# Service difficulty reports: N396US, cancelled Apr 27, 2006

A list on [N396US, cancelled Apr 27, 2006](https://openairdocs.org/deregistered/N396US-2006-04-27.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR USAA200511003](https://openairdocs.org/sdr/USAA200511003.md): Skin · cracked · Nov 2, 2005 · N396US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > A 2.5 INCH CRACK FOUND IN FUSELAGE SKIN. INSTALLED EXT SKIN DOUBLER PER SRM 53-00-01 FIG 2.
- [SDR USAA200511002](https://openairdocs.org/sdr/USAA200511002.md): Skin · cracked · Oct 31, 2005 · N396US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > 2.5 INCH CRACK FOUND AT STA 727E AT STRINGER 23L. REPAIR: INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 FIG. 201.
- [SDR USAA200511001](https://openairdocs.org/sdr/USAA200511001.md): Skin · cracked · Oct 31, 2005 · N396US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > 1.5 INCH CRACK FOUND STA 867 AT STRINGER S23R. REPAIR: INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 FIG. 201.
- [SDR SB05088](https://openairdocs.org/sdr/SB05088.md): Battery Pack · discharged · Aug 7, 2005 · N396US · Boeing 7373B7 · Emergency Lighting
  > PIT - MAINTENANCE REPORTED THE FORWARDED EMERGENCY LIGHTS NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD.
- [SDR USAA050177](https://openairdocs.org/sdr/USAA050177.md): Skin · cracked · Jan 27, 2005 · N396US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED, STATION 727D STRINGER S24L. INSTALLED DOUBLER IAW SRM 53-00-01. (M)
- [SDR SB04152](https://openairdocs.org/sdr/SB04152.md): Pump · leaking · Nov 7, 2004 · N396US · Boeing 7373B7 · Hydraulic Pump (Electric/Engine), Main
  > BOS - FLT2039 - ON CLIMB-OUT FROM BOS, EN ROUTE TO DCA, THE B SYSTEM HYDRAULIC FLUID BEGAN TO DECREASE AND THE B SYSTEM ENGINE DRIVEN PUMP LOW PRESSURE LIGHT AND MASTER CAUTION LIGHT ILLUMINATED. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT BOS. FLIGH
- [SDR USA2004F00049](https://openairdocs.org/sdr/USA2004F00049.md): Panel · loose · May 16, 2004 · N396US · Boeing 7373B7 · Nacelle/Pylon, Plate/Skin
  > (2) SECONDS PRIOR TO TOUCHDOWN, A PASSENGER REPORTED THAT TWO PANELS DEPARTED THE NR 1 ENGINE PYLON. ONE PANEL WAS REPORTED THO HAVE STRUCK THE LT HORIZONTAL STABILIZER LEADING EDGE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 1 ENGINE P
- [SDR USAA040199](https://openairdocs.org/sdr/USAA040199.md): Vertical Support · cracked · Apr 26, 2004 · N396US · Boeing 7373B7 · Fuselage Main, Structure
  > SUPPORT (1.5 INCH CRACKED) CRACKED. VERTICAL SUPPORT AT LBL 5.7.
- [SDR USAASB03188](https://openairdocs.org/sdr/USAASB03188.md): Socket · inoperative · Oct 19, 2003 · N396US · Boeing 7373B7 · Emergency Lighting
  > DURING EMERGENCY LIGHT, BULLNOSE, AT ROW 9 INOPERATIVE. MAINTENANCE REPAIRED A SHORT AT THE LIGHT SOCKET AND PROGRAMMED THE SOCKET FOR REPLACEMENT. (M)
- [SDR USAA030170](https://openairdocs.org/sdr/USAA030170.md): Skin · cracked · Aug 21, 2003 · N396US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > FOUND SKIN CRACKED 3 INCHES,.5 INCH BELOW STRINGER S12L, FORWARD OF FS 520. INSTALLED DOUBLER PER SRM 53-00-01 FIG 201 AND 202. (M)
- [SDR USAA030161](https://openairdocs.org/sdr/USAA030161.md): Skin · cracked · Aug 18, 2003 · N396US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > FOUND SKIN CRACKED 3 INCHES, FORWARD OF FS 520,.500 INCH BELOW S12L. INSTALLED DOUBLER PER SRM 53-00-01. (M)
- [SDR USAA030002](https://openairdocs.org/sdr/USAA030002.md): Skin · cracked · Jan 6, 2003 · N396US · Boeing 7373B7 · Leading Edge Devices
  > PIT - FOUND SKIN CRACKED.5 INCH IN TWO PLACES, NR 6 SLAT LOWER LEADING EDGE SKIN NEAR ACTUATOR FITTING. REPAIRED WITH FILLER AND DOUBLER PER SRM 57-43-01 FIG 206. (M)
- [SDR USAA020074](https://openairdocs.org/sdr/USAA020074.md): Skin · cracked · Feb 15, 2002 · N396US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 2 INCHES, SKIN AT S19R, BS 753-755, SECTION 46. INSTALLED DOUBLER PER SRM 53-00-01, FIG 225 AND STRINGER REPAIR CHANNEL PER 53-00-03 PAGE 213. (M)
- [SDR USAASB01341](https://openairdocs.org/sdr/USAASB01341.md): Light · inoperative · Dec 19, 2001 · N396US · Boeing 7373B7 · Emergency Lighting
  > PHL - FOUND SEAT MOUNTED EMERGENCY EXIT SIGN INOPERATIVE AT LEFT OVERWING EXIT. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB01344](https://openairdocs.org/sdr/USAASB01344.md): O-Ring · failed · Dec 18, 2001 · N396US · Boeing 7373B7 · Air Distribution System
  > PHL - FLT 735 - EN ROUTE FROM ROT TO PHL, CREW REPORTED A STRONG EXHAUST SMELL THROUGH OUT THE CABIN THAT DID NOT DISSIPATE THE ENTIRE FLIGHT. MAINTENANCE FOUND THE RIGHT TURBO FAN DRAIN SEEPING. REMOVED AND REPLACED O-RING. CLEANED PACK BAY ON RIGHT SIDE A
- [SDR USAASB00272](https://openairdocs.org/sdr/USAASB00272.md): Battery Pack · discharged · Sep 25, 2000 · N396US · Boeing 7373B7 · Emergency Lighting
  > ALB - MAINTENANCE FOUND THE LEFT OVERWING EXIT SIGN, THE CENTER AISLE EXIT SIGN ON CEILING AT ROW 10 AND RIGHT SIDE BULL NOSE LIGHTS AT ROW 16, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)
- [SDR USAASB00027](https://openairdocs.org/sdr/USAASB00027.md): Valve · failed · Jan 29, 2000 · N396US · Boeing 7373B7 · Waste Disposal System
  > EN ROUTE, EXPERIENCED UNCOMMANDED NR 2 ENG SHUTDOWN. CAPT DECLARED AN EMERGENCY, DIVERTED TO PHL. TOTAL SINGLE ENG TIME WAS 20 MIN. AT GATE, STREAKS OF BLUE ICE WERE NOTICED DOWN THE SIDE OF A/C AND FWD LAV DOOR WAS BULGING WITH BLUE ICE. MX DETERMINED THE
- [SDR USAA990970](https://openairdocs.org/sdr/USAA990970.md): Skin · cracked · Sep 4, 1999 · N396US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PHL - DURING RON, FOUND 1.5 INCH CRACK ON SKIN AT STATION 747 STRINGER 25R. REPAIRED WITH EXTERNAL DOUBLER PER SRM 53-00-01 FIG 202. (M)
- [SDR USAA980647](https://openairdocs.org/sdr/USAA980647.md): Floorbeam · corroded · Dec 18, 1998 · N396US · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION UNDER SIDE FLOORBEAM STATION 986 LBL 3. CORROSION TASK NR C 53-107-02. INSTALLED 'T' CAP PER SRM 53-00-51 FIG 202. (M)
- [SDR USAA980641](https://openairdocs.org/sdr/USAA980641.md): Frame · cracked · Dec 18, 1998 · N396US · Boeing 7373B7 · Fuselage Main, Frame
  > CLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH HOLE IN FRAME/APU BLEED DUCT STATION 1040. INSTALLED REPAIR DOUBLER PER EA 63138 AND TR 53-80-02. (M)
- [SDR USAA980640](https://openairdocs.org/sdr/USAA980640.md): Floorbeam · corroded · Dec 18, 1998 · N396US · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 88 INCH BY 1 INCH BS 1016 RBL 6 FLOORBEAM, CORROSION TASK NR C53-107-02. T-CAP FLOORBEAM REPLACED PER TR 53-10-05. (M)
- [SDR USAA980639](https://openairdocs.org/sdr/USAA980639.md): Frame · cracked · Dec 18, 1998 · N396US · Boeing 7373B7 · Fuselage Main, Frame
  > CLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK BS 727 STRINGER 14L FRAME WEB. INSTALLED FILLER AND DOUBLER PER EA 63060. (M)
- [SDR USAA980638](https://openairdocs.org/sdr/USAA980638.md): Angle · corroded · Dec 18, 1998 · N396US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION ON SURFACE STATION 222 RT 27 INCH ABOVE FLOORLINE ANGLE. CORROSION TASK NR C53-101-01. REMOVED SURFACE CORROSION PER SRM 51-10-6. (M)
- [SDR USAA980624](https://openairdocs.org/sdr/USAA980624.md): Web · cracked · Dec 18, 1998 · N396US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.75 INCH CRACK MLG WHEEL WELL LBL 30 WEB PANEL. INSTALLED WEB AND STIFFENER PER EA 63025 AND SRM 53-60-51. (M)
- [SDR USAA980623](https://openairdocs.org/sdr/USAA980623.md): Frame · cracked · Dec 18, 1998 · N396US · Boeing 7373B7 · Fuselage Main, Frame
  > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK BS 867, 1 INCH ABOVE S 9R FRAME. INSTALLED DOUBLER AND FILLER PLUG PER SRM 53-00-07 FIG 202. (M)
- [SDR USAA980622](https://openairdocs.org/sdr/USAA980622.md): Frame · cracked · Dec 18, 1998 · N396US · Boeing 7373B7 · Fuselage Main, Frame
  > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK BS 440, 1 INCH ABOVE S 9R FRAME WEB. INSTALLED DOUBLER PER SRM 53-00-07. (M)
- [SDR USAA980621](https://openairdocs.org/sdr/USAA980621.md): Frame · cracked · Dec 18, 1998 · N396US · Boeing 7373B7 · Fuselage Main, Frame
  > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK BS 480, 1 INCH ABOVE S 9L FRAME WEB. INSTALLED DOUBLER PER SRM 53-00-07. (M)
- [SDR USAA980620](https://openairdocs.org/sdr/USAA980620.md): Frame · cracked · Dec 18, 1998 · N396US · Boeing 7373B7 · Fuselage Main, Frame
  > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK BS 380, 1 INCH ABOVE S 9R FRAME WEB. FABRICATED A FILLER AND DOUBLER PER SRM 53-00-07. (M)
- [SDR USAA980619](https://openairdocs.org/sdr/USAA980619.md): Frame · cracked · Dec 18, 1998 · N396US · Boeing 7373B7 · Fuselage Main, Frame
  > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK BS 807, S 9L FRAME. INSTALLED FILLER AND DOUBLER PER SRM 53-00-07 FIG 202. (M)
- [SDR USAA980618](https://openairdocs.org/sdr/USAA980618.md): Frame · cracked · Dec 18, 1998 · N396US · Boeing 7373B7 · Fuselage Main, Frame
  > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK BS 907, S 9L FRAME. INSTALLED FILLER AND DOUBLER PER SRM 53-00-07 FIG 202. (M)
- [SDR USAA980617](https://openairdocs.org/sdr/USAA980617.md): Angle · cracked · Dec 18, 1998 · N396US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK NOSE WHEEL WELL, NOSE GEAR ACTUATOR SUPPORT STRUCTURE ANGLE. REPLACED GUSSET AND ACTUATOR MOUNT PER BOEING DRAWING 65-45819. (M)
- [SDR USAA980616](https://openairdocs.org/sdr/USAA980616.md): Frame · cracked · Dec 18, 1998 · N396US · Boeing 7373B7 · Fuselage Main, Frame
  > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK BS 887, S 9R FRAME. INSTALLED FILLER AND DOUBLER PER SRM 53-00-07 FIG 202. (M)
- [SDR USAA980608](https://openairdocs.org/sdr/USAA980608.md): Frame · cracked · Dec 18, 1998 · N396US · Boeing 7373B7 · Fuselage Main, Frame
  > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.5 INCH BY 20 INCH CORROSION AREA AND A.25 INCH CRACK STATION 295 TO STATION 360 RBL 60 INNER CHORD ANGLE. CORROSION TASK NR C53-107-02. INSTALLED PART PER SRM 51-10-02. (M)
- [SDR USAA980607](https://openairdocs.org/sdr/USAA980607.md): Clip · cracked · Dec 18, 1998 · N396US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK STATION 639 STRINGER 4L STRINGER TIE CLIP. INSTALLED PART PER SRM 51-10-2. (M)
- [SDR USAA980379](https://openairdocs.org/sdr/USAA980379.md): Skin · cracked · Aug 30, 1998 · N396US · Boeing 7373B7 · Landing Gear Doors
  > TPA - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND.125 INCH CRACK ON DOOR OUTER SKIN FORWARD SERVICE DOOR LOWER HINGE CUTOUT AFT UPPER CORNER. INSTALLED DOUBLER MADE FROM.063 2024 T-3 PER EA 62369 AND SB 737-52-1096. (M)
- [SDR USAA980378](https://openairdocs.org/sdr/USAA980378.md): Skin · cracked · Aug 30, 1998 · N396US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > TPA - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND AN.25 INCH CRACK IN EXTERNAL SKIN AFT OF EQUIPMENT COOLING DUCT OUTLET STATION 380 LBL 30. INSTALLED DOUBLER OF.100 2024 T-3 PER EA 62368 SB 737-53-1117 REV 1. (M)
- [SDR USAA950551](https://openairdocs.org/sdr/USAA950551.md): Sill · corroded · May 22, 1995 · N396US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND DOOR SILL SKIN CORRODED BS 794-847 IN AFT CARGO DOOR CUTOUT. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)
- [SDR USAA950554](https://openairdocs.org/sdr/USAA950554.md): Intercostal · corroded · May 5, 1995 · N396US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TOTAL AREA OF CORROSION.25 INCH BY 10 INCH, 6 INTERCOSTALS CORRODED AND NUTPLATE HOLES BS 294-344, 3 AT LBL 11 BS 294-344, 3 AT RBL 11 BS 294-344. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROS
- [SDR USAA950556](https://openairdocs.org/sdr/USAA950556.md): Intercostal · corroded · May 4, 1995 · N396US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA ON INTERCOSTAL AT CABIN BS 907 THROUGH 947 RBL 10 INCHES. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA950555](https://openairdocs.org/sdr/USAA950555.md): Intercostal · corrosion · May 3, 1995 · N396US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION OUT OF LIMITS.25 INCH BY 10 INCHES ON INTERCOSTAL AT BS 947 THROUGH 967 RBL 10 INCHES. REPAIRED PER SRM 51-10-0. CORROSION TASK NR C53-108-02, CORROSION LEVEL 2. (M)
- [SDR USAA950553](https://openairdocs.org/sdr/USAA950553.md): Angle · corroded · May 1, 1995 · N396US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 60 INCH CORRODED AREA S-17L, BS 312-372 (FORWARD ENTRY DOOR SILL ANGLE). REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA950552](https://openairdocs.org/sdr/USAA950552.md): Floorbeam · corroded · May 1, 1995 · N396US · Boeing 7373B7 · Fuselage Main, Floor Beam
  > INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO 1 INCH BY 2 INCH CORRODED AREA, BS 328 FLOORBEAM, RBL 14 AND RBL 21. REPAIRED PER TR 53-10-03 AND SRM 53-10-51. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)

## 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 = 'N396US' AND deregistration_id = 'N396US-2006-04-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N396US-2006-04-27/reports

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