# Service difficulty reports: N24343, cancelled May 20, 2015

A list on [N24343, cancelled May 20, 2015](https://openairdocs.org/deregistered/N24343-2015-05-20.md).

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

- [SDR C7WA200400085](https://openairdocs.org/sdr/C7WA200400085.md): Clamp · loose · Nov 3, 2004 · N24343 · Boeing 737231 · Pneumatic Distribution System
  > AIR RETURN: UNABLE TO PRESSURE IN FLIGHT. ATTEMPIED TO CONTROL CABIN MANUALLY WITH FULL INCREASE PRESSURE NO HELP. RESECURED LOOSE DUCT AT LT MIX VALVE. OPS CHECK GOOD ON THE GROUND IAW MM.
- [SDR C7WA200400065](https://openairdocs.org/sdr/C7WA200400065.md): Clamp · loose · Nov 3, 2004 · N24343 · Boeing 737231 · Pneumatic Distribution System
  > AIR RETURN, UNABLE TO PRESSURIZE IN FLIGHT. ATTEMPTED TO CONTROL CABIN MANUALLY WITH FULL INCREASE PRESSURE, NO HELP. RESECURED LOOSE DUCT AT LT MIX VALVE. OPS CHECK GOOD ON THE GROUND IAW MM 21-10-05.
- [SDR C7WA200400084](https://openairdocs.org/sdr/C7WA200400084.md): Landing Gear · malfunctioned · Nov 2, 2004 · N24343 · Boeing 737231 · Nose/Tail Landing Gear
  > NOSE LANDING GEAR FAILED TO EXTEND NORMALLY. RED NOSE GEAR UNSAFE LIGHT ON MANUALLY LOWERED NOSE LANDING GEAR IAW AOM. INSPECTED NOSE GEAR ACTUATOR, LOCKING ACTUATOR AND LINKAGE NO DAMAGE NOTED. LUBRICATED NOSE GEAR TRUNIONS, ACTUATOR AND DRAGBRACE AS NEEDE
- [SDR C7WA200400064](https://openairdocs.org/sdr/C7WA200400064.md): Landing Gear · lack of lube · Nov 2, 2004 · N24343 · Boeing 737231 · Landing Gear Retraction/Extension System
  > NOSE LANDING GEAR FAILED TO EXTEND NORMALLY. RED NOSE GEAR UNSAFE LIGHT ON. MANUALLY LOWERED NOSE LANDING GEAR IAW AOM VOL 1. INSPECTED NOSE GEAR ACTUATOR, LOCKING ACTUATOR AND LINKAGE NO DAMAGE NOTED. LUBRICATED NOSE GEAR TRUNNIONS, ACTUATOR AND DRAG BRAC
- [SDR C7WA200400063](https://openairdocs.org/sdr/C7WA200400063.md): Seal Plate · damaged · Oct 25, 2004 · N24343 · Boeing 727231 · Elevator Control System
  > LOSS OF SYSTEM A HYDRAULIC PRESSURE AND QUANITY IN FLIGHT. FOUND DAMAGED PLATE SEAL AT LT ELEVATOR POWER PACKAGE. REMOVED AND REPLACED SEAL PLATE.
- [SDR C7WA200300050](https://openairdocs.org/sdr/C7WA200300050.md): Bypass Switch · inoperative · Dec 24, 2003 · N24343 · Boeing 737231 · Turbine Engine Oil System
  > NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED AT CRUISE. A PRECAUTIONARY ENGINE SHUTDOWN WAS ACCOMPLISHED. INSPECTED NR 2 ENGINE INLET AND EXHAUST NO DEFECTS NOTED. CHECKED MAIN OIL SCREEN FOR DEBRIS, NONE FOUND. REMOVED AND REPLACED LOW OIL PRESSURE SWI
- [SDR C7WA200200003](https://openairdocs.org/sdr/C7WA200200003.md): Start Valve · stuck · Jul 3, 2002 · N24343 · Boeing 727231 · Engine Start Valves/Controls
  > NR 3 ENGINE BLEED TRIP OCCURED ON CLIMB OUT WITH CLIMB POWER. STABILIZED IT WITH SWITCHING THE BLEED. LATER NR 3 ENGINE FIRE IND ILLUMINATED. RETARDED NR 3 THROTTLE, LIGHT WENT OUT. FLIGHT CONTINUED WITHOUT INCIDENT. MAINTENANCE FOUND NR 3 START VALVE STU
- [SDR 2001F00170](https://openairdocs.org/sdr/2001F00170.md): Adi · inoperative · Jul 9, 2001 · N24343 · Boeing 727231 · Integrated Flight System
  > DURING CLIMB-OUT, NR 2 ADI BECAME INOPERATIVE. AIRCRAFT RETURNED TO MIAMI WITHOUT INCIDENT OR EMERGENCY. TROUBLESHOT TO FAULTY NR 2 ADI. REMOVED AND REPLACED ADI AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR 2001F00157](https://openairdocs.org/sdr/2001F00157.md): Flap · damaged · Jun 27, 2001 · N24343 · Boeing 727231 · Trailing Edge Flaps
  > RIGHT INBOARD TRAILING EDGE FLAP HALF OF HONEYCOMB MISSING AND OTHER HALF DAMAGED, UPON LANDING IN (GYE). ALL THREE ENGINES INSPECTED. REMOVED AND REPLACED FLAP ASSEMBLY OPS AND RIGGED IAW MM 27-51-00. RETURNED AIRCRAFT TO SERVICE. (M)
- [SDR 20000818SH003](https://openairdocs.org/sdr/20000818SH003.md): Web · corroded · May 10, 2000 · N24343 · Boeing 727231 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK, CORROSION NOTED ON SHEAR WEB RBL 24, STA 1140 - STA 1183. (X)
- [SDR 20000801SH008](https://openairdocs.org/sdr/20000801SH008.md): Frame · corroded · May 10, 2000 · N24343 · Boeing 727231 · Fuselage Main, Frame
  > DURING A C-CHECK CORROSION WAS NOTED ON FRAME AT STA 970, STR 29 - STR 30R. (X)
- [SDR 20000801SH007](https://openairdocs.org/sdr/20000801SH007.md): Frame · corroded · May 10, 2000 · N24343 · Boeing 727231 · Fuselage Main, Frame
  > DURING A C-CHECK, CORROSION WAS NOTED ON FRAME STA 950A BETWEEN STR 28 - STR 29R. (X)
- [SDR 20000801SH006](https://openairdocs.org/sdr/20000801SH006.md): Fitting · corroded · May 10, 2000 · N24343 · Boeing 727231 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A C-CHECK, CORROSION WAS NOTED ON NR 2 CARGO DOOR SILL TIE DOWNS. (X)
- [SDR 20000801SH005](https://openairdocs.org/sdr/20000801SH005.md): Door Frame · corroded · May 10, 2000 · N24343 · Boeing 727231 · Fuselage Main, Structure
  > DURING A C-CHECK, CORROSION WAS NOTED ON UPPER R2 DOOR SILL. (X)
- [SDR 20000801SH004](https://openairdocs.org/sdr/20000801SH004.md): Floorbeam · corroded · May 10, 2000 · N24343 · Boeing 727231 · Fuselage Main, Floor Beam
  > DURING A C-CHECK, CORROSION WAS NOTED ON FLOORBEAM AT STA 344, RBL 14. (X)
- [SDR 20000801SH003](https://openairdocs.org/sdr/20000801SH003.md): Skin · corroded · May 10, 2000 · N24343 · Boeing 727231 · Fuselage Main, Plate/Skin
  > DURING A C-CHECK, CORROSION WAS NOTED ON FUSELAGE SKIN STA 720B, STR 26 - STR 27R. (X)
- [SDR 20000801SH002](https://openairdocs.org/sdr/20000801SH002.md): Floorbeam · corroded · May 10, 2000 · N24343 · Boeing 727231 · Fuselage Main, Floor Beam
  > DURING A C-CHECK, CORROSION NOTED ON FLOOR CHORD, FLOOR SURROUNDING OF FE''''S AFT SEAT TRACK AREA. (X)
- [SDR 20000801SH001](https://openairdocs.org/sdr/20000801SH001.md): Stringer · corroded · May 10, 2000 · N24343 · Boeing 727231 · Fuselage Main, Longeron/Stringer
  > DURING A C-CHECK, CORROSION WAS NOTED ON STR 28L AT STA 480 - STA 500. (X)
- [SDR 20000731SH040](https://openairdocs.org/sdr/20000731SH040.md): Web · corroded · May 10, 2000 · N24343 · Boeing 727231 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK, CORROSION WAS NOTED ON SUPPORT WEB STA 580 - STA 600 BETWEEN STR 27L AND STR 28L. (X)
- [SDR 20000731SH039](https://openairdocs.org/sdr/20000731SH039.md): Frame · corroded · May 10, 2000 · N24343 · Boeing 727231 · Fuselage Main, Frame
  > DURING A C-CHECK, CORROSION WAS NOTED ON FRAME AT BS 720B BETWEEN STR 27L AND STR 28L. (X)
- [SDR 20000731SH038](https://openairdocs.org/sdr/20000731SH038.md): Mount · corroded · May 10, 2000 · N24343 · Boeing 727231 · Passenger/Crew Doors
  > DURING A C-CHECK, CORROSION WAS NOTED ON THE L-2 DOOR HANDLE MOUNTS. (X)
- [SDR 20000731SH037](https://openairdocs.org/sdr/20000731SH037.md): Floorbeam · corroded · May 10, 2000 · N24343 · Boeing 727231 · Fuselage Main, Floor Beam
  > DURING A C-CHECK, CORROSION WAS NOTED ON FLOORBEAM AT STA 380 FROM RT MOPSILL AND R-1 DOOR TO BL ZERO. (X)
- [SDR 20000731SH036](https://openairdocs.org/sdr/20000731SH036.md): Floor Support · corroded · May 10, 2000 · N24343 · Boeing 727231 · Fuselage Main, Floor Beam
  > DURING A C-CHECK, CORROSION WAS NOTED ON FLOOR SUPPORT, STA 400 - STA 420, BETWEEN BL ZERO AND RBL 24.75. (X)
- [SDR 20000731SH035](https://openairdocs.org/sdr/20000731SH035.md): Sill · corroded · May 10, 2000 · N24343 · Boeing 727231 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK, CORROSION WAS NOTED ON L-2 DOOR MOP SILL. (X)
- [SDR 20000731SH034](https://openairdocs.org/sdr/20000731SH034.md): Seat Track · corroded · May 10, 2000 · N24343 · Boeing 727231 · Flight Compartment Equipment
  > DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK, INBOARD, LEFT STA 1030 - STA 1110, AND OUTBOARD TRACK. (X)
- [SDR 20000731SH033](https://openairdocs.org/sdr/20000731SH033.md): Frame · corroded · May 10, 2000 · N24343 · Boeing 727231 · Fuselage Main, Frame
  > DURING A C-CHECK, CORROSION WAS NOTED ON FRAME AT STA 970 - STA 990, STR 29L. OUTBOARD FLANGE, ALSO NOTED ON STR 29R. (X)
- [SDR 20000731SH032](https://openairdocs.org/sdr/20000731SH032.md): Skin · corroded · May 10, 2000 · N24343 · Boeing 727231 · Fuselage Main, Plate/Skin
  > DURING A C-CHECK, CORROSION WAS NOTED ON SKIN BETWEEN STR 27 - STR 28L OF STA 480 - STA 500. (X)
- [SDR TWAA9901504](https://openairdocs.org/sdr/TWAA9901504.md): Slide · low press · Jan 21, 1999 · N24343 · Boeing 727231 · Escape Slide
  > THE FORWARD LEFT CABIN DOOR EVACUATION SLIDE BOTTLE PRESSURE WAS LOW. REPLACED THE SLIDE. CHECK-C 1-4-99 MCI.
- [SDR TWAA9814501](https://openairdocs.org/sdr/TWAA9814501.md): Skin · missing · Jul 25, 1998 · N24343 · Boeing 727231 · Trailing Edge Flaps
  > RT WING INBD MID FLAP HAD PIECE OF SKIN MISSING, 4 IN BY 16 IN, TOP OTBD EDGE. REPAIRED RT MID FLAP PER BOEING 727 SRM 51-40-6. CHECK-C 2-13-98 MCI.
- [SDR TWAA9804405](https://openairdocs.org/sdr/TWAA9804405.md): Support · corroded · Feb 5, 1998 · N24343 · Boeing 727231 · Fuselage Miscellaneous Structure
  > MCI - DURING C-CHECK MAINTENANCE AT CABIN FLOOR PANEL INBOARD OF FWD ENTRY DOORWAY, THE FLOOR SUPPORT HAD CORROSION. REMOVED CORROSION BY REPLACEMENT OF SUPPORT. INSTALLED NEW PART SRM 51-10-01. (M)
- [SDR TWAA9804406](https://openairdocs.org/sdr/TWAA9804406.md): Angle · corroded · Feb 1, 1998 · N24343 · Boeing 727231 · Fuselage Miscellaneous Structure
  > MCI - DURING C-CHECK MAINTENANCE, FOUND FORMER CAP WITH CORROSION AT FS 344, RBL 46 TO 63. REPLACED FORMER CAP ANGLE PER SRM 51-10-1. (M)
- [SDR TWAA9800301](https://openairdocs.org/sdr/TWAA9800301.md): Computer · failed · Jan 3, 1998 · N24343 · Boeing 727231 · Elevator Control System
  > FLT 475 - STL - DURING CLIMB, SYSTEM 'A' HYDRAULIC LOW PRESSURE LIGHTS ILLUMINATED WITH AN ASSOCIATED HYD QTY LOSS. FUEL DUMPING WAS USED. FOUND THE ELEVATOR FEEL COMPUTER WITH A RUPTURED SEAL. REPLACED FEEL COMPUTER P/N 401-60272-8. OPERATIONAL CHECK NORM
- [SDR TWAA9711713](https://openairdocs.org/sdr/TWAA9711713.md): Splice · corroded · Sep 30, 1997 · N24343 · Boeing 727231 · Fuselage Miscellaneous Structure
  > MCI - REMOVED CORROSION AND INSTALLED STRINGER SPLICE AT STRINGER 27L STATION 720D/720E. (M)
- [SDR TWAA9804002](https://openairdocs.org/sdr/TWAA9804002.md): Bulkhead Beam · cracked · Jan 31, 1997 · N24343 · Boeing 727231 · Fuselage Main, Bulkhead
  > MCI - DURING C-CHECK MAINTENANCE, THE AFT PRESSURE BULKHEAD FS 1183 BBL08 VERTICAL BEAM WAS CRACKED AT LOWER END. INSTALLED REPAIR ANGLES PER SB 727-53-0175, AND SRM 51-10-01 AND SRM 51-10-02. (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 = 'N24343' AND deregistration_id = 'N24343-2015-05-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N24343-2015-05-20/reports

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