# Service difficulty reports: N546FF

A list on [N546FF](https://openairdocs.org/aircraft/N546FF.md).

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

Page 1 of 2 · 80 reports

- [SDR VNAA202610230005](https://openairdocs.org/sdr/VNAA202610230005.md): Skin · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION ON STRUCTURE INNER SKIN AREA WHERE MAIN AVIONICS COMPARTMENT DOOR SEAT STRUCTURE INNER SKIN AREA WHERE MAIN AVIONICS COMPARTMENT DOOR SEAT WAS REPAIRED PER REO: 670-53-21-242 REV: - C.
- [SDR VNA2026F00010](https://openairdocs.org/sdr/VNA2026F00010.md): Skin · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION ON STRUCTURE INNER SKIN AREA WHERE MAIN AVIONICS COMPARTMENT DOOR SEAT STRUCTURE INNER SKIN AREA WHERE MAIN AVIONICS COMPARTMENT DOOR SEAT WAS REPAIRED PER REO: 670-53-21-242 REV: - C.
- [SDR VNAA202610230004](https://openairdocs.org/sdr/VNAA202610230004.md): Strap · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON STRUCTURE WHERE ACCESS PANEL 195AB SEAT CORROSION ON STRUCTURE WHERE ACCESS PANEL 195AB SEAT WAS REMOVED PER CRJ 700 SRM 51-21-06-001-001-A01 AND EVALUATED (SEAT BTW FS 847) WITHIN OF LIMIT AND SEAT BTW FS 849 TO FS 879 WAS EVALUATED OUT OF LIMITS
- [SDR VNAA202610230003](https://openairdocs.org/sdr/VNAA202610230003.md): Support · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Aerodynamic Fairings
  > CORROSION ON FAIRING SUPPORT (FRAMES) 2 EAS STA BS 629 AND 661 AND DIAFRAGMA 1EA BTW FS 629-FS 661 (SEATLEMENT AREA, UNDER ACCESS PANELS 191 AB, 191BB AND 192BB) SUMMARY:CORROSION WAS REMOVED PER 51-42-06-001-001-A01 AREA WAS EVALUATE PER SRM 53-82-55-101-0
- [SDR VNAA202610230002](https://openairdocs.org/sdr/VNAA202610230002.md): Bracket · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Main Landing Gear
  > CORROSION ON ANTI-ROTATION BEAM ASSY ON LT FWD DOOR HINGE AT NLG W/W. CORROSION ON ANTI-ROTATION BEAM ASSY WAS REMOVED IAW SRM 51-21-06-001-001-A01. AND AREA IT IS OUT LIMITS PER SRM 53-00-00-101-001-A01 AND ANTI-ROTATION BEAM ASSY ON LT FWD DOOR HINGE AT NLG
- [SDR VNAA202610230001](https://openairdocs.org/sdr/VNAA202610230001.md): Hinge · corroded · Oct 23, 2026 · N546FF · Cndair CL6002C10 · Wing, Control Surface Attach Fittings
  > "IN REF TASK TRFKE00AXBMU: AFTER REMOVAL OF BUSHINGS THE MOUNTING HOLES FOR HINGES ASSY # 3 (2EA) ON RH AILERON REAR SPAR WERE OVERSIZED AND AFTER REMOVAL OF BUSHINGS THE MOUNTING HOLES FOR HINGE ASSY 2# S (1EA) ON LH AILERON REAR SPAR WAS OVERSIZED ON HOLES
- [SDR VNAA2026050617501](https://openairdocs.org/sdr/VNAA2026050617501.md): Steering Sys · faulted · May 5, 2026 · N546FF · Cndair CL6002C10 · Landing Gear Steering System
  > NOSE WHEEL STEERING INOP. JACK NOSE OF AIRCRAFT TO DUE NLG GEAR SWING IAW AMM 32-30-00-865-802-A01. OPS CHECK GOOD. DID STEERING BITE TEST IAW AMM 32-50-00-740-801-A01. OPS CHECK GOOD AT THIS TIME. OPS CHECK GOOD DURING TAXI NO ISSUES FAULT DIDN€™T RECUR.
- [SDR VNAA2025122611101](https://openairdocs.org/sdr/VNAA2025122611101.md): Transducer · leaking · Dec 24, 2025 · N546FF · Cndair CL6002C10 · Hydraulic System, Main
  > HYD SYSTEM 2 LOW PRESSURE CAUTION MSG. IN FLIGHT. EMER DECLARED. / UPON ARRIVAL TO AIRCRAFT CLEANED AFFECTED AREA AND FOUND LEAK COMING FROM THE SYSTEM #2 PRESSURE TRANSDUCER. FOUND THE PRESSURE TRANSDUCER TO BE LOOSE AND HAD A CRUSHED O-RING. REPLACED O-RING
- [SDR VNAA2025091411101](https://openairdocs.org/sdr/VNAA2025091411101.md): Safety Valve · faulted · Sep 10, 2025 · N546FF · Cndair CL6002C10 · Cabin Pressure Control System
  > CABIN PRESSURIZATION FAILED IN DESCENT INTO BHM. APPROX 15000FT PRESSURIZATION BECAME ERRATIC AND CABIN ALT STARTED TO INCREASE. AT 8500FT AMBER CABIN ALT THEN RED CABIN ALT. RAN QRC/ARH FOR CABIN ALT. REMOVED AND REPLACED NR 2 SAFTEY VALVE IAW AMM 21-32-03-0
- [SDR VNAA2025072311101](https://openairdocs.org/sdr/VNAA2025072311101.md): Duct · leaking · Jul 17, 2025 · N546FF · Cndair CL6002C10 · Pneumatic System
  > L BLEED DUCT CAUTION MSG IN FLIGHT. / UPON LEAK CHECK FOUND LEAK AT LH CONNECTOR DUCT FWD OF FLOW CONTROL VALVE AND AT APU BLEED AIR CHECK VALVE. REMOVED AND REPLACED CONNECTOR DUCT IAW AMM 36-19-03-000/400. PERFORMED LEAK TEST IAW AMM 36-10-00-790-801. LEAK
- [SDR VNAA2025041411102](https://openairdocs.org/sdr/VNAA2025041411102.md): Anti-Skid Sys · faulted · Apr 13, 2025 · N546FF · Cndair CL6002C10 · Brake Anti-Skid Section
  > A\SKID FAULT IN FLIGHT. PERFORMED HYDRAULIC SYS 1,2,AND 3 BLEED IAW AMM 29-10-00-870-801-A01 AND 29-10-00-870-802-A01. ACCOMPLISHED GVI OF BRAKE-UNIT ASSEMBLY WEAR-PIN INDICATOR IAW CRJ 700 AMM 32-43-26-210-801-A01. NO DEFECTS NOTED AT THIS TIME. FLT CREW CO
- [SDR VNAA202504140037](https://openairdocs.org/sdr/VNAA202504140037.md): Post · corroded · Apr 7, 2025 · N546FF · Cndair CL6002C10 · Fuselage Main, Structure
  > VERTICAL POST LBL12 IS CORRODED AT F.S.280 FRAME AND STRINGER 25L REMOVED VERTICLE POST AT LBL12 AND INSTALLED NEW SERVICEABLE VERTICLE POST P/N CC670-34180-7 AT LBL12 F.S 280 WITH NEW IAW CRJ 700 SRM 51-42-13-001-001-A01 AND 51-42-21-001-001-A01
- [SDR VNAA202504140036](https://openairdocs.org/sdr/VNAA202504140036.md): Lock Fastener · sheared · Apr 7, 2025 · N546FF · Cndair CL6002C10 · Leading Edge Devices
  > LOCK FASTENER HEAD IS SHEARED AT RIGHT SLAT LEADING EDGE AT SLAT TRACK 1-1 POSITION. CORRECTIVE ACTION: REPLACED RH LE SLAT PANEL SHEARED RIVET AT SLAT TRACK 1-1 WITH A NEW SERVICEABLE HI-LITE PN: PLT1092-6 IAW MHIRJ CRJ 700 REO 670-57-42-2041 REV-- DATED 03/2
- [SDR VNAA202504140035](https://openairdocs.org/sdr/VNAA202504140035.md): Stringer Clip · corroded · Apr 7, 2025 · N546FF · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > GUSSET AT STR 20 FS 333 FOUND TO BE DAMAGED REQUIRES REPLACEMENT. FABRICATED NEW SERVICEABLE GUSSET P.O.#5-39394 IAW CRJ 700 SRM 51-24-36-001-001-A01. DRILLED AND LOCATED HOLES IN NEW SERVICEABLE GUSSET IAW CRJ 700 SRM 51-40-11-001-001-A01. PRIMED AND PAINTE
- [SDR VNAA202504140034](https://openairdocs.org/sdr/VNAA202504140034.md): Bulkhead Web · corroded · Apr 7, 2025 · N546FF · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > FS 280 LH LOWER WEB HAS CORRSION. REPAIRED LH LOWER WEB IAW CRJ 700 SRM 53-11-10-201-004-A01
- [SDR VNAA202504140033](https://openairdocs.org/sdr/VNAA202504140033.md): Floorbeam · corroded · Apr 7, 2025 · N546FF · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS 280.00 FWD FLOOR SUPPORT J-ANGLE IS SEVERELY CORRODED. REQUIRES REPLACEMENT. ORIGINAL MATERIAL THICKNESS IS.063. REMOVED DAMAGE DEPTH IS.018. MAX ALLOWED IS.006. REMAINING THICKNESS IS.045. REMOVED AND REPLACE FS 280.00 FWD FLOOR SUPPORT J-ANGLE P/N C
- [SDR VNAA202504140032](https://openairdocs.org/sdr/VNAA202504140032.md): Intercostal · corroded · Apr 7, 2025 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > HN00228605 DISCREPANCY: INTERCOSTAL AT STRINGER 20R BETWEEN F.S.319-F.S.333 HAS LIGHT CORROSION AROUND RIVET HEAD ADJACENT TO GS328. CORRECTIVE ACTION: REMOVE INTERCOSTAL AT STRINGER 20R BETWEEN F.S.319-333 IAW CRJ700 SRM 51-42-06-001-001-A01 & 51-42-21-001-00
- [SDR VNAA202504140031](https://openairdocs.org/sdr/VNAA202504140031.md): Intercostal · corroded · Apr 7, 2025 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > HN00228604 DISCREPANCY: INTERCOSTAL AT STRINGER 20R IS CORRODED BETWEEN F.S.310-319 CORRECTIVE ACTION: REMOVE INTERCOSTAL AT STRINGER 20R BETWEEN F.S.310-319 AND INSTALLED NEW SERVICEABLE INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-23-00-001-001-A01,
- [SDR VNAA202504140030](https://openairdocs.org/sdr/VNAA202504140030.md): Angle · corroded · Apr 7, 2025 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CLIP/KLEAT (ANGLE) @ FS310.00 STGR 20, FOUND TO BE CHAFED, CORRODED, REQUIRES R&R CORRECTIVE ACTION: DRILLED, LOCATED, AND INSTALLED NEW SERVICEABLE P/N(SH670-32046-3) CLIP/KLEAT(ANGLE) @ FS310.00 STGR 20 IAW CRJ700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A
- [SDR VNAA2024051511101](https://openairdocs.org/sdr/VNAA2024051511101.md): Selector Valve · unserviceable · May 13, 2024 · N546FF · Cndair CL6002C10 · Landing Gear Retraction/Extension System
  > HAD GEAR DISAGREE WARNING MSG AT GEAR RETRACTION. RAN QRC\QRH. GEAR SUCCESSFULLY LOCKED IN DOWN POSITION / INTERROGATED MDC FOUND B1 005969. PREFORMED TROUBLESHOOTING IAW CRJ 700 FIM 32-31-00-810-804. PREFORMED OPERATIONAL CHECK IF THE LANDING GEAR EXTENSIO
- [SDR VNAA202308311112](https://openairdocs.org/sdr/VNAA202308311112.md): Unknown · unknown · Aug 30, 2023 · N546FF · Cndair CL6002C10 · Air Distribution System
  > SMOKE/ABNORMAL SMELL IN THE COCKPIT FIM FASK NEEDS TO BE C/W DUE TO POSSIBLE ARCING. PERFORMED SMOKE/ABNORMAL SMELL IN THE COCKPIT CHECK IAW CRJ700 FIM 21-21-00-810-806-A01 AND CHECK GOOD.NO SIGN OF SMOKE OR BURN.
- [SDR VNAA202211209992](https://openairdocs.org/sdr/VNAA202211209992.md): Seat Track · corroded · Oct 17, 2022 · N546FF · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL (SEVERAL LOCATIONS), PAX CABIN. (REF. FS661+13" TO FS708+5").
- [SDR VNAA202211209991](https://openairdocs.org/sdr/VNAA202211209991.md): Skin Panel · nicked · Oct 17, 2022 · N546FF · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > NICKS ON FWD CARGO CUT OUT SURROUND SKIN (FWD, REAR & UPPER FRAMES).
- [SDR VNAA2022112099910](https://openairdocs.org/sdr/VNAA2022112099910.md): Stringer Splice · corroded · Oct 16, 2022 · N546FF · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > AFTER REMOVAL OF STRINGER 21RH, CORROSION WAS FOUND ON STGR SPLICE 21R AT FS 333.00 ON MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURE
- [SDR VNAA202211209998](https://openairdocs.org/sdr/VNAA202211209998.md): Seat Track · corroded · Oct 9, 2022 · N546FF · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL RBL9 & BTW FS485 - FS581.. AT PAX CAB.
- [SDR VNAA202211209997](https://openairdocs.org/sdr/VNAA202211209997.md): Seat Track · corroded · Oct 9, 2022 · N546FF · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL LBL9 & BTW FS485 - FS581. AT PAX CAB.
- [SDR VNAA202211209996](https://openairdocs.org/sdr/VNAA202211209996.md): Seat Track · corroded · Oct 9, 2022 · N546FF · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL LBL27 & BTW FS581 - FS693. AT PAX CAB.
- [SDR VNAA202211209995](https://openairdocs.org/sdr/VNAA202211209995.md): Seat Track · corroded · Oct 9, 2022 · N546FF · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL LBL27 & BTW FS485 - FS581. AT PAX CAB.
- [SDR VNAA202211209994](https://openairdocs.org/sdr/VNAA202211209994.md): Seat Track · corroded · Oct 9, 2022 · N546FF · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL LBL27 & BTW FS364 - FS485. AT PAX CAB
- [SDR VNAA202211209999](https://openairdocs.org/sdr/VNAA202211209999.md): Intercostal · corroded · Oct 8, 2022 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION AT INTERCOSTAL (3 EAS) BETWEEN STRG 25L TO STRG 25R AND BETWEEN FS 349 TO FS364.
- [SDR VNAA202211209993](https://openairdocs.org/sdr/VNAA202211209993.md): Seat Track · corroded · Oct 8, 2022 · N546FF · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL BTW FS661+13" TO FS708+5”
- [SDR VNAA2022112099918](https://openairdocs.org/sdr/VNAA2022112099918.md): Frame · corroded · Oct 5, 2022 · N546FF · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION ON FRAME AT FS 1015.00 BTW STGR 26LH AND 26RH ON AFT CARGO COMPARTMENT INTERNAL STRUCTURE
- [SDR VNAA2022112099917](https://openairdocs.org/sdr/VNAA2022112099917.md): Frame · corroded · Oct 5, 2022 · N546FF · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION ON FRAME AT FS 1047.00 BTW STGR 25LH AND 24LH ON AFT CARGO COMPARTMENT INTERNAL STRUCTURE
- [SDR VNAA2022112099915](https://openairdocs.org/sdr/VNAA2022112099915.md): Frame · corroded · Oct 5, 2022 · N546FF · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION ON FRAME FS 1088.20 BTW STGR 26LH AND 26RH ON AFT CARGO COMPARTMENT INTERNAL STRUCTURE
- [SDR VNAA2022030310111](https://openairdocs.org/sdr/VNAA2022030310111.md): Windshield · unserviceable · Mar 1, 2022 · N546FF · Cndair CL6002C10 · Flight Compartment Windows
  > ON DECENT INTO DCA CA SIDE WINDSHIELD ARCHED AND OVERHEATED. DECLARED EMERGENCY LANDED WITHOUT INCIDENT. TAXI TO GATE MX HAS BEEN CALLED. TRUCKES ROLLED AIRCRAFT CANNOT BE FERRIED. ORF ROAD TRIP IS BE PUT TOGETHER. / REPLACED CAPT WINDSHIELD IAW CRJ 700 AMM 56
- [SDR VNAA202105311112](https://openairdocs.org/sdr/VNAA202105311112.md): Windshield · sparks · May 29, 2021 · N546FF · Cndair CL6002C10 · Flight Compartment Windows
  > ON APPROACH INTO CVG, CAPTAIN AND FO STARTED SEEING SPARKS COMING FROM THE FRONT RIGHT WINDSCREEN. RAN THE QRH AND DECLARED. LANDED SAFELY AND HAD FIRE AND RESCUE CHECK THEIR WINDSHIELD FOR HEAT. CREW NOTICED A VISIBLE CRACK. MX HAS BEEN ADVISED. REMOVED AND
- [SDR VNAA2020041811101](https://openairdocs.org/sdr/VNAA2020041811101.md): Cooling Fan · failed · Apr 16, 2020 · N546FF · Cndair CL6002C10 · Air Distribution Fan
  > BURNING SMELL IN COCKPIT WITH DISPLAY COOL MSG. REMOVED AND REPLACED #2 DISPLAY COOLING FAN IAW CRJ-700 AMM. OPS CHECK GOOD.
- [SDR VNAA2020041111101](https://openairdocs.org/sdr/VNAA2020041111101.md): Hydraulic Line · damaged · Apr 9, 2020 · N546FF · Cndair CL6002C10 · Hydraulic System, Main
  > HYDRAULIC 3B LOW PRESSURE CAUTION JUST AFTER TAKING HIGH SPEED EXIT C10 36R. FIRE DEPARTMENT TRUCKS NEEDED TO ASSIST IN ENVIRONMENTAL FLUID SPILL. HAZMAT CLEANED UP ON C11. AIRCRAFT NEEDED TOW TEAM TO MAKE IT TO GATE IN CLT. REMOVED AND REPLACED FLEXIBLE HOSE
- [SDR VNAA2020010951102](https://openairdocs.org/sdr/VNAA2020010951102.md): Connector · dirty · Jan 5, 2020 · N546FF · Cndair CL6002C10 · Flight Control System Wiring
  > ON THE ARRIVAL AT FL060, STAB TRIM RUNAWAY. THE CREW RAN THE QRH AND DECIDED TO DIVERT TO IAD FOR THE LONGER RUNWAY. CREW DECLARED AN EMERGENCY. CABI DID NOT BRACE, TRUCKS DID ROLL. FLIGHT LANDED ON RWY 1C WITHOUT FURTHER INCIDENT AND WAS ABLE TO TAXI TO GA
- [SDR VNAA2019032899901](https://openairdocs.org/sdr/VNAA2019032899901.md): Door Sill · corroded · Mar 28, 2019 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > ALT CARGO DOOR SILL CORRODED ON AFT END, UPPER SURFACE. REPLACED AFT CARGO BAY DOOR TOWER SILL.
- [SDR VNAA2018122321102](https://openairdocs.org/sdr/VNAA2018122321102.md): Filter · dirty · Dec 22, 2018 · N546FF · Cndair CL6002C10 · Air Distribution System
  > AFTER PUSHBACK, CREW REPORTED A BURNING SMELL. MAINTENANCE REPLACED BOTH RECIRC FAN FILTERS. OPS CHECK GOOD NO ODORS NOTED.
- [SDR VNAA2018101611102](https://openairdocs.org/sdr/VNAA2018101611102.md): Acm · malfunctioned · Oct 16, 2018 · N546FF · Cndair CL6002C10 · Cabin Cooling System
  > ON GROUND EMERGENCY DECLARED IN DCA AFTER SMOKE PRESENT ON THE FLIGHTDECK AND REPORTS OF A BURNING PLASTIC SMELL. NO VISIBLE FIRE. MX WENT TO INSPECT AND FOUND THE LT PACK MAKING A GRINDING NOISE. MX R&R LH ACM. OPS CHECK GOOD.
- [SDR VNAA2018090311101](https://openairdocs.org/sdr/VNAA2018090311101.md): Unknown · malfunctioned · Sep 3, 2018 · N546FF · Cndair CL6002C10 · Flight Control System
  > DURING CLIMBOUT, CAPTAIN NOTICED THAT THE FLIGHT CONTROLS WERE ACTING SLUGGISH REQUIRING 3 TO 4 TIMES THE AMOUNT OF FORCE NEEDED TO MAKE THE AIRCRAFT TURN. DID NOT FOLLOW THE QRH AND THE STATION DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT.
- [SDR VNAA2017071411101](https://openairdocs.org/sdr/VNAA2017071411101.md): Acm · failed · Jul 14, 2017 · N546FF · Cndair CL6002C10 · Cabin Cooling System
  > ON APU START THE CREW RECEIVED A RIGHT AIR CONDITIONING PACK AUTO FAILED WITH THE PACK TEMPERATURE GOING TO 99 DEGREES. CAUSING SMOKE AND FUMES TO FILL THE CABIN.
- [SDR VNAA2016123000049](https://openairdocs.org/sdr/VNAA2016123000049.md): Screw · stripped · Dec 30, 2016 · N546FF · Cndair CL6002C10 · Emergency Lighting
  > EMERGENCY EXIT LIGHT SIGN IS HANGING DOWN. REMOVED AND REPLACED STRIPPED SCREW.
- [SDR VNAA2016120200005](https://openairdocs.org/sdr/VNAA2016120200005.md): Intercostal · cracked · Dec 2, 2016 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LEFT PACK WATER INJECTION LINE CLAMP BRACKET CRACKED. REPAIRED THE INTERCOSTAL AT STRINGER 9L, BS 1144 - 1154.48 AND PERFORMED CHECKS IAW THE AMM.
- [SDR VNAA2016120200004](https://openairdocs.org/sdr/VNAA2016120200004.md): Bulkhead Web · corroded · Dec 2, 2016 · N546FF · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > RIGHT BS 280 BULKHEAD WEB CORRODED. MAINTENANCE REMOVED AND REPLACED BULKHEAD WEB AND PERFORMED CHECKS IAW THE AMM.
- [SDR VNAA2016113000040](https://openairdocs.org/sdr/VNAA2016113000040.md): Floor Support · cracked · Nov 30, 2016 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > COCKPIT FLOOR SUPPORT RIGHT SIDE IS CRACKED. MAINTENANCE PERFORMED A MAJOR REPAIR IAW AMM.
- [SDR VNAA2016113000039](https://openairdocs.org/sdr/VNAA2016113000039.md): Floor Support · cracked · Nov 30, 2016 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > COCKPIT FLOOR SUPPORT LEFT SIDE IS CRACKED. MAINTENANCE PERFORMED A MAJOR REPAIR IAW THE AMM.
- [SDR VNAA2016112500036](https://openairdocs.org/sdr/VNAA2016112500036.md): Drag Angle · cracked · Nov 25, 2016 · N546FF · Cndair CL6002C10 · Vertical Stabilizer
  > RIGHT FORWARD VERTICAL STABILIZER DRAG ANGLE CRACKED. MAINTENANCE REPAIRED THE DRAG ANGLE AND PERFORMED CHECKS IAW THE AMM.

Next page: https://openairdocs.org/aircraft/N546FF/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N546FF' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N546FF/reports

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