N357QS, cancelled Aug 24, 2004
Service difficulty reports · 21
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 = 'N357QS' AND deregistration_id = 'N357QS-2004-08-24' 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 = 'N357QS' AND deregistration_id = 'N357QS-2004-08-24' 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 RYN2002F00004Stringer · corrodedSTRINGER EXFOLIATED BETWEEN BS 1148 TO BS 1166 BETWEEN STRINGER 3L AND 4L IN THE AFT CABIN CROWN AREA. ACCOMPLISHED FUSELAGE STRINGER REPAIR BS 1148 TO 1166 BETWEEN STRINGER 3L AND 4L. DUE TO CORROSION IAW SRM. (MATERIAL USED 301 CRESS .5000 HARD .050 INCH,SDR 2002F00848Fitting · crackedFOUND CRACK AROUND C2 DOOR FORWARD UPPER HINGE ATTACH POINT AT BS 1070 STRINGER 20R AND 19R. ACCOMPLISHED C2 DOOR FORWARD FRAME REPAIR AT BS 1070 STRINGER 20R AND 19R IAW B727 SRM 53-10-2, FIGURE 5. (M)SDR 2002F00841Stringer · damagedHOLE FOUND IN LOWER RADIUS AT BS 370 STRINGER 6R. ACCOMPLISHED FUSELAGE STRINGER REPAIR AT BS 370, STRINGER 6R IAW B727 SRM 53-10-2, FIGURE 2. (M)SDR 2002F00847Structure · corrodedLEFT NOSE WHEEL WELL VERTICAL WEB EXFOLIATED AT INTERSECTION WITH UPPER NOSE CHORD AS VIEWED FROM DOG HOUSE AT BS 315 DUE TO CORROSION. ACCOMPLISHED NOSE WHEEL WELL LEFT VERTICAL WEB REPAIR DUE TO CORROSION IAW B727 SRM 53-10-2, FIGURE 1. (M)SDR 2002F00846Pressure Panel · corrodedNOSE WHEEL WELL SKIN CRACKED LEFT SIDE AT STATION 243.7. ACCOMPLISHED NOSE WHEEL WELL RIGHT SIDE SKIN REPAIR AT BS 243.7 IAW B727 SRM 51-40-2, FIGURE 1. (M)SDR 2002F00845Pressure Panel · crackedNOSE WHEEL WELL RIGHT SIDE SKIN HAS A VERTICAL CRACK AT STATION 270. ACCOMPLISHED NOSE WHEEL WELL RIGHT SIDE SKIN REPAIR AT BS 270 IAW B727 SRM 51-40-2, FIGURE 1 AND 53-10-2, FIGURE 2. (M)SDR 2002F00844Pressure Panel · corrodedDUE TO CORROSION, RIGHT NOSE WHEEL WELL VERTICAL WEB EXFOLIATED AT INTERSECTION WITH UPPER NOSE CHORD AS VIEWED FROM DOG HOUSE BS 315. ACCOMPLISHED RIGHT NOSE WHEEL WELL VERTICAL WEB REPAIR IAW B727 SRM 53-10-2 FIGURE 1. (M)SDR 2002F00843Frame · corrodedRIGHT NOSE WHEEL WELL, MID CHORD EXFOLIATED AT INTERSECTION OF RIGHT WEB AND FLOOR WEB AS VIEWED FROM DOG HOUSE. ACCOMPLISHED RIGHT NOSE WHEEL WELL MID CHORD REPLACEMENT IAW B727 SRM 51-30-2 AND 51-20-4. (M)SDR 2002F00842Skin · corrodedBULGING AND PILLOWING SKIN ON STRINGER 8L AT BS 1166 THROUGH BS 1183. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 1166 TO BS 1183 STRINGER 8L DUE TO CORROSION IAW B727 SRM 53-30-3, FIGURE 3. (M)SDR 2002F00840Skin · corrodedBULGING SKIN ALONG STRINGER 10L AT BS 920 THROUGH 1005 DUE TO CORROSION. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 920 TO BS 1005 AT STRIGNER 10L IAW B727 SRM 53-30-3 FIG 14. (M)SDR RYN2002F00000Support · damagedAT MAIN CARGO DOOR FORWARD ACTUATOR, FORWARD AND AFT SUPPORT BLOCK ON DOOR STATION 540, 5 BOLTS HAVE OBLONGED/ELONGATED HOLES AND 1 LOOSE BOLT. ACCOMPLISHED MAIN CARGO DOOR FORWARD ACTUATOR SUPPORT BLOCK ATTACH INTERCOSTALS (2 EACH: FORWARD AND AFT) REPLACEMSDR 2001F00391Frame · corrodedRIGHT NOSE WHEEL WELL, MID CHORD EXFOLIATED AT INTERSECTION OF RIGHT WEB AND FLOOR WEB AS VIEWED FROM DOG HOUSE. ACCOMPLISHED RIGHT NOSE WHEEL WELL MID CHORD REPLACEMENT IAW B727 SRM 51-30-2 AND 51-20-4. (M)SDR RYN2002F00003Skin · corrodedBULGING SKIN/DISHED FASTENER AT BS 1176 THRU BS 1183, STRINGER 20L THRU 21L UNDER AFT LAV SERVICE VALVE. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 1176 TO BS 1183 STRINGER 20L TO STRINGER 21L DUE TO CORROSION. (MATERIAL USED 2024-T3. 071, 28 INCHES X 30 INSDR RYN2002F00002Skin · damagedBULGING AND PILLOWING SKIN AT BS 1085 THRU BS 1110 ALONG FASTENER ROWS AT STRINGER 17R THRU 19R ON EXTERNAL FUSELAGE. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 1085 TO BS 1110 BETWEEN STRINGER 17R AND 19R DUE TO CORROSION IAW MFG ENGINEERING RO. (MATERIAL USSDR RYN2002F00001Skin · damagedBULGING/PILLOWING SKIN ALONG STRINGER 4L AT LAP JOINT BS 1130 THRU BS 1183. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 1130 TO BS 1183 STRINGER 4L DUE TO CORROSION IAW SRM. (MATERIAL USED 2024-T3 .050 INCH, 98 INCHES X 9.1250 INCHES)SDR 2001F00201Flap · out of adjMODERATE VIBRATION DURING CLIMB-OUT, ABOVE 260 KNOTS. VIBRATION STOPPED WHEN APPLYING SPEED BRAKES. FUEL DUMPED. RETURNED TO AIRPORT WITH NO INCIDENT. ADJUSTED UPPER ECCENTRICS ON INBOARD RIGHT FLAP. OPERATIONAL CHECK GOOD. (M)SDR 20010112SG042Bulb · damagedFLT 736 - IAD - NR 1 SMOKE DETECTOR WILL NOT TEST. REMVOED AND REPLACED NR 1 SMOKE DETECTOR BULB. SYSTEM OPERATES NORMAL. (M)SDR 20010112SG064Fire Detector · malfunctionedFLT 640 - GRR - LOWER CARGO COMPARTMENT FIRE DETECTOR HAS YELLOW MAINTENANCE LIGHT AND NO GREEN SYSTEM LIGHT. REMOVED AND REPLACED LOWER AFT CARGO FORWARD DETECTOR. SYSTEM STILL SHOWS MAIN CONTROL FAULT LIGHT. REMAINS ON DEFERRAL. (M)SDR 20000718AP003Valve · brokenFLT 649 - AIR RETURN TO OMA, ON CLIMB-OUT AT 1000 FEET AGL FLAPS 2 DEGREES WERE SELECTED AND A SPLIT FLAP CONDITION OCCURRED. SMOKE BEGAN TO FILL THE COCKPIT, AND EMERGENCY WAS DECLARED AND AN IMMEDIATE RETURN INITIATED. INSPECTED NR 1 AND NR 3 PRECOOLER REGSDR 99ZZZM742Bulb · burnedFLT 701 - IND- NR 1 SMOKE DETECTOR WON'T SELF TEST. RELAMPED TEST BULBS. (M)SDR 96ZZZM1326Door · unsecuredUNABLE TO PRESSURIZE AIRCRAFT. AIRCRAFT MADE AN ATB INTO DAYTON. RESEATED E/E COMPARTMENT DOOR.
Back to N357QS, cancelled Aug 24, 2004