N733TW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| AMERISTAR AIR CARGO, INC. (MJYA) | Operator | on 2008-01-08 | Operator named in NTSB report |
Accident & incident history
Operated by Ameristar Air Cargo, Inc. (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
36 reports on file, 2005-09-19 – 2011-10-05.
Part: SKIN — SCRATCHED (BS 846) · airframe 73,218 hrs · 79,758 cycles
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.
Part: STRINGER — CORRODED (BS 727 S22L) · corrosion level 2 · airframe 73,218 hrs · 79,758 cycles
AFT CARGO COMPT, BS 727A+2 WITH S22L CORRODED. THE PART CORRODED WAS REPLACED, WO Z10226, ITEM 1-78.
Part: STRINGER SPLICE — CORRODED (BS 907 S25R) · corrosion level 2 · airframe 73,218 hrs · 79,758 cycles
AFT CARGO COMPT. BS 907 S25L WITH SPLICE CORRODED. THE PART CORRODED WAS REPLACED, WO Z10266, ITEM 1-79.
Part: FITTING — CORRODED (ZONE 600) · corrosion level 2 · airframe 73,218 hrs · 79,758 cycles
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.
Part: FRAME — CRACKED (ZONE 100) · airframe 73,218 hrs · 79,758 cycles
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.
Part: SHEAR TIE — CORRODED (BS 727A S21-22L) · corrosion level 2 · airframe 73,218 hrs · 79,758 cycles
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.
Part: SKIN — SCRATCHED (ZONE 200) · airframe 73,218 hrs · 79,758 cycles
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.
Part: SKIN — DENTED (ZONE 100) · airframe 73,218 hrs · 79,758 cycles
LOWER FUSELAGE BS 816, STRINGER 20 SKIN WITH DENT. A PERMANENT REPAIR IS INSTALLED FOLLOWING MFG REPAIR GUIDELINES UNDER WO Z10226, ITEM 1-44.
Part: SKIN — DENTED (ZONE 100) · airframe 73,218 hrs · 79,758 cycles
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.
Part: SKIN — DENTED (ZONE 100) · airframe 73,218 hrs · 79,758 cycles
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.
Part: ANGLE — CRACKED (ZONE 100) · airframe 73,218 hrs · 79,758 cycles
PAX CABIN BS 597 BETWEEN S-17L AND S-18L WITH ANGLE CRACKED. THE PART CRACKED WAS REPLACED.
Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 73,218 hrs · 79,758 cycles
PAX CABIN BS 1006 STRINGERS CLIP CRACKED. THE PARTS WERE REPLACED.
Part: BEAM — CRACKED (ZONE 200) · airframe 73,218 hrs · 79,758 cycles
UPPER FUSELAGE BS 578, RBL 65 STUB BEAM UPPER CHORD CRACKED. THE PART CRACKED WAS REPLACED.
Earlier reports · 2005–2010 · 23 reports
2010
Part: SIGN — OUT OF POSITION (COCKPIT) · airframe 72,680 hrs · 79,448 cycles
EMERGENCY EXIT SIGN IN COCKPIT FELL OUT.
2009
Part: SKIN — DENTED (FUSELAGE) · airframe 72,505 hrs · 79,339 cycles
FUSELAGE SKIN WITH DENT AT BS 1043 BETWEEN STR 16LT AND STR 17LT.
Part: SKIN — CRACKED (ENTRY DOOR) · airframe 72,506 hrs · 79,339 cycles
AFT ENTRY DOOR UPPER HINGE SKIN CRACKED.
Part: SKIN — CRACKED (FUSELAGE) · airframe 72,505 hrs · 79,339 cycles
LOWER FUSELAGE SKIN WITH CRACK AT BS 891, S-23RT.
Part: SKIN — DELAMINATED (AILERON) · airframe 72,505 hrs · 79,339 cycles
LEFT WING TRAILING EDGE SECTION, AILERON UPPER SURFACE SKIN DELAMINATED AT STA WBL 518.850 AND WBL 504.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,505 hrs · 79,339 cycles
LOWER FUSELAGE E&E COMPARTMENT AT BS 324, STR 28R WITH CORROSION.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,505 hrs · 79,339 cycles
LOWER FUSELAGE AFT CARGO COMPARTMENT DOOR LOWER CUTOUT FROM BS 795 TO BS 847 ANGLE CORRODED.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 72,505 hrs · 79,339 cycles
LOWER FUSELAGE RT MAIN WHEEL WELL AFT BULKHEAD WEB WITH CRACK IN BS 727 RBL 6 WL 160.
Part: FRAME — CORRODED (FUSELAGE) · airframe 72,505 hrs · 79,339 cycles
LOWER FUSELAGE FWD CARGO COMPARTMENT BS 440 BETWEEN STR 24 AND 25 RIGHT SIDE, FRAME CORRODED.
Part: STRINGER CLIP — CRACKED (ZONE 100) · airframe 72,505 hrs · 79,339 cycles
LOWER FUSELAGE AFT CARGO COMPARTMENT BS 887 STRINGER 24 RT CLIP CRACKED.
2006
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,568 hrs · 78,841 cycles
FORWARD ENTRY EMERGENCY EXIT LIGHT INOPERATIVE.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 71,425 hrs · 78,747 cycles
AFT DOOR EXTERIOR EMERGENCY LIGHTS INOPERATIVE.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 71,277 hrs · 78,644 cycles
CENTER AISLE EMERGENCY EXIT LIGHT AT OVERWING EXIT INOP. CHANGED BATTERY PACK.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 71,215 hrs · 78,603 cycles
FORWARD EMERGENCY AISLE LIGHT INOP.
Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 71,226 hrs · 78,611 cycles
AFTER TAKEOFF HYDRAULIC MASTER CAUTION LIGHT ILLUMINATED, LOST A-SYSTEM HYDRAULIC QUANTITY.
2005
Part: RIB — CRACKED (NR 4 SLAT) · airframe 71,127 hrs · 78,547 cycles
RT WING, SLAT NR 4 RIB CRACKED AT SLAT STA 0.28.
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 71,127 hrs · 78,547 cycles
RT WING INBOARD MID FLAP TRAILING EDGE P/N: 65-71902-42, S/N BN5, DELAMINATED AT WBL 132.
Part: STRINGER CLIP — CRACKED (BS 332) · airframe 71,127 hrs · 78,547 cycles
FORWARD SERVICE DOORWAY AREA, STA 332 STRINGER 8R AREA, T-CLIP IS CRACKED.
Part: RIB — CRACKED (TE FLAP)
RT WING AT WBL STA 364, OUTBOARD MID FLAP RIB CRACKED.
Part: PANEL — DELAMINATED (RT WING) · airframe 71,127 hrs · 78,547 cycles
RT WING FIXED PANEL P/N: 65-50818-316, DELAMINATED AT WS 465.
Part: BULKHEAD — CRACKED (BS 1016) · airframe 71,127 hrs · 78,547 cycles
BS 1016 AFT PRESSURE BULKHEAD WEB TO Y-CHORD ATTACHMENT CRACKED.
Part: PLATE — WORN (NR 2 PYLON) · airframe 71,127 hrs · 78,547 cycles
ENGINE NR 2 PYLON FWD SECTION WITH PLATE WORN.
Part: BULKHEAD — CRACKED (BS 1016) · airframe 71,127 hrs · 78,547 cycles
BS 1016 AFT PRESSURE BULKHEAD WEB TO "Y" CHORD ATTACHMENT CRACKED.