Service Difficulty Reports
December 13, 2010
PILOTS REPORTED THAT THEY NOTICED A SMOKE IN THE COCKPIT AFTER AN ODOR AND VISUAL LEAK OF SMOKE WAS NOTICED COMING FROM
December 23, 2014
MAJOR REPAIR. DURING A SCHEDULED INSPECTION FOUND DENT IN THE RT HORIZONTAL STAB LE 3.25 INCHES BY 1.375 INCHES, DENT A
May 23, 2011
MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A DENT AT FS 316 AND WL 159, APPROX 2.25" * 2.25
June 10, 2002
BOTH PROPS WOULD NOT REACH 1700 RPM. ADJUSTED PROP RPM LEVER, OPS CHECKED SYSTEM SATISFACTORY.
October 01, 1999
PILOT REPORTED THE PILOT'S ALTIMETER TO BE READING 150 FEET HIGH. REMOVED AND REPLACED PILOT'S ALTIMETER. SUBSEQUENT BE
April 08, 2005
ON ROUTINE STRUCTURAL INSPECTION, THE AIRSTAIR DOOR HAS CORROSION ON INNER SKIN NEAR HANDLE. AFFECTED AREA IS APPROX 5.
October 07, 2010
MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A CRACK IN THE FRAME AT STRINGER CUTOUT 10R AND FS 456, .4" IN
June 07, 2016
PILOT REPORTED THAT THEY HAD NO NLG INDICATIONS ON GEAR EXTENSION, RAN ABNORMAL CHECKLIST, DECLARED AN EMER & LANDED WIT
October 07, 2011
"SUP" - SIG EVENT - PILOT REPORTED THAT THE NR2 T-HANDLE ILLUMINATED IN FLIGHT, NO INDICATION OF A FIRE WAS VISIBLE, WIT
September 21, 2011
PILOT REPORTED THAT THE AIRSTAIR DOOR SNUBBER PSI WAS BELOW 1000 PSI. MX SERVICED THE SYS IAW BMM 12-10-00, SYS WITHIN
July 25, 2012
DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE UPPER CARGO DOOR FRAME ON THE FWD SIDE AT APPROX FS 459, 3"
November 01, 2010
MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A .5" CRACK IN THE SKIN 5" LEFT OF BOTTOM CENTER
October 29, 2012
BIRD STRIKE ON LT OTBD WING FROM WS 192.74 TO APPROX 201.74, APPROX .5" IN DEPTH. REPAIRED IAW EO 12-1900-57-011. MAJ
December 20, 2002
LT ENGINE LOW OIL PRESSURE ANNUNCIATOR WITH MASTER WARNING, REMOVED AND REPLACED LT ENGINE.
February 13, 2001
RETURN TO BLOCK, WILL NOT PRESSURIZE. INSPECTED FOUND LOOSE CONNECTION ON SQUAT SWITCH. TIGHTENED, OPS CHECKED SYSTEM
September 07, 2011
PILOT REPORTED THAT THE BULB IN THE LT AUTOFEATHER ANNC IS BURNED OUT. MX REPLACED THE BULB IAW BMM 33-10-01, OPS CHECK
July 25, 2012
DURING A SCHEDULED ROUTINE INSP, FOUND A CRACK IN THE FWD LWR LT PRESSURE BULKHEAD AT FS 84, 2" IN LENGTH. REPAIRED THE
February 13, 2014
DURING A SCHEDULED INSPECTION, FOUND TWO CRACKS IN THE FUSELAGE FRAME ON EITHER SIDE OF STRINGER 2L AT FS 378.25, ONE IN
March 25, 2014
PILOT REPORTED THAT THERE WAS A HOT ELEC SMELL COMING FROM THE FIRST OFFICER'S SIDE OF THE COCKPIT, POSSIBLE FROM THE CB
November 26, 2012
PILOT REPORTED THAT THE CARGO DOOR CAME OPEN IN FLIGHT, LANDED SAFELY. MAINTENANCE REPLACED ALL PARTS AND FRAMES REQ IA
August 16, 2011
PILOT REPORTED THAT DURING APPROACH THE LT PROP WAS CYCLING IN AND OUT OF FEATHER WITH ABOUT 500LBS OF TORQUE. R & R LT
June 17, 2002
PAX DOOR WOULD NOT OPEN. INSPECTED FOUND INNER DOOR CABLE BROKEN. REPLACED INNER DOOR CABLES.
July 26, 2012
DURING A SCHEDULED ROUTINE INSPECTION FOUND THE SKIN CRACKED IN THE UPPER CABIN FUSELAGE AT FS 273.25, BETWEEN STRINGER
September 18, 2012
DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE UPPER CARGO DOOR FRAME ON THE FWD SIDE AT APPROX FS 459, 3"
October 06, 2010
MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A CRACK IN THE 6A EMERGENCY EXIT DOOR SKIN, LOWER FWD RADIUS, 1
October 09, 2012
DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB LT SPAR CAP ANGLE AT 20 PERCENT CHORD AT VSS
September 29, 2011
NR 2 T-HANDLE ILLUMINATED IN FLIGHT. ENGINE SECURED, FIRE EXTINGUISHER ACTIVATED, T-HANDLE REMAINED ILLUMINATED. LIGHT
July 08, 2011
PILOT REPORTED THAT THE UPPER AFT AIRSTAIR DOOR CABLE COVER IS TORN. MX REPLACED THE UPPER AFT AIRSTAIR DOOR CABLE IAW
February 13, 2014
DURING A SCHEDULED INSPECTION FOUND A CRACK BS 107 AND STRINGER 8R FRAME, 0.5 INCH IN LENGTH. REPAIRED IAW EO 13-1900-
April 27, 2005
DURING ROUTINE INSPECTION, UNDER FUSELAGE SKIN CORROSION WAS FOUND WHERE SKIN BONDS TO AIRCRAFT STRUCTURE FS 243-249 AT
March 31, 2010
SUSPECTED AUTOFEATHER - PILOTS REPORTED THAT UPON SHORT FINAL WITH TORQUE BETWEEN 800-1000, PROPELLER WENT IN AND OUT OF
November 29, 2011
PILOT REPORTED THAT FUEL WAS LEAKING FROM THE BOTTOM OF THE ENGINE. MX TIGHTED A LOOSE FUEL LINE, LEAK AND OPS CHECKED
July 25, 2012
DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FWD LWR RT PRESSURE BULKHEAD AT FS 84, 1" IN LENGTH. REPAIR
October 06, 2010
MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND CRACK IN FRAME AT FS 327.63, 1" BELOW FLOORBOARD ON RT SIDE, 2
February 10, 2009
SUP - SIGNIFICANT EVENT - SUSPECTED AUTOFEATHER - UPON APPROACH WITH AUTOFEATHER ARMED BOTH TOQUE GAUGES AT 1000 THE RIG
October 05, 2010
MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A .5" BY .375" BURN HOLE IN THE T/E OF THE ELEVATOR 9" INBD OF
April 30, 2009
PILOTS REPORTED THAT UPON TAKEOFF POWER UP ABOVE 2500 LBS. FOR TAKEOFF THE AFX DISABLE LIGHT ILLUMINATED AND THE NR 2 EN
December 01, 2011
RIGHT AUTOFEATHER WILL NOT TEST DURING RUN UP. MX REPLACED THE RT ENGINE AUTOFEATHER LOW PRESSURE SWITCH.
April 21, 2016
PILOT REPORTED THAT THEY HAD UNSCHEDULED AUTOFEATHER CYCLING ON FINAL. PERFORMED AUTOFEATHER OPERATIONAL CHECKS & COULD
July 20, 2000
GYRO REMOVED FOR PRECESSING, NO FURTHER INFORMATION IS AVAILABLE. (X)
July 26, 2011
PILOT REPORTED THAT WHILE REDUCING POWER FROM 1200 LBS TORQUE TO IDLE NR1 ENGINE TRIED TO AUTOFEATHER. MX R & R LT & RT
April 20, 2009
AFTER TAKEOFF, PROP GAUGE FOR NR 1 ENGINE DROPPED TO 0 RPM AND REMAINED THERE FOR THE REMAINDER OF THE FLIGHT AND TAXI.
November 29, 2011
PILOT REPORTED THAT THERE WAS A FUEL LEAK ON THE LT ENGINE. MX REPLACED THE LP FUEL PUMP.
July 11, 2011
LT ENG AUTO FEATHERED ON FINAL, EACH ENGINE SET TO 300 LBS, ADVANCED TO 1000 LBS, LT ENG AUTO FX UNTIL POWER ADVANCED AB
July 20, 2011
PILOT REPORTED THAT WHEN THEY REDUCED POWER FROM 1200 TO IDLE THE LT ENGINE TRIED TO AUTOFEATHER, DISENGAGED AUTOFEATHER
October 07, 2011
"SUP" - SIG EVENT - PILOT REPORTED THAT THE NR 2 TEE HANDLE ILLUMINATED, SHUTDOWN RT ENGINE AND ACTUATED EXTINGUISHER, V
May 11, 2005
AFTER DEPARTURE, ON CLIMB-OUT FLT CREW NOTICED LEFT ENGINE OIL PRESSURE FLUCTUATIONS, FOLLOWED BY LOW LEFT OIL PRESSURE
February 13, 2014
DURING A SCHEDULED INSPECTION, FOUND TWO CRACKS IN FUSELAGE SKIN, PROTRUDING OUT OF 2 RIVETS AT FS 150.6 STRINGER 1, 0.
June 17, 2002
NR 1 ITT INDICATES HOT ENG ON CLIMB. ADJUSTED TRIM STICK.
February 17, 2009
RT ENG AUTO FEATHERED ON APPROACH.
September 23, 2011
PILOT REPORTED THAT THE CABIN DOOR SNUBBER IS AT 700LBS. MX REPLACED THE DOOR SNUBBER DUE TO LEAKING SEALS IAW BMM 52-1
October 07, 2011
PILOT REPORTED THAT WHILE CLIMBING THE MASTER WARNING AND NR 2 T-HANDLE ILLUMINATED, EMERGENCY DECLARED, NR 2 ENGINE WAS
May 07, 2009
PILOTS REPORTED THAT THE RT ENGINE ATTEMPTED TO AUTOFEATHER ON ABOUT A 3 NAUTICAL MILE FINAL. THE AFX DISABLE ANNUNCIATO
January 20, 2009
DURING ROUTINE MX, A CRACK WAS FOUND ON THE UPPER FUSELAGE AT FS 151.00 NEAR CENTER LINE APPROX 1.6 INCHES LONG AND ONE
July 25, 2012
DURING A SCHEDULED ROUTINE INSPECTION, FOUND THE SKIN CRACKED AT THE EMERGENCY EXIT DOOR 6C SKIN AT THE LWR AFT CORNER,
July 13, 2011
PILOT REPORTED THAT THE AUTOFEATHER CYCLED ABOUT 5 TIMES ON FINAL APPROACH INTO DEN, RPM DROPPED FROM 1700 TO 1400 ON NR
October 13, 2010
MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A CRACK IN THE FRAME AT THE STRINGER CUTOUT 4R AT FS 288, .4" I
July 08, 2011
PILOT REPORTED THAT THE LT ENGINE AUTOFEATHERED ON FINAL, EACH ENGINE SET TO 300LBS, ADVACED TO 1000 LBS LT ENGINE AUTOF
February 13, 2014
DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE FUSELAGE FRAME ANGLE IN THE BEND RADIUS AT FS 451 AND STRINGER 10R,
February 02, 2015
THE CABIN DOOR SNUBBER IS READING 200 PSI LOW & THE DOOR IS HARD TO CLOSE. SERVICED THE CABIN DOOR STRUT AS NEEDED IAW
April 10, 2001
RIGHT ENGINE COMPRESSOR STALLING. RECLASSED BLEED VALVE TEST FLIGHT SATISFACTORY.
April 23, 2003
RIGHT ANTI-ICE ANNUNCIATOR ILLUMINATED. ADJUSTED RT ICE VANE SENSE SWITCHES, OPS CK GOOD.
February 17, 2009
SUSPECTED AUTO FEATHER - PILOTS REPORTED THAT THE RT PROPELLER AUTO FEATHERED IN FLIGHT WITH CORRESPONDING ENGINE ISSUE.
April 24, 2012
PILOT REPORTED THAT AFTER TAKEOFF AT 5000 FT, NR 1 ENGINE SHUTDOWN, RAN CHECKLIST, DECLARED EMERGENCY, RETURNED TO DEPAR
July 30, 2012
DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE LT INBD WING AUX RIB AT WS 29.00 AND FS 288, 1.1" IN LENGTH.
May 15, 2014
DURING A SCHEDULED INSPECTION MAINTENANCE FOUND A CRACK AT FS 456 LT SIDE LOWER FRAME, 1.5 INCHES IN LENGTH. REPAIRED T
May 18, 2004
NR 1 ENG WON'T MAKE TAKEOFF POWER, R & R TRIM STICK PN 3053995CL10.
February 18, 2004
FO'S WINDSHIELD CRACKED, R & R WINDSHIELD RT PN 129-5025-2
October 17, 2011
PILOT REPORTED THAT THE CAPT'S LIFE PRESERVER POUCH IS RIPPED. MX REPLACE THE PRESERVER.
April 30, 2009
BURNING PLASTIC ODOR WHEN MODE CONTROLLER & BLOWERS ON. MAINTENANCE REMOVED FLOORBOARDS OVER THE FORWARD AND AFT VENT
February 09, 2015
DURING A SCHEDULED INSPECTION FOUND A BURN HOLE IN THE RT ELEVATOR TOP OTBD SKIN TE 1.5 INCH WIDE BY .75 INCHES LONG IN
October 07, 2010
MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A CRACK IN THE FRAME ANGLE AT STRINGER 13L AND FS 177.35, UNDE
February 13, 2014
DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE FRAME LT SIDE OF FS 107 BY STRINGER 8L, .125 INCH IN LENGTH. REPAI
June 16, 2009
MAJOR REPAIR, DURING NORMAL LINE OPERATIONS A DENT WAS FOUND JUST FWD AND UNDER THE CARGO DOOR AT FS 446.5 1 INCH ABOVE
March 05, 2009
MAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A CRACK WAS FOUND ON THE LEFT FUSELAGE SKIN AT FS 273.25 AT STRINGER
September 27, 2011
PILOT REPORTED THAT WITH GEAR IN UP POSITION AND AUTO FEATHER SWITCH IN OFF POSITION. AUTO FEATHER OFF ANNUNCIATOR ILLU
October 24, 2011
PILOT REPORTED THAT DURING THE PROP OVERSPEED TEST ON THE RT SIDE THE AFX DISABLE LIGHT ILLUMINATED. MX REPLACED THE AF
January 22, 2013
PILOT REPORTED THE THE F/O'S EMERGENCY LIGHTS ARE INOPERATIVE. MX REPLACED THE BULB AND REPAIRED A WIRE, OPS CHECKED GO
August 07, 2003
NR 1 TORQUE INDICATOR FAILED. REMOVED AND REPLACED NR 1 TORQUE IND.
April 15, 2005
UPON APPROACH, LANDING GEAR WAS SELECTED DOWN AND CREW NOTED THAT NOSE GEAR SHOWED NO INTRANSIT OR GREEN DOWN AND LOCKED
August 10, 2011
DURING THE OVERSPEED TEST ON THE RT ENGINE THE AUTOFEATHER DISABLE ANNUNCIATOR ILLUMINATED. MX REPLACED THE AFX PCB IAW
February 13, 2014
DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE EXIT DOOR 4C, UPPER FWD CORNER, 1.5 INCHES IN LENGTH. REPAIRED IAW
March 21, 2008
DURING STRUCTURAL INSP MAINT FOUND CORROSION ON THE RT WING SPAR AT APPROX WS 126.5. MAINTENANCE REMOVED CORROSION AND
May 05, 2009
RT ENGINE ATTEMPTED TO AUTOFEATHER ON ABOUT A CLOSE FINAL THE AFX DISABLE ANNUNCIATOR ILLUMINATED WHEN THIS OCCURED AND
May 15, 2014
DURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE CARGO DOOR AFT LOWER FRAME AT FS 509.50 AT THE INTERSECTION OF THE
February 13, 2014
DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE RT FWD SPAR CAP ANGLE ON THE VERTICAL STAB 2ND FROM TOP RIVET, .125
March 24, 2009
PILOTS REPORTED THAT WHILE ADDING TAKEOFF POWER THE RIGHT ENGINE WENT INTO FEATHER THROUGH APPROXIMATELY 1500 LB OF. TOR
February 13, 2014
DURING A SCHEDULED INSPECTION FOUND TWO CRACKS IN FUSELAGE FRAME, STRINGER 8L BS 438.25, .999 INCH IN LENGTH. REPAIRE
April 27, 2009
ON SHORT FINAL WITH PROPELLERS AT 1700 , THE NR 2 PROPELLER SEEMED LIKE IT TRIED TO FEATHER MOMENTARILY TWO OR THREE TIM
May 05, 2000
NR 1 ENGINE SHUTDOWN DUE TO LOSS OF OIL PRESSURE AND OIL PRESSURE ILLUMINATING. THE ENGINE WAS REPLACED AFTER IT WAS FO
June 19, 2002
LEFT BLEED-AIR FAILURE. REPAIRED DAMAGED ENA TUBING AT WING, OPS GOOD.
April 04, 2013
DURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE HORIZONTAL STAB AFT WEB AT THE 10 & 2 O'CLOCK POSITION AR
July 25, 2012
DURING A SCHEDULED ROUTINE INSP, FOUND A CRACK IN THE BELLY SKIN AT FS 303, IB 2.5" FROM SKIN EDGE, 4.25" IN LENGTH. RE