N470AA

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,570 hrs · 41,618 cycles

REFERENCE WC 5403 EGRESS POWER SUPPLY AB5-3 FAILED TEST. REPLACED EGRESS POWER SUPPLY AB5-3 BATTERY PACK IAW AMM 33-60-98. TESTED OK.

Part: FRAME — CRACKED (FUSELAGE) · airframe 75,174 hrs · 40,239 cycles

CRACK IN CANTED FRAME 1463 LONGERON 18L, STOP DRILLED & INSTALLED DOUBLER IAW SRM 53-01-00-001 FIGURE 2 SHEET 4.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 75,174 hrs · 40,239 cycles

SHEAR TIE CRACKED IN RADIUS, FWD SIDE OF STATION 1380 ABOVE LONGERON 14 RT. INSTALLED DOUBLER REPAIR IAW AARD 53-10-00-20.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 72,119 hrs · 38,410 cycles

FWD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY B5-23. OPERATIONS CHECKED NORMAL.

Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 72,119 hrs · 38,410 cycles

FWD CABIN PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.

Part: CASTING — CRACKED (LE SLAT TRACK) · airframe 71,566 hrs · 38,072 cycles

RT WING NR 4 SLAT TRACK INBD CASTING CRACKED. INSTALLED NEW INBD NR 4 SLAT TRACK CASTING IAW AARD 51-00-05. REPAIR 1 & DRAWING 9937490.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,566 hrs · 38,072 cycles

EXTERNAL LONGERON 20 CRACKED IN RT WHEEL WELL. STOP DRILLED CRACK & INSTALLED DOUBLER IAW AARD 53-10-00-18.

Part: SHUTOFF VALVE — DAMAGED (HYDRAULIC SYS) · airframe 70,307 hrs · 37,368 cycles

DEN - CREW REPORTED RIGHT HYDRAULIC FLUID LOSS DURING CRUISE. EMERGENCY DECLARED FLIGHT LANDED DEN WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RUDDER SHUT OFF VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 68,757 hrs · 36,508 cycles

DFW - CREW REPORTED AT 31,000 FEET RED CABIN ALTITUDE LIGHT ILLUMINATED AND WARNING HORN WENT OFF. ACCOMPLISHED EMERGENCY DESCENT. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER ONE AND TWO PRESSURE CONTROLLERS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: TERMINAL — LOOSE (EMERGENCY LIGHT) · airframe 68,190 hrs · 36,197 cycles

OVERHEAD EMERGENCY LIGHTS FROM ROWS 12 TO 18 CAME ON WITH SWITCH OFF. TIGHTENED LOOSE TERMINALS ON BATTERY PACK B5-101. OPS CHECK NORMAL.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,939 hrs · 36,053 cycles

RIGHT CUSP STATION 913 CORRODED. INSTALLED DOUBLER PER AARD 53-10-00 REPAIR 16.

Part: CASTING — CRACKED (SPOILER) · airframe 67,939 hrs · 36,053 cycles

RIGHT WING GROUND SPOILER CENTER CASTING IS CRACKED INBOAD SIDE FORWARD END. INSTALLED DOUBLER PER AARD 57-20-00-15.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 67,939 hrs · 36,053 cycles

CRACK IN LONGERON 2 LEFT AT STATION 160. ACCOMPLISHED SPLICE REPAIR PER SRM 53-02-00 FIGURE 18.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,939 hrs · 36,053 cycles

FORWARD MEMBRANE, OUTBOARD OF NUMBER 6 SEAT TRACK, STATIONS 200 TO 218 CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-15.

Part: TRACK — CORRODED (FUSELAGE) · airframe 67,939 hrs · 36,053 cycles

CORROSION ON OUTBOARD LIPS AND CENTER OF LEFT TIEDOWN TRACK, STATIONS 1212 TO 1322. INSTALLED REPLACEMENT LEFT TIEDOWN TRACK PER AARD 51-10-00-5.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 67,939 hrs · 36,053 cycles

RIGHT CUSP AT STATION 913 CRACKED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MEMBRANE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,939 hrs · 36,053 cycles

CORROSION ON SUBFLOOR UNDER G1 GALLEY DRAIN PAN. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: STRAP — GOUGED (FUSELAGE) · airframe 67,939 hrs · 36,053 cycles

STRAP FOR STATION 1147 FRAME HAS SCREW GAUGE. INSTALLED NEW STRAP PER AARD 51-10-00-5.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 67,939 hrs · 36,053 cycles

CRACK IN LONGERON 4 LEFT AT STATION 200. ACCOMPLISHED SPLICE REPAIR PER SRM 53-02-00 FIGURE 18.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,939 hrs · 36,053 cycles

SEAT TRACK NUMBER 4 FROM STATIONS 233 TO 238 CORRODED. INSTALLED NEW SEAT TRACK NUMBER 4 FROM STATIONS 200 TO 264 PER SRM 53-05-00.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,939 hrs · 36,053 cycles

MID CARGO DOOR BEAM CORRODED. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-10-00-3.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 67,939 hrs · 36,053 cycles

CRACK IN LONGERON 4 LEFT AT STATION 200. INSTALLED NEW LONGERON 4 LEFT FROM APPROXIMATELY STATIONS 165 TO 228 PER SRM 53-02-00 FIGURE 18.

Part: MEMBRANE — CORRODED (FUSELAGE) · airframe 67,939 hrs · 36,053 cycles

FORWARD MEMBRANE, OUTBOARD OF NUMBER 6 SEAT TRACK, STATIONS 200 TO 218 CORRODED. INSTALLED REPAIR DOUBLER FROM STATIONS 200 TO 218 RIGHT BUTTLINES 46 TO 57 PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (G2 GALLEY) · airframe 67,939 hrs · 36,053 cycles

G2 GALLEY FORWARD OUTBOARD MOUNT AT STATION 215 CORRODE. INSTALLED REPLACEMENT G2 GALLEY MOUNT AT STATION 215 SEAT TRACK NUMBER 6 PER AARD 51-10-00-5.

Part: CUSP WEB — CORRODED (FUSELAGE) · airframe 67,939 hrs · 36,053 cycles

RIGHT CUSP CORRODED STATIONS 218 TO 221 OUTBOARD OF NUMBER 6 SEAT TRACK. REPLACED RIGHT CUSP SHEET FROM STATIONS 218 TO 237 PER AARD 51-10-00-5.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,939 hrs · 36,053 cycles

WEB TANG STATION 207 AT LONGERON 15 LEFT CRACKED. INSTALLED REPAIR STRAP PER AARD 53-10-00-11.

Part: WEB — CRACKED (FUSELAGE) · airframe 67,939 hrs · 36,053 cycles

WEB TANG STATION 207 AT LONGERON 11 LEFT CRACKED. INSTALLED REPAIR STRAP PER AARD 53-10-00-11.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 67,939 hrs · 36,053 cycles

CORROSION TOP OF GALLEY TIEDOWN STATION 218 12 INCHES INBOARD OF NUMBER 4 SEAT TRACK. INSTALLED NEW GALLEY MOUNT PER AARD 51-10-00-5.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 67,939 hrs · 36,053 cycles

CORROSION TOP OF GALLEY TIEDOWN STATION 210 12 INCHES INBOARD OF NUMBER 4 SEAT TRACK. INSTALLED NEW GALLEY MOUNT PER AARD 51-10-00-5.

Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 67,939 hrs · 36,053 cycles

SUBFLOOR UNDER GALLEY TIEDOWN STATION 218 12 INCHES INBOARD OF NUMBER 4 SEAT TRACK CRACKED. FABRICATED AND INTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: SENSOR — DEFECTIVE (NLG) · airframe 67,841 hrs · 36,004 cycles

PIT - CREW REPORTED NOSE LANDING GEAR FAILED TO RETRACT. EMERGENCY DECLARED FLIGHT RETURNED PIT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NOSE LOCKED GEAR SENSOR D1-32 AND CONNECTOR P1-1157. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,910 hrs · 33,844 cycles

LEFT WHALEBONE TO KEEL BEAM ANGLE CRACKED. REMOVED AND REPLACED ANGLE PER SRM 51-01-00.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 62,438 hrs · 33,061 cycles

AFT CATWALK AND OVERHEAD TAIL EMERGENCY LIGHTS INOPERATIVE DURING TEST OF EMERGENCY EVACUATION LIGHTS SYSTEM. RESEATED BATTERY PACK AND SYSTEM RECHARGED PER NORMAL OPERATION. RETEST CHECKS GOOD.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 61,833 hrs · 32,736 cycles

AFT JUMPSEAT FLASHLIGHT SECURITY STRAP BROKEN. REPLACED SECURITY STRAP.

Part: SHROUD — MISSING (CABIN) · airframe 61,556 hrs · 32,585 cycles

EMERGENCY LIGHTS AT SEAT 8D MISSING SHROUD. REPLACED SHROUD AT SEAT 8D.

Part: SHROUD — MISSING (CABIN) · airframe 61,556 hrs · 32,585 cycles

EMERGENCY LIGHT AT SEAT 24D MISSING SHROUD. REPLACED SHROUD AT SEAT 24D.

Part: SHROUD — MISSING (CABIN) · airframe 61,556 hrs · 32,585 cycles

EMERGENCY LIGHT AT SEAT 19D MISSING SHROUD. REPLACED SHROUD AT SEAT 19D.

Part: SWITCH — INOPERATIVE (OIL SYSTEM) · airframe 60,292 hrs · 31,878 cycles

TUL - INFLIGHT SAT-ORD. LEFT ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED. EMERGENCY DECLARED, LANDED TUL WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NEW FILTER. FOUND OIL DIFFERENTIAL SWITCH BAD REPLACED WITH SWI3004.

Part: RESERVOIR — LOW PRESSURE (RT HYD SYSTEM)

PHX INFLIGHT T2435/08OCT - LOST RIGHT HYDRAULIC SYSTEM. RIGHT HYDRAULIC PRESSURE LOW AND RUDDER MANUAL LIGHTS ILLUMINATED. LANDED PHX WITHOUT INCIDENT. LANDED WITH GEAR DOOR EXTENDED. INSPECTED GEAR DOORS WITH NO DAMAGE NOTED. BLED AIR FROM RIGHT HYDRAULIC RESERVOIR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: HOOK AND LOOP — INOPERATIVE (CABIN)

MSP - LEFT NUMBER ONE DOOR SLIDE HOOK AND LOOP STRIP INOPERATIVE. REPLACED LEFT NR 1 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (FLASHLIGHT)

ORD - EMERGENCY FLASHLIGHT AT FIRST CLASS INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: STRAP — BROKEN (FLASHLIGHT)

LGA - EMERGENCY FLASHLIGHT AT AFT SERVICE DOOR HAS BROKEN STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: LENS — MISSING (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHT AT SEAT 22D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY EXIT LIGHTS AT AFT STAIRWELL INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS AT AFT STAIRWELL. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SHROUD — MISSING (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHT AT SEAT 22D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MOTOR — INOPERATIVE (TRIM SYSTEM)

DFW - RUNAWAY STABILIZER TRIM. RUN WAY NOSE DOWN. STOPPED WITH CONTROL WHEEL SWITCHES IN NOSE UP. AUTOPILOT NEVER USED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED ALTERNATE STABILIZER TRIM MOTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MOTOR — INOPERATIVE (ZONE 400)

DFW - UNCOMMON NOSE DOWN PRIMARY TRIM MOVEMENTS DURING FINAL APPROACH. PRIMARY STABILIZER TRIM DISCONNECTED. REPLACED PRIMARY STABILIZER TRIM DRIVE MOTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: PROXIMITY SENSOR — INOPERATIVE (MLG)

DFW INFLIGHT T490/21AUG, NOSE LANDING GEAR INDICATION. TRIED TO RECYCLE GEAR TWO TIMES. SECOND TIME LEFT THE GEAR DOWN AND RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED PROXIMITY SENSOR FOR NOSE LANDING GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SAT - OVERHEAD EMERGENCY LIGHTS FROM ROWS 22 TO 27 INOPERATIVE. REPLACED BATTERY PACK FOR OVERHEAD EMERGENCY LIGHTS FROM ROWS 22 TO 27. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

DFW - OVERHEAD EMERGENCY LIGHTS AT ROWS 23 TO 26 INOPERATIVE. CLEANED CONTACTS AND RECHARGED BATTERY FOR OVERHEAD EMERGENCY LIGHTS AT ROWS 23 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING WAS INOPERATIVE AT SEAT ROWS 18 THROUGH 20. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: SOCKET — INOPERATIVE (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 23D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY — DISCHARGED (CABIN)

ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS ROW 18, 20, 21 AND 28 INOPERATIVE. REPLACED EMERGENCY EXIT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LANDING GEAR — VIBRATION (NOSE)

MIA - FLT 1606 - AFTER ROTATION, NOSE LANDING GEAR VIBRATIONS. DIVERTED AND LANDED MIA WITHOUT INCIDENT. ACCOMPLISHED GEAR SWING. UNABLE TO DUPLICATE DISCREPANCY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: SENSOR — DEFECTIVE (NLG)

DFW - FLT 2049 - EN ROUTE ATL-DFW - NOSE GEAR RED LIGHT FLICKERED ON CLIMB-OUT AND DURING CRUISE. LANDED DFW WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR UPLOCK SENSOR AND PSEU. ACCOMPLISHED PSEU BITE CHECK. ACCOMPLISHED SEVERAL NOSE LANDING GEAR RETRACTIONS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: AIR DIST — SMOKE (CABIN)

DFW - FLT 1955 - EN ROUTE DFW-SFO, APPROACHING 10,000 FT, CREW NOTED SMOKE ODOR IN COCKPIT, FOLLOWED BY FLIGHT ATTENDANT REPORT OF SMOKE IN CABIN. FAINT VISUAL OF SMOKE IN COCKPIT. STRONG ODOR IN CABIN. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. RAN ENGINES, OPERATED PACKS, INSPECTED ACMS, RECIRCULATING FAN AND ELECTRICAL COMPONENTS IN AIR CONDITIONING. UNABLE TO DUPLICATE OR FIND ANY DISCREPANCIES. AIRCRAFT RETURN TO SERVICE DEPENDENT ON FUNCTIONAL CHECK FLIGHT FINDINGS. PERFORMED FUNCTIONAL CHECK FLIGHT, WITH NO SMOKE NOTED. (M)