N237SW

Part: LIGHT — DISCONNECTED (CABIN) · airframe 35,262 hrs · 48,300 cycles

THE FWD RED & FIRST TWO WHITE EMERGENCY FLOOR LIGHTS DO NOT ILLUMINATE. FLT 5498 RECONNECTED FWD FLOOR EMERGENCY LIGHT,

Part: FRAME — CRACKED (RT NACELLE) · airframe 34,488 hrs · 47,408 cycles

RIGHT ENGINE NACELLE FRAME ONE IS CRACKED AT OUTBOARD SIDE. (C-CHECK) REPLACED RIGHT ENGINE NACELLE FRAME ONE IN REFERENCE TO S/B.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 34,488 hrs · 47,408 cycles

PASSENGER DOOR ENTRANCE LOWER THRESHOLD INTERNAL ANGLE PIECE HAS CORROSION. (C-CHECK) REPLACED PASSENGER DOOR ENTRANCE LOWER THRESHOLD INTERNAL ANGLE IN REFERENCE TO 120 SRM.

Part: PROXIMITY SENSOR — FAILED (RT MLG) · airframe 34,477 hrs · 47,397 cycles

RIGHT MAIN GEAR "A" GREEN INDICATION STAYS ILLUMINATED WITH GEAR UP AND LOCKED. (FLT 5622) REPLACED RIGHT MLG DOWNLOCK "A" PROXIMITY SENSOR AND WIRING HARNESS IN REFERENCE TO AMM.

Part: HANDLE — DIRTY (CABIN DOOR) · airframe 34,434 hrs · 47,346 cycles

MAIN CABIN DOOR DIFFICULT TO OPERATE. (FLT 5511) CLEANED AND LUBED MAIN CABIN DOOR OUTER AND INNER HANDLES, AND LUBED BOTH FWD AND AFT HINGE ARMS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,542 hrs · 46,158 cycles

FORWARD FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE. (FLT 7811) RELAMPED EMERGENCY LIGHT.

Part: SIGN — BROKEN (CABIN) · airframe 33,090 hrs · 45,639 cycles

EMERGENCY "EXIT" SIGN AT ROW 6 FELL DOWN. (FLT 5568) REPLACED BROKEN EMERGENCY EXIT SIGN AT ROW 6.

Part: BRAKE — SEIZED (MLG) · airframe 32,820 hrs · 45,285 cycles

NR 4 MAIN WHEEL LOCKED UP. (SERVICE) REPLACED NR 4 BRAKE ASSEMBLY AND NR 4 & NR 3 MAIN WHEEL ASSEMBLIES. P/N 2-1661, S/N OFF 1491; NR 4 P/N 3-1544, S/N OFF 1700; NR 3 P/N 3-1544, S/N OFF 1508.

Part: BRAKE ASSY — SEIZED (NR 4) · airframe 32,779 hrs · 45,237 cycles

NR 4 MLG BRAKE ASSEMBLY SEIZED. (FLT 5421) REPLACED NR 4 BRAKE ASSEMBLY AND NR 4 MAIN WHEEL ASSEMBLY. P/N 2-1661, S/N OFF 1067 / P/N 3-1544, S/N OFF 0992

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,764 hrs · 43,979 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 3 OUT. (FLT 6471) RELAMPED EMERGENCY LIGHT.

Part: SPAR CAP — CRACKED (LT WING) · airframe 32,070 hrs · 44,357 cycles

LEFT WING FORWARD UPPER SPAR CAP CRACKED AT INBOARD WING TO NACELLE AREA. (C-CHECK) REPAIRED LEFT WING FORWARD UPPER SPAR CAP PER ETD2010-120/10844 AND ST51-900-1001.

Part: FITTING — CRACKED (RT NACELLE) · airframe 31,966 hrs · 44,239 cycles

RIGHT NACELLE WHEEL WELL INBOARD SIDE STRUCTURAL FITTING IS CRACKED. (C-CHECK) REPLACED RIGHT NACELLE WHEEL WELL INBOARD SIDE STRUCTURAL FITTING PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 31,164 hrs · 43,262 cycles

SEAT 9C EMERGENCY EXIT LIGHT BROKE. (FLT 6840) REMOVED AND REPLACED EMERGENCY LIGHT.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 31,164 hrs · 43,262 cycles

ONE WHITE LIGHT AT ROW 9 ON THE EMERGENCY FLOOR STRIP IS INOPERATIVE. (FLT 6678) REPOSITIONED BULB.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,183 hrs · 42,082 cycles

FOUR CABIN EMERGENCY FLOOR LIGHTS INOP. (FLT 7764) REPLACED EMERGENCY BATTERY PACK. P/N: D366-01-001, S/N ON: 843, S/N OFF: 437.

Part: CAP — LOOSE (EMERGENCY LIGHTS) · airframe 30,146 hrs · 42,037 cycles

FORWARD EMERGENCY LIGHTS INOP. (FLT 7772) TIGHTENED EMERGENCY LIGHT FUSE CAP.

Part: WIRE — BROKEN (CABIN) · airframe 29,418 hrs · 41,156 cycles

ROW NINE OVERHEAD EMERGENCY LIGHT INOP. (FLT 6236) REPLACED BROKEN WIRE (GND) IN OVERHEAD BIN SEAT 9BC.

Part: MANIFOLD — LEAKING (APU) · airframe 28,924 hrs · 40,499 cycles

STRONG FUEL SMELL IN CABIN. (FLT 6290)REPLACED APU FUEL NOZZLE MANIFOLD.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 28,602 hrs · 40,050 cycles

FLT 7803 - ROW 6 EMERGENCY LIGHTS INOP. NO DEFECTS FOUND.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 28,320 hrs · 39,686 cycles

FLT 5512 - BOTH AFT CEILING EMERGENCY LIGHTS INOP. RELAMPED.

Part: STRINGER — CRACKED (LT WING) · airframe 28,808 hrs · 40,337 cycles

C-CHECK, LEFT OUTBOARD WING STRINGER NR 10 CRACKED. REPAIRED PER IC 2009-120/01709.

Part: STRINGER — CRACKED (RT WING) · airframe 28,808 hrs · 40,337 cycles

C-CHECK, RT WING STRINGER CRACKED. REPAIRED PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 28,808 hrs · 40,337 cycles

C-CHECK, SHEAR CLIP BEHIND LEFT DV WINDOW CRACKED. REPLACED PER SRM.

Part: FRAME — CRACKED (LT NACELLE) · airframe 28,808 hrs · 40,337 cycles

C-CHECK, LEFT NACELLE FRAME NR 1 CRACKED. REPLACED PER SRM.

Part: ACTUATOR — MALFUNCTIONED (RUDDER) · airframe 27,624 hrs · 38,805 cycles

AFTER TAKEOFF, AT APPROXIMATELY 130 KTS, RIGHT RUDDER JAMMED (FLT 5416). REPLACED BLUE SYSTEM RUDDER ACTUATOR. VPN 308140-1003, S/N ON 0581, S/N OFF 0701.

Part: STRUCTURE — CRACKED (NACELLE FLAP) · airframe 27,369 hrs · 38,493 cycles

CRACK IN LEFT NACELLE FLAP. REPLACED LEFT NACELLE FLAP IAW EMB 120 MM 27-50-03.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 27,306 hrs · 38,409 cycles

LEFT WINDSHIELD SHATTERED DURING TAXI. FLIGHT 3418. REPLACED WINDSHIELD ASSEMBLY IAW 56-10-00. P/N: NP-151311-1, S/N OFF: 04114H2865.

Part: ACTUATOR — FAILED (LT MLG) · airframe 27,132 hrs · 38,193 cycles

FLT 3618 - RECEIVED A LEFT MAIN DISAGREEMENT LIGHT ON CLIMB-OUT. REPLACED LEFT MAIN LANDING GEAR ACTUATOR IAW 32-32-10. OPS AND LEAK CHECK GOOD.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 26,539 hrs · 37,466 cycles

FLT 5778 - LAV FIRE ALARM IS ACTIVATING INTERMITTENTLY. REPLACED LAV SMOKE DETECTOR. OPS CHECK GOOD.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 26,495 hrs · 37,414 cycles

FLT 3731 - ON FINAL DESCENT, AUTO PRESSURIZATION SYSTEM WENT INOP. REPLACED AUTO PRESSURIZATION CONTROLLER IAW 21-30-07, P/N 222DIT011400 S/N OFF 290.

Part: SIGN — BROKEN (EMERGENCY EXIT) · airframe 26,322 hrs · 37,234 cycles

FLT 3715 - EMERGENCY EXIT SIGN IS BROKEN AT ROW 6. REPLACED EXIT SIGN WITH A SERVICEABLE UNIT. OPS CHECK GOOD.

Part: RCCB — NOISY (COCKPIT) · airframe 25,913 hrs · 36,749 cycles

FLT 5740 - RCCB BEGAN TO CHATTER IN FLIGHT WITH A BURNING SMELL. INSPECTED AND OPERATED ALL RCCB'S IN LEFT SIDE PANEL. NO DEFECTS NOTED.

Part: ROD END — CORRODED (LT ELEVATOR) · airframe 25,369 hrs · 36,095 cycles

BOTH ROD ENDS ON AFT LEFT ELEVATOR TRIM TAB HORN ARE CORRODED AND WORN, FOUND AT C-CHECK. REPLACED BOTH ROD ENDS ON LEFT ELEVATOR TRIM TAB WITH SERVICEABLE UNIT IAW MM 27-32-00.

Part: SIGN — BROKEN (CABIN) · airframe 24,735 hrs · 35,297 cycles

FOUND MAIN CABIN DOOR EXIT PLACARD IS BROKEN. INSTALLED SERVICEABLE LENSE.

Part: MECHANISM — BINDING (PAX DOOR) · airframe 22,484 hrs · 32,478 cycles

MAIN CABIN DOOR COULD NOT BE OPENED FROM THE INSIDE. INSPECTED LATCH MECHANISMS ON PAX DOOR. NO DISCREPNACIES NOTED, CLEANED AND LUBED CAMS AND ASSOCIATED LINKAGES. PAX DOOR OPERATES NORMALLY.

Part: SERVO — MALFUNCTIONED (ELEVATOR) · airframe 22,227 hrs · 32,181 cycles

INFLIGHT WITH AUTOPILOT ON CAPT SIDE ACFT WOULD MOMENTARILY PITCH UP THEN QUICKLY BACK DOWN TO ORIGINAL FLIGHT ATTITUDE. REPLACED ELEVATOR SERVO AND ATTITUDE AND HEADING COMPUTER 1. OPERATIONAL CHECK IAW 22-10-00 GOOD. PN 622-6190-204 SN OFF 2738 PN 622-5734-002 SN OFF 1G57X.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,448 hrs · 29,710 cycles

EMERGENCY LIGHT OUT, LEFT SIDE 1ST WHITE ONE AT MAIN DOOR. RELAMPED EMERGENCY LIGHT, OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAP) · airframe 19,185 hrs · 27,797 cycles

FLAP DISAGREEMENT RETRACTING FLAPS ON GROUND. REMOVED AND REPLACED LEFT NACELLE FLAP ACTUATOR IAW EMB 120 MM 27-50-08. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 18,690 hrs · 27,021 cycles

RECEIVED FLAP CONTROL FAULT ON GROUND AFTER START UP WITH ASSOCIATED FLAP MAP AND OUTBOARD PAIR SECOND ROW (10 DEGREES) LIGHT FLASHING ON OVERHEAD PANEL. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR. OPERATIONAL CHECKS GOOD IAW EMB 120 MM 27-50-00.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAP) · airframe 18,659 hrs · 26,974 cycles

FLAP CONTROL FAULT ON OUTBOARD PAIR FLAPS IN CRUISE FLIGHT. REPLACED FCU. OPERATIONAL CHECKS GOOD.

Part: BRACKET — CRACKED (NACELLE) · airframe 18,549 hrs · 26,811 cycles

RT HYDRAULIC PACK VERTICAL MOUNT BRACKET IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INBOARD HALF OF VERTICAL MOUNT BRACKET ASSY PER SRM 51-40-02.

Part: CONTROL PANEL — MALFUNCTIONED (AUTO PILOT) · airframe 18,295 hrs · 26,437 cycles

AUTO PILOT, EITHER SIDE, WILL NOT HOLD ALTITUDE. REPLACED APP-65 WITH A SERVICEABLE UNIT. OPS CHECK GOOD.

Part: ANNUNCIATOR — MALFUNCTIONED (TE FLAPS) · airframe 17,954 hrs · 25,866 cycles

ON APPROACH AT 130 KIAS SELECTED FLAP 45, GOT FLAP LIGHT ON MAP WITH ASSOCIATED CONTROL FAULT FLAP WARNING INDICATION. FLAPS OPERATED NORMALLY ON GROUND. REPLACED FLAP ANNUNCIATOR WITH A SERVICEABLE UNIT. OP CHECK GOOD. S/N OFF: 0074.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 17,954 hrs · 25,866 cycles

CAPTAIN'S AP FAILS IN FLIGHT. REMOVED AND REPLACED AUTOPILOT NR 1 COMPUTER WITH SERVICEABLE UNIT. OPS CHECK GOOD IAW MM 22-10-00.

Part: HANDLE — MALFUNCTIONED (TE FLAP) · airframe 17,917 hrs · 25,808 cycles

FLAPS DO NOT RESPOND TO FLAP HANDLE. FLAP 15 SELECTED. FLAPS REMAIN UP. REMOVED FLAP HANDLE AND INSTALLED A SERVICEABLE UNIT. OPS CHECKS GOOD.

Part: BALLAST — FAILED (GALLEY) · airframe 17,866 hrs · 25,724 cycles

GALLEY LIGHT AND COFFEE POTS WENT OUT/INOP AND SMOKE WAS SMELLED IN CABIN. FOUND GALLEY BALLAST TO BE BAD. REMOVED AND REPLACED BALLAST IAW MM 25-30-04. OPS CHECK GOOD.

Part: TERMINAL — DAMAGED (EMERGENCY LIGHT) · airframe 17,822 hrs · 25,658 cycles

EXIT ROW 9 OVERHEAD BIN MOUNTED EMERGENCY EXIT LIGHT SIGN INOPERATIVE. REPAIRED WIRE TERMINAL IN OVERHEAD. OPS CHECKS OKAY.

Part: ACTUATOR — MALFUNCTIONED (TE FLAP) · airframe 17,716 hrs · 25,512 cycles

GREEN HYDRAULIC SYSTEM LOST ALL FLUID AFTER LANDING. NOTICED ASSOCIATED ALARMS AND LIGHTS. REPLACED RIGHT OUTBOARD ACTUATOR IAW AMM 27-53-05. OPS AND LEAK CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,595 hrs · 25,329 cycles

ONE OF TWO RED LIGHTS INOP AT FORWARD MAIN CABIN DOOR. REPLACED BULB AT INOP (RED) FORWARD FLOOR EMERGENCY LIGHTING STRIP. OPS CHECK GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 14,812 hrs · 20,994 cycles

LEFT SIDE AFT SECTION OF SEAT RAIL NEEDS TO BE REPLACED DUE TO CORROSION. REMOVED AND REPLACED SEAT RAIL IAW MM 53-01-05.

Part: ROLLER — CORRODED (T/E FLAP) · airframe 14,812 hrs · 20,994 cycles

LEFT OUTBOARD FLAP OUTBOARD ROLLER HAS CORROSION PITTING. REMOVED AND REPLACED OUTBOARD FLAP ROLLER IAW MM 27-50-12.

Part: ACTUATOR — OUT OF ADJ (LT MLG) · airframe 13,825 hrs · 19,509 cycles

LT MLG WOULD NOT RETRACT AFTER TAKEOFF. SYSTEM A&B LIGHTS INDICATED RED WITH GEAR HANDLE IN THE UP POSITION. RETURNED TO SMX. SHORTENED LEFT MAIN GEAR ACTUATOR ROD END 1/2 TURN. CYCLED GEAR MULTIPLE TIMES. OPS CHECKS GOOD.

Part: FAIRING — DEPARTED (AILERON) · airframe 12,380 hrs · 17,379 cycles

IN FLIGHT, FELT STRANGE VIBRATION FOR A FEW SECONDS. UPON CONDUCTING POST FLIGHT INSPECTION, FOUND A SECTION OF UPPER AILERON FAIRING MISSING. REMOVED DAMAGED LEFT AILERON UPPER FAIRING AND REPLACED WITH SERVICEABLE UNIT.

Part: PROBE — FAILED (LT ENGINE TORQUE) · airframe 11,819 hrs · 16,577 cycles

DURING TAKEOFF ROLL JUST AFTER TORQUE REACHED 80 PERCENT AND 100 PERCENT , FIRST OFFICER SAW TORQUE ON NR 1 (LEFT) ENGINE DROP. DIGITAL DROPPED TO 4 PERCENT AND ANALOG DROPPED TO 10 PERCENT BUT WAS FLUCTUATING. JUST AS TAKEOFF WAS ABORTED THE LEFT ENGINE LOST THRUST AND YAWED LEFT AS POWER WAS BROUGHT TO FLIGHT IDLE. ENGINE PARAMETERS APPEARED NORMAL ON TAXI BACK TO RAMP. INSTALLED SERVICEABLE TORQUE SIGNAL CONDITIONER. ALSO INSTALLED SERVICEABLE TORQUE PROBE. PERFORMED FULL POWER RUN. OPS CHECKS GOOD. S/N ON: 1730.

Part: SWITCH — OUT OF ADJ (CARGO DOOR) · airframe 11,636 hrs · 16,299 cycles

CARGO DOOR LIGHT AND AURAL WARNING ON TAKEOFF. ABORTED TAKEOFF. (DEFERRED CARGO DOOR LIGHT.) ADJUSTED FORWARD CARGO DOOR MICROSWITCH. OPS CHECK GOOD. PLACARD REMOVED.

Part: PUMP — FAILED (RT ENGINE) · airframe 11,218 hrs · 15,692 cycles

AFTER TAKEOFF, RIGHT ENGINE SURGING. TORQUE FLUCTUATION 10 - 15 PERCENT, NH FLUCTUATION. RETURNED TO SLC. REMOVED AND REPLACED THE HMU AND THE FUEL PUMP ON THE RIGHT ENGINE IAW EMB MM 73-21-00 AND RII 13-301. P/N ON: PUMP 3040627 HMU 786390-10, S/N ON: PUMP 1739M HMU M80201 P/N OFF: PUMP 5009986 HMU 786390-4 S/N OFF: PUMP 2572 HMU M80514.

Part: ACTUATOR — FAILED (LT MLG) · airframe 11,183 hrs · 15,644 cycles

AFTER TAKEOFF, LEFT MAIN LANDING GEAR RED LIGHT UNSAFE LIGHT WOULD NOT EXTINGUISH ASSOCIATED WITH CONTINOUS LOUD NOISE. WHEN LANDING GEAR HANDLE LOWERED OBSERVED GREEN GEAR SAFE INDICATION. REPLACED LEFT MLG ACTUATOR IAW MM 37-32-1. OPS AND LEAK CHECKS GOOD. P/N ON: 19597-000-07, S/N ON: 120, S/N OFF: 659

Part: LANDING GEAR — MALFUNCTIONED (LEFT) · airframe 11,146 hrs · 15,583 cycles

AFTER TAKEOFF, THE LEFT MAIN GEAR LIGHT REMAINED RED AND A VIBRATION WAS FELT IN THE AIR. RETURNED TO RDD. COULD NOT DUPLICATE PROBLEM. PERFORMED TEN GEAR SWING CYCLES. SYSTEM CHECKS OK.

Part: PCU — FAILED (RT ENGINE) · airframe 10,712 hrs · 14,990 cycles

AFTER TAKEOFF TORQUE FLUCTUATED AS MUCH AS 15 PERCENT CONTINUOUSLY RIGHT ENGINE. RETURNED TO FIELD. REPLACED RIGHT ENGINE PCU IAW MM 61-21-00 AND CARD RII 61-304. OPS CHECKS GOOD. P/N ON: 782490-46, S/N ON: 910985, S/N OFF: 890661.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,550 hrs · 14,779 cycles

LEFT HAND FLOOR EMERGENCY LIGHTING HAS ONE LIGHT OUT. RE-INSTALLED LEFT HAND FLOOR EMERGENCY LIGHTING BULB IAW MM 3351001, OPS CHECK GOOD.

Part: ACTUATOR — FAILED (LT MLG)

DURING GEAR RETRACTION, AFTER GEAR UP LIGHTS ARE OUT MOMENTARILY, LEFT MAIN INTRANSIT LIGHT CAME BACK ON. CYCLED GEAR AND ALL STAYED OUT NORMAL. RETURNED TO SLC, REPLACED LEFT MLG ACTUATOR PER MM 32-32-10. CYCLED GEAR AND INDICATION AND OPERATION CHECKS GOOD.

Part: WIRE — BROKEN (LT INTAKE)

INFLIGHT LEFT INTAKE DE-ICE INOP AND MULTIPLE WING AND STAB DE-ICE LIGHTS INOP CAME ON. RECYCLED AND CHANGED TIMERS BUT ALL STILL INOP. RETURNED TO LAX. CLEANED ALL EJECTORS AND CHECKED FOR LEAKS. ALL FOUND NORMAL. REPLACED RIGHT ENGINE EJECTOR DUE TO BROKEN WIRE. PERFORMED GROUND RUN FOR 20 MINUTES AND ALL CHECKS GOOD.

Part: RETRACT MECH — OUT OF ADJUST (LT MLG)

AT TAKEOFF ON GEAR RETRACTION, LEFT MAIN LANDING GEAR RED A AND B LIGHTS STAY ON. RECYCLED GEAR NO HELP. RETURNED TO SLC. FOUND UPLOCK HOOK/UPLOCK ACTUATOR CYLINDER ADJUSTMENT OFF. ADJUSTED ROLLER PER MM 32-32-09. OPS CHECKS GOOD.

Part: PROX SENSOR — FAILED (LT MLG)

AFTER DEPARTURE, RETRACTED GEAR, LEFT MAIN A AND B INDICATED RED GEAR NOT FULLY RETRACTED. RETURNED TO SLC. REMOVED AND REPLACED LANDING GEAR RELAY BOX AND REMOVED AND REPLACED LEFT MAIN LANDING GEAR UPLOCK A AND B PROXIMITY SENSOR PER MM 32-61-07. OPERATED GEAR. OPS CHECKS GOOD WITH NO FAULTS NOTED.

Part: VALVE — FAILED (CABIN)

AUTO AND MANUAL PRESSURIZATION INOP. RETURNED TO THE GATE IN SLC. REMOVED AND REPLACED ELECTRO/PNEUMATIC VALVE IAW MM 21-30-3. AUTO AND MANUAL PRESSURIZATION OPS CHECKS GOOD.

Part: CROSSBEAM — CORRODED (FWD LAVATORY)

FORWARD LAVATORY FLOOR CROSSBEAM CORRODED. REMOVED AND REPLACED FORWARD LAVATORY FLOOR CROSSBEAM IAW SRM 51-00-00.

Part: STRAP — CORRODED (CARGO COMPT)

CENTER BUTT STRAP IN FORWARD CARGO CORRODED. REMOVED AND REPLACED CENTER BUTT STRAP IN FORWARD CARGO IAW SRM 51-00-00.

Part: STRAP — CORRODED (CABIN)

RIGHT SIDE BUTT STRAP IN AFT CABIN AREA CORRODED. REMOVED AND REPLACED RIGHT SIDE BUTT STRAP IN AFT CABIN AREA IAW SRM 51-40-02.

Part: STRAP — CORRODED (CABIN)

CENTER BUTT STRAP IN AFT CABIN AREA CORRODED. REMOVED AND REPLACED CENTER BUTT STRAP IN AFT CABIN AREA IAW MM 51-00-00.

Part: UPLOCK CAM — DAMAGED (RT MLG DOOR)

AFTER DEPARTURE UPON BRINGING GEAR HANDLE TO UP POSITION, BOTH A AND B INTRANSIT LIGHTS ILLUMINATED FOR RT MAIN, ACCOMPANIED BY LOUD RUMBLE. RETURNED TO FIELD. FOUND GEAR UPLOCK CAMS AND FORWARD PART OF RIGHT GEAR DOORS TO BE IN POOR CONDITION AND BINDING. RECONDITIONED HOOK AND ROLLERS, INSPECTED REST OF LANDING GEAR SYSTEM IAW MM 32. ALL ELSE FOUND GOOD. PERFORMED SEVERAL GEAR SWINGS WITH NO PROBLEMS NOTED.

Part: AHC 85 — MALFUNCTIONED (RIGHT)

FIRST OFFICER'S HSI OSCILLATES MORE THAN 60 DEGREES WITH HDG FLAG ANNUNCIATED. RMI ON CAPTAIN'S SIDE SIMULTANEOUSLY FLAGGED. RETURNED TO LAX. SWAPPED AHC 85 SIDE TO SIDE FOR TROUBLESHOOTING AND PROBLEM FOLLOWED. SWAPPED BACK AND REPLACED NR 2 AHC 85. REORIENTED AND OPS CHECKS GOOD.

Part: PRESSURE SWITCH — FAILED (LT PROP)

LEFT PROPELLER DE-ICE INOP LIGHT REMAINS ILLUMINATED WHEN SYSTEM IN USE IN BOTH TIMER 1 AND TIMER 2. RETURNED TO FIELD AFTER TAKEOFF. REMOVED AND REPLACED LEFT OIL PRESSURE SWITCH, OPS AND LEAKS CHECKS GOOD.