N551NN
Service difficulty reports · 73
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 = 'N551NN' 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 = 'N551NN' 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 VNAA202608310026Fitting · corrodedCORROSION FLOOR FITTING IN FWD ACCESS 305 (1EA) ON GALLEY 3 AND WARDROBE. FLOOR FITTING IN FWD ACCESS 305 (1 EA) ON GALLEY 3 AND WARDROBE WAS REPLACED PER CMM 25-33-3I0.SDR VNAA202608310025Rib · crackedCRACKED DOUBLER, RIB SS 27.75 AT INBD FIXED LEADING-EDGE RT WING. DOUBLER, RIB SS 27.75 AT INBD FIXED LEADING-EDGE, RT WING WAS REPLACED IAW SRM 51-42-06-001-001-A01. SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01.SDR VNAA202608310024Bushing · abnormalIN REFERENCE TO TRFKE00BN3TB: FABRICATE BUSHINGS ON LUGS L2 & R2 FROM AILERONS RT & LT. BUSHINGS ON LUGS L2 & R2 FROM AILERONS RT & LT WERE FABRICATED IAW REO 670-57-61-237, REV -.SDR VNAA202608310022Floorbeam · corrodedCORROSION ON UPPER FACE, FLOORBEAM ANGLE BS 280 AT COCKPIT. FLOORBEAM ANGLE WAS REMOVED IAW SRM 51-21-06-001-001-A01 AND OUT OF LIMITS IAW SRM 53-00-00-101-001-A01 AND REPLACED IAW SRM 51-42-06-001-001-A01.SDR VNAA202608310023Hinge Fitting · corrodedAFTER REMOVAL NLG AFT DOOR, CORROSION ON HING FITTING LT WAS FOUND. DUE TO EXCESSIVE DAMAGE ON HINGE FITTING LT WAS REPLACED IAW SRM 53-00-00-101-001-A01 AND SRM 51-41-02-001-001-A01.SDR VNAA202608310021Floor Support · crackedCRACKED ON FLOOR SUPPORT, RBL 12 BTWN BS 221.73 - 229 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL 79.50) WAS FOUND. CRACK ON FLOOR SUPPORT WAS REPAIRED IAW REO 690-53-11-2237. REV -.SDR VNAA202608310020Stringer · corrodedINITIAL INSPECTION: CORROSION ON STRINGER 24R, BS453 - 469 AT FWD CARGO BAY. STRINGER 24R, BS 453 - 469 WAS REPAIRED IAW SRM 53-00-03-201-001-A02.SDR VNAA202608310019Bracket · corrodedCORROSION ON MACHINED BRACKET (8EAS) OF FLOOR STRUCTURE AT FWD CARGO BAY BTWN BS 517 - 661 + 16.00 AND STR 22L TO 26R. ON MACHINED BRACKET (4EAS) OF FLOOR STRUCTURE AT FWD CARGO COMPARTMENT BTW FS517.00 TO FS661.00 + 16.00 AND STGR 22LH TO 26RH PAINT WERE REMSDR VNAA202608310018Seat Track · corrodedCORROSION ON SEAT TRACKS, RBL 9, BS 485 - 581, BS 582 - 669, BS 708 - 847+16 - 977. DUE TO EXCESSIVE DAMAGE ON SEAT TRACKS (7 EAS) WERE REPLACED IAW SRM 53-31-49-101-001-A02, AND AMM 53-00-49-400-801 (CONFIG A12).SDR VNAA202608310017Seat Track · corrodedCORROSION ON SEAT TRACK LBL 27, BS 485 - 533. DUE TO EXCESSIVE DAMAGE ON THE SEAT TRACK WAS REPLACED IAW SRM 53-31-49-101-001-A02, & AMM 53-00-49-400-801 (CONFIG A04).SDR VNAA202608310016Seat Track · corrodedCORROSION ON SEAT TRACK LBL 9 BTWN BS 485 - 581, 582 - 669, 708 - 847+16 - 977. THE SEAT TRACK EVALUATED WITH EXCESSIVE DAMAGE IAW SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02, SRM 53-41-49-101-001-A02, SRM 53-51-49-101-001-A02, & REPLACED IAW AMM 5SDR VNAA202608310015Seat Track · corrodedCORROSION ON LT SEAT TRACK, BS 744 - 762, BS 847 - 852, BS 853 - 913. DUE TO EXCESSIVE DAMAGE ON THE SEAT TRACKS WERE REPLACED IAW SRM 53-41-49-101-001-A02, & AMM 53-00-49-400-801, (CONFIG A12).SDR VNAA202608310014Seat Track · corrodedCORROSION ON RT SIDE SEAT TRACK BTWN BS 744 - 762, BS 847 - 852, BS 853 - 977. DUE TO EXCESSIVE DAMAGE ON THE SEAT TRACK (6 EA) MUST BE REPLACED.SDR VNAA202608310013Door Sill · corrodedCORROSION ON LOWER SILL BTW FS1000.00 AND FS1047.00 AT AFT BAGGAGE DOOR CUTOUT. CORROSION ON LOWER SILL BTW BS 1000 AND 1047 AT AFT CARGO DOOR CUTOUT WAS REMOVED IAW SRM 51-21-06-001-001-A01, & EVALUATED OUT OF LIMITS IAW SRM 53-61-23-201-001-A01, & REPLACEDSDR VNAA202608310012Seat Track · corrodedCORROSION ON THE SEAT TRACK LBL 9, BS 364 - 480.50, AS WELL AS ON THE SEAT TRACK AT RBL 9, BS 349 - 480.50. SEAT TRACK LBL 9, BS 364 - 480.50. AS WELL AS ON THE SEAT TRACK AT RBL 9, BS 349 - 480.50. WERE EVALUATED WITH EXCESIVE DAMAGE IAW SRM 53-21-49-101-SDR VNAA202608310011Seat Track · corrodedCORROSION ON RT SIDE SEAT TRACKS (4EA) BTW BS 379 TO 669. DUE TO EXCESIVE DAMAGE ON RH SIDE SEAT TRACKS (4EA) BTW STA FS 379 TO FS 669, SEAT TRACKS WERE REPLACED IAW SRM 53-21-49-101-001-A01 AND SECTION OF SIDE SEAT TRACKS RT (4EA) WERE INSTALLED BTW BS 379 SDR VNAA202608310010Seat Track · corrodedCORROSION ON LT SIDE SEAT TRACKS (5 EA) BTWN BS 379 - 669. DUE TO EXCESSIVE DAMAGE ON THE SEAT TRACKS WERE REPLACED IAW SRM 53-21-49-101-001-A01, & AMM 53-00-49-400-801, (CONFIG A12).SDR VNAA202608310009Slat Track · corrodedCORRODED SLAT TRACKS, 1 - 2 LT, 2 - 2 LT, 1 - 2 RT, AND 2 - 2 RT AT LT & RT WINGS. SLAT TRACK 1 - 2 LT REPAIRED IAW REO 690-57-42-1456, REV-, SLAT TRACK 2 - 2 LT REPAIRED IAW REO 690-57-42-1454, REV A (VISUALLY INSPECT AT INTERVALS NOT TO EXCEED 4000 FLIGHT SDR VNAA202608310008Web · crackedCRACK AT UPPER WEB OF ADG COMPARTMENT, BELOW OF SUPPORT AREA OF ADG PUMP. CRACK AT UPPER WEB OF ADG COMPARTMENT, BELOW OF SUPPORT AREA OF ADG PUMP WAS REPAIRED PER CRJ-900 REO 670-53-11-509 REV -E AND REO 690-53-11-2239 REV -.SDR VNAA202608310007Shim · wornWEAR ON SHIM IN SETTLEMENT AREA OF LATCH OF THE ACCESS PANEL 444CT AND 444CB AT RT ENGINE. WEAR ON SHIM IN SETTLEMENT AREA OF LATCH OF THE ACCESS PANEL 444CT AND 444CB AT RH ENG WERE BLEND OUT PER SRM 51-12-00-001-001-A01, ACCESS PANEL 444CT AT RH ENG WAS ESDR VNAA202608310006Skin · damagedRIGHT WING TRAILING EDGE DRILL STARTS UNDER PANEL 698BB WITHIN 2008 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IAW APPROVED PROCEDURES OR REPLACE PART. A NEW RFTS MUST BE SUBMITTED FOR THE DRILL START ON THE TRAILING EDGE 6SDR VNAA202608310005Skin · damaged2008FH PERM REPAIR, PANEL 698BB HAS DAMAGED COUNTERSINK WITHIN 2008 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IAW APPROVED PROCEDURES OR REPLACE PART. THE DAMAGED COUNTERSINK FOR PANEL 698BB WILL REQUIRE A NEW RFTS TO SDR VNAA202608310004Hinge · damagedPASSENGER DOOR SURROUND STRUCTURE - HINGE REPLACEMENT REPLACE THE PASSENGER DOOR HINGE. THE PASSENGER DOOR HINGE WAS REPLACED IAW SRM 53-21-23-201-007-A01.SDR VNAA202608310003Door Frame · scratched3600FH PERM REPAIR - TEMPORARY DISPOSITION FOR BLENDED SCRATCH DAMAGE TO FUSELAGE SKIN FWD PAX DOOR CUTOUT CORNER AT FS 310 & STR 17L - STR 18L THE SUBJECT REWORKED CONDITION IS STRUCTURALLY ACCEPTABLE FOR 3600 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF THSDR VNAA202608310002Retainer · crackedCRACK AND MISSING MATERIAL FWD/AFT CORNER, RETAINER SEAL CENTER CARGO DOOR. RETAINER SEAL AT FWD/ AFT CENTER CARGO DOOR WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01SDR VNAA202608310001Retainer · crackedCRACK AND MISSING MATERIAL FWD & AFT CORNERS, RETAINER SEAL FWD CARGO DOOR. RETAINER SEAL AT FWD & AFT CORNERS OF FWD CARGO DOOR WAS REPLACED IAW SRM 51-42-06-001-001-A01.SDR VNAA2025071511101Control Unit · failedDIV-FLAPS FAIL CAUTION AND SLATS FAIL CAUTION WHEN SELECTING FLAPS UP. SLATS AT 20 AND FLAPS AT 1. / REMOVED AND REPLACED SFECU1 IAW CRJ 900 AMM 27-51-05-000/400-801-A01. PERFORMED SEVERAL OPS CHECKS AND FAULT COULD NOT BE DUPLICATED. VERIFIED ALL FLAP ACTUATOSDR VNAA2024052911101Seal · leakingSTEERING INOP DURING APPROACH AND LANDING / FOUND NLG STRUT BOTTOMED, EVIDENCE OF FLUID LEAK. PERFORMED SEAL REPACK OF NLG IAW T.O. 32-079-002-19 REV. E. LEAK CHECK GOOD. ALSO PERFORMED NLG EXTENSION/RETRACTION IAW CRJ9 AMM 32ˆ’30ˆ’00ˆ’865ˆ’802 AND OPERATISDR VNAA202306230013Skin · dentedSEVERAL DENTS ON FUSELAGE SKIN (18 LH AND 13 RH), SETTLEMNT AREA OF LEFT AND RIGTH VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5%, BTW STGR 22LH TO STGR 21LH.
SEVERAL DENTS ON FUSELAGE SKIN (18 LH AND 13 RH), SETTLEMNT AREA OF LEFT ASDR VNAA202306230012Skin · unknownSCRIBE LINE ON FUSELAGE SKIN, SETTLEMNT AREA OF LEFT VENTRAL FIN FAIRING BTW FS 1162.00 TO FS 1192.00, BTW STGR 22LH TO STGR 21LH. SCRIBE LINE ON FUSELAGE SKIN, SETTLEMNT AREA OF LEFT VENTRAL FIN FAIRING BTW FS 1162.00 TO FS 1192.00, BTW STGR 22LH TO STGR 21LSDR VNAA202306230009Crossbeam · corrodedCORROSION ON CROSSBEAM AT FS 280.00 BTW RBL 9.00 AND LBL 9.00. CROSSBEAM AT FS 280.00 BTW RBL 9.00 AND LBL 9.00 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01SDR VNAA202306230008Angle · corrodedCORROSION AT LOWER MID CAP BETWEEN FS 310.00 AND FS 349.00 ON SURROUND STRUCTURE OF PASSENGER DOOR. LOWER MID CAP BETWEEN FS 310.00 AND FS 349.00 ON SURROUND STRUCTURE OF MESSENGER DOOR WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01 AND SRM 51-42-06-001-0SDR VNAA202306220010Beam · crackedCRACK ON COCKPIT FLOOR LONGITUDINAL BEAM (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR LONGITUDINAL BEAM (LBL12) TO CROSSBEAM FS 280 WAS REPAIRED PER REO 670-53-11-896.REV. - - AND REO 690-53-11-1561. REV. - -SDR VNAA202306220001Floorbeam · corrodedCORROSION ON FLOOR PANEL SUPPORT ANGLE UPPER FACE AT FS280.00 BTW RBL 9.00 AND LBL 9.00. FLOOR PANEL SUPPORT ANGLE UPPER FACE AT FS280.00 BTW RBL 9.00 AND LBL 9.00 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-42-21-001-001-A01SDR VNAA202306220002Unknown · corrodedCORROSION ON UPPER AND LOWER SURFACE AT RH LOWER SILL BTW FS 280 AND FS 295. RH LOWER SILL BTW FS 280 AND FS 295 WAS REPAIRED PER CRJ-900 SRM 53-21-43-201-002-A01SDR VNAA202306230010Skin · nickedSEVERAL NICKS ON LOWER/FWD FACE OF RH INBOARD FLAP FROM FLS 15.00 TO FLS 65.50. LOWER/FWD FACE OF RH INBOARD FLAP FROM FLS 15.00 TO FLS 65.50 WAS REPAIRED PER CRJ-900 SRM 57-52-01-201-005-A01SDR VNAA202306230006Floorbeam · corrodedCORROSION AT LBL27.00 FLOOR BEAM BTW FS 1000.00/1031.00. LBL27.00 FLOOR BEAM BTW FS 1000.00/1031.00 WAS REPAIRED PER EA 23-C9-53-0630 REV. IR SECTION III-PERMANENT REPAIRSDR VNAA202306220003Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) ON LEFT VERTICAL STABILIZER TO FUSELAGSDR VNAA202306230014Stringer Splice · corrodedCORROSION ON STRINGER SPLICE BTW STGR 21RH, FS333.00 AT E/E COMPARTMENT.
STRINGER SPLICE BTW STGR 21RH, FS333.00 AT E/E COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01SDR VNAA202306230003Intercostal · corrodedCORROSION INTERCOSTAL AT STGR 20RH BTW FS310.00 TO FS349.00. INTERCOSTAL AT STGR 20RH BTW FS310.00 TO FS349.00 WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01SDR VNAA202306230007Seat Track · corrodedCORROSION ON SEAT RAIL RLB 9.00 AND LBL 9.00 FROM FS 847.00 TO FS 977.00. SEAT RAIL RLB 9.00 AND LBL 9.00 FROM FS 847.00 TO FS 977.00 WERE REPLACE PER CRJ-900 AMM 53-00-49SDR VNAA202306230005Seat Track · corrodedCORROSION ON SIDE SEAT RAIL STGR 15 RH FROM FS 744.15 TO FS 761.85
SIDE SEAT RAIL STGR 15 RH FROM FS 744.15 TO FS 761.85 WAS REPLACED PER CRJ-900 AMM 53-00-49SDR VNAA202306230004Seat Track · corrodedCORROSION ON SIDE SEAT RAIL STGR 15 RH FROM FS 575.00 TO FS 661.00 + 16.00
SIDE SEAT RAIL STGR 15 RH FROM FS 575.00 TO FS 661.00 + 16.00 WAS REPLACED PER CRJ-900 AMM 53-00-49SDR VNAA202306230002Seat Track · corrodedCORROSION ON SIDE SEAT RAIL STGR 15 RH FROM FS 785.15 TO FS 847.00 + 8.40. SIDE SEAT RAIL STGR 15 RH FROM FS 785.15 TO FS 847.00 + 8.40. WAS REPLACED PER CRJ-900 AMM 53-00-49SDR VNAA202306230001Seat Track · corrodedCORROSION ON SIDE SEAT RAIL STGR 15 LH FROM FS 785.15 TO FS 847.00 + 8.40. SIDE SEAT RAIL STGR 15 LH FROM FS 785.15 TO FS 847.00 + 8.40. WAS REPLACED PER CRJ-900 AMM 53-00-49SDR VNAA202306230015Canister · crackedCRACK IN CANISTER WELDED NO.3, IN STA. WS 148 OF INTERNAL RH MAIN FUEL TANK. CANISTER WELDED NO.3, IN STA. WS 148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. --SDR VNAA202306230011Canister · crackedCRACK IN CANISTER WELDED NO.3, IN STA. WS 148 OF INTERNAL RH MAIN FUEL TANK. CANISTER WELDED NO.3, IN STA. WS 148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. --SDR VNAA202306220009Intercostal · chafedAFTER REMOVAL OF FWD LAVATORY, CHAFFING DAMAGE ON INTERCOSTAL SECTION BTW FS 364.00 TO FS 379.00 AT STGR 4 RH. INTERCOSTAL SECTION BTW FS 364.00 TO FS 379.00 AT STGR 4 RH WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND REPLACED PER EA 23-CSDR VNAA202306220008Angle · corrodedCORROSION ON ANGLE MOUNTING BTW FS319.70 TO FS349.00 ON GALLEY SERVICE DOOR AREA. ANGLE MOUNTING WAS EVALUATED PER CRJ-900 SRM 53-21-23-101-002-A02 AND CRJ-900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01SDR VNAA202306220007Stringer · corrodedCORROSION ON STGR 21RH BTW FS421.00 TO FS437.00. DUE TO EXCESSIVE CORROSION STRINGER 21RH BTW FS=394 TO FS=475 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACE PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
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