N733TW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Ameristar Air Cargo, Inc. | Operator | 2008-01-08 – 2008-01-08 | Operator named in NTSB report |
| AMERISTAR AIR CARGO, INC. (MJYA) | Operator | 2008-01-08 – 2008-01-08 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
AFT CARGO COMPT. BS 907 S25L WITH SPLICE CORRODED. THE PART CORRODED WAS REPLACED, WO Z10266, ITEM 1-79.
UPPER FUSELAGE SKIN WITH SCRATCH AT BS 846 BETWEEN S3-2R. A PERMANENT REPAIR IS REQUIRED IAW MFG REPAIR GUIDLINES UNDER WO Z10226, ITEM 2-153.
UPPER FUSELAGE BS 827 AND BS 838 BTWN S2-3L SKIN WITH SCRATCH. A PERMANENT REPAIR IS INSTALLED IAW REPAIR GUIDELINES UNDER WO Z10226, ITEM 2-134.
SECTION 43, FWD C/C BS 380 FRAME WITH UPPER FLANGE CRACKED AT S26R. A PERMANENT IS INSTALLED IAW SRM 51-40-3, FIG 1 GUIDELINES UNDER WO Z10226, ITEM 1-112.
RT WING REAR SPAR AT RSS 436 AND RSS 260 AND LT WING AT RSS 260 FLAP TRACK FITTING OTBD HOLES CORRODED. THE PARTS DAMAGED WERE REPLACEMENT, WO Z10226, ITEM'S 6-90, 5-96, 6-89.
AFT CARGO COMPT, BS 727A+2 WITH S22L CORRODED. THE PART CORRODED WAS REPLACED, WO Z10226, ITEM 1-78.
AFT CARGO COMPT BS 727A FRAME WITH SHEAR TIE CORRODED BETWEEN S-21L AND S-22L. THE PART CORRODED WAS REPLACED, WO Z10226, ITEM 1-77.
LOWER FUSELAGE AT STA 819 BETWEEN STRINGER 22L AND STRINGER 23L SKIN WITH DENT. A PERMANENT REPAIR IS INSTALLED IAW REPAIR GUIDELINES UNDER WO Z10226 ITEM 1-43.
LOWER FUSELAGE STA 774, BETWEEN STRINGER 24L AND STRINGER 25L SKIN WITH DENT. A PERMANENT REPAIR IS INSTALLED FOLLOWING MFG REPAIR GUIDELINES UNDER WO Z10226, ITEM 1-101.
LOWER FUSELAGE BS 816, STRINGER 20 SKIN WITH DENT. A PERMANENT REPAIR IS INSTALLED FOLLOWING MFG REPAIR GUIDELINES UNDER WO Z10226, ITEM 1-44.
PAX CABIN BS 1006 STRINGERS CLIP CRACKED. THE PARTS WERE REPLACED.
PAX CABIN BS 597 BETWEEN S-17L AND S-18L WITH ANGLE CRACKED. THE PART CRACKED WAS REPLACED.
UPPER FUSELAGE BS 578, RBL 65 STUB BEAM UPPER CHORD CRACKED. THE PART CRACKED WAS REPLACED.
EMERGENCY EXIT SIGN IN COCKPIT FELL OUT.
FUSELAGE SKIN WITH DENT AT BS 1043 BETWEEN STR 16LT AND STR 17LT.
AFT ENTRY DOOR UPPER HINGE SKIN CRACKED.
LEFT WING TRAILING EDGE SECTION, AILERON UPPER SURFACE SKIN DELAMINATED AT STA WBL 518.850 AND WBL 504.
LOWER FUSELAGE SKIN WITH CRACK AT BS 891, S-23RT.
LOWER FUSELAGE E&E COMPARTMENT AT BS 324, STR 28R WITH CORROSION.
LOWER FUSELAGE AFT CARGO COMPARTMENT DOOR LOWER CUTOUT FROM BS 795 TO BS 847 ANGLE CORRODED.
LOWER FUSELAGE AFT CARGO COMPARTMENT BS 887 STRINGER 24 RT CLIP CRACKED.
LOWER FUSELAGE RT MAIN WHEEL WELL AFT BULKHEAD WEB WITH CRACK IN BS 727 RBL 6 WL 160.
LOWER FUSELAGE FWD CARGO COMPARTMENT BS 440 BETWEEN STR 24 AND 25 RIGHT SIDE, FRAME CORRODED.
FORWARD ENTRY EMERGENCY EXIT LIGHT INOPERATIVE.
AFT DOOR EXTERIOR EMERGENCY LIGHTS INOPERATIVE.
CENTER AISLE EMERGENCY EXIT LIGHT AT OVERWING EXIT INOP. CHANGED BATTERY PACK.
FORWARD EMERGENCY AISLE LIGHT INOP.
AFTER TAKEOFF HYDRAULIC MASTER CAUTION LIGHT ILLUMINATED, LOST A-SYSTEM HYDRAULIC QUANTITY.
RT WING INBOARD MID FLAP TRAILING EDGE P/N: 65-71902-42, S/N BN5, DELAMINATED AT WBL 132.
RT WING, SLAT NR 4 RIB CRACKED AT SLAT STA 0.28.
BS 1016 AFT PRESSURE BULKHEAD WEB TO Y-CHORD ATTACHMENT CRACKED.
ENGINE NR 2 PYLON FWD SECTION WITH PLATE WORN.
RT WING FIXED PANEL P/N: 65-50818-316, DELAMINATED AT WS 465.
BS 1016 AFT PRESSURE BULKHEAD WEB TO "Y" CHORD ATTACHMENT CRACKED.
RT WING AT WBL STA 364, OUTBOARD MID FLAP RIB CRACKED.
FORWARD SERVICE DOORWAY AREA, STA 332 STRINGER 8R AREA, T-CLIP IS CRACKED.