N448AM

Part: SKIN — CORRODED (RT WING) · airframe 32,706 hrs · 32,512 cycles

DURING MX INSPECTION, FOUND CORROSION AT RT WING BOTTOM T/E BETWEEN RIB 6 AND 10. ACFT REMOVED FROM SERVICE. INSTALLED RT WING T/E RIB 8-10 PANEL JIC 53-93-00 RAI-10000. ACFT RETURNED TO SERVICE.

Part: SKIN — CORRODED (RT WING) · airframe 32,706 hrs · 32,512 cycles

DURING MX INSPECTION, FOUND CORROSION AT THE RT WING L/E BETWEEN RIB 4-5. THE ACFT WAS REMOVED FROM SERVICE. CLEANED AND TREATED RT WING L/E BETWEEN RIB 4-5 NO MATERIAL WAS REMOVED IAW SRM 51-21-42. THE ACFT WAS RETURNED TO SERVICE.

Part: DRAIN VALVE — CORRODED (RT WING) · airframe 32,706 hrs · 32,512 cycles

DURING MX INSP FOUND THE RT WING INBD AFT WATER DRAIN VALVE WITH CORROSION. THE ACFT WAS REMOVED FROM SERVICE. CLEANED AND TREATED RT WING INBD AFT WATER DRAIN VALVE NO MATERIAL WAS REMOVED IAW SRM 51-21-42. THE ACFT WAS RETURNED TO SERVICE.

Part: HINGE — CORRODED (ACCESS PANEL) · airframe 32,706 hrs · 32,512 cycles

DURING MX INSP, FOUND THE T/E ACCESS PANEL HINGE CORRODED. THE ACFT WAS REMOVED FROM SERVICE. CLEANED AND TREATED CORROSION AT T/E ACCESS PANEL HINGE IAW SRM 51-21-42. NO MATERIAL REMOVED. THE ACFT WAS RETURNED TO SERVICE.

Part: RIB — CORRODED (LT WING) · airframe 32,706 hrs · 32,512 cycles

DURING MX INSP FOUND CORROSION SPOT AT LT WING NEAR RIB 6 CENTER AREA. THE ACFT WAS REMOVED FROM SERVICE. CLEANED AND TREATED CORROSION AT LT WING NEAR RIB 6 CENTER AREA IAW SRM 51-21-42. NO MATERIAL REMOVED. THE ACFT WAS RETURNED TO SERVICE.

Part: FASTENER — CORRODED (RT WING) · airframe 32,706 hrs · 32,512 cycles

DURING MX INSPECTION, FOUND THE RT WING FASTENERS AT T/E BETWEEN RIB 8-13 WITH CORROSION. ACFT REMOVED FROM SERVICE. INSTALLED RT WING T/E RIB 8-10 PANEL JIC 53-93-00 RAI-10000. ACFT RETURNED TO SERVICE.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 32,706 hrs · 32,512 cycles

DURING MX INSPECTION, FOUND CORROSION ON THE RT T/E ACCESS PANEL HINGE NEAR RIB 5-6. THE ACFT WAS REMOVED FROM SERVICE. CLEANED AND TREATED RT WING T/E ACCESS PANEL HINGE NEAR RIB 5-6. NO MATERIAL WAS REMOVED IAW SRM 51-21-42. THE ACFT WAS RETURNED TO SERVICE.

Part: RIB — CORRODED (LT WING) · airframe 32,706 hrs · 32,512 cycles

DURING MX INSP FOUND CORROSION AROUND FASTENER AT LT WING T/E NEAR RIB 8 AREA. THE ACFT WAS REMOVED FROM SERVICE. CLEANED AND TREATED CORROSION AT LT WING T/E FASTENER NEAR RIB 8 AREA IAW SRM 51-21-42. NO MATERIAL REMOVED. THE ACFT WAS RETURNED TO SERVICE.

Part: DRAIN VALVE — CORRODED (LT WING) · airframe 32,706 hrs · 32,512 cycles

DURING MX INSP FOUND THE LT WING INBD WATER DRAIN VALVE BOTH WITH CORROSION. THE ACFT WAS REMOVED FROM SERVICE. CLEANED AND TREATED CORROSION AT LT WING INBD WATER DRAIN VALVE IAW SRM 51-21-42. NO MATERIAL REMOVED. THE ACFT WAS RETURNED TO SERVICE.

Part: PUMP — CORRODED (RT WING) · airframe 32,706 hrs · 32,512 cycles

DURING MX INS FOUND THE RT WING ELECTRIC FUEL PUMP WITH CORROSION AROUND FASTENERS (BOLT). THE ACFT WAS REMOVED FROM SERVICE. CLEANED AND TREATED RT WING ELECTRIC FUEL PUMP AROUND FASTENER (BOLT) NO MATERIAL WAS REMOVED IAW SRM 51-21-42. THE ACFT WAS RETURNED TO SERVICE.

Part: PUMP — CORRODED (LT WING) · airframe 32,706 hrs · 32,512 cycles

DURING MX INSPECTION, FOUND THE LT WING ELECTRIC FUEL PUMP WITH CORROSION AROUND FASTENERS (BOLT). THE ACFT WAS REMOVED FROM SERVICE. CLEANED AND TREATED CORROSION AT LT WING ELECTRIC FUEL PUMP IAW SRM 51-21-42. NO MATERIAL REMOVED.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 32,651 hrs · 32,651 cycles

FLIGHT 4847, CREW REPORTED THE SERVICE DOOR EMERGECNY GROUND FLOOD LIGHT LENS CRACKED AND WAS INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. R & R SERVICE DOOR GROUND FLOOD LIGHT IAW JIC 33-50-00. THE OPS CHECKED GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: HANDLE — INOPERATIVE (ESCAPE HATCH) · airframe 32,648 hrs · 32,442 cycles

THE CREW REPORTED THE EMERGENCY ESCAPE HANDLE WAS BROKEN. THE ACFT WAS REMOVED FROM SERVICE. EMERGENCY ESCAPE HANDLE MISSING SCREW INSTALLED IAW MM 52-22-10. THE AFT WAS RETURNED TO SERVICE.

Part: CHANNEL — CORRODED (TAIL CONE) · airframe 32,493 hrs · 32,272 cycles

DURING MX INSPECTION, FOUND THE TAIL CONE NUTPLATE GANG LT AND RT CHANNELS TO HAVE CORROSION BEYOND LIMITS. THE ACFT WAS REMOVED FROM SERVICE. REPLACED DAMAGED SECTIONS OF LT AND RT TAIL CONE NUTPLATE GANG CHANNELS IAW MM 53-91-30, SRM 53-91-24 AND EO E2-5300-319. THE ACFT WAS RETURNED TO SERVICE.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 32,056 hrs · 31,743 cycles

DURING MX INSPECTION, FOUND THE EMERGENCY LIGHT (GROUND FLOOD LIGHT) ON PASSENGER STAIRS ENTRY DOOR INOPERATIVE. ACFT REMOVED FROM SERVICE. SECURED WIRE TO PIN " E " C/P 253VC. OPS CHECKED GOOD IAW AWM 52-71-01 AND AMM 33-51-00. ACFT RETURNED TO SERVICE.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 32,012 hrs · 31,699 cycles

THE CREW REPORTED THE END CAP ON THE FLOOR EMERGENCY EXIT LIGHT IN FRONT OF THE AFT GALLEY CART IS MISSING. THE ACFT WAS REMOVED FROM SERVICE. INSTALLED END CAP EMERGENCY LIGHT IN FRONT OF AFT GALLEY CART IAW 25-28-21 RAI 10000-006. THE ACFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,955 hrs · 31,639 cycles

DURING MAINTENANCE INSPECTION, FOUND PAX DOOR EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY 62W1 IAW JIC 33-51-21 AND REMOVED AND REPLACED THE EMERGENCY PASSENGER DOOR LIGHT ASSEMBLY, IAW JIC 52-11-00. THE OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 31,838 hrs · 31,505 cycles

DURING B INSPECTION, FOUND THE EMERGENCY FLOOR LIGHT STRIP MISSING END CAP IN GALLEY AREA. THE ACFT WAS REMOVED FROM SERVICE. INSTALLED EMERGENCY FLOOR LIGHT STRIP END CAP IN GALLEY AREA IAW JIC 25-28-21 RAI 10000. THE ACFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 31,793 hrs · 31,453 cycles

ON FLIGHT 4962, THE CREW REPORTED THE EMERGENCY LIGHT OUTSIDE SERVICE DOOR CHECK FOR LOOSE CONNECTION HAS TO BE HIT ON THE OUTSIDE TO WORK. THE ACFT WAS REMOVED FROM SERVICE. RE-SECURED LOOSE BULB, OPS CK NORMAL IAW AMM 33-50-00. THE ACFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,766 hrs · 31,419 cycles

THE CREW REPORTED THE EXIT FLOOD LIGHT ON MAIN ENTRY DOOR STAIRS INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. RELAMPED FLOOD LIGHT ON PASSENGER DOOR STAIRS. THE OPS CHECK WAS GOOD IAW JIC 33-00-00. THE ACFT WAS RETURNED TO SERVICE.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 31,766 hrs · 31,419 cycles

DURING B INSPECTION, FOUND THE EMERGENCY FLOOR LIGHT STRIP END CAP MISSING AT GALLEY AREA. THE ACFT WAS REMOVED FROM SERVICE. INSTALLED EMERGENCY FLOOR LIGHT STRIP END CAP AT GALLERY IAW CMM 33-52-10. THE OPS CHECKED GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 31,703 hrs · 31,346 cycles

DURING B-INSPECTION, FOUND THE EMERGENCY FLOOR LIGHT STRIP MISSING AN END CAP IN GALLEY AREA. THE ACFT WAS REMOVED FROM SERVICE. FOUND MISSING EMERGENCY FLOOR LIGHT STRIP END CAP AND REINSTALLED IN GALLEY AREA IAW JIC 25-28-21 RAI 11000. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 31,675 hrs · 31,314 cycles

THE CREW REPORTED THAT ON CLIMBOUT, AFTER TAKEOFF THERE WAS A BIG BIRD STRIKE ON NOSE OF ACFT. THE CREW ELECTED TO RETURN TO DEPARTURE AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPAIRED DAMAGE IAW EO E2-53MR-312 AND EO E2-53MR-313. ACFT RETURNED TO SERVICE.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 31,475 hrs · 31,071 cycles

ON FLIGHT 4925, THE CREW REPORTED THE COVER OVER AFT FLOOR EMERGENCY EXIT LIGHT IN FRONT OF AFT GALLEY CART IS MISSING. THE ACFT WAS REMOVED FROM SERVICE. INSTALLED COVER ON AFT FLOOR EMERGENCY LIGHT IAW ATR 72 JIC 33-51-24. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 31,361 hrs · 30,935 cycles

DURING B-INSP FOUND THE EMERGENCY FLOOR LIGHT STRIP MISSING END CAP IN GALLEY AREA. THE ACFT WAS REMOVED FROM SERVICE. FOUND END CAP AND RE-INSTALLED EMERGENCY FLOOR LIGHT END CAP IN GALLEY AREA IAW JIC 25-28-21, RAI 10000. THE ACFT WAS RETURNED TO SERVICE.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,333 hrs · 30,905 cycles

DURING MX INSPECTION, FOUND THE EMERGENCY LIGHTS TOGGLE SWITCH CANNED. THE ACFT WAS REMOVED FROM SERVICE. INSTALLED EMERGENCY LIGHT TOGGLE SWITCH REF CANNED TAG 88210 IAW MM 20-45-11. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 31,297 hrs · 30,859 cycles

THE CREW REPORTED THAT ON POST FLIGHT, FOUND THE EMERGENCY EXIT LIGHTS AT PASSENGER ENTRY DOOR ARE INOPERATIVE. ACFT REMOVED FROM SERVICE. REMOVED AND INSTALLED EMERGENCY LIGHTING POWER SUPPLY IAW JIC33-51-21-RAI-10000. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: DOOR — MISSING (MLG) · airframe 31,203 hrs · 30,749 cycles

ON POST FLT INSPECTION, FOUND UPPER LT GEAR DOOR MISSING. INSTALLED LT FOLDABLE MLG DOOR IAW SRM 52-81-00. GEAR SWING PERFORMED, OPS CHECK GOOD. REF JIC 07-11-00, JUP 10000.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,050 hrs · 30,567 cycles

PAX DOOR EMERGENCY LIGHT INOPERATIVE. R & R PAX DOOR LIGHT ASSY IAW 33-51-24-RAI-10000.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 31,036 hrs · 30,555 cycles

EMERGENCY LIGHT ON THE STAIRS FLICKERS. RE-LAMPED EMERGENCY LIGHT ON PAX/ CREW STAIR IAW MM 33-50-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,025 hrs · 30,543 cycles

EMERGENCY FLOOD LIGHT ON THE MAIN CABIN DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT BULB AT PAX DOOR IAW AMM 33-51-24.

Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 30,801 hrs · 30,296 cycles

EMERGENCY LIGHT ON THE MAIN CABIN DOOR INOP IS OUT REPEAT WRITE UP. RESECURED LIGHT BULB 33-50-00.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 30,797 hrs · 30,294 cycles

EMERGENCY EXIT LIGHT LT SIDE OF ACFT IS OUT. PERFORMED OPS CHECK OF EMERGENCY EXIT LIGHTS IAW JIC 33-50-00, OPT 10000, OPS CHECK GOOD AND W/C EX335000-OPT-10000.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 30,797 hrs · 30,294 cycles

EMERGENCY EXIT LIGHT IN STAIRS IS OUT. PERFORMED OPS CHECK OF EMERGENCY EXIT LIGHTS IAW JIC 33-50-00, OPT 10000. OPS CHECKED GOOD AND W/C EX335000-OPT-10000.

Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 30,672 hrs · 30,153 cycles

EMERGENCY LIGHT ON STAIRS IS OUT. RESECURED BULB IAW JIC 33-00-00. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,588 hrs · 30,059 cycles

AIRSTAIR/ DOOR EMERGENCY LIGHT INOPERATIVE. RELAMPED AIRSTAIR/ DOOR IAW MM 33-50-00.

Part: BATTERY — FAULTED · airframe 30,582 hrs · 300,055 cycles

EMERGENCY BATTERY CHARGE FAULT IN FLIGHT. R & R EMERGENCY BATTERY IAW W/C EX-243185-RAI-10020-002.

Part: LATCH — BROKEN (EMERGENCY LIGHT)

REAR PANEL EMERGENCY LIGHT PUSH BUTTON LATCH IS BROKEN. R & R SWITCH BASE ON REAR PANEL EMERGENCY LIGHT PUSH BUTTON.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 30,243 hrs · 29,698 cycles

F/O WINDSHIELD CRACKED AND MONOFILAMENTS STARTED TO BURNED ON WINDSHIELD. REPLACED F/O WINDSHIELD IAW JIC 56-11-00. LEAK CHECK SATISFACTORY.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 28,346 hrs · 27,396 cycles

ELECTRICAL SMOKE ODOR IN COCKPIT. AWAITING NRWC FOR FURTHER DETAILS.

Part: GROUND WIRE — FAILED (GPU) · airframe 28,346 hrs · 27,396 cycles

ELECTRICAL SMOKE ODOR IN COCKPIT. R & R GPU GROUND CABLE 440VN IAW JIC NR 24-46-11.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 27,361 hrs · 26,258 cycles

UPON FLAP RETRACTION DURING CLIMB FLAP ASSY LIGHT ILLUMINATED WITH CAUTION. EMERGENCY DECLARED. RETURN TO DEPARTURE, PERFORMED 0 DEGREE FLAP LANDING. PERFORMED ADJUSTMENT OF RT FLAP POSITION TRANSMITTER IAW MM JIC NR 27-55-71. OPS TEST FOUND OK IAW MM JIC NR 27-21-00.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 26,765 hrs · 25,595 cycles

DURING CLIMB-OUT NOTICED CAPT FRONT WINDSHIELD SHOWING MULTIPLE SPIDER CRACKS ALONG WITH BURN MARKS AROUND ENTIRE WINDSHIELD. REMOVED AND REPLACED CAPT WINDSHIELD AS PER JIC NR 56-11-00-RAI-10000. OPS CHECK AND LEAKS CHECK GOOD.

Part: FIRE DETECTOR — FALSE ACTIVATION (NR 2 NACELLE) · airframe 26,728 hrs · 25,551 cycles

AT THE GATE NAC OVHEAT LIGHT ON. AS PER AOM VOL 1 CONDITION LEVER MAX RPW, THEN ENGINE FIRE NR 2 LIGHT ON. FOLLOWED EMERGENCY PROCEDURES CHECK LIST (ENGINE FIRE) CONDITION LEVER FUEL SHUT OFF. PULLED FIRE HANDLE, LIGHT OUT. INSPECTED NR 2 ENGINE AND NACELLE. NO EVIDENCE OF FIRE FOUND. PERFORMED OPS CHECK OF NR 2 ENG FIRE DETECTION SYSTEM IAW ATR 72 JIC 26-12-00. OPT CK GOOD ALSO GROUND RUN NR 2 ENG FOR 30 MINUTES IAW JIC NR 72-00-00. NO DEFECTS NOTED. SUSPECT 40 KTS TAIL WIND CAUSE THE PROBLEM.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 25,188 hrs · 25,926 cycles

ONE OF THE FLOOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED FLOOR EMERGENCY LAMP IAW JIC NR 33-50-00.

Part: SIGN — INOPERATIVE (SERVICE DOOR) · airframe 24,426 hrs · 23,202 cycles

SERVICE DOOR EMERGENCY EXIT SIGN INOPERATIVE. RAI SERVICE DOOR EMERGENCY EXIT SIGN IAW JIC 33-51-00. OPT OK IAW JIC 33-50-00.

Part: INDICATOR — FAILED (COCKPIT) · airframe 24,167 hrs · 22,972 cycles

DURING T/O ROLL, F/O'S EHSI WENT BLANK. ABORTED TAKEOFF AND RETURNED TO BLOCK. REMOVED AND REPLACED F/O EHSI AND PERFORMED OPT CK IAW JIC NR 34-75-81 AND FOUND SYSTEM WORKING PROPERLY.

Part: SKIN — CORRODED · corrosion level 2 · airframe 23,465 hrs · 22,340 cycles

LOCK FASTERNER COLLARS CORRODED UNDERNEATH TOP SKIN O/B OF RIB 24 ACCESS VIA PANEL 624 AB. LOCK FASTERNER COLLARS REPLACED UNDERNEATH TOP SKIN O/B OF RIB AS PER SRM 51-25-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,465 hrs · 22,340 cycles

RIGHT SEAT TRACK BETWEEN FRAME 36-39 CORRODED. REPLACED RIGHT SEAT TRACK AS PER SRM 51-25-04.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,465 hrs · 22,340 cycles

FOUND FRAME 36 FLOORBEAM CORRODED. FRAME 36 FLOOR SPLICED AS PER SRM 55-00-00.

Part: FRAME — CORRODED (RT WING) · corrosion level 2 · airframe 23,465 hrs · 22,340 cycles

AILERON CONTROL QUADRANT CORRODED RT FRAME 27 AND 28 WING RIB 1 AND 2. REPLACED QUADRANT ASSY ON AUTO-PILOT ROLL CONTROL SYSTEM IAW AMM JIC 27-11-23 RAI 10000.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,465 hrs · 22,340 cycles

FOUND FRAME 39 FLOORBEAM CORRODED. FRAME 39 FLOORBEAM REPAIRED AS PER SRM 53-00-00 FIG 450.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,465 hrs · 22,340 cycles

FOUND LT BETWEEN FRAME 36 AND 39 SEAT TRACK CORRODED. SEAT TRACK LT BETWEEN FRAME 36 AND 39 REPLACED AS PER SRM 51-25-04.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,465 hrs · 22,340 cycles

FOUND FRAME 38 FLOORBEAM CORRODED. FRAME 38 FLOORBEAM REPAIRED AS PER SRM 53-00-00 FIG 450.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,465 hrs · 22,340 cycles

GUTTER AND DOUBLER ARE CORRODED BETWEEN FRAME 13 AND 17 AT CARGO DOOR. DOUBLER BETWEEN FRAME 13 AND 17 AT CARGO DOOR REPLACED AS PER SRM 51-25-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,465 hrs · 22,340 cycles

FOUND LT FRAME 39 TO 41 SEAT TRACK CORRODED. SEAT TRACK LT FRAME 39 - 41 REPLACED AS PER SRM 51-25-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,465 hrs · 22,340 cycles

CORROSION FOUND ON LT I/B SEAT TRACK AT FRAME 17. SEAT TRACK LT I/B ON FRAME 13 - 23 REPLACED IAW SRM 51-25-04.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,465 hrs · 22,340 cycles

FOUND FRAME 39 BETWEEN STRINGER LT 21 AND RT 21 CORRODED. FRAME 39 REPAIRED AS PER SRM 53-61-40 FIG 415 WITH SECTION OF NEW FRAME SEGMENT.

Part: FIRE LOOP — FALSE ACTIVATION (RT ENGINE)

AFTER LANDING, RT ENGINE FIRE WARNING LIGHT FLASHED ON FOR ONE SECOND. CREW SHUTDOWN ENGINE AS PRECAUTIONARY ACTION. DEFERRED RT ENGINE FIRE LOOP (B) SYSTEM IAW MEL. (K)

Part: SWITCH — INTERMITTENT (CENTER PEDESTAL)

( REF NR: SDR2005064) ON TAKEOFF ROLL, THE ATPCS DID NOT ARM. TAKEOFF ABORTED. REPLACED MICROSWITCH BOX UNIT. (K)

Part: AUTOFEATHER SYS — INOPERATIVE

AUTOMATIC TAKEOFF POWER CONTROL SYSTEM (ATPCS) DID NOT ARM DURING TAKEOFF POWER. REPLACED AUTO FEATHERING UNIT. (K)

Part: O-RING — DAMAGED (HYD SYSTEM)

ON FINAL APPROACH, HYDRAULIC BLUE SYSTEM LOW PRESSURE INDICATION CAME ON. AIRCRAFT LANDED WITHOUT PROBLEM. REPLACED HYDRAULIC MODULE PRESSURE SWITCH O-RING THAT WAS FOUND LEAKING. (M)

Part: WIRE HARNESS — BURNED (FIRE DETECT SYS)

ON APPROACH INTO EIS, RT ENGINE FIRE INDICATION ILLUMINATED. ENGINE SHUTDOWN AND INDICATION DISAPPEARED. NO EMERGENCY DECLARED NEITHER EXTINGUISHER DISCHARGED. REPLACED ENGINE ELECTRIC HARNESS. (K)

Part: UNIVERSAL JOINT — LOOSE (LT MLG ASSY)

DISCREPANCY: LT MAIN GEAR SHOCK PIN OUT OF PLACE. IT WAS RUBBING WITH LT OB TIRE ASSEMBLY. REMOVED AND REPLACED LT LANDING GEAR UNIVERSAL JOINT AND PINS.

Part: SEAT TRACK — CORRODED (FRAME 31-35)

CORROSION ON LEFT AFT INBOARD SEAT TRACK, FROM FRAME 31 TO35. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS, IAW SRM 51-21-42. REMOVED AND INSTALLED SEAT TRACK IAW EO NR E9-5300-013 R4. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

FLOORBEAM 38 HAS CORROSION AROUND SCREW HOLES UPPER AND LOWER SURFACES. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-42. REMOVED AND INSTALLED FLOORBEAM IAW SRM 51-25-01. (M)

Part: SUPPORT — CORRO DED (FRAME 36-39)

SERVICE DOOR SIDE, FLOOR SUPPORT, BETWEEN FRAME 36 AND 39,HAS CORROSION. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS, IAW SRM 51-00-00. REMOVED AND INSTALLED FLOOR SUPPORT IAW SRM 52-25-01. (M)

Part: SUPPORT — CORRODED (FRAME 36-39)

PAX DOOR SIDE, FLOOR SUPPORTS, BETWEEN FRAMES 36 AND 39 HAVE CORROSION. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-61-00.REMOVED AND INSTALLED SUPPORT IAW SRM 52-25-01. (M)

Part: SUPPORT — CORRODED (FRAME 36-39)

PASSENGER DOOR, SIDE PLATE, HAS CORROSION ON DRAIN TRACK. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS, IAW SRM 53-61-00. REMOVED AND INSTALLED DRAIN TRACK IAW SRM 52-25-01. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-8 INSPECTION, FOUND THE ELFT AFT INBOARD AND OUTBOARD, AND THE LEFT FORWARD OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-8 INSPECTION, FOUND THE ELFT AFT INBOARD AND OUTBOARD, AND THE LEFT FORWARD OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (CABIN)

SAW - DURING CPCP-8 INSPECTION, FOUND THE RIGHT AND LEFT SIDE OF FLOORBEAM 36 CORRODED. REMOVED AND REPLACED FLOORBEAM. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING CPCP-8 INSPECTION, FOUND THE ELFT AFT INBOARD AND OUTBOARD, AND THE LEFT FORWARD OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: AIR DISTRIBUTION — ODOR (CABIN)

DFW - FLT 3535 - FLT ATTENDANT REPORTS AN ELECTRICAL SMOKE SMELL IN THE CABIN. INSPECTED AND FOUND NO EVIDENCE OF SMOKE/SMELL IN CABIN. ALL LIGHTS WORKING OK. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SOCKET — FAILED (CABIN)

DFW - FLT 3650 - PASSENGER ENTRANCE EMERGENCY LIGHT INOPERATIVE. RAI AIRSTAIR EMERGENCY LIGHT SOCKET ASSEMBLY. A/C RETURNED TO SERVICE. (M)

Part: MFC — FAILED (NR 2 ENGINE)

LBB - FLT 3818 - DURING BOARDING, CREW NOTICED AND SMELLED SMOKE IN CABIN, FOLLOWED BY AVIONICS SMOKE WARNING. CREW SHUTDOWN NR 2 ENGINE AND DEPLANED. REMOVED AND REPLACED NR 2 MFC AND OPS CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — FAILED (AIRSTAIR)

RAI'D LIGHT ASSY OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)