N627NK
Registered owner: BANK OF UTAH TRUSTEE, UT (owner ≠ operator)
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
CORRODED STRINGER 37L BTWN FR 63 & 64. PERFORMED PERMANENT REPAIR ON THE STRINGER IAW SRM 53-41-13-300-010. DWGS D534770320, E53470342, R53470320, E53474160, & EA 53-0019.
CRACK INDICATION ON RT FRAME 68 STOP FITTING 6 AT AFT GALLEY AREA FROM LOWER INBD HOLE OF DOOR RAF-01 60233854-02 GENERATED. -PERFORMED REPAIR ON RH FRAM 68 LOWER INBOARD HOLE OF DOOR FITTING 6 AT AFT GALLEY AREA IAW SRM 53-41-12-300-008 SRM 53-41-12-300-010, DWG D534800820, & AMM 52-13-31-400-002-A REPAIR IS CATEGORY B INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 24500FC (FH NO RELEVANT) SUBSEQUENT INSPECTION AT INTERVAL OF 10700FC IAW SRM 53-41-12-205-009
CORROSION ON LOWER SILL LOCATED AT FR. 68 STR. 23R IN AFT GALLEY. PERFORMED PERMANENT REPAIR AT THE GALLEY SILL FR68 AT LEVEL STR 23R AT AFT GALLEY AREA IAW SRM 53-41-14-300-001. THIS REPAIR IS CATEGORY A, INSPECTION NOT REQUIRED.
CORRODED SEAT TRACK -Y254, FR 12 - FR 24 FWD GALLEY AREA. REPLACED SEAT TRACK -Y254, FR 12 - FR 24 AT FWD GALLEY AREA IAW SRM 51-72-11, SRM 51-42-11, AND DWGS D53111462, D53135202, & D53212367.
CORROSION SEAT TRACK +Y254, FR 12 - FR 24 AT FWD GALLEY AREA. REPLACED SEAT TRACK IAW SRM 51-42-11 AND DWG D53112816.
CORRODED SEAT TRACK, +Y1292, FR 12 TO FR 24 AT FWD GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-72-11, SRM 51-42-11, & DWG D53212367, D53111472, D53135202, & D53112627.
CORROSION ON HINGE FITTING 1, 2, 3, & 5 LT ELEVATOR. REPAIRED THE HINGE FITTING NR 1, 2, 3, & 5 LT ELEVATOR IAW SRM 55-26-41-300-004.
CORROSION FOUN ON BOTH HOLES OF HINGE FITTING 4 OF LT ELEVATOR, RAF01 6023860-2 CREATED. REPAIRED AND REPLACED BUSHINGS (2 EA) ON HINGE FITTING #4 AT LH ELEVATOR IAW A320 SRM 55-26-41-300-005
CORROSION FOUN ON BOTH HOLES OF IB ACTUATOR AND OUTBOARD ACTUATOR ATTACH FITTINGS OF LH ELEVATOR, REPAIRED BY SRM 55-26-47-300-002, RAF01 6023862-2 CREATED.-REPAIRED INBOARD AND OUTBOARD ACTUATOR FITTING OF LH ELEVATOR IAW A320 SRM 55-26-47-300-002
CORROSION FOUN ON BOTH HOLES OF IB ACTUATOR AND OUTBOARD ACTUATOR ATTACH FITTINGS OF RH ELEVATOR, REPAIRED BY SRM 55-26-47-300-002. RAF01 6023862-2 CREATED.-REPAIRED INBOARD AND OUTBOARD ACTUATOR FITTINGS OF RH ELEVATOR IAW A320 SRM 55-26-47-300-002
CORROSION FOUND ON BOTH HOLES OF HINGE FITTINGS 4 OF RT ELEVATOR, REPAIRED AND REPLACED BUSHINGS (2 EA) ON HINGE FITTING NR 4 AT RT ELEVATOR IAW SRM 53-26-41-300-005.
CORROSION FOUND ON BOTH HOLES OF HINGE FITTING 6 OF RT ELEVATOR, REPAIRED INBD LUG BORE AND REPLACED BUSHINGS (2 EA) ON HINGE FITTING NR 6 AT RT ELEVATOR IAW SRM 53-26-41-300-006.
CORROSION SEAT TRACK -Y1292 LOCATED FR 12 TO FR 24 AT FWD GALLEY AREA. REPLACED THE SEAT TRACK -Y1292, FR12 TO FR24 FWD GALLET AREA IAW SRM 51-42-11, DWG D53114407, D53135202, D53212367, AND D53925046.
CORROSION FOUN ON BOTH HOLES OF HINGE FITTING NR 6 OF LT ELEVATOR, FINAL HOLE DIAMETER IS 14.500MM. REPAIRED AND REPLACED BUSHINGS (2 EA) ON HINGE FITTING #6 AT LT ELEVATOR IAW SRM 55-26-41-300-006.
CORROSION FOUND ON HINGE FITTINGS 1, 3, & 5 REPAIRED IAW SRM 55-26-41-300-004.
CORROSION SEAT TRACK, +Y765, FR 12 TO FR 24. REPLACED SEAT TRACK IAW SRM 51-42-11, DWGS D53215367, D53114404, & D53135202.
CORRODED DUMMY RAIL, Y503.2 AT FWD GALLEY AREA. REPLACED DUMMY RAIL Y503.2 LOC. FWD GALLEY AREA BTW FR12 TO FR16 IAW SRM 51-42-11, DWG D53114410, DWG D53114411, AND DWG D53110984.
FA IS AFT REPORTED A SMELL OF DIRTY CLOTHS DURING TAKE OFF AND THEN GOT SICK. TWO OTHER FA'S GET SICK BEFORE FUME EVENT PROCEDURE WAS APPLYED . TAKE OFF POWER AND CLIMB POWER THROUGH RAIN. -PER TSM 05-50-00-810-831-A, THE CAUSE OF THE ODOR WAS FOUND TO BE COMING FROM THE APU. PERFORMED INSPECTION OF APU AND FOUND EVIDENCE OF DE-ICING FLUID NEAR APU FLAP. CLEANED THE AREA AND PERFORMED A PACK BURNOUT. NO MORE ODOR AT THIS TIME. A/C OK FOR SERVICE.
"FA MEGAPHONE INSPECTION EXPIRED-R&R MEGAPHONE AMM 25-65-51 OPS OK"
INSTALLATION OF THE PERSONAL COMPUTER MEMORY CARD (PCMCIA) OF THE FDIMU/DMU -R/R EPSU.
FUME EVENT ON ARRIVAL TO FLL ABOUT 4,000 MSL. PACK 1 COCKPIT AFFECTED.-R&R RECIRCULATION FILTER CARTRIDGE PER AMM 21-21-41. PERFORMED PACK DECONTAMINATION PER AMM 21-00-00. NO DEFECTS NOTED AT THIS TIME.
"DURING PYLON NO 2 EWIS INSPECTION FOUND COMBO SEAL DUCT CLAMP CHAFFING WITH THE PYLON RIB 08-09 WALL SKIN -VERIFIED LTPR NR # 5001214933-0020 HAS BEEN ACCOMPLISHED. "
FUME OR VAPOR OR ODOR EMANATING FROM REAR GALLEY CAUSING CREW & PAX TO BECOME VERY SICK.-PERFORMED INSPECTION TO CHECK FOR ODORS, VAPOR OK FUMES ISOLATED , NO ODORS OR FUMES NOTED. ALL PERFORMED IAW TSN 05-50-00-810-831-A. AC OK FOR SERVICE. MOC # 109053. Q6TR841X
RT OVERWING SLIDE DEPLOYED DURING OTHER MAINTENANCE ON DOOR LH OUTBD BRAKE ASSY WORN TO LIMITS-REMOVED AND REPLACED R/H OVERWING SLIDE IAW AMM 25-62-42.OPS CK GOOD. R&R RESERVOIR DUE TO SLIDE CHANGE IAW AMM 25-62-46.OPS CK GOOD
AFT GALLEY FLASHLIGHT DEAD ( FLASHLIGHT AND HOLDERS (FLIGHT DECK OR CABIN) )-R/R AFT SWIVEL FA FLASHLIGHT IAW CMM 25-60-13. OPS CHECK GOOD. THIS CLEARS DMI # 2876650-01. PLACARD REMOVED MOC NOTIFIED.
AFT MEGAPHONE AT ZONE K SIREN PIN SHEARED.-R&R AFT MEGAPHONE AT ZONE K IAW SPIRIT AIRLINES EMERG EQUIP LAYOUT DRAWING A320-EMER-EQUIP REV IR.
CRUISING AT FL350 FLIGHT ATTENDANT REPORTED STRONG SMOKE SMELL (NON-VISABLE) SHORTLY AFTER CAPT AND FO SMELLED SAME ODOR. IT RESEMBLED BURNNG ELECTRICAL SMELL REMOVAL OF SMOKE/FUMES COM PROCEDURE WAS INITIATED. - AFTER CABIN FANS OFF AND PACK FLOW HIGH SMELL BEGAN TO DISSIPATE. DIVERTED TO PIT AND LANDED AIRCRAFT WITOUT FURTHER INCIDENTS. ( POTABLE WATER SYSTEMS POTABLE WATER SYSTEMS - INDIVIDUAL COMPONENTS ). -INSPECTED AIRCRAFT AS PER AMM 05-50-00-991-01601-00A. FOUND AIR COMPRESSOR HOT AND HAS ODOR. DEACTIVATED COMPRESSOR BY C/B F01. SEE ITEM 2 FOR DEFERRAL.
DESCENDING INTO BURBANK THROUGH 7,000' WE RECEIVED LGCIU 2 FAULT. ASSOCIATED BY REVERSER 2 INOPERABLE. RETURNED TO LAS VEGAS. R & R LGCIU 2, PER AMM 32-31-71. R & R PROXIMITY SENSORS 27GA AND 29GA, PER AMM 32-31-73. NO FAULTS AT THIS TIME.
HYDRAULIC RESERVOIR LO LEVEL ECAM. PERFORMED INSPECTION OF HYDRAULIC, IAW AMM 29-00-00. FOUND LEAK AT HP MANIFILD ON YELLOW SYSTEM. R & R YELLOW HP MANIFOLD, IAW AMM 29-13-14. OPERATIONS CHECK & LEAK CHECK GOOD NO FAULTS OR LEAKS NOTED AT THIS TIME.
FUME EVENT ON FINAL PERFORMED SUPP PROCEDURE CHECKLIST-INSPECTED ENGINES FUSELAGES AND APU NO LEAKS NOTED APU TEST PERFORMED NO EVIDENCE OF SMELL ENGINES RUN UP PERFORMED AND PACKS BURNT OUT NO SMELL NOTED IAW AC MM TSM 05-50-00 AC OK FOR SERVICE
F/A NOTICED SMELL IN AFT CABIN-PERFORMED TSM 05-50-00-810-831-A RAN BOTH ENGINES AND APU BLEED SYSTEM IAW AMM 71-00-00. NO ODER DETECTED.
MUSTY SOCK ODOR, DESCENDING OUT OF 18,000 FT, VERY STRONG BY 12,000 FT. CABIN AND COCKPIT CREW SMELLED THE ODOR. PERFORMED TSM 05-50-00. NO ODOR NOTED. ACFT OK FOR SERVICE.
FLIGHT ATTENDANT NOTICED A SOCK ODOR DURING DESENT, WAS NOT NOTICED IN COCKPIT. PERFORMED A FAULT ISOLATION IAW TSM 05-50-00. NO ODOR NOTICED. ACFT OK FOR SERVICE.
FOUND ACFT DOOR CLOSED AND ACFT WITH A STRONG ODOR IN MAIN CABIN, APU WAS ON, BLEEDS OFF, NO GROUND AIR. PERFORMED TSM 05-50-810-831-A, TYPE 2 AND FOUND THE APU WITH OIL LEAKING AT THE PRESSURE SWITCH. RAN THE NR 1 AND 2 ENGINES WITH PACKS ON IAW AMM 71-00-00. NO ODOR NOTED OR DEFECTS. R & R THE RECIRCULATION FILTERS IAW AMM 21-21-41.
FWD O/B FA JS FLASHLIGHT FLASHES RED (FLASH LIGHT AND HOLDERS. REMOVED AND REPLACED FWD O/B FA JS FLASHLIGHT (GREEN) IAW CMM 25-60-13. OPS CHECK GOOD.
FWD O/B FA JS FLASHLIGHT FLASHES RED ( FLASHLIGHT AND HOLDERS (FLIGHT DECK OR CABIN) ). REMOVED AND REPLACED FWB O/B FA JS GREEN FLASH LIGHT IAW CMM 25-60-13 OPS CHECK GOOD PLACARD REMOVED MOC NOTIFIED.
FUME EVENT AT COCKPIT AUX CABIN REPORT DIRTY ODOR THRU OUT INTEN SECEL WITH MAX THRUST REVERSER BOTH, PACK OFF DURING TAXI, . PERFORMED INDICATION OF CAUSE OF CABIN ODOR IAW TSM 05-50-00-810-831-A. THE NR 2 PACK AT FAULT.
FUME EVENT ON LANDING FA'S REPORT DIRTY SOCK ODOR THROUGHOUT CABIN. IAW TSM 05-50-00-810-831 FAULT ISOLATION PROCEDURE SUSPECT THE NR 2 PACK CAUSING THE FUMES.
FA'S REPORTED AN ODOR DURING DESCENT, IN THE BACK OF THE CABIN AND FRONT. WHEN PACK WERE SELECTED OFF IT SEEMS TO DISSAPATE. PERFORMED OPS TEST OF PACK SYSTEMS 1 & 2, WITH APU, ODOR DETECTED. GVI OF APU SHOWS LEAK AROUND LOP DRIPPINS ONTO AIR DUCT. CLEANED AS REQUIRED. PERFORMED ENGINE 1&2 RUN WITH BLEEDS 1&2 + PACK 1+2, NO SMELL DETECTED W/ OUT APU. ALL PER AMM 49-90-00-600-004-A/49-00-00-710-008-A/71-00-00-710-043-A/-047-A, CHECKS OK NO ODOR IN SYS 1 OR 2 W/ OUT APU
FUMES IN COCKPIT AND CABIN AT 6000 FEET ON ARRIVAL. APPEARED TO DISSIPATE WITH PACK 1 TURNED OFF. PERFORMED ENGINE RUN IAW AMM 71-00-00. ISOLATED THE NR 1 PACK, NO ODOR NOTED. ISOLATED PACK NR 2, NO ODOR NOTED. PERFORMED OPS CHECK OF APU IAW AMM 49-00-00. ISOLATED NR 1 PACK NO ODOR NOTED. ISOLATED THE NR 2 PACK. NO ODOR NOTED. AIRCRAFT OK FOR SERVICE.
FIRST OFFICER`S OXYGEN MASK IS MISSING A PART ON THE FRONT. REMOVED & REPLACED THE OXYGEN MASK IAW AMM 35-12-14. OPS CHECKED GOOD.
R1 DOOR ASSIST HANDLE BROKEN. R & R THE ASSIST HANDLE IAW AMM 25-23-00-15300-00-A
STRONG SMELL OF FUMES REPORTED IN AFT GALLEY BY FA. COULD NOT SMELL IN COCKPIT OR FORWARD GALLEY. SEEMED TO OCCUR AS APU AVAIL LIGHT WAS EXTINGUISHING. BOTH ENGINES WERE RUNNING. PER TSM# 05-50-00-810-831-A. VISUALLY INSPECTED APU COMPARTMENT, NO LEAKS NOTED. NO LEAKS FROM ENGINE DRAINS. ENGINE RUN & PARAMETERS OK. ATTEMPTED TO DUPLICATE ODOR SMELL BY ISOLATING BLEED AIR WITH APU AND BOTH ENGINES WITH APU & GROUND. ISOLATED BOTH PACKS 1&2. NO ODORS NOTED. INSPECTED AFT GALLEY EQUIPMENT. ALL CHECKS OK. COULD NOT DUPLICATE ODOR. ACFT OK FOR SERVICE.
ROW 15 ABC OXYGEN MASK DID NOT DEPLOY DURING DROP CHECK. R & R EMERGENCY OXYGEN CONTAINER IAW AMM 35-21-41. DROP TEST GOOD.
OXYGEN MASK ROWS 2F & D FELL ON T/O. PERFORMED O2 MASK DROP TEST OPS CHECK OK. REPACK ROW 2F & D AS REQUIRED REF AMM 35-23-00 AND 35-21-41