# Service difficulty reports: N526AU, cancelled Aug 25, 2008

A list on [N526AU, cancelled Aug 25, 2008](https://openairdocs.org/deregistered/N526AU-2008-08-25.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 · 86 reports

- [SDR USAA920081310](https://openairdocs.org/sdr/USAA920081310.md): Battery · discharged · Jul 2, 2008 · N526AU · Boeing 7373B7 · Emergency Lighting
  > MCN - B01 - EEL - SEVERAL EMERGENCY LIGHTS OUT IN CABIN. REPLACED CENTER EMERGENCY BATTERY IAW B737 AMM 33-51-51-2. (S)
- [SDR USAA920080651](https://openairdocs.org/sdr/USAA920080651.md): Skin · cracked · Mar 20, 2008 · N526AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - MAJOR REPAIR - C6 CHECK - CRACKED FUSELAGE SKIN BS 727E, S22L. REPAIRED FUSELAGE SKIN, BS 727E. S22L IAW B737 SRM 53-00-01.
- [SDR USAA920080652](https://openairdocs.org/sdr/USAA920080652.md): Flap · delaminated · Mar 16, 2008 · N526AU · Boeing 7373B7 · Trailing Edge Flaps
  > CLT - MAJOR REPAIR - C6 CHECK - RIGHT WING OUTBOARD TRAILING EDGE FLAP HAS AREA OF DELAMINATION. REPLACED RIGHT WING OUTBOARD TRAILING EDGE FLAP IAW B737 SRM 27-51-39.
- [SDR SB07084](https://openairdocs.org/sdr/SB07084.md): Light · none · Sep 28, 2007 · N526AU · Boeing 7373B7 · Light System Wiring
  > DFW - MAINTENANCE REPORTED THE FLOOR EMERGENCY ESCAPE PATH LIGHTING AT SEAT ROWS 9 AND 11, LEFT-HAND SIDE, INOPERATIVE. MAINTENANCE FOUND THAT THIS IS A NORMAL SITUATION. THESE LIGHTS ARE NOT OPERATIONAL PER MM 33-51-12-0, SECTION 3, PARAGRAPH A, SENTENCE 4.
- [SDR USAA070260](https://openairdocs.org/sdr/USAA070260.md): Skin · cracked · Apr 4, 2007 · N526AU · Boeing 7373B7 · Leading Edge Devices
  > SEVERAL.125 INCH CRACKS, NR 2 SLAT LOWER TRAILING EDGE SKIN BETWEEN HET TUBE & INBOARD AUX TRACK HAS CRACK. CUT OUT DAMAGE & INSTALLED DOUBLER PER SRM 57-43-01, DEFECT SIZE:.125 INCH.
- [SDR USAA200701004](https://openairdocs.org/sdr/USAA200701004.md): Tie Clip · cracked · Jan 19, 2007 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > A 1 INCH CRACK FOUND AT STA 294.5, STR 11, CLIP. REMOVED & REPLACED CRACKED TIE CLIP PER EO 5305V203 (DROP-IN A/C).
- [SDR USAASB06102](https://openairdocs.org/sdr/USAASB06102.md): Windshield · cracked · Oct 19, 2006 · N526AU · Boeing 7373B7 · Flight Compartment Windows
  > PHL FLT1428 - EN ROUTE FROM RDU TO PHL, CREW REPORTED THE CAPTAINS'S NR 1 WINDOW OUTER PANE CRACKED. OBSERVED ARCING FROM THE UPPER RIGHT SIDE, THEN CRACKING. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S WINDSHIELD
- [SDR USAA060591](https://openairdocs.org/sdr/USAA060591.md): Skin · cracked · Apr 18, 2006 · N526AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > FOUND SKIN CRACKED, BS 328 S17R. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER IAW SRM 53-10-01 REP 2, DEFECT SIZE:.75".
- [SDR USAA050880](https://openairdocs.org/sdr/USAA050880.md): Flange · worn · Jul 14, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Keel
  > CLT - Q2 - KEELBEAM FLANGE, 60 INCHES SURFACE WEAR. FUSELAGE KEELBEAM LT OB FLANGE STA 664-727. INSTALLED REPAIR STRAP IAW EA. (K)
- [SDR USAA050838](https://openairdocs.org/sdr/USAA050838.md): Stiffener · corroded · Jul 7, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - FOUND STIFFENER CORRODED 2 INCHES, STATION 227.8, BL 0 ON VERTICAL STIFFENER. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS IAW EA 69945. (M)
- [SDR USAA050839](https://openairdocs.org/sdr/USAA050839.md): Beam · cracked · Jul 7, 2005 · N526AU · Boeing 7373B7 · Ailerons
  > CLT - FOUND BEAM CRACKED 1.25 INCH, AFT OF RIGHT AILERON AT TRAILING EDGE. INSTALLED A NEW BEAM IAW SRM 57-51-02. (M)
- [SDR USAA050840](https://openairdocs.org/sdr/USAA050840.md): Angle · corroded · Jul 7, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - FOUND TRANSITION ANGLE CORRODED, TRANSITION ANGLE IN AFT CARGO BETWEEN STATION 727C AND STATION 827. REMOVED DAMAGE, INSTALLED TRANSITION ANGLE IAW SRM 51-10-02. (M)
- [SDR USAA050841](https://openairdocs.org/sdr/USAA050841.md): Floorbeam · corroded · Jul 7, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM TEE CAP CORRODED 1 INCH, AT BS 986.5, LBL 31. REMOVED AND REPLACED UPPER T-CAP OF FLOORBEAM IAW TYPICAL REPAIR 53-10-05, SRM 53-00-51. (M)
- [SDR USAA050842](https://openairdocs.org/sdr/USAA050842.md): Intercostal · cracked · Jul 7, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - FOUND INTERCOSTAL SUPPORT CRACKED 1.4 INCHES, FS 295 AT STRINGER S16L. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 53-10-15M SRM 51-10-02. (M)
- [SDR USAA050843](https://openairdocs.org/sdr/USAA050843.md): Stiffener · corroded · Jul 7, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - FOUND STIFFENER CORRODED 2 INCHES, STATION 227.8, BL 0 ON VERTICAL STIFFENER. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS IAW EA 69945. (M)
- [SDR USAA050844](https://openairdocs.org/sdr/USAA050844.md): Angle · corroded · Jul 7, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > FOUND CHORD ANGLE CORRODED.8 INCHES, LOWER CHORD ANGLE AT BS 227.8. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR PARTS IAW EA 96645 AND BOEING DWG 69-38740. (M)
- [SDR USAA050845](https://openairdocs.org/sdr/USAA050845.md): Intercostal · corroded · Jul 7, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - FOUND INTERCOSTAL CORRODED 6 INCHES, AFT OF FORWARD E/E DOOR AT BL 0, BS 219.8 TO 227.8. REMOVED CORRODED INTERCOSTAL. FABRICATED AND INSTALLED NEW PART IAW EA 96645 AND BOEING DWG 69-38740. (M)
- [SDR USAA050846](https://openairdocs.org/sdr/USAA050846.md): Skin · delaminated · Jul 7, 2005 · N526AU · Boeing 7373B7 · Elevator, Plate/Skin
  > CLT - FOUND ELEVATOR TOP SKIN CRACKED 3 INCHES TOP SURFACE. MAJOR, COMPOSITE REPAIR IAW EA 96681. (M)
- [SDR USAA050832](https://openairdocs.org/sdr/USAA050832.md): Stringer · corroded · Jul 5, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND STRINGER CORRODED 12 INCHES, CARGO FLOOR STRINGERS AT STATION 773. REPLACED OUT OF LIMITS STRINGER SECTIONS IAW SRM 53-60-53 AND TR 53-10-06B. (M)
- [SDR USAA050833](https://openairdocs.org/sdr/USAA050833.md): Angle · corroded · Jul 5, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - FOUND TRANSITION ANGLE CORRODED 8 INCHES, IN AFT CARGO BETWEEN STATION 727C AND STATION 827. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-10-02. (M)
- [SDR USAA050834](https://openairdocs.org/sdr/USAA050834.md): Web · corroded · Jul 5, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB CORRODED 10 INCHES, UNDER STRAP AT THE AFT CARGO COMPARTMENT DOOR OPENING. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW PART IAW BOEING DWG 65-47957 AND SRM 51-10-02. (M)
- [SDR USAA050835](https://openairdocs.org/sdr/USAA050835.md): Stringer · corroded · Jul 5, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > CLT - FOUND STRINGERS CORRODED 12 INCHES, CARGO FLOOR STRINGERS AT STATION 773. REPLACE OUT OF LIMITS STRINGER SECTION IAW SRM 53-60-53 AND TR 53-10-06B. (M)
- [SDR USAA050823](https://openairdocs.org/sdr/USAA050823.md): Skin · dented · Jul 1, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN DENTED 2 INCHES BY 2 INCHES, DENT ONE BS 500-500A, S20R-S21R, DENT 2 AND 3 AT BS 500A-500B S19R-S20R. CUT OUT THREE DENTS, FABRICATED TRIPLERS, SIZE OF REPAIR IS 44.5 INCH BY 23 AT 10.22 LBS IAW SRM 53-00-01. (M)
- [SDR USAA050819](https://openairdocs.org/sdr/USAA050819.md): Angle · corroded · Jun 30, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - FOUND TRANSITION ANGLE CORRODED 8 INCHES, IN AFT CARGO BETWEEN STATION 727C AND AND STATION 827. REMOVED CORRODED ANGLE AND INSTALLED NEW ANGLE IAW SRM 51-10-02. (M)
- [SDR USAA050820](https://openairdocs.org/sdr/USAA050820.md): Web · corroded · Jun 30, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - FOUND WEB CORRODED 10 INCHES, WEB UNDER STRAP AT THE AFT CARGO COMPARTMENT DOOR OPENING. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW PART IAW BOEING DWG 65-47957 AND SRM 51-10-02. (M)
- [SDR USAA050812](https://openairdocs.org/sdr/USAA050812.md): Support Angle · cracked · Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - Q2 - SUPPORT ANGLE, 1 INCH, CRACK, STA 540 AND STR 22R. FABRICATED AND INSTALLED REPAIR PART. (K)
- [SDR USAA050811](https://openairdocs.org/sdr/USAA050811.md): Bracket · worn · Jun 29, 2005 · N526AU · Boeing 7373B7 · Wing, Attach Fittings
  > CLT - Q2 - ANGLE BRACKET, 2 INCHES X 3 INCHES, WORN AND CHAFED AREA, LWR WING PANEL OB OF NR 2 FLAP TRACK. FABRICATED AND INSTALLED NEW ANGLE IAW SRM. (K)
- [SDR USAA050810](https://openairdocs.org/sdr/USAA050810.md): Skate Angle · worn · Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage, Stabilizer Attach Fittings
  > CLT - Q2 - SKATE ANGLE, 2 INCHES X 4 INCHES, WORN AREA, AFT END OF THE RT SKATE ANGLE AT THE BASE OF THE VERTICAL FIN TO FUSELAGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS. (K)
- [SDR USAA050809](https://openairdocs.org/sdr/USAA050809.md): Angle · corroded · Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - Q2 - L-ANGLE, 6 INCH FRETTING, L-ANGLE AT BS 1016 FORWARD OF THE RT FWD VERTICAL FIN MOUNT. FABRICATED AND REPLACED NEW L ANGLE. (K)
- [SDR USAA050808](https://openairdocs.org/sdr/USAA050808.md): Angle · cracked · Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - Q2 - HORIZONTAL ANGLE, 1 INCH CRACK, STA 695 LT OF BL0. REMOVED FABRICATED AND INSTALLED NEW L ANGLE IAW DWG. (K)
- [SDR USAA050807](https://openairdocs.org/sdr/USAA050807.md): Floor Support · cracked · Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - Q2 - FLOOR SUPPORT, 1 INCH CRACK, FLOOR SUPPORT AT STA 500D IN A/C DISTRIBUTION BAY. REMOVED DAMAGED WEB, FABRICATED NEW WEB IAW SRM. (K)
- [SDR USAA050806](https://openairdocs.org/sdr/USAA050806.md): Intercostal · dented · Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - Q2 - INTERCOSTAL, 2 INCHES X 1 INCH, DENT, STR 25L BETWEEN FRAMES 440 AND 420. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DRWG. (K)
- [SDR USAA050805](https://openairdocs.org/sdr/USAA050805.md): Mount · corroded · Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Attach Fittings
  > CLT - Q2 - LAV MOUNT, 1 INCH X 3 INCHES, CORROSION, LT AFT LAV OB MOUNT. FABRICATED AND INSTALLED NEW MOUNT IAW WITH DRWG. (K)
- [SDR USAA050804](https://openairdocs.org/sdr/USAA050804.md): Threshold · corroded · Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - Q2 - WEB, 48 INCHES, CORROSION FWD ENTRY DOORWAY THRESHOLD WEB. FABRICATED WEB AND ASSOCIATED REPAIR PARTS AND INSTALLED DRWG IAW SRM. (K)
- [SDR USAA050803](https://openairdocs.org/sdr/USAA050803.md): Stringer · corroded · Jun 29, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > CLT - Q2 - CARGO FLOOR STRINGER, 6 INCH, CORROSION, AFT CARGO FLOOR STRINGERS AT STA 736 FROM LBBL 17.2 TO RBBL 13.8. REMOVED AND TREATED CORROSION IAW SRM. (K)
- [SDR USAA050781](https://openairdocs.org/sdr/USAA050781.md): Splice · cracked · Jun 20, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - FOUND STRINGER SPLICE CRACKED,.4 INCH AND.3 INCH, STATION 908, S4L. REMOVED OLD STRINGER SPLICE, INSTALL NEW SPLICE IAW SRM 53-00-01 FIG 229. (M)
- [SDR USAA050780](https://openairdocs.org/sdr/USAA050780.md): Channel · worn · Jun 20, 2005 · N526AU · Boeing 7373B7 · Fuselage, Stabilizer Attach Fittings
  > CLT - FOUND L-CHANNEL FRETTING WEAR.5 INCH BY 3 INCHES, FORWARD OF THE LEFT FORWARD VERTICAL FIN MOUNT AT BS 1016 NR 2412. FABRICATED NEW ANGLE AND INSTALLED IAW SRM 53-20-05. (M)
- [SDR USAA050779](https://openairdocs.org/sdr/USAA050779.md): Tear Strap · debonded · Jun 20, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Structure
  > CLT - FOUND TEAR STRAP DISBOND 15 INCHES, BS 867-887, S17-19 RT. INSTALLED RIVETS THROUGH SKIN AND STRAPS AS REQUIRED IAW SRM 53-00-01 FIG 225. (M)
- [SDR USAA050778](https://openairdocs.org/sdr/USAA050778.md): Tear Strap · debonded · Jun 20, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Structure
  > CLT - FOUND TEAR STRAP DISBOND 8 INCHES, BS 857, S16R-S17R. INSTALLED RIVETS TO SECURE IAW SRM 53-00-01, FIG 225 DET 3. (M)
- [SDR USAA050777](https://openairdocs.org/sdr/USAA050777.md): Tear Strap · debonded · Jun 20, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Structure
  > CLT - FOUND DEBONDED TEAR STRAP 11 INCHES, BS 877, S16R-17R. ADDED RIVETS IAW SRM 53-00-01 FIG 225 DET 3. (M)
- [SDR USAA050775](https://openairdocs.org/sdr/USAA050775.md): Frame · cracked · Jun 20, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Frame
  > CLT - FOUND FRAME CRACKED.25 INCH, STATION 827 STRINGER 9L. CUT OUT CRACK, INSTALLED NEW REPAIR ANGLES IAW 53-10-20B. (M)
- [SDR USAA050774](https://openairdocs.org/sdr/USAA050774.md): Floorbeam · corroded · Jun 16, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > FOUND FLOORBEAM CORRODED 3 INCHES, BS 967, LBL 43. FABRICATED NEW T-CAP FOR FLOORBEAM PER SRM 53-00-51, SAME AS PREVIOUS REPAIR. (M)
- [SDR USAA050773](https://openairdocs.org/sdr/USAA050773.md): Skin · gouged · Jun 16, 2005 · N526AU · Boeing 7373B7 · Trailing Edge Flaps
  > CLT - FOUND SKIN GOUGED.125 INCH BY 1 INCH BY.060 INCH, LEADING EDGE RADIUS OF LEFT FOR FLAP.22 INCH FROM INBOARD END. REMOVED DAMAGED AREA, 2.5 INCH BY 1 INCH, INSTALLED EXTERNAL DOUBLER 7.5 INCH BY 6 INCHES IAW SRM 57-53-01 FIG 201. (M)
- [SDR USAA050772](https://openairdocs.org/sdr/USAA050772.md): Angle · corroded · Jun 16, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - FOUND TRANSITIONAL ANGLE CORRODED 2 SQUARE INCHES, UNDERSIDE OF NUTPLATE OF RIGHT TRANSITION ANGLE AT DOOR FRAME BS 496. REMOVED DAMAGE, FABRICATED REPAIR AND REPLACEMENT PART INSTALLED IAW 737 SRM 51-10-02. (M)
- [SDR USAA050771](https://openairdocs.org/sdr/USAA050771.md): Angle · corroded · Jun 16, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - FOUND TRANSITION ANGLE CORRODED 3 INCHES, RT TRANSITION ANGLE AT BS 492.4. REMOVED DAMAGED PART. FABRICATED AND INSTALLED NEW PART IAW 737 SRM 51-10-02. (M)
- [SDR USAA050770](https://openairdocs.org/sdr/USAA050770.md): Support Angle · cracked · Jun 16, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - FOUND SUPPORT ANGLE CRACKED 1 INCH, LOWER EDGE OF INTERCOSTAL AT FORWARD SIDE OF STATION 328, RBL 32. REMOVED DAMAGED STIFFENER, FABRICATED REPLACEMENT PART, AND INSTALLED. (M)
- [SDR USAA050769](https://openairdocs.org/sdr/USAA050769.md): Floorbeam · corroded · Jun 16, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CLT - FOUND FLOORBEAM T-CAP CORRODED 1 INCH, AT BS 986.5, LBL 31. REMOVED AND REPLACED UPPER T-CAP OF FLOORBEAM IAW TYPICAL REPAIR 53-10-05 AND SRM 53-00-51. (M)
- [SDR USAA050749](https://openairdocs.org/sdr/USAA050749.md): Angle · cracked · Jun 9, 2005 · N526AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - FOUND L-ANGLE CRACKED 4 INCHES, RT SIDE STATION 291.5-295.5 AT FLOOR LEVEL. REMOVED DAMAGED. FABRICATED AND INSTALLED REPAIR PART IAW BOEING DWG 69-37402. (M)
- [SDR USAA050742](https://openairdocs.org/sdr/USAA050742.md): Skin · cracked · Jun 8, 2005 · N526AU · Boeing 7373B7 · Nacelle/Pylon, Bulkhead/Firewall
  > CLT - FOUND SKIN CRACKED 1 INCH, NR 2 PYLON LEADING EDGE SKIN. TRIMMED OUT DAMAGE FABRICATED AND INSTALLED FILLER AND DOUBLER. (M)
- [SDR USAA050743](https://openairdocs.org/sdr/USAA050743.md): Stringer Clip · cracked · Jun 8, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, Attach Fittings
  > CLT - FOUND TIE CLIP CRACKED.5 INCH, STATION 480 STRINGER 15R. REPLACED TIE CLIP IAW SRM 51-10-02. (M)

Next page: https://openairdocs.org/deregistered/N526AU-2008-08-25/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 = 'N526AU' AND deregistration_id = 'N526AU-2008-08-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N526AU-2008-08-25/reports

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