N903AR

BOEING 747-428F No injuries — Skylease Cargo

Operated by Skylease Cargo (per NTSB report)

Not yet finalized — may be revised.

PIPER PA-23 No injuries Part 91 — operator not named in the NTSB record

ATA 5310

Part: DOOR FRAME — PUNCTURED (ZONE 100) · airframe 82,978 hrs · 11,949 cycles

DURING INSPECTION OF AFT CARGO DOOR, FOUND FRAME PUNCTURE HOLE AND CRACK ON AFT SECTION OF CARGO DOOR SKIN.

ATA 5310

Part: SPAR — CORRODED (ZONE 100) · airframe 82,978 hrs · 11,949 cycles

LOWER FUSELAGE CENTER WING, FRONT SPAR AT STA RBBL 127.50, LOWER PANEL CORROSION.

ATA 5230

Part: SKIN — PUNCTURED (ZONE 800) · airframe 82,978 hrs · 11,949 cycles

DURING INSPECTION OF AFT CARGO DOOR, FRAME FOUND PUNCTURED HOLE AND CRACK ON AFT SECTION OF CARGO DOOR SKIN.

ATA 2810

Part: FUEL TANK — CORRODED (CENTER) · airframe 82,978 hrs · 11,949 cycles

LOWER FUSELAGE LEFT CENTER TANK STA. 987 (APROX), SHOWS CORROSION ,MKD 66, FWD SPAR.

ATA 5330

Part: SKIN — CORRODED (ZONE 100) · airframe 82,978 hrs · 11,949 cycles

LOWER FUSELAGE CENTER WING FRONT SPAR AT STA. RBBL 127.50, LOWER PANEL CORROSION.

ATA 5310

Part: SPAR — CORRODED (ZONE 100) · corrosion level 2 · airframe 82,978 hrs · 11,949 cycles

LOWER FUSELAGE AT LH AND RH FWD SPAR OF CENTER TANK AT STA. 987 (APROX), SHOWS CORROSION.

ATA 2121

Part: FAN — FAILED (ZONE 100)

DURING T/O CLIMB , ELECTRICAL ODOR FOLLOWING BY " EE CLNG SUPP FAN" ON STATUS PAGE.-

ATA 4940

Part: STARTER — DAMAGED (APU) · airframe 53,931 hrs · 7,439 cycles

AIRCRAFT WAS BEING PREPARED FOR DEPARTURE. APU WAS STARTED AND APPROXIMATELY 5 MINUTES LATER, THE APU FIRE INDICATION ACTIVATED AND THE FLIGHT CREW PULLED THE APU FIRE T-HANDLE. THE APU FIRE BOTTLE HAD ALREADY AUTOMATICALLY ACTIVATED. UPON INSPECTION OF THE APU AND ITS AREA WAS FOUND THAT THE STARTER HAD BROKEN LOOSE AT ITS MOUNTING AT THE APU. IT APPEARED THAT AS A RESULT OF THE STARTER'S MOVEMENT UPON BREAKING LOOSE, IT DAMAGED A FUEL LINE, WHICH CAUSED A FUEL LEAK, WHICH IN TURN CAUSED THE FIRE. THE FIRE WAS EXTINGUISHED BY THE FIRE SUPPRESSION SYSTEM. AS A RESULT OF THE FIRE, THE RT INBD ELEVATOR WAS DAMAGED, AS WELL AS BOTH OF THE APU LOWER ACCESS DOORS. THE APU DOORS WERE R & R, AS WAS THE RT INBD ELEVATOR. THE APU WAS DEACTIVATED AND DEFERRED, AND WILL BE R & R UPON THE AIRPLANE'S ARRIVAL. TROUBLESHOOTING IS CURRENTLY IN PROGRESS TO DETERMINE THE CAUSE OF THE STARTER FAILURE.

ATA 2160

Part: CONTROLLER — INOPERATIVE (CABIN TEMP) · airframe 53,520 hrs · 7,364 cycles

DURING CRUISE, UPPER CABIN AND ALL DECKS TEMPERATURE EXCEEDED 60 DEGREES C. RETURNED TO DEPARTURE. EMERGENCY NOT DECLARED. TROUBLESHOOTING FOUND A DEFECTIVE ZONE TEMPERATURE CONTROLLER. CONTROLLER WAS REMOVED AND REPLACED, OPERATIONAL SYSTEM CHECK SATISFACTORILY PERFORMED PER AMM 21-61-01 AND 21-61-00, AIRPLANE RETURNED TO SERVICE.

ATA 3442

Part: RADAR — MALFUNCTIONED (WX) · airframe 49,601 hrs · 6,558 cycles

AFTER TAKEOFF ALL SYSTEMS WERE NORMAL. ONCE A RT TURN HEADING 120 DEGREES WAS INITIATED, THE CREW RECEIVED A "RADAR FAIL" MESSAGE WHILE IN THE TURN. AFTER A CLIMB OF 10,000 FT, THE CREW WAS UNSUCCESSFUL IN FIXING THE PROBLEM. AFTER DISCUSSING THE DUAL RADAR FAILURE WITH THE FLIGHT FOLLOWER THE CREW DECIDED TO RETURN TO DEPARTURE DUE TO NIGHT OPERATIONS AND WEATHER FORECASTED ALONG ROUTE AND AT DESTINATION. NO FUEL DUMP WAS REQUIRED. R & R WEATHER RADAR ANTENNA IAW AMM 34-34-03, OPS CHECK GOOD AND TEST PASSED.

ATA 3297

Part: WIRE — CHAFED (LT MLG) · airframe 48,546 hrs · 6,330 cycles

THE CREW REPORTED THAT AFTER TAKEOFF, ATTEMPTED TO RAISE THE GEAR AND AN EICAS MESSAGE "GEAR TILT" DISPLAYED. FOLLOWED THE QRH PROCEDURES, LANDED WITHOUT ANY FURTHER INCIDENT. REPAIRED CHAFED WIRE AT LT WING LANDING GEAR JUNCTION BOX. OPS CHECKED NORMAL.