# Service difficulty reports: N302WA, cancelled Jan 17, 2018

A list on [N302WA, cancelled Jan 17, 2018](https://openairdocs.org/deregistered/N302WA-2018-01-17.md).

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

- [SDR DL733050107](https://openairdocs.org/sdr/DL733050107.md): Connector · damaged · Feb 14, 2005 · N302WA · Boeing 737347 · Emergency Lighting
  > EMERGENCY PATH LIGHTING INOP AT 22D/E/F. FOUND ON ROUTINE MAINTENANCE INSPECTION. REPAIRED DAMAGED SIDEWALL CONNECTOR AT 22D/E/F.
- [SDR DL733040604](https://openairdocs.org/sdr/DL733040604.md): Odor · detected · Jun 26, 2004 · N302WA · Boeing 737347 · Buffet/Galleys
  > FLIGHT ATTENDANT SMELLS BURNING ODOR IN AFT GALLEY. INSPECTED AFT GALLEY EQUIPMENT FOR DEFECTS, NONE NOTED. NO SMELL PRESENT. APPLIANCES AND LIGHTS ALL CHECK NORMAL. OK FOR SERVICE.
- [SDR DL733040060](https://openairdocs.org/sdr/DL733040060.md): Skin · cracked · Jan 17, 2004 · N302WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH A CRACK JUST BELOW STRINGER 23R ALONG THE EDGE OF THE BONDED SKIN WAFFLE DOUBLER BETWEEN FS 727D & 727E. THE DAMAGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 386104-14, REV A.
- [SDR DL733040007](https://openairdocs.org/sdr/DL733040007.md): Tire · cut · Jan 4, 2004 · N302WA · Boeing 737347 · Tire
  > ON L/O FOUND NR 2 MLG TIRE CUT BEYOND LIMITS. REMOVED AND REPLACED NR 2 MLG TIRE PER MM.
- [SDR DL733030852](https://openairdocs.org/sdr/DL733030852.md): Wire Harness · inoperative · Sep 17, 2003 · N302WA · Boeing 737347 · Light System Wiring
  > WHILE REPOSITIONING HARNESS AT SEAT ROW 27 PINS PULLED OUT OF HARNESS AND SHORTED POWER SUPPLY. REPLACED HARNESS AT SEAT ROW 27 AND POWER SUPPLY/BATTERY PER M/M.
- [SDR DL733020273](https://openairdocs.org/sdr/DL733020273.md): Attach Fitting · corroded · Mar 8, 2002 · N302WA · Boeing 737347 · Vertical Stabilizer, Attach Fittings
  > THE VERTICAL STABILIZER ATTACH LUGS AND THE FUSELAGE CLEVIS LUGS WERE FOUND TO BE CORRODED DURING AN INSPECTION. THE LUG BORES WERE OVERSIZED AND THE FACES SPOTFACED TO REMOVE THE CORROSION AND OVERSIZED BUSHINGS WERE INSTALLED.
- [SDR DL733011356](https://openairdocs.org/sdr/DL733011356.md): Safety Switch · out of adj · Aug 18, 2001 · N302WA · Boeing 737347 · Landing Gear Position and Warning
  > UPON DEPARTURE ATL LDG WOULD NOT RETRACT. GEAR HANDLE WOULD ONLY RAISE TO THE OFF POSITION. ADJUSTED AND TESTED GROUND SPOILER INTERLOCK AND SAFETY SWITCHES. REF MM 27-62-51-5 AND E2-09-01-5. ALL CHECKS OK.
- [SDR DL733010437](https://openairdocs.org/sdr/DL733010437.md): Skin · cracked · Mar 15, 2001 · N302WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > INSPECTIONS OF THE HORIZONTAL STABILIZER CUTOUT SURROUND STRUCTURE REVEALED A CRACK IN THE STRINGER 12L STRAP. ADDITIONAL TOOLING DAMAGE WAS FOUND ON THE STRINGER 12L UPPER CHORD. THE DAMAGED SECTION OF CHORD WAS REMOVED. THESTRAP WAS REPAIRED WITH A DOU
- [SDR DL733000922](https://openairdocs.org/sdr/DL733000922.md): Bulkhead · cracked · May 7, 2000 · N302WA · Boeing 737347 · Fuselage Main, Bulkhead
  > THE FS 178 BULKHEAD WEB WAS FOUND WITH TYPICAL FASTENER CRACKING IN THE WEB AT WL 234 AT LBL AND RBL 9. THE CRACKS ARE TYPICAL OF BAC S/B 737-53A1173. THE CRACKED AREAS OF WEB WERE TRIMMED OUT AND REPAIRED WITH ALUMINUM DOUBLERS PER B737 SRM 53-10-08, FIG 20
- [SDR DL733000258](https://openairdocs.org/sdr/DL733000258.md): Valve · failed · Feb 3, 2000 · N302WA · Boeing 737347 · Hydraulic Indicating System
  > HYD SYS B PRESS DROPPED TO ZERO WITH ASSOCIATED LOW PRESS LIGHTS ILLUMINATED. REPLACED B SYSTEM PRESSURE RELIEF VALVE.
- [SDR DL733991981](https://openairdocs.org/sdr/DL733991981.md): Control Panel · failed · Sep 7, 1999 · N302WA · Boeing 737347 · Cabin Pressure Control System
  > ON DESCENT, AUTO PRESS FAIL MADE UNPRESSURIZED LANDING. REPLACED PRESS CONTROL PANEL. CKS NORMAL.
- [SDR DL733990506](https://openairdocs.org/sdr/DL733990506.md): Line · leaking · Mar 10, 1999 · N302WA · Boeing 737347 · Hydraulic System, Main
  > AFTER INITIAL GEAR RETRACTION, NOSE GEAR RE-EXTENDED WITH GEAR HANDLE IN THE UP POSITION. RECYCLED GEAR HANDLE HAD NO EFFECT. NOSE GEAR REMAINED DOWN AND LOCKED. FOUND NOSE GEAR UPLOCK ACT UPPER LINE LEAKING HYD FLUID. LINE REPLACED.
- [SDR DL733990247](https://openairdocs.org/sdr/DL733990247.md): Skin · cracked · Feb 4, 1999 · N302WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN AND UNDERLYING STEEL GUSSET WERE FOUND WITH A.20 INCH CRACK AT THE UPPER AFT CORNER OF THE L1 COCKPIT WINDOW CUTOUT. THE CRACK WAS ROUTED OUT AND REPAIRED WITH A STEEL DOUBLER AND ALUMINUM TRIPLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 3666
- [SDR DL733981991](https://openairdocs.org/sdr/DL733981991.md): Wire · damaged · Sep 26, 1998 · N302WA · Boeing 737347 · Light System Wiring
  > EMERGENCY TRACK LIGHT WIRE AT SEAT ROW 25DEF FOUND DAMAGED. PERFORMED APPROVED REPAIR PER BOEING STANDARD WIRING MANUAL. SYSTEM OPERATES NORMAL.
- [SDR DL733981006](https://openairdocs.org/sdr/DL733981006.md): Bulkhead Web · cracked · May 12, 1998 · N302WA · Boeing 737347 · Fuselage Main, Bulkhead
  > FOUR CRACKS FOUND IN THE BLKHD WEB AT FS 178. THE CRACKS ARE LOCATED AT WL 200 AND WL 188, BETWEEN LBL 5.7 AND RBL 5.7. REPAIRED PER ERA 331672-14.
- [SDR DL733981005](https://openairdocs.org/sdr/DL733981005.md): Bulkhead Web · corroded · May 12, 1998 · N302WA · Boeing 737347 · Fuselage Main, Bulkhead
  > AFT PRESSURE BLKHD AT FS 1016 WAS FOUND CORRODED AND CRACKED AT BL 0. REPAIRED PER ERA 331673-14.
- [SDR DL733981004](https://openairdocs.org/sdr/DL733981004.md): Skin · worn · May 12, 1998 · N302WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT THE BLADE SEAL FUSELAGE INTERFACE WAS FOUND TO HAVE AN EXISTING REPAIR (REF 5-72770-3). WEAR WAS FOUND FWD OF THE REPAIR. REPAIRED PER ERA 331664-14.
- [SDR DL733972182](https://openairdocs.org/sdr/DL733972182.md): Boot Seal · failed · Oct 24, 1997 · N302WA · Boeing 737347 · Air Distribution System
  > LOST ALL PRESSURIZATION AT 30000 FEET, NORMAL DUCT PRESS. NO BLEED OR PACK TRIP. FOUND RUPTURED BOOT SEAL ON APU P DOME PRESSURE DUCT. REPLACED SEAL. PRESSURIZED A/C TO 6 PSI. CKS NORMAL. NO FURTHER LEAKS FOUND.
- [SDR DL733970233](https://openairdocs.org/sdr/DL733970233.md): Power Supply · inoperative · Feb 7, 1997 · N302WA · Boeing 737347 · Emergency Lighting
  > WHILE PERFORMING NR 5 AD SVC CK ON SHIP 202, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP FROM ROW 1 IN F/CLASS TO ROW 12 IN Y/CLASS INOP. FOUND POWER SUPPLY FOR EMERGENCY TRACK LIGHTING INOP. REPLACED PWR SUPPLY, EMERGENCY EVACUATION LIGHTS SYS OPS NML.
- [SDR DL733961628](https://openairdocs.org/sdr/DL733961628.md): Skin · cracked · Apr 6, 1996 · N302WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > THE SKIN AT THE COOLING DUCT CUTOUT, FS 379 BL 0, WAS FOUND CRACKED AT THE AFT EDGE OF THE CUTOUT. THE CRACK IS APPROX.5 IN LENGTH AND IS TYPICAL OF CRACKS DESCRIBED IN BACO S/B 737-53-1117 R-1. THE CRACK WILL BE STOP DRILLED AND A PERMANENT REPAIR WILL BE
- [SDR DL733960710](https://openairdocs.org/sdr/DL733960710.md): Ballast · smoking · Mar 30, 1996 · N302WA · Boeing 737347 · Passenger Compartment Lighting
  > SIDEWALL LIGHTS ROW 23 TO 25 MOMENTARILY WENT OUT AND SMOKED. PULLED AND COLLARED C/B FOR RT SIDE, FWD TO MCO. REPLACED BALLAST AND RELAMPED, OPERATION NORMAL.
- [SDR DL733960416](https://openairdocs.org/sdr/DL733960416.md): Door · cracked · Feb 13, 1996 · N302WA · Boeing 737347 · Cargo/Baggage Doors
  > DURING OVERHAUL, THE AFT LOWER FRAME ON THE C1 DOOR WAS DISCOVERED TO HAVE A 1.5 INCH CRACK IN THE RADIUS. IN ACCORDANCE WITH BACO S/B 737-52-1100 REV 2, THE CROSS BEAM WAS MODIFIED AND THE FRAME WAS REPLACED.
- [SDR DL733960062](https://openairdocs.org/sdr/DL733960062.md): Control Cable · loose · Jan 10, 1996 · N302WA · Boeing 737347 · Landing Gear Retraction/Extension System
  > GEAR DOWN 3 RED AND 3 GREEN LIGHTS. RECYCLED OK 3 GREEN, HAPPENED ON 2 APPROACHS. CORRECTED CABLE TENSION FOR LANDING GEAR ACTUATOR, GEAR SWING NORMAL.
- [SDR DL733954382](https://openairdocs.org/sdr/DL733954382.md): Door Frame · crack · Nov 11, 1995 · N302WA · Boeing 737347 · Fuselage Miscellaneous Structure
  > THE AFT CARGO DOOR OPENING FORWARD FRAME WAS FOUND WITH A.5 INCH CRACK AT THE NR 5 STOP FITTING. THE FRAME IS MADE FROM A 0.071 7075-T6 CLAD MATERIAL. THIS ER/A WILL ALLOW THE USE OF THE SRM TYPICAL FORMED SECTION REPAIR.

## 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 = 'N302WA' AND deregistration_id = 'N302WA-2018-01-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N302WA-2018-01-17/reports

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