER CUT OUT, DISCOVERED DURING C-CHECK INSPECTION. REPAIRED RIB IAW SRM 51-70-05 AND RII 54-900-1000.

Part: MOUNT — CRACKED (RT NACELLE) · airframe 18,307 hrs · 26,281 cycles

RIGHT NACELLE DECK AT OUTBOARD AFT TAIL PIPE MOUNT CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ON RIGHT NACELLE DECK AT OUTBOARD AFT TAIL PIPE MOUNT PER SRM 54-20-01 AND RII 54-900-1000 AND SRM 51-40-02 .

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,307 hrs · 26,281 cycles

SEAT TRACK FOR SEAT 11A HAS CORROSION AT SEAT, DISCOVERED DURING C-CHECK INSPECTION. REPLACED FLOOR SEAT TRACK AT SEAT 11A PER EMBRAER APPROVED REPAIR NO EST 186/96.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,210 hrs · 24,880 cycles

EMERGENCY LIGHT INOP OVER SEAT 9C. REPLACED BULB. OPERATIONAL CHECKS GOOD.

Part: TRIM SYSTEM — OUT OF RIG (ELEVATOR) · airframe 16,633 hrs · 24,007 cycles

TRIM AURAL WARNING GOES OFF WITH TRIM IN THE GREEN BAND UP TO THE 15% INDICATOR. ADJUSTED ELEVATOR TRIM WHEEL, ADJUSTED RT ELEVATOR TRIM TAB AND ADJUSTED LT AND RT ELEVATOR TRIM PROX SENSORS IAW EMB 120 MM 27-32-00. OPERATIONAL CHECK GOOD.

Part: TORQUE TUBE — BINDING (PAX DOOR) · airframe 15,914 hrs · 23,108 cycles

FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. REPLACED INTERMEDIATE TORQUE TUBE AND BUSHING ON MAIN CABIN DOOR IAW AMM 52-11-00. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 15,263 hrs · 22,284 cycles

FLAP DISAGREEMENT ON INBOARD PAIR WHEN RETRACTING FLAPS. REPLACED LEFT INBOARD FLAP ACTUATOR IAW MM 27-50-07. OPERATIONAL CHECK GOOD.

Part: FRAME — CRACKED (COCKPIT) · airframe 15,256 hrs · 22,277 cycles

LT COCKPIT FLOOR PROP CRACKED AT FRAME 13, ITEM FOUND AT C-CHECK INSPECTION. REMOVED LT COCKPIT FRAME 13 AND REPAIRED PER SRM 53-10-10, MM 51-22-00, 51-30-01.

Part: SELECTOR — MALFUNCTIONED (TE FLAP) · airframe 14,386 hrs · 21,079 cycles

FLAPS DO NOT COME DOWN. REMOVED AND REPLACED FLAP SELECTOR LEVER ASSY WITH SERVICEABLE UNIT REF NR 27-50-00. OPERATIONAL CHECK GOOD.

Part: ODOR — DETECTED (GALLEY) · airframe 12,902 hrs · 19,195 cycles

ELECTRIC BURNING ODOR COMING FROM GALLEY. INSPECTED COFFEE POT PLUGS. SERVICED AND INSTALLED JUGS COULD NOT DUPLICATE. OPS CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,796 hrs · 19,036 cycles

FLOOR EMERGENCY LAMP OUT AT 8A. REMOVED AND REPLACED FLOOR EMERGENCY LIGHT AT SEAT 8A. CHECKS GOOD IAW 33-50-00.

Part: PROCESSOR — MALFUNCTIONED (NR 2 TCAS) · airframe 12,314 hrs · 18,334 cycles

IN FLIGHT THE AP FAILED ON THE F/O'S SIDE, FOLLOWED BY A FLIGHT DIRECTOR FLAG ON THE F/O SIDE. THE 1 AMP CB ON AHRS 2 WAS POPPED. REPLACED AND SECURED TCAS PROCESSOR. OPS CHECKED OPERATION OF AUTOPILOT SYSTEM ON GROUND. ALL CHECKS GOOD AND CB'S REMAINED SET.

Part: BRACKET — CRACKED (RT HYD BAY) · airframe 11,785 hrs · 17,566 cycles

RIGHT HYD BAY CROSS BRACKET CRACKED AT INBOARD SIDE OUT OF LIMITS. DISCOVERED DURING C-CHECK. REMOVED AND REPLACED RIGHT HYD BAY CROSS BRACKET IAW SRM 51-10-02 & 51-40-00.

Part: CLIP — CRACKED (FUSELAGE) · airframe 11,785 hrs · 17,566 cycles

LEFT SKIN SUPPORT CLIP CRACKED AT FRAME 12, BEHIND DV WINDOW. DISCOVERED DURING C-CHECK. REMOVED AND REPLACED LEFT SKIN SUPPORT CLIP AT FRAME 12 BEHIND DV WINDOW WITH A SERVICEABLE UNIT IAW SRM 51-10-02, 51-40-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 11,785 hrs · 17,566 cycles

RIGHT FRAME 9 CLIP UNDER DV WINDOW CRACKED. DISCOVERED DURING C-CHECK. REPAIRED FRAME 9 RIGHT SIDE PER SERVICE BULLETIN 120-53-007 REV 00 DATED 21 JUL 99.

Part: FRAME — CRACKED (FUSELAGE) · airframe 11,785 hrs · 17,566 cycles

LEFT FRAME 9 CLIP UNDER DV WINDOW CRACKED. DISCOVERED DURING C-CHECK. REPAIRED FRAME 9 LEFT SIDE PER SERVICE BULLETIN 120-53-0073 REV 00 DATED 21 JUL 99.

Part: SERVO — MALFUNCTIONED (AUTOPILOT) · airframe 11,737 hrs · 17,482 cycles

ELECTRIC TRIM FAILED ON BOTH SIDES. INSTALLED A SERVICEABLE SERVO IAW 27-00-06 AND OPS CHECK GOOD. P/N ON 622-5734-002, S/N ON 7105 OFF 5806.

Part: ACTUATOR — MALFUNCTIONED (MLG DOOR) · airframe 11,719 hrs · 17,456 cycles

LEFT MAIN LANDING GEAR WOULD NOT RETRACT ON DEPARTURE.ADJUSTED LEFT MAIN LANDING GEAR INBOARD DOOR ACTUATOR. OPS CHECKS GOOD..

Part: LANDING GEAR — MALFUNCTIONED (LEFT) · airframe 11,604 hrs · 17,268 cycles

LEFT LANDING GEARS A AND B RED AND A AND B GREEN REMAINED ILLUMINATED AFTER LANDING GEAR LEVER WAS RETRACTED. ALSO FELT VIBRATION COMING FROM LEFT SIDE OF AIRCRAFT. ALL LIGHTS NORMAL WHEN LEVER WAS IN DOWN POSITION. PERFORMED SEVERAL GEAR SWINGS WITH NO PROBLEMS FOUND. ALL WORK PERFORMED IAW EMB MM CHAPTER 32. UNABLE TO DUPLICATE DISCREPANCY.

Part: SEQUENCE VALVE — FAILED (LT MLG DOOR) · airframe 11,012 hrs · 16,368 cycles

ON DEPARTURE ON GEAR RETRACTION LEFT GEAR WOULDN`T COME UP ON FIRST ATTEMPT WITH BOTH LT AND RT A AND B RED INDICTAION LIGHT ON BOTH A AND B GREEN LIGHT ON. LEFT GEAR DOOR DID NOT APPEAR TO OPEN. CYCLED GEAR AND GEAR RETRACTED. ADJUSTED LEFT GEAR INBOARD DOOR SEQUENCE VALVE. OPERATED LANDING GEAR. OPS CHECK GOOD.

Part: SEQUENCE VALVE — LACK OF LUBE (MLG DOOR) · airframe 10,987 hrs · 16,330 cycles

LEFT MAIN GEAR REQUIRED THREE ATTEMPTS BEFORE RETRACTING. IT APPEARED THAT THE INBOARD GEAR DOOR WAS NOT OPENING. CYCLED LANDING GEAR NUMEROUS TIMES WITHOUT DEFECT. CLEANED AND LUBRICATED SEQUENCE VALVE AND PLUNGERS ON ALL GEAR. OPS CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 10,554 hrs · 15,649 cycles

CENTER EMERGENCY LIGHTS DO NOT TURN ON. FOUND BROKEN WIRE ON EMERGENCY LIGHT FLOOR TRACK. REPAIRED BROKEN WIRE IAW EMB120 WM 20-00-00. OPS CHECK GOOD.

Part: STRUCTURE — CRACKED (LT TE FLAP) · airframe 10,511 hrs · 15,583 cycles

FOUND LEFT INBOARD FLAP INBOARD BUTTE DOOR CRACKED. REMOVED AND REPLACED LEFT INBOARD FLAP INBOARD BUTTE DOOR BEARING BRACKET WITH NEW BRACKET IAW EMB120 MM 20-10-01. P/N: 120-22883-001.

Part: ACTUATOR — FROZEN (ELEVATOR TRIM) · airframe 10,195 hrs · 15,090 cycles

AT 16,000 IN ICING CONDITIONS THE ELEVATOR TRIM JAMMED IN MANUAL MODE. ELECTRIC TRIM WORKED NORMALLY AFTER LEAVING ICING CONDITIONS. REMOVED AND REPLACED RIGHT AND LEFT ELEVATOR TRIM ACTUATORS IAW EMB MM 27-32-02. OPS CHECK GOOD.

Part: PROXIMITY SWITCH — MALFUNCTIONED (LT MLG) · airframe 9,920 hrs · 14,667 cycles

AFTER TAKEOFF, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION WHEN SELECTED. HAD TO SELECT DOWNLOCK RELEASE TO SELECT GEAR HANDLE TO THE UP POSITION. REPLACED LT LANDING GEAR PROXIMITY SWITCH PER EMB 120 32-41-01. OPS CHECK GOOD.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 9,761 hrs · 14,411 cycles

CARGO DOOR ILLUMINATED WITH SUBSEQUENT DOOR AURAL WARNING DURING TAKEOFF. ABORTED TAKEOFF. ADJUSTED FORWARD MICROSWITCH AND TARGET. OPS CHECK GOOD IAW MM 52-72-03.

Part: COMPUTER — MALFUNCTIONED (E/E BAY) · airframe 8,315 hrs · 12,154 cycles

CAPTAIN'S SIDE RMI FLAG, FIRST OFFICER'S FD FLAG, NR 2 AHARS 26 VAC CB POPPED. REPLACED TCAS PROCESSOR WITH SERVICEABLE UNIT. ALSO REPLACED NR 1 INVERTER WITH SERVICEABLE UNIT. ALL CIRCUIT BREAKERS REMAINED SET THROUGH ALL SYSTEM OPERATIONAL CHECKS.

Part: HANDLE — STUCK (MLG) · airframe 7,468 hrs · 10,882 cycles

GEAR HANDLE WOULD NOT GO TO UP POSITION AFTER TAKEOFF. USED DOWNLOCK RELEASE TO RAISE GEAR. INSPECTED LANDING GEAR FOR DEFECTS; NONE NOTED. INSPECTED AIR GROUND SWITCHES AND HARNESS. ALL FOUND GOOD. PERFORMED SEVERAL GEAR SWINGS. ALL CHECKS FOUND GOOD.

Part: SIGN — BROKEN (CABIN) · airframe 4,024 hrs · 5,748 cycles

6BC EMERGENCY EXIT LIGHT SIGN BROKEN. REPLACED AND SECURED EMERGENCY EXIT SIGN AT 6BC. OPS CHECK GOOD. PN 10-1301-15.

Part: PROXIMITY SENSOR — FAULTY (ELEVATOR TRIM) · airframe 6,554 hrs · 9,553 cycles

TAKEOFF AURAL WARNING FOR TRIM WHEN POWER LEVERS ARE ADVANCED NO MATTER WHERE TRIM IS SET IN GREEN ARC. REMOVED AND REPLACED RIGHT ELEVATOR TRIM PROXIMITY SENSOR. OPS CHECK GOOD IAW 27-32-05.

Part: ARM — OUT OF ADJ (FUEL DOOR) · airframe 5,724 hrs · 8,355 cycles

ON TAKEOFF ROLL APPROXIMATELY 80 KNOTS ''DOOR'' LIGHT ILLUMINATED. ABORTED TAKEOFF. ADJUSTED OUTBOARD FUEL DOOR MICROSWITCH ARM. OPS CHECK GOOD.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 5,647 hrs · 8,236 cycles

WHILE ON AUTOPILOT WITH FMS COUPLED DURING DESCENT AIRCRAFT BEGAN AN UNCOMMANDED RIGHT TURN OF 25 DEGREES BANK. DISCONNECTION OF AUTOPILOT RESULTED IN SIGNIFICANT UNCOMMANDED YAW REQUIRING UNUSUAL AMOUNTS OF LEFT RUDDER AND AILERON CONTROL PRESSURES CONDITIONS SUBSIDED AFTER ABOUT ONE MINUTE. REMAINDER OF FLIGHT NORMAL WITHOUT USE OF AP-YAW. LAX MX- AUTOPILOT DEFERRED DUE TO ABOVE DISCREPENCY. INSPECTED AUTOPILOT CONTROL SYSTEM IAW EMB MM 22-10-00 ALL FOUND GOOD INCLUDING ALL FUNCTIONAL CHECKS. ALSO INSPECTED RUDDER CONTROL SYSTEM IAW EMB MM 27-20-00 THROUGH 27-24-00. ALL FOUND GOOD INCLUDING ALL FUNCTIONAL CHECKS. DUE TO THE NATURE OF DISCREPANCY AUTOPILOT WILL BE DEFERRED PER MEL 22-11-1.

Part: REGULATOR — FAILED (DEICE SYSTEM)

RIGHT DUCT LEAK LIGHT ON IN FLIGHT. RETURNED TO LAX. REPLACED DE-ICE PRESS REGULATOR AND VENTURI TUBE ASSY. REMOVED ALL PANELS, CLEARED SENSORS, RAN ENGINE AND CHECKED FOR LEAKS, NONE FOUND. REINSTALLED ALL PANELS, RAN ENGINE AT FULL POWER FOR 15 MINUTES. OPS CHECK GOOD, PN ON: 3819668, SN: RF2264, SN OFF: RF1815 PRESS REG PN ON: 12050481001 VENTURI TUBE.

Part: ACTUATOR — MALFUNCTIONED (ELEVATOR)

TRIM WHEEL FROZE AT ALTITUDE, THROUGH DESCENT. REPLACED BOTH ELEVATOR TRIM ACTUATORS WITH SERVICEABLE UNITS IAW MM 273702.

Part: SEAL — MISSING (CARGO DOOR)

AT FLIGHT 240 EXPERIENCED RAPID DEPRESSURIZATION. RETURNED TO SFO. DISCOVERED PART OF CARGO DOOR SEAL MISSING. REPAIRED CARGO DOOR SEAL BOTTOM. CHECKED PRESSURE SYSTEM ON GROUND, OPS CHECKS GOOD.