N170GL

Part: CABLE — WORN (AIRSTAIR DOOR) · airframe 38,480 hrs · 47,876 cycles

MAINTENANCE REPORTED THAT THE UPPER AFT DOOR CABLE NEEDS TO BE REPLACED. REMOVED AND REPLACED THE UPPER AFT AIRSTAIR DOOR HANDRAIL CABLE IAW MM 52-10-01.

Part: PIN — BROKEN (AIRSTAIR DOOR) · airframe 38,298 hrs · 47,687 cycles

MAINTENANCE REPORTED THAT THE LOWER AIRSTAIR DOOR STRUT PIN WAS BROKEN. REMOVED AND REPLACED THE LOWER DOOR SNUBBER BRACKET ASSEMBLY (P/N: 129-514117-9) BY REMOVING ATTACHING HARDWARE BY TURNING ALL SCREWS COUNTER-CLOCKWISE UNTIL REMOVED AND SLIDING THE BRACKET OUT OF POSITION. INSTALLED THE NEW BRACKET IN REVERSE ORDER. ATTACHED SNUBBER TO BRACKET IAW TC 1900-5710.01 ITEM 10 AND OPS CHECKED THE PAX DOOR IAW TC 1900-5210.01 ITEM 15. OPS CHECK GOOD.

Part: BOLT — UNSECURE (AIRSTAIR DOOR) · airframe 37,455 hrs · 46,782 cycles

PILOT REPORTED THAT A BOLT FELL OUT OF THE AIR STAIR DOOR COUNTER BALANCE. REPLACED THE BOLT & WASHER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,427 hrs · 46,752 cycles

MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE SKIN CRACKED AT FS 100.500, JUST BELOW FIRST OFFICERS WINDSHIELD, BOTTOM OTBD CORNER, .625" IN LENGTH. REPAIRED IAW EO 15-1900-53-15.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,427 hrs · 46,752 cycles

MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE LT BELLY SKIN AT APPROX FS 303.25 & BL 29.06, 1.25" IN LENGTH. REPAIRED IAW EO 15-1900-53-017.

Part: COVER — WORN (FUEL NOZZLE)

FUEL NOZZLE SHEATHS HAVE SIGNS OF CONTACTING THE TOP OF THE FUEL NOZZLE & THE SHEATH DOME AREA.

Part: SKIN — CRACKED (EMERGENCY EXIT) · airframe 37,427 hrs · 46,752 cycles

MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND A CRACK AT THE EMERGENCY EXIT 6A SKIN, AT THE INNER LOWER FWD CORNER, .55" IN LENGTH. REPAIRED IAW EO 15-1900-52-001.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,427 hrs · 46,752 cycles

MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND 3 CRACKS IN THE LT FUSELAGE SKIN, AT THE LT VORTEX GENERATOR, LOCATED BETWEEN FS 232.25 & 248.25, LOCATED AT THE BOTTOM OF STRINGER 12L, TOTAL 3.35" IN LENGTH. REPAIRED IAW EO 15-1900-53-016.

Part: SKIN — CRACKED (EMERGENCY EXIT) · airframe 37,427 hrs · 46,752 cycles

MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE EMERGENCY EXIT 6C SKIN, CRACKED AT THE INNER LOWER AFT CORNER, .8" INCHES LENGTH. REPAIRED IAW EO 15-1900-52-002.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 37,427 hrs · 46,752 cycles

MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND 2 CRACKS AT CANT BULKHEAD, AT FS 588.10 AT JUNCTION WITH STRINGER 8R, CANT BULKHEAD AT FIRST FASTENER TOP SIDE AT STRINGER 8R & AT FIRST FASTENER BELOW STRINGER 8R, BOTTOM CRACK RADIATES UPWARD & DOWNWARD FROM FASTENER, 1.05" IN TOTAL LENGTH. REPAIRED IAW EO 15-1900-53-018.

Part: BULKHEAD — DENTED (FUSELAGE) · airframe 37,427 hrs · 46,752 cycles

MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND DENTS AT BULKHEAD AT FS 84.00, BETWEEN THE FIRST & SECOND DOUBLER FROM THE LT OTBD EDGE. DENT AREA IS 4" FROM LT TO RT & 6.7" UP & DOWN, DEEPEST DENTED AREA MEASURES AT APPROX .23". ALSO FOUND TWO SMALL DENTS BETWEEN SECOND & THIRD DOUBLER FROM LT OTBD EDGE, MEASURING APPROX 4" & 6" UP FROM BOTTOM SHELF. REPAIRED IAW EO 15-1900-53-014.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 37,427 hrs · 46,752 cycles

MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THAT THE ANGLE LOCATED AT FS 150.60 IS CRACKED IN AN AREA AT THE AIRSTAIR DOOR STRUT UPPER MOUNT BRACKETS, LOWER AFT SCREW HOLE. REPAIRED IAW EO 15-1900-53-009.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 37,427 hrs · 46,752 cycles

MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THAT THE AIRSTAIR DOOR FRAME LOWER FWD CORNER AREA, FS 150 & STRINGER 11L, IS CRACKED APPROX .50 INCHES IN LENGTH. CRACK RADIATES OTBD FROM THE CUT OUT. THE CUT OUT IS APPROX 3 INCHES UPWARD FROM THE LOWER END OF THE FRAME. REPAIRED IAW EO 15-1900-53-013.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,427 hrs · 46,752 cycles

MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE INNER SKIN AT FS 150.60, BETWEEN STRINGERS 7L & 6L IS CRACKED, APPROX 1.5" IN LENGTH AT THE AIR STAIR DOOR STRUT'S UPPER MOUNT BRACKETS, LOWER AFT ATTACHING SCREW HOLE ACCESS. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.

Part: SKIN — CORRODED (FUSELAGE) · airframe 37,427 hrs · 46,752 cycles

MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND BELLY CORROSION AT FS 243.25 & STRINGER 15L. REPAIRED IAW EO 15-1900-52-012.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,427 hrs · 46,752 cycles

MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND A CRACK ON THE FWD FRAME FLANGE AT FS 177.35 BETWEEN STRINGER 14L & 13L, 1" IN LENGTH. REPAIRED IAW EO 15-1900-53-011.

Part: CONTROL CABLE — BROKEN (ZONE 100) · airframe 37,018 hrs · 46,267 cycles

PILOT REPORTED THAT THE RUDDER AILERON INTERCONNECT CABLE BROKE. REPLACED THE AILERON RUDDER INTERCONNECT CABLE PN NAS323-13-0250 IAW MM 27-10-08.

Part: WIRE HARNESS — DAMAGED (BRAKES) · airframe 35,982 hrs · 45,049 cycles

PILOT REPORTED THAT WITH ANTI-SKID ON BRAKES TOTALLY INOPERATIVE. BRAKES WORK NORNALLY WITH ANTI-SKID OFF. FOUND LT TRANSDUCER HARMESS DAMAGED. R & R WIRE HARNESS AND TRANSDUCER CONNECTIONS IAW AIM 14 PARA 14.3.9 OPS CHECKED GOOD.

Part: MOTOR — INOPERATIVE (MLG) · airframe 35,524 hrs · 44,519 cycles

PILOT REPORTED THAT THE LANDING GEAR FAILED TO EXTEND WHEN GEAR HANDLE WAS SELECTED TO DOWN POSITION, NO INTRANSIT LIGHT INDICATION AND NO GREEN LIGHTS, RAN CHECKLIST AND MANUALLY EXTENDED GEAR. MX R & R THE POWER PACK MOTOR AND TIME DELAY PCB, OPS CHECKED GOOD.

Part: SKIN — CORRODED (BS 228.25) · airframe 344,449 hrs · 43,279 cycles

DURING A SCHEDULED ROUTINE INSP FOUND BELLY SKIN CORROSION AT FS 228.25 AND STRINGER 16. REPAIRED IAW EO 12-1900-53-076. MAJOR REPAIR

Part: STRINGER — CORRODED (BS 228.25-213.25) · airframe 34,449 hrs · 43,279 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND STRINGER 16 CORRODED BETWEEN FS 228.25 AND 213.25. REPAIRED IAW EO 12-1900-53-077. MAJOR REPAIR.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 34,449 hrs · 43,279 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE LT INBD WING, LOWER INBD ATTACH ANGLE, JUST FWD OF FWD WING SPAR AT BL 29, 1.1" IN LENGTH. REPAIRED IAW EO 12-1900-57-012. MAJOR REPAIR.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 34,449 hrs · 43,279 cycles

DURING A SCHEDULED ROUTINE INSP, FOUND A CRACK IN THE RT SPAR CAP ON VERTICAL STAB AT TOP HOLE, .5" IN LENGTH. REPAIRED IAW EO 12-1900-55-069. MAJOR REPAIR.

Part: WEB — CRACKED (HORIZONTAL STAB) · airframe 34,449 hrs · 43,279 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE AFT HORIZONTAL STAB WEB, 0.125" IN LENGTH. REPAIRED IAW EO 12-1900-558-070. MAJOR REPAIR.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 33,884 hrs · 42,575 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS ON THE VERTICAL STAB LT FWD SPAR CAP ANGLE, (1) RADIATES UPWARD FROM THE UPPER FASTENER TO THE EDGE OF THE SPAR CAP ANGLE, RADIATES DOWNWARD FROM THE SECOND FASTENER, VSS 84.10 AT 20 PERCENT CHORD, .875" IN LENGTH. REPAIRED IAW FR-CO-02528, REV 1, STEP 1. MAJOR REPAIR.

Part: BULB — BURNED OUT (INSTRUMENT PANEL) · airframe 33,646 hrs · 42,282 cycles

CAPTAIN'S SIDE INSTRUMENT EMERGENCY LIGHTS BURNED OUT AND 1 INST INDIRECT LIGHT BULB. MX REPLACED THE BULB, OPS CHECKED GOOD.

Part: DAMPER — WORN (ZONE 700) · airframe 32,707 hrs · 41,181 cycles

EXPERIENCED VIOLENT NOSE WHEEL SHIMMY DURING TO AT APPX V1. CONTINUED UNTIL SHORTLY AFTER GEAR RETRACTION. MX REPLACED THE NLG TIRE IAW TC 1900-3240.00 AND REPLACED SHIMMY DAMPER IAW MM 32-20-03.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 32,707 hrs · 41,181 cycles

MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND FOUR CRACKS AT A MACHINED HOLE AT 2, 8, 10, & 4 O'CLOCK POSITIONS AT THE HORIZONTAL STAB AFT SPAR WEB AT HSS 0.0, .73" IN LENGTH.

Part: PLACARD — DISLODGED (CABIN) · airframe 31,786 hrs · 40,126 cycles

PILOT REPORTED THAT THE EMERGENCY PLACARD FELL OFF AT 3C. MX REPLACED THE PLACARD IAW AIM 5-16-0.

Part: SEAL — LEAKING (PAX DOOR) · airframe 31,708 hrs · 39,977 cycles

PILOT REPORTED THAT THE DOOR SEAL IS LEAKING IN FLIGHT. MX SEAL, LEAK CHECKED GOOD IAW BMM 52-10-06.

Part: SEAL — WORN (PAX DOOR) · airframe 31,650 hrs · 39,968 cycles

PILOT REPORTED THAT THE CABIN DOOR SEAL MAKES EXCESSIVE NOISE WITH CABIN PRESSURIZED ABOVE 3.5 PSID. MX INSPECTED AND FOUND A BAD SEAL ON THE NR1 ADF ANTENNA, REPLACED SEAL, IAW TC 1900-3411.00-3, LEAK CHECKS GOOD.

Part: SEAL — FAILED (PAX DOOR) · airframe 31,563 hrs · 39,852 cycles

PILOT REPORTED THAT THE CABIN DOOR SQUEALS IN FLIGHT. EXCESSIVE AMOUNT OF SEALANT ON DOOR SEAL, REMOVED SEALANT AND RESEALED THE DOOR SEAL, IAW BMM 52-10-04.

Part: SEAL — UNSECURE (PAX DOOR) · airframe 31,559 hrs · 39,848 cycles

PILOT REPORTED THAT THE CABIN DOOR SQUEALS IN FLIGHT. MX RESECURED THE DOOR SEAL IAW BMM 52-10-04.

Part: CABLE — DAMAGED (PAX DOOR) · airframe 31,559 hrs · 39,848 cycles

PILOT REPORTED THAT THE UPPER DOOR CABLE SHEATHING IS PEALING. MX REPLACED THE CABLE IAW BMM 52-10-02.

Part: FRAME — CRACKED (BS 183.25) · airframe 31,464 hrs · 39,726 cycles

DURING A SCHEDULED ROUTINE INSP MX FOUND A CRACK IN THE FRAME AT FS 183.25 AND STRINGER CUTOUT 9AR, .3" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-051 MATERIALS UTILIZED ARE INCLUDED IN THE EO. MAJOR REPAIR

Part: SOLENOID — DIRTY (PROPELLER) · airframe 31,274 hrs · 39,512 cycles

PILOT REPORTED THAT WHEN THE POWER IS PULLED BACK TO IDLE DURING THE FLARE THE NR 2 PROP STAYS AT 1700 RPM AND WHILE THE NR 1 COMES DOWN THROUGH 1600 RPM. MX CLEANED, INSP, AND LUBED THE FLIGHT IDLE STOP SOLENOID, OPS CHECKED GOOD IAW RUN SHEET, ALL CHECKS GOOD.

Part: SOLENOID — DIRTY (LOW PITCH) · airframe 31,274 hrs · 39,512 cycles

PILOT REPORTED THAT WHEN THE POWER IS PULLED BACK TO IDLE DURING THE FLARE THE NR 2 PROP STAYS AT 1700 RPM AND WHILE THE NR 1 COMES DOWN SLOWLY. MX CLEANED THE LOW PITCH SOLENOID, PERFORMED ENGINE RUN SHEET 1900-RUN-WORKSHEET FEG 212, OPS CK GOOD.

Part: BEARING — SEIZED (VENT BLOWER)

DURING SCHEDULED BRUSH, CHANGE THE REPAIR THE TECH NOTED NOISE FROM THE BEARINGS. INSP REVEALED THE ARMATURE, 1 OF THE (COMMUTATOR END) BEARINGS HAD FAILED. A VISUAL INSP OF THE BEARING REVEALED THE GREASE HAD SEEPED PAST THE SEALED AREA AND THE BEARING WOULD NOT SPIN FREELY BY HAND. BOTH BEARINGS WERE R & R NO OTHER DISCREPANCIES NOTED.

Part: AUTOFEATHER SYS — MALFUNCTIONED (RT PROPELLER) · airframe 29,906 hrs · 37,924 cycles

PILOT REPORTED THE THE RIGHT ENGINE CYCLED IN AND OUT OF FEATHER MULTIPLE TIMES ON SHORT FINAL, STARTED WITH TORQ AT 1K AND STOPPED WHEN BROUGHT ABOVE 2K TORQ, N1 AT 90-91% AT THAT TIME. MAINTENANCE INSPECTED THE LOW PITCH SOLONOID IAW MM 61-20-00, PERFORMED OPERATION CHECK OF AUTOFEATHER SYSTEM IAW MM 61-21-00, ALL CHECKS GOOD, OK FOR SERVICE.

Part: HOLDER — CORRODED (FUSE) · airframe 29,537 hrs · 37,487 cycles

PILOT REPORTED THAT THE RT SIDE INSTRUMENT EMERGENCY LIGHTS DO NOT TURN ON WITH THE SWITCH. MX INSPECTED AND FOUND CORROSION ON THE FUSE HOLDER, REPLACED HOT BATTERY BUSS FUSE HOLDER PN 4532 IAW BMM 24-31-00, OPS CHECKS GOOD.

Part: HOLDER — FAILED (BATTERY BUSS) · airframe 29,537 hrs · 37,487 cycles

RT SIDE INST EMERGENCY LIGHTS DO NOT TURN ON WITH SWITCH. MX INSPECTED AND FOUND CORROSION ON THE FUSE HOLDER, REPLACED HOT BATTERY BUSS FUSE HOLDER PN 4532 IAW BMM 24-31-00, OPS CHECKS GOOD.

Part: FRAME — CRACKED (ZONE 100) · airframe 28,687 hrs · 36,499 cycles

MAJOR REPAIR - DURING ROUTINE SCHEDULED MX, A CRACK WAS FOUND IN A FRAME AT FS 456 AND STR 10R. CRACK IS APPROX .3" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-011. MATERIALS UTILIZED ARE INCLUDED IN THE EO.

Part: FRAME — CRACKED (ZONE 100) · airframe 28,687 hrs · 36,499 cycles

MAJOR REPAIR - DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND IN THE BEND RADIUS OF A FRAME AT FS 451 JUST ABOVE STRINGER 10R. CRACK IS APPROX .9" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-012. MATERIALS UTILIZED ARE INCLUDED IN THE EO.

Part: ANGLE — CRACKED (ZONE 100) · airframe 28,687 hrs · 36,499 cycles

DURING ROUTINE SCHEDULED MX THE RT HEAVY ANGLE WAS FOUND CRACKED IN THE BEND RADIUS AT THE FWD END OF THE ANGLE AT FS 288.0. THE CRACK IS APPROX 1.3" IN LENGTH. A CRACK AT FS 303 WAS ALSO PRESENT .5". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W EO 10-1900-53-009. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.

Part: SKIN — DEBONDED (ZONE 800) · airframe 28,687 hrs · 36,499 cycles

DURING ROUTINE SCHEDULED MX THE AIRSTAIR DOOR AREA FROM THE TOP STEP HINGE TO THE LOWER EDGE. THE INNER SKIN IS DEBONDED. MX R & R THE AIRSTAIR DOOR BOND ASSY IAW MM 52-10-03.

Part: ANGLE — CRACKED (ZONE 500) · airframe 28,687 hrs · 36,499 cycles

MAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE THE LEFT HAND HEAVY ANGLE WAS FOUND CRACKED IN THE BEND RADIUS AT THE FORWARD END OF THE ANGLE AT F.S. 288.0. THE CRACK IS APPROXIMATELY 1.5" IN LENGTH.

Part: ANGLE — CRACKED (ZONE 100) · airframe 28,687 hrs · 36,499 cycles

DURING ROUTINE SCHEDULED MX THE LT HEAVY ANGLE WAS FOUND CRACKED IN THE BEND RADIUS AT THE FWD END OF THE ANGLE AT FS 288.0. THE CRACK IS APPROX 1.5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W EO 10-1900-53-010. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.

Part: SWITCH — FAULTED (MLG) · airframe 27,765 hrs · 35,364 cycles

AIR TURNBACK - PILOTS REPORTED THAT UPON TAKEOFF AND CLIMBING THAT THE GEAR HANDLE IN TRANSIT LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTION. MAINTENANCE REMOVED AND REPLACED THE NOSE AND RIGHT HAND MAIN UPLOCK SWITCHES. MAINTENANCE RIGGED THE SWITCHES AND THE OPERATIONAL CHECKS WERE GOOD REFERENCE 1900D MM 32-60-00-201. RII INSPECTION COMPLIED WITH PER TASKCARD 4.3.8 FOR THE INSTALLATION AND RIGGING.

Part: SWITCH — DIRTY (NR 2 PROPELLER) · airframe 26,747 hrs · 33,974 cycles

PILOTS REPORTED THAT THE RT ENGINE NR 2 PROPELLER VIOLENTLY CYCLES IN AND OUT OF FEATHER. PROPS WERE FULL FWD, IDLE SLOWLY INCREASING, CAUSED YAWING AT 1500 FT ON APPROACH. MX CLEANED POWER LEVER AUTOFEATHER MICROSWITCHES AND PERFORMED OPSL CHECK OF AUTOFEATHER SYSTEM IAW MM 61-21-00. ALL CHECKS WERE GOOD.

Part: WARNING HORN — FALSE ACTIVATION (STALL WARNING) · airframe 26,730 hrs · 33,951 cycles

PILOTS REPORTED THAT THE STALL WARNING CAME ON AT WEIGHT OFF WHEELS AND STAYED ON. RETURNED TO DEN. MAINTENANCE TESTED THE STALL WARNING SYSTEM ON GROUND. JACKED AIRCRAFT AND OPERATED STALL WARNING STALL LIFT TRANSDUCER MANUALLY AND FOUND THAT STALL HORN SILENCES. OPERATION NORMAL IAW 77-31-00. OPERATIONAL CHECK FLIGHT WAS ALSO PERFORMED.

Part: CONNECTOR — DIRTY (RT ENGINE) · airframe 26,321 hrs · 33,412 cycles

ENGINE SHUTDOWN - DIVERSION, OIL PRESSURE ON THE NR2 ENG WAS READING BETWEEN 60 AND 40 PSI WHEN THEY LEVELED OFF AT CRUISE, IT EVENTUALLY WENT TO "0" PSI. OIL TEMP WAS OK AND LOW OIL PRESSURE ANNUNCIATOR DID NOT ILLUMINATE UNTIL ENG SHUTDOWN. MX REMOVED AND INSPECTED CONNECTOR PLUG TO OIL PRESSURE TRANSDUCER, REINSTALLED AND PERFORMED ENG RUNS WITH FLIGHT CREW, OPS CHECK WAS NORMAL IAW MM 79-30-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 26,208 hrs · 33,255 cycles

MAJOR REPAIR - FUSELAGE FRAME CRACKED APPROX .400 INCH IN LENGTH AT THE STRINGER 10R CUTOUT AT FS 164. MX REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE IAW SRM 51-70 AT F.S. 164 AND STRINGER 10R. REPAIR APPROX 5.5 INCHES BY 2.5 INCHES OUT OF 2024 T3 ALUMINAUM, .071 INCH, MS20470AD RIVETS. RII INSP COMPLIED IAW TASKCARD 8.2.1.

Part: ACM — CONTAMINATED (CABIN AIR) · airframe 23,093 hrs · 29,293 cycles

PILOTS REPORTED A STRONG EXHAUST ODOR IN CABIN WITH HEAT TURNED ON. MAINTENANCE REMOVED EXCESS WATER IN ACM AND CLEANED OBSTRUCTION IN WATER NOZZLE ASSEMBLY. OPERATIONAL CHECK OF THE SYSTEM IAW 21-40-00 AND 21-50-00 WAS GOOD.

Part: ANGLE — CRACKED (BS 288) · airframe 22,912 hrs · 29,077 cycles

UPON ROUTINE INSPECTION MAINTENANCE DISCOVERED CRACK AT RT FS 288 WL 70.0. LENGTH OF CRACK 1.75 INCHES. UPON COMPLETION OF REPAIRE RII INSPECTION IS REQUIRED. [OPEN]

Part: ANGLE — CRACKED (BS 288) · airframe 22,912 hrs · 29,077 cycles

UPON ROUTINE INSPECTION, MAINTENANCE DISCOVERED CRACK AT LT FS 288 WL.70.0. LENGTH OF CRACK 1.75 NR. UPON COMPLETION OF REPAIRE RII INSPECTION IS REQUIRED. MAINTENANCE REPAIRED AFFECTED AREA AT FS 288 WS 70.0 IAW SRM 53-90-23-001. IWO NR 94109. RII COMPLIED IAW TASKCARD 8.2.1. INSPECTION SATISFACTORY.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,912 hrs · 29,077 cycles

UPON ROUTINE INSPECTION MAINTENANCE DISCOVERED CRACK AT RT FS 288 WL 70.0. LENGTH OF CRACK 1.75 INCHES. UPON COMPLETION OF REPAIRE RII INSPECTION IS REQUIRED. MAINTENANCE REPAIRED AFFECTED AREA AT FS 288 WS 70.0 IAW SRM 53-90-23-001. IWO NR 94109. RII COMPLIED WITH IAW TASKCARD 8.2.1, INSPECTION SATISFACTORY.

Part: ACM — CONTAMINATED · airframe 22,905 hrs · 29,069 cycles

AIR RETURN - FLIGHT 5134 - ENROUTE FROM LBF TO DEN PILOTS REPORTED SMOKE/MIST IN THE CABIN AFTER DEPARTURE. MAINTENANCE TROUBLESHOT THE ISSUE AND FOUND NO SMOKE, HOWEVER, MIST WAS WAS REPORTED AND MAINTENANCE FOUND AN EXCESSIVE AMOUNT OF MOISTURE IN THE AIR CYCLE MACHINE. MAINTENANCE REMOVED MOISTURE PERFORMED A SYSTEM OPERATIONAL CHECK. REFERENCE 1900D MM 21-50. OPERATIONAL CHECK GOOD.

Part: UNKNOWN — UNKNOWN (CABIN) · airframe 21,338 hrs · 27,202 cycles

SMOKE / STEAM IN CABIN FROM ROWS 2-7, STOPPED WHEN ENVIROMENTAL SYSTEM WAS TURNED OFF. OPERATIONAL CHECK OF ENVIROMENTAL SYSTEM SATISFACTORY, NO FAULTS FOUND.

Part: UPLOCK SWITCH — OUT OF ADJUST (MLG) · airframe 19,608 hrs · 25,144 cycles

GEAR INTRANSIT LIGHT ILLUMINATED, CYCLED GEAR ALL GEAR CAME UP, TRANSIT LIGHT REMAINED ILLUMINATED. PERFORMED GEAR SWING, NOSE GEAR UPLOCK SWITCH REQUIRED ADJUSTMENT.

Part: LATCH — DAMAGED (CARGO DOOR) · airframe 17,158 hrs · 22,393 cycles

CARGO DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT, R & R SAFETY LATCH PN 114-514046-1 OPS CK GOOD

Part: WARNING LIGHT — ILLUMINATED (RT ENVIRO SYS) · airframe 16,762 hrs · 21,944 cycles

RT ENVIRO FAIL ANNC ILLUM, GROUND RAN ACFT AT FULL PWR SETTING WITH RAPID POWER ADVANCES AND ACCELERATION COULD NOT GET RT ENVIRO FULL OPS CK GOOD.

Part: ANNUNCIATOR — ACTIVATED (ENVIR SYS) · airframe 16,681 hrs · 21,848 cycles

RT ENVIRO FAIL ANNC ILLUM ON TAKEOFF, PERFORMED GROUND PERFORMANCE RUN. OPS CK GOOD.

Part: INDICATOR — INTERMITTENT (AIRSPEED) · airframe 16,627 hrs · 21,789 cycles

CAPT HAS NO AIRSPEED INDICATION, ASI STARTED WORKING ABOUT HALF WAY ON FERRY FLIGHT. DID PITOT STATIC TEST OPS CK GOOD.

Part: INDICATOR — INTERMITTENT (AIRSPEED) · airframe 16,627 hrs · 21,789 cycles

CAPT HAS NO AIRSPEED IND, ASI STARTED WORKING ABOUT HALF WAY TO DEN ON FERRY FLIGHT. DID PITOT STATIC TEST, OPS CK GOOD

Part: GOVERNOR — OUT OF RIG (RT ENGINE) · airframe 16,162 hrs · 21,298 cycles

RT ENGINE FUEL FLOW AND PROP TORQUE FLUX, RIGGED RT GOV INTERCONNECT.

Part: TUBE — DAMAGED (BLEED AIR) · airframe 15,614 hrs · 20,712 cycles

RIGHT BLEED AIR FAIL. REPAIRED SPLIT EVA TUBING, OPS CK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 15,558 hrs · 20,657 cycles

CRACK IN BELLY SKIN NEAR COMM ANT. REPAIRED CRACK IAW BEECH SRM.

Part: CIRCUIT BREAKER — TRIPPED (IGNITER) · airframe 15,255 hrs · 20,344 cycles

RT IGNITER POWER CIRCUIT BREAKER POPPED W/N RESET, R&R RT IGNITER CB

Part: BRUSH BLOCK · airframe 15,003 hrs · 20,060 cycles

LH PROP DEICE INOP, REPLACED BRUSH BLOCK

Part: INVERTER · airframe 14,639 hrs · 19,632 cycles

LH INVERTER FAILED, R&R INVERTER

Part: SKIN — BIRD STRIKE (FUSELAGE) · airframe 13,955 hrs · 18,749 cycles

BIRD STRIKE RT ENG ON ROLL, INSP A/C NO DAMAGE FOUND

Part: COMPUTER — MALFUNCTIONED (E/E BAY) · airframe 13,853 hrs · 18,600 cycles

F/O'S FLIGHT DIRECTOR FROZE, ALL FCP LIGHTS LIT UP, AP FAIL ILL THEN FD FLAGGED ON EHSI. RERACKED DPU.

Part: SWITCH — INOPERATIVE · airframe 12,930 hrs · 17,342 cycles

LEFT PUSH TO-TALK SWITCH FAILED REPLACED OPS CHECKED SATISFACTORY

Part: TORQUE LINK — DAMAGED (LT MLG) · airframe 12,818 hrs · 17,190 cycles

LEFT MAIN TORQUE KNEE SEPARATED DURING TAXI. REPLACED, OPS CHECKED SATISFACTORY.

Part: INDICATOR — ERRATIC (#2) · airframe 12,375 hrs · 16,722 cycles

RIGHT ENGIN TORQUE INDICATOR ERRATIC, REPLACED INDICATOR OPS CHECKED SYSTEM SATISFACTORY

Part: DUCT — DAMAGED (BLEED AIR) · airframe 11,710 hrs · 16,002 cycles

RIGHT BLEED AIR FAILURE AND LOSS OF PRESSURIZATION. REPAIRED EVA TUBING, OPS CHECKED SYSTEM SATISFACTORY.

Part: HYDRAULIC LINE — DEFECTIVE (HYDRAULIC SYS) · airframe 11,224 hrs · 15,383 cycles

LANDING GEAR RELAY CB POPS WHEN GEAR SELECTED DOWN REPLACED LT MLG ACTUATOR HYDRAULIC LINE, OPS CHECKED SYSTEM SATISFACTORY

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 10,894 hrs · 14,951 cycles

CABIN PRESSURIZATION SPIKED SEVERAL TIMES AFTER T/O. REPLACED PRESSURE CONTROLLER, OPS CHECKED SYSTEM SATISFACTORY.

Part: SWITCH — DIRTY (RT 'T' HANDLE)

RIGHT 'T' HANDLE ILLUMINATE RETURNED TO GATE. CLEANED MICROSWITCHES ON 'T' HANDLE AND REPAIRED GROUND WIRE AT LOOP. (M)

Part: BLEED AIR VALVE — DIRTY (ENGINE)

MCW - ENGINE WENT TO 1800 LBS TORQUE ON APPROACH. CLEANED BLEED AIR VALVE. (M)

Part: HANDLE — LACK OF LUBE (COCKPIT)

DEN - OXYGEN PULL HANDLE HARD TO PULL. DISASSEMBLED HANDLE CLEANED, INSPECTED AND REASSEMBLED. (M)

Part: PRESS SWITCH — FAILED (HYD PWR PACK)

LANDING GEAR WILL NOT RETRACT. FERRIED AIRCRAFT FROM DVL TO SPW. REMOVED AND REPLACED PRESSURE SWITCH, OPS CHECK GOOD. (X)

Part: EVA TUBE — CHAFED (LEFT)

RDU - LEFT 'BLEED AIR FAIL' IN FLIGHT. MAINTENANCE REPAIRED TWO LEAKS DUE TO CHAFING IN EVA TUBING. (M)

Part: BULB — FAILED (COCKPIT)

RDU - INSTRUMENT EMERGENCY LIGHTS INOP. INSTALLED NEW BULB ON INSTRUMENT INDIRECT ROW. (M)

Part: AIR DISTRIBUTION — CONDENSATION (CABIN)

RDU - SMOKE IN CABIN. MAINTENANCE FOUND CONDENSATION IN CABIN. (M)

Part: TRUSS — CRACKED (LT ENGINE)

RDU - FOUND .75 INCH CRACK IN LEFT ENGINE TRUSS. REMOVED AND REPLACED LEFT TRUSS ASSY. (M)

Part: CONTROL CABLE — OUT OF ADJ (ELEVATOR TRIM)

RDU - ELEVATOR TRIM JAMMED DURING FLIGHT, WOULD NOT MOVE MANUALLY OR ELECTRICALLY. MAINTENANCE FOUND LOOSE RUDDER SADDLE CABLE INTERFERRING WITH ELEVATOR TRIM CABLE. SADDLE CABLE WAS TIGHTENED AND TRIM OPERATION WAS NORMAL. (X)

Part: BLEED AIR LIGHT — ILLUMINATED (LEFT)

RDU - LEFT BLEED AIR FAIL ANNUNCIATOR ILLUMINATED IN FLIGHT. MAINTENANCE MEL'D SYSTEM. (M)

Part: FUEL CONTROL — FAILED (RT ENGINE)

RDU - RIGHT TORQUE FLUCTUATIONS OF 600 TO 700 LBS. HIGH ITT WHEN TORQUE IS ABOVE 2000 FT/LBS. MAINTENANCE REMOVED AND REPLACED FCU. OPERATIONAL CHECKS NORMAL. (M)

Part: BLEED VLV — STICKING (RT ENGINE)

AVL - RIGHT ENGINE DOES NOT MAKE TORQUE, ONLY UP TO 2900 FEET LBS TORQUE. MAINTENANCE REMOVED, CLEANED AND REPLACED BLEED VALVE. OPERATES NORMALLY. (M)

Part: FUEL CONTL — MALFUNCTIONED (LT ENGINE)

CHS - AFTER DEPARTURE ON CLIMB-OUT, LEFT ENGINE STUCK AT 3600 TORQUE. N1 STAYED AT 95 PERCENT. MAINTENANCE REMOVED AND REPLACED HIGH PRESSURE FUEL PUMP AND FCU. OPERATIONAL CHECKED GOOD. REFERENCE GLBA96166.

Part: FUEL PUMP — MALFUNCTIONED (LT ENGINE)

CHS - AFTER DEPARTURE ON CLIMB-OUT LEFT ENGINE STUCK AT 3600 TORQUE. N1 STAYED AT 95 PERCENT. MAINTENANCE REMOVED AND REPLACED HIGH PRESSURE FUEL PUMP AND FCU. OPERATIONAL CHECKED GOOD. (M)

Part: ANN LIGHT — ILLUMINATED (LT/RT BLEED AIR)

RDU - BOTH BLEED AIR FAIL ANNUNCIATORS ILLUMINATED IN FLIGHT. CYCLED BLEED SWITCHES TO ENVIRONMENTAL OFF AND BOTH ANNUNCIATORS REMAINED ILLUMINATED. MAINTENANCE COULD NOT DUPLICATE. (M)

Part: TACHOMETER — MALFUNCTIONED (RT ENGINE)

HHH - CREW ABORTED TAKEOFF BECAUSE RIGHT RPM INDICATOR DROPPED TO ZERO. MAINTENANCE COULD NOT DUPLICATE. OPS CHECK WAS GOOD. (X)