N133YV

Part: SPAR — CORRODED (LT WING)

REPAIRED CORRSION ON LT WING MAIN SPAR FWD FLANGE AT WS. 126 AND AFT FLANGE AT WS. 117 IAW FR-CO-01467 REV.1

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 21,756 hrs · 32,772 cycles

SEAT TRACK REPAIR AT STATION LOCATION 190, 257, 369, 220, 264. REPAIRED IAW EA REPAIR 1900D 133-1 REV 1.

Part: RIB — CORRODED (RT WING)

CORROSION RT WING LEADING EDGE RIB LOWER FLANGE, AT WS 124.588. REPAIRED IAW REPORT 6452-1 REV. 1R.

Part: INDICATOR — FAILED (PROPELLER) · airframe 19,238 hrs · 28,607 cycles

UPON TAXI OFF ROLL, CREW OBSERVED LEFT PROP RPM INDICATOR STUCK AT 1300 RPM. ABORTED TAKEOFF AND RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED PROP TACH INDICATOR.

Part: STRUT WIPER — LOOSE (MLG) · airframe 19,229 hrs · 28,592 cycles

ON A WALK AROUND (PREFLIGHT) THE CREW DISCOVERED THE STRUT WIPER WAS LOOSE. MAINTENANCE REMOVED AND REPLACED THE RT MAIN LANDING GEAR ASSEMBLY.

Part: MASTER CYLINDER — DEFECTIVE (RIGHT) · airframe 18,319 hrs · 26,923 cycles

ON PREFLIGHT, CREW FOUND RIGHT BRAKE SPONGING FIRST FLIGHT OF THE DAY. REMOVED AND REPLACED FO'S RIGHT HAND MASTER CYLINDER, P/N 90-380001-33 S/N 6675 P/N MS27039-1-21 S/N 2931 (OFF), P/N MS20392-2C23 P/N NA815-4D.

Part: HOSE — DEFECTIVE (RT BRAKE) · airframe 18,310 hrs · 26,896 cycles

UPON TAXI IN TO MSS, CREW EXPERIENCED WEAK BRAKING ACTION ON RT BRAKE, CONTIUED TO GATE W/ NO FURTHER INCIDENT. REMOVED AND REPLACED BRAKE HOSE AT BRAKE ASSY. OPS CK GOOD.

Part: MASTER CYLINDER — CONTAMINATED (RT BRAKE) · airframe 18,310 hrs · 26,896 cycles

UPON TAXI IN, CREW EXPERIENCED WEAK BRAKING ACTION ON THE RT BRAKE, CONTINUED TO GATE WITH NO FURTHER INCIDENT. BLED MASTER CYLINDER.

Part: BRAKE — WEAK (RIGHT) · airframe 18,305 hrs · 26,888 cycles

CREW REPORTED F/O AND CAPT RIGHT BRAKES WEAK. REMOVED AND REPLACED BOTH RT BRAKES P/N 114-388024-1 (ON) S/N SEP92-1204 (ON). P/N 114-388024-1 (OFF) S/N AUG94-1598 (OFF). P/N 114-388024-1 (ON) S/N OCT90-978 (ON). P/N 114-388024-1 (OFF) S/N JUN90-793 (OFF)

Part: BRAKE ASSY — MALFUNCTIONED (MLG) · airframe 18,295 hrs · 26,872 cycles

ON TAXI RIGHT BRAKES FELT SPONGY. BLED BRAKES AND SERVICED FLUID.

Part: COWLING — SEPARATED (LT ENGINE) · airframe 17,658 hrs · 25,835 cycles

PILOT RECEIVED REPORT FROM PASSENGER THAT PART OF THE LT ENG COWL MAY HAVE BLOWN OFF. PILOT CONTINUED TO DESTINATION AND LANDED WITH NO FURTHER INCIDENT. UPON IMMEDIATE WALK AROUND FOUND THAT LT ENG OB COWLING PANEL WAS MISSING AND HAD DEPARTED AIRCRAFT IN FLIGHT. INSTALLED NEW TOP CENTER COWL/FABRICATED P/N 118-910028-3 AND 129-910043-601.

Part: INDICATOR — MALFUNCTIONED (TE FLAPS) · airframe 17,632 hrs · 25,784 cycles

UPON APPROACH, FLAP POSITION INDICATOR WOULD NOT INDICATE BEYOND 10 DEGREES DOWN. PILOT ACCOMPLISHED TOWER FLYBY FOR FLAP POSITION VERIFICATION. AIRCRAFT LANDED WITH FLAPS DOWN FULL WITH NO FURTHER INCIDENT. REMOVED AND REPLACED FLAP INDICATOR, OPS CHECK NORMAL. P/N 129-380002-1, S/N 542.

Part: UPLOCK SWITCH — MALFUNCTIONED (LT MLG) · airframe 17,573 hrs · 25,681 cycles

AFTER TAKEOFF FROM CLT TO LWB, GEAR WAS SELECTED UP, GEAR HANDLE INTRANSIT LIGHT REMAINED ILLUM. AIRCRAFT THEN RETURNED TO CLT. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE. REMOVED AND REPLACED LEFT HAND MAIN LANDING GEAR UPLOCK SWITCH. P/N 101-384137-7, S/N 1170.

Part: FIRE LOOP — DAMAGED (ENGINES) · airframe 17,439 hrs · 25,406 cycles

ON TAXI OUT RT FIRE WALL T-HANDLE ILLUMINATED. BOTH ENGINES SHUT DOWN. PAX DEPLANED. AIRCRAFT WAS TOWED BACK TO GATE WITH NO FURTHER INCIDENT. FOUND & ELIMINATED LEAK, R&R FWD FIRE LOOP.

Part: WARNING LIGHT — FALSE ACTIVATION (RT ENG FIRE) · airframe 17,439 hrs · 25,406 cycles

UPON TAXI RT FIREWALL FUEL VALVE ILLUMINATED. NO FIRE WAS VISUALLY NOTED AT NR 2 ENG. LT & RT FIRE EXTINGUISHING BOTTLES WERE DISCHARGED TO NR 2 ENG. AIRCRAFT SHUTDOWN ON TAXI WAY. PAX EVACUATED ON TAXI WAY. R & R FIRE BOTTLES SQUIBS.

Part: FIRE DETECTOR — FALSE ACTIVATION (CABIN) · airframe 17,316 hrs · 25,175 cycles

ON TAXI FIRE WARNING WAS INDICATED AT NR 2 ENGINE FOR APPROX 20 SECONDS THEN NORMAL. NO FIRE NOTICED BY CREW. RETURNED TO GATE WITH NO FURTHER INCIDENT. R&R'D FIRE DETECT/CONTROL BOX&A-319 PCB.

Part: FASTENER — CORRODED (FUSELAGE) · airframe 16,888 hrs · 24,411 cycles

DURING SCHEDULED D-STRUCTURAL INSPECTION, SEVEN FASTENERS AT RWS 125-131 WERE FOUND TO HAVE EVIDENCE OF CORROSION.

Part: FASTENER — CORRODED (FUSELAGE) · airframe 16,888 hrs · 24,411 cycles

DURING SCHEDULED D-STRUCTURAL INSPECTION, THREE FASTENERS AT RWS 102 WAS FOUND TO HAVE EVIDENCE OF CORROSION.

Part: FASTENER — CORRODED (FUSELAGE) · airframe 16,888 hrs · 24,411 cycles

DURING SCHEDULED STRUCTURAL INSPECTION, TWO FASTENERS AT LWS 55 WERE FOUND TO HAVE EVIDENCE OF CORROSION.

Part: RIVET — SHEARED (FUSELAGE) · airframe 16,888 hrs · 24,411 cycles

DURING SCHEDULED ABCD STRUCTURAL INSPECTION, THE RIGHT SIDE WINDOW FINGER DOUBLER WAS FOUND TO HAVE ONE SHEARED RIVET.

Part: FASTENER — CORRODED (FUSELAGE) · airframe 16,888 hrs · 24,411 cycles

DURING SCHEDULED D-STRUCTURAL INSPECTION, FASTENERS AT LWS 102 WAS FOUND TO HAVE EVIDENCE OF CORROSION.

Part: DOUBLER — DEBONDED (FUSELAGE) · airframe 16,888 hrs · 24,411 cycles

DURING SCHEDULED ABCD STRUCTURAL INSPECTION, ONE RIGHT BONDED DOUBLER WAS FOUND TO BE DISBONDED.

Part: FASTENER — CORRODED (FUSELAGE) · airframe 16,888 hrs · 24,411 cycles

DURING SCHEDULED D-STRUCTURAL INSPECTION, FASTENER AT LWS 124 WAS FOUND TO HAVE EVIDENCE OF CORROSION.

Part: FASTENER — CORRODED (FUSELAGE) · airframe 16,888 hrs · 24,411 cycles

DURING SCHEDULED D-STRUCTURAL INSPECTION, TWO FASTENERS AT RWS 124 WERE FOUND TO HAVE EVIDENCE OF CORROSION.

Part: RIVET — SHEARED (FUSELAGE) · airframe 16,888 hrs · 24,411 cycles

DURING SCHEDULED ABCD STRUCTURAL INSPECTION, THE RIGHT SIDE HEAVY ANGLE HAD ONE SHEARED RIVET.

Part: DOUBLER — DELAMINATED (FUSELAGE) · airframe 16,888 hrs · 24,411 cycles

DURING SCHEDULED ABCD STRUCTURAL INSPECTION, THE LEFT DOUBLER WAS FOUND TO BE DISBONDED.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 16,888 hrs · 24,411 cycles

DURING SCHEDULED ABCD STRUCTURAL INSPECTION, THE LEFT AFT SEAT TRACK WAS FOUND TO BE DAMAGED.

Part: FASTENER — CORRODED (FUSELAGE) · airframe 16,888 hrs · 24,411 cycles

DURING SCHEDULED D-STRUCTURAL INSPECTION, FASTENER AT LWS 128 WAS FOUND TO HAVE EVIDENCE OF CORROSION.

Part: FASTENER — CORRODED (FUSELAGE) · airframe 16,888 hrs · 24,411 cycles

DURING SCHEDULED D-STRUCTURAL INSPECTION, TWO FASTENERS AT RWS 105 WERE FOUND TO HAVE EVIDENCE OF CORROSION.

Part: BRAKE — WEAK (MLG) · airframe 16,741 hrs · 1,480 cycles

CREW REPORTED BRAKES ON RT SIDE FELT SPONGY. MAINT. BLEED BRAKES AND FOUND NO LEAKS. OPS CK NORMAL

Part: BRAKE — WEAK (MLG) · airframe 16,733 hrs · 1,471 cycles

AFTER LANDING CAPT REPORTED BRAKES WEAK. MAINTENANCE BLED BRAKES. OPS CK NORMAL. (BLED BRAKES CAPT SIDE AND SERVICED RESERVOIR).

Part: FIRE WARNING — ACTIVATED (CCOKPIT) · airframe 16,699 hrs · 24,195 cycles

DURING TAXI TO RUNWAY FOR TAKEOFF CREW OBSERVED THE ILLUMINATION OF THE RT ENG FIRE HANDLE. CREW ACCOMPLISHED THE EMERGENCY PROCEDURES FOR ENG FIRE. SECURED THE ENG AND RETURNED TO GATE. REMOVED AND REPLACED NR 2 ENG FIRE BOTTLE/SQUIB P/N 30100023, S/N 29392A1.

Part: CONTROL UNIT — FAILED (T/E FLAPS) · airframe 16,627 hrs · 24,115 cycles

AFTER TAKE OFF CREW TRIED TO RETRACT THE FLAPS. THE FLAPS WOULD NOT RETRACT. AIRCRAFT RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENTS.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 1,637 hrs · 23,798 cycles

RIB AT CSS 39.289 CRACKED AT STRG P/N 101-640000-45 STRG P/N 101-640000-39 (2EA CRACKS ON THIS RIB)

Part: RIB — CRACKED (VERTICAL STAB) · airframe 1,637 hrs · 23,798 cycles

RIB AT CSS 54.026 CRACKED AT STRG P/N 101-640000-47 STRG P/N 101-640000-42 STRG P/N 101-640000-46 LT SIDE (3EA CRACKS ON THIS RIB)

Part: BRAKE ASSY — CONTAMINATED (RT MLG) · airframe 15,910 hrs · 23,246 cycles

THE RIGHT BRAKES GO FLAT WHEN PRESSURE WAS APPLIED. MAINTENANCE BLED THE BRAKES. NO PARTS WERE USED, THEREFORE NO TEARDOWN REPORT WILL BE REQUIRED.

Part: STRUCTURE — BIRD STRIKE (HORIZONTAL STAB) · airframe 15,137 hrs · 22,222 cycles

ON FLIGHT 5437 FROM KANSAS CITY MISSOURI, THE CREW THOUGHT THEY HAD A BIRD STRIKE AND DIVERTED TO SALINA KANSAS DUE TO WEATHER CONDITIONS. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. UPON POSTFLIGHT INSPECTION, THE CREW REPORTED DAMAGE TO THE VERITCAL AND HORIZONTAL STABILIZERS. FURTHER POSTFLIGHT INSPECTION, THE RT ENGINE NACELLE WAS FOUND TO HAVE THE ICE LIGHT PANEL MISSING. THE CORRECTIVE ACTION WAS THAT MAINTENANCE REMOVED AND REPAIRED THE HORIZONTAL AND VERTICAL STABILIZER. NO TEARDOWN REPORT WILL BE REQUIRED.

Part: STRUCTURE — DAMAGED (VERTICAL STAB) · airframe 15,137 hrs · 22,222 cycles

ON FLIGHT 5437 FROM KANSAS CITY MISSOURI, THE CREW THOUGHT THEY HAD A BIRD STRIKE AND DIVERTED TO SALINA KANSAS DUE TO WEATHER CONDITIONS. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. UPON POSTFLIGHT INSPECTION, THE CREW REPORTED DAMAGE TO THE VERTICAL AND HORIZONTAL STABILIZERS. FURTHER POSTFLIGHT INSPECTION, THE RIGHT ENGINE NACELLE WAS FOUND TO HAVE THE ICE LIGHT PANEL MISSING. THE CORRECTIVE ACTION WAS THAT MAINTENANCE REMOVED AND REPAIRED THE HORIZONTAL AND VERTICAL STABILIZERS. NO TEARDOWN REPORT WILL BE REQUIRED.

Part: SPAR — CHAFED (WING) · airframe 15,300 hrs · 22,434 cycles

UPON A ROUTINE INSPECTION MAINTENANCE DISCOVERED THE RIGHT SPAR CHAFED ON THE FORWARD SIDE. ALSO THE RT WING MAIN SPAR CHAFED BY FUEL PRESSURE. THE CORRECTIVE ACTION WAS THAT THEY BLENDED OUT THE CHAFFED AREA IN ACCORDANCE TO RAYTHEON FIELD REPAIR. NO TEARDOWN REPORT WILL BE REQUIRED.

Part: SKIN — DELAMINATED (EMERGENCY EXIT) · airframe 15,279 hrs · 22,415 cycles

WHILE INBOUND FROM PONCA CITY, OKLAHOMA TO ENID OKLAHOMA ON FLIGHT 2501, SEAT 4F EMERGENCY EXIT OUTER SKIN PEELED OFF AND DEPARTED FROM THE AIRCRAFT WHILE INFLIGHT. THE CREW DECLARED AN EMERGENCY LANDING. THERE WAS NO FURTHER INCIDENT. MAINTENANCE FOUND HOLES IN VERTICAL FAIRING. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT DOOR. NO TEARDOWN REPORT WILL BE REQUIRED.

Part: CABLE — OUT OF ADJ (AIRSTAIR DOOR)

FLT 5299 - IAD-SYR - DURING STANDARD PREFLIGHT INSPECTION, THE CREW NOTED THEY HAD A BINDING AT THE PAX DOOR. THE AIRCRAFT WAS FERRIED TO RDG AND MAINTENANCE FOUND THE COUNTER CABLE TO BE SHORT. MAINTENANCE THEN ADJUSTED THE COUNTER BALANCE CABLE, OPS CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: GYRO — FAILED (LT/RT)

FLT 5415 - PHL-LEB - AFTER TAKEOFF FROM BOS, THE CREW NOTED THAT BOTH DIRECTIONAL GYROS WERE DRIFTING AT AN EXTREME RATE. THE CREW NOTIFIED THE TOWER THEY WERE RETURNING TO BOS AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BOTH DIRECTIONAL GYROS. OPS CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: PIN — DAMAGED (PAX DOOR)

FLT 5299 - IAD-SYR - PRIOR TO DEPARTURE, CREW REPORTED THAT THE EXTERIOR DOOR HANDLE SPINS FREELY. MAINTENANCE INSPECTED THE DOOR HANDLE AND COULD NOT DUPLICATE THE DISCREPANCY, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. THAT EVENING DURING ROUTINE MAINTENANCE IN RDG, THE DOOR HANDLE WAS RE-INSPECTED. MAINTENANCE FOUND THAT THE HANDLE WAS OPERATIONAL BUT THE PIN WAS DAMAGED. THE DOOR HANDLE WAS RELACED. OPS CHECKED GOOD. (M)

Part: ATTACH BRACKET — EXCESS WEAR (RT FLAP)

FLEET CAMPAIGN, 'MAINTENANCE INSPECTED THE LT AND RT OTBD FLAP ATTACHMENT BRACKETS AND THE AFT ROLLER BEARING IAW RAYTHEON ACFT CO (RAC) SAFETY COMMUNIQUE NR 137 DATED MAY, 1997. FOUND ATTACHMENT BRACKETS WITH EXCESSIVE WEAR AND AFT ROLLER BEARINGS BINDING. AFFECTED COMPONENTS P/NS ARE BRACKET, LT INBD AND RT INBD, INBD HINGE, PN 35-165050-31. BRACKET, LT LTBD AND RT INBD, INBD HINGE, PN 35-165050-30. BRACKET, LT INBD AND RT OTBD, OTBD HINGE, PN 35-165050-35. BRACKET, LT OTBD AND RT INBD, OTBD HINGE, PN 35-165050-34. AFT BEARING ASSY, PN 114-521039-1. REF: CONTROL NR MASA97045. PART CYCLES, 5,908. ACFT TC, 7,788.

Part: ATTACH BRACKET — EXCESS WEAR (LT FLAP)

FLEET CAMPAIGN, 'MAINTENANCE INSPECTED THE LT AND RT OTBD FLAP ATTACHMENT BRACKETS AND THE AFT ROLLER BEARING IAW RAYTHEON ACFT CO (RAC) SAFETY COMMUNIQUE NR 137 DATED MAY, 1997. FOUND ATTACHMENT BRACKETS WITH EXCESSIVE WEAR AND AFT ROLLER BEARINGS BINDING. AFFECTED COMPONENTS P/NS ARE BRACKET, LT INBD AND RT INBD, INBD HINGE, PN 35-165050-31. BRACKET, LT LTBD AND RT INBD, INBD HINGE, PN 35-165050-30. BRACKET, LT INBD AND RT OTBD, OTBD HINGE, PN 35-165050-35. BRACKET, LT OTBD AND RT INBD, OTBD HINGE, PN 35-165050-34. AFT BEARING ASSY, PN 114-521039-1. REF: CONTROL NR MASA97045. PART CYCLES, 7,786. ACFT TC, 7,786.

Part: ACM — SEIZED (LT INBD WING)

ACM WILL NOT BLOW COOL AIR. FOUND ACM TURBINE SEIZED. REMOVED AND REPLACED ACM WITH OVERHAULED SERVICEABLE ACM. OPERATIONAL CHECK GOOD. ORIGINAL ACM HAD FULL OIL AND PROPERLY SERVICED. S/N OFF, 940911.