N563SW

Part: SIGN — BROKEN (CABIN) · airframe 33,174 hrs · 46,541 cycles

LOWER EMERGENCY EXIT SIGN IN ROW 9 IS BROKEN. FLT 5356 REPLACED LOWER EMERGENCY EXIT SIGN IN ROW 9.

Part: SIGN — BROKEN (CABIN) · airframe 33,021 hrs · 46,326 cycles

EMERGENCY EXIT ROW SIGN AT SEAT 6C IS BROKEN. FLT 5348 RELAMPED EMERGENCY EXIT SIGN AT SEAT 6C.

Part: COVER — MISSING (EXIT SIGN) · airframe 32,941 hrs · 46,216 cycles

COVER ON LIGHTED EMERGENCY EXIT SIGN LOWER LT OF 6C EXIT DOOR MISSING. FLT 5384 INSTALLED EMERGENCY EXIT SIGN COVER AT LOWER LEFT OF 6C.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,656 hrs · 45,824 cycles

FLOOR EMERGENCY LIGHT IN THE FRONT CABIN AREA IS BURNED OUT. FLT#5234 RELAMPED.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 32,444 hrs · 45,525 cycles

RT FORWARD FS FIRST BUTT STRAP UNDER LAVATORY HAS CORROSION. C-CHECK SPLICED SERVICEABLE BUTT STRAP FROM CABIN COCKPIT BULKHEAD TO BEGINNING OF PASSENGER SEAT TRACKS ON RT FORWARD FS FIRST BUTT STRAP UNDER LAVATORY. SEE ATTACHED ETD.

Part: FITTING — CRACKED (RT WING) · airframe 32,444 hrs · 45,525 cycles

RT WING FUEL TANK UPPER CLIP IS CRACKED AT RIB 20. C-CHECK REPLACED RT WING FUEL TANK UPPER CLIP AT RIB 20.

Part: FITTING — CRACKED (LT WING) · airframe 32,444 hrs · 45,525 cycles

LT WING FUEL TANK UPPER CLIP ON RIB 21 IS CRACKED. C-CHECK REPLACED LT WING FUEL TANK UPPER CLIP AT RIB 21.

Part: FITTING — CRACKED (LT WING) · airframe 32,444 hrs · 45,525 cycles

LT WING FUEL TANK UPPER CLIP IS CRACKED. C-CHECK REPLACED LT WING FUEL TANK UPPER CLIP AT RIB 23.

Part: CONTROL MODULE — FAILED (LANDING GEAR) · airframe 32,056 hrs · 44,992 cycles

RIGHT MLG WILL NOT RETRACT. (SERVICE) REPLACED LANDING GEAR CONTROL MODULE AND ADJUSTED RT MLG UPLOCK PROX SENSOR IAW AMM. P/N: 120-38594-501 S/N ON: 120293 S/N OFF: 120345

Part: WIRE — DAMAGED (CABIN) · airframe 31,699 hrs · 44,489 cycles

FORWARD EMERGENCY FLOOR LIGHT DOES NOT ILLUMINATE. (FLT 7354) REPAIRED WIRE ON FORWARD FLOOR EMERGENCY LIGHT.

Part: SEQUENCE VALVE — DIRTY (RT MLG) · airframe 31,271 hrs · 43,876 cycles

AFTER TAKEOFF RIGHT MAIN GEAR DID NOT RETRACT, CYCLED GEAR ONCE, AFTER APPROXIMATELY 5-6 SECORDS AFTER RAISING THE LEVER THE GEAR RETRACTED. (FLT 5648) CLEANED RIGHT MLG I/B AND O/B SEQUENCE VALVE PLUNGERS AND ADJUSTED O/B SEQUENCE VALVE PLUNGER AS REQUIRED.

Part: ACTUATOR — FAILED (RT MLG) · airframe 31,157 hrs · 43,732 cycles

ON GEAR RETRACTION RT MLG TRANSIT LIGHT STAYED ON AND RT MLG CYCLED UP AND DOWN FOR APPROXIMATELY 20 TO 30 SECONDS. (FLT 5470) REPLACED THE RT MLG RETRACTION ACTUATOR. P/N: 19595-000-07 S/N ON: 609 S/N OFF: 421

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,029 hrs · 43,564 cycles

EMERGENCY LIGHT 2B BURNED OUT. (FLT 5505) RELAMPED EMERGENCY LIGHT.

Part: WIRE — BROKEN (CABIN) · airframe 30,820 hrs · 43,241 cycles

FLOOR LEVEL EMERGENCY LIGHTING NEAR MAIN CABIN DOOR IS INOPERATIVE. (FLT 6387) FOUND BROKEN WIRE ON FORWARD FLOOR EMERGENCY LIGHT AND REPAIRED WIRE.

Part: WIRE — BROKEN (CABIN) · airframe 30,802 hrs · 43,216 cycles

FORWARD RED EMERGENCY LIGHT STRIP IS INOPERATIVE. (SERVICE) FOUND BROKEN WIRE AT FORWARD EMERGENCY LIGHT STRIP. REPLACED LIGHT SOCKET ASSEMBLY.

Part: WIRE — BROKEN (CABIN) · airframe 30,708 hrs · 43,089 cycles

EMERGENCY LIGHT ON FLOOR IN FRONT OF GALLEY ARE INOPERATIVE. (SERVICE) FOUND BROKEN CRIMP ON FRONT OF GALLEY FLOOR EMERGENCY LIGHT. RE-CRIMPED WIRE.

Part: ROLLER — MISSING (COCKPIT WINDOW) · airframe 30,518 hrs · 42,810 cycles

FIRST OFFICER'S DV WINDOW DIFFICULT TO OPEN. (FLT 6294) FOUND TOP ROLLER ON FIRST OFFICER'S DV WINDOW MISSING. INSTALLED NEW ROLLER.

Part: WIRE — BROKEN (CABIN) · airframe 29,884 hrs · 41,952 cycles

OVERHEAD EXIT EMERGENCY LIGHT AT ROW 9 IS INOPERATIVE. (FLT 5358) REPAIRED BROKEN WIRE AT 9BC AS NEEDED.

Part: DUCT — BLOWN (BLEED AIR SYS) · airframe 29,522 hrs · 41,437 cycles

RIGHT ENGINE OVERWING BLEED DUCT BLOWN OUT. (FLT 5638) REPLACED RIGHT BLEED DUCT AT RIGHT WING TO FUSELAGE SIDE PANEL.

Part: CONTROL MODULE — FAILED (LANDING GEAR) · airframe 29,508 hrs · 41,413 cycles

USED DOWNLOCK RELEASE TO GET GEAR TO RETRACT. (FLT 6263) REPLACED LANDING GEAR CONTROL MODULE PER AMM. PN 120-38594-501 SN OFF: 366605

Part: ALTIMETER — FAULTY (NR 1) · airframe 27,585 hrs · 38,758 cycles

ALTIMETERS WERE MORE THAN 200FT FROM EACH OTHER. (FLT 6362) REPLACED NR 1 ALTIMETER. P/N 1190AM1, S/N OFF AG271.

Part: WIRE — BROKEN (CABIN) · airframe 25,683 hrs · 36,071 cycles

FIRST TWO WHITE EMERGENCY PATH LIGHTS INOP. (FLT 6662) REPAIRED BROKEN WIRE.

Part: RELAY — OVERHEATED (APU FEEDER) · airframe 25,618 hrs · 35,980 cycles

FLIGHT DECK STARTED TO HAVE AN ELECTRICAL BURN SMELL. (FLT 6207) REPLACED APU FEEDER PROTECTION RELAY.

Part: SKIN — CRACKED (TE FLAP) · airframe 25,450 hrs · 35,739 cycles

LEFT NACELLE FLAP CRACKED LOWER SURFACE, NEAR OUTBOARD HINGE ARM. (C CHECK) INSTALLED DOUBLER PER SRM.

Part: FRAME — CRACKED (NACELLE) · airframe 25,450 hrs · 35,739 cycles

RIGHT ENGINE FRAME OUTBOARD SIDE CRACKED. (C CHECK) REPLACED RIGHT ENGINE FRAME PER SRM.

Part: SKIN — CORRODED (MAIN DOOR) · airframe 25,450 hrs · 35,739 cycles

MAIN DOOR SKIN CORRODED BEYOND LIMITS. (C CHECK) RE-SKINNED DOOR PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 25,450 hrs · 35,739 cycles

FRAME 16 RIGHT CENTER, LEFT CENTER, AND RIGHT OUTBOARD SECTIONS CORRODED. (C CHECK) REPLACED FRAME SECTIONS PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 25,450 hrs · 35,739 cycles

STRINGER 19L AT PASSENGER ENTRY CORRODED. (C CHECK) REPAIRED PER SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 25,450 hrs · 35,739 cycles

LEFT AND RIGHT SEAT TRACKS CORRODED. (C CHECK) REPLACED SECTIONS PER EMB CPM.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 25,450 hrs · 35,739 cycles

RIGHT BUTT STRAP BETWEEN FRAME 13 AND 16 CORRODED. (C CHECK) REPLACED RIGHT BUTT STRAP BETWEEN FRAME 13 AND 16 PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 25,450 hrs · 35,739 cycles

STRINGER 18L AT PASSENGER ENTRY DOOR CORRODED. (C CHECK) REPLACED STRINGER SECTION PER SRM.

Part: RELAY — BURNED (COCKPIT) · airframe 24,906 hrs · 34,957 cycles

BURNED FEEDER PROTECTION RELAY FOR APU FOUND IN COCKPIT. (FLT 6326) REPLACED RELAY.

Part: CONNECTOR — BROKEN (CABIN) · airframe 23,852 hrs · 33,437 cycles

EMERGENCY LIGHT INOP. (FLT 6138) REPAIRED CONNECTION.

Part: MECHANISM — BINDING (PAX DOOR) · airframe 23,645 hrs · 33,159 cycles

FLT 7779 - MAIN DOOR HARD TO OPEN AND CLOSE. LUBRICATED DOOR MECHANISM.

Part: LINKAGE — LACK OF LUBE (PAX DOOR) · airframe 23,645 hrs · 33,159 cycles

FLT 6485 - MAIN CABIN DOOR HANDLE STIFF. LUBED DOOR HANDLE LINKAGE.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 23,396 hrs · 32,829 cycles

FLT 5450 - MAIN ENTRY DOOR DIFFICULT TO OPEN. LUBRICATED.

Part: LIGHT — FAULTY (CABIN) · airframe 23,352 hrs · 32,765 cycles

FLT 7755 - MOST FWD FLOOR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSEMBLY.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,542 hrs · 31,735 cycles

ENTRY EMERGENCY LIGHT INOP (FLT 5708). RELAMPED EMERGENCY LIGHT.

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · airframe 22,115 hrs · 31,158 cycles

BUTT STRAP AT PAX DOOR ENTRANCE HAS SIGNS EXFOLIATION. (FOUND AT C-CHECK) REPLACED BUTT STRAP AT PAX DOOR ENTRANCE IAW SRM 51-10-02.

Part: ACTUATOR — FLUCTUATES (PROPELLER) · airframe 21,996 hrs · 31,007 cycles

NR 2 PROP HAS MINOR FLUCTUATIONS. (FLIGHT NR 3618) REPLACED RT PROP ACTUATOR IAW MM 61-13-04. OPS AND LEAK CHECK GOOD.

Part: WINDSHIELD — LEAKING (COCKPIT) · airframe 21,933 hrs · 30,931 cycles

AUTO PRESSURIZATION WILL NOT HOLD PRESSURE CORRECTLY. (FLT 5460) REPLACED LEFT WINDSHIELD AS REQUIRED PER MM 56-10-01.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 20,649 hrs · 29,242 cycles

FLT 5417 - WHITE FLOOR EMERGENCY LIGHTS ARE INOP BELOW GALLEY. REPAIRED FLOOR EMERGENCY LIGHT WIRING. OPS CHECK GOOD.

Part: A/C PACK — SMOKE (RIGHT) · airframe 19,908 hrs · 28,332 cycles

RIGHT PACK BLOWS SMOKE IN THE CABIN. RAN RIGHT PACK IN HOT/COLD AND AUTO/MANUAL MODES. NO SMOKE NOTED.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 19,450 hrs · 27,744 cycles

A GOOD PORTION OF THE EMERGENCY LIGHT SYSTEM DOES NOT TEST. REPLACED NR 2 BATTERY PACK IAW MM 33-50-02. OPERATIONAL CHECKS GOOD.

Part: BUTTSTRAP — CORRODED (FUSLEAGE) · airframe 18,565 hrs · 26,657 cycles

BUTTSTRAP UNDER LAV CORRODED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED BUTTSTRAP UNDER LAV IAW 51-10-02 PG 3 SEC 3A.

Part: FRAME — CRACKED (RT NACELLE) · airframe 18,565 hrs · 26,657 cycles

RIGHT OUTBOARD NACELLE FRAME CRACKED, BENEATH WING B-BRACKET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER ON RIGHT OUTBOARD NACELLE FRAME HYDRAULIC LINE STANDOFF (B-BRACKET) IAW EMB 120 SRM 51-10-02 PG 2 SECT 2B.

Part: FRAME — CRACKED (RT NACELLE) · airframe 18,565 hrs · 26,657 cycles

RIGHT INBOARD NACELLE FRAME CRACKED BENEATH WING B-BRACKET, DISCOVERED DURING C-CHECK INSPECTION. APPLIED DOUBLER AT RIGHT INBOARD NACELLE FRAME IAW SRM 120 51-10-02, PG 2 SEC 2B.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,472 hrs · 26,545 cycles

FORWARD RED LIGHT ON FLOOR LIGHT EMERGENCY EXIT INOP. REPLACED LAMP IN FORWARD RED LIGHT FLOOR EMERGENCY LIGHTING IAW EMB 120 MM 33-51-01. OPERATIONAL CHECKS GOOD.

Part: SIGN — MISSING (CABIN) · airframe 16,948 hrs · 24,678 cycles

ILLUMINATE EXIT SIGN (LOWER) AT 6A MISSING. REPLACED LIGHT ASSY. AS REQUIRED. OPERATIONAL CHECKS GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,362 hrs · 22,746 cycles

EXIT SIGN AT ROW 9 IS BROKEN. REPLACED SIGN, OPERATIONAL CHECK GOOD.

Part: SERVO — INOPERATIVE (STICK SHAKER) · airframe 15,173 hrs · 22,506 cycles

CAPTAINS STICK SHAKER IS INOPERATIVE. REPLACED CAPTAINS STICK SHAKER. OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 14,646 hrs · 21,805 cycles

EMERGENCY LIGHT STRIP A BEAM MAIN CABIN DOOR IS INOPERATIVE. REPAIRED WIRE TO THE FORWARD RED LIGHT EMERGENCY LIGHT FLOOR STRIP. OPERATIONAL TEST GOOD.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 14,646 hrs · 21,805 cycles

ON APPROACH, RECEIVED CONTROL FAULT, ADVANCED SWS FLAP LIGHT ON THE MAP. REMOVED AND REPLACED LT NACELLE ACTUATOR AND FLAP CONTROL COMPUTER IAW MM 27-50-00. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 14,577 hrs · 21,726 cycles

ONE FLOOR EMGERGENCY LIGHT INOPERATIVE. RELAMPED AFFECTED ASSEMBLY AS NEEDED, OPERATIONAL CHECK GOOD IAW EMB 120 MM 33-51-01.

Part: ACTUATOR — MALFUNCTIONED (NACELLE FLAP) · airframe 14,408 hrs · 21,474 cycles

FLAP DISAGREEMENT EVERY TIME FLAPS ARE PUT UP. REMOVED AND REPLACED LT NACELLE FLAP ACTUATOR IAW MM 27-50-00, OPERATIONAL CHECKED GOOD.

Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHT) · airframe 13,852 hrs · 20,798 cycles

FORWARD EMERGENCY LIGHT WON`T TEST. REMOVED AND REPLACED FORWARD BATTERY PACK FOR EMERGENCY LIGHTS PER EMB 120 MM 24-33-01. OPERATIONAL CHECK GOOD. P/N D366-04-001, S/N OFF 893/03-91.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 13,757 hrs · 20,681 cycles

MIDDLE SECTION EMERGENCY LIGHTS IN CABIN INOP. REPLACED MIDDLE EMERGENCY LIGHT BATTERY PACK WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.

Part: PANEL — BROKEN (EMERGENCY LIGHT) · airframe 13,373 hrs · 20,170 cycles

EMERGENCY LIGHT PANEL ON FLOOR IN GALLEY BROKEN. REMOVED AND REPLACED FORWARD EMERGENCY LIGHT ON FLOOR AT GALLEY IAW EMB 120 MM 20-10-00. OPS CHECK GOOD.

Part: COMPUTER — FAULTY (AUTOPILOT SYS) · airframe 13,029 hrs · 19,610 cycles

AIRCRAFT OSCILLATES UP AND DOWN WITH NR 2 AUTOPILOT ENGAGED. COMMAND BARS MOVE AROUND. REPLACED NR 2 APC-65B WITH SERVICEABLE UNIT. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 12,929 hrs · 19,469 cycles

AUTO PILOT AURAL WARNING AND TRIPLE CHIME WHEN SELECTED TO F/O SIDE. INSTALLED SERVICEABLE APC-65. OPS CHECK GOOD. S/N OFF: 2736.

Part: SERVO — MALFUNCTIONED (STICK SHAKER) · airframe 12,463 hrs · 18,740 cycles

F/O'S STICK SHAKER (CLACKER) ON TEST FUNCTION WEAK AND SOMETIMES NOTHING AT ALL. REPLACED F/O'S STICK SHAKER. OPS TEST GOOD.

Part: SUPPORT — CRACKED (HYD PACK) · airframe 11,832 hrs · 17,747 cycles

RT HYDRAULIC PACK LOWER SUPPORT, CRACKED IB EDGE. (DISCOVERED DURING C-CHECK)REPLACED RIGHT HYD PACK LOWER SUPPORT.

Part: FRAME — CRACKED (LT NACELLE) · airframe 11,832 hrs · 17,747 cycles

REINFORCEMENT FRAME FOR LT HYD PACK FWD FIREWALL, LT SIDE CRACKED AT HYD PRESS LINE FITTING POINT. (DISCOVERED DURING C-CHECK) INSTALLED REPAIR DOUBLER IAW IC 2003-12012138. SEE RII 54-301 & M337. P/N: 120-18896-001

Part: HINGE — CRACKED (LEFT FLAP) · airframe 10,904 hrs · 16,286 cycles

LEFT NACELLE FLAP BY INBOARD HINGE IS CRACKED. FOUND DURING LINE INSPECTION. REPLACED NACELLE FLAP WITH SERVICEABLE UNIT IAW MM 27-50-02. OPS CHECK GOOD AT THIS TIME.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 10,840 hrs · 16,168 cycles

APU START WAS ABORTED DUE TO A HUNG START. UPON INSPECTION, FOUND SMOKE AND FIRED EXTINGUISHER BOTTLE. INSPECTED APU AREA, NO OBVIOUS DEFECTS NOTED. REMOVED AND REPLACED APU FIRE BOTTLE AS PER EMB MM 26-21-00. REMOVED AND REPLACED MAIN BATTERY IAW MM 24-32-01.

Part: WARNING LIGHT — ILLUMINATED (PAX DOOR) · airframe 10,718 hrs · 15,972 cycles

CLIMBING THROUGH 11,000 FT, THE FORWARD DOOR LIGHT ILLUMINATED. FOLLOWED QRH PROCEDURE. LIGHT WOULD NOT EXTINGUISH. RETURNED TO LAX. CHECKED CABIN DOOR WARNING SYSTEM. PRESSURIZED AIRCRAFT TO 7.0 PSID. NO WARNINGS NOTED. OK FOR CONTINUED SERVICE.

Part: BLOWER — FAILED (A/C BAY) · airframe 10,374 hrs · 15,407 cycles

RIGHT PACK FAIL ON THE GROUND. SMALL AMOUNT OF SMOKE IN CABIN. INSTALLED SERVICEABLE GROUND COOLING FAN ON RIGHT PACK. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 10,084 hrs · 14,937 cycles

EMERGENCY EXIT SIGNS AND FLOOR EMERGENCY FLOOR LIGHTS ON BATTERY NR 2 INOP. REPLACED MIDDLE BATTERY PACK. OPS CHECK GOOD ON CABIN EMERGENCY LIGHT.

Part: WINDOW — LACK OF LUBE (LEFT) · airframe 9,895 hrs · 14,657 cycles

LEFT DIRECT VISION WINDOW IS HARD TO IMPOSSIBLE TO OPEN. LUBED WINDOW AND MADE IT EASIER TO OPEN. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (E/E BAY) · airframe 9,697 hrs · 14,336 cycles

TCAS TESTS OK, BUT REPORTS NO TARGETS IN THE AIR. REPLACED AND INITIALIZED TCAS PROCESSOR. OPS CHECK GOOD IAW MM 34-46-00.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 9,714 hrs · 14,367 cycles

AUTOFEATHER WARNING ON TAKEOFF - ABORTED TAKEOFF AND RETURNED TO GATE. PERFORMED STATIC ENGINE RUN AT TAKEOFF SETTINGS, COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK GOOD.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 8,922 hrs · 13,137 cycles

LOST GREEN HYD SYSTEM. LEFT MAIN HYD PUMP LOW PRESS LIGHT ILLUMINATED. PER QRH, TURNED LEFT ELEC HYD PUMP ON. AFTER A FEW MINUTES, GREEN HYD QUANTITY DROPPED TO ZERO (EMPTY). EXTENDED GEAR MANUALLY AND MADE EMER LANDING. PRESSURE LINE TO HYDRAULIC RESERVOIR REPLACED. REPLACED LEFT ENGINE HYD DRIVEN PUMP. SERVICED HYDRAULIC FLUID. STEERING CHECK FLAPS, BRAKES, RUDDER CHECKS GOOD. LEAK CHECK GOOD. P/N ON 3-022-29, S/N ON MX-598526, S/N OFF MX-580-77.

Part: PRESSURE SWITCH — MALFUNCTIONED (HORIZ STAB) · airframe 8,662 hrs · 12,767 cycles

LEFT INBOARD HORIZONTAL DEICE BOOT INOP. INSTALLED SERVICEABLE PRESSURE SWITCH FOR LEFT INBOARD HORIZONTAL DEICE BOOT IAW MM 30-10-05. LEAK CHECK & OPS CHECK OF DEICE BOOT GOOD.

Part: SEAL — FAILED (CARGO DOOR) · airframe 4,066 hrs · 5,796 cycles

CABIN ALT LIGHT ILLUMINATED AND OXYGEN MASKS DEPLOYED. FOUND CARGO DOOR SEAL BLOWN OUT AT TOP AFT PORTION AND BOTTOM AFT PORTION. REPAIRED SEAL AS NEEDED. PRESSURIZED AIRCRAFT AND STOWED OXYGEN MASKS. OPS CHECKS GOOD.

Part: TRANSMITTER — FAILED (AILERON CONTROL) · airframe 7,820 hrs · 11,532 cycles

DURING TAXI CHECK , TAXIING OUT AILERON CONTROL ONLY MOVES 1/2 WAY TO RIGHT - ''SPRINGY'' FEELING. FOUND LEFT AILERON FDR INPUT SHAFT UNSECURED AND BENT UNSERVICEABLE. REPLACED ROTARY VARIABLE INTENSITY TRANSMITTER (RVIT) ARM AND BELLCRANK INPUT SHAFT WITH SERVICEABLE UNITS. ADJUSTED RVIT AS REQD IAW MM 31-30-00. OPS CHECK GOOD AT THIS TIME.

Part: DC BUS — FAILED (E&E COMP)

ON CLIMB-OUT (90,00+) ELECTRIC LIGHT ON MAP ILLUMINATED, EMERGENCY BUS OFF LIGHT ILLUMINATED. ELECTRIC BUSSES OFF RELAYS EMERGENCY BUSSES 1 CB POPPED. ELECTRIC DC INDICATION (EMERGENCY) 1 POPPED. DIVERTED TO FAT. REPLACED EMERGENCY DC BUS 1 OFF RELAY (K0439). OPS CHECKS GOOD IAW MM 24-52-00.

Part: DUCT — LEAKING (LT ENGINE)

DUCT LEAK LIGHT ILLUMINATED IN FLIGHT. FOLLOWED QRH INSTRUCTIONS AND DUCT LEAK LIGHT EXTINGUISHED. RETURNED TO LAX. REPOSITIONED CLAMP AT HEAT EXCHANGER INLET. RAN LEFT ENGINE AT MAXIMUM RPM IN AUTO/NORM WITH BLEED AND PACKS ON. OPS CHECKS GOOD AT THIS TIME.

Part: REGULATOR — FAILED (LT ENGINE)

LEFT BLEED DUCT LEAK LIGHT ILLUMINATED IN FLIGHT. FOLLOWED QRH PROCEDURES BUT DUCT LEAK LIGHT REMAINED ON. SHUT DOWN LEFT ENGINE AS PER QRH. RETURNED TO LAX. DUPLICATED PROBLEM ON GROUND AFTER 5 MINUTES AT CLIMB POWER. REPLACED LT 18 PSI REGULATOR. RAN AT CLIMB POWER FOR 15 MIN. OPS CHECK GOOD.

Part: WINDSHIELD — FAILED (RT COCKPIT)

AT 23,000 FT COPILOT'S WINDSHIELD (OUTER PART) SHATTERED (NO IMPACT). LANDED IN ONT WITHOUT INCIDENT. REMOVED AND REPLACED COPILOT'S WINDSHIELD TO MM 56-10-01, ALL CHECKS GOOD.