# Service difficulty reports: N514AU, cancelled Jul 2, 2008

A list on [N514AU, cancelled Jul 2, 2008](https://openairdocs.org/deregistered/N514AU-2008-07-02.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 · 87 reports

- [SDR 2008FA0000435](https://openairdocs.org/sdr/2008FA0000435.md): Cylinder · cracked · Jun 27, 2008 · N514AU · Boeing 7373B7 · Main Landing Gear Strut/Axle/Truck
  > AFTER AIRCRAFT TOW, FLUID WAS OBSERVED LEAKING FROM.5 INCH CRACK (APPROXIMATE) IN THE OUTER CYLINDER OF THE LT MLG SHOCK STRUT. THE CRACK IS LOCATED APPROXIMATELY 26 INCHES BELOW THE SHOCK STRUT AIR VALVE. (K)
- [SDR USAA920081115](https://openairdocs.org/sdr/USAA920081115.md): Stringer · cracked · May 9, 2008 · N514AU · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > MCN - MAJOR REPAIR - B1 CHECK - CRACKED STRINGER, BS 927, S22L. REPAIRED STRINGER, BS 927, S22L IAW B737 SRM 53-00-03 FIGURE 201.
- [SDR USAA920081163](https://openairdocs.org/sdr/USAA920081163.md): Frame · cracked · Apr 24, 2008 · N514AU · Boeing 7373B7 · Fuselage Main, Frame
  > MCN - MAJOR REPAIR - LEASE RETURN - CRACKED FRAME, BS 492, S24R. REPLACED FRAME, BS 492, S24R IAW B737 SRM 51-40-02.
- [SDR USAA920070832](https://openairdocs.org/sdr/USAA920070832.md): Web · cracked · Sep 12, 2007 · N514AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - MAJOR REPAIR - NR 6007491, CRACKED WEB, BS 294.5, S7L. REPLACED WEB, BS 294.5, S7L IAW B737-300 SRM 51-40-02.
- [SDR USAA920070831](https://openairdocs.org/sdr/USAA920070831.md): Tie Clip · cracked · Sep 11, 2007 · N514AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - MAJOR REPAIR - NR 6007482, CRACKED FRAME TIE CLIP, BS 360, S14L - S15L. REPLACED FRAME TIE CLIP, BS 360, S14L - S15L IAW B737-300 SRM 51-40-02.
- [SDR USAA920070830](https://openairdocs.org/sdr/USAA920070830.md): Fitting · cracked · Sep 11, 2007 · N514AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - MAJOR REPAIR - NR 6007479, CRACKED UPPER AND LOWER FRAME CHANNEL CLIPS, BS 348 - BS 351, S16L. REPLACED UPPER AND LOWER FRAME CHANNEL CLIPS, BS 348 - BS 351, S16L IAW B737-300 SRM 51-40-02.
- [SDR USAA920070829](https://openairdocs.org/sdr/USAA920070829.md): Door Frame · cracked · Sep 11, 2007 · N514AU · Boeing 7373B7 · Fuselage Main, Structure
  > CLT - MAJOR REPAIR - NR 6007659, CRACKED WEB, BS 294.5, S12L, FORWARD ENTRY DOOR CUTOUT FORWARD FRAME. REPAIRED WEB, BS 294.5, S12L, FORWARD ENTRY DOOR CUTOUT FORWARD FRAME IAW B737-300 SRM 51-10-02.
- [SDR USAA920070828](https://openairdocs.org/sdr/USAA920070828.md): Door Frame · cracked · Sep 11, 2007 · N514AU · Boeing 7373B7 · Fuselage Main, Structure
  > CLT - MAJOR REPAIR - NR 6007658, CRACKED WEB, BS 294.5, S15L, FORWARD ENTRY DOOR CUTOUT FORWARD FRAME. REPAIRED WEB, BS 294.5, S15L, FORWARD ENTRY DOOR CUTOUT FORWARD FRAME IAW B737-300 SRM 51-10-02.
- [SDR USAA070580](https://openairdocs.org/sdr/USAA070580.md): Beam · cracked · Jul 24, 2007 · N514AU · Boeing 7373B7 · Fuselage, Landing Gear Attach Fittings
  > STA 259.5 AT NOSE W/W CEILING WL 192.5, BL 0, RADIUS OF NOSE GEAR ACT BEAM. REPLACED GUSSET PER SRM 51-10-02, DEFECT SIZE:.75 INCH.
- [SDR USAA061396](https://openairdocs.org/sdr/USAA061396.md): Frame · cracked · Dec 5, 2006 · N514AU · Boeing 7373B7 · Fuselage Main, Frame
  > STA 492.4 S24R CRACKED. REPAIRED IAW SRM 53-30-15 EA 98295, DEFECT SIZE:.50 INCH.
- [SDR SB06097](https://openairdocs.org/sdr/SB06097.md): Switch · shorted · Oct 6, 2006 · N514AU · Boeing 7373B7 · Fire Detection
  > CLT - FLT1770 EN ROUTE FROM MYR TO CLT, CREW REPORTED THAT BOTH THE CAPTAIN'S AND FIRST OFFICER'S FIRE WARNING LIGHTS FLASH CONSTANTLY DURING FLIGHT AND WHILE TAXING AFTER LANDING. SEEMS TO BE ASSOCIATED WITH TURBULENCE IN FLIGHT AND BUMPS ON THE TAXIWAYS AN
- [SDR USAA050063](https://openairdocs.org/sdr/USAA050063.md): Skin · delaminated · Jan 7, 2005 · N514AU · Boeing 7373B7 · Leading Edge Devices
  > PIT - FOUND TOP SKIN CORE BOND DELAMINATED 3 INCHES BY 3 INCHES, NR 5 SLAT OUTBOARD TRAILING EDGE. REMOVED DAMAGE, INSTALLED NEW CORE, FILLERS, DOUBLERS PER SRM 51-70-10. (M)
- [SDR USAA050218A](https://openairdocs.org/sdr/USAA050218A.md): Skin · cracked · Dec 31, 2004 · N514AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 1.375 INCH, FS 727D STRINGER 23R. INSTALLED DOUBLER IAW SRM 53-00-01. (M)
- [SDR USAA041032](https://openairdocs.org/sdr/USAA041032.md): Skin Panel · damaged · Nov 24, 2004 · N514AU · Boeing 7373B7 · Ailerons
  > PIT - Q2 - TOP SKIN PANEL, 2 INCH SQ SINGLE LAYER, COMPOSITE DAMAGE, LT AILERON TOP SKIN PANEL AT TAB CONTROL ROD FAIRING MOUNT SURFACE. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR PLYS, RESTORES FINISH IAW SRM.
- [SDR USAA041031](https://openairdocs.org/sdr/USAA041031.md): Spar · damaged · Nov 24, 2004 · N514AU · Boeing 7373B7 · Ailerons
  > PIT - Q2 - SPAR, 2 INCHES X 1 INCH AREA, COMPOSITE DAMAGE/ DELAMINATION, LT AILERON, LEADING EDGE SPAR 34 INCH FROM OB END, UPPER FLANGE. INSTALLED REPAIR PLYS AND EXTRA IAW EA AND SRM.
- [SDR USAA040701](https://openairdocs.org/sdr/USAA040701.md): Floor Support · bent · Oct 6, 2004 · N514AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > SUPPORT,.2500 INCH X 20 INCH AREA, BENT/LIFTING METAL, BS540 BETWEEN IB AND OB SEAT TRACKS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-10-2.
- [SDR USAA040655](https://openairdocs.org/sdr/USAA040655.md): Doubler · cracked · Sep 22, 2004 · N514AU · Boeing 7373B7 · Nacelle/Pylon, Plate/Skin
  > PIT - FOUND DOUBLER AND SKIN CRACKED.75 INCH LONG, OPENING FOR ACCESS PANEL 5727L, LEFT PYLON NACELLE STATION 180 OUTBOARD SIDE. DOUBLER INSTALLED PER TYPICAL REPAIR 54-30-07. (M)
- [SDR USAA040653](https://openairdocs.org/sdr/USAA040653.md): Beltframe · cracked · Sep 22, 2004 · N514AU · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - FOUND BELTFRAME CRACKED.125 INCH, IN FRAME AT FS 767 LOWER OVERHEAD BIN ATTACH POINT, RIGHT SIDE. INSTALLED REPAIR ANGLES 1 AND 2 PER TYPICAL REPAIR 53-10-20A. (M)
- [SDR USAA040652](https://openairdocs.org/sdr/USAA040652.md): Window Frame · cracked · Sep 22, 2004 · N514AU · Boeing 7373B7 · Fuselage Main, Structure
  > PIT - FOUND WINDOW FRAME CRACKED.25 INCH, UPPER OUTBOARD CORNER OF CAPTAIN WINDOW FRAME. REMOVED DAMAGE, DOUBLER INSTALLED PER SRM 53-10-01. (M)
- [SDR USAA040706](https://openairdocs.org/sdr/USAA040706.md): Fitting · corroded · Sep 21, 2004 · N514AU · Boeing 7373B7 · Horizontal Stabilizer, Attach Fittings
  > PIT - Q2, R-1 LUG.1250 BY.2500 INCH AREA, CORROSION; NO LEVEL OR TASK, RT HORIZ STAB R-1 LUG. CLEANED CORROSION, REMOVED AND REPLACED BUSHING, CAB PLATED IAW SRM 55-10-10, NDTM 0-4-53-10.
- [SDR USAA040705](https://openairdocs.org/sdr/USAA040705.md): Floor Support · corroded · Sep 21, 2004 · N514AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT,Q2, FLOOR SUPPORT.1250 INCH X.2500 INCH AREA, CORROSION, LEVEL 1; TASK NR C53-107-02. FLOOR SUPPORT, BETWEEN STA 312 AND 344, APPROX. 10 INCHES LT OF CENTER. CLEANED, TREATED, PRIMED AND REPLACED FLOOR SUPPORT IAW SRM 53-10-06B.
- [SDR USAA040677](https://openairdocs.org/sdr/USAA040677.md): Anchor Fitting · corroded · Sep 21, 2004 · N514AU · Boeing 7373B7 · Fuselage Main, Attach Fittings
  > ANCHOR FITTINGS; CORROSION; LEVEL 1; TASK NR C53-107-02, ANCHOR FITTINGS AT STA 993R. REPLACED FITTINGS IAW SRM 51-10-2.
- [SDR USAA040657](https://openairdocs.org/sdr/USAA040657.md): Floor Support · cracked · Sep 21, 2004 · N514AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND FLOOR SUPPORT HAS TWO CRACKS.25 INCH, NR 6 SLAT BOARD, 1 AT 4 INCH AND 1 AT 5 INCH OUTBOARD OF DEICING TUBE, 1 AT 5 INCH. CLEANED, TREATED AND PRIMED, REPLACED FLOOR SUPPORT. (M)
- [SDR USAA040654](https://openairdocs.org/sdr/USAA040654.md): Attach Angle · cracked · Sep 21, 2004 · N514AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND ATTACH ANGLE CRACKED 1 INCH LONG, BS 538, STRINGER 22, PACK RAM AIR INLET AREA. FABRICATED AND INSTALLED REPAIR ANGLES PER TR 53-50-03. (M)
- [SDR USAA040635](https://openairdocs.org/sdr/USAA040635.md): Rib · cracked · Sep 19, 2004 · N514AU · Boeing 7373B7 · Wing, Rib/Bulkhead
  > PIT - FOUND RIB CRACKED.5 INCH, RIGHT WING AT RIB STATION 135.5, LOWER CHORD. DOUBLER INSTALLED PER EA 79058. (M)
- [SDR USAA040645](https://openairdocs.org/sdr/USAA040645.md): Keelbeam · worn · Sep 18, 2004 · N514AU · Boeing 7373B7 · Fuselage Main, Keel
  > PIT - FOUND KEEL BEAM.1875 INCH DIAMETER METAL WEAR AROUND FASTENER HOLES, L/N KEEL BEAM LOWER FLANGE BETWEEN BS 704-727. DOUBLER STRAP INSTALLED PER EA 79006. (M)
- [SDR USAA040644](https://openairdocs.org/sdr/USAA040644.md): Keelbeam · worn · Sep 18, 2004 · N514AU · Boeing 7373B7 · Fuselage Main, Keel
  > PIT - FOUND KEEL BEAM WITH DEEP METAL WEAR.1875 INCH AT FASTENER HOLES, KEEL BEAM LOEWR FLANGE BETWEEN BS 727-704. INSTALLED STRAP DOUBLER PER EA 79007. (M)
- [SDR USAA040658](https://openairdocs.org/sdr/USAA040658.md): Spar · cracked · Sep 18, 2004 · N514AU · Boeing 7373B7 · Wing Spar
  > PIT - FOUND UPPER CHORD CRACKED MORE THAN.343, BUT LESS THAN.6285, NR 2 HOLE, LEFT REAR SPAR UPPER CHORD AT RSS 224.14. OVERSIZED HOLE, INSTALLED FILLER, INSTALLED WING SKIN DOUBLER PER EA 78987. (M)
- [SDR USAA040656](https://openairdocs.org/sdr/USAA040656.md): Fitting · cracked · Sep 18, 2004 · N514AU · Boeing 7373B7 · Fuselage, Landing Gear Attach Fittings
  > PIT - FOUND FITTING CRACKED.5 INCH, RT MLG SUPPORT FITTING NR 2 HOLE 5:30 POSITION. REPLACED RT MLG SUPPORT FITTING AND INSTALLED UPPER WING CHORD DOUBLER PER EO 5702V054, EA 78985 AND 78986. (M)
- [SDR USAA040647](https://openairdocs.org/sdr/USAA040647.md): Web · corroded · Sep 14, 2004 · N514AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND WEB CORRODED BETWEEN STATION 794 TO 847, BETWEEN STATION 794 TO 847. WEB AND STRAP REPLACEMENT ON AIR CARGO DOOR SILL PER DWG 65-47957. (M)
- [SDR USAA040702](https://openairdocs.org/sdr/USAA040702.md): Structure · worn · Sep 10, 2004 · N514AU · Boeing 7373B7 · Rudder, Plate/Skin
  > RUDDER, 1 INCH LENGTH, WEAR WITH KNIFE EDGING, LOWER TR EDGE. SCALED DAMAGE IAW EA79025.
- [SDR USAA040638](https://openairdocs.org/sdr/USAA040638.md): Skin · chafed · Sep 10, 2004 · N514AU · Boeing 7373B7 · Rudder, Plate/Skin
  > PIT - FOUND RUDDER COMPOSITE CHAFED 1 INCH BY.125 INCH, RUDDER LOEWR LEFT EDGE 9.5 INCHES FROM TRAILING EDGE. INSTALLED REPAIR PLYS, REINSTALLED HARDWARE AND REFINISHED PER SRM 51-70-17 AND EA 79025. (M)
- [SDR USAA040662](https://openairdocs.org/sdr/USAA040662.md): Skin · chafed · Sep 10, 2004 · N514AU · Boeing 7373B7 · Rudder, Plate/Skin
  > PIT - FOUND RUDDER WITH CHAFE MARKS.25 INCH BY.20 INCH, STATION 174 AT LEFT LEADING EDGE. REMOVED DAMAGE AND APPLIED REPAIR PLYS PER EA 79025 AND SRM 51-70-17. (M)
- [SDR USAA040661](https://openairdocs.org/sdr/USAA040661.md): Skin · damaged · Sep 10, 2004 · N514AU · Boeing 7373B7 · Rudder, Plate/Skin
  > PIT - FOUND RUDDER WITH COMPOSITE DAMAGE 4 INCH BY 5 INCH SINGLE LAYER, STATION 170 PLUS 10 INCHES FROM T/E RT SIDE. REMOVED DAMAGE AND INSTALLED REPAIR PLYS PER EA 79025 AND SRM 51-70-17. (M)
- [SDR USAA040660](https://openairdocs.org/sdr/USAA040660.md): Skin · damaged · Sep 10, 2004 · N514AU · Boeing 7373B7 · Rudder, Plate/Skin
  > PIT - FOUND RUDDER WITH COMPOSITE DAMAGE 5.25 INCH BY 1.5 INCH SINGLE LAYER, STATION 180 PLUS 10 INCHES FROM T/E RT SIDE. REMOVED DAMAGE AND INSTALLED REPAIR PLYS PER EA 79025 AND SRM 51-70-17. (M)
- [SDR USAA040659](https://openairdocs.org/sdr/USAA040659.md): Structure · cracked · Sep 10, 2004 · N514AU · Boeing 7373B7 · Rudder Structure
  > PIT - FOUND RUDDER CRACKED 1 INCH WITH DELAMINATION, LOWER LEFT LEADING EDGE. REMOVED DAMAGE, INSTALLED REPAIR PLYS PER EA 79025, SRM 51-70-17. (M)
- [SDR USAA040700](https://openairdocs.org/sdr/USAA040700.md): Support Angle · corroded · Sep 7, 2004 · N514AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > ANGLE SUPPORT,.1250 INCH X.1250 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-202-01, BS 794, S-25R. REPLACED ANGLE IAW SRM 51-40-02.
- [SDR USAA040704](https://openairdocs.org/sdr/USAA040704.md): Angle · cracked · Sep 3, 2004 · N514AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > ANGLE, 1.5 INCH LONG CRACK, RT WING ROOT, BS 540 AT S22R, AFT END. INSTALLED REPAIR ANGLE DOUBLER IAW T/R 53-50-03.
- [SDR USAA040675](https://openairdocs.org/sdr/USAA040675.md): Hinge Fitting · worn · Sep 3, 2004 · N514AU · Boeing 7373B7 · Wing, Attach Fittings
  > HINGE FITTING WORN.0625 INCH AT PIVOT POINT NR 5 GROUND SPOILER OB AND WBL 169.25. FABRICATED NEW PART IAW MFG DRG 69-39228.
- [SDR USAA040663](https://openairdocs.org/sdr/USAA040663.md): Angle · cracked · Sep 3, 2004 · N514AU · Boeing 7373B7 · Fuselage Main, Attach Fittings
  > PIT - FOUND ANGLE CRACKED 2 INCHES, RT WING ROOT, BS 540 AT S22R. REPLACED CREASE BEAM SECTION PER SRM 51-40-00. (M)
- [SDR USAA040703](https://openairdocs.org/sdr/USAA040703.md): Floor Support · cracked · Sep 2, 2004 · N514AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT,.5 INCH CRACK, DAMAGE AREA FLOORBEAM, STA727B, LBBL 8-10. MODIFIED REPAIR ANGLE IAW TR 53-10-06B, INSTALLED DOUBLER.
- [SDR USAA040708](https://openairdocs.org/sdr/USAA040708.md): Floorbeam · corroded · Sep 1, 2004 · N514AU · Boeing 7373B7 · Fuselage Main, Floor Beam
  > T-CAP, 1 INCH BY 1 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, STA 328 BL 0, RBL 59 INCH, 3 AREAS. INSTALLED NEW T CAP PER SRM 53-10-51.
- [SDR USAA040637](https://openairdocs.org/sdr/USAA040637.md): Skin · chafed · Aug 31, 2004 · N514AU · Boeing 7373B7 · Rudder, Plate/Skin
  > PIT - FOUND RUDDER CHAFED 1 INCH BY.125 INCH, LOWER LT EDGE 9.5 INCH FROM TRAILING EDGE. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR PLYS, SEAL REPAIR AND REFINISH PER SRM 51-70-17. (M)
- [SDR USAA040643](https://openairdocs.org/sdr/USAA040643.md): Stiffener · corroded · Aug 31, 2004 · N514AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND STIFFENER CORRODED 1 INCH BY 1 INCH AREA, FLOOR SUPPORT BETWEEN STATION 312-328 RBL 11. REPLACED STIFFENER PER SRM 51-40-02. CORROSION LEVEL 1, TASK NR C53-107-02. (M)
- [SDR USAA040639](https://openairdocs.org/sdr/USAA040639.md): Skin · cracked · Aug 31, 2004 · N514AU · Boeing 7373B7 · Rudder, Plate/Skin
  > PIT - FOUND RUDDER CRACKED WITH DELAMINATION AND PEELING, RUDDER LOWER LEFT LEADING EDGE. INSTALLED REPAIR PLYS, SEAL REPAIR AND REFINISH PER SRM 51-70-17 AND EA 79025. (M)
- [SDR USAA040669](https://openairdocs.org/sdr/USAA040669.md): Bushing · corroded · Aug 30, 2004 · N514AU · Boeing 7373B7 · Horizontal Stabilizer Structure
  > PIT - FOUND BUSHING CORRODED.25 INCH BY.125 INCH AREA, LEFT HORIZONTAL NR 12 LUG. NEW BUSHING INSTALLED PER SRM 55-10-10. (M)
- [SDR USAA040668](https://openairdocs.org/sdr/USAA040668.md): Bushing · corroded · Aug 30, 2004 · N514AU · Boeing 7373B7 · Horizontal Stabilizer Structure
  > PIT - FOUND BUSHING CORRODED.125 INCH BY.125 INCH AREA, LEFT HORIZ STABILIZER STAB NR 9 LUG. MADE NEW BUSHING PER SRM 55-10-10. (M)
- [SDR USAA040666](https://openairdocs.org/sdr/USAA040666.md): Bushing · corroded · Aug 30, 2004 · N514AU · Boeing 7373B7 · Horizontal Stabilizer Structure
  > PIT - FOUND BUSHING CORRODED.25 INCH BY.25 INCH AREA, RIGHT HORIZ STAB R10 LUG. MADE NEW BUSHING AMS 4640 PER SRM 55-10-10. (M)
- [SDR USAA040665](https://openairdocs.org/sdr/USAA040665.md): Bushing · corroded · Aug 30, 2004 · N514AU · Boeing 7373B7 · Horizontal Stabilizer Structure
  > PIT - FOUND BUSHING CORRODED.125 INCH BY.125 INCH, RIGHT HORIZ STAB, R-8 CLEVIS BUSHING. MADE NEW BUSHINGS WITH AMS 4640 PER SRM 55-10-10. (M)
- [SDR USAA040664](https://openairdocs.org/sdr/USAA040664.md): Bushing · corroded · Aug 30, 2004 · N514AU · Boeing 7373B7 · Horizontal Stabilizer Structure
  > PIT - FOUND BUSHING CORRODED.125 INCH BY.125 INCH AREA, RT HORIZ STAB R-10 LUG. NEW BUSHING INSTALLED PER SRM 55-10-10. (M)

Next page: https://openairdocs.org/deregistered/N514AU-2008-07-02/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 = 'N514AU' AND deregistration_id = 'N514AU-2008-07-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N514AU-2008-07-02/reports

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