N286SC, cancelled Jan 3, 2018
Service difficulty reports · 198
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 = 'N286SC' AND deregistration_id = 'N286SC-2018-01-03' 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 = 'N286SC' AND deregistration_id = 'N286SC-2018-01-03' 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 C8GA2011000001Control Cable · out of adjustDURING APPROACH, WITH THE GEAR LEVER PLACED IN THE DOWN POSITION, THE GREEN LANDING GEAR INDICATION LIGHTS WERE ILLUMINATED AS WELL AS THE RED INDICATION LIGHTS ON THE FWD PANEL AND THE ENGINEERS PANEL. THE LANDING GEAR WAS CYCLED WITH THE SAME INDICATIONS, A SDR FOTR20006NR2095Skin · dented(FOTR) DENT ON LT FUSELAGE SKIN BS 1319 STR 9L. REPAIRED ON FASI WO 20006. N/R 02095- R & R PREVIOUS REPAIR TO LT FUSELAGE SKIN AT STA 1319 STR 9L IAW SRM 53-30-3 FIG 1, REV 102. MATERIAL USED: 2024-T3, 0.063", DIM: 9.250" X 8.750".SDR FOTR20006NR2059Skin · debondedRT WING INBD AILERON TAB LOWER SURFACE DISBONDED 22 INCHES FROM OTBD END. REPAIRED ON FASI WO 20006, N/R 02059. REPAIRED RT WING INBD AILERON TAB AT WBL 280 BY HOT BONDING REPAIR IAW B727 SRM 51-40-20, REV 102. MATERIAL USED: FILLER- 2024-T3, 0.010, DIM: 4.SDR FOTR20006NR2054Structure · crackedRT WING INBD MID FLAP LOWER T/E CHORD CRACKED WBL 100. REPAIRED ON FASI WO 20006, N/R 02054. REMOVED AND REPLACED RT WING INBD MID-FLAP LOWER T/E CHORD SECTION AT WS 100.0 IAW B727 SRM 51-30-5 AND 57-50-2, FIG 5, REV 102. MATERIAL USED: BAC1503-10046 7075-TSDR FOTR20006NR2033Skin · debondedRT WING NR 9 SPOILER LOWER SURFACE HAS DISBONDED DOUBLER JUST AFT OF ACTUATOR ATTACH FITTING. REPAIRED ON FASI WO 20006, N/R 02033. REPAIRED RT WING NR 9 SPOILER LOWER SURFACE AT WBL 113 BY HOT BY 8.0.SDR FOTR20006NR2031Skin · debondedLT INBD AFT FLAP LOWER SURFACE HAS DISBONDED AREA AT WBL 135. REPAIRED ON ASI WO 20006, N/R 02031. INSTALLED HOT BONDED REPAIR TO LEFT INBD AFT FLAP LOWER SURFACE AT WBL 135 IAW B727 SRM 51-40-20, PARA 20 AND 51-40-23, REV 102. MATERIAL USED: CORE; 5052-4.4-SDR FOTR20006NR2028Skin · puncturedRT ELEVATOR LOWER SKIN WORN THRU AT ELEV STA 78 NEAR CENTER OF ELEVATOR. REPAIRED ON FASI WO 20006, N/R 02028. INSTALLED REPAIR DOUBLER ON RIGHT ELEVATOR LOWER SURFACE AT ELEV STA 78, IAW B727 SRM 55-20-3 FIG 4, REV 102. MATERIAL USED: 2024-T3, DIM; 4.325 BSDR FOTR20006NR2027Frame · damagedUPPER CABIN FRAME DAMAGED AT BS 380 STR 5L. REPAIRED ON FASI WO 20006. N/R 02027. INSTALLED REPAIR ANGLE TO FUSELAGE FRAME AT BS 380, STR 5L IAW B727 SRM 53-10-4 FIG 1, REV 102. MATERIAL USED; 7075-O, HEAT TREATED TO T-6 CONDITION. DIM.; 11 BY 1 BY 0.063.SDR FOTR20006NR2023Skin · debondedRT OTBD AILERON TAB, UPPER SURFACE INBD END HAS AREA OF DISBOND. REPAIRED ON FASI WO 20006. N/R 02023, INSTALLED HOT BONDED REPAIR TO RT OTBD AILERON TAB UPPER SURFACE AT INBD END IAW SRM 51-40-20 PARA 20, REV 102. MATERIAL USED: CORE; 5052-44-3/16 DIM. 13" SDR FOTR20006NR2021Skin · puncturedRT WING OTBD FORE FLAP HAS SEVERAL GOUGES. REPAIRED ON FASI W/0 NR 20006, N/R 02021" INSTALLED REPAIR DOUBLER TO RT WING OTBD FORE FLAP AT WS 465 IAW SRM 57-50-2 FIG 4 AND 57-50-4 FIG 1, REV 102. MATERIAL USED; 2024-T3, DIM.; 3.5" X 3.75" X 0.063".SDR FOTR20006NR2020Stringer Clip · puncturedFRAME TO STR. BRACKET HAS HOLE IN RADIUS AT STA. 672 STR. 13L. REPAIRED ON FASI W/O NR 20006, N/R 02020- R & R SUPPORT ANGLE AT STA 672 STR 13L IAW SRM 51-30-2, REV 102 AND DWG AE4899 DATED 6/29/92.SDR FOTR20006NR2016Skin · gougedLT WING NR 4 SLAT OTBD END GOUGED. REPAIRED ON W/O NR 20006, N/R 02016- R & R LT WING NR4 SLAT OTBD RIB IAW SRM 51-30-2, REV 102 WITH PN 65-17286-13.SDR FOTR20006NR2013Wedge · delaminatedRT AILERON OTBD T/E WEDGE HAS AREA OF DISBOND ON UPPER INBD END. REPAIRED ON FASI W/O NR 20006, N/R 02013. INSTALLED HOT BONDED REPAIR TO RIGHT WING OTBD AILERON TRAILING EDGE WEDGE UPPER OTBD END IAW B727 SRM 51-40-20 PARA. 8 AND PARA 20 REV 102. MATERIAL SDR FOTR20006NR2012Skin · delaminatedRT OTBD AILERON T/E WEDGE HAS AREA OF DISBOND ON UPPER SURFACE. REPAIRED ON FASI W/O NR 20006, NR 02012 - INSTALLED HOT BONDED REPAIR TO RT WING OTBD AILERON T/E WEDGE UPPER SURFACE IAW SRM 51-40-20 PARA 8 AND PARA 20 REV 102. MATERIAL USED: 2024 T3, 0.012". SDR FOTR20006NR2011Skin · delaminatedRT WING OTBD AFT FLAP IS DELAMINATED AT STA WBL 338. REPAIRED ON FASI W/O NR 20006, N/R 2011 INSTALLED HOT BONDED REPAIR TO RT WING OTBD AFT FLAP AT WBL 228 IAW SRM 51-40-20 PARA 7 AND PARA 20 REV 102. MATERIAL USED: 7075-T7, 0.012". DIM ; FILLER; 1" X 4", DOUSDR FOTR20006NR1992Skin · dentedRT WING INBD FLAP LOWER SURFACE IS DENTED AT WS 135. REPAIRED ON FASI W/O 20006, N/R 01992, INSTALLED HOT BONDED REPAIR TO LOWER SURFACE OF RT INBD AFT FLAP AT WS 135 IAW SRM 51-40-20 PARA 7, PARA 8 AND PARA 20, REV 102. MATERIAL USED: 7075-T6, 0.016". DIM; FSDR FOTR20006NR1984Stringer · corrodedAFT AIRSTAIR AT BS 1323 CENTER STRINGER AT LOWER END CORRODED. REPAIRED ON FSAI W/O NR 20006, N/R 01984. REPAIRED STRINGER AT AFT STAIRS STA 1323 IAW B727 SRM 53-10-3 FIG 1 AND 52-10-1 FIG 3, REV 102. MATERIAL USED: STRINGER; BAC1498-138 7075-T62, DIM: 12.0SDR FOTR20006NR1976Web · crackedLT SIDE OF FUSELAGE INTERIOR WEB CRACKED JUST ABOVE NR 2 ENG "S" DUCT AT BS 1303. REPAIRED ON FASI W/O NR 20006, N/R 01976. INSTALLED REPAIR DOUBLER TO CRACKED WEB ABOVE NR 2 ENGINE S DUCT AT BS 1303 IAW B727 SRM 51-40-2, FIG 1, REV 102. MATERIAL USED: DOUBSDR FOTR20006NR1972Doubler · crackedL1 DOOR UPPER HINGE SKIN DOUBLER CRACKED LOWER CORNER. REPAIRED ON FASI W/O NR 20006, N/R 01972. REPLACED EXTERNAL DOUBLER AT LEFT FORWARD ENTRY DOOR UPPER HINGE CUTOUT AT BS 303 IAW S/B 727-53A0198 REV. 3 DUE TO CRACK. MATERIAL USED: 3011/2 HD STAINLESS STSDR FOTR20006NR1971Shear Tie · crackedSTA 600 STR 16L SHEAR TIE CRACKED. REPAIRED ON FASI W/O NR 20006, NR 01971, REPLACED CRACKED SHEAR TIE AND DOUBLER AT BS 680, STR 16L IAW B727 SRM 53-20-2 FIG 3 AND 53-10-4 FIG 11, REV 102. MATERIAL USED: 7075-O, HEAT TREATED TO T6 CONDITION. DIM.; DOUBLER; SDR FOTR20006NR1969Stringer Clip · crackedSTA 700 STR. 16L STR CLIP CRACKED. REPAIRED ON FASI W/O NR 20006,NR 01969. REPLACED CRACKED STRINGER CLIPS AT BS 700 STR 16L IAW DRAWING NR 66-11809 REV B AND B727 SRM 51-30-2 REV 102. MATERIAL USED; 7075-T6, DIM.; 4.6 BY 3.1 BY 0.040.SDR FOTR20006NR1965Frame · dentedSTA 720A STR 16R FRAME IS DENTED. REPAIRED ON FASI W/O NR 20006, NR 01965. INSTALLED REPAIR DOUBLER TO FRAME AT BS 720A, STR 16R, DUE TO DENT, IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1.SDR FOTR20006NR1962Frame · gougedLEFT UPPER CABIN FRAME GOUGED AT BS 670 BETWEEN STR 5L AND 6L. REPAIRED ON FASI W/O 20006, N/R 01962. REMOVED AND REPLACED FUSELAGE FRAME AT BS 670 BETWEEN STR 4L TO STR 14L WITH P/N AE2330-11 IAW AEI DRAWING AE4899 CHANGE H DATED 06/29/1992, DUE TO GOUGING .SDR FOTR20006NR1862Frame · bentSTA 420 FRAME BENT AT STR 7R. REPAIRED ON FASI W/O NR 20006, NR 01862. INSTALLED REPAIR DOUBLER TO FRAME AT BS 420, STR 7R, DUE TO DENT, IAW B727 SRM 53-10-2 FIG 3 AND 53-10-4 FIG 2, REV 102. MATERIAL USED: DOUBLER 7075-O, HEAT TREATED TO T6 CONDITION. DIMSDR FOTR20006NR1850Structure · puncturedRT INBD AFT FLAP LOWER SURFACE IS PUNCTURED NEAR INBD END. REPAIRED ON FASI W/O NR 20006, NR 01850. INSTALLED HOT BONDED REPAIR TO RIGHT INBD AFT FLAP LOWER SURFACE AT WBL 75 IAW B727 SRM 51-40-20 PARA 20, REV 102. MATERIAL USED: 2024-T3, 0.012 THICK, 3 DIASDR FOTR20006NR5780Web · corrodedLT MOP SILL CORRODED UNDERSIDE STA 1130 BELOW FLOOR. REPAIRED ON FASI WO 20006, N/R 05780. REMOVED AND REPLACED WEB BETWEEN STA 1110 TO 1130 IAW B727 SRM 53-10-2 FIG 5, 51-30-5, 51-30-6 AND 51-10-1, REV 102. MATERIAL USED: 7075-T6, 0.063, DIM: 18.620 BY 7.0SDR FOTR20006NR5718Floorbeam · crackedMAIN CABIN OVERWING FLOORBEAM T-CHORD CRACKED AT BS 760 RBL.45.5. REPAIRED ON FASI W/O NR 20006, N/R 05718. REMOVED AND REPLACED MAIN CABIN FLOORBEAM T-CHORD AT STA 760.9 IAW BOEING DWG 65-16279 REV A. MATERIAL USED: BAC1506-1108, DIM: 110.0 L.SDR FOTR20006NR5753Angle · corrodedSTA 1166 AT STR 17 WEB AREA CORRODED. REPAIRED ON FASI W/O NR 20006, N/R 005753. REMOVED AND REPLACED UPPER ANGLE AND LOWER CHANNEL SUPPORT AT STA 1166, STR 17R IAW B727 SRM 53-10-1-FIG. 1, 51-20-1 AND 53-10-2, REV 102. MATERIAL USED: CHANNEL; 7075-T6, 0.08SDR FOTR20006NR 5760Floorbeam · damagedSTA 1070 FLOORBEAM DOUBLE DRILLED HOLE RBL.50. REPAIRED ON FASI W/O NR 20006, N/R 04858. REMOVED AND REPLACED UPPER SUPPORT FITTING AT RT LOWER TORQUE BOX WEB AT VENTRAL STAIRS STA 1263 WITH P/N 65C27137-1 IAW B727 SRM 53-10-2, REV 102.SDR FOTR20006NR1842Frame · dentedMAIN CABIN FRAME BS 280 FLANGE IS DENTED AT STR 6R. REPAIRED ON FASI W/ONR 20006, NR 01842. INTALLED REPAIR DOUBLER TO FRAME AT BS 380, STR 6R, DUE TO DENT, IAW B727 SRM 53-10-2 FIG 3 AND 53-10-4 FIG 2, REV 102. MATERIAL USED: DOUBLER 7075-O, HEAT TREATED TSDR FOTR20006NR1841Frame · dentedMAIN CABIN FRAME BS.400 FLANGE IS DENTED AT STR 6R. REPAIRED ON FASI W/O 20006,NR 01841 INSTALLED REPAIR DOUBLER TO FRAME AT BS 400, STR 6R, DUE TO DENT, IAW SRM 53-10-2 FIG 3 AND 53-10-4 FIG 2, REV 102. MATERIAL USED: DOUBLER 7075-O, HEAT TREATED TO T6 CONDISDR FOTR20006NR1798Intercostal · crackedAFT PIT HAS A CRACK AT INTERCOSTAL STR 23L BETWEEN BS 950D TO 950E. REPAIRED ON FASI W/O NR20006, NR01798. R & R CRACKED INTERCOSTAL BETWEEN BS 950D TO BS 950E, STR 23L IAW SRM 51-20-1 FIG 1 REV 102 AND DWG NR 65-56125. MATERIAL USED: 7075-T6, DIM.; 19.5 X 4 SDR FOTR20006NR1795Skin · crackedLT OTBD FOREFLAP WBL 348 CRACK ON SKIN FWD OF FITTING. REPAIRED ON FASI W/O NR 20006,NR 01795 - INSTALLED REPAIR DOUBLER TO LT OTBD FOREFLAP AT WS 348 IAW SRM 57-50-4 FIG 7 REV 102. MATERIAL USED: 2024-T3, DIM.; 6 X 4 X 0.063.SDR FOTR20006NR1794Skin · crackedRT OTBD FORE FLAP WBL 348 CRACK ON SKIN FWD OF FITTING. REPAIRED ON FASI W/O 20006, NR 01794. INSTALLED REPAIR DOUBLER TO RT OTBD FOREFLAP AT WS 348 IAW SRM 57-50-2, FIG 4 AND 57-50-4 FIG 1 REV 102. MATERIAL USED: 2024-T3, DIM.; 5 X 3 X 0.063.SDR FOTR20006NR1778Skin · delaminatedRT OTBD AILERON T/E WEDGE PUNCTURED ON LOWER SURFACE. REPAIRED ON FASI W/O NR 20006, NR 01778 - INSTALLED HOT BONDED REPAIR DOUBLER TO RT OTBD AILERON TAB IAW SRM 51-40-20 PARA 7, 20 AND 22, REV 102. MATERIAL USED: 2024-T3, 0.012” THICK, DIM.; 3 X 3. CALCULATSDR FOTR20006NR5683Panel · delaminatedNR 6 SPOILER PANEL LOWER SKIN DOUBLER BELOW ACTUATOR ATTACH FITTING IS DISBONDED. REPAIRED ON FASI WO 20006, N/R 05683. INSTALLED BONDED REPAIR TO NR 6 SPOILER PANEL LOWER SKIN DOUBLER BELOW ACTUATOR ATTACH FITTING AT WBL 110 IAW B727 SRM 51-40-20. MATERIASDR FOTR20006NR5666Skin · delaminatedLT INBD AILERON TAB HAS DELAMINATION LOWER SURFACE CENTER. REPAIRED ON FASI WO 20006, N/R 05666. INSTALLED HOT BONDED REPAIR TO LT WING INBD AILERON TAB LOWER SURFACE AT WBL 275 IAW B727 SRM 51-40-20, REV 102. MATERIAL USED: DOUBLER; 2024-T3, 0.012, DIM: 7.SDR FOTR20006NR5665Skin · delaminatedLT IB AILERON TAB LOWER SURFACE OTBD HAS DELAMINATION AREA-MARKED. REPAIRED ON FASI WO 20006. N/R 05665- INSTALLED HOT BONDED REPAIR TO LT WING INBD AILERON TAB LOWER SURFACE AT WBL 295 IAW SRM 51-40-20, REV 102. MATERIAL USED: DOUBLER; 2024-T3, 0.012", DIM: SDR FOTR20006NR5664Skin · delaminatedLT INBD AILERON TAB LOWER SURFACE INBD HAS DELAMINATION. REPAIRED ON FASI WO 20006, N/R 05664. INSTALLED HOT BONDED REPAIR TO LT WING INBD AILERON TAB LOWER SURFACE AT WBL 250 BY IAW B727 SRM 51-40-20, REV 102. MATERIAL USED: DOUBLER; 2024-T3, 0.012, DIM: 1SDR FOTR20006NR5661Skin · crackedFUSELAGE STA 1096 AT STRINGER 1 FIRST FAIRING FASTENER RT SKIN HAS CRACKS. REPAIRED ON FASI WO 20006, N/R 05661. REPAIRED FUSELAGE SKIN AT STA 1096, STR 1 IAW BOEING S/B 727-53A0204 REV 3. MATERIAL USED: 2024-T3, 0.063, DIM: 13.50 BY 11.25. CUT OUT DIM: 3.SDR FOTR20006NR5649Stringer Clip · gougedSTR TIE CLIP GOUGED STA 440 STR 4R. REPAIRED ON FASI WO 20006, N/R 05649. REMOVED AND REPLACED STRINGER TO FRAME CLIP AT STR 4R, STA 440 IAW BOEING DWG 65-45313 REV E AND B727 SRM 51-30-2. MATERIAL USED: 7075-T6, 0.032, DIM: 3.60 BY 1.80.SDR FOTR20006NR5647Stringer Clip · crackedSTR TIE CLIP CRACK STA 460 STR 2R. REPAIRED ON FASI WO 20006 N/R 05647. REMOVED AND REPLACED STRINGER TO FRAME CLIP AT STR 2R, STA 460 IAW BOEING DWG 65-45313 REV E AND B727 SRM 51-30-2. MATERIAL USED: 7075-T6, 0.032, DIM: 3.60 BY 1.80.SDR FOTR20006NR5633Stringer Clip · crackedCABIN AREA STA 700, STRINGER 7L FRAME TO STRINGER BRACKET IS CRACKED. REPAIRED ON FASI WO 20006. N/R 05633- R & R STRINGER TO FRAME CLIP AT STR 7L, STA 700 IAW DWG 65-45313 REV E AND SRM 51-30-2. MATERIAL USED: 7075-T6, 0.032", DIM: 3.60" X 1.80".SDR FOTR20006NR5630Stringer · crackedCABIN AREA STA 720B FWD OF LIGHT HOUSING, STRINGER 15L IS CRACKED. REPAIRED ON FASI WO 20006. N/R 05630- REPAIRED STR 15L AT STA 720B IAW SRM 53-10-3 FIG 5 AND 51-30-2. MATERIAL USED: ANGLE; 7075-T6, 0.040", DIM: 6.0".SDR FOTR20006NR5629Stringer · crackedCABIN AREA STA 720C AFT OF LIGHT HSG, STRINGER 15L IS CRACKED. REPAIRED ON FASI WO20006. N/R 05629- REPAIRED STR 15L AT STA 720C IAW SRM 53-10-3 FIG 5 AND 51-30-2. MATERIAL USED: CHANNEL; 7075-T6, 0.040", DIM: 6.0" X 0.750", RADIUS FILLER; 7075-T6, 0.080", DISDR FOTR20006NR5443Frame · puncturedAFT PIT FRAME PUNCTURED STR 27L BS 1130. REPAIRED ON FASI WO 20006, N/R 05443. REPAIRED AFT CARGO COMPARTMENT FRAME AT STR 27L, STA 1130 IAW B727 SRM 53-10-2 FIG 5 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: ANGLE DOUBLER; 7075-T6, 0.063, DIM: 12.25 BY 4.125SDR FOTR20006NR5442Shear Tie · corrodedAFT PIT FRAME SHEAR TIE HAS SURFACE CORROSION BETWEEN STR 30 AND 28R. REPAIRED ON FASI WO 20006, N/R 05442. REMOVED AND REPLACED AFT CARGO COMPARTMENT FRAME SHEAR TIE AND DRAIN MAST SUPPORT CHANNEL AT STA 1148 BETWEEN STR 28R AND STR 30 IAW B727 SRM 53-10-4 SDR FOTR20006NR5604Frame · dentedFWD CARGO COPT FRAME 720A HAS 2 DENTS IN THE UPPER FLANGE BETWEEN STR 24L-25L. REPAIRED ON FASI WO20006. N/R 05604- REPAIRED FRAME AT STA 720A BETWEEN STR 24L AND 25L IAW SRM 51-30-2 AND 51-40-3 FIG. 1, REV 102. MATERIAL USED: DOUBLER; 7075-T6, 0.050", DIM: 3SDR FOTR20006NR5600Frame · dentedFWD CARGO COMPT FRAME BS 680 UPPER FLANGE IS DENTED AND WEB IS BENT BETWEEN STR 23L-24L. REPAIRED ON FASI WO20006. N/R 05600- REPAIRED FRAME AT STA 680 BETWEEN STR 23L AND 24L IAW B727 SRM 53-10-2 FIG. 3 AND 51-40-3 FIG. 1, REV. 102. MATERIAL USED: DOUBLER; 70SDR FOTR20006NR5599Frame · dentedFWD CARGO COMPT FRAME BS 680 HAS 4 DENTS IN THE UPPER FLANGE BETWEEN STR 23R-25R, WEB IS BENT. REPAIRED ON FASI WO20006, N/R 05599. REPAIRED FRAME AT STA 680 BETWEEN STR 23R AND 25R IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1, REV 102. MATERIAL USED: DOUBL
Back to N286SC, cancelled Jan 3, 2018