N264AE

Part: LIGHT — FAILED (CABIN)

SBP - CABIN EMERGENCY LIGHTS 35LN AT ROW 4A WOULD NOT ILLUMINATE DURING TEST. REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW SAAB AMM 33-50. OPS CHECK GOOD. (M)

Part: CLAMP — BROKEN (RT ENGINE)

SBP - DURING PS CHECK, MAINTENANCE FOUND THE RIGHT ENGINE EXHAUST MIXER DUCT MISSING. THE ATTACHMENT CLAMP WAS FOUND TO BE BROKEN ALLOWING THE MIXER DUCT TO SLIDE THROUGH THE TAIL PIPE. NO DAMAGE TO THE TAIL PIPE WAS NOTED. REPLACED THE MIXER DUCT AND ATTACHMENT CLAMP. ALSO, REPLACED THE AFT LOWER SHROUD DUE TO CHAFING BY THE BROKEN CLAMP. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (ROW 11) · airframe 19,623 hrs · 19,833 cycles

LAX - FLT 3021 - DISC - ROW 11C FLOOR LIGHT INOPERATIVE. C/A - REMOVED AND REPLACED BULB. OPS CHECK GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (X)

Part: LIGHT — MISSING (ROW 8BC)

SBP - EMERGENCY LIGHT AT SEAT 8BC IS MISSING. REPLACED EMERGENCY LIGHT PANEL ASSEMBLY. OPERATIONAL CHECKED GOOD. (X)

Part: SKIN — DENTED (FUSELAGE)

ABI - DENT IN LEFT SIDE OF FUSELAGE SKIN FORWARD OF AND BELOW THE CARGO DOOR. PERFORMED AN EDDY CURRENT INSPECTION OF THE AREA TO BE REPAIRED. NO INDICATIONS OF CRACKS FOUND. PERFORMED A CUTOUT OF THE DAMAGED SKIN AND RE-EDDY CURRENT THE AREA, NO INDICATIONS OF CRACKS WERE NOTED. FABRICATED A REPAIR PLATE 12 INCH BY .5 INCH, .050 THICK. APPLIED ALODINE AND ONE COAT OF EPOXY PRIMER. CLEANED REPAIR AREA AN PLATE, FAY SEALED, REPOSITIONED AND INSTALLED RIVETS WET. EDGE SEALED REPAIR AND APPLIED ONE COAT OF EPOXY PRIMER AND ONE COAT OF TOP COAT TO EXTERIOR SURFACES. WORK DONE IAW SAAB 340 SRM 53-70-10, PAGE 215 AND STANDARD SRM PROCEDURES. AIRCRAFT OK FOR SERVICE. (M)

Part: BULB — FAILED (CABIN)

DFW - FLT 3638 - EMERGENCY FLOOR PROXIMITY LIGH TAT SEAT 10 B/C DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BULB — FAILED (SEAT 10C)

SAW - FOUND EMERGENCY LIGHT ABOVE SEAT 10C DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD. (M)

Part: SKIN — DENTED (BS 608)

ABI - DURING HMBV INSPECTION, DENT WAS FOUND AT RIGHT AFT FS 608. EDDY CURRENT REVEALED A CRACK INDICATION. CUT OUT DAMAGE AND INSTALLED REPAIR PLATE 25.5 INCHES BY 21 INCHES. AIRCRAFT RETURNED TO SERVICE. TOTAL TIME: 15,388.4 HOURS. TOTAL CYCLES: 14,564. (X)

Part: SKIN — DENTED (BS 853)

ABI - DURING HMBV, FOUND TWO DENTS ON RIGHT SIDE OF TAILCONE UPPER SKIN JUST FORWARD OF FS 853. DYE PENETRANT INSPECTION REVEALED NO DEFECTS. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PLATE AND TWO FILLER PLATES. AIRCRAFT RETURNED TO SERVICE. TOTAL TIME: 15,388.4 HOURS. RORAL CYCLES: 14,564. (X)

Part: SKIN — DENTED (BS 340)

ABI - DURING HMBV INSPECTION, MAINTENANCE FOUND A DENT ON RT HAND SIDE OF FUSELAGE AFT OF ICE SHIELD AT FS 340. CUT OUT DAMAGED AREA. PERFORMED EDDY CURRENT INSPECTION AND INSTALLED A REPAIR 12.5 INCHES BY 7.0 INCHES WIDE. ACFT TT: 15,388.4 HRS. ACFT TC: 14,564. (X)

Part: SEAT TRACK — CORRODED (BS 658)

ABI - DURING HMBV INSPECTION, SEAT TRACK BL 18.3L AT STA 658 WAS FOUND CORRODED BEYOND LIMITS. CUT OUT 46 INCH SECTION OF CORRODED SEAT TRACK. INSTALLED NEW 46 INCH EXTRUSION AND 15 INCH U-BEAM. ACFT TT: 15,388.4 HRS. ACFT TC: 14,564. (X)

Part: SEAT TRACK — CORRODED (BS 297)

ABI - DURING HMBV INSPECTION, SEAT TRACK BL ZERO AT STA 297 WAS FOUND CORRODED BEYOND LIMITS. CUT OUT 55 INCH SECTION OF CORRODED SEAT TRACK. FABRICATED AND INSTALLED 55 INCH EXTRUSION AND 15 INCH U-BEAM. ACFT TT: 15,388.4 HOURS. ACFT TC: 14,564. (X)

Part: SKIN — DENTED (BS 733)

ABI - DURING HMBV INSPECTION, MAINTENANCE FOUND A DENT ON LT HAND SIDE OF FUSELAGE AT FS 733. CUT OUT DAMAGED AREA. PERFORMED EDDY CURRENT INSPECTION AND INSTALLED A REPAIR 8.25 INCHES BY 8.0 INCHES WIDE. ACFT TT: 15,388.4 HRS. ACFT TC: 14,564. (X)

Part: SEAT TRACK — CORRODED (BS 297)

ABI - DURING HMBV INSPECTION, SEAT TRACK BL 18.3L AT STA 297 WAS FOUND CORRODED BEYOND LIMITS. CUT OUT 11 INCH SECTION OF CORRODED SEAT TRACK. FABRICATED AND INSTALLED 11 INCH EXTRUSION AND 15 INCH U-BEAM. ACFT TT: 15,388.4 HOURS. ACFT TC: 14,564. (X)

Part: BRAKE ASSY — FAILED (LT MLG)

RFD - MECHANIC REPORTS DURING INSPECTION, NR 2 BRAKE INNER STATOR FAILED. SPINS FREELY WITH BRAKE ROTORS. MAINTENANCE REPLACED BRAKE ASSEMBLY.