# Service difficulty reports: N512AU, cancelled May 19, 2011

A list on [N512AU, cancelled May 19, 2011](https://openairdocs.org/deregistered/N512AU-2011-05-19.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 · 116 reports

- [SDR USAA920081570](https://openairdocs.org/sdr/USAA920081570.md): Skin · cracked · Aug 25, 2008 · N512AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - RON - MAJOR REPAIR - LOG 4393963 - FUSELAGE SKIN CRACKED AT BS761 & 765, S19R. REPAIRED FUSELAGE SKIN AT BS761 & 765, S19R IAW B737 SRM 53-00-01 REPAIR 31, TEMPORARY REVISION 53-33.
- [SDR USAA920081399](https://openairdocs.org/sdr/USAA920081399.md): Battery Pack · discharged · Jul 22, 2008 · N512AU · Boeing 7373B7 · Emergency Lighting
  > FLT 1465 CLT-IND- EEL - AFT EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK FOR THE AFT EMERGENCY EXIT LIGHT. OPERATIONAL CHECK WAS GOOD. (A)
- [SDR USAA920080904](https://openairdocs.org/sdr/USAA920080904.md): Slide · low · Apr 18, 2008 · N512AU · Boeing 7373B7 · Escape Slide
  > FLT NR 9186 PIT - EES - AFT LT SERVICE DOOR SLIDE HAS LOW PRESSURE. MAINTENANCE REMOVED AND REPLACED THE AFT LT SERVICE DOOR SLIDE.
- [SDR USAA920080755](https://openairdocs.org/sdr/USAA920080755.md): Wire · broken · Apr 6, 2008 · N512AU · Boeing 7373B7 · Light System Wiring
  > FLT 1452 - TPA-DCA - EEL - 19C EMERGENCY EXIT LIGHT INOP. MAINTENANCE REPAIRED BROKEN WIRE AND RELAMPED. OPERATIONAL CHECK WAS GOOD.
- [SDR USAA920071165](https://openairdocs.org/sdr/USAA920071165.md): Skin · cracked · Nov 17, 2007 · N512AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - MAJOR REPAIR - CRACKED FUSELAGE SKIN, BS 520, S10R. REPAIRED FUSELAGE SKIN, BS 520, S10R IAW B737 SRM 53-00, FIGURE 31.
- [SDR USAA070700](https://openairdocs.org/sdr/USAA070700.md): Stiffener · corroded · Aug 30, 2007 · N512AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > STA 328, LBL 10, FLOOR SUPPORT STIFFENER HAS CORROSION. REMOVED & REPLACED WITH NEW STIFFENER PER SRM 51-10-02; CORR TASK C53-107-02, DEFECT SIZE: 2" X 12".
- [SDR USAA070706](https://openairdocs.org/sdr/USAA070706.md): Stringer Clip · corroded · Aug 30, 2007 · N512AU · Boeing 7373B7 · Fuselage Main, Attach Fittings
  > STA 747 S28L, STRINGER TIE CLIP HAS CORROSION. REMOVED & REPLACED STRINGER TIE CLIP PER SRM 51-20-01, 51-10-02; CORR TASK C53-202-01, DEFECT SIZE:.5 INCH.
- [SDR USAA070705](https://openairdocs.org/sdr/USAA070705.md): Floor Support · corroded · Aug 30, 2007 · N512AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > STA 312, RBL 12 HAS CORROSION. REMOVED & REPLACED WITH NEW PART PER SRM 51-10-02; CORR TASK C53-107-02, DEFECT SIZE: 6 INCHES.
- [SDR USAA070704](https://openairdocs.org/sdr/USAA070704.md): Floor Support · corroded · Aug 30, 2007 · N512AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT STA 312 LBL 10 CORRODED. REMOVED DAMAGED AREA & REPLACED WITH NEW FLOOR SUPPORT PER SRM 51-01-02; CORR TSK C53-107-02, DEFECT SIZE: 6 INCHES.
- [SDR USAA070703](https://openairdocs.org/sdr/USAA070703.md): Mount · corroded · Aug 30, 2007 · N512AU · Boeing 7373B7 · Fuselage Main, Attach Fittings
  > STA 986.5 + 7, S17L & S17R, LT & RT INBOARD & OUTBOARD AFT LAV MOUNTS CORRODED. REMOVED & REPLACED MOUNTS PER SRM 51-20-01, 51-10-02; CORR TASK C53-107-02, DEFECT SIZE: 1 INCH.
- [SDR USAA070701](https://openairdocs.org/sdr/USAA070701.md): Angle · corroded · Aug 30, 2007 · N512AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > BS 312 - 360 LBL 55, CHORD ANGLE HAS CORROSION. REMOVED DAMAGED PARTS & INSTALLED NEW PARTS PER SRM 51-20-01; 51-20-00; CORR TASK C53-107-02, DEFECT SIZE: 3 X 36 INCHES.
- [SDR USAA070692](https://openairdocs.org/sdr/USAA070692.md): Floorbeam · corroded · Aug 30, 2007 · N512AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > STA 328, BL 0 HAS CORROSION. REMOVED DAMAGE ON T-CAP, INSTALLED FILLER/ANGLE REPAIR PARTS PER SRM 53-10-51; CORR TASK C53-107-02; DEFECT SIZE: 3 INCHES.
- [SDR USAA070699](https://openairdocs.org/sdr/USAA070699.md): Slat · eroded · Aug 30, 2007 · N512AU · Boeing 7373B7 · Trailing Edge Flaps
  > ERODED SKIN & DISBOND, NR 4 SLAT T/E WEDGE, LOWER SURFACE I/B SIDE OF SLAT. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER SRM 51-70-10; TR 57-42-03, DEFECT SIZE: 2 X 3 INCHES.
- [SDR USAA070698](https://openairdocs.org/sdr/USAA070698.md): Fitting · corroded · Aug 30, 2007 · N512AU · Boeing 7373B7 · Emergency Equipment
  > MED AFT GIRT BAR ATTACH POINTS, CORROSION AROUND ATTACH HOLE. REMOVED & REPLACED GIRT BAR BASE FITTING PER SRM 51-20-00; COR TASK C53-107-02, DEFECT SIZE:.250 INCH.
- [SDR USAA070697](https://openairdocs.org/sdr/USAA070697.md): Floorbeam · corroded · Aug 30, 2007 · N512AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > STA 328, BL 50, FLOORBEAM T-CAP HAS CORROSION. REMOVED PREVIOUS REPAIR & INSTALLED/SPLICED IN NEW T-CAP PER SRM 53-10-50 FIG 201; CORR TASK C53-107, DEFECT SIZE: 24 INCHES.
- [SDR USAA070696](https://openairdocs.org/sdr/USAA070696.md): Floorbeam · corroded · Aug 30, 2007 · N512AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > STA 986.5, LBL 32 THRU RBL 34 HAS CORROSION. INSTALLED FILLER & DOUBLER PER TYP 51-70-12; CORR TASK C53-107-02, DEFECT SIZE: 2 X 2 INCHES.
- [SDR USAA070695](https://openairdocs.org/sdr/USAA070695.md): Channel · corroded · Aug 30, 2007 · N512AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > STA 344 - 312, FWD ENTRY WAY, SHORT U-CHANNEL BEAM HAS CORROSION. REMOVED & REPLACED WITH NEW CHANNEL PER SRM 51-10-02, 51-40-03; CORR TASK C53-107-02, DEFECT SIZE:.750 INCH.
- [SDR USAA070694](https://openairdocs.org/sdr/USAA070694.md): Angle · corroded · Aug 30, 2007 · N512AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > STA 344 - 312 FWD ENTRY WAY, LT SIDE HAS CORROSION. REPLACED DAMAGED Z-ANGLE WITH NEW PER SRM 51-10-02, 51-40-03; CORR TASK C53-107-02, DEFECT SIZE:.750 INCH.
- [SDR USAA070693](https://openairdocs.org/sdr/USAA070693.md): Frame · corroded · Aug 30, 2007 · N512AU · Boeing 7373B7 · Fuselage Main, Frame
  > STA 727E, LBBL 8 ON FRAME WHERE IT ATTACHES TO SKIN EXFOLIATED. FABRICATED REPAIR PART & INSTALLED PER SRM 53-60-07; CORR TASK C53-208-01, DEFECT SIZE: 1 INCH.
- [SDR USAA070702](https://openairdocs.org/sdr/USAA070702.md): Stringer Clip · corroded · Aug 30, 2007 · N512AU · Boeing 7373B7 · Fuselage Main, Attach Fittings
  > STA 767, S26L, STRINGER TIE CLIP HAS CORROSION. REPLACED STRINGER TIE CLIP PER SRM 51-20-01, 51-10-02; CORR TASK C53-202-01, DEFECT SIZE:.5 INCH.
- [SDR USAA070677](https://openairdocs.org/sdr/USAA070677.md): Skin · cracked · Aug 28, 2007 · N512AU · Boeing 7373B7 · Nacelle/Pylon, Plate/Skin
  > PYLON ABOVE NR 2 ENGINE O/B SIDE OF LOAD FITTING PIN HAS CRACK. REMOVED REPAIR, CLEANED AREA, INSTALLED REPAIR WET WITH SEALANT PER TR 57-41-02, DEFECT SIZE:.5 INCH.
- [SDR USAA070688](https://openairdocs.org/sdr/USAA070688.md): Skin · damaged · Aug 28, 2007 · N512AU · Boeing 7373B7 · Wing, Plate/Skin
  > WS 72, RIGHT WING, LOWER SURF, Z-ANGLE 3 FWD ATTACH FASTENERS ELONGATED. REMOVED FASTENERS, OVERSIZE & COLD WORK HOLES, & INSTALLED FIRST-OVER FASTENERS PER SRM 51-40-02, 51-40, DEFECT SIZE:.125 INCHES.
- [SDR USAA070687](https://openairdocs.org/sdr/USAA070687.md): Skin · damaged · Aug 28, 2007 · N512AU · Boeing 7373B7 · Wing, Plate/Skin
  > THREE WORKING FASTENER RIGHT WING TO CENTER SECTION Z-ANGLE AT WS 72, AFT 3 FASTENERS ELONGATED. OVERSIZED FIRST OVER, COLD WORKED HOLES & INSTALLED NEW FASTENERS PER SRM 51-40-02, 51-40-03, 51-40-, DEFECT SIZE:.125 INCH
- [SDR USAA070686](https://openairdocs.org/sdr/USAA070686.md): Wedge · debonded · Aug 28, 2007 · N512AU · Boeing 7373B7 · Leading Edge Devices
  > NR 3 SLAT UPPER OUTBOARD WEDGE DISBONDED. INSTALLED REPAIR PARTS PER SRM 51-70-17, 51-70-10, DEFECT SIZE: 1.5 X 2 INCHES.
- [SDR USAA070685](https://openairdocs.org/sdr/USAA070685.md): Skin · damaged · Aug 28, 2007 · N512AU · Boeing 7373B7 · Leading Edge Devices
  > NR 4 SLAT T/E WEDGE HAS ERODED SKIN & DISBOND ON LOWER SURFACE I/B SIDE OF SLAT. REMOVED DISBONDED AREA, INSTALLED REPAIR PARTS PER TR 57-42-03, SRM 51-70-10, DEFECT SIZE: 2 X 3 INCHES.
- [SDR USAA070683](https://openairdocs.org/sdr/USAA070683.md): Skin · gouged · Aug 28, 2007 · N512AU · Boeing 7373B7 · Leading Edge Devices
  > NR 2 SLAT O/B END UPPER SURFACE, SLAT WEDGE SKIN, GROOVE/GOUGE. INSTALLED NEW CORE FILLER & NEW UPPER SURFACE BONDED DOUBLER PER SRM 57-43-01, 51-70-10, DEFECT SIZE: 1.25 X.250 INCH.
- [SDR USAA070682](https://openairdocs.org/sdr/USAA070682.md): Skin · damaged · Aug 28, 2007 · N512AU · Boeing 7373B7 · Elevator, Plate/Skin
  > UPPER SURFACE, LOCATED 19.5 INCHES FWD OF ELEV TAB T/E & 37 INCHES OUTBOARD OF INBOARD T/E TIP HAS DAMAGE. REPAIR INSTALLED CONFORMS TO SRM 55-20-01 REPAIR 1, DEFECT SIZE: 5 INCH DIA.
- [SDR USAA070681](https://openairdocs.org/sdr/USAA070681.md): Skin · damaged · Aug 28, 2007 · N512AU · Boeing 7373B7 · Elevator, Plate/Skin
  > RIGHT ELEV UPPER SKIN, UPPER SURFACE LOCATED 12 INCHES FWD OF T/E & 16 INCHES INBOARD T/E TIP HAS DAMAGE. REPAIR INSTALLED CONFORMS TO SRM 55-20-01 REPAIR 1, DEFECT SIZE: 8 INCH DIA.
- [SDR USAA070680](https://openairdocs.org/sdr/USAA070680.md): Seat Track · cracked · Aug 28, 2007 · N512AU · Boeing 7373B7 · Fuselage, Seat/Cargo Attach Fittings
  > STA 727B RBL 24.75 HAS CRACK. INSTALLED FABRICATED REPAIR PARTS PER EA 98824, DEFECT SIZE: 3 INCH.
- [SDR USAA070678](https://openairdocs.org/sdr/USAA070678.md): Skin · cracked · Aug 28, 2007 · N512AU · Boeing 7373B7 · Wing, Plate/Skin
  > LEFT WING FIXED LEADING EDGE LOWER SKIN PANEL AT SLAT STA 3.25 HAS CRACK. REMOVED DAMAGE, FAB'D & INSTALLED REPAIR PARTS PER BOEING TR 57-41-02, DEFECT SIZE:.75 INCH.
- [SDR USAA070676](https://openairdocs.org/sdr/USAA070676.md): Stiffener · cracked · Aug 28, 2007 · N512AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > STA 294 BETWEEN STR S10R & S11R, ANGLE STIFFENER HAS CRACK. REMOVED & REPLACED ANGLE STIFFENER WITH NEW PART PER SRM 51-10-02, DEFECT SIZE:.5 INCH.
- [SDR USAA070675](https://openairdocs.org/sdr/USAA070675.md): Door Frame · cracked · Aug 28, 2007 · N512AU · Boeing 7373B7 · Fuselage Main, Structure
  > BS 492.4 STR 24R FWD CARGO DOOR FRAME HAS CRACK. DEFECTIVE PART REPLACED WITH IDENTICAL PART; INSTALLED NEW FRAME PER SRM 5-40-00, 53-00-53, DEFECT SIZE:.75 INCH.
- [SDR USAA070674](https://openairdocs.org/sdr/USAA070674.md): Web · cracked · Aug 28, 2007 · N512AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > STA 294.5, S7L HAS CRACK. FABRICATED NEW WEB AND INSTALLED PER BOEING DWG 65-17684, DEFECT SIZE:.350 INCH.
- [SDR USAA070673](https://openairdocs.org/sdr/USAA070673.md): Intercostal · cracked · Aug 28, 2007 · N512AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > BS 500 BENEATH RIGHT TRANSITION ANGLE, INTERCOSTAL BAFFLE HAS CRACK. FABRICATED NEW INTERCOSTAL BAFFLE DEFECT SIZE:.375 INCH.
- [SDR USAA070672](https://openairdocs.org/sdr/USAA070672.md): Frame · cracked · Aug 28, 2007 · N512AU · Boeing 7373B7 · Fuselage Main, Frame
  > STA 867 AT I/B FASTENER FOR A/C SUPPORT BRACKET, BETWEEN STR 8 & 9R HAS CRACK. INSTALLED TYPICAL FRAME REPAIR DOUBLER PARTS PER TR 53-10-20E, DEFECT SIZE:.125 INCH.
- [SDR USAA070671](https://openairdocs.org/sdr/USAA070671.md): Stringer Splice · cracked · Aug 28, 2007 · N512AU · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > STA 360 S14L, STRINGER SPLICE HAS CRACK. DRILLED UP NEW PART & INSTALLED PER SRM 51-40-02, DEFECT SIZE:.500 INCH.
- [SDR USAA070670](https://openairdocs.org/sdr/USAA070670.md): Structure · cracked · Aug 28, 2007 · N512AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > THE 500A AND 500B AT STR 26L AT LIGHTENING HOLE HAS CRACK. MANUFACTURED NEW PART PER SRM 53-30-04, 51-10-02, DEFECT SIZE:.375 INCH.
- [SDR USAA070669](https://openairdocs.org/sdr/USAA070669.md): Door Frame · cracked · Aug 28, 2007 · N512AU · Boeing 7373B7 · Passenger/Crew Doors
  > FWD PAX DOOR FRAME CRACKED AT NR 6 STOP PIN CUTOUT. INSTALLED DOUBLER REPAIR PER EA 98819, DEFECT SIZE:.125 INCH.
- [SDR USAA070668](https://openairdocs.org/sdr/USAA070668.md): Door Frame · cracked · Aug 28, 2007 · N512AU · Boeing 7373B7 · Passenger/Crew Doors
  > FWD PAX DOOR FRAME CRACKED AT NR 5 STOP PIN CUTOUT. INSTALLED DOUBLER REPAIR PER EA 98819, DEFECT SIZE:.125 INCH.
- [SDR USAA070667](https://openairdocs.org/sdr/USAA070667.md): Door Frame · cracked · Aug 28, 2007 · N512AU · Boeing 7373B7 · Passenger/Crew Doors
  > FWD PAX DOOR FRAME CRACKED AT NR 7 STOP PIN CUTOUT. INSTALLED DOUBLER REPAIR PER EA 98819, DEFECT SIZE:.125 INCH.
- [SDR USAA070679](https://openairdocs.org/sdr/USAA070679.md): Skin · cracked · Aug 28, 2007 · N512AU · Boeing 7373B7 · Leading Edge Devices
  > NR 6 SLAT, LOWER T/E AT OUTBOARD END, CRACKED AT RIVET HOLES. INSTALLED FILLER/DOUBLER REPAIR PER SRM 57-43-01, DEFECT SIZE:.125 INCH.
- [SDR USAA070665](https://openairdocs.org/sdr/USAA070665.md): Door Frame · cracked · Aug 24, 2007 · N512AU · Boeing 7373B7 · Passenger/Crew Doors
  > FWD PASSENGER DOOR FRAME CRACKED AT 37 STOP PIN CUTOUT, L1 DOOR, FWD ENTRY DOOR. INSTALLED DOUBLER REPAIR PER EA 98819, DEFECT SIZE:.125 INCH.
- [SDR USAA070660](https://openairdocs.org/sdr/USAA070660.md): Stringer · cracked · Aug 23, 2007 · N512AU · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > STR 15L AT STA 360 HAS CRACK. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SM 51-40-00, DEFECT SIZE: 0.7 INCH.
- [SDR USAA070661](https://openairdocs.org/sdr/USAA070661.md): Fitting · cracked · Aug 23, 2007 · N512AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLIP AT STA 947.5 STR 24L, FWD OF WATER SERVICE PANEL HAS CRACK. FAB'D NEW ANGLE PER BOEING DWG 65-51626 & INSTALLED PER SRM 51-10-02, DEFECT SIZE:.25 INCH.
- [SDR USAA070662](https://openairdocs.org/sdr/USAA070662.md): Stringer · cracked · Aug 23, 2007 · N512AU · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > STA 500 & 500A STR 26L AT LIGHTENING HOLE HAS CRACK. MANUFACTURED NEW PART PER SRM 51-10-02, 53-30-04, DEFECT SIZE:.5 INCH.
- [SDR USAA070663](https://openairdocs.org/sdr/USAA070663.md): Bulkhead · cracked · Aug 23, 2007 · N512AU · Boeing 7373B7 · Fuselage Main, Bulkhead
  > STA 727 RBL 40 FWD BULKHEAD, AFT CARGO CRACKED. FABRICATED WEB STIFFENER BRACKET & INSTALLED PER SRM 52-40-02, DEFECT SIZE: 1 INCH.
- [SDR USAA200705U13](https://openairdocs.org/sdr/USAA200705U13.md): Skin · cracked · May 28, 2007 · N512AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > ONE CRACK APPROX 16 INCHES LONG AT STA 500 BL 0 AT LOWER FWD VHF ANTENNA. [SUP 06-07-07] INSTALLED EXTERNAL DOUBLER 11" X 31" PER EA 84619.
- [SDR SB07009](https://openairdocs.org/sdr/SB07009.md): Light · inoperative · Jan 27, 2007 · N512AU · Boeing 7373B7 · Emergency Lighting
  > CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHT ON SEAT ROW 15, LEFT-HAND SIDE WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.
- [SDR USAA061192](https://openairdocs.org/sdr/USAA061192.md): Skin · punctured · Sep 26, 2006 · N512AU · Boeing 7373B7 · Elevator, Plate/Skin
  > RT ELEVATOR UPPER SURFACE APPROX 19.5 INCHES FROM ROOT AND 18.0 INCHES FROM TAB TRAIL. COMPOSITE REPAIR IAW SRM 51-70-17, DEFECT SIZE:.200" X.050".
- [SDR USAA061193](https://openairdocs.org/sdr/USAA061193.md): Skin · cracked · Sep 26, 2006 · N512AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > STA 727D AND 727E ABOVE S-24L CRACKED. INSTALLED DOUBLER IAW EA 98091, DEFECT SIZE: 3.5 INCHES.

Next page: https://openairdocs.org/deregistered/N512AU-2011-05-19/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 = 'N512AU' AND deregistration_id = 'N512AU-2011-05-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N512AU-2011-05-19/reports

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