N197SW

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 36,444 hrs · 45,530 cycles

EMERGENCY EXIT LIGHT (OVERHEAD) AT ROW 6C INOPERATIVE. RELAMPED BULB, OPERATIONAL CHECK GOOD.

Part: ROLLER — DIRTY (PAX DOOR) · airframe 36,200 hrs · 45,245 cycles

MAIN CABIN DOOR IS HARD TO OPEN/CLOSE. CLEANED MAIN CABIN DOOR ROLLERS AND ACTUATORS. RELUBED ROLLERS AND LOCKING MECHANISM. OPERATIONAL CHECK GOOD IAW 52-00-00.

Part: ANNUNCIATOR — MALFUNCTIONED (TE FLAPS) · airframe 35,346 hrs · 44,174 cycles

UPON SELECTING FLAPS 15 DEGREES ON TAXI, WITH THE FLAP SELECTOR IN THE 15 DETENT, NO MOVEMENT ON FLAP COMMAND OR ON INDICATOR. REMOVED AND REPLACED FLAP ANNUNCIATOR ASSEMBLY IAW 27-50-05. OPS CHECKED GOOD.

Part: ANNUNCIATOR — FAULTY (COCKPIT) · airframe 34,896 hrs · 43,625 cycles

IN CRUISE FLIGHT, FLAP ADV SWS, AND CONTROL FAULT LIGHTS ILLUMINATED. RESET THE SYSTEM PER QRH, 5 MINUTES LATER, FLAP ADV SWS, CONTROL FAULT, ASYMMETRY, AND FLAP DISAGREEMENT ALL ILLUMINATED. ALSO HAD ERRATIC READINGS ON FLAP INDICATOR. REMOVED AND REPLACED FLAP ANNUNCIATOR IAW EMB MM 27-50-05. OPS CHECKS GOOD.

Part: FAN — FAILED (LT PACK) · airframe 34,812 hrs · 43,527 cycles

LEFT PACK EMITTING SMOKE THROUGH VENTS WHILE ON GROUND. REPLACED LEFT PACK GROUND COOLING FAN. OPS CHECKS GOOD.

Part: COMPUTER — OUT OF ADJUST (NR 2 AHRS) · airframe 34,805 hrs · 43,515 cycles

COPILOT'S COMPUTER FLAG CAME ON AUTOPILOT, WOULD NOT ENGAGE. REORIENTED NR 2 AHRS COMPUTER. AUTO PILOT OPS CHECKS GOOD.

Part: ATTACH BRACKET — CRACKED (LT NACELLE) · airframe 34,663 hrs · 43,327 cycles

ATTACH BRACKET CRACKED AT LEFT NACELLE OUTBOARD OF WHEEL WELL AT 3RD RIVET FROM BOTTOM (INTERIOR OF WALL). DISCOVERED DURING C-CHECK INSPECTION. REPAIRED BRACKET LOCATED AT LEFT NACELLE OUTBOARD OF WHEEL WELL IAW EMB120 SRM 54-10-03 PAGE 202 FIG 201 SHEET 1.

Part: RIB — CRACKED (RT WING) · airframe 34,663 hrs · 43,327 cycles

RIGHT FORWARD MOST OUTBOARD SMALL FUEL PANEL, RIB INSIDE WING CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED RIGHT MOST OUTBOARD NOSE RIB WEB IAW SRM 120 57-20-07 PG 210 FIG 203.

Part: BRACKET — CRACKED (LT NACELLE) · airframe 34,663 hrs · 43,327 cycles

INTERIOR BRACKET CRACKED AT LEFT NACELLE OUTBOARD OF WHEEL WELL SUPPORT. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW SRM 54-10-03 FIG 201. P/N 120-41419-001.

Part: FRAME — CRACKED (LT NACELLE) · airframe 34,631 hrs · 43,291 cycles

LEFT MLG, OUTBOARD LOWER NACELLE FRAME CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED LOWER NACELLE FRAME IAW 120 SRM 51-10-02 PG 3 SEC 3A & RII CARD 54-301.

Part: CRADLE — CRACKED (NACELLE) · airframe 34,663 hrs · 43,327 cycles

RIGHT OUTBOARD EXHAUST CRADLE OUTBOARD CORNER IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED EXTERNAL DOUBLER IAW EMB SRM 51-10-02.

Part: FRAME — CRACKED (RT NACELLE) · airframe 34,631 hrs · 43,291 cycles

RIGHT NACELLE (WHEEL WELL) OUTBOARD UPPER FRAME CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED RIGHT NACELLE (WHEEL WELL) OUTBOARD UPPER AFT FRAME IAW EMB120 SRM 54-10-03 PAGE 202 FIG 201 SHEET 1.

Part: FRAME — CRACKED (LT NACELLE) · airframe 34,631 hrs · 43,291 cycles

LEFT ENGINE FRAME NR 1 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED LEFT ENGINE FRAME NR 1 IAW EMB120 SRM 51-10-02 PG 3 SEC 3A AND S/B 120-54-0036 AND RII CARD 54-301.

Part: RIB — CRACKED (LT WING) · airframe 34,663 hrs · 43,327 cycles

CRACKED RIB AT RIVET OUTBOARD OF SMALL FUEL ACCESS PANEL NR 3 OF LEFT WING. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED LEFT NOSE RIB WEB NR 19 IAW EMBRAER REF 1C2004-120/0414 AND SRM 57-20-07 AND CARD RII 28-301.

Part: CLIP — CRACKED (LT WING) · airframe 34,631 hrs · 43,291 cycles

LEFT WING SHEAR CLIP AT STATION YA-5825 CRACKED OUTBOARD OF FUEL PANEL 4 MIDDLE SECTION. DISCOVERED DURING C-CHECK INSPECTION. REPLACED AND SEALED SHEAR CLIP IAW 120 SRM 51-10-02 AND RII CARD 28-301.

Part: CONTROL UNIT — MALFUNCTIONED (T/E FLAP) · airframe 34,150 hrs · 42,686 cycles

AFTER LANDING NAC FLAPS CONTROL FAULTED AND WOULD NOT RESET. REMOVED FLAP COMPUTER AND INSTALLED A SERVICEABLE UNIT. OPS CHECKS GOOD. P/N: 307500-1007, S/N OFF: 169.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 34,090 hrs · 42,590 cycles

CENTER EMERGENCY LIGHTS ARE INOP. REPLACED CENTER ELBP WITH SERVICEABLE UNIT. OPS CHECK GOOD.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 33,549 hrs · 41,945 cycles

FORWARD SECTION OF EMERGENCY LIGHTS IN CABIN ARE INOPERATIVE. REPLACED BLOWN FUSE. OPS CHECK GOOD. P/N: 1AFUSE

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 33,354 hrs · 41,676 cycles

FLAP CONTROL FAULT DURING FLAP BITE TEST AND WILL NOT RESET. INSTALLED FLAP CONTROL UNIT IAW EMB 120 MM 27-50-06. OPS CHECKS GOOD. S/N OFF: 0230.

Part: CONTROL PANEL — MALFUNCTIONED (AUTOPILOT) · airframe 33,336 hrs · 41,653 cycles

BOTH AUTPILOTS TURN RIGHT, UNCOMMANDED, DO NOT FOLLOW COMMAND BARS. REPLACED APP-65. OPS CHECK GOOD IAW AMM 22-00-00.

Part: BRACKET — CRACKED (TE FLAP ROLLER) · airframe 32,725 hrs · 40,933 cycles

INBOARD FLAP FOLLOWER ROLLER BRACKETS CRACKED ON LEFT SIDE. REMOVED AND REPLACED INBOARD FLAP FOLLOWER ROLLER BRACKETS AT BOTH ENDS IAW SRM 51-10-03 AND 51-40-02. PN: 120-22884-001.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 32,122 hrs · 40,171 cycles

AUTO PRESSURIZATION UNABLE TO CONTROL PRESSURE. CONTRACT MAINTENANCE PERFORMED MX PROCEDURE FOR DEFERRAL. NEXT FLIGHT RETURNED TO GJT WITH MANUAL PRESSURIZATION INOPERATIVE REMOVED AND REPLACED ELECTRO OUTFLOW VALVE IAW MM 21-30-03. OPS CHECK GOOD.

Part: BOOT — FAILED (DE-ICE SYSTEM) · airframe 31,788 hrs · 39,774 cycles

INBOARD LEFT AND RIGHT STAB AND INBOARD LEFT AND RIGHT WING LEADING EDGE DEICERS FAILED IN FLIGHT ON BOTH TIMERS. RETURNED TO SLC. REMOVED & REPLACED RIGHT WING OUTBOARD DEICE, LEFT OUTBOARD DEICE BOOT & RIGHT HORIZONTAL STAB DEICE BOOT WITH SERVICEABLE UNIT. OPERATED DEICE BOOT SYSTEM. OPS CHECK GOOD.

Part: RECEPTACLE — MELTED (CABIN) · airframe 30,842 hrs · 38,686 cycles

SMOKE SMELL IN CABIN. FOUND A LIGHT RECEPTACLE MELTED. REPLACED LIGHT RECEPTACLE AT SEAT 5A. OPS CHECK GOOD.

Part: PRESSURE SWITCH — DEFECTIVE (LEFT) · airframe 30,616 hrs · 38,414 cycles

IN CLIMBOUT THROUGH FL20, THE LEFT POWER LEVER WOULD NOT RESPOND TO THROTTLE INPUT. SWITCHED THE LEFT EEC TO MANUAL AND THE ENGINE REQUIRED POWER. SELECTED MANUAL ON THE RIGHT ENGINE EEC AND RETURNED TO DEN. REMOVED AND REPLACED LEFT 14,000 FT PRESSURE SWITCH IAW MM 73-23-01. OPS CHECK OF PRESSURE SWITCH GOOD AND ENGINE EEC OPS CHECK GOOD.

Part: BOOT — LEAKING (HORIZ STAB) · airframe 30,183 hrs · 37,844 cycles

VERTICAL FIN AND RIGHT OUTBOARD STAB DEICE BOOTS FAIL ON BOTH TIMERS. REMOVED & REPLACED RIGHT HORIZONTAL DEICE BOOT IAW EMB 30-10-00 & FAST BOOT INSTRUCTION. OPS CHECK GOOD.

Part: BOOT — LEAKING (HORIZ STAB) · airframe 30,159 hrs · 37,817 cycles

LEADING EDGE DEICE BOOTS FAILED (VERTICAL FIN AND RIGHT OB STAB) BOTH TIMERS. INSPECTED HORIZONTAL AND VERTICAL STAB. DEICE BOOTS. FOUND RIGHT OUTBOARD BOOT TO HAVE HOLE AND LEAKY PATCH. REPAIRED RIGHT OUTBOARD BOOT IAW 30-00-00. OPS CHECK GOOD.

Part: CONTROL CABLE — FAULTY (RT ENGINE) · airframe 30,159 hrs · 37,817 cycles

RIGHT POWER LEVER WOULD NOT RETARD TO FLIGHT IDLE IN CRUISE FL22.0 OAT-15. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN CHECK. INSPECTED CABLE FROM POWER LEVER AND ENGINE QUADRANT. CYCLED POWER LEVER SEVERAL TIMES. INSPECTED CABLE FROM ENGINE QUADRANT TO HMU. CABLE WAS TIGHT. REMOVED AND REPLACED CABLE ASSEMBLY IAW 76-10-02. OPS CHECK GOOD.

Part: WARNING LIGHT — ILLUMINATED (PAX DOOR) · airframe 3,927 hrs · 5,131 cycles

ON TAKEOFF, THE FORWARD DOOR LIGHT ILLUMINATED WITH ASSOCIATED AURAL WARNINGS, THE TAKEOFF WAS ABORTED. THE DOOR WAS CHECKED CLOSED AND THE FORWARD DOOR WARNING INDICATION WAS DEFERRED PER MX CONTROL 52-70-1C, MC 021.INSPECTED WIRING & MICRO SWITCHES FOR SECURITY. NO FAULTS FOUND. CLEANED AND LUBED FORWARD DOOR MICRO SWITCHES AS NEEDED. OPS CHECKS GOOD.

Part: COMPARATOR — FAULTY (COCKPIT) · airframe 28,900 hrs · 36,285 cycles

UPON ADDING TAKEOFF POWER CAPT'S EADI AND EHSI FAILED AND CAME BACK ON LINE. AFTER 100 PERCENT TORQUE AND DOUBLE CHECK OF ALL INSTRUMENTS, TAKEOFF ROLL WAS COMMENCED AND ABORTED AFTER CAPT EHSI CHANGED HDG FROM 250 TO 270 DEGREES. INSTALLED AND REORIENTED SERVICEABLE AHC-85 AND PERFORMED RUN UP TO 100 PERCENT TORQUE SEVERAL TIMES WITH NO ABNORMALITIES NOTED. S/N ON 1336, S/N OFF 1726. OPS CHECK GOOD.

Part: FLAP TRACK — DIRTY (T/E FLAPS) · airframe 28,538 hrs · 35,753 cycles

FLAPS WOULD NOT EXTEND TO 45 DEGREES INBOUND TO CARLSBAD. COMPLIED WITH QRH PROCEDURE FOR FLAP DISAGREEMENT. RETURNED TO LAX. EXAMINED FLAP TRACKS AND ROLLERS FOR OUTBOARD FLAPS AND CLEANED AS NEEDED. OPERATED FLAP SYSTEMS 12 TIMES IAW 27-50-00 AND OPS CHECK GOOD AT THIS TIME.

Part: TARGET — OUT OF ADJ (CARGO DOOR) · airframe 28,538 hrs · 35,753 cycles

CARGO DOOR LIGHT ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF. LIGHT GOES ON AND OFF INTERMITTENTLY. ADJUSTED STRIKER PLATE ON CARGO LIGHT SWITCH. CYCLED DOOR NUMEROUS TIMES. OPS CHECK GOOD.

Part: ACTUATOR — SEIZED (RUDDER TRIM) · airframe 28,207 hrs · 35,301 cycles

RUDDER TRIM FROZE IN ZERO POSITION IN FLIGHT. FLIGHT CONDITIONS VMC AT 7000 FEET. AFTER 10 MINUTES RUDDER TRIM WORKED FINE. INSPECTED RUDDER TRIMMING SYSTEM IAW EMB120 MM 27-23-00. WIPED MOISTURE FROM LINEAR ACTUATOR. RUDDER TRIM SYSTEM OPS CHECK GOOD.

Part: SIGNAL COND UNIT — FAILED (RIGHT) · airframe 27,799 hrs · 34,742 cycles

RIGHT TORQUE GAUGE WOULD NOT DROP BELOW 76 PERCENT TORQUE. ALL OTHER GAUGES WERE NORMAL. AFTER ABOUT 5 MINUTES, WHEN WE BEGAN DESCENT, LEFT PROP WENT TO FEATHER. TURNED OFF AUTOFEATHER SYSTEM AND EVERYTHING RETURNED TO NORMAL. DIDN'T SEE LEFT TORQUE EXCEED 104 PERCENT REPLACED RIGHT TORQUE SIGNAL CONDITIONER UNIT. FOUND TORQUE NOT TO EXCEED LIMITS 05-10-00. RAN ENGINES FOUND ENGINE AND AUTO FEATHER TO OPERATE NORMAL. OPS CHECKS SCU IAW MM 71-00-00. OPS CHECKS GOOD.PN ON: 30005-0000-57 SN ON: MM5055 SNOFF: 799

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 27,606 hrs · 34,505 cycles

MOMENTARY FLAP LIGHT ON MAP ASSOCIATED WITH FLAP RETRACTION IN AIR/GROUND. REPLACED INLINE HYDRAULIC FILTER FOR INBOARD FLAPS AS REQUIRED. OPS CHECK FAILED. REPLACED LEFT AND RIGHT INBOARD FLAP ACTUATORS IAW MM 27-50-07, EMB 120 MM RII 27-307. OPERATIONS CHECKS GOOD ON FLAP SYSTEM. P/N ON: RT 320300-1005, S/N ON: 0188, S/N OFF: 0109, P/N ON: LT 320300-1005, S/N ON: 1176, S/N OFF: 0723.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAP) · airframe 27,626 hrs · 34,535 cycles

INBOARD DISAGREEMENT ON FLAP RETRACTION. REPLACED FCU. OPERATED FLAPS SEVERAL TIMES, OPS CHECKS GOOD. P/N 307500-10175-1, S/N ON: 0160, S/N OFF: 0276.

Part: INDICATOR — FAILED (COCKPIT) · airframe 26,901 hrs · 33,581 cycles

ANALOG AND DIGITAL READING ON RIGHT NP GAUGE FAILED. RETURNED TO FAT. REMOVED AND REPLACED RIGHT NP GAUGE. OPS CHECKS GOOD. P/N ON: SEL-OC29DH, S/N: 511, S/N OFF: 123.

Part: FLAP — MALFUNCTIONED (LT WING)

FLAP ASYMMETRY LEFT OUTBOARD AFTER TAKEOFF. RETURNED TO PIH. RESET FLAP SYSTEM. CYCLED UP AND DOWN 5 FAULT FREE CYCLES. CHECKED FLAP TRACKS AND ROLLERS, CHECKED GOOD. COULD NOT DUPLICATE DISCREPANCY.

Part: TQ SIG COND — MALFUNCTIONED (RT ENGINE)

EXPERIENCED PLUS AND MINUS 10 TO 12 PERCENT TORQUE FLUCTUATIONS ON RIGHT ENGINE AT CLIMB POWER SETTINGS. FLUCTUATIONS CAUSED REDUCED POWER SETTINGS. RETURNED TO GJT. FLUCTUATIONS OCCURRED BETWEEN 8,500 FT AND 10,000 FT. REMOVED AND REPLACED THE TORQUE SIGNAL CONDITION UNIT IAW 77-11-1. RAN ENGINE AND OPS CHECKS GOOD.

Part: ACTUATOR — MALFUNCTIONED (RUDDER)

ON DEPARTURE OUT OF SLC, RIGHT RUDDER PEDAL STUCK AT APPROX ONE-HALF TRAVEL. RUDDER WOULD CENTER BUT WOULD NOT GO PAST ONE-HALF TRAVEL. FOLLOWED QRH AND UPON SELECTION OF BLUE RUDDER SYSTEM TO OFF, RUDDER TRAVEL WAS NORMAL. RETURNED TO SLC. REMOVED AND REPLACED RUDDER ACTUATOR FOR BLUE SYSTEM. LEAK CHECKS GOOD.

Part: EHSI — MALFUNCTIONED (LEFT COCKPIT)

CAPTAIN'S EHSI WILL NOT INITIALIZE THEN CORRECTED ITS SELF ON THE GROUND, BUT TWICE DISCONNECTED AUTOPILOT IN FLIGHT. WHEN NR 1 GYRO COMPUTER FLAG APPEARED NR 1 HSI LOST HEADING. RETURNED TO SLC. RERACKED NR 1 AHC85 AND REINITIALIZED REORIENTED. PERFORMED AHRS TEST CHECK OK.

Part: REGULATOR — FAILED (GREEN HYD SYST)

LOW LEVEL AND LOW PRESSURE LIGHT CAME ON GREEN SYSTEM. DECLARED AN EMERGENCY AND LANDED IN SLC WITHOUT INCIDENT. REPLACED HYDRAULIC HEAD PRESSURE REGULATOR AND DRAINED WATER FROM SYSTEM, OPS CHECKS GOOD.

Part: VALVE — FAILED (LT ENGINE)

LEFT ENGINE INLET DEICER INOP. ANNUNCIATION IN FLIGHT AND RETURNED TO SLC. REMOVED AND REPLACED LEFT ENGINE FLOW CONTROL VALVE IAW EMB 120 MM 30-10-04. OP, CHECK GOOD.

Part: RETRACT MECH — MALFUNCTIONED (TE FLAPS)

AFTER TAKEOFF FLAPS WOULD NOT RETRACT. CONTROL FAULT ON OVERHEAD ILLUMINATED. FLAP AND ADVANCED STALL WARNING LIGHT ON MAP. FOLLOWED QRH PROCEDURE. RETURNED TO FIELD COULDN'T DUPLICATE PROBLEM. CANNON PLUGS VISUALLY CHECKED GOOD AT OUTBOARD AND INBOARD ACTUATORS. OPS CHECKS GOOD.

Part: INDICATOR — MALFUNCTIONED (LT ENGINE)

LEFT ENGINE NL ON TAKEOFF SHOWED 110 PERCENT TO 115 PERCENT. RETURNED TO SLC. REPLACED LEFT HAND NL/NH INDICATOR. RAN ENGINE, OPS CHECKS GOOD.

Part: ACTUATOR — FAILED (RE FLAPS)

SELECTING FLAPS DOWN, NACELLES WOULD NOT EXTEND CAUSING DISAGREEMENT. WHEN FLAPS ARE RETRACTED THE INBOARDS LAG. CYCLED FLAPS SEVERAL TIMES ON GROUND AND UNABLE TO DUPLICATE. OHMED WIRE FROM CONTROL BOX TO ANNUNCIATOR, CHECKS GOOD. OHMED WIRING FROM CONTROL BOX TO ACTUATORS AND FOUND MEGA OHM READINGS ON ALL PINS FROM LEFT NACELLE ACTUATOR TO GROUND. DISCONNECTED PLUG AT ACTUATOR, READINGS CHECKS GOOD. REPLACED LEFT NACELLE FLAP ACTUATOR PER MM 27-50.

Part: SWITCH — MALFUNCTIONED (TE FLAPS)

AT 400 FT CALLED FOR FLAPS UP AND GOT FLAP ASYMMETRY INDICATION. RETURNED TO LAX. INSTALLED SERVICEABLE FLAP HANDLE ASSEMBLY. CYCLED FLAPS EXTENSIVELY WITH NO ASYMMETRY NOTED. OPS CHECKS GOOD.

Part: CONNECTOR — WATER CONTAM (RT TE FLAP)

RIGHT NACELLE FLAP DEPLOYED (UNCOMMANDED) AT 210 KTS ON APPROACH TO LAX. FOUND WATER IN RIGHT NACELLE FLAP ACTUATOR CANNON PLUG. CLEANED, RECONNECTED AND CYCLED FLAPS NUMEROUS TIMES. OPS CHECKS GOOD AT THIS TIME WITH NO FAULTS NOTED.

Part: ACTUATOR — FAILED (TE FLAPS)

FLAP SELECTION RESULTED IN NO DEPLOYMENT OF NACELLE FLAPS ON APPROACH. REPLACED RIGHT NACELLE FLAP ACTUATOR. ALL CHECKS GOOD WITH NO LEAKS NOTED.

Part: SEAT TRACK — CORRODED (CABIN)

AREA UNDER LAVATORY FLOOR PANEL SEAT TRACK IS SHOWING SIGNS OF CORROSION. REMOVED AND REPLACED BUTT STRAP UNDER LAVATORY WITH A NEW BUTT STRAP AIW MM 51-00-00.

Part: SILL — CORRODED (CABIN)

FLOOR SILL AGAINST WALL BEHIND LAVATORY HAS CORROSION. REMOVED FLOOR SILL AGAINST WALL BEHIND LAVATORY AND REPLACED WITH A NEW FLOOR SILL IAW MM 51-00-00.

Part: UPLOCK SWITCH — FAILED (RT MLG)

RIGHT MAIN GEAR WOULD NOT COME UP. SYSTEM-A TRANSIT LIGHT STAYED ILLUMINATED. CYCLED GEAR WITH NO EFFECT. RETURNED TO SMF. REPLACED RIGHT MAIN LANDING GEAR UPLOCK PROXIMITY SWITCH WITH A SERVICEABLE UNIT AND SWUNG GEAR NUMEROUS TIMES, OPS CHECKS GOOD.

Part: LUMINARE — BURN DAMAGE (CABIN LIGHT)

AIRCRAFT HAD REPORTED AN ELECTRICAL ODOR IN THE CABIN NEAR ROW 6. THE MECHANIC INSPECTED THE CABIN TO PINPOINT THE ORIGIN OF THE SMELL. HE FOUND A BURNT SPOT ON THE OVERHEAD PANEL ABOVE SEAT 5A. AFTER REMOVING THE PANEL, HE DISCOVERED A BURNT SOCKET ON THE LUMINARIES. THIS LUMINARY HAD SERVICE LETTER SL-BC5-0618-901-33-01 INSTALLED ON 8-31-96. THERE HAS BEEN NO MAINTENANCE PERFORMED IN THAT LOCATION SINCE THE INSTALLATION OF THE SERVICE LETTER. IN LATER DISCUSSION WITH THE MECHANIC ON THE CONDITION OF THE LAMP AND SOCKET WHEN DISCOVERED. IT WAS MENTIONED THE LAMP END WAS NOT DAMAGED OR DISCOLORED.

Part: CLIPS — BROKEN (RT WING)

RT WING RIB NR 15 HAS BROKEN CLIPS. REPLACED ALL BROKEN CLIPS ON RT WING RIB 15.

Part: CABLES — WORN (RT ELEVATOR)

RT ELEVATOR OUTBOARD AFT SECTION WORN. REMOVED AND REPLACED RT ELEVATOR OUTBOARD AFT CABLE. TIGHTENED CABLES.

Part: CLIPS — BROKEN (LT WING)

LT WING RIB NR 16 HAS BROKEN CLIPS. REMOVED AND REPLACED SIX WING SKIN SUPPORT BRACKET CLIPS ON RIB NR 16, LT WING.

Part: CLIPS — BROKEN (LT WING)

LT WING'S RIB NR 15 HAS BROKEN CLIPS. REMOVED AND REPLACED THREE WING SKIN SUPPORT BRACKET CLIPS ON RIB NR 15.

Part: LINEAR ACTUATOR — MALFUNCTIONED (RUDDER TRIM)

RUDDER TRIM CABLE INBOARD AFT SECTION WORN. INSTALLED RUDDER TRIM ACTUATOR AND ATTACHING CABLES. ADJUSTED CABLE TENSIONS TO 40 POUNDS.

Part: CLIPS — BROKEN (RT WING)

RT WING RIB NR 16 HAS BROKEN CLIPS. REPLACED ALL BROKEN CLIPS ON RT WING RIB 16.

Part: LINEAR ACTUATOR — MALFUNCTIONED (RUDDER TRIM)

RUDDER CABLE OUTBOARD AFT SECTION WORN. INSTALLED RUDDER TRIM ACTUATOR AND ATTACHING CABLES. ADJUSTED CABLE TENSIONS TO 40 POUNDS AND ALL WORKS NORMAL.

Part: FUEL LINE — FAILED (RT ENGINE)

ON TAKEOFF ROLL AT APPROX 60 KNOTS, THE RIGHT ENGINE FAILED. ABORTED TAKEOFF AND RETURNED TO GATE. FOUND OIL AND FUEL LEAKING FROM THE RIGHT ENGINE NACELLE. REMOVED AND REPLACED HMU FUEL LINE. GROUND RAN THE NR TWO ENGINE AT FULL POWER. LEAK AND OPERATIONALLY CHECKS GOOD.