# Service difficulty reports: N243US, cancelled Sep 13, 2004

A list on [N243US, cancelled Sep 13, 2004](https://openairdocs.org/deregistered/N243US-2004-09-13.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 · 100 reports

- [SDR USAA010751](https://openairdocs.org/sdr/USAA010751.md): Bulkhead · cracked · Jun 16, 2001 · N243US · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - FOUND BULKHEAD WEB WITH NUMEROUS CRACKS RANGING FROM.125 INCH TO.75 INCH, BS 178 WL 207 TO 234, LBL 12.6 TO RBL 11.7. DAMAGE REMOVED, REPAIR DOUBLER INSTALLED PER EO 5300V153, EA 69807 AND 69774. (M)
- [SDR USAA010752](https://openairdocs.org/sdr/USAA010752.md): Frame · cracked · Jun 16, 2001 · N243US · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND VERTICAL CHORD WITH TWO CRACKS EACH 1 INCH LONG, BS 178 WL 181 AT RBL 5.7 AND WL 184 AT LBL 5.7. DAMAGE REMOVED, INSTALLED REPAIR ANGLES ADN STRAPS PER EO 5300V155. (M)
- [SDR USAA010753](https://openairdocs.org/sdr/USAA010753.md): Frame · cracked · Jun 16, 2001 · N243US · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND SIDE CHORDS WITH TWO CRACKS.25 INCH AT RBL 26, 1 INCH AT LBL 24, BS 178 WL 195 AT LBL 24 AND WL 207 AT RBL 26. DAMAGED SECTION REMOVED, INSTALLED CHORD SPLICE REPAIR PER EO 5300V157. (M)
- [SDR USAASB01086](https://openairdocs.org/sdr/USAASB01086.md): Duct · failed · Mar 23, 2001 · N243US · Boeing 737201 · Air Distribution System
  > PBI - FLT 2990 - EN ROUTE FROM LGA TO PBI, APPROXIMATELY ONE HOUR INTO FLIGHT, THE FLIGHT ATTENDANT ADVISED THE CREW OF AN ELECTRICAL SMELL IN MID-CABIN. CREW COOLED DOWN CABIN AND SMELL DISSIPATED. FLIGHT ATTENDANT ADVISDED THAT ONLY A FAINT ODOR REMAINED.
- [SDR USAASB01085](https://openairdocs.org/sdr/USAASB01085.md): Bleed Valve · faulty · Mar 22, 2001 · N243US · Boeing 737201 · Compressor Bleed Valve
  > LGA - FLT 2721 - ON TAKEOFF FROM LGA, EN ROUTE TO FLL, THE AUTO THROTTLE DISENGAGED AND THE NR 1 ENGINE EPR PULLED BACK TO 1.88. THERE WAS NO RESPONSE TO THROTTLE MOVEMENT. CONDITIONS WERE A BLEEDS-OFF NON-PRESSURIZED TAKEOFF. THEN ON CLIMB-OUT, AFTER BLEED
- [SDR USAASB00351](https://openairdocs.org/sdr/USAASB00351.md): Engine · failed · Dec 18, 2000 · N243US · Boeing 737201 · Engine (Turbine/Turboprop)
  > FLL - FLT 2828 - ON CLIMB-OUT FROM FLL, EN ROUTE TO BOS, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL AND HIGH EGT. CAPTAIN SHUTDOWN THE NR 2 ENGINE, DECLARED AN EMERGENCY AND ADVISED THE FLIGHT ATTENDANTS THEY WERE RETURNING TO FIELD AT FLL. CAPTAIN FIRED
- [SDR USAA002076](https://openairdocs.org/sdr/USAA002076.md): Stringer · corroded · Dec 6, 2000 · N243US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > TPA - FOUND STRINGER CORRODED 2 INCHES BY 3 INCHES, STATION 965, STRINGER 27R. CORROSION LEVEL 2. SPLICED IN SECTION PER SRM 53-10-3 PAGE 4 FIG 1. (M)
- [SDR USAASB00270](https://openairdocs.org/sdr/USAASB00270.md): Gyro · faulty · Sep 22, 2000 · N243US · Boeing 737201 · Directional Gyro and Indicating System
  > BWI - FLT 2821 - ON CLIMB-OUT FROM BWI, THE HEADING COMPARATOR LIGHT ILLUMINATED. CAPTAINS AND FIRST OFFICERS COMPASS SYSTEM SPLIT 30 DEGREES APART AND REMAINED THAT WAY FOR 10 MINUTES. CAPTAINS ADVISED BWI THAT HE WAS RETURNING TO FIELD. JUST PRIOR TO LAND
- [SDR USAASB00214](https://openairdocs.org/sdr/USAASB00214.md): Handle · failed · Aug 10, 2000 · N243US · Boeing 737201 · Landing Gear Selector
  > BOS - FLT 2602 - CAPTAIN REPORTED THAT AFTER TAKEOFF, THE LANDING GEAR HANDLE WOULD NOT MOVE PAST THE OFF POSITION TO RETRACT THE LANDING GEAR. CREW ACCOMPLISHED ABNORMAL PROCEDURES AND RETURNED TO FIELD AT BOS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EM
- [SDR USAA000188](https://openairdocs.org/sdr/USAA000188.md): Frame · cracked · Feb 11, 2000 · N243US · Boeing 737201 · Fuselage Main, Frame
  > CLT - FOUND 1 INCH CRACK, STATION 727 STRINGER 24R CHORD ANGLE. INSTALLED NEW CHORD AND DOUBLER PER EA 66451 AND SRM 51-40-2. (M)
- [SDR USAA000137](https://openairdocs.org/sdr/USAA000137.md): Floorbeam · corroded · Feb 3, 2000 · N243US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - Q-1, BS 1016 LT LENGTH OF FLOORBEAM HAS CORROSION LEVEL 1. REPLACED WEB, T-CAP PER TR 53-60-02 AND SRM 51-40-02. (M)
- [SDR USAA000136](https://openairdocs.org/sdr/USAA000136.md): Seat Track · corroded · Feb 3, 2000 · N243US · Boeing 737201 · Fuselage, Seat/Cargo Attach Fittings
  > CLT - Q-1, FOUND CORROSION AT RBL 39 STATION 1000 TO 1014 FLOOR SEAT TRACK 1 INCH BY 14 INCH CORROSION LEVEL 1. INSTALLED NEW SEAT TRACK PER SRM 51-10-2 AND 51-30-03. (M)
- [SDR USAA000135](https://openairdocs.org/sdr/USAA000135.md): Skin · cracked · Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Main, Plate/Skin
  > CLT - Q-1, FOUND.25 INCH CRACK, LOWER FORWARD CORNER AFT ENTRY DOOR CUTOUT. REPLACED PARTS PER SRM 53-30-3 FIG 24. (M)
- [SDR USAA000134](https://openairdocs.org/sdr/USAA000134.md): Fitting · cracked · Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - Q-1, FOUND.5 INCH CRACK, LOWER DOOR STOP FITTING. REPLACED FITTING PER DRAWING 6517685. (M)
- [SDR USAA000133](https://openairdocs.org/sdr/USAA000133.md): Tie Clip · cracked · Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - Q,1, FOUND.1 INCH CRACK STATION 578, STRINGER 7R TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-1 AND EO 5393G227. (M)
- [SDR USAA000132](https://openairdocs.org/sdr/USAA000132.md): Strap · cracked · Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - Q-1, FOUND 1 INCH CRACK, STRINGER 5A JUST AFT STATION 1138. INSTALLED REPAIR DOUBLER PER EA66501 AND SRM 53-00-1. (M)
- [SDR USAA000131](https://openairdocs.org/sdr/USAA000131.md): Tie Clip · cracked · Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - Q-1, STRINGER 17 TIE CLIP AT STATION 1138, HAS 1 INCH CRACK. REPLACED TIE CLIP PER SRM 51-10-1. (M)
- [SDR USAA000130](https://openairdocs.org/sdr/USAA000130.md): Tie Clip · cracked · Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - Q-1, STRINGER 161 TIE CLIP AT STATION 1138, HAS A.75 INCH CRACK. REPLACED TIE CLIP PER SRM 51-40-1. (M)
- [SDR USAA000129](https://openairdocs.org/sdr/USAA000129.md): Shear Tie · cracked · Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - Q-1, STATION 1104 STRINGER 161 INBOARD SIDE FRAME SHEAR TIE HAS A.5 INCH CRACK. INSTALLED SHEAR TIE PER SRM 51-10-1. (M)
- [SDR USAA000128](https://openairdocs.org/sdr/USAA000128.md): Tie Clip · cracked · Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - Q-1, STRINGER 21 AT FRAME 616 TIE CLIP HAS A.5 INCH CRACK. REPLACED TIE CLIP PER EO5393G227 PART 3. (M)
- [SDR USAA000127](https://openairdocs.org/sdr/USAA000127.md): Floorbeam · cracked · Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Main, Floor Beam
  > CLT - Q-1, STATION 707, LBL 25, WL 202.5 FLOORBEAM WEB HAS A 1.5 INCH CRACK. REPLACED PARTS PER SRM 51-40-2. (M)
- [SDR USAA000126](https://openairdocs.org/sdr/USAA000126.md): Frame · cracked · Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Main, Frame
  > CLT - Q-1, STATION 663 BULKHEAD UPPER FRAME RBL 23, WL 201.5 HAS A.5 INCH CRACK. REPLACED VERTICAL ANGLES AND CHORD PER BOEING 65C37732. (M)
- [SDR USAA000125](https://openairdocs.org/sdr/USAA000125.md): Crease Beam · cracked · Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - Q-1, STRINGER 17R CREASE BEAM 8 INCH AFT STATION 639 FRAME CREASE BEAM WEB HAS A.375 INCH CRACK AT WL 208. REPLACED WEB PER SRM 51-10-02. (M)
- [SDR USAA000124](https://openairdocs.org/sdr/USAA000124.md): Shear Tie · cracked · Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - Q-1, STATION 520 FORWARD CARGO PIT BULKHEAD STRINGER 24R SHEAR TIE HAS A.375 INCH CRACK. INSTALLED CLIP PER SRM 51-10-02 AND BOEING 6551298. (M)
- [SDR USAA000123](https://openairdocs.org/sdr/USAA000123.md): Crease Beam · cracked · Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - Q-1, FOUND STRINGER 17R STATION 639 FRAME WL 208 CREASE BEAM WEB HAS A 1 INCH CRACK. REPLACED WEB AND ANGLE PER SRM 51-10-01 AND 51-40-04. (M)
- [SDR USAA000122](https://openairdocs.org/sdr/USAA000122.md): Tie Clip · cracked · Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - Q-1, STATION 597 STRINGER 8R TIE CLIP HAS A.1 INCH CRACK. REPLACED STRINGER CLIP PER EO5393G227 PART 3. (M)
- [SDR USAA000121](https://openairdocs.org/sdr/USAA000121.md): Frame · cracked · Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Main, Frame
  > CLT - Q-1, STRINGER 15R AT SKIN FASTENER FORWARD STATION 540 FRAME HAS A.25 INCH CRACK. INSTALLED REPAIR SPLICE PER EA66436 AND SRM 53-10-3 FIG 1. (M)
- [SDR USAA000120](https://openairdocs.org/sdr/USAA000120.md): Frame · cracked · Feb 2, 2000 · N243US · Boeing 737201 · Fuselage Main, Frame
  > CLT - Q-1, STATION 726, S18AL AT L/B CHORD FRAME HAS A.5 INCH CRACK. REPLACED SHELF PER EO5393G256 AND SRM 51-10-9. (M)
- [SDR USAA000114](https://openairdocs.org/sdr/USAA000114.md): Angle · cracked · Jan 27, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - Q-1, BS 178, LBL 5, WL 184 ANGLE HAS A 1.5 INCH CRACK. INSTALLED REPAIR ANGLE AND STRAP PER EA 66497. (M)
- [SDR USAA000113](https://openairdocs.org/sdr/USAA000113.md): Beam · cracked · Jan 27, 2000 · N243US · Boeing 737201 · Fuselage Main, Structure
  > CLT - Q-1, STATION 178, LBL 5.25, WL 188 BEAM HAS A 1 INCH CRACK. INSTALLED REPAIR ANGLE AND FILLER PER EA 66497. (M)
- [SDR USAA000092](https://openairdocs.org/sdr/USAA000092.md): Stringer · cracked · Jan 26, 2000 · N243US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > CLT - Q-1 - BS 533.5 AND 532.5, STR 151, STRINGER HAS 2 EACH.25 INCH CRACKS. SPLICED NEW STRINGER PER EACH 66436 AND SRM 53-10-3 FIG 1. (X)
- [SDR USAA000090](https://openairdocs.org/sdr/USAA000090.md): Bulkhead · cracked · Jan 26, 2000 · N243US · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - Q-1 - STA 727, LBL 23, WL 202, BULKHEAD HAS A.50 INCH CRACK. INSTALLED REPAIR DOUBLER PER TR 53-10-03. (X)
- [SDR USAA000089](https://openairdocs.org/sdr/USAA000089.md): Bulkhead · cracked · Jan 26, 2000 · N243US · Boeing 737201 · Fuselage Main, Bulkhead
  > CLT - Q-1 - STA 727, RBL 23, WL 202. BULKHEAD HAS A.50 INCH CRACK. INSTALLED REPAIR DOUBLER PER TR 53-10-03. (X)
- [SDR USAA000088](https://openairdocs.org/sdr/USAA000088.md): Beam · corroded · Jan 26, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous Structure
  > CLT - Q-1 - BS236, RBL 6, WL189, TRANSVERSE BEAM HAS 1 INCH BY.50 INCH OF CORROSION. REPAIRED PER SRM 51-10-1. (X)
- [SDR USAA000068](https://openairdocs.org/sdr/USAA000068.md): Angle · cracked · Jan 19, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous Structure
  > ANGLE CRACKED AT BS 727, RT BUTTLINE 1 WATERLINE 202. INSTALLED REPAIR ANGLE PER TR 53-10-03 A. (M)
- [SDR USAA000049](https://openairdocs.org/sdr/USAA000049.md): Web · cracked · Jan 18, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous Structure
  > WEB CRACKED AT BS 350, STRINGER 15 LT. INSTALLED NEW WEB SKIN PER SRM 51-10-01. (M)
- [SDR USAA000048](https://openairdocs.org/sdr/USAA000048.md): Bulkhead · cracked · Jan 18, 2000 · N243US · Boeing 737201 · Fuselage Main, Bulkhead
  > BULKHEAD CRACKED AT BS 663, LT BUTTLINE 23, WATERLINE 201.5. INSTALLED SPLICE ANGLE PER TR 57-10-03. (M)
- [SDR USAA000047](https://openairdocs.org/sdr/USAA000047.md): Floorbeam · corroded · Jan 18, 2000 · N243US · Boeing 737201 · Fuselage Main, Floor Beam
  > FLOORBEAM CORRODED AT BS 986, RT BUTTLINE 47, LT BUTTLINE 12. INSTALLED NEW T-CAP PER TR 53-60-1 AND EA 66459. (M)
- [SDR USAA000034](https://openairdocs.org/sdr/USAA000034.md): Splice · corroded · Jan 14, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous Structure
  > SPLICE CORRODED AT BS 359, STRINGER 27L. REPLACED STRINGER SPLICE PER SRM 53-10-3. (M)
- [SDR USAA000031](https://openairdocs.org/sdr/USAA000031.md): Web · cracked · Jan 13, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous Structure
  > WEB FOUND CRACKED AT BS 578, LBL 58, 59, 60, 60.5, WL 205.5. INSTALLED DOUBLER PER SRM 51-40-2. (M)
- [SDR USAA000030](https://openairdocs.org/sdr/USAA000030.md): Frame · cracked · Jan 13, 2000 · N243US · Boeing 737201 · Fuselage Main, Frame
  > FOUND FRAME CRACKED AT BS 400, STRINGER 25L. INSTALLED DOUBLER PER SRM 51-40-3. (M)
- [SDR USAA000029](https://openairdocs.org/sdr/USAA000029.md): Stringer · cracked · Jan 13, 2000 · N243US · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 15 RIGHT CRACKED AT BBS 533.5.. REPAIRED PER EA 66436 AND SRM 53-10-3 FIG 1. (M)
- [SDR USAA000028](https://openairdocs.org/sdr/USAA000028.md): Web · cracked · Jan 13, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous Structure
  > FOUND WEB CRACKED AT BS 639, WL 208, RBL 63. REPLACED WEBPER SRM 51-10-1. (M)
- [SDR USAA000027](https://openairdocs.org/sdr/USAA000027.md): Intercostal · cracked · Jan 13, 2000 · N243US · Boeing 737201 · Fuselage Main, Structure
  > INTERCOSTAL FOUND CRACKED AT BS 278, STRINGER 14R. REPLACED PART PER SRM 51-10-1. (M)
- [SDR USAA000026](https://openairdocs.org/sdr/USAA000026.md): Angle · cracked · Jan 13, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous Structure
  > FOUND ANGLE CRACKED AT BS 350, WL 216, RBL 65. REPAIRED PER SRM 51-30-2. (M)
- [SDR USAA000025](https://openairdocs.org/sdr/USAA000025.md): Fitting · cracked · Jan 13, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous Structure
  > FOUND FITTING CRACKED AT BS 348.2, WL 216, RBL 61. REPAIRED PER SRM 51-30-2. (M)
- [SDR USAA000024](https://openairdocs.org/sdr/USAA000024.md): Web · cracked · Jan 13, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous Structure
  > WEB FOUND CRACKED AT BS 350, LBL 61, WL 216. REPAIRED PERSRM 51-30-2. (M)
- [SDR USAA000023](https://openairdocs.org/sdr/USAA000023.md): Angle · cracked · Jan 13, 2000 · N243US · Boeing 737201 · Fuselage Miscellaneous Structure
  > FOUND ANGLE CRACKED AT BS 727, WL 202, RBL 8..5. REPAIREDPER SRM 51-30-2. (M)
- [SDR USAA000022](https://openairdocs.org/sdr/USAA000022.md): Bulkhead · cracked · Jan 13, 2000 · N243US · Boeing 737201 · Fuselage Main, Bulkhead
  > FOUND BULKHEAD CRACKED. INSTALLED REPAIR KIT PER DWG 65C37732. (M)
- [SDR USAA991480](https://openairdocs.org/sdr/USAA991480.md): Frame · cracked · Jan 12, 2000 · N243US · Boeing 737201 · Fuselage Main, Frame
  > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FUOND A.125 INCH CRACK FORWARD SERVICE DOOR FORWARD CUTOUT STUB FRAME BETWEEN STRINGER 11R AND 12R OUTBOARD CHORD ANGLE STATION 290. REMOVED AND REPLACED ANGLE PER REPAIR DOCUMENT 51-10-01. (M)

Next page: https://openairdocs.org/deregistered/N243US-2004-09-13/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 = 'N243US' AND deregistration_id = 'N243US-2004-09-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N243US-2004-09-13/reports

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