# Service difficulty reports: N573SA, cancelled Nov 23, 2010

A list on [N573SA, cancelled Nov 23, 2010](https://openairdocs.org/deregistered/N573SA-2010-11-23.md).

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

- [SDR S9BA2008032](https://openairdocs.org/sdr/S9BA2008032.md): Gasket · failed · Nov 8, 2008 · N573SA · Dhav DHC6300 · Engine Oil Cooler
  > LOST NR 2 OIL PRESSURE AND TORQUE PRESSURE OIL ON ENGINE COWLING AND RIGHT FLOAT. FOUND OIL COOLER RETURN LINE GASKET LEAKING. REMOVED AND REPLACED GASKET, SERVICED ENGINE WITH 4 QUARTS OF OIL. LEAK CHECK SATISFACTORY. PROPELLER WAS FEATHERED AND ENGINE WAS
- [SDR S9B2008F00000](https://openairdocs.org/sdr/S9B2008F00000.md): Fuse · burned · Jun 9, 2008 · N573SA · Dhav DHC6 · Air Distribution Fan
  > AIR CONDITION CABIN FAN INOPERATIVE ON HIGH, MAKES A BURNING SMELL ON LOW. REPLACED 3 BLOWN FUSES WITH NEW. GROUND OPS CHECK, NO ODORS OR DISCREPANCIES NOTED. (K)
- [SDR S9BA2008022](https://openairdocs.org/sdr/S9BA2008022.md): Float · leaking · May 29, 2008 · N573SA · Dhav DHC6300 · Wheel/Ski/Float
  > "OPEN" LEFT FLOAT BAY NR 6 LEAKING. REMOVED AND REPLACED FLOAT. WILL UPDATE AFTER FLOAT INSPECTION, EMERGENCY MEASURE EXECUTED NO. AIRCRAFT GROUNDED. FLIGHT NA.
- [SDR S9BA2008021](https://openairdocs.org/sdr/S9BA2008021.md): Mount · failed · May 27, 2008 · N573SA · Dhav DHC6300 · Engine Mount Section
  > RT SPINNER NOTED MISALIGNED. REMOVED AND REPLACED TOP ENGINE MOUNT INSPECTED ALL RIGGING AND WIRING. EMERGENCY MEASURES EXECUTED, RETURNED TO DOCK. AIRCRAFT GROUNDED, RETURNED TO SERVICE NEXT DAY. FLIGHT NR 189
- [SDR S9BA20080019](https://openairdocs.org/sdr/S9BA20080019.md): Longeron · cracked · May 19, 2008 · N573SA · Dhav DHC6300 · Nacelle/Pylon, Longeron/Stringer
  > RT ENGINE, OB NACELLE LONGERON CRACKED. REPLACED WITH FACTORY NEW PART IAW AC43.13-1B SECTION 4 PARA 4-57 FIG 4-6 AND 4-9. (PN C6W1512-S142) NO EMERGENCY MEASURES EXECUTED, AIRCRAFT GROUNDED.
- [SDR S9BA200800016](https://openairdocs.org/sdr/S9BA200800016.md): Attach Bracket · corroded · Apr 10, 2008 · N573SA · Dhav DHC6 · Empennage Structure
  > DURING CAMP INSPECTION, FOUND CORROSION ON LT AFT (SEA FIN) ATTACHMENT BRACKET. REMOVED AND REPLACED SEA FIN ATTACHMENT BRACKET. EMERGENCY DECLARED? NO, AIRCRAFT GROUNDED, REPAIRED DURING INSPECTION NO.
- [SDR S9BA200800017](https://openairdocs.org/sdr/S9BA200800017.md): Spar · corroded · Apr 10, 2008 · N573SA · Dhav DHC6 · Horizontal Stabilizer, Spar/Rib
  > DURING CAMP INSPECTION FOUND CORROSION ON LT AFT STABILIZATION SPARE WHERE THE SEA FIN ATTACHMENT BRACKET IS LOCATED. REMOVED AND REPLACED OUTER HORIZONTAL REAR SPAR IAW AC 43 13 1B CHP. 7. EMERGENCY DECLARED? NO AIRCRAFT GROUNDED? NOT REPAIRED DURING INSPECTI
- [SDR S9BA200800014](https://openairdocs.org/sdr/S9BA200800014.md): Clevis Pin · missing · Mar 3, 2008 · N573SA · Dhav DHC6 · Wheel/Ski/Float
  > FLT 170, HEARD A POP IN THE AREA OF THE FLYING WIRE. CLEVIS PIN AT LEFT UPPER FLYING WIRE FOUND MISSING UPON LANDING. REMOVED AND REPLACED FLYING WIRES PN 13A0200-079 UPPER FRONT DRAG FITTING 13A02469-001 AND DRAG WIRE SHIM PN 13A02078-002. EMERGENCY WAS N
- [SDR S9BA20080010](https://openairdocs.org/sdr/S9BA20080010.md): Rib · corroded · Feb 11, 2008 · N573SA · Dhav DHC6 · Wing, Rib/Bulkhead
  > CPCP INSP, RT WING FWD RIB AT STA.85 CORRODED. REMOVED AND REPLACED RIB WITH NEW PART IAW AC43-14, CHAPTER 4 PARA 4-57.
- [SDR S9BA20080009](https://openairdocs.org/sdr/S9BA20080009.md): Rib · corroded · Feb 11, 2008 · N573SA · Dhav DHC6 · Wing, Rib/Bulkhead
  > CPCP INSPECTION, RT WING FWD RIB AT STA 72.5 CORRODED. REMOVED AND REPLACED RIB WITH NEW PART IAW AC43-14, CHAPTER 4 PARA 4-57.
- [SDR S9BA20080006](https://openairdocs.org/sdr/S9BA20080006.md): Longeron · corroded · Feb 11, 2008 · N573SA · Dhav DHC6 · Nacelle/Pylon, Longeron/Stringer
  > CPCP INSPECTION, LT NACELLE LONGERONS CORRODED. REMOVED AND REPLACED LT AND RT LONGERON IAW SRM 57-30-00 AND AC43-14, CHAPTER 4 PARA 4-57.
- [SDR S9BA20080003](https://openairdocs.org/sdr/S9BA20080003.md): Skin · corroded · Feb 11, 2008 · N573SA · Dhav DHC6 · Wing, Plate/Skin
  > CPCP INSPECTION, LT WING CORRUGATION AT WS 65 TO 125 CORRODED. REPAIRED CORRUGATION BETWEEN WS 65 AND 125 IAW SRM 57-30-00 FIG 4 AND RD6-57-077. EMERGENCY MEASURES EXECUTED? NO. AIRCRAFT GROUNDED? YES.
- [SDR S9BA20080004](https://openairdocs.org/sdr/S9BA20080004.md): Skin · corroded · Feb 11, 2008 · N573SA · Dhav DHC6 · Nacelle/Pylon, Plate/Skin
  > CPCP INSPECTION, LT WING, LT AND RT NACELLE SKINS CORRODED. REMOVED AND REPLACED NACELLE SKINS AND SPLICED SKINS IAW RD6-54-004 AND AC 43-13, PARA 4-57.
- [SDR S9BA20080012](https://openairdocs.org/sdr/S9BA20080012.md): Skin · corroded · Feb 11, 2008 · N573SA · Dhav DHC6 · Wing, Plate/Skin
  > CPCP INSPECTION, RT WING IB FWD SKIN CORRODED WS STA. 35.15 TO 185. REPLACED SKIN IAW SRM CH 57-30-00 FIG 1AND RD 6-57-164. EMERGENCY MEASURES EXECUTED? NO. AIRCRAFT GROUNDED? YES.
- [SDR S9BA20080011](https://openairdocs.org/sdr/S9BA20080011.md): Skin · corroded · Feb 11, 2008 · N573SA · Dhav DHC6 · Wing, Plate/Skin
  > CPCP INSPECTION; RT WING FWD CORRUGATION AT WS 58 CORRODED. REPAIRED CORRUGATION AT WS 58 WITH FACTORY NEW PART IAW SRM 57-30-00 PAGE 4. EMERGENCY MEASURES EXECUTED? NO AIRCRAFT GROUNDED? YES.
- [SDR S9BA20080008](https://openairdocs.org/sdr/S9BA20080008.md): Mount · corroded · Feb 11, 2008 · N573SA · Dhav DHC6 · Engine Mount Section
  > CPCP INSP, LT NACELLE OB MOTOR MOUNT CORRODED. REMOVED AND REPLACED ENG MOUNT IAW RD 6-54-006. EMERGENCY MEASURES EXECUTED? NO AIRCRAFT GROUNDED? YES
- [SDR S9BA20080005](https://openairdocs.org/sdr/S9BA20080005.md): Frame · corroded · Feb 11, 2008 · N573SA · Dhav DHC6 · Nacelle/Pylon, Frame/Spar/Rib
  > CPCP INSPECTION, LT NACELLE HOOPFRAME CORRODED. REMOVED AND REPLACED HOOP FRAME IAW SRM 57-30-00 PAGE 1 AND AC 43-13, PARA 4-57. AC GROUNDED, YES.
- [SDR S9BA200800002](https://openairdocs.org/sdr/S9BA200800002.md): Spar · corroded · Feb 11, 2008 · N573SA · Dhav DHC6 · Wing Spar
  > CPCP INSPECTION, FWD LT WING SPAR HAS CORROSION BETWEEN STATIONS 72.5 AND WS 135. REPLACED AND SPLICED FWD SPAR WS 72.5 TO 135 IAW RD6-57-191. AIRCRAFT GROUNDED, YES.
- [SDR S9BA200800001](https://openairdocs.org/sdr/S9BA200800001.md): Skin · corroded · Feb 11, 2008 · N573SA · Dhav DHC6 · Wing, Plate/Skin
  > CPCP INSPECTION, LT FWD SKIN ON LT WING IS CORRODED AT WS 63.5. REPLACED LOWER SKIN FROM RIB 1 (STA 35.15) TO RIB 10 (STA 147.5) SPLICED SKIN AT RIB 2 (STA 47.5) AIRCRAFT GROUNDED? YES
- [SDR S9BA200800007](https://openairdocs.org/sdr/S9BA200800007.md): Spar · corroded · Feb 11, 2008 · N573SA · Dhav DHC6 · Wing Spar
  > CPCP INSPECTION, RT WING NOSE SPAR CORRODED WS 35.15 TO WS 135. REPLACED NOSE SPAR WITH FACTORY NEW PART IAW AC43.13-1B CHAP 4 PARA 4-57. EMERGENCY MEASURES EXECUTED. NO AIRCRAFT GROUNDED.
- [SDR S9BA200700021](https://openairdocs.org/sdr/S9BA200700021.md): Skin · corroded · Oct 16, 2007 · N573SA · Dhav DHC6 · Trailing Edge Flaps
  > RT TRAILING FLAP SKIN CORRODED AT ATTACHMENT HINGE FITTING. REMOVED AND REPLACED RT TRAILING FLAP.
- [SDR S9BA200700022](https://openairdocs.org/sdr/S9BA200700022.md): Skin · corroded · Oct 16, 2007 · N573SA · Dhav DHC6 · Wing, Plate/Skin
  > RT WING BOTTOM SKIN CORRODED AT BOTTOM IB WING ROOT STATION 47.5. REMOVED AND REPLACED BOTTOM SKIN IB WING ROOT FROM RIB 2 TO RIB 1 IAW RD6-57-164.
- [SDR S9BA200700017](https://openairdocs.org/sdr/S9BA200700017.md): Relay · burned · Sep 24, 2007 · N573SA · Dhav DHC6300 · Air Conditioning System Wiring
  > SMOKE ODOR IN CABIN. FOUND A/C RELAY BURNED UP. DEFERRED AIR CONDITIONING IAW MEL 21-1 WILL PROVIDE SUPPLEMENTAL INFORMATION WHEN GENERATED. REMOVED AND REPLACED RELAY M83536/9-026M. NO SN THIS ACTION CLEARED DMI 8743 ACTT 19842.6 ACTC 43532
- [SDR S9BA200700016](https://openairdocs.org/sdr/S9BA200700016.md): Attach Bracket · corroded · Sep 17, 2007 · N573SA · Dhav DHC6 · Rudder/Tab, Attach Fittings
  > RUDDER MID HINGE ATTACHMENT BRACKET CORRODED. REMOVED AND REPLACED RUDDER MID HINGE ATTACHMENT BRACKET.
- [SDR S9BA200700015](https://openairdocs.org/sdr/S9BA200700015.md): Spar · corroded · Sep 17, 2007 · N573SA · Dhav DHC6 · Horizontal Stabilizer, Spar/Rib
  > CORROSION FOUND ON FORWARD SPAR OF HORIZONTAL STABILIZER AT SEA FIN MOUNT. (STATION 92) REMOVED AND REPLACED HORIZONTAL STABILIZER.
- [SDR S9BA1307](https://openairdocs.org/sdr/S9BA1307.md): Hinge Fitting · corroded · Jul 24, 2007 · N573SA · Dhav DHC6 · Trailing Edge Flaps
  > OB HINGE ARM ON RT FLAP CORRODED, REMOVED AND REPLACED HINGE ARM.
- [SDR S9BA1207](https://openairdocs.org/sdr/S9BA1207.md): Hinge Fitting · corroded · Jul 24, 2007 · N573SA · Dhav DHC6 · Trailing Edge Flaps
  > RT FWD FLAP IB HINGE ARM HAS CORROSION ON IT. REMOVED AND REPLACED HINGE ARM.
- [SDR S9BA1107](https://openairdocs.org/sdr/S9BA1107.md): Washer · worn · Jul 10, 2007 · N573SA · Dhav DHC6 · Trailing Edge Flap Control System
  > AFTER COMMENCING DESCENT, FUSELAGE VIBRATION FELT PRIMARILY ON LT SIDE OF AIRCRAFT AT 185 KNOTS. FOUND PLAY IN THE IB FLAP FUSELAGE MOUNTING POINT. REPLACED SPECIAL WASHER. PN C6WFM1111-27. CHECK FLIGHT OK.
- [SDR S9BA0507](https://openairdocs.org/sdr/S9BA0507.md): Hinge · corroded · May 6, 2007 · N573SA · Dhav DHC6 · Rudder Structure
  > RUDDER MID HINGE PLATE AND BEARING ASSY CORRODED
- [SDR S9BA00906](https://openairdocs.org/sdr/S9BA00906.md): Hinge · corroded · Nov 6, 2006 · N573SA · Dhav DHC6300 · Trailing Edge Flaps
  > DURING INSPECTION, FOUND LT IB FORE FLAP IB HINGE (PN 6WFM1109-33) WITH ATTACHED RIB CORRODED.
- [SDR S9BA00806](https://openairdocs.org/sdr/S9BA00806.md): Hinge · corroded · Nov 6, 2006 · N573SA · Dhav DHC6300 · Trailing Edge Flaps
  > DURING INSPECTION, FOUND LT IB FORE FLAP OB HINGE (PN C6WF1101045) CORRODED.
- [SDR S9BA01006](https://openairdocs.org/sdr/S9BA01006.md): Bushing · worn · Oct 17, 2006 · N573SA · Dhav DHC6 · Wheel/Ski/Float
  > AT 123 KNOTS FELT OSCILLATION, OBSERVED LT WING BOUNCING UP AND DOWN. FOUND LT (V) STRUT BUSHING WORN. SEE WORK PACKAGE 10/17/06 TO 11/07/06. RELEASED AIRCRAFT FOR FUNCTIONAL CHECK FLIGHT. FUNCTIONAL CHECK FLIGHT WAS SATISFACTORY.
- [SDR S9BA00206](https://openairdocs.org/sdr/S9BA00206.md): Bolt · worn · Sep 25, 2006 · N573SA · Dhav DHC6 · Wing Main, Frame Structure
  > AT 150 KNOTS, NOTICED INCREASING STRUCTURAL VIBRATION. OBSERVED LT WING SHAKING. THIS AIRCRAFT WAS INSPECTED AND FOUND SAFE FOR SPECIAL FLIGHT FROM SPB (SST) TO STX (SSB). REMOVED LT WING. INSPECTED LT WING ATTACH FITTINGS, BUSHINGS AND SPARS. REPLACED LT W

## 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 = 'N573SA' AND deregistration_id = 'N573SA-2010-11-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N573SA-2010-11-23/reports

---
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