N229SW

Part: FRAME — CORRODED (FRM 21) · airframe 41,293 hrs · 58,180 cycles

DURING A ROUTINE INSPECTION, CORROSION WAS NOTED AT FRAME 21, BETWEEN STRINGERS 20 AND 21R. CORROSION DAMAGE WAS REMOVED AND REPAIRED IAW SRM 53-00-01.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 39,771 hrs · 57,306 cycles

CABIN EMERGENCY LIGHT AFT FEMALE CONNECTOR IS BROKEN OFF WIRES FROM AIRFRAME. INSTALLED CONNECTOR AND REPLACED THE TERMINAL CONNECTOR IAW AMM.

Part: SHEAR TIE — CORRODED (FRAME 38) · airframe 39,771 hrs · 57,306 cycles

BELLY SKIN SHEAR TIE CORRODED AT FRAME 38. REPLACED SHEAR TIE IAW SRM.

Part: STRINGER — DAMAGED (FRAMES 43-45) · airframe 39,771 hrs · 57,306 cycles

STRINGER 20R IS DAMAGED BETWEEN FRAMES 43 AND 45. REPAIRED STRINGER IAW SRM.

Part: STRINGER — DAMAGED (FRAMES 43-45) · airframe 39,771 hrs · 57,306 cycles

STRINGER 21R IS DAMAGED BETWEEN FRAMES 43 - 45. REPAIRED STRINGER IAW SRM.

Part: STRINGER — DAMAGED (FRAMES 43-45) · airframe 39,771 hrs · 57,306 cycles

STRINGER 19L IS DAMAGED BETWEEN FRAMES 43 - 45. REPAIRED STRINGER IAW SRM.

Part: SKIN — DAMAGED (BS 1531) · airframe 39,771 hrs · 57,306 cycles

LOWER SKIN ON LEFT SIDE AND FWD OF BS 1531.8 IS DAMAGED. REPAIRED SKIN IAW ETD.

Part: SKIN — DAMAGED (BS 1531) · airframe 39,771 hrs · 57,306 cycles

LOWER SKIN ON RIGHT SIDE AND FWD OF BS 1531.8 IS DAMAGED. REPLACED LOWER SKIN IAW SRM.

Part: STRINGER — DAMAGED (FRAMES 43-45) · airframe 39,771 hrs · 57,306 cycles

STRINGER 21L IS DAMAGED BETWEEN FRAMES 43 - 45. REPAIRED STRINGER IAW SRM.

Part: STRINGER — DAMAGED (FRAMES 43-45) · airframe 39,771 hrs · 57,306 cycles

STRINGER 20L IS DAMAGED BETWEEN FRAMES 43 - 45. REPAIRED STRINGER IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,704 hrs · 57,219 cycles

WHITE EMERGENCY LIGHT ON FLOOR BY SEAT 4A IS BURNED OUT. FLT 6233 RELAMPED.

Part: UNKNOWN — ODOR (LAVATORY) · airframe 39,664 hrs · 57,166 cycles

BURNING SMELL COMING FROM LAVATORY. FLT 6246 AIR OUT AIRCRAFT, NO NEW ODOR, SUSPECT AIRCRAFT HEATING TO EMIT BURNING ODOR.

Part: WIRE — BROKEN (CABIN) · airframe 39,272 hrs · 56,607 cycles

EMERGENCY OVERHEAD LIGHTING AT ROW 8 ABC DOES NOT ILLUMINATE. FLT 5371 REPAIRED BROKEN WIRE ON LIGHT ASSEMBLY AT ROW 8 ABC.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,238 hrs · 56,554 cycles

EMERGENCY OVERHEAD LIGHTS IN ROW 9 SEATS B-C ARE BURNED OUT. FLT 6346 RELAMPED.

Part: DRAIN — BROKEN (NACELLE) · airframe 39,122 hrs · 56,414 cycles

BLUE HYDRAULIC SYSTEM NACELLE DRAIN IS CRACKED & BROKEN. C-CHECK REPLACED NACELLE DRAIN MASS ON RT OTBD NACELLE FOR BLUE HYDRAULIC SYSTEM IAW SRM.

Part: STRINGER — CRACKED (RT WING) · airframe 39,122 hrs · 56,414 cycles

RT WING HAS A CRACKED STRINGER FWD OF FUEL ACCESS PANEL CUTOUT NR 2. C-CHECK REPAIRED STRINGER NR 10 ON RT WING FWD OF NR 2 FUEL ACCESS PANEL IAW SRM.

Part: FIREWALL — CHAFED (RT NACELLE) · airframe 39,122 hrs · 56,414 cycles

RT ENGINE FIRE WALL IS CHAFED AT 12 O CLOCK POSITION. C-CHECK REPAIRED IAW ETD.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 39,122 hrs · 56,414 cycles

STRINGER 18L CORRODED NEAR FRAME 13A. C-CHECK SPLICED IN NEW FRONT SECTION OF STRINGER 18L IAW SRM.

Part: FIREWALL — CRACKED (LT NACELLE) · airframe 39,122 hrs · 56,414 cycles

LT GEAR WELL THRU ACCESS 434 FZ, FIREWALL HAS CRACKS. C-CHECK REPLACED UPPER SUPPORT BULKHEAD AT LT NACELLE FRAME 14 PART 120 32357-001 IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 39,122 hrs · 56,414 cycles

FOUND A CRACK UNDER THE CAPTAINS DV WINDOW LOWER CHANNEL ON A RIB BRACKET RIGHT NEXT TO THE TILLER HANDLE. C-CHECK NEW FRAME NR 9 SPLICED IN AT UPPER END AT LT DV WINDOW LOWER CHANNEL NEXT TO TILLER HANDLE IAW SRM.

Part: COWLING — CRACKED (LT ENGINE) · airframe 39,122 hrs · 56,414 cycles

LT EXHAUST MIDDLE COWL IS CRACKED OUT IN THE AREA BY OTBD COWL PIN LATCH RECEPTACLE AREA. C-CHECK REPAIRED LT EXHAUST MIDDLE COWL OTBD DOOR AFT PIN FRAME IAW SRM.

Part: SKIN — DAMAGED (RT NACELLE) · airframe 39,122 hrs · 56,414 cycles

RT NACELLE OTBD FWD & ABOVE MLG DOOR OVERSIZED RIVETS PULLING THROUGH SKIN. C-CHECK DOUBLER INSTALLED OVER AREA & INTERNAL TO BRING RIVETS BACK TO ORIGINAL SIZE IAW SRM.

Part: FITTING — CRACKED (LT NACELLE) · airframe 39,122 hrs · 56,414 cycles

LT NACELLE INBD FITTING CRACKED. C-CHECK REPLACED STRUCTURAL COMPONENT IAW SRM. REPLACED INBD FITTING PN 120-22916-002 AT LT NACELLE IAW SRM.

Part: FRAME — CHAFED (RT COWLING) · airframe 39,122 hrs · 56,414 cycles

RT AFT EXHAUST COWL FRAME CHAFFED. C-CHECK REPAIRED IAW SRM.

Part: SUPPORT FRAME — CRACKED (HYDRAULIC PACK) · airframe 39,122 hrs · 56,414 cycles

RT HYDRAULIC PACK LOWER SUPPORT FRAME CRACKED. C-CHECK REPLACED RT HYDRAULIC PACK LOWER SUPPORT FRAME & SECURED IAW SRM.

Part: CHANNEL — CRACKED (PAX DOOR) · airframe 39,122 hrs · 56,414 cycles

PAX DOOR CRACKED & MINOR CORROSION AT BAY 18. C-CHECK INSTALLED NEW CHANNEL PN 120-21059-001 AT PAX DOOR BAY 18 IAW SRM. CLEANED & REMOVED MINOR CORROSION ALSO TREATED AFFECTED AREAS IAW CPM.

Part: SKIN — CRACKED (RT WING) · airframe 39,122 hrs · 56,414 cycles

RT WING SKIN CLEAT CRACKED, TOP & INBD PANEL 5. C-CHECK REPLACED 1 UPPER SKIN CLEAT PN120-17063-009 ON RT WING INBD OF NR 5 FUEL PANEL IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 39,122 hrs · 56,414 cycles

RT WING SKIN CLEAT BOTTOM AFT INBD OF FUEL PANEL NR 4 CRACKED. C-CHECK REPLACED SKIN CLEAT ON RT WING INBD OF NR 4 FUEL PANEL BOTTOM IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 39,122 hrs · 56,414 cycles

LT WING L3 FUEL PANEL HAS 2 OTBD UPPER & ONE INBD SKIN CLEAT CRACKED. C-CHECK REPLACED SKIN CLEATS ON LT WING AT NR 3 FUEL PANEL UPPER OTBD IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 39,122 hrs · 56,414 cycles

RT WING SKIN CLEAT TOP 2ND AFT AT PANEL 2 CRACKED. C-CHECK REPLACED 1 UPPER SKIN CLEAT ON RT WING AFT OF NR 2 FUEL ACCESS PANEL IAW SRM.

Part: CHANNEL — CRACKED (RT NACELLE) · airframe 39,122 hrs · 56,414 cycles

RT NACELLE, INBD SIDE, CHANNEL CRACKED NEAR FWD ENGINE MOUNT. C-CHECK REPLACED ANGLE PN 120-35340-001 AT RT NACELLE, INBD SIDE, CHANNEL NEAR FWD ENGINE MOUNT IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 39,122 hrs · 56,414 cycles

RT WING SKIN CLEAT TOP MID OTBD OF FUEL STICK NR 4 CRACKED. C-CHECK REPLACED 1 UPPER SKIN CLEAT SUPPORT BRACKET PN 120-17063-009 ON RT WING OTBD OF NR 4 FUEL STICK IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 39,122 hrs · 56,414 cycles

LT WING L2 FUEL PANEL HAS 2 OTBD UPPER SKIN CLEATS CRACKED, C-CHECK REPLACED SKIN CLEATS ON LT WING NR 2 FUEL PANEL UPPER OTBD IAW SRM.

Part: FLAP — CHAFED (RT NACELLE) · airframe 39,122 hrs · 56,414 cycles

RT NACELLE FLAP EXTERIOR SIDE CHAFED NEAR INBD HINGE. C-CHECK REPLACED RT NACELLE FLAP IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 39,122 hrs · 56,414 cycles

RT WING SKIN CLEAT TOP MID OTBD OF FUEL PANEL NR 4 CRACKED. C-CHECK REPLACED 1 UPPER SKIN CLEAT PN120-17063-009 ON RT WING OTBD OF NR 4 FUEL PANEL IAW SRM.

Part: SKIN — CRACKED (LT WING) · airframe 39,122 hrs · 56,414 cycles

LT WING FUEL PANEL L4 FROM OTBD NACELLE HAS FOUR CRACKED SKIN CLEATS ON UPPER INBD SIDE OF BAY. C-CHECK REPLACED SKIN CLEATS ON LT WING FUEL PANEL NR 4 UPPER INBD IAW SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 39,122 hrs · 56,414 cycles

STRINGER 19L AT FRAME 13A HAS CORROSION. C-CHECK SPLICED NEW FRONT SECTION OF STRINGER 19L IAW SRM.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 39,122 hrs · 56,414 cycles

CORROSION ON CENTER FLOOR BUTT STRAP BETWEEN FRAME 31 TO FRAME 37. C-CHECK REPLACED BUTT STRAP PN 120-46163-001 AT FUSELAGE CENTER FLOOR BETWEEN FRAME 31 TO FRAME 37 IAW SRM.

Part: FRAME — CHAFED (FUSELAGE) · airframe 39,122 hrs · 56,414 cycles

CHAFED FRAME ON RT HYD BAY FWD SIDE. C-CHECK REPLACED RT HYD BAY FWD CUT OUT FRAME PN 120-44444-002 IAW SRM.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 39,122 hrs · 56,414 cycles

RT WING, RIB 21, 3 UPPER FWD MOST SKIN CLEAT SUPPORT BRACKETS CRACKED. C-CHECK REPLACED 3 SKIN CLEAT SUPPORT BRACKETS PN120-17062-613 & 120-17063-609 ON RT WING AT RIB 21 FIRST THREE FWD IAW SRM.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 39,122 hrs · 56,414 cycles

RT WING RIB 20, 2ND FWD MOST, UPPER SKIN CLEAT SUPPORT BRACKET CRACKED. C-CHECK REPLACED 1 UPPER SKIN CLEATS SUPPORT BRACKET PN120-17063-009 AT RT WING RIB 20 IAW SRM.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 39,122 hrs · 56,414 cycles

RT WING RIB 22, 2ND & 3RD FWD MOST, UPPER SKIN CLEAT SUPPORT BRACKETS CRACKED. C-CHECK REPLACED 2 UPPER SKIN CLEATS SUPPORT BRACKET PN120-17063-009 AT RT WING RIB 22 IAW SRM.

Part: SIGN — BROKEN (CABIN) · airframe 38,848 hrs · 55,999 cycles

FLOOR LEVEL EXIT ROW SIGN SEAT 6C IS BROKEN. FLT#5362 RELAMPED.

Part: WIRE — DAMAGED (OIL INDICATION) · airframe 38,502 hrs · 55,524 cycles

LEFT ENGINE HIGH OIL PRESSURE INDICATION ON THE GAUGE, NO MAP WARNING INDICATION. SHUTDOWN LT ENGINE, DECLARED AN EMERGENCY AND CONTINUED ON. UNDER THE FLOORBOARD OF SEAT 2A FOUND WIRES W11O-1779-24, W110-260-24, W110-0859-24 AND W110-4637-24 CHAFFED TO AIRFRAME. REPAIRED WIRES W110-1779-24, W110-0260-24, W110-0859-24 AND W110-4637-24 IAW EMB WDM. ALL FOUR WIRES OHMED AND MEGGED OUT GOOD. PERFORMED ENG RUNS FOR OIL PRESSURE INDICATIONS WITH AIRCRAFT PRESSURIZATION WITH NO FAULT INDICATION NOTED. OPS CHECK GOOD.

Part: TERMINAL — DAMAGED (EXIT SIGN) · airframe 38,159 hrs · 55,010 cycles

EMERGENCY EXIT LIGHT IN FORWARD CABIN DOES NOT ILLUMINATE. (FLT 5387) REPAIRED TERMINAL END ON EMERGENCY EXIT SIGN IN CABIN FORWARD OF SEAT 1 C/B.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,650 hrs · 54,278 cycles

EMERGENCY OVERHEAD LIGHT OVER MAIN CABIN DOOR BURNED OUT. (FLT 5458) RELAMPED EMERGENCY LIGHT.

Part: WIRE — DAMAGED (CABIN) · airframe 37,527 hrs · 54,112 cycles

SECOND RED FLOOR TRACK LIGHT INOPERATIVE. (SERVICE) REPAIRED WIRE ON FLOOR EMERGENCY TRACK LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,502 hrs · 54,073 cycles

EMERGENCY LIGHT ON FLOOR AT 2A BURNED OUT. (FLT 5321) RELAMPED EMERGENCY LIGHT.

Part: WIRE — LOOSE (CABIN) · airframe 37,422 hrs · 53,958 cycles

LOOSE WIRES COMING OUT OF THE EMERGENCY FLOOR LIGHTS IN ROW 1. EMERGENCY LIGHTS ASSOCIATED WITH THE LOOSE WIRES ARE INOPERATIVE. (FLT 3453) RECONNECTED WIRES FOR THE EMERGENCY FLOOR LIGHT LEVEL IN ROW 1.

Part: SIGN — UNSECURE (CABIN) · airframe 35,784 hrs · 51,666 cycles

EXIT SIGN AT 6A FELL OFF OVER PASSENGER SEAT. (FLT 6262) RE-SECURED EXIT SIGN OVER PASSENGER SEAT 6A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,494 hrs · 51,279 cycles

OVERHEAD EMERGENCY LIGHT AT 6A IS OUT. (FLT 6317) RELAMPED EMERGENCY LIGHT.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 35,567 hrs · 51,393 cycles

CORROSION IN LAV AREA ON RIGHT OUTBOARD BUTTSTRAP. (C-CHECK) REPLACED RIGHT OUTBOARD BUTTSTRAP OF LAV AREA.

Part: INERTIA REEL — STUCK (COCKPIT) · airframe 35,473 hrs · 51,251 cycles

CAPTAIN'S SHOULDER HARNESS INERTIAL REEL WILL NOT RELEASE. (FLT 5338) REPLACED CAPTAIN'S SHOULDER HARNESS / INERTIA REEL ASSEMBLY.

Part: SEQUENCE VALVE — OUT OF ADJUST (LT MLG) · airframe 34,853 hrs · 50,377 cycles

LEFT MAIN GEAR FAILED TO RETRACT. (FLT 5319) ADJUSTED LEFT GEAR SEQUENCE VALVES.

Part: DUCT — BURST (BLEED AIR SYS) · airframe 34,565 hrs · 49,947 cycles

RIGHT ENGINE BLEED DUCT FAILURE. (FLT 6264) REPLACED RIGHT ENGINE BLEED DUCT ASSEMBLY. (P/N 120-50475-013) REPLACED RIGHT ENGINE PRESSURE REGULATING SHUT-OFF VALVE. (P/N 3214414-3, S/N 972).

Part: BOLT — OUT OF ADJUST (LT MLG) · airframe 34,501 hrs · 49,851 cycles

LEFT MAIN GEAR DID NOT RETRACT. (FLT 5490) ADJUSTED LEFT MAIN LANDING GEAR OUTBOARD SEQUENCE VALVE ACTUATING BOLT.

Part: SKIN — CORRODED (FUSELAGE) · airframe 33,713 hrs · 48,775 cycles

FOUND CORROSION ON FUSELAGE TO THE RIGHT OF SPINE JUST FORWARD OF LAV SERVICE ACCESS PANEL AND LOWER CENTER FUSELAGE SKIN AT STATION 30. (SERVICE) REPAIRED CORROSION ON FUSELAGE PER ETD AND SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,610 hrs · 48,633 cycles

FLOOR LEVEL EMERGENCY LIGHT AT 11A IS OUT. (FLT 6814) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,181 hrs · 48,032 cycles

FORWARD FLOOR LEVEL RED EMERGENCY LIGHT INOPERATIVE. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: WIRE — BROKEN (CABIN) · airframe 32,850 hrs · 47,579 cycles

EMERGENCY EXIT LIGHT AT ROW 9, INOPERATIVE. (FLT 6832) REPAIRED BROKEN WIRE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,793 hrs · 47,499 cycles

EMERGENCY LIGHT OVER 9C INOPERATIVE. (FLT 6653) RELAMPED EMERGENCY LIGHT.

Part: STRINGER — CRACKED (RT WING) · airframe 32,771 hrs · 47,468 cycles

RIGHT WING INBOARD STRINGER NR 10 CRACKED AT DEFUEL PANEL. (C-CHECK) REPAIRED RIGHT WING INBOARD STRINGER NR 10 AT DEFUEL PANEL PER SRM.

Part: LIGHT — NOT SEATED (CABIN) · airframe 32,345 hrs · 46,873 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 9 EXIT INOP. (FLT 6317) RE-SEATED BULB.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,284 hrs · 46,777 cycles

FORWARD RED EMERGENCY LIGHT INOP. (FLT 6312) REPLACED FORWARD EMERGENCY LIGHT FIXTURE ON FLOOR.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,284 hrs · 46,777 cycles

MIDDLE SECTION OF EMERGENCY FLOOR LIGHTS INOP. (FLT 6409) REPLACED MIDDLE BATTERY PACK.

Part: MECHANISM — LACK OF LUBE (CABIN DOOR) · airframe 32,121 hrs · 46,552 cycles

MAIN CABIN DOOR LEVER HARD TO OPEN. (FLT 6822) LUBRICATED MAIN CABIN DOOR MECHANISM.

Part: HANDLE — LACK OF LUBE (CABIN DOOR) · airframe 32,091 hrs · 46,508 cycles

MAIN CABIN DOOR HANDLE DIFFICULT TO OPEN. (FLT 6821) LUBRICATED DOOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,091 hrs · 46,508 cycles

OVERHEAD EXIT ROW LIGHT INOP AT SEAT 9B AND 9C. (FLT 5879) RELAMPED OVERHEAD EXIT LIGHT.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 31,939 hrs · 46,282 cycles

FOUR FLOOR EMERGENCY LIGHTS INOP BETWEEN ROWS 4 AND 5. (FLT 6318) RESEATED CONNECTOR.

Part: WIRE — LOOSE (CABIN) · airframe 31,263 hrs · 45,292 cycles

FORWARD BULKHEAD EMERGENCY LIGHT WIRE LOOSE. (FLT 5965) RE-SECURED WIRE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 29,932 hrs · 43,380 cycles

FLT 6338 - RIGHT EXTERIOR EMERGENCY LIGHT INOP. REPLACED AFT ELBP.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 29,892 hrs · 43,329 cycles

FLT 5970 - OVERHEAD BIN EMERGENCY EXIT SIGN INOP. REPAIRED BROKEN WIRE AT OVERHEAD BIN.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 29,796 hrs · 43,209 cycles

EMERGENCY LIGHTS INOP. REPLACED ELBP, PN D366-04-001, SN OFF 794.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 29,613 hrs · 42,959 cycles

C-CHECK, PASSENGER DOOR ENTRANCE THRESHOLD LOWER FRAME CORRODED. REPLACED PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 29,613 hrs · 42,959 cycles

C-CHECK, FRAME 32 CENTER BELLY OF AIRCRAFT HAS ONE SKIN SUPPORT CORRODED. REPLACED SUPPORT PER SRM.

Part: BUTTSTRAP — CORRODED (CARGO BAY) · airframe 29,613 hrs · 42,959 cycles

C-CHECK, CARGO COMPARTMENT LEFT OUTBOARD FLOOR BUTT STRAP CORRODED. REPLACED PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,613 hrs · 42,959 cycles

C-CHECK, 2 CROSS MEMBERS AT FRAME 37 HAVE CRACKS AND CORROSION. REPLACED CROSSMEMBERS PER SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,613 hrs · 42,959 cycles

C-CHECK, RIGHT SIDE FLOOR SEAT TRACK MOST FORWARD SECTION CORRODED AND FLAKING UP. REPLACED PER EMB EST-186/96.

Part: BUTTSTRAP — CORRODED · airframe 29,613 hrs · 42,959 cycles

C-CHECK, BUTT STRAPS BETWEEN LAV AND GALLEY CORRODED. REPLACED PER SRM.

Part: STRINGER — CRACKED (LT WING) · airframe 28,578 hrs · 41,557 cycles

LEFT WING STRINGER 8 IS CRACKED INBOARD OF RIB 5. REPAIRED STRINGER ON LEFT WING PER EMB 120 SRM 57-20-03 FIG 202.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 27,708 hrs · 40,364 cycles

FLT 5714 - TWO SECTIONS OF FLOOR EMERGENCY LIGHT TRACK ARE INOP. REPLACED FORWARD EMERGENCY BATTERY WITH SERVICEABLE UNIT. OPS CHECKS GOOD.

Part: ACTUATOR — LEAKING (TE FLAPS) · airframe 27,461 hrs · 40,028 cycles

FLT 5608 - LOST BLUE SYSTEM HYDRAULIC FLUID AFTER SELECTING FLAPS 15 ON APPROACH. REPLACED RIGHT NACELLE FLAP ACTUATOR IAW 27-50-03.

Part: UNKNOWN — ODOR (CABIN) · airframe 27,047 hrs · 39,432 cycles

PASSENGERS AND FLIGHT ATTENDANT COMPLAINED OF SMOKE IN THE CABIN WITH AN ELECTRICAL BURNING ODOR, FLIGHT NR 5727. RAN RIGHT PACK WITH APU AIR FOR 30 MIN. RAN EACH ENGINE WITH PACKS ON AT 30 MIN EACH. NO BURNING OR OVERHEAT ODOR NOTED AT THIS TIME.

Part: BEARING — CORRODED (LT AILERON) · airframe 26,011 hrs · 37,946 cycles

LEFT AILERON QUADRANT BEARINGS ARE CORRODED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED BEARINGS ON LEFT AILERON QUADRANT ASSEMBLY.

Part: SKIN — CORRODED (FUSELAGE) · airframe 26,011 hrs · 37,946 cycles

UNDER FLOOR BETWEEN STATION 38 AND 39 FOUND HOLE CORRODED THROUGH SKIN, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER EMB IC2007-120/1728D AND EMB 120 SRM 51-40-02.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,882 hrs · 34,834 cycles

MIDDLE EMERGENCY LIGHTS OUT. REPLACED MIDDLE EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD.

Part: LIGHT — CRACKED (CABIN) · airframe 23,690 hrs · 34,524 cycles

FOUND EXIT ROW LIGHT CRACKED. REPLACED EXIT ROW LIGHT AS NEEDED.

Part: CONTROL PANEL — MALFUNCTIONED (STALL WARNING) · airframe 23,643 hrs · 34,459 cycles

DURING FLIGHT, STALL WARN INDICATOR ON MAP CAME ON. REPLACED STALL WARNING SWITCH PANEL. OPERATIONAL CHECK GOOD IAW MM 27-34-00. P/N 120-34428-505; S/N OFF 120-287.

Part: FRAME — CRACKED (FR 13) · airframe 22,572 hrs · 32,808 cycles

ANGLE OPPOSITE FROM COCKPIT LT FLOOR PROP AT FRAME 13 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE OPPOSITE FROM COCKPIT LT FLOOR PROP AT FRAME 13 IAW SRM 51-40-02.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 21,868 hrs · 31,729 cycles

CENTER SECTION OF CABIN EMERGENCY LIGHTS APPEAR INOPERATIVE. REPLACED MIDDLE ELBP IAW MM 24-33-01. OPERATIONAL CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (AUTOPILOT) · airframe 19,762 hrs · 28,428 cycles

FIRST OFFICER'S SIDE AUTO PILOT HAD SEVERAL -TRIM FAIL- AURAL WARNINGS WITH ASSOCIATED RED -TRIM- FAIL LIGHTS. REPLACED FIRST OFFICER'S AUTO PILOT COMPUTER. OPS CHECK GOOD.

Part: SERVO — INOPERATIVE (STICK SHAKER) · airframe 19,762 hrs · 28,428 cycles

NR 2 STALL SHAKER INOP. REPLACED FIRST OFFICER'S STICK SHAKER SERVO PER MM 27-00-00. OPS CHECK GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 19,266 hrs · 27,668 cycles

CABIN CENTER FLOORBEAM FLOORBOARD SUPPORT HAS CORROSION (AFT OF MUFFLER ASSY). (DISCOVERED DURING C-CHECK INSPECTION)REPLACED CENTER BEAM BUTT STRAPS, 2 EACH, 1 FORWARD AND 1 AFT OF LAVATORY IAW 120 SRM 51-10-02 PG 3 SEC 3.

Part: FRAME — CRACKED (RT NACELLE) · airframe 19,266 hrs · 27,668 cycles

RT NACELLE FRAME CRACKED AFT CENTER JUST BELOW JET PIPE. DISCOVERED DURING C-CHECK INSPECTION. DOUBLER REINFORCEMENT INSTALLED AT AFFECTED RT NACELLE AREA IAW EMB120 SRM 51-40-02.

Part: SIGN — INOPERATIVE (CABIN) · airframe 18,562 hrs · 26,570 cycles

MAIN ENTRYWAY EMERGENCY EXIT SIGN DOES NOT ILLUMINATE. REPLACED EMERGENCY EXIT SIGN WITH A SERVICEABLE UNIT AT PAX DOOR . OPS TEST GOOD.

Part: FCU — MALFUNCTIONED (LT FLAPS) · airframe 17,483 hrs · 24,915 cycles

LEFT INBOARD FLAP POSITIONS ITSELF TO 45 DEGREES. ASYMMETRY SHOWN IN FLAP (OVERHEAD) WINDOW. INSTALLED SERVICEABLE FLAP CONTROL UNIT. GROUND OPS CHECK GOOD.

Part: YOKE — CRACKED (CONTROL COLUMN) · airframe 17,037 hrs · 24,233 cycles

CAPTAINS YOKE IS CRACKED. REMOVED AND REPLACED CAPTAIN'S YOKE IAW 07-11-01. OPS CHECK GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 16,326 hrs · 23,085 cycles

PRIOR TO BRAKE RELEASE ON TAKEOFF, THE AUTOFEATHER GREEN ARMED LIGHT WAS ILLUMINATED. IMMEDIATELY AFTER BRAKE RELEASE, THE AURAL WARNING FOR AUTOFEATHER SOUNDED AND TAKEOFF WAS ABORTED. REMOVED AND REPLACED AURAL WARNING UNIT WITH SERVICEABLE UNIT. PERFORMED ENGINE RUN-UP AT TAKEOFF POWER SETTINGS WITH AUTO FEATHER SYSTEM ARMED. ALL CHECKS GOOD, NO AUTOFEATHER AURAL WARNING. AUTO FEATHER FUNCTIONAL CHECK GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LT MLG) · airframe 15,723 hrs · 22,170 cycles

LEFT LANDING GEAR B RED LIGHT CAME ON INTERMITTENTLY. ADJUSTED B DOWNLOCK PROXIMITY SENSOR GAP. VERIFIED A AND B PROXIMITY SENSOR STRIKER PLATE ADJUSTMENT CHECKS GOOD. NO OTHER DEFECTS NOTED. OPS CHECK GOOD IAW 32-61-01.

Part: CLIP — CRACKED (FUSELAGE) · airframe 15,643 hrs · 22,041 cycles

FRAME 9 SKIN CLIP CRACKED ON COPILOT'S SIDE.

Part: WEB — CRACKED (RT NACELLE) · airframe 15,643 hrs · 22,041 cycles

NACELLE WEB ON INBOARD RIGHT NACELLE CRACKED. INSTALLED NEW INBOARD FITTING AFT OF FRAME 13 AT NACELLE STATION 2425, SRM 51-10-02 AND 51-40-02.

Part: COMPARATOR — FAULTY (NR 2) · airframe 15,593 hrs · 21,956 cycles

DURING FLIGHT, ATT DISPLAY ON MAP CAME ON. A/P DISCONNECTED, GYRO AND COMPUTER FLAGS ON COPILOT'S ADI, HDG FLAG ON COPILOT'S HSI. AFTER A/P DISCONNECT FLAGS WENT AWAY, BUT DURING TURNS F/O'S ATT IND STAYED STRAIGHT AND LVL. F/O COMMAND BARS SHOW BELOW AIRPLANE SYMBOL. REPLACED NR 2 AHC85 WITH SERVICEABLE UNIT. OPS CHECK GOOD ON TAXI. S/N OFF: 2731.

Part: COMPARATOR — FAILED (NR 2) · airframe 15,593 hrs · 21,956 cycles

F/O ADI WON'T DISPLAY A/C ATT TURNING GAUGES GYRO, COMP AND HDG FLAGS. REPLACED NR 2 AHC85 WITH SERVICEABLE UNIT. OPS CHECK GOOD ON TAXI. S/N OFF: 2731.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 15,492 hrs · 21,812 cycles

ABORTED TAKEOFF DUE TO TAKEOFF AURAL WARNING. AURAL WARNING CB FOUND POPPED. COMPLIED WITH TEST OF AURAL WARNING UNIT PER EMB MM 31-53-00. OPS CHECK GOOD AT THIS TIME.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 14,248 hrs · 20,011 cycles

WHEN FLAPS WERE SELECTED TO 15 DEGREES ON APPROACH, FLAP DISAGREEMENT WAS NOTED FOLLOWED BY LOSS OF BLUE HYDRAULIC SYSTEM. REPLACED RIGHT NACELLE FLAP ACTUATOR IAW EMB 120 MM 27-50-00. OPS AND LEAK CHECK GOOD. SERVICED BLUE HYDRAULIC RESERVOIR AND CHECKED HYDRAULIC PUMPS. ALL CHECKS GOOD. P/N ON 343100-1001, S/N ON 0177, S/N OFF 0210.

Part: BOOT — FAILED (LT ENGINE) · airframe 13,940 hrs · 19,570 cycles

OVER VTU IN ICING CONDITIONS, BOTH ENGINE DEICE BOOTS FAILED. RECYCLED SWITCHES, LEFT ENGINE DEICE BOOT FAILED AND RIGHT ONE WORKED NORMALLY. RETURNED TO LAX. REPLACED LEFT ENGINE INLET DUCT WITH SERVICEABLE UNIT. S/N OFF 080 ON 213. RAN ENGINE, OPS CHECKS GOOD.

Part: COMPUTER — FAULTY (STALL WARNING) · airframe 13,672 hrs · 19,175 cycles

AFTER TAKEOFF STALL WARNING LIGHT WITH ASSOCIATED TRIPLE CHIME WENT ON THEN OFF. REPEATED EVERY FEW MINUTES, BUT NO STALL WARNING PANEL LIGHT. REPLACED NUMBER TWO STALL WARNING COMPUTER WITH SERVICEABLE UNIT. ALSO, REPLACED STALL WARNING CONTROL PANEL WITH SERVICEABLE ASSEMBLY. ALL CHECKS AND TESTS FOUND GOOD. COMP SN ON 748, SN OFF 751, CONT PANEL SN ON 120-092R, SN OFF 083366999.

Part: ACTUATOR — FAILED (RUDDER) · airframe 13,503 hrs · 18,919 cycles

DURING DESCENT, RUDDER REQUIRED FULL NOSE LEFT RUDDER TRIM TRAVEL TO STOP. RUDDER TRIM INEFFECTIVE. PERFORMED RUDDER ACT HEALTH CHECK, AND PCU CHECK IAW EMB 120 MM 27-22-00. FOUND GREEN RUDDER ACTUATOR TO FAIL. REMOVED AND REPLACED GREEN RUDDER ACTUATOR WITH A SERVICEABLE PART. CHECKED OPERATION OF RUDDER AND RUDDER TRIM SATISFACTORY REF EMB MM 27-22-02. P/N ON: 308140-1003, S/N ON: 00026, S/N OFF 0650. PERFORMED OPS CHECK ON RUDDER AND RUDDER TRIM. WITH AUTOPILOT YAW ENGAGED SEEMS TO OPERATE A LITTLE SLOW USING RUDDER TRIM WHEEL. ALL OTHER FUNCTIONS OPERATE NORMAL. REPLACED RUDDER SERVO IAW MM 22-10-00, OPS CHECK GOOD. P/N ON: 622-5734-002, S/N ON: 1604, S/N OFF: 7835.

Part: CONTROL BOX — MALFUNCTIONED (LANDING GEAR) · airframe 13,503 hrs · 18,919 cycles

UPON RETRACTION AFTER TAKEOFF ALL OF THE LANDING GEAR RED AND GREEN LIGHTS ILLUMINATE WITHOUT COMPLETING GEAR RETRACTION. WHEN RECYCLED, LANDING GEAR ONLY RETRACTS AFTER ABOUT A 5 SECOND DELAY AND EXTENDS NORMALLY. PERFORMED MULTIPLE GEAR SWINGS, COULD NOT DUPLICATE. REPLACED LANDING GEAR CONTROL BOX FOR TROUBLESHOOTING. OPS CHECK GOOD. P/N 120-38594-501, S/N ON: 120060, OFF: 148922-305.

Part: LATCH — LOOSE (FUEL DOOR) · airframe 13,286 hrs · 18,588 cycles

AT 90 KNOTS TAKEOFF ROLL, GOT DOOR WARNING ON MAP AND FLASHING MASTER WARNING. NO TRIPLE CHIME LIGHT WENT OFF ON DECELERATION. FOUND INBOARD FUEL SERVICE DOOR AFT CAMLOC TO BE LOOSE AND PUSHED THROUGH. REPLACED CAMLOC AND ADJUSTED SWITCH ON OUTBOARD FUEL SERVICE DOOR. OPS CHECKS GOOD.

Part: COMPUTER — FAILED (AHRS) · airframe 12,919 hrs · 18,057 cycles

INTERMITTENT HDG AND ATT FLAGS AND COMPUTER FLAG ATT INDICATOR WANDERING ON CAPTAINS SIDE. ABORTED TAKEOFF. REPLACED NUMBER ONE AHRS COMPUTER. OPS CHECK GOOD. P/N 622-6190-204, S/N 2746.

Part: INDICATOR — FLUCTUATES (RT ENG TORQUE) · airframe 12,531 hrs · 17,492 cycles

RIGHT ENGINE TORQUE GAUGE INDICATION FLUCTUATES WHILE VIBRATION FELT DURING CLIMBOUT. RETURNED TO SBA. INSTALLED SCU AND TORQUE PROBE IAW 61-23-00 AND 71-00-00. PERFORMED RUN TEST AND GROUND POWER TEST. OPS CHECKS GOOD. NO ABNORMAL VIBRATIONS FELT. (S/N MM4430) (S/N 1324) OFF - SCU (S/N MM1850) (S/N 0553) OFF - PROBE.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 11,916 hrs · 16,615 cycles

C-CHECK, CABIN EMERGENCY LIGHT ON RIGHT FORWARD EXIT BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT RIGHT HAND OVERWING EMERGENCY EXIT WITH SERVICEABLE UNIT. OPS CHECK GOOD. (P/N 10130115) MR #24634.

Part: ENGINE — MALFUNCTIONED (LEFT)

PULLING POWER BACK AT 6,000 FEET, TORQUE DROPPED AND AIRCRAFT YAWED. RETURNED TO SFO. PERFORMED POWER RUN ON LEFT ENGINE, ON GROUND AND COULD NOT DUPLICATE DISCREPANCY. DEFERRED LEFT EEC FOR TROUBLESHOOTING AS PER MEL 73211.

Part: ACTUATOR — FAILED (RUDDER)

AFTER TAKEOFF IN CLIMB, RIGHT RUDDER LOCKED AND RESTRICTED IN FORWARD TRAVEL. RETURNED TO SAN. REPLACED BLUE HYDRAULIC SYSTEM RUDDER ACTUATOR PER MM 27-22-02. NO LEAKS NOTED.

Part: TQ PROBE — FAILED (RT ENGINE)

DURING FLIGHT, RIGHT TORQUE FLUCTUATES FROM 64 PERCENTS DOWN TO 0 PERCENTS (ANALOG AND DIGITAL). RETURNED TO SFO. REPLACED RIGHT ENGINE TORQUE PROBE. OPS CHECKED GOOD ON ENGINE RUN.

Part: TRANSDUCER — FAILED (LT ENGINE)

LEFT OIL PRESSURE DROPPED TO APPROXIMATELY 50 PSI AND STAYED IN YELLOW ARC. DIVERTED FROM MRY TO SBA. REPLACED LEFT OIL PRESSURE TRANSDUCER. PERFORMED RUNS AT ALL POWER SETTINGS, OPS AND LEAK CHECKS GOOD.

Part: DOOR SEAL — LOOSE (CARGO COMPT)

CABIN WOULD NOT PRESSURIZE AND CABIN ALT REMAINED AT 10,000 THROUGH OUT CLIMB. RESECURED ELECTRO PNEUMATIC VALVE CLOSED AS PER MEL 21-30-01, GROUND RUN SHOWS MANUAL CHECKS GOOD. FOUND LOOSE SECTION OF CARGO DOOR SEAL. PRESSURIZED ACFT TO 5.0 PSID IN AUTO AND MANUAL, OPS CHECKS GOOD. RESTORED ELECTRO PNEUMATIC VALVE TO NORMAL.