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N708FR

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2015 Airbus A321-211 · CFM International CFM56-5B3/3 series

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© OpenStreetMap
Registered owner
Wilmington Trust Co Trustee
Location
Wilmington, DE
Owner type
Corporation
Serial number
7042
Year built
2015
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
March 24, 2016
Certificate issued
August 28, 2018
Expires
August 31, 2028
Mode S code
A972D3
Airbus A321-211Airframe model · 199 seats · 2 engines · 106 registeredTCDS A28NMAirframe · Airbus A321-211Engine modelCFM International CFM56-5B3/3 series

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every CFM International CFM56-5B3/3 model are included below.

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Airworthiness directives that may apply · 281

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1996In forceSuperseded2026
See all 421 ADs

Information bulletins that may apply · 6

Advisory, not mandatory.

Historical bulletins · 1
SAIB NE-08-17R2Turbine Section - Propulsion Technology LLC Unapproved RepairIssued Mar 7, 2011

NTSB investigations

No NTSB investigations matched to N708FRMatched 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 A321-211 aircraft

FAA incident reports

No FAA accident or incident reports matched to N708FRMatched 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 A321-211 aircraft

Service difficulty reports · 9

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR F3LA202505090230Actuator · defectiveENTERED ON LP506396 ITEM 1-REF LP506394 ITEM 1 UNCOMMANDED RUDDER MOVEMENT IN FLIGHT FL350 M 0.77 SMOOTH AIR RUDDER TRIM WENT TO LEFT 2.3 DEGREES AND THEN MOVED TO THE LEFT 1.8 DEGREES. MAINTENANCE ACTION AS ENTERED ON LP506396, ITEM 1 REMOVED AND REPLACED RMay 9, 2025 · N708FR · Airbus A321211 · Rudder Tab Control SystemSDR F3LA2022030200002Floorbeam · corrodedDISCREPANCY: REFERENCE PEMCO N/R 11998.0364 FS 68-Y160.5 LONGITUDINAL BEAM CORRODED ON UPPER SURFACE OF BEAM CAP. CORRECTIVE ACTION: REMOVED AND REPLACED FS 68-Y160.5 LONGITUDINAL BEAM IAW A321 SRM 51-42-11Jan 29, 2022 · N708FR · Airbus A300* · Fuselage Main, StructureSDR F3LA2022012600100Floorbeam · corrodedDISCREPANCY: REFERENCE PEMCO N/R #11998.0367 FR66-FR-70-Y765 LONGITUDINAL BEAM CORRODED ON UPPER SURFACE OF BEAM CAP. CORRECTIVE ACTION: EVALUATED & REPLACED WET AREA FLOOR BEAM Y765 FR66-FR70 IAW A321 SRM 53-00-14-283-002, 51-44-11 & 51-72-11-911-001Jan 29, 2022 · N708FR · Airbus A321211 · Fuselage Main, StructureSDR F3LA2022012600099Floorbeam · corrodedDISCREPANCY: REFERENCE PEMCO N/R 11998.0366 LONGITUDINAL BEAM FROM FS 65-FS 66-Y919 CORRODED AROUND AFT MOUNTING LUG HOLE. CORRECTIVE ACTION: EVALUATED & REMOVED AND REPLACED LONGITUDIONAL BEAM FROM FR65-66-Y919 IAW A321 SRM 53-00-14-283-002 & SRM 51-72-11-911Jan 29, 2022 · N708FR · Airbus A321211 · Fuselage Main, StructureSDR F3LA2022012600098Floorbeam · corrodedDISCREPANCY: REFERENCE PEMCO N/R# 11998.0363 FR66-FR70 Y65 LONGITUDINAL BEAM CORRODED ON UPPER SURFACE OF BEAM CAP. CORRECTIVE ACTION: EVALUATED & REPLACED WET AREA FLOORBEAM Y765 FR66 TO FR70 IAW A321 SRM 53-00-14-283-002, 51-44-11 & 51-72-11-911-001Jan 29, 2022 · N708FR · Airbus A321211 · Fuselage Main, StructureSDR F3LA2022011700101Floorbeam · corrodedDISCREPANCY: REFERENCE PEMCO N/R #11998.0298 FWD WET AREA: FLOORBEAM Y-254 MAIN BEAM CORRODED BETWEEN FR12-FR16. CORRECTIVE ACTION:REPAIRED Y-254 FLOOR BEAM AT FR16 IAW A321 SRM 53-11-14-300-001 PER DOSSIER REF 81021673Jan 28, 2022 · N708FR · Airbus A321211 · Fuselage Main, StructureSDR F3LA2022011700097Floorbeam · corrodedDISCREPANCY: REFERENCE PEMCO NR#11998.0300 FWD WET AREA: FLOORBEAM Y-254 MAIN BEAM CORRODED BETWEEN FR12-FR16 CORRECTIVE ACTION:REMOVED CORROSION AREA, AFTER EVALUATION FOUND TO BE OUT OF LIMITS OF CLIP-NUT AROUND IAW A 321 SRM 53-11-14-283-007. REMOVED AND REJan 28, 2022 · N708FR · Airbus A321211 · Fuselage Main, StructureSDR F3LA2022011700096Floorbeam · corrodedDISCREPANCY: REFERENCE PEMCO NR#11998.0297 FWD WET AREA: FLOORBEAM Y-1292 MAIN BEAM CORRODED BETWEEN FR12-FR18 CORRECTIVE ACTION: EVALUATED AND REPAIRED FWD WET AREA FLOOR BEAM Y-1292 BETWEEN FR-12 AND FR-18 IAW A321 SRM 53-11-15-300-005 PER AIRBUS DOSSIER#81Jan 28, 2022 · N708FR · Airbus A321211 · Fuselage Main, StructureSDR F3LA2022011700089None · noneREFERENCE LOG PAGE LP 206435 ITEM 2, IN FLIGHT ENG 1 STALL ECAM WITH VIBRATIONS, OIL PRESSURE XX, LOUD NOISE ASSOCIATED WITH THE STALL. ALTITUDE WAS 25,000. - AIRCRAFT IS GROUNDED. CORRECTIVE ACTION: REMOVED AND REPLACED #1 ENGINE ASSEMBLY REF MP71042-01, MP7Jan 15, 2022 · N708FR · Airbus A321211 · Engine Fuel and Control

STCs that may be installed · 223

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 223 STCs