# Service difficulty reports: N547NN

A list on [N547NN](https://openairdocs.org/aircraft/N547NN.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 · 61 reports

- [SDR VNAA2026102126801](https://openairdocs.org/sdr/VNAA2026102126801.md): Actuator · tripped · Oct 18, 2026 · N547NN · Cndair CL6002D24 · Trailing Edge Flap Actuator
  > FLAPS FAIL MSG DURING CRUISE, RAN QRH AND FLAPS DID NOT EXTEND PAST FLAPS 1 POSITION C/A REPLACED #4 FLAP ACTUATOR.
- [SDR VNAA2026101926602](https://openairdocs.org/sdr/VNAA2026101926602.md): Pdu · unserviceable · Oct 17, 2026 · N547NN · Cndair CL6002D24 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION MSG DURING CRUISE C/A T/S B1 006551 IAW CRJ 900 FIM 27ˆ’52ˆ’09ˆ’810ˆ’802. REMOVED AND REPLACED FLAP PDU IAW CRJ 900 AMM 27€“52€“37€“000/400€“801. OPS TEST GOOD NO DEFECTS NOTED. NO FLAP HALF SPEED OR FLAP FAIL MSG.
- [SDR VNAA2026010611101](https://openairdocs.org/sdr/VNAA2026010611101.md): Controller · faulted · Jan 3, 2026 · N547NN · Cndair CL6002D24 · Pitot/Static Anti-Ice System
  > RIGHT PITOT HEAT CAUTION MSG. REMOVED AND REPLACED RT ADSHC IAW AMM 30-31-15-000/400-801. OPS CHECK GOOD. CYCLED AC AND RT PITOT HEAT NO FAULT.
- [SDR VNAA2025051611101](https://openairdocs.org/sdr/VNAA2025051611101.md): Windshield · arced · May 14, 2025 · N547NN · Cndair CL6002D24 · Flight Compartment Windows
  > RIGHT WINDSHIELD HEAT ARCING IN FLIGHT BOTTOM SIDE. / REMOVED AND REPLACED RH WINDSHIELD IAW CRJ 900 AMM 56-11-01-000/400-801-A01-PSA. OPS CHECK AND LEAKS CHECKS GOOD. PRESSURE CHECK GOOD IAW CRJ 900 AMM 21-31-00-910-801-A02-PSA/ 21-31-00-910-802. NO FURTHER D
- [SDR VNAA2024102211102](https://openairdocs.org/sdr/VNAA2024102211102.md): Outflow Valve · malfunctioned · Oct 22, 2024 · N547NN · Cndair CL6002D24 · Pressure Regulator/Outflow Valve
  > CABIN ALT CAUTION THROUGH 10000FT. CABIN ALT WARNING ABOVE 11000 / FOUND GROUND VALVE TO BE DEFERRED IN THE WRONG POSITION. PERFORMED PRESSURIZATION OF THE A/C IAW CRJ-900 AMM 21-31-00-910-801-A02-PSA. PRESSURIZATION WAS GOOD. NO DEFECTS NOTED
- [SDR VNAA2024101111101](https://openairdocs.org/sdr/VNAA2024101111101.md): Smoke Detector · false activation · Oct 10, 2024 · N547NN · Cndair CL6002D24 · Smoke Detection
  > SMOKE AFT LAV WARNING MESSAGE IN FLIGHT AND ON GROUND MULTIPLE TIMES / CYCLED CBP-1 D9, AND PERFORMED OPS CHECK IAW CRJ 900 AMM 26-16-00-710-801-A01. OPS CHECK GOOD. FAULT COULD NOT DUPLICATE.
- [SDR VNAA202409020010](https://openairdocs.org/sdr/VNAA202409020010.md): Skin · dented · Jul 31, 2024 · N547NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DURING DETAILED VISUAL INSPECTION OF THE FUSELAGE SKIN IN REFERENCE TO JOB CARD TRFKE0080LHU/// DENT ON FUSELAGE SKIN FS 394.00 BLWN STGR 19 LH AND 20LH. DENT ON FUSELAGE SKIN FS 394.00 BLWN STGR 19 LH AND 20LH WAS REPAIRED PER REO 690-53-21-1823 REV--
- [SDR VNAA202409010016](https://openairdocs.org/sdr/VNAA202409010016.md): Plate · corroded · Jul 21, 2024 · N547NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON PLATE (2EAS) LBL3.5, FS540 AND FS650 OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. CORROSION ON PLATE (2EAS) LBL3.5, FS540 AND FS650 OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WAS EVALUATED OUT LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 THER
- [SDR VNAA202409020008](https://openairdocs.org/sdr/VNAA202409020008.md): Fitting · corroded · Jul 13, 2024 · N547NN · Cndair CL6002D24 · Wing, Control Surface Attach Fittings
  > AFTER REMOVAL OF LH AILERON BUSHINGS AN BEARINGS, CORROSION AND WEAR WERE FOUND ON LUG BORE OF L 1, L2, L4, LS AND L6 OF CENTER HINGE FITTINGS OF LEFT AILERON. LUG BORE OF L1, L2, LS AND L6 OF CENTER HINGE FITTINGS OF LEFT AILERON WERE REPAIRED PER PER REO 67
- [SDR VNAA202409020007](https://openairdocs.org/sdr/VNAA202409020007.md): Fitting · corroded · Jul 13, 2024 · N547NN · Cndair CL6002D24 · Wing, Attach Fittings
  > AFTER REMOTION OF BUSHINGS AND BEARINGS ON RH AILERON///CORROSION ON LUGS R1, R2, R5 AND R6. RH AILERON LUGS R1, R2, R5 AND R6 WERE REPAIRED PER REO 670-57-61-237 REV - - NOTES F
- [SDR VNAA202409020006](https://openairdocs.org/sdr/VNAA202409020006.md): Seat Track · corroded · Jul 13, 2024 · N547NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS RBL9 BTW FS 477.40 - FS 677.00 (3EA) AT PASSENGER CABIN. SEAT RAILS RBL9 BTW FS 477.40 - FS 677.00 (3EA) AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND CRJ900 SRM 53-41-49-101-001-A02 AND WERE
- [SDR VNAA202409020005](https://openairdocs.org/sdr/VNAA202409020005.md): Seat Track · corroded · Jul 13, 2024 · N547NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS LBL27 BTW FS 477.40 - FS 581.00 (2EA) AT PASSENGER CABIN. CORROSION ON SEAT RAILS LBL27 BTW FS 477.40 - FS 581.00 (2EA) AT PASSENGER CABIN. WAS EVALUATE PER CRJ-900 SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 AND REPLACED
- [SDR VNAA202409020004](https://openairdocs.org/sdr/VNAA202409020004.md): Seat Track · corroded · Jul 13, 2024 · N547NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAILS LBL9 BTW FS 581.00 - FS 677.40 (3 EAS) AT PASSENGER CABIN. CORROSION ON SEAT RAILS LBL9 BTW FS 581.00 - FS 677.40 (3 EAS) AT PASSENGER CABIN. WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND CRJ-900 SRM 53-41-49-101-0
- [SDR VNAA202409020003](https://openairdocs.org/sdr/VNAA202409020003.md): Seat Track · corroded · Jul 13, 2024 · N547NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT TRACK BTW FS 379.00 - FS 677.00 (4 EAS) AT PASSENGER CABIN. CORROSION ON LH SIDE SEAT TRACK BTW FS 379.00 - FS 677.00 (4 EAS) AT PASSENGER CABIN. WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01 AND CRJ-900 SRM 53-31-49
- [SDR VNAA202409020001](https://openairdocs.org/sdr/VNAA202409020001.md): Seat Track · corroded · Jul 13, 2024 · N547NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL BTW FS 669.40 TO FS 977.00 AND STGR 15LH AT CABIN PAX. CORROSION ON SEAT RAIL BTW FS 669.40 TO FS 977.00 AND STGR 15LH AT CABIN PAX.
- [SDR VNAA202409010029](https://openairdocs.org/sdr/VNAA202409010029.md): Skin · dented · Jul 13, 2024 · N547NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > SEVERAL DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY RH VENTRAL FIN FAIRING. CORRECTIVE ACTION: SEVERAL DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY RH VENTRAL FIN FAIRING. WERE REPAIRED PER REO 670-51-00-085 REV -A AND PER REO 690-53-00-569 REV -
- [SDR VNAA202409010028](https://openairdocs.org/sdr/VNAA202409010028.md): Skin · dented · Jul 13, 2024 · N547NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > SEVERAL DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY LH VENTRAL FIN FAIRING. SEVERAL DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY LH VENTRAL FIN FAIRING WERE REPAIRED PER REO 670-51-00-085 REV -A AND PER REO 690-53-71-079 REV -
- [SDR VNAA202409010026](https://openairdocs.org/sdr/VNAA202409010026.md): Seat Track · corroded · Jul 13, 2024 · N547NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL OF LBL9 BTW FS349.00 TO FS 477.40. SEAT RAIL OF LBL9 BTW FS349.00 TO FS 477.40 WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49 CONF(A12).
- [SDR VNAA202409010027](https://openairdocs.org/sdr/VNAA202409010027.md): Floor Support · corroded · Jul 12, 2024 · N547NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON GALLEY FLOOR SUPPORTS (4EAS) LOCATED BTW FS 280.00 - FS 295.00 AND AT FUSELAGE FLOOR STRUCTURE. GALLEY FLOOR SUPPORTS (4EAS) LOCATED BTW FS 280.00 - FS 295.00 AND AT FUSELAGE FLOOR STRUCTURE WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01
- [SDR VNAA202409010025](https://openairdocs.org/sdr/VNAA202409010025.md): Floor Support · corroded · Jul 12, 2024 · N547NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER FACE OF FLOOR SUPORT RBL 9.00 BTW FS 1000.00 TO FS 1069.75 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. UPPER FACE OF FLOOR SUPPORT RBL 9.00 BTW FS 1000.00 TO FS 1069.75 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-61-1
- [SDR VNAA202409010022](https://openairdocs.org/sdr/VNAA202409010022.md): Frame · corroded · Jul 12, 2024 · N547NN · Cndair CL6002D24 · Fuselage Main, Frame
  > CORROSION ON FRAME FS1088.20 BTWN STGR 27 AND STGR 25LH AT AFT BAGGAGE BAY COMPARTMENT. CORROSION ON FRAME FS1088.20 BTWN STGR 27 AND STGR 25LH AT AFT BAGGAGE BAY COMPARTMENT WAS REMOVED PER CRJ 900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PE
- [SDR VNAA202409010020](https://openairdocs.org/sdr/VNAA202409010020.md): Floorbeam · corroded · Jul 12, 2024 · N547NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR SUPPORT FS=281 BETWEEN STGR 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT. FLOOR SUPPORT FS=281 BETWEEN STGR 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01
- [SDR VNAA202409010019](https://openairdocs.org/sdr/VNAA202409010019.md): Beam · corroded · Jul 12, 2024 · N547NN · Cndair CL6002D24 · Fuselage Main, Structure
  > CORROSION ON BEAM SIDE AT AFT BAGGAGE BAY COMPARTMENT FLOOR STRUCTURE. BEAM SIDE AT AFT BAGGAGE BAY COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-61-1431 REV - -
- [SDR VNAA202409010017](https://openairdocs.org/sdr/VNAA202409010017.md): Skin · corroded · Jul 12, 2024 · N547NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL SKIN CUT OUT, (SEAL SEATLEMENT AREA), DOOR SURROUND STRUCTURE, MAIN AVIONICS COMPARTMENT. CORROSION ON INTERNAL SKIN CUT OUT, (SEAL SEATLEMENT AREA), DOOR SURROUND STRUCTURE, MAIN AVIONICS COMPARTMENT WAS REMOVED AND FOUND WHITHIN LIMITS
- [SDR VNAA202409010011](https://openairdocs.org/sdr/VNAA202409010011.md): Floorbeam · corroded · Jul 12, 2024 · N547NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM FS280 (RBL9 TO LBL9) AT CABIN FLOOR STRUCTURE. FLOORBEAM FS280 (RBL9 TO LBL9) AT CABIN FLOOR STRUCTURE IT IS OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 THEREFORE WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-10-
- [SDR VNAA202409010007](https://openairdocs.org/sdr/VNAA202409010007.md): Duct · cracked · Jul 12, 2024 · N547NN · Cndair CL6002D24 · Fuel Storage
  > CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. AFT REFUEL DUCT MOUNTING SUPPORT BTW FS 677.00 TO FS 669.40, BTW STGR 22RH AND 21RH. (SM) WAS REPAIRED PER PER. REO. 690-28-25-023 REV.--
- [SDR VNAA202409010024](https://openairdocs.org/sdr/VNAA202409010024.md): Floor Support · corroded · Jul 11, 2024 · N547NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER FACE OF FLOOR SUPPORTLBL 9.00 BTW FS 1000.00 TO FS 1069.75 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. FLOOR SUPPORT LBL 9.00 BTW FS 1000.00 TO FS 1069.75 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-61-1435 REV: - -
- [SDR VNAA202409010023](https://openairdocs.org/sdr/VNAA202409010023.md): Floor Support · corroded · Jul 11, 2024 · N547NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER FACE OF FLOOR SUPPORT LBL 27 BTW FS 1000.00 TO FS 1069.75.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. FLOOR SUPPORTLBL 27 BTW FS 1000.00 TO FS 1069.75.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-61-1434 REV - -
- [SDR VNAA202409010018](https://openairdocs.org/sdr/VNAA202409010018.md): Fitting · corroded · Jul 11, 2024 · N547NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON JACK FITTING SUPPORTS (2EAS) BTW FS=265.00 AND FS=280.00 AT AT MAIN AVIONICS COMPARTMENT. (E/E). JACK FITTING SUPPORTS (2EAS) BTW FS=265.00 AND FS=280.00 AT AT MAIN AVIONICS COMPARTMENT. (E/E) WERE REPAIRED PER REO 690-53-11-1831 REV. --
- [SDR VNAA202409010013](https://openairdocs.org/sdr/VNAA202409010013.md): Floor Support · corroded · Jul 11, 2024 · N547NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT RBL12.0 AND LBL12.0 BTW FS260 TO FS280 AT FLIGHT COMPARTMENT. CORROSION ON FLOOR SUPPORT RBL12.0 AND LBL12.0 BTW FS260 TO FS280 AT FLIGHT COMPARTMENT WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01. ON FLOOR SUPPORT LBL12.0 BTW FS26
- [SDR VNAA202409020009](https://openairdocs.org/sdr/VNAA202409020009.md): Retainer · corroded · Jul 10, 2024 · N547NN · Cndair CL6002D24 · Cargo/Baggage Doors
  > AFTER SEAL AT AFT BAGGAGE BAY DOOR REMOVAL, CORROSION ON AFT RETAINER SEAL CORNER LWR AND RETAINER SEAL LWR. AFT RETAINER SEAL CORNER LWR AND RETAINER SEAL LWR WERE EVALUATED OUT LIMITS PER CRJ-900 SRM 51-42-21-001-001-A01 THEREFORE WERE REPLACED PER CRJ-900
- [SDR VNAA202409010015](https://openairdocs.org/sdr/VNAA202409010015.md): Bracket · corroded · Jul 10, 2024 · N547NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKETS, MACHINED (10EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT. BRACKETS, MACHINED (2EAS) (P/N:SH670-33389-1) WERE CLEANED AND NO DAMAGES WERE FOUND PER CRJ-900 SRM 51-26-00-001-001-A01, AND BRACKETS MACHINED (8EAS) WERE EVALUATED OUT
- [SDR VNAA202409010012](https://openairdocs.org/sdr/VNAA202409010012.md): Floorbeam · corroded · Jul 10, 2024 · N547NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION ON RH CROSSBEAM FS 280 AT COCKPIT CABIN FLOOR. CORROSION ON RH CROSSBEAM FS 280 AT COCKPIT CABIN FLOOR WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 THEREFORE RH CROSSBEAM FS 280 WAS REPLACED PER PER CRJ-900 SRM 51-42-06-001-001-A01,
- [SDR VNAA202409010010](https://openairdocs.org/sdr/VNAA202409010010.md): Floor Support · cracked · Jul 10, 2024 · N547NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR ST
- [SDR VNAA202409010009](https://openairdocs.org/sdr/VNAA202409010009.md): Floorbeam · cracked · Jul 10, 2024 · N547NN · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACKED CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CENTER COCKPIT FLOOR BEAM RBL12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1808. REV.--
- [SDR VNAA202409010008](https://openairdocs.org/sdr/VNAA202409010008.md): Intercostal · worn · Jul 10, 2024 · N547NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > WORN INTERCOSTAL LOCATED AT STRINGER 3 RH BTW FS 364.00 TO FS 379.00 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE. INTERCOSTAL LOCATED AT STRINGER 3 RH BTW FS 364.00 TO FS 379.00 AT PASSENGER COMPARTMENT INTERNAL STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-06-
- [SDR VNAA202409010002](https://openairdocs.org/sdr/VNAA202409010002.md): Skin · nicked · Jul 10, 2024 · N547NN · Cndair CL6002D24 · Trailing Edge Flaps
  > SEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT RH WING. LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5 AT RH WING WAS BLENDED OUT PER CRJ900 SRM 51-12-00-001-001-A01, BTW FLS 45.00 TO FLS 65.5 WAS EVALUATED WITHIN LMIMITS PER C
- [SDR VNAA202409010004](https://openairdocs.org/sdr/VNAA202409010004.md): Shield · chafed · Jul 9, 2024 · N547NN · Cndair CL6002D24 · Nacelle/Pylon, Main Frame
  > MULTIPLE CHAFFING ON RH ENGINE LWR FWD CORE COWL FIRE SHIELD. RH ENGINE LWR FWD CORE COWL FIRE SHIELD WAS REPAIRED PER EA 23-C9-54-0901 REV IR AND REO 690-54-23-387 REV --
- [SDR VNAA202409010003](https://openairdocs.org/sdr/VNAA202409010003.md): Skin · dented · Jul 9, 2024 · N547NN · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DENT ON SKIN LWR BELLY PANEL. SKIN LWR BELLY PANEL WAS REPAIRED PER REO 690-53-11-1823 REV --
- [SDR VNAA202409010001](https://openairdocs.org/sdr/VNAA202409010001.md): Drag Angle · cracked · Jun 30, 2024 · N547NN · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous Structure
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FDW DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT/FDW DRAG ANGLES BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM WERE R
- [SDR VNAA202409020002](https://openairdocs.org/sdr/VNAA202409020002.md): Seat Track · corroded · Jun 16, 2024 · N547NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT TRACK BTW FS 379.00 - FS 677.00 (6 EAS) AT PASSENGER CABIN. RIGHT SIDE SEAT TRACK BTW FS 379.00 - FS 677.00 AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND WERE REPLACED PER CRJ900 AMM 53-00-49
- [SDR VNAA202409010030](https://openairdocs.org/sdr/VNAA202409010030.md): Seat Track · corroded · Jun 16, 2024 · N547NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT RAIL BTW FS 669.40 TO FS 977.00 AND STGR 15RH AT CABIN PAX. SEAT RAIL BTW FS 669.40 TO FS 977.00 AND STGR 15RH AT CABIN PAX WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND WERE REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A1
- [SDR VNAA202409010021](https://openairdocs.org/sdr/VNAA202409010021.md): Plate · corroded · Jun 16, 2024 · N547NN · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON PLATE (3EAS) AT AF BAGGAGE BAY COMPARMENT FLOOR STRUCTURE. PLATE (3EAS) AT AF BAGGAGE BAY COMPARMENT WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-32-58-101-001-A01 AND WERE REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-0
- [SDR VNAA202409010006](https://openairdocs.org/sdr/VNAA202409010006.md): Rib · cracked · Jun 16, 2024 · N547NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK ON OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT RH WING. OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT RH WING WAS REPAIRED PER REO 690-57-51-363 REV. - -
- [SDR VNAA202409010005](https://openairdocs.org/sdr/VNAA202409010005.md): Rib · cracked · Jun 16, 2024 · N547NN · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > CRACK ON OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT LH WING. OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT LH WING WAS REPAIRED PER REO 690-57-51-362 REV. - -
- [SDR VNAA202307311112](https://openairdocs.org/sdr/VNAA202307311112.md): Dcu · faulted · Jul 30, 2023 · N547NN · Cndair CL6002D24 · Elevator Control System
  > ELEVATOR SPLIT CAUTION IN FLIGHT WITH A CAS MISCOMPARE STATUS / R & R BOTH DCU'S IAW CRJ 900 AMM 31-41-04-000/400-801-A01. PERFORMED OPS TEST IAW AMM 31-41-04-710-801-A02. OPS TEST GOOD AT THIS TIME
- [SDR VNAA202302171111](https://openairdocs.org/sdr/VNAA202302171111.md): Sensor · unserviceable · Feb 16, 2023 · N547NN · Cndair CL6002D24 · Stabilizer Control System
  > DURING CLIMB OUT THEY RECEIVED A CAUTION ELEVATOR SPLIT MESSAGE AND A CAS MISCOMP STATUS MSG. REMOVED AND REPLACED LH AND RH ELEVATOR POSITION TRANSMITTERS IAW CRJ900 AMM 27-34-10-000/400-801
- [SDR VNAA202302091111](https://openairdocs.org/sdr/VNAA202302091111.md): None · none · Feb 6, 2023 · N547NN · Cndair CL6002D24 · Elevator Control System
  > CLIMBING OUT FROM CLT RCVD ELEVATOR SPLIT CAUTION MSG NORMAL ELEVATOR INPUT BEING APPLIED. CLIMBING LEFT TURN BETWEEN 6K AND 8K FT AT 250 KTS. COMPLETED DOUBLE TENSIONING OF ELEVATOR CONTROL CABLES IAW CRJ900 AMM 21-31-00-750-801
- [SDR VNAA202110051112](https://openairdocs.org/sdr/VNAA202110051112.md): Transmitter · faulted · Oct 2, 2021 · N547NN · Cndair CL6002D24 · Elevator Control System
  > SHORTLY AFTER TAKEOFF CREW RECEIVED AN "ELEVATOR SPLIT CAUTION MESSAGE". THEY DECLARED EMERGENCY AND RETURNED TO SAV. THEY DID NOT LAND OVERWEIGHT AND RETURNED TO THE GATE WITHOUT FURTHER ISSUE. NO FURTHER INFORMATION AT THIS TIME. ELEVATOR SPLIT CAUTION MSG
- [SDR VNAA2020102011118](https://openairdocs.org/sdr/VNAA2020102011118.md): Warning Message · false activation · Oct 18, 2020 · N547NN · Cndair CL6002D24 · Engine Oil Temperature
  > PRECAUTIONARY ENGINE SHUTDOWN DUE TO HIGH OIL TEMPERATURE. AIR RETURN TO CLT FOR RT ENGINE OIL HIGH TEMPERATURE. REMOVED AND REPLACED DCU 1, IAW CRJ 900 AMM 31-41-04-000/400-801. OPERATIONS CHECKED GOOD. PERFORMED OPERATIONS CHECK OF DCU 1, IAW CRJ 900 AMM

Next page: https://openairdocs.org/aircraft/N547NN/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 = 'N547NN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N547NN/reports

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