N208AU, cancelled Jul 20, 2000
Service difficulty reports · 98
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 = 'N208AU' AND deregistration_id = 'N208AU-2000-07-20' 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 = 'N208AU' AND deregistration_id = 'N208AU-2000-07-20' 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 P2EA99348Skin · delaminatedSJO - LEFT WING OUTBOARD FLIPPER FLAPPER DELAMINATED. DEFECT SIZE, LENGTH 9 INCH, WIDTH 7.25 INCH. REPAIRED FLIPPER FLAPPER PER COOPESA EO COO-CMP-3-57-711-99, DATED DECEMBER 7, 1999. (M)SDR P2EA99344Frame · crackedSJO - C-CHECK, FRAME CRACKED AT BS 967, BETWEEN STRINGER 20/21LT. DEFECT SIZE, LENGTH 3.5 INCH, WIDTH .16 INCH, DEPTH .63 INCH. REPAIRED FUSELAGE SECTION AT BS 967, BETWEEN STRINGER 19 AND 21 LEFT PER SRM 51-40-3. (M)SDR P2EA99337Seat Track · corrodedSJO - C-CHECK, SEAT TRACK CORRODED FROM BS 360 TO BS 380, LBL 35 INCHES. DEFECT SIZE, LENGTH 8 INCHES, WIDTH 2.25 INCHES, DEPTH .200 INCHES. REPAIRED SEAT TRACK SECTION FROM BS 344 TO BS 380, LBL 25 INCHES PER SRM 53-10-5, FIG 2. (M)SDR P2EA99356Skin · disbondedSJO - DURING C-CHECK, RIGHT AILERON INBOARD TRAILING EDGE DISBONDED AT REAR SPAR AREA. REPAIRED RIGHT AILERON PER SRM 51-40-6, PAR 5. (M)SDR P2EA99347Frame · crackedSJO - FORWARD CARGO DOOR FRAME CRACKED AT AFT FRAME, DEFECT SIZE, LENGTH .750 INCH. REPAIRED FORWARD CARGO DOOR BETWEEN BEAM NR 1 AND BEAM NR 3 PER SRM 51-40-3 FIG 1. (M)SDR P2EA99346Rib · crackedSJO - SLAT TRACK RIB CRACKED AT RIGHT WING FRONT SPAR SS356. DEFECT SIZE, LENGTH 1.5 INCH, WIDTH .32 INCH. REPLACED RIB AT SS 356 OUTBOARD TRACK PER SRM 51-30-2. (M)SDR P2EA99338Floorbeam · corrodedSJO - C-CHECK, FLOORBEAM UPPER CHORD CORRODED AT BS 344, WL 208, BETWEEN LBL 32 AND BL 0. DEFECT SIZE, LENGTH 15 INCHES, WIDTH 1.5 INCH, DEPTH .050 INCH. REPAIRED FLOORBEAM AT BS 344, BETWEEN RBL 9 INCHES AND LBL 40 INCHES PER SRM 53-10-2, FIG 7. (M)SDR P2EA99334Intercostal · crackedSJO - FORWARD SERVICE DOOR INTERCOSTAL CRACKED AT BEAM 3. ANGLE REPLACED PER SRM 51-10-1 PAGE 5, 51-30-2 PAGE 8. (M)SDR P2EA99341Skin · crackedSJO - C-CHECK, FUSELAGE SKIN CRACK FROM BS 764 TO BS 767 BETWEEN STRINGER 18 AND 19 LEFT. DEFECT SIZE, LENGTH 3 INCH, WIDTH .032 INCH, DEPTH .028 INCH. REPAIRED FUSELAGE SKIN SECTION FROM BS 759.5 TO BS 771, BETWEEN STRINGER 18 LT AND 20 LT PER COOPESA EO COSDR P2EA99339Skin · scratchedSJO - C-CHECK, E/E DOOR WITH DEEP SCRATCHES AND MISSING MATERIAL. DEFECT SIZE, LENGTH 1.125 INCH, WIDTH .250 INCH, DEPTH .040 INCH. REPLACED DOOR SKIN PER SRM 51-10-1 PAGE 5 AND PER SRM 51-30-2. (M)SDR P2EA99309Detent Arm · out of adjustMDW - FLT 277 - FLAPS 1 THROUGH 25 SELECTED, NR 6 LEADING EDGE SLAT EXTENDS CROOKED. FLAPS 30 THROUGH 40 SELECTED, NR 6 LEADING EDGE SLAT GOES TO FULL EXTEND. ADJUSTED DETENT ARMS ON NR 6 L/E SLAT PER MM 27-81-0A. OPS CHECKS NORMAL. (X)SDR P2EA99216Mechanism · out of adjustMDW - FLT 586 - NR 6 LEADING EDGE SLAT WOULD NOT EXTEND IN FLIGHT UNTIL FLAPS 30 POSITION WAS SELECTED. ADJUSTED TENSION ON NR 6 SLAT DETENT ARMS PER MM 27-81-0. SLATS OPERATE NORMALLY. (X)SDR P2EA99199Connector · looseDEN - FLT 305 - EMERGENCY DECLARED (APU PREVIOUSLY DEFERRED) LANDING UNEVENTFUL AT SCHEDULED DESTINATION. LEFT ENGINE DRIVEN GENERATOR DROPPED OFF LINE IN FLIGHT AND WOULD NOT RESET. SWAPPED APU GCU WITH NR 1 ENGINE GCU. RAN NR 1 ENGINE. GENERATOR OPS CHECSDR P2EA99127Keel Beam · corrodedSJO - DURING Q-CHECK, A SECTION OF THE KEEL BEAM AT BS 630, RBL 5 WAS FOUND WITH CORROSION. THE AREA WAS REPAIRED AS PER COOPESA EO C00-3-53-176-99 AND BOEING FAX NR COO-SJO-0384RR. (M)SDR P2EA99091Bolt · wornSJO - DURING Q-CHECK, THE NR 2 ENGINE, AFT MOUNT ATTACH BOLT, WAS FOUND WITH WEAR. NR 2 ENGINE AFT MOUNT ATTACH BOLT REPLACED IAW MM 71-21-11. (M)SDR P2EA99083Skin · damagedSJO - DURING Q-CHECK, A SKIN REPAIR AT BS 500A, STRINGER 26R, WAS REMOVED FOR INVESTIGATION. AREA WAS CLEANED, INSPECTED AND REPAIRED AS PER SRM 53-30-3, FIGURE 16. (M)SDR P2EA99101Panel · delaminatedSJO - DURING Q-CHECK, THE RIGHT WING FIXED TRAILING EDGE PANEL, P/N 65-70947-24 WAS FOUND DELAMINATED. THE PANEL WAS REPAIRED IW EO NR COO-CMP-3-57-159-99. (M)SDR P2EA99100Skin · delaminatedSJO - DURING Q-CHECK, THE LEFT WING NR 2 TRAILING EDGE SLAT WAS FOUND WITH DELAMINATION. THE SLAT WAS REPAIRED IAW EO NR COO-CMP-3-57-149-99. (M)SDR P2EA99111Skin · delaminatedSJO - DURIGN Q-CHECK RIGHT AILERON WAS FOUND WITH DELAMINATION. AILERON WAS REPAIRED AS PER COOPESA NR COO-CMP-3-57-151-99. (M)SDR P2EA99097Skin · delaminatedSJO - DURING Q-CHECK, FLIGHT SPOILER NR 3 WAS FOUND WITH DELAMINATION. FLIGHT SPOILER REPAIRED AS PER COOPESA EO NR COO-CMP-3-57-150-00. (M)SDR P2EA99092Bolts · wornSJO - DURING Q-CHECK, NR 2 ENGINE, FORWARD MOUNT THRUST LINKS ATTACH BOLTS FOUND WITH WEAR. REPLACED ATTACH BOLTS AS PER MM 71-20-11. (M)SDR P2EA99089Bolt · wornSJO - DURING Q-CHECK, ENGINE NR 1 FORWARD MOUNT THRUST LINK ATTACH BOLTS FOUND WITH WEAR. BOLTS REPLACED AS PER MM 71-20-11. (M)SDR P2EA99118Mechanism · corrodedSJO - DURING Q-CHECK, THE R2 DOOR HANDLE MECHANISM HOUSING WAS FOUND WITH CORROSION AT THE LOWER TORQUE TUBE POSITION. REWORKED BEARING BORE AND MOUNTING HOLES AS PER OHM 52-46-05. (M)SDR P2EA99117Bearing · corrodedSJO - DURING Q-CHECK, THE R1 DOOR WAS FOUND WITH CORROSION ON THE UPPER TORQUE TUBE BEARING POSITION. THE BEARING BORE AND MOUNTING HOLES WERE REWORKED AS PER OHM 52-46-06. (M)SDR P2EA99106Skin · delaminatedSJO - DURING Q-CHECK, DELAMINATION WAS FOUND ON THE LEFT AILERON. THE AILERON WAS REPAIRED PER COOPESA EO COO-CMP-3-57-127-99. (M)SDR P2EA99084Bulkhead Chord · crackedSJO - DURING Q-CHECK, A CRACK WAS FOUND ON THE BS 178 PRESSURE BULKHEAD, FORWARD SIDE, LOWER HORIZONTAL CHORD. CRACK WAS REPAIRED IAW SRM 51-40-4 FIGURE 1. (M)SDR P2EA99126Support · wornSJO - DURING Q-CHECK, THE NR 1 ENGINE THRUST REVERSER, RIGHT ACTUATOR SUPPORT WAS WORN TO LIMITS. THE ACTUATOR SUPPORT WAS REPLACED IAW SRM 51-10-1. (M)SDR P2EA99107Skin · crackedSJO - DURING Q-CHECK, LFEC DETECTED A CRACK IN A FASTENER HOLE AT BS 492.4, BETWEEN STRINGERS 23 AND 24 RIGHT. THE AREA WAS REPAIRED AS PER COOPESA EO NR COO-2-53-157-99 AND BOEING FAX NR COO-SJO-99-0319. (M)SDR P2EA99125Firewall · wornSJO - DURING Q-CHECK, THE NR 2 ENGINE PYLON FORWARD FIREWALL WAS FOUND WORN. THE FIREWALL PANEL WAS REPAIRED AS PER COOPESA EO NR 3-54-189-99 AND BOEING FAX COO-SJO-99-0389. (M)SDR P2EA99124Intercostal · corrodedSJO - DURING Q-CHECK, A STIFFENER AND INTERCOSTAL IN THE E/E COMPARTMENT BETWEEN BS 294.5 AND BS 312 AT STRINGER WERE FOUND WITH CORROSION. THE INTERCOSTAL AND STIFFENER WERE REPLACED AS PER SRM 51-30-2. (M)SDR P2EA99099Bulkhead Web · crackedSJO - DURING Q-CHECK, A CRACK WAS FOUND ON THE WEB OF THE PRESSURE BULKHEAD AT BS 294.5 BETWEEN STRINGER 27 AND 28 RT IN THE E/E COMPARTMENT. WEB SECTION WAS REPAIRED IAW EO NR COO-3-53-146-99 AND BOEING FAX NR COO-SJO-99-0293. (M)SDR P2EA99085Rib · crackedSJO - DURING Q-CHECK, A RIB WAS FOUND CRACKED IN THE RIGHT WING INTERNAL AREA AT WS 505 UPPER FLANGE. THE CRACK WAS REPAIRED IAW SRM 57-10-7 FIG 1. (M)SDR P2EA99123Frame · crackedSJO - DURING Q-CHECK, THE BS 685 RIGHT FRAME FITTING WAS FOUND CRACKED. THE CRACK WAS REPAIRED AS PER BOEING FAX NR COO-SJO-99-0388RR AND COOPESA EO NR COO-3-53-155-99. (M)SDR P2EA99119Skin · crackedSJO - DURING Q-CHECK, THE L1 DOOR CUT OUT LOWER AFT CORNER OUTER SKIN WAS FOUND CRACKED. THE SKIN WAS REPAIRED FROM BS 322 TO 355 IAW SB 53-1083 REV 3, PART IV AND DRAWING NR 65C27253. (M)SDR P2EA99098Floorbeam · crackedSJO - DURING Q-CHECK, THE UPPER FLANGE OF THE FLOORBEAM AT BS 668.75, LBL 25 WAS FOUND CRACKED. REPAIRED FLOORBEAM AS PER COOPESA EO NR COO-3-53-154-99 AND BOEING FAX NR COO-SJO-98-0993RR. (M)SDR P2EA99122Skin · corrodedSJO - DURING Q-CHECK, THE RIGHT WING OUTBOARD MID-FLAP SKIN AT WS 497 WAS BULGED. REPAIRED SKIN AS PER BOEING FAX COO-SJO-99-0330RR. (M)SDR P2EA99116Mechanism · corrodedSJO - DURING Q-CHECK, THE L2 DOOR HANDLE MECHANISM HOUSING HAD CORROSION AT LOWER TORQUE TUBE BEARING HOLE. THE HOLE AND BUSHING WERE REWORKED IAW OHM 52-16-03. (M)SDR P2EA99115Skin · crackedSJO - DURING Q-CHECK, A CRACK WAS FOUND AT THE LEFT WING, INBOARD MID FLAP LE SKIN AT INBOARD TRACK CUTOUT. THE CRACK WAS REPAIRED IAW BOEING FAX COO-SJO-99-0279RR. (M)SDR P2EA99114Skin · crackedSJO - DURING Q-CHECK, A CRACK WAS FOUND AT THE LEFT WING, OUTBOARD MIDFLAP LE SKIN AT OUTBOARD TRACK CUTOUT. THE CRACK WAS REPAIRED IAW BOEING FAX NR COO-SJO-99-0279RR. (M)SDR P2EA99105Skin · wornSJO - DURING Q-CHECK, THE SKIN ON THE LEADING EDGE OF THE RIGHT WING OUTBOARD FOREFLAP WAS FOUND WITH WEAR. THE SKIN WAS REPAIRED FROM WSL 498 TO 505 AS PER SRM 57-50-40- FIG 1. (M)SDR P2EA99104Rib · crackedSJO - DURING Q-CHECK, LEFT WING OUTBOARD MID FLAP INTERNAL LE RIB AT WBL 298 WAS FOUND CRACKED. RIB REPLACED AS PER SRM 51-10-1 PAGE 5. (M)SDR P2EA99103Rib · crackedSJO - DURING Q-CHECK, THE LEFT INBOARD MID FLAP STRUCTURE, FOREFLAP CENTER TRACK SUPPORT FITTING RIB (INBOARD) WAS CRACKED AT TWO PLACES. RIB REPLACED AS PER SRM 51-10-1 PAGE 5. (M)SDR P2EA99093Stringer · corrodedSJO - DURING Q-CHECK, A REPAIR LOCATED AT BS 767, STRINGER 9L WAS REMOVED FOR INVESTIGATION. AREA WAS CLEANED, INSPECTED AND REPAIRED AS PER SRM 53-30-3 FIG 6. (M)SDR P2EA99080Skin · damagedSJO - DURING Q-CHECK, AN EXISTING SKIN REPAIR LOCATED AT BS 727A, STRINGER 8R, WAS REMOVED FOR INVESTIGATION. AREA WAS CLEANED, INSPECTED AND A PERMANENT REPAIR WAS INSTALLED AS PER SRM 53-30-3 FIGURE 6. (M)SDR P2EA99895Cargo Track · corrodedSJO - DURING Q-CHECK, THE FORWARD CARGO COMPARTMENT CARGO TRACK AT BS 468, RBL 14, WAS FOUND WITH CORROSION. THE TRACK WAS REPAIRED AS PER SRM 53-10-5 FIG 5. (M)SDR P2EA99121Splice · crackedSJO - DURING Q-CHECK, THE STRINGER SPLICE AT BS 359, STRINGER 14L WAS FOUND CRACKED. THE STRINGER SPLICE WAS REPLACED AS PER SRM 51-10-1 PAGE 5. (M)SDR P2EA99112Stringer · corrodedSJO - DURING Q-CHECK, TO VERIFY SRM COMPLIANCE, A REPAIR AT BS 1016 STRINGER 18L WAS REMOVED FOR INVESTIGATION. THE AREA WAS CLEANED, INSPECTED, AND REPAIRED AS PER COOPESA EO NR COO-3-53-152-99. (M)SDR P2EA99110Web · crackedSJO - DURING Q-CHECK, A CRACK WAS FOUND ON THE NLG WHEEL WELL UPPER WEB AT BS 278, RBL 10. THE UPPER WEB WAS REPAIRED IAW COOPESA EO NR COO-SJO-99-0267. (M)SDR P2EA99109Skin · crackedSJO - DURING Q-CHECK, A CRACK WAS FOUND ON THE RIGHT WING INBOARD MIDFLAP, LE SKIN AT WBL 87.75. CRACK REPAIRED IAW BOEING FAX COO-SJO-99-0280. (M)SDR P2EA99102Rib · crackedSJO - DURING Q-CHECK, RIGHT WING, UPPER CHANNEL OF THE LE RIB AT WS 213 WAS FOUND CRACKED. THE CHANNEL WAS REPLACED IAW SRM 51-10-1 PAGE 5. (M)
Back to N208AU, cancelled Jul 20, 2000