N261GL

Part: HANDLE — CORRODED (PAX DOOR) · airframe 37,985 hrs · 46,182 cycles

DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND CORROSION AROUND AND THROUGH BOLTS OF INTERIOR HANDLE BELLCRANK ASSY. ON AIRSTAIR DOOR, THE BELLCRANK ATTACHMENT HAS BEEN MODIFIED BY SB 129-4020-1 USING KIT 129-4020, (ONCE THEY OPEN IT UP IT MIGHT BE A PART REPLACEMENT INSTEAD OF A MAJOR REPAIR).

Part: FRAME — CRACKED (BS 183.25) · airframe 37,985 hrs · 46,182 cycles

DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND FUSELAGE FRAME AT BS 183.25 BETWEEN STRINGERS 2R AND 3R CRACKED AT THE INBOARD LOWER CORNER AREA OF DUCT CUTOUT, FRAME COMPLETELY CRACKED, 2" IN LENGTH. MAJOR REPAIR.

Part: ELBOW — CRACKED (RT ENGINE) · airframe 36,814 hrs · 44,908 cycles

WHILE IN CRUISE RT ENG LOW OIL PSI LIGHT CAME ON WITH NO OTHER ABNORMALITIES NOTED, IE LOUD BANG FLUX IN PWR, LOOKED OIL PSI GAUGE NOTICED GAUGE RAPIDLY DECREASING TO ZERO. REACHED FOR EMCK LIST NOTICED TORQUE GOING TO ZERO PROCEEDED TO EMER MEM ITEMS. SECURED RT ENG, EMER DECLARED. TROUBLE SHOT TO RT ENG PWR SECTION HIGH PRESS OIL LINE ELBOW, BROKEN VERIFIED ENG WAS 6 QUARTS LOW BY ADDING 6 QUARTS OF OIL WHICH BROUGHT OIL LEVEL TO 2 BELOW. TURN ENG OVER VERIFIED OIL LEAKING FROM PSI HIGH PRESS LINE ELBOW. PULLED RGB CHIP DETECTOR & VERIFIED NO METALLIC DEBRIS PULLED PS, STRAINER & FOUND NO METALLIC DEBRIS. INSTALLED NEW HIGH PRESS OIL LINE ELBOW & O RINGS. REINSTALLED CHIP DETECTOR, OIL STRAINER & OIL FILTER. RAN ENG FOR 10 MINUTES AT 80% POWER, VERIFIED NO FLUCTUATION IAW MCP 5.12.0 SECT B & MM 72-00-00. INSPECTED CHIP DETECTOR & OIL STRAINER AFTER THE RUN AT 80% FOUND NO METALLIC DEBRIS FOUND. REINSTALLED CHIP DETECTOR & OIL STRAINER & SAFETIED BOTH. REINSTALLED NEW OIL FILTER & O RING IAW MM 72-0-00 SECTION R ITEM D. MX REPLACED THE ENG SN OFF 114357/114267.

Part: UNKNOWN — MALFUNCTIONED (RT ENGINE) · airframe 36,814 hrs · 44,908 cycles

WHILE IN CRUISE RT ENG LOW OIL PSI LIGHT CAME ON WITH NO OTHER ABNORMALITIES NOTED, IE LOUD BANG FLUX IN POWER, LOOKED OIL PSI GAUGE NOTICED GAUGE RAPIDLY DECREASING TO ZERO. REACHED FOR EMER CHECK LIST NOTICED TORQUE GOING TO ZERO PROCEEDED TO EMER MEM ITEMS SECURED RT ENG, EMER DECLARED. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.

Part: LINE — RUPTURED (HYD SYSTEM) · airframe 36,492 hrs · 44,530 cycles

LANDING GEAR FAILED TO EXTEND NORMALLY, GEAR INTRANSIT LIGHT ILLUMINATED, WITH GEAR SELECTED DOWN. TRANSIT LIGHT FAILED TO EXTINGUISH NORMALLY, HYD FLUID LOW ANNUNCIATOR ILLUMINATED. PERFORMED MANUAL GEAR EXTENSION, GEAR IND WERE NORMAL. ON LANDING, FOUND HYD FLUID ON RT GEAR. MAINTENANCE FOUND RETRACT LINE RUPTURED, REPLACED HYD LINE IAW MM 20-06-00, SERVICED HYD RESERVOIR IAW MM 12-10-00 (5), PERFORMED GEAR SWINGS NUMEROUS TIMES IAW AIM 10-32-01, OPS AND LEAK CHECKED GOOD.

Part: STRINGER — CORRODED (BS 243) · airframe 35,855 hrs · 43,794 cycles

DURING A SCHEDULED INSPECTION FOUND CORROSION ON STRINGER 16 AT FS 243.25, RUNS APPROX 6 INCHES. REPAIRED IAW EO 13-1900-53-075. MAJOR REPAIR.

Part: SKIN — CORRODED (ZONE 100) · airframe 35,855 hrs · 43,794 cycles

DURING A SCHEDULED INSPECTION, FOUND BELLY SKIN CORRODED AT FS 243.25 AND STRINGER 16. REPAIRED IAW EO 13-1900-53-076. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 368.25-370.25) · airframe 35,245 hrs · 43,432 cycles

DURING A SCHEDULED INSPECTION, FOUND STRINGER 15L FLANGE DAMAGED AT 2 LOCATIONS FROM THE VENT BLOWER BRACKET, CHAFED AT FS 368.25 AND 370.25, CHAFED HALF WAY THROUGH STRINGER FLANGE. REPAIRED IAW EO 13-1900-53-056. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 370.25-378.25) · airframe 35,245 hrs · 43,432 cycles

DURING A SCHEDULED INSPECTION, FOUND STRINGER 16 CHAFED AT FOUR LOCATIONS FROM THE VENT BLOWER DUCT HARDWARE-SCREWS, DAMAGE AT TOP OF STRINGER BETWEEN BS 370.25 AND 378.25. REPAIRED IAW. EO 13-1900-53-056. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 368.25-370.25) · airframe 35,245 hrs · 43,432 cycles

DURING A SCHEDULED INSPECTION, FOUND BELLY SKIN AT FS 368.25 - 370.25 HAS TWO HOLES WORN THRU SKIN, HOLES NEXT TO STRINGER 15L, FWD AREA, HOLE J SHAPED IS .85" IN LENGTH, AFT WORN AREA HOLE IS .3" IN LENGTH. REPAIRED AREA IAW EO 13-1900-53-056. MAJOR REPAIR.

Part: SKIN — DAMAGED (BS 370) · airframe 38,492 hrs · 43,366 cycles

DURING A SCHEDULED INSPECTION, FOUND BELLY SKIN CHAFED, FWD OF FS 370.25 BETWEEN STRINGER 15--16L. REPAIRED IAW EO 13-1900-53-056.

Part: SKIN — CRACKED (BS 288) · airframe 34,989 hrs · 42,782 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RT LOWER BELLY SKIN OVER THE WING SPAR AT FS 288, 2.25 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-041. MAJOR REPAIR.

Part: FRAME — CRACKED (BS 107) · airframe 43,989 hrs · 42,782 cycles

DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT FS 107 AT THE INTERSECTION OF LONGERON UNDER RT FINGER DOUBLER, .5" IN LENGTH. REPAIRED IAW EO 13-1900-53-040. MAJOR REPAIR.

Part: SPAR CAP — CRACKED (VERTICAL STAB) · airframe 34,989 hrs · 42,782 cycles

DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE SPAR CAP, RT VERT STAB, SECOND FASTENER DOWN FROM THE TOP, .375" IN LENGTH. REPAIRED IAW EO 13-1900-55-015. MAJOR REPAIR.

Part: RIB — CHAFED (WING) · airframe 43,989 hrs · 42,782 cycles

DURING A SCHEDULED ROUTINE INSPECTION FOUND CHAFED AREA ON THE LT RIB 1 AT JUNCTION WITH WING SPAR, FLANGE PORTION OF RIB 1 WORN DOWN TO DOUBLER FLANGE, 1.5"*.75" AREA. REPAIRED IAW EO 13-1900-57-011. MAJOR REPAIR.

Part: DIODE — FAILED (EMERGENCY LIGHTS) · airframe 34,188 hrs · 41,848 cycles

PILOT REPORTED THAT THE INST EMERGENCY LIGHTS FAILED TO ILLUMINATE WITH THE INSTRUMENT EMERGENCY LIGHT SWITCH. MX REPLACED DIODES, OPS CHECKED GOOD.

Part: FUSE — INOPERATIVE (INSTRUMENT LIGHT) · airframe 34,167 hrs · 41,822 cycles

PILOT REPORTED THAT THE EMERGENCY INSTRUMENT LIGHTS ARE INOPERATIVE. MX REPLACED THE HOT BATTERY FUSE, OPS CHECKED GOOD.

Part: CURRENT LIMITER — FAILED · airframe 33,875 hrs · 41,477 cycles

PILOT REPORTED THAT 2 MINUTES INTO CRUISE, HAD SMOKE AND FUMES IN COCKPIT AND COMING FROM THE EYEBALL VENTS IN CABIN, CLOSED LT BLEED AIR AND SMOKE CLEARED, DECLARED EMERGENCY, LANDED WITH NO FURTHER INCIDENT. MX REPLACED THE CURRENT LIMITER AND AFT BLOWER, OPS CHECKED GOOD.

Part: BULB — MISSING (EMERGENCY LIGHT) · airframe 33,792 hrs · 41,382 cycles

PILOT REPORTED THAT THE INSTRUMENT EMERGENCY LIGHT BULB IS MISSING. MX REPLACED THE BULB, OPS CK GOOD.

Part: ATTACH FITTING — CRACKED (HORIZONTAL STAB) · airframe 33,457 hrs · 40,985 cycles

DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT SPAR CAP ON VERTICAL STAB AT HORIZONTAL STAB ATTACHMENT FITTING AT 2ND FASTENER FROM TOP, VSS 84.10 AT 20 PERCENT CHORD, .875" IN LENGTH. REPAIRED IAW FR-CO-02526, REV 1, STEP 1. MAJOR REPAIR.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 33,457 hrs · 40,985 cycles

DURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE VERTICAL STAB RT SIDE AFT LWR SPAR SKIN 8.5" UP FROM BOTTOM, 3" IN LENGTH. REPAIRED IAW EO 12-1900-55-038. MAJOR REPAIR.

Part: SPAR — CRACKED (HORIZONTAL STAB) · airframe 32,087 hrs · 39,419 cycles

DURING A SCHEDULED ROUTINE INSPECTION FOUND 4 CRACKS ON THE HORIZONTAL STAB REAR SPAR WEB AROUND ACCESS HOLE AT HSS. 00.0. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-55-002. MATERIALS UTILIZED ARE INCLUDED IN THE EO. MAJOR REPAIR

Part: SKIN — CORRODED (BS 198.25) · airframe 32,087 hrs · 39,419 cycles

DURING A SCHEDULED ROUTINE INSP FOUND BELLY CORROSION AT FS 198.25 BETWEEN STRINGER 15 AND 16L, AREA BETWEEN A DOUBLE ROW OF FASTENERS, AREA .75" BY .5". REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-011. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER. MAJOR REPAIR

Part: DOOR FRAME — CRACKED (BS 176) · airframe 32,087 hrs · 39,419 cycles

DURING A SCHEDULED ROUTINE INSPECTION FOUND THE A/S DOOR ENTRANCE LOWER FRAME CRACKED IN THE AFT CORNER AT FS 176 AND STRINGER 11L, .1250" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 12-1900-53-010. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER. MAJOR REPAIR

Part: DOOR — OPEN (EMERGENCY EXIT) · airframe 31,654 hrs · 38,920 cycles

DURING THE PASSENGER BRIEFING (WITH ENGINES NOT RUNNING), A PASSENGER OPENED UP THE 6C EMERGENCY EXIT DOOR. MX REINSTALLED THE EMERGENCY EXIT DOOR.

Part: SEAL — DIRTY (PAX DOOR) · airframe 31,422 hrs · 38,656 cycles

PILOT REPORTED THAT THE CABIN DOOR WAS SQUEELING IN FLIGHT. MX CLEANED THE DOOR SEAL, PRESSURIZATION CHECKS GOOD, OK FOR SERVICE.

Part: DOOR FRAME — CRACKED (BS 460 S3L) · airframe 30,408 hrs · 37,479 cycles

MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE UPPER GARGO DOOR FUSELAGE FRAME AT FS 460 AND STRINGER 3L CRACKED 1.3" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-026. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.

Part: BLOWER — WORN (FWD) · airframe 30,043 hrs · 37,041 cycles

PILOT REPORTED THAT WHEN BLOWER IS PLACED TO AUTO, IT GAVE OFF AN ELECTRICAL ODOR, WHEN TURNED OFF, ODOR WENT AWAY. MAINTENANCE REPLACED THE FORWARD BLOWER ASSY IAW AIM 21-02 AND CW CORROSION INSPECTION.

Part: BULB — MISSING (CABIN LIGHTS)

PILOT REPORTED THAT ONE OF THERE EMERGENCY LIGHTS ON THE CAPTAIN'S SIDE IS MISSING A BULB. MAINTENANCE REPLACED THE MISSING BULB PN 1864 AND FILTER PN D165-100-2 IAW BMM 33-10-04, OPERATIONAL CHECKS GOOD.

Part: ENGINE — LOW TORQUE (LEFT) · airframe 29,136 hrs · 35,979 cycles

INCREASING POWER ON APPROACH, LT ENGINE REMAINED AROUND 500 LBS TORQUE, DID NOT RESPOND TO POWER LEVER INPUT WHILE RT ENGINE SPOOLED TO APPROX 1200 TORQUE. LT ENGINE AUTOFX TRIGGERED AND TOOK APPROX 2-3 INCHES OF POWER LEVER MOVEMENT TO GET LT ENGINE TO RESPOND TO INPUT. MAINTENANCE OBSERVED CREW PERFORMING RUN UP PER MM 61-21-00, SYSTEM OPERATIONAL CHECKS GOOD.

Part: SKIN — CRACKED (EMERGENCY EXIT) · airframe 29,090 hrs · 35,929 cycles

MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A CRACK IN THE LOWER FWD SKIN ON THE 6A EMERGENCY EXIT DOOR, 1.2" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-52-005. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.

Part: FRAME — CRACKED (ZONE 100) · airframe 29,090 hrs · 35,929 cycles

DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A THE CARGO PARTITION FUSELAGE ATTACH POINT HOLES ARE WORN, TOP LEFT, TOP CENTER, AND TOP RIGHT. MAINTENANCE INSPECTED AND FOUND THE REPAIR TO BE A MINOR REPAIR - REPAIRED PARTITION ATTACH POINTS, TOP, TOP RIGHT AND TOP LEFT. ATTACHING WITH RIVETS PN MS20470 E5 AND CR2839 CW-5 IAW SRM 51-40-02 AND 51-40-03.

Part: FRAME — CRACKED (BS 288) · airframe 29,090 hrs · 35,929 cycles

MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A CRACK ON THE LT HEAVY FRAME ANGLE AT FS 288 FWD BEND RADIUS, 1.4" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-053. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.

Part: SKIN — DENTED (FUSELAGE) · airframe 28,092 hrs · 34,765 cycles

MAJOR REPAIR - DURING A POSTFLIGHT INSP, A DENT WAS FOUND ON THE LT SIDE OF THE ACFT 6" AFT OF THE FWD CARGO DOOR BULKHEAD 6" FROM THE BOTTOM, APPROX 2" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 10-1900-53-008. RII INSPECTIONS COMPLIED WITH IAW EO 10-1900-53-008. MATERIALS UTILIZED ARE INCLUDED IN THE EO.

Part: SKIN — DENTED (ZONE 100) · airframe 28,092 hrs · 34,765 cycles

DURING A POSTFLIGHT INSP, A DENT WAS FOUND ON THE LT SIDE OF THE ACFT 6" AFT OF THE FWD CARGO DOOR BULKHEAD 6" FROM THE BOTTOM, APPROX 2" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 10-1900-53-008. RII INSPECTIONS COMPLIED WITH IAW EO10-1900-53-008. MATERIALS UTILIZED ARE INCLUDED IN THE EO.

Part: DOOR LATCH — LACK OF LUBE (EMERGENCY EXIT) · airframe 27,129 hrs · 33,506 cycles

DURING ROUTINE SCHEDULED MAINTENANCE THE EMERGENCY EXT DOOR 6C DID NOT OPEN PROPERLY. MAINTENANCE LUBED THE LATCH MECHANICAL SHAFT, RE-INSTALLED THE DOOR I.A.W. BMM 52-20-00 STEPS A-C FOR REMOVAL AND INSTALLATION AND I.A.W. 52-20-01 STEP D FOR LUBING. NO RIGGING WAS REQUIRED. OPERATIONAL CHECK OF THE DOOR WAS GOOD.

Part: DOOR — STIFF (EMERGENCY EXIT) · airframe 27,129 hrs · 33,506 cycles

DURING ROUTINE SCHEDULED MAINTENANCE THE EMERGENCY EXT DOOR 4C DID NOT OPEN PROPERLY. MAINTENANCE LUBED THE LATCH MECHANICAL SHAFT, RE-INSTALLED THE DOOR IAW MM 52-20-00 STEPS A-C FOR REMOVAL AND INSTALLATION AND IAW 52-20-01 STEP D FOR LUBING. NO RIGGING WAS REQUIRED. OPERATIONAL CHECK OF THE DOOR WAS GOOD.

Part: HANDLE — MISALIGNED (MLG) · airframe 26,435 hrs · 32,585 cycles

FLT 5091 - ENROUTE, PILOTS REPORTED THAT THE GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE J-HOOK DID RELEASE. THEY TRIED A COUPLE TIME TO GET THE GEAR TO COME UP. MAINTENANCE RE-STOWED THE EMERGENCY HANDLE AND INSPECTED THE LT AND RIGHT SAFETY SWITCHES. GEAR SWINGS WERE PERFORMED MULTIPLE TIMES WITH NO DICREPTIMES WITH NO DESCREPANCIES NOTED. REFERENCE MM 32-20-00. OPERATIONAL CHES WERE GOOD.

Part: SKIN — CRACKED (ZONE 100) · airframe 26,291 hrs · 32,391 cycles

DURING A SCHEDULED STRUCTURAL CHECK MX DISCOVERED A CRACK ON THE LT FUSELAGE SKIN JUST INBD OF THE LT WING BOTTOM WING PANEL AT F.S. 303.25. CRACK APPROXIMATELY 2.250 INCHES IN LENGTH. MX REPAIRED THE CRACK ON THE LT FUSELAGE SKIN JUST INBD OF THE LT WING BOTTOM WING PANEL AT F.S. 303.25 IAW GLA EO-09-1900-53-004.

Part: FRAME — CRACKED (ZONE 100) · airframe 26,291 hrs · 32,391 cycles

DURING A SCHEDULED STRUCTURAL CHECK, MX DISCOVERED A CRACK ON THE RT HEAVY ANGLE AT FA 288.0. LENGTH OF CRACK APPROX 1.5 INCH LONG. MX REPAIRED THE RT HEAVY ANGLE AT FA 288.0. IAW. EO-09-1900-53-003. REPAIR AREA APPROXIMATELY 13.5 INCH LONG OUT OF PN 114-430002-7180. RII INSPECTIONS COMPLIED WITH. MATERIALS UTILIZED INCLUDE AND 10133-1033-2024 T-4, EA9303.3 NA ADHESIVE, ALODINE, MS20470AD5 AND MS20470AD6, CR3553P6N RIVETS.

Part: FRAME — BENT (BS 496 S3L) · airframe 24,081 hrs · 29,449 cycles

FRAME SECTION AT FS 469 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 469 STRINGER 3L IAW SRM 51-40. P/N 129-40044-75.

Part: FRAME — BENT (BS 495 S3L) · airframe 24,081 hrs · 29,449 cycles

FRAME SECTION AT FS 495.75 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 495.75 STRINGER 3L IAW SRM 51-40. P/N 129-440044-71.

Part: FRAME — BENT (BS 469 S3L) · airframe 24,081 hrs · 29,449 cycles

FRAME SECTION AT FS 469 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 469 STRINGER 3L IAW SRM 51-40. P/N NR 129-440044-75.

Part: FRAME — BENT (BS 482 S3L) · airframe 24,081 hrs · 29,449 cycles

FRAME SECTION AT FS 482.75 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 482.75 STRINGER 3L IAW SRM 51-40. P/N 129-440044-73

Part: FRAME — BENT (BS 482 S3L) · airframe 24,081 hrs · 29,449 cycles

FRAME SECTION AT FS 482.75 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 482.75 STRINGER 3L IAW SRM 51-40. P/N 129-440044-73.

Part: FRAME — BENT (BS495 S3L) · airframe 24,081 hrs · 29,449 cycles

FRAME SECTION AT FS. 495.75 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 495.75 STRINGER 3L IAW SRM 51-40. PN 129-440044-71.

Part: HINGE FITTING — DAMAGED (CARGO DOOR) · airframe 23,104 hrs · 28,191 cycles

CARGO DOOR HINGE HALF FORWARD AND AFT LUGS MISSING AND SEVERAL LOOSE RIVETS. MAINTENANCE REPLACED HINGE HALF ON CARGO DOOR IAW SRM 52-90. RII INSPECTION COMPLIED WITH IAW TASKCARD 8.2.1. IWO NR 94171, L/P NR 207464.

Part: STRINGER SPLICE — CORRODED (BS 246-250) · airframe 23,104 hrs · 28,191 cycles

BELLY CORROSION FOUND AT APPROXIMATELY FS 246 TO FS 250 ON STRINGER 15R. MAINTENANCE REPLACED DAMAGED STRINGER SECTION PER ENGINEERING ORDER 07-UE261-01. APPROXIMATE STRINGER REPLACEMENT 15" WITH 11" NEW STRINGER SPLICE. PART NUMBER 131686. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.

Part: FRAME — CRACKED (BS 177) · airframe 23,104 hrs · 28,191 cycles

FRAME CRACKED AT STRINGER CUTOUT FS 177 AT STRINGER 9AR. REPAIRED FRAME AT STRINGER RELIEF HOLE FS 177 AND STRINGER 9AR IAW 1900D SRM 51-70. REPAIR DIMENSIONS 4.5 BY 2.5 . 2024 T-3 .080. RII COMPLIED WITH IAW TASKCARD 8.2.1.

Part: DOUBLER — CRACKED (BS 288-327) · airframe 20,551 hrs · 25,029 cycles

STRUCTURAL INSPECTION - LEFT ( 114-430002-7180) AND RIGHT (114-430002-7179) HEAVY DOUBLERS CRACKED F.S. 288-327 & WL 100, REPAIR PENDING, REPLACED DOUBLERS

Part: SKIN — CORRODED (BS 214 S16L) · corrosion level 2 · airframe 20,551 hrs · 25,029 cycles

CORROSION FOUND AT FS 214, OUTER SKIN & STRINGER 16, REPAIR PENDING, INSTALL FLUSH PATCH APPROXIMATLY 12" X 12"

Part: STRINGER — CORRODED (FUSELAGE) · airframe 17,674 hrs · 21,692 cycles

INTERNAL LOWER SKIN TO STRINGER CORROSION FOUND DURING ROUTINE INSPECTION. CORROSION LOCATED BETWEEN BONDED STRINGER 16 AND FUSELAGE SKIN, BETWEEN FS 220 AND FS 236. CORROSION APPROX. 6 INCHES TO 8 INCHES IN LENGTH.

Part: TIRE — SEPARATED (MAIN WHEEL ASSY) · airframe 15,292 hrs · 19,102 cycles

NR 2 TIRE TREAD CAME OFF. REMOVED AND REPLACED NR 1 & 2 WHEEL ASSY.

Part: ANNUNCIATOR — ILLUMINATED (FUEL QTY) · airframe 15,157 hrs · 18,967 cycles

FUEL QTY ANNUNCIATOR ILLUMINATED, PREFORMED OPERATIONAL RUN-UP OF A/C CND TEST OF SYSTEM OK.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 14,780 hrs · 18,581 cycles

RT WINDSHIELD CRACKED IN FLIGHT.

Part: SPLICE — DAMAGED (EVA TUBE) · airframe 13,981 hrs · 17,726 cycles

LEFT BLEED AIR FAIL ANNUCIATOR ILLUMINATED, REPAIRED EVA TUBE SPLICE

Part: WHEEL — VIBRATION (NLG) · airframe 13,981 hrs · 17,726 cycles

A/C VIBRATING IN CLIMB, R&R NOSE WHEEL ASSY

Part: ACTUATOR — FAILED (RT MLG) · airframe 13,563 hrs · 17,274 cycles

GEAR WARNING RT SIDE AFTER LANDING, R&R MLG ACTUATOR.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 13,335 hrs · 17,043 cycles

CAPTAIN'S WINDSHIELD CRACKED IN FLIGHT, DIVERTED A/C TO FMN, FERRY TO CYS. REMOVED AND REPLACED WINDSHIELD

Part: SWITCH — MALFUNCTIONED (TE FLAPS) · airframe 13,190 hrs · 16,889 cycles

FLAP STUCK AT 35 PERCENT, CHANGED FLAP SWITCH OPS CHECK GOOD

Part: TUBE — DAMAGED (BLEED AIR) · airframe 12,999 hrs · 16,695 cycles

RIGHT BLEED AIR FAIL ON TAKEOFF. REPAIRED EVA TUBING, OPS CHECKED SYSTEM SATISFACTORY.

Part: SOLENOID — DIRTY (AIR CONDITIONING) · airframe 12,755 hrs · 16,448 cycles

RIGHT ENVIRO FAIL. CLEANED PRESSURE SOLENOID, OPS CHECKED SYSTEM SATISFACTORY.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 12,737 hrs · 16,430 cycles

RIGHT ENVIRONMENTAL FAIL ON T/O ROLL. RESET OVERPRESS LED ON BLEED AIR.

Part: PROBE — DEFECTIVE (RT ENGINE) · airframe 11,396 hrs · 14,831 cycles

RIGHT ENGINE TEMP LIMITED ON T/O. REPLACED TRIM PROBE, OPS CHECKED SYSTEM SATISFACTORY.

Part: BYPASS VALVE — INOPERATIVE (RT ACM) · airframe 10,355 hrs · 13,766 cycles

CABIN HEAT NOT WORKING. REMOVED AND REPLACED ACM BYPASS VALVE, OPS CHECKED GOOD.

Part: CONTROL UNIT — FAILED (CABIN PRESSURE) · airframe 9,931 hrs · 13,326 cycles

RETURN TO BLOCK, WOULD NOT PRESSURIZE. CND ON GROUND, OPS CHECKED SYSTEM GOOD.