N556NN

Service difficulty reports · 79

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

Query with SQL
duckdb -csv -c "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 = 'N556NN' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR VNAA2026073121902Engine · vibrationRIGHT ENGINE N1 FAN VIB UPTO 2.2 / PERFORMED STIFFNESS CHECK AND VIBE CHECK PER AMM 72-21-02-200-803-A01-PSA AND PPGRM 71-00-00-720-806-A01. NO DEFECTS NOTED.Jul 30, 2026 · N556NN · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR VNAA2025091111102Window · arcedRH SIDE WINDOW HAS BURN MARK FROM ARCING ON LOWER BUS BAR / REMOVED RH FLIGHT COMPARTMENT SIDE WINDOW IAW AMM 56-12-01-000-801-A01-PSA. INSTALLED RH FLIGHT COMPARTMENT SIDE WINDOW IAW AMM 56-12-01-400-801-A01-PSA.Sep 7, 2025 · N556NN · Cndair CL6002D24 · Flight Compartment WindowsSDR VNAA2024031311102Skin · dentedDENT RH FUSELAGE MIDWAY BETWEEN SERVICE DOOR AND WING ROOT / REPAIRED RH FUSELAGE SKIN BETWEEN FS 432.00 - FS 453.00 AND STR 16R - STR 18R IAW REO 690-53-21-1738. REPAIRED RH FLOOR SILL BETWEEN FS 432.00 - FS 442.00 AND STR 17R IAW SRM 53-00-45.Mar 12, 2024 · N556NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA2023120411101Heater · unserviceableGALLEY HEATER OVHT CAME ON ACCOMPANIED BY A HOT SMELL / REMOVED AND REPLACED GALLEY HEATER IAW CRJ 900 AMM 21-23-64-000/400-801. OPS CHECK GOOD. LEAK CHECK GOOD.Dec 2, 2023 · N556NN · Cndair CL6002D24 · Heating SystemSDR VNAA202311290001Plate · corrodedCORROSION ON PLATE ASSY (1EA) BTW STGR#27 TO STGR#26LH AND FS517.00, CORROSION ON PLATE ASSY (1EA) BTW FS533.00 TO FS549.00 AND STGR#25RH TO STGR#24RH, CORROSION ON PLATE ASSY (1EA) BTW FS565.00 TO FS581.00 AND STGR#27 TO STGR#26LH, CORROSION ON PLATE ASSY (2ENov 16, 2023 · N556NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202311280005Skin · dentedSEVERAL NICKS AND DENTS ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5. NICKS ON LOWER SKIN OF LH INBOARD FLAP FLS 42.00 TO FLS 65.5 WERE BLENDED OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND WERE EVALUATED WITHIN LIMITS PER CRJ900 SRM 57-52-01-101-001-Nov 8, 2023 · N556NN · Cndair CL6002D24 · Trailing Edge FlapsSDR VNAA202311290026Post · crackedCRACK ON RIVET AREA AT BULKHEAD DOOR POST BTW RBL9 AND FS 280.00. DAMAGED DOOR POST WAS REPAIRED PER REO 690-53-11-1625 REV. --Oct 19, 2023 · N556NN · Cndair CL6002D24 · Fuselage Main, StructureSDR VNAA202311290029Hinge Fitting · wornWEAR ON HINGES 2,3 AND CRACKS ON SUPPORT ANGLES (2E/A). HINGES 2,3 (AILERON CENTER HINGE FITTING ASSY AND LEADING EDGE RIBLET AT AIL STA 329.975, RHS) WERE REPAIRED PER REO NUMBER 690-57-61-306 REV. - - AND EA 23-C9-57-0530 REV. B. SECTION III PERMANENT REPAIOct 16, 2023 · N556NN · Cndair CL6002D24 · AileronsSDR VNAA202311290023Frame · corrodedCORROSION ON FRAME FS 847.00+16 BTW STGR 25L-25R. CORROSION ON FRAME FS 847.00+16 BTW STGR 25L-25R WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-51-06-101-003-A05 AND WAS REPAIRED PER CRJ-900 SRM 53-00-06-201-001-A03Oct 12, 2023 · N556NN · Cndair CL6002D24 · Fuselage Main, FrameSDR VNAA202311290021Skin · corrodedCORROSION ON DOOR SILL BTW FS517.00 TO FS565.00 AT SURROUND STRUCTURE FWD CARGO DOOR. CORROSION ON DOOR SILL BTW FS517.00 TO FS565.00 AT SURROUND STRUCTURE FWD CARGO DOOR WAS REMOVED PER EA 23-C9-53-1536 REV. IROct 12, 2023 · N556NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202311290020Frame · corrodedCORROSION ON FRAME AT FS661.00+90.00 BTW STGR#26LH/RH FWD CARGO COMP. CORROSION ON FRAME AT FS661.00+90.00 BTW STGR#26LH/RH FWD CARGO COMP WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-06-101-003-A04 AND WAOct 12, 2023 · N556NN · Cndair CL6002D24 · Fuselage Main, FrameSDR VNAA202311290017Skin · dentedSEVERAL DENTS (2EAS) ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING LH. SEVERAL DENTS (2EAS) ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING LH WERE REPAIRED PER EA 23-C9-53-1542 REV. IROct 12, 2023 · N556NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202311290013Frame · corrodedCORROSION ON FRAME FS 847.00+48 BTW STGR 25L-25R. CORROSION ON FRAME FS 847.00+48 BTW STGR 25L-25R WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-51-06-101-003-A05 AND WAS REPAIRED PER CRJ900 SRM 53-00-06-201-001-A03Oct 12, 2023 · N556NN · Cndair CL6002D24 · Fuselage Main, FrameSDR VNAA20231128012Seat Track · corrodedCORROSION & SCRATCHES ON SIDE SEAT RAIL LH (SEVERAL LOCATIONS) BTW FS409 TO FS761. SIDE SEAT RAIL LH BTW FS409 TO FS761 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 AND WAS REPLACED PEROct 12, 2023 · N556NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202311290025Hinge Fitting · corrodedBORE OF HINGE 2 (INBD/OUTBD)AND 3(INBD) AT AILERON. HINGE 2 AND HINGE 3 POSITION LUGS THEY ARE INCORRECTLY NAMED; SEE REPAIR REO 670-57-61-237 REV. -. THE DAMAGE REPORTS IS ON CENTER HINGE FITTING POSITION LUGS "R1", "R2" AND LUG "R5", THEREFORE BORE LUGS R1Oct 11, 2023 · N556NN · Cndair CL6002D24 · AileronsSDR VNAA202311290012Seat Track · corrodedCORROSION ON SIDE SEAT RAIL 15 LH BTW FS 897.70 TO FS 954 AT PASSENGER CABIN. CORROSION ON SIDE SEAT RAIL 15 LH BTW FS 897.70 TO FS 954 AT PASSENGER CABIN. WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-51-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-Oct 11, 2023 · N556NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202311290011Seat Track · corrodedCORROSION ON SIDE SEAT RAIL 15 LH BTW FS 847.00 + 8.40 TO FS 897.70 AT PASSENGER CABIN. CORROSION ON SIDE SEAT RAIL 15 LH BTW FS 847.00 + 8.40 TO FS 897.70 AT PASSENGER CABIN WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-51-49-101-001-A02 AND WAS REPLACED POct 11, 2023 · N556NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202311290010Seat Track · corrodedCORROSION ON SIDE SEAT RAIL 15 LH BTW FS 785.15 TO FS 847.00 + 8.40 AT PASSENGER CABIN. CORROSION ON SIDE SEAT RAIL 15 LH BTW FS 785.15 TO FS 847.00 + 8.40 AT PASSENGER CABIN WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND WAS REPLACED POct 11, 2023 · N556NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202311290009Seat Track · corrodedCORROSION ON SIDE SEAT RAIL 15 RH BTW FS897.70 TO FS 954 AT PASSENGER CABIN. SIDE SEAT RAIL 15 RH BTW FS897.70 TO FS 954 AT PASSENGER CABIN WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-51-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)Oct 11, 2023 · N556NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202311290008Seat Track · corrodedCORROSION ON SIDE SEAT RAIL 15 RH BTW FS 847.00 + 8.40 TO FS 897.70 AT PASSENGER CABIN. SIDE SEAT RAIL 15 RH BTW FS 847.00 + 8.40 TO FS 897.70 AT PASSENGER CABIN WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-51-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 5Oct 11, 2023 · N556NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202311290007Seat Track · corrodedCORROSION ON SIDE SEAT RAIL 15 RH BTW FS 785.15 TO FS 847.00 + 8.40 AT PASSENGER CABIN. SIDE SEAT RAIL 15 RH BTW FS 785.15 TO FS 847.00 + 8.40 AT PASSENGER CABIN WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND WAS REPLACED PER CRJ900 AMM 5Oct 11, 2023 · N556NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202311290006Seat Track · corrodedCORROSION AND SCRATCHES ON SEAT TRACK RBL 9.00 BTW FS 847 + 16 TO FS 954 AT PASSENGER CABIN. CORROSION AND SCRATCHES ON SEAT TRACK RBL 9.00 BTW FS 847 + 16 TO FS 954 AT PASSENGER CABIN WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND CRJ90Oct 11, 2023 · N556NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202311290005Seat Track · corrodedCORROSION ON SEAT TRACK LBL 9.00 BTW FS 847.00 TO FS 954 AT PASSENGER CABIN. CORROSION ON SEAT TRACK LBL 9.00 BTW FS 847.00 TO FS 954 AT PASSENGER CABIN WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-51-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-Oct 11, 2023 · N556NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202311290003Seat Track · corrodedCORROSION AT RBL9 SEAT RAIL BETWEEN FS661.00+32- FS677. CORROSION AT RBL9 SEAT RAIL BETWEEN FS661.00+32- FS677. WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)Oct 11, 2023 · N556NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20231128011Seat Track · corrodedCORROSION & SCRATCHES ON SIDE SEAT RAIL RH (SEVERAL LOCATIONS) BTW FS409 TO FS761. CORROSION & SCRATCHES ON SIDE SEAT RAIL RH (SEVERAL LOCATIONS) BTW FS409 TO FS761. WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01; CRJ900 SRM 53-31-49-101-00Oct 11, 2023 · N556NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20231128007Seat Track · corrodedCORROSION AT RBL9 SEAT RAIL BETWEEN FS481- FS581. CORROSION AT RBL9 SEAT RAIL BETWEEN FS481- FS581 WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12).Oct 11, 2023 · N556NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202311280012Beam · crackedCRACK ON COCKPIT FLOOR LONGITUDINAL BEAM RH (RBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM RH (RBL12) TO CROSSBEAM FS 280 WAS REPAIRED PER REO 690-53-11-1616 REV. --Oct 11, 2023 · N556NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA20231128006Seat Track · corrodedCORROSION AT LBL 27 SEAT RAIL BETWEEN FS485- FS581. CORROSION AT LBL 27 SEAT RAIL BETWEEN FS485- FS581 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)Oct 11, 2023 · N556NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202311280010Skin · corrodedCORROSION ON INTERNAL SKIN CUT OUT, DOOR SURROUND STRUCTURE, MAIN AVIONIC COMPARTMENT. CORROSION ON INTERNAL SKIN CUT OUT, DOOR SURROUND STRUCTURE, MAIN AVIONIC COMPARTMENT WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS REPAIRED PER REO 690-53-21-032Oct 11, 2023 · N556NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA20231128005Seat Track · corrodedCORROSION AT RBL9 SEAT RAIL BETWEEN FS349 - FS477. RBL9 SEAT RAIL BETWEEN FS349 - FS477 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)Oct 11, 2023 · N556NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202311280008Skin · nickedSEVERAL NICKS BTW FS225.00 TO FS 265.00 AND BTW STGR#25 LH TO STGR#25 RH EXTERNAL FUSELAGE. NICKS BTW FS225.00 TO FS 265.00 AND BTW STGR#25 LH TO STGR#25 RH EXTERNAL FUSELAGE WERE BLENDED OUT PER REO 690-53-11-1627 REV. --Oct 11, 2023 · N556NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA20231128004Seat Track · corrodedCORROSION AT LBL 27 SEAT RAIL BETWEEN FS364-FS485. CORROSION AT LBL 27 SEAT RAIL BETWEEN FS364-FS485 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)Oct 11, 2023 · N556NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20231128003Seat Track · corrodedCORROSION AT LBL9 SEAT RAIL BETWEEN FS485-581. CORROSION WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-49-101-001-A02 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)Oct 11, 2023 · N556NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20231128002Intercostal · corrodedCORROSION ON INTERCOSTAL ATTACHED TO STRINGER 20RH IN STA. FS= 310 TO FS= 319.70 WAS FOUND. CORROSION REMOVED PER CRJ900 SRM 51-21-06-001-001-A01; WAS EVALUATED PER CRJ900 SRM 53-21-23-101-002-A02 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01Oct 11, 2023 · N556NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA20231128001Door Frame · corrodedCORROSION ON KICKPLATE AND MID CAP AT SURROUND STRUCTURE PASSENGER DOOR. CORROSION REMOVED PER CRJ900 SRM 51-21-06-001-001-A01; WERE EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-001-A02 AND WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND PER CROct 11, 2023 · N556NN · Cndair CL6002D24 · Fuselage Main, StructureSDR VNAA20231128010Seat Track · corrodedCORROSION AT LBL9 SEAT RAIL BETWEEN FS364 - FS485. SEAT RAIL BETWEEN AT LBL9 FS364 - FS485 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01 AND WAS REPLACED PER CRJ900 AMM 53-00-49 (CONFIG A12)Oct 10, 2023 · N556NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202311280011Beam · crackedCRACK ON COCKPIT FLOOR LONGITUDINAL BEAM LH (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM LH (LBL12) TO CROSSBEAM FS 280 WAS REPAIRED PER REO 690-53-11-1616 REV. --Oct 9, 2023 · N556NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202311290028Hinge Fitting · excess playDAMAGE T: ELONGATED HOLES DURING ADJUSTMENT OF THE NEW HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION, IN REF TO NRC: 00191. HINGE FITTING NO. 2 AND NO. 3 AT VERTICAL STABILIZER REAR SPAR MIDDLE SECTION WERE REPLACED PER RIL #21Oct 6, 2023 · N556NN · Cndair CL6002D24 · Vertical StabilizerSDR VNAA202311290027Angle · corrodedAFTER LOWER SILL OF AFT BAGGAGE BAY DOOR REMOVAL IN REF NRC 00105, CORROSION ON UPPER/LOWER FACE AT INNER CHORD 2 E/A (MID/AFT) WAS FOUND. DUE TO DAMAGE IS NOT ALLOWED PER CRJ900 SRM 53-61-23-101-001-A01, INNER CHORD MID AND AFT WERE REPLACED PER CRJ900 SRM 5Oct 6, 2023 · N556NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202311290024Frame · corrodedCORROSION ON FRAME FS 847.00+32 BTW STGR 25L-25R. CORROSION ON FRAME FS 847.00+32 BTW STGR 25L-25R WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-51-06-101-003-A05 AND WAS REPAIRED PER CRJ-900 SRM 53-00-06-201-001-A03.Oct 6, 2023 · N556NN · Cndair CL6002D24 · Fuselage Main, FrameSDR VNAA202311290022Canister · crackedCRACK IN CANISTER WELDED NO.3, IN STA. WS 148 OF INTERNAL RH MAIN FUEL TANK. (SM). CANISTER WELDED NO.3, IN STA. WS 148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. --Oct 6, 2023 · N556NN · Cndair CL6002D24 · Wing Miscellaneous StructureSDR VNAA202311290019Frame · corrodedCORROSION ON FRAME (BOTH SIDES) AT FS661.00+62.00 BTW STGR#26LH/RH FWD CARGO COMP. SUMMARY: CORROSION ON FRAME (BOTH SIDES) AT FS661.00+62.00 BTW STGR#26LH/RH FWD CARGO COMP WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, WAS EVALUATED OUT OF LIMITS PER CRJ9Oct 6, 2023 · N556NN · Cndair CL6002D24 · Fuselage Main, FrameSDR VNAA202311290018Bracket · corrodedCORROSION ON BRAKET MACHINED (1EA) BTW FS645.00 TO FS661.00 AND STGR#27 TO STGR#26LH, CORROSION ON BRAKET MACHINED (1EA) BTW FS533.00 TO FS549.00 AND STGR#27 TO STGR#26LH FWD CARGO COMP. CORROSION ON BRACKETS (2EAS) WAS REMOVED PER CRJ900 SRM 51-21-06-001-001Oct 6, 2023 · N556NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202311290016Skin · dentedSEVERAL DENTS (8EAS) ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING RH. DENTS (8EAS) ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING RH WERE REPAIRED PER EA 23-C9-53-1553 REV. IROct 6, 2023 · N556NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA202311290015Rib · crackedCRACK ON RIB LEADING EDGE SS57.16 WAS FOUND AT LH WING. RIB LEADING EDGE SS57.16 AT LH WING WAS REPAIRED PER REO 690-57-41-240. REV. --Oct 6, 2023 · N556NN · Cndair CL6002D24 · Wing, Rib/BulkheadSDR VNAA202311290014Rib · crackedCRACK ON RIB LEADING EDGE SS57.16 WAS FOUND AT RH WING. RIB LEADING EDGE SS57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-240. REV. --CRACK ON RIB LEADING EDGE SS57.16 WAS FOUND AT RH WING RIB LEADING EDGE SS57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-2Oct 6, 2023 · N556NN · Cndair CL6002D24 · Wing, Rib/BulkheadSDR VNAA202311290004Floor Support · corrodedCORROSION ON FLOOR SUPPORT LBL 27 BTW FS 1000.00- FS 1047.00. CORROSION ON FLOOR SUPPORT LBL 27 BTW FS 1000.00- FS 1047.00 WAS REPAIRED PER EA 23-C9-53-1531 REV. IROct 6, 2023 · N556NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202311290002Frame · corrodedCORROSION ON FRAME(BOTH SIDES) AT FS661.00+46.00 BTW STGR#27 TO STGR#26RH FWD CARGO COMP. CORROSION ON FRAME FS 661.00+46.00 BTW STGR 27-26R WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01; WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-31-06-101-003-A04 ANDOct 6, 2023 · N556NN · Cndair CL6002D24 · Fuselage Main, FrameSDR VNAA20231128009Floor Support · corrodedCORROSION ON FLOOR PANEL SUPPORT ANGLE BTW FS280 AND STGR 26L-26R AT MAIN AVIONICS COMPARTMENT. CORROSION ON FLOOR PANEL SUPPORT ANGLE BTW FS280 AND STGR 26L-26R WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01; WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-0Oct 6, 2023 · N556NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202311280009Skin · nickedPERM REPAIR BEFORE 20,505.22 FH - RH IB FLAP WITHIN 1458.07 FHS FROM IR (BEFORE 20,505.22 FH), REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. RH INBOARD LOWER SKIN WAS REPAIRED PER CRJ-900 SRM 57-52-01-201-005-A01 IN REFERENCE Oct 6, 2023 · N556NN · Cndair CL6002D24 · Trailing Edge Flaps
Back to N556NN