# Service difficulty reports: N592US, cancelled Mar 28, 2008

A list on [N592US, cancelled Mar 28, 2008](https://openairdocs.org/deregistered/N592US-2008-03-28.md).

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

- [SDR SB07056](https://openairdocs.org/sdr/SB07056.md): Windshield · cracked · Jul 15, 2007 · N592US · Boeing 737301 · Flight Compartment Windows
  > CHS - FLT - 1575 DURING CRUISE, EN ROUTE FROM DCA TO JAX, THE CAPTAIN'S NR 1 WINDSHIELD OUTER PANE CRACKED. CREW COMPLIED WITH QUICK REFERENCE HANDBOOK PROCEDURES AND DIVERTED TO CHS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINT
- [SDR SB07051](https://openairdocs.org/sdr/SB07051.md): Wire · broken · Jul 7, 2007 · N592US · Boeing 737301 · Light System Wiring
  > MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHT AT ROW 12, LT SIDE, INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT SEAT ROW 12, LT SIDE. OPERATIONAL CHECK GOOD.
- [SDR USAA061205](https://openairdocs.org/sdr/USAA061205.md): Skin · cracked · Oct 5, 2006 · N592US · Boeing 737301 · Fuselage Main, Plate/Skin
  > FOUND CRACK BS 727D STRINGER 23L, DEFECT SIZE: 2".
- [SDR USAA061206](https://openairdocs.org/sdr/USAA061206.md): Skin · cracked · Oct 5, 2006 · N592US · Boeing 737301 · Fuselage Main, Plate/Skin
  > FOUND FUSELAGE SKIN CRACKED, BS 727D STINGER 23R. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW EA 98130, DEFECT SIZE: 2".
- [SDR USAA061207](https://openairdocs.org/sdr/USAA061207.md): Skin · cracked · Oct 5, 2006 · N592US · Boeing 737301 · Fuselage Main, Plate/Skin
  > FOUND SKIN CRACKED RADIO RACK EXHAUST CUTOUT. INSTALLED DOUBLER IAW EA 98129, DEFECT SIZE: 1".
- [SDR USAA061201](https://openairdocs.org/sdr/USAA061201.md): Frame · corroded · Oct 4, 2006 · N592US · Boeing 737301 · Fuselage Main, Frame
  > FOUND FRAME STA 380 BETWEEN STR 28R AND 28L. REMOVED DAMAGE, INSTALLED REPAIR PARTS IAW SRM 53-00-07 REPAIR 3, DEFECT SIZE: 2" BY 4".
- [SDR USAA061202](https://openairdocs.org/sdr/USAA061202.md): Skin · cracked · Oct 4, 2006 · N592US · Boeing 737301 · Fuselage Main, Plate/Skin
  > FOUND CRACK BS 727D STRINGER 23R. REMOVED DAMAGE, AND INSTALLED REPAIR DOUBLER PER EA 98130, DEFECT SIZE: 2".
- [SDR SB06095](https://openairdocs.org/sdr/SB06095.md): Switch · dirty · Oct 4, 2006 · N592US · Boeing 737301 · Trailing Edge Flap Control System
  > ON APPROACH, CREW REPORTED AN ASYMMETRICAL FLAP INDICATION AS THE TRAILING EDGE FLAPS LOCKED OUT. LT FLAP WAS INDICATING 15 UNITS AND THE RT FLAP 10 UNITS. PILOT REPORTED THERE WAS NO CONTROL ISSUE WITH THE FLAPS LOCKED OUT. FLIGHT LANDED WITHOUT FURTHER INCID
- [SDR SB06083](https://openairdocs.org/sdr/SB06083.md): Transmitter · faulty · Aug 28, 2006 · N592US · Boeing 737301 · Trailing Flap Position Indicating System
  > PHL - FLT238 - ON APPROACH TO PHL FROM DFW, CREW REPORTED THE FLAPS WOULD NOT MOVE FROM 10 UNITS TO 15 UNITS WHEN SELECTED. CREW EXECUTED A MISSED APPROACH, AND DURING GO-AROUND, FLAPS ADJUSTED THEMSELVES AND INDICATED 15 UNITS. FLIGHT MADE A FLAPS 15 LANDIN
- [SDR SB06055](https://openairdocs.org/sdr/SB06055.md): Transmitter · faulty · May 30, 2006 · N592US · Boeing 737301 · Trailing Flap Position Indicating System
  > ORF - FLT32 - ON APPROACH TO ORF, CREW REPORTED A FLAP ASYMMETRY LOCKOUT. FLIGHT LANDED WITHOUT INCIDENT AT 2 UNITS FLAP POSITION. MAINTENANCE CHECKED WIRING TO BOTH FLAP TRANSMITTERS AND JACKSCREW BALLNUTS FOR DEFECTS. NO DEFECTS NOTED. REMOVED AND REPLAC
- [SDR SB06053](https://openairdocs.org/sdr/SB06053.md): Light · corroded · May 20, 2006 · N592US · Boeing 737301 · Emergency Lighting
  > FLL - MAINTENANCE REPORTED THE LEFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE CLEANED CORROSION FROM BULBS AT LEFT EXTERIOR OVERWING EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.
- [SDR SB06052](https://openairdocs.org/sdr/SB06052.md): Indicator · faulty · May 19, 2006 · N592US · Boeing 737301 · Trailing Flap Position Indicating System
  > ON APPROACH TO PHL FROM ORD, AS CREW SELECTED FLAPS TO 10 UNITS FROM 5 UNITS, REPORTED THE RIGHT FLAP POSITION NEEDLE STOPPED AT 7 UNITS WHILE THE LEFT FLAP POSITION NEEDLE STOPPED AT 9 UNITS. LEADING EDGE FLAPS WENT TO FULL EXTEND NORMALLY. NO ASYMMETRICAL
- [SDR SB06017](https://openairdocs.org/sdr/SB06017.md): Bottle · low · Feb 15, 2006 · N592US · Boeing 737301 · Escape Slide
  > PIT - MAINTENANCE REPORTED THE MAIN ENTRY DOOR ESCAPE SLIDE BOTTLE PRESSURE SHOWS NO GO. MAINTENANCE REMOVED AND REPLACED THE MAIN ENTRY DOOR ESCAPE SLIDE PER MM 25-61-35. PRESSURE CHECKS GOOD.
- [SDR USAA051406](https://openairdocs.org/sdr/USAA051406.md): Skin · punctured · Nov 15, 2005 · N592US · Boeing 737301 · Leading Edge Devices
  > RIGHT WING LEADING EDGE ABOVE NR 4 LEADING EDGE FLAP, APPROX L/E STA 205 DENTED. REMOVED EXISTING REPAIR, CUT OUT DAMAGE, INSTALLED FILLER & DOUBLER PER EA 96961. DEFECT SIZE:.6"L X.4"W X.080"D, 2.5"L X 1"W X.100"D DENT & PUNCTURE,.75"L X.3"W.
- [SDR USAA051405](https://openairdocs.org/sdr/USAA051405.md): Skin · cracked · Nov 15, 2005 · N592US · Boeing 737301 · Fuselage Main, Plate/Skin
  > FWD SERVICE DOOR BOTTOM HINGE CUTOUT SKIN CRACKED. FABRICATED DOUBLER & FILLER PER SRM 52-00-01, 52-10-01. DEFECT SIZE:.250 INCH.
- [SDR USAA051404](https://openairdocs.org/sdr/USAA051404.md): Angle · cracked · Nov 15, 2005 · N592US · Boeing 737301 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR BELOW FLOOR AT BS 616 LEFT SIDE CRACKED. REMOVED & REPLACED ANGLE, INSTALLED FILLER PER SRM 51-40-02 & TYP REP 53-62-01. DEFECT SIZE:.5 INCH.
- [SDR USAA051403](https://openairdocs.org/sdr/USAA051403.md): Floorbeam · corroded · Nov 15, 2005 · N592US · Boeing 737301 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM TEE STA 986.5 RBL 20-30 CORRODED. REMOVED & REPLACED TEE PER TYP REP 53-60-01. DEFECT SIZE: 10 INCHES.
- [SDR USAA051221](https://openairdocs.org/sdr/USAA051221.md): Angle · corroded · Oct 19, 2005 · N592US · Boeing 737301 · Fuselage Miscellaneous Structure
  > STA 907 TO 1006; NO TASK OF LEVEL, CORROSION. FABRICATED PART PER TR 549929, DWG 6941226, SRM 51-40-02, 53-60-15, DEFECT SIZE: 2L X 0.5W X.049 INCH DEEP.
- [SDR USAA051220](https://openairdocs.org/sdr/USAA051220.md): Skin · debonded · Oct 19, 2005 · N592US · Boeing 737301 · Passenger/Crew Doors
  > FWD ENTRY DOOR INNER WALL AT LWR SKIN DISBONDED. FABRICATED REPAIR DOUBLER, FILLER PER TR 52-10-16, DEFECT SIZE: 0.250 INCH.
- [SDR SB04161](https://openairdocs.org/sdr/SB04161.md): Duct · disconnected · Dec 5, 2004 · N592US · Boeing 737301 · Air Distribution System
  > MCO FLT1222 EN ROUTE FROM PBI TO DCA, AT FL370, THE CABIN ALTITUDE WARNING HORN SOUNDED. CREW COULD NOT CONTROL CABIN ALTITUDE AND BOTH PACKS WERE ACTING ABNORMAL. THEY ALSO RECEIVED A DUCT OVERHEAT. CREW ACCOMPLISHED AN EMERGENCY DESCENT TO REGAIN CONTROL O
- [SDR USAA040407](https://openairdocs.org/sdr/USAA040407.md): Skin · cracked · Aug 6, 2004 · N592US · Boeing 737301 · Leading Edge Devices
  > PIT - FOUND L/E SLAT CRACKED 3.5 INCHES, OUTBOARD, LOWER, TRAILING EDGE, NR 4 SLAT ASSEMBLY. INSTALLED DOUBLER PER SRM 57-43-01. (M)
- [SDR USAA030214](https://openairdocs.org/sdr/USAA030214.md): Stiffener · corroded · Oct 17, 2003 · N592US · Boeing 737301 · Fuselage Main, Bulkhead
  > FOUND RADIAL STIFFENER CORRODED 2 INCH BY 1 INCH AREA, AFT PRESS BULKHEAD STATION 1016 AT BL 0. INSTALLED SPLICE SECTION AND REPAIR DOUBLERS PER EO 5302V112 AND BOEING DWG 65C28106 AND EA 77188. (M)
- [SDR USAASB03142](https://openairdocs.org/sdr/USAASB03142.md): Bearing · worn · Aug 21, 2003 · N592US · Boeing 737301 · Brake Anti-Skid Section
  > UPON TOUCHDOWN AT ORF, FROM PHL, THE NR 2 MAIN LANDING GEAR TIRE BLEW. THE AIRCRAFT WAS OPERATING WITH MEL'S ON THE ANIT-SKID AND AUTO BRAKE SYSTEM. AIRCRAFT HAD TO BE TOWED INTO THE GATE FROM THE TAXIWAY. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND NO DA
- [SDR USAASB03127](https://openairdocs.org/sdr/USAASB03127.md): Charger · inoperative · Aug 3, 2003 · N592US · Boeing 737301 · Emergency Lighting
  > PIT - MAINTENANCE REPORTED THE FORWARD ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY. ALSO, REPAIRED A PUSHED BACK CONNECTOR PIN. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB0301A](https://openairdocs.org/sdr/USAASB0301A.md): Charger · inoperative · Jul 11, 2003 · N592US · Boeing 737301 · Emergency Lighting
  > PIT - MAINTENANCE REPORTED THE FORWARD ENTRY DOOR EXTERIOR ESCAPE SLIDE LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB03077](https://openairdocs.org/sdr/USAASB03077.md): Light · inoperative · Jun 10, 2003 · N592US · Boeing 737301 · Emergency Lighting
  > MAINTENANCE FOUND THE MAIN ENTRY DOOR EXTERIOR ESCAPE SLIDE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERAITONAL CHECK GOOD. (M)
- [SDR USAASB02203](https://openairdocs.org/sdr/USAASB02203.md): Light · inoperative · Nov 4, 2002 · N592US · Boeing 737301 · Emergency Lighting
  > IND - MAINTENANCE FOUND THE EMERGENCY LIGHT (ROUND BUTTON LIGHT) ON THE FORWARD CLOSET INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT (ROUND BUTTON LIGHT) ASSEMBLY. OPERATIONAL CHECK GOOD. (M)
- [SDR USAA011329](https://openairdocs.org/sdr/USAA011329.md): Flap · delaminated · Oct 11, 2001 · N592US · Boeing 737301 · Trailing Edge Flaps
  > PIT - FOUND INBOARD AFT FLAP DELAMINATED 15 INCHES BY 7 INCHES ROLLER AND 24 INCHES FROM INBOARD END, INBOARD AFT FLAP, BOTTOM SURFACES SKIN, INBOARD ROLLER SUPT. REPAIRED PER EA 72583, SRM 51-70-10, SRM 57-43-01 FIG 1. (M)
- [SDR USAASB01007](https://openairdocs.org/sdr/USAASB01007.md): Pump · failed · Jan 15, 2001 · N592US · Boeing 737301 · Hydraulic Pump (Electric/Engine), Main
  > PIT - FLT 9228 - DURING CRUISE, EN ROUTE FROM YUL-YYZ, THE NR 2 ELECTRIC HYDRAULIC PUMP OVERHEAT LIGHT ILLUMINATED. DECISION WAS MADE FOR FLIGHT TO DIVERT TO PIT. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DELCARED. MAINTENANCE REMOVED AND REPLACED T
- [SDR USAASB00155](https://openairdocs.org/sdr/USAASB00155.md): Outflow Valve · failed · Jun 2, 2000 · N592US · Boeing 737301 · Pressure Regulator/Outflow Valve
  > PIT - FLT 1031 - FLIGHT WAS EN ROUTE FROM IAH TO PIT, WITH BOTH PACKS IN HIGHT FOR MAXIMUM COOLING. UPON REACHING FL370, CREW TURNED BOTH PACKS TO AUTO AND THE CABIN CLIMBED ABOVE 10,000 FEET WITH WARNING HORN SOUNDING. AN EMERGENCY DESCENT WAS ACCOMPLISHED.
- [SDR USAASB99183](https://openairdocs.org/sdr/USAASB99183.md): Charger · failed · Jul 24, 1999 · N592US · Boeing 737301 · Emergency Lighting
  > BDL - MAINTENANCE FOUND THE AISLE EMERGENCY LIGHTS AT SEAT ROWS 17 THROUGH 20 INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AT STA 962L. OPERATIONAL CHECKED GOOD. (X)
- [SDR USAASB99115](https://openairdocs.org/sdr/USAASB99115.md): Battery Pack · discharged · Apr 29, 1999 · N592US · Boeing 737301 · Emergency Lighting
  > ALB - MAINTENANCE FOUND THE FOLLOWING EMERGENCY LIGHTS INOPERATIVE, FORWARD EXIT SIGNS IN FORWARD GALLEY, SEAT ROW 1 LOW LEVEL EVACUATION LIGHT, MAIN ENTRY DOOR EXIT SIGN, ESCAPE SLIDE LIGHT FOR FORWARD SERVICE DOOR, SEAT ROWS 2 AND 3 BULLNOSE LIGHTS, EXTERIOR
- [SDR USAASB99082](https://openairdocs.org/sdr/USAASB99082.md): Battery Pack · discharged · Mar 28, 1999 · N592US · Boeing 737301 · Emergency Lighting
  > ALB - MAINTENANCE FOUND THE LOWER SIDEWALL EMERGENCY EXIT SIGNS FOR THE FORWARD ENTRY DOOR AND SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB98100](https://openairdocs.org/sdr/USAASB98100.md): Charger · failed · Apr 18, 1998 · N592US · Boeing 737301 · Emergency Lighting
  > CLE - MAINTENANCE FOUND THE EMERGENCY AISLE LIGHTS INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE M1132 EMERGENCY LIGHT CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (X)
- [SDR USAA970297](https://openairdocs.org/sdr/USAA970297.md): Floor Beam · corrosion · Oct 10, 1997 · N592US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - DURING Q-6 VISUAL INSPECTION, FOUND CORROSION AROUND SCREW HOLES ON FLOOR BEAM STA 344 RBL 2 AND 10. CORROSION TASK NR C53-107-02. REMOVED AND REPLACED T-CAP PER TYPICAL REPAIR DOCUMENT 53-10-03. (X)
- [SDR USAA970296](https://openairdocs.org/sdr/USAA970296.md): Floor Beam · corrosion · Oct 10, 1997 · N592US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - DURING Q-6 VISUAL INSPECTION, FOUND CORROSION AROUND SCREW HOLES ON FLOOR BEAM STA 344 LBL 9.5, 21, 28, AND 49. CORROSION TASK NR C53-107-02. REMOVED AND REPLACED T-CAP PER TYPICAL REPAIR DOCUMENT 53-10-03. (X)
- [SDR USAA970295](https://openairdocs.org/sdr/USAA970295.md): Floor Beam · corrosion · Oct 10, 1997 · N592US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - DURING Q-6 VISUAL INSPECTION, FOUND A CORRODED AREA OF 6 INCH BY 3 INCH STA 947 BL ZERO ON FLOOR BEAM. CORROSION TASK NR C53-107-02. INSTALLED DOUBLER ON FLOOR BEAM 947 LBL 8- RBL 8 PER SRM 53-00-51. (X)
- [SDR USAASB96192](https://openairdocs.org/sdr/USAASB96192.md): Door · not closed · Sep 13, 1996 · N592US · Boeing 737301 · Accessory Compartment Doors
  > CLT - FLT 1635 - AIRCRAFT DEVELOPED AN AIRFRAME VIBRATION AT LEVEL OFF AT FL 260. AFTER CHECKING THAT ALL AIRCRAFT SYSTEMS WERE NORMAL, THE CAPTAIN DECIDED TO DIVERT TO CLT. THE CAPTAIN BELIEVED THERE WAS AN ACCESS DOOR OPEN. THE FLIGHT LANDED WITH NO FURTH
- [SDR USAASB95005](https://openairdocs.org/sdr/USAASB95005.md): Oil Qty Xmitter · failed · Oct 28, 1995 · N592US · Boeing 737301 · Engine Oil Indicating System
  > STL - FLT NR 0091 - EN ROUTE FROM PIT TO SAN, NR 2 ENGINE OIL QUANTITY FELL TO ZERO AND OIL PRESSURE WAS FLUCTUATING BETWEEN 35 AND 40 PSI. FLIGHT CREW ACCOMPLISHED A PRECAUTIONARY ENGINE SHUTDOWN AND DIVERTED TO STL WHERE LANDING WAS WITHOUT INCIDENT. MAINT
- [SDR USAA950544](https://openairdocs.org/sdr/USAA950544.md): Control Unit · failed · May 29, 1995 · N592US · Boeing 737301 · Brake Anti-Skid Section
  > BWI - FLT 126 - FLIGHT EN ROUTE MCO TO DCA WHEN ANTI-SKID INOP LIGHT ILLUMINATED. FLIGHT DIVERTED TO BWI DUE TO RUNWAY LENGTH. MAINTENANCE REPLACED ANTI-SKID CONTROL UNIT. (M)
- [SDR USAA950448](https://openairdocs.org/sdr/USAA950448.md): Circuit Breaker · failed · Apr 29, 1995 · N592US · Boeing 737301 · Engine Oil Indicating System
  > PHL - FLT 941 - FLIGHT EN ROUTE BOS TO DCA, WHEN NR 1 ENGINE OIL TEMPERATURE AND PRESSURE INDICATORS DROPPED TO ZERO. CREW SHUT DOWN NR 1 ENGINE AND DIVERTED TO PHL WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE RESET D8 CIRCUIT BREAKER. ALL ENGINE
- [SDR USAA950382](https://openairdocs.org/sdr/USAA950382.md): Csd · failed · Apr 18, 1995 · N592US · Boeing 737301 · Alternator-Generator Drive
  > PIT - FLT 1669 - AFTER TAKEOFF FROM PHL EN ROUTE TO LAS, NR 1 CSD LOW OIL PRESSURE LIGHT ILLUMINATED FOLLOWED BY NR 1 ENGINE GENERATOR DROPPING OFF LINE. CREW DISCONNECTED NR 1 CSD AND DIVERTED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE R

## 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 = 'N592US' AND deregistration_id = 'N592US-2008-03-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N592US-2008-03-28/reports

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