N297SW

Part: SMOKE DETECTOR — NO TEST (CARGO BAY) · airframe 37,162 hrs · 51,860 cycles

CARGO SMOKE TEST INOPERATIVE. R & R NR 2 SMOKE DETECTOR IN CARGO BAY IAW AMM.

Part: CONNECTOR — DIRTY (SMOKE DETECTOR) · airframe 37,118 hrs · 51,803 cycles

AFT CARGO SMOKE DETECTOR WILL NOT TEST. CLEANED ELECTRICAL CONNECTOR ON 2 SMOKE DETECTOR. OPS CHECK GOOD.

Part: GROUND STUD — LOOSE (CABIN) · airframe 36,227 hrs · 50,632 cycles

EMERGENCY EXIT SIGN ROW 6A DOES NOT ILLUMINATE. FLT 5427 SECURED THE GROUND STUD FOR THE EMERGENCY EXIT SIGN AT ROW 6A.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 36,204 hrs · 50,594 cycles

CARGO DOOR FRAME CRACKED. C-CHECK REPLACED CARGO DOOR FRAME A STRUCTURAL COMPONENT IAW SRM.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 36,204 hrs · 50,594 cycles

MAIN CABIN DOOR ROTATING ARM ATTACH SUPPORT FITTING CRACKED. C-CHECK REPLACED MAIN CABIN DOOR CUT OUT LOWER FITTING FRAME PN 120-18804-001 IAW SRM.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 36,204 hrs · 50,594 cycles

SHEET METAL DAMAGE TO FRAME 46A AT LOWER LT SIDE, BELLOW AFT CARGO PARTITION. C-CHECK REMOVED DAMAGED SECTION OF FRAME 46A AT STRINGER 20L & SPLICED IN NEW SECTION WITH ORIGINAL FRAME MATERIAL IAW ETD.

Part: SPAR — CRACKED (LT WING) · airframe 36,204 hrs · 50,594 cycles

LT WING AUX SPAR INBD OF NACELLE CRACKED AT HI-LOK IN CORNER INBD OF POWER CONDITION CABLE CAGE. C-CHECK REPAIRED LT WING UPPER AUX SPAR JUST INBD OF NACELLE IAW ETD.

Part: SUPPORT — CRACKED (LT NACELLE) · airframe 36,204 hrs · 50,594 cycles

LT NACELLE GEAR WELL FIREWALL BULKHEAD EXHAUST CRADLE FRAME CRACKED, ZONE 433. C-CHECK REPLACED LT NACELLE GEAR WELL FIREWALL SUPPORT PN 120-32357-001 IAW SRM.

Part: DOOR FRAME — CORRODED (CABIN DOOR) · airframe 36,204 hrs · 50,594 cycles

MAIN CABIN DOOR HAS CORROSION IN BAY 7. C-CHECK REPLACED LOWER FRAME IAW SRM.

Part: STRINGER — CRACKED (LT NACELLE) · airframe 36,204 hrs · 50,594 cycles

LT NACELLE GEAR WELL OTBD HORIZONTAL FRAME CRACKED. C-CHECK REPAIRED LT NACELLE, OTBD STRINGER WEB 3L IAW SRM.

Part: SUPPORT — CRACKED (LT WING) · airframe 36,204 hrs · 50,594 cycles

LT WING NR 3 FUEL CELL HAS 1 SKIN SUPPORT CRACKED AFT INBD SIDE OF PANEL. C-CHECK REPLACED 1 SKIN SUPPORT INBD OF NR 3 FUEL ACCESS PANEL 1 STRINGER AFT PN 120-61341-617 IAW SRM.

Part: RIB — CRACKED (LT WING) · airframe 36,204 hrs · 50,594 cycles

LT WING NR 17 RIB UPPER SURFACE FWD WEB RIB CRACKED AT RIVET. C-CHECK REPLACED FWD RIB WEB PN 120-17058-001 AT LT WING NR 17 RIB IAW SRM & AMM.

Part: REPAIR — DAMAGED (RUDDER) · airframe 36,204 hrs · 50,594 cycles

PREVIOUS REPAIR ON RUDDER HAS A NUTPLATE WITH PULLED RIVETS, LT SIDE OF RUDDER. C-CHECK FABRICATED NEW REPAIR DOUBLER.

Part: CLEAT — CRACKED (RT WING) · airframe 36,204 hrs · 50,594 cycles

RT WING NR 6 FUEL PANEL INBD FWD UPPER SKIN CLEAT CRACKED. C-CHECK REPLACED UPPER SKIN CLEAT PN 120-17063-611 ON RT WING FWD INBD OF NR 6 FUEL ACCESS PANEL IAW SRM & AMM.

Part: CLEAT — CRACKED (RT WING) · airframe 36,204 hrs · 50,594 cycles

RT WING NR 5 FUEL PANEL INBD FWD UPPER TWO SKIN CLEATS CRACKED. C-CHECK REPLACED TWO UPPER SKIN CLEATS PN 120-17062-613 & 120-17063-609 ON RT WING FWD INBD OF NR 5 FUEL ACCESS PANEL IAW AMM & SRM.

Part: CLEAT — CRACKED (RT WING) · airframe 36,204 hrs · 50,594 cycles

RT WING NR 3 FUEL PANEL AFT OTBD SKIN CLEAT CRACKED. C-CHECK REPLACED LOWER SKIN CLEAT PN 120-61344-606 ON RT WING OTBD AFT OF NR 3 FUEL ACCESS PANEL IAW AMM & SRM.

Part: WEB — CHAFED (LT NACELLE) · airframe 36,204 hrs · 50,594 cycles

LT MLG BAY OTBD WEBBING CHAFED BEYOND LIMITS. C-CHECK REPLACED LT NACELLE OTBD GEAR WELL WEBBING IAW SRM.

Part: CLEAT — CRACKED (RT WING) · airframe 36,204 hrs · 50,594 cycles

RT WING HAS FOUR LEAKING RIVETS BY THE NR 4 FUEL PANEL & LOWER SKIN CLEAT CRACKED AT RIB 18. C-CHECK REPLACED LOWER SKIN CLEAT PN 120-61345-615 ON RT WING AT RIB 18 IAW AMM & SRM.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 36,197 hrs · 50,583 cycles

EMERGENCY LIGHT ON FLOOR IN ROW 7 IS DIM. SERVICED REPOSITION LAMP INTO LAMP HOLDER AT ROW 7 FLOOR LEVEL 3 LIGHT.

Part: ENGINE — FAILED (RIGHT) · airframe 35,558 hrs · 49,798 cycles

ON DESCENT SMOKE ENTERED CABIN. RAN QRH LANDED WITHOUT FURTHER INCIDENT. REPLACED RT ENGINE IAW AMM.

Part: UNKNOWN — SMOKE (CABIN) · airframe 35,539 hrs · 49,781 cycles

ENGINE BLEED IN AUTO AND PACKS IN LOW, SMOKE BEGAN FILLING CABIN. SMOKE STOPPED AFTER SELECTING ENGINE BLEEDS TO LOW. RAN BOTH ENGINES WITH BLEED IN AUTO MODE. NO DEFECTS NOTED. ANY POWER SETTING, COULD NOT DUPLICATE DISCREPANCY ON THE GROUND.

Part: UNKNOWN — SMOKE (CABIN) · airframe 35,455 hrs · 49,675 cycles

SMOKE IN CABIN, APU OFF, ENGINE BLEED AUTO, PACKS NORM, TEMP CONTROLLER MANUAL, COLD IN PAX CABIN, TURNED RIGHT PACK OFF. SMOKE CLEARED. NO FURTHER PROBLEMS. (FLT 5309) RAN RT PACK IAW AMM AND COULD NOT DUPLICATE SMOKE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 35,416 hrs · 49,621 cycles

SMOKE REPORTED IN THE CABIN, THE TOILET SMOKE DETECTOR WENT OFF. DECLARED AN EMERGENCY. SMOKE DISSIPATED DURING LANDING. (FLT 6367) NO SMELL OF SMOKE IN CABIN, PULLED LIGHT PANEL IN LAV AND INSPECTED WIRING, NO DEFECTS NOTED, INSPECTED LIGHTS IN AFT OF CABIN NO DEFECTS NOTED, RAN AC PACKS IN COLD AND HOT NO DEFECTS NOTED - RAN ENGINES WITH AC PACKS IN HOT AND COLD NO DEFECTS NOTED. COULD NOT DUPLICATE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 35,015 hrs · 49,047 cycles

SMOKE DETECTOR IN LAV WENT OFF. NO SIGNS OF SMOKE. (FLT 5315) NO SIGNS OF SMOKE OR SMELL, COULD NOT DUPLICATE, REPLACED LAV SMOKE DETECTOR BATTERY AS A PRECAUTION IAW AMM.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 34,927 hrs · 48,948 cycles

CAPT'S SIDE WINDSHIELD CRACKED. (FLT 7386) NEW WINDSHIELD INSTALLED ON CAPT'S SIDE.

Part: SIGN — BROKEN (CABIN) · airframe 34,750 hrs · 48,743 cycles

EXIT SIGN ON WALL AT 6C BROKEN. (FLT 5355) REPLACED EXIT SIGN AT SEAT 6BC.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 34,683 hrs · 48,656 cycles

SMOKE DETECTOR WENT OFF. (FLT 5645) REPLACED LAV SMOKE DETECTOR BATTERY.

Part: HYDRAULIC SYSTEM — CONTAMINATED (GREEN SYS) · airframe 34,591 hrs · 48,547 cycles

MAIN CABIN DOOR WILL NOT FREE FALL DOWN. (FLT 7759) BLED AIR FROM GREEN HYDRAULIC SYSTEM.

Part: SIGN — MISSING (CABIN) · airframe 34,164 hrs · 48,014 cycles

EMERGENCY SIGN AT 6A MISSING. (FLT 6283) REPLACED EMERGENCY EXIT SIGN AT 6A IN REFERENCE TO AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,263 hrs · 46,888 cycles

EMERGENCY LIGHT BELOW FLIGHT ATTENDANT JUMPSEAT IS OUT. (FLT 7765) RELAMPED EMERGENCY LIGHT.

Part: WIRE — BROKEN (CABIN) · airframe 33,263 hrs · 46,888 cycles

EXIT SIGN ON BIN DOOR AT ROW 9 IS OUT. (SERVICE) REPAIRED BROKEN WIRE.

Part: BEARING — FAILED (CABIN DOOR) · airframe 33,036 hrs · 46,565 cycles

MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE. (FLT 7781) REPLACED BEARINGS ON TORQUE TUBE.

Part: WIRE — BROKEN (CABIN) · airframe 32,975 hrs · 46,497 cycles

OVERHEAD EMERGENCY EXIT LIGHT PANEL AT ROW 9 IS OUT. (FLT 6264) REPAIRED TERMINAL WIRE AT EMERGENCY EXIT ROW 9.

Part: ALTIMETER — FAILED (COCKPIT) · airframe 32,921 hrs · 46,421 cycles

FIRST OFFICER VSI JUMPS 300 FEET PER MINUTE WHENEVER ALTIMETER SETTING IS ADJUSTED. (FLT 5516) REPLACED THE ALTIMETER.

Part: SCREW — OUT OF ADJUST (LT MLG) · airframe 32,617 hrs · 46,030 cycles

LEFT MAIN LANDING GEAR WOULD NOT RETRACT. (FLT 5438) ADJUSTED LEFT MAIN GEAR UP LOCK ROLLER ADJUSTMENT SCREW.

Part: CONNECTOR — CONTAMINATED (BLEED AIR SYS) · airframe 32,608 hrs · 46,019 cycles

RIGHT ENGINE DUCT LEAK INDICATION. CREW FOLLOWED QRH AND SHUT RIGHT ENGINE DOWN. (FLT 5505) CLEANED MOISTURE FROM RIGHT ENGINE DUCT LEAK SENSOR CONNECTOR.

Part: RIB — CRACKED (RT WING) · airframe 32,556 hrs · 45,957 cycles

RIGHT WING INBOARD LEADING EDGE INBOARD RIB IS CRACKED. (C-CHECK) REPLACED INBOARD RIB ON RIGHT WING INBOARD LEADING EDGE WITH A SERVICEABLE UNIT.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 31,730 hrs · 44,869 cycles

ABOUT AN 1 INCH HOLE IN FUSELAGE AROUND 1.5 FEET ABOVE THE CARGO DOOR FRAME 44 STRINGER 3. (SERVICE) REPAIRED FUSELAGE SKIN AT ABOUT FRAME 44 & STRINGER 3 PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 31,584 hrs · 44,686 cycles

RIGHT SIDE ROW 6 EMERGENCY EXIT LIGHT ASSEMBLY IS BROKEN. (FLT 6679) REPLACED EMERGENCY EXIT LIGHT ASSEMBLY.

Part: STIFFENER — CRACKED (NACELLE) · airframe 29,630 hrs · 42,395 cycles

RIGHT NACELLE HYDRAULIC RESERVOIR ATTACH FRAME LOWER STIFFENER CRACKED. (C CHECK) REPLACED STIFFENER PER SRM.

Part: SUPPORT — CRACKED (RT WING) · airframe 29,619 hrs · 42,381 cycles

STRINGER TO RIB ANGLE CRACKED AT RIGHT NR 1 FUEL CELL FORWARD STRINGER. (C CHECK)REPLACED STRINGER RIB SUPPORT PER SRM.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 29,619 hrs · 42,381 cycles

LEFT BUTT STRAP, FRAMES 16 TO 17, CORRODED. (C CHECK)REPLACED BUTT STRAP PER SRM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 29,630 hrs · 42,395 cycles

SKIN CLEATS BELOW CABIN FLOOR IN ZONE 131 CORRODED. (C CHECK) REPLACED PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 29,630 hrs · 42,395 cycles

STRINGER 19 BELOW PASSENGER DOOR CORRODED. (C CHECK) REPLACED STRINGER SECTION PER SRM.

Part: SKIN — CRACKED (NACELLE) · airframe 29,619 hrs · 42,381 cycles

RIGHT AFT NACELLE, OUTBOARD SIDE, SKIN CRACKED. (C CHECK)REPLACED RIB AND SKIN PER SRM.

Part: HANDLE — LACK OF LUBE (MAIN DOOR) · airframe 29,551 hrs · 42,305 cycles

MAIN DOOR DIFFICULT TO OPEN FROM OUTSIDE. (FLT 6828) LUBED OUTER HANDLE ASSEMBLY.

Part: WIRE — LOOSE (CABIN) · airframe 29,351 hrs · 42,067 cycles

EMERGENCY LIGHT OVER 6A INOP. (FLT 6236) RE-SECURED WIRE AT LIGHT ASSEMBLY.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 29,288 hrs · 42,000 cycles

MAIN DOOR IS DIFFICULT TO OPEN AND CLOSE. (FLT 6063) LUBRICATED MAIN DOOR.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 29,138 hrs · 41,808 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. (FLT 6848) LUBED ROLLER AND PIVOT POINTS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,987 hrs · 41,636 cycles

EMERGENCY FLOOR LIGHTS DIM. (FLT 6515) CHARGED EMERGENCY BATTERY PACK WITH AIRCRAFT POWER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,935 hrs · 41,570 cycles

FLOOR EMERGENCY LIGHT INOP AT ROW 9. (FLT 6238) RELAMPED EMERGENCY LIGHT.

Part: STOP FITTING — OUT OF ADJUST (CABIN DOOR) · airframe 28,130 hrs · 40,546 cycles

CABIN DOOR IS DIFFICULT TO OPEN. (FLT 6347) ADJUSTED TOP AFT DOOR STOP.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 27,046 hrs · 39,048 cycles

FLT 7770 - OVERHEAD EMERGENCY EXIT LIGHT OVER SEAT 6A INOP. REPAIRED BROKEN WIRE.

Part: A/C PACK — CONTAMINATED · airframe 27,015 hrs · 39,012 cycles

FLT 7761 - UPON ROTATION, THE COCKPIT AND CABIN FILLED WITH SMOKE FROM WHAT APPEARED TO BE DE-ICE FLUID. RAN BOTH PACKS ON GROUND UNTIL DEICE FLUID ODOR ABATED; NO MORE SMOKE WAS DETECTED.

Part: DOOR — LACK OF LUBE (MCD) · airframe 26,593 hrs · 38,506 cycles

MCD HARD TO OPEN FROM INSIDE. (FLT 5441)LUBED DOOR.

Part: SENSOR — BURNED (ICE PROTECTION) · airframe 26,273 hrs · 38,099 cycles

ICE PROTECTION CURRENT SENSOR ASSEMBLY CHARRED AND DETERIORATED. C-CHECK, REPLACED LEFT ICE PROTECTION CURRENT SENSOR.

Part: O-RING — DAMAGED (TRANSFER TUBE) · airframe 26,199 hrs · 37,990 cycles

RT ENGINE NP SURGED AFTER TAKE-OFF. (FLIGHT NR 5702) REPLACED TRANSFER TUBE O-RINGS AND ADJUSTED PCU IAW AMM 61-10-02. OPS CHECK GOOD.

Part: BATTERY — WEAK (SMOKE DETECTOR) · airframe 26,053 hrs · 37,773 cycles

FLT 5722 - LAVATORY SMOKE DETECTOR SOUNDS INTERMITTENTLY. REPLACED LAV SMOKE DETECTOR BATTERY. OPS CHECKS GOOD.

Part: ROD END — CORRODED (PAX DOOR) · airframe 25,816 hrs · 37,475 cycles

FLT 3569 - CABIN DOOR IS HARD TO OPEN FROM THE INSIDE. REPLACED CORRODED TORQUE TUBE ROD ENDS AND BEARINGS. OPS CHECK GOOD.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 25,752 hrs · 37,398 cycles

FLT 3573 - SMOKE REPORTED IN THE CABIN WHEN PACKS WERE RAN OFF OF APU. REMOVED EXCESS OIL FROM APU RESERVOIR. RAN APU AND BOTH PACKS FOR 15 MINUTES WITH NO EVIDENCE OF SMOKE.

Part: WIRE — BURNED · airframe 25,336 hrs · 36,896 cycles

AUXILLARY RELAY BOX SPLICE SPBG-08 SHOWS SIGNS OF OVERHEATING. REPLACED SPLICE SPBG-08 WITH A SERVICEABLE UNIT.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 25,336 hrs · 36,896 cycles

FLT 5465 - EMERGENCY EXIT SIGN ON FORWARD BULKHEAD IS INOP. RESECURED WIRING AS REQUIRED. OPS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (ELEVATOR TRIM) · airframe 25,165 hrs · 36,670 cycles

ELEVATOR TRIM IS DIFFICULT TO MOVE TOWARDS THE "NOSE UP" POSITION IN FLIGHT, FLIGHT NR 3677. REPLACED BOTH TRIM ACTUATORS AS WELL AS THE LEFT DAMPENER ASSEMBLY. OPS CHECKS GOOD.

Part: SIGN — BROKEN (CABIN) · airframe 25,159 hrs · 36,662 cycles

LEFT LOWER PAX DOOR INTERIOR EXIT SIGN IS BROKEN. REPLACED LEFT EMERGENCY EXIT DOOR LIGHT AS REQUIRED. OPS CHECK GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 24,870 hrs · 36,265 cycles

ROW 9 EMERGENCY EXIT LIGHTS ARE INTERMITTENT, FLIGHT NR 5708. REPAIRED BROKEN WIRE BEHIND EXIT SIGN. OPS CHECK GOOD.

Part: COOLING FAN — SMOKE (CABIN) · airframe 23,731 hrs · 34,745 cycles

SMOKE IN CABIN AFTER LANDING. REPLACED LEFT GROUND COOLING FAN IAW MM 21-51-03. OPS CHECKS GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 23,429 hrs · 34,373 cycles

LEFT OVERWING EMERGENCY INTERIOR "EXIT" LIGHT FAILS TO COME ON. REPAIRED WIRE NR 2 ON BACK OF SIGN. OPERATIONAL CHECK GOOD.

Part: SUPPORT ANGLE — CRACKED (DOOR THRESHOLD) · airframe 22,914 hrs · 33,661 cycles

PAX - DOOR THRESHOLD SUPPORT ANGLE IN FUSELAGE FRAME CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED PAX DOOR SUPPORT ANGLE IAW SRM 120 51-10-02 PG 3 SEC 3B.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 22,914 hrs · 33,661 cycles

FRAME BEHIND CAPT'S DV WINDOW CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED FRAME BEHIND CAPT'S DV WINDOW IAW SRM 120 51-10-02 PG 3 SEC 3A AND RII 53-800-1000.

Part: SKIN — CRACKED (FUSELAGE) · airframe 22,914 hrs · 33,661 cycles

FUSELAGE SKIN CLEAT CRACKED ABOVE AND FORWARD OF CARGO DOOR CUT OUT DISCOVERED DURING C-CHECK INSPECTION. NEW SKIN CLEAT INSTALLED IAW SRM 120 51-40-02, ALSO IAW RII CARD 53-800-1000.

Part: FLOW DIVIDER — ODOR (APU) · airframe 22,694 hrs · 33,363 cycles

AFTER STARTING APU ON THE GROUND, NOTICED STRONG FUEL SMELL IN THE AIRCRAFT. REMOVED AND REPLACED APU FLOW DIVIDER IAW ALLIED SIGNAL MM 49-30-58. OPERATIONAL CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,288 hrs · 32,844 cycles

EMERGENCY EXIT LIGHT AT ROW 9C IS BROKEN. REPLACED EMERGENCY EXIT LIGHT AT ROW 9C. OPERATIONAL CHECKS GOOD.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 21,284 hrs · 31,419 cycles

STALL WARNING LIGHT ON MAP AND ASSOCIATED AURAL WARNING INFLIGHT. REPLACED NR 2 STALL WARNING COMPUTER AND STALL WARNING TEST PANEL. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 18,730 hrs · 27,498 cycles

F/A REPORT, CENTER SECTION OF EMERGENCY LIGHTS INOPERATIVE. REPLACED CENTER ELBP. OPERATIONAL CHECK GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (EMERGENCY BRAKE) · airframe 17,115 hrs · 25,069 cycles

ELECTRIC ODOR & SMOKE COMING FROM CENTER CONSOLE. REMOVED AND REPLACED PRESS SYSTEM/EMERGENCY PARK BRAKE PANEL AND LIGHTING ASSEMBLY WITH A SERVICEABLE UNIT. OPS CHECK GOOD. P/N 120-40220-001.

Part: RIB — CRACKED (RT WING LE) · airframe 15,998 hrs · 23,483 cycles

RT IB LEADING EDGE RIB IS CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) DOUBLER REINFORCEMENTS ADDED TO ABOVE MENTIONED RIB AREA IAW EMB120 SRM 51-10-02.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 15,959 hrs · 23,423 cycles

PAX DOOR AFT SIDE FRAME 5 HAS A L BRACKET CRACKED. (DISCOVERED DURING C-CHECK)PERFORMED PATCH REPAIR IAW 120 SRM 52-10-02 FIG. 203 AND CARD RII 52-301.

Part: RIB — CRACKED (LT WING LE) · airframe 15,998 hrs · 23,483 cycles

LT IB LEADING EDGE RIB IS CRACKED. (DISCOVERED DURING C-CHECK INSPECTION)INSTALLED REINFORCEMENT DOUBLER ON LEFT IB LEADING EDGE RIB IAW 51-10-02.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 15,959 hrs · 23,423 cycles

RT ANGLE CRACKED COCKPIT ENTRY BELOW FLOOR. (DISCOVERED DURING C-CHECK INSPECTION)APPLIED DOUBLER TO RT BRACKET BELOW FLOOR AT COCKPIT IAW SRM 12051-10-02.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 15,959 hrs · 23,423 cycles

LT ANGLE CRACKED COCKPIT ENTRY BELOW FLOOR. (DISCOVERED DURING C-CHECK INSPECTION) APPLIED DOUBLER TO LT BRACKET BELOW FLOOR AT COCKPIT IAW SRM120 51-10-02 .

Part: ROD — OUT OF ADJUST (NACELLE FLAP) · airframe 15,426 hrs · 22,586 cycles

EXCESSIVE SLACK NOTED IN MOVEMENT OF LEFT NACELLE FLAP. REPLACED LEFT NACELLE FLAP ACTUATOR ROD END IAW EMB 120 MM 27-50-00. OPS CHECK GOOD.

Part: WARNING LIGHT — ILLUMINATED (RT ENGINE) · airframe 14,679 hrs · 21,446 cycles

AT 90 KTS ON TAKEOFF ROLL RECEIVED AN OIL PRESSURE AURAL WARNING. UNABLE TO DETERMINE WHICH ENGINE IT WAS. TAKEOFF WAS ABORTED. OIL PRESSURE WAS IN THE NORMAL RANGE IN BOTH ENGINES. DETERMINED RIGHT ENGINE TO BE THE CAUSE OF OIL LOW PRESSURE WARNING. REPLACED RIGHT ENGINE DUE TO PREVIOUS HISTORY IAW MM 71-00-00. OPS CHECK GOOD. LEAK CHECK GOOD.

Part: ENGINE — LACK OF LUBE (NR 1) · airframe 14,620 hrs · 21,361 cycles

ON TAKEOFF ROLL AT ABOUT 90 KTS, RECEIVED A TRIPLE CHIME AND OIL AURAL WARNING. ABORTED TAKEOFF (NO MAP PANEL LIGHT). OIL PRESSURE GAUGE INDICATED IN GREEN AREA. REPLACED RIGHT ENGINE OIL PRESSURE SWITCH AND CARBON SEAL WITH SERVICEABLE UNITS. ADDED 2 QUARTS OF OIL TO RIGHT ENGINE AND 1 QUART TO LEFT ENGINE. PERFORMED ENGINE RUNUP OF BOTH ENGINES. ALL PARAMETERS FOUND TO BE WITHIN LIMITS. NO WARNINGS. LEAK CHECK AND OPS CHECK GOOD.

Part: SEAL — LEAKING (RT STARTER GEN) · airframe 14,592 hrs · 21,317 cycles

TWO ABORTED TAKEOFFS IN A ROW FOR TRIPLE CHIME 'OIL'. ADDED OIL TWO LEGS PRIOR. ON SHUTDOWN NR 2 ENGINE WAS AT 'ADD 3'. REPLACED RT ENGINE STARTER GEN GEARSHAFT SEAL IAW PRATT & WHITNEY MM 72-20-00. NO OTHER SIGNS OF EXTERNAL OIL LEAKS NOTED AT THIS TIME. ADDED 2 QUARTS OIL TO THE RIGHT ENGINE.

Part: FUEL HEATER — FAILED (RT ENGINE) · airframe 14,555 hrs · 21,253 cycles

RECEIVED LOW OIL AURAL WARNING ON TAKEOFF ROLL, AS WELL AS OIL PRESS NR 2 RED MAP LIGHT. ABORTED TAKEOFF. DUE TO HIGH OIL CONSUMPTION ON RT ENGINE, REPLACED RT ENGINE FUEL OIL HEATER ASSEMBLY AND INSPECT CENTRIFUGAL BREATHER SHAFT WHERE CARBON SEAL RIDES FOR SCORING.  ADDED TWO QUARTS OF OIL. REMOVED AND REPLACED RIGHT ENGINE FUEL OIL HEATER IAW 73-12-00 EMB 120 MM. LEAK CHECK GOOD. NO LEAKS NOTED. PN: 3120075-02 SN OFF: WA14980 SN ON: WA16483.

Part: ENGINE — LACK OF LUBE (NR 2) · airframe 14,588 hrs · 21,309 cycles

RECEIVED A LOW OIL AURAL WARNING ON TAKEOFF ROLL WITH OIL PRESS NR 2 RED MAP LIGHT. ABORTED TAKEOFF. OIL PRESSURE REMAINED IN THE NORMAL RANGE. ADDED TWO QUARTS OF OIL. RAN ENGINE. ALL CHECKS GOOD.

Part: OIL SYSTEM — LOW (NR 2 ENGINE) · airframe 14,496 hrs · 21,159 cycles

''OIL PRESSURE NR 2'' MESSAGE ILLUMINATED ON TAKEOFF ROLL AT APPROXIMATELY 60-70 KTS. ABORTED TAKEOFF. OIL PRESSURE GAUGE INDICATION WAS WITHIN NORMAL RANGE. ADDED 2 QUARTS OF OIL TO THE RT ENGINE. RAN ENGINE AT 100 PERCENT TORQUE. NO DEFECTS NOTED.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 13,678 hrs · 19,897 cycles

TRIPLE CHIME OIL AURAL WARNING WITH MAP LIGHT AT 85 KIAS ON TAKEOFF. ABORTED TAKEOFF. CHECKED OIL SERVICING, CHECKED OIL PRESSURE SWITCH, ASSOCIATED WIRING AND PRESSURE LINES. RAN ENGINES AND PILOT PERFORMED HIGH SPEED TAXI AT 85 KTS. ALL SYSTEMS WORKING AND INDICATING PROPERLY. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 13,538 hrs · 19,678 cycles

STICK SHAKER CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF. REPLACED NR 1 STALL WARNING COMPUTER SYSTEM. OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 13,305 hrs · 19,306 cycles

ON CLIMBOUT RECEIVED A FIRST OFFICER HEADING FLAG ACCOMPANIED BY ATT DISPLAY MAP LIGHT AND INTERMITTENT TCAS FAIL. RETURNED TO FAT. PERFORMED REINITIALIZATION OF FIRST OFFICER'S AHRS. OPS CHECK GOOD.

Part: PITOT TUBE — CORRODED (LT & RT) · airframe 12,260 hrs · 17,812 cycles

LEFT AND RIGHT PITOT TUBES EXCESSIVELY CORRODED. REPLACED PITOT/STATIC TUBES IAW MM 34-11-01. TESTED GOOD IAW 34-11-00 (LEAK CHECK, OP CHECK). VERIFIED HEATER OPERATIONAL. P/N: 856NF, 85NB1 S/N: 159057, 165026.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 12,265 hrs · 17,821 cycles

BUTT STRAP CENTER BETWEEN FRAMES 34-38 HAS LARGE AMOUNTS OF CORROSION AND NEEDS REPLACED. REMOVED AND REPLACED BUTT STRAP BETWEEN FRAMES 34-38 IAW SRM 51-00-00 AND 51-40-02. P/N: 27929-001.

Part: CONTROL CABLE — WORN (ELEVATOR) · airframe 12,260 hrs · 17,812 cycles

RIGHT OUTBOARD AND INBOARD ELEVATOR CABLES ARE WORN AT REAR PRESSURE BULKHEAD. REMOVED AND REPLACED RIGHT SIDE ELEVATOR CABLES WITH A SERVICEABLE CABLES IAW MM 27-00-01.

Part: CONTROL CABLE — WORN (AILERON) · airframe 12,265 hrs · 17,821 cycles

RIGHT AILERON UPPER AND LOWER CABLES WORN. REMOVED AND REPLACED RIGHT UPPER AND LOWER AILERON CABLES IAW MM 27-00-01.

Part: CONTROL CABLE — WORN (AILERON TRIM) · airframe 12,265 hrs · 17,821 cycles

AILERON TRIM CABLES WORN AT RIGHT NACELLE FEED THROUGH. REMOVED AND REPLACED TRIM CABLES FROM TRIM KNOB TO AILERON TRIM ACTUATOR IAW EMB MM 27-12-00 AND RII 27-301.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 12,265 hrs · 17,821 cycles

BUTT STRAP RIGHT SIDE BETWEEN FRAMES 30-34 HAS LARGE AMOUNTS OF CORROSION AND NEEDS REPLACED. INSTALLED NEW BUTT STRAP IAW SRM 51-00-00 AND 51-40-02. P/N: 120-46163-003.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 12,260 hrs · 17,812 cycles

BUTT STRAP BETWEEN FRAMES 34-38 ON RIGHT SIDE NEEDS REPLACED DUE TO A LARGE AMOUNT OF CORROSION. REMOVED AND REPLACED BUTT STRAP BETWEEN FRAMES 34-38 IAW SRM 51-00-00 AND 51-40-02. P/N: 120-46163-001.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 12,260 hrs · 17,812 cycles

BUTT STRAP ON LEFT SIDE HAS LARGE AMOUNT OF CORROSION AND NEEDS REPLACED BETWEEN FRAMES 34-38. FABRICATED AND INSTALLED BUTT STRAP BETWEEN FRAMES 34-38 IAW SRM 51-00-00 AND 51-40-02. P/N: 120-46163-001.

Part: CONTROL CABLE — WORN (AILERON) · airframe 12,265 hrs · 17,821 cycles

LEFT AILERON CABLES UPPER AND LOWER AT NACELLE WORN. REMOVED AND REPLACED LEFT UPPER AND LOWER AILERON CABLES WITH SERVICEABLE CABLES IAW MM 27-00-01.

Part: SILL — CORRODED (FUSELAGE) · airframe 12,260 hrs · 17,812 cycles

BUTT STRAP BETWEEN FRAMES 39-44 HAS LARGE AMOUNT OF CORROSION AND NEED REPLACED ON RIGHT SIDE (SILL). REPLACED SILL WITH A NEW PART IAW EMB SRM 51-00-00 AND 51-40-02. P/N: 120-06158-002.

Part: SOLENOID — BROKEN (FLAP ACTUATOR) · airframe 12,028 hrs · 17,459 cycles

DURING APPROACH AFTER NORMAL GEAR EXTENSION FLAPS WERE SELECTED TO 15 DEGREES. A FLAP DISAGREEMENT WITH WARNINGS WAS OBSERVED FOLLOWED BY A HYDRAULIC WARNING AND COMPLETE LOSS OF BLUE SYSTEM HYDRAULICS. APPROXIMATE 10 MINUTES AFTER INITIAL FAILURE A LEFT ANTI-SKID INOP WARNING WAS OBSERVED.FOUND RIGHT NACELLE FLAP ACTUATOR TO HAVE A BROKEN SOLENOID. REPLACED ACTUATOR IAW MM 27-50-00. REPLACED RIGHT ENGINE DRIVEN HYDRAULIC PUMP ALL HYDRAULIC FILTERS. RAN ENGINE AND NO LEAKS NOTED. FLAPS OPS CHECK GOOD AND NO ANTI-SKID WARNINGS NOTED

Part: TURBINE — FAILED (APU) · airframe 11,988 hrs · 17,397 cycles

APU FIRE ON GROUND AFTER APPARENTLY NORMAL STARTUP - NO FIRE INDICATION OBSERVED ON FIRE DETECTION SYSTEM. FIRE WAS OBSERVED EXTERNALLY. FIRE EXTINGUISHER WAS DISCHARGED FOLLOWING QRH PROCEDURE.INSPECTED APU AND SURROUNDING AREA. FOUND TURBINE FAILURE. NO OTHER DAMAGE NOTED. INSPECTED RUDDER AND SKIN SURFACES. NO DAMAGE NOTED. MEL APU PER 49-00-1. PULLED APU CONTROL CB & SECURED.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 11,163 hrs · 16,181 cycles

WHEN AUTOMATIC PRESSURIZATION REACHES 4.0 PSI, CABIN RATE GOES UP AND DOWN 72000 FT/MIN. REPLACED PNEUMATIC OUTFLOW VALVE IAW CARD RII 21-303. OPS CHECK GOOD. P/N: 2093K010800, S/N ON: 075, S/N OFF: 395.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 9,739 hrs · 14,137 cycles

ANTI SKID OUTBOARD AND MAP BRAKE LIGHT CAME ON, BASE TO FINAL TURN ON APPROACH (2 APPS) ALL INOP LIGHTS GO OUT WHEN GEAR IS RAISED. DIVERTED FROM SBA TO SMX. REMOVED AND REPLACED LANDING GEAR SELECTOR IAW 32-31-03. PERFORMED GEAR SWINGS. OPS CHECKS GOOD. (P/N 120-38294-501) ON, (S/N 120088) ON, (S/N 120333) OFF.

Part: OIL CAP — LOOSE (RT ENGINE) · airframe 9,685 hrs · 14,055 cycles

AFTER TAKEOFF, RIGHT ENGINE OIL PRESSURE FLUCTUATED AND WENT TO ZERO. RETURNED TO SAN. AFTER LANDING SHUT DOWN ENGINE. CLEANED RIGHT ENGINE AND FOUND OIL CAP HALF OFF. SERVICED RIGHT ENGINE WITH 2.5 GALLONS. RAN ENGINE, NO LEAKS NOTED. NO PRESSURE FLUCTUATIONS. REPLACED OIL CAP AS PRECAUTION.

Part: RELAY — FAILED (MAIN BATTERY)

BATTERY OFF BUS ILLUMINATED IN FLIGHT, RETURNED TO SFO. REPLACED K0022 RELAY AND MAIN BATTERY, RAN SYSTEM. OPS CK GOOD, PN ON: 40769, SN 49107, SN OFF: 44722.

Part: SEAL — LOOSE (LT ENGINE)

LEFT ENGINE TRAILING SMOKE. RETURNED TO SFO. FOUND OIL IN BREATHER TUBE. REPLACED OIL BREATHER CARBON SEAL. LEFT ENGINE RUN UP OPS CHECKS GOOD IAW MM 72-20-00.

Part: SEAL — FAILED (NR 1 ENGINE)

ATC REPORTED BLACK SMOKE COMING FROM NR 1 ENGINE ON INITIAL CLIMB-OUT. REPORTED CONFIRMED BY OTHER PILOTS ON GROUND. RETURNED FOR LANDING AT SBA. NO COCKPIT INDICATIONS OF ENGINE FIRE ON NR 1. REPLACED GARLOCK SEAL FOR AIR OIL SEPARATOR BLEEDER TUBE. PERFORMED OPS AND LEAK CHECK. OPS CHECK GOOD. NO LEAK NOTED.

Part: SEAL — FAILED (LT ENG BREATHER)

CREW REPORTS SMOKE FROM LEFT ENGINE EXHAUST AT TAKEOFF POWER. RETURNED TO SFO, REMOVED AND REPLACED LEFT ENGINE BREATHER TUBE CARBON SEAL IAW MM 72-20-00. OPS CHECKS GOOD.

Part: ANTI ICE SYST — MALFUNCTIONED (RIGHT)

INBOARD RIGHT STABILIZER INBOARD RIGHT WING, AND RIGHT ENGINE AIR INLET FAILED. PERFORMED QRH. UNSUCCESSFUL RE-TRY. RETURNED TO FIELD. RAN AIRCRAFT DE-ICE SYSTEMS IAW MM 30-10-00, DE-ICE OPS CHECKS GOOD.