# Service difficulty reports: N339US, cancelled Nov 19, 2003

A list on [N339US, cancelled Nov 19, 2003](https://openairdocs.org/deregistered/N339US-2003-11-19.md).

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

- [SDR USAASB02192](https://openairdocs.org/sdr/USAASB02192.md): Safety Switch · failed · Oct 23, 2002 · N339US · Boeing 737301 · Landing Gear Position and Warning
  > PIT - FLT 1591 - EN ROUTE, SEVERAL DISCREPANCIES THAT INDICATE THE A/C LOGIC WAS IN GROUND MODE. CB`S WERE NORMAL. AIRCRAFT STARTED TO DEPRESSURIZE AT FL280. NO OFF TIME ON ACARS. NO TCAS. TRANSPONDER WAS REPORTED INOP BY ATC. ENGINE LOW IDLE WAS IN THE
- [SDR USAA011052](https://openairdocs.org/sdr/USAA011052.md): Skin · Aug 9, 2001 · N339US · Boeing 737301 · Fuselage Structure (General)
  > CLT - FOUND SKIN DAMAGED 1 INCH, BETWEEN BS 28L AND BS 28R BS 380. INSTALLED.100 INCH THICK 2024 T3 DOUBLER PER TR 53-30-07, SB 737-53-1117 REV 1. (M)
- [SDR USAA011066](https://openairdocs.org/sdr/USAA011066.md): Skin · cracked · Aug 6, 2001 · N339US · Boeing 737301 · Fuselage Main, Plate/Skin
  > TPA - FOUND 1 INCH CRACK IN SKIN AFT OF EQUIPMENT COOLING EXH, LOWER LOBE SKIN BETWEEN S28L AND 28R STATION 380. INSTALLED DOUBLER PER TYPICAL REPAIR 53-30-07, SB 737-53-1117 REV 1. (M)
- [SDR USAA010418](https://openairdocs.org/sdr/USAA010418.md): Door Frame · cracked · Mar 31, 2001 · N339US · Boeing 737301 · Cargo/Baggage Doors
  > PIT - FOUND FORWARD CORNER FRAME CRACKED 1 INCH AND.25 INCH, FORWARD CARGO DOOR LOWER FWD CORNER TOP FLANGE. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER EO 5290X045. (M)
- [SDR USAASB01014](https://openairdocs.org/sdr/USAASB01014.md): Regulator · failed · Jan 21, 2001 · N339US · Boeing 737301 · Pneumatic Distribution System
  > BWI - FLT 1801 - EN ROUTE FROM BOS-ATL, THE CREW HAD TROUBLE MAINTAINING CABIN PRESSURIZATION. AT FL230, THE RIGHT BLEED PRESSURE WENT TO 30 PSI WHILE THE LEFT STAYED AT 0. CABIN ALTITUDE CLIMBED TO OVER 10,000 FEET AND SET OFF THE CABIN ALTITUDE WARNING HOR
- [SDR USAA001392](https://openairdocs.org/sdr/USAA001392.md): Skin · cracked · Aug 29, 2000 · N339US · Boeing 737301 · Fuselage Main, Plate/Skin
  > TPA - FOUND SKIN CRACKED.800 INCH, AFT SERVICE LOWER HINGE CUTOUT STATION 947.5 STRINGER 10R. INSTALLED DOUBLER PER SRM 53-60-01 FIG 207. (M)
- [SDR USAASB99238](https://openairdocs.org/sdr/USAASB99238.md): Fairing · missing · Sep 27, 1999 · N339US · Boeing 737301 · Aerodynamic Fairings
  > BOS - FLT 8053 - FLIGHT RETURNED TO FIELD AT BOS DUE TO A LOUD HIGH PITCH HUMMING NOISE AND VIBRATION AROUND CABIN WINDOW AT SEAT ROW 9ABC. VIBRATION AND HUMMING NOISE DECREASED UNDER 10,000 FT AND 220 KNOTS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENA
- [SDR USAA990926](https://openairdocs.org/sdr/USAA990926.md): Angle · corroded · Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH FORWARD OF STATION 251 FRAME, RBL 16, WL 157 ALONG INBOARD ROW OF FASTENERS RIGHT LOWER CHORD ANGLE. CORROSION LEVEL 2. REPLACED RIGHT LOWER CHORD ANGLE IN NLG WHEEL WELL PER SRM 51-70-12 FIG 1
- [SDR USAA990910](https://openairdocs.org/sdr/USAA990910.md): Chord · corroded · Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AT STATION 270, RBL 2.5 - LBL 2.5 Z-CHORD. CORROSION LEVEL 1. REPAIRED REPLACEMENT 'Z' CHORD PER EA 65414 AND TR 53-20-04. (M)
- [SDR USAA990882](https://openairdocs.org/sdr/USAA990882.md): Web · cracked · Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A.5 INCH CRACK SHEAR BEAM WEB SHELF 18A AFT WW BULKHEAD. INSTALLED DOUBLER PER EA 65323. (M)
- [SDR USAA990877](https://openairdocs.org/sdr/USAA990877.md): Skin · cracked · Sep 3, 1999 · N339US · Boeing 737301 · Service Doors
  > CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND.25 INCH CRACK AFT SERVICE DOOR FORWARD EDGE 30 INCH BELOW TOP SKIN. INSTALLED DOUBLER PER SRM 52-10-01. (M)
- [SDR USAA990876](https://openairdocs.org/sdr/USAA990876.md): Floorbeam · corroded · Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A.25 INCH BY.25 INCH AREA OF CORROSION STATIO N1006, LBL 26 FLOORBEAM. CORROSION LEVEL 1. INSTALLED REPAIR STRAP PER EA 65360 AND SRM 53-00-51 FIG 203. (M)
- [SDR USAA990875](https://openairdocs.org/sdr/USAA990875.md): Floorbeam · corroded · Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Main, Floor Beam
  > CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION LBL 21, 28, 35, 42 AND 45, BS 344, WL 208.1 FLOORBEAM. CORROSION LEVEL 1. INSTALLED NEW SECTION OF T-CAP WITH REPAIR ANGLES PER SRM 53-10-51. (M)
- [SDR USAA990855](https://openairdocs.org/sdr/USAA990855.md): Angle · cracked · Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A CRACK AT BS 289.5 STRINGER 10R WEB ANGLE. INSTALLED NEW WEB ANGLE PER SRM 51-10-02. (M)
- [SDR USAA990843](https://openairdocs.org/sdr/USAA990843.md): Tie Clip · cracked · Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A.5 INCH CRACK STATION 616, STRINGER 8L TIE CLIP. REPLACED CLIP PER SRM 51-40-02. (M)
- [SDR USAA990842](https://openairdocs.org/sdr/USAA990842.md): Tie Clip · cracked · Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK STATION 616, STRINGER 4R TIE CLIP. REPLACED CLIP PER SRM 51-40-02. (M)
- [SDR USAA990841](https://openairdocs.org/sdr/USAA990841.md): Clip · cracked · Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A CRACKED CLIP STATION 663.75 AT STRINGER 10R. REPLACED CLP PER SRM 51-10-02. (M)
- [SDR USAA990840](https://openairdocs.org/sdr/USAA990840.md): Clip · cracked · Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A CRACKED CLIP STATION 727D STRINGER 4R. REPLACED CLIP PER SRM 51-10-02. (M)
- [SDR USAA990839](https://openairdocs.org/sdr/USAA990839.md): Frame · cracked · Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK AT STATION 887, STRINGER 9L FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (M)
- [SDR USAA990838](https://openairdocs.org/sdr/USAA990838.md): Splice · cracked · Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK AT STATION 907, STRINGER 5R SPLICE. REPLACED SPLICE PER SRM 51-00-02. (M)
- [SDR USAA990837](https://openairdocs.org/sdr/USAA990837.md): Splice · cracked · Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK AT STATION 907, STRINGER 4L SPLICE. REPLACED SPLICE PER SRM 51-00-02. (M)
- [SDR USAA990824](https://openairdocs.org/sdr/USAA990824.md): Shear Tie · cracked · Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK IN SHEAR TIE STATION 639 STRINGER 7R AND 8R. REPAIRED PER SRM 51-40-02. (M)
- [SDR USAA990823](https://openairdocs.org/sdr/USAA990823.md): Frame · cracked · Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK STATION 727D STRINGER 7R FRAME AND TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M)
- [SDR USAA990822](https://openairdocs.org/sdr/USAA990822.md): Frame · cracked · Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Main, Frame
  > CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK STATION 727A STRINGER 3R FRAME AND TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M)
- [SDR USAA990821](https://openairdocs.org/sdr/USAA990821.md): Tie Clip · cracked · Sep 3, 1999 · N339US · Boeing 737301 · Fuselage Miscellaneous Structure
  > CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK STATION 639 STRINGER 5L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)
- [SDR USAASB99164](https://openairdocs.org/sdr/USAASB99164.md): Engine · fatigued · Jul 6, 1999 · N339US · Boeing 737301 · Engine (Turbine/Turboprop)
  > BOS - FLT 221 - JUST AFTER TAKEOFF, CREW ENCOUNTERED A WINDSHEAR ON DEPARTURE AND APPLIED FIREWALL POWER FOR A PERIOD APPROXIMATELY 10 SECONDS. CAPTAIN FELT HE OVERBOOSTED THE ENGINES AND ELECTED TO RETURN TO FIELD AT BOS. FLIGHT LANDED WITHOUT FURTHER INCID
- [SDR USAA990221](https://openairdocs.org/sdr/USAA990221.md): Skin · cracked · Mar 2, 1999 · N339US · Boeing 737301 · Service Doors
  > CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK EXTERNAL SKIN FORWARD SERVICE DOOR LOWER HINGE CUTOUT. INSTALLED DOUBLER PER EA 64060 AND SB 52-1096. (M)
- [SDR USAA980344](https://openairdocs.org/sdr/USAA980344.md): Skin · cracked · Aug 17, 1998 · N339US · Boeing 737301 · Fuselage Main, Plate/Skin
  > CLT - DURING DAILY CHECK VISUAL INSPECTION, FOUND A 5 INCH CRACK BL 0 BETWEEN STATION 727D AND 727E ON FUSELAGE SKIN. INSTALLED DOUBLER PER SRM 53-00-01. (M)
- [SDR USAASB97266](https://openairdocs.org/sdr/USAASB97266.md): Light · inoperative · Sep 25, 1997 · N339US · Boeing 737301 · Emergency Lighting
  > CLT - EXIT LIGHT INOPERATIVE AT SEAT 10 A,B,C. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (X)
- [SDR USAASB97235](https://openairdocs.org/sdr/USAASB97235.md): Battery Pack · discharged · Aug 28, 1997 · N339US · Boeing 737301 · Emergency Lighting
  > DCA - FIRST CLASS LOW LEVEL LIGHTING FOUND INOP DURING RON MAINTENANCE. REPLACED BATTERY PACK. SYSTEM OPERATIONALLY CHECKED OK. (M)
- [SDR USAA951010](https://openairdocs.org/sdr/USAA951010.md): Floor Beam · corrosion · Sep 21, 1995 · N339US · Boeing 737301 · Fuselage Main, Floor Beam
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION EXCEEDING LIMITS AROUND HOLE, BS 958 RBL 7.5. FABRICATED NEW INTERCOSTAL FROM BAC1506-437075-T6 AND INSTALLED. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA951013](https://openairdocs.org/sdr/USAA951013.md): Angle · corrosion · Sep 19, 1995 · N339US · Boeing 737301 · Fuselage Miscellaneous Structure
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 20 INCHES AT BS 947.5 TO BS 992.5 LBL 53 AFT ENTRY DOOR. REPAIRED PER BOEING DRAWING 65-52878. CORROSION LEVEL 2. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. (M)
- [SDR USAA951011](https://openairdocs.org/sdr/USAA951011.md): Angle · corrosion · Sep 13, 1995 · N339US · Boeing 737301 · Fuselage Miscellaneous Structure
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 5 INCHES AT STATION 370 AT FORWARD ENTRY THRESHOLD. REPLACED Z-ANGLE. REPAIRED PER BOEING DRAWING 65C80735. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA951009](https://openairdocs.org/sdr/USAA951009.md): Floor Beam · corrosion · Sep 13, 1995 · N339US · Boeing 737301 · Fuselage Main, Floor Beam
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCHES AT STATION 294.5 LBL 20 INCHES. CUT OUT CORROSION AND INSTALLED DOUBLER AND FILLER. REPAIRED PER SRM 53-10-51. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA951012](https://openairdocs.org/sdr/USAA951012.md): Angle · corrosion · Sep 12, 1995 · N339US · Boeing 737301 · Fuselage Miscellaneous Structure
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 24 INCHES AT FORWARD SERVICE DOOR THRESHOLD. REPLACED Z-ANGLE. REPAIRED PER BOEING DRAWING NR 6545875. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M)
- [SDR USAA951007](https://openairdocs.org/sdr/USAA951007.md): Floor Beam · corrosion · Sep 8, 1995 · N339US · Boeing 737301 · Fuselage Main, Floor Beam
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 18 INCHES STATION 986.5 BL ZERO TO LBL 24 INCHES. REPLACED UPPER T-CAP. REPAIRED PER SRM 53-00-51. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M)
- [SDR USAA951008](https://openairdocs.org/sdr/USAA951008.md): Floor Beam · corrosion · Sep 6, 1995 · N339US · Boeing 737301 · Fuselage Main, Floor Beam
  > INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 36 INCHES STATION 344 LBL 24 INCHES TO RBL 12 INCHES. REPLACED UPPER T-CAP OF BEAM. REPAIRED PER TR 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)
- [SDR USAA950384](https://openairdocs.org/sdr/USAA950384.md): Eel Assy · inoperative · Apr 19, 1995 · N339US · Boeing 737301 · Emergency Lighting
  > PIT - EMERGENCY EXIT LIGHT AT EXIT ROW INOPERATIVE. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT AT EXIT ROW. OPS CHECKS NORMAL. (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 = 'N339US' AND deregistration_id = 'N339US-2003-11-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N339US-2003-11-19/reports

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