N550NN
Service difficulty reports · 89
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 = 'N550NN' 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.
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 = 'N550NN' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR VNAA2026082823701Pcu · bindingINBD FLT SPOILERS CAUTION. INTERROGATED MDC, TROUBLESHOT B1 007910 IAW FIM 27-64-01-810-812-A01. PERFORMED SPOST 1 AND OPS TEST OF MULTI-FUNCTION SPOILERS IAW AMM 27-64-00-710-801. OPS TEST GOOD, FAULT/JAM DID NOT REOCCUR.SDR VNAA2026041316002Display · faultedMFD FAILURE IN FLIGHT / REMOVED AND REPLACED CAPT MFD EFD 2 IAW AMM 31-61-01-000/400-801-A02, PERFORMED OPERATIONAL TEST IAW AMM 31-61-01-710-801-A03, OPS CHECK GOOD.SDR VNAA2025102811102Window · crackedCAPT SIDE WINDOW CRACKED AT FL340. DECLARED EMERGENCY. / REMOVED AND REPLACED THE LH SIDE WINDOW IAW CRJ900 AMM 56-12-01-000/400-801-A01-PSA. LEAK CHECK GOOD. PERFORMED OPS CHECK OF TEMPERATURE CONTROLLER IAW CRJ900 AMM 30-41-06-710-801-A01, OPS CHECK GOOD.SDR VNAA20251005027Bracket · crackedCRACKS ON CANISTER ON SLAT TRACK 1-3 INSIDE LH WING MAIN FUEL TANK WS= 148. CANISTER ON SLAT TRACK 1-3 INSIDE LH WING MAIN FUEL TANK WS= 148 WAS REPAIRED PER REO 670-57-42-577. REV. - -SDR VNAA2025F00017Angle · corrodedCORROSION ON ANGLE INNER SIDE OF LH LANDING GEAR PRESSURE SWITCH AND SETTLEMENT AREA ANGLE OF ACCESS PANEL 542AZ. CORROSION ON ANGLE INNER SIDE OF LH LANDING GEAR PRESSURE SWITCH WAS REMOVED PER SRM 51-21-06-001-001-A01 AND EVALUATED WITHIN LIMITS PER SRM 5SDR VNAA2025F00016Static Wick · corrodedCORROSION ON SETTLEMENT BASE OF STATIC DISCHARGE WS353.00 AT RH WING. BASE OF STATIC DISCHARGE WS353.00 AT RH WING WAS EVALUATED PER CRJ-900 SRM 53-21-43-101-001-A03 AND REPLACED PER CRJ-900 AMM 23-61-01-400-802-A02.SDR VNAA20251004002Drag Angle · crackedCRACK WAS FOUND AFFECTING AFT DRAG ANGLES AT LH VERTICAL STAB BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. PERMANENT REPAIR WAS PERFORMED IN ACCORDANCE WITH CRJ- 900 SRM 55-31-00-201-001-A01.SDR VNAA20251005023Lug · corrodedAFTER REMOTION OF BUSHINGS OF LH AILERON, CORROSION ON HOUSING OF LUGS : CENTER LUGS L1, L2, L3, L4,L5 L6 ALSO ON HINGE 4 UPPER AND LOWER HOUSING LUGS AT LH AILERON. HOUSINGS WERE CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01 AND REPAIRED PER REO: 670-57-61-23SDR VNAA20251004026Lug · damagedTO PERFORM OVERSIZE BEARINGS INSTALLATON; REWORK LUG BORE OF INBOARD FITTING AT RH AILERON TO INSTALL BEARING P/N: KSC327108B-02. LUG BORE OF INBOARD FITTING AT RH AILERON WAS REWORKED AND PREPARE TO SPHERICAL BEARING P/N: KSC327108B-02 PER REO 690-57-61-440.SDR VNAA20251004025Lug · corrodedAFTER REMOTION OF BUSHINGS OF LT AILERON, CORROSION ON HOUSING OF LUGS : CENTER LUGS L1, L2, L3, L4,L5 L6 ALSO ON HINGE 4 UPPER AND LOWER HOUSING LUGS AT LT AILERON. HOUSINGS WERE CLEANED PER CRJ 900 SRM 51-26-00-001-001-A01 AND REPAIRED PER REO: 670-57-61-23SDR VNAA20251005026Seat Track · corrodedCORROSION ON FLOOR SEAT RAILS BTW FS 349 TO FS 977 AT RBL 9 PASSENGER CABIN. FLOOR SEAT RAILS BTW FS 349 TO FS 977 AT RBL 9 PASSENGER CABIN WERE REPLACED PER CRJ900 AMM 53-00-49-400-801, CRJ900 AMM 53-00-49-000-801 AND CRJ900 SRM 53-41-49-101-001-A02SDR VNAA20251005025Seat Track · corrodedCORROSION ON FLOOR SEAT RAILS BTW FS 364 TO FS 693 AT LBL 27 PASSENGER CABIN. NEW SECTIONS FLOOR SEAT RAILS BTW FS 364 TO FS 693 AT LBL 27 PASSENGER CABIN WERE REPLACED PER CRJ900 SRM 53-41-49-101-001-A02, CRJ900 AMM 53-00-49-000-801 AND CRJ900 AMMM 53-00-49SDR VNAA20251005022Skin · damagedPREVIOUS REWORK (3EA) BTW STGR 17R TO 16R AND FS 656, FS 661+17, FS 661+46 AT EXTERNAL FUSELAGE WERE REPLACED PER CRJ-900 SRM 53-00-00-201-003-A03 AND REPAIRED PER CRJ 900 SRM 53-00-01-201-001-A03.SDR VNAA20251005021Skin · damagedPREVIOUS REWORK (3EA) BTW STGR 19R TO 17R AND FS 581, FS 603, FS 635 AT EXTERNAL FUSELAGE. PREVIOUS REWORK (3EA) BTW STGR 19R TO 17R AND FS 581, FS 603, FS 635 AT EXTERNAL FUSELAGE WERE REPLACED PER CRJ-900 SRM 53-00-00-201-003-A03 AND REPAIRED PER CRJ 900 SSDR VNAA20251005020Skin · damagedPREVIOUS REWORK (3EA) BTW STGR 20R TO 18R AND FS 385, FS 427, FS 453 AT EXTERNAL FUSELAGE. PREVIOUS REWORK (2EA) BTW STGR 20R TO 18R AND FS 385 AND FS 427 AT EXTERNAL FUSELAGE WERE REPAIRED PER REO 690-53-21-2018 REV - - AND FASTENER (1 EA) BTW STGR 20R TO SDR VNAA20251005019Skin · damagedPREVIOUS REWORK (2EA) BTW STGR 22L TO 20L AND FS 596, FS 606 AT EXTERNAL FUSELAGE. PREVIOUS REWORK (2EA) BTW STGR 22L TO 20L AND FS 596, FS 606 AT EXTERNAL FUSELAGE WERE EVALUATED PER CRJ900 SRM 53-31-01-101-003-A04 AND REPAIRED PER REO 690-53-31-1071 REV.-.SDR VNAA20251005018Skin · damagedPREVIOUS REWORK (4EA) BTW STGR 18L TO 17L AND FS 517, FS 563. FS 575, FS 638 AT EXTERNAL FUSELAGE. FASTENERS (2 EAS) BTW STGR 18L TO 17L AND FS 563. FS 575 AT EXTERNAL FUSELAGE WERE REPLACED PER CRJ900 SRM 53-00-00-201-003-A03, PREVIOUS REWORK BTW STGR 18L TOSDR VNAA20251005017Skin · damagedREVIUS REWORK (2EA) BTW STGR 19L TO 17L AND FS 477.40 AT FWD FUSELAGE. PREVIUS REWORK (2EA) BTW STGR 19L TO 17L AND FS 477.40 AT FWD FUSELAGE WERE REPAIRED PER REO 690-53-00-636 REV - -SDR VNAA20251005016Skin · damagedPREVIOUS REWORK (2EA) BTW STGR 21L TO 20L AND FS 280 TO FS 326 AT FWD FUSELAGE. REWORK BTW STGR 21L TO 20L AND FS 326 AT FWD FUSELAGE WAS REPAIRED PER REO 690-53-21-2030REV - - AND REWORK BTW STGR 21L TO 20L AND FS 326 AT FWD FUSELAGE WAS REPAIRED WITH NRC SDR VNAA20251005015Skin · damagedPREVIOUS REWORK (1EA) IN STGR 23L AND FS 211 AT FWD FUSELAGE. LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN BTW FS202.75 - FS280.00 AND BTW STR20L-STR23L WERE REPAIRED PER REO 670-53-11-2059 REV - -SDR VNAA20251005009Seat Track · corrodedCORROSION ON FLOOR SEAT RAILS BTW FS 549 TO FS 977 AT LBL 9 PASSENGER CABIN. SECTIONS FLOOR SEAT RAILS BTW FS 549 TO FS 977 AT LBL 9 PASSENGER WERE REPLACED PER CRJ900 SRM 53-41-49-101-001-A02, CRJ900 AMM 53-00-49-000-801 AND CRJ900 AMM 53-00-49-400-801.SDR VNAA20251005008Seat Track · corrodedCORROSION ON LH SIDE SEAT RAILS BTW FS 485 TO FS 977 AT PASSENGER CABIN. LH SIDE SEAT RAILS BTW FS 485 TO FS 977 AT PASSENGER CABIN DUE TO EXCESSIVE DAMAGE WERE FOUND OUT OF LIMITS IAW SRM 53-41-49-101-001-A02 AND SRM 53-31-49-101-001-A02 THEREFORE WERE REPLSDR VNAA20251005007Support Bracket · crackedCRACK ON CANISTER WELDED NO. 3 IN STA WS 148.00 OF INTERNAL RH MAIN FUEL TANK. CANISTER WELDED NO. 3 IN STA WS 148.00 OF INTERNAL RH MAIN FUEL TANK. WAS REPAIRED PER REO 670-57-42-577 REV - -SDR VNAA20251004027Seat Track · corrodedLUG BORE OF INBOARD FITTING AT RH AILERON WAS REWORKED AND PREPARE TO SPHERICAL BEARING P/N: KSC327108B-02 PER REO 690-57-61-440. NEW SECTIONS FLOOR SEAT RAILS BTW FS 364 TO FS 693 AT LBL 27 PASSENGER CABIN WERE REPLACED PER CRJ900 SRM 53-41-49-101-001-A02, CSDR VNAA20251004024Skin · damagedPREVIOUS REWORK (3EA) BTW STGR 17R TO 16R AND FS 656, FS 661+17, FS 661+46 AT EXTERNAL FUSELAGE. PREVIOUS REWORK (3EA) BTW STGR 17R TO 16R AND FS 656, FS 661+17, FS 661+46 AT EXTERNAL FUSELAGE WERE REPLACED PER SRM 53-00-00-201-003-A03 AND REPAIRED PER SRM 5SDR VNAA20251004023Skin · damagedDISCREPANCY; PREVIOUS REWORK (3EA) BTW STGR 19R TO 17R AND FS 581, FS 603, FS 635 AT EXTERNAL FUSELAGE . PREVIOUS REWORK (3EA) BTW STGR 19R TO 17R AND FS 581, FS 603, FS 635 AT EXTERNAL FUSELAGE WERE REPLACED PER SRM 53-00-00-201-003-A03 AND REPAIRED PER SRMSDR VNAA20251004022Skin · damagedPREVIOUS REWORK (3EA) BTW STGR 20R TO 18R AND FS 385, FS 427, FS 453 AT EXTERNAL FUSELAGE . EA) BTW STGR 20R TO 18R AND FS 453 AT EXTERNAL FUSELAGE WAS REPLACED PER CRJ900 SRM 53-00-00-201-003-A03SDR VNAA20251004021Skin · damagedPREVIOUS REWORK (2EA) BTW STGR 22L TO 20L AND FS 596, FS 606 AT EXTERNAL FUSELAGE. PREVIOUS REWORK (2EA) BTW STGR 22L TO 20L AND FS 596, FS 606 AT EXTERNAL FUSELAGE WERE EVALUATED PER CRJ900 SRM 53-31-01-101-003-A04 AND REPAIRED PER REO 690-53-31-1071 REV.-.SDR VNAA20251004020Skin · damagedPREVIOUS REWORK (4EA) BTW STGR 18L TO 17L AND FS 517, FS 563. FS 575, FS 638 AT EXTERNAL FUSELAGE FASTENERS (2 EAS) BTW STGR 18L TO 17L AND FS 563. FS 575 AT EXTERNAL FUSELAGE WERE REPLACED PER CRJ900 SRM 53-00-00-201-003-A03, PREVIOUS REWORK BTW STGR 18L TOSDR VNAA20251004019Skin · damagedPREVIOUS REWORK (2EA) BTW STGR 19L TO 17L AND FS 477.40 AT FWD FUSELAGE. PREVIUS REWORK (2EA) BTW STGR 19L TO 17L AND FS 477.40 AT FWD FUSELAGE WERE REPAIRED PER REO 690-53-00-636 REV - -SDR VNAA20251004018Skin · crackedPREVIOUS REWORK (2EA) BTW STGR 21L TO 20L AND FS 280 TO FS 326 AT FWD FUSELAGE. REWORK BTW STGR 21L TO 20L AND FS 326 AT FWD FUSELAGE WAS REPAIRED PER REO 690-53-21-2030 REV - , AND REWORK BTW STGR 21L TO 20L AND FS 326 AT FWD FUSELAGE WAS REPAIRED WITH NRSDR VNAA20251004017Skin · damagedPREVIOUS REWORK (1EA) IN STGR 23L AND FS 211 AT FWD FUSELAGE. LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN BTW FS202.75 - FS280.00 AND BTW STR20L-STR23L WERE REPAIRED PER REO 670-53-11-2059 REV - -SDR VNAA20251004011Seat Track · corrodedCORROSION ON FLOOR SEAT RAILS BTW FS 549 TO FS 977 AT LBL 9 PASSENGER CABIN. SECTIONS FLOOR SEAT RAILS BTW FS 549 TO FS 977 AT LBL 9 PASSENGER WERE REPLACED PER CRJ900 SRM 53-41-49-101-001-A02, AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.SDR VNAA20251004010Seat Track · corrodedCORROSION ON LH SIDE SEAT RAILS BTW FS 485 TO FS 977 AT PASSENGER CABIN. LT SIDE SEAT RAILS BTW FS 485 TO FS 977 AT PASSENGER CABIN DUE TO EXCESSIVE DAMAGE WERE FOUND OUT OF LIMITS PER CRJ900 SRM 53-41-49-101-001-A02 AND SRM 53-31-49-101-001-A02 THEREFORE WERSDR VNAA20251004009Support Bracket · crackedCRACK ON CANISTER WELDED NO. 3 IN STA WS 148.00 OF INTERNAL RH MAIN FUEL TANK.. CANISTER WELDED NO. 3 IN STA WS 148.00 OF INTERNAL RH MAIN FUEL TANK. WAS REPAIRED PER REO 670-57-42-577 REV - -SDR VNAA20251005024Lug · damagedPERFORM OVERSIZE BEARINGS INSTALLATON; REWORK LUG BORE OF INBOARD FITTING AT RH AILERON TO INSTALL BEARING P/N: KSC327108B-02. LUG BORE OF INBOARD FITTING AT RH AILERON WAS REWORKED AND PREPARE TO SPHERICAL BEARING P/N: KSC327108B-02 PER REO 690-57-61-440SDR VNAA20251005006Stiffener · out of limitsWEAR ON STIFFENER BELOW ACCESS PANEL 326 AL LH SIDE VERTICAL STAB AREA EMPENNAGE. STIFFENER BELOW ACCESS PANEL 326 AL LH SIDE VERTICAL STAB AREA EMPENNAGE WAS REPAIRED PER REO 690-55-32-210 REV - -SDR VNAA20251004008Stiffener · wornDISCREPANCY: WEAR ON STIFFENER BELOW ACCESS PANEL 326 AL LH SIDE VERTICAL STAB AREA EMPENNAGE.. STIFFENER BELOW ACCESS PANEL 326 AL LH SIDE VERTICAL STAB AREA EMPENNAGE WAS REPAIRED PER REO 690-55-32-210 REV - .SDR VNAA20251005004Stringer · damagedHOLE THROUGH STGR 25RH AT FRAME AT FS 319.00 ON MAIN AVIONICS COMPARTMENT. STGR 25RH AT FRAME AT FS 319.00 ON MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01.SDR VNAA20251005003Rib · crackedCRACK ON RIB LEADING EDGE UPPER FACE SS=57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV. - . CRACK ON RIB LEADING EDGE UPPER FACE SS=57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV. - - .SDR VNAA20251005002Rib · crackedCRACK WAS FOUND ON RIB LEADING EDGE SS57.16 UPPER FACE T LH WING. CRACK WAS FOUND ON RIB LEADING EDGE SS57.16 UPPER FACE LH WING WAS REPAIRED PER REO 690-57-41-240 REV - -.SDR VNAA20251004006Stringer · damagedHOLE THROUGH STGR 25RH AT FRAME AT FS 319.00 ON MAIN AVIONICS COMPARTMENT. STGR 25RH AT FRAME AT FS 319.00 ON MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01.SDR VNAA20251004005Rib · crackedCRACK ON RIB LEADING EDGE UPPER FACE SS=57.16 AT RH WING. CRACK ON RIB LEADING EDGE UPPER FACE SS=57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV. - - .SDR VNAA20251004004Rib · crackedCRACK WAS FOUND ON RIB LEADING EDGE SS57.16 UPPER FACE T LH WING. CRACK WAS FOUND ON RIB LEADING EDGE SS57.16 UPPER FACE T LH WING WAS REPAIRED PER REO 690-57-41-240 REV - -.SDR VNAA20251004001Rib · crackedCRACK WAS FOUND AFFECTING AFT DRAG ANGLES AT LT VERTICAL STABILIZER BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. PERMANENT REPAIR PERFORMED IN ACCORDANCE WITH CRJ-900 SRM 55-31-00-201-001-A01.SDR VNAA20251005012Floorbeam · crackedCRACK ON FLOOR BEAM RBL 12, FS 280 AT FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CRACK ON FLOOR BEAM RBL 12, FS 280 AT FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT THEREFORE WAS REPLACED PER REPAIR PER REO 690-53-11-2052 REV. -SDR VNAA20251005005Intercostal · out of limitsCORROSION ON INTERCOSTALS (2 EAS) IN STA. FS= 349 TO FS= 364 BTWN STGR 26RH TO 26LH AT MAIN AVIONICS COMPARTMENT. CORROSION ON INTERCOSTAL IN STA. FS= 349 TO FS= 364 BTWN STGR 26RH AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-ASDR VNAA20251005001Support Angle · crackedCRACK ON ANGLE SUPPORT ON FS1098.20 AND STGR24RH ON INTERNAL FUSELAGE STRUCTURE AT AFT EQUIPMENT COMPARTMENT. ANGLE SUPPORT ON FS1098.20 AND STGR24RH ON INTERNAL FUSELAGE STRUCTURE AT AFT EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-ASDR VNAA20251004015Skin · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM WSDR VNAA20251004014Floorbeam · crackedDISCREPANCY: CRACK ON FLOOR BEAM RBL 12, FS 280 AT FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CORRECTIVE ACTION: CRACK ON FLOOR BEAM RBL 12, FS 280 AT FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT THEREFORE WAS REPLACED PER REPAIR P
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