# Service difficulty reports: N357QS, cancelled Aug 24, 2004

A list on [N357QS, cancelled Aug 24, 2004](https://openairdocs.org/deregistered/N357QS-2004-08-24.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR RYN2002F00004](https://openairdocs.org/sdr/RYN2002F00004.md): Stringer · corroded · Aug 14, 2001 · N357QS · Boeing 72721 · Standard Practices/Structures
  > STRINGER 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 2002F00848](https://openairdocs.org/sdr/2002F00848.md): Fitting · cracked · Aug 13, 2001 · N357QS · Boeing 72721 · Fuselage Main, Structure
  > FOUND 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 2002F00841](https://openairdocs.org/sdr/2002F00841.md): Stringer · damaged · Aug 6, 2001 · N357QS · Boeing 72721 · Fuselage Main, Longeron/Stringer
  > HOLE 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 2002F00847](https://openairdocs.org/sdr/2002F00847.md): Structure · corroded · Aug 5, 2001 · N357QS · Boeing 72721 · Fuselage Main, Structure
  > LEFT 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 2002F00846](https://openairdocs.org/sdr/2002F00846.md): Pressure Panel · corroded · Aug 5, 2001 · N357QS · Boeing 72721 · Fuselage Main, Bulkhead
  > NOSE 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 2002F00845](https://openairdocs.org/sdr/2002F00845.md): Pressure Panel · cracked · Aug 5, 2001 · N357QS · Boeing 72721 · Fuselage Main, Bulkhead
  > NOSE 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 2002F00844](https://openairdocs.org/sdr/2002F00844.md): Pressure Panel · corroded · Aug 5, 2001 · N357QS · Boeing 72721 · Fuselage Main, Bulkhead
  > DUE 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 2002F00843](https://openairdocs.org/sdr/2002F00843.md): Frame · corroded · Aug 5, 2001 · N357QS · Boeing 72721 · Fuselage Main, Frame
  > RIGHT 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 2002F00842](https://openairdocs.org/sdr/2002F00842.md): Skin · corroded · Aug 5, 2001 · N357QS · Boeing 72721 · Fuselage Main, Plate/Skin
  > BULGING 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 2002F00840](https://openairdocs.org/sdr/2002F00840.md): Skin · corroded · Aug 5, 2001 · N357QS · Boeing 72721 · Fuselage Main, Plate/Skin
  > BULGING 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 RYN2002F00000](https://openairdocs.org/sdr/RYN2002F00000.md): Support · damaged · Aug 5, 2001 · N357QS · Boeing 72721 · Cargo/Baggage Doors
  > AT 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) REPLACEM
- [SDR 2001F00391](https://openairdocs.org/sdr/2001F00391.md): Frame · corroded · Aug 5, 2001 · N357QS · Boeing 72721 · Fuselage Main, Frame
  > RIGHT 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 RYN2002F00003](https://openairdocs.org/sdr/RYN2002F00003.md): Skin · corroded · Aug 5, 2001 · N357QS · Boeing 72721 · Standard Practices/Structures
  > BULGING 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 IN
- [SDR RYN2002F00002](https://openairdocs.org/sdr/RYN2002F00002.md): Skin · damaged · Aug 5, 2001 · N357QS · Boeing 72721 · Standard Practices/Structures
  > BULGING 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 US
- [SDR RYN2002F00001](https://openairdocs.org/sdr/RYN2002F00001.md): Skin · damaged · Aug 5, 2001 · N357QS · Boeing 72721 · Standard Practices/Structures
  > BULGING/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 2001F00201](https://openairdocs.org/sdr/2001F00201.md): Flap · out of adj · Jul 14, 2001 · N357QS · Boeing 72721 · Trailing Edge Flap Control System
  > MODERATE 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 20010112SG042](https://openairdocs.org/sdr/20010112SG042.md): Bulb · damaged · Dec 1, 2000 · N357QS · Boeing 72721 · Smoke Detection
  > FLT 736 - IAD - NR 1 SMOKE DETECTOR WILL NOT TEST. REMVOED AND REPLACED NR 1 SMOKE DETECTOR BULB. SYSTEM OPERATES NORMAL. (M)
- [SDR 20010112SG064](https://openairdocs.org/sdr/20010112SG064.md): Fire Detector · malfunctioned · Nov 23, 2000 · N357QS · Boeing 72721 · Fire Detection
  > FLT 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 20000718AP003](https://openairdocs.org/sdr/20000718AP003.md): Valve · broken · Apr 21, 2000 · N357QS · Boeing 72721 · Cabin Cooling System
  > FLT 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 REG
- [SDR 99ZZZM742](https://openairdocs.org/sdr/99ZZZM742.md): Bulb · burned · Aug 19, 1999 · N357QS · Boeing 72721 · Smoke Detection
  > FLT 701 - IND- NR 1 SMOKE DETECTOR WON'T SELF TEST. RELAMPED TEST BULBS. (M)
- [SDR 96ZZZM1326](https://openairdocs.org/sdr/96ZZZM1326.md): Door · unsecured · Aug 22, 1996 · N357QS · Boeing 72721 · Electrical/Electronic Compartment Doors
  > UNABLE TO PRESSURIZE AIRCRAFT. AIRCRAFT MADE AN ATB INTO DAYTON. RESEATED E/E COMPARTMENT DOOR.

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N357QS-2004-08-24/reports

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