N167YV

Part: SWITCH — DIRTY (TE FLAPS) · airframe 20,113 hrs · 36,655 cycles

AFTER T/O, FLAPS STUCK AT 17 DEGREES. CREW CALLED IT IN AND TOWER DECLARED EMERGENCY. EMERGENCY WAS THEN IMMEDIATELY TERMINATED A/C FLEW ITS ROUTE, ARRIVED ON TIME, NO FURTHER INCIDENT. (DIRECTED BY FAA TO ENTER AS AN SDR, INITIALLY ENTERED AS AN MIS) CLEANED LT/RT FLAP SAFETY SWITCHES ADJUSTED RT SAFETY SWITCHES, OPS CK NORMAL.

Part: ANNUNCIATOR — INOPERATIVE (MLG) · airframe 19,542 hrs · 35,772 cycles

UPON GEAR EXTENSION FOR LANDING INTO PIT, CREW NOTED NOSE GEAR ANNUNCIATOR DID NOT SHOW GEAR DOWN AND LOCKED. CREW C/W EMERGENCY CHECKLIST AND DECLAIRED AN EMERGENCY. THE AIRCRAFT LANDED SAFELY INTO PIT WITH NO FURTHER INCIDENTS. MAINTENANCE WAS CALLED AND REMOVED AND REPLACED ANNUNICATOR ASSY.

Part: SPAR — UNKNOWN (BS 288) · airframe 19,294 hrs · 35,367 cycles

INSTALLED SHIM FILLER BETWEEN MAIN SPAR LOWER FLANGE AND SKIN. INSTALLED DOUBLER ON LOWER MAIN SPAR SKIN. REPAIRED IAW MFG ENG. REPORT NR 6386-1 REV. 1R DATED 10/04/06.

Part: FRAME — CORRODED (BS 288) · airframe 19,294 hrs · 35,367 cycles

CORROSION, FRAME AFT FACE. FS 288.0 AT APPROX. LBL 26.0 AND RBL 25.0. FOUND DURING INSPECTION REPAIRED IAW MFG FR.CO.01399 REV. 1.

Part: SPAR CAP — CORRODED (LT WING) · airframe 19,294 hrs · 35,367 cycles

CORROSION FOUND ON WING LOWER MAIN SPAR CAP, FORWARD FACE AT APPROXIMATELY LBL 19.75 / RBL 16.4. FOUND DURING INSPECTION. REPAIRED IAW MFG FR-CO-01398-REV. 2

Part: FRAME — CORRODED (BS 213) · airframe 19,294 hrs · 35,367 cycles

CORROSION FUSELAGE FRAME AT FS 213.25 (LBL 8.4) CORROSION FOUND DURING INSPECTION. REPAIRED IAW MFG FR.CO.01423 REV. 1.

Part: HANDLE — DETACHED (PAX DOOR)

AFTER PAX WERE BOARDED AND STATION WENT TO CLOSE THE PAX DOOR THE HANDLE DETACHED. MAINTENANCE WAS CALLED, INSPECTED CABIN DOOR HANDLE, RESECURED DOOR HANDLE RETAINER RING. DOOR OPS CHECKED NORMAL. WORK DONE IAW BMM 52-10-00.

Part: SKIN — LIGHTNING STRIKE (BS 143-177)

LIGHTING STRIKE DAMAGE REPAIRED IAW WITH RAYTHEON FR-CO-01356 REV 1.

Part: WARNING LIGHT — FALSE ACTIVATION (COCKPIT) · airframe 17,343 hrs · 32,200 cycles

TAXIED INTO GATE WHEN MASTER WARNING FLASHER ILLUMINATED INDICATING FIRE IN RT ENG. FIREWALL FUEL VALVE WAS ILLUMINATED. DECLARED AN EMERGENCY, ACCOMPLISHED APPROPRIATE CHECKLISTS & CONDUCTED AN ORDERLY DEBARKATION WHILE DIRECTING PASSENGERS AWAY FROM PLANE. DFW GROUND OPS THEN COORDINATED THE TRANSPORTATION OF PASSENGERS AND FLIGHT CREW TO THE GATE AREA. THERE WERE NO INJURIES TO ANY PASSENGERS OR CREW AND THE PLANE WAS TOWED TO THE GATE AREA FOR MAINTENANCE INSPECTION. MAINTENANCE RINSED THE ENGINE, INSPECTED AND FOUND NO DEFECTS THAT WERE NOTED. UNABLE TO DUPLICATE THE WRITE UP, BUT REMOVED AND REPLACED THE FIRE BOTTLE.

Part: BULB — BURNED OUT (MLG INDICATOR) · airframe 16,912 hrs · 31,559 cycles

UPON GEAR EXTENSION FOR LANDING IN PIT, CREW NOTED NOSE GEAR ANNUNCIATOR DID NOT SHOW GEAR DOWN AND LOCKED. CREW C/W EMERGENCY CHECKLIST AND DECLARED AN EMERGENCY. LANDED SAFELY WITH NO FURTHER INCIDENT. MAINTENANCE FOUND BULBS BAD. MAINTENANCE RELAMPED ANNUNCIATOR AND PERFORMED GEAR SWING. OPS CHECK NORMAL.

Part: SQUAT SWITCH — MALFUNCTIONED (MLG) · airframe 14,497 hrs · 27,612 cycles

AFTER TAKE OFF GEAR UP. SELECTED GEAR WOULD NOT RETRACT. C/B RESEATED AND ANOTHER ATTEMP WAS MADE WITH THE SAME RESULT. ACFT RETURNED TO FIELD WITH 3 GREENS LANDED WITH NO FURTHER INCIDENTS.(REMOVED AND REPLACED RIGHT SQUAT SWITCH)

Part: RIB — CRACKED (VERTICAL STAB) · airframe 14,247 hrs · 27,283 cycles

WHILE PERFORMING INSP IN THE VERTICAL STAB., THE RIB FLNAGE AT CANTED STAB. STA 39.289 WAS FOUND CRACKED IN ONE PLACE ON THE RT SIDE AT THE FWD SIDE,. REPAIRED CRACK TO RIB FLANGE ACCORDANCE TO BEECH SRM P/N 114-590021-91, 51-70-03

Part: RIB — CRACKED (VERTICAL STAB) · airframe 14,247 hrs · 27,283 cycles

WHILE PERFORMING INSP IN THE VERT. STAB., THE RIB FLNAGE AT CANTED STAB. STA 54.026 WAS FOUND CRACKED IN THREE PLACES ON THE RT SIDE NEAR THE FWD, CENTER, AND AFT STRG. REPAIRED CRACKS TO RIB FLANGE ACCORDANCE TO BEECH SRM P/N 114-590021-9, 51-70-03

Part: RIB — CRACKED (VERTICAL STAB) · airframe 14,247 hrs · 27,283 cycles

WHILE PERFORMING INSP IN THE VERTICAL STAB., THE RIB FLNAGE AT CANTED STAB. STA 39.289 WAS FOUND CRACKED IN ONE PLACE ON THE LT SIDE AT THE CENTER STRG,. REPAIRED CRACK TO RIB FLANGE ACCORDANCE TO BEECH SRM P/N 114-590021-91, 51-70-03

Part: CABLE — OUT OF ADJ (AIRSTAIR DOOR)

CBE/LBE - FLT 5916 - UPON EXITING AIRCRAFT, THE CREW FOUND THE AIRSTAIR DOOR WOULD NOT OPEN. PIT MAINTENANCE WORKED THE DOOR OPEN AND DEPLANED THE PASSENGERS. MAINTENANCE RIGGED THE DOOR CABLES. THE AIRCRAFT WAS RETURNED TO SERVICE. (X)

Part: WIRE — CHAFED (COCKPIT)

PIT/FKL - FLT 5926 - THE CREW REPORTED SMOKE COMING FROM THE CAPTAIN'S SIDE INSTRUMENT PANEL. MAINTENANCE REPAIRED A CHAFED WIRE TO THE INSTRUMENT INDIRECT LIGHT SOCKET, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (X)

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, 6,962. ACFT TC, 6,962.

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, 6,962. ACFT TC, 6,962.