N607CZ
Service difficulty reports · 147
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 = 'N607CZ' 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 = 'N607CZ' 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 SWIA2026011300006Warning Message · false activationIN ICING CONDITION RECIEVED ANTI ICE WING FAIL CAUTION. RAN QRH AND MESSAGE PERSISTED. (FLIGHT 3792) ARRIVED AT ACFT WITH NO CURRENT FAULT. INTERROGATED CMC & FOUND NO ASSOCIATED FAULT CODE WITH ANTI-ICE WING FAIL MESSAGE. TROUBLESHOT ANTI-ICE FAIL CAUTION SDR SWI2026F00045Anti-Ice System · warning messageIN ICING CONDITION RECIEVED ANTI ICE WING FAIL CAUTION. RAN QRH AND MESSAGE PERSISTED. (FLIGHT 3792) OPENSDR SWIA20250707611Beam · corrodedFORWARD CARGO DOOR CUTOUT LOWER BEAM HAS CORROSION DAMAGE UNDER FORWARD MOST LATCH FITTING AND AT UPPER EDGE ABOVE THE 2 CENTER LATCH FITTINGS. (C-CHECK RO 07/03/2025)REMOVED AND REPLACED FORWARD CARGO DOOR CUTOUT LOWER BEAM, REF SRM 51-40-08. REPLACED WITH NSDR SWI2025F00858Doubler · corrodedRH COCKPIT FLOOR DOUBLER HAS CORROSION AROUND RIVETS INBOARD AND OUTBOARD OF THE CO-PILOT CONTROL YOKES BETWEEN FRAMES 8-9 AND AFT OF THE CO-PILOT INBOARD SEAT TRACK BETWEEN FR11-12. (C-CHECK RO 07/03/2025)PERFORMED RH COCKPIT FLOOR DOUBLER REPAIR. REF EMB SRSDR SWI2025F00857Control Column · corrodedLH COCKPIT FLOOR DOUBLER HAS CORROSION AROUND RIVETS INBOARD AND OUTBOARD OF THE PILOT CONTROL YOKE, BETWEEN FRAMES 8 AND 9. (C-CHECK RO 07/03/2025)PERFORMED COCKPIT DOUBLER REPAIR REF SRM 53-10-10/REPAIR 07P. SEE CONTINUATION CARD FOR WORK PERFORMED.SDR SWI2025F00856Floor Support · corrodedAFT CARGO FR 77 BETWEEN STGR 29L AND 29R L/H FLOOR SUPPORT CORRODED (C-CHECK RO 07/03/2025)REMOVED AND REPLACED FR 77 BETWEEN STGR 29L AND 29R L/H FLOOR SUPPORT. REF. SRM 51-40-08. SEE CONTINUE CARD FOR ADDITIONAL WORK PERFORMED.SDR SWIA20250707608Skin · corrodedREAR FUSELAGE FR 90 TO FR 91 STGR 29L TO STGR 29R SKIN CORRODED IN FRONT OF REAR SPLICESDR SWI2025F00864Floor Support · corrodedAFT CARGO FR 81 STGR 29R AND STGR 29L L/H FLOOR SUPPORT CORRODED (C-CHECK RO 07/03/2025)REMOVED AND REPLACED FR 81 STGR 29R AND STGR 29L L/H FLOOR SUPPORT. REF. SRM 51-40-08. SEE CONTINUE CARD FOR ADDITIONAL WORK PERFORMED.REPLACED WITH FACTORY REPLACEMENT PASDR SWI2025F00863Skin · crackedSUSPECTED CRACK LH WING LOWER SKIN AT WHEEL WELL CUTOUT RIB 3 (C-CHECK RO 07/03/2025)REMOVED CRACK ON LH WING LOWER SKIN BY CUTTING AWAY DAMAGED AREA. FABRICATED, DRILLED AND INSTALL FILLER/DOUBLER/TRIPLER REPAIR ON LOWER SKIN. REF: ETD2025-170-922726 REV: A SDR SWI2025F00862Shear Tie · corrodedFWD CARGO HAS 1EA CORRODED SHEAR CLIP AT FR 22, STGR 27R-26R. (C-CHECK RO 07/03/2025)REMOVED AND REPLACED SHEAR CLIP AT FR 22, STGR 27R-26R. REF. SRM 51-40-08. SEE CONTINUE CARD FOR ADDITIONAL WORK PERFORMED. SHEAR CLIP REPLACED WITH OEM PART, NO CHANGE IN WESDR SWI2025F00861Support · corrodedREAR FUSELAGE BETWEEN FR 86 AND FR 87 STGR 27R AND 29R HEATED DRAIN MAST FWD SUPPORT CORRODED (C-CHECK RO 07/03/2025)REMOVED AND REPLACED FR 86 AND FR 87 STGR 27R AND 29R HEATED DRAIN MAST FWD SUPPORT. SRM 51-40-08. SEE CONTINUE CARD FOR ADDITIONAL WORK PERFSDR SWI2025F00860Shear Tie · corrodedREAR FUSELAGE FR 87 STRG 28R TO STGR 29R SHEAR CLIP CORRODED (C-CHECK RO 07/03/2025)REMOVED AND REPLACE REAR FUSELAGE FR 87 STRG 28R TO STGR 29R SHEAR CLIP. REF SRM 51-40-08. (SEE CONTINUE CARD FOR ALL ACCOMPLISHED). REPLACED WITH OEM PART. NO CHANGE IN WIEGSDR SWI2025F00859Floor Support · corrodedAFT CARGO FR 82 STGR 29R AND STGR 29L R/H FLOOR SUPPORT CORRODED (C-CHECK RO 07/03/2025)REMOVED AND REPLACED FR 82 STGR 29R AND STGR 29L R/H FLOOR SUPPORT. REF. SRM 51-40-08. SEE CONTINUE CARD FOR ADDITIONAL WORK PERFORMED.REPAIRED WITH FACTORY REPLACEMENT PASDR SWIA20250707607Floor Support · corrodedAFT CARGO FR 82 STGR 29R AND STGR 29L L/H FLOOR SUPPORT CORRODED (C-CHECK RO 07/03/2025)REMOVED AND REPLACED FR 82 STGR 29R AND STGR 29L L/H FLOOR SUPPORT. REF. SRM 51-40-08. SEE CONTINUE CARD FOR ADDITIONAL WORK PERFORMED. REPAIRED WITH FACTORY REPLACEMENT PSDR SWI2025F00869Flap Track · wornRH WING FLAP TRACK 2A I/B HAS THICKNESS REDUCTION WEAR OF 1.2MM MAX ALONG AFT SIDE AND IS OUT OF LIMITS. ASSET# TC2-10390, DUE 7-3-25. (C-CHECK RO 07/03/2025)REMOVED AND REPLACED RH WING FLAP TRACK 2A I/B. REF AMM:57-54-25 T. WRENCH:TC2-7219 C/D:3-12-26SDR SWIA20250707605Flap Track · gougedLH WING FLAP TRACK 1A HAS MULTIPLE GOUGING IN RADIUS OF TRACK AND IS OUT OF LIMITS. (C-CHECK RO 07/03/2025)REMOVED AND REPLACED LH WING FLAP TRACK 1A. REF AMM:57-54-25 T. WRENCH:TC2-7219 C/D:3-12-26SDR SWI2025F00868Beam · corrodedFWD CARGO DOOR CUTOUT, LOWER HORIZONTAL BEAM HAS 2EA SPOTS OF CORROSION FROM FR 24-27 AS MARKED. (C-CHECK RO 07/03/2025)REMOVED AND REPLACED FORWARD CARGO DOOR CUTOUT LOWER BEAM FORWARD AND AFT FINGER DOUBLERS, REF SRM 51-40-08. REPLACED WITH NEW OEM PART. NOSDR SWI2025F00867Seat Track · corrodedRH SEAT TRACK CORRODED 5.0€? AFT OF FRAME 13 AND RBL +11.75€?. (C-CHECK RO 07/03/2025)CUT OUT DADMAGED SECTION OF R/H I/B SEAT TRACK UPPER CAP BETWEEN FR13-14, INSTALLED DOUBLER, REINFORCEMENT ANGLE, AND FLOOR REINFORCEMENT BRACKET ON R/H I/B SEAT TRACK BETSDR SWI2025F00866Floorbeam · corrodedRH AFT WET AREA BEAM HAS CORROSION AROUND NUTPLATE HOLE CLOSET TO FRAME 87 (C-CHECK RO 07/03/2025)REMOVED AND REPLACED RH AFT WET AREA BEAM BETWEEN FR87-89 REF. EMB SRM 51-40-08. REPLACED WITH OEM PARTS, DOES NOT AFFECT WEGHT AND BALANCE.SDR SWI2025F00865Shear Tie · corrodedFWD CARGO HAS 1EA CORRODED SHEAR CLIP AT FR 21, STGR 27R-26R. (C-CHECK RO 07/03/2025)REMOVED AND REPLACED FWD CARGO HAS 1 SHEAR CLIP AT FR 21, STGR 27R-26R. REF SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED. SEE CONTINUED SDR SWIA20250707604Shear Tie · corrodedFWD CARGO HAS 1EA CORRODED SHEAR CLIP AT FR 22, STGR 28R-27R. (C-CHECK RO 07/03/2025)REMOVED AND REPLACED FWD CARGO HAS SHEAR CLIP AT FR 22, STGR 28R-27R. REF SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED. SEE CONTINUATIOSDR SWIA202507070602Skin · crackedR/H WING LOWER SKIN BETWEEN RIB 5 AND RIB 6 AT SPAT 2 HAS A SUSPECTED CRACK (C-CHECK RO 07/03/2025)REPAIRED R/H WING LOWER SKIN BETWEEN RIB 5-6 AT SPAR 2 BY APPLYING REPAIR EXTERNAL DOUBLER.SEE CONTINUATION CARD FOR WORK PERFORMED. REF ETD2025-170-922499SDR SWIA202266438None · scoredL/H HORIZONTAL STABILIZER HINGE LUG BORE IS SCORED. (C-CHECK RO 9/02/2022) REPAIRED LEFT HAND HORIZONTAL HINGE LUG BORE. REF SRM 55-10-02/REPAIR 01P. SEE CP 25221830 FOR FABRICATION AND INSALLATION OF BUSHINGS.SDR SWIA202266437None · scoredL/H AFT HORIZONTAL STABILIZER HINGE FITTING IS SCORED ON THE INBOARD SIDE AS MARKED. (C-CHECK RO 9/02/2022) REPAIRED L/F AFT HORIZONTAL STABILIZER HINGE FITTING ON THE INBOARD SIDE. RED ETD2022-170-025386. SEE CONTINUATION CARD FOR WORK PERFORMED. NO SDR SWIA202266436None · gougedLH OB LATERAL SEAT TRACK HAS GOUGES/CORRODED AS MARKED BETWEEN FRAMES 34-60 (C-CHECK RO 9/02/2022) / REMOVED AND REPLACED LH OB SEAT TRACK AT FR 34-60. REF E MB SRM 51-40-08. OEM PART REPLACEMENT, NO CHANGE IN WEIGHT.SDR SWIA202266435None · corrodedCORROSION ON AND AROUND DOME NUTS FOR FWD WI-FI ANTENNA BETWEEN FRAMES 21 AND 22 AND STRINGERS 27R AND 28R INSIDE FORWARD CARGO (C-CHECK RO 9/02/2022) REMOVED AND REPLACED DOUBLER AND 2 EA STIFFENERS BETWEEN FRAMES 21 AND 22 AND STRINGERS 27R AND 28R INSDR SWIA202266434None · damagedRH IB SEAT TRACK SECTION FROM FR 23-34 IS DAMAGED. SEE THE CONTINUATION IN CAMP FOR LOCATIONS. (C-CHECK RO 9/02/2022) REMOVED AND REPLACED RH IB SEAT TRACK SECTION FROM FR 23-34 REF EMB SRM 51-40-08. REPLACD WITH OEM PART NO CHANGE TO WEIGHT AND BALANCESDR SWIA202266433None · damagedRH OB SEAT TRACK SECTION FROM FR 23-34 IS DAMAGED. SEE THE CONTINUATION IN CAMP FOR LOCATIONS. (C-CHECK RO 9/02/2022) REMOVED AND REPLACED RH OB SEAT TRACK AT FR 23-34. REF EMB SRM 51-40-08SDR SWIA202266432None · damagedRH OB SEAT TRACK SECTION FROM FR 21-23 IS DAMAGED. SEE THE CONTINUATION IN CAMP FOR LOCATIONS. (C-CHECK RO 9/02/2022) REMOVED AND REPLACED RH OB SEAT TRACK SECTION FROM FR 21-23 REF EMB SRM 51-40-08SDR SWIA202266431None · damagedLH OB SEAT TRACK SECTION FROM FR 19-21 IS DAMAGED. SEE THE CONTINUATION IN CAMP FOR LOCATIONS. (C-CHECK RO 9/02/2022) REMOVED AND REPLACED LH OB SEAT TRACK SECTION FROM FR 19-21 REF SRM 51-40-08. RESSTORED SURFACE PROTECTION REF SRM 51-23-06. WORK DONE SDR SWIA202266430None · gougedFWD AVIONICS HATCH SKIN IS GOUGED WITH A DENT (C-CHECK RO 9/02/2022) REPAIRED FWD AVIONICS HATCH REF ETD 2022-170-025288. REINSPECTION REQUIREMENTS- EXTERNAL AND INTERNAL, DET, THRESHOLD OF 7500 FC, INTERVAL OF 7500 FC. THIS IS AN ADDITIONAL AND SPECIFSDR SWIA202266429None · dentedDENT MEASURING 1.625" W AND .025" D LOCATED 3.5" ABOVE STGR 18L AND .5" AFT OF FR 10. EVALUATE AND REPAIR OR ELIMINATE EVIDENCE USING STANDARD PRACTICES. SEE ADM# N607CZ-6931 (C-CHECK RO 9/02/2022) PERFROMED A PERMANENT REPAIR BY REMOVING AND REPLACING SDR C77A2020011300001Warning Message · illuminatedFLAP FAIL MSG ON CLIMBOUT RETRACTION. FLAPS AT 0.SDR C77A2019112600001Battery · inoperativeFO FLASHLIGHT INOP, AND IS MISSING INSP PLACARD. REPLACED FO FLASHLIGHT PLACARD IAW GMM 12-1-6. REPLACED FO FLASHLIGHT BATTERY IAW 33-51-01 A/C OK FOR SERVICESDR C77A2020031300036Door Sill · corrodedE175-5300-237-THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING FORWARD CABIN FLOOR STRUCTURE: P/N 170-05663-003 RH FLOOR SILL, P/N 170-04071-001 FR15 FLOOR SUPPORT, P/N 170-SDR C77A2020031200035Shear Tie · corrodedDURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED ON SEVERAL SHEAR CLIPS IN THE LOWER AFT CARGO COMPARTMENT. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF THE CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING ASDR C77A2020031200034Shear Tie · corrodedDURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED ON SEVERAL SHEAR CLIPS IN THE LOWER AFT CARGO COMPARTMENT. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF THE CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING ASDR C77A2020031200033Shear Tie · corrodedDURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED ON SEVERAL SHEAR CLIPS IN THE LOWER AFT CARGO COMPARTMENT. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF THE CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING ASDR C77A2020031200032Shear Tie · corrodedDURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED ON SEVERAL SHEAR CLIPS IN THE LOWER AFT CARGO COMPARTMENT. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF THE CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING ASDR C77A2020031200031Shear Tie · corrodedDURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED ON SEVERAL SHEAR CLIPS IN THE LOWER AFT CARGO COMPARTMENT. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF THE CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING ASDR C77A2019050800002Beam · corrodedDURING HEAVY MAINTENANCE CORROSION WAS FOUND ON BEAM (P/N 170-66280-001) AT S-28R BETWEEN FRAME 80 (X = 21192) AND FRAME 81 (X = 21617). THE CORROSION WAS BLENDED OUT RESULTING IN TWO BLEND OUTS. THE FIRST BLEND OUT IS 2.9" L X 1.0" W, X .05" D AND THE SECONSDR C77A2019050800001Frame · corrodedDURING HEAVY MAINTENANCE CORROSION WAS FOUND ON FRAME 80 (P/N 170-65422-003) AT S-28R. THE CORROSION WAS BLENDED OUT WITH A MAXIMUM DEPTH OF .066" FROM A NOMINAL THICKNESS OF .118" WHICH IS OUT OF LIMITS. THE CORRODED FRAME WAS REMOVED AND REPLACED WITH A NESDR C77A2019050600004Crossbeam · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE TO THE FR17 CROSSBEAM UPPER FLANGE DISCOVERED DURING BASIC CHECK. THE DAMAGE WAS REMOVED BY BLEND OUT WITH THE FOLLOWING APPROXIMATE DIMENSIONS: 0.750 INCH XSDR C77A2019050600002Fitting · corrodedCORROSION HAS BEEN FOUND ON THE AFT CARGO DOORWAY– FWD FITTING P/N 170-85492-403, CENTER FITTING P/N 170-85251-401, AND/OR AFT FITTING P/N 170-85493-403 ON SEVERAL AIRCRAFT DURING BASIC CHECK. SINCE CLASSIFIES THESE FITTINGS AS PSES, HAS CLASSIFIED REPLACEMENTSDR C77A2019050600001Crossbeam · corrodedEO E175-53MR-185 REV IR WAS RELEASED TO REPAIR CORROSION DAMAGE TO THE UPPER FLANGE OF THE FR17 CROSSBEAM BY CUTOUT AND DOUBLER INSTALLATION IN ACCORDANCE WITH ETD2015-170-050159. DURING A SUBSEQUENT INSPECTION OF THE AREA DURING THE B6 BASIC CHECK, NEW CORROSSDR C77A2020031400037Seat Track · corrodedDURING BASIC CHECK AT EAMS, CORROSION WAS DISCOVERED AT A PREVIOUS REPAIR DOUBLER ON FORWARD FUSELAGE LH IB SEAT TRACK BEAM (P/N 170-03264-001) AT FR17 IN THE FORWARD WET AREA FLOOR STRUCTURE. REFERENCE ETD2019-170-055163 FIGURE 1 FOR THE DAMAGE LOCATION AND DSDR C77A2019050400001Seat Track · corrodedCORROSION HAS BEEN FOUND ON THE CABIN RT SEAT TRACK P/N 170-02056-008 DURING BASIC CHECK. SINCE CLASSIFIES THIS SEAT TRACK AS PSE, HAS CLASSIFIED REPLACEMENT OF THIS TRACK AS A MAJOR REPAIR. IN LIEU OF CONTINUING TO WRITE INDIVIDUAL EO’S FOR EACH AIRCRAFT. THISDR C77A2019042900001Seat Track · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE ON CONDITION REPAIR OF CORROSION OR OTHER DAMAGE TO THE FORWARD FUSELAGE LT LATERAL SEAT TRACK P/N 170-20955-001. THE PERMANENT REPAIR WILL BE ACCOMPLISHED BY DIRECT REPLACEMENT OF THE AFFECTED SDR C77A2019050300002Crossbeam · corrodedEO E175-53MR-184 REV 1 WAS RELEASED TO REPAIR CORROSION DAMAGE TO THE UPPER FLANGE OF THE FR14 CROSSBEAM BY CUTOUT AND DOUBLER INSTALLATION IN ACCORDANCE WITH ETD2015-170-048470B. DURING A SUBSEQUENT INSPECTION OF THE AREA DURING THE B6 BASIC CHECK, NEW CORROSSDR C77A2019050300001Crossbeam · corrodedDURING INSPECTION DURING THE B6 BASIC CHECK, CORROSION DAMAGE WAS FOUND AT THE UPPER FLANGE OF THE FR11 CROSSBEAM. REFERENCE ETD2019-170-055897B FIGURE 1 FOR DETAILS. REQUESTED AND RECEIVED ETD2019-170-055897B TO REPAIR THE DAMAGE. THIS EO IS BEING ISSUED TO P
Back to N607CZ