# Service difficulty reports: N352US, cancelled Sep 6, 2006

A list on [N352US, cancelled Sep 6, 2006](https://openairdocs.org/deregistered/N352US-2006-09-06.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 2 · 78 reports

- [SDR SB05131](https://openairdocs.org/sdr/SB05131.md): Power Supply · inoperative · Oct 13, 2005 · N352US · Boeing 737301 · Emergency Lighting
  > MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 12 THROUGH 16 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD.
- [SDR SB05123](https://openairdocs.org/sdr/SB05123.md): Battery Pack · discharged · Sep 26, 2005 · N352US · Boeing 737301 · Emergency Lighting
  > PHL - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT ABOVE THE L2 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK PER MM 33-51-51. OPERATIONAL CHECK GOOD.
- [SDR SB05112](https://openairdocs.org/sdr/SB05112.md): Outflow Valve · leaking · Sep 9, 2005 · N352US · Boeing 737301 · Pressure Regulator/Outflow Valve
  > AIRCRAFT WOULD NOT MAINTAIN CABIN PRESSURIZATION. AT FL030, CABIN ALTITUDE CLIMBED 1,200 FEET PER MINUTE WITH OUTFLOW VALVE FULLY CLOSED. CREW DESCENDED BELOW FL020 BEFORE CABIN ALTITUDE WOULD DESCEND BELOW 8,000 FEET. FLIGHT CONTINUED. MX PRESSURIZED AIRC
- [SDR USAA040844](https://openairdocs.org/sdr/USAA040844.md): Skin · cracked · Nov 12, 2004 · N352US · Boeing 737301 · Service Doors
  > FWD SERVICE DOOR SKIN,.1875 INCH CRACK, UPPER HINGE CUTOUT, LWR RADIUS TO DRAIN HOLE. INSTALLED DOUBLER IAW TYP REP 52-10-13.
- [SDR USAA041040](https://openairdocs.org/sdr/USAA041040.md): Skin · gouged · Nov 11, 2004 · N352US · Boeing 737301 · Elevator, Plate/Skin
  > PIT - Q4 - LOWER SKIN SURFACE, SINGLE LAYER COMPOSITE DAMAGE.75 INCH GOUGE, RT ELEVATOR AT 84.5 AND 4 - 5 INCH IN FROM FWD SPAR. PREPARED DAMAGED AREA, APPLIED WET LAY UP REPAIR IAW SRM AND EA.
- [SDR USAA041039](https://openairdocs.org/sdr/USAA041039.md): Skin · gouged · Nov 11, 2004 · N352US · Boeing 737301 · Elevator, Plate/Skin
  > PIT - Q4 -LOWER SKIN SURFACE, SINGLER LAYER COMPOSITE DAMAGE.50 INCH GOUGE. RT ELEVATOR AT STA 62 AND 15 INCHES FROM FWD SPAR. PREPARED DAMAGED AREA, APPLIED WET LAY UP REPAIR PER SRM AND EA.
- [SDR USAA041038](https://openairdocs.org/sdr/USAA041038.md): Skin · gouged · Nov 11, 2004 · N352US · Boeing 737301 · Elevator, Plate/Skin
  > PIT - Q4 - LOWER SKIN SURFACE, SINGLE LAYER COMPOSITE DAMAGE.50 INCH GOUGE, RT ELEVATOR AT STA 71 AND 10 INCHES FROM FWD SPAR. PREPARED DAMAGED AREA, APPLIED WET LAY UP REPAIR IAW SRM AND EA.
- [SDR USAA041037](https://openairdocs.org/sdr/USAA041037.md): Skin · damaged · Nov 11, 2004 · N352US · Boeing 737301 · Elevator, Plate/Skin
  > PIT - Q4 - LOWER SKIN SURFACE, SINGLE LAYER COMPOSITE, 2 GOUGES 1.25 INCHES, COMPOSITE DAMAGE, 2 GOUGES, RT ELEVATOR AT STA 70 AND 8 TO 9 INCHES FROM FWD SPAR. PREPARED DAMAGED AREA, SUPPLIED WET LAY UP REPAIR IAW SRM AND EA.
- [SDR USAA041036](https://openairdocs.org/sdr/USAA041036.md): Skin · damaged · Nov 11, 2004 · N352US · Boeing 737301 · Elevator, Plate/Skin
  > PIT - Q4 - LOWER SKIN SURFACE, COMPOSITE DAMAGE,.3750 INCH GOUGE, COMPOSITE DAMAGE - SINGLE LAYER, RT ELEVATOR AT STA 64 + 7 INCH FROM FWD SPAR. REPAIRED DAMAGED AREA, APPLIED WET LAY UP REPAIR PER SRM AND EA.
- [SDR USAA041035](https://openairdocs.org/sdr/USAA041035.md): Skin · damaged · Nov 11, 2004 · N352US · Boeing 737301 · Elevator, Plate/Skin
  > PIT - Q4 - LOWER SKIN, COMPOSIT DAMAGE.3750 INCH GOUGING. COMPOSITE DAMAGE - SINGLE LAYER RT ELEVATOR AT STA 68 + 6 INCHES FROM FWD SPAR LOWER SKIN. PREPARED DAMAGED AREA, APPLIED WET LAY UP REPAIR IAW SRM AND EA.
- [SDR USAA041034](https://openairdocs.org/sdr/USAA041034.md): Skin · delaminated · Nov 11, 2004 · N352US · Boeing 737301 · Elevator, Plate/Skin
  > PIT - Q4 - LOWER SKIN SURFACE, 2 INCH SQ DELAMINATION, RT LELVATOR 41 INCH FROM IB END AND 13 INCH AFT OF L/E. REMOVED DAMAGED SKIN AND CORE, INSTALLED SER COR, REPLACEMENT SKIN PANEL IAW SRM, EA.
- [SDR USAA040973](https://openairdocs.org/sdr/USAA040973.md): Fitting · cracked · Nov 11, 2004 · N352US · Boeing 737301 · Fuselage, Landing Gear Attach Fittings
  > PIT- Q4 - MLG SUPPORT BEAM AFT FITTING,.0625 INCH CRACK (2) HOLES ON MLG SUPPORT AFT BEAM FITTING, 12 O`CLOCK AND 9 O`CLOCK. REPLACED LT MGL SUPPORT BEAM AFT FITTING IAW EO 5702V054.
- [SDR USAA040972](https://openairdocs.org/sdr/USAA040972.md): Spar · cracked · Nov 11, 2004 · N352US · Boeing 737301 · Wing Spar
  > PIT - Q4 - LT SPAR UPPER CHORD,.0625 INCH CRACK; NR 2 HOLE VERTICAL LEG OF LT SPAR UPPER CHORD AT MLG SUPPORT. INSTALLED FATIGUE ENHANCEMENT PLATE IAW EA 79286A.
- [SDR USAA040971](https://openairdocs.org/sdr/USAA040971.md): Doubler · cracked · Nov 11, 2004 · N352US · Boeing 737301 · Wing, Plate/Skin
  > PIT - Q4 - DOUBLER,.25 INCH LONG CRACKS (2 EA), RT WING FUEL PANEL REBATE PANEL NR 8817R. INSTALLED EXT DOUBLER.125 THICK IAW EA 79453.
- [SDR USAA040875](https://openairdocs.org/sdr/USAA040875.md): Flange · cracked · Nov 11, 2004 · N352US · Boeing 737301 · Wing Miscellaneous Structure
  > FUEL PLATE FLANGE, (2 EA).189 INCH IN LENGTH, CRACK (2) FUEL PANEL NR 881, 17R, 6 O`CLOCK AND 12 O`CLOCK POSITIONS. STOP DRILLED CRACKS, TRIMMED SKIN PANEL, INSTALLED FILLER AND DOUBLER IAW EA 79453.
- [SDR USAA040874](https://openairdocs.org/sdr/USAA040874.md): Stiffener · cracked · Nov 3, 2004 · N352US · Boeing 737301 · Fuselage Miscellaneous Structure
  > STIFFENER,.1250 INCH CRACK, LBL 5.7 IB AND OB SIDE 8 INCH IN FROM BOTTOM. STRAPS, ANGLES AND FILLERS INSTALLED ON BOTH SIDES OF VERT CORD IAW EO 5300V155 AND EA 79321.
- [SDR USAA040856](https://openairdocs.org/sdr/USAA040856.md): Frame · cracked · Oct 30, 2004 · N352US · Boeing 737301 · Fuselage Main, Frame
  > PIT - Q4 - FRAME,.2500 INCH CRACK. CRACK EMANATING FROM FASTENER, FRAME STA 867 AND STR 9L. INSTALLED DOUBLERS IAW TYP REP 53-10-20A.
- [SDR USAA040855](https://openairdocs.org/sdr/USAA040855.md): Frame · cracked · Oct 30, 2004 · N352US · Boeing 737301 · Fuselage Main, Frame
  > PIT - Q4 - FRAME,.1250 INCH CRACK, STA 787 AND STR 9L. INSTALLED DOUBLERS IAE TYP REP 53-10-20A.
- [SDR USAA040854](https://openairdocs.org/sdr/USAA040854.md): Frame · cracked · Oct 30, 2004 · N352US · Boeing 737301 · Fuselage Main, Frame
  > FRAME,.3750 INCH CRACK, STA 540 BETWEEN RT IB SEAT TRACK, RBL 24.75 AND CRT FLOOR SUPPORT BEAM BL 0. DEFECTIVE PART, REPLACED WITH IDENT PN IAW MFG DWG 65-46819.
- [SDR USAA040857](https://openairdocs.org/sdr/USAA040857.md): Frame · cracked · Oct 30, 2004 · N352US · Boeing 737301 · Fuselage Main, Structure
  > PIT - Q4, FRAME,.1250 INCH CRACK, EMANATING FROM FASTENER, FRAME STA 847, STR 9L. INSTALLED DOUBLERS IAW TYPE REP 53-10-20A.
- [SDR USAA040862](https://openairdocs.org/sdr/USAA040862.md): Angle · worn · Oct 28, 2004 · N352US · Boeing 737301 · Fuselage Miscellaneous Structure
  > ANGLE, 4, DEEP WEAR MARKS, VERT SUPPORT Z, VERT OB LEG AT AFT LEG GEAR WELL CUTOUT CORNER. DEFECTIVE PART REPLACED WITH IDENT PART IAW MFG DWG 65-48690.
- [SDR USAA040864](https://openairdocs.org/sdr/USAA040864.md): Skate Angle · chafed · Oct 25, 2004 · N352US · Boeing 737301 · Fuselage Miscellaneous Structure
  > SKATE ANGLE, 11 INCHES LONG, EXCESSIVELY DEEP CHAFE MARK, 1104 TO 1121, STR 2 L.
- [SDR USAA040845](https://openairdocs.org/sdr/USAA040845.md): Frame · cracked · Oct 22, 2004 · N352US · Boeing 737301 · Fuselage Main, Frame
  > FRAME,.5 INCH CRACK, STR 9 LT AT FRAME, STA 767. REMOVED DAMAGE AND INSTALLED REPAIR ANGLES IAW TR 53-10-20A.
- [SDR USAA040863](https://openairdocs.org/sdr/USAA040863.md): Skin · gouged · Oct 22, 2004 · N352US · Boeing 737301 · Fuselage Main, Plate/Skin
  > Q4, SKIN, 16 INCHES W BY 22 INCHES L, GOUGES, STA 887 BETWEEN S35R AND S27R. REMOVED DAMAGE, INSTALLED DOUBLER IAW SRM 53-00-01.
- [SDR USAA040853](https://openairdocs.org/sdr/USAA040853.md): Frame · cracked · Oct 21, 2004 · N352US · Boeing 737301 · Fuselage Main, Frame
  > FRAME.2500 INCH LONG CRACK BS 360 ON FRAME BETWEEN S8L AND S9L. INSTALLED REPAIR ANGLES IAE TYP REP 53-10-20A.
- [SDR USAA040851](https://openairdocs.org/sdr/USAA040851.md): Frame · cracked · Oct 21, 2004 · N352US · Boeing 737301 · Fuselage Main, Frame
  > FRAME,.1250 INCH CRACK, CRACKED AROUND RIVET AT FRAME AT STA 827, STR 9L. REMOVED CRACK AND INSTALLED REPAIR ANGLES IAW TR 53-10-20A.
- [SDR USAA040850](https://openairdocs.org/sdr/USAA040850.md): Stringer · cracked · Oct 21, 2004 · N352US · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > STRINGER,.5 INCH LONG CRACK, STR 7L AT BS 1010. INSTALLED REPAIR ANGLE IAW 53-00-03.
- [SDR USAA040849](https://openairdocs.org/sdr/USAA040849.md): Frame · cracked · Oct 21, 2004 · N352US · Boeing 737301 · Fuselage Main, Frame
  > FRAME.2500 INCH CRACK, FRAME STA 787 AND STR 9R, CRACK EMANATING FROM FASTENER. INSTALLED REPAIR DOUBLER IAW TR 53-10-20A.
- [SDR USAA040861](https://openairdocs.org/sdr/USAA040861.md): Attach Bracket · damaged · Oct 21, 2004 · N352US · Boeing 737301 · Spoilers
  > PIT - Q4, ATTACH BRACKET, MIGRATING AND MISSING BUSHINGS. RT MLG SUPPORT BEAM, SPOILER ACT ATTACH BRACKET. REPLACED SPOILER ACTUATOR ATTACH BRACKET IAW MFG DWG 63895.
- [SDR USAA040860](https://openairdocs.org/sdr/USAA040860.md): Fitting · worn · Oct 21, 2004 · N352US · Boeing 737301 · Wing, Landing Gear Attach Fittings
  > PIT - Q4, STAB BEAM FITTING, WORN BUSHING. STAB BEAM LUG, RT MLG SUPPORT BEAM. REPLACED STAB BEAM FITTING IAW AMM 57-15-00-434.
- [SDR USAA040859](https://openairdocs.org/sdr/USAA040859.md): Hanger Assy · worn · Oct 21, 2004 · N352US · Boeing 737301 · Fuselage, Landing Gear Attach Fittings
  > PIT - Q4, WALKING BEAM HANGAR, WORN BUSHINGS. RT MAIN LANDING SUPPORT BEAM. REPLACED WALKING BEAM HANGAR IAW AMM 57-15-00-434.
- [SDR USAA040952](https://openairdocs.org/sdr/USAA040952.md): Stringer · cracked · Oct 20, 2004 · N352US · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > PIT - Q4 - STRINGER,.1250 INCH CRACKS, CRACKS IN STRING AROUND FASTENERS, STA 907, STR 4R. DEFECTIVE PART REPLACED WITH IDENT PART IAW MFG DWG 65-45772.
- [SDR USAA040872](https://openairdocs.org/sdr/USAA040872.md): Skate Angle · chafed · Oct 20, 2004 · N352US · Boeing 737301 · Fuselage Miscellaneous Structure
  > PIT - Q4 - SKATE ANGLE, 10 INCHES, CHAFED, 1006 TO 1016 BETWEEN STR 2L AND 3L. FABRICATED NEW ANGLE IAW MFG ENG DWG 65-548423.
- [SDR USAA040873](https://openairdocs.org/sdr/USAA040873.md): Skate Angle · chafed · Oct 20, 2004 · N352US · Boeing 737301 · Fuselage Miscellaneous Structure
  > SKATE ANGLE, 10 INCHES OF CHAFING, 1006 TO 1016 BETWEEN STR 2R AND 3R. FABRICATED NEW ANGLE FROM ENG DWG 65548424.
- [SDR USAA040876](https://openairdocs.org/sdr/USAA040876.md): Stringer · cracked · Oct 20, 2004 · N352US · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > PIT - Q4, STRINGER,.1250 INCH CRACK, STA 907, STR4L, AROUND FASTENERS. DEFECTIVE PART REPLACED WITH IDENT PART IAW DWG 65-52988.
- [SDR USAA040848](https://openairdocs.org/sdr/USAA040848.md): Frame · cracked · Oct 19, 2004 · N352US · Boeing 737301 · Fuselage Main, Frame
  > FRAME,.5 INCH CRACK, FRAME STA907,STR9L, CRACK EMANATING FROM FASTENER. CUTOUT CRACKED AREA AND INSTALLED REPAIR ANGLES IAW T.R. 53-10-20A.
- [SDR USAA040882](https://openairdocs.org/sdr/USAA040882.md): Fitting · corroded · Oct 19, 2004 · N352US · Boeing 737301 · Wing, Landing Gear Attach Fittings
  > PIT - Q4, FITTING, 1 INCH BY.5 INCH AREA, CORROSION; NO LEVEL OR TASK. RT WING AFT SPAR OB BUSHING BORE FTG WALKING BEAM HANGAR LUG AT STA 202. REMOVED AND REPLACED FITTING IAW MFG DWG 6545321 AND SRM 51-20-25.
- [SDR USAA040858](https://openairdocs.org/sdr/USAA040858.md): Bracket · cracked · Oct 19, 2004 · N352US · Boeing 737301 · Wing Miscellaneous Structure
  > BRACKET, 1 INCH CRACK, LT WING SPAR (AFT) STA 218, MFG NEW BRACKET IAW J020-37-20.
- [SDR USAA040847](https://openairdocs.org/sdr/USAA040847.md): Intercostal · cracked · Oct 18, 2004 · N352US · Boeing 737301 · Fuselage Miscellaneous Structure
  > INTERCOSTAL,.5 INCH CRACK, STA 947.5, LBL43. REPLACED INTERCOSTAL IAW SRM 51-70-11.
- [SDR USAA040883](https://openairdocs.org/sdr/USAA040883.md): Stringer · corroded · Oct 18, 2004 · N352US · Boeing 737301 · Fuselage Main, Longeron/Stringer
  > STRINGER, 6 INCHES FULL WIDTH AND SIDES, CORROSION; LEVEL 1; TASK NR C53-208-01, STR 27 R JUST FWD OF FRAME, STA 1006. CUT STR REPAIR SECTION TO FIT AND INSTALLED REPAIR IAW 53-00-03.
- [SDR USAA040880](https://openairdocs.org/sdr/USAA040880.md): Fitting · corroded · Oct 18, 2004 · N352US · Boeing 737301 · Fuselage Main, Attach Fittings
  > PIT - Q4, LAV FLOOR ANCHOR FITTING, 2 AREAS, 1 INCH BY 2 INCHES, CORRODED; LEVEL 1; TASK NR C53-107-02, LT AFT LAV STA 986.5. REMOVED AND REPLACED FITTING (2 EA) IAW SRM 51-10-02.
- [SDR USAA040881](https://openairdocs.org/sdr/USAA040881.md): Anchor Fitting · corroded · Oct 18, 2004 · N352US · Boeing 737301 · Fuselage Main, Attach Fittings
  > PIT - Q4, LAV FLOOR ANCHOR FITTING, 2 INCHES BY 2 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, RT LAV FLOOR STA 1016.
- [SDR USAA040877](https://openairdocs.org/sdr/USAA040877.md): Floorbeam · cracked · Oct 16, 2004 · N352US · Boeing 737301 · Fuselage Main, Floor Beam
  > PIT - Q4, BEAM, ABOUT.5 INCH, CRACKED, FLOOR SUPPORT BEAM, STA 540 AND LT OB SEAT TRACK. DEFECTIVE PART REPLACED WITH IDENT PART IAW DWG 65-46819-4.
- [SDR USAA040741](https://openairdocs.org/sdr/USAA040741.md): Door Frame · cracked · Oct 15, 2004 · N352US · Boeing 737301 · Fuselage Main, Structure
  > PIT, Q4, EDGE FRAME SERVICE DOOR,.5 INCH CRACK, EDGE FRAME CRACKED, FWD SERVICE DOOR AFT EDGE FRAME, MID STOP AREA. INSTALLED DOUBLER IAW TYPE REP 52-10-11.
- [SDR USAA040852](https://openairdocs.org/sdr/USAA040852.md): Door Frame · cracked · Oct 14, 2004 · N352US · Boeing 737301 · Fuselage Main, Structure
  > PIT - Q4 - DOOR EDGE FRAME,.5 INCH CRACK, FWD SERVICE DOOR AFT END FRAME AT MIDSTOP FITTING. ROUTED OUT CRACK, INSTALLED DOUBLER IAW TYP REP 52-10-11.
- [SDR USAA040878](https://openairdocs.org/sdr/USAA040878.md): Attach Bracket · cracked · Oct 14, 2004 · N352US · Boeing 737301 · Fuselage Main, Attach Fittings
  > ATTACH BRACKET,.5 INCH LONG CRACK, S10L, STA 360. MANUFACTURED ATTACH BRACKET IAW SRM 51-40-03.
- [SDR USAA040884](https://openairdocs.org/sdr/USAA040884.md): Floorbeam · corroded · Oct 12, 2004 · N352US · Boeing 737301 · Fuselage Main, Floor Beam
  > FLOORBEAM, 2 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, LBL 30.5 BETWEEN STA 947.5 AND 967. REMOVED AND REPLACED DEFECTIVE PART WITH IDENT PART IAW SRM 51-10-02.
- [SDR USAA040885](https://openairdocs.org/sdr/USAA040885.md): Floor Support · corroded · Oct 12, 2004 · N352US · Boeing 737301 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT, 4 INCHES BY 1 INCH, CORROSION; LEVEL 1; TASK NR C53-107-02, RBL 17.61, STA 986.5 TO 967. REMOVED AND REPLACED DEFECTIVE PART WITH IDENT PART IAW SRM 51-10-02.
- [SDR USAA040886](https://openairdocs.org/sdr/USAA040886.md): Support · corroded · Oct 12, 2004 · N352US · Boeing 737301 · Fuselage Miscellaneous Structure
  > SUPPORT, 5 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, LBL 25 BETWEEN STA 947.5 AND 967.
- [SDR USAA040846](https://openairdocs.org/sdr/USAA040846.md): Frame · cracked · Oct 11, 2004 · N352US · Boeing 737301 · Fuselage Main, Frame
  > FRAME, 1.7500 INCH CRACK, BS 787, STR 9L. REPAIRED IAW TYP REP 53-10-20A.

Next page: https://openairdocs.org/deregistered/N352US-2006-09-06/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 = 'N352US' AND deregistration_id = 'N352US-2006-09-06'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N352US-2006-09-06/reports

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