# Service difficulty reports: N309WA, cancelled Nov 2, 2006

A list on [N309WA, cancelled Nov 2, 2006](https://openairdocs.org/deregistered/N309WA-2006-11-02.md).

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

- [SDR DL733050659](https://openairdocs.org/sdr/DL733050659.md): Skin · cracked · Oct 20, 2005 · N309WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > A CRACK WAS FOUND IN THE FUSELAGE SKIN. CRACK IS APPROX 2 INCHES LONG AFT OF BS 727D, JUST BELOW STR 23L. REPAIRED WITH DOUBLER PER ER/A 451209-14AD, REF AD 2004-18-06.
- [SDR DL733050637](https://openairdocs.org/sdr/DL733050637.md): Skin · cracked · Oct 19, 2005 · N309WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACK WAS FOUND AT CHEM MILL LINE AT BS 727E, STR 24R. CRACK IS 3 INCHES LONG. DOULBER INSTALLED PER ER/A 451199-14AD, AD 2004-18-06, AND SRM 53-00-01.
- [SDR DL733050497](https://openairdocs.org/sdr/DL733050497.md): Indicator · unserviceable · Aug 29, 2005 · N309WA · Boeing 737347 · Engine Oil Pressure
  > DURING T/O ROLL AFTER 80 KTS NR 2 OIL PRESS ROLLED BACK TO BELOW THE RED DIAL. ALL OTHER IND NORMAL. CONTINUED T/O AND PERFORMED LOP CK LIST PROCEDURE PER QRH. ENG SHUTDOWN AND RETURNED TO DTW. SWAP INDICATORS. PROBLEM FOLLOWED. REPLACED NR 2 OIL PRESS I
- [SDR DL733050214](https://openairdocs.org/sdr/DL733050214.md): Circuit Breaker · tripped · Apr 11, 2005 · N309WA · Boeing 737347 · DC Power Distribution System
  > ON CLIMBOUT, BATTERY ON DC- IRS LIGHTS ILLUMINATED. BATTERY VOLTS ZERO. RETURNED TO SLC. MTC IN WORK. FOUND HOT BATTERY BUS C/B POPPED P18 PNL. RESET C/B. PERFORMING DC POWER CHECK.
- [SDR DL733050137](https://openairdocs.org/sdr/DL733050137.md): Apu · fuses · Feb 27, 2005 · N309WA · Boeing 737347 · Airborne Auxiliary Power Unit (APU) System
  > CREW REPORTS FUMES IN CABIN WHILE AT THE GATE. DEPLANED PASSENGERS AND TURNED OVER TO MAINTENANCE. REPLACED APU PER MM.
- [SDR DL733040617](https://openairdocs.org/sdr/DL733040617.md): Skin · cracked · Jun 30, 2004 · N309WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT STA 767 AND STR 22R AT A CHEM MILL LOCATION. REPAIRED IN ACCORDANCE WITH ERA 091533-14.
- [SDR DL733040616](https://openairdocs.org/sdr/DL733040616.md): Skin · cracked · Jun 30, 2004 · N309WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT CHEM MILL LINE AT STA 727E BETWEEN STR 23L AND 25L. REPAIRED IAW 091565-14.
- [SDR DL733040311](https://openairdocs.org/sdr/DL733040311.md): Psu · inoperative · Apr 5, 2004 · N309WA · Boeing 737347 · Passenger Oxygen System
  > PAX SEAT 19DEF 02 MASKS DID NOT DEPLOY WHEN SWITCH IN COCKPIT PUSHED. REPLACED PSU.
- [SDR DL733040216](https://openairdocs.org/sdr/DL733040216.md): Wire · shorted · Mar 5, 2004 · N309WA · Boeing 737347 · Buffet/Galleys
  > AFT OVEN RIGHT SIDE DOUBLE HAD SMOKE COMING FROM BEHIND OVEN CONTROL. REMOVED OVEN, FOUND BURNED WIRES. REPAIRED SAME.
- [SDR DL733030331](https://openairdocs.org/sdr/DL733030331.md): Skin · gouged · Apr 2, 2003 · N309WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > DURING HMV INSPECTIONS, THREE (3) DENTS WERE FOUND IN THE FUSELAGE SKIN BETWEEN FS 757 AND 767 IN THE BAY BETWEEN STRINGERS 20R AND 21R. ADDITIONALLY, FOUR (4) DENTS WERE FOUND BETWEEN FS 757 AND 767 IN THE BAY BETWEEN STRINGERS 21R AND 22R. ALL DENTS WERE W
- [SDR DL733030330](https://openairdocs.org/sdr/DL733030330.md): Fitting · misaligned · Apr 2, 2003 · N309WA · Boeing 737347 · Vertical Stabilizer, Attach Fittings
  > VERTICAL STABILIZER REAR TERMINAL FITTING LUGS WERE DETERMINED TO HAVE UNDERGONE PREVIOUS REWORK WHICH LEFT THE LUG THICKNESS LESS THAN BLUEPRINT SPECIFICATIONS AT EACH OF THE FOUR LUGS. AREA INSPECTED AND NEW BUSHINGS WERE FABRICATED PER DAL ER/A 384672-14 T
- [SDR DL733030328](https://openairdocs.org/sdr/DL733030328.md): Skin · cracked · Apr 1, 2003 · N309WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF PERMANENT REPAIR OF FUSELAGE SKIN/DOUBLER CRACKING, ADDITIONAL CRACK WAS FOUND IN BOTH. THE DAMAGE WAS TRIMMED OUT AND TWO EXTERNAL DOUBLERS WERE INSTALLED WITH SOLID FASTENERS PER ER/A 366481-14, REV C.
- [SDR DL733030322](https://openairdocs.org/sdr/DL733030322.md): Skin · dented · Apr 1, 2003 · N309WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > A DENT WAS FOUND IN THE FUSELAGE SKIN BETWEEN STA 1000 AND 1016 AND BETWEEN STRINGERS 13L AND 14L THE DENT IS CUT OUT AND EXTERNAL DOUBLER AND FILLER ARE INSTALLED SIMILAR TO B737-200 SRM 53-30-3, FIG 48 BUT IN ACCORDANCE WITH ER/A 384711-14.
- [SDR DL733030321](https://openairdocs.org/sdr/DL733030321.md): Skin · dented · Apr 1, 2003 · N309WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > REPAIR OF DENTA DENT WAS FOUND IN THE FUSELAGE SKIN BETWEEN STRINGER 17L AND 18L AT STA 360. THE DENTED MATERIAL WAS CUT OUT AND TWO EXTERNAL ALUMINUM DOUBLERS WERE INSTALLED PER ER/A 384678-14.
- [SDR DL733030320](https://openairdocs.org/sdr/DL733030320.md): Skin · worn · Mar 31, 2003 · N309WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WITH AN AREA OF WEAR BETWEEN FS 857 & 877 NEAR STRINGER 1. THE DAMAGE WAS BLENDED SMOOTH AND AN AREA CUTOUT. THE DAMAGE WAS REPAIRED WITH AN ALUMINUM EXTERNAL REPAIR DOUBLER PER ER/A 384701-14, REV A.
- [SDR DL733030317](https://openairdocs.org/sdr/DL733030317.md): Skin · cracked · Mar 30, 2003 · N309WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND DENTED AND CRACKED AT THE LOWER FWD CORNER OF THE C2 DOOR OPENING. THE DAMAGE WAS REMOVED WITH A 1.5 X 1 INCH CUTOUT TO THE CORNER THROUGH THE BONDED SKIN ASSY AND UNDERLYING BEAR STRAP. THE CORNER WAS REPAIRED WITH MULTIPLE ALUM
- [SDR DL733030314](https://openairdocs.org/sdr/DL733030314.md): Skin · dented · Mar 29, 2003 · N309WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND DENTED NEAR FS 470 BETWEEN STRINGERS 22L & 23L. THE DENT WAS REMOVED WITH A 7 INCHES CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 384681-14, REV A.
- [SDR DL733030313](https://openairdocs.org/sdr/DL733030313.md): Fitting · corroded · Mar 29, 2003 · N309WA · Boeing 737347 · Nacelle/Pylon, Attach Fittings
  > THE AFT LUG OF THE CROWN BEAM FITTING ON THE NR 2 ENGINE PYLON WAS FOUND WITH CORROSION IN THE HOLE BORE. THE BORE WAS OVERSIZED TO 3.10 INCH TO REMOVE THE CORROSION. A STEEL REPAIR BUSHING WAS INSTALLED AND THEN A NEW BEARING. THE REPAIR WAS ACCOMPLISHED P
- [SDR DL733020608](https://openairdocs.org/sdr/DL733020608.md): Proximity Sensor · faulty · May 30, 2002 · N309WA · Boeing 737347 · Door Warning System
  > FWD CARGO DOOR LIGHT CAME ON DURING T/O AT 130 KTS. CONTINUED T/O AND RETURNED TO AIRPORT. CARGO DOOR IND LIGHT INTERMITTENT. REPLACED FWD CARGO DOOR SENSOR PER M/M, DOOR IND OPS NORMAL.
- [SDR DL733001656](https://openairdocs.org/sdr/DL733001656.md): Bushing · worn · Aug 26, 2000 · N309WA · Boeing 737347 · Nacelle/Pylon, Attach Fittings
  > THE STRUT CROWN BEAM ON THE NR 1 ENGINE PYLON WAS FOUND WITH A MIGRATED BUSHING. THE BUSHING WAS REMOVED AND WEAR DAMAGE DISCOVERED IN THE BORE. THE BORE WAS OVERSIZED TO REMOVE ALL DAMAGE AND AN OVERSIZE BUSHING INSTALLED. THE REPAIR WAS ACCOMPLISHED
- [SDR DL733990437](https://openairdocs.org/sdr/DL733990437.md): Skin · cracked · Mar 3, 1999 · N309WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN WAS FOUND CRACKED AROUND THE AFT EDGE OF THE E/E COMPT COOLING AIR EXHAUST DUCT CUTOUT AT BS 380, BL 0.0. THE CRACK EXTENDS AFT FROM THE EDGE OF CUTOUT. REPAIRED PER ERA 366476-14, REV B.
- [SDR DL733990436](https://openairdocs.org/sdr/DL733990436.md): Bulkhead Web · cracked · Mar 3, 1999 · N309WA · Boeing 737347 · Fuselage Main, Bulkhead
  > BS 178 BLKHD WEB WAS FOUND WITH 6 CRACKS, MAX CRACK CUTOUT WAS 1.6 BY 1. REPAIRED PER ERA 332820-14.
- [SDR DL733990387](https://openairdocs.org/sdr/DL733990387.md): Intercostal · cracked · Feb 24, 1999 · N309WA · Boeing 737347 · Fuselage Miscellaneous Structure
  > R1 DOOR INTERCOSTAL AT STRINGER 8A FOUND CRACKED AT STA 334. CRACK REPAIRED PER S/B 737-53A1108 (REF ERA 332823-14AD). ACTION TAKEN, 332823-14AD.
- [SDR DL733990386](https://openairdocs.org/sdr/DL733990386.md): Skin · cracked · Feb 23, 1999 · N309WA · Boeing 737347 · Nacelle/Pylon, Plate/Skin
  > CRACK IN NR 1 PYLON STRUT SKIN AT THE ACCESS OPENING 5727L. ACTION TAKEN, 332810-14.
- [SDR DL733971795](https://openairdocs.org/sdr/DL733971795.md): Oven Controller · malfunctioned · Sep 13, 1997 · N309WA · Boeing 737347 · Buffet/Galleys
  > ELECTRICAL SMELL AND SMOKE EMITTING FROM F/C GALLEY. COTNTRACT MTC CHECKING SAME. REPLACED BOTH CONTROLLERS.
- [SDR DL733960632](https://openairdocs.org/sdr/DL733960632.md): Track Lights · inoperative · Mar 21, 1996 · N309WA · Boeing 737347 · Emergency Lighting
  > ON AIRCRAFT ARRIVAL, EMERGENCY PATH TRACK LIGHTING INOP. CONTRACT MTC CALLED OUT, PARTS SENT BUT WERE UNABLE TO CORRECT PROBLEM. FLIGHT FERRIED TO DFW. REPLACED AFT CABIN FLOOR TRACK LIGHTING POWER SUPPLY AND BATTERIES, REPLACED BOTH AFT EMRGENCY LIGHTING P
- [SDR DL733961622](https://openairdocs.org/sdr/DL733961622.md): Skin · worn · Feb 22, 1996 · N309WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN (0.036 CLAD 2024-T3) UNDERNEATH THE VERTICAL STABILIZER FORWARD FAIRING FROM FS 870 TO 890 WAS FOUND WORN BEYOND B737-300 SRM 53-00-01 LIMITATIONS. THE WEAR WAS FOUND TO HAVE A MAXIMUM DEPTH OF APPROXIMATELY 0.012. ER/A WILL REPAIR THE DAMAGED
- [SDR DL733960043](https://openairdocs.org/sdr/DL733960043.md): Engine · fod · Jan 6, 1996 · N309WA · Boeing 737347 · Engine (Turbine/Turboprop)
  > SHORTLY AFTER T/O, AN ELEC ODOR DEVELOPED IN THE CABIN. COMPLIED WITH CHECKLIST. REMOVED SMALL AMOUNT OF COMPUTER PAPER FROM NR 2 ENG. RAN ENGINE PER PFHB, NO ODOR PRESENT. RAN ALL ELEC SYS AND A/C PACKS, NO PROBLEM FOUND. INSPECTED ENG PER M/M.
- [SDR DL733970009](https://openairdocs.org/sdr/DL733970009.md): Fire Detector · shorted · Jan 3, 1996 · N309WA · Boeing 737347 · Fire Detection
  > LAV FIRE WARNING LIGHT AND CHIME CAME ON TWICE DURING FLIGHT WITHOUT CAUSE. REPLACED FORWARD LAV DETECTOR UNIT, OPERATIONAL TEST NORMAL.
- [SDR DL733950825](https://openairdocs.org/sdr/DL733950825.md): Floor Support · cracked · Feb 20, 1995 · N309WA · Boeing 737347 · Fuselage Miscellaneous Structure
  > AT HMV, FOUND AFT B/B FLOOR SUPPORT CRACKED AT TIE DOWN FITTING STA 727B LT AND 727D RT. REPAIRED PER SRM 53-00-53 FIG 202.
- [SDR DL733950766](https://openairdocs.org/sdr/DL733950766.md): Seat Track · corroded · Feb 20, 1995 · N309WA · Boeing 737347 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND AT H.M.V. RT I/B SEAT TRACK CORRODED AT FS 328. REPAIRED PER SRM 53-00-52 PG 202.
- [SDR DL733950765](https://openairdocs.org/sdr/DL733950765.md): Seat Track · corroded · Feb 20, 1995 · N309WA · Boeing 737347 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND AT H.M.V. RT CTR SEAT TRACK CORRODED BETWEEN STA 328 AND 344. REPAIRED PER SRM 53-00-52 PG 202.
- [SDR DL733950893](https://openairdocs.org/sdr/DL733950893.md): Skin · dented · Feb 18, 1995 · N309WA · Boeing 737347 · Spoilers
  > DURING ROUTINE INSPECTION, SEVERAL SMALL DENTS AND ONE SKIN PUNCTURE WERE FOUND ON INSIDE SKIN OF I/B SPOILER. DAMAGE WAS CAUSED FROM DEBRIS THROWN FROM THE MAIN LANDING GEAR. REPAIRED THE DAMAGE PER SRM 57-50-5.
- [SDR DL733950770](https://openairdocs.org/sdr/DL733950770.md): Skin · cracked · Feb 17, 1995 · N309WA · Boeing 737347 · Elevator, Plate/Skin
  > LT ELEVATOR TAB HINGE OPENINGS CRACKED SEVERAL PLACES. FOUND AT H.M.V. REPAIRED PER SRM 55-20-01.
- [SDR DL733950772](https://openairdocs.org/sdr/DL733950772.md): Skin · damaged · Feb 16, 1995 · N309WA · Boeing 737347 · Elevator, Plate/Skin
  > RT ELEVATOR TAB HAS COMPOSITE BROKEN OUT AT HINGE OPENINGS. FOUND AT H.M.V. REPAIRED PER SRM 51-40-15.
- [SDR DL733950769](https://openairdocs.org/sdr/DL733950769.md): Skin · damaged · Feb 16, 1995 · N309WA · Boeing 737347 · Elevator, Plate/Skin
  > FOUND AT H.M.V. RT ELEVATOR HAS SCAB PATCH ON BOTTOM SURFACE OF COMPOSITE. REPAIRED PER SRM 51-70-17.
- [SDR DL733950768](https://openairdocs.org/sdr/DL733950768.md): Te Skin · damaged · Feb 16, 1995 · N309WA · Boeing 737347 · Elevator, Plate/Skin
  > LT ELEVATOR HAS INBOARD TRAILING EDGE DAMAGED. FOUND AT H.M.V. REPAIRED PER SRM 55-20-01. PART DAMAGED DURING ROUTING.
- [SDR DL733950767](https://openairdocs.org/sdr/DL733950767.md): Floor Support · corroded · Feb 16, 1995 · N309WA · Boeing 737347 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CORRODED LBL 25 FS 947-967. FOUND AT H.M.V. REPAIRED PER SRM 53-00-52 FIG 204.
- [SDR DL733950764](https://openairdocs.org/sdr/DL733950764.md): Seat Track · corroded · Feb 16, 1995 · N309WA · Boeing 737347 · Fuselage, Seat/Cargo Attach Fittings
  > LT I/B SEAT TRACK CORRODED AT F.S. 947. FOUND AT H.M.V. REPAIRED PER SRM 53-00-52.
- [SDR DL733950711](https://openairdocs.org/sdr/DL733950711.md): Floor Beam · corroded · Feb 16, 1995 · N309WA · Boeing 737347 · Fuselage Main, Floor Beam
  > FOUND AT HMV, FLOOR BEAM CORRODED AT FS 328. CORROSION AT BL 0 AND RIGHT OF BL. REPAIRED PER SRM 53-00-51 FIG 205.
- [SDR DL733953045](https://openairdocs.org/sdr/DL733953045.md): Le Skin · worn · Feb 15, 1995 · N309WA · Boeing 737347 · Trailing Edge Flaps
  > NR 1 FOREFLAP, L/E WORN 14 INCHES FROM O/B END AND 56 INCHES FROM I/B END. REPAIRED PER SRM 57-53-01 FIG 201, AT HMV SHOP INSPECTION.
- [SDR DL733950783](https://openairdocs.org/sdr/DL733950783.md): Wedge · delaminated · Feb 15, 1995 · N309WA · Boeing 737347 · Trailing Edge Flaps
  > AT HMV, FOUND FLAP TRAILING EDGE WEDGE DELAMINATED AT ITS OUTBOARD END. REPAIRED PER SRM 57-53-02.

## 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 = 'N309WA' AND deregistration_id = 'N309WA-2006-11-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N309WA-2006-11-02/reports

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