# Service difficulty reports: N575US, cancelled Apr 8, 2010

A list on [N575US, cancelled Apr 8, 2010](https://openairdocs.org/deregistered/N575US-2010-04-08.md).

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

- [SDR SB05074](https://openairdocs.org/sdr/SB05074.md): Outflow Valve · faulty · Jun 20, 2005 · N575US · Boeing 737301 · Pressure Regulator/Outflow Valve
  > AT FL330, CREW REPORTED CABIN BEGAN A 6,000 FPM CLIMB. AUTO FAIL LIGHT ILLUMINATED ALONG WITH STANDBY ON LIGHT. CREW SWITCHED TO MANUAL AC/DC PRESSURIZATION MODE AND CONFIRMED OUTFLOW VALVE FULLY CLOSED. CREW APPLIED THRUST ON ENGINES AND DESCENDED TO LOWER
- [SDR SB05073](https://openairdocs.org/sdr/SB05073.md): Outflow Valve · failed · Jun 19, 2005 · N575US · Boeing 737301 · Pressure Regulator/Outflow Valve
  > EN ROUTE FROM CLT TO BUF, 100 MILES SOUTH OF PIT, AIRCRAFT LOST AUTO AND STANDBY PRESSURIZATION MODES. HOWEVER, CREW WAS ABLE TO REGAIN CONTROL IN MANUAL PRESSURIZATION MODE AT FL230. DUE TO OPERATIONAL CONCERNS, FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FUR
- [SDR SB05070](https://openairdocs.org/sdr/SB05070.md): Outflow Valve · inoperative · Jun 14, 2005 · N575US · Boeing 737301 · Pressure Regulator/Outflow Valve
  > EN ROUTE WITH THE AUTO PRESSURIZATION ON MEL, LOST CONTROL OF STANDBY PRESSURIZATION MODE. CABIN ALTITUDE BEGAN TO CLIMB, PILOT REQUESTED AN EMERGENCY DESCENT. REGAINED PRESSURIZATION CONTROL AT APPROX FL280. LANDED WITHOUT INCIDENT. MX CLEARED MEL WITH RE
- [SDR USAA050750](https://openairdocs.org/sdr/USAA050750.md): Skin · cracked · Jun 9, 2005 · N575US · Boeing 737301 · Service Doors
  > CLT - FOUND FORWARD SERVICE DOOR SKIN CRACKED.620 INCH, UPPER HINGE CUTOUT. REPAIR DOUBLER INSTALLED IAW TR 52-10-13. (M)
- [SDR SB05058](https://openairdocs.org/sdr/SB05058.md): Cable · inoperative · May 8, 2005 · N575US · Boeing 737301 · Escape Slide
  > PIT - THE R2 DOOR SLIDE LANYARD WOULD NOT RELEASE. MAINTENANCE REPLACED THE SLIDE.
- [SDR USAA040362](https://openairdocs.org/sdr/USAA040362.md): Frame · cracked · Jul 26, 2004 · N575US · Boeing 737301 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED APPROX 1.025 INCH, STATION 663.75. INSTALLED REPAIR ANGLE PER EA 78568. (M)
- [SDR USAA04337](https://openairdocs.org/sdr/USAA04337.md): Skin · damaged · Jun 22, 2004 · N575US · Boeing 737301 · Fuselage Main, Plate/Skin
  > FOUND PROBLEM WITH PREVIOUS REPAIR AT BS 470, STRINGER 8L TO 9L. REPAIRED PER SRM 53-00-01 FIGURE 201. (M)
- [SDR USAA04336](https://openairdocs.org/sdr/USAA04336.md): Spar · damaged · Jun 22, 2004 · N575US · Boeing 737301 · Horizontal Stabilizer, Spar/Rib
  > PIT - FOUND PROBLEM WITH PREVIOUS REPAIR ON LOWER SKIN OF THE RIGHT HORIZONTAL STAB AT REAR SPAR LOWER SURFACE. REPAIRED PER SRM FIUTE 204 DETAIL NR 1. (M)
- [SDR USAA040304](https://openairdocs.org/sdr/USAA040304.md): Skin · delaminated · Jun 15, 2004 · N575US · Boeing 737301 · Wing, Plate/Skin
  > PIT - FOUND WING DELAMINATION 1 SQUARE INCH, NR 3 SLAT INBOARD END TRAILING EDGE. REMOVED DAMAGE, INSTALLED FILLER INTERNAL DOUBLER AND NEW CORE AND TOP DOUBLER PER SRM 51-70-10. (M)
- [SDR USAA040305](https://openairdocs.org/sdr/USAA040305.md): Skin · delaminated · Jun 15, 2004 · N575US · Boeing 737301 · Wing, Plate/Skin
  > PIT - FOUND WING DELAMINATED 1.5 SQUARE INCH, TOP SURFACE AT OUTBOARD TRACK AREA TRAILING EDGE OF NR 3 SLAT. REMOVED DAMAGE. INSTALLED FILLER/CORE MATERIAL, INSTALLED TOP DOUBLER PER SRM 51-70-10. (M)
- [SDR USAA040281](https://openairdocs.org/sdr/USAA040281.md): Stiffener · corroded · Jun 8, 2004 · N575US · Boeing 737301 · Fuselage Main, Bulkhead
  > PIT - FOUND BULKHEAD STIFFENER 1 INCH BY 2 INCH AREA, STATION 1016 LBL 0. REMOVED CORROSION AND INSTALLED REPAIR PER BOEING DWG 65C28106. (M)
- [SDR USAA040303](https://openairdocs.org/sdr/USAA040303.md): Skin · dented · Jun 3, 2004 · N575US · Boeing 737301 · Elevator, Plate/Skin
  > PIT - FOUND SKIN DENTED WITH DELAMINATION TWO AREAS 2 INCHES BY 1.5 INCH AND 1 INCH BY 1.375 INCH AREA, LEFT ELEVATOR LOWER SURFACE BETWEEN 176/200. REMOVED DISBONDED SKIN AND CORE, REPLACED CORE MATERIAL AND NEW DOUBLERS PER SRM 55-20-01 AND EA 78563. (M)
- [SDR USAASB03169](https://openairdocs.org/sdr/USAASB03169.md): Battery · weak · Sep 17, 2003 · N575US · Boeing 737301 · Emergency Lighting
  > FOUND LT OVERWING AND FORWARD ENTRY EMERGENCY LIGHT BATTERIES WEAK. MAINTENANCE REPLACED THE BATTERIES. (M)
- [SDR USAASB03069](https://openairdocs.org/sdr/USAASB03069.md): Charger · inoperative · May 25, 2003 · N575US · Boeing 737301 · Emergency Lighting
  > CLT - MAINTENANCE REPORTED THE RIGHT EMERGENCY LIGHTS AT THE OVERWING EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB02119](https://openairdocs.org/sdr/USAASB02119.md): Splice · damaged · Jun 22, 2002 · N575US · Boeing 737301 · Light System Wiring
  > TPA - MAINTENANCE FOUND THE SEAT END EMERGENCY EXIT LIGHT AT THE EMERGENCY EXIT ROW INOPERATIVE. MAINTENANCE REPLACED A BAD SPLICE. OPERATIONAL CHECK GOOD. (M)
- [SDR USA2002F00055](https://openairdocs.org/sdr/USA2002F00055.md): Uplock Sensor · faulty · Jun 9, 2002 · N575US · Boeing 737301 · Landing Gear Position and Warning
  > ENROUTE, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND REPORTED THE GEAR OPERATED NORMALLY. LIGHT EXTINGUISHED WHEN GEAR HANDLE WAS PLACED TO DOWN POSITION. FLIGHT CONTINUED AND LANDED WITHOUT FUR
- [SDR USA2002F00047](https://openairdocs.org/sdr/USA2002F00047.md): Connector · faulty · Jun 1, 2002 · N575US · Boeing 737301 · Engine EGT/TIT Indicating System
  > AFTER TAKEOFF, THE NR 2 ENGINE EGT RED LIGHT ILLUMINATED AS EGT WENT TO 1,067 DEGREES. CREW REDUCED THROTTLE AND EGT RETURNED TO NORMAL. ALL OTHER ENGINE INDICATIONS WERE WITHIN NORMAL LIMITS. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. N
- [SDR USAASB01305](https://openairdocs.org/sdr/USAASB01305.md): Battery Pack · discharged · Nov 1, 2001 · N575US · Boeing 737301 · Emergency Lighting
  > PHL - MAINTENANCE FOUND THE AISLE EMERGENCY LIGHTS, IN THE CABIN, INOPERATIVE. MAINTENANCE FOUND SEVERAL BATTERY PACKS DISCHARGED. REMOVED AND REPLACED BATTERY PACKS IN ASSOCIATION WITH MM 33-51-01. OPS CHECK GOOD. (M)
- [SDR USAASB01218](https://openairdocs.org/sdr/USAASB01218.md): Power Unit · failed · Aug 1, 2001 · N575US · Boeing 737301 · Escape Slide
  > CLT - DURING ANNUAL OPERATIONAL CHECK OF THE FORWARD RIGHT SERVICE DOOR ESCAPE SLIDE, THE SLIDE DEPLOYED NORMALLY BUT THE SLIDE MOUNTED EMERGENCY LIGHTS FAILED TO ILLUMINATE. SLIDE OPERATIONAL CHECK FAILED. MAINTENANCE FOUND THE POWER UNIT ASSEMBLY FOR THE E
- [SDR USAASB01065](https://openairdocs.org/sdr/USAASB01065.md): Switch · faulty · Feb 27, 2001 · N575US · Boeing 737301 · Leading Edge Slat Position Indicating System
  > CLT - FLT 1625 - EN ROUTE FROM CLT-JAX, AS CREW RETRACTED THE FLAPS/SLATS, THE NR 6 LEADING EDGE SLAT INTRANSIT LIGHT ILLUMINATED ON THE FORWARD AND OVERHEAD PANELS AND WOULD NOT EXTINGUISH. THE CREW VISUALLY LOOKED AT THE SLATS ON THE WINGS AND APPEARED TO B
- [SDR USAASB01060](https://openairdocs.org/sdr/USAASB01060.md): Controller · faulty · Feb 25, 2001 · N575US · Boeing 737301 · Cabin Pressure Controller
  > CLT - FLT 1262 - ON CLIMB-OUT FROM PBI, EN ROUTE TO PHL, PRESSURIZATION WAS UNCONTROLLABLE WITH THE RIGHT PACK AS THE LEFT PACK WAS ON MEL. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLAC
- [SDR USAASB00025](https://openairdocs.org/sdr/USAASB00025.md): Indicator · failed · Jan 28, 2000 · N575US · Boeing 737301 · Trailing Flap Position Indicating System
  > GSO - FLT 1462 - ON APPROACH INTO GSO, A FLAP ASYMMETRY OCCURRED. SPLIT FLAPS OF 1 DEGREE LEFT AND 25 DEGREES RIGHT WAS INDICATED. FLAP HANDLE WAS LOCKED OUT ALSO. THERE WAS NO INDICATION OF LEADING EDGE DEVICES ON OVERHEAD OR FORWARD PANEL. FIRST OFFICERS
- [SDR USAASB99084](https://openairdocs.org/sdr/USAASB99084.md): Mechanism · not latched · Mar 31, 1999 · N575US · Boeing 737301 · Service Doors
  > EWR - FLT 605 - AFTER TAKEOFF, CLIMBING THROUGH 2000 FEET, THE AUTO FAIL LIGHT ILLUMINATED. CREW COULD NOT CONTROL CABIN PRESSURIZATION IN STANDBY OR MANUAL MODE. FLIGHT RETURNED TO FIELD TO EWR AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED
- [SDR USAASB98207](https://openairdocs.org/sdr/USAASB98207.md): Air Distr · odor · Aug 11, 1998 · N575US · Boeing 737301 · Air Distribution System
  > CLT - FLT 1267 - ON TAKEOFF FROM LGA, CREW NOTICED A STRONG SMELL OF RUBBER BURNING IN THE COCKPIT AND THE CABIN. THERE WERE NO SIGNS OF SMOKE SMELL AND THE APU WAS OFF AT THE TIME. SMELL DISSIPATED ON CLIMB-OUT. FLIGHT CONTINUED ONTO CLT AND LANDED WITHOUT
- [SDR USAASB98195](https://openairdocs.org/sdr/USAASB98195.md): Battery Pack · discharged · Jul 22, 1998 · N575US · Boeing 737301 · Emergency Lighting
  > ROC - MAINTENANCE FOUND ALL THE EMERGENCY LIGHTS CONTROLLED BY POWER SUPPLY M1132 FAIL AFTER 10-15 SECONDS OF OPERATION. ALSO FOUND THE AISLE BULLNOSE EMERGENCY LIGHT AT STATION 590L INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN POWER SUPPLY M11
- [SDR USAA970001](https://openairdocs.org/sdr/USAA970001.md): Bulkhead · cracked · Jan 4, 1997 · N575US · Boeing 737301 · Fuselage Main, Bulkhead
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO CRACKS APPROXIMATELY 2 INCHES IN LENGTH AT BS 178 LBL 6 INCHES WL 200 BULKHEAD. REPAIRED PER T/R 53-10-07 REV A. (M)
- [SDR USAA970000](https://openairdocs.org/sdr/USAA970000.md): Bulkhead · cracked · Jan 4, 1997 · N575US · Boeing 737301 · Fuselage Main, Bulkhead
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO CRACKS APPROXIMATELY 2 INCHES AT BS 178 BULKHEAD RBL 6 INCHES WL 200. REPAIRED PER T/R 53-10-07 REV A SRM 51-10-02 PAGE 19. (M)
- [SDR USAASB97005](https://openairdocs.org/sdr/USAASB97005.md): Oil Line · leaking · Jan 3, 1997 · N575US · Boeing 737301 · Engine Oil Pressure
  > INT - FL 7901 - FLIGHT WAS IN THE PROCESS OF COMPLYING WITH TEST HOP PROCEDURES, AFTER A HEAVY MAINTENANCE VISIT, WHEN THE CREW NOTICED A RAPID OIL QTY LOSS IN THE NR 2 ENGINE. CREW SHUT DOWN THE NR 2 ENGINE AND RETURNED TO FIELD AT INT. NO EMERGENCY WAS DECL
- [SDR USAASB96174](https://openairdocs.org/sdr/USAASB96174.md): Power Supply · inoperative · Sep 1, 1996 · N575US · Boeing 737301 · Emergency Lighting
  > PHL - MAINTENANCE FOUND THE EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT INOP AT THE AFT RIGHT SERVICE DOOR. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY IN THE AFT OVERHEAD CABIN. OPS CHECK GOOD. (M)

## 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 = 'N575US' AND deregistration_id = 'N575US-2010-04-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N575US-2010-04-08/reports

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