N405YK
Service difficulty reports · 133
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 = 'N405YK' 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 = 'N405YK' 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 NACA2024070300008Window Frame · corrodedCORROSION AT RH WINDOWS PLUG PANE (R40), BETWEEN STA907 AND STA927 (L:1.2",W:0.5")(L:0.8",W:0.5")(0.8",W:0.4"). REPLACED PLUG IAW PEMCO SRM 51-10-02SDR NACA2024070300007Tip Cap · corrodedCORROSION(1.0" X 1.0" IN AREA) AT HORIZONTAL STABILIZER TIP TRAILING EDGE AT STAB BL 248.81 REPLACED HORIZONTAL STAB TIP PER AMM 55-10-11SDR NACA2024070300006Retainer · corrodedR/H AFT OVERWING EMERGENCY EXIT HATCH GOT CORROSION AROUND LOW PART OF SEAL RING. CLEANED REWORK AREA AND INSTALLED REPAIRED PARTS IAW SRM 51-70-11SDR NACA2024070300005Plug · corrodedCABIN WINDOW PLUG CORRODED #L40 STA 927+6" S-11L+4" CORROSION AREA 3.0"X1.5" COULD NOT KEEP WINDOW PLUG TO REQUIRED THICKNESS, REPLACED IAW PEMCO SRM 51-10-02SDR NACA2024070300004Skin · bulgedRH WING NO.4 SLAT OUTER SKIN BULGE AROUND FASTENER HOLE AT SLAT STA 100.77. CUT AND REMOVED DAMAGED PART OF SKIN, MADE DOUBLER AND FILLER, INSTALLED WITH SEALANT IAW EO 57-110 REV 1RSDR NACA2024070300003Angle · crackedAFT CARGO DOOR STRAP ANGLE CRACKED 1.0" ON AFT/LOWER SIDE AT BS847 S23R+7", REPLACED STRAP ANGLE IAW IPC 53-13-00-004 & SRM 51-40-02SDR NACA2024070300002Ring · corrodedR/H AFT OVERWING EMERGENCY EXIT HATCH GOT CORROSION AROUN LOW PART OF SEAL RING. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-70-11SDR NACA2024070300001Ring · corrodedL/H FWD OVERWING EMERGENCY EXIT HATCH GOT CORROSION AROUN LOW PART OF SEAL RING. REMOVED DAMAGED AREA AND CONDITIONED CHECK NORMAL. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-70-11SDR NACA2024070200002Panel · bulgedBULGE ON NO.1 ENG LH THRUST REVERSER UPPER BIFURCATION PANEL AT NAC STA 256. INSTALLED FILLER AND DOUBLER IAW SRM 54-30-02SDR NACA2024070200001Panel · bulgedBULGE ON NO.1 ENG RH THRUST REVERSER UPPER BIFURCATION PANEL AT NAC STA 256 . CUTOUT DAMAGED AREA MADE FILLER AND DOUBLER AND INSTALLED FILLER AND DOUBLER IAW SRM 54-30-02SDR NACA2024011700001Actuator · crackedSYSTEM A HYDRAULIC FAILURE. FOUND 1 EACH SPOILER ACTUATOR CRACKED/SPLIT OFF AT TOP OF ACTUATOR. REPLACED ACTUATOR IAW AMM 27-12-74 OPS AND LEAK CHECK GOOD. NO TIME INFO, PART UNKNOWN TO TRAX.SDR NACA2023052200001Unknown · unknownWHILE PUSHING BACK, THE AC CONTACTED THE STEEL STAND WITH THE RH AILERON. PERFORMED CONDITIONAL INSPECTION IAW AMM 05-51-54. DISCOVERED DAMAGE ON TRAILING EDGE OF RH AILERON 20 3/8" FROM OB EDGE, 2 3/16" WIDE, 3/8" DEEP. REMOVED AND REPLACED RH AILERON IAW AMMSDR 2023F00012Bulkhead · crackedAPPROX 2" CRACK ON INBD FLANGE OF VERTICAL CHORD RADIUS, LBL 5.7 WL 184 ON STA 178 BULKHEAD.SDR 2023F00003Skin · debondedFUSELAGE SKIN DISBONDED BETWEEN BS360 AND BS500C AT THE UPPER ROW OF FASTENERS OF THE S19R LAP SEAM.SDR 2022F00513Web · corrodedLEFT MLG SUPPORT BEAM LINK SUPPORT TO FUSELAGE FRAME INBD CHORD AND SKIN BELOW FUSE STUB FRAME BS 695 EXFOLIATED.SDR 2022F00521Door Frame · damagedELONGATED DAMAGED HOLES FOUND AT MULTIPLE LOCATIONS ON BS
348.2 DOOR FRAME, FORWARD SIDE PER BOEING SB 737-53A1240 AND
SB 737-53-0029 CRITERIA.SDR 2022F00520Skin · debondedSHIN DISBONDED BETWEEN BS 360 AND BS 500C, S-14L TO S-19-LSDR 2022F00501Floorbeam · corrodedCORROSION ON UPPER SURFACE OF UPPER FLANGE AT FLOORBEAM BS 294.5 LBL 11.10.SDR 2022F00497Frame · crackedREFERENCE AD2019-08-03 (G) (2) & SB 737-53A1361 FOR A CRACK FOUND ON FRAME INNER CHORD FORWARD RADIUS, BS 380 ABOVE S19R.SDR 2022F00498Frame · crackedREFERENCE AD2019-08-02(H) AND BOEING SB 737-53A1360 FOR A CRACK ON FRAME BS440 STRINGER CUT OUT ABOVE S16RSDR 2022F00499Skin · debondedSKIN DISBONDED BETWEEN BS 727 AND BS 727G AT UPPER ROR OF FASTENERS AT S-25R LAP SEAMSDR 2022F00519Frame · crackedCRACK FOUND AT THE FLANGE OF R/H SIDE FRAME AT STA 360, BETWEEN STRINGER 15 AND 16.SDR 2022F00518Frame · crackedREFERENCE AD2019-08-02(H) AND SB 737-53A1360 FOR A CRACK ON FRAME BS277 STRINGER CUT OUT ABOVE S16LSDR 2022F00511Floorbeam · crackedCRACK FOUND ON BS312 FLOOR BEAM LOWER CHORDSDR 2022F00508Frame · corrodedCORROSION @ BS7270 R/H B.W STRINGER 23-24 R/HSDR 2022F00506Channel · corrodedCORROSION @ FWD CARGO Z STRINGER BS500G LBL6SDR 2022F00505Frame · crackedCRACK ON FRAME INNER CHORD FORWARD RADIUS ABOVE S20L AND IN ANGLE ATTACHMENT AT S21L, BS 380.SDR 2022F00504Shear Tie · crackedCRACKED FRAME SHEAR TIE @ BS440 BETWEEN STRINGER 23L AND 24LSDR 2022F00503Shear Tie · crackedCRACKED FRAME SHEAR TIE @ BS480 BETWEEN STRINGER 23L AND 24LSDR NACA202212080500Skin · debondedFUSELAGE SKIN DISBOND BS360 AND BS500C AT UPPER ROR OF FASTENERS AT THE S-26L LAP SEAM.SDR 2022F00483Doubler · crackedREFERENCE AD 2015-06-07 & PEMCO SB 737-53-0036 FIG 5 FOR CRACK FOUND IN INTERNAL DOUBLER ON 1 HOLE LOCATED UPPER AFT CORNER OF AIR STAIR CUT OUTSDR 2022F00482Access Panel · corrodedCORROSION FOUND ON ANTI ICE DUCT ACCESS PANEL ON SLAT 3,SDR 2022F00481Plate · brokenFORWARD ENTRY DOOR LWR PLATE-SEAL BROKENSDR 2022F00480Shear Tie · crackedCRACK ON THE HOLE AT FRAME SHEAR TIE AT BS 380, S25R & S26RSDR 2022F00479Angle · crackedLH SIDE H-STAB I/B CLOSURE RIB ATTACH UPPER ANGLE CRACKED @
STAB BS67.54+5" OUTBOARDSDR 2022F00469Access Panel · corroded#2 PYLON ACCESS PANEL 5843 CORRODEDSDR 2022F00470Floor Support · corrodedCORROSION AT FLOOR CHANNEL BS 727E AT RBL 8.10SDR 2022F00471Floor Support · corrodedCORROSION AT FLOOR CHANNEL BS 727E AT LBL3SDR 2022F00458Channel · corroded"Z" CHANNEL CORRODED AT B.S 500G, LBL 22" AT FWD CARGO PITSDR NACA2022110900450Skin · corrodedLEFT WING UPPER SKIN AT WS368 AND FRONT SPAR HAS CORROSION.SDR 2022F00446Hinge Fitting · damagedR/H HOR. STAB #6 ELEVATOR HINGE ATTACH FITTING HAS ELONGATED HOLES.SDR 2022F00430Skin · debondedFUSELAGE SKIN DISBONDED BETWEEN BS 908-916, AT UPPER ROW OF FASTENERS OF THE S-10L LAP SEAMSDR 2022F00424Angle · crackedANGLE CRACKED BETWEEN BS1088-1104 IN APU BAY JUST OUTBOARD OF TORQUE BOX ON L/H SIDESDR 2022F00423Channel · corrodedCHANNEL CORRODED AT BS 1088 UPPER WEB L/H SIDE IN APU BAYSDR 2022FA0000648Channel · corrodedCHANNEL CORRODED AT BS1104 UPPER WEB L/H SIDE IN APU BAYSDR 2022FA0000647Mount · crackedCRACK FOUND IN SIDE ROLLER MOUNT @ STA 400 RBL63SDR 2022F00415Stringer · damagedS-20L STRINGER DAMAGED BETWEEN BS 440-460SDR 2022F00414Frame · corrodedCORROSION FOUND ON BOTTOM FLANGE OF FRAME BS727F BETWEEN S26R AND 27R IN AFT CARGO PITSDR 2022F00413Bracket · crackedAFT CARGO DOOR NET LOWER RETAINER BRACKETS CRACKED-CORRODEDSDR 2022FA0000645Stringer Clip · crackedCRACK ON STRINGER CLIP BS277 S15L
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