Service Difficulty Reports
May 21, 2008
RT UPPER ICE SHIELD DIVIDED INTO (2) PIECES AT APPROXIMATE LOCATION OF STRINGER 8R FROM F.S. 183.25 TO F.S. 220.75. MAIN
February 23, 2004
FLAPS STUCK AT 17 DEG, PENDING CORRECTIVE ACTION
September 15, 2011
LANDING GEAR FAILED TO EXTEND ON APPROACH. DID NOT HEAR THE PUMP TURN ON WHEN MOVING THE LANDING GEAR CONTROL HANDLE.
May 08, 2014
DURING A SCHEDULED INSPECTION MX ACCOMPLISH PROACTIVE REPAIR TO THE RT VERTICAL SPAR CAP ANGLE IAW EO 14-1900-55-001. S
May 19, 2004
LOOSE WIRE CAUSED SPARK ON F.O. YOKE, REMOVED BROKEN WIRE OPS CK GOOD
November 29, 2011
PILOT REPORTED THEAT THE CABIN DOOR ANNUNCIATOR EXTINGUISHES WHEN DOOR IS OPEN AND HANDLE IS CLOSED. MX REPAIRED SPLIC
August 30, 2001
UNCOMMANDED YAW DAMP. REPAIRED CHAFED WIRE.
November 13, 2012
DURING A SCHEDULED ROUTINE INSPECTION FOUND VERT STAB LT SPAR CAP ANGLE AT THE 20 PERCENT CHORD IS CRACKED AT THE UPPER
May 18, 2004
RT N1 INDICATOR SPIKED & FROZE AT 98 PERCENT, PREFORMED OPS CK FOUND NO DEFECTS SWAPPED GAUGES PN 130-380044-5 CND
May 07, 2014
DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE PAX DOOR CUTOUT LOWER FRAME AT APPROXIMATELY FS 172 LOWER AFT CORNE
July 19, 2013
PILOT REPORTED A FOUL ODOR EMINATING FROM THE ENVIROMENTAL SYS WITH A NOTIABLE VIBRATION IN THE BACK OF THE ACFT. MX CL
August 30, 2001
AFTER T/O YAW DAMP/RUDDER BOOST ENGAGED. REPAIRED CHAFED WIRE AT YAW DAMP SWITCH RACK.
September 15, 2009
MAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A CRACK WAS FOUND ON THE BELLY SKIN AT B.L. 29.0 AND F.S. 303.25. CR
April 30, 2009
PILOTS REPORTED THE THE LEFT DC GENERATOR FELL OFFLINE ON TAKEOFF ROLL. MAINTENANCE PERFORMED AN OPERATIONAL CHECK PER
May 21, 2008
STRINGER 10R CRACKED AT F.S. 451. CRACK LENGTH APPROXIMATELY.5 INCH. MAINT REPAIRED STRINGER 10R FLANGE AT F.S. 451 I.A.
November 28, 2014
DURING A SCHEDULED INSPECTION MAINTENANCE FOUND A LIGHTNING STRIKE ON THE OTBD RT ELEVATOR TE JUST OTBD OF THE OTBD MOST
December 03, 2009
MX DISCOVERED THAT THERE WAS CHAFING ON THE FWD RT SIDE OF THE RT MLG BRACE CTR TUBE APPROX 11 INCHES FROM TOP. CHAFE I
July 03, 2000
FIRST OFFICERS EADI DISPLAY IS INTERMITTENT WITH ALL FLAGS ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFI
June 22, 2011
MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND A CRACK IN THE BELLY SKIN AT FS 300 AND RT WING I
September 21, 2011
PILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR DOES NOT EXTINGUISH. MX REPAIRED MULTIPLE WIRES TO SPLICE D436, REPLACED
August 30, 2001
LEFT ITT INDICATOR FAILED ON T/O. REPLACED INDICATOR.
May 07, 2014
DURING A SCHEDULED INSPECTION, FOUND THE EMERGENCY DOOR CRACKED, 4C AT THE RT FWD ASSEMBLY, 1.125 INCHES IN LENGTH. RE
November 14, 2012
DURING A SCHEDULED ROUTINE INSPECTION, FOUND THE RT LONGERON AT JUNCTION WITH RT ANGLE AT FS 107.00 CRACKED FROM THE IN
August 01, 2011
PILOT REPORTED THAT THE CABIN DOOR STRAP SUPPORT ON THE LT SIDE IS COMING APART. MX REINSTALLED A FASTENER ON THE LT CA
January 14, 2014
PILOT REPORTED THAT THE RT FIRE LOOP AND TEE HANDLE ANNUNCIATORS FLICKERED DURING CLIMB OUT. MAINTENANCE TROUBLESHOT SYS
June 22, 2011
MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND CRACKS AT F.S. 456 BETWEEN STRINGERS 3L AND 4L AT
March 13, 2009
FLIGHT 5014- NO AIRSPEED INDICATION ON CA AIRSPEED ON T/O ROLL. MAINTENANCE REMOVED AND REPLACED THE NR 1 AIRSPEED INDI
May 21, 2008
FUSELAGE FRAME AT FS 451 CRACKED ON THE TOP SIDEOF STRINGER 10R. CRACK APPROXIMATELY 1.1 INCH LENGTH. MAINT REPAIRED FU
May 07, 2014
DURING A SCHEDULED INSPECTION, FOUND TWO CRACKS AT BS 150 & STRINGER 1 EXTERIOR FUSELAGE SKIN PROTRUDING OUT OF RIVETS
July 03, 2012
DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE HORIZONTAL STAB AFT WEB AT HSS 0.00, 2" IN LENGTH. REPAIRED
May 21, 2008
FUSELAGE FRAME CRACK AT FS 163.97 AT STRINGER 9R CUTOUT. CRACK APPROXIMATELY .5 INCH IN LENGTH. MAINT REPAIRED FUSELAGE
June 22, 2011
MAJOR REPAIR. DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND A CRACK IN THE FRAME AT FS 456 AND S10R, .5" IN
November 14, 2012
DURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS AT THE RT ANGLE AT FS 107.00 AS IT ATTACHES TO THE LONGERON, RT A
September 18, 2012
DURING A SCHEDULED INSPECTION, FOUND LT LWR FWD PRESSURE BULKHEAD IS CRACKED ALONG THE INBD EDGE DOUBLE ROW OF FASTENER,
May 07, 2009
RIGHT ENVIRO FAIL ANNUNCIATOR ILLUMINATED DURING TAKEOFF WITH TAKEOFF POWER AND BLEED AIR VALVES CLOSED. MAINTENANCE RE-
April 23, 2001
RIGHT FUEL PRESSURE ANNUNCIATOR ILLUMINATED. REPLACED ENGINE DRIVEN FUEL PUMP, OPS CHECKED SYSTEM GOOD. RETURNED TO SE
March 13, 2009
PILOTS REPORTED THAT THE FLAPS STUCK INTERMITTENTLY AT 17 DEGREES AND EVENTUALLY CAME UP UPON LANDING. MAINTENANCE REMOV
January 11, 2012
CABIN DOOR ANNUNCIATOR ILLUMINATED ON DESCENT THEN EXTINGUISHED SHORTLY AFTER. MX CLEANED THE SWITCH, OPS CHECKED GOOD.
August 23, 2001
YAW DAMP ENGAGED ON T/O, REPLACE RELAY DMO8 PN LMD-7111-P AND MODULE K010 PN# LMD-5000-P OPS CHECK SYSTEM SATISFACTORY
February 22, 2005
NR 1 ENG COMPRESSOR STALLS, SHUT DOWN ENG IN FLT RETURNED TO DEN. REMOVED AND REPLACED ENG PN PT6A-67D.
May 22, 2008
FUSELAGE FRAME AT FS 177.3 CRACKED AT STRINGER 9R CUTOUT. CRACK APPROXIMATELY .6 INCH IN LENGTH. MAINTENANCE REPAIRED FU
June 14, 2010
PILOTS REPORTED, WHILE PERFORMING A 2ND START FOR NR 2 ENG. NR 2 STARTER SEEMED TO TURN ON & OFF VERY QUICKLY WHEN IGNIT
June 27, 2011
MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE AS DOOR SKIN DEBONDED AT THE LOWER BOTTOM, DE
January 22, 2000
MILIBAR AND INCHES OF MERCURY SCALES DO NOT MATCH (I.E., 29.92 IN HG SHOWS 0993 MB INSTEAD OF 1013 MB).
October 26, 2011
PILOT REPORTED THAT DURING RUNUP THE AFX DISABLE ANNUNCIATOR WON'T ILLUMINATE ON THE RT AUTOFEATHER TEST. MX RERACKED T
May 07, 2014
DURING A SCHEDULED INSPECTION FOUND A CRACK AT BS 183 & STRINGER 9R FRAME ANGLE, .375 INCHES IN LENGTH. REPAIRED IAW EO
November 14, 2012
DURING A SCHEDULED ROUTINE INSPECTION, FOUND CRACK ON THE LT SIDEWALL AT FS 107.00, LT ANGLE UPPER INBD FLANGE PORTION I
March 24, 2005
DURING ROUTINE STRUCTURAL "I" INSPECTION, FOUR CRACKS WERE IDENTIFIED EMANATING FROM THE DE-ICE HOLE ON THE HORIZONTAL C
February 05, 2004
LT ENGINE ITT EXCEEDED 900C ON ADVANCEMENT OF POWER ON TAKE OFF ROLL, REMOVED AND REPLACED LT ITT GAUGE.
January 20, 2004
FLAPS STUCK AT 17 DEG, PENDING CORRECTIVE ACTION
March 19, 2008
ENGINE SHUTDOWN, FLT 5041 ENROUTE 10 MILES OUT ON FINAL THE NR1 ENGINE FEATHERED INFLIGHT AND THE PILOTS PERFORMED THE E
October 01, 1999
FLIGHT CREW REPORTED THE COMPASS CARD DID NOT MOVE IN THE FREE OR SLAVED MODES WHEN THE AIRCRAFT WAS TURNED. REMOVED AN
August 26, 2010
PILOT REPORTED THAT UPON APPROACH, RT POWER LEVER STUCK WITH AN OVERTORQUE INDICATION, PERFORMED PRECAUTIONARY RT ENGINE
May 07, 2014
DURING A SCHEDULED INSPECTION, MX FOUND THE LT AFT SKIN DENTED AT BS 446 BETWEEN STRINGERS 11-12L. REPAIREDS IAW EO 14
September 18, 2012
DURING A SCHEDULED ROUTINE INSPECTION FOUND RT LWR FWD PRESSURE BULKHEAD CRACKED AROUND FASTENERS ALONG THE BULKHEADS IN
December 07, 2004
CRACK IN FUSELAGE SKIN FWD AND LEFT OF LWR COMM ANTENNA, PERFORMED MAJOR REPAIR TO FUSELAGE SKIN.
July 18, 2007
ABORTED TAKEOFF, FLIGHT 5063, UPON TAKEOFF PILOTS REPORTED THAT THE LT TORQUE INDICATOR STUCK AND WOULD NOT WORK CORRECT