N231YV

Part: MASTER CYLINDER — WORN (BRAKE SYSTEM) · airframe 38,668 hrs · 48,597 cycles

PILOT REPORTED THAT THE CAPTAINS SIDE LT BRAKE PEDAL IS NOT HOLDING & WENT TO THE FLOOR. REPLACED THE CAPTAINS LT BRAKE CYLINDER IAW 32-40-06, PN 90-380001-33 & SN 2912 OFF, SN 3549 ON, BRAKE BLEED & OPERATIONS CHECKED GOOD.

Part: PCB — FAULTY (AUTOFEATHER SYS) · airframe 38,558 hrs · 48,472 cycles

PILOT REPORTED THAT THE AUTOFEATHER ARMED WITH N1 ABOUT 95%, AFX DISABLE ILLUMINATED & RT AUTOFEATHER FAILED TO ARM. REPLACED PCB A123, PN ON & OFF 129-364091-9, SN OFF 446C95, SN ON 925I94, IAW AIM 10-24-01. VERIFIED RIGGING OF ARMING SWITCHES IAW MM 61-21-02. OPERATIONAL CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (AUTOFEATHER SYS) · airframe 38,557 hrs · 48,471 cycles

PILOT REPORTED THAT AFTER TAKEOFF, POWER WAS APPLIED, AFX DISABLE ANNUNCIATOR ILLUMINATED & RT AUTOFEATHER DISARMED, THEN REARMED. THEN AFTER ROTATION, RT AUTOFEATHER DISARMED. ON CLIMB OUT SYS REARMED FOR THE REMAINDER OF THE FLIGHT. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.

Part: CONTROL HANDLE — BROKEN (COCKPIT) · airframe 38,440 hrs · 48,348 cycles

PILOT REPORTED THAT THE LG FAILED TO EXTEND NORMALLY, FOLLOWED CHECKLIST. PERFORMED MANUAL EXTENSION, DOWN WITH 3 GREENS. JACKED ACFT RETRACTED GEAR 10 TIMES, NO DEFECTS NOTED. CHECKED CONTINUITY OF WIRES IAW WDM 32-31-01-01 & 32-31-0202, FROM A316 TO P532, FROM ELEC EQPT NACELLE & A184, J206 TO K3 RELAY TO LG MOTOR G1A6 & G2A6N, FROM P200 LANDING CTRL TO LT, RT, & NOSE DOWN & LOCK SWITCHES, NO DEFECTS NOTED. R & R LANDING CTRL HANDLE IAW MI 32-01.

Part: SPAR — CORRODED (RT WING) · airframe 38,430 hrs · 48,335 cycles

MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE RT REAR WING SPAR OTBD WEB CORRODED. REPAIRED IAW EO 15-1900-57-003.

Part: SPAR CAP — CORRODED (RT WING) · airframe 38,430 hrs · 48,335 cycles

MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE RT REAR LOWER WING SPAR CAP FROM WING STATION 215.08 - 310. CORROSION ON THE AFT FLANGE GOING UP ON THE TEE. REPAIRED IAW EO 15-1900-57-003.

Part: STRUCTURE — DAMAGED (BS 531-557.5) · airframe 38,025 hrs · 47,883 cycles

DURING A SCHEDULED INSPECTION FOUND MULTIPLE FASTENER HOLES ELONGATED BETWEEN BS 531 - 557.5. ELONGATION RANGING FROM .20 INCHES TO .30 INCHES, FASTENER HOLES ARE FOR THE LT FWD VENTRAL FIND, INBD & OTBD OF STRINGER 12L. REPAIRED IAW EO 14-1900-52-043. MAJOR REPAIR.

Part: SKIN — CRACKED (BS 549.25) · airframe 38,025 hrs · 47,883 cycles

DURING A SCHEDULED INSPECTION FOUND CRACK IN THE LT AFT FUSELAGE SKIN AT BS 549.25 BETWEEN STRINGERS 12 - 13L, 1.1 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-043. MAJOR REPAIR.

Part: SKIN — CRACKED (EMERGENCY EXIT) · airframe 38,025 hrs · 47,883 cycles

DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE EMERGENCY EXIT DOOR 6C RT AFT INSIDE SKIN 0.875 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-52-005. MAJOR REPAIR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,047 hrs · 47,883 cycles

DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE FUSELAGE SKIN AT FS 249.25 & STRINGER 12L UNDER LT VORTEX GEN 1.75 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-042. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,025 hrs · 47,883 cycles

DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE UPPER FWD CORNER OF A/S DOOR CUT OUT FS 150.6 PROTRUDING UPWARD .75 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-040. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 38,025 hrs · 47,883 cycles

DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE CANTED BULKHEAD AT FS 588.10 & STRINGER 8L .65 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-041. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.

Part: SPAR — CRACKED (HORIZ STAB) · airframe 38,025 hrs · 47,883 cycles

DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE AFT CTR HORIZONTAL STAB SPAR WEB, .125 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-55-011. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.

Part: BULKHEAD — BUCKLED (FUSELAGE) · airframe 38,025 hrs · 47,883 cycles

DURING A SCHEDULED INSPECTION FOUND THE CANTED BULKHEAD AT FS 588.10 BUCKLED FROM STRINGER 12R TO STRINGER 11L. PREVIOUS REPAIR DOUBLER BETWEEN STRINGER 11L & 13L BUCKLED. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-039. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 38,025 hrs · 47,883 cycles

DURING A SCHEDULED INSPECTION FOUND 2 CRACKS IN THE FUSELAGE FRAME AT FS 183.25 AT 2 LOCATIONS. 1ST AT INBD CORNER AREA AT ENVIRONMENTAL DUCT CUT OUT, ONE CRACK IS FROM CUT OUT ALL THE WAY THROUGH THE BEND RADIUS TO THE EDGE FRAME. SECOND IS FROM FASTENER INBD FROM 1ST CRACK, THIS CRACK RADIATES DOWNWARD FROM FASTENER, TOTAL LENGTH 3.75 INCHES. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-038. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 37,891 hrs · 47,727 cycles

DURING A SCHEDULED INSPECTION FOUND A LIGHTNING STRIKE ON THE OTBD TE LT ELEVATOR JUST OTBD OF THE MOST OTBD STATIC WICK. SKIN HAS .5 INCH X .25 INCH DAMAGE STARTING INBD OF THE FIBERGLASS END CAP & TRAVELING OUTWARD UNDER THE END CAP, DAMAGING THE END CAP. THE END CAP ALSO HAS AN EXIT HOLE 0.125 INCH IN DIAMETER. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-27-003. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.

Part: SKIN — DAMAGED (RT WING) · airframe 37,891 hrs · 47,727 cycles

DURING A SCHEDULED INSPECTION MAINTENANCE, FOUND WING SKIN BENT UPWARDS ON TRAILING EDGE BETWEEN WS 114.25 & 124.25. REPAIRED IAW EO 14-1900-57-006.

Part: FRAME — CRACKED (BS 456) · airframe 35,330 hrs · 44,776 cycles

MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FUSELAGE FRAME AT FS 456 AT THE GAS STRUT UPPER INBD NUTPLATE BETWEEN STRINGERS 3L AND 4L, .75" IN LENGTH. REPAIRED IAW EO 13-1900-53-002.

Part: FRAME — CRACKED (BS 107) · airframe 35,330 hrs · 44,776 cycles

DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT FS 107 AND STRINGER 8R, FRAME CRACK PROTRUDING OUT OF RIVET, .5 INCH IN LENGTH. REPAIRED IAW EO 13-1900-53-007.

Part: FRAME — CRACKED (BS 107) · airframe 35,330 hrs · 44,776 cycles

DURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS AT FS 107 AND STRINGER 8L IN THE BEND RADIUS, CRACK PROTRUDING OUT OF RIVET, 1.25 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-008.

Part: RIB — CRACKED (LT WING) · airframe 33,334 hrs · 42,412 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AT THE LT CENTER WING L/E INBD RIB AND REINFORCEMENT STRAP 1.5" FWD OF SPAR, 1" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-57-002. MAJOR REPAIR.

Part: SPAR CAP — CHAFED (LT WING) · airframe 33,334 hrs · 42,412 cycles

MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CHAFE ON THE LT WING FWD LOWER SPAR CAP AT BL 29.5, APPROX 1" BY .312" AT WIDEST POINT, .125" TO .187" DEEP AT DEEPEST POINT. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-57-001.

Part: CABLE — FRAYED (PAX DOOR) · airframe 32,701 hrs · 41,667 cycles

PILOT REPORTED THAT THE TOP AFT AIRSTAIR DOOR CABLE IS FRAYED. MX REPLACED THE TOP AFT DOOR CABLE, OPS CHECKED GOOD.

Part: SKIN — DEBONDED (WINGLET) · airframe 32,238 hrs

MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP MX FOUND THE RT WINGLET DEBONDED AT THE INBD EDGES AND A HOLE IN THE L/E NEXT TO THE UNDER LIGHT DAM. MX REPLACED, AND REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-57-009. MATERIALS UTILIZED ARE INCLUDED IN THE EO.

Part: RAIL — WORN (DOOR STAIR) · airframe 32,238 hrs · 41,150 cycles

AIRSTAIR DOOR AFT UPPER HAND RAIL WORN. MX REPLACED THE RAIL IAW BMM 52-10-02, OPS CK GOOD.

Part: SCREW — MISSING (PAX DOOR) · airframe 32,188 hrs · 41,097 cycles

PILOT REPORTED THAT A SCREW WAS MISSING FROM THE CABIN DOOR. MX REPLACED THE SCREW.

Part: GOVERNOR — INOPERATIVE (OVERSPEED) · airframe 32,168 hrs · 41,076 cycles

PILOT REPORTED THAT DURING THE AFX TEST, RT PROP DID NOT FEATHER. MX RESEATED A173 PCB IAW MI 24-01 AND REPLACED THE RT OVERSPEED GOV IAW BMM 61-20-01, PN: 210961C SN:11403305, OPS CK GOOD.

Part: CAP — DAMAGED (RT STABILON) · airframe 32,102 hrs

MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND THE RT STABILON END CAP DAMAGED FROM TE FWD 10.7" AND FROM T/E OTBD TIP 7" GOING 2.5" PAST SPLICE. MX REPLACED, REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW. EO 11-1900-55-005. MATERIALS UTILIZED ARE INCLUDED IN THE EO.

Part: SWITCH — INOPERATIVE (AUTOFEATHER SYS) · airframe 32,108 hrs · 41,015 cycles

PILOT REPORTED THAT THE LT AUTOFEATHER INTERMITTENT AFX REPEATER AND LT AUTOFEATHER ANNC WENT OFF DURING TAKEOFF ROLL, ABORTED AND EXITED RUNWAY. MX REPLACE THE LT POWER LEVER AFX ARMING MICRO SWITCH, PN: 15M1 IAW BMM 61-21-02, OPS AND RIG CK GOOD.

Part: PCB — INOPERATIVE (AUTOFEATHERING) · airframe 32,108 hrs · 41,015 cycles

PILOT REPORTED THAT THE LT AUTOFEATHER SYS DID NOT ARM ON TAKEOFF ROLL. MX REPLACED PCB A123 IAW AIM MI 24-01.

Part: PCB — INOPERATIVE (AUTOFEATHER SYS) · airframe 32,108 hrs · 41,015 cycles

PILOT REPORTED THAT ON DECENT THE RT AUTOFEATHER DID NOT ARM. MX REPLACED PCB A123 PN: 129-304091-9 SN: 735599 IAW AIM MI 24-01, OPS CK GOOD.

Part: PCB — INOPERATIVE (LT AUTOFEATHER) · airframe 32,036 hrs · 40,936 cycles

PILOT REPORTED THAT THE LT AUTOFEATHER DISARMED ON TAKEOFF ROLL AT 65 KNOTS, ABORTED TAKEOFF. MX WAS ABLE TO DUPLICATE BY MOVING J2 CONNECTOR OF A123PCB, R & R CONNECTOR J2 PH: 3-582151-1, REF BMM 61-05-01 AND R & R A123 PCB REF AIM MI24-01 PN 129-3640919, PERFORMED AUTOFEATHER CKS REF BMM 61-21-01.

Part: CONNECTOR — GROUNDED (AUTOFEATHER SYS) · airframe 32,036 hrs · 40,936 cycles

PILOT REPORTED THAT WITH THE GEAR HANDLE IN THE UP POSITION "AUTOFEATHER OFF" ANNUNCIATOR ILLUMINATED WITH THE AUTOFEATHER SWITCH IN THE ARM AND OFF POSITION. MX T'S FOUND THE SOCKET INSIDE THE UPLOCK PLUG SHORTING TOGETHER, REPAIRED SOCKET AND PLUG PN MS3126F10-6S ON EXISTING UPLOCK HARNESS IAW EO-11-1900-32-001, PERFORMED SWITCH RIGGING IAW TC 1900-3260.00, OPS CHECKED GOOD.

Part: SKIN — DEBONDED (PAX DOOR) · airframe 32,036 hrs · 40,936 cycles

MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND THE AIRSTAIR DOOR EXTERIOR SKIN DEBONDING IN A 7" X 7" AREA AROUND THE PRESSURE LOCK. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-52-003. MATERIALS UTILIZED ARE INCLUDED IN THE EO.

Part: FRAME — CRACKED (BS 456) · airframe 32,036 hrs · 40,936 cycles

MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND A CRACK IN THE FUSELAGE FRAME AT FS 456 AND STRINGER 10R, .2" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-042 MATERIALS UTILIZED ARE INCLUDED IN THE EO.

Part: FRAME — CRACKED (PAX DOOR) · airframe 32,036 hrs · 40,936 cycles

MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP MX FOUND A CRACK IN THE AIR STAIR DOOR LOWER FRAME AT THE LOWER AFT CORNER, .75" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-043 MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.

Part: SKIN — CRACKED (EMERGENCY EXIT) · airframe 32,036 hrs · 40,936 cycles

MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND A CRACK IN THE INNER SKIN OF THE EMERGENCY EXIT AT 6A, VERT LENGTH 3.25"M ABD HORZ 3". MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-52-007. MATERIALS UTILIZED ARE INCLUDED IN THE EO.

Part: VALVE — INOPERATIVE (MLG) · airframe 30,295 hrs · 38,945 cycles

PILOT REPORTED THAT THE LANDING GEAR DID NOT EXTEND ON FINAL APPROACH, GEAR FAILED TO EXTEND AND LANDING GEAR RELAY TRIPPED, GEAR WAS MANUALLY EXTENDED SUCCESSFULLY WITH 3 GREEN LIGHTS INDICATED. MX REMOVED LANDING GEAR SERVICE VALVE PN 101-388008-3, SN 2206 AND INSTALLED OVERHAULED PN 101-388008-3 SN 2315, LEAK AND OPS CHECKS GOOD IAW BMM 32-30-16.

Part: POWERPACK — FAILED (MLG) · airframe 30,293 hrs · 38,941 cycles

PILOT REPORTED THAT THE LANDING GEAR DID NOT EXTEND ON FINAL APPROACH, INTRANSIT LIGHT WAS ON AND NOTICED THAT THE GEAR RELAY CB POPPED, EXTENDED THE LANDING GEAR MANUALLY, LANDED SAFELY. MAINTENANCE CONFIRMED DISCREPANCY, TROUBLESHOT SYSTEM TO HYDRAULIC POWER PACK INTERNAL SELECTOR VALUE, REPLACED HYDRAULIC POWER PACK ASSY PN 114-388000-9 SN ON MX-549646A SN OFF MX62452A IAW BMM 32-30-02, SWUNG GEAR 10 TIMES, OPERATIONAL CHECKS GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 29,825 hrs · 38,405 cycles

PILOT REPORTED AFTER LANDING THAT THE EMERGENCY INSTRUMENT LIGHT SECOND FROM THE LEFT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT IAW 1900 AMM 33-10-00, PART NUMBER D165-100-2, OPERATIONAL TEST OF THE SUBSEQUENT SYSTEM CHECKS GOOD.

Part: SKIN — CRACKED (BS 290) · airframe 29,139 hrs · 37,556 cycles

MAJOR REPAIR - DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND BETWEEN 2 RIVETS AT FS 290 AND BL 30L ON THE BOTTOM OF THE LT LOWER FUSELAGE AFT OF THE FWD WING SPAR, CRACK APPROX .4" IN LENGTH. MAINT REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIONS IAW EO 09-120-53-005. MATERIALS UTLIZED ARE LISTED IN THE EO.

Part: SKIN — CRACKED (BS 265 S13R) · airframe 29,139 hrs · 37,556 cycles

DURING ROUTINE SCHEDULED MX, A SMALL CRACK IN THE SKIN WAS FOUND AT FS 265 2.5" OTBD OF STR 13R. CRACK APPROX .250" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIONS IAW EO 09-120-53-004. MATERIALS UTLIZED ARE LISTED IN THE EO.

Part: STRINGER — CRACKED (BS 288 S4R) · airframe 29,139 hrs · 37,556 cycles

MAJOR REPAIR - DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND AT STRINGER 4R CUTOUT AT FS 288. IT EXTENDS OUTWARD AND DOWNWARD AT A 45 DEG ANGLE. CRACK IS APPROX .4" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED REQUIRED RII INSPECTIONS IAW EO 09-120-53-003. MATERIALS UTLIZED ARE LISTED IN THE EO.

Part: FRAME — CRACKED (ZONE 100) · airframe 29,139 hrs · 37,556 cycles

MAJOR REPAIR - DURING ROUTINE SCHEDULED MX 2 CRACKS WERE FOUND AT THE AIRSTAIR DOOR FUSELAGE FRAME AT FS 150 AT THE LWR STRUT MOUNT AREA. CRACKS MEASURE 1" AND 1.25" RESPECTIVELY. MX REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIONS IAW EO 09-120-53-002. MATERIALS UTILIZED ARE LISTED IN THE EO.

Part: FRAME — CRACKED (BS 164) · airframe 29,139 hrs · 37,556 cycles

MAJOR REPAIR - DURING ROUTINE SCHEDULED MX CRACK WAS FOUND IN THE RT SIDEWALL FRAME AT TS 164 AND STRINGER 9AR CUTOUT. CRACK IS APPROX 1.75" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIONS IAW EO 09-120-53-001. MATERIALS UTLIZED ARE LISTED IN THE EO.

Part: SKIN — CRACKED (ZONE 200) · airframe 29,139 hrs · 37,556 cycles

MAJOR REPAIR - DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND IN THE UPPER FUSELAGE DOME SKIN AT FAS 150. CRACK IS APPROX.3" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIONS IAW EO 09-120-53-040. MATERIALS UTLIZED ARE LISTED IN THE EO.

Part: SWITCH — DETERIORATED (MLG) · airframe 28,660 hrs · 37,513 cycles

UPON APPROACH THE PILOTS REPORTED THAT THE LANDING GEAR WOULD NOT COME DOWN. THEY PERFORMED CHECKLISTS AND HAND PUMPED THE GEAR DOWN. ALL 3 GREEN ANNUNCIATORS ILLUMINATED. MX REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE IAW MM 31-10-00-201 SECTION 5 AND THE OPS CHECK WAS GOOD IAW MM 32-30-00.

Part: INDICATOR — INOPERATIVE (NR 2 PROP) · airframe 28,936 hrs · 37,303 cycles

UPON APPLICATION OF TAKEOFF POWER ON RUNWAY, THE NR 2 PROP GAUGE WENT TO ZERO.

Part: DISPLAY — FAILED (EHSI) · airframe 28,669 hrs · 36,949 cycles

AIR RETURN - PILOTS REPORTED THE CAPTAINS EHSI WENT OUT FOLLOWED BY SMOKE IN THE COCKPIT. TURNING THE PILOTS SIDE SCREENS OFF STOPPED THE SMOKE. IT APPEARED TO THE PILOTS THAT THE CAPTAINS SIDE MIC (HEADSET) WAS LOSING IT'S EFFECTIVENESS AS WELL. OPEN

Part: WIRE — CHAFED (MLG) · airframe 28,658 hrs · 36,934 cycles

AIR RETURN - PILOTS REPORTED THE LANDING GEAR RELAY POPPED AND A MANUAL GEAR EXTENSION WAS PERFORMED. MAINTENANCE REPAIRED A BROKEN WIRE AT THE THE HYDRAULIC POWER PACK SHUTTLE VALVE IAW MM 20-13-00. MAINTENANCE PERFORMED A GEAR RETRACTION AND EXTENSION TEST PER MM 32-30-00.201. OPERATIONAL CHECK WAS GOOD.

Part: POWERPACK — FAILED (MLG) · airframe 28,366 hrs · 36,530 cycles

PILOTS REPORTED THAT THE GEAR HANDLE DID NOT OPERATE THE GEAR AND WOULD NOT EXTEND. A MANUAL EXTENSION OF GEAR WAS PERFORMED. MX REMOVED AND REPLACEDTHE LANDING GEAR PWR PACK ASSY AND OPS CHECKED THROUGH SEVERAL GEAR EXTENSIONS AND RETRACTIONS IAW MM 32-30-02.

Part: ALTIMETER — INOPERATIVE (COCKPIT) · airframe 27,346 hrs · 35,217 cycles

FLIGHT 5096 - PILOTS REPORTED THAT THE FIRST OFFICERS ALTIMETER WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS ALTIMETER IAW MM 31-10-00. PERFORMED ENCODER CHECK WHICH OPERATIONALLY CHECKED GOOD IAW FAR 43 APPENDIX (E) (A) & (C) (A). MAINTENANCE PERFORMED ALTIMETER PITOT STATIC LEAK CHECK IAW GLA GMM 9.4.28. NO LEAKS NOTED.

Part: SEAT TRACK — CRACKED (BS 160-164) · airframe 26,984 hrs · 34,748 cycles

MAJOR REPAIR - LT CENTER SEAT TRACK SUPPORT TAB IS BROKEN OFF FROM SEAT TRACK AT F.S.160 TO F.S. 164. MAINTENANCE REPAIRED THE LEFT HAND CENTER SEAT TRACK SUPPORT TAB AT F.S. 162 TO F.S. 164 IAW SRM 53-90. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.

Part: SEAT TRACK — CRACKED (BS 187-190) · airframe 26,984 hrs · 34,748 cycles

MAJOR REPAIR - LT CENTER SEAT TRACK SUPPORT TAB IS BROKEN OFF FROM SEAT TRACK AT F.S. 187.5 TO 190.5. MAINTENANCE REPAIRED LEFT CENTER SEAT TRACK SUPPORT TAB AT APPROXIMATELY F.S. 189 TO 191 IAW SRM 53-90. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.

Part: SKIN — CRACKED (ZONE 100) · airframe 26,984 hrs · 34,748 cycles

MAJOR REPAIR - DURING CONFORMITY INSPECTIONS MX DISCOVERED THE FUSELAGE SKIN ON THE LT SIDE OF THE NR 2 COMM ANTENNA TO BE CRACKED APPROXIMATELY 2.5 " IN LENGTH AT F.S. 393.25. MAINTENANCE REPAIRED CRACK ON FUSELAGE SKIN UNDER NR 2 COMM ANTENNA IAW E.O. 03-17 REV. 1.

Part: SPAR — CRACKED (HORIZ STAB) · airframe 26,984 hrs · 34,748 cycles

MAJOR REPAIR HORIZONTAL STABILIZER SPAR WEB CRACKED APPROXIMATELY .250" IN LENGTH. MAINTENANCE REPAIRED HORIZONTAL STABILIZER MAIN SPAR WEB IAW BEECH 1900D SRM 55-91. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.

Part: UNKNOWN — ODOR (COCKPIT)

FLIGHT 5406 PBI/FLL. DURING FLIGHT LIGHT FUEL ODOR INSIDE ACFT. INSPECTED FUEL AUX TANKS. RAN ENGS WITH BLEEDS OPEN. NO FUEL ODOR DETECTED. (S)

Part: UNKNOWN — ODOR (CABIN)

FLIGHT 5406 PBI/FLL, DURING FLIGHT LIGHT FUEL ODOR INSIDE ACFT. INSPECTED FUEL AUX TANKS, RAN ENGS WITH BLEEDS OPEN. NO FUEL ODOR DETECTED. (S)

Part: WIRE — SHORTED · airframe 26,215 hrs · 33,924 cycles

FLIGHT: 9275, DURING APPROACH LANDING GEAR WOULD NOT COME DOWN, CIRCUIT BREAKER POPPED. MANUALLY EXTENDED LANDING GEAR. LANDED WITHOUT INCIDENT. REPAIRED SHORTED WIRE G15F22 ON CABIN SIDEWALL NEAR MAIN DOOR. OPERATIONAL CHECK GOOD NO DEFECTS NOTED.

Part: WIRE — CHAFED (LT WING) · airframe 26,208 hrs · 33,916 cycles

FLIGHT: 5401, AFTER TAKEOFF, LANDING GEAR FAILED TO RETRACT. LANDING GEAR CIRCUIT BREAKER POPPED, UNABLE TO RESET. RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. REPAIRED CHAFED WIRE G15C22 AT LT WING ROOT. OPS CHECK NORMAL.

Part: CONTROL SWITCH — INOPERATIVE (COCKPIT) · airframe 26,206 hrs · 33,914 cycles

FLIGHT: 9280, DOING A GO AROUND, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION UNLESS THE DOWN LOCK RELEASE SWITCH WAS USED, THE GEAR FAILED TO RETRACT WITH THE HANDLE IN THE UP POSITION, LANDING GEAR CIRCUIT BREAKER POPPED. REPLACED LANDING GEAR HANDLE CONTROL SWITCH. OPERATIONAL CHECK GOOD.

Part: LONGERON — CRACKED (BS 107) · airframe 26,176 hrs · 33,883 cycles

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED TWO INCH CRACK ON COCKPIT RIGHT UPPER LONGERON AT FS 107.0 AND WL 119.0. REMOVED DAMAGED SECTION OF LONGERON AND INSTALLED FILLER PROFILE TO MATCH REMOVED SECTION OF LONGERON. FABRICATED AND INSTALLED REINFORCEMENT ANGLE IN ACCORDANCE WITH FAA APPROVED DATA CONTAINED IN BEECHCRAFT FIELD REPAIR FR-CO-01729, REV 2.

Part: CONTROL COLUMN — OBSTRUCTED · airframe 26,174 hrs · 33,882 cycles

FLT NR 9188, ON FINAL APPROACH CONTROL COLUMN JAMMED. REQUIRED STRENGTH OF BOTH CREW MEMBERS TO OVER COME. MAINT DETERMINED THAT A WIRE BUNDLE FROM UNDER AND FWD OF THE INSTRUMENT PANEL WAS INTERFERING WITH THE CONTROL COLUMN. THE WIRE BUNDLE WAS POSITIONED AND SECURED UP AND OUT OF THE WAY. OPERATIONAL FLIGHT SATISFACTORY.

Part: BLEED AIR SYS — CONTAMINATED · airframe 25,805 hrs · 33,489 cycles

FLIGHT: 5401, DURING FLIGHT, FUNKY SMOKE ODOR IN THE COCKPIT WITH BLEED OPEN. CLEANED RESIDUAL OIL, FROM OIL SERVICING.

Part: HINGE BRACKET — CORRODED (RT ELEVATOR) · airframe 25,579 hrs · 33,245 cycles

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT ELEVATOR OB HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR OB HINGE BRACKET.

Part: HINGE BRACKET — CORRODED (RT ELEVATOR) · airframe 25,579 hrs · 33,245 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RT ELEVATOR CTR HINGE BRACKET EXFOILATED. REPLACED RT ELEVATOR CTR HINGE BRACKET.

Part: CONTACT — DIRTY (NLG ANNUNCIATOR) · airframe 25,146 hrs · 32,766 cycles

FLIGHT: 9188, DURING LANDING NOSE LANDING GEAR ANNUNCIATOR FAILED TO ILLUMINATE. CLEANED ANNUNCIATOR CONTACTS. OPERATIONAL CHECK GOOD.

Part: POWERPACK — DEFECTIVE (MLG) · airframe 24,533 hrs · 32,083 cycles

FLIGHT: 9174, AFTER TAKEOFF, LANDING GEAR WILL NOT RETRACT. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR POWER PACK MOTOR. LANDING GEAR OPERATIONAL CHECK NORMAL.

Part: WIRE — LOOSE (FIRE BOTTLE) · airframe 24,387 hrs · 31,917 cycles

FLIGHT: 9278, DURING FLIGHT, RT DISCHARGE LIGHT ILLUMINATED INTERMITTENTLY. CONTINUED TO DESTINATION, LANDED WITHOUT INCIDENT. SECURED LOOSE WIRE AT THE RT FIRE BOTTLE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 24,082 hrs · 31,561 cycles

FLIGHT: 9308 MIA/EYW - DURING APPROACH ODOR IN COCKPIT. PERFORMED ENGINE RUN WITH CAPTAIN CHECK BLEED SYSTEM ALL ELECTRICAL ON, CHECKED OIL AND BRAKE FLUID NO ODORS AT THIS TIME.

Part: ACM — ODOR

FLIGHT:9265 PBI/MHH DURING FLIGHT SMELLED BURNING IN THE AIRCRAFT. DIVERTED TO FPO LANDED WITHOUT INCIDENT. FOUND ACM BLOWING FULL HOT CAUSING AIR CONDITION DUCTS AND PLASTIC VENTS TO EMIT BURNING SMELL FROM UNDER FLOOR VENTS. REPLACED ACM OPERATIONAL CHECK NORMAL.

Part: CONNECTOR — LOOSE (ELEVATOR TRIM)

FLT - 9292 - JAX/TPA - AFTER TAKEOFF, WHILE ADJUSTING THE ELEVATOR TRIM FROM CLIMB TO LEVEL FLIGHT, THE YOKE WAS PULLED AWAY FROM THE FIRST OFFICERS HANDS. IT WAS IF THE TRIMMING CABLE SNAPPED INTO A NEW POSITION. DETERMINED BACK SHELL WIRE BUNDLE CLAMP EAR FOR THE GPWS ELECTRICAL CONNECTOR J726/P371, BELOW TCAS INDICATOR, WAS MOMENTARILY CAUGHT INSIDE THE CONTROL COLUMN ASSEMBLY VERTICAL TUBE. SECURED CONNECTOR J726/P371 OUT OF THE WAY. VERIFIED SUFFICIENT CLEARANCE OF CONTROL COLUMN THROUGH OUT FULL TRAVEL SWEEPS. (M)

Part: WIRE — CHAFED (DEFROST HANDLE) · airframe 18,673 hrs · 25,381 cycles

WHILE TAXING FOR TAKEOFF CREW NOTED ARCING BY F/O'S DEFROST HANDLE AND RETURNED TO GATE. REPAIRED CHAFED WIRES AND REPOSITIONED AS NEEDED.

Part: SOLENOID — DIRTY (LOW PITCH) · airframe 17,373 hrs · 23,966 cycles

ON TAKEOFF ROLL IN TAMPA FLORIDA ON FLIGHT 5536, THE LT ENGINE POWER LEVER FULL FORWARD WOULD ONLY GO TO 2000 LBS OF TORQUE AND 1500 PROP RPM. THE CREW ABORTED THE TAKEOFF AND RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE CLEANED AND LUBED THE LOW PITCH SOLENOID. NO PARTS WERE USED.

Part: SWITCH — OUT OF ADJUST (STALL WARNING) · airframe 16,259 hrs · 22,486 cycles

ON FLIGHT 9415 FROM PANAMA CITY FLORIDA TO PENSACOLA FLORIDA, AFTER TAKEOFF FROM PANAMA CITY FLORIDA, THE STALL WARNING WENT OFF AND WOULD NOT SILENCE. THE AIRCRAFT RETURNED TO FIELD WITH NO FURTHER INCIDENT. MAINTENANCE RE-ADJUSTED THE SWITCHES. NO PARTS WERE USED, THEREFORE NO TEARDOWN REPORT WILL BE REQUIRED.

Part: SPAR CAP — CHAFED (WING) · airframe 15,441 hrs · 21,503 cycles

UPON A SERVICE INSPECTION MAINTENANCE FOUND THE LEFT AND RIGHT LOWER SPAR CAP BEHIND THE NACELLE INNER FEN WAS CHAFED. BLENDED, ALODINED AND PRIMED BOTH OF THE LOWER WING SPAR CAP IN ACCORDANCE WITH RAYTHEON FIELD REPAIR. REFERENCE NUMBER JV/0215-03. NO TEARDOWN REPORT WILL BE REQUIRED.

Part: WIRE — FAILED (MLG ACTUATOR) · airframe 14,835 hrs · 20,574 cycles

UPON LANDING IN PITTSBURGH, THE CREW REPORTED THAT THE NOSE GEAR ANNUNCIATOR DID NOT ILLUMINATE IN GEAR DOWN POSITION. THE BULB WAS THEN CHECKED WHICH WAS FOUND TO BE OKAY. THE CREW MANUALLY LOWERED THE GEAR PER THE CHECKLIST. THEN THEY DECLARED AN EMERGENCY LANDING IN PITTSBURGH WITHOUT INCIDENT. REMOVED AND REPLACED THE NOSE GEAR ACTUATOR / SWUNG GEAR. THE TEARDOWN REPORT REVEALED THAT THEY FOUND SWITCH WIRES BROKEN OFF AT SWITCH. CORROSION ON BARREL IS EXCESSIVE AND MUST BE REPLACED.

Part: ACTUATOR — FAILED (NLG) · airframe 14,835 hrs · 20,574 cycles

UPON LANDING, FLIGHT 5533, THE CREW REPORTED THAT THE NOSE GEAR ANNUNCIATOR DID NOT ILLUMINATE IN GEAR DOWN POSITION. THE BULB WAS THEN CHECKED WHICH WAS FOUND TO BE OKAY. THE CREW MANUALLY LOWERED THE GEAR PER THE CHECKLIST. THEN DECLARED AN EMERGENCY LANDING IN PITTSBURGH, PENNSYLVANIA WITHOUT INCIDENT. REMOVED AND REPLACED THE NOSE GEAR ACTUATOR/SWUNG GEAR.

Part: SWITCH — DIRTY (PAX DOOR)

DURING THE INITIAL CLIMB, THE CABIN DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. THE CREW THEN RETURNED TO THE FIELD WITHOUT ANY FURTHER INCIDENT. NO TEARDOWN REPORT IS REQUIRED. THE CORRECTIVE ACTION WAS THAT THE DOOR SWITCH WAS CLEANED.

Part: SKIN — CRACKED (TE FLAP)

OVERNIGHT MAINTENANCE IN ICT, FOUND A .5 INCH CRACK EXTENDING FROM A RIVET ON THE RT INBOARD FLAP DOVETAIL. REPAIRED IAW AMWA TO 1900-27-00-0001. (M)

Part: BRACKETS — WORN (LT TE FLAP)

DURING BEECH TEMP. REV. 5-6, INSPECTION FOUND LEFT OUTBOARD FLAP ATTACHING BRACKETS WORN. REPLACED BRACKETS IAW T.O. 1900-27-00-0001 AND ADDED DOUBLER IAW T.O. 1900-27-50-0001. (X)

Part: DOVETAIL BLKHD — CRACKED (RT TE FLAP)

DURING BEECH TEMP. REV. 5-6 INSPECTION, FOUND DOVETAIL BULKHEAD HAD 2 CRACKS. ONE CRACK IS 2 INCHES LONG, 12 INCHES FROM OUTBOARD EDGE. THE OTHER IS .50 INCH, 22 INCHES FROM OUTBOARD EDGE. STOP-DRILLED CRACKS. REPAIRED IAW AMWA TO 1900-27-00-0001. (X)

Part: BULKHEAD — CRACKED (TE FLAP)

DURING BEECH TEMP REV 5-6, INSPECTION FOUND THAT THE DOVETAIL BULKHEAD WAS CRACKED, IT WAS PATCHED IAW AMWA TO 1900-27-00-0001.

Part: FLAP — CRACKED (RT WING)

DURING ROUTINE INSPECTION, RIGHT INBOARD FLAP WAS FOUND TO HAVE A 2.2 INCH CRACK ON THE TRAILING EDGE. REPAIRED IAW SRM AND AMW. (M)

Part: ACTUATOR SWITCH — FAILED (NLG)

WHEN CREW SELECTED GEAR DOWN ON APPROACH TO ICT, THE NOSE GEAR DID NOT SHOW DOWN AND LOCKED. CREW LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE INDICATION SWITCH HAD FAILED. ACTUATOR WAS REMOVED AND REPLACED. AIRCRAFT WAS RETURNED TO SERVICE.