N195GL

Part: DOOR FRAME — CRACKED (AIRSTAIR) · airframe 40,370 hrs · 50,112 cycles

MAJOR REPAIR - MAINTENANCE NOTED THAT THE FUSELAGE DOOR FRAME WAS CRACKED AT STRINGER 11L AND FS 171.0. CRACK IS APPROXIMATELY 1.1 INCHES IN LENGTH. ** SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAPERWORK. **

Part: HINGE — LOOSE (PAX DOOR) · airframe 40,127 hrs · 49,828 cycles

MAINTENANCE REPORTED THAT THE AIRCRAFT SIDE OF THE AIRSTAIR DOOR HINGE HAD AFT RIVETS WHICH WERE LOOSE. REMOVED AND REPLACED LOOSE RIVETS REF SRM 51-40-03.

Part: CABLE — WORN (PAX DOOR) · airframe 40,085 hrs · 49,779 cycles

MAINTENANCE REPORTED THAT THE UPPER FWD AIRSTAIR CABLE IS WORN. REMOVED AND REPLACED THE UPPER FWD AIRSTAIR CABLE IAW AMM 52-10-02. PN OFF/ON: 1440-42GLA, NSN.

Part: CABLE — WORN (PAX DOOR) · airframe 40,085 hrs · 49,779 cycles

MAINTENANCE REPORTED THAT THE UPPER AFT AIRSTAIR CABLE IS WORN. REMOVED AND REPLACED THE UPPER AFT AIRSTAIR CABLE IAW AMM 52-10-02.

Part: CIRCUIT BREAKER — POPPED (COCKPIT) · airframe 40,007 hrs · 49,676 cycles

SIG EVENT, THE CREW DECLARED AN EMERGENCY ON APPROACH FOR LANDING [GEAR] FAILED TO EXTEND NORMALLY. IN TRANSIT LIGHT ILLUMINATED. MAINTENANCE FOUND 60A(CB11) POPPED, INSPECTED WIRES FROM BUS BAR TO C/B TO GEAR MOTOR, NO FAULTS FOUND AIM 14.3. RESET C/B 11 & C/B 2. PERFORMED GEAR SWINGS REF MI 32-01, COULD NOT DUPLICATE. FOR MX RELIABILITY, R&R LANDING GEAR POWERPACK MOTOR P/N: 571302, S/N OFF: 1420A, S/N ON: 334A REF BMM 32-30-04 & LDG RELAY (K3) P/N: MS24171-D1, S/N OFF: UE195, S/N ON: 16-006 BY REMOVING HARDWARE & INSTALLING TO SECURE RELAY & WIRES. PERFORMED GEAR SWINGS REF MI 32-01, OPS CHECK GOOD.

Part: PRESSURE SWITCH — DIRTY (RT PROPELLER) · airframe 39,945 hrs · 49,596 cycles

THE CREW NOTED THAT THEY EXPERIENCED AN UNSCHEDULED AUTOFEATHER CYCLING DURING APPROACH TO LAND. THE ISSUE OCCURRED ON THE RIGHT ENGINE. MAINTENANCE REMOVED AND INSTALLED RIGHT ENGINE COWL IAW TC 1900-7100.10 STEPS 1, 2, 13, AND 14. CLEANED RIGHT LOW PRESSURE SWITCH IAW MM 61-21-01. CLEANED AND LUBED LOW PITCH SOLENOID IAW FCD 1900-09-79-01 STEPS 5 AND 13. CREW OPS CHECKED GOOD.

Part: CABLE — BROKEN (PAX DOOR) · airframe 39,856 hrs · 49,487 cycles

MAINTENANCE NOTED THAT THE LOWER FWD AIRSTAIR DOOR CABLE WAS BROKEN.

Part: CABLE — BROKEN (AIRSTAIR DOOR) · airframe 39,846 hrs · 49,476 cycles

SIG EVENT, PILOT REPORTED THAT THE A/S DOOR CABLE BROKE. ** SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAPERWORK. **

Part: SNUBBER — DISCONNECTED (PAX DOOR) · airframe 39,309 hrs · 48,884 cycles

PILOT REPORTED THAT THE AIRSTAIR DOOR SNUBBER ARM CENTER PIVOT BOLT WAS DISCONNECTED. OPEN

Part: SKIN — CRACKED (BS 238-248) · airframe 38,048 hrs · 47,560 cycles

DURING A SCHEDULED INSPECTION MX FOUND 2 CRACKS IN THE LT FUSELAGE SKIN UNDER THE VORTEX GEN MOUNT AREA. FWD SKIN CRACK IS .9" IN LENGTH AT FS 238.25, STRINGER 12L, & AFT SKIN CRACK IS 1.0" IN LENGTH AT FS 248.25, STRINGER 12L, CRACK 1.9" IN TOTAL LENGTH. REPAIRED THE SKIN IAW EO 15-1900-53-005. MAJOR REPAIR.

Part: FRAME — CRACKED (BS 163.975) · airframe 38,048 hrs · 47,560 cycles

DURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE FUSELAGE FRAME REPAIR & FRAME AT FS 163.975, STRINGER 10R, FRAME CRACK BEYOND STOP DRILL, .65" IN LENGTH. REPAIRED THE FRAME IAW EO 15-1900-53-004. MAJOR REPAIR.

Part: FRAME — CRACKED (BS 177.35) · airframe 38,048 hrs · 47,560 cycles

DURING A SCHEDULED INSPECTION, MX FOUND A CRACK IN THE FUSELAGE FRAME AT FS 177.35 IN THE BEND RADIUS AT THE OTBD END OF THE FRAME, 1.25" IN LENGTH. REPAIRED THE FRAME IAW EO 15-1900-53-003. MAJOR REPAIR.

Part: CHANNEL — CRACKED (BS 177) · airframe 38,048 hrs · 47,560 cycles

DURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE FUSELAGE CHANNEL AT BS 177.35, IN THE BEND RADIUS AT THE OTBD END OF THE CHANNEL, 1.2 INCH IN LENGTH. REPAIRED IAW EO 15-1900-53-002. MAJOR REPAIR.

Part: SNUBBER — LOW PRESSURE (CABIN DOOR) · airframe 38,017 hrs · 47,523 cycles

THE AIR STAIR DOOR OPENS REALLY FAST & FOUND THAT THE DOOR SNUBBER PRESS READ 500 PSI. SERVICED THE AIR STAIR DOOR SNUBBER AS NEEDED IAW MI 52-01. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: BRAKE SYS — MALFUNCTIONED (MLG) · airframe 37,363 hrs · 46,764 cycles

SIG EVENT PILOT REPORTED THAT THE RT BRAKE PEDAL GOES COMPLETELY TO THE FLOOR ON THE CAPTAIN`S & FIRST OFFICER'S SIDE, RIGHT BRAKE COMPLETELY INEFFECTIVE. SUPPLEMENT INFORMATION ION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.

Part: SKIN — DAMAGED (LT WING) · airframe 37,013 hrs · 46,365 cycles

DURING A SCHEDULED INSPECTION, FOUND A DENT FROM A BIRD STRIKE ON THE LT WING L/E BETWEEN WS 236.62 AND 223.48 AND HAS A FUEL LEAK DUE TO THE DAMAGE. REPAIRED IAW EO 13-1900-57-019. MAJOR REPAIR

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 35,052 hrs · 44,093 cycles

DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT THE EDGE OF A LIGHTNING HOLE, HORIZONTAL STABILIZER AFT SPAR WEB CENTERLINE AT HSS 0.00, .1" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-068.

Part: SKIN — CORRODED (FUSELAGE) · airframe 35,052 hrs · 44,093 cycles

DURING A SCHEDULED ROUTINE INSPECTION FOUND CORROSION AT FS 228.25, ON SKIN, CORROSION FOUND JUST OTBD OF THIS REPAIR, STRINER 14R 4" OTBD. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-075. MAJOR REPAIR

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 35,052 hrs · 44,093 cycles

DURING A SCHEDULED ROUTINE INSPECTION FOUND 2 CRACKS IN THE RT SPAR CAP ANGLE ON VERT STAB AT SECOND FASTENER FROM THE TOP, 1.25" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-067. MAJOR REPAIR

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 35,052 hrs · 44,093 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE LT SPAR CAP ANGLE ON VERTICAL STAB AT SECOND FASTENER FROM THE TOP, .75" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-066. MAJOR REPAIR

Part: SKIN — CORRODED (BS 243.25 S16L) · airframe 35,052 hrs · 44,093 cycles

DURING A SCHEDULED ROUTINE INSPECTION FOUND BELLY CORROSION AT FS 243.25, APPROX 1" LEFT OF STRINGER 16. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-074. MAJOR REPAIR

Part: FILTER — LEAKING (FUEL SYSTEM) · airframe 32,746 hrs · 41,386 cycles

PILOT REPORTED THAT THERE IS A FUEL LEAK AROUND THE NR 1 ENG FUEL FILTER. MX REPLACED THE NR1 ENG FUEL FILTER.

Part: SWITCH — OUT OF ADJUST (DOOR WARNING) · airframe 32,100 hrs · 40,604 cycles

PILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR ILLUMINATED WHEN TAKEOFF POWER WAS APPLIED. MX ADJUSTED THE DOOR LATCH SWITCH IAW MM 52-70-00, OPS CK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,066 hrs · 40,558 cycles

PILOT REPORTED THAT THE INSTRUMENT EMERGENCY LIGHTS ARE INOP ON THE F/O'S SIDE. MX REPLACED THE LAMP IAW BMM 33-10-04, OPS CK GOOD.

Part: SKIN — CRACKED (EMERGENCY EXIT) · airframe 32,066 hrs · 40,558 cycles

MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND THE EMERGENCY EXIT AT SEAT 6A SKIN CRACKED IN LOWER FWD CORNER, 1.25" INCHES IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-52-009. MATERIALS UTILIZED ARE INCLUDED IN THE EO.

Part: FRAME — CRACKED (BS 509.5) · airframe 32,066 hrs · 40,558 cycles

MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND A CRACK IN THE CARGO DOOR UPPER FRAME AT FS 509.50 BETWEEN STRINGERS 3L & 4L, 3.75" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-050. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.

Part: PROPELLER — MALFUNCTIONED (FEATHERING SYS) · airframe 32,028 hrs · 40,511 cycles

THE PILOT REPORTED THAT ON APPROACH, AT 500' AGL WITH BOTH TORQUES AROUND 750LBS THE RT ENGINE CYCLED INTO AND OUT OF FEATHER TWICE, ADDED POWER TO 1500LBS AND IT STOPPED. MX FOUND LT ENGINE HIGH & LOW TORQUES OUT OF RIG, RERIGGED POWER LEVERS IAW AIM 7.2.4 & 7.2.5, OPS CHECKED GOOD.

Part: PRESSURE SWITCH — MALFUNCTIONED (AUTOFEATHER SYS) · airframe 30,701 hrs · 38,892 cycles

LT SIDE PROP AUTOFEATHER W/ 1000LBS TQ SHORT FINAL. STOPPED AUTOFEATHERING ABOVE 1000 LBS TQ. MX INSPECTED THE SYS AND ADJUSTED THE FLIGHT IDLE TORQUE IAW AIM CH 7 SEC 2.5, PARA 2 AND REPLACED THE LOW PRESS SWITCH, RAN ENGINES, OPS CHECK GOOD IAW BMM.

Part: SKIN — CRACKED · airframe 30,448 hrs · 38,102 cycles

MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A 1.1" CRACK IN THE LOWER LEFT FUSELAGE SKIN AT B.L. 26.8 AND F.S. 301.6. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-052. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.

Part: SKIN — DEBONDED (AIRSTAIR DOOR) · airframe 30,448 hrs · 38,702 cycles

DURING A SCHEDULED ROUNTINE INSP, FOUND THE AIRSTAIR DOOR SKIN DEBONDING ON THE LOWER AFT, APPROX 19" IN LENGTH. MX REPLACED THE AIRSTAIR DOOR BONDED SKIN IAW BMM 52-10-03 AND COMPLIED WITH SB 52-3094, OPS CHECKS GOOD.

Part: SPAR — DAMAGED (LT WING) · airframe 30,447 hrs · 38,702 cycles

MAJOR REPAIR UPON SUBSEQUENT INSPECTION MAINTENANCE FOUND LEFT FORWARD SPAR AFT LOWER FLANGE FOUND TO HAVE BEEN DAMAGED BY LEFT DRAG BRACE NEXT TO UPLOCK BRACKET IN LEFT WHEEL WELL. DAMAGE AT BL 107.0 TO 99.0 AND 104.5 TO 101.5 DELAMINATION IS APPROX 8 " LONG AND 3" OF SPAR IS MISSING. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-57-006. MATERIALS UTILIZED ARE INCLUDED IN THE EO.

Part: ARM — FAILED (LT MLG) · airframe 30,448 hrs · 38,701 cycles

SIG EVENT - UPON LANDING IN "DEN" THE LEFT HAND MAIN LANDING GEAR COLLAPSED CAUSING SIGNIFICANT DAMAGE TO THE LEFT MAIN LANDING GEAR AND ASSOCIATED SPAR AREA. IT HAS BEEN ISOLATED AT THIS TIME TO A FAILURE OF THE UPPER DRAG BRACE "A" ARM ASSEMBLY LUGS WHICH BROKE CAUSING THE GEAR TO PARTIALLY COLLAPSE. MX REPLACED THE LT DRAG BRACE ASSY IAW TC 1900-3210.02, OPS CHECK OK.

Part: SWITCH — DETERIORATED (AUTOFEATHER SYS) · airframe 30,255 hrs · 38,483 cycles

PILOTS REPORTED THAT THE RIGHT AUTOFEATHER CYCLED DURING LANDING. MAINTENANCE REMOVED AND REPLACED THE LEFT PRESSURE SWITCH. THE OPERATIONAL CHECK WAS GOOD IAW BMM 61-21-01. P/N ON AND OFF 50-389121-47. S/N OFF 0112.

Part: SWITCH — MALFUNCTIONED (AUTOFEATHER SYS) · airframe 30,255 hrs · 38,483 cycles

PILOTS REPORTED THAT THE AUTOFEATHER SEQUENCE CYCLED MULTIPLE TIMES DURING LANDING FLARE. MAINTENANCE ADJUSTED THE RIGHT AUTOFEATHER ARMING SWITCH IN THE PEDESTAL IAW BMM 61-21-02. OPERATIONAL CHECK WAS GOOD.

Part: SPAR — DAMAGED (ZONE 500) · airframe 29,267 hrs · 37,310 cycles

DURING ROUTINE SCHEDULED MX, DISCOVERED 2 LOCK FASTENER HOLES MISDRILLED (HOLES ARE STEPPED) AT/ON THE LT WING, AFT WING SPAR ON THE FWD SIDE OF THE SPAR AT WS 127.288 AND 129.588. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIONS I.A.W. E.O. 09-1900-57-006. MATERIALS UTILIZED FOR THE REPAIR ARE INCLUDED IN THE ENGINEERING ORDER.

Part: SPAR — DAMAGED (ZONE 500) · airframe 29,267 hrs · 37,310 cycles

DURING ROUTINE SCHEDULED MAINTENANCE AFTER REMOVAL OF A FASTENER, PART OF AN EXISTING RIVET WAS IN THE HOLE UPON REMOVING THE RIVET THE DIAMETER OF THE HOLE WAS FOUND TO BE APPROXIMATELY .230" ACROSS AT LEFT HAND WING SPAR W.S. 114.250. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIONS I.A.W. E.O. 09-1900-57-006. MATERIALS UTILIZED FOR THE REPAIR ARE INCLUDED IN THE ENGINEERING ORDER.

Part: SPAR — DAMAGED (ZONE 500) · airframe 29,267 hrs · 37,310 cycles

DURING ROUTINE SCHEDULED MAINTENANCE AFTER REMOVAL OF A FASTENER, A HOLE WAS FOUND TO BE STEPPED AND OVERSIZED AT THE LEFT HAND WING SPAR W.S. 104.0. APPROXIMATE DIAMETER OF .230". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIONS I.A.W. E.O. 09-1900-57-006. MATERIALS UTILIZED FOR THE REPAIR ARE INCLUDED IN THE ENGINEERING ORDER.

Part: SPAR — DAMAGED (LT WING) · airframe 29,267 hrs · 37,310 cycles

DURING ROUTINE SCHEDULED MX, A STEPPED LOCK FASTENER WAS FOUND IN THE LT WING SPAR AT WS 124.588. DEPTH OF THE STEP IS APPROX .150" DEEP. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIONS I.A.W. E.O. 09-1900-57-006. MATERIALS UTILIZED FOR THE REPAIR ARE INCLUDED IN THE ENGINEERING ORDER.

Part: ANGLE — CRACKED (ZONE 100) · airframe 29,267 hrs · 37,310 cycles

DURING ROUTINE SCHEDULED MAINTENANCE A RIGHT HAND HEAVY ANGLE WAS FOUND CRACKED IN THE RADIUS AT F.S. 303.25. CRACK LENGTH APPROXIMATELY 2" LONG EXTENDING 1" FORWARD AND OF AFT OF F.S. 303.25. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIONS I.A.W. E.O. 09-0900-53-028. MATERIALS UTILIZED FOR THE REPAIR ARE INCLUDED IN THE ENGINEERING ORDER.

Part: LATCH — OUT OF RIG (EMERGENCY EXIT) · airframe 28,816 hrs · 36,731 cycles

PILOTS REPORTED THAT THE 6C EMERGENCY EXIT HANDLE APPEARED TO BE UNLOCKED FROM THE OUTSIDE. MX RIGGED THE 6C DOOR LATCH AND OPS CHECKED GOOD.

Part: HANDLE — LOOSE (EMERGENCY EXIT) · airframe 28,811 hrs · 36,364 cycles

DURING ROUTINE WALK AROUND PILOTS REPORTED THAT LT OVERWING EXIT HANDLE APPEARED TO BE UNSECURED. MX ENSURED THAT LATCH WAS SECURED MM 52-20-00. SUBSEQUENT INSP BY PILOTS RESULTED IN OBSERVANCE THAT HANDLE BECAME UNSECURED SPONTANEOUSLY. MX REMOVED AND INSP 6A EXIT DOOR AND RIGGED DOOR BY MEANS OF LOLLIPOP CONNECTING INTERNAL AND EXTERNAL HANDLE. PERFORMED OPS CHECK WHICH WAS GOOD MM 52-20-00/01.

Part: TACH GENERATOR — DETERIORATED (PROPELLER) · airframe 28,594 hrs · 36,429 cycles

ABORTED TAKEOFF, PILOTS REPORTED THAT AT TAKEOFF POWER THE PROPELLER RPM ON THE LT SIDE EXCEEDED 2000 RPM AND THE TAKEOFF WAS ABORTED. MX REMOVED AND REPLACED NR 1 PROPELLER TACH GENERATOR IAW 67D MM 70-00-00. OPS AND LEAK CHECKS WERE GOOD IAW MM 77-10-00.

Part: INDICATOR — MALFUNCTIONED (NR 2 TORQUE) · airframe 28,389 hrs · 36,180 cycles

NR 2 TORQUE GAUGE DROPPED TO 0 ON TAKEOFF ROLL. THE NR 2 TORQUE GAUGE DROPPED TO ZERO. MX REMOVED AND REPLACED THE NR 2 TORQUE GAUGE IAW MM 31-10-00. OPS CHECK WAS GOOD.

Part: KEEL — CRACKED (FUSELAGE) · airframe 27,837 hrs · 35,465 cycles

MAJOR REPAIR - DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND ON THE LEFT INBOARD KEEL. MAINTENANCE REPAIRED THE LEFT HAND INBOARD KEEL AT FS 321 IAW ENGINEERING ORDER 09-195-01.

Part: ANGLE — CRACKED (BS 288)

LT HEAVY ANGLE CRACKED APPROX 1.125 INCH IN LENGTH AT FORWARD BEND RADIUS AT FS 288.0. REPAIRED LT HEAVY ANGLE AT FS 288 IAW SRM 53.90. REPAIR AREA APPROX 13.125 INCH LONG. RII INSPECTION CP,[;OED WOTJ OAW TASKCARD NR 8.2.1. (K)

Part: SKIN — MISREPAIRED (BS 126-131) · airframe 23,747 hrs · 30,181 cycles

UPON ROUTINE INSPECTIONS MAINTENANCE FOUND THAT A REPAIR MUST CONFORM WITH SRM TECHNICAL DATA SPECIFICATIONS AT FS 126 TO FS 131.3 STRINGER 3R TO APPROXIMATELY 3 INCHES IB OF STRINGER 2R ABOVE PILOTS WINDSHIELD. MAINTENANCE REPAIRED THE AFFECTED AREA AT FS 177.3 RT STRINGER 9AL RELIEF HOLE PER BEECH 1900D SRM 51-70 AND TC 8.2.1.

Part: STRINGER — CRACKED (BS 163) · airframe 23,747 hrs · 30,181 cycles

UPON ROUTINE INSPECTIONS MAINTENANCE FOUND A STRINGER RELIEF HOLE CRACKED AT FS 163.9 RT STRINGER 9AL. MAINTENANCE REPAIRED THE AFFECTED AREA AT FS 163.9 RT STRINGER 9AL RELIEF HOLE IAW SRM 51-70 AND TC 8.2.1.

Part: STRINGER — CRACKED (BS 177) · airframe 23,747 hrs · 30,181 cycles

UPON ROUTINE INSPECTIONS, MAINTENANCE FOUND A STRINGER RELIEF HOLE CRACKED AT FS 177.3 RT STRINGER 9AL. MAINTENANCE REPAIRED THE AFFECTED AREA AT FS 177.3 RT STRINGER 9AL RELIEF HOLE IAW SRM 51-70 AND TC 8.2.1.

Part: SKIN — CRACKED (BS 298) · airframe 23,747 hrs · 30,181 cycles

UPON ROUTINE INSPECTION MAINTENANCE FOUND THE BELLY SKIN CRACKED AT APPROXIMATELY F.S. 298.0, B.L. 27.0. MAINTENANCE REPAIRED BELLY SKIN AT APPROXIMATELY F.S.298.0 B.L. 27.0 PER BEECH SRM 51-70. RII INSPECTION COMPLIED WITH PER TC 8.2.1.

Part: SKIN — CORRODED (BS 228) · airframe 23,747 hrs · 30,181 cycles

UPON ROUTINE MAINTENANCE, EVIDENCE OF CORROSION WAS FOUND ON THE BELLY OF THE AIRCRAFT AT APPROXIMATELY FS 228.25, 1.5 INCHES ON RT SIDE OF STRINGER 16.

Part: SKIN — CORRODED (BS 228) · airframe 23,747 hrs · 30,181 cycles

MAJOR REPAIR - UPON ROUTINE MAINTENANCE, EVIDENCE OF CORROSION WAS FOUND ON THE BELLY OF THE AIRCRAFT AT APPROXIMATELY FS 228.25, 1.5 INCHES ON RT SIDE OF STRINGER 16. MAINTENANCE REPAIRED THE BELLY SKIN FROM APPROXIMATELY F.S. 228.25 ON RIGHT HAND SIDE OF STRINGER 16 I.A.W. BEECH 1900D SRM 51-70. RII INSPECTION COMPLIED WITH PER TC 8.2.1.

Part: ANGLE — CRACKED (AIRSTAIR) · airframe 23,747 hrs · 30,181 cycles

UPON ROUTINE INSPECTION MAINTENANCE FOUND AN AIRSTAIR DOOR ENTRANCE ANGLE CRACKED AT FS 150.6 AND RT STRINGER 9AL. MAINTENANCE AIRSTAIR DOOR ENTRANCE ANGLE IAW BEECH 1900D SRM 53-90. RII INSPECTION COMPLIED WITH PER TC 8.2.1.

Part: SKIN — DELAMINATED (PAX DOOR) · airframe 23,747 hrs · 30,181 cycles

MAJOR REPAIR - UPON ROUTINE INSPECTION MAINTENANCE FOUND A DELAMINATION ON THE AIRSTAIR DOOR SKIN BELOW THE EXTERIOR DOOR HANDLE. MAINTENANCE REPAIRED AIRSTAIR DOOR SKIN IAW BEECH 1900D SRM 52-10. RII COMPLIED WITH PER TC 8.2.1.

Part: SMOKE — DETECTED (COCKPIT) · airframe 21,757 hrs · 27,770 cycles

SMOKE REPORTED IN COCKPIT, PERFORMED HIGH POWER ENGINE RUN UP WITH ELECTRICAL SYSTEMS ENERGIZED, NO FAULTS FOUND.

Part: TUBE — FAILED (BLEED AIR) · airframe 17,725 hrs · 23,184 cycles

LT BLEED AIR FAILED, REMOVED AND REPLACED BLEED TUBE PN 129-910033-15.

Part: TUBE — FAILED (LT BLEED) · airframe 17,725 hrs · 23,183 cycles

LT BLEED FAIL, REPAIRED EVA TUBING PN 131823E6M02060.

Part: RADOME — BIRD STRIKE (NOSE) · airframe 17,691 hrs · 23,144 cycles

BIRD STRIKE, DAMAGED RT I/B WING, RT O/B WING AND RADOME. REPLACED LT INBD LEADING EDGE PN 114-120028-23

Part: TRANSMITTER — MALFUNCTIONED (ENGINE TORQUE) · airframe 17,487 hrs · 22,821 cycles

NR 1 ENG WILL NOT MAKE TAKE OFF POWER, R&R NR 1 TORQUE TRANSMITTER

Part: INDICATOR — FAILED (TORQUE) · airframe 17,487 hrs · 22,821 cycles

NR 1 TORQUE GAUGE QUIT AFTER TAKEOFF, REMOVED AND REPLACED TORQUE INDICATOR.

Part: CONTROLLER — MALFUNCTIONED (ENVIRO SYS) · airframe 17,157 hrs · 22,412 cycles

RIGHT ENVIRO FAIL ANNUNCIATOR ILLUMINATED. REMOVED AND REPLACED A317 PCB, OPS CHECK GOOD.

Part: TRANSMITTER — FAILED (FUEL FLOWMETER) · airframe 16,851 hrs · 22,084 cycles

RT FUEL FLOW INDICATOR SHOWS ZERO INOP, R&R RT FUEL FLOW TRANSMITTER

Part: SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 16,730 hrs · 21,954 cycles

CARGO DOOR ANNUN ILLUM IN FLIGHT. ADJUSTED CARGO DOOR DOORSILL SWITCH.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 16,650 hrs · 21,868 cycles

CARGO DOOR ANNUN ILLUMINATED. ADJUSTED DOOR JAMB SWITCH, OPS CHECK GOOD.

Part: WINDSHIELD · airframe 16,547 hrs · 21,761 cycles

#1 WINDSHIELD CRACKED, REPLACED #1 WINDSHIELD

Part: GAS GENERATOR — SEIZED (LT ENGINE) · airframe 15,615 hrs · 20,775 cycles

LEFT ENGINE FAILED ON TAKE OFF, R&R GAS GENERATOR AND POWER SECTION.

Part: TUBE — DAMAGED (BLEED AIR) · airframe 150,972 hrs · 20,224 cycles

LEFT BLEED AIR FAIL ANNUNCIATION ILLUMINATED. REPAIRED EVA TUBING, OPS CHECKED SATISFACTORY.

Part: BYPASS VALVE — LEAKING (A/C BAY) · airframe 14,957 hrs · 20,063 cycles

LEFT ENVIRONMENTAL FAIL. REPLACED BYPASS VALVE.

Part: SWITCH — MALFUNCTIONED (LANDING GEAR) · airframe 14,205 hrs · 19,221 cycles

LANDING GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH. REPLACED UPLOCK SWITCH, OPS CHECKED SYSTEM SATISFACTORY.

Part: PUMP — FAILED (LT ENGINE) · airframe 14,080 hrs · 19,084 cycles

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

Part: FUEL CAP — LEAKING (RIGHT O/B WING) · airframe 14,055 hrs · 19,057 cycles

LEFT O/B FUEL CAP LEAKING, REPLACED FUEL CAP

Part: ALTIMETER — INACCURATE (CAPTAINS) · airframe 13,516 hrs · 18,469 cycles

400 FOOT SPLIT CAPTAINS ALTIMETER, REPLACED OPS CHECKED SYSTEM SATISFACTORY

Part: CIRCUIT BOARD — INTERMITTENT (A119) · airframe 13,163 hrs · 18,088 cycles

WARNIG HORN AND INTRANSIT LIGHT WITH GEAR RETRACTED, REPLACED PCB OPS CHECKED SATISFACTORY

Part: WHEEL — BLOWN (#3) · airframe 13,025 hrs · 17,943 cycles

RIGHT MAIN GEAR SMOKING AFTER LANDING, REPLACED #3 WHEEL ASSEMBLY OPS CHECKED SYSTEM SATISFACTORY

Part: PROBE — FAILED (LT ENGINE) · airframe 12,931 hrs · 17,851 cycles

LEFT ENGINE OVERTEMP ON T/O. REPLACED TRIM PROBE.

Part: CIRCUIT BOARD — FAULTY (COCKPIT) · airframe 12,762 hrs · 17,681 cycles

GEAR WARNING HORN WHEN GEAR IS RETRACTED. REPLACED RELAY BOARD.

Part: WIRE — LOOSE (LT ENGINE) · airframe 12,650 hrs · 17,564 cycles

LT ITT ABOVE 780 DEG IN CLIMB WITH TQ SET AT 2200 LBS (ANTI-ICE ON). RETURNED TO BLOCK. FOUND WIRE LOOSE ON ITT PROBE. PERFORMED MAINTENANCE, OPS CHECKED GOOD.

Part: DOOR — OPEN (SERVICE DOOR) · airframe 12,517 hrs · 17,425 cycles

RIGHT OIL SERVICE DOOR OPENED DURING CLIMBOUT. RESECURED DOOR, OPS CHECKED GOOD.

Part: WARNING LIGHT — MALFUNCTIONED (COCKPIT) · airframe 12,245 hrs · 17,138 cycles

NOSE GEAR LIGHTS TOOK TWO CYCLES TO ILLUMINATE. INSPECTED GEAR SYSTEM CND.

Part: WIRE — LOOSE (COCKPIT) · airframe 12,076 hrs · 16,963 cycles

RETURN TO BLOCK - LEFT GENERATOR FELL OFF LINE. INSPECTED FOUND LOOSE WIRES ON DC PWR PANEL. OPS CHECKED GOOD.

Part: STARTER GEN — FAILED (LT ENGINE) · airframe 12,049 hrs · 16,941 cycles

LEFT DC GENERATOR ANNUCIATOR ILLUMINATED INFLIGHT WOULD NOT RESET. REPLACED STARTER-GEN, OPS CHECKED GOOD.

Part: OXYGEN MASK — DEPLOYED (CABIN) · airframe 12,049 hrs · 16,941 cycles

PASSENGER O2 MASK DEPLOYED INFLIGHT. RESECURED MASK, OPS CHECKED SYSTEM GOOD.

Part: SWITCH — INOPERATIVE (NLG ACTUATOR) · airframe 11,866 hrs · 16,745 cycles

NOSE GEAR ANNUNCIATOR DID NOT ILLUMINATE WITH GEAR SELECT DOWN. INSPECTED FOUND FAULTY ACTUATOR SWITCH. REMOVED AND REPLACED ACTUATOR, OPS CHECKED SYSTEM GOOD.

Part: CIRCUIT BOARD — INOPERATIVE (CABIN PRESSURE)

IN CRUISE FLIGHT CREW REPORTED DUAL ENVIRONMENTAL FAIL INDICATION. PRESSURIZATION SYSTEM FAILED. FOUND ENVIRONMENTAL SYSTEM PRINTED CIRCUIT BOARD INOPERATIVE. REPLACED CIRCUIT BOARD. OPERATIONAL CHECK GOOD. (M)

Part: ALTIMETER — FAILED (LT COCKPIT)

CAPTAIN'S ALTIMETER FLAGGED DURING DESCENT. REMOVED AND REPLACED ALTIMETER. SYSTEM TESTS SATISFACTORY. SUBSEQUENT BENCH TESTS WERE UNABLE TO CONFIRM PROBLEM. THIS WAS THE THIRD SUCH FAILURE OF THIS INSTRUMENT IN THE PAST 9 MONTHS (714 HOURS) OF OPERATION. P/N KEA-346/066-03062-0008.