# Service difficulty reports: N527AU, cancelled Mar 30, 2011

A list on [N527AU, cancelled Mar 30, 2011](https://openairdocs.org/deregistered/N527AU-2011-03-30.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 · 82 reports

- [SDR USAA2008123092338](https://openairdocs.org/sdr/USAA2008123092338.md): Skin · cracked · Dec 30, 2008 · N527AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - MAJOR REPAIR - RON - NR 6095204, CRACKED FUSELAGE SKIN AT BS 727E, S24L. REPAIRED FUSELAGE SKIN AT BS 727E, S24L IAW B737 SRM 53-00-01-2R-31.
- [SDR USAA2008121692235](https://openairdocs.org/sdr/USAA2008121692235.md): Skin · cracked · Dec 15, 2008 · N527AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - RON - MAJOR REPAIR - CRACK IN FUSELAGE SKIN AT BS 727D, LBL 24. REPAIRED FUSELAGE SKIN AT BS 727D, LBL 24 IAW B737 SRM 53-00-01 REPAIR 31.
- [SDR USAA920080906](https://openairdocs.org/sdr/USAA920080906.md): Charger · failed · Apr 21, 2008 · N527AU · Boeing 7373B7 · Emergency Lighting
  > MX CHECK - PHL - RIGHT HAND MIDDLE EMERGENCY EXIT LIGHT INOP. MX REPLACED THE BATTERY CHARGER, OPERATIONAL CHECK WAS GOOD.
- [SDR USAA920080196](https://openairdocs.org/sdr/USAA920080196.md): Skin · corroded · Jan 18, 2008 · N527AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - MAJOR REPAIR - RON - CORROSION ON FUSELAGE SKIN, BS 986, S27L - S27R. REPAIRED FUSELAGE SKIN, BS S27L - S27R IAW USAIRWAYS EA 1000160.
- [SDR USAA920080195](https://openairdocs.org/sdr/USAA920080195.md): Shear Tie · corroded · Jan 18, 2008 · N527AU · Boeing 7373B7 · Fuselage Internal Mounting Structure
  > CLT - MAJOR REPAIR - RON - CORROSION ON SHEAR TIE, BS 986, S27L - S27R. REPAIRED SHEAR TIE, BS S27L - S27R IAW B737 SRM 53-00-07.
- [SDR SB07059](https://openairdocs.org/sdr/SB07059.md): Circuit Card · unknown · Aug 3, 2007 · N527AU · Boeing 7373B7 · Landing Gear Position and Warning
  > PHL FLT1407 - AFTER TAKEOFF FROM PHL, CREW RECEIVED BOTH MAIN LANDING GEAR RED UNSAFE LIGHTS AFTER RAISING GEAR AND RETURNING GEAR LEVER TO OFF POSITION. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES, CONSULTED MAINTENANCE AND RETURNED TO FIELD AT PHL
- [SDR SB07040](https://openairdocs.org/sdr/SB07040.md): Slide · no test · May 18, 2007 · N527AU · Boeing 7373B7 · Escape Slide
  > PHL - THE FORWARD RIGHT HAND SERVICE DOOR EMERGENCY ESCAPE SLIDE FAILED THE ANNUAL OPERATIONAL TEST WHEN IT TWISTED DURING DEPLOYMENT. MAINTENANCE REPLACED THE SLIDE. INSPECTED OK FOR SERVICE.
- [SDR USAA200609003](https://openairdocs.org/sdr/USAA200609003.md): Skin · cracked · Sep 17, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > FOUND 1.8750 INCH LONG CRACK IN SKIN AT STA 727 LONGERON 22L. CUT OUT CRACKED AREA/HFEC/INSTALLED DOUBLER IAW SRM 53-00-01.
- [SDR USAA060580](https://openairdocs.org/sdr/USAA060580.md): Structure · punctured · Apr 10, 2006 · N527AU · Boeing 7373B7 · Spoilers
  > OUTBOARD OF NR 5 SPOILER PUNCTURED. REMOVED DAMAGE, INSTALLED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: 2 INCH.
- [SDR USAA060448](https://openairdocs.org/sdr/USAA060448.md): Skin · punctured · Mar 10, 2006 · N527AU · Boeing 7373B7 · Spoilers
  > NR 6 SPOILER TOP CENTER OF SPOILER PANEL PUNCTURE. MAJOR REPAIR, IAW TR 27-60-01, DEFECT SIZE: 1 INCH.
- [SDR USAA060446](https://openairdocs.org/sdr/USAA060446.md): Skin · punctured · Mar 10, 2006 · N527AU · Boeing 7373B7 · Spoilers
  > OUTBOARD OF NR 5 SPOILER PUNCTURE. REMOVED DAMAGE INSTALLED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: 2 INCHES.
- [SDR USAA060445](https://openairdocs.org/sdr/USAA060445.md): Skin · delaminated · Mar 9, 2006 · N527AU · Boeing 7373B7 · Wing, Plate/Skin
  > STA WBL 170-160 AND 181 UPPER FIXED WING T/E DELAMINATED. REMOVED DAMAGE AND APPLIED A COMPOSITE REPAIR IAW EA 78270, DEFECT SIZE: 3 INCHES.
- [SDR USAA060409](https://openairdocs.org/sdr/USAA060409.md): Repair · unknown · Mar 6, 2006 · N527AU · Boeing 7373B7 · Standard Practices/Structures
  > RIGHT ELEVATOR LOWER SURFACE 9 INCHES I/B OF O/B END AND 16 INCHES AFT OF FRONT SPAR. PREVIOUS REPAIR IAW SRM 55-20-01-2, DEFECT SIZE: 2.5 INCHES.
- [SDR USAA060410](https://openairdocs.org/sdr/USAA060410.md): Repair · unknown · Mar 6, 2006 · N527AU · Boeing 7373B7 · Standard Practices/Structures
  > RIGHT ELEVATOR LOWER SURFACE 59 INCHES I/B OF O/B END AND 10 INCHES AFT OF RIGHT. PREVIOUS REPAIR IAW SRM 55-20-01-2, DEFECT SIZE: 6 INCHES.
- [SDR USAA060411](https://openairdocs.org/sdr/USAA060411.md): Repair · unknown · Mar 6, 2006 · N527AU · Boeing 7373B7 · Standard Practices/Structures
  > RIGHT ELEVATOR, LOWER SURFACE 30 INCHES O/B OF I/B END AND 12 INCHES AFT OF RIGHT DAMAGED. PREVIOUS REPAIR IAW SRM 55-20-01-2, DEFECT SIZE: 6 INCHES.
- [SDR USAA060412](https://openairdocs.org/sdr/USAA060412.md): Repair · unknown · Mar 6, 2006 · N527AU · Boeing 7373B7 · Empennage Structure
  > RIGHT ELEVATOR LOWER SURFACE 59 INCHES I/B OF O/B END AND 10 INCHES AFT OF FRONT SPAR DAMAGED. PREVIOUS REPAIR IAW SRM 55-20-01-2, DEFECT SIZE: 6 INCHES.
- [SDR USAA060407](https://openairdocs.org/sdr/USAA060407.md): Rib · cracked · Mar 3, 2006 · N527AU · Boeing 7373B7 · Wing, Rib/Bulkhead
  > IN SPAR LOWER AFT SUPPORT RIB 135.5 CRACKED. REPAIRED IAW 97467, DEFECT SIZE: 1.250 INCH.
- [SDR USAA060388](https://openairdocs.org/sdr/USAA060388.md): Door Frame · cracked · Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Structure
  > FOUND AFT CARGO DOOR/AFT FRAME CRACKED STA 847 STR 24R. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-70-13, DEFECT SIZE: 1".
- [SDR USAA060390](https://openairdocs.org/sdr/USAA060390.md): Fitting · cracked · Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage, Landing Gear Attach Fittings
  > FOUND CRACK RIGHT MAIN LANDING GEAR SUPPORT FITTING AT HOLE B/2. INSTALLED REPAIR PER TR 57-40-13 REV A, DEFECT SIZE:.125".
- [SDR USAA060380](https://openairdocs.org/sdr/USAA060380.md): Frame · cracked · Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Frame
  > FOUND FRAME CRACKED BS 787 BETWEEN S-8R AND S9-R AT OVERHEAD BIN ATTACH POINT. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES IAW TR 53-10-20C, DEFECT SIZE:.125".
- [SDR USAA060389](https://openairdocs.org/sdr/USAA060389.md): Angle · corroded · Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON TRANSITION ANGLE STA 767-790 AT NUT PLATES. REMOVED CORROSION AND INSTALLED REPAIR PARTS IAW SRM 51-10-02, DEFECT SIZE:.250".
- [SDR USAA060371](https://openairdocs.org/sdr/USAA060371.md): Frame · cracked · Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Frame
  > FOUND CRACK BS 380 BETWEEN S-8R AND S-9R AT OVERHEAD BIN LOWER ATTACH. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES IAW TR 53-10-20C, DEFECT SIZE:.125 INCH.
- [SDR USAA060382](https://openairdocs.org/sdr/USAA060382.md): Frame · cracked · Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Frame
  > FOUND FRAME CRACKED LT BODY STA 480. REMOVED AND REPLACED PSU BRACKET WITH FABRICATED PARTS IAW TR 53-10-20C, DEFECT SIZE:.250 INCH.
- [SDR USAA060383](https://openairdocs.org/sdr/USAA060383.md): Bracket · cracked · Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Attach Fittings
  > FOUND CRACKED PSU RAIL BRACKET AT RT BODY STA 480. REMOVED AND REPLACED PSU RAIL BRACKET WITH FABRICATED IAW TR 53-10-20C, DEFECT SIZE:.250 INCH.
- [SDR USAA060384](https://openairdocs.org/sdr/USAA060384.md): Frame · cracked · Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Frame
  > FOUND CRACK AT FRAME STA 827 BETWEEN S8L. FABRICATED FRAME REPAIR ANGLES AND INSTALLED PER T/R 53-10-20C, DEFECT SIZE:.125 INCH.
- [SDR USAA060385](https://openairdocs.org/sdr/USAA060385.md): Frame · cracked · Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Frame
  > FOUND CRACK STA 807 BETWEEN S8L-9L AT OVERHEAD BIN LOWER ATTACH POINT. REMOVED AND REPLACED FRAME SUPPORT BRACKETS IAW TR 53-10-20C, DEFECT SIZE: 1 INCH.
- [SDR USAA060386](https://openairdocs.org/sdr/USAA060386.md): Intercostal · cracked · Mar 1, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > AD 2005-20-03 INSP/REPAIR OF INTERCOSTALS FOUND CRACK COMMON TO MAIN ENTRY DOOR. REMOVED AND REPLACED CRACKED INTERCOSTAL WEB AND STRAP WITH FABRICATED PARTS IAW SRM 53-10-04 REPAIR DEFECT SIZE:.25.
- [SDR USAA060356](https://openairdocs.org/sdr/USAA060356.md): Clip · cracked · Feb 24, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > FWD SIDE OF BS 294.5 AND STR 11L. REMOVED CRACKED CLIP, FABRICATED AND INSTALLED NEW CLIP IAW BOEING DWG 69-62054, DEFECT SIZE:.50 INCH.
- [SDR USAA060357](https://openairdocs.org/sdr/USAA060357.md): Splice · cracked · Feb 24, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > BS 907 AND STR 4R CRACKED. REMOVED OLD SPLICE AND DRILLED AND INSTALLED REPAIR PARTS IAW SRM 51-40-02, DEFECT SIZE:.50 INCH.
- [SDR USAA060358](https://openairdocs.org/sdr/USAA060358.md): Bracket · cracked · Feb 24, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > AFT FACE OF E-1-3 RACK CENTER WEB CRACKED. REMOVED DAMAGED BRACKET, FABRICATED AND INSTALLED REPAIR PARTS BOEING DWG 69-42159, DEFECT SIZE:.50 INCH.
- [SDR USAA060353](https://openairdocs.org/sdr/USAA060353.md): Floorbeam · corroded · Feb 24, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > BS 312 FLOORBEAM CORRODED FROM RBL 8 TO RBL 36. MAJOR REPAIR SRM 53-10-51 FIG 201, REPAIR 5, DEFECT SIZE:.25 INCH.
- [SDR USAA060329](https://openairdocs.org/sdr/USAA060329.md): Bracket · cracked · Feb 22, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > AFT FACE OF E-1-3 RACK CENTER WEB CRACKED. REMOVED DAMAGED BRACKET, FABRICATED AND INSTALLED REPAIR PARTS IAW BOEING DWG 69-42159, DEFECT SIZE:.25 INCH.
- [SDR USAA060332](https://openairdocs.org/sdr/USAA060332.md): Channel · cracked · Feb 22, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > STRINGER 15L AND BS 360 CRACKED. REMOVED AND REPLACED WITH NEW EXTENSION CHANNEL IAW DGW 65-61777, DEFECT SIZE:.25 INCH.
- [SDR USAA060331](https://openairdocs.org/sdr/USAA060331.md): Angle · cracked · Feb 22, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > BS 360 S-14 LT. REMOVED AND REPLACED WITH NEW ANGLE IAW DWG 65-4566 AND SRM 51-10-02, DEFECT SIZE:.25 INCH.
- [SDR USAA060330](https://openairdocs.org/sdr/USAA060330.md): Angle · cracked · Feb 22, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > AT 13L AND BS 360 CRACKED. REMOVED CRACKED ANGLE, REPLACED WITH NEW ANGLE IAW DWG 69-48204 AND SRM 51-10-02, DEFECT SIZE:.25 INCH.
- [SDR USAA060314](https://openairdocs.org/sdr/USAA060314.md): Tie Clip · cracked · Feb 21, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > FOUND CRACK BS 343 AT STRINGER 11R. REMOVED FABRICATED AND INSTALLED TIE CLIP IAW BOEING DWG 69-38939-5 AND SRM 51-10-02, DEFECT SIZE:.025".
- [SDR USAA060328](https://openairdocs.org/sdr/USAA060328.md): Angle · corroded · Feb 21, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > FOUND Z-ANGLE CORRODED STA 967-987 AT STR 17L. INSTALLED NEW Z ANGLE PER SRM 51-10-02, DEFECT SIZE: 2" BY 20".
- [SDR USAA060322](https://openairdocs.org/sdr/USAA060322.md): Frame · cracked · Feb 21, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Frame
  > FOUND FRAME CRACKED STA 847 BETWEEN S8R AND 9R. REPAIRED PER 53-10-20C DEFECT SIZE:.25".
- [SDR USAA060321](https://openairdocs.org/sdr/USAA060321.md): Angle · cracked · Feb 21, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > FOUND ANGLE CRACKED INSIDE OF FRAME, 294.5 R AT S17R. INSTALLED NEW ANGLE IAW SRM 51-40-02, DEFECT SIZE:.25".
- [SDR USAA060281](https://openairdocs.org/sdr/USAA060281.md): Pan · corroded · Feb 16, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > LEFT PAN STA 987 LBL 37 CORROSION AT NUT PLATE. BLENDED, ALODINED, PRIMED AND PAINTED IAW SRM 51-10-02. DEFECT SIZE: 1"X1.5"
- [SDR USAA060287](https://openairdocs.org/sdr/USAA060287.md): Skin · corroded · Feb 16, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > NR 2 VHF ANTENNA. REMOVE CORROSION, TREATED AND PAINTED IAW SRM 51-10-02. DEFECT SIZE: 6"X2"
- [SDR USAA060284](https://openairdocs.org/sdr/USAA060284.md): Skin · corroded · Feb 16, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > NR 1 VHF ANTENNA. REMOVED CORROSION TREATED AND PAINTED IAW SRM 51-10-02. DEFECT SIZE: 6"X2"
- [SDR USAA060280](https://openairdocs.org/sdr/USAA060280.md): Angle · corroded · Feb 16, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > STA 984 AND STA967. REMOVED LIGHT CORROSION LESS THEN.002 IAW SRM 51-10-02. DEFECT SIZE:.002"
- [SDR USAA060278](https://openairdocs.org/sdr/USAA060278.md): Floorbeam · corroded · Feb 16, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > STA 957 RBL 18 TO RBL 44. REMOVED SURFACE CORROSION IAW SRM 51-10-02. DEFECT SIZE:
- [SDR USAA060277](https://openairdocs.org/sdr/USAA060277.md): Floorbeam · corroded · Feb 16, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > STA 967 LBL28 TO LBL44. REMOVED LIGHT CORROSION LESS THEN.002 IAW SRM 53-60-51. DEFECT SIZE:.002
- [SDR USAA060274](https://openairdocs.org/sdr/USAA060274.md): Web · cracked · Feb 16, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > BS 294.5 AND S12L WEB IS CRACKED. CUT OUT DAMAGED WEB, HFEC, FABRICATED REPLACEMENT PART AND INSTALLED IAW SRM 51-40-02. DEFECT SIZE: 1 INCH
- [SDR USAA060273](https://openairdocs.org/sdr/USAA060273.md): Skin · cracked · Feb 16, 2006 · N527AU · Boeing 7373B7 · Leading Edge Devices
  > LOWER SURFACE OF NR 6 SLAT, INBOARD END AT STOP PADS. REMOVED AFFECTED RIVETS, CUT OUT DAMAGE FABRICATED REPAIR PANEL AND INSTALLED IAW SRM 57-43-01 R-6. DEFECT SIZE:.250 INCH
- [SDR USAA060283](https://openairdocs.org/sdr/USAA060283.md): Floorbeam · corroded · Feb 16, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > T-CAP 967 CORROSION AT RBL 5 AND RBL 28. REPAIRED AND BLENDED LIGHT CORROSION IAW SRM 53-60-51. DEFECT SIZE:.002"
- [SDR USAA060255](https://openairdocs.org/sdr/USAA060255.md): Floorbeam · corroded · Feb 15, 2006 · N527AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > STA 98.7 RBL 2 TO RBL 36 CORROSION. REMOVED CORROSION IAW SRM 53-60-51, DEFECT SIZE:.002.
- [SDR USAA060253](https://openairdocs.org/sdr/USAA060253.md): Web · cracked · Feb 15, 2006 · N527AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > BS 294.5 AND S16L CRACKED. REMOVED AND REPLACED WEB IAW SRM 51-10-02, DEFECT SIZE:.500 INCH.

Next page: https://openairdocs.org/deregistered/N527AU-2011-03-30/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 = 'N527AU' AND deregistration_id = 'N527AU-2011-03-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N527AU-2011-03-30/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.