N587NK
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Spirit Airlines LLC | Operator | 2016-01-29 – 2016-01-29 | Operator named in NTSB report |
| SPIRIT AIRLINES, LLC (GTIA) | Operator | 2016-01-29 – 2016-01-29 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
CORROSION ON TOP BEAM AT TWO HARD POINTS NEAR FRAME 66. REMOVED CORROSION FROM FLOOR BEAM IAW A321 SRM 51-78-00 AND FOUND TO BE OUT OF LIMITS. REPLACED WITH NEW FLOOR BEAM PN D5347709400800 IAW A321 SRM 51-42-11.
LEFT WING CORROSION UPPER WING BETWEEN RIB 15 - 16. REPAIRED IAW EO 5721-1718.
REPLACED THE RT MLG ACTUATOR ANCHOR FITTING DUE TO CORROSION IAW EO 5726-1644.
REPLACED THE LT MLG ACTUATOR ANCHOR FITTING DUE TO CORROSION IAW EO 5726-1644.
CORROSION ON TOP BEAM Y-465 AT FRAME 66. REMOVED AND REPLACED THE BEAM IAW SRM 51-42-11.
CORROSION ON TOP BEAM 71292 AT FRAME 16. REMOVED AND REPLACED BEAM IAW SRM 51-41-00, 51-20-00.
CORROSIONB ON TOP BEAM Y765 AT FRAME 68. REMOVED AND REPLACED BEAM IAW SRM 51-72-11.
CORROSION ON TOP BEAM Y765 AT FRAME 66. REMOVED AND REPLACED THE BEAM IAW SRM 51-42-11, 52-21-11.
L4 DOOR SILL CORRODED FWD OF DOOR FRAME. L4 DOOR SILL REMOVED AND REPLACED IAW SRM 51-42-11.
CORROSION ON TOP BEAM Y1292 AT FRAME 66. REMOVED AND REPLACED THE BEAM IAW SRM 51-42-11.
CORROSION ON TOP BEAM - Y512 AT FRAME 66. REMOVED AND REPLACED TOP BEAM IAW SRM 51-42-11.
26B OXYGEN MASK PANEL WONT STAY UP. SECURED PSU PANEL IAW AMM 35-21-43.
R1, L2, R4 SERVICE DOOR REQUIRES SERVICING DOOR ASSIST BOTTLE LOW PRESSURE.. SERVICED R1, L2, R4 DOORS IAW 52-10-00-614-001-A. SERVICED TO PROPER PRESSURE"
DURING FLIGHT, NR 2 ENGINE OIL QUANTITY DECREASED. FLASHING ADVISORY BEGAN AT 5.0 LOWEST LEVEL NOTED WAS 3.5 QTS ON APPROACH NR 2 PSI AND TEMP WERE NORMAL. AFTER ENGINE SHUTDOWN OIL QTY WAS AT 10QTS. SERVICED THE OIL QTY WITH 12 QTS OF OIL IAW AMM 12-13-79 PB301.A. EXAMINE ENGINE, NO LEAKS NOTED. INSPECTED FCOC, NO DEFECTS NOTED IAW AMM 79-21-43-200-010-B. R & R OIL SCAVENGE PUMP IAW AMM 79-22-41. LEAK CHECKED GOOD IAW AMM 71-00-00-710-012. REMOVED & REPLACED NR 2 ENG DEOILER BREATHER SEAL ASSY IAW AMM 72-60-31 PB401. REMOVED & REPLACED NR 4 BEARING SCAVENGE VALVE IAW AMM 79-23-51 PB401. PERFORMED BORESCOPE INSPECTION OF NR 2 ENG HP COMPRESSOR IAW 72-00-00-200-016B. NO DEFECTS NOTED. PERFORMED BORESCOPE INSPECTION OF STAGE 1 HPT BLADES, DUCT SEGMENTS STAGE 2 HPT BLADES, DUCT SEGMENTS INSIDE COMBUSTION CHAMBER, & HP TURBINE STAGE 1 VANES IAW AMM 72-00-00-00-200-013/ 014, 015, NO DEFECTS NOTED. ACCOMPLISHED HIGH POWER ASSURANCE TEST IAW AMM 71-00-00-710-013-C, TESTED OK. PERFORM ENGINE RUN AT FLIGHT IDLE FOR 45 MINUTES IAW AMM 71-00-00, TESTED OK. OIL COMBUSION WAS 0.5 OIL QTS FOR 1 HOUR OF ENG RUNNING. FLIGHT TESTED SATISFACTORY.
F/A REPORTED SMELLY SOCKS ROW 24 AFT. LATE ON APPROACH 5000 FEET IDEL POWER BOTHE PACKS RUNNING. PERFORMED TSM 05-50-00-810-831-A. ISOLATED PACKS, ENGINES. PERFORMED ENGINE IDLE RUN IAW AMM 71-00-00-860-823-A. NO DIRTY SOCK SMELL OR ODORS DETECTED. A/C OK FOR SERVICE.
CAPTAIN`S O2 MASK LEAKS. R & R O2 CAPTAIN`S MASK IAW AMM 35-12-41, ALL CHECKS OK.
L-2 DOOR DAMPING CYLINDER LOW. SERVICED L-2 DOOR DAMPING CYLANDER IAW AMM 52-10-00. OPS CHECK GOOD.
L2 DOOR DAMPER CYLINDER LOW IN CHARGE. SERVICED L-2 DOOR DAMPER CYLINDER WITH NITROGEN IAW AMM 52-10-00-614-001-A.
L4 DOOR ASSIST BOTTLE IS LOW. SERVICED L4 DOOR ASSIST BOTTLE IAW AMM 52-10-00.
O2 MASKS IN CABIN ROW 12ABC COLLAPSED, PASSENGER OXYGEN STORAGE MODULES. PERFORMED REPACKED OF O2 MASK IN ROW 12 ABC IAW AMM 35-21-43, AND PERFORMED OPS CHECK OF MANUAL MASK RELEASED IAW AMM 35-23-00, ALL CHECKS NORMAL, NO DEFECTS NOTED, THIS CLEARS DMI 5817514, MOC NOTIFIED, PLACARD REMOVED.
CORROSION FOUND ON UPPPER SURFACE OF BOTTOM SKIN PANEL 3. INSPECT BETWEEN REAR SPAR AND + BETWEEN RIB 5 + THE MLG GEAR SUPPORT RIB ON THE RT WING. EO 5721-1518, REV 0, DATED 23 NOV 2015 CORROSION REPAIR ON RT WING BOTTOM SKIN PANEL 3 ACCOMPLISHED MWI 5780409 OPENED FOR 180 DAYS IAW STEP 5 OF THIS EO.
FWD F/A NR 1 POSITION EMERGENCY FLASHLIGHT WILL NOT TEST OR ILLUMINATE. R & R THE FLASHLIGHT IAW CMM 25-60-02. OPS CHECKED GOOD.
R1 PAX DOOR ASSIST BOTTLE DIAPHRAM RUPTURED. R & R R1 DOOR ASSIST BOTTLE DIAPHRAM IAW AMM 52-11-14, PB 401. BOTTLE CHARGED TO 1740 PSI AT 20' C. NO LEAKS NOTED.
PAX OXYGEN MASK ABOVE ROW 26ABC FELL DOWN IN FLIGHT. PERFORMED OPS TEST OF THE PASSENGER EMERGENCY OXYGEN SYS IAW AMM 35-23-00-710-050-A. OPS CHECK GOOD. NO DEFECTS NOTED. ALL MASKS RESTOWED AS REQUIRED IAW AMM 35-21-43-550-801-A.
F/A REPORTED L4 DOOR MEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-65-51.
DURING REMOVAL OF RIGHT ROLLER TRACK FOUND CROSSBEAM SECTION OF FRAME 48 FLANGE CRACKED. REPAIRED IAW EO 5341-1405, REV-00.
NR 2 OBSERVER OXYGEN MASK INOPERATIVE. R & R NR 2 OBSERVER OXYGEN MASK IAW AMM. NO HELP. R & R NR 2 OBSERVER OXYGEN MASK STOWAGE BOX IAW AMM. OPS & LEAK CK GOOD.
OXYGEN MASKS DROPPED ON LANDING, SEATS 9ABC AND 14. PERFORMED MANUAL DROP CHECK OF PAX OXYGEN MASK IAW AMM 35-23-00-710-001. ALL CHECKS GOOD.
FWD MEGAPHONE VOLUME KNOB MISSING. R & R MEGAPHONE KNOB IAW CMM. OPS CHECKED GOOD.
R1 DOOR ASSIST ACCUMULATOR BOTTLE LOW. SERVICED THE R1 DOOR ASSIST ACCUMULATOR IAW AMM.
R1 DOOR ASSIST ACCUMULATOR BOTTLE LOW. SERVICED BOTTLE IAW AMM.
F/A MEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 2565-51-920-001.
F/O OXYGEN MASK HEADBAND BROKEN. R & R MASK ASSY IAW MM 35-12-40-000-002-A & 35-12-41-400-002-A. OPS CHECKED GOOD.
EPSU 11WL, BATTERY FAILED, OPS CHECK. R & R EPSU BATTERY AT 11WL IAW ACFT MM. OPâS CHECKED GOOD.
R3 DOOR ARMING LEVER IS LOOSE. SECURED ARMING LEVER IAW ACFT MM, OK FOR SERVICE.
DURING PREFLIGHT F/A FOUND FRONT MEGAPHONE VOLUME BUTTON MISSING. INSTALLED NEW VOLUME BUTTOM ON THE FRONT MEGAPHONE.
BOTH AFT EMERGENCY EXIT DOOR OPEN ASSIST ACTUATORS DIAPHRAGM RUPTURED. R & R DIAPHRAGMS IN BOTH AFT EMERGENCY EXIT DOORS ASSIST ACTUATORS IAW AMM.
FLOOR LIGHT BY ROW 16 RT INOPERATIVE. SECURED LIGHT IAW AMM 33-51-21-400-001-A.
FOUND R4 DOOR ASSIST PRESSURE LOW. SERVICED R4 DOOR ASSIST IAW AMM 52-10-00-614-001-A LEAK CHECK GOOD.
R3 DOOR WILL NOT LATCH. REMOVED AND REINSTALLED DOOR PIN ON R3 OPS CHECK GOOD IAW AMM 52-10-00, PB 201 SECTION 4/2(A).
R4 DOOR PASSENGER DOOR ASSIST CYLINDER PSI 1000. SERVICED RT DOOR WITH NITROGEN TO REQUIRED LEVEL IAW AMM 52-10-00-614-001-A LEAK CHECKED OK AT THIS TIME.
R4 DOOR EMERGENCY ACCUMLUATOR PRESSURE LOW. SERVICED DOOR EMERGENCY ACCUMULATOR IAW AMM 52-10-00-614-001.
L2 DOOR EMERGENCY ACCUMULATOR PRESSURE LOW. SERVICED DOOR EMERGENCY ACCUMULATOR IAW AMM 52-10-00-614-001.
FOUND R3 DOOR SLIDE INFLATION RESERVOIR BELOW PROPER PRESSURE. R & R R3 DOOR SLIDE RESERVOIR REF AMM 25-62-49-400-001A. OPS CHECKED OK.
L2 DOOR ASSIST ACCUMULATOR HAS LOW PRESSURE. SERVICED L2 DOOR PRESSURE IAW AMM 52-10-00-614-001.
R & R EPSU 15WL BATTERY OPS CHECKED OK REF AMM 33-51-38-400-002A.
L4 EXIT SIGN LENS BROKEN. REINTALLED EXIT SING LENS AT L4 DOOR REF 33-51-13-400-001.
L2 DOOR ACCUMULATOR PRESSURE REQUIRE SERVICE. SERVICED L2 DOOR ACCUMULATOR PRESSURE IAW AMM 52-10-00-614-001.
R4 DOOR ACTUATOR PRESSURE LOW. SERVICED R4 DOOR ACTUATOR TO PROPER PRESSURE IAW AMM 52-10-00-614-001.
BATTERY/EPSU (14WC) MID R CLASS I MESSAGE. R & R EPSU BATTERY PACK (14WL) IAW AMM 33-51-000-002-A AND 33-51-38-400-002-A. EPSU SYS TESTED OK.
PAX DOOR RT AFT LOW ON PRESSURE. SERVICED PAX DOOR RT AFT TO PROPER PRESSURE IAW AMM 52-10-00-614-001.
L2 DOOR ASSIST BOTTLE LOW. SERVICED L2 DOOR PRESSURE IAW AMM 52-10-00-614-001.
ENGINE NR 2, PYLON UPPER SIDE (AT PRECOOLER AREA LT SIDE) BETWEEN PYLON STA 537 AND STA 608, SUPPORT ANGLE WITH CRACK. NOTE: THE SUPPORT ANGLE CRACK REQUIRES A MAJOR REPAIR.
ENGINE NR 1, AFT PYLON SECTION LOWER AFT FIXED FAIRING WITH CRACK. MAJOR REPAIR.
ENGINE NR 1, PYLON UPPER SIDE (AT PRECOOLER AREA RT SIDE) BETWEEN PYLON STA 537/RIB07 AND STA 608/RIB08, SUPPORT ANGLE WITH CRACK. NOTE: THE SUPPORT ANGLE CRACK REQUIRES A MAJOR REPAIR.
RT WING, RIB 16 L/E PANEL, LOWER SURFACE WITH CRACK. MAJOR REPAIR.
LT WING, RIB 16 L/E PANEL, LOWER SURFACE WITH CRACK. MAJOR REPAIR.
PAX CABIN, UPPER REAR FUSELAGE, AFT SERVICE AREA BETWEEN FR67 AND FR68 -Y52 FLOORBEAM WITH CORROSION. NOTE: THE FLOORBEAM CORROSION REQUIRES A MAJOR REPAIR.
RT WING, WX1835.15 FALSE REAR SPAR AND GEAR RIB LEVEL, BETWEEN RIB 3 AND RIB 4, TOP SKIN CORRODED. NOTE: THE TOP SKIN CORROSION REWORKS REQUIRE MAJOR REPAIR IAW MM INSTRUCTIONS.
RT WING, MLG ATTACHMENTS, RETRACTION JACK ANCHORAGE FITTING BORE WITH CORROSION. IT IS LOCATED ON INNER REAR SPAR BETWEEN RIB 2 AND RIB 3. NOTE: THE ANCHORAGE FITTING'S REWORK (PN 57259162001) REQUIRES A MAJOR REPAIR.
LT WING, MLG ATTACMENTS, RETRACTION JACK ANCHORAGE FITTING BORE WITH CORROSION. IT IS LOCATED ON INNER REAR SPAR BETWEEN RIB 2 AND RIB 3. NOTE: THE ANCHORAGE FITTING'S REWORK (PN D57259162000) REQUIRES MAJOR REPAIR IAW ACFT INSTRUCTIONS.
PAX CABIN, UPPER REAR FUSELAGE, AFT SERVICE AREA FR66+3" -Y52 FLOORBEAM WITH CORROSION. NOTE: THE BEAM CORROSION REQUIRES A MAJOR REPAIR.
PAX CABIN, UPPER REAR FUSELAGE, RT AFT PASSENGER DOOR LOWER SILL STA 3848 -Y59 FR66 FLOORBEAM WITH CORROSION. NOTE: THE FLOORBEAM CORROSION REQUIRES A MAJOR REPAIR IAW MM INSTRUCTIONS.
ENGINE NR 2, OTBD/RT THRUST REVERSER C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. NOTE: THE BUMPER WEAR REQUIRES A MAJOR REPAIR.
ENGINE NR 2, INBD/LT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. NOTE: THE BUMPER WEAR REQUIRES A MAJOR REPAIR.
ENG NR1, INBD/RT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. NOTE: THE WEAR REQUIRES A MAJOR REPAIR.
ENGINE NR 1, OTBD/ LT THRUST REVERSE C-DUCT, PAN-DOWN ENGINE BUMPER WITH WEAR. NOTE: THE WEAR REQUIRES A MAJOR REPAIR.
PAX CABIN, UPPER REAR FUSELAGE, AFT SERVICE AREA BETWEEN FR68 AND FR69 -Y52 FLOORBEAM WITH CORROSION. NOTE: THE BEAM CORROSION REQUIRES A MAJOR REPAIR.
ENG NR 2, PYLON AFT FIXED FAIRING , INBD AND OTD LATERAL SKIN PANEL WITH CORROSION. NOTE: THE PANELS' CORROSION REQUIRES A MAJOR REPAIR.
ENGINE NR1, PYLON AFT FIXED FAIRING, OTBD AND INBD LATERAL SKIN PANEL WITH CORROSION. NOTE: THE PANELS' CORROSION REQUIRES A MAJOR REPAIR.
RT SHEAR PLATE AT APPROX -Y1400 BETWEEN FR69 AND FR70 CRACKED/REMOVED AND REPLACED SHEAR PLATE.
FLOOR SUPPORT AT -Y765 BETWEEN FR66 AND FR70 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT.
FLOOR SUPPORT CORROSION AT -Y1292 BETWEEN FR68 AND FR69 / REMOVED AND REPLACED FLOOR SUPPORT.
RT FLOOR SUPORT AT -Y1292 BETWEEN FR66 AND FR68 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT.
LT SHEAR PLATE AT APPROX Y1400 BETWEEN FR69 AND FR70 CRACKED/ REMOVED AND REPLACED SHEAR PLATE.
FRAME 69 LT AND RT HAVE EVIDENCE OF CORROSION. REMOVED AND REPLACED SHEAR PLATES. (K)
FOUND NR 4 MAIN TIRE WORN TO LIMITS, WHEN TIRE WAS REMOVED FOUND NR4 MLG AXLE SLEEVE CRACKED. DAMAGED LENGTH MEASUREMENT IS NOT BEYOND .238 INCH, ACCOMPLISHED NDT INSPECTION OF NR4 AXLE SLEEVE, NO CRACK PROPAGATION BEYOND VISIBLE MEASUREMENT OF .238 INCH. (K)
R1 DOOR NOT SHOWING CLOSED INFLIGHT ON ECAM. RECYCLED EMERGENCY LIGHT TEST SWITCH ON FAP AND DOOR LIGHTS WORKED NORMALLY. PERFORMED ADJUSTMENT OF R1 DOOR PROX SWITCH PER AMM. SYSTEM OPS CHECK GOOD, LP NR 179708-3. (M)