# Service difficulty reports: N408US, cancelled Sep 8, 2003

A list on [N408US, cancelled Sep 8, 2003](https://openairdocs.org/deregistered/N408US-2003-09-08.md).

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

- [SDR USA2002F00052](https://openairdocs.org/sdr/USA2002F00052.md): Sensor · cut · Jun 5, 2002 · N408US · Boeing 737401 · Landing Gear Position and Warning
  > AFTER TAKEOFF, AT APPROXIMATELY 100 FEET, CAPTAIN ATTEMPTED TO RAISE THE LANDING GEAR BUT THE GEAR HANDLE FAILED TO RETRACT. CAPTAIN ATTEMPTED TO RAISE THE LANDING GEAR BUT THE GEAR HANDLE FAILED TO RETRACT. CAPTAIN CONTINUED FLIGHT TO 5,000 FEET AND STILL W
- [SDR USA2002F00054](https://openairdocs.org/sdr/USA2002F00054.md): Circuit Board · faulty · Jun 3, 2002 · N408US · Boeing 737401 · Landing Gear Position and Warning
  > AFTER TAKEOFF, CREW COULD NOT GET THE LANDING GEAR SELECTOR HANDLE TO MOVE PAST THE OFF POSITION TO RAISE THE GEAR. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND NOTED THAT THE TAKEOFF WARNING HORN DID NOT SOUND WITH THE FLAPS UP. HOWEVER, THERE WAS
- [SDR USAASB02081](https://openairdocs.org/sdr/USAASB02081.md): Wire · damaged · Apr 24, 2002 · N408US · Boeing 737401 · Air Conditioning System Wiring
  > CLT - FLT 1050 - CLIMBING OUT OF CLT, PASSING FL270, AIRCRAFT LOST PRESSURIZATION. CREW PERFORMED AN EMERGENCY DESCENT TO 10,000 FEET. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPAIRED NUMEROUS LEAKS AT THE FORWARD AND AFT ENT
- [SDR USAASB02030](https://openairdocs.org/sdr/USAASB02030.md): Vane · damaged · Feb 10, 2002 · N408US · Boeing 737401 · Stall Warning System
  > BUF - FLT 437 - ON ROTATION OUT OF BUF, EN ROUTE TO PHL, THE FIRST OFFICER REPORTED THE AIRCRAFT WENT INTO A CONTINUOUS STICK SHAKER MODE. CAPTAIN CHECKED FLAP SETTINGS AND FOUND NO INDICATIONS OF ANY OTHER ABNORMALITIES OTHER THAN THE STICK SHAKER WARNING.
- [SDR USAASB01223](https://openairdocs.org/sdr/USAASB01223.md): Socket · defective · Aug 6, 2001 · N408US · Boeing 737401 · Emergency Lighting
  > CLT - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHT, THAT ILLUMINATES THE AREA AFT OF THE FLAPS, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY EXIT LIGHT SOCKET. OPS CHECK GOOD. (M)
- [SDR USAA010776](https://openairdocs.org/sdr/USAA010776.md): Bulkhead · cracked · Jul 2, 2001 · N408US · Boeing 737401 · Fuselage Main, Bulkhead
  > CLT - FOUND BULKHEAD WEB CRACKED NUMEROUS AREAS.5 INCH TO 1.5 INCH, BS 178, WL 186 TO 234, LBL 12 TO RBL 6.5. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER AND FILLERS PER EO 5300V153 AND EA 69888. (M)
- [SDR USAA010777](https://openairdocs.org/sdr/USAA010777.md): Frame · cracked · Jul 2, 2001 · N408US · Boeing 737401 · Fuselage Main, Frame
  > CLT - FOUND SIDE CHORDS CRACKED TWO PLACES 1.5 INCH EACH, BS 178 WL 207 LEFT AND RIGHT. DAMAGE REMOVED, SPLICED IN NEW CHORD SECTION PER EO 5300V157. (M)
- [SDR USAA010778](https://openairdocs.org/sdr/USAA010778.md): Pressure Panel · cracked · Jul 2, 2001 · N408US · Boeing 737401 · Fuselage Main, Bulkhead
  > CLT - FOUND FLOORWEB CRACKED.5 INCH, BS 178 WL 207 LEFT SIDE. REMOVED AND REPLACED WEB PER EO 5300V157. (M)
- [SDR USAA010779](https://openairdocs.org/sdr/USAA010779.md): Web · cracked · Jul 2, 2001 · N408US · Boeing 737401 · Fuselage Structure (General)
  > CLT - FOUND WEB CRACKED.5 INCH, BS 178 WL 207 AT RIGHT SIDE CHORD. DAMAGE REMOVED, INSTALLED DOUBLER PER EO 5300V157. (M)
- [SDR USAASB00277](https://openairdocs.org/sdr/USAASB00277.md): Battery Pack · discharged · Sep 28, 2000 · N408US · Boeing 737401 · Emergency Lighting
  > PVD - MAINTENANCE FOUND THE FOLLOWING EMERGENCY LIGHTS INOPERATIVE, RIGHT OVERWING INTERIOR LIGHT, CEILING BULLNOSE LIGHT AT SEAT ROW 9 LEFT, LEFT EXTERIOR AFT OVERWING LIGHT AND SEAT ROW 11 LEFT EXIT IDENTIFIER LIGHT. MAINTENANCE REMOVED AND REPLACED THE BAT
- [SDR USAASB00201](https://openairdocs.org/sdr/USAASB00201.md): Fitting · worn · Jul 29, 2000 · N408US · Boeing 737401 · Elevator Tab, Attach Fittings
  > CLT - FLT 532 - ON CLIMB-OUT FROM SRQ, EN ROUTE TO CLT, A/C BEGAN TO EXPERIENCE AN AIRFRAME VIBRATION. VIBRATION BECAME ABNORMALLY PRONOUNCED WITH CONSTANT INTENSITY REGARDLESS OF AIRSPEED OR POWER SETTING. VIBRATION WAS MOST EVIDENT IN THE AFT GALLEY AND TA
- [SDR USAASB99111](https://openairdocs.org/sdr/USAASB99111.md): Battery Charger · failed · Apr 21, 1999 · N408US · Boeing 737401 · Emergency Lighting
  > IAH - MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY EXIT LIGHTING AT SEAT ROWS 12 THROUGH 19 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER AT STATION 747, LEFT SIDE. OPERATIONAL CHECK GOOD. (M)
- [SDR USAASB98303](https://openairdocs.org/sdr/USAASB98303.md): Battery Pack · discharged · Oct 5, 1998 · N408US · Boeing 737401 · Emergency Lighting
  > IAH - MAINTENANCE FOUND THE AFT LEFT SERVICE DOOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)
- [SDR USAA980358](https://openairdocs.org/sdr/USAA980358.md): Frame · cracked · Aug 24, 1998 · N408US · Boeing 737401 · Fuselage Main, Frame
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A SMALL CRACK.25 INCH AT RIVET HOLE FUSELAGE FRAME 500A BETWEEN S8L AND S9L. CUT OUT DAMAGE FILL AND DOUBLER PER SRM 53-00-07 FIG 202. (M)
- [SDR USAA980357](https://openairdocs.org/sdr/USAA980357.md): Floorbeam · corroded · Aug 24, 1998 · N408US · Boeing 737401 · Fuselage Main, Floor Beam
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION AROUND CLIP NUT HOLE.5 INCH BY.5 INCH STATION 328 FLOORBEAM UPPER CHORD BL0. CORROSION TASK NR C53-107-02. INSTALLED DOUBLER PER SRM 53-10-51 FIG 206. (M)
- [SDR USAA980356](https://openairdocs.org/sdr/USAA980356.md): Floorbeam · corroded · Aug 24, 1998 · N408US · Boeing 737401 · Fuselage Main, Floor Beam
  > CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION ON STATION 967 LBBL 5-0 FLOORBEAM. CORROSION TASK NR C53-107-02. REPAIRED ONE FLANGE UPPER CHORD PER SRM 53-00-51 FIG 203. (M)
- [SDR USAA980355](https://openairdocs.org/sdr/USAA980355.md): Floorbeam · corroded · Aug 24, 1998 · N408US · Boeing 737401 · Fuselage Main, Floor Beam
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND.5 INCH BY.5 INCH AREA OF CORROSION AROUND NUTPLATE HOLES STATION 312 LBL 12 TO RBL 12 FLOORBEAM UPPER CHORD. CORROSION TASK NR C53-107-02. SPLICED IN A NEW 'T' CAP SECTION PER SRM 53-10-51. (M)
- [SDR USAA980354](https://openairdocs.org/sdr/USAA980354.md): Frame · cracked · Aug 24, 1998 · N408US · Boeing 737401 · Fuselage Main, Frame
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK BS 727G BETWEEN STRINGER 8R AND STRINGER 9R FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M)
- [SDR USAA980353](https://openairdocs.org/sdr/USAA980353.md): Frame · cracked · Aug 24, 1998 · N408US · Boeing 737401 · Fuselage Main, Frame
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK BS 727E BETWEEN S8R AND S9R FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M)
- [SDR USAA980352](https://openairdocs.org/sdr/USAA980352.md): Frame · cracked · Aug 24, 1998 · N408US · Boeing 737401 · Fuselage Main, Frame
  > CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK BS 787 BETWEEN S8R AND S9R FRAME. INSTALLED DOUBLER PER SRM 53-00-07. (M)
- [SDR USAA980351](https://openairdocs.org/sdr/USAA980351.md): Frame · cracked · Aug 24, 1998 · N408US · Boeing 737401 · Fuselage Main, Frame
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK BS 867 BETWEEN S8R AND S9R FRAME. INSTALLED DOUBLER PER SRM 53-00-07. (M)
- [SDR USAA980350](https://openairdocs.org/sdr/USAA980350.md): Frame · cracked · Aug 24, 1998 · N408US · Boeing 737401 · Fuselage Main, Frame
  > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK BS 827 BETWEEN S8R AND S9R ON FRAME. INSTALLED DOUBLER PER SRM 53-00-07. (M)
- [SDR USAA980348](https://openairdocs.org/sdr/USAA980348.md): Frame · cracked · Aug 24, 1998 · N408US · Boeing 737401 · Fuselage Main, Frame
  > CLT - DURING A Q-3 CHECK VISUAL INSPECTION FOUND A SMALL CRACK.250 INCH AT RIVET HOLE FUSELAGE FRAME 380 BETWEEN S8L AND S9L. CUT OUT DAMAGED AREA AND REPAIRED WITH FILLER AND DOUBLER PER SRM 53-00-07 FIG 202. (X)
- [SDR USAASB98146](https://openairdocs.org/sdr/USAASB98146.md): Air Filter · dirty · Jun 6, 1998 · N408US · Boeing 737401 · Fuel Storage
  > MCI - FLT 165 - EN ROUTE TO PHX, CREW COULD NOT TRANSFER FUEL OUT OF THE AUXILIARY FUEL TANK. CREW PULLED ALL AUXILIARY FUEL TANK CIRCUIT BREAKERS AND RESET THEM PER MAINTENANCE CONTROL. COULD NOT RESET AFT TRANSFER CIRCUIT BREAKER ON FIRST ATTEMPT, BUT BREA
- [SDR USAASB97255](https://openairdocs.org/sdr/USAASB97255.md): Window · cracked · Sep 16, 1997 · N408US · Boeing 737401 · Flight Compartment Windows
  > CLT (FL 1515) - AT 28,000 FEET, THE CAPTAIN'S WINDSHIELD CRACKED. HIS VISION WAS OBSCURED AND THE AIRCRAFT RETURNED TO FIELD (CLT). THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MTC REPLACED THE LEFT NR 1 WINDOW ASSEMBLY. LEAK AND OPS CHECK GOOD. (X)
- [SDR USAASB95033](https://openairdocs.org/sdr/USAASB95033.md): Egt Ind · high · Dec 30, 1995 · N408US · Boeing 737401 · Engine EGT/TIT Indicating System
  > FLT 818 - PIT - FLIGHT DIVERTED TO PIT DUE TO NR 1 ENGINE HIGH EGT. (M)
- [SDR USAA950461](https://openairdocs.org/sdr/USAA950461.md): Eel Fuse · inoperative · May 8, 1995 · N408US · Boeing 737401 · Emergency Lighting
  > PVD - ROWS 10, 11, 12L AISLE MARKER EMERGENCY LIGHTS INOPERATIVE AND EMERGENCY LIGHT FOR LEFT ESCAPE WINDOW INOPERATIVE. MAINTENANCE REPLACED FUSE IN BATTERY PACK M1479 AT STATION 598. (W)

## 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 = 'N408US' AND deregistration_id = 'N408US-2003-09-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N408US-2003-09-08/reports

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