# Service difficulty reports: N506AU, cancelled Sep 29, 2010

A list on [N506AU, cancelled Sep 29, 2010](https://openairdocs.org/deregistered/N506AU-2010-09-29.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 3 · 104 reports

- [SDR USAA2010070991391](https://openairdocs.org/sdr/USAA2010070991391.md): Screw · loose · Jul 9, 2010 · N506AU · Boeing 7373B7 · Emergency Lighting
  > MCN - WEEKLY - EEL - EMERGENCY LIGHTS WILL NOT HOLD A CHARGE IN ROWS 1 THRU 4 & AFT CABIN BULL NOSES LAST 4 POSITIONS DO NOT STAY ILLUMINATED FOR REQUIRED TIME SPAN. TIGHTENED LOOSE SCREW ON LOAD SIDE OF EMERGENCY LIGHTS BREAKER, EMERGENCY LIGHTS NOW STAY ON
- [SDR USAA20100709SB113](https://openairdocs.org/sdr/USAA20100709SB113.md): Screw · loose · Jul 8, 2010 · N506AU · Boeing 7373B7 · Emergency Lighting
  > MCN - MAINTENANCE REPORTED THE EMERGENCY LIGHTS WON'T HOLD A CHARGE AT SEAT ROWS 1 TO 4 AND AT AFT CABIN BULLNOSE IN LAST FOUR POSITIONS. EMERGENCY LIGHTS DON'T STAY ILLUMINATED FOR REQUIRED TIME SPAN. MAINTENANCE FOUND AND TIGHTENED LOOSE SCREW ON LOAD SIDE
- [SDR USAA20100505SB066](https://openairdocs.org/sdr/USAA20100505SB066.md): Battery · faulty · May 3, 2010 · N506AU · Boeing 7373B7 · Smoke Detection
  > CLT - PILOT REPORTED THAT THE RIGHT AFT LAVATORY SMOKE DETECTOR WENT OFF DURING TAXI-OUT. MAINTENANCE REMOVED AND REPLACED THE BATTERY FOR THE RIGHT AFT LAVATORY SMOKE DETECTOR. OPERATIONAL CHECK GOOD.
- [SDR USAA2009092492616](https://openairdocs.org/sdr/USAA2009092492616.md): Stringer · corroded · Sep 22, 2009 · N506AU · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > CLT - C6 - MAJOR REPAIR - CORROSION ON STRINGER BETWEEN BS 978 TO BS 1016, S27L. REPLACED STRINGER BETWEEN BS 978 TO BS 1016, S27L IAW B737 SRM 53-00-03.
- [SDR USAA2009092392601](https://openairdocs.org/sdr/USAA2009092392601.md): Tie Clip · cracked · Sep 22, 2009 · N506AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - C5 - MAJOR REPAIR - CRACK ON STRINGER TIE CLIPS AT BS 986 & BS 1006, S27L. REPLACED STRINGER TIE CLIPS AT BS 986 & BS 1006, S27L IAW BOEING DWG 65-46567.
- [SDR USAA2009092492615](https://openairdocs.org/sdr/USAA2009092492615.md): Skin · corroded · Sep 21, 2009 · N506AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - C6 - MAJOR REPAIR - CORROSION ON FUSELAGE SKIN BETWEEN BS 1016 TO BS 953 & BETWEEN S25L TO S25R. REPAIRED FUSELAGE SKIN BETWEEN BS 1016 TO BS 953 & BETWEEN S25L TO S25R IAW EA 101415.
- [SDR USAA2009012990220](https://openairdocs.org/sdr/USAA2009012990220.md): Skin · cracked · Jan 28, 2009 · N506AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - LINE - MAJOR REPAIR - A 3 INCH CRACK IN FUSELAGE SKIN AT AFT LOWER CORNER OF R1 DOOR, BS 328, WL 208, S17R. REPAIRED FUSELAGE SKIN AT AFT LOWER CORNER OF R1 DOOR, BS 328, WL 208, S17R IAW B737 SRM 53-10-01.
- [SDR USAA920081704](https://openairdocs.org/sdr/USAA920081704.md): Skin · cracked · Sep 21, 2008 · N506AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - C5 - MAJOR REPAIR, CRACK ON FUSELAGE SKIN AT BS 727E BELOW S23L. REPAIRED FUSELAGE SKIN AT BS 727E BELOW S23L IAW B737 SRM 53-00-01 REPAIR NR 31 TEMPORARY REVISION NR 53-33.
- [SDR USAA920081401](https://openairdocs.org/sdr/USAA920081401.md): Battery · discharged · Jul 22, 2008 · N506AU · Boeing 7373B7 · Emergency Equipment
  > FLT 1640 (CLT-EWR) - EMERG EQUIP - EMERGENCY FLASHLIGHT IN AFT GALLEY LIGHT NOT BLINKING. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE AFT GALLEY FLASHLIGHT. OPERATIONAL CHECK WAS GOOD. (A)
- [SDR USAA920080671](https://openairdocs.org/sdr/USAA920080671.md): Stringer · corroded · Mar 22, 2008 · N506AU · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > CLT - MAJOR REPAIR - RON - CORROSION ON STRINGER, BS 1006 - BS 1016, S26R. REPAIRED STRINGER, BS 1006 - BS 1016, S26R IAW B737 SRM 53-60-03.
- [SDR USAA920071350](https://openairdocs.org/sdr/USAA920071350.md): Skin · cracked · Dec 18, 2007 · N506AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - MAJOR REPAIR - A CRACK FOUND ON FUSELAGE SKIN AT BS 520 S10L. INSTALLED REPAIR ON FUSELAGE SKIN AT BS 520, S10L.
- [SDR USAA920070902](https://openairdocs.org/sdr/USAA920070902.md): Skin · cracked · Oct 6, 2007 · N506AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - MAJOR REPAIR - C-4 CHECK, CRACKED FUSELAGE SKIN, BS 767, S21R. REPAIRED FUSELAGE SKIN, BS 767, S21R IAW B737-300 SRM 53-00-01.
- [SDR USAA920070901](https://openairdocs.org/sdr/USAA920070901.md): Web · cracked · Oct 6, 2007 · N506AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - MAJOR REPAIR -C-4 CHECK, CRACKED WEB, BS 727, S18A RIGHT. REPLACED WEB, BS 727, S18A RIGHT IAW B737-300 SRM 51-10-02 AND 51-40-00.
- [SDR USAA920070905](https://openairdocs.org/sdr/USAA920070905.md): Skin · cracked · Oct 5, 2007 · N506AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - MAJOR REPAIR - C-4 CHECK, CRACKED FUSELAGE SKIN, BS 727E - BS 747, S25R. REPAIRED FUSELAGE SKIN, BS 727E - BS 747, S25R IAW B737-300 SRM 53-00-01 REPAIR 31.
- [SDR USAA920070904](https://openairdocs.org/sdr/USAA920070904.md): Strap · cracked · Oct 5, 2007 · N506AU · Boeing 7373B7 · Fuselage Main, Frame
  > CLT - MAJOR REPAIR - C-4 CHECK, CRACKED FRAME STRAP, BS 312, S13L. REPLACED FRAME STRAP, BS 312, S13L IAW BOEING DRAWING 65-17684.
- [SDR USAA920070903](https://openairdocs.org/sdr/USAA920070903.md): Stringer · cracked · Oct 5, 2007 · N506AU · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > CLT - MAJOR REPAIR - C-4 CHECK, CRACKED STRINGER WEB, BS 727, S18A LEFT. REPAIRED STRINGER WEB, BS 727, S18A LEFT IAW USAIRWAYS EA 98912.
- [SDR USAA070664](https://openairdocs.org/sdr/USAA070664.md): Skin · cracked · Aug 24, 2007 · N506AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > STA 727D + 17" TO +19",.5 INCH ABOVE STR 22L CENTER LINE HAS CRACK. DOUBLER REPAIR FROM.050 2024-TS INSTALLED PER SRM 53-00-01, REP 31, DEFECT SIZE: 2 INCHES.
- [SDR SB07071](https://openairdocs.org/sdr/SB07071.md): Solenoid · faulty · Aug 22, 2007 · N506AU · Boeing 7373B7 · Landing Gear Selector
  > CLT - AFTER TAKEOFF FROM CLT, DURING GEAR RETRACTION FROM UP TO OFF, CREW RECEIVED TWO MAIN LANDING GEAR RED LIGHTS AND A LEFT MAIN LANDING GEAR GREEN LIGHT. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACE
- [SDR SB07062](https://openairdocs.org/sdr/SB07062.md): Light · inoperative · Aug 8, 2007 · N506AU · Boeing 7373B7 · Emergency Lighting
  > DCA - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. MAINTENANCE REPAIRED THE LIGHT ASSEMBLY AT SEAT 22C. OPERATIONAL CHECK GOOD.
- [SDR SB07032](https://openairdocs.org/sdr/SB07032.md): Battery Pack · discharged · Apr 19, 2007 · N506AU · Boeing 7373B7 · Emergency Lighting
  > BOS - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE AFT RIGHT REAR GALLEY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT BATTERY PACK. OPERATIONAL CHECK GOOD.
- [SDR SB07026](https://openairdocs.org/sdr/SB07026.md): Battery Pack · discharged · Apr 10, 2007 · N506AU · Boeing 7373B7 · Emergency Lighting
  > CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AFT OF SEAT ROW 16 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK FOR AFT SECTION OF SEAT MOUNTED EMERGENCY LIGHTS. OPERATIONAL CHECK GOOD.
- [SDR USAA061348](https://openairdocs.org/sdr/USAA061348.md): Panel · cracked · Nov 20, 2006 · N506AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > STA 685 AT KEELBEAM PANEL CRACKED. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED IAW BOEING DWG 65-45866, DEFECT SIZE: 2 INCHES.
- [SDR USAA061334](https://openairdocs.org/sdr/USAA061334.md): Tee Fitting · cracked · Nov 13, 2006 · N506AU · Boeing 7373B7 · Wing, Attach Fittings
  > LEFT WING STA 135 INTERNAL CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW EA 98206, DEFECT SIZE: 2 INCHES.
- [SDR USAA061335](https://openairdocs.org/sdr/USAA061335.md): Angle · cracked · Nov 13, 2006 · N506AU · Boeing 7373B7 · Wing, Attach Fittings
  > LOWER TEE ANGLE INSIDE OF RIGHT WING FUEL TANK AT WS 135 CRACKED. REMOVED DAMAGE, FABRICATED REPAIR TEE, FILLER AND DOUBLER AND INSTALLED IAW EA 98207, DEFECT SIZE: 2.0 INCH.
- [SDR USAA061336](https://openairdocs.org/sdr/USAA061336.md): Spar · cracked · Nov 13, 2006 · N506AU · Boeing 7373B7 · Wing Spar
  > LEFT WING REAR SPAR STA 223 CRACKED. REMOVED AND REPLACED IMG BEAM SUPPORT FITTING PER EA 98203, DEFECT SIZE:.125 INCH.
- [SDR USAA061331](https://openairdocs.org/sdr/USAA061331.md): Door Frame · cracked · Nov 7, 2006 · N506AU · Boeing 7373B7 · Fuselage Main, Structure
  > FWD SERVICE DOOR FWD STUB FRAME CRACKED. REMOVED DAMAGED FRAME AND FABRICATED REPAIR PARTS AND INSTALLED NEW FRAME IAW SRM 51-20-01, DEFECT SIZE:.125 INCH.
- [SDR USAA061332](https://openairdocs.org/sdr/USAA061332.md): Intercostal · cracked · Nov 7, 2006 · N506AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > BS 344 STR 3R CRACKED. REMOVED DAMAGED INTERCOSTAL AND FABRICATED INTERCOSTAL/WEB IAW EA 98233, DEFECT SIZE:.25 INCH.
- [SDR USAA061320](https://openairdocs.org/sdr/USAA061320.md): Intercostal · cracked · Nov 6, 2006 · N506AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > BS 294.5 AND STR 7L CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-02, DEFECT SIZE: 1 INCH.
- [SDR USAA061325](https://openairdocs.org/sdr/USAA061325.md): Skin · delaminated · Nov 6, 2006 · N506AU · Boeing 7373B7 · Trailing Edge Flaps
  > LEFT I/B AFT FLAP O/B END LWR SIDE DELAMINATED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: 5.250 X 11 INCHES.
- [SDR USAA061324](https://openairdocs.org/sdr/USAA061324.md): Intercostal · cracked · Nov 6, 2006 · N506AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > STR 14 BETWEEN STA 277 AND STA 294.5 CRACKED. REMOVED DAMAGED INTERCOSTAL AND INSTALLED NEW PART IAW DWG 65-45807, DEFECT SIZE:.250 INCH.
- [SDR USAA061323](https://openairdocs.org/sdr/USAA061323.md): Spar · cracked · Nov 6, 2006 · N506AU · Boeing 7373B7 · Wing, Landing Gear Attach Fittings
  > LEFT LG REAR SPAR UPPER CHORD CRACKED. REAMED AND REWORKED FASTENER HOLE IAW EO 5702V054, DEFECT SIZE:.25 INCH.
- [SDR USAA061321](https://openairdocs.org/sdr/USAA061321.md): Skin · cracked · Nov 6, 2006 · N506AU · Boeing 7373B7 · Service Doors
  > FWD GALLEY DOOR INNER SKIN CRACKED. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW TR 52-10-16, DEFECT SIZE: 1 INCH.
- [SDR USAA061310](https://openairdocs.org/sdr/USAA061310.md): Structure · cracked · Nov 6, 2006 · N506AU · Boeing 7373B7 · Wing Miscellaneous Structure
  > LEFT WING STA 135 INTERNAL CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW EA 98206, DEFECT SIZE: 2.5 INCHES.
- [SDR USAA061319](https://openairdocs.org/sdr/USAA061319.md): Skin · cracked · Nov 6, 2006 · N506AU · Boeing 7373B7 · Service Doors
  > FWD GALLEY DOOR INNER SKIN CRACKED. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW TR 52-10-16, DEFECT SIZE: 1 INCH.
- [SDR USAA061318](https://openairdocs.org/sdr/USAA061318.md): Frame · cracked · Nov 6, 2006 · N506AU · Boeing 7373B7 · Fuselage Main, Frame
  > BS 291.5 BETWEEN STR 11R AND 10R CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW DWG 65-45807, DEFECT SIZE: 2 INCHES.
- [SDR USAA061317](https://openairdocs.org/sdr/USAA061317.md): Angle · corroded · Nov 6, 2006 · N506AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > STA 312 360 AT ENTRY DOOR HAS CORROSION. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM 51-10-02 LEVEL 1 C53-107-02, DEFECT SIZE: 48 INCHES.
- [SDR USAA061316](https://openairdocs.org/sdr/USAA061316.md): Support Angle · cracked · Nov 6, 2006 · N506AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > BETWEEN STA 291.5 AND LOWER STUB FRAME FOR RIGHT SERVICE DOOR CUTOUT. FABRICATED REPAIR ANGLE AND INSTALLED IAW SRM 51-10-02, DEFECT SIZE: 1 INCH.
- [SDR USAA061315](https://openairdocs.org/sdr/USAA061315.md): Angle · cracked · Nov 6, 2006 · N506AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > STA 360 STR 15L ANGLE CRACKED. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM 51-10-02, DEFECT SIZE: 1 INCH.
- [SDR USAA061313](https://openairdocs.org/sdr/USAA061313.md): Angle · corroded · Nov 6, 2006 · N506AU · Boeing 7373B7 · Fuselage Main, Structure
  > STA 312 TO 360 AT ENTRY DOOR HAS CORROSION. REMOVE AND REPLACE IAW SRM 51-10-02 LEVEL 1 C53-107-02, DEFECT SIZE: 48 INCHES.
- [SDR USAA061312](https://openairdocs.org/sdr/USAA061312.md): Angle · corroded · Nov 6, 2006 · N506AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > AFT CARGO RT SIDE FROM STA 747-767 HAS CORROSION. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW SRM 53-30-53 LEVEL 2 C53-202-01, DEFECT SIZE: 20 INCHES.
- [SDR USAA061311](https://openairdocs.org/sdr/USAA061311.md): Floorbeam · corroded · Nov 6, 2006 · N506AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > STA 344 24 INCHES FROM LEFT OF BUTT LINE -0- HAS CORROSION. INSTALLED NEW T-CAP SECTION, IAW SRM 53-10-51 FIG 201 LEVEL 1 C53-107-02, DEFECT SIZE: 1 X 1 INCH.
- [SDR USAA061322](https://openairdocs.org/sdr/USAA061322.md): Spar · cracked · Nov 6, 2006 · N506AU · Boeing 7373B7 · Wing, Landing Gear Attach Fittings
  > LEFT LG REAR SPAR UPPER CHORD CRACKED. REAMED AND REWORKED FASTENER HOLE IAW EO 5702V054, DEFECT SIZE:.25 INCH.
- [SDR USAA061299](https://openairdocs.org/sdr/USAA061299.md): Angle · corroded · Nov 1, 2006 · N506AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > AFT RIGHT DOOR ZEE ANGLE BETWEEN STA 917.5 TO STA 1006 CORROSION. REMOVED DAMAGED ZEE ANGLE AND REPLACED WITH NEW ANGLE IAW SRM 51-40-02 C53-107-02 LEVEL 1, DEFECT SIZE: 12 X 3 INCHES.
- [SDR USAA061300](https://openairdocs.org/sdr/USAA061300.md): Angle · cracked · Nov 1, 2006 · N506AU · Boeing 7373B7 · Wing Miscellaneous Structure
  > LOWER TEE ANGLE INSIDE OF RIGHT WING FUEL TANK AT WS 135. REMOVED DAMAGE, FABRICATED REPAIR TEE, FILLER AND DOUBLER INSTALLED IAW EA 98207, DEFECT SIZE: 2.0 INCHES.
- [SDR USAA061301](https://openairdocs.org/sdr/USAA061301.md): Floor Support · corroded · Nov 1, 2006 · N506AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > AFT CARGO RT SIDE FROM STA 747 TO 767 CORROSION. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS LEVEL 2 C53-202-01, DEFECT SIZE: 20 INCHES.
- [SDR USAA061302](https://openairdocs.org/sdr/USAA061302.md): Keelbeam · cracked · Nov 1, 2006 · N506AU · Boeing 7373B7 · Fuselage Main, Keel
  > STA 685 AT KEEL BEAM CRACKED. REMOVED AND REPLACED DAMAGE, DEFECT SIZE: 2 INCHES.
- [SDR USAA061303](https://openairdocs.org/sdr/USAA061303.md): Skin · delaminated · Nov 1, 2006 · N506AU · Boeing 7373B7 · Trailing Edge Flaps
  > LEFT I/B AFT FLAP O/B END LWR SIDE DELAMINATED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: 5.250 X 11 INCHES.
- [SDR USAA061304](https://openairdocs.org/sdr/USAA061304.md): Floorbeam · corroded · Nov 1, 2006 · N506AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > STA 312 BUTT LINE 0 CORROSION. REMOVED DAMAGED SECTION OF TEE CAP AND INSTALLED REPAIR PARTS IAW SRM 53-10-51 LEVEL 2 C53-107-02, DEFECT SIZE:.25 INCH.
- [SDR USAA061305](https://openairdocs.org/sdr/USAA061305.md): Door Frame · cracked · Nov 1, 2006 · N506AU · Boeing 7373B7 · Fuselage Main, Structure
  > FWD CARGO DOOR FRAME AT STA 440 STR 24R LOWER O/B HOLE CRACKED. REMOVED DAMAGE FRAME AND INSTALLED NEW FRAME IAW DWG 6-15224, DEFECT SIZE: 1 INCH.
- [SDR USAA061292](https://openairdocs.org/sdr/USAA061292.md): Angle · corroded · Oct 30, 2006 · N506AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > FOUND Z-ANGLES CORRODED, MAIN ENTRY DOOR SILL SUPPORT STRUCTURE. INSTALLED BLENDED MINOR SURFACE CORROSION IAW SRM 51-10-02 LEVEL 1 C53-107-01, DEFECT SIZE: 10" BY.50".

Next page: https://openairdocs.org/deregistered/N506AU-2010-09-29/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 = 'N506AU' AND deregistration_id = 'N506AU-2010-09-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N506AU-2010-09-29/reports

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