N212SW

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 33,814 hrs · 41,844 cycles

FLOOR LEVEL EMERGENCY LIGHTS AT AFT -E- EXIT AFT RED LIGHT DOES NOT ILLUMINATE AND FIRST WHITE LIGHT AFT OF OVERWING EXIT DOES NOT ILLUMINATE. RELAMPED AFT RED LIGHT AND FIRST WHITE LIGHT AFT OF OVERWING EXIT AS REQUIRED. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 33,709 hrs · 41,723 cycles

FOUND FLOOR LEVEL EMERGENCY LIGHT INOP BEHIND ROW 6 (WHITE). INSTALLED A NEW LAMP IN THE LIGHT ASSY, OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 33,709 hrs · 41,723 cycles

ONE FLOOR LEVEL EMERG. LIGHT INOP AT SEAT 9 (RED).INSTALLED A NEW LAMP IN THE LIGHT ASSY. OPERATIONAL CHECK GOOD.

Part: LINKAGE — BINDING (PAX DOOR) · airframe 33,709 hrs · 41,723 cycles

FOUND MAIN CABIN DOOR VERY DIFFICULT TO OPEN FROM INSIDE. LUBED DOOR LINKAGE, OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAP) · airframe 33,540 hrs · 41,489 cycles

LEFT NACELLE FLAP DISAGREE. REPLACED THE LEFT NACELLE FLAP ACTUATOR IAW MM 27-50-08. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 33,345 hrs · 41,209 cycles

AFT CABIN EMERGENCY LIGHTS GO DIM DURING TEST (INOP). REPLACED AFT ELBP. OPERATIONAL CHECK GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 33,280 hrs · 41,113 cycles

EXIT LIGHTS AT SEATS 5A AND 5C DO NOT ILLUMINATE. INSTALLED SERVICEABLE BATTERY MIDDLE POSITION, OPERATIONAL CHECK GOOD.

Part: SIGN — MISSING (CABIN) · airframe 32,873 hrs · 40,579 cycles

EXIT SIGN AT 6C MISSING. REPLACED EXIT SIGN AT 6C AS REQUIRED.

Part: ANNUNCIATOR — MALFUNCTIONED (TE FLAPS) · airframe 32,625 hrs · 40,266 cycles

CREW REPORTS FLAP CONTROL FAULTS DURING FLAP MOVEMENT. REPLACED FLAP ANNUNCIATOR ASSY. OPERATIONAL CHECK GOOD IAW EMB MM 27-50-05.

Part: ACTUATOR — FAILED (NACELLE FLAPS) · airframe 32,560 hrs · 40,191 cycles

RIGHT NAC FLAP HYD FAILURE. INSTALLED HYDRAULIC ACTUATOR ON RT NACELLE FLAP. OPERATIONAL CHECKS ARE GOOD IAW 27-50-00.

Part: SERVO — MALFUNCTIONED (RUDDER) · airframe 31,156 hrs · 38,355 cycles

RUDDER PEDAL BINDING TO THE LEFT. REMOVED AND REPLACED RUDDER SERVO IAW EMB MM 22-10-05. OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (RUDDER) · airframe 31,156 hrs · 38,355 cycles

RIGHT RUDDER JAMMED AFTER TAKEOFF. REMOVED AND REPLACED RUDDER PCU IAW 27-22-01.

Part: HMU — MALFUNCTIONED (LT ENGINE) · airframe 29,876 hrs · 36,683 cycles

DURING CRUISE, PARTIAL POWER LOSS ON LEFT ENG. FUEL FLOW AROUND 70, TORQUE SHOWING 0 AND REDUCED T6, NP NH AND NL VALUES. NO MAP LIGHTS. REMOVED LEFT HMU AND INSTALLED A SERVICEABLE UNIT, IAW MM 73-21-00 AND RII CARD 73-301. OPS CHECKS GOOD.

Part: ACTUATOR — MALFUNCTIONED (RUDDER) · airframe 29,470 hrs · 36,172 cycles

ON TAKEOFF ROLL FIRST OFFICER EXPERIENCED A STIFF RIGHT RUDDER INPUT THEN A TEMPORARY FREEZE (STOP) THEN UNCOMMANDED LEFT RUDDER INPUT/BUMP. ALL SYSTEMS OK DURING FLIGHT. REPLACED GREEN SYSTEM RUDDER ACTUATOR IAW MM 27-22-02. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 29,184 hrs · 35,816 cycles

F/O'S YAW SYSTEM DISENGAGES. REPLACED NR 2 AUTOPILOT COMPUTER IAW MM 22-10-02. OPS CHECK GOOD.

Part: FRAME — CRACKED (RT NACELLE) · airframe 29,076 hrs · 35,700 cycles

RIGHT NACELLE FRAME NR 1 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT NACELLE FRAME NR 1 IAW SB 120-54-0036 PART 2. C/W CARD RII 54-301.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 28,792 hrs · 35,349 cycles

F/O AUTO PILOT COMMAND BARS WENT DOWN (PITCH), ALSO ATTITUDE INDICATOR F/O SIDE SHOWED 15 DEGREES CLIMB. A/C FOLLOWED F/O COMMAND BARS AND PITCHED DOWN. DISCONNECTED A/P. REMOVED AND REPLACED NR 2 AUTOPILOT COMPUTER APC 65B. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,184 hrs · 34,586 cycles

EMERGENCY LIGHTS ''EXIT'' SIGNS ROW 6 ILLUMINATE ONLY VERY BRIEFLY THEN EXTINGUISH. REMOVED AND REPLACED ROW 6 BATTERY PACK. OPS CHECK GOOD ON EMERGENCY LIGHTS.

Part: GCU — INOPERATIVE (RT GENERATOR) · airframe 27,553 hrs · 33,819 cycles

AFTER TAKEOFF, RIGHT GEN LOAD RESET DROPPING OFF AND COMING BACK ON WITH A SINGLE CHIME AND ELEC LIGHT ON MAP. DEF RIGHT GEN PER MEL 24-30-1. REMOVED AND REPLACED NR 2 GCU IAW 24-30-02. OPS CHECK GOOD. P/N: 51539-014A, S/N OFF: 96545, S/N ON: 5272.

Part: SWITCH — MALFUNCTIONED (CABIN PRESSURE) · airframe 27,473 hrs · 33,726 cycles

PRESSURIZATION COULD NOT KEEP CABIN BELOW 12000 FT ON CLIMBOUT WITH APU BLEED. F/A REPORTED SMOKE AND ODOR AT REAR OF CABIN JUST AFTER TURNBACK TO GJT. AT 16-17K AND ABOVE THE MAIN CABIN DOOR PRODUCED AN AIR LEAK. RETURNED TO GJT. REMOVED AND REPLACED RATE/MANUAL DUMP SWITCH. PRESSURE CHECKED AIRCRAFT IAW MM 21-30-00 USING TEST BENCH TO 4 PSID. CHECKED PRESSURIZATION ON GROUND WITH APU ONLY. CHECKED PRESSURIZATION ON GROUND WITH BOTH ENGINES IAW MM 21-30-00. OPS CHECKED ON GROUND GOOD. P/N OFF: MS27788-21P.

Part: CONNECTOR — LOOSE (TORQUE SIGNAL CO) · airframe 27,275 hrs · 33,477 cycles

ON TAKEOFF RECEIVED AN AUTOFEATHER WARNING. ABORTED THE TAKEOFF AND RETURNED TO THE GATE. FOUND CONNECTOR ON LT ENGINE TORQUE SIGNAL CONDITIONER LOOSE. RE-TIGHTENED, RAN AND OPS CHECKS GOOD.

Part: ACTUATOR — FAILED (RUDDER) · airframe 26,755 hrs · 32,856 cycles

RIGHT RUDDER PEDAL JAMMED AFTER TAKEOFF. RETURNED TO RAP. PERFORMED RUDDER SYSTEM HEALTH CHECK PER MM 27-22-00. FOUND BLUE SYSTEM RUDDER ACTUATOR BAD. REMOVED AND REPLACED BLUE SYSTEM ACTUATOR IAW MM 27-22-02. OPS CHECK AND LEAK CHECK GOOD. CLOSED AND SECURED ALL PANELS.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 26,653 hrs · 32,733 cycles

''HIGH SPEED'' AURAL WARNING SOUNDED ON TAKEOFF ROLL AT ABOUT 80 KNOTS. ABORTED TAKEOFF & RETURNED TO GATE. REPLACED CAPT'S AIRSPEED INDICATOR IAW MM 34-12-01. OPS AND LEAK CHECKS GOOD.

Part: GUIDE — BENT (T/E FLAP) · airframe 26,585 hrs · 32,653 cycles

RIGHT OUTBOARD FLAP ROLLER GUIDE BENT. INSTALLED NEW BRACKET FOR INBOARD ROLLER, RT OUTBOARD FLAP MOVEABLE CHANNEL. OPERATED FLAPS. OPS CHECK GOOD AT THIS TIME.

Part: CONNECTOR — LOOSE (LT ENGINE) · airframe 25,714 hrs · 31,616 cycles

LEFT T6 GAUGE ERRATIC AND INTERMITTENT ON BOTH THE DIGITAL AND ANALOG DISPLAYS. RETURNED TO SLC. FOUND LEFT ENGINE T6 CONNECTION LOOSE. RETORQUED NUTS AND COMPLIED WITH ENGINE RUN. OPS CHECK GOOD.

Part: RELAY — FAILED (INDICATOR) · airframe 25,142 hrs · 30,939 cycles

ABORTED TAKEOFF DUE TO AUTOFEATHER AURAL WARNING AND NO GREEN ARMED LIGHT. SUBSEQUENT RUN UP PRODUCED NO GREEN ARMED LIGHT. REF WDM 61-23-00 REPLACED RELAY K0161 - ARMED INDICATOR RELAY. OPS CHECKS PER MM 61-23-26. AUTOFEATHER SYSTEM TEST WITH ENGINE RUNNING AND WITH ENGINE NOT RUNNING. OPS CHECK GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 25,113 hrs · 30,903 cycles

ON TAKEOFF ROLL, TAKEOFF AURAL WARNING AUTO FEATHER SOUNDED. AUTO FEATHER SWITCH IS ON POSITION. INSPECTED RELAY K0161 RECEPTACLE AND PERFORMED EXTENSIVE RUNS. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 24,992 hrs · 30,749 cycles

LEFT DEICE LIGHT INOP. FLYING INTO ICING CONDITIONS, DIVERTED TO SMF. RELAMPED THE LEFT DEICE LIGHT. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (NR 1) · airframe 24,992 hrs · 30,749 cycles

RUDDER TRIM INEFFECTIVE WITH YAW ENGAGED. RUDDER KICKS OVER WHEN DISENGAGED. REPLACED NR 1 AHRS. SYSTEM OPS CHECKS GOOD IAW 22-10-00/34-25-00. P/N ON 622-6190-214, S/N ON 1359, S/N OFF 2792.

Part: TARGET — OUT OF ADJ (NLG) · airframe 24,863 hrs · 30,569 cycles

UPON GEAR RETRACTION A FLUTTERING VIBRATION WAS HEARD. NOSE GEAR RED A & B CIRCUITS LIGHTS WERE BOTH ILLUMINATED. CYCLED GEAR DOWN AND RETURNED TO LAND AT SGU. ADJUSTED NOSE LANDING GEAR UPLOCK TARGETS. SWUNG GEAR SEVERAL TIMES IAW MM 32-30-00. OPS CHECK GOOD AT THIS TIME.

Part: CONTROL PANEL — FAILED (AUTOPILOT SYS) · airframe 23,704 hrs · 29,164 cycles

AIRCRAFT NOSE PITCHES DOWN ABNORMALLY FAST AND STEEP WHEN USING THE A/P ROCKER SWITCH TO NOSE DOWN. NORMAL PITCH CHANGE WHEN ROCKING UP. DEFERRED PER MEL 22-11-1, MC 021. REMOVED AND REPLACED APP-65A CONTROL PANEL. SYSTEM OPS CHECK GOOD IAW EMB120 MM CHAPTER 22-10-04.P/N: 622-6684-006 S/N ON: 2255 S/N OFF: 1689.

Part: BOOT — FAILED (LT ENGINE) · airframe 23,704 hrs · 29,164 cycles

LEFT ENGINE INTAKE BOOT FAILED ON CLIMB OUT. RETURNED TO SLC. REMOVED LEFT ENGINE INLET AND INSTALLED UNIVERSAL COWL ON LEFT ENGINE IAW BR124B-71. OPS CHECK GOOD.

Part: ROLLER — WORN (T/E FLAP) · airframe 23,587 hrs · 29,025 cycles

AFTER T/O WHEN SELECTING FLAPS UP, OUTBOARD PAIR DISAGREEMENT WOULD NOT CLEAR AFTER QRH PROCEDURE. RETURNED TO SLC. TROUBLESHOOT SYSTEM, FOUND LEFT OUTBOARD FLAP TRACKS AND ROLLERS WORN. REMOVED AND REPLACED (4) FLAP ROLLERS, (3) FLAP TRACKS. ROLLER P/N PE61026-1 IAW EMB 120 MM 27-50-12. P/N ON 120-33507-0035, P/N OFF 120-33045-501. P/N ON 120-33045-501, P/N OFF 120-333501-003. P/N ON 120-33018-001, P/N OFF 120-3304-001.

Part: ACTUATOR — DEFECTIVE (T/E FLAP) · airframe 23,528 hrs · 28,949 cycles

FLAP ASYMMETRY ON OUTBOARD PAIR OF FLAPS ON FLAP RETRACTION DEPARTING CODY. FOLLOWED QRH, CYCLED FLAPS AND PROBLEM CORRECTED. CONTINUED ON TO SLC. REMOVE AND REPLACE LEFT OUTBOARD FLAP ACTUATOR. OPS CHECKS GOOD. P/N ON 343000-1003, S/N ON 0520, S/N OFF 0244.

Part: SERVO — DEFECTIVE (RUDDER) · airframe 23,571 hrs · 29,004 cycles

IN CRUISE FLIGHT, WITH AUTOPILOT ON, EXPERIENCED A SUDDEN YAW MOVEMENT AND BALL WENT OUT OF CENTER. RETRIMMED WITH NO PROBLEMS. THEN IN DESCENT, WITH AUTOPILOT OFF, NOTICED TRIM WOULD NOT CENTER BALL. THEN 2 OR 3 MINUTES LATER THERE WAS ANOTHER SUDDEN YAW. AP WAS OFF ON DESCENT, BUT YAW DAMPER WAS ON THROUGHOUT FLIGHT. FERRIED TO SLC FOR MAINTENANCE. REPLACED RUDDER TRIM SERVO IAW MM 32-10-05. OPS CHECKS GOOD. P/N, S/N ON 8092, OFF 5875.

Part: BOOT — FAILED (ANTI-ICE SYS) · airframe 23,310 hrs · 28,691 cycles

RIGHT INBOARD STABILIZER BOOT FAILS IN BOTH TIMERS 1 AND 2 IN BOTH THE HEAVY AND LIGHT POSITIONS. RETURNED TO SLC. REMOVED AND REPLACED LEFT WING INBOARD DEICE BOOT IAW MM 30-10-00 AND RII 30-301. OPS CHECK GOOD. P/N ON P29S-705135-25, S/N ON MP19510, S/N OFF MB26310.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,215 hrs · 28,572 cycles

AFT EMERGENCY LIGHTS DO NOT TEST. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY PACK IAW 33-50-02. OPS CHECKS GOOD. P/N D366-04-001, S/N OFF 891 ON 1166.

Part: HARNESS — DAMAGED (LT MLG) · airframe 22,679 hrs · 27,943 cycles

LEFT MAIN GEAR INDICATION LIGHT (A) WOULD NOT EXTINGUISH. RECYCLED GEAR BUT UNABLE TO GET A THREE GREEN INDICAITON. GEAR WOULD NOT DROP UNTIL ELECTRICALLY OVERRODE LANDING GEAR. RETURNED TO SLC. REMOVED AND REPLACED LEFT MAIN LANDING GEAR A-HARNESS IAW MM 32-61-01. OPS CHECKS GOOD. P/N ON: 120-41127-001

Part: CONNECTOR — CONTAMINATED (TE FLAP ACTUATOR) · airframe 22,381 hrs · 27,607 cycles

ON DEPARTURE FROM SLC THE FLAPS WOULD NOT RETRACT PROPERLY. THE OUTBOARD PAIR STAYED AT THE 2 LIGHT BAR POSITON. PERFORMED QRH PROCEDURE FOR DISAGREEMENT AND THEY WOULD NOT RETRACT. RETURNED TO SLC AND FLAPS FUNCTIONED NORMALLY FOR LANDING. FOUND DEICE FLUID IN OUTBOARD CANNON PLUG. CLEANED CANNON PLUGS OF OUTBOARD AND INBOARD ACTUATOR. OPERATED FLAPS SEVERAL TIMES. FLAPS CHECKED GOOD.

Part: INDICATOR — FAILED (NAV SYSTEM) · airframe 21,799 hrs · 26,925 cycles

NUMBER TWO NAV SYSTEM FAILED INFLIGHT. ''''NAV'''' FLAG WITHOUT IDENT FEATURE ON ALL VOR AND ILS FREQUENCIES. RETURNED TO SLC. INSTALLED SERVICEABLE VIR-32 NAV BOX IAW MM 34-54-00. NUMBER TWO NAV SYSTEM OPS CHECKS GOOD. (S/N 14919) ON, (S/N 10605) OFF.

Part: SEAL — LEAKING (PAX DOOR) · airframe 21,730 hrs · 26,850 cycles

AT CRUISE ALTITUDE OF 24,000 FEET CABIN BEGAN TO DEPRESSURIZE AT 2000 + FT/MIN. EXECUTED EMERGENCY DESCENT TO LOWER ALTITUDE AND THEN FOLLOWED QRH PROCDURE. AT LOWER ALTITUDE CABIN BEGAN TO REPRESSURIZE. COMPLIED WITH CABIN PRESSURIZATION LEAK DOWN CHECK IAW MM 21-30-00. VISUAL CHECK OF ALL DOOR SEALS FOR DAMAGE AND CONDITION. ALL CHECKS GOOD IN MANUAL MODE.

Part: INDICATOR — MALFUNCTIONED (RT ENGINE TORQUE) · airframe 21,469 hrs · 26,544 cycles

TORQUE METER RIGHT SIDE INDICATES 180 PERCENT DURING TAKEOFF. ABORTED TAKEOFF. SWAPPED LEFT AND RIGHT TORQUE METERS. PERFORMED TWO POWER RUNS. OPS CHECKS NORMAL DURING BOTH RUNS.

Part: WARNING SYSTEM — ACTIVATED (AUTO FEATHER) · airframe 21,314 hrs · 26,377 cycles

AT TAKEOFF AUTO FEATHER AURAL WARNING SOUNDED. ABORTED TAKEOFF. RAN BOTH ENGINES IAW MM 71-00-00 AND 61-00-00. THE AUTO FEATHER SYSTEM OPS CHECKED GOOD. IAW MM 61-23-20. ALSO, INSPECTED WIRING ON BOTH ENGINES. NO DISCREPANCIES NOTED AT THIS TIME.

Part: ROLLER — SEIZED (RT TE FLAP)

AFTER TAKEOFF FROM SUN, OUTBOARD PAIR OF FLAPS DISAGREED WITH OTHERS. SLIGHT CONTROLABILITY PROBLEM. AFTER RUNNING QRH PROCEDURES, FLAPS WERE STILL DOWN. DIVERTED TO TWF. INSPECTED RIGHT OUTBOARD FLAP. FOUND OUTBOARD UPPER ROLLER SEIZED. SPRAYED PENETRATING FLUID ON ROLLER AND WORKED ROLLER FREE. CYCLED FLAPS FIVE TIMES WITH NO FAULTS.

Part: HSI — MALFUNCTIONED (LEFT)

LEFT SIDE TOTAL F/S FAILURE, ADI AND GYRO FLAG HSI, HDG DISPLAY. DIVERTED FROM RNO TO SLC. REPLACED AHC 85 ON LEFT SIDE. OPS CHECKS GOOD.

Part: DEICE SYST — MALFUNCTIONED (LT & RT PROP)

DURING CLIMBOUT, EXPERIENCED SEVERE ICING AND SIGNIFICANT VIBRATION ON PROPS. ADJUSTED PROP RPM SEVERAL TIMES, VIBRATION CONTINUED. DESCENDED INTO WARMER AIR AND THE ICE MELTED AND OPS WERE NORMAL. RETURNED TO SLC. INSPECTED SURFACE DEICE AND PROP DEICE. PERFORMED OPERATIONAL CHECK OF ALL DEICE SYSTEMS, ALL CHECKS NORMAL. TESTED IAW 30 AND 30-60-00.

Part: PCU — LEAKING (LT PROP)

LEFT OIL PRESSURE DROPPED BETWEEN 52 AND 45 PSI IN FLIGHT. RETURNED TO SLC. FOUND THE PCU TO BE LEAKING OIL. REMOVED AND REPLACED PCU. RAN THE LEFT ENG IAW MM 71-00-00 AND 61-00-00. OPS AND LEAK CHECK GOOD.

Part: CONTROLLER — MALFUNCTIONED (CABIN)

AIRCRAFT WOULD NOT PRESSURIZE IN EITHER MANUAL OR AUTO. RETURNED TO SLC. REPLACED PRESSURIZATION CONTROL. PRESSURIZED AIRCRAFT, OPS CKS GOOD.

Part: CURRENT SENSOR — FAILED (AOA HEATER)

AFTER TAKEOFF, RIGHT AOA HEATER CIRCUIT BREAKER POPS. RETURNED TO SLC. REMOVED AND REPLACED RIGHT CURRENT SENSOR ASSEMBLY. TESTED AOA IAW MM 30-32. OPS CHECKS GOOD.

Part: SERVO — JAMMED (AUTO PILOT)

RUDDER PEDALS LOCKED DURING APPROACH AND LANDING. WAS ABLE TO REGAIN CONTROL WITH TILLER ON THE RUN WAY. FOUND RUDDER SERVO JAMMED. REPLACED RUDDER SERVO. OPS CHECKS GOOD.

Part: SEAL — FAILED (CARGO DOOR)

CLIMBING THROUGH F230, CABIN ALTITUDE STARTED A 2500-3500 MINUTE CLIMB. SWITCHED TO MANUAL, NO HELP. CABIN CONTINUED CLIMB. PERFORMED DESCENT, MASKS FELL. LANDED UNPRESSURIZED. NO DOOR LIGHTS NO OTHER UNUSUAL WITH A/C PERFORMANCE. FOUND CARGO DOOR SEAL BLOWN OUT ON LOWER SIDE OF CARGO DOOR. REPLACED BENT RETAINING STRIP FOR CARGO DOOR SEAL.

Part: RUDDER LIGHT — ILLUMINATED (COCKPIT)

RUDDER LIGHT ON MAP ASSOCIATED WITH RUDDER OVER BOOST ON OVER HEAD ILLUMINATED IN FLIGHT. RETURNED TO SLC. PERFORMED RUDDER OVER BOOST TEST IAW MM 27-22-00. INSPECTED IAW FAULT ISOLATION MANUAL 27-24-90 WITH PITOT STATIC PRESSURE. NO FAULT FOUND AT THIS TIME. OPS CHECKS GOOD.

Part: PACK — MALFUNCTIONED (LEFT)

ON TAKEOFF LEFT BLEED OVERHEAT ILLUMINATED AND EXTREMELY HOT AIR CAME OUT OF AIR CONDITIONING VENTS AND BLEED EYELETS. RETURNED TO SLC. OPERATED BOTH PACKS FROM APU BLEED. NO FAULT FOUND. PACKS OPERATE NORMAL.

Part: ANTENNA — CORRODED (NR 2 TRANSPONDER)

REMOVE NR 2 TRANSPONDER ANTENNA DUE TO CORROSION. REMOVED AND REPLACED NR 2 TRANSPONDER ANTENNA, OPS CHECKS GOOD.

Part: PROX SWITCH — FAILED (LT MLG)

AFTER DEPARTURE WITH GEAR HANDLE IN UP POSITION, LEFT MAIN GEAR INTRANSIT LIGHT A-SYSTEM ILLUMINATED, ACCOMPANIED BY RUMBLING NOISE. CYCLING GEAR DUPLICATED PROBLEM. RETURNED TO FIELD. REPLACED LEFT GEAR UPLOCK A-PROX SWITCH, OPS CHECKS GOOD.

Part: ACTUATOR — FAILED (LT MLG)

AFTER DEPARTURE, LEFT MAIN LANDING GEAR WOULD NOT RETRACT. GEAR DOORS SEEMED TO BE OPEN, BUT NOT CLOSING. LANDING GEAR CAME DOWN WITHOUT ANY PROBLEM. REPLACED LEFT GEAR ACTUATOR AND LEFT GEAR SHUTOFF VALUE IAW MM 32-32-11, OPS CHECK AND LEAK CHECK GOOD.

Part: LATCH MECH — MALFUNCTIONED (NLG)

NOSE LANDING GEAR WOULD NOT CYCLE UP AND RED TRANSIENT 'A' AND 'B' LIGHTS STAYED ON. JACKED AIRCRAFT AND INSPECTED GEAR DOORS AND LATCHING MECHANISMS, FOUND NO DEFECTS. CYCLED GEAR NUMEROUS TIMES IN HANGER, ALL CHECKS NORMAL. DID FIND LANDING GEAR LT HAND DOOR LATCH DISCONNECTED AFTER GOING BACK TO GATE AND INSPECTING. DOOR WAS HANGING DOWN. RELATCHED DOOR.

Part: SEQUENCE VALVE — FAILED (RT MLG)

AFTER TAKEOFF, RIGHT MAIN GEAR WOULD NOT RETRACT AND RED LIGHT STAYED ON. TOWER VERIFIED THAT GEAR DID NOT RETRACT. REPLACED RIGHT MAIN LANDING GEAR OUTBOARD SEQUENCE VALVE. CYCLED GEAR SEVERAL TIMES, OPS CHECK GOOD AND TEST FLIGHT SATISFACTORY.

Part: PROX SENSOR — FAILED (NLG)

AFTER TAKEOFF AT LAX, NOSE GEAR WOULD NOT COME UP. CYCLED GEAR SEVERAL TIMES AND GEAR WOULD NOT CYCLE UP OR DOWN. ELECTRICALLY OVERRIDED GEAR SUCCESSFULLY AND RETURNED TO LAX WITHOUT INCIDENT. REPLACED A-SYSTEM DOWN INDICATION PROXIMITY SENSOR. CYCLED GEAR SEVERAL TIMES, OPS CHECK GOOD.

Part: CONTROL CABLE — WORN (RUDDER)

RT RUDDER INBD AFT CABLE WORN. REPLACED RT RUDDER INBD AFT CABLE PER MM 27-00-01.

Part: CONTROL CABLE — WORN (RUDDER)

RT RUDDER AFT OUTBD CABLE WORN. REPLACED RT RUDDER OUTBD AFT CABLE PER MM 27-00-01.

Part: CLIPS — CRACKED (LT WING)

LT WING RIB 15 HAS THREE CRACKED WING SUPPORT CLIPS. REPLACED 3 WING SUPPORT CLIPS ON LT WING RIB 15, IAW SB 120-57-0031.

Part: CLIPS — CRACKED (RT WING)

RT WING RIB 16 HAS 2 CRACKED WING SUPPORT CLIPS ON BOTTOM. REPLACED 2 WING SUPPORT CLIPS ON RT WING RIB 16 IAW SB 120-57-0031.

Part: CLIPS — CRACKED (RT WING)

RT WING RIB 15 HAS 3 CRACKED WING SUPPORT CLIPS ON BOTTOM. REPLACED 3 WING SUPPORT CLIPS ON RT WING RIB 15.

Part: CLIPS — CRACKED (LT WING)

LT WING RIB 16 HAS THREE CRACKED WING SUPPORT CLIPS ON UPPER SIDE. REPLACED THREE WING SUPPORT CLIPS ON LT WING RIB 16 IAW SB 120-57-0031, CLIPS INSTALLED.

Part: TIP — DAMAGED (RT WING)

RT WING TIP DAMAGED AND DELAMINATING, NEEDS TO BE REPLACED. FITTED NEW WING TIP FOR RT WING.

Part: FITTING — BROKEN (RT TE FLAP)

RIGHT OUTBOARD NACELLE FLAP BELL CRANK BROKEN AT HARD MOUNT. REPLACED RT NACELLE FLAP IAW MM 27-50-02 AND PER RII CARD NUMBER 18. OPERATIONALLY CHECKS GOOD.

Part: STARTER GEN — FAILED (LEFT)

LOST THE LEFT GENERATOR ON DESCENT. GENERATOR WILL NOT RESET. REPLACED THE LEFT STARTER/GENERATOR. OPERATIONALLY CHECKS GOOD.

Part: FLOW VALVE LINE — LOOSE (RT ENGINE)

3 MIN AFTER TO, RIGHT DUCT LEAK WARNING CAME ON. DECREASED POWER AND LIGHT STAYED ON. SHUT DOWN THE RIGHT ENGINE AND RETURNED TO FIELD. LIGHT STAYED ON FOR FOUR MINUTES AFTER ENGINE SHUT DOWN. TIGHTENED LOOSE LINE ON FLOW VALUE. OPS CHECKS GOOD. SEE FL 75723.

Part: RETRACT MECH — LACK OF LUBE (TE FLAPS)

AFTER TAKEOFF FLAPS WOULD NOT RETRACT. THERE WAS A DISAGREEMENT BETWEEN OUTBD NACELLE AND INBOARD FLAPS. FAULT CLEARED AFTER LANDING. INSPECTED OUTBD FLAPS. CLEANED AND LUBRICATED ROLLERS. CYCLED FLAPS SEVERAL TIMES. OPS CHECKS GOOD. SEE FL 75711 FOR MECH SIGN OFF.