- Registered owner
- Wilmington Trust Co Trustee
- Location
- Wilmington, DE
- Owner type
- Corporation
- Serial number
- 7179
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- June 17, 2016
- Certificate issued
- June 28, 2018
- Expires
- June 30, 2028
- Mode S code
- A97C9A
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.
On this page
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.
| 1996 | 1 |
|---|---|
| 1997 | 2 |
| 1998 | 2 |
| 1999 | 4 |
| 2000 | 10 |
| 2001 | 7 |
| 2002 | 11 |
| 2003 | 3 |
| 2004 | 15 |
| 2005 | 15 |
| 2006 | 14 |
| 2007 | 15 |
| 2008 | 8 |
| 2009 | 13 |
| 2010 | 6 |
| 2011 | 12 |
| 2012 | 10 |
| 2013 | 14 |
| 2014 | 17 |
| 2015 | 17 |
| 2016 | 22 |
| 2017 | 24 |
| 2018 | 27 |
| 2019 | 20 |
| 2020 | 24 |
| 2021 | 16 |
| 2022 | 21 |
| 2023 | 18 |
| 2024 | 14 |
| 2025 | 22 |
| 2026 | 17 |
See all 421 ADs
Information bulletins that may apply · 6
Advisory, not mandatory.
Airframe · Airbus A321-211
SAIB NE-19-03Escape Slide Maintenance Tasks and Intervals - JASC 2565SAIB NM-14-21Communications: Honeywell RTA 44D VHF TransceiversSAIB 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 CFM56-5B3/3 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 N710FRMatched 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 · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR F3LA202511060323Throttle · fodTHIRD WRITE-UP THRUST LEVERS STIFF. REQUIRES SO MUCH FORCE TO COME OUT OF REVERSE THAT LEVERS INADVERTENTLY GO TO CLIMB DETENT. PERFORMED ENGINE THROTTLE CONTROL LEVERS TROUBLESHOOT AND ADJUSTED THE MECHANICAL LINKAGE PER AMM 76-11-00-820-044-A ADJUSTMENT WISDR F3LA2024040300044Unknown · odorAIRCRAFT WAS GROUNDED DUE TO FUME EVENT AFTER ENGINE START UP. PERFORMED TSM 05-50-00-810-813-A AND PERFORMED TYPE 7 INSPECTION ALSO PERFORMED PACK BURN OUT, ENGINE RUNS AND RAN APU. NO ODOR NOTED. A/C OK FOR SERVICE.SDR F3LA2022063000064Shear Plate · corrodedDISCREPANCY: REFERENCE PEMCO N/R# 12509.0391 R/H LATERAL SHEAR PLATE AT STA. 69 TO STA. 70 HAS 2 E.A SPOTS AO CORROCION
CORRECTIVE ACTION: REMOVED AND REPLACED R/H LATERAL SHEAR PLATE AT STA69 - STA70 IAW SRM 51-72-11-911-001SDR F3LA2022063000065Floorbeam · corrodedDISCREPANCY: REFERENCE PEMCO N/R# 12509.0393 CABIN FLOOR BEAM -Y765 AT STA. 66 TO STA. 68 HAVE MULTIPLE SPOTS OF CORROSION OVER TOP SURFACE.
CORRECTIVE ACTION: REMOVED AND REPLACED CABIN FLOORBEAM -Y765 STA66 TO STA68 IAW AIRBUS SRM 51-72-11-911-001SDR F3LA2022051600036Slide Raft · burnedDISCREPANCY: REFERENCE LP 215183 DOOR L1 SLIDE WILL NOT ARM
CORRECTIVE ACTION: REMOVED AND REPLACED L1 DOOR SLIDE OPS CHECK GOOD. A/C OK FOR SERVICE. TORQUE WRENCH S/N 217101623 CAL DUE 23NOV22SDR F3LA2022011700103Slide · detachedDISCREPANCY: DOOR 1R WAS UNABLE TO BE ARMED WHEN FA PRESSED ARMING LEVER IN TO POSITION. CORRECTIVE ACTION: ADJUSTED GIRT BAR REF AMM 25-62-44-400-007-A OPS CHECK OF SLIDE/ARM DISARM GOOD AT THIS TIME. A/C OK FOR SERVICE.SDR F3LA2020120100047Proximity Sensor · malfunctionedITEM 2: RED UNLOCK LIGHT ON MAIN LANDING GEAR INDICATOR STAYED ON FOR 2 MINUTES AFTER GEAR DOWN ALTITUDE WAS 2200 MSL SPEED WAS 170 KTS. CORRECTIVE ACTION: REF LP 146003 ITEM 1,2,3 FOR R & R OF PROX SENSORS. REF LP 146004 ITEM 1 FOR R & R OF ANNUNCIATOR LIGHTSDR F3LA201907180054A/C Pack · faultyDISCREPENCY: LP1206133-1: ON DECENT CHEMICAL SMELL FLIGHT DECK AND CABIN. CORRECTIVE ACTION: LP1206133-1: PERFORMED T/S PER TSM 05-50-00-810-831A, FAULT ISOLATED TO PACK 1, DEACTIVATED PACK 1 IAW AMM 21-51-00-040-002-A. PACK 1 PLACED ON DEFERRAL AS CN 115268SDR F3LA2019010700005Drain Valve · leakingDISCREPANCY: REFERENCE LOG PAGE LP1149776 ITEM 1, IN FLIGHT AT CRUISE FL360, "HYD G RSVR LO LVL". PERFORMED MANUAL GEAR EXTENSION FOR LANDING. CORRECTIVE ACTION: REPLACED THE DRAIN VALVE, GREEN HYDRAULIC RESEVOIR, REFERENCE AMM 29-11-41-000-004-A AND 29-11-41-SDR F3LA2018082100394Unknown · odorAIR TURN BACK DUE TO THE FA REPORTED A ROTTEN EGG, DIRTY SOCK ODOR. DURING CLIMB OUT, WITH BOTH PACKS ON. AFTER TURNING THE NR 2 PACK OFF, THE ODOR WAS STILL APPARENT AND RETURNED TO DEPARTURE. PERFORMED IDENTIFICATION OF CABIN ODOR IAW AMM 05-50-00-810-83SDR F3LA2017121400263Smoke Detector · false indicationDISCREPANCY: PILOTS DECLARED AN EMERGENCY AND DIVERTED TO GEG DUE TO AFT CARGO SMOKE DETECTION/INDICATION.
CORRECTIVE ACTION: INSPECTED FWD AND AFT CARGO PITS FOR SIGNS OF SMOKE, FIRE AND FUMES. CARGO PITS FWD AND AFT EMPTY. R & R THE SMOKE DETECTORS.
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