N210GL

Part: CHECK VALVE — LEAKING (FUEL SYSTEM) · airframe 37,766 hrs · 45,788 cycles

SIG EVENT, PILOT REPORTED THAT THERE WAS A STRONG SMELL OF FUEL IN CABIN. REMOVED FLOORBOARDS & INSPECTED FUEL TRANSFER LINES, PRESSURIZED & LEAK CHECKED FUEL LINES, NO DISCREPANCIES NOTED. INOPERATIVE LT & RT ENG ACCESSORIES FOR FUEL LEAKS, NO LEAKS NOTED ATT. STARTED ENGS & PERFORMED CHECKS, NO FUEL SMELL IN THE BLEED AIR, SHUTDOWN ENGS & INSPECTED LT & RT FUEL NOZZLES & FLOW DIVIDERS FOR FUEL LEAKS, NO LEAKS NOTED. INSPECTED LT & RT PURGE CANS FUEL CHECK VLVS, ONE OF THE LT ENG PURGE CAN CHECK VLVS NOT HOLDING. R & R CHECK VLV, CLEANED CABIN SEATS, SEAT BACKS & ARM RESTS. ALSO AERATED & DEODORIZED CABIN CARPETS, RETURNED ACFT TO AIRWORTHY CONDITION, NO MORE FUEL SMELL NOTED ATT.

Part: MOTOR — FAULTY (TE FLAP) · airframe 36,391 hrs · 44,306 cycles

PILOT REPORTED THAT THERE WAS A STRONG BURNING SMELL COMING FROM THE CABIN & IS IRRITATING TO TO EYES. TROUBLESHOT BURNING SMELL COMING FROM FLAP GEAR BOX MOTOR ASSEMBLY. R & R FLAP GEAR BOX MOTOR ASSEMBLY PN 100-524073-1 SN OFF 5693, IAW BMM 27-50-03 OPERATIONS CHECKED GOOD.

Part: MOTOR — FAULTY (TE FLAP) · airframe 36,365 hrs · 44,276 cycles

PILOT REPORTED THAT WHEN THEY WENT TO EXTEND THE FLAPS HAD A STRONG ELECTRICAL SMELL & THE FLAPS DID NOT EXTEND. MAINTENANCE R&R FLAP GEAR BOX MOTOR P/N 100-524073-1 S/N OFF 6137 S/N ON. 5693 OPS CHECK GOOD AT THIS TIME REF 1900DMM 27-50-03.

Part: SKIN — CRACKED (BS 288) · airframe 35,720 hrs · 43,552 cycles

DURING A SCHEDULED INSPECTION, FOUND THE LT LOWER BELLY SKIN AT FS 288 CRACKED, 1.75" IN LENGTH. REPAIRED IAW EO 13-1900-53-059. MAJOR REPAIR.

Part: FIRE LOOP — CHAFED · airframe 35,691 hrs · 43,522 cycles

SIG EVENT - PILOT REPORTED THAT THE RT FIREWALL FUEL VALVE T-HANDLE FLICKERED ON AND OFF IN FLIGHT. MX TESTED FIRE LOOP ON RT SIDE, TESTED NORMAL. INSPECTED FWD AND AFT LOOP FOUND CHAFE ON TOP SIDE OF FWD LOOP. R & R LOOP IAW BMM 26-10-01. OPS CHECK GOOD AT THIS TIME PN 244-12886.

Part: PRESSURE BLKHD — CRACKED (BS 84) · airframe 35,174 hrs · 42,962 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND 7 CRACKS IN THE FWD PRESSURE BULKHEAD, LT WEB AT FS 84.00, CRACKS AT INBD EDGE OF WEB ATTACHING FASTENERS, 3.5" IN LENGTH. REPAIRED IAW EO 13-1900-53-044. MAJOR REPAIR.

Part: PRESSURE BLKHD — CRACKED (BS 84) · airframe 35,174 hrs · 42,962 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND 4 CRACKS IN THE FWD PRESSURE BULKHEAD, RT WEB AT FS 84.00, CRACKS AT THE INBD EDGE OF WEB ATTACHING FASTENERS, 2" IN LENGTH. REPAIRED IAW EO 13-1900-53-044. MAJOR REPAIR.

Part: FRAME — CRACKED (BS 509) · airframe 35,174 hrs · 42,962 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 CRACKS AT THE CARGO DOOR FUSELAGE FRAME AT FS 509 BETWEEN STRINGER 4L & 5L, LOCATED IN THE BEND RADIUS OF THE FRAME, 1" IN LENGTH. REPAIRED IAW EO 13-1900-53-042. MAJOR REPAIR.

Part: FRAME — CRACKED (BS 177) · airframe 35,174 hrs · 42,962 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FUSELAGE FRAME AT FS 177.35 IN THE BEND RADIUS, 1" LENGTH. REPAIRED IAW EO 13-1900-53-043. MAJOR REPAIR.

Part: STRUCTURE — CRACKED (HORIZONTAL STAB) · airframe 34,858 hrs · 42,599 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE TEE SECTION OF THE LT HORIZONTAL STAB LOWER AT HSS 5.000 AND 10.5 PERCENT AT A SCREW HOLE, .5" IN LENGTH. REPAIRED IAW EO 13-1900-55-011. MAJOR REPAIR.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 34,856 hrs · 42,598 cycles

DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK EXTENDING FROM A SCREW HOLE ON THE TOP SIDE OF THE LT HORIZONTAL STAB AT HSS 5.000 AND 10.5 PERCENT CHORD, ON THE FLANGE FOR PANEL 332 BTC ON THE FORWARD LT CORNER, .25" IN LENGTH. REPAIRED IAW EO 13-1900-55-009. MAJOR REPAIR.

Part: STRUCTURE — CRACKED (HORIZONTAL STAB) · airframe 34,856 hrs · 42,598 cycles

DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE RT HORIZONTAL STAB LOWER TEE SECTION AT HSS 5.000 AND 10.5 PERCENT CHORD, 1.5" IN LENGTH. REPAIRED IAW EO 13-1900-55-010. MAJOR REPAIR.

Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 34,135 hrs · 41,734 cycles

DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT FWD SPAR CAP ANGLE, RADIATES FROM THE UPPER FWD TASTENER UPWARD TO EDGE OF SPAR CAP, .375" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW FR-CO-02586, STEP 1. MAJOR REPAIR

Part: SKIN — BURNED (LT ELEVATOR) · airframe 33,525 hrs · 40,989 cycles

.5 X .5 INCH BURN HOLE IN TOP AND BOTTOM SKIN, 3.8750" CENTER FROM OTBD TIP OF LT ELEVATOR T/E. REPAIRED THE AFFECTED AREA IAW EO 12-1900-27-002.

Part: SKIN — DAMAGED (BS 288-327) · airframe 32,528 hrs · 39,837 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND THE RT FUSELAGE FS 288 HAS ELONGATED HOLES FROM ATTACHING FAIRING PANEL TO FS 327. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-019. MATERIALS UTILIZED ARE INCLUDED IN THE EO. MAJOR REPAIR

Part: FAIRING — DAMAGED (FUSELAGE) · airframe 32,528 hrs · 39,837 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND A HOLE IN THE FUSELAGE FARING, RT SIDE UNDER AFT WING, AFT OF FS 363.250, 2.25 INCHES JUST ABOVE STRINGER 1R, .687 BY .25. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-018. MATERIALS UTILIZED ARE INCLUDED IN THE EO. MAJOR REPAIR

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 32,528 hrs · 39,839 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. ED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-55-008. MATERIALS UTILIZED ARE INCLUDED IN THE EO.

Part: ATTACH FITTING — CRACKED (CARGO DOOR) · airframe 32,528 hrs · 39,837 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AT THE NUTPLATE, FWD CARGO DOOR SNUBBER FUSELAGE ATTACH POINT, UPPER IB NUTPLATE FS 456, .35" IN LENGTH. REPAIRED IAW EO 12-1900-53-014. MAJOR REPAIR

Part: SKIN — CHAFED (FUSELAGE) · airframe 32,528 hrs · 39,837 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 RIVET HEADS CHAFING ON A PREVIOUS REPAIR OF THE LOWER RT WING WHERE THE FUSELAGE MEETS THE WING. REPAIRED IAW EO 12-1900-53-014. MAJOR REPAIR.

Part: FRAME — CRACKED · airframe 32,528 hrs · 39,837 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FRAME AT FS 150.6 BETWEEN STRINGERS 2R AND 3R, .9" IN LENGTH. REPAIRED IAW EO 12-1900-53-016. MAJOR REPAIR

Part: DOUBLER — CRACKED (BS 288) · airframe 32,528 hrs · 39,837 cycles

MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RT DOUBLER, FWD END, FS 288, 1.2" IN LENGTH. REPAIRED IAW EO 12-1900-53-017.

Part: SKIN — CRACKED (BS 303.25) · airframe 32,528 hrs · 39,837 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FUSELAGE SKIN, LT BELLY AT FS 303.25 WHERE THE FUSELAGE MEETS THE WING, 5" IN LENGTH. REPAIRED IAW EO 12-1900-53-015. MAJOR REPAIR

Part: WARNING LIGHT — FALSE ACTIVATION (MLG) · airframe 32,365 hrs · 39,655 cycles

PILOT REPORTED THAT THE GEAR INTRANSIT LIGHT ILLUMINATED IN FLIGHT, RAN CHECKLIST, GEAR OPERATED NORMALLY TO THE EXTENDED POSITION, EMERGENCY DECLARED, LANDED SAFELY. MX COULD NOT DUPLICATE, REPLACED THE NLG UPLOCK SWITCH IAW TC 1900-3260.00, OPS CHECKED GOOD.

Part: CIRCUIT BOARD — DAMAGED (MLG) · airframe 32,322 hrs · 39,599 cycles

PILOT REPORTED THAT THE LANDING GEAR DID NOT EXTEND WHEN SELECTED AND RELAY CIRCUIT BREAKER TRIPPED, MANUALLY EXTENDED GEAR, NO IN-TRANSIT LIGHTS, LANDED SAFELY. MX REPLACED THE PCB A116 AND THE LANDING GEAR RELAY, OPS CK GOOD.

Part: ACTUATOR — INOPERATIVE (LT MLG) · airframe 31,918 hrs · 39,125 cycles

PILOT REPORTED THAT THE LEFT GEAR INDICATION DID NOT SHOW DOWN AND LOCKED UNTIL APPROX 25 SECONDS AFTER THE HANGLE WAS PLACED IN THE DOWN POSITION. MX REPLACED THE LT MLG ACTUATOR IAW TC 1900-3230.10, PN: 114-300041-15, SN: 0561A, OPS CK GOOD.

Part: SOLENOID — DIRTY (PROPELLER PITCH) · airframe 31,867 hrs · 39,067 cycles

PILOT REPORTED THAT THE ACFT YAWED TO THE LT IN THE LANDING FLARE. MX CLEANED THE LOW PITCH SOLENOID, OPS CHECKED GOOD.

Part: WIRE — CHAFED (PAX DOOR) · airframe 31,248 hrs · 38,330 cycles

PILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR REMAINS EXTINGUISHED WHEN THE DOOR IS OPENED UP UNTIL ABOUT A FOOT OPEN. MX INSPECTED WIRE AT AIRSTAIR DOOR FOUND 4 CHAFED WIRES, REPAIRED WIRE. PERFORMED CABIN DOOR AM LIGHTING SYS CK, OPS CK GOOD REF CHAP 14, SECT 14.3.0 & REF 52-70-00.

Part: SWITCH — INOPERATIVE (ANNUNCIATOR) · airframe 31,211 hrs · 38,286 cycles

PILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR GOES OUT WITHOUT LOCKING THE DOOR. MX CLEANED THE MICRO SWITCHES, OPS CK GOOD.

Part: SWITCH — INOPERATIVE (ANNUNCIATOR) · airframe 31,207 hrs · 38,280 cycles

PILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR WENT OUT BEFORE THE DOOR WAS LOCKED. MX CLEANED THE CABIN DOOR MICRO SWITCH REF AIM 14.3.0, OK FOR SERVICE.

Part: ACTUATOR — INOPERATIVE (MLG) · airframe 31,174 hrs · 38,239 cycles

PILOT REPORTED THAT THE LT MLG BOTH GREEN "L" AND "H" ANNUNCIATORS FLICKERED THEN EXTINGUISHED THEN REILLUMINATED, NO UNSAFE INDICATIONS ON APPROACH & LANDING. MX REPLACED THE LT MLG ACTUATOR, OPS AND RIG CKS IAW TC. 1900-3230.10.

Part: SWITCH — OUT OF RIG (MLG) · airframe 31,068 hrs · 38,113 cycles

PILOT REPORTED THAT UPON RAISING THE LANDING GEAR WHILE FLAPS AT 17 DEGREES. TAKEOFF GEAR WARNING HORN SOUNDED AND COULD NOT BE SILENCED. IN TRANSIT LIGHT REMAINED ILLUMINATED UNTIL FLAPS 0 DEGREES WAS OBTAINED. MX RIGGED LANDING GEAR WARNING HORN FLAP POSITION SWITCH IAW MM 27-50-07.

Part: SWITCH — STUCK (CABIN DOOR) · airframe 30,912 hrs · 37,931 cycles

PILOT REPORTED THAT WITH THE CABIN DOOR OPEN THE CABIN ANNC DID NOT ILLUMINATE. MX CLEANED THE MICRO SWITCH, SYS OPS CK GOOD.

Part: KEELBEAM — GOUGED (FUSELAGE) · airframe 30,912 hrs · 37,931 cycles

MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, MX FOUND A GOUGE IN THE RT OTBD KEEL BY A CLAMP ON THE RETRACT/EXTEND LINE FOR THE LT MLG ACTUATOR. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-57-006. MATERIALS UTILIZED ARE INCLUDED IN THE EO.

Part: KEELBEAM — GOUGED (FUSELAGE) · airframe 30,912 hrs · 37,931 cycles

MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, MX FOUND A GOUGE IN THE LT OTBD KEEL BY A CLAMP ON THE RETRACT/EXTEND LINE FOR THE LT MLG ACTUATOR. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-57-005. MATERIALS UTILIZED ARE INCLUDED IN THE EO.

Part: BLEED AIR SYS — INOPERATIVE (LEFT) · airframe 29,946 hrs · 36,782 cycles

CLIMBING THROUGH 20,000 FT COULDN'T GET CABIN TO QUIT CLIMBING, HAD TO DEPLOY MASKS & RETURN TO DEPARTURE, DIR STUCK AT 3.4 PSI WOULD NOT GO HIGHER. STOWED & RELOCKED MASKS IAW MM 35-20-01. RAN ENG & PRESSURIZED - NO AIR FROM LT BLEED, REMOVED ORIFICE PLATE FROM BLEED AIR DUCT, RAN ENGINES PER TC 1900-7100.10, SYS OPS CK GOOD IAW BMM 21-30-00.

Part: FUEL SYS — LEAKING (RT NACELLE) · airframe 29,321 hrs · 36,066 cycles

OVERWHELMING ODORS OF JET FUEL PRESENT IN CABIN COCKPIT EXTREMELY BAD TO A POINT OF BEING NAUSEATING AND AFFECTING SAFETY SLOW DRIP UNDER RT NACELLE DIFFERENT AREA THAN REPAIR.

Part: FASTENER — LOOSE (RT WING)

SIG EVENT - PILOT REPORTED THAT AN OVERWHELMING ODOR OF FUEL ENTER THE CABIN AND COCKPIT. MAINTENANCE FOUND LOOSE FASTENERS JUST OUTBOARD OF RT NACELLE AT FORWARD SPAR, REPLACED FASTENERS AND SEALED AREA, REFUELED, NO LEAKS OR ODOR PRESENT IAW SRM 51-10-00, CHECKS GOOD PER BMM 28-10-00 (1)(A).

Part: BULKHEAD — BUCKLED (BS 531) · airframe 29,236 hrs · 35,956 cycles

MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A BULKHEAD AT FS 531 AFT CARGO FLOORBOARD FORWARD SUPPORT BUCKLED ABOUT 11/32" AT TOP, TOTAL DAMAGE AREA ABOUT 26" IN LENGTH, AND A .5" CRACK IN THE RADIUS 12" FROM RT SIDE. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-047. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.

Part: BULKHEAD — CRACKED (BS 531) · airframe 29,236 hrs · 35,956 cycles

DURING A SCHEDULED ROUTINE INSPECTION A CRACK WAS FOUND AT THE AFT CARGO BAY FLOORBOARD FORWARD SUPPORT BULKHEAD AT F.S. 531.0 LH SIDE WHERE IT ATTACHES TO THE FRAME, 13/16" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-048. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER. MAJOR REPAIR.

Part: SKIN — CRACKED (EMERGENCY EXIT) · airframe 29,236 hrs · 35,956 cycles

MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK IN THE SKIN WAS FOUND ON THE EMERGENCY EXIT DOOR 6A, LOWER FORWARD CORNER, 2" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-52-003. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.

Part: FRAME — CRACKED (BS 456 S10R) · airframe 29,236 hrs · 35,956 cycles

MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, A2 CRACKS WAS FOUND IN THE FRAME AT FS 456 AND STRINGER 10R CUTOUT, .45" AND .5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-046. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.

Part: FRAME — CRACKED (BS 303) · airframe 29,236 hrs · 35,956 cycles

DURING A SCHEDULED ROUNTINE INSP A CRACK WAS FOUND IN THE FRAME ANGLE AT FS 303, .5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-045. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.

Part: SKIN — PUNCTURED (PAX DOOR)

COMPONENT MAJOR REPAIR - UPON RECEIVING A SERVICEABLE AIRSTAIR DOOR THAT WAS PURCHASED, IT WAS DETERMINED THAT IT REQUIRED A MAJOR REPAIR ON THE EXTERIOR DOOR SKIN DUE TO 3 SCRATCHES AND 1 PUNCTURE THROUGH THE SKIN. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-52-002. MATERIALS UTILIZED ARE INCLUDED IN THE EO.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 27,369 hrs · 33,712 cycles

PILOTS REPORTED THAT A STRONG FUEL ODOR FROM THE VENTS IN THE FLIGHT DECK AND CABIN WAS PRESENT. MAINTENANCE INSPECTED THE NR 1 AND 2 ENGINES FOR LEAKS OF WHICH NONE WERE FOUND AND SUBSEQUENTLY PERFORMED INDIVIDUAL ENGINE RUNS WITH NO FUEL ODORS NOTED. REFERENCE MM 71-10-00. AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — CORRODED (ENTRY DOOR) · airframe 26,557 hrs · 32,636 cycles

MAJOR REPAIR - AIRSTAIR DOOR WAS FOUND CORRODED ON LOWER END CLOSURE AREA. MAINTENANCE REMOVED A SECTION OF THE LOWER INNER DOOR PAN, CLEANED CORROSIONFROM INNER MATERIAL, INTALLED NEW LOWERE DOOR PAN AND INSTALLED THE HINGE ASSEMBLY IAW EO 09-1900-52-001.

Part: PRESSURE SWITCH — WORN (NR 2 ENGINE) · airframe 26,725 hrs · 32,854 cycles

ON APPROACH AT 500 LBS TORQUE, WHILE LEVELING ALTITUDE AND ADVANCING POWER THE R/H ENGINE ATTEMPTED FEATHER CAUSING CYCLES SIMILAR TO AUTOFEATHER TEST. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND AUTOFEATHER LOW PRESSURE SWITCH AND COMPLIED WITH FCD 1900-09-61-01 & FCD 1900-08-61-01. PERFORMED GROUND RUNS AND PERFORMED AUTOFEATHER TEST IAW MM 61-20-00. OPERATIONAL CHECK WAS GOOD.

Part: CIRCUIT BOARD — SHORTED (AUTOFEATHER) · airframe 26,315 hrs · 32,313 cycles

SUSPECTED AUTO FEATHER - PILOTS REPORTED THAT ON SHORT FINAL THE RT ENGINE CYCLED IN AND OUT OF FEATHER. MX R&R THE A123 PRINTED CIRCUIT BOARD AND OPS CHECKED THE SYSTEM IAW MM 61-21-00.

Part: SWITCH — DIRTY (AUTOFEATHER SYS) · airframe 26,151 hrs · 32,091 cycles

SIGNIFICANT EVENT - PILOTS REPORTED THAT THE RT ENG AUTOFEATHERED IN FLIGHT AND CAUSED SURGES AND EXTREME YAWING MOTION. MX CLEANED AFX SWITCHES IAW BMM 61-21-01-201. OPS CHECKS WERE OK.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 23,963 hrs · 29,141 cycles

SMOKE/ODOR - PILOTS REPORTED THE GLARESHIELD INSTRUMENT EMERGENCY LIGHTS WERE SMOKING ON THE GROUND AFTER STARTING ENGINES. REMOVED EMERGENCY FUSE F127. MAINTENANCE REMOVED EMERGENCY FUSE F127 AND REMOVED AND REPLACED BULB IAW MM 33-10. OPERATIONAL CHECK GOOD.

Part: FRAME — CRACKED (BS 177) · airframe 23,368 hrs · 28,423 cycles

FUSELAGE FRAME CRACKED APPROXIMATELY .8 INCH IN LENGTH AT FS 177 AT STRINGER 9AR. CRACKED AT STRINGER CUTOUT ON FRAME. REPAIRED FUSELAGE FRAME CRACK AT STRINGER RELIEF HOL AT F.S. 177 STRINGER 9AR. REPAIR APPROXIMATELY 4.4 INCH BY 2.5 INCH .080 2024 T-3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 23,368 hrs · 28,423 cycles

FRAME CRACKED AT FS 164 AT STRINGER 9AL. CRACK LENGTH APPROXIMATELY 4 INCHES. 09-26-07 REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE FS 164 AT STRINGER 9AR IAW BEECH 1900D SRM 51-70. REAPIR APPROXIMATELY 2.5" BY 4.1" .080 2024 T-3.

Part: ANGLE — CRACKED (BS 288) · airframe 23,368 hrs · 28,423 cycles

LT HEAVY ANGLE CRACKED AT FS STA 288.0 FORWARD END IN BEND RADIUS. 09-26-07 CRACK APPROXIMATELY 1.75" IN LENGTH. MAINTENANCE INSTALLED REPAIR ANGLE I.A.W. BEECH SRM 53-90-23. REPAIR LENGTH 13.8 INCHES. .080 2024-0.

Part: STRUCTURE — CRUSHED (RT ELEVATOR) · airframe 22,492 hrs · 27,371 cycles

RT ELEVATOR TRAILING EDGE DAMAGED APPROXIMATELY 9 INCHES OB OF TRIM TAB. DAMAGED AREA APPROXIMATELY 1 INCH BY 1.2500 INCH. MAINTENANCE REMOVED 2 INCH BY 1.5 INCH AREA OF TRAILING EDGE SKIN AND INSTALLED INSERTION REPAIR PER BEECH 1900D SRM 55-90-03. RII INSPECTION COMPLIED WITH PER T.C. 8.2.1.

Part: FUEL TANK — LEAKING (RIGHT) · airframe 20,807 hrs · 25,264 cycles

RIGHT AUX TANK FUEL LEAK FROM WEEP HOLE. VISUALLY INSPECTED AFFECTED SYSTEM AND FOUND SAFE FOR INTENDED FERRY FLIGHT GRI TO CYS.

Part: ALTIMETER — FAILED (COCKPIT) · airframe 18,055 hrs · 22,116 cycles

FO'S ALTIMETER SMOKED INSIDE OF GLASS AND CB POPPED. REMOVED AND REPLACED FO'S ALTIMETER PN 570-24929-412.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 17,384 hrs · 21,387 cycles

FO'S WINDSHIELD CRACKED AND CAUGHT ON FIRE, R&R WINDSHIELD PN 101-384025-22

Part: LINE — LEAKING (FUEL SYSTEM) · airframe 17,107 hrs · 21,083 cycles

FUEL LINE PN 118920000330 CHAFED ON ACM DUCT ASSY COUPLING CREATING A FUEL LEAK, CHANGED FUEL LINE AND REPOSITIONED DUCT COUPLING AND SPIRAL WRAPPED FUEL LINE

Part: A/C PACK — FAILED (A/C BAY) · airframe 14,138 hrs · 17,685 cycles

RIGHT ENVIRO FAIL.

Part: WHEEL · airframe 14,086 hrs · 17,625 cycles

AFTER TAKE OFF,NOSE WHEEL VIBRATION, R&R NOSE WHEEL ASSY.

Part: WHEEL — VIBRATION (NLG) · airframe 14,086 hrs · 17,625 cycles

AFTER TAKEOFF, NOSE WHEEL VIBRATION. REMOVED AND REPLACED NOSE WHEEL ASSY.

Part: COMPUTER — FAILED (COCKPIT) · airframe 13,431 hrs · 16,932 cycles

COPILOTS EFIS DISPLAY FAILED INFLIGHT. REPLACED DPU, OPS CHECKED SYSTEM SATISFACTORY.