# Service difficulty reports: N373US, cancelled Jul 3, 2006

A list on [N373US, cancelled Jul 3, 2006](https://openairdocs.org/deregistered/N373US-2006-07-03.md).

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

Page 1 of 2 · 67 reports

- [SDR USAA200511006](https://openairdocs.org/sdr/USAA200511006.md): Skin · cracked · Nov 15, 2005 · N373US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > A 2 INCH CRACK IN FUSELAGE SKIN AT STA 892, 6 INCH BELOW STR 24R. INSTALLED REPAIR DOUBLERS PER SRM 53-00-01 FIG 201.
- [SDR SAA200511006](https://openairdocs.org/sdr/SAA200511006.md): Skin · cracked · Nov 15, 2005 · N373US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > A 2 INCH CRACK IN FUSELAGE SKIN AT STA 892, 6 INCHES BELOW STR 24R. INSTALLED REPAIR DOUBLERS PER SRM 53-00-01 FIG 201.
- [SDR USAA050675](https://openairdocs.org/sdr/USAA050675.md): Skin · gouged · May 22, 2005 · N373US · Boeing 7373B7 · Trailing Edge Flaps
  > CLT - FOUND FLAP SKIN GOUGED 1 INCH BY.5 INCH, TOP SKIN OF RIGHT OUTBOARD FOREFLAP. COMPOSITE REPAIR IAW 737-3 SRM 57-53-02 DETAIL XV, TABLE VI. (M)
- [SDR USAA050668](https://openairdocs.org/sdr/USAA050668.md): Skin · debonded · May 20, 2005 · N373US · Boeing 7373B7 · Elevator, Plate/Skin
  > CLT - FOUND ELEVATOR SKIN DISBOND 1 INCH, LEFT ELEVATOR LOWER SURFACE 6.2 INCHES FROM THE OUTBOARD EDGE. COMPOSITE REPAIR IAW SRM 51-70-17. (M)
- [SDR USAA050667](https://openairdocs.org/sdr/USAA050667.md): Skin · cracked · May 20, 2005 · N373US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED.750 INCH, STATION 330, STRINGER 17R. FABRICATED AND INSTALLED SKIN DOUBLERS PER SRM 53-10-01. (M)
- [SDR SB0534](https://openairdocs.org/sdr/SB0534.md): Socket · inoperative · Mar 3, 2005 · N373US · Boeing 7373B7 · Emergency Lighting
  > MCO - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT 12ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT SOCKET AT SEAT 12ABC. OPERATIONAL CHECK GOOD.
- [SDR SB05035](https://openairdocs.org/sdr/SB05035.md): Socket · inoperative · Mar 3, 2005 · N373US · Boeing 7373B7 · Emergency Lighting
  > MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT 12ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT SOCKET AT SEAT 12ABC. OPERATIONAL CHECK GOOD.
- [SDR USAA040112](https://openairdocs.org/sdr/USAA040112.md): Skin · cracked · Apr 5, 2004 · N373US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > FOUND SKIN CRACKED.600 INCH LONG, S-23L AT FS 744. REPAIR DOUBLER INSTALLED PER SRM 53-00-01, FIG 229. (M)
- [SDR USAA040113](https://openairdocs.org/sdr/USAA040113.md): Skin · cracked · Apr 5, 2004 · N373US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > FOUND SKIN CRACKED 1.250 INCH LONG, 3 INCHES FORWARD OF FS 727E ADJACENT TO S-24L. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M)
- [SDR USAA040107](https://openairdocs.org/sdr/USAA040107.md): Skin · cracked · Apr 5, 2004 · N373US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > FOUND SKIN CRACKED 1.250 INCH LONG, INSTALLED DOUBLER PER SRM. 53-00-01, FIG 229. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M)
- [SDR USAA040111](https://openairdocs.org/sdr/USAA040111.md): Skin · cracked · Apr 4, 2004 · N373US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED.600 INCH LONG, S22R 12 INCHES AFT OF FS 727D. INSTALLED DOUBLER PER SRM 53-00-01. (M)
- [SDR USAA040110](https://openairdocs.org/sdr/USAA040110.md): Skin · cracked · Apr 3, 2004 · N373US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > FOUND SKIN CRACKED 1.450 INCH LONG, FS 891 ADJACENT OT S23R. INSTALLED DOUBLER PER SRM 53-00-01. (M)
- [SDR USAA030223](https://openairdocs.org/sdr/USAA030223.md): Skin · cracked · Nov 11, 2003 · N373US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED 2.5 INCHES STATION 765 ABOVE STRINGER 19R. CRACK CUT OUT AND DOUBLER INSTALLED PER SRM 53-00-01. (M)
- [SDR USAA030204](https://openairdocs.org/sdr/USAA030204.md): Skin · cracked · Sep 26, 2003 · N373US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED.25 INCH, AFT SERVICE DOOR UPPER HINGE STATION 951. INSTALLED DOUBLER PER SRM 53-60-01 FIG 205. (M)
- [SDR USAASB03115](https://openairdocs.org/sdr/USAASB03115.md): Clamp · loose · Jul 19, 2003 · N373US · Boeing 7373B7 · Pneumatic Distribution System
  > ON CLIMB-OUT FROM PIT, AT FL170, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. LIGHT EXTINGUISHED WHEN THROTTLE WAS RETARDED. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MAINTENANCE TIGHTENED A LOOSE PNEUMA
- [SDR USAASB03102](https://openairdocs.org/sdr/USAASB03102.md): Charger · inoperative · Jul 5, 2003 · N373US · Boeing 7373B7 · Emergency Lighting
  > PHL - MAINTENANCE REPORTED THE EMERGENCY EXIT AISLE LIGHTS AT SEAT ROWS 12 THROUGH 16 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK, P/N 201301A, AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M)
- [SDR USAASB03072](https://openairdocs.org/sdr/USAASB03072.md): Light · inoperative · May 31, 2003 · N373US · Boeing 7373B7 · Emergency Lighting
  > PILOT REPORTED THE EMERGENCY EXIT LIGHT AT SEAT 12C INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)
- [SDR USAA020464](https://openairdocs.org/sdr/USAA020464.md): Skin · cracked · Nov 21, 2002 · N373US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED 2 INCHES, RIGHT SIDE STATION 727E STRINGER 24 RT. CUTOUT DAMAGE, INSTALLED DOUBLER AND FILLER PER SRM 53-00-01 FIG 225. (M)
- [SDR USAASB02162](https://openairdocs.org/sdr/USAASB02162.md): Socket · shorted · Aug 27, 2002 · N373US · Boeing 7373B7 · Emergency Lighting
  > GSO - MAINTENANCE FOUND THE BULLNOSE EMERGENCY LIGHTS AT SEAT ROWS 12, 16 AND 20 INOPERATIVE. MAINTENANCE FOUND THE LIGHT SOCKET AT SEAT ROW 16 SHORTED. REPAIRED LIGHT SOCKET AND REPLACED ONE BATTERY PACK AND TWO POWER SUPPLIES. OPERATIONAL CHECK NORMAL.
- [SDR USAA020327](https://openairdocs.org/sdr/USAA020327.md): Skin · cracked · Aug 14, 2002 · N373US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED 3.5 INCH, S25R BETWEEN STATION 727E AND 747. INSTALLED DOUBLER PER SRM 53-00-01 FIG 2. (M)
- [SDR USAA020252](https://openairdocs.org/sdr/USAA020252.md): Bulkhead · corroded · Jun 18, 2002 · N373US · Boeing 7373B7 · Fuselage Main, Bulkhead
  > PIT - FOUND Y-CHORD AND BULKHEAD CORRODED, BS 1016 AFT PRESSURE BULKHEAD AT FLOOR LINE CENTER. CORROSION LEVEL 2, REMOVED CORROSION AND INSTALLED DOUBLERS PER EA 74025. (M)
- [SDR USAA020210](https://openairdocs.org/sdr/USAA020210.md): Stiffener · corroded · Jun 5, 2002 · N373US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND STIFFENER CORRODED 3 INCH BY 3 INCH AREA, AFT PRESS BULKHEAD STIFFENER BS 1018 BL 00. INSTALLED DOUBLER, SPLICED SECTION OF STIFFENER PER BOEING DRAWING 65C28106. (M)
- [SDR USAA020209](https://openairdocs.org/sdr/USAA020209.md): Bulkhead · corroded · Jun 5, 2002 · N373US · Boeing 7373B7 · Fuselage Main, Bulkhead
  > PIT - FOUND CHORDS AND WEBS CORRODED 5 INCH BY 6 INCH AREA, FORWARD SIDE AFT PRESSURE BULKHEAD BS 1018 BL 00 4 INCH BY 5 INCH. CORROSION LEVEL 2. BULKHEAD WEB AND CHORDS INSTALLED DOUBLERS PER EA 74025. (M)
- [SDR USAA020208](https://openairdocs.org/sdr/USAA020208.md): Bulkhead · cracked · Jun 4, 2002 · N373US · Boeing 7373B7 · Fuselage Main, Bulkhead
  > PIT - FOUND SKIN CRACKED 1.125 INCH BY 6.625 INCH CRACK, BETWEEN STRINGER 16 AND 17 OUTERSKIN STATION 178. DOUBLER INSTALLED PER EO 5300V157. (M)
- [SDR USAA020207](https://openairdocs.org/sdr/USAA020207.md): Bulkhead · cracked · Jun 4, 2002 · N373US · Boeing 7373B7 · Fuselage Main, Bulkhead
  > PIT - FOUND SKIN CRACKED 7.875 INCH BY 6.75 INCH, BETWEEN STRINGER 16/17, OUTER SKIN STATION 178. DOUBLER INSTALLED PER EO 5300V157. (M)
- [SDR USAA020224](https://openairdocs.org/sdr/USAA020224.md): Floor Support · corroded · May 31, 2002 · N373US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND SUPPORT CORRODED ENTIRE SURFACE, DIAGONAL FLOOR SUPPORT RBBL 12, STATION 987-1016. FOUND DEFECTIVE PART REPLACED WITH IDENT PART NR. CORRODED LEVEL 1, TASK NR C53-107-02. (M)
- [SDR USAA020254](https://openairdocs.org/sdr/USAA020254.md): Clip · corroded · May 30, 2002 · N373US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND CLIP CORRODED, STATION 727E BETWEEN S26R AND S27R. DOUBLER TREATED PER SRM 53-00-07 PAGES 210-212. (M)
- [SDR USAA020260](https://openairdocs.org/sdr/USAA020260.md): Stringer · cracked · May 18, 2002 · N373US · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > PIT - FOUND STRINGER CRACKED.25 INCH, STATION 663 STRINGER 2R. INSTALLED DOUBLERS PER SRM 53-00-07 FIG 209. (M)
- [SDR USAA020259](https://openairdocs.org/sdr/USAA020259.md): Intercostal · cracked · May 15, 2002 · N373US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND INTERCOSTAL CRACKED 1 INCH, UPPER AFT FLANGE INTERCOSTAL BL 0 STATION 294.5-312. INSTALLED NEW INTERCOSTAL PER SRM 51-10-02. (M)
- [SDR USAA020205](https://openairdocs.org/sdr/USAA020205.md): Intercostal · cracked · May 15, 2002 · N373US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND INTERCOSTAL CRACKED 1.5 INCH, JUST ABOVE AFT ENTRANCE DOOR BS 967. INSTALLED NEW ATTACH ANGLE. (M)
- [SDR USAA020261](https://openairdocs.org/sdr/USAA020261.md): Frame · cracked · May 14, 2002 · N373US · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED TWO PLACES.125 INCH AND.25 INCH, STATION 380 BETWEEN S8R AND S9R. INSTALLED DOUBLER PER SRM 53-00-07. (M)
- [SDR USAA020256](https://openairdocs.org/sdr/USAA020256.md): Seat Track · corroded · May 14, 2002 · N373US · Boeing 7373B7 · Fuselage, Seat/Cargo Attach Fittings
  > PIT - FOUND LEFT INBOARD SEAT TRACK, STATION 827-945 LBBL 24. CORROSION LEVEL 2. SPLICED IN SECTION OF TRACK PER SRM 53-00-52. (M)
- [SDR USAA020204](https://openairdocs.org/sdr/USAA020204.md): Keelbeam · corroded · May 10, 2002 · N373US · Boeing 7373B7 · Fuselage Main, Keel
  > PIT - FOUND KEEL BEAM CORRODED 3 INCHES BY 1 INCH CORRODED, 13.5.546 STRINGER 28L. CORROSION LEVEL 2, TASK NR C53-212-01. REMOVED DAMAGED AREA, INSTALLED NEW SECTION AND INSTALLED DOUBLER PER EA 73807. (M)
- [SDR USAA020253](https://openairdocs.org/sdr/USAA020253.md): Crease Beam · corroded · May 8, 2002 · N373US · Boeing 7373B7 · Fuselage Main, Structure
  > PIT - FOUND CREASE BEAM CORRODED, STATION 277-360. DEFECTIVE PART REPLACED WITH IDENT PART. (M)
- [SDR USAA020175](https://openairdocs.org/sdr/USAA020175.md): Skin · cracked · May 6, 2002 · N373US · Boeing 7373B7 · Leading Edge Devices
  > PIT - FOUND SKIN CRACKED IN 13 SMALL CONTINUOUS PLACES, RIGHT WING, NR 6 SLAT, LOWER SURFACE SLAT STATION 299.10-314. REMOVED DAMAGED SKIN PER SRM 57-43-01. (M)
- [SDR USAA020257](https://openairdocs.org/sdr/USAA020257.md): Frame · cracked · May 4, 2002 · N373US · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED.25 INCH, STATION 767 BETWEEN S8L AND S9L AT PSU SUPPORT BRACKET. INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14A. (M)
- [SDR USAA020258](https://openairdocs.org/sdr/USAA020258.md): Frame · cracked · May 2, 2002 · N373US · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED.25 INCH, STATION 480 BETWEEN S8R AND S9R. CUT OUT CRACK, INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14A. (M)
- [SDR USAA020176](https://openairdocs.org/sdr/USAA020176.md): Frame · cracked · May 2, 2002 · N373US · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - FOUND Z-FRAME CRACKED.25 INCH, STATION 807 BETWEEN S8R AND S9R. CUT OUT CRACKED, INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14A. (M)
- [SDR USAA020255](https://openairdocs.org/sdr/USAA020255.md): Floor Support · corroded · May 1, 2002 · N373US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > IT - FOUND FLOOR SUPPORT CORRODED, STATION 727-787 AND 787-827 ABOVE S25L. SPLICED IN NEW SECTION PER SRM 53-60-53. (M)
- [SDR USAA020174](https://openairdocs.org/sdr/USAA020174.md): Arm · corroded · Apr 29, 2002 · N373US · Boeing 7373B7 · Rudder Structure
  > PIT - FOUND RUDDER BALANCE ARM WITH CORROSION 3 INCH BY 12 INCH AREA, RUDDER BALANCE ARM STRUCTURE. CORROSION LEVEL 2. RUDDER REPLACED AND INSTALLED PER JOB CARD. (M)
- [SDR USAA020173](https://openairdocs.org/sdr/USAA020173.md): Angle · cracked · Apr 18, 2002 · N373US · Boeing 7373B7 · Vertical Stabilizer Miscellaneous Structure
  > PIT - FOUND DRAG ANGLE CRACKED.5 INCH, SECTION 48, RIGHT SIDE, AFT OF AFT LUGS FOR VERTICAL STABILIZER. FILLERS AND STRAPS INSTALLED ON BOTH SIDES OF DRAG ANGLE PER TYPICAL REPAIR 53-80-03. (M)
- [SDR USAA020206](https://openairdocs.org/sdr/USAA020206.md): Angle · cracked · Apr 17, 2002 · N373US · Boeing 7373B7 · Empennage Flight Control Surfaces, Attach Fittings
  > PIT - FOUND DRAG ANGLE CRACKED.25 INCH, SECT 48 DRAG ANGLE LIGHT SIDE 10 INCH BEHIND ATTACH LUG. REPAIRED FILLER AND STRAPS ON OUTSIDE AND INSIDE OF DRAG ANGLE PER TYPICAL REPAIR 53-80-03. (M)
- [SDR USAASB01175](https://openairdocs.org/sdr/USAASB01175.md): Fuel Cell · leaking · Jun 15, 2001 · N373US · Boeing 7373B7 · Fuel Storage
  > CLT - FLT 1290 - AFTER TAKEOFF, FUEL WAS REPORTED STREAMING OUT OF THE LEFT WING BY AN AMERICAN FLIGHT BEHIND AND WAS ALSO CONFIRMED BY THE CLT TOWER. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO FIELD AT CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENT.
- [SDR USAASB01116](https://openairdocs.org/sdr/USAASB01116.md): Charger · failed · Apr 27, 2001 · N373US · Boeing 7373B7 · Emergency Lighting
  > PHL - MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHTS AT ROWS 1 THROUGH 4 INOPERATIVE AND THE EMERGENCY LIGHTS AT THE FORWARD ENTRY AND SERVICE DOORS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 2013-1A) AND CHAGER ASSEMBLY AT STATION
- [SDR USAASB1017](https://openairdocs.org/sdr/USAASB1017.md): Throttle Cable · failed · Jan 22, 2001 · N373US · Boeing 7373B7 · Power Lever
  > EWR - FLT 1024 - EN ROUTE FROM DCA TO ALB, THE NR 2 THRUST LEVER STUCK AT CLIMB POWER. CREW DISENGAGED AUTO THROTTLES BUT WAS STILL UNABLE TO RETARD THRUST LEVER. CREW DECLARED AN EMERGENCY, ACCOMPLISHED ENGINE SHUTDOWN CHECKLIST AND SHUTDOWN THE NR 2 ENGINE
- [SDR USAASB00274](https://openairdocs.org/sdr/USAASB00274.md): Swivel · broken · Sep 25, 2000 · N373US · Boeing 7373B7 · Hydraulic System, Main
  > BOS - FLT 1090 - EN ROUTE FROM PHL TO BOS, FLT LOST A-SYSTEM HYDRAULIC QUANTITY AND PRESSURE. MX CONTROL ADVISED THAT FLIGHT SHOULD PROCEED TO ORIGIN OR DESTINATION, WHICHEVER WAS CLOSER. FLIGHT WAS CLOSER TO BOS, SO IT CONTINUED ONTO BOS. FLIGHT LANDED WIT
- [SDR USAA001319](https://openairdocs.org/sdr/USAA001319.md): Bulkhead · cracked · Aug 24, 2000 · N373US · Boeing 7373B7 · Fuselage Main, Bulkhead
  > CLT - FOUND BULKHEAD WEB CRACKED.75 INCH, STATION 178 RBL.5, WL 188. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-10-08. (M)
- [SDR USAA000959](https://openairdocs.org/sdr/USAA000959.md): Frame · corroded · Jun 26, 2000 · N373US · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - FOUND FRAME CORRODED 4 INCHES BY 3 INCHES, STATION 1006 AT STRINGER 18 AND 19 RIGHT SIDE. CORROSION LEVEL 2, TASK NR C53-206-01. CUT FRAME AND REPLACED PER SRM 51-20-05, SRM 51-40, SRM 53-00-07 FIG 201. (M)
- [SDR USAASB00098](https://openairdocs.org/sdr/USAASB00098.md): Light · shorted · Apr 3, 2000 · N373US · Boeing 7373B7 · Flight Compartment Lighting
  > IAH - FLT 2231 - ON CLIMB-OUT FROM IAH, AT APPROXIMATELY 9,000 FEET, CAPTAIN REPORTED THERE WAS A LOUD POP AND SPARKS THAT DROPPED DOWN ON THE FIRST OFFICER FROM THE OVERHEAD PANEL. AT 18,000 FEET, ALL APPEARED TO BE OPERATING NORMAL. NO SMOKE OR SMELL OF AN
- [SDR USAA990180](https://openairdocs.org/sdr/USAA990180.md): Web · cracked · Mar 5, 1999 · N373US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - DURING DROP IN VISUAL INSPECTION, FOUND A 4 INCH CRACK AT BS 233, BL 0, WL 192.5 WEB. INSTALLED DOUBLER PER BOEING SRM 51-70-13. (M)

Next page: https://openairdocs.org/deregistered/N373US-2006-07-03/reports.md?page=2

## 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 = 'N373US' AND deregistration_id = 'N373US-2006-07-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N373US-2006-07-03/reports

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