N247GL

Part: CABLE — FRAYED (PAX DOOR) · airframe 39,183 hrs · 47,257 cycles

MAINTENANCE REPORTED THAT THE AIRSTAIR DOOR LOWER FORWARD HANDRAIL CABLE WAS FRAYED. REMOVED AND REPLACED THE HANDRAIL CABLE IAW BMM 52-10-02.

Part: UNKNOWN — ODOR (CABIN) · airframe 39,138 hrs · 47,203 cycles

PILOTS REPORTED THAT THERE WAS A LINGERING, FOUL, MOLDY STENCH IN THE COCKPIT AND CABIN. THOUGHT TO BE COMING FROM THE BLOWER VENTS. THE ODOR WAS NOTED AS VERY NAUSEATING AND FATIGUING FOR THE CREW TO FLY IN. MAINTENANCE CLEANED AREAS FORWARD AND AFT OF THE MAIN SPAR UNDER FLOOR. REMOVED BROWN SMELLY SUBSTANCE WITH ALCOHOL AND A SCRUBBER PAD. APPLIED CPC TO CLEANED AREAS.

Part: CABLE — LOOSE (PAX DOOR) · airframe 38,882 hrs · 46,916 cycles

MAINTENANCE DISCOVERED THAT THE PASSENGER DOOR AFT CABLES WERE LOOSE AND REQUIRE ADJUSTMENT. TIGHTENED PASSENGER DOOR AFT CABLE IAW AMM 52-10-02.

Part: SKIN — CRACKED (LE SLAT) · airframe 37,810 hrs · 45,697 cycles

FOUND THE LT INBD LE INSIDE SKIN HAS SEVERAL AREAS OF CHAFING FROM THE CONTROL CABLES RUBBING & HOLES, A .5" SHALLOW HOLE & CHAFE MARKS, A .375", .125" HOLES IN SKIN ONLY, SHALLOW HOLE, SMALL .25" WEAR HOLE, .75" TEAR IN THE EDGE OF THE SKIN & A CRACK, .25" IN LENGTH. REPAIRED IAW EO 15-1900-57-002.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 37,810 hrs · 45,697 cycles

MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND A 2.8" CRACK IN AN ANGLE AT FS 456.0, AT FWD CARGO FLOOR LEVEL. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 15-1900-53-008.

Part: FRAME — CRACKED (BS 107) · airframe 37,808 hrs · 45,697 cycles

DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE FRAME AT FS 107 BY STRINGER 8L, PROTRUDING OUT OF RIVET ON EITHER SIDE, .25" IN LENGTH. REPAIRED IAW EO 15-1900-53-007. MAJOR REPAIR.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 37,810 hrs · 45,697 cycles

MAJOR REPAIR, DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE FRAME AT FS 509.5, AFT SIDE OF CARGO DOOR FRAME AT MID-CARGO FLOOR LEVEL, .7" IN LENGTH. REPAIRED THE AFFECTED AREA. PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 15-1900-53-006.

Part: PRINTED CKT BOARD — FAULTY (ZONE 600) · airframe 37,397 hrs · 45,255 cycles

PILOT REPORTED THAT ON CLIMB OUT AFX DISABLE LIGHT ILLUMINATED, N1 ABOVE 91% ON THE RT SIDE. REPLACED PCB A123, PN 129-364091-9, SN ON 993-F-94, SN OFF 799-C-93 IAW MI 34-01, SYS OPERATIONS CHECK GOOD.

Part: SPAR CAP — MECHANIC ERROR (LT WING) · airframe 36,843 hrs · 44,681 cycles

MAJOR REPAIR DURING A SCHEDULED INSPECTION FOUND THE LT WING SPAR AFT CAP AT WS 12325 FASTENER HOLE MISSED DRILLED THROUGH THE WING SKIN & WING SPAR CAP. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-57-003. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.

Part: FRAME — CRACKED (BS 164) · airframe 34,828 hrs · 42,375 cycles

DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE FRAME AT FS 164 AND STRINGER 10R, 0.375" IN LENGTH. REPAIRED IAW EO 13-1900-53-028. MAJOR REPAIR.

Part: FRAME — CRACKED (BS 451) · airframe 34,828 hrs · 42,375 cycles

DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT FS 451 AND STRINGER 10R FRAME, .5" IN LENGTH. REPAIRED IAW EO 13-1900-53-027. MAJOR REPAIR.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 34,828 hrs · 42,375 cycles

DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE RT SPAR CAP AT THE SECOND FASTENER, FWD VERT STAB, 0.375" IN LENGTH. REPAIRED IAW EO 13-1900-55-008. MAJOR REPAIR.

Part: UPLOCK SWITCH — INOPERATIVE (NLG) · airframe 34,518 hrs · 42,005 cycles

PILOT REPORTED THAT ON LANDING, LOWERED THE GEAR, INTRANSIT LIGHT CAME ON AND WENT OUT, GOT GREEN ON MAINS, NOT ON NOSE, MANUALLY EXTENDED GEAR AND STILL NO GREEN ON NOSE. MX REPLACED THE NOSE UPLOCK SWITCH, OPS CK GOOD.

Part: SKIN — CRACKED (LT ELEVATOR)

DURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 CRACKS ON A LT ELEVATOR ASSY IN THE T/E, APPROX 23.1875" OTBD OF TRIM TAB OTBD CUTOUT, ON BOTH SIDES OF THE ELEVATOR SKIN, (TOP AND BOTTOM SIDES), 1" IN LENGTH. REPAIRED IAW EO 13-1900-27-001. MAJOR REPAIR.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 33,638 hrs · 40,967 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE LT FWD SPAR CAP ANGLE AT THE VERT STAB AT VSS 84.10 AND THE 20 PERCENT AT THE SECOND FASTENER, CRACK RADIATES DOWNWARD FROM FASTENER, .375" IN LENGTH. REPAIRED IAW FR-CO-02530, REV 1, STEP 1. MAJOR REPAIR.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 32,517 hrs · 39,644 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND 5 TO 7 CRACKS RADIATING FROM THE CENTER LIGHTNING HOLE ON THE STAB REAR SPAR CENTER WEB, 2.5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-55-009. MATERIALS UTILIZED ARE INCLUDED IN THE EO. MAJOR REPAIR

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 32,517 hrs · 39,644 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 CRACKS ON MAIN SPAR WEB AT HSS 3.0L AND 3.0R, 1 INCH IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-55-010. MATERIALS UTILIZED ARE INCLUDED IN THE EO. MAJOR REPAIR

Part: FRAME — CRACKED (BS 456) · airframe 31,893 hrs · 38,908 cycles

DURING A SCHEDULED ROUTINE INSPECTION FOUND THE AFT FUSELAGE FRAME AT FS 456 CRACKED AT THE FWD GAS STRUT MOUNT UPPER INBD NUT PLATE, BETWEEN STRINGER 4L AND 5L, 2 CRACKS 1" AND .2" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-067. MATERIALS UTILIZED ARE INCLUDED IN THE EO. MAJOR REPAIR.

Part: TERMINAL — BROKEN (AIRSTAIR DOOR) · airframe 31,810 hrs · 38,814 cycles

ALL THE INSPECTION LIGHTS IN THE AIRSTAIR DOOR SYS ARE INOPERATIVE. MX FOUND A BROKEN TERMINAL WIRE ON THE DOOR, MX REPLACED THE TERMINAL AND OPS CHECKED GOOD.

Part: STALL WARNING — FALSE ACTIVATION · airframe 31,485 hrs · 38,443 cycles

PILOT REPORTED THAT AT 80 KNOTS IAS THE STALL WARNING HORN SOUNDED AND THE TAKEOFF WAS ABORTED. MX TROUBLESHOT THE SYS, COULD NOT DUPLICATE, CHECKED CONNECTORS ON THE SWITCH HARNESSES, ATTACHED A BREAKOUT BOX, NO DEFECTS FOUND, RESECURED SQUAT SWITCH HARNESS, IAW BMM 27-34-00, SYS OK FOR SERVICE.

Part: HOUSING — TORN (PAX DOOR) · airframe 31,224 hrs · 38,134 cycles

PILOT REPORTED THAT THE AIRSTAIR CABLE HOUSING IS RIPPED, UPPER AFT. MX REPLACED THE UPPER AFT CABLE IAW BMM 52-10-02, PN: 1440-10GLA.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 30,275 hrs · 37,028 cycles

PILOT REPORTED THAT ON DECENT PASSENGER OXYGEN MASKS DEPLAYED INADVERTENTLY. MAINTENANCE REPACKED ALL PAX O2 MASKS IN CONTAINERS IAW BMM 35-20-01.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,757 hrs · 36,402 cycles

EMERGENCY LIGHT BULB DID NOT TEST. MAINTENANCE REPLACED THE BULB PN 1864, REF MM 31-10-00, OPS CHECK GOOD.

Part: SKIN — DENTED (ZONE 100) · airframe 29,086 hrs · 35,627 cycles

MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, A DENT ON RT SIDE OF FUSELAGE AT FS 531 BETWEEN STRINGER 11R AND 10R WAS FOUND. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-049. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.

Part: TUBE — DETERIORATED (BLEED SYS) · airframe 27,283 hrs · 33,367 cycles

ABORTED TAKEOFF- AIRCRAFT 247GL DID AN ABORTED TAKEOFF IN HVR FLT 5186 FOR RT BLEED AIR FAIL ANNUNCIATOR ILLUMINATING. CREW RETURNED TO GATE AND CALLED MX. THE CREW AND MX AGREED THAT IT COULD BE MEL'D UNDER 21-3-2 CAT B. THE CREW BEFORE DOING THE MEL RAN THE AIRCRAFT FOR THE "O" PROCEDURE OF THE MEL AND CONFIRMED AIRCRAFT WAS IN OPERATING ORDER TO DO THE MEL. RT BLEED WAS MEL'D. PILOTS REPORTED THAT THEY OBSERVED A RIGHT HAND BLEED AIR FAIL ANNUNCIATOR ILLUMINATED ON TAKEOFF. PILOTS PERFORMED MEMORY ITEMS AND QRH ITEMS AND THE LIGHT REMAINED ILLUMINATED. MAINTENANCE ORIGINALLY PLACED THE ITEM ON MEL 21-3-2 CATEGORY B. MAINTENANCE ULTIMATELY REPAIRED THE RIGHT HAND LEADING EDGE EVA TUBING IAW 26-11-00.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 27,208 hrs · 33,273 cycles

ACFT WOULD NOT PRESSURIZE DURING CLIMB OUT. MX SECURED THE RT OUTFLOW VALVE THAT WAS FOUND LOOSE IAW MM 21-30-01-201. AN OPS TEST FLIGHT WAS CONDUCTED AND FOUND TO BE SATISFACTORY.

Part: SHUTOFF VALVE — DETERIORATED (NR 1) · airframe 26,649 hrs · 32,544 cycles

AT 400 FT, TURNED BLEEDS ON AN LT ENVIRO FAIL ANNUN ILLUMINATED, TRIED TO RESET SEVERAL TIMES IAW THE CHECKLIST, DID NOT RESET, RETURNED TO DEPARTURE AND TRANSFERED THE ISSUE TO DML NR 35433 PER MEL 21-14 CAT C ALL O PROCEDURES COMPLIED WITH. MX REMOVED AND REPLACED THE LT PRSOV PN 114-380059-5 SN ON 0154B OFF 0456B IAW BMM 21-11-03 OPS CHECKS WERE GOOD. MX CLEARED THE DML AND THE PLACARD WAS REMOVED.

Part: DOOR FRAME — CRACKED (BS 456-509) · airframe 26,354 hrs · 32,153 cycles

DURING SCHEDULED STRUCTURAL INSP MX DISCOVERED CRACKS AROUND THE CARGO DOOR UPPER FRAME AT FWD CORNER AREA AT FS 456 AND UPPER FRAME AFT CORNER AT FS 509. APPROXIMATE CRACK LENGTHS 5 INCHES AND 2.75 INCHES RESPECTIVELY. MX REPAIRED THE AFFECTED AREAS IAW EO-09-1900-53-002. MATERIALS UTILIZED INCLUDE PN'S 129-440043-1, MS20470AD5, AC240 B1/2 SEALANT, 9309-3NA, NAS1097-4,NAS1097-5, CR3212-5, CR3212-4,CR3214-4, MS20470D-5 AND NAS1330C3KB116.

Part: SKIN — CRACKED (ZONE 200) · airframe 26,354 hrs · 32,153 cycles

MAJOR REPAIR - SKIN CRACKS ON TOP OF FUSELAGE AT F.S. 150.6 AT STRINGER 1 WERE FOUND DURING SCHEDULED STRUCTURAL CHECK. RIVET HEAD WAS SHEARED WITH CRACKS STARTING AT SAID RIVET AND ANOTHER CRACK AT A RIVET SAME LOCATION OTHER SIDE OF STRINGER 1. MAINTENANCE REPAIRED THE AFFECTED AREA IAW EO-09-1900-53-001. RII INSPECTION COMPLIED WITH PER TASKCARD 4.3.7.

Part: RELAY — FAULTY (LANDING GEAR) · airframe 25,831 hrs · 31,470 cycles

SIGNIFICANT EVENT - ENROUTE FROM PGA TO FMN THE PILOTS REPORTED THAT THE GEAR RELAY CIRCUIT BREAKER POPPED TWICE AND THEY HAD TO MANUALLY EXTEND THE GEAR. MX REMOVED AND REPLACED THE LANDING GEAR RELAY IAW MFG MX 32-30. OPS CHECKS WERE GOOD.

Part: LATCH — FAILED (PAX DOOR) · airframe 23,269 hrs · 28,211 cycles

EES - FLIGHT 5041 (DEN) PILOTS REPORTED THE MAIN CABIN DOOR COULD NOT BE OPENED FROM THE INSIDE. MAINTENANCE CLEANED THE PUSH BUTTON SWITCH AND OPERATIONALLY CHECKED THE DOOR. OPS GOOD IAW MM 52-10-00.

Part: STRINGER — CRACKED (BS 451 S10R) · airframe 23,170 hrs · 28,100 cycles

STRINGER 10R CRACKED AT FS 451 IAW CRACK IS ABOUT .5 IN LONG AT STRINGER RELIEF CUTOUT. CRACKED AT STRINGER FLANGE. REPAIRED STRINGER FLANGE AT FS 451 IAW. 1900D SRM 51-70. REPAIR DIMENSIONS APPROXIMATELY 9.375 IN BY 1 IN. 2024 T-3 .050. RII COMPLIED WITH IAW TASKCARD 8.2.1.

Part: ANGLE — CRACKED (BS 288) · airframe 23,170 hrs · 28,100 cycles

LT HEAVY ANGLE CRACKED AT FS 288. CRACK LENGTH APPROXIMATELY 1.75 INCH. MAINTENANCE REPAIRED LT HEAVY ANGLE AT FS 288 IAW 1900D SRM 53-90. REPAIR DIMENSIONS APPROXIMATELY 13.5 INCHES. RII COMPLIED WITH IAW TASKCARD 8.2.1.

Part: FRAME — CRACKED (BS 451 S10R) · airframe 23,170 hrs · 28,100 cycles

FRAME AT FS 451.0 CRACKED AT STRINGER 10R RELIEF CUTOUT CRACK IS .6250 IN LONG. MAINTENANCE REPAIRED FRAME FLANGE AT FS 451.0 IAW 1900D SRM 51-70. REPAIR APPROXIMATELY 6 INCH BY 2 INCH 2024 T3 .063. RII COMPLIED WITH IAW TASKCARD 8.2.1.

Part: SKIN — DAMAGED (BS 423) · airframe 22,534 hrs · 27,330 cycles

HOLE IN FUSELAGE ON THE RT SIDE FORWARD OF FS 423.25 AND 2 INCHES ABOVE STRINGER 12R. APPROXIMATELY 1 INCH V SHAPE HOLE/CUT. MAINTENANCE REPAIRED AFFECTED AREA WITH A FLUSH REPAIR IAW MFG SRM 51-70. RII COMPLIED WITH IAW TASKCARD 8.2.1. HOLE CUTOUT SIZE 1.3 INCH X 1.3 INCH.

Part: HYDRAULIC LINE — DEFECTIVE (RT MLG) · airframe 22,148 hrs · 26,889 cycles

FLIGHT 5128, ENROUTE, PILOTS REPORTED THAT WHILE INFLIGHT MAIN GEAR EXTENDED AND THE LANDING GEAR RELAY CIRCUIT BREAKER POPPED. CREW MANUALLY EXTENDED GEAR TO ACHIEVE A (3) GREEN CONFIGURATION. MAINTENANCE REMOVED AND REPLACED A FLEXIBLE HYDRAULIC LINE IN THE RT GEAR AREA AND PERFORMED AN OPERATIONAL CHECK IAW MM 32-30-10. OPERATIONAL AND LEAK CHECK GOOD.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 19,112 hrs · 23,165 cycles

LEFT WINDSHEILD OUTER PLY SHATTERED. REPLACED WINDSHEILD.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 17,929 hrs · 21,856 cycles

DURING ROUTINE STRUCTURAL INSPECTION, ALL THREE EMERGENCY EXIT WINDOW PANS WERE FOUND TO HAVE CRACKS AROUND THE RADIUS. WINDOW PANS WERE REPLACED, AIRCRAFT RETURNED TO SERVICE.

Part: HANDLE — CORRODED (AIRSTAIR DOOR) · airframe 17,477 hrs · 21,364 cycles

AIRSTAIR DOOR HANDLE SHOWS SIGN OF CORROSION, REMOVED CORROSION AND REPAIRED.

Part: ENGINE — OVERTEMP (LEFT) · airframe 16,714 hrs · 20,490 cycles

LT ENGINE TEMP LIMITED AT TAKE OFF, PREFORMED GROUND RUN ALL PARAMETERS WITHIN LIMITS

Part: INDICATOR — STUCK (AIRSPEED) · airframe 16,621 hrs · 20,383 cycles

NR 2 ASI STUCK AT ZERO, R&R NR 2 ASI PN 130-380005-7

Part: STATIC WICK — DAMAGED (COMM SYSTEM) · airframe 16,466 hrs · 20,220 cycles

STATIC IN BOTH COMM'S BOTH NAV'S FAILED IN PRECIP, R&R STATIC WICKS PN 101-380053-9

Part: RADIO — MALFUNCTIONED (COMM SYSTEM) · airframe 16,466 hrs · 20,220 cycles

STATIC IN BOTH COMM'S BOTH NAVS FAILED PRECIP, R & R STATIC WICKS

Part: INDICATOR — STUCK (AIRSPEED) · airframe 16,399 hrs · 20,150 cycles

FO'S ASI STUCK AT ZERO, PREFORMED PITOT CK OPS CK GOOD

Part: INDICATOR — SMOKE (AIR SPEED) · airframe 16,393 hrs · 20,144 cycles

NR 2 ASI STAYED AT ZERO & TOWER REPORTED OF SMOKE ON TAKE OFF ROLL, R&R NR 2 ASI GROUND RAN ACFT INSP ENG NO PROBLEMS NOTED

Part: IDLER GEAR — STICKING (AILERON TRIM) · airframe 16,380 hrs · 20,218 cycles

AILERON TRIM CATCHES AND STICKS, R&R IDLER GEAR ASSY. OPS CK GOOD

Part: INDICATOR — FAILED (COCKPIT) · airframe 16,322 hrs · 20,070 cycles

FAILURE OF FIRST OFFICER'S A/S INDICATOR. PERFORMED GROUND CHECK, FOUND NO DEFECTS.

Part: INDICATOR — SLOW (AIRSPEED) · airframe 16,017 hrs · 19,749 cycles

FO'S AIRSPEED IND SLOW, TURNED PITOT HEAT ON FOR LONGER PERIOD OPS CK GOOD PN 130-380005-7

Part: INDICATOR — FAILED (COCKPIT) · airframe 15,983 hrs · 19,715 cycles

FO'S AIRSPEED FAILED TO WORK ON TAKE OFF, REMOVED AND WARMED FO'S AIRSPEED IND PN1303800057 INSTALLED ASI RUN UP ON PITOT STATIC TEST OPS CK GOOD.

Part: SWITCH — INOPERATIVE (TE FLAPS) · airframe 15,035 hrs · 18,719 cycles

FLAPS WOULD NOT RETRACT BEYOND 17 DEG. REPLACED THE SPLIT FLAP LINKS ON BOTH SIDES.

Part: WINDSHIELD — CRACKED · airframe 13,245 hrs · 16,819 cycles

#2 WINDSHIELD CRACKED AT 24,000, REPLACED WINDSHIELD

Part: WINDSHIELD — CRACKED (COPILOT) · airframe 13,117 hrs · 16,687 cycles

COPILOT WINDSHIELD CRACKED, REPLACED WINDSHIELD

Part: CONTROL CABLE — LACK OF LUBE (NR 2 PROPELLER) · airframe 13,012 hrs · 16,586 cycles

NR 2 PROP CANNOT REGULATE PROP RPM AT A HIGHER RPM. T/S CLEANED AND LUBRICATED PROP CABLES AND ROD ENDS AT RIGHT ENGINE.

Part: TRANSDUCER — INTERMITTENT (STALL WARNING) · airframe 12,856 hrs · 16,419 cycles

STALL WARNING INTERMITTENT. REPLACED TRANSDUCER.

Part: TRANSMITTER — INTERMITTENT (TORQUE INDICATOR) · airframe 12,305 hrs · 15,816 cycles

RT TORQUE INDICATOR FAILED, REPLACED TRANSMITTER OPS CHECKED SYSTEM SATISFACTORY

Part: PRESSURE SWITCH — FAILED (LEFT) · airframe 12,152 hrs · 15,651 cycles

AUTO FEATHER LIGHT ILLUMINATED INFLIGHT. REPLACED HIGH PRESSURE SWITCH, OPS CHECKED SYSTEM SATISFACTORY.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 12,055 hrs · 15,544 cycles

FLAPS WOULD NOT EXTEND. REPLACED RIGHT I/B ACTUATOR, OPS CHECKED SYSTEM SATISFACTORY.

Part: PUMP — FAILED (RT ENGINE) · airframe 12,021 hrs · 15,509 cycles

RIGHT LOW PRESSURE FUEL LIGHT ILLUMINATED. REPLACED FUEL PUMP, OPS CHECKED SYSTEM SATISFACTORY.

Part: VANE — DIRTY (STALL WARNING) · airframe 11,340 hrs · 14,792 cycles

STALL WARNING WOULD NOT SILENCE. CLEANED STALL VANE, OPS CHECKED SYSTEM SATISFACTORY.

Part: INDICATOR — MALFUNCTIONED (COCKPIT) · airframe 10,598 hrs · 13,968 cycles

LEFT ENGINE ITT INDICATION HIGH AFTER T/O, PERFORMED ENGINE RUN ALL PARAMITERS WITHIN LIMITS. RETURNED TO SERVICE.

Part: ALTIMETER — FAILED (COCKPIT) · airframe 10,245 hrs · 13,594 cycles

CAPTAINS ALTIMETER FAILED INFLIGHT. REPLACED INDICATOR.

Part: DAMPENER — MALFUNCTIONED (AUTOPILOT SYS) · airframe 10,060 hrs · 13,388 cycles

YAW DAMP ENGAGED ON T/O ROLL. COULD NOT DUPLICATE FAILURE. RETURNED TO SERVICE.

Part: GYRO — INOPERATIVE (COCKPIT) · airframe 9,907 hrs · 13,214 cycles

RETURN TO BLOCK - NR 1 VG FAILED. REMOVED AND REPLACED VERTICAL GYRO.

Part: CONTROL HANDLE — INTERMITTENT (INSTRUMENT PNL)

LANDING GEAR HANDLE HAD TO BE MOVED TO THE EXTEND POSITION SEVERAL TIMES BEFORE THE LANDING GEAR WOULD EXTEND. REPLACED THE LANDING GEAR SELECT HANDLE. RETRACTION/EXTENSION CHECKED GOOD. (M)

Part: ALTIMETER — INACCURATE (COCKPIT)

PILOT WRITE-UP WAS ''GIVES ERRONEOUS READINGS AND FAILNG TCAS''. BENCH CHECK INDICATED ENCODER PULSES B4 AND C1 INOPERATIVE AND ALTIMETER IS 50 FEET HIGH (30 FEET OUT OF LIMITS) FROM -1,000 FEET TO 2,000 FEET. UNIT WAS SENT FOR REPAIR. (X)