# Service difficulty reports: N548NN

A list on [N548NN](https://openairdocs.org/aircraft/N548NN.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 · 71 reports

- [SDR VNAA2025112811101](https://openairdocs.org/sdr/VNAA2025112811101.md): Heater · odor · Nov 24, 2025 · N548NN · Cndair CL6002D24 · Heating System
  > GALLEY HEATER OVERHEATED AFTER TAKEOFF CAUSING BURNING SMELL. BREAKER CPB-2 B11 POPPED / REMOVED AND REPLACED GALLEY HEATER IAW CRJ900 AMM 21-23-64-000/400-801-A04. OPS TEST GOOD AT THIS TIME.
- [SDR VNAA202503080001](https://openairdocs.org/sdr/VNAA202503080001.md): Hinge · gouged · Mar 8, 2025 · N548NN · Cndair CL6002D24 · Fuselage, Door Hinge
  > PASSENGER DOOR HINGE IS GOUGED. DAMAGE IS LOCATED ON DOOR HINGE HALF, 5TH LUG FROM THE FRONT. REPAIRED HINGE BY COMPLYING WITH BOMBARDIER REO 670-52-11-511 REV -E DATED 8/2/2017 TYPE I REPAIR.
- [SDR VNAA202409240041](https://openairdocs.org/sdr/VNAA202409240041.md): Bulkhead Web · corroded · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > CORROSION ON LH LOWER WEB AT BULKHEAD FS 280.00 LBL12 ABOVE FLOOR. LH LOWER WEB AT BULKHEAD FS280 LBL12 WAS REPAIRED PER CRJ900 SRM 53-11-10-201-004-A01.
- [SDR VNAA202409240015](https://openairdocs.org/sdr/VNAA202409240015.md): Bulkhead Web · corroded · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > CORROSION ON LH LOWER WEB AT BULKHEAD FS 280.00 LBL12 ABOVE FLOOR. LH LOWER WEB AT BULKHEAD FS280 LBL12 WAS REPAIRED PER CRJ900 SRM 53-11-10-201-004-A01.
- [SDR VNAA202409240040](https://openairdocs.org/sdr/VNAA202409240040.md): Crossbeam · corroded · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Main, Structure
  > DURING BULKHEAD DOOR POSTS LOWER SECTION LBL12 AT FS280.00 REMOVAL, CORROSION WAS FOUND ON LH CROSSBEAM OF FS 280.00. CROSSBEAM LH FS280.00 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01.
- [SDR VNAA202409240039](https://openairdocs.org/sdr/VNAA202409240039.md): Floorbeam · corroded · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > DURING BULKHEAD DOOR POSTS LOWER SECTION LBL12 AT FS280.00 REMOVAL, CORROSION WAS FOUND ON CENTER FLOOR SUPPORT OF FS 280.00. CENTER FLOOR SUPPORT OF FS 280.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND MUST BE REPLACED ON NRC00169.
- [SDR VNAA202409240038](https://openairdocs.org/sdr/VNAA202409240038.md): Seat Track · corroded · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL AT RBL9 FROM FS 349.00 TO FS 699.40 AT CABIN PAX. DUE TO NOT PERMISIBLE DAMAGE ON SEAT RAIL AT RBL9 FROM FS 349.00 TO FS 699.40 AT CABIN PAX PER CRJ900 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02, AND SRM 53-41-49-101-001-A02 WE
- [SDR VNAA202409240037](https://openairdocs.org/sdr/VNAA202409240037.md): Seat Track · corroded · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL AT LBL9 FROM FS 374.00 TO FS 699.40 AT CABIN PAX. SEAT RAIL OF RBL9 BTW FS374.00 TO FS 699.40 (SEAS) ARE OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01, CRJ900 SRM 53-31-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ 900 AMM 53-00-4
- [SDR VNAA202409240036](https://openairdocs.org/sdr/VNAA202409240036.md): Floor Support · corroded · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER FACE OF FLOOR BEAM RBL9 BTW FS1000 TO FS1088 AT AFT BAGGAGE BAY CARGO COMPARTMENT FLOOR STRUCTURE. CORROSION ON UPPER FACE OF FLOOR BEAM RBL9 BTW FS1000 TO FS1088 AT AFT BAGGAGE BAY CARGO COMPARTMENT FLOOR STRUCTURE WAS REMOVED PER CRJ900 S
- [SDR VNAA202409240035](https://openairdocs.org/sdr/VNAA202409240035.md): Floor Support · corroded · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER FACE OF FLOOR BEAM LBL9 BTW FS1000 TO FS1069 AT AFT BAGGAGE BAY CARGO COMPARTMENT FLOOR STRUCTURE. FLOOR BEAM LBL9 BTW FS1000 TO FS1069 AT AFT BAGGAGE BAY CARGO COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-61-43-101-001-A02 AND
- [SDR VNAA202409240034](https://openairdocs.org/sdr/VNAA202409240034.md): Bulkhead · corroded · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > CORROSION ON BULKHEAD DOOR POSTS LOWER SECTION LBL12 AT FS280.00. BULKHEAD DOOR POSTS LOWER SECTION LBL12 AT FS280.00 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 PAR.6 C, CRJ-900 SRM 51-42-21-001-001-A01 PAR.6 C AND CRJ-900 SRM 51-42-13-001-001-A01 PAR.
- [SDR VNAA202409240014](https://openairdocs.org/sdr/VNAA202409240014.md): Bulkhead · corroded · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > CORROSION ON BULKHEAD DOOR POSTS LOWER SECTION LBL12 AT FS280.00. BULKHEAD DOOR POSTS LOWER SECTION LBL12 AT FS280.00 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 PAR.6 C, CRJ-900 SRM 51-42-21-001-001-A01 PAR.6 C AND CRJ-900 SRM 51-42-13-001-001-A01 PAR.6
- [SDR VNAA202409240033](https://openairdocs.org/sdr/VNAA202409240033.md): Canister · cracked · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuel Storage
  > CRACK ON CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK. CRACK ON CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV.- -
- [SDR VNAA202409240032](https://openairdocs.org/sdr/VNAA202409240032.md): Hinge · cracked · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > CRACK ON HINGE AT STEP PLATE C2 AND ILLEGIBLE BLACK/YELLOW MARCKING AND DECAL OF FLAP STEP PLATE AT AFT CARGO. HINGE AT STEP PLATE C2 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND PAINT WAS RESTORED PER CRJ900 SRM 51-25-01-001-001-A01-PSA AND DECAL WAS
- [SDR VNAA202409240013](https://openairdocs.org/sdr/VNAA202409240013.md): Hinge · cracked · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > CRACK ON HINGE AT STEP PLATE C2 AND ILLEGIBLE BLACK/YELLOW MARCKING AND DECAL OF FLAP STEP PLATE AT AFT CARGO. HINGE AT STEP PLATE C2 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND PAINT WAS RESTORED PER CRJ900 SRM 51-25-01-001-001-A01-PSA AND DECAL WAS
- [SDR VNAA202409240031](https://openairdocs.org/sdr/VNAA202409240031.md): Canister · cracked · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuel Storage
  > CRACKS ON CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL RH MAIN FUEL TANK. CRACKS ON CANISTER, WELDED NO.3 IN STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV.- -
- [SDR VNAA202409240030](https://openairdocs.org/sdr/VNAA202409240030.md): Support · cracked · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT, BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. REFUEL DUCT MOUNTING SUPPORT WAS REPAIRED PER REO 690-28-25-024 REV --.
- [SDR VNAA202409240012](https://openairdocs.org/sdr/VNAA202409240012.md): Support · cracked · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT, BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. REFUEL DUCT MOUNTING SUPPORT WAS REPAIRED PER REO 690-28-25-024 REV --.
- [SDR VNAA202409240029](https://openairdocs.org/sdr/VNAA202409240029.md): Floorbeam · cracked · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > DURING INSPECTION OF THE RC: 53-21-301-JIC: CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM (RBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR LONGITUDINAL BEAM RBL12 WAS REPAIRED PER REO 690-53-11-1835 REV.--
- [SDR VNAA202409240028](https://openairdocs.org/sdr/VNAA202409240028.md): Floorbeam · cracked · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > DURING INSPECTION OF THE RC: 53-21-301-JIC: CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR LONGITUDINAL BEAM LBL12 WAS REPAIRED PER REO 690-53-11-1836 REV--.
- [SDR VNAA202409240027](https://openairdocs.org/sdr/VNAA202409240027.md): Seat Track · corroded · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL LBL27 FROM FS 364.00 TO FS699.40 AT CABIN PAX.SEAT RAIL LBL27 FROM FS 364.00 TO FS699.40 (SEAS) AT CABIN PAX ARE OUT OFF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01, CRJ900 SRM 53-31-49-101-001-A02, CRJ900 SRM 53-41-49-101-001-A02 THEREF
- [SDR VNAA202409240026](https://openairdocs.org/sdr/VNAA202409240026.md): Floor Support · corroded · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SILL BTW FS280.00 - FS310.00 ON RIGHT SIDE. FLOOR SILL BTW FS280.00 - FS310.00 ON RIGHT SIDE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-45-201-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A
- [SDR VNAA202409240025](https://openairdocs.org/sdr/VNAA202409240025.md): Splice · corroded · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON SPLICES (2EA) BTW FS865 - FS881 AND RBL9 - LBL9 AT CABIN PAX. SPLICES (2EAS) BTW FS865 - FS881 AND RBL9/LBL9 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-51-43-101-001-A02; WERE FABRICATED PER SNIEO DRAWING SH670-32161 CT0001-01 MW13 REV 2021-0
- [SDR VNAA202409240024](https://openairdocs.org/sdr/VNAA202409240024.md): Seat Track · corroded · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL BLW FS744.15 TO FS 969.00 (&EA)LH SIDE SEAT RAIL BLW FS744.15 TO FS 969.00 (&EA) ARE OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND CRJ900 SRM 53-51-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A1
- [SDR VNAA202409240023](https://openairdocs.org/sdr/VNAA202409240023.md): Seat Track · corroded · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA). LH SIDE SAT RAILS BTW FS379 TO FS720 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01; CRJ900 SRM 53-31-49-101-001-A02; CRJ900 SRM 53-41-49-101-001-A02 AND WERE REPLACED PER CRJ90
- [SDR VNAA202409240022](https://openairdocs.org/sdr/VNAA202409240022.md): Seat Track · corroded · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL BTW FS379.00 TO FS 720.85 (5EA). RH SIDE SAT RAILS BTW FS379 TO FS720 WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A02; CRJ900 SRM 53-31-49-101-001-A02; CRJ900 SRM 53-41-49-101-001-A02 AND WERE REPLACED PER CRJ90
- [SDR VNAA202409240021](https://openairdocs.org/sdr/VNAA202409240021.md): Seat Track · corroded · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (&EA). RH SIDE SEAT RAIL BTW FS744.15 TO FS 969.00 (&EA) ARE OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND CRJ900 SRM 53-51-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG
- [SDR VNAA202409240020](https://openairdocs.org/sdr/VNAA202409240020.md): Floor Support · corroded · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER FACE OF FLOOR BEAM LBL27 BTW FS1000 TO FS1047 AT AFT BAGGAGE BAY CARGO COMPARTMENT FLOOR STRUCTURE. CORROSION ON UPPER FACE OF FLOOR BEAM LBL27 BTW FS1000 TO FS1047 AT AFTBAGGAGEBAYCARGOCOMPARTMENT FLOOR STRUCTURE WAS REMOVED PER CRJ-900 SR
- [SDR VNAA202409240019](https://openairdocs.org/sdr/VNAA202409240019.md): Intercostal · corroded · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL (2 EAS) ATTACHED TO STRINGER 20RH IN STA. FS 310.00 TO FS 349.00 AT MAIN AVIONICS COMPARTMENT. (E/E) (W1). INTERCOSTAL BTW FS319 TO FS349 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-002-A02 AND WAS REPLACED PER CRJ900 SRM
- [SDR VNAA202409240018](https://openairdocs.org/sdr/VNAA202409240018.md): Bulkhead · corroded · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > DURING INSPECTION OF THE RC: 53-21-301-JIC: IT WAS DETECTED CORROSION ON BULKHEAD DOOR POSTS LOWER SECTION RBL12 AT FS280.00. BULKHEAD DOOR POST LOWER SECTION RBL12 WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01.
- [SDR VNAA202409240017](https://openairdocs.org/sdr/VNAA202409240017.md): Plate · corroded · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKETS MACHINED (7EAS) AND PLATE (1 EA) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. BRACKETS MACHINED (5EAS) AND PLATE (1EA) WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND PER CRJ900 SRM 51-42-22-001-001-A01 AND BRACKET MACHINED (2EA
- [SDR VNAA202409240016](https://openairdocs.org/sdr/VNAA202409240016.md): Plate · corroded · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR PLATE AT SERVICE DOOR(R1). CORROSION ON FLOOR PLATE WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND WAS REPAIRED PER EA:A1-690-53-00096 REV - - SECTION III PERMANENT
- [SDR VNAA202409240011](https://openairdocs.org/sdr/VNAA202409240011.md): Arm · nicked · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > WEAR AND NICKS ON FWD / AFT COUNTERBALANCE ARMS AT FWR & CTR BAGGAGE BAY DOORS. FWD / AFT COUNTERBALANCE ARMS AT FWR & CTR BAGGAGE BAY DOORS WERE REPAIRED PER REO 690-52-35-444 REV. -- AND REO 690-52-35-445 REV. --
- [SDR VNAA202409240010](https://openairdocs.org/sdr/VNAA202409240010.md): Skin · damaged · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKES ON FUSELAGE SKIN, LOCATED BTW FS310.00 TO FS319.70 AND STGR 26LH TO 25LH (1EA), FS379 TO FS409 AND STGR 26RH TO 25LH (3EAS), FS250 TO FS235 AND STGR 26LH TO 25LH (1EA). LIGHTNING STRIKES ON FUSELAGE SKIN, LOCATED BTW FS310.00 TO FS319.70 AND
- [SDR VNAA202409240009](https://openairdocs.org/sdr/VNAA202409240009.md): Skin · nicked · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Wing, Plate/Skin
  > SEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT RH WING. NICKS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT RH WING WERE BLEND OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND SECTION BTW FLS15.00 TO FLS 30.00 WAS EVALUATED OUT
- [SDR VNAA202409240008](https://openairdocs.org/sdr/VNAA202409240008.md): Angle · cracked · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE PREVIOUS REPAIR BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM. PREVIOUS REPAIR ON LH VERTICAL AFT DRAG ANGLE WAS REPLACED PER CRJ 900 SRM 55-31-00-201-001-A01
- [SDR VNAA202409240007](https://openairdocs.org/sdr/VNAA202409240007.md): Angle · cracked · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM. RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE WAS REPAIRED PER CRJ 900 SRM 55-31-00-201-001-A01
- [SDR VNAA202409240006](https://openairdocs.org/sdr/VNAA202409240006.md): Helicoil · damaged · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Structure (General)
  > 8000FH PERM REPAIR - SPEED TAPE APPLIED - REPAIR DAMAGED JACKING PAD HELICOIL INSERT LHS AND/OR RHS PERFORM PERM REPAIR OF DAMAGED JACKING PAD HELICOIL INSERT-RHS IAW REO 670-57-22-004. JACKING FITTING HELICOIL INSERT WAS EVALUATED OUT OF LIMITS PER REO 670-5
- [SDR VNAA202409240005](https://openairdocs.org/sdr/VNAA202409240005.md): Skin · damaged · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN BETWEEN FS 295 - FS 613 AND STR 23L - STR24R. LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN BETWEEN FS 295 - FS 613 AND STR 23L - STR24R WAS REPAIRED PER CRJ900 SRM 53-00-00-201-003-A03 AND PER REO 690-53-31-877 REV.--
- [SDR VNAA202409240004](https://openairdocs.org/sdr/VNAA202409240004.md): Skin · damaged · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > REF TO TRFKE00BP99M: 2500FH PERM REPAIR - TEMPORARY DISPOSITION FOR BLENDED LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN AT STR23L BETWEEN FS1069.75 - FS1088.20 WITHIN 2500, PERFORM A PERM REPAIR IAW APPROVED PROCEDURES. LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN
- [SDR VNAA202409240003](https://openairdocs.org/sdr/VNAA202409240003.md): Skin · damaged · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FUSELAGE LIGHTNING STRIKE DAMAGE, FS169.00 TO FS1162.00. FUSELAGE LIGHTNING STRIKE DAMAGE, FS169.00 TO FS1162.00 WAS REPAIRED PER REO 690-53-21-1829 REV.--
- [SDR VNAA202409240002](https://openairdocs.org/sdr/VNAA202409240002.md): Skin · damaged · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN BETWEEN FS985.00 - FS1000.00 AT STR 23L. LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN BETWEEN FS985.00 - FS1000.00 AT STR 23L WAS REPAIRED PER REO 690-53-61-1451 REV.--
- [SDR VNAA202409240001](https://openairdocs.org/sdr/VNAA202409240001.md): Hinge Fitting · gouged · Sep 24, 2024 · N548NN · Cndair CL6002D24 · Fuselage, Door Hinge
  > SPS21.80 OUTBOARD HINGE FITTING GOUGE DAMAGE 1. PERMANENT REPAIR WAS ACCOMPLISHED ON RH WING T/E OUTBD HINGE FITTINGS AT SS21.80 PER REO 690-57-51-378 REV. --
- [SDR VNAA2023112911101](https://openairdocs.org/sdr/VNAA2023112911101.md): Display · failed · Nov 26, 2023 · N548NN · Cndair CL6002D24 · Central Display
  > UPON TURNING ON FFD, CA NOTICED BURNING SMELL IN FLIGHT DECK. I LOOKED DOWN AND SEE DISPLAY FAN ON STANDBY. FO'S MFD HAD BURNED OUT / VERIFIED EFD4, SECONDARY EICAS DISPLAY COMPLETELY BLANK. INTERROGATED MDC, FOUND FAULT CODE B1-006507 FOR EICAS DISPLAY 2/INTE
- [SDR VNAA202308251112](https://openairdocs.org/sdr/VNAA202308251112.md): Sensor · unserviceable · Aug 22, 2023 · N548NN · Cndair CL6002D24 · Landing Gear Brake System
  > BRAKE OVHT WARNING MSG IN FLIGHT (RH INBD) / REMOVED AND REPLACE BRAKE TEMP SENSOR IAW CRJ 900 32-46-01-00/400-801-A01-PSA. OPS CHECK GOOD. THIS CLEARS MEL
- [SDR VNAA202207071111](https://openairdocs.org/sdr/VNAA202207071111.md): Engine · noise · Jul 5, 2022 · N548NN · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > A/C WAS FLYING AT FL340 AT.81MACH FOR ABOUT 30MIN AND HEARD A LOUD BANG. IMMEDIATELY NOTICED HI ENG VIB AND ITT IN LFT ENG. PROCEEDED TO RUN THE QRH FOR A LFT ENG SHUTDOWN. NO FIRE WAS DETECTED. THE CREW DECLARED AN EMERGENCY AND CONTINUED ONTO CLT. PIC MADE
- [SDR VNAA202203261111](https://openairdocs.org/sdr/VNAA202203261111.md): Manifold · unserviceable · Mar 23, 2022 · N548NN · Cndair CL6002D24 · Steering Unit
  > ON APPROACH INTO CLT, NOSE WHEEL STEERING INOP MESSAGE WAS RECEIVED. THEY NOTIFIED ATC AND ATC DECLARED AN EMERGENCY FOR THE FLIGHT. FLIGHT LANDED WITHOUT ISSUE AND WAS ABLE TO GET OFF THE ACTIVE RUNWAY AND GET THE NOSE STEERING RESET. THEY WERE ABLE TO TAXI T
- [SDR VNAA202203029992](https://openairdocs.org/sdr/VNAA202203029992.md): Fastener · abnormal · Mar 2, 2022 · N548NN · Cndair CL6002D24 · Fuselage Main, Structure
  > LIGHTNING STRIKE TO RH BELLY FUSELAGE FASTENER AT FS265 BETWEEN STGR24 AND STRGR23. REPAIRED IAW EA 22-C9-53-0237 AND REPLACEMENT OF FASTENER.
- [SDR VNAA202203029991](https://openairdocs.org/sdr/VNAA202203029991.md): Skin · cracked · Mar 2, 2022 · N548NN · Cndair CL600* · Passenger/Crew Doors
  > REPAIR TO PAX DOOR INNER SKIN BTW FS310.00 - FS318.57 & BTW DD1A - DD1. SKIN REPLACED.
- [SDR VNAA202110221113](https://openairdocs.org/sdr/VNAA202110221113.md): Transducer · loose · Oct 20, 2021 · N548NN · Cndair CL6002D24 · Brake Anti-Skid Section
  > ON APPROACH TO RWY 36L IN CLT AT THE FINAL APPROACH FIX AT 8000', RECEIVED ANTI-SKIB INBOARD MESSAGE. RAN QRH AND DECLARED AN EMERGENCY. TRUCKS ROLLED. PASSENGERS DID NOT BRACE. MESSAGE WENT AWAY AT 1500'. FLIGHT LANDED WITHOUT INCIDENT AND CANCELLED THE EMERG

Next page: https://openairdocs.org/aircraft/N548NN/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 = 'N548NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N548NN/reports

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