# Service difficulty reports: N525AU, cancelled Nov 6, 2007

A list on [N525AU, cancelled Nov 6, 2007](https://openairdocs.org/deregistered/N525AU-2007-11-06.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 · 118 reports

- [SDR USAA200703007](https://openairdocs.org/sdr/USAA200703007.md): Skin · cracked · Mar 27, 2007 · N525AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > FOUND 3 INCH CRACK AT STA 767 STR 21L SKIN. REPAIRED PER SRM 53-00-01, REPAIR 31, TR 53-60-03A.
- [SDR USAA20703006](https://openairdocs.org/sdr/USAA20703006.md): Skin · cracked · Mar 26, 2007 · N525AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > A 1 INCH CRACK FOUND RT SIDE OF FUSELAGE, STA 767, STR 21R. REPAIRED AS PER BAC SRM 53-00-01 REPAIR 31.
- [SDR USAASB06120](https://openairdocs.org/sdr/USAASB06120.md): Lamp · burned out · Nov 30, 2006 · N525AU · Boeing 7373B7 · Landing Gear Position and Warning
  > PIT FLT1904 - ON APPROACH TO PIT FROM CLT, DURING GEAR EXTENSION, CAPTAIN REPORTED HE DID NOT RECEIVE GREEN LIGHTS FOR ALL THREE OF THE GEAR. THE RIGHT MAIN LANDING GEAR INDICATION LIGHT WOULD NOT ILLUMINATE. CREW REQUESTED A FLY-BY THE ATC TOWER FOR VISUAL
- [SDR USAA061218](https://openairdocs.org/sdr/USAA061218.md): Skin · cracked · Oct 16, 2006 · N525AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > AT 2 INCHES FWD OF BS 727E AT S24R CRACK. INSTALLED REPAIR DOUBLER IAW EA 98168, DEFECT SIZE: 2 INCHES.
- [SDR USAA051409](https://openairdocs.org/sdr/USAA051409.md): Spar · cracked · Nov 22, 2005 · N525AU · Boeing 7373B7 · Wing Spar
  > LBL 135.5, 12 INCHES FWD FROM REAR SPAR CRACKED. MAJOR REPAIR, REMOVED DAMAGE, INSTALLED REPAIR TEE, FILLERS, AND VERT STIFFENER IAW EA 97047. DEFECT SIZE: 1.5 INCH.
- [SDR USAA051377](https://openairdocs.org/sdr/USAA051377.md): Angle · corroded · Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > LEFT TRANSITION ANGLE, STA 727D-807 CORRODED. FABRICATED NEW TRANS ANGLE AND INSTALLED IAW SRM 53-60-53, SRM 51-10-02. DEFECT SIZE:.500 INCH AREA CORROSION AT EACH FASTENER.
- [SDR USAA051378](https://openairdocs.org/sdr/USAA051378.md): Floor Support · corroded · Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > BS 500D BETWEEN 26L AND 26R CORRODED. REMOVED DAMAGED PART AND INSTALLED NEW ANGLE IAW SRM 53-30-53 AND SRM 53-00-53. DEFECT SIZE: CORROSION AREAS APPROXIMATELY 1 INCH IN DIAMETER.
- [SDR USAA051379](https://openairdocs.org/sdr/USAA051379.md): Angle · corroded · Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Attach Fittings
  > TOP OF TRANSITION ANGLE BETWEEN STA 767 AND 787 CORRODED. REMOVED DAMAGED SECTION, FAB AND REPLACED WITH NEW SECTION IAW SRM 51-10-2 & BOEING DWG 65-47957. DEFECT SIZE: SPOTS OF CORROSION APPROXIMATELY.125 INCH IN DIAMETER.
- [SDR USAA051380](https://openairdocs.org/sdr/USAA051380.md): Door Frame · cracked · Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Structure
  > AFT CARGO DOOR FRAME AFT WEBBING CRACKED. FABRICATED AND INSTALLED NEW WEBBING IAW SRM 51-70-13. DEFECT SIZE: 1 INCH CRACK.
- [SDR USAA051381](https://openairdocs.org/sdr/USAA051381.md): Angle · corroded · Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Attach Fittings
  > RBL 13.80, STA 787-847 CORRODED. CUT OUT DAMAGED SECTION AND SPLICE IN NEW SECTION IAW SRM 53-00-53 FIG 201. DEFECT SIZE: 6 INCH CORROSION.
- [SDR USAA051382](https://openairdocs.org/sdr/USAA051382.md): Shear Tie · corroded · Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Internal Mounting Structure
  > STA 727E BETWEEN STRINGER 27L TO 27R CORRODED. INSTALLED REPAIR PARTS PER SRM 53-00-07. DEFECT SIZE: 2 INCH LONG AREA OF CORROSION.
- [SDR USAA051383](https://openairdocs.org/sdr/USAA051383.md): Support · corroded · Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > STA 294-312, LBL 12 CORRODED. REPLACE INTERCOSTAL MEMBER AND T-FITTING IAW SRM 51-10-02. DEFECT SIZE: INTERCOSTAL HAS A 70 INCH AREA OF CORROSION.
- [SDR USAA051384](https://openairdocs.org/sdr/USAA051384.md): Angle · cracked · Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > BS 294; S-17R; ATTACHED TO OUTBOARD SIDE OF ZEE ANGLE CRACKED. PART REPLACED WITH IDENTICAL PART IAW SRM 51-10-02. DEFECT SIZE: 1.5 INCH CRACK IN A 4 INCH LONG ANGLE.
- [SDR USAA051385](https://openairdocs.org/sdr/USAA051385.md): Angle · corroded · Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > BS 300-353; ZEE ANGLE AT S-17L CORRODED. REPLACED WITH IDENTICAL PART, REMOVED CORRODED ZEE ANGLE WITH NEW IAW SRM 51-10-02 BOEING DWG 65-17688. DEFECT SIZE: APPROX 1 X 43 INCH CORRODED AREA.
- [SDR USAA051386](https://openairdocs.org/sdr/USAA051386.md): Angle · corroded · Nov 15, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Structure
  > TRANSITION ANGLE 727B THRU 727D CORRODED. FABRICATED AND INSTALLED REPAIR PART IAW SRM 53-60-53, DEFECT SIZE: 1 INCH CORROSION.
- [SDR USAA051366](https://openairdocs.org/sdr/USAA051366.md): Angle · corroded · Nov 11, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > FOUND CORROSION BS 300-353 ZEE ANGLE AT S-17L. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED CORRODED ZEE ANGLE IAW 65-17688, DEFECT SIZE: 1 BY 43 INCHES.
- [SDR USAA051365](https://openairdocs.org/sdr/USAA051365.md): Angle · corroded · Nov 11, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON R-1 DOOR THRESHOLD INNER CHORD ANGLE BS 296. REPAIR, DEFECTIVE PART REPLACED WITH IDENTICAL PARTY IAW SRM 51-10-02, DEFECT SIZE: 2" BY 5".
- [SDR USAA051364](https://openairdocs.org/sdr/USAA051364.md): Web · cracked · Nov 11, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > FOUND CRACK FUSELAGE STATION 353 STRINGER 16 LEFT. REPAIR, CUT WEB TO REMOVE DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-04, EA 97004 DEFECT SIZE: 2.1".
- [SDR USAA051363](https://openairdocs.org/sdr/USAA051363.md): Intercostal · cracked · Nov 10, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > STA 344, STA 360, BL0 MAJOR REPAIR, FABRICATED NEW REPAIR PARTS IAW SRM 51-70-11, DEFECT SIZE:.250".
- [SDR USAA051362](https://openairdocs.org/sdr/USAA051362.md): Frame · damaged · Nov 10, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Frame
  > FOUND HOLE IN FRAME STA 380, S15L. ENLARGED HOLE TO.125 AND INSTALLED RIVET IAW EA 97066, DEFECT SIZE:.100".
- [SDR USAA051355](https://openairdocs.org/sdr/USAA051355.md): Attach Angle · cracked · Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Attach Fittings
  > FOUND STR 25L AND FRAME AT BS 380 CRACKED. FABRICATED AND INSTALLED NEW ANGLE BOEING DWG 69-38780 AND SRM 53-00-01, DEFECT SIZE: 1".
- [SDR USAA051354](https://openairdocs.org/sdr/USAA051354.md): Floorbeam · corroded · Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > FOUND STA 344, LBL42-RBL31; AROUND CLIP NUT HOLES IN FLOOR BEAM CORRODED. REMOVED CORRODED OUT OF LIMITS SECTION OF "T" CAP FROM LBL31 TO RBL31 IAW SRM 53-10-51, FIG 201, DEFECT SIZE: 1" BY 1".
- [SDR USAA051356](https://openairdocs.org/sdr/USAA051356.md): Floorbeam · cracked · Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > FOUND BS28/LBL27 CRACKED. FABRICATED AND INSTALLED STIFFENER IAW SRM 51-10-02, DEFECT SIZE: 1".
- [SDR USAA051357](https://openairdocs.org/sdr/USAA051357.md): Stringer Clip · cracked · Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Attach Fittings
  > CRACK FOUND STATION 343 AT STRINGER 11R. STRINGER TIE CLIP WAS FABRICATED IAW BOEING DRAWING 69-38939-5, DEFECT SIZE:.025.
- [SDR USAA051359](https://openairdocs.org/sdr/USAA051359.md): Floorbeam · corroded · Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > FOUND STA 344, LBL 42-RBL3, AROUND CLIP NUT HOLES IN FLOORBEAM. REMOVED AND REPLACED T-CAP FROM LBL 1 TO RBL 32 IAW SRM 53-10-51, FIG 201, DEFECT SIZE: 1" BY 1".
- [SDR USAA051360](https://openairdocs.org/sdr/USAA051360.md): Intercostal · cracked · Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > FOUND CRACK BS312 BL0 CABIN FLOOR SUPPORT STRUCTURE. CUTOUT CRACKED AREA, FABRICATED AND INSTALLED REPAIR IAW SRM 51-70-11, DEFECT SIZE:.25".
- [SDR USAA051361](https://openairdocs.org/sdr/USAA051361.md): Stiffener · cracked · Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > FOUND STA 328 LBL45 FWD ENTRY FLOOR SUPPORT STRUCTURE CRACKED. REPAIR, FABRICATED NEW L-ANGLE AND INSTALLED IAW SRM 51-10-02 BOEING DWR 65-45812 DEFECT SIZE:.250"
- [SDR USAA051358](https://openairdocs.org/sdr/USAA051358.md): Floorbeam · corroded · Nov 9, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > FOUND CORROSION BS 328 AT RBL 15 AND 12. FABRICATED SPLICE ANGLES AND INSTALLED SPLICE ANGLES AND "T" CAP IAW SRM 53-10-51, DEFECT SIZE: 7" BY.65".
- [SDR USAA051352](https://openairdocs.org/sdr/USAA051352.md): Angle · cracked · Nov 8, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > FOUND STA 350 AT STRINGER 16L CRACKED. REMOVED, FAB, HEAT TREATED AND INST NEW ANGLE IAW SRM 51-10-02, DWG 69-26555 JOB CARD J020-37-20, DEFECT SIZE:.250" CRACK.
- [SDR USAA051351](https://openairdocs.org/sdr/USAA051351.md): Channel · cracked · Nov 8, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > FOUND BS 360; S15L CRACKED. REMOVED CRACKED CHANNEL AND INSTALLED NEW CHANNEL IAW SRM 51-10-02, DEFECT SIZE: APPROX 1" CRACK.
- [SDR USAA051339](https://openairdocs.org/sdr/USAA051339.md): Skin · damaged · Nov 7, 2005 · N525AU · Boeing 7373B7 · Rudder, Plate/Skin
  > LEFT RUDDER SKIN 96 INCHES FROM THE BASE AND 11 INCHES FROM THE TRAILING EDGE DAMAGED. REMOVED DAMAGED, LAID UP AND INSTALLED REPAIR IAW SRM 55-40-01. DEFECT SIZE: 1.5 INCH.
- [SDR USAA051340](https://openairdocs.org/sdr/USAA051340.md): Skin · delaminated · Nov 7, 2005 · N525AU · Boeing 7373B7 · Rudder, Plate/Skin
  > LEFT RUDDER SKIN 99 INCHES FROM THE BASE AND 19 INCHES IN FROM THE TRAILING EDGE DELAMINATED. REMOVED DAMAGE, LAID UP AND INSTALLED REPAIR IAW SRM 55-40-01. DEFECT SIZE: 6 INCHES.
- [SDR USAA051341](https://openairdocs.org/sdr/USAA051341.md): Skin · gouged · Nov 7, 2005 · N525AU · Boeing 7373B7 · Trailing Edge Flaps
  > WEDGE SKIN 13.5 INCH FROM THE OUTBOARD END GOUGED. REMOVED SKIN AND DAMAGED CORE, INSTALLED CORE, FILLER AND DOUBLER IAW SRM 57-50-15 REV A. DEFECT SIZE: 4.3 X.5 INCH.
- [SDR USAA051342](https://openairdocs.org/sdr/USAA051342.md): Floorbeam · corroded · Nov 7, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > BS 312, WL 208, LBL 16 TO RBL 16 LEVEL 1 CORROSION. SPLICED IN REPLACEMENT EXTRUSION IAW SRM 53-10-51 FIG 201. DEFECT SIZE:.50 X.50 INCH.
- [SDR USAA051333](https://openairdocs.org/sdr/USAA051333.md): Tie Clip · cracked · Nov 4, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > FUSELAGE STATION 277 STRINGER 10R. REMOVED AND REPLACED STRINGER TIE CLIP IAW SRM 51-10-02. DEFECT SIZE:.075 INCH.
- [SDR USAA051334](https://openairdocs.org/sdr/USAA051334.md): Frame · cracked · Nov 4, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Frame
  > BETWEEN STRINGERS S-8R AND S-9R STA 480. CUT OUT DAMAGE, INSTALL FRAME DOUBLERS IAW TR 53-10-20. DEFECT SIZE:.5 INCH.
- [SDR USAA051326](https://openairdocs.org/sdr/USAA051326.md): Skin · cracked · Nov 3, 2005 · N525AU · Boeing 7373B7 · Leading Edge Devices
  > IN LOWER SKIN OF NR 5 SLAT AT RIVET, ADJACENT TO SLAT ACTUATOR ATTACH. A 30.25 X 3.75 INCH REPAIR DOUBLER ON LOWER SKIN AT CTR OF SLAT ADJ TO ACTUATOR ATTACH IAW SRM 57-43-01. DEFECT SIZE:.250 INCH LONG CRACK AT RIVET.
- [SDR USAA051327](https://openairdocs.org/sdr/USAA051327.md): Skin · cracked · Nov 3, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > FLOOR SKIN, STA 665, LBL 30. REMOVED DAMAGE, INSTALL FILLER DOUBLER & STIFFENER IAW TYPE REPAIR 53-60-04. DEFECT SIZE:.500 INCH CRACK.
- [SDR USAA051331](https://openairdocs.org/sdr/USAA051331.md): Skin · cracked · Nov 3, 2005 · N525AU · Boeing 7373B7 · Leading Edge Devices
  > LOWER SKIN T/E CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-43-01 FIG 201, DEFECT SIZE: 6 INCH CRACK.
- [SDR USAA051332](https://openairdocs.org/sdr/USAA051332.md): Trim Tab · delaminated · Nov 3, 2005 · N525AU · Boeing 7373B7 · Aileron Tabs
  > OUTBOARD T/E CORNER DELAMINATED. ROUTED TO COMPOSITE FOR REPAIR IAW SRM 51-70-06 REPAIR NR 6 DEFECT SIZE: 3 INCHES DELAM.
- [SDR USAA051319](https://openairdocs.org/sdr/USAA051319.md): Bracket · cracked · Nov 2, 2005 · N525AU · Boeing 7373B7 · Passenger/Crew Doors
  > LOWER FWD CORNER OF MAIN ENTRY DOOR. FABRICATED AND INSTALLED NEW BRACKET IAW SRM 51-10-02. DEFECT SIZE:.50 INCH.
- [SDR USAA051320](https://openairdocs.org/sdr/USAA051320.md): Angle · damaged · Nov 2, 2005 · N525AU · Boeing 7373B7 · Vertical Stabilizer
  > FOUND VERT STAB TRANSITION ANGLE LEFT SIDE AFT OF REAR ATTACH POINT. FABRICATED AND INSTALLED NEW ANGLE IAW TR 53-20-05A, DEFECT SIZE: 12".
- [SDR USAA051321](https://openairdocs.org/sdr/USAA051321.md): Stringer · cracked · Nov 2, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > S-5AR B.S. 1138 ACTION: INTERIM REPAIR WAS PREVIOUSLY INSTALLED IAW EA 73450B IAW EA 73450B. LENGTH UNKNOWN.
- [SDR USAA051289](https://openairdocs.org/sdr/USAA051289.md): Angle · corroded · Nov 1, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > FOUND Z-ANGLE CORRODED, STA 955 TO 990. REMOVED CORRODED PART AND INSTALLED NEW PART AND REPAIR PARTS IAW SRM 53-60-15, DEFECT SIZE: CORROSION ON "Z" ANGLE 1 INCH BY 1 INCH.
- [SDR USAA051291](https://openairdocs.org/sdr/USAA051291.md): Floorbeam · corroded · Nov 1, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > FOUND FLOORBEAM CORRODED STA 986.5 AT LT DOOR SILL AREA. REPLACED ENTIRE T-CAP IAW TR 53-10-05B, DEFECT SIZE:.500" AREA OF CORROSION AROUND SEVERAL SCREW HOLES.
- [SDR USAA051292](https://openairdocs.org/sdr/USAA051292.md): Angle · corroded · Nov 1, 2005 · N525AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > FOUND CORROSION STA 955 TO 990, LBL 53. REMOVED DAMAGED PARTS AND INSTALLED NEW PARTS IAW SRM 51-10-02, DEFECT SIZE: NUMEROUS AREAS OF CORROSION THROUGHOUT THE PART/TYPICAL 1/2" DIA OF CORROSION.
- [SDR USAA051293](https://openairdocs.org/sdr/USAA051293.md): Angle · corroded · Nov 1, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Attach Fittings
  > FOUND Z-ANGLE CORRODED, FLOOR STRUCTURE AT L2 DOOR, STA 986 AND LBL 53. REMOVED CORRODED PART AND INSTALLED NEW PART IAW SRM 51-10-02, DEFECT SIZE: 1" BY 3" AREA OF CORROSION.
- [SDR USAA051294](https://openairdocs.org/sdr/USAA051294.md): Skin · debonded · Nov 1, 2005 · N525AU · Boeing 7373B7 · Leading Edge Devices
  > FOUND DISBOND O/B END OF T/E WEDGE. REMOVED DAMAGE, FAB AND INSTALLED REPAIR PARTS IAW TR 51-30-03, DEFECT SIZE: 2" BY 5" DISBOND.
- [SDR USAA051295](https://openairdocs.org/sdr/USAA051295.md): Skin · debonded · Nov 1, 2005 · N525AU · Boeing 7373B7 · Leading Edge Devices
  > FOUND SLAT DISBOND, T/E WEDGE O/B END. REMOVED DAMAGE, FAB AND INSTALLED REPAIR PARTS IAW TR 57-42-04, DEFECT SIZE: 3" X 5" DISBOND.
- [SDR USAA051296](https://openairdocs.org/sdr/USAA051296.md): Crease Beam · corroded · Nov 1, 2005 · N525AU · Boeing 7373B7 · Fuselage Main, Structure
  > AROUND RIVET HEADS AT CREASE BEAM BS 500B+8 S17L. REMOVED CORROSION AND TREATED AREA IAW SRM 51-20-01, DEFECT SIZE: APPROXIMATE 1/16" DIA SPOTS OF CORROSION.

Next page: https://openairdocs.org/deregistered/N525AU-2007-11-06/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 = 'N525AU' AND deregistration_id = 'N525AU-2007-11-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N525AU-2007-11-06/reports

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