N549AX
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
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, 2005-01-02 – 2011-08-25.
Part: SKIN — SCRATCHED (BS 1436 S10L) · airframe 57,402 hrs · 18,928 cycles
FUSELAGE SKIN, BS 1436 S10L, SCRATCHED. REPAIR CARRIED OUT AS PER E.A. F-5330-153402. REPAIR IS CLASSIFIED AS MAJOR.
Part: SPLICE PLATE — DAMAGED (ZONE 200) · airframe 57,402 hrs · 18,928 cycles
FUSELAGE BUTT JOINT SPLICE PLATE AT STA 780, STR 8L TO 9L HAS SCRIBE LINE WITH MAX DEPTH OF 0.0025". R & R IAW SRM 51-40-02, REV 103. REPAIR IS CLASSIFIED AS MAJOR.
Part: STRINGER — GOUGED (BS 417 S2R) · airframe 57,402 hrs · 18,928 cycles
CABIN, STRINGER 2R AT STA 417 HAS GOUGE NEAR FRAME. REPAIRED IAW EA F-5310-152522. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — DAMAGED (BS 780) · airframe 57,402 hrs · 18,928 cycles
FUSELAGE, BUTT JOINT SPLICE PLATE AT STA 780, S8R TO 9R HAS SCRIBE LINE WITH MAX DEPTH OF 0.0038. DAMAGED BUTT JOINT SPLICE PLATE REMOVED AND REPLACED IAW SRM 51-40-02 REV. 103. REPAIR IS CLASSIFIED AS MAJOR.
Part: STRINGER — DAMAGED (ZONE 200) · airframe 57,402 hrs · 18,928 cycles
CABIN, STR 1 AT STA 416 HAS TOOLING MARKS IN THE SIDE OF STRINGER. REPAIRED IAW EA F-5310-152521. REPAIR IS CLASSIFIED AS MAJOR.
Part: FRAME — DAMAGED (ZONE 200) · airframe 57,402 hrs · 18,928 cycles
CABIN, STA 1280, LT FRAME HAS TOOLING MARKS BETWEEN STR 15L AND 16L ON FRAME FLANGE. DAMAGED REPAIRED IAW EA F-5310-152523. REPAIR IS CLASSIFIED AS MAJOR.
Part: SHIM — MIGRATED (ZONE 400) · airframe 57,402 hrs · 18,928 cycles
NR 2 NACELLE STRUT BETWEEN MID BULKHEAD LOWER FLANGE AND STIFFENER AT PPSTA 174.3. FOUND WITH INBD SHIMS MIGRATION. R & R IAW EA F-5450-152561. REPAIR IS CLASSIFIED AS MAJOR.
Part: SHIM — MIGRATED (NR 1 PYLON) · airframe 57,402 hrs · 18,928 cycles
NR 1 PYLON MID-BULKHEAD LOWER FLANGE INBD AFT AND FWD SIDE AT PPSTA 174.30 FOUND WITH SHIMS MIGRATION. SHIMS REPLACED IAW SRM 54-50-90 REPAIR 7, REV 103. REPAIR IS CLASSIFIED AS MAJOR.
Part: FLOOR PANEL — CORRODED (ZONE 200) · corrosion level 2 · airframe 57,402 hrs · 18,928 cycles
CABIN, DECK PLATE CORROSION, STA 1715, RBL 58 TO LBL 58. REPAIR CARRIED OUT IAW SRM 53-60-51 REPAIR 2 FIG 201, REV 103. REPAIR IS CLASSIFIED AS MAJOR.
Part: SHIM — MIGRATED (ZONE 400) · airframe 57,402 hrs · 18,928 cycles
2 PYLON NACELLE BETWEEN MID BULKHEAD UPPER FLANGE AND INNER WEB SKIN AT PPSTA 174.3 FOUND WITH SHIMS MIGRATION. SHIMS R & R IAW EA F-5450-152561. REPAIR IS CLASSIFIED AS MAJOR.
Part: SHIM — MIGRATED (ZONE 400) · airframe 57,402 hrs · 18,928 cycles
NR 2 NACELLE STRUT UPPER SPAR FITTING AT PPSTA 174.0 FOUND WITH OTBD SIDE HORIZ SHIMS MIGRATION. DAMAGED SHIMS R & R IAW SRM 54-50-90, REPAIR 6, FIG 201, REV 103 AND EA F-5450-152561. REPAIR IS CLASSIFIED AS MAJOR.
Part: SHIM — MIGRATED (ZONE 400) · airframe 57,402 hrs · 18,928 cycles
NR 2 NACELLE STRUT BETWEEN MID BULKHEAD LOWER FLANGE AND STIFFENER AT PPSTA 174.3. FOUND WITH OTBD SHIMS MIGRATION. SHIMS R & R IAW EA F-5450-152561. REPAIR CLASSIFIED AS MAJOR.
Part: SHIM — MIGRATED (ZONE 400) · airframe 57,402 hrs · 18,928 cycles
1 PYLON MID BULKHEAD LOWER FLANGE OUTBD AFT SIDE AT PPSTA 174.30 FOUND WITH SHIMS MIGRATION. R & R IAW SRM 54-50-90. REPAIR 7, REV. 103. REPAIR IS CLASSIFIED AS MAJOR.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 57,402 hrs · 18,928 cycles
CABIN, FLOORBEAM AT STA 365 RBL 58 HAS CORROSION. FLOORBEAM R & R IAW SRM 51-40-02, REV. 103. REPAIR IS CLASSIFIED AS MAJOR.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 57,402 hrs · 18,928 cycles
CABIN, FLOORBEAM AT STA 345, HAS CORROSION ON UPPER CHORD LBL 01 TO LBL 24. R & R IAW SRM 51-40-02, REV 103. REPAIR IS CLASSIFIED AS MAJOR.
Part: STRINGER SPLICE — CRACKED (BS 1668-1695) · airframe 57,402 hrs · 18,928 cycles
CABIN, STRINGER SPLICE AT STR 18R STA 1668 TO STA 1695 HAS CRACK THROUGH STRINGER TIE STRAP FASTENER HOLE. CRACKED STRINGER SPLICE R & R IAW SRM 51-40-02, REV 103. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — CORRODED (ZONE 400) · airframe 57,402 hrs · 18,928 cycles
NR 1 PYLON NAC STRUT STRUCTURE OTBD ACCESS HOLE FOR PANEL NR 433AL CUT-OUT INNER EDGES FOUND WITH CORROSION. R & R IAW E.A. F-5450-152562. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — CORRODED (ZONE 400) · airframe 57,402 hrs · 18,928 cycles
NR 1 PYLON NAC STRUT INBD INNER SIDE SKIN AT PPSTA 144.4 - PPSTA 174.30 FOUND WITH CORROSION. SKIN R & R IAW EA 5450-152562. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — CORRODED (ZONE 400) · airframe 57,402 hrs · 18,928 cycles
NR 2 PYLON NAC STRUT STRUCTURE OTBD ACCESS HOLE FOR PANEL NR 443AR CUT-OUT INNER EDGES FOUND WITH CORROSION. PANEL R & R IAW EA F-5450-152563. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — CORRODED (ZONE 400) · airframe 57,402 hrs · 18,928 cycles
NR 1 PYLON NAC STRUT STRUCTURE INBD ACCESS HOLE FOR PANEL NR 433GR CUT-OUT INNER EDGES FOUND WITH CORROSION. SKIN PANEL R & R IAW SRM 51-40-02 REV 103 AND EA F-5450-145386. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — CORRODED (ZONE 400) · airframe 57,402 hrs · 18,928 cycles
NR 2 PYLON NAC STRUT STRUCTURE INBD ACCESS HOLE FOR PANEL NR 443GL CUT-OUT INNER EDGES FOUND WITH CORROSION. SKIN R & R IAW SRM 51-40-02 REV.103 AND DWG 311N5002, REV E. REPAIR IS CLASSIFIED AS MAJOR.
Part: SKIN — CORRODED (ZONE 400) · airframe 57,402 hrs · 18,928 cycles
NR 2 PYLON NAC STRUT INBD INNER SIDE SKIN AT PP STA 136.7 - PP STA 174.30 FOUND WITH CORROSION. SKIN R & R IAW SRM 51-40-02, REV 103 AND DWG 311N5002, REV E. REPAIR IS CLASSIFIED AS MAJOR.
Earlier reports · 2005–2010 · 14 reports
2010
Part: CONTROL MODULE — FAILED (ZONE 500) · airframe 57,270 hrs · 18,895 cycles
AIR RETURN DUE TO SPOILERS EICAS AND MESSAGE OVERHEAD. R & R ED NR 2 PCA AND LT NR2 ISCM IAW MM 27-61 AND 27-09. OPS CHECK GOOD.
Part: ENGINE — VIBRATION (RIGHT) · airframe 56,222 hrs · 18,699 cycles
RT ENGINE BANK AND SHUDDER CLIMBING THROUGH 1600', N1 VIB AT 2.9 IN YELLOW ARC. LEVELED AT 1900' REDUCED POWER, VIBRATION RETURNED TO NORMAL.
2009
Part: WINDOW — FAILED (COCKPIT) · airframe 55,565 hrs · 18,550 cycles
F/O WINDSHIELD SHATTERED DURING FLIGHT. REMOVED AND REPLACED F/O WINDSHIELD IAW MM 56-11. (PRECAUTIONARY: REMOVED AND REPLACED HEAT CONTROL UNIT, OPS CHECK GOOD IAW MM 30-41, DUE TO THE R-1 WINDSHIELD BEING REPLACED).
Part: SKIN — DAMAGED (BS 1493) · airframe 54,614 hrs · 18,350 cycles
REPAIR DENT STA 1493 524L AND 25-L EXTERIOR SKIN. CUT OUT DAMAGED AREA OF EXTERIOR SKIN STA 1493 STR 24L AND 25L. FABRICATED REPAIR PARTS AND INSTALL IAW SRM 53-00-01, FIG 201, REPAIR NR 4.
Part: ACCESS PANEL — DAMAGED (FUSELAGE) · airframe 54,614 hrs · 18,350 cycles
KEELBEAM ACCESS PANEL NR 139 AL HAS EDGE DAMAGE ON RT AND LT SIDES. SANDED, CLEANED AND PREPED KEELBEAM PANEL NR 139 AL IAW SRM 51-70-03, PG 6-8, APPLIED REPAIR IAW SRM 51-70-03 PG 9-13 AND RESTORED FINISH IAW SRM 51-70-03 PG 13.
Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 54,614 hrs · 18,350 cycles
AFT LAV SERVICE DOOR ANGLE BETWEEN LATCHES IS CORRODED. REPLACED AFT LAV SERVICE DOOR ANGLE BETWEEN LATCHES IAW SRM 52-40-02-13.
Part: STANCHION — CRACKED (BULKHEAD) · airframe 54,614 hrs · 18,350 cycles
FWD PIT, AFT BULKHEAD CTR STANTION CRACKED. REMOVED AND INSTALLED FWD PIT, AFT BULKHEAD CTR STANTION IAW 51-40-02.
Part: SCUFF PLATE — CRACKED (L2 DOORWAY) · airframe 54,614 hrs · 18,350 cycles
L2 DOOR SCUFF PLATE CRACKED 2 PLACES. INSTALLED REPAIRED L2 DOOR SCUFF PLATE IAW MM 53-13-01-424-003.
Part: SUPPORT — BROKEN (BS 1200) · airframe 54,614 hrs · 18,350 cycles
ECS DUCT SUPPORT BROKEN AT STA 1200 IN AFT CARGO COMPARTMENT ON LT SIDE . REPLACED ECS DUCT SUPPORT AT STA 1200 IAW 21-33-01.
Part: SPOILER SYS — INOPERATIVE (NR 11) · airframe 54,427 hrs · 18,316 cycles
AFTER TAKEOFF, WHILE BANKING RT, SPOILERS EICAS ILLUMINATED, WITH OBVIOUS FLIGHT CONTROL FEELING. COMPLETED QRH AND VERFIED SPOILER PANEL FLOAT VISUALLY. PERFROMED SCH BITE FOUND 1R PCA AT FAULT. VERIFIED NR 11 SPOILER DOES NOT EXTENEDED. REMOVED AND REPLACED NR11 PCA IAW MM 27-61. OPS AND LEAK CHECK OK. SWAPPED SPOILER CONTROL MODULE - PRECAUTIONARY.
2008
Part: CIRCUIT CARD — FAULTY (BLEED AIR SYS) · airframe 53,345 hrs · 18,102 cycles
EICAS L ENG BLEED OFF. T/S PER FIM 36-10. VISUALLY CHECK PRSOV, NO LEAK NOTED. RESEATED ECS BLEED LT CONFIG CARD. RAN ENGINE. OPS CHECK NORMAL. LT PACK OPERATION NORMAL. REPLACED LT ENG BLEED CARD IAW MM REF 36-10 GRND OPS OF BLEED SYSTEM GOOD AT THIS TIME. R&R LT ENG REVERSE FLOW CONTROL VALVE IAW MM REF 36-11, GROUND OPS CK GOOD.
2005
Part: GUIDE ARM — OUT OF ADJUST (EMERGENCY DOOR) · airframe 46,056 hrs · 16,670 cycles
NR 2 RT ENTRY DOOR FAILED TO FULLY OPEN DURING EVACUATION TEST. PERFORMED COMPLETE DOOR ADJUSTMENT TEST AND ADJUSTED R2 DOOR IAW MM 52-11 PERFORMED OPERATIONAL TEST OF R2 DOOR SLIDE IAW OAI CARD NR 75TC-0890. THE ROOT CAUSE FOR THE FAILURE TO DEPLOY WAS THAT THE DOOR WAS OBSTRUCTED BY THE LOWER SLIDE SKIRT WHEN ATTEMPTING TO DEPLOY SLIDE. ADJUSTMENTS WERE MADE TO THE GUIDE ARM TO ALLOW FOR ADDITIONAL CLEARANCE FOR THE DOOR TO COCK OPEN ENOUGH TO ALLOW CLEARANCE FOR THE LOWER SLIDE SKIRT. NOTE: AIRCRAFT DOOR WAS WITHIN MM LIMITS BOTH BEFORE AND AFTER RIGGING.
Part: GUIDE ARM — OUT OF ADJUST (R2 DOOR) · airframe 46,056 hrs · 16,670 cycles
NR 2 RT ENTRY DOOR FAILED TO FULLY OPEN DURING EVACUATION TEST. PERFORMED COMPLETE DOOR ADJUSTMENT TEST AND ADJUSTED R2 DOOR IAW B757 M/M 52-11, PERFORMED OPERATIONAL TEST OF R2 DOOR SLIDE IAW OAI CARD 75TC-0890. THE ROOT CAUSE FOR THE FAILURE TO DEPLOY WAS THAT THE DOOR WAS OBSTRUCTED BY THE LOWER SLIDE SKIRT WHEN ATTEMPTING TO DEPLOY SLIDE. ADJUSTMENTS WERE MADE TO THE GUIDE ARM TO ALLOW FOR ADDITIONAL CLEARANCE FOR THE DOOR TO COCK OPEN ENOUGH TO ALLOW CLEARANCE FOR THE LOWER SLIDE SKIRT. NOTE: AIRCRAFT DOOR WAS WITHIN MAINTENANCE MANUAL LIMITS BOTH BEFORE AND AFTER RIGGING.
Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 44,813 hrs · 16,321 cycles
TRAILING EDGE FLAP DISAGREE EICAS MESSAGE ON APPROACH WHEN FLAPS 20 WERE SELECTED SPEED APPROX 190 KIAS. INDICATOR SHOWED 17 DEGREES WHEN LIGHT CAME ON. APPROACH WAS DISCONTINUED DECLARED EMERGENCY AND ADVISED ATC OF NATURE OF PROBLEM.