N412FE

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO DOOR) · airframe 33,220 hrs · 18,395 cycles

SOON AFTER T/O GOT ECAM ALERT FOR AFT CARGO DOOR NOT CLOSED. AFT CARGO SW FAULT AND AN AMBER DOOR LIGHT FOR AFT CARGO ON RT ECAM. ACN RELEASED FOR SERVICE IAW MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 05NOV05 MEL 52-71-01: AFT DOOR CLOSED AND LOCKED INDICATION ON ECAM DOOR PAGE, INOP. AFT DOOR VISUALLY CHECKED CLOSED AND LOCKED.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO DOOR) · airframe 33,220 hrs · 18,395 cycles

SOON AFTER T/O GOT ECAM ALERT FOR AFT CARGO NOT CLOSED AFT CRAGO SW FAULT AND AN AMBER DOOR LIGHT FOR AFT CARGO ON RT ECAM. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 05NOV05 "MEL 52-71-01: (IDENTIFY) AFT DOOR CLOSED AND LOCKED INDICATION ON ECAM DOOR PAGE INOP. AFT DOOR VISUALLY CHECKED CLOSED AND LOCKED.

Part: DOOR — MALFUNCTIONED (CARGO BAY) · airframe 33,218 hrs · 18,393 cycles

SOON AFTER T/O GOT ECAM ALERT FOR AFT CARGO NOT CLOSED AFT CARGO SW FAULT AND AN AMBER DOOR LIGHT FO R AFT CARGO ON RT ECAM. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 05NOV05 MEL 52-71-01: AFT DOOR CLOSED AND LOCKED INDICATION ON ECAM DOOR PAGE - INOP. AFT DOOR VISUALLY CHECKED CLOSED AND LOCKED. NOTE: NO CABIN PRESS PROBLEMS NOTED.

Part: PANEL — DAMAGED (RT WING) · airframe 32,097 hrs · 17,742 cycles

PANEL LAND 650KB HAS 6EA ELONGATED HOLES (RT WING). REPAIRED HOLES IAW EA 6-5710-81998 AND A310 SRM 51-40-44 FIG 1.

Part: PANEL — DAMAGED (LT WING) · airframe 32,097 hrs · 17,742 cycles

PANEL LAND 550JB HAS 1EA ELONGATED HOLE (LT WING). REPAIRED HOLE IAW EA 6-5710-81998.

Part: PANEL — DAMAGED (RT WING) · airframe 32,097 hrs · 17,742 cycles

PANEL LAND 650JB HAS 2EA ELONGATED HOLES. REPAIRED 2EA ELONGATED HOLES IAW EA 6-5710-81998

Part: PYLON — CRACKED (NR 1 ENGINE) · airframe 32,016 hrs · 17,699 cycles

NR 1 ENGINE AFT UPPER PYLON HAS CRACKED UNDER PNL 473CL. STOP DRILLED CRACK AND INSTALLED U-CHANNEL IAW A310/200 SRM 54-50-00 AND 54-54-11 FIG 201 AND 54-54-51 FIG 206 BETWEEN PYLON STA 1059 AND STA 1115.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,016 hrs · 17,699 cycles

UPPER MAIN CABIN FR48 BETWEEN TRACK D & E HAS 1EA DUMMY TRACK WITH CORROSION BEYOND REPAIRABLE LIMITS. REMOVED AND REPLACED DUMMY TRACK IAW A310 SRM 51-72-10.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,016 hrs · 17,699 cycles

UPPER MAIN CABIN BETWEEN D & E HAS 3EA DUMMY TRACK WITH CORROSION (LEVEL 2) AND 1EA DUMMY TRACK CRACKED (2 INCHES IN LENGTH) BETWEEN FR 52 AND 53. REMOVED AND REPLACED 4EA DUMMY TRACKS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,016 hrs · 17,699 cycles

MAIN CABIN CARGO FLOOR 3 AREAS OF CORROSION ON SEAT TRACKS AT FR66 AND FR67 ZONE 251 TRACK F. REMOVED DAMAGED SECTION AND INSTALLED NEW SECTION IAW SRM 53-10-16

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,016 hrs · 17,699 cycles

MDC ON RT SEAT TRACK NR 3 FR53 NOTED CORROSION INSIDE SCALLOP HOLES AND ON FLANGE. REMOVED DAMAGED SECTION AND INSTALLED NEW SECTION IAW A310/200 SRM 53-10-16.

Part: TEE FITTING — CORRODED (COCKPIT DOOR) · corrosion level 2 · airframe 32,016 hrs · 17,699 cycles

REF. SNRM N00243 MDCC T-CAP JUST AFT OF COCKPIT DOOR HAS LEVEL 2 CORROSION REMOVED CORROED T-CAP SECTION INSTALLED A SPLICE IN SECTION IAW A310/200 SRM 53- 12-15, 51-40-20, AND 51-75-10

Part: COALESCER BAG — DIRTY (CABIN AIR) · airframe 31,497 hrs · 17,378 cycles

ON TAKEOFF ROLL STRONG ODOR OF OIL OR AIR CONDITIONING SMOKE IN COCKPIT, REJECTED TAKEOFF. NO SIGN OF SMOKE COMING FROM VENTS, NO SMOKE WARNINGS, ALL INDICATIONS APPEAR NORMAL, RETURNED TO RAMP. FOUND NR 1 AND NR 2 PACK WATER SEPARATOR BAGS VERY DIRTY. REMOVED AND REPLACED WATER SEPARATOR BAGS IAW MM 21-51-16-4, OPS CHECK NORMAL. NO SIGN OF SMOKE OR OTHER SIGN OF ABNORMAL ODORS, OK FOR SERVICE.

Part: THRUST REVERSER — MALFUNCTIONED (NR 1 ENGINE) · airframe 31,237 hrs · 17,231 cycles

1 ENG ON T/O, N1 DID NOT REACH T/O PWR. ENG N1 90 PRCT. ENG 2 N1 100 PRCT. TRIED TO MATCH N1 BY PUSHING UP 1 THROTTLE WHICH CAUSED 1 EGT TO RISE TO CAUTION RANGE ABOUT 890, RETARDED THROTTLES AT THAT TIME ECAM WARNING HP VALVE FAULT -OFF, 1 HP VALVE SELECTED OFF , 1 HP VALVE SWITCH FAULT LIGHT CAME ON. ECAM ADVISORY TEMP 245 FOLLOWED BY 1 ENG LOOP B LIGHT, FOLLOWED BY NR 1 ENG FIRE INDICATION ON ECAM AND OVERHEAD PANEL. REDUCE THROTTLES TO IDLE. FIRE INDICATION WENT OUT. RETURNED TO LAND KMIA. PYLON INSPECTION SEE WRI 05-50/6316. REVERSER REMOVED AND REPLACED SEE WRI 78-30/6317. CORE COWL REMOVED AND REPLACED SEE WRI 71-10/6321.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 29,579 hrs · 16,259 cycles

AIRCRAFT WOULD NOT PRESSURIZE. NR 1 FWD AND AFT OUTFLOW VALVE INDICATED FULL OPEN. PERFORMED FUNCTIONAL CHECK OF NR 1 AND NR 2 PRESSURIZATION CONTROLLERS. NR 1 SYSTEM CONTROLLER CONTINUOUSLY SHOWS THE AIRCRAFT AT AN ELEVATION OF 400 FT WHEN IT SHOULD READ APPROX 620'. SWAPPED CONTROLLERS AND PROBLEM FOLLOWED. PUT NEW CONTROL FROM STOCK IN NR 1POSITION BUT IT WAS BAD FROM STOCK. PUT OLD ONE BACK IN POS NR 1. NEW CONTROLLER ON ORDER. REMOVED AND REPLACED RELAYS 159GB AND 144GB PER STANDARD MX PRACTICES.

Part: LIGHT — ILLUMINATED (M/D DOOR) · airframe 29,087 hrs · 15,997 cycles

02-51 AFTER T/O MAIN DECK DOOR LIGHT CAME ON. A/C RELEASED PER MEL 52-9.

Part: SYMBOL GENERATOR — INOPERATIVE (COCKPIT) · airframe 29,029 hrs · 15,973 cycles

LOST F/O'S PRIMARY FLT AND NAV DISPLAY. EFIS SGU NR 2 INOP. RELEASED PER MEL 34-7.

Part: SWITCH — FAILED (MLG)

ON T/O, L/G WOULD NOT RETRACT DESPITE SEVERAL RECYCLES ON SYS 1 AND 2 C/B'S. RESET BOX AND FAULTED SAME UNITS. REMOVED AND REPLACED PROXIMITY DETECTOR UNIT PER MM. OPS CK GOOD.

Part: RELAY — FAILED (PITOT HEAT)

99-293 - ON DEPT GDL, F/O PITOT HEAT FAILED, THEN NR 1 ATS TRIPPED. WOULD NOT RESET. REMOVED AND REPLACED NOSE GEAR RELAY 153GB IAW MM. ALL CK GOOD, OK FOR SERVICE.