N321DH
Registered owner: UMB BANK NA 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
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.
20 reports on file, 2020-05-18 – 2024-10-15.
Part: SKIN — DAMAGED (ZONE 200) · airframe 22,771 hrs · 10,209 cycles
AIRCRAFT 3021, FOUND LIGHTENING STRIKE DAMAGE @ FRAME 24 STRINGER 6 BURN ON SKIN. CORRECTIVE ACTION: INSPECTED DAMAGE AS PER A321 SRM 53-00-11. PERFORMED PERMANENT REPAIR AS PER A321 SRM 53-21-11-300. (LP 5785554)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 19,986 hrs · 9,067 cycles
SHIP 3021 L4 DOOR ASSIST CYL REQUIRES SVC. CORRECTIVE ACTION: SERVICED L4 DOOR ASSIST CYL IAW A321 AMM 52-10-00. OK FOR SERVICE. (4853031)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 19,986 hrs · 9,067 cycles
SHIP 3021 R1 DOOR ASSIST CYL REQUIRES SVC. CORRECTIVE ACTION: SERVICED R1 DOOR ASSIST CYL IAW A321 AMM 52-10-00. OK FOR SERVICE. (4853030)
Earlier reports · 2020–2023 · 17 reports
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 19,482 hrs · 8,860 cycles
SHIP 3021 SKIN WAS DAMAGED BY TOW BAR. CORRECTIVE ACTION: COMPLIED WITH ERA 600716-00. (2859085)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 18,154 hrs · 8,325 cycles
AFT RH ESCAPE SLIDE LIGHTING IS INOP. REPLACED SLIDE/RAFT AFT RH AS PER AMDS CARD #2561-4002-RA AND PERFORMED OPERATIONAL TEST EPSU AFT POSITION ASPER AMDS CARD #2561-4002-RA STEP 13.C TEST IS GOOD PLACARD REMOVED. RII INSPECTION COMPLETE 117432 AE232QC. JOB COMPLETE. (LP# 4948534)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 18,094 hrs · 8,300 cycles
CORROSION FLOOR BEAM +Y765 LOCATED BTW FR 66 TO FR 70 AT AFT GALLEY A. REPLACED FLOOR BEAM Y765 LOCATED BTW FR 66 TO FR 70 AT AFT GALLEY AREA AS PER A321 SRM 51-72-11 AND DWG# D534 72001, RELEASEDATE: 07-DEC-21, ISSUE: W, DWG# D383 70017, RELEASE DATE: 25-NOV-98, ISSUE: K, DWG# D534 72679. MEASURES OF DEEPEST CORROSION OF FLOOR BEAM Y765 ARE L: 1.729 INCH, W:0.673 INCH, D: 0.020 INCH. (LP# 2837715)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 18,094 hrs · 8,300 cycles
CORROSION FLOOR BEAM -Y765 LOCATED BTW FR 66 TO FR 70 AT AFT GALLEY AREA. REPLACED FLOOR BEAM -Y765 LOCATED BTW FR 66 TO FR 70 AT AFT GALLEY AREA (SSI 534147) AS PER SRM A321. 51-72-11 AND DRAWING 53472001 RELEASE DATE 07 DEC. (LP#2824265)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 18,094 hrs · 8,300 cycles
CRACK SHEAR PLATE STR 23 L LOCATED BTW FR 69 TO FR 70 AT AFT GALLEY AREA. REPLACED SHEAR PLATE AND FASTENERS STR 23 L LOCATED BTW FR 69 TO FR 70 AT AFT GALLEY AREA AS PER A321 SRM 51-42-11-801, SRM51-72-11-911-001 AND DWG D53474180 RELEASE DATE 14-JUL-22 ISSUE Z RII INSPECTION COMPLETE. (LP# 2809729)
2022
Part: NONE — NONE · airframe 15,210 hrs · 7,085 cycles
WHILE UNDER TOW ON PUSHBACK TOW BAR BROKE LOOSE AND AIRCRAFT ROLLED FWD IMPACTING TUG. INSPECTED NOSE LANDING GEAR PER A321 AMM 32-2 (101690). R & R TOW FITTING ASSY PER A321 AMM 32-41. (101690) TRANSFERRED TO NON-ROUTINE #1. STRUCTURAL REPAIR AND NON-ROUTINE #2 NOSE LANDING GEAR REPAIR. REF TOPP 50-30-05 (471692). SUMMARY: NOSE LANDING GEAR REPAIRS COMPLETED ON LOG PAGE 2315534. FUSELAGE REPAIRS COMPLETED ON ER/A 600713-14 REV ORIGINAL AND ER/A 600716 -14 REV ORIGINAL. ALL REQUIRED INSPECTIONS HAVE BEEN COMPLETED. JOB COMPLETE. REPAIR INSTALLATION OK, RII COMPLETE.QC1440. (LP# 8704688)
Part: NONE — NONE · airframe 15,210 hrs · 7,085 cycles
STRINGER 43 R DAMAGED FROM FRAME 28-29. REF LOG PAGE 8074668. REMOVED STR 43R FR 28 - 29 (491375) MATCH DRILLED "NEW" AIRBUS OE STRINGER 43R AND APPLIED TOPCOAT TO EXPOSED METAL (471692). OK TO INSTALL STR 43R (QC 1440). INSTALLED STRINGER SECTION PER A321 SRM 51-72-11-911-001. (LP# 2336648)
Part: NONE — NONE · airframe 15,199 hrs · 7,080 cycles
SHEAR CLIP BENT AND RIVETS DAMAGED, FWD BAG BIN FRAME 28 BETWEEN S41 AND S42. REMOVED SHEAR CLIP (CLEAT) (471692). MATCH DRILLED "NEW" CLIP CLEAT, APPLIED TOP COAT TO EXPOSED METAL (471692). OKAY TO INSTALL SHEAR CLIP (QC 1440). INSTALLED "NEW" AIRBUS OE CLEAT PER A321 SRM 51-72-11-911-001. ALSO, REF ER/A 600716-14 REV ORG. (LP# 2336604)
Part: NONE — NONE · airframe 15,199 hrs · 7,080 cycles
SKIN CLIP BENT AND RIVETS SHEARED, FWD BAGBIN FRAME STA 24A STRINGER 42R AND 43R. REMOVED DAMAGED CLIP AND ASSOCIATED FASTENERS (471692). MATCH DRILLED "NEW" CLIP AND TREATED EXPOSED METAL (471692). OKAY TO INSTALL CLIP (QC 1440). INSTALLED AIRBUS OE CLIP; REF A321 SRM 51-72-11-911-001. (LP# 2336592)
Part: NONE — NONE · airframe 15,199 hrs · 7,080 cycles
STRINGER CRACKED FWD BAG BIN. STR 42R APROX 9.5" FORWARD OF FRAME STA 28. REMOVED CRACKED SECTION (491375). C/W HFEC SCAN OF STRINGER 42 AT CUTOUT PER STEP 6 OF PRI 600716-14 REV 1. NO CRACKS NOTED ( QC1440). OKAY TO TREAT AND PAINT (QC5111). APPLIED ALODINE, PRIMER AND TOPCOAT (471692). OKAY TO INSTALL REPAIR PARTS (QC 1440). FABRICATED REPAIR PARTS AND INSTALLED PARTS PER A321 SRM 53-21-13-300-018 ALSO, REF ER/A 600716-14 REV ORG. (LP# 2336588)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 18,365 hrs · 8,407 cycles
DAMAGE TOLERANCE EVAULATION (DTE) TRACKING LOG FOR ER/A 600713- 14 COVERING REPAIR OF THE FUSELAGE SKIN NEAR C1 CARGO DOOR CUTOUT FR27-FR29 BTWN STRINGERS 39R AND 42L. REPAIR APPROVAL IS LIMITED TO 12 MONTHS SERVICE ONLY FROM 25-JUL -2022. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE OF THIS REPAIR LONGER THAN 12 MONTHS FROM REPAIR ACCOMPLISHMENT. ER/A 600713-14AD IS NOW AT REVISION A, WHICH REMOVES THE DTE RESTRICTION. OK TO CLOSE THIS LOG-PAGE. (LP# 2336128)
Part: NONE — NONE · airframe 15,199 hrs · 7,080 cycles
FRAME STIFFENER BENT. STR 41R FWD BAG BIN APROX 5" FWD OF STA 28. REMOVED WEB AT STRINGER 41 (471692). NEW WEB FABRICATED PER AIRBUS DRAWING D532305242 (PMSG) (471692). MATCH DRILLED NEW WEB AND APPLIED TOPCOAT TO EXPOSED METAL (471672). OKAY TO INSTALL PARTS (QC 1440). INSTALLED NEW WEB PER A321 SRM 51-72-11-911-001. (LP# 2336598)
Part: NONE — NONE · airframe 15,210 hrs · 7,085 cycles
STRINGER 41R DAMAGED FROM FRAME 28-29. REF LOF PAGE 8704668. REMOVED DAMAGED SECTION OF STRINGER 41 PER A321 SRM 51-42-11 ( 471692). C/W STR 41 OPEN HOLE INSP OR REMOVED FASTENERS IAW A321 NDTM 51-10-01 AND CUT OFF EDGES IAW A321 NDTM 51-10-08. NO CRACK INDICATIONS (QC 5285. OKAY TO TREAT AND PRIME (QC 5111). APPLIED ALODINE , PRIMER AND POLY TOP COAT TO REPAIR PARTS ( 471692). OKAY TO INSTALL PARTS (QC1440) INSTALLED STRINGER 41 REPAIR PARTS. REF ER/A 600716-14 REV ORG. (LP# 2336612)
Part: NONE — NONE · airframe 14,434 hrs · 6,747 cycles
SEAT ROW 3A FWD EMER LIGHT HAS RED LED. REMOVED & REPLACED SEAT MOUNTED EMER LIGHT REF A321 IPC 33-51-09 . OPS CK GOOD. (LP# 8595654)
2020
Part: GIRT BAR — OBSTRUCTED (L1 DOOR) · airframe 9,672 hrs · 4,580 cycles
SHIP 3021, L1 DOOR DO NOT ARMING. CORRECTIVE ACTION: MEGAPHONE STRAP FOUND AROUND GRID BAR, OK FOR SVC. PERFORMED L1 DOOR OPS TEST, OPS CHECK NORMAL.
Part: LATCH — FOD (L4 DOOR) · airframe 9,515 hrs · 4,502 cycles
SLIDE@DOOR 4L WILL NOT ARM. HANDLE HAS SPRINGY MOVEMENT UP. CORRECTIVE ACTION: REMOVED DEBRIS FROM LWR ARMING LATCH. OPS CHECKS GOOD. REF A320 AMM 52-71
Part: HOUSING — BROKEN (EMERGENCY LIGHT) · airframe 8,842 hrs · 4,232 cycles
(AIRCRAFT 3021, L/P 4613096) EMERGENCY LGT HOUSING BROKEN AT 29 A-B-C. CORRECTIVE ACTION: RPLCD HOUSING, REF IPC A321 33-50.