# Service difficulty reports: N332DL, cancelled Jul 10, 2009

A list on [N332DL, cancelled Jul 10, 2009](https://openairdocs.org/deregistered/N332DL-2009-07-10.md).

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

- [SDR DL73S050393](https://openairdocs.org/sdr/DL73S050393.md): Wire · broken · Jul 22, 2005 · N332DL · Boeing 737232 · Light System Wiring
  > SEAT MOUNTED EMERGENCY PATH LIGHTS INOP FROM ROW 2 THRU 14. REPLACED FUSES IN SEAT TRACK POWER SUPPLY AND REPAIRED WIRING IN RT SEAT TRACK BETWEEN 12-13 DEF.
- [SDR DL73S041060](https://openairdocs.org/sdr/DL73S041060.md): Frame · cracked · Nov 23, 2004 · N332DL · Boeing 737232 · Cargo/Baggage Doors
  > A 1 INCH CRACK WAS FOUND IN THE WEB OF THE UPPER FRAME EMANATING FROM A FASTENER HOLE COMMON TO THE UPPER AND LOWER FRAME LAP JOINT. THE CRACK WAS STOP DRILLED AND THE FRAME REPAIRED WITH 2 TITANIUM REPAIR ANGLES PER ER/A 095286-14.
- [SDR DL73S040206](https://openairdocs.org/sdr/DL73S040206.md): Skin · cracked · Feb 27, 2004 · N332DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE STRINGER 4L & 4R SKIN LAP JOINTS WERE FOUND WITH SEVERAL CRACKS BETWEEN FS 540 & 727 WHEN INSPECTED PER AD 2003-08-15. THE CRACKED LAP JOINTS WERE CUTOUT IN THEIR ENTIRETY AND REPAIRED WITH EXTERNAL ALUMINUM DOUBLERS PER BAC S/B 737-53A1177 AND PER ER/A 3
- [SDR DL73K011228](https://openairdocs.org/sdr/DL73K011228.md): Controller · failed · Jul 25, 2001 · N332DL · Boeing 737232 · Cabin Pressure Controller
  > UNABLE TO PRESSURIZE AIRCRAFT WITH LEFT PACK. REPLACED PRESSURIZATION CONTROLLER, GROUND OPS OK. CLEANED RT PACK COMPRESSOR DISCHARGE SW S2. RT PACK OPS OK.
- [SDR DL73K010726](https://openairdocs.org/sdr/DL73K010726.md): Skin · cracked · May 4, 2001 · N332DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > A.5 INCH CRACK WAS FOUND IN THE BONDED SKIN OF THE UPPER HINGE CUTOUT OF THE AFT ENTRY DOOR CUTOUT. THE CRACK WAS REMOVED WITH A SMALL CUTOUT. THE AREA WAS REPAIRED WITH AN EXTERNAL CRES STEEL DOUBLER PER ER/A 380735-14, REV A.
- [SDR DL73K010725](https://openairdocs.org/sdr/DL73K010725.md): Skin · cracked · May 4, 2001 · N332DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > A TYPICAL CRACK WAS FOUND IN THE BONDED SKIN AND UNDERLYING BEAR STRAP IN THE LOWER FWD CORNER OF THE AFT GALLEY DOOR CUTOUT. THE CRACK WAS REMOVED WITH A 1.2 X 1.3 INCH CUTOUT IN ALL LAYERS. THE AREA WAS REPAIRED WITH THREE EXTERNAL ALUMINUM DOUBLERS PER
- [SDR DL73K002245](https://openairdocs.org/sdr/DL73K002245.md): Switch · failed · Nov 17, 2000 · N332DL · Boeing 737232 · Leading Edge Slat Position Indicating System
  > AFTER T/O CREW HAD SLAT INTRANSIT LIGHTS ON NR 2 AND NR 6 SLAT AFTER RETRACTION. REPLACED NR 2 SLAT ROD END SWITCH AND SLAT INDICATION BOX, ALL INDICATIONS NOW NORMAL.
- [SDR DL73K001658](https://openairdocs.org/sdr/DL73K001658.md): Circuit Breaker · damaged · Aug 26, 2000 · N332DL · Boeing 737232 · DC Generating System
  > SVC CK FAILS STEP 13 BATT VOLTAGE CK. REPLACED BATTERY, CHARGER, AND C/B C167 BATTERY TRANSFER CONTROL. REPLACED BATTERY BUS CIRCUIT BREAKER C20. RAN TEST OPS NORMAL.
- [SDR DL73K000706](https://openairdocs.org/sdr/DL73K000706.md): Skin · dented · Apr 12, 2000 · N332DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE AFT EDGE OF THE CARGO DOOR CUTOUT WAS STRUCK BY GROUND EQUIPMENT BETWEEN STRINGERS 20R & 21R. THE DAMAGE WAS REMOVED WITH A 1 WIDE X 9 TALL CUTOUT IN THE SKIN ASSY AND BEARSTRAP. THE DAMAGE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS IN
- [SDR DL73K992698](https://openairdocs.org/sdr/DL73K992698.md): Fitting · corroded · Dec 8, 1999 · N332DL · Boeing 737232 · Fuselage, Landing Gear Attach Fittings
  > THE STRUT ATTACH LUG OF THE RT MAIN LANDING GEAR SIDE STRUT SUPPORT FITTING AT FS 685 WAS FOUND WITH CORROSION IN THE LUG BORE AND ON THE LUG FACES. THE BORE WAS OVERSIZED AND THE LUG FACES MACHINED TO REMOVE THE CORROSION. A REPAIR BUSHING WAS INSTALLED A
- [SDR DL73S982090](https://openairdocs.org/sdr/DL73S982090.md): Fitting · damaged · Oct 8, 1998 · N332DL · Boeing 737232 · Fuselage, Landing Gear Attach Fittings
  > THE LT MLG SIDE STRUT SUPPORT FITTING AT BS 685 WAS DAMAGED BY TOOL MARKS. REPAIRED PER ERA 332329-14.
- [SDR DL73S982089](https://openairdocs.org/sdr/DL73S982089.md): Skin · damaged · Oct 8, 1998 · N332DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > C2 DOOR CUTOUT WAS WITH AN EXISTING REPAIR ALONG THE FWD EDGE. UPON REMOVAL OF THE REPAIR ADDITIONAL DAMAGE WAS FOUND. REPAIRED PER ERA 332286-14.
- [SDR DL73S982088](https://openairdocs.org/sdr/DL73S982088.md): Frame · cracked · Oct 8, 1998 · N332DL · Boeing 737232 · Fuselage Main, Frame
  > CRACK FOUND IN THE FAIL/SAFE CHORD OF THE STA 907 FRAME AT APPROX S13R. REPAIRED PER ERA 332297-14.
- [SDR DL73S982087](https://openairdocs.org/sdr/DL73S982087.md): Frame · damaged · Oct 8, 1998 · N332DL · Boeing 737232 · Fuselage Main, Frame
  > DURING MODIFICATION OF THE FUSELAGE FRAMES SEVERAL WERE DAMAGED. THE DAMAGE REQUIRED TRIMMING OFF/OUT THE TOOLING DAMAGE. REPAIRED PER ERA 332294-14.
- [SDR DL73S982086](https://openairdocs.org/sdr/DL73S982086.md): Frame · cracked · Oct 8, 1998 · N332DL · Boeing 737232 · Fuselage Main, Frame
  > STA 440 FRAME WEB FOUND CRACKED AT A TOOLING HOLE BETWEEN S13R - 14R. REPAIRED PER ERA 332298-14.
- [SDR DL73S981313](https://openairdocs.org/sdr/DL73S981313.md): Heat Valve · inoperative · Jun 21, 1998 · N332DL · Boeing 737232 · Fuel Heater
  > DURING FLIGHT, NR 1 ENGINE OIL TEMP WAS INDICATING IN AMBER RANGE. PERFORMED POM PROCEDURES, AFTER 15 MINUTES ELAPSED SHUT NR 1 ENGINE DOWN. REPLACED LT ENGINE FUEL HEAT VALVE. RAN ENGINE, CHECKS OK.
- [SDR DL73S980922](https://openairdocs.org/sdr/DL73S980922.md): Skin · dented · Apr 23, 1998 · N332DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN AT STRINGER 21L AND BETWEEN FS 927 AND 947.8 WAS DAMAGED BY GROUND EQUIPMENT. THE DAMAGED SKIN WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 364605-14. THE UNDERLYING STRINGER WAS REPAIRED PER B737 SRM 53-10-3.
- [SDR DL73S970492](https://openairdocs.org/sdr/DL73S970492.md): Engine · fod · Mar 16, 1997 · N332DL · Boeing 737232 · Engine (Turbine/Turboprop)
  > AFTER TAKEOFF, HAD BURNING SMELL IN CABIN LIKE OVENS, BUT OVENS WERE NOT ON, FELT A SIDEWAY KICK AND A LOUD BANG. DECLARED EMERGENCY. RETURNED TO CVG. NO ABNORMAL ENG INDICATIONS. ON RETURN, PASSENGER REPORTED SEEING A BAG SUCKED INTO AN ENG ON TAXI OUT.
- [SDR DL73S962270](https://openairdocs.org/sdr/DL73S962270.md): Attach Fitting · cracked · Oct 3, 1996 · N332DL · Boeing 737232 · Wing, Landing Gear Attach Fittings
  > RIGHT WING OB AFT SUPPORT FITTING FOR THE MAIN LANDING GEAR BEAM WAS FOUND CRACKED. CRACKING TYPICAL TO THAT DESCRIBED IN BOEING SERVICE BULLETIN 737-57-1216. A/C 332 IDENTIFIED AS A GROUP 5 BY THE SERVICE BULLETIN. THE CRACKED FITTING WILL REMAIN IN SERVIC
- [SDR DL73S954777](https://openairdocs.org/sdr/DL73S954777.md): Light · inop · Dec 27, 1995 · N332DL · Boeing 737232 · Emergency Lighting
  > LEFT AFT DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED. CHECKS NORMAL.
- [SDR DL73S951842](https://openairdocs.org/sdr/DL73S951842.md): Flap Skin · damaged · Apr 24, 1995 · N332DL · Boeing 737232 · Trailing Edge Flaps
  > DURING SHOP INSP, RT WING NR 4 AFT FLAP WAS FOUND WITH A TIME LIMITED REPAIR 10 INCHES FROM THE IN/B END ON THE L/E OF FLAP. INSTALLED PERMANENT REPAIR PER SRM 57-50-4 FIG 5.
- [SDR DL73S952137](https://openairdocs.org/sdr/DL73S952137.md): Te Wedge · delaminated · Apr 22, 1995 · N332DL · Boeing 737232 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, NR 4 AFT FLAP T/E WEDGE WAS FOUND DELAMINATED 10 FROM THE INBD END OF FLAP. REPAIRED PER SRM 51-70-10.
- [SDR DL73S952136](https://openairdocs.org/sdr/DL73S952136.md): Te Wedge · damaged · Apr 22, 1995 · N332DL · Boeing 737232 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, NR 4 AFT FLAP WAS FOUND WITH T/E WEDGE WITH DAMAGE TO O/B AFT CORNER. REPAIRED PER SRM 57-53-01.
- [SDR DL73S952135](https://openairdocs.org/sdr/DL73S952135.md): Le Skin · damaged · Apr 22, 1995 · N332DL · Boeing 737232 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, NR 4 AFT FLAP WAS FOUND WITH TIME LIMITED REPAIR ON L/E AT 16 FROM THE I/B END OF FLAP. REPAIRED PER SRM 57-50-4 FIG 5.
- [SDR DL73S951641](https://openairdocs.org/sdr/DL73S951641.md): Computer · failed · Apr 19, 1995 · N332DL · Boeing 737232 · Elevator Control System
  > ON CLIMBOUT HAD ELEV, FEEL DIFF. PRESSURE LITE ON. RETURNED DFW, REPLACED FEEL COMPUTER, FOR RETURN TO SERVICE.
- [SDR DL73S951091](https://openairdocs.org/sdr/DL73S951091.md): Windshield · failed · Mar 13, 1995 · N332DL · Boeing 737232 · Flight Compartment Windows
  > DURING CRUISE, HEARD BURNING NOISE AND HAS ACRID SMELL IN FLT DECK, THEN HAD SMOKE AT R-1 WINDOW TERMINAL BLOCK, LANDED BNA, FOUND R-1 WINDOW TERMINAL BURNED. RELACED R-1 WINDOW, CONTROLLER AND CIRCUIT BREAKER. OPERATION NORMAL.

## 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 = 'N332DL' AND deregistration_id = 'N332DL-2009-07-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N332DL-2009-07-10/reports

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