N522FE
Service difficulty reports · 338
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 = 'N522FE' 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 = 'N522FE' 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 FDEA200909273390Door Frame · chafedNR 2 ENGINE DOOR JAMB AREAS AT APPROX 5 O'CLOCK POSITION CHAFED. REPAIRED PER EA1-5450-133871 (MAJOR REPAIR).SDR FDEA200909213347Seat Track · damagedMAIN DECK CARGO COMPARTMENT, SEAT TRACK FOUND DAMAGED AT STA 1241, X = -47.5. REPAIRED IAW SRM 53-00-52, FIG201. REPAIR 1, REV 41 (MAJOR REPAIR).SDR FDEA200909173312Shear Tie · corrodedAFT CARGO COMPARTMENT - STA 1953 FROM LONGERON 50 LT TO LONGERON 49 RT FRAME SHEAR CLIP FOUND CORROSION. REPAIRED IAW SRM 51-31-01 REV 41.SDR FDEA200909153300Access Panel · crackedRT WING NR 3 SLAT AREA, STA XOS 464 L/E UPPER ACCESS CUT OUT FOR WING ANTI ICE TELESCOPIC DUCT CRACKED AT 02 CORNERS. REPAIR IAW SRM 57-40-01, FIG 201 REV 41.SDR FDEA200909153299Fitting · crackedLWR VERT STAB, RT SIDE FWD FLANGE OF UPPER REAR SPAR CAP BETWEEN FIRST AND SECOND LOWEST FASTENER FOUND APPROX 1 INCH CRACKED. RT LWR VERTICAL STABILIZER FWD FLANGE UPPER REAR SPAR CAP AREA REPAIRED IAW SRM 55-30-02, FIGURE 201, REPAIR 3, REVISION 41. FABRSDR 08FDEA01118Frame · dentedMAIN DECK LEFT FRAME AT BS 1721 S12L FOUND DENTED. REPAIRED AS PER SRM 53-30-00, FIG.1, VOL.1. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00, FIG.1, VOL.1. REPAIR CLASSIFIED AS MAJOR ASDR 08FDEA01117Frame · chafedMAIN DECK LT FRAME AT STATION 535 , BETWEEN L23-24L, 1 CHAFED MARK FOUND. REPAIRED AS PER DRAWING SRZ-53-503. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 08FDEA01116Frame · chafedMAIN DECK LEFT FRAME AT BS 535, BETWEEN L19-20L, 01 EACH CHAFED MARK FOUND NEAR 9G NET YOKE. REPAIRED AS PER DRAWING SRZ-53-503. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 08FDEA01115Frame · dentedMAIN DECK LEFT FRAME AT STATION 1661, STRINGER 12 LEFT FOUND DENTED. REPAIRED AS PER SRM 53-30-00, FIG.1, VOL.1. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00, FIG.1, VOL.1. REPAIR CLASSIFSDR 08FDEA01114Frame · dentedMAIN DECK RIGHT FRAME AT BS 1721 S12R FOUND DENTED. REPAIRED AS PER SRM 53-30-00, FIG.1, VOL.1. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00, FIG.1, VOL.1. REPAIR CLASSIFIED AS MAJOR AS PSDR 08FDEA01113Frame · dentedMAIN DECK RIGHT FRAME AT STATION 1681, STRINGER 12 RIGHT FOUND DENTED. REPAIRED AS PER SRM 53-30-00, FIG.1, VOL.1. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00, FIG.1, VOL.1. REPAIR CLASSSDR 08FDEA01087Skin · crackedLEFT WING LEADING EDGE ANTI-ICE TELESCOPIC DUCT DOOR CUT OUT CORNER SKIN CRACKED. REPAIRED AS PER SRM 57-10-00, FIGURE 43, VOLUME 1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 06FDEA03785Skin · damagedFOUND CTR CARGO DOOR JAMB CUT OUT LOWER AFT EXTERIOR SKIN EDGES FOUND DAMAGED. AREA TRIMMED OUT 0.50"X 6 AS PER SRM 53-50-00 FIG.16 VOL.I AND FOUND WITHIN LIMIT. NEW DOUBLERS FABRICATED AS PER SRM 53-50-00 VOL.I. HOLES PICKED UP AS PER SRM 51-31-01 VOL.IISDR 06FDEA03770Skin · chafedRT WING L/E NR 1 SLAT AFT SKIN FOUND CHAFING MARKS. REPAIRED AS PER SRM 57-10-00. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.SDR 06FDEA03701Skin · damagedFWD CARGO DOOR JAMB CUT OUT AFT LOWER OUTER SKIN EDGES FOUND WITH SLIGHT DAMAGE. CARGO DOOR JAMB CUT OUT AFT LOWER SKIN EDGES AREA TRIMMED OUT 3 LOCATIONS AS PER SRM 53-50-00 AND FOUND OUT OF LIMITS PER SRM 53-00-01 FIG.1A VOL.I FABRICATED NEW DOUBLER AS SDR 06FDEA03700Frame · crackedSTA 859 LONGERON 6 BETWEEN FRAME AND LONGERON ATTACHMENT HOLE 1, FOUND CRACK. REPAIR CARRIED OUT AS PER E.A.1-5330-103545. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR 06FDEA03377Hinge Bracket · corrodedRT WING O/B FLAP O/B HINGE (WING SIDE) ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA03376Hinge Bracket · corrodedRT WING O/B FLAP O/B HINGE (WING SIDE) ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA03375Hinge Bracket · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE) PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04 PG.621-622. BUSHING FABRICATED AND INSTALLED AS PER EA1-5750-104709 TEE REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-1SDR 06FDEA03356Skin · dentedFOUND UPPER FUSELAGE EXTERIOR, DENT MARK ON EXTERNAL SKIN STA 859 TO STA 875 BETWEEN LONGERON 10R AND 11R. REPAIR DOUBLERS AND 3 PCS. FINGER DOUBLERS INSTALLED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA03354Hinge · corrodedRT WING O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMITS AS PER CMM 57-44-08 PG.602-607 AND WITHIN DAC DWG AWRC0502 LIMITS. REPAIR CARRIED OUT AS PER CMM 57-44-08 AND REPAIR CLASSIFIED AS MINORSDR 06FDEA03353Hinge · corrodedRT WING I/B FLAP O/B HINGE (WING SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-07. REPAIR CARRIED OUT AS PER EA 1-5750-104703. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.SDR 06FDEA03352Hinge · corrodedRT WING I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG 442-444. ORIGINAL THK 1.1875" FINAL 1.257" MAX ALLOWABLE 1.220". BUSHING FABRICATED AND INSTALLED AS PESDR 06FDEA03351Hinge · corrodedLT WING I/B FLAP O/B HINGE (WING SIDE), PIVOT HOLE SPOT FACE FOUND CORRODED. LT FWD I/B FLAP O/B HINGE PIVOT HOLE SPOTFACE CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-07 PG.403-404. ORIGINAL THK I/B 0.461" O/B 0.435" REMAINING THK I/B 0.445" SDR 06FDEA03350Hinge · corrodedLEFT WING I/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 PG.442-444. ORIGINAL THK 1.187" FINAL 1.257" MAX ALLOWABLE 1.220". BUSHING FABRICATED AND INSTALLED AS PERSDR 06FDEA03324Hinge · corrodedLT WING O/B FLAP O/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. LT FWD O/B FLAP O/B HINGE BARREL NUT HOLE SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09 PG.402-408 AND FOUND WITHIN DAC DWG ARC0503 LIMITS. ORIGINAL THK I/B 0.408" REMSDR 06FDEA03323Hinge · corrodedLT WING O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 PG.402-408. ORIGINAL THK 1.2695" FINAL 1.314" MAX ALLOWABLE 1.190". BUSHING FABRICATED AND INSTALLED AS PERSDR 06FDEA03321Hinge · corrodedLT WING O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 PG.402-408. ORIGINAL THK 1.1885" FINAL 1.2155" MAX ALLOWABLE 1.190". BUSHING FABRICATED AND INSTALLED AS PERSDR 06FDEA03320Hinge · corrodedLT WING O/B FLAP I/B HINGE (WING SIDE), LWR ATTACHMENT SPOT FACE FOUND CORRODED. LT FWD O/B FLAP I/B HINGE LOWER MOUNT SPOTFACE CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 AND WITHIN DAC DWG ARC 0502 LIMITS. SHIMS FABRICATED AND INSTALLED SDR 06FDEA03234Doubler · crackedCTR LANDING GEAR LT BULKHEAD FWD CUTOUT DOUBLER SUSPECT CRACK. CTR LANDING GEAR L/H BULKHEAD FWD CUTOUT DOUBLER REMOVED AND REPLACED AS PER SRM 51-33-01 AND 51-35-01 VOL.II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA03181Skin · damagedEXISTING REPAIR FOUND ON RHW I/B FLAP ASSY UPPER SURFACE O/B SEGMENT.SDR 06FDEA03180Skin · damagedEXISTING REPAIR FOUND ON RHW I/B FLAP ASSY LWR SURFACE, 63" FROM O/B, 31" FROM T/E.SDR 06FDEA03179Skin · dentedLHW I/B FLAP ASSY O/B SEGMENT LWR SURFACE FOUND MULTIPLE DENTS. LT WING I/B FLAP ASSY O/B SEGMENT LOWER SURFACE MULTIPLE DENTS REPAIRED AS PER SRM 57-10-00 FIG.2 VOL. I. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100.SDR 06FDEA03160Skin · damagedRT HORIZ STAB REMOVABLE L/E NR 341DT FOUND WITH EXISTING EXTERIOR DOUBLER INSTALLED. RT HORIZONTAL STAB REMOVEABLE L/E #341DT EXISTING EXTERIOR DOUBLER REMOVED AS PER SRM 51-31-01 VOL.II. WEB AND RIBS REMOVED AND REWORKED AS PER SRM 55-20-00 VOL.I FIG.5SDR 06FDEA03158Block · damagedFOUND EXISTING REPAIR AT CENTER LANDING GEAR PILLOW BLOCK. CTR LANDING GEAR PILLOW BLOCK REMOVED AND REPLACED AS PER CMM 32-15-01 AND OPERATIONAL CHECK CARRIED OUT AS PER AMM 32-31-00 FOUND SATISFACTORY. CLASSIFIED MINOR REPAIR AS PER GMM 6-2-100.SDR 06FDEA03120Skin · damagedEXISTING DOUBLER REPAIR FOUND AT STA 1937 AND STA 1959 AFT LAV AIR EXHAUST PORT. REPAIR CARRIED OUT AS PER E.A.1-5330-103543 TITLE: SKINS AND PLATES- VACUUM WASTE PORTS DELETION AT BS 1937 AND BS 1959 RESPECTIVELY, BETWEEN LONGERON 39R AND 40R. REPAIR CSDR 06FDEA03119Spar Cap · corrodedHORIZONTAL STAB BARREL NUT BORE NR 01 RT FOUND CORROSION. REPAIRED AS PER E.A.1-5510-95657 ATTACHMENT 2 - A.D. 2003-22-08 - STABILIZER- HORIZONTAL STABILIZER - BARREL NUT BORE REWORK/REPAIR. CLASSIFIED MAJOR REPAIR PER GMM 6-2-100.SDR 06FDEA03118Seat Track · corrodedAFT CABIN CORROSION ON SEAT TRACK CROWN AT STA 1341 TO STA 1358 X=- 75. REMOVED CORROSION AND FOUND EXCEED LIMIT AS PER SRM 53-70-00 FIG.3 VOL.1 AND CARRIED OUT REPAIR BY FABRICATING NEW SEAT TRACK AND SPLICE AS PER SRM 53-70-00 FIG.1 VOL.I. REPAIR CLSDR 06FDEA03117Seat Track · corrodedMID-CABIN CORROSION ON SEAT TRACK BASE AND CROWN AT STA 745 TO STA 832 RBL 27.5". REMOVED CORROSION AND FOUND EXCEED LIMIT AS PER SRM 53-70-00 FIG.3 VOL.I AND CARRY OUT REPAIR BY FABRICATING NEW SEAT TRACK AND SPLICE AS PER SRM 53-70-00 FIG.1 VOL.I. SDR 06FDEA03116Seat Track · corrodedFOUND CABIN SEAT TRACK FLANGE, BASE AND CROWN FOUND CORRODED AT STA 808 TO STA 859 RBL 8.5". CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIG.3 VOL.I AND CARRIED OUT REPAIR BY FABRICATING NEW SEAT TRACK AND SPLICE AS PER SRM 53-70-00 FIGSDR 06FDEA02994Stringer · crackedCRACK FOUND AT THE END OF STRINGER 7 APPROX 1" OF LT WING TANK AT XORS 952 DURING HFEC INSPECTION. LHW TANK END OF STRINGER 7 CRACK AT XORS 952 REPAIRED AS PER SRM 57-20-00 FIG 10 OPT 1 VOL I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA02995Spar Cap · corrodedHORIZ STAB CONSTANT SECTION BARREL NUT NR 1 LT BORE CORROSION EXCEEDED THE LIMIT PER EO1-5510-7-5000 D1 PT1. HORIZONTAL STABILIZER CONSTANT SECTION BARREL NUT NR 1 LT BORE REPAIRED AS PER EA1-5510-95657 ATTACHMENT 1-A.D 2003-22-08- STABILIZERS, HORIZONTAL STASDR 06FDEA02993Seat Track · corrodedCORROSION FOUND ON SEAT TRACK FLANGE AND CROWN AT STA 859 TO STA 824 RBL 27.5. REMOVED CORROSION AND FOUND EXCEED LIMIT AS PER SRM 53-70-00 FIG 3 VOL I AND CARRIED OUT. REPAIR BY FABRICATING NEW SEAT TRACK AND SPLICE AS PER SRM 53-70-00 FIG VOL.I. CLASSIFISDR 06FDEA2995Structure · corrodedHORZ STAB CONSTANT SECTION BARREL NUT NR 1 R BORE CORROSION EXCEEDED THE LIMIT IAW EO 1-5510-7-5000 D1 P1.SDR 06FDEA2994Stringer · crackedSNRM N00786: CRACK FOUND AT THE END OF STRINGER 7 APPROX. 1 INCH OF LT WING TANK AT XORS 952 DURING HFEC INSPECTION.SDR 06FDEA2993Seat Track · corrodedCORROSION FOUND ON SEAT TRACK FLANGE AND CROWN AT STA 859 TO STA 824 RBL 27.5.SDR 06FDEA02970Seat Track · corrodedSEAT TRACK FLANGE AND CROWN FOUND CORRODED ON STA 919 TO STA 1019 LBL 8.5. REMOVED CORROSION AND FOUND EXCEED LIMIT AS PER SRM 53-70-00 FIG 3 VOL.I AND CARRIED OUT REPAIR BY FABRICATING NEW SEAT TRACK AND SPLICE AS PER SRM 53-70-00 FIG 1 VOL.I. CLASSIFIED MASDR 06FDEA02971Seat Track · corrodedSEAT TRACK BASE AND CROWN FOUND CORRODED ON STA 939 TO STA 1019 RBL 8.5. REMOVED CORROSION AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIG 3 VOL I AND CARRIED OUT REPAIR BY FABRICATING NEW SEAT TRACK AND SPLICE AS PER SRM 53-70-00 FIG 1 VOL.1. CLASSIFIED MASDR 06FDEA2970Seat Track · corrodedSEAT TRACK FLANGE AND CROWN FOUND CORRODED ON STA 919 TO STA 1019 LBL 8.5.SDR 06FDEA2971Seat Track · corrodedSEAT TRACK BASE AND CROWN FOUND CORRODED ON STA 939 TO STA 1019 RBL 8.5.
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