N737TW

Part: FIRE WARNING — ACTIVATED (COCKPIT) · airframe 71,754 hrs · 65,611 cycles

FLIGHT 9604 - WHILE EN ROUTE (CRUISE) FROM ATL TO ADS AN UNSCHEDULED LANDING IN SHV WAS ENCOUNTERED DUE TO NR 1 ENGINE FIRE LIGHT ILLUMINATION AND THE FIRE BELL RINGING. FOLLOWED THE AAC QRH MEMORY ITEMS AND UPON PULLING FIRE HANDLE THE LIGHT EXTINGUISHED. DECLARED EMERGENCY AND DIVERTED TO SHV. UPON LANDING FIRE AND RESCUE DID NOT OBSERVE ANY FIRE OR SMOKE.

Part: CSD — OVERTEMP (NR 1 ENGINE) · airframe 71,685 hrs · 65,563 cycles

DURING CLIMB, THE NR 1 CSD HIGH OIL TEMP LIGHT ILLUMINATED.

Part: GEARBOX — LEAKING (NR 1 ENGINE) · airframe 71,565 hrs · 65,490 cycles

DURING CRUISE ENGINE OIL QUANTITY DROPPED TO ZERO.

Part: GROUND STUD — DETACHED (BATTERY) · airframe 70,818 hrs · 65,011 cycles

BATTERY VOLTS BELOW MINIMUMS FOUND GROUND LUG DETACHED FROM FORMED SECTION REPAIRED FORMED SECTION IAW BOEING SRM 51-40-3 PG 5 FIG 1 SHEETS 1-5.

Part: FLAP TRACK — CORRODED (LT WING) · airframe 70,152 hrs · 64,582 cycles

LT WING OB FLAP OUTBD TRACK AFT ATTACH BOLT HOLE CORRODED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 70,152 hrs · 64,582 cycles

NUMEROUS CRACKS AT FWD PRESSURE BULKHEAD BS 178.

Part: CARRIAGE — CORRODED (TE FLAP) · airframe 70,152 hrs · 64,582 cycles

RT OUTBD FLAP OUTBD CARRIAGE SPINDLE CORROSION AROUND BOLT HOLE.

Part: SKIN — DELAMINATED (E/E BAY DOOR) · airframe 70,152 hrs · 64,582 cycles

RT AC BAY DOOR DELAMINATED FROM BS 556 TO BS 596.

Part: SKIN — DELAMINATED (RT WING AILERON) · airframe 70,152 hrs · 64,582 cycles

RT WING AILERON DELAMINATED AT WBL 481

Part: PANEL — DELAMINATED (LT WING) · airframe 70,152 hrs · 64,582 cycles

L MLG T/E UPPER FIXED PANEL DELAMINATED ON UPPER AND LOWER SKIN.

Part: ACOUSTIC PANEL — CORRODED (NR 1 ENGINE) · airframe 70,152 hrs · 64,582 cycles

NR 1 ENG NOSE COWL ACOUSTIC PANEL CORRODED 6 TO 9 O'CLOCK.

Part: PANEL — CORRODED (RUDDER) · airframe 70,152 hrs · 64,582 cycles

RUDDER PANEL CORRODED STA 86-59, STA 121-64.

Part: ACCESS PANEL — CRACKED (LT WING TE FLAP) · airframe 70,152 hrs · 64,582 cycles

LT WING TE MID FLAP ACCESS PANEL CRACKED AT WBL 127.

Part: PANEL — DELAMINATED (LT WING TE FLAPS) · airframe 70,152 hrs · 64,582 cycles

LT WING INBD TE MID FLAP PANEL DELAMINATED AT WBL 121.

Part: DOOR — DELAMINATED (A/C BAY) · airframe 70,152 hrs · 64,582 cycles

LT AC BAY DOOR DELAMINATED AT BS 634.

Part: SPLICE PLATE — CRACKED (FLOORBEAM) · airframe 70,152 hrs · 64,582 cycles

SPLICE PLATE CRACKED BS 540 AT S21L-S22L.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 70,152 hrs · 64,582 cycles

INTERCOSTAL CRACKED BS 178-188 AT WL 195 L/R.

Part: ATTACH FITTING — CRACKED (TE FLAP) · airframe 70,152 hrs · 64,582 cycles

RT IB FLAP IB TORQUE TUBE ATTACH FITTING CRACKED.

Part: GIMBAL JOINT — CRACKED (LT FLAP CARRIER) · airframe 70,152 hrs · 64,582 cycles

LT WING IB FLAP OB CARRIER GIMABL CRACKED.

Part: SUPPORT — CRACKED (RT TE FLAP) · airframe 70,152 hrs · 64,582 cycles

RT IB FLAP OB GIMBAL SUPPORT CRACKED.

Part: STATIC WICK — CORRODED (HORIZONTAL STAB) · airframe 70,152 hrs · 64,582 cycles

STATIC WICK BASE CORRODED ON RT HORIZ STAB.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 70,152 hrs · 64,582 cycles

RIB CRACKED RT HORIZ STAB LE STA 109.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 70,152 hrs · 64,582 cycles

INTERCOSTAL CORRODED BETWEEN BS727A-727B AT S25L-26L.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 70,152 hrs · 64,582 cycles

FLOOR SUPPORT ANGLE CRACKED BS 947.5 RBL16.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,152 hrs · 64,582 cycles

ANGLE CRACKED AT BS 251.6 LBL 29.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,152 hrs · 64,582 cycles

ANGLE CRACKED AT BS 727B LBL 24 FLOORBEAM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 70,152 hrs · 64,582 cycles

FLOOR SUPPORT ANGLE CORRODED BS 947.5 LBL33.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 70,152 hrs · 64,582 cycles

ANGLE CRACKED RBL 24 AT FLOORBEAM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 70,152 hrs · 64,582 cycles

SUPPORT ANGLE CRACKED BS 727+4 BETWEEN S23R-S24R.

Part: SKIN — CRACKED (FUSELAGE) · airframe 69,627 hrs · 64,233 cycles

ONE CRACK EMINATING FROM RIVET HOLE IN SKIN PANEL APPROXIMATELY 0.125 INCH IN LENGTH AT BS 258 BETWEEN S-19L AND S-20L. REPLACED SKIN PANEL FROM BS223 TO BS259.5 S-19L TO S-24L PER BOEING MESSAGE CGG-ADS-03-00005H. FAA FORM 8110-3 ISSUED.

Part: TANK — OVERSERVICED · airframe 68,909 hrs · 63,789 cycles

On departure aircraft was notified by the Tower that aircraft was streaming fuel out of left wing tip area, Fuel stream was verified and called for immediate return to YIP. Declared an emergency. Landed normal not high energy stop or overweight. Maitenance determined that center wing tank had been overfueled. Sumped Surge tanks on both wings and inspected for leaks. System checked normal.

Part: SKIN — CORRODED (RT WING)

RIGHT WING CENTER SECTION, LOWER SKIN CORRODED.

Part: DOUBLER — DELAMINATED (FUSELAGE)

LOWER NOSE COMPARTMENT, BONDED DOUBLER WITH DELAMINATION, FROM BS 241 TO BS 247, BETWEEN RBL 17 AND RBL 20.

Part: STRINGER — CORRODED (FUSELAGE)

FORWARD CARGO COMPARTMENT STRINGER 19R CORRODED, AT BS 500A+14.

Part: SKIN — CRACKED (FUSELAGE)

FUSELAGE SKIN, HOLES CRACKED AND MISSING MATERIAL AT UPPER SKIN, LAP JOINT AREA.

Part: SKIN — DELAMINATED (RT MLG DOOR)

RIGHT WING, MAIN LANDING GEAR INNER DOOR PN 6552201, SN BN 325 INNER SKIN DELAMINATED.

Part: DOUBLER — DELAMINATED (FUSELAGE)

CARGO CABIN BONDED DOUBLER WITH DELAMINATION, FROM BS 927 TO BS 947 AND BETWEEN STR 14L AND STR 15L.

Part: BULKHEAD — CRACKED (FUSELAGE)

FUSELAGE, PRESSURE BULKHEAD WEB WITH CRACK AT BS 178, WL 233.5 BETWEEN RBL 10 AND RBL 13.

Part: DOUBLER — DELAMINATED (FUSELAGE)

CARGO CABIN BONDED DOUBLER WITH DELAMINATION AT BS 937 AND BETWEEN STR 6R AND STR 7R.

Part: FRAME — CRACKED (FUSELAGE)

MAIN CARGO CABIN FRAME CRACKED AT BS 277, BETWEEN S9L, AND S10L.

Part: FLOORBEAM — CORRODED (FUSELAGE)

MAIN CARGO CABIN FLOOR BEAM WITH CORROSION AT BS 312, LBL 58, WL 204.

Part: ANGLE — CORRODED (FUSELAGE)

ELECTRONIC EQUIPMENT COMPARTMENT AT STA 352, STR 27R ANGLE WITH CORROSION.

Part: BEAM — CRACKED (ENTRY DOOR)

AFT ENTRY DOOR BEAM NR 2, INSIDE CHORD CRACKED.

Part: BULKHEAD — CRACKED (FUSELAGE)

BS 1016, BULKHEAD WEB CRACKED.

Part: DOUBLER — DELAMINATED (FUSELAGE)

CARGO CABIN BONDED DOUBLER WITH DELAMINATION, FROM BS 995 TO BS 1006 AND BETWEEN STR 8L AND STR 10L.

Part: DOUBLER — DELAMINATED (FUSELAGE)

CARGO CABIN BONDED DOUBLER WITH DELAMINATION, FROM BS 639 TO BS 655 AND BETWEEN STR 9L AND STR 8L.

Part: DOUBLER — DELAMINATED (FUSELAGE)

CARGO CABIN BONDED DOUBLER WITH DELAMINATION, FROM BS 995 TO BS 1006 AND BETWEEN STR 8R AND STR 10R.

Part: RIB — CRACKED (T/E FLAP)

RIGHT WING, INBOARD MID FLAP RIB CRACKED AT WBL 120.24.

Part: DOUBLER — DELAMINATED (FUSELAGE)

LOWER NOSE COMPARTMENT, BONDED DOUBLER WITH DELAMINATION, FROM BS 211 TO BS 203, BETWEEN LBL 16 AND LBL 20.

Part: DOUBLER — DELAMINATED (FUSELAGE)

CARGO CABIN BONDED DOUBLER WITH DELAMINATION, FROM BS 500 TO BS 500A AND BETWEEN STR 3L AND STR 6L.

Part: FRAME — CORRODED (FUSELAGE)

LOWER NOSE COMPARTMENT, AT BS 222, WL 168, LBL 18 FRAME WITH CORROSION.

Part: BULKHEAD — CRACKED (FUSELAGE)

UPPER FUSELAGE AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6L, AT AFT FASTENER ROWS ATTACHMENT TO THE Y CHORD.

Part: DOUBLER — CRACKED (FUSELAGE)

MAIN CARGO CABIN, FORWARD ENTRY DOOR UPPER HINGE CUTOUT INTERNAL DOUBLER WITH CRACK.

Part: SKIN — DELAMINATED (AILERON)

RIGHT WING, AILERON PN 65-46454-2, SN 306 UPPER SKIN WITH DELAMINATIONS.

Part: RIB — CRACKED (T/E FLAP)

LEFT WING, INBOARD MID FLAP RIB CRACKED AT WBL 86.74.

Part: SKIN — DELAMINATED (T/E FLAP)

RIGHT WING, OUTBOARD FLIPPER FLAP, PN 6571950, SN BN-137 SKIN DELAMINATED.

Part: SKIN — DELAMINATED (RT SPOILER)

RIGHT WING, FLIGHT SPOILER NR 6, PN 65-79952-7 UPPER AND LOWER SKIN WITH DELAMINATIONS.

Part: RIB — CRACKED (T/E FLAP)

RIGHT WING, INBOARD MID FLAP RIB CRACKED AT WBL 86.74.