N572AA

Part: DOOR — DAMAGED (NLG) · airframe 69,341 hrs · 30,732 cycles

TUS - CREW REPORTED AIRFRAME VIBRATION AT FORWARD LANDING GEAR. RETURNED TUS WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND EXTERIOR POWER NOSE GEAR DOORS WITH LOOSE HINGE PIN. REPLACED BOTH FORWARD NOSE GEAR DOORS AND ADJUSTED. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: BEAM — CRACKED (ZONE 800) · airframe 68,586 hrs · 30,409 cycles

FORWARD SERVICE DOOR HAS A CRACKED UPPER BEAM AT FORWARD END. REMOVED AND STOP DRILLED CRACK REPLACED BEAM UPPER DOOR.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 68,587 hrs · 30,409 cycles

CORROSION AND HOLE PUNCTURE IN LEFT CUSP AT STATION 853 TO 864. REPAIRED PER AARD 53-20-00-16.

Part: BEAM — CRACKED (ZONE 800) · airframe 68,586 hrs · 30,409 cycles

FORWARD ENTRY DOOR NR 2 BEAM AFT END CRACKED. STOP DRILLED, DOUBLER INSTALLED.

Part: PAN — CRACKED (ZONE 100) · airframe 68,586 hrs · 30,409 cycles

AFT CARGO DOOR PAN CRACKED. DOUBLER INSTALLED.

Part: ANGLE — CRACKED (ZONE 100) · airframe 68,586 hrs · 30,409 cycles

FORWARD CARGO DOOR LOWER STOP ANGLE CRACKED. REMOVED AND REPLACED ANGLE.

Part: FRAME — CRACKED (ZONE 100) · airframe 68,586 hrs · 30,409 cycles

LEFT OVERWING FUSELAGE FRAME CRACKED STATION 864. REMOVED AND REPLACED LEFT STATION 864 FRAME PER SRM 51-01-00.

Part: ANGLE — CRACKED (ZONE 800) · airframe 68,587 hrs · 30,409 cycles

CARGO DOOR LOWER STOP ANGLE CRACKED. INSTALLED SERVICEABLE ANGLE.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 68,587 hrs · 30,409 cycles

CORROSION ON LEFT CUSP AT STATION 237 TO 256. REPAIRED PER AARD 53-20-00-16.

Part: ANGLE — CORRODED (ZONE 100) · airframe 68,587 hrs · 30,409 cycles

AFT CARGO DOOR THRESHOLD CHORD ANGLE CORRODED FROM STATION 1155 TO 1212. REPLACED BEAM PER AARD 53-10-00-3.

Part: MOUNT — CORRODED (ZONE 100) · airframe 68,587 hrs · 30,409 cycles

CABIN, CORROSION ON G-2 GALLEY AFT INBOARD FLOOR MOUNT. REPLACED GALLEY MOUNT.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 68,587 hrs · 30,409 cycles

CORROSION ON NUMBER 2 SEAT TRACK STATION 1194 TO 1202. REPLACED SECTION OF SEAT TRACK FROM STATION 1183 TO 1224.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 68,587 hrs · 30,409 cycles

CABIN, CORROSION ON LEFT CUSP AT STATION 1055 TO 1060. INSTALLED A SERVICEABLE CUSP SHEET FROM 1022 TO 1098.

Part: ANGLE — CORRODED (ZONE 100) · airframe 68,587 hrs · 30,409 cycles

MID-CARGO, CORROSION ON CARGO DOOR CUTOUT THRESHOLD CHORD ANGLE STATION 636 TO 680. REPAIRED PER AARD 53-10-00-3.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 68,587 hrs · 30,409 cycles

CABIN, NUMBER 5 SEAT TRACK OUT OF LIMITS AT STATION 233 TO 237. INSTALLED NEW SECTION OF SEAT TRACK FROM STATION 200 TO 245.

Part: TEE FITTING — CORRODED (ZONE 100) · airframe 68,587 hrs · 30,409 cycles

AFT CARGO, CORROSION ON TEE FITTING STATION 1155 LONGERON 28R. INSTALLED SERVICEABLE TEE FITTING PER SRM 51-01-00.

Part: STRUCTURE — CRACKED (ZONE 100) · airframe 68,587 hrs · 30,409 cycles

CRACK IN SUBFLOOR AT STATION 200. REPAIRED PER AARD 53-20-00-16.

Part: MOUNT — CORRODED (ZONE 100) · airframe 68,587 hrs · 30,409 cycles

CABIN, CORROSION ON G-2 GALLEY AFT INBOARD MOUNT UNDER SUBFLOOR. INSTALLED A SERVICABLE MOUNT PER SRM 51-01-00.

Part: ANGLE — CRACKED (ZONE 100) · airframe 68,587 hrs · 30,409 cycles

AFT ACCESSORY, CRACK IN TEE ANGLE BELOW PIVOT OF VENTRAL STAIRS TORQUE TUBE, LEFT SIDE BETWEEN CANT FRAME 1485 AND 1497. INSTALLED SERVICABLE ANGLE PER SRM 51-01-00.

Part: LONGERON — CRACKED (ZONE 200) · airframe 68,587 hrs · 30,409 cycles

LONGERON 4L CRACKED AT STATION 200. REPAIRED PER SRM 53-02-00.

Part: CUSP WEB — CRACKED (ZONE 100) · airframe 68,587 hrs · 30,409 cycles

CABIN, 2 CRACKS IN LEFT CUSP AT STATION 223 TO 227. INSTALLED SERVICEABLE CUSP SHEET.

Part: MOUNT — CORRODED (ZONE 100) · airframe 68,587 hrs · 30,409 cycles

CABIN, G-1 GALLEY INBOARD MOUNT CORRODED AT STATION 160. REMOVED AND INSTALLED A SERVICEABLE MOUNT.

Part: CUSP WEB — CRACKED (ZONE 100) · airframe 68,587 hrs · 30,409 cycles

CABIN, CRACK IN RIGHT CUSP STATION 218. REPAIRED PER AARD 53-20-00-16.

Part: INTERCOSTAL — CRACKED (ZONE 100) · airframe 68,587 hrs · 30,409 cycles

AFT CARGO, INTERCOSTAL CRACKED AT FASTENER HOLES STATION 1287 TO 1309 (CEILING CENTER). INSTALLED A SERVICEABLE INTERCOSTAL.

Part: ANGLE — CRACKED (ZONE 200) · airframe 68,587 hrs · 30,409 cycles

AFT ACCESSORY, ANGLE CRACKED ON AFT END, ABOVE ELEVATOR ACCUMULATOR CUTOUT, CANT FRAME STATION 1474. REMOVED AND INSTALLED A SERVICEABLE ANGLE PER SRM 51-01.

Part: SEAT TRACK — CRACKED (ZONE 100) · airframe 68,587 hrs · 30,409 cycles

CABIN, NUMBER 4 SEAT TRACK HAS BROKEN EAR AT STATION 980. INSTALLED REPAIR PLUG PER AARD 53-20-00-10.

Part: CUSP WEB — CORRODED (ZONE 100) · airframe 68,587 hrs · 30,409 cycles

CORROSION ON CUSP STATION 201. REPAIRED PER AARD53-20-00-16.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 68,587 hrs · 30,409 cycles

FORWARD ENTRY DOOR JAMB, AFT WEB CRACKED AT STATION 208. REPAIRED PER AARD 53-10-00-11.

Part: MOUNT — CORRODED (ZONE 100) · airframe 68,587 hrs · 30,409 cycles

CABIN, CORROSION ON G-2 GALLEY FORWARD INBOARD FLOOR MOUNT STATION 207. INSTALLED SERVICEABLE GALLEY MOUNT PER SRM 51-01.

Part: SEAT TRACK — BROKEN (ZONE 100) · airframe 68,586 hrs · 30,409 cycles

NUMBER 6 SEAT TRACK TANG BROKEN AT STATION 672 TO 673. INSTALLED NEW SEAT TRACK PER AARD 53-20-00-10.

Part: SEAT TRACK — BROKEN (ZONE 100) · airframe 68,586 hrs · 30,409 cycles

NUMBER 4 SEAT TRACK TANG BROKE OFF STATION 948-949. INSTALLED NEW SEAT TRACK PER AARD 53-20-00-10.

Part: SEAT TRACK — BROKEN (ZONE 100) · airframe 68,586 hrs · 30,409 cycles

NR 4 SEAT TRACK ATTACH LUG BROKEN OFF AT STATION 672. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 68,586 hrs · 30,409 cycles

CABIN, CENTER FLOORBOARD SUPPORT IS CRACKED AT STATION 905. REMOVED AND REPLACED SUPPORT WITH SERVICEABLE SUPPORT.

Part: LONGERON — CORRODED (ZONE 100) · airframe 68,587 hrs · 30,409 cycles

CORROSION ON LONGERON 30 STATION 218 TO 225. REPLACED 18 INCHES OF LONGERON 30 PER SRM 53-14-01.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

BOS - EMERGENCY EXIT LIGHT AT SEAT ROW 8 INOPERATIVE. REPAIRED CONNECTOR FOR EMERGENCY EXIT LIGHT AT SEAT ROW 8. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)

BOS - EMERGENCY EXIT LIGHT AT SEAT ROW 31 INOPERATIVE. REPAIRED CONNECTOR FOR EMERGENCY EXIT LIGHT AT SEAT ROW 31. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE)

STL INFLIGHT T335/26JAN ORD TO SAT. UNABLE TO MAINTAIN PRESSURIZATION MANUALLY. BOTH PRESSURIZATION AUTO CONTROLLERS WERE INOPERATIVE. ALL OXYGEN MASKS DROPPED. LANDED STL WITHOUT INCIDENT. REPLACED NUMBER ONE AND TWO CABIN PRESSURE CONTROLLERS AND OUTFLOW VALVE ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

ORD - EMERGENCY LIGHTS IN CEILING ABOVE SEATS 19, 20, AND 21DEF INOPERATIVE. REPLACED BATTERY PACK B5104 FOR EMERGENCY LIGHTS IN CEILING ABOVE SEATS 19, 20, 21DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SENSOR — OUT OF ADJUST (MLG)

ORD - INFLIGHT ON GEAR RETRACTION NOSE GEAR INDICATOR REMAINED RED. DOORS REMAINED OPEN (AIR NOISE). NOSE LANDING GEAR INDICATED RETRACTED. STALL INDICATED FAILURE AND AUTO SPOILER DO NOT USE ILLUMINATED. PERFORMED FULL STRUT SERVICE. JACKED NOSE GEAR AND SWUNG NOSE GEAR SEVERAL CYCLES. ADJUSTED NOSE GEAR LOCK SENSOR GAP. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

SEA - AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (CABIN)

ORD - LAST ROWS OF EMERGENCY LIGHTS REMAIN ON WHEN A/C IS POWERED DOWN. REPLACED BATTERY PACK AND CHARGER FOR AFT SEAT LIGHTS AB-5. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: MODULE — INOPERATIVE (CABIN)

ORD - EMERGENCY PATH SEAT LIGHTING FROM SEATS 20D-29D IS DIM. REPLACED MODULE AND BATTERY FOR EMERGENCY PATH SEAT LIGHTING FROM SEATS 20D-29D. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DAMAGED (EMERGENCY LIGHT)

EGRESS EMERGENCY LIGHT AT ROW 16 INOPERATIVE. SPLICED WIRES UNDER SEAT FOR EMERGENCY EGRESS LIGHT AT ROW 16. SYSTEM GROUND CHECKED NORMAL OPERATION. CLOSED

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

DURING OVERNIGHT MAINTENANCE, FOUND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED TAILCONE EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY B5-28. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WIRE — INOPERATIVE (EMERGENCY LIGHT)

DFW - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 14D INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: DUCT (AFT ACCESSORY)

ORD - FLT 1666 - EN ROUTE ORD-ALB, TAIL COMPARTMENT HIGH TEMP LIGHT ILLUMINATED DURING CLIMB-OUT AT 24,000 FEET. RETURNED AND LANDED ORD WITHOUT INCIDENT. REPLACED UPPER RETURN SYSTEM AIR CONDITIONING DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WEB — CORRODED (FUSELAGE)

TUL - FOUND CORROSION ON SUBFLOOR AT APPROX STATION 188 UNDER FLOORBOARD SUPPORT ANGLE AT FORWARD ENTRY DOOR. INSTALLED DOUBLER PER AARD 53-00-00-02 AND SRM 53-01 FIG 4 SHEET 3. (M)

Part: DOOR FRAME — GOUGED (FUSELAGE)

TUL - FOUND GOUGE IN LIGHTENING HOLE AROUND DOOR CUTOUT, STATION 629-636 STRINGER 24R. REPAIRED GOUGE PER SRM 51-70-4 (WEB). (M)

Part: WEB — DAMAGED (FUSELAGE)

TUL - FOUND TOOLING MARKS IN WEB, VERTICAL, STATION 905 LBL 51.5. INSTALLED DOUBLER PER SRM 51-70-4. (M)

Part: DOOR FRAME — WORN (FUSELAGE)

TUL - FOUND FORWARD DOOR STOP HOLE IN DOOR BEAM IS WORN, BS 655. INSTALLED DOUBLER AND HI-LOCKS PER AARD 53-10-00-16. (M)

Part: FRAME — DAMAGED (FUSELAGE)

TUL - FOUND FRAME WORN STATION 1418 AT LONGERON 21R. BLENDED OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-03. (M)

Part: SKIN — DAMAGED (FUSELAGE)

TUL - FOUND AREA OF DAMAGE FUSELAGE SKIN WITH DENT AND GOUGES STATION 251 LONGERON 3L INTERIM REPAIR (PREVIOUSLY), ACCOMPLISHED PER SRM 53-04. REMOVED CLASS 3 REPAIR DOUBLER AND INSTALLED INTERNAL FINGER DOUBLER AND EXTERNAL DOUBLER PER SRM 53-04 FIG 38 SHEET 25. (M)

Part: WEB — CRACKED (FUSELAGE)

TUL - FOUND CRACK BETWEEN LIGHTENING HOLES ON RIGHT CUSP AT 1302 9 INCHES INBOARD OF FUSELAGE. INSTALLED DOUBLER PER SRM 53-01 AND AARD 53-00-00-02. (M)

Part: FRAME — CHAFED (FUSELAGE)

TUL - FOUND WEAR MARK IN FRAME FROM HYD LINE CLAMP. BLENDED OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-03 FIG 5. (M)

Part: FRAME — DENTED (FUSELAGE)

TUL - FOUND DENT IN RADIUS OF BELL FRAME STATION 1098 3 INCHES LEFT OF NR 1 LONG. INSTALLED DOUBLER REPAIR STATION 1098 PER AARD 53-10-00-14. (M)

Part: SEAT TRACK — CORRODED (CABIN)

TUL - FOUND CORROSION ON SEAT TRACK NR 4 AT STATION 234-235. BLENDED OUT CORROSION PER SRM 51-10-3. INSTALLED PLUG REPAIR PER SRM 53-05 FIG 4A ALODINED AND PRIMED PER SRM 51-10-3. (M)

Part: COALESCER — DIRTY (ACM BAY)

DFW - FLT 1887 - DURING TAKEOFF, STRONG SMELL AND HAZE IN CABIN AND COCKPIT. DISSIPATED IN CLIMB. REMOVED AND REPLACED WATER SEPARATOR BAGS. ACCOMPLISHED PACK BURN. NO ODORS NOTED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — LOOSE (CABIN)

SFO - DURING OVERNIGHT CHECK, FLOOR TRACK EMERGENCY LIGHTS AT FORWARD GALLEY TO ROW 20D ARE INTERMITTENT. RECONNECTED AND LOCKED DETACHED STRIP LIGHT CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: LIGHT — BROKEN (CABIN)

ORD - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 7 AND 12 FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BETWEEN PASSENGER SEAT ROWS 7 AND 12. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)

Part: CONNECTOR — LOOSE (CABIN)

PHX - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 7D AND 12D INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 12D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: CONNECTOR — BROKEN (CABIN)

DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY FORWARD GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)