N215SW

Part: HINGE — CRACKED (NACELLE FLAP) · airframe 34,710 hrs · 45,698 cycles

FLT 3677 - RIGHT NACELLE FLAP INBOARD HINGE IS CRACKED. REPLACED RIGHT NACELLE FLAP IAW 27-50-03. PN 120-34383-002.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 33,202 hrs · 43,857 cycles

EXIT SIGN LOCATED IN DOOR OF OVERHEAD BIN AT ROW 9 IS NOT WORKING. REPAIRED WIRING. OPERATIONAL CHECK GOOD.

Part: STRINGER — CRACKED (LT NACELLE) · airframe 33,068 hrs · 43,683 cycles

LEFT ENGINE MID COWL FORWARD OUTBOARD STRINGER CRACKED, DISCOVERED DURING E-6 INSPECTION. REPLACED FORWARD OUTBOARD STRINGER AT LEFT ENGINE MID COWL IAW SRM 51-40-02 SEE RII 54-900-1000.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 32,812 hrs · 43,323 cycles

FLIGHT ATTENDANT REPORTED OVERHEATED ODOR COMING OUT OF HOT JUGS. SWITCH WAS TURNED OFF AND ODOR DISAPPEARED. REPLACED HOT JUG WITH SERVICEABLE UNIT IAW 25-60-00. OPERATIONAL CHECKS GOOD.

Part: BEAM — CRACKED (RT NACELLE) · airframe 32,676 hrs · 43,133 cycles

RIGHT NACELLE INBOARD BEAM AT HYDRAULIC BAY IS CRACKED, DISCOVERED DURING A-CHECK INSPECTION. REPLACED RIGHT NACELLE INBOARD BEAM AT HYD BAY PER SRM 51-40-02 AND SEE RII 54-900-1000.

Part: RIB — CRACKED (LT WING) · airframe 32,723 hrs · 43,202 cycles

LEFT WING INBOARD LEADING EDGE RIB IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION NEW RIB INSTALLED IAW SRM 120 51-10-02, PG 3, SEC 3A.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 32,723 hrs · 43,202 cycles

CRACK IN PAX DOOR FRAME BELOW AFT STEP SUPPORT, DISCOVERED DURING C-CHECK INSPECTION. NEW FRAME INSTALLED IAW SRM 120 51-10-02, PG 3, SEC 3.A AND RII CARD 52-800-1000.

Part: RIB — CRACKED (RT WING) · airframe 32,723 hrs · 43,202 cycles

RIGHT WING INBOARD LEADING EDGE RIB IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. NEW RIB INSTALLED IAW SRM 120 51-10-02, PG 3, SEC 3 A.

Part: BUSS — MALFUNCTIONED · airframe 32,560 hrs · 42,981 cycles

SELECTED GEAR DOWN AND LOST NR 2 T6 AND NR 2 TORQUE GAUGES WITH SEVERAL MAP LIGHTS AND TAKEOFF AURAL WARNINGS AND ELECTRICAL EMERGENCY BUSS ILLUMINATED. GEAR DID NOT INDICATE DOWN AND LOCKED. RESET EMERGENCY BUSS 2 CB AND CHANGED RELAY K0519 EMERGENCY BUSS 2 CONTACTOR. ALL SYSTEM'S OPERATIONAL CHECKS GOOD.

Part: RELAY — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,897 hrs · 40,588 cycles

FLIGHT ATTENDANT EMERGENCY LIGHTS WOULD NOT WORK WHEN TEST WAS SELECTED. REPLACED RELAY K0201 IAW WMM 33-51-00. OPERATIONAL CHECK GOOD.

Part: SOCKET — DAMAGED (FLAP ACT CONNECT) · airframe 29,751 hrs · 39,036 cycles

"CONTROL FAULT" IN CRUISE PORTION OF FLIGHT OF BOTH OUTBOARD AND NACELLE FLAPS. REPLACED ALL SOCKETS IN ALL 6 FLAP ACTUATOR CONNECTORS. OPERATIONAL CHECK GOOD. REF EMB 120 WDM 20-21-00 AND 20-50-00 AND MM 27-50-00.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 29,684 hrs · 38,959 cycles

FLAP CONTROL FAULT AT ALTITUDE. REPLACED FLAP CONTROL COMPUTER IAW EMB 120 MM 27-50-06. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — DIRTY (TE FLAP ACTUATOR) · airframe 29,364 hrs · 38,549 cycles

ON TAXI OUT, FLAP DISAGREEMENT WHEN FLAP LEVER SELECTED TO FLAPS 15 DEGREES POSITION. CLEANED ALL FLAP ACTUATORS CONNECTORS. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 29,296 hrs · 38,474 cycles

FLAP CONTROL FAULT ON OUTBOARD FLAPS. REPLACED FLAP CONTROL LEVER & FCU IAW MM 27-50-06 & 27-50-01. OPERATIONAL CHECKS GOOD. P/N 120-64207-615; S/N OFF 120278.

Part: ARM — BINDING (PAX DOOR) · airframe 28,832 hrs · 37,911 cycles

MAIN CABIN DOOR EXTREMELY DIFFICULT TO OPEN AND CLOSE. INSTALLED NEW ROTATING ARMS IAW 52-10-00. OPERATIONAL CHECK GOOD.

Part: MECHANISM — DIRTY (PAX DOOR) · airframe 28,817 hrs · 37,893 cycles

F/A REPORTS MCD IS DIFFICULT TO OPEN AND CLOSE WITH RED HANDLE. LUBRICATED DOOR IAW MM 12-21-15. TURNED HYDRAULIC ON, HELD THE PUSH BUTTON FOR DOOR ASSIST UNTIL THE DOOR MADE CONTACT WITH MICROSWITCH. OPERATIONAL CHECK GOOD.

Part: MECHANISM — DIRTY (PAX DOOR) · airframe 28,781 hrs · 37,853 cycles

MAIN CABIN DOOR HARD TO OPEN. CHECKED DOOR, CLEANED AND LUBED ROLLERS, LUBED HANDLE, OPERATIONAL CHECK SATISFACTORY.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAP) · airframe 28,528 hrs · 37,564 cycles

FLAP DISAGREEMENT WHILE EXTENDING FLAPS TO 15 DEGREES. INSTALLED SERVICEABLE LEFT INBOARD FLAP ACTUATOR IAW EMB MM 27-50-00. OPERATIONAL CHECK GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (STALL WARNING) · airframe 28,462 hrs · 37,459 cycles

NR 1 STALL WARNING STAYS ON MAP AFTER TESTING. REMOVED AND REPLACED STALL WARNING PANEL. OPERATIONAL CHECK GOOD. P/N 120-34428-505, S/N OFF 120-291.

Part: SMOKE — DETECTED (CABIN/COCKPIT) · airframe 28,198 hrs · 37,113 cycles

DURING ENGINE START, CABIN FILLED WITH SMOKE. INSPECTED BOTH LT AND RT PACKS FOUND OPERATING NORMAL. STARTED RT ENGINE. OPERATIONAL CHECKS GOOD.

Part: ODOR — DETECTED (COCKPIT) · airframe 28,059 hrs · 36,944 cycles

ON TAKEOFF ROLL BOTH PILOTS SMELLED SMOKE AND LAV SMOKE DETECT ALARM SOUNDED. C/B POPPED. REMOVED AND REPLACED RCCB 0208 WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.

Part: HANDLE — DIRTY (MAIN CABIN DOOR) · airframe 27,956 hrs · 36,824 cycles

FA CAN NOT OPEN MAIN CABIN DOOR. HANDLE ONLY MOVES .2500 IN BEFORE STICKING. LUBED PASSENGER DOOR. OPERATIONAL CHECK GOOD.

Part: PROXIMITY SENSOR — MALFUNCTIONED (ELEVATOR) · airframe 27,752 hrs · 36,586 cycles

WHEN TAXIING TO GATE, TRIM AURAL WARNING GOING OFF IN GREEN BAND. REMOVED AND REPLACED BOTH ELEVATOR TRIM PROXIMITY SENSORS IAW EMB 120 MM 27-32-05. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (OB FLAPS) · airframe 27,692 hrs · 36,500 cycles

OB FLAPS DID NOT EXTEND WHEN ANY OF THE FLAPS SETTINGS WAS SELECTED. REMOVED AND REPLACED FCU IAW MM 27-50-06. OPERATIONAL CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 27,485 hrs · 36,207 cycles

RIGHT WINDSHIELD SHATTERED. REMOVED AND REPLACED RIGHT WINDSHIELD IAW EMB MM 56-10-01. OPERATIONAL CHECK GOOD.

Part: SMOKE DETECTOR — ACTIVATED (LAVATORY) · airframe 27,350 hrs · 36,048 cycles

LAVATORY SMOKE ALARM WENT OFF. TURNED OFF PACKS. SMOKE ALARM STOPPED AFTER A FEW MINUTES. RAN APU AND ENGINES AND BOTH PACKS FOR 45 MINS. OPERATIONAL CHECKED GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 27,191 hrs · 35,830 cycles

RIGHT WINDSHIELD CRACKED. REMOVED AND REPLACED RIGHT WINDSHIELD IAW EMB MM 56-10-01. P/N ON&OFF: NP-151311-2, S/N OFF: 98099H2740.

Part: AHRS — MALFUNCTIONED (E/E BAY) · airframe 26,695 hrs · 35,232 cycles

INTERMITTENT COMPUTER FLAG ON CAPT ATTITUDE INDICATOR. AUTOPILOT DISENGAGED WITH FLAG. REPLACED AHRS, OPS CHECK GOOD. WORK DONE IAW MM 34-21-01.

Part: PIN — LOOSE (CONNECTOR) · airframe 26,447 hrs · 34,923 cycles

F/O'S AUTOPILOT DOES NOT CAPTURE GLIDE SLOPE. GS ARM STAYS ILLUMINATED THRU-OUT APPROACH. RE-INSERTED AND SECURED PIN 44 OF P0175 BACK INTO CONNECTOR OF A/P COMPUTER NR 2. OPS CHECK GOOD IAW 22-10-00.

Part: COMPUTER — FAULTY (AUTOPILOT SYS) · airframe 26,049 hrs · 34,403 cycles

CAPTAIN'S AUTOPILOT FAILED IN FLIGHT DURING CLIMB. REMOVED AND REPLACED CAPTAIN'S APC-65B. OPS CHECKS GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 26,054 hrs · 34,411 cycles

PAX ENTRY AREA; FLOORBOARD FRAMES, CORROSION AT VARIOUS LOCATIONS AS MARKED. DISCOVERED DURING C-CHECK. REPLACED CENTER FLOORBOARD BRACKET AFT OF GALLEY AND REMOVED, TREATED AND PRIMED NUMEROUS SURFACE CORROSION AREAS IAW SRM 51-10-02.

Part: ODOR — DETECTED (CABIN) · airframe 25,979 hrs · 34,290 cycles

TAXIING OUT IN AUTO/NORM (FOR LESS THAN 1 MINUTE) DETECTED SMOKE. TURNED PACKS BACK TO LOW/LOW. NO ABNORMAL INDICATION ON PNEUMATIC PANEL BUT F/A REPORTED SMOKE IN CABIN & SMOKE IN LAV. TURNED OFF RECIRCS & PACKS, RETURNED TO GATE. SMOKE REMAINED BUT NO NEW SMOKE. FOUND PACKS TO BE FROZEN (ICED UP). DEFROSTED PACKS. COULDN'T DUPLICATE ANY PROBLEMS.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 25,915 hrs · 34,195 cycles

CAPTAINS AUTOPILOT PITCH IS ERRATIC IN LEVEL FLIGHT PITCH CHANGED +/- 2 DEGREES. REPLACED CAPT AHC 85. OPS CHECK GOOD.

Part: CONNECTOR — BURNED (COFFEMAKER) · airframe 25,902 hrs · 34,178 cycles

SMOKE COMING FROM TOP OF COFFEE JUG (NR 2). STOPPED WHEN SWITCH WAS TURNED OFF. CLEANED GALLEY COFFEE JUG CONNECTOR. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 25,902 hrs · 34,178 cycles

F/O'S FLIGHT DIRECTOR WILL NOT CAPTURE GLIDE SLOPE. REPLACED F/O'S AUTOPILOT COMPUTER. SYSTEM TESTS NORMALLY PER MM 22-11-00.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 25,758 hrs · 33,990 cycles

FO AUTOPILOT FLIGHT DIRECTOR NOSE DOWN 10 DEGREES. AUTOPILOT FAIL AND TRIM FAIL MASTER WARN ON MAP ASSOC WITH RED TRIM AND AP LIGHTS ALSO GREEN VS AND AMBER DIS. REMOVED AND REPLACED NR 2 APC 65B IAW 22-10-00. OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 25,190 hrs · 33,298 cycles

FLOOR LEVEL RED COURTESY LIGHT BY FLIGHT ATTENDANT'S SEAT IS INOP. REMOVED AND REPLACED BULB IN FLOOR LEVEL RED COURTESY LIGHT WITH SERVICEABLE UNIT. OPS CHECK GOOD AT THIS TIME.

Part: WINDOW — CRACKED (COCKPIT) · airframe 23,597 hrs · 31,344 cycles

RIGHT DV WINDOW CRACKED. REMOVED AND REPLACED RIGHT DV WINDOW. PERFORMED LEAK CHECK TO 6 PSI. NO LEAKS NOTED. SERVICEABLE AT THIS TIME.

Part: ACCESS DOOR — MISSING (HYD SYSTEM) · airframe 23,510 hrs · 31,240 cycles

POST FLIGHT INSPECTION - LEFT HYDRAULIC PANEL MISSING. TRIMMED NEW DOOR TO FIT AND INSTALLED NEW LATCHES, CAMLOCKS AND NEW HINGE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 22,933 hrs · 30,574 cycles

AT 26,000 MSL, THE CAPTAIN'S WINDSHIELD CRACKED. REMOVED AND REPLACED THE LEFT WINDSHIELD. OPS CHECK GOOD.

Part: INDICATOR — FAILED (COCKPIT) · airframe 22,642 hrs · 30,234 cycles

AFTER DEPARTURE LEFT NP NEEDLE WAS READING -0-. RETURNED TO SLC. REMOVED AND REPLACED NR 1 NP INDICATOR. OPS CHECK GOOD.

Part: CONNECTOR — DIRTY (FLAP ACTUATOR) · airframe 22,128 hrs · 29,641 cycles

FLAP DISAGREEMENT ON AFTER TAKEOFF FLAP RETRACTION. REQUIRED QRH PROCEDURE TO CORRECT. INSPECTED FLAP. CLEANED CONNECTORS FROM ACTUATOR CANNON PLUGS. RAN FLAPS SEVERAL TIMES. OPS CHECK GOOD AT THIS TIME.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 21,986 hrs · 29,437 cycles

AUTOPILOT TRIM RED LIGHTS CAME ON DURING TAKE OFF, ABORTED. CYCLED AUTO PILOT CIRCUIT BREAKERS OPS CHECK GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 21,982 hrs · 29,427 cycles

ULTRASONIC INSPECTION OF FRAME 21 FROM STRINGER 20L TO 20R FOUND 2 AREAS, 1 APPROX 1 INCH IN LENGTH BETWEEN FASTENERS TOTAL LOSS OF BACKWALL IN AREA AND SECOND APPROX 1/2 INCH IN LENGTH BETWEEN FASTENERS LOWEST READING .030 INCH. COMPLIED WITH REPAIR FOR FRAME 21 FROM STRINGER 20L TO 20R IAW SRM 53-00-01 PER SB 120-53-0065.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 21,598 hrs · 28,969 cycles

FLAP CONTROL FAULT IN CRUISE FLIGHT. DID NOT RESET AS PER QRH PROCEDURE. OUTBOARD FLAPS REMAINED IN UP POSITION THROUGHOUT APPROACH AND LANDING.REMOVED AND REPLACED ANNUNCIATOR. REMOVED LEFT INBOARD FLAP AND REPLACED ALL BEARINGS AND LEFT INBOARD MOVEABLE TRACK IAW 27-50-00. FLAP SYSTEM OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 21,557 hrs · 28,919 cycles

AFTER FLAP RETRACTION AFTER TAKEOFF INBOARD FLAP DISAGREEMENT. ATTEMPTED CONTROL WITH FLAP HANDLE PER QRH TO NO EFFECT.TROUBLESHOT FLAP SYSTEM IAW MM 27-50-01 AND IAW FIM 27-50-01. COULD NOT GET A FAILURE. ALSO REPLACED FLAP CONTROL UNIT. OPS CHECK GOOD.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 21,506 hrs · 28,862 cycles

RIGHT ENGINE WOULD NOT POWER UP FOR TAKEOFF. RAN BOTH ENGINES THROUGH ALL PARAMETERS WITH EEC'S ON AND ALSO WITH EEC'S OFF. NO FAULTS NOTED. OPS CHECK GOOD.

Part: HMU — MALFUNCTIONED (LEFT ENGINE) · airframe 21,454 hrs · 28,800 cycles

LEFT ENGINE WOULD NOT PRODUCE OVER 40 PERCENT TORQUE BEFORE T/O AURAL WARNING SOUNDED. THIS HAPPENED TWICE. T/O WAS ABORTED TWICE.REMOVED THE LEFT ENGINE HMU AND INSTALLED A SERVICEABLE HMU. GROUND OPS CHECK AND LEAK CHECK GOOD IAW EMB MM 73-21-00.

Part: COMPUTER — MALFUNCTIONED (AHRS) · airframe 21,393 hrs · 28,728 cycles

DURING CLIMBOUT FOS ADI ERRATIC + - 5 DEGREES OF PITCH WITH NO ASSOCIATED FAILURE FLAGS. FOLLOW UP: AFTER TAKEOFF FOS ADI ROLLED TO 50 DEGREES BANK, 30 DEGREES NOSE UP. ATTITUDE DISPLAY LIGHT ON MAP. FOLLOWED QRH PROCEDURE AND RETURNED FOR LANDING.REMOVE AND REPLACE NR 2 AHRS COMPUTER IAW 34-21-00. OPS CHECK GOOD. FOLLOW UP: REMOVE AND REPLACE NR 2 AHRS COMPUTER (SUSPECT PREVIOUS UNIT WAS BAD OFF THE SHELF) IAW 34-21-00. OPS CHECK GOOD. PN ON 622-6190-204, SN ON 2100, SN OFF 2662.

Part: FLOW VALVE — INOPERATIVE (DEICE BOOTS) · airframe 21,393 hrs · 28,728 cycles

LEFT AND RIGHT INBOARD STABILIZER DEICE BOOTS INOP INFLIGHT AT FL 200.REMOVED AND REPLACED FLOW CONTROL VALVE FOR HORIZONTAL STABILIZER IAW MM 32-20-04. OPS CHECK SATISFACTORY.

Part: PCU — DEFECTIVE (LT ENGINE) · airframe 4,143 hrs · 5,269 cycles

LEFT ENGINE TORQUE FLUCTUATION AT +30 TO -30 PERCENT ON CLIMBOUT. RETURNED TO SLC FOR NORMAL LANDING. ATTEMPTED TO FLY WITH EEC'S OFF, NO CHANGE. REMOVED AND REPLACED PCU ON LEFT ENGINE. OPS CHECKS, LEAK CHECKS GOOD. P/N: 782490-46 S/N ON: 900528 S/N OFF: 851019.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 21,314 hrs · 28,640 cycles

ON DEPARTURE, FLAP DISAGREEMENT - INBOARD. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR IAW MM 27-50-02. LEAK AND OPS CHECK SATISFACTORY.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 4,043 hrs · 5,150 cycles

T6 WARNING OCCURRED AFTER ROTATION WITH TAKEOFF POWER AT CHART VALUE. PEEKED AT 816 DEGREES C AND REDUCED POWER RIGHT SIDE. RAN AIRCRAFT TO TARGET TORQUE IN SLC. BLEEDS CLOSED. MADE 100 PERCENT TORQUE. AT 796 DEGREES T6 WITHIN LIMITS PER MM 71-00-00.

Part: PROXIMITY SENSOR — FAILED (RT MLG) · airframe 20,952 hrs · 28,171 cycles

RIGHT MAIN GEAR POSITION INDICATOR DISAGREED WITH GEAR HANDLE POSITION (A&B RED LIGHTS ON) UP. TRIED RECYCLE 2 TIMES PER QRH WITH NO SUCCESS. ADJUSTED RIGHT INBOARD SEQUENCE VALVE IAW 32-32-04. REMOVE AND REPLACE RIGHT B-UPLOCK PROXIMITY SENSOR IAW 32-61-01. OPS CHECK GOOD.

Part: ACTUATOR — FAILED (RUDDER) · airframe 20,740 hrs · 27,920 cycles

RUDDER BLUE SYSTEM INOP. (PILOT REPORTED RUDDER ACTUATOR LOCKED UP IN FLIGHT.) RUDDER PCU STARTING TO LEAK AND TESTS ON THE LOW END OF THE RUDDER HEALTH CHECK FOR BLUE SYSTEM. REMOVED AND REPLACED BLUE SYSTEM RUDDER ACTUATOR IAW EMB MM 27-22-024. PERFORMED RUDDER HYDRAULIC SYSTEM HEALTH CHECK IAW EMB MM 27-22-00 TO C/W FCD 00-09-27R2. RUDDER HEALTH CHECK PASSED. OPS CHECK GOOD OF RUDDER SYSTEM. ALL PANELS VERIFIED CLOSED. LEAK CHECK GOOD. REMOVED RUDDER PCU AND INSTALLED SERVICEABLE UNIT IAW MM 27-22-11 AND RII 27-312. OPS AND LEAK CHECK GOOD. ALSO PERFORMED RUDDER HEALTH CHECK IAW MM 27-22-00. CHECKED GOOD. P/N: 32100-1003, S/N ON: 0215A, S/N OFF: 0287.

Part: CONNECTOR — DAMAGED (CENTRAL WARNING) · airframe 20,129 hrs · 27,124 cycles

ON TAKEOFF ROLL RECEIVED A TRIPLE CHIME WITH AURAL TRIM WARNING. AIRCRAFT TRIM WAS SELECTED IN GREEN ARC TO 34 PERCENT. ABORTED TAKEOFF. FOUND PIN-L AT PO349 SEVERED. INSTALLED NEW PINS AT JO349 AND PO349 IAW 20-00-00. GROUND OPS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 19,830 hrs · 26,764 cycles

WHEN TAXIING AIRCRAFT TO GATE, OPERATED FLAPS TOWARD DOWN POSITION AND RECEIVED CONTROL FAULT ON OUTBOARD PAIR. TRIED CLEARING AND RESETTING, BUT IT WOULD NOT. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-09. OPS AND LEAK CHECK GOOD. P/N: 343000-1003 S/N ON: 0297 S/N OFF: 0554

Part: FLAP — MALFUNCTIONED (LEFT) · airframe 19,824 hrs · 26,757 cycles

WHILE TAXIING AIRCRAFT TO GATE CYCLED FLAPS 25 TO 0 DEGREES AND RECEIVED DISAGREEMENT ON OUTBOARD FLAPS. REMOVED AND REPLACED LEFT NACELLE FLAP WITH A SERVICEABLE UNIT IAW EMB MM 27-50-08 AND RTT 27-307. OPS AND LEAKS CHECKS GOOD.

Part: ROLLER — DAMAGED (TE FLAP TRACK) · airframe 19,830 hrs · 26,764 cycles

OUTBOARD FLAPS DISAGREEMENT ON CLIMB OUT FLAP RETRACTION. RETURNED TO SLC. REPLACED ALL ROLLERS ON LEFT AND RIGHT OUTBOARD FLAPS AND ONE MOVEABLE FLAP TRACK ON LEFT OUTBOARD FLAP. CYCLED FLAPS. OPS CHECKS GOOD.

Part: SELECTOR SWITCH — FAILED (TE FLAPS) · airframe 19,822 hrs · 26,753 cycles

ON DEPARTURE JUST AFTER ROTATION OUTBOARD FLAPS SENSED A CONTROL FAULT. (WOULD NOT RESET). RETURNED TO SLC. REMOVED AND REPLACED FLAP SELECTOR IAW MM 27-50-01. REMOVED AND REPLACED LEFT AND RIGHT OUTBOARD FLAP ACTUATOR ASSEMBLIES IAW MM 27-50-09. MEGGED WIRE HARNESS LEFT AND RIGHT OUTBOARD ACTUATORS. OPS CHECKS GOOD. NO LEAKS NOTED.

Part: CONNECTOR — DIRTY (TE FLAPS) · airframe 19,790 hrs · 26,718 cycles

ON APPROACH TO TWF WHEN SELECTING FLAPS TO 25 DEGREES WE GOT A FLAP CONTROL FAULT AND IT WOULD NOT RESET EVEN AFTER LANDING. RE-RACKED FLAP CONTROL BOX. CLEANED CANNON PLUGS (OUTBOARD FLAPS). FUNCTION TEST GOOD.

Part: CONNECTOR — CONTAMINATED (TE FLAPS) · airframe 19,631 hrs · 26,539 cycles

ON CLIMBOUT, DIFFICULTY BRINGING UP FLAPS. CLEANED GLYCOL FROM ACTUATOR CANNON PLUGS. FOUND SYSTEM TO OPERATE NORMAL.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 19,615 hrs · 26,519 cycles

LEFT HAND DIRECT VISION WINDSHIELD SIDE POST IS CRACKED. DISCOVERED DURING E003 INSPECTION. FIT AND INSTALLED A .125 ALUM DOUBLER FOR THE LEFT WINDSHIELD SIDE POST IAW EA BR028B-53.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 19,615 hrs · 26,519 cycles

RIGHT HAND DIRECT VISION WINDSHIELD SIDE POST IS CRACKED. DISCOVERED DURING E003 INSPECTION. FIT AND INSTALLED A .125 ALUM DOUBLER FOR THE RIGHT WINDSHIELD SIDE POST IAW EA BR028B-53.

Part: ACTUATOR — FAILED (RUDDER TRIM) · airframe 17,777 hrs · 24,399 cycles

WHILE DESCENDING INTO SUN LOST RUDDER TRIM CONTROL. RETURNED TO SLC. THIRTY MINUTES LATER, DESCENDING INTO SLC, TRIM CONTROL REGAINED. REPLACED RUDDER TRIM ACTUATOR IAW MM 272302 AND 272000, OPS CHECKS GOOD ON GROUND. (P/N 5298) (S/N 334) ON.

Part: PRESSURIZATION — MALFUNCTIONED (CABIN)

LOST CABIN PRESSURIZATION DURING CLIMB AT 7000 AGL. CABIN ALTITUDE AT 6500. RETURNED TO LAX. PRESSURIZED AIRCRAFT. ALL CHECKS GOOD AT THIS TIME.

Part: DUCT LIGHT — ILLUMINATED (LT PACK)

LEFT DUCT LEAK LIGHT ON MAP CAME ON 7 MIN AFTER TAKEOFF. RETURNED TO AIRPORT AND LIGHT EXTINGUISHED JUST BEFORE TOUCHDOWN. DEFERRED LEFT A/C PACK PER MEL 36-21-1.

Part: ROLLERS — WORN (LT TE FLAP)

AFTER DEPARTURE, SELECTED FLAPS 0 DEG AND GOT A FLAP DISAGREEMENT. INBOARD PAIR DID NOT RETRACT COMPLETELY. RETURNED TO PSP. INSPECTED FLAP ROLLERS AND FOUND LEFT OUTBOARD FLAP ROLLER WORN. INSTALLED NEW ROLLER ON LEFT OUTBOARD FLAP, OPS CHECKS GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS)

AFTER DEPARTURE, SELECTED FLAPS TO 0 DEGREES AND GOT A FLAP DISAGREEMENT. CALLED MAINTENANCE CONTROL THROUGH ATLANTA RADIO AND WAS TOLD TO RETURN TO LAX. GOT A ROLL TO THE RIGHT WHEN SELECTING FLAPS 15 DEG FROM FLAPS 0 DEG. REPLACED FLAP CONTROL UNIT AND OPERATED FLAPS SEVERAL TIMES, OPS CHECKS GOOD.

Part: REGULATOR — FAILED (RT ENGINE)

RIGHT ENGINE DUCT LEAKAGE LIGHT ILLUMINATED AFTER TAKEOFF AND REMAINED ON AFTER ACCOMPLISHING CHECKLIST PROCEDURE. SHUT RIGHT ENGINE DOWN AND RETURNED TO AIRPORT. FOUND 18 PSI REGULATOR LOWER HOUSING APART. REASSEMBLED HOUSING AND RAN ENGINE, NO LEAKS NOTED.

Part: OIL PRESS REG — OUT OF ADJUST (NR 1 ENGINE)

AT ROTATION, OIL AURAL WARNING AND OIL PRESSURE NR 1 MAP LIGHT ILLUMINATED. ENGINE NR 1 OIL PRESSURE NEEDLE GAUGE WENT TO 20 PSI AND FLUCTUATED BETWEEN 20 AND 40 PSI. WE THEN PROCEEDED TO PERFORM PRECAUTIONARY ENGINE SHUT DOWN PROCEDURES AND RETURNED TO GJT. INSPECTED ENGINE, FOUND 3 QTS LOW ON OIL. ADDED 3 QTS AND PERFORMED GROUND RUN. DURING GROUND RUN NOTICED LEFT ENGINE OIL PRESSURE HIGH IN YELLOW ARC. REMOVED ONE SHIM FROM OIL PRESSURE REGULATOR AND PERFORMED GROUND RUN AT 85 PERCENT TQ FOR 10 MIN. LEFT ENGINE OIL PRESSURE AND TEMPERATURE NORMAL.

Part: STRAP — CORRODED (CABIN)

CORROSION AND CRACK IN CENTER BUTT STRAP, FORWARD GALLEY AREA. CUT OUT DAMAGED AREA FABRICATED A FILLER AND DOUBLER AND INSTALLED ON CENTER BUTT STRAP FORWARD OF GALLEY AREA IAW SRM 51-00-00.

Part: CONNECTOR — LOOSE (TE FLAPS)

RETURNED TO SLC AFTER FLAP FAULT INDICATION. REMOVED OUTBOARD CANNON PLUGS FOR ACTUATORS AND FOUND SOME MOISTURE. CLEANED CANNON PLUGS AND CONNECTORS ACCOMPLISHED BIT TEST IAW MM 27-50-00. NO FAULT FOUND AT THIS TIME, OPS CHECKS GOOD. ALSO, INSPECTED ALL ROLLERS AND TRACKS.

Part: CONNECTOR — FAILED (LT TE FLAP)

FLAP DISAGREEMENT ON TAKEOFF. RETURNED TO FIELD. REPLACED CONNECTOR FOR LEFT INBOARD FLAP ACTUATOR, OPS CHECKS GOOD.

Part: DISAGREE LIGHT — MALFUNCTIONED (TE FLAPS)

ON DEPARTURE AFTER SELECTING FLAPS UP, RECEIVED DISAGREEMENT LIGHT. PERFORMED ORH PROCEDURES, DISAGREEMENT DID NOT GO AWAY. UPON LANDING DISAGREEMENT WENT OUT. INSPECTED FLAP ROLLERS AND TRACKS OPS CHECKS IN MAINT MODE. NO FAULTS FOUND. CYCLED FLAPS NUMEROUS TIMES, OPS CHECKS PER MM 27-50-00.