- Registered owner
- Umb Bank Na Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 7095
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- May 13, 2016
- Certificate issued
- November 21, 2024
- Expires
- November 30, 2031
- Mode S code
- A21432
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56-5B4/3 model are included below.
On this page
Airworthiness directives that may apply · 381
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1990 | 5 |
|---|---|
| 1991 | 1 |
| 1992 | 6 |
| 1993 | 10 |
| 1994 | 10 |
| 1995 | 4 |
| 1996 | 5 |
| 1997 | 9 |
| 1998 | 20 |
| 1999 | 14 |
| 2000 | 13 |
| 2001 | 8 |
| 2002 | 12 |
| 2003 | 3 |
| 2004 | 23 |
| 2005 | 20 |
| 2006 | 13 |
| 2007 | 16 |
| 2008 | 9 |
| 2009 | 13 |
| 2010 | 7 |
| 2011 | 12 |
| 2012 | 12 |
| 2013 | 17 |
| 2014 | 18 |
| 2015 | 23 |
| 2016 | 25 |
| 2017 | 24 |
| 2018 | 31 |
| 2019 | 23 |
| 2020 | 29 |
| 2021 | 16 |
| 2022 | 22 |
| 2023 | 19 |
| 2024 | 15 |
| 2025 | 21 |
| 2026 | 17 |
See all 545 ADs
Information bulletins that may apply · 8
Advisory, not mandatory.
Airframe · Airbus A320-214
SAIB NE-19-03Escape Slide Maintenance Tasks and Intervals - JASC 2565SAIB NM-15-02Cabin Equipment/FurnishingsSAIB NM-14-21Communications: Honeywell RTA 44D VHF TransceiversSAIB NM-13-24Air Conditioning System: Air Distribution FanSAIB NM-13-03Hydraulic Power System: Power Transfer UnitSAIB NM-06-57Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.Engine · CFM International CFM56-5B4/3 series
SAIB NE-08-17R3Turbine Section - Propulsion Technology LLC Unapproved RepairSAIB NE-12-29Engine Fuel Distribution CFM56-5B LPTACC Fuel ManifoldHistorical bulletins · 1
NTSB investigations
No NTSB investigations matched to N233FRMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Airbus A320-214 aircraft
FAA incident reports
No FAA accident or incident reports matched to N233FRMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Airbus A320-214 aircraft
Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR F3LA2024012800010Engine · bird ingestionDISCREPANCY REFERENCE LP369793, ITEM 1: AIR TURN BACK FOR BIRD STRIKE OUT OF MCO. NO ABNORMAL ENGINE INDICATIONS NOTED, BUT THERE WAS A BURNING SMELL IN CABIN. MAINTENANCE ACTION: FOUND BIRD REMAINS AROUND ENG #2. PERFORMED ENG BORESCOPE (REF LP369795, ITEM 3SDR F3LA2023230100014A/C Pack · odorDURING CRUISE. TURNED UP COCKPIT HEAT, IMMEDIATELY GOT AN ODOR OF HOT DUCTING IN COCKPIT. TURNED HOT DOWN &ODOR SEEMED TO DISSIPATE. PERFORMED ELIMINATION OF ODOR IN FLT DECK/CABIN. PACK 1 SUSPECTED. TURNED OFF PACK 1 IAW QRL, NO ODOR DETECTED. LT PACK OFF FOSDR F3LA2023230100013Hydraulic Line · looseSTRONG BURNING ODOR REPORT BY ALL FAS IN CABIN. COCKPIT ALSO BEGAN TO SMELL. TURNED OFF PACKS, DID NO SOLVE PROBLEM. AIR DIVERT TP PHX. NO SMOKE OR FLAME. IAW TSM 05-50-00-810-810-831-A, FOUND ODOR EVENT TO BE TYPE 7. PERFORMED CHECK FOR LEAKS OF HYD CMPNTSSDR F3LA2022281200174Pressure Switch · defectiveAT THE GATE ECAM FOR EXCESSIVE RESIDUAL CABIN PRESSURE AS WELL AS THE RED CABIN PRESSURE LIGHT FLASHING ON ALL DOORS, OUTFLOW VALVE SHOWED FULLY OPEN. REMOVED AND REPLACED CABIN PRESSURE DETECTION PRESSURE SWITCH (14WN) OPS TEST GOOD, REF. AMM 52-73-12-000-0SDR F3LA2022030400003Slide Raft · faultyDISCREPANCY: LP195777 ITEM 2. DURING RON MAINTENANCE, L1 DOOR SLIDE FAILED EPSU TEST
CORRECTIVE ACTION: REMOVED AND REPLACED L1 DOOR SLIDE, OP'S CHECK GOOD. TORQUE WRENCH S/N F9TAB2940C. REF AMM 25-62-44-000-012-A AND 25-62-44-400-007-ASDR F3LA2022012600093Floorbeam · corrodedDISCREPANCY: REF PEMCO N/R #11918.0285 FWD FUSELAGE UNDERNEATH FLOOR BOARDS, AT FR 16 DUMMY BEAM FWD SECTION ABOUT 6 INCHES AREA CORRODED.
CORRECTIVE ACTION: REMOVED AND REPLACED FWD FUSELAGE UNDRENEATH FLOOR BOARDS AT FR 16 DUMMY BEAM FWD SECTION IAW A320 SRSDR F3LA2022012600090Plate · corrodedDISCREPANCY: REF PEMCO N/R #11918.0293 AFT FUSELAGE R/H SIDE BETWEEN FR 69 AND FR 70 SHEAR PLATE WEB CORRODED AT SEVERAL ATTACHMENT HOLES.
CORRECTIVE ACTION: REMOVED AND REPLACED SHERE WEB PLATE BETWEEN FRO 69 AND FR70 FUSELAGE R/H IAW A320 SRM 51-42-11.SDR F3LA2022012600091Plate · corrodedDISCREPANCY: REFERENCE PEMCO N/R #11918.0288 AFT FUSELAGE L/H SIDE AT FR 70 SHEAR WEB CORRODED AT END NEXT TO RIVET ATTACHMENT.
CORRECTIVE ACTION: CORRODED SHERE WEB REMOVED AND REPLACED AND PAINTED, VOR CABLES DISPLACED AND REINSTALLED, OPS CHECK GOOD IAW A3SDR F3LA2022012600092Floorbeam · corrodedDISCREPANCY: REFERENCE PEMCO N/R# 11918.0289 AFT FUSELAGE L/H SIDE AT FR68, (Y765) FLOOR BEAM CORRODED
CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR BEAM L/H FR68 (Y765) IAW A-320 SRM 51-42-11, SRM 51-74-00, SRM 53-00-14-283-002SDR F3LA2021061400043Brake Assy · defectiveDISCREPANCY: DURING TAXI IN AFTER LANDING, PARKING BRAKE WAS APPLIED. WHEN RELEASED THE RIGHT BRAKES STUCK AND CHATTERED. WE STOPPED THE AIRCRAFT. BRAKES HEATED TO 595 DEGREES. WHEN COOLED BELOW 500 DEGREES WE TAXIED TO THE GATE. FOUND #3 BRAKE ASSEMBLY DRSDR F3LA2020021090007Power Supply · unknownL1 DOOR (EPSU (10WL) WILL NOT PASS SYSTEM TEST. PERFORMED OPS CHECK OF EPSU (10WL) PER TSM 33-51-00-810-282-A. OPS CHECK GOOD, NO DEFECTS NOTED.SDR F3LA2018122600483Battery · failedDISCREPANCY: REFERENCE LOG PAGE LP1133269 ITEM 1. FAILED EPSU SYSTEM TEST.
CORRECTIVE ACTION: REMOVED AND REPLACED EPSU 10WL AND EPSU 12WL. OPS CHECK GOOD. REF AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A./END/SDR F3LA2018061400356Battery Pack · inoperativeEPSU 10WL FORWARD LEFT, FAILED TO TEST. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-38 PB 401. OPS CHECKED GOOD.SDR F3LA2018061400355Power Supply · no testEPSU 13WL AFT LEFT FAILED TO TEST. REMOVED AND REPLACED THE R1 DOOR SLIDE IAW AMM 25-62-44-400-007-A. OPS TESTED OK.
STCs that may be installed · 301
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 301 STCs