N608NN
Service difficulty reports · 35
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 = 'N608NN' 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 = 'N608NN' 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 VNAA202608200025Lug · corrodedAFTER RT AILERON BUSHINGS REMOVAL WAS FOUND CORROSION ON LUG BORE R2 AT CENTER FITTING RT AILERON. LUG BORE R2 AT CENTER FITTING, RH AILERON WAS REPAIRED PER REO 670-57-61-237 REV.-- "SDR VNAA202608200024Fitting · corrodedCORROSION ON CENTER FITTING OF LH AILERON L5 LUG BORE. REPAIRED PER REO 670-57-61-237SDR VNAA202608200023Fitting · corrodedCORRODED FLOOR FITTING IN AFT ACCESS 107 OUTSIDE (1EA) ON GALLEY 1. FLOOR FITTING IN AFT ACCESS 107 OUTSIDE (1EA) ON GALLEY WAS FABRICATED AND INSTALLED PER EA NO:2531-2026-0889 REV: - - SECTION III PERMANENT REPAIR.SDR VNAA202608200022Fitting · corrodedCORROSION FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1. FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-21."SDR VNAA202608200021Bearing · wornFREE PLAY ON BEARINGS OF RUDDER HINGES NR 2 AND 3 AT REAR SPAR OF VERTICAL STABILIZER. BEARINGS OF RUDDER HINGES NR 2 AND 3 AT REAR SPAR OF VERTICAL STABILIZER WERE REPLACED PER RIL #1213 REV. NC.SDR VNAA202608200020Floor Support · crackedCRACK ON FLOOR SUPPORT RBL 12, BTW BS 221.73 - 229, (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL 79.50) AT FWD FUSELAGE INTERNAL STRUCTURE. FLOOR SUPORT RBL 12.0 BTW BS 221.73 - 229 (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL 79.50) AT FWD FUSELAGE INTERNALSDR VNAA202608200019Canister · crackedCRACK ON CANISTER WELDED NO.3 IN STA WS=148 AT INTERNAL LH MAIN FUEL TANK. CRACK ON CANISTER WELDED NO.3 IN STA WS=148 AT INTERNAL LT MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV -.SDR VNAA202608200018Seat Track · corrodedWEAR RH SEAT RAIL FS 847.00 +16.00 TO 977.00 AT PAX CABIN. RT SEAT RAIL FS 847.00 +16.00 TO 977.00 AT PAX CABIN. WAS EVALUATED OUT OF LIMITS PER SRM 53-51-49-101-001-A02 AND REPLACED PER AMM 53-00-49.SDR VNAA202608200017Seat Track · corrodedCORROSION ON LT SIDE RAIL BTW FS=700 TO FS=379 AT CPAX. CORROSION ON LH SIDE RAIL BTW FS=700 TO FS=379 AT CPAX. WERE EVALUATED OUT OF LIMITS PER SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 REPLACED PER AMM 53-00-49.SDR VNAA202608200016Seat Track · corrodedCORROSION ON LT SIDE RAIL BTW FS=881 TO FS=785 AT CPAX. CORROSION ON LH SIDE RAIL BTW FS=881 TO FS=785 AT CPAX WAS EVALUATED OUT OF LIMITS PER SRM 53-41-49-101-001-A02 REPLACED PER AMM 53-00-49.SDR VNAA202608200015Seat Track · corrodedCORROSION ON RH SIDE RAIL BTW FS=744 TO FS=761 AT CPAX. CORROSION ON RH SIDE RAIL BTW FS=744 TO FS=761 AT CPAX. WERE EVALUATED OUT OF LIMITS PER SRM 53-41-49-101-001-A02 REPLACED PER AMM 53-00-49.SDR VNAA202608200014Seat Track · corrodedCORROSION ON RH SIDE RAIL BTW FS=421 TO 485 , FS=501 TO FS=570 , FS=610 TO FS=720 AT CPAX. RIGHT SIDE RAIL BTW FS=421 TO 485 , FS=501 TO FS=570 , FS=610 TO FS=720 AT CPAX WERE REPLACED PER CRJ900 AMM 53-00-49"SDR VNAA202608200013Seat Track · corrodedCORROSION ON SEAT RAIL LBL=26 BTW FS=486 TO FS=597 AT CPAX. CORROSION ON SEAT RAIL LBL=26 BTW FS=486 TO FS=597 AT CPAX. WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49.SDR VNAA202608200012Seat Track · corrodedCORROSION ON SEAT RAIL LBL=10 BTW FS=598 TO FS=669.40 AT CPAX. CORROSION ON SEAT RAIL LBL=10 BTW FS=598 TO FS=669.40 AT CPAX. WAS EVALUATED OUT OF LIMITS PER SRM 53-31-49-101-001-A02 REPLACED PER AMM 53-00-49.SDR VNAA202608200011Seat Track · corrodedCORROSION ON SEAT RAIL RBL9.00 BTW FS=486 TO FS=597, FS=598 TO FS=669.40 AT CPAX. CORROSION ON SEAT RAIL RBL9.00 BTW FS=486 TO FS=597, FS=598 TO FS=669.40 AT CPAX WAS EVALUATED OUT OF LIMITS PER SRM 53-31-49-101-001-A02 REPLACED PER AMM 53-00-49.SDR VNAA202608200010Seat Track · corrodedCORROSION ON SEAT RAIL LBL=26 BTW FS=364 TO FS=485 AT PAX CABIN. CORROSION ON SEAT RAIL LBL=26 BTW FS=364 TO FS=485 AT CPAX WAS EVALUATED OUT OF LIMITS PER SRM 53-21-49-101-001-A02. AND SRM 53-31-49-101-001-A02 REPLACED PER AMM 53-00-49.SDR VNAA202608200009Seat Track · corrodedCORROSION ON SEAT TRACK LBL 9 BTW BS 379 - 485 AT CPAX. CORROSION ON SEAT TRACK LBL 9 BTW BS 379 - 485 AT CPAX. WAS EVALUATED OUT OF LIMITS PER SRM 53-21-49-101-001-A02 AND SRM 53-31-49-101-001-A02 REPLACED IAW AMM 53-00-49.SDR VNAA202608200008Seat Track · corrodedCORROSION ON SEAT TRACK RBL9, BTW BS 349 - 485 AT CPAX. CORROSION ON SEAT TRACK RBL9.00 BTW FS=349 TO FS=485 AT CPAX. WAS EVALUATED OUT OF LIMITS IAW SRM 53-21-49-101-001-A02 AND SRM 53-31-49-101-001-A02 REPLACED IAW AMM 53-00-49.SDR VNAA202608200007Floor Support · crackedCRACK ON COCKPIT FLOOR LONGITUDINAL BEAM (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-2234 SDR VNAA202608200006Rib · crackedCRACK ON RIB LEADING EDGE SS 57.16 AT RH WING. CRACK ON RIB LEADING EDGE SS 57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV. -.SDR VNAA202608200005Rib · crackedCRACK ON RIB LEADING EDGE SS 57.16 AT LH WING. RIB LEADING EDGE SS 57.16 AT LH WING WAS REPAIRED PER REO 690-57-41-240 REV -.SDR VNAA202608200004Web · crackedCRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193. ELECTRICAL BAY FLOOR WEB RIGHT SIDE WAS REPAIRED PER SRM 53-11-43-201-001-A01SDR VNAA202608200003Skin · damagedSEVERAL NICKS, EROSION AND WEAR ON LOWER SKIN OF LH INBOARD FLAP FLS 15.5 TO FLS 75.5 WAS REPAIRED PER CRJ900 SRM 57-52-01-201-005-A01SDR VNAA202608200002Tail Cone · dentedDENT IN TAILCONE WAS REPAIRED IAW REO 690-53-84-062 REV -.SDR VNAA202608200001Door · crackedDOOR WASTE ASSEMBLY WAS REPAIRED PER EA NO: 2542-2026-0913 REV. -SDR VNAA202305220012Hinge · elongatedAFTER HINGE REMOVAL IN REF. NRC 00005, ELONGATED HOLES (3EAS) WAS FOUND. ELONGATED HOLES (3EAS) WERE REPAIRED PER REO 690-53-21-1626 REV.-ASDR VNAA202305220011Stringer · damagedDENTS 2 (EA´S) ON INBOARD FLAP, LOWER SKIN. AT WS 29.00 TO WS 68.00. 3.5 IN FROM T.E. DENTS (2 EAS) ON INBOARD FLAP, LOWER SKIN AT WS 29.00 TO WS 68.00 WERE EVALUATED AS FOLLOWS: DENT 1 (BTW FLS25.50 AND FLS30.00) WAS EVALUATED WITHIN LIMITS PER CRJ900 SRM 57SDR VNAA202305220010Skin · crackedSEVERAL NICKS ON LOWER SKIN OF AFT FUSELAGE BTW FS 977.00 TO 1051.3 AND STG 21 RH TO STR 27. NICKS ON LOWER SKIN OF AFT FUSELAGE BTW FS 977.00 TO 1051.3 AND STG 21 RH TO STR 27 WERE REPAIRED PER EA EA 23-C9-53-0562-IR ; EA 23-C9-53-0565-IR ;EA 23-C9-53-0566-ISDR VNAA202305220009Skin · crackedWEAR MARK ON EXTERNAL FUSELAGE SKING BTW FS897-FS913 AND BTW STGR 26L-27. WEAR ON EXTERNAL FUSELAGE SKIN BTW FS897 TO FS913 AND STGR 26L TO STGR 27 WAS REPAIRED PER EA 23-C9-53-0554 REV. IRSDR VNAA2023052202Seat Track · wornCORROSION WAS FOUND BETWEEN THE FOLLOWING STATIONS: FROM FS 785.15 TO FS 797.00 OF THE R/H SIDE SEAT RAIL. CORRECTIVE ACTION: R/H SIDE SEAT RAIL FROM FS 785.15 TO FS 797.00 WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND WAS REPLACED PER CSDR VNAA2023052201Seat Track · worn"DISC.- CORROSION ON SEAT RAIL RBL 9 BTW F.S.349.00 TO F.S. 359.00. CA- SEAT RAIL RBL 9 BTW F.S.349.00 TO F.S. 359.00 WAS EVALUATED OUT OF LIMITS PER CRJ/900 SRM 53-21-49-101-001-A01 AND WAS REPLACED PER CRJ/900 AMM 53-00-49-000-801 ( CONFIG A12 ) AND CRJ-900SDR VNAA202109301111Sensor · faultedCREW GOT A BRAKE TEMP OVER HEAT MESSAGE ON TAKE OFF IN CLT. THEY WERE BETWEEN 30-40KTS WHEN THEY REJECTED THEY TAKE OFF AND NOTIFIED ATC OF THE ISSUE. THEY EXITED THE RUNWAY AND PARKED AT A HARD STAND WHERE EMERGENCY VEHICLES WERE ON STANDBY MONITORING THE BRASDR VNAA202104271112Skin · gougedDURING OVERNIGHT MAINTENANCE, MX REPORTED A GOUGE ON THE AC SKIN GOUGE LOCATED AT FS581-FS597 STGR20L Ï¿½ STGR21L THE GOUGE DIMENSIONS ARE AS FOLLOWS .781"L X .375"W X .0085"D. THE AC SKIN (P/N SH690-33202-19) IS FABRICATED FROM 2024-T3 .150Ï¿½, CHEM MILLED DSDR VNAA202103121111Tire · failedCREW REPORTED RH OUTBOARD MLG TIRE BLOWN ON LANDING. REMOVED AND REPLACE RH OB WHEEL ASSEMBLYSDR VNAA2020040241102Gcu · malfunctionedDURING CRUISE TO MKE THE CAPT REPORTED A IDG 1, GEN 1, AC BUS 1 MAGENTA FAULT. HE DIVERTED TO DAY PER OUR REQUEST. MX HAD TO TROUBLESHOOT, RE-RACKED IDG 1 AND IDG 2 GENERATOR CONTROL UNIT IAW CRJ 900 AMM. OPS TEST GOOD AT THIS TIME.
Back to N608NN