# Service difficulty reports: N394US, cancelled Jul 18, 2006

A list on [N394US, cancelled Jul 18, 2006](https://openairdocs.org/deregistered/N394US-2006-07-18.md).

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

- [SDR SB05116](https://openairdocs.org/sdr/SB05116.md): Bracket · missing · Sep 19, 2005 · N394US · Boeing 7373B7 · Escape Slide
  > ORD - PILOT REPORTED MISSING HARDWARE FOR THE FORWARD BRACKET OF THE R2 SERVICE DOOR ESCAPE SLIDE. MAINTENANCE REPLACED MISSING HARDWARE FOR THE FORWARD BRACKET OF THE R2 SERVICE DOOR ESCAPE SLIDE.
- [SDR USAA050452](https://openairdocs.org/sdr/USAA050452.md): Frame · broken · Apr 2, 2005 · N394US · Boeing 7373B7 · Fuselage Main, Frame
  > CLT - FOUND FORMER BROKEN, STATION 535 WL 165, LBL 60. REPLACED FORMER. (M)
- [SDR SB05032](https://openairdocs.org/sdr/SB05032.md): Circuit Breaker · burned · Feb 23, 2005 · N394US · Boeing 7373B7 · AC Power Distribution System
  > AFTER LANDING CREW STOPPED A/C ON TAXIWAY & REPORTED TO INBOUND RAMP, FIRE & SMOKE IN COCKPIT. CREW STATED, "ON TAXI-IN, FIRE ERUPTED FROM F/O LWR C/B PNL. USED PORTABLE HALON FIRE EXTINGUISHER & EVACUATED A/C. ENG 1 & 2 & APU FIRE EXTINGUISHER BOTTLES DISCH
- [SDR USAA040834](https://openairdocs.org/sdr/USAA040834.md): Skin · cracked · Oct 8, 2004 · N394US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > SKIN, 1 INCH CRACK, BS 727D, STR 22R. INSTALLED DOUBLER IAW SRM 53-00-01. INSTALLED DOUBLER IAW SRM 53-00-01.
- [SDR USAA040507](https://openairdocs.org/sdr/USAA040507.md): Skin · cracked · Aug 12, 2004 · N394US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED 1.250 INCH, STATION 727D, STRINGER 23L. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M)
- [SDR USAA040360](https://openairdocs.org/sdr/USAA040360.md): Skin · cracked · Jul 26, 2004 · N394US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED APPROXIMATELY.375 INCH CRACK, AFT CARGO DOOR FORWARD FRAME CUTOUT. REMOVED EXISTING REPAIR AND INSTALLED DOUBLER PER EA 78434. (M)
- [SDR USAA040344](https://openairdocs.org/sdr/USAA040344.md): Skin · cracked · Jul 16, 2004 · N394US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN CRACKED 2 INCHES, TWO 4.5 INCHES AFT OF 867, 1 INCH BELOW STRINGER 15R. INSTALLED DOUBLER PER SRM 53-00-01 DETAIL XI. (M)
- [SDR USAA040206](https://openairdocs.org/sdr/USAA040206.md): Skin · cracked · May 6, 2004 · N394US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > SERVICE DOOR CUTOUT (.2500 INCH CRACK) AFT CORNER AT STA 332.101 FWD TO DOOR CUTOUT. REPAIRED IAW 53-10-01 FIG 202, PAGE 207.
- [SDR USAA030218](https://openairdocs.org/sdr/USAA030218.md): Skin · cracked · Oct 28, 2003 · N394US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > FOUND SKIN CRACKED 2.375 INCH, STATION 740 AND S23R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M)
- [SDR USAASB03074](https://openairdocs.org/sdr/USAASB03074.md): Odor · detected · Jun 7, 2003 · N394US · Boeing 7373B7 · Air Distribution System
  > TEN MINUTES AFTER TAKEOFF FROM CLT, FLIGHT ATTENDANT REPORTED AN ELECTICAL ODOR ALONG WITH A SLIGHT HAZE IN THE CABIN FROM SEAT ROWS 4 THROUGH 14. AS A PRECAUTION, CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT CLT. FLIGHT LANDED WITHOUT FURTHER INCIDEN
- [SDR USAA030080](https://openairdocs.org/sdr/USAA030080.md): Skin · cracked · May 22, 2003 · N394US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > FOUND SKIN CRAKCED.75 INCH LONG CRACK, SKIN AFT ENTRY DOOR LOWER HINGE CUTOUT STATION 947.5, STRINGER 14L. DOUBLER AND TRIPLER INSTALLED AND PAINTED PER SRM 53-60-01 AND EA 76329. (M)
- [SDR USAA030081](https://openairdocs.org/sdr/USAA030081.md): Skin · cracked · May 22, 2003 · N394US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED.75 INCH LONG, SKIN AFT SERVICE DOOR LOEWR HINGE CUTOUT STATION 947.5, STRINGER 14R. DOUBLE AND TRIPLER INSTALLED AND PAINTED PER SRM 53-60-01. (M)
- [SDR USAASB02186](https://openairdocs.org/sdr/USAASB02186.md): Slide · malfunctioned · Sep 30, 2002 · N394US · Boeing 7373B7 · Escape Slide
  > DURING ANNUAL OPERATIONAL CHECK OF THE FORWARD RIGHT SERVICE DOOR ESCAPE SLIDE, THE SLIDE APPEARED TO HAVE PREMATURELY INFLATED AND BECAME TWISTED 90 DEGREES. DOOR BECAME DIFFICULT TO OPEN FULLY ONCE SLIDE BEGAN TO INFLATE. SLIDE OPERATIONAL CHECK FAILED. M
- [SDR USA2002F00092](https://openairdocs.org/sdr/USA2002F00092.md): Slide · failed · Sep 30, 2002 · N394US · Boeing 7373B7 · Escape Slide
  > DURING ANNUAL OPERATIONAL CHECK OF THE FORWARD RIGHT SERVICE DOOR ESCAPE SLIDE, THE SLIDE APPEARED TO HAVE PREMATURELY INFLATED AND BECAME TWISTED 90 DEGREES. DOOR BECAME DIFFICULT TO OPEN FULLY ONCE SLIDE BEGAN TO INFLATE. SLIDE OPERATIONAL CHECK FAILED. M
- [SDR USAASB02115](https://openairdocs.org/sdr/USAASB02115.md): Wire · broken · Jun 16, 2002 · N394US · Boeing 7373B7 · Light System Wiring
  > CLT - FOUND MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 20C INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE UNDER SEAT ROW 20C. OPERATIONAL CHECK GOOD. (M)
- [SDR USAA020198](https://openairdocs.org/sdr/USAA020198.md): Stringer · cracked · May 22, 2002 · N394US · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > PIT - FOUND SHELF WITH.25 INCH CRACK ON EACH SIDE OF FASTENER, AFT END OF S18 LEFT SHELF AT AFT INBOARD FASTENER. REPLACED 18A SHELF ASSEMBLY PER SRM 51-40-02. (M)
- [SDR USAA020191](https://openairdocs.org/sdr/USAA020191.md): Frame · corroded · May 21, 2002 · N394US · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED 1 INCH BY 3 INCH CORRODED AREA, FS 500B, BETWEEN STRINGERS 27L AND 28L. REMOVED CORROSION PER SRM 51-40-02. (M)
- [SDR USAA020199](https://openairdocs.org/sdr/USAA020199.md): Stringer · corroded · May 21, 2002 · N394US · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > PIT - FOUND SHELF WITH 3 AREAS OF CORROSION, 1 INCH ROUND, 2 INCH BY 2 INCH, 2 INCH BY 3 INCH, 6 INCHES TO 8 INCHES AFT OF STATION 706 ON LEFT 18A SHELF. REMOVED CORROSION PER SRM 51-10-02. (M)
- [SDR USAA020200](https://openairdocs.org/sdr/USAA020200.md): Stringer · corroded · May 21, 2002 · N394US · Boeing 7373B7 · Fuselage Main, Longeron/Stringer
  > PIT - FOUND 1 INCH ROUND CORRODED AREA, BETWEEN STATION 695 AND 706 ON LEFT SIDE 18A SHELF INBOARD. REMOVED CORROSION PER SRM 51-10-02. (M)
- [SDR USAA020192](https://openairdocs.org/sdr/USAA020192.md): Frame · corroded · May 21, 2002 · N394US · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - FOUND FRAME CORRODED 1 INCH BY 1 INCH CORRODED AREA, STATION 500B, BETWEEN STRINGERS 28L AND 28R. INSTALLED FABRICATED SHEAR TIE PER SRM 51-70-11. (M)
- [SDR USAA020193](https://openairdocs.org/sdr/USAA020193.md): Frame · cracked · May 21, 2002 · N394US · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED.5 INCH, FS 887 RIGHT AT STRINGER 9R. INSTALLED FRAME DOUBLER PER T/R 53-10-14A. (M)
- [SDR USAA020194](https://openairdocs.org/sdr/USAA020194.md): Frame · cracked · May 21, 2002 · N394US · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED.5 INCH, FS 827 RIGHT AT STRINGER 9R. INSTALLED FRAME DOUBLER PER T/R 53-10-14A. (M)
- [SDR USAA020195](https://openairdocs.org/sdr/USAA020195.md): Support · cracked · May 21, 2002 · N394US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > PIT - FOUND ANTENNA SUPPORT ZEE 1.25 INCH CRACK, HORIZONTAL LEG OF ANTENNA ZEE SUPPORT STATION 727D AND 727C. REPLACED ZEE SUPPORT PER SRM 51-40-05. (M)
- [SDR USAA020196](https://openairdocs.org/sdr/USAA020196.md): Doubler · cracked · May 21, 2002 · N394US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > PIT - FOUND DOUBLER CRACKED 1 INCH, ANTENNA DOUBLER BETWEEN STATION 727D AND 727E. REPLACED ZEE SUPPORT AND MOUNT BRACKET PER SRM 51-40-05. (M)
- [SDR USAA020197](https://openairdocs.org/sdr/USAA020197.md): Frame · cracked · May 21, 2002 · N394US · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED 1 INCH, FRAME 807 LEFT AT FASTENER STRINGER 9. INSTALLED ANGLES, SHIMS, STRAP PER T/R 53-10-14A. (M)
- [SDR USAA020216](https://openairdocs.org/sdr/USAA020216.md): Doubler · corroded · May 21, 2002 · N394US · Boeing 7373B7 · Fuselage Main, Structure
  > PIT - FOUND ANTENNA DOUBLER CORRODED SIX.25 INCH BY.25 INCH AREAS, ANTENNA MOUNT NUTPLATE BRACKETS BETWEEN STATION 727D. REMOVED CORROSION AND REPLACED CHANNEL PER SRM 53-30-53, 51-40-05. CORROSION LEVEL 1, TASK NR C53-208-01. (M)
- [SDR USAA020171](https://openairdocs.org/sdr/USAA020171.md): Skin · corroded · Apr 24, 2002 · N394US · Boeing 7373B7 · Rudder, Plate/Skin
  > PIT - FOUND RIB AND SKIN WITH HEAVY CORROSION 4 INCHES LONG BY 1 INCH WIDE, RUDDER COUNTER BALANCE STRUCTURE, RUDDER STATION 121.64. LEVEL 2 CORROSION. (M)
- [SDR USAA020170](https://openairdocs.org/sdr/USAA020170.md): Frame · cracked · Apr 15, 2002 · N394US · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - FOUND FRAME CRACKED.062 INCH, FRAME 480 LEFT SIDE BETWEEN S8L AND S9L. REPAIRED PER TYPICAL REPAIR 53-10-14A. (M)
- [SDR USAA020172](https://openairdocs.org/sdr/USAA020172.md): Frame · cracked · Apr 15, 2002 · N394US · Boeing 7373B7 · Fuselage Main, Frame
  > PIT - FOND FRAME CRACKED.064 INCHES LONG, FRAME 400 RIGHT SIDE BETWEEN S8R AND S9R. ACCOMPLISHED TYPICAL REPAIR 53-10-14A. (M)
- [SDR USAASB01115](https://openairdocs.org/sdr/USAASB01115.md): Fuse · blown · Apr 27, 2001 · N394US · Boeing 7373B7 · Emergency Lighting
  > TPA - MAINTENANCE FOUND THE FORWARD EMERGENCY EGRESS LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TWO 5 AMPS FUSES. OPS CHECK GOOD. (M)
- [SDR USAASB01114](https://openairdocs.org/sdr/USAASB01114.md): Light · inoperative · Apr 27, 2001 · N394US · Boeing 7373B7 · Emergency Lighting
  > TPA - MAINTENANCE FOUND SEAT 5C EMERGENCY SEAT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED SPLICE. OPS CHECK GOOD. (M)
- [SDR USAASB01106](https://openairdocs.org/sdr/USAASB01106.md): Transmission · failed · Apr 20, 2001 · N394US · Boeing 7373B7 · Trailing Edge Flap Control System
  > IAD - FLT 1083 - ON APPROACH TO DCA, CAPTAIN REPORTED THAT THE FLAPS WERE STUCK AT 10 DEGREES. CREW CHECKED ALL CIRCUIT BREAKERS AND TRIED ALTERNATE METHOD WITH NO HELP. FLIGHT DIVERTED TO IAD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED.
- [SDR USAA000850](https://openairdocs.org/sdr/USAA000850.md): Skin · cracked · Jun 14, 2000 · N394US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - FOUND SKIN FUSELAGE CRACKED 1.5 INCH, BS 727D PLUS 17.5 INCH JUST ABOVE STRINGER 23R. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-00-01 FIG 202 AND TR 53-60-03. (M)
- [SDR USAA000451](https://openairdocs.org/sdr/USAA000451.md): Skin · cracked · Mar 23, 2000 · N394US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - FOUND FUSELAGE SKIN CRACKED 2.125 INCHES, STRINGER 24L JUST FORWARD OF BS 727E. INSTALLED EXTERNAL DOUBLER PER EA 66901. (M)
- [SDR USAASB99215](https://openairdocs.org/sdr/USAASB99215.md): Stud · loose · Aug 31, 1999 · N394US · Boeing 7373B7 · Engine Oil Indicating System
  > DFW - FLT 870 - CAPTAIN REPORTED THAT AFTER TAKEOFF FROM DFW AND CLIMBING THROUGH 17,000 FT, THE NR 1 ENGINE OIL TEMPERATURE ROSE ABOVE THE RED RADIAL. CREW SHUTDOWN THE NR 1 ENGINE, DECLARED AN EMERGENCY AND RETURNED TO FIELD AT DFW. FLIGHT LANDED WITHOUT F
- [SDR USAA990798](https://openairdocs.org/sdr/USAA990798.md): Skin · cracked · Aug 3, 1999 · N394US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > TPA - DURING CX-1 CHECK EDDY CURRENT, FOUND A.25 INCH CRACK BELLY SKIN AFT EQUIPMENT COOLING EXHAUST STA 380 FUSELAGE SKIN. INSTALLED REPAIRED DOUBLER PER TR 53-30-07. (X)
- [SDR USAA990279](https://openairdocs.org/sdr/USAA990279.md): Skin · cracked · Mar 31, 1999 · N394US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - DURING A RON VISUAL INSPECTION, FOUND A 1.25 INCH CRACK LEFT SIDE OF FUSELAGE AT STRINGER 24L, 24 INCHES AFT OF AFT WING TO BODY FAIRING SKIN. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-00-01. (M)
- [SDR USAA980371](https://openairdocs.org/sdr/USAA980371.md): Beam · corroded · Aug 27, 1998 · N394US · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON UPPER SURFACE OF CREASEBEAM INNER CHORD RBBL BETWEEN STATION 294.5 TO STATION 331. CORROSION TASK NR C53-107-02. INSTALLED SPLICE PER DRAWING 6545875 AND SRM 51-10-02. (M)
- [SDR USAA980370](https://openairdocs.org/sdr/USAA980370.md): Floorbeam · corroded · Aug 27, 1998 · N394US · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A.5 INCH BY.5 INCH BY 11 INCH AREA OF CORROSION ON UPPER FLOORBEAM CHORD STATION 1016 LBL 15, CORROSION TASK NR C53-107-02. INSTALLED 11.5 INCH DOUBLER PER SRM 53-00-51 FIG 203. (M)
- [SDR USAA980369](https://openairdocs.org/sdr/USAA980369.md): Floorbeam · corroded · Aug 27, 1998 · N394US · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON 'T' CAP OF FLOORBEAM 65 INCH BY 3.5 INCH STATION 312 LBL 8 RBL 56 FLOORBEAM UPPER CHORD. CORROSION TASK NR C53-107-02. FABRICATED 'T' CAP ANGLES PER TR 53-10-03. (M)
- [SDR USAA980368](https://openairdocs.org/sdr/USAA980368.md): Floorbeam · corroded · Aug 27, 1998 · N394US · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND FLOORBEAM BOARD SCREW HOLES.5 INBY.5 BY 70 INCH STATION 328 BETWEEN RBL 14 TO RBL 56 UPPER CHORD. CORROSION TASK NR C53-107-02. SPLICED IN NEW 'T' CAP SECTION PER SRM 53-10-51. (M)
- [SDR USAA980367](https://openairdocs.org/sdr/USAA980367.md): Floorbeam · corroded · Aug 27, 1998 · N394US · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND FLOORBOARD SCREW HOLES.5 INCH BY.5 INCH BY 25 INCH STATION 344 BETWEEN LBL 14 TO RBL 11 UPPER CHORD FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED NEW 'T' CAP AND SPLICED ANGLES PER TR 53
- [SDR USAA980366](https://openairdocs.org/sdr/USAA980366.md): Skin · cracked · Aug 27, 1998 · N394US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AFT SERVICE DOOR INSIDE UPPER FRAME SKIN, UPPER HINGE ARM CLOSEOUT. INSTALLED DOUBLER PER TYPICAL REPAIR 53-30-07 AND EA 62249. (M)
- [SDR USAA980174](https://openairdocs.org/sdr/USAA980174.md): Skin · cracked · Apr 25, 1998 · N394US · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > CLT - DURING RON VISUAL INSPECTION, FOUND A 2.675 INCH CRACK IN THE SKIN AT RIGHT BS 727D AT S23R. INSTALLED DOUBLER PER REPAIR DOCUMENT EA 61668. (X)
- [SDR USAASB97318](https://openairdocs.org/sdr/USAASB97318.md): Battery Pack · discharged · Nov 21, 1997 · N394US · Boeing 7373B7 · Emergency Lighting
  > PVD - MAINTENANCE FOUND THE AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)
- [SDR USAASB97046](https://openairdocs.org/sdr/USAASB97046.md): Seal · leaking · Feb 12, 1997 · N394US · Boeing 7373B7 · Electrical/Electronic Compartment Doors
  > LGA - FLT 2238 - DURING CLIMB, AIRCRAFT WOULD NOT PRESSURIZE AND RETURNED TO FIELD AT LGA. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE E/E DOOR SEAL LEAKING EXCESSIVELY. REPOSITIONED DOOR SEAL PER MM 52-48-41 AND 52-09-12. PERFORMED LEAK C
- [SDR USAASB96246](https://openairdocs.org/sdr/USAASB96246.md): Engine · bird strike · Nov 26, 1996 · N394US · Boeing 7373B7 · Engine (Turbine/Turboprop)
  > DAB - FLT 282 - UPON ROTATION WITH THE NOSE JUST OFF THE RUNWAY, THE AIRCRAFT STRUCK A FLOCK OF BIRDS. SEVERE VIBRATION WAS FELT FROM THE NR 2 ENGINE. THE CAPTAIN DID NOT SHUT DOWN THE ENGINE BUT KEPT IT IN IDLE WHILE THEY RETURNED TO FIELD AT DAB. NO EMERG

## 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 = 'N394US' AND deregistration_id = 'N394US-2006-07-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N394US-2006-07-18/reports

---
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