# Service difficulty reports: N589US, cancelled Jul 22, 2008

A list on [N589US, cancelled Jul 22, 2008](https://openairdocs.org/deregistered/N589US-2008-07-22.md).

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

- [SDR USAA920080551](https://openairdocs.org/sdr/USAA920080551.md): Filter · leaking · Mar 2, 2008 · N589US · Boeing 737301 · Hydraulic Quantity Indicator
  > FLT NR 1767- AIR TURNBACK - ON TAKEOFF RAISING LANDING GEAR "A" HYDRAULIC QUANTITY WENT TO ZERO. ENGINE DRIVEN PUMP LIGHT ILLUMINATED. PUMP TURNED OFF. MX DICOVERED THE "A" HYDRAULIC SYSTEM EMDP ACOUSTIC FILTER LEAKING. MX REPLACED THE EMDP ACOUSTIC FILTER.
- [SDR USAA920080511](https://openairdocs.org/sdr/USAA920080511.md): Stringer Clip · cracked · Feb 22, 2008 · N589US · Boeing 737301 · Fuselage Main, Attach Fittings
  > CLT - MAJOR REPAIR - C1 CHECK - CRACKED STRINGER TIE EXTENSION, BS 360, S15R. REPLACED STRINGER TIE EXTENSION, BS 360, S15R IAW B737 SRM 51-10-02.
- [SDR USAA920080507](https://openairdocs.org/sdr/USAA920080507.md): Stringer Clip · cracked · Feb 22, 2008 · N589US · Boeing 737301 · Fuselage Main, Attach Fittings
  > CLT - MAJOR REPAIR - C1 CHECK - CRACKED STRINGER TIE CLIP, BS 348, S15R. REPLACED STRINGER TIE CLIP, BS 348, S15R IAW B737 SRM 51-10-02.
- [SDR USAA920080502](https://openairdocs.org/sdr/USAA920080502.md): Attach Fitting · cracked · Feb 21, 2008 · N589US · Boeing 737301 · Fuselage Main, Attach Fittings
  > CLT - MAJOR REPAIR - C1 CHECK - CRACKED FORWARD ENTRY DOOR CUT OUT INTERCOSTAL UPPER AND LOWER ATTACH CLIPS, BS 348.20. REPLACED FORWARD ENTRY DOOR CUT OUT INTERCOSTAL UPPER AND LOWER ATTACH CLIP, BS 348.20 IAW B737 SRM 51-10-02.
- [SDR USAA920080501](https://openairdocs.org/sdr/USAA920080501.md): Web · cracked · Feb 21, 2008 · N589US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - MAJOR REPAIR - C1 CHECK - CRACKED WEB, BS 294.5, S16L. REPLACED WEB, BS 294.5, S16L IAW B737 SRM 51-10-02.
- [SDR USAA920080500](https://openairdocs.org/sdr/USAA920080500.md): Skin · cracked · Feb 21, 2008 · N589US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - MAJOR REPAIR - C1 CHECK - CRACKED FUSELAGE SKIN, BS 754, S24R. REPAIRED FUSELAGE SKIN, BS 754, S24R IAW B737 SRM 53-00-01 REPAIR.
- [SDR USAA920080503](https://openairdocs.org/sdr/USAA920080503.md): Stringer Clip · cracked · Feb 19, 2008 · N589US · Boeing 737301 · Fuselage Main, Attach Fittings
  > CLT - MAJOR REPAIR - C1 CHECK - CRACKED STRINGER CLIP, BS 360, S14L. REPLACED STRINGER CLIP, BS 360, S14L IAW B737 SRM 51-10-02.
- [SDR SB07091](https://openairdocs.org/sdr/SB07091.md): Battery Pack · discharged · Oct 15, 2007 · N589US · Boeing 737301 · Emergency Lighting
  > CLT - MAINTENANCE REPORTED A FORWARD CABIN EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD OUTBOARD BATTERY PACK. OPERATIONAL CHECK GOOD.
- [SDR SB07085](https://openairdocs.org/sdr/SB07085.md): Outflow Valve · malfunctioned · Sep 30, 2007 · N589US · Boeing 7373B7 · Pressure Regulator/Outflow Valve
  > FLT 1253 CLT - ORF ON DEPARTURE AIRCRAFT DID NOT PRESSURIZE. RETURN TO CLT. RESET PRESSURIZATION SYSTEM. NO FURTHER FAULTS.
- [SDR USAA070226](https://openairdocs.org/sdr/USAA070226.md): Frame · cracked · Mar 20, 2007 · N589US · Boeing 737301 · Fuselage Main, Frame
  > BS 492, S-24R HAS CRACK. FABRICATED & INSTALLED REPAIR ANGLES PER EA 98533, DEFECT SIZE:.5 INCH.
- [SDR USAA070221](https://openairdocs.org/sdr/USAA070221.md): Floorbeam · corroded · Mar 19, 2007 · N589US · Boeing 737301 · Fuselage Main, Floor Beam
  > STA 986 HAS CORROSION. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER EA 98538; CORR TASK C53-107-02; LEVEL 2, DEFECT SIZE:.5 INCH DIA.
- [SDR USAA070178](https://openairdocs.org/sdr/USAA070178.md): Frame · cracked · Mar 13, 2007 · N589US · Boeing 737301 · Fuselage Main, Frame
  > BS 492 S-24R CRACKED. FAB'D & INSTALLED REPAIR ANGLES PER EA 98533, DEFECT SIZE:.5 INCH CRACK.
- [SDR USAA070070](https://openairdocs.org/sdr/USAA070070.md): Vertical Beam · cracked · Jan 30, 2007 · N589US · Boeing 737301 · Fuselage Main, Structure
  > FOUND CRACK LT VERTICAL BEAM BETWEEN 5.7 LBL AND WL 184. REMOVED CRACK VERTICAL BEAM AND INSTALLED REPAIR KIT CPN 1131156 PER EO 5300V155, DEFECT SIZE: 2".
- [SDR USAA070046](https://openairdocs.org/sdr/USAA070046.md): Skin · cracked · Jan 22, 2007 · N589US · Boeing 737301 · Fuselage Main, Plate/Skin
  > BS 727D S-21L, BS 727E S-22L CRACKED. REPAIR DOUBLER/TRIPLER INSTALLED 28 X 24 INCHES PER TYPICAL 53-60-03A, DEFECT SIZE: 3 INCHES (2) EACH.
- [SDR USAA070045](https://openairdocs.org/sdr/USAA070045.md): Skin · cracked · Jan 22, 2007 · N589US · Boeing 737301 · Fuselage Main, Plate/Skin
  > BS 727E AND S-21R CRACKED. INSTALLED REPAIR DOUBLER 12' X 10" PER SRM 53-00-01 FIG 201, DEFECT SIZE: 4 INCHES.
- [SDR USAA200606006](https://openairdocs.org/sdr/USAA200606006.md): Skin · delaminated · Jun 13, 2006 · N589US · Boeing 737301 · Leading Edge Devices
  > 3.5" L BY 1.4" W DELAMINATION AT OUTBD AFT UPPER SKIN AT NR 5 SLAT TRAILING EDGE. REPAIRED PER EA 82529.
- [SDR SB06056](https://openairdocs.org/sdr/SB06056.md): Switch · faulty · Jun 3, 2006 · N589US · Boeing 737301 · Emergency Lighting
  > CLT - PILOT REPORTED THE FLOOR TRACK EMERGENCY LIGHTS REMAIN ILLUMINATED. MAINTENANCE FOUND THE S7 EMERGENCY LIGHT SWITCH FAULTY. THE SWITCH WAS PROVIDING A GROUND TO PIN 4 OF EACH BATTERY PACK WHILE IN THE ARMED POSITION. REMOVED AND REPLACED S7 EMERGENCY
- [SDR USAA200605003](https://openairdocs.org/sdr/USAA200605003.md): Skin · cracked · May 24, 2006 · N589US · Boeing 737301 · Leading Edge Devices
  > MULTIPLE NUMBER OF CRACKS, TOT APPROX LENGTH 2 INCHES, AT LOWER TIE SURFACE AT ACTUATOR, NR 3 SLAT SKIN. INSTALLED FILLER AND DOUBLER PER SRM 57-43-01, REPAIR 06.
- [SDR SB05092](https://openairdocs.org/sdr/SB05092.md): Odor · detected · Aug 11, 2005 · N589US · Boeing 737301 · Air Distribution System
  > CREW REPORTED A SLIGHT ELECTRICAL/BURNING ODOR IN THE AFT GALLEY. CREW TURNED GALLEY POWER OFF AND ODOR DISSIPATED. MAINTENANCE TURNED GALLEY POWER ON AND INVESTIGATED PROBLEM. COULD NOT VERIFY OR FIND ANY SOURCE OF THE ODOR. AIRCRAFT OK FOR SERVICE.
- [SDR USAA050738](https://openairdocs.org/sdr/USAA050738.md): Channel · cracked · Jun 7, 2005 · N589US · Boeing 737301 · Leading Edge Devices
  > CLT - C4- CHANNEL, 1 INCH CRACK, NR 3 SLAT JUST BELOW ROD END ACTUATOR ATTACHMENT POINT (L) CHANNEL. FABRICATED AND INSTALLED NEW CHANNEL. (K)
- [SDR SB04143](https://openairdocs.org/sdr/SB04143.md): Converter · defective · Oct 11, 2004 · N589US · Boeing 737301 · Integrated Flight System
  > CLT - FLT528 - THIRTY MINUTES AFTER TAKEOFF FROM CLT, EN ROUTE TO MCI, THE FIRST OFFICERS ADI FAILED WITH INTERMITTENT FLAGS IN VIEW. CREW DECIDED TO RETURN TO FIELD AT CLT WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTE
- [SDR USAA040278](https://openairdocs.org/sdr/USAA040278.md): Stiffener · corroded · Jun 4, 2004 · N589US · Boeing 737301 · Fuselage Miscellaneous Structure
  > FOUND RADIAL STIFFENER CORRODED 1 INCH, STATION 1016, AFT PRESS BULKHEAD CENTER RADIAL AT BL 0. MANUFACTURED AND INSTALLED REPAIR ANGLES TO REPLACED SECTION PER EO 5302V112A. (M)
- [SDR USAA040279](https://openairdocs.org/sdr/USAA040279.md): Bulkhead · corroded · Jun 4, 2004 · N589US · Boeing 737301 · Fuselage Main, Bulkhead
  > PIT - FOUND WEB CORRODED.25 INCH AREA, STATION 1016, AFT PRESSURE BULKHEAD WEB AT BL 0 UNDER STIFFENER. REMOVED FASTENERS BURNISHED AREA, TREATED, PRIMED, RE-INSTALLED FASTENERS PER EO 5302V112A. (M)
- [SDR USAA040280](https://openairdocs.org/sdr/USAA040280.md): Splice · cracked · May 29, 2004 · N589US · Boeing 737301 · Fuselage Miscellaneous Structure
  > PIT - FOUND STRINGER SPLICE CRACKED 1 INCH, STRINGER 4 LEFT, FRAME STATION 907 IN CENTER FLANGE OF STRINGER SPLICE. REMOVED AND REPLACED PART PER OM-26 AND J3-58-53513-C-001. (M)
- [SDR USAA040297](https://openairdocs.org/sdr/USAA040297.md): Skin · delaminated · May 27, 2004 · N589US · Boeing 737301 · Leading Edge Devices
  > PIT - FOUND SKIN AND CORE DELAMINATED 4 INCHES BY 4 INCHES, NR 5 SLAT OUTBOARD END TRAILING EDGE SECTION. INSTALLED NEW CORE PER SRM 51-20-10. (M)
- [SDR USAA040298](https://openairdocs.org/sdr/USAA040298.md): Skin · delaminated · May 26, 2004 · N589US · Boeing 737301 · Leading Edge Devices
  > PIT - FOUND SURFACE TO CORE DELAMINATION 3 INCHES BY 2.5 INCH AREA, NR 4 SLAT TOP SURFACE INBOARD TRAILING EDGE. INSTALLED NEW CORE AND EXT DOUBLER PER SRM 51-70-10. (M)
- [SDR USAA040301](https://openairdocs.org/sdr/USAA040301.md): Skin · delaminated · May 26, 2004 · N589US · Boeing 737301 · Leading Edge Devices
  > PIT - FOUND SKIN TO CORE BOND WITH 1 INCH DIAMETER AND.75 INCH DIAMETER, LEFT WING NR 2 SLAT TOP SURFACE INBOARD AND OUTBOARD T/E CORNERS. REMOVED EXT SKIN AND DAMAGED CORE, INSTALLED NEW PER SRM 51-70-10. (M)
- [SDR USAA040189](https://openairdocs.org/sdr/USAA040189.md): Skin · cracked · May 5, 2004 · N589US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 1.8125 INCH CRACK STATION 727D, STRINGER 24R. DOUBLER INSTALLED PER SRM 53-00-01, DETAIL X1, FIG 229. (M)
- [SDR USAASB03182](https://openairdocs.org/sdr/USAASB03182.md): Proximity Sensor · inoperative · Oct 15, 2003 · N589US · Boeing 737301 · Landing Gear Position and Warning
  > ON CLIMB-OUT FROM CLT, EN ROUTE TO IAH, CREW RECEIVED A NOSE LANDING GEAR RED UNSAFE LIGHT WHEN GEAR WAS RETRACTED. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND RECYCLED GEAR. RECEIVED THREE GREEN LIGHTS WHEN GEAR WAS DOWN AND WHEN GEAR WAS BROUGHT U
- [SDR USAASB02212](https://openairdocs.org/sdr/USAASB02212.md): Charger · inoperative · Nov 27, 2002 · N589US · Boeing 737301 · Emergency Lighting
  > IND - MAINTENANCE FOUND THE EMERGENCY EXIT IDENTIFIER LIGHTS FOR THE LEFT OVERWING EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M)
- [SDR USAA020178](https://openairdocs.org/sdr/USAA020178.md): Skin · cracked · Apr 18, 2002 · N589US · Boeing 737301 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED 1 INCH, FS 360-380 AND BL 0 - S28 LEFT. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 53-30-07 AND EA 73832. (M)
- [SDR USAASB02018](https://openairdocs.org/sdr/USAASB02018.md): Nut · broken · Jan 19, 2002 · N589US · Boeing 737301 · Service Doors
  > MKE - FLT 1242 - ON CLIMB-OUT FROM MKE, EN ROUTE TO CLT, THE AIRCRAFT WOULD PRESSURIZE. A LOUD AIR NOISE COULD ALSO BE HEARD FROM THE AFT RIGHT SERVICE DOOR AREA. FLIGHT RETURNED TO FIELD AT MKE AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED
- [SDR USAASB01311](https://openairdocs.org/sdr/USAASB01311.md): Battery Pack · discharged · Nov 11, 2001 · N589US · Boeing 737301 · Emergency Lighting
  > CLE - MAINTENANCE FOUND THE EMERGENCY LIGHT ABOVE THE FORWARD ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB01292](https://openairdocs.org/sdr/USAASB01292.md): Light · inoperative · Oct 11, 2001 · N589US · Boeing 737301 · Emergency Lighting
  > TPA - MAINTENANCE FOUND THE EXTERIOR AFT SERVICE DOOR ESCAPE SLIDE LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR AFT SERVICE DOOR ESCAPE LIGHT ASSY (SOCKET AND REFLECTOR ASSY). OPS CHECK GOOD. (M)
- [SDR USAASB00358](https://openairdocs.org/sdr/USAASB00358.md): Uplock Sensor · faulty · Dec 25, 2000 · N589US · Boeing 737301 · Landing Gear Position and Warning
  > CLT - FLT 458 - DURING CLIMB-OUT FROM YYZ, THE RIGHT MAIN LANDING GEAR RED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. CREW EXTENDED AND RETRACTED GEAR TWICE. THE RED LIGHT EXTINGUISHED UPON GEAR EXTENSION BUT RE-ILLUMINATED WHEN GEAR HANDLE WAS UP AD
- [SDR USAA001435](https://openairdocs.org/sdr/USAA001435.md): Angle · corroded · Aug 30, 2000 · N589US · Boeing 737301 · Fuselage Miscellaneous Structure
  > PIT - FOUND Z-ANGLE CORRODED 1 INCH BY 1 INCH, STATION 950 AFT ENTRY DOOR TOP SURFACE. CORROSION LEVEL 1, TASK NR C53-107-02. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 53-60-51 AND 51-40-02. (M)
- [SDR USAASB99138](https://openairdocs.org/sdr/USAASB99138.md): Battery · discharged · Jun 5, 1999 · N589US · Boeing 737301 · Battery/Charger System
  > DEN - FLT 621 - EN ROUTE FROM LAS TO PHL, CREW REPORTED A STRONG ODOR OF ELECTRICAL FUMES IN THE CABIN. CREW DECLARED AN EMERGENCY AND DIVERTED TO DEN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE MAIN AIRCRAFT BATTERY TO HAVE AN INTERNAL S
- [SDR 99ZZZM377](https://openairdocs.org/sdr/99ZZZM377.md): Battery Charger · failed · Jun 5, 1999 · N589US · Boeing 737301 · Battery/Charger System
  > DEN - FLT 621 - EN ROUTE FROM LAS TO PHL, CREW REPORTED A STRONG ODOR OF ELECTRICAL FUMES IN THE CABIN. CREW DECLARED AN EMERGENCY AND DIVERTED TO DEN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE MAIN AIRCRAFT BATTERY TO HAVE AN INTERNAL S
- [SDR USAASB98103](https://openairdocs.org/sdr/USAASB98103.md): Check Valve · failed · Apr 25, 1998 · N589US · Boeing 737301 · Landing Gear Retraction/Extension System
  > PIT - FL8051 - AFTER TAKEOFF AND LANDING GEAR 'UP' SELECTED, THE NOSE GEAR FAILED TO RETRACT. SELECTED GEAR 'DOWN' AND PERFORMED CHECKLIST. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE
- [SDR USAASB96101](https://openairdocs.org/sdr/USAASB96101.md): R278 Relay · malfunctioned · Jun 5, 1996 · N589US · Boeing 737301 · Landing Gear Retraction/Extension System
  > CLT - FL 1405 - CREW COULD NOT RAISE GEAR USING NORMAL PROCEDURES. ALTERNATE PROCEDURES WORKED, HOWEVER, THE TAKEOFF WARNING HORN SOUNDED. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURHTER INCIDENT. MAINTENANCE REPLACED THE R432 AND R276 RELAYS AND PERFORME
- [SDR 96ZZZM1016](https://openairdocs.org/sdr/96ZZZM1016.md): R432 Relay · malfunctioned · Jun 5, 1996 · N589US · Boeing 737301 · Landing Gear Retraction/Extension System
  > CLT - FL 1405 - CREW COULD NOT RAISE GEAR USING NORMAL PROCEDURES. ALTERNATE PROCEDURES WORKED, HOWEVER, THE TAKEOFF WARNING HORN SOUNDED. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURHTER INCIDENT. MAINTENANCE REPLACED THE R432 AND R276 RELAYS AND PERFORME
- [SDR USAASB96100](https://openairdocs.org/sdr/USAASB96100.md): Connector · failed · Jun 4, 1996 · N589US · Boeing 737301 · Landing Gear Retraction/Extension System
  > CLT - FLT 765 - CREW COULD NOT RAISE GEAR OR PRESSURIZE AIRCRAFT AFTER TAKEOFF. FLIGHT RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED PINS 3 AND 4 IN CONNECTOR D4574P. GEAR SWING ACCOMPLISHED. (X)
- [SDR USAASB95010](https://openairdocs.org/sdr/USAASB95010.md): Contl Alternator · leaking · Nov 7, 1995 · N589US · Boeing 737301 · Engine RPM Indicating System
  > PIT - FLT 0223 - EN ROUTE IND TO BWI, NR 2 ENGINE OIL QUANTITY FELL TO ZERO AND OIL PRESSURE DROPPED TO RED LINE. FLIGHT CREW SHUT DOWN NR 2 ENGINE AND DIVERTED TO PIT. LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED RT ENGINE N2 ALTERNATOR AND ROTOR DUE
- [SDR USAA950760](https://openairdocs.org/sdr/USAA950760.md): Temp Bulb · faulty · Jul 14, 1995 · N589US · Boeing 737301 · Alternator-Generator Drive
  > OKC - FLT 1409 - THE NR 1 ENGINE CSD HIGH OIL TEMPERATURE LIGHT ILLUMINATED. THE CSD WAS DISCONNECTED AND FLIGHT DIVERTED TO OKC. MAINTENANCE REPLACED THE TEMPERATURE BULB. OPERATIONS CHECKED GOOD. (X)
- [SDR USAA950157](https://openairdocs.org/sdr/USAA950157.md): Fan Blades · bird strike · Feb 23, 1995 · N589US · Boeing 737301 · Landing Gear Retraction/Extension System
  > LGA - FLT 488 - AT 500 FEET ON CLIMB-OUT, HAD A SUDDEN LOUD RUMBLE AND HIGH VIBRATION IN NR 2 ENGINE. WHEN POWER HAS REDUCED AT LEVEL OFF, NOISE DECREASED AND VIBRATION DECREASED TO NORMAL LEVELS. SUSPECTED BIRDSTRIKE. FLIGHT RETURNED TO LGA WHERE LANDING 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 = 'N589US' AND deregistration_id = 'N589US-2008-07-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N589US-2008-07-22/reports

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