# Service difficulty reports: N308WA, cancelled Jan 3, 2018

A list on [N308WA, cancelled Jan 3, 2018](https://openairdocs.org/deregistered/N308WA-2018-01-03.md).

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

- [SDR DL733060111](https://openairdocs.org/sdr/DL733060111.md): Duct · unknown · Feb 9, 2006 · N308WA · Boeing 737347 · Air Distribution System
  > UNABLE TO MAINTAIN PRESSURIZATION WITH LT PACK AT FL 240. RT PACK CURRENTLY ON MCO. REPAIRING RT PACK. REPLACED DUCT ON RT PACK CLEARED MCO ON RT PACK A/C PRESSURIZATION CHECK NORMAL.
- [SDR DL733060098](https://openairdocs.org/sdr/DL733060098.md): Actuator · broken · Feb 2, 2006 · N308WA · Boeing 737347 · Drag Control Actuator
  > NR 4 O/B SPOILER ACTUATOR BROKE OFF AT REAR HINGE POINT, CAUSING HINGE POINT TO BREAK AT SPOILER PANEL. REPLACED BOTH UNITS. ACTUATOR P/N 273001083.
- [SDR DL733050524](https://openairdocs.org/sdr/DL733050524.md): Skin · cracked · Sep 6, 2005 · N308WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > CRACK FOUND IN FUSELAGE SKIN AT CHEM-MIL WHILE ACCOMP OPN 57546. CRACK REPORTED TO BE 1.5 INCH LONG, LOCATED AT FS 727E, S-24L. REPAIRED PER SRM 53-00-01, FIGURE 201. RELATED TO AD 2004-18-06, S/B 737-53A1210, & S/B 737-53-1065.
- [SDR DL733050523](https://openairdocs.org/sdr/DL733050523.md): Skin · cracked · Sep 6, 2005 · N308WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > CRACK WAS FOUND IN THE FUSELAGE SKIN WHILE DOING OPN 57546 INSPECTIONS. REPAIRED PER SRM 53-00-01, FIGURE 201. REF AD 2004-18-06 / S/B 737-53A1210 / 737-53-1065.
- [SDR DL733050323](https://openairdocs.org/sdr/DL733050323.md): Outflow Valve · unserviceable · Jun 13, 2005 · N308WA · Boeing 737347 · Pressure Regulator/Outflow Valve
  > AIRCRAFT WOULD NOT PRESSURIZE. FOUND AUTO FLOW CONTROL VALVE NOT CLOSING PER CABIN PRESS LEAK TEST 05-51-91-702. REPLACED VALVE PER MM 21-58-31. OP CK OK. AIRCRAFT PRESSURIZED ON GROUND PER MM.
- [SDR DL733040746](https://openairdocs.org/sdr/DL733040746.md): Skin · cracked · Aug 7, 2004 · N308WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > A SKIN CRACK WAS FOUND ALONG THE THE MILL LINE OF THE UNDERLYING BONDED DOUBLER JUST AFT OF FS 727D AND BELOW STRINGER 23L. THE CRACK WAS REMOVED WITH A 1.5 X 2.5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 092528-1
- [SDR DL733030353](https://openairdocs.org/sdr/DL733030353.md): Power Supply · inoperative · Apr 11, 2003 · N308WA · Boeing 737347 · Emergency Lighting
  > AFT CABIN EMERGENCY LIGHT INOPERATIVE, RELAMPED NO HELP R & R POWER SUPPLY LIGHT OPS NORMAL.
- [SDR DL733030199](https://openairdocs.org/sdr/DL733030199.md): Smoke Detector · malfunctioned · Feb 26, 2003 · N308WA · Boeing 737347 · Smoke Detection
  > RT AFT LAV SMOKE DETECTOR LIGHT AND CHIME CAME ON AND OFF IN FLT. REPLACED SMOKE DETECTOR UNIT
- [SDR DL733030147](https://openairdocs.org/sdr/DL733030147.md): Fitting · corroded · Feb 12, 2003 · N308WA · Boeing 737347 · Fuselage, Stabilizer Attach Fittings
  > CORROSION WAS FOUND IN THE BORES OF BOTH THE LT AND RT PRIMARY FORWARD CLEVIS LUGS. THE LHS PRIMARY FORWARD CLEVIS LUG WAS OVERSIZED TO A DIAMETER OF 1.440 INCH TO REMOVE THE CORROSION. THE RHS PRIMARY FORWARD CLEVIS LUG WAS OVERSIZED TO A DIAMETER OF 1.408
- [SDR DL733030146](https://openairdocs.org/sdr/DL733030146.md): Fitting · corroded · Feb 12, 2003 · N308WA · Boeing 737347 · Vertical Stabilizer, Attach Fittings
  > CORROSION WAS FOUND IN THE BORES OF BOTH THE REAR SPAR LT AND RT PRIMARY AND FAIL-SAFE FIN LUGS. THE BORES WERE ENLARGED TO REMOVE CORROSION. ALSO, THE FORWARD FACE OF THE LHS PRIMARY FIN LUG WAS SPOTFACED TO REMOVE CORROSION. REPAIR BUSHINGS WERE INSTALLED
- [SDR DL733011754](https://openairdocs.org/sdr/DL733011754.md): Sensor · dirty · Nov 3, 2001 · N308WA · Boeing 737347 · Door Warning System
  > CLIMBING THRU 4000 FT FWD CARGO LIGHT ILLUMINATED. RETURNED FOR LANDING. MAINTENANCE CONFIRMED DOOR CLOSED AND LOCKED. CLEANED FWD SENSOR OF FOREIGN SUBSTANCE, OP CHECKS GOOD.
- [SDR DL733011450](https://openairdocs.org/sdr/DL733011450.md): Skin · gouged · Aug 31, 2001 · N308WA · Boeing 737347 · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN / FS 907-1156 / STRG. 25L-25R: TAIL STRIKE REPAIR THE FUSELAGE SKIN SUFFERED A TAIL STRIKE ON TAKEOFF WHICH RESULTED IN MULTIPLE GOUGES, SCRAPES, AND HOLES IN THE FUSELAGE SKIN FROM F
- [SDR DL733010136](https://openairdocs.org/sdr/DL733010136.md): Bulkhead · cracked · Jan 24, 2001 · N308WA · Boeing 737347 · Fuselage Main, Bulkhead
  > WHILE ACCOMPLISHING INSPECTIONS OF THE FS 178 BULKHEAD WEB A CRACK WAS FOUND AT RBL 5.7 AND WL 211. THE CRACK WAS LOCATED ABOVE AND EXISTING DOUBLER REPAIR FOR CRACKS BELOW WL 205. THE NEW CRACK WAS REMOVED WITH A 1 INCH CUTOUT AND THE EXISTING REPAIR DOUBLE
- [SDR DL733010095](https://openairdocs.org/sdr/DL733010095.md): Frame · cracked · Jan 18, 2001 · N308WA · Boeing 737347 · Fuselage Main, Frame
  > THE FS 178 BULKHEAD LT SIDE CHORD WAS FOUND WITH A.5 INCH VERTICAL CRACK IN THE RADIUS OF THE CHORD. A NEW SECTION OF SIDE CHORD WAS SPLICED IN PER THE REQUIREMENTS OF BAC S/B 737-53A1173 AND DOCUMENTED PER ER/A 379791-14AD.
- [SDR DL733992265](https://openairdocs.org/sdr/DL733992265.md): Actuator · cracked · Oct 11, 1999 · N308WA · Boeing 737347 · Drag Control Actuator
  > AFTER LANDING, LOST HYD SYS A GROUND PERSONNEL REPORTED LEAK RT WING AREA. FOUND NR 8 GROUND SPOILER ACT LEAKING, REPLACED SAME..
- [SDR DL733981852](https://openairdocs.org/sdr/DL733981852.md): Engine · failed · Sep 7, 1998 · N308WA · Boeing 737347 · Engine (Turbine/Turboprop)
  > AT 1500 FT NR 1 ENGINE LOUD BANG AND OVERTEMP TO 930 CELSIUS. FOLLOWED BY VIBRATION WITH THROTTLE REDUCED IDLE INDICATIONS NORM FOR 4-5 MIN THEN VIBRATION IND WENT TO 3. A/C STARTED TO SHAKE. ENG SHUT DOWN. PAX REPORTED FLAMES AT TIME OF COMPRESSOR STALL T
- [SDR DL733981773](https://openairdocs.org/sdr/DL733981773.md): Line · ruptured · Aug 27, 1998 · N308WA · Boeing 737347 · Landing Gear Retraction/Extension System
  > LOST A-SYS HYD PRESS AND QTY JUST AFTER RAISING GEAR ON T/O. FOUND RT GEAR UP LINE TO ACT RUPTURED. REPLACED LINE, BOTH A-SYS CASE DRAIN CHECK OK. LEAK CHECKED PUMPS, CHECK OK.
- [SDR DL733970554](https://openairdocs.org/sdr/DL733970554.md): Battery · discharged · Mar 25, 1997 · N308WA · Boeing 737347 · Emergency Lighting
  > FWD EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY AND BULB, OPS OK.
- [SDR DL733950388](https://openairdocs.org/sdr/DL733950388.md): Skin · dented · Jan 12, 1995 · N308WA · Boeing 737347 · Trailing Edge Flaps
  > DURING HMV SHOP INSPECTION, RIGHT WING NR 3 FORE FLAP WAS FOUND WITH DENTED SKIN, LOWER LEADING EDGE JUST OUTBOARD OF INBOARD ATTACH POINT. REPAIRED PER SRM 57-53-01 FIG 201.
- [SDR DL733950213](https://openairdocs.org/sdr/DL733950213.md): Skin · punctured · Jan 10, 1995 · N308WA · Boeing 737347 · Elevator, Plate/Skin
  > DURING HMV, FOUNG SMALL PUNCTURE AND FIBER DAMAGE IN LEFT ELEVATOR UPPER SURFACE. LOCATED 3 FEET FROM INBOARD AND 7 INCHES FROM SPAR AFT. REPAIRED ELEVATOR PUNCTURE PER SRM 55-20-01 IN REF TO 51-70-17.
- [SDR DL733950160](https://openairdocs.org/sdr/DL733950160.md): Attach Fitting · cracked · Jan 10, 1995 · N308WA · Boeing 737347 · Wing, Landing Gear Attach Fittings
  > DURING ROUTINE INSPECTION AT HMV, THE RT WING O/B AFT SUPPORT FITTING FOR THE MAIN LANDING GEAR BEAM WAS FOUND CRACKED. THE CRACKED FITTING WILL REMAIN IN SERVICE PER S/B 737-57-1216 AND WILL BE REPAIRED PER S/B REQUIREMENTS.
- [SDR DL733950119](https://openairdocs.org/sdr/DL733950119.md): Seat Track · corrosion · Jan 8, 1995 · N308WA · Boeing 737347 · Fuselage, Seat/Cargo Attach Fittings
  > AT HMV, CORROSION WAS FOUND ON SEAT TRACK HORIZONTAL FLANGE AT STA 344 LBL 20. REMOVED OLD SECTION, FABRICATED NEW SEAT TRACK AND INSTALLED SEAT TRACK PER SRM53-00-52.
- [SDR DL733950069](https://openairdocs.org/sdr/DL733950069.md): Floor Beam · corroded · Jan 5, 1995 · N308WA · Boeing 737347 · Fuselage Main, Floor Beam
  > DURING HMV, CORROSION WAS FOUND ON A FLOOR BEAM AT FS 328 AROUND FASTENER HOLES FROM LEFT TO RIGHT SIDE OF THE FUSELAGE. REPAIRS INVOLVED TREAT AND PAINT LBL49 PER PS 900-2 NR 5 AND REPAIR LBL 36 AND RT OUTBOARD END PER SRM 53-00-51 FIG 205.
- [SDR DL733950212](https://openairdocs.org/sdr/DL733950212.md): Le Slat · cracked · Jan 4, 1995 · N308WA · Boeing 737347 · Leading Edge Devices
  > AT HMV, FOUND NR 5 LEADING EDGE SLAT CRACKED ON BOTTOM ALONG FASTENERS. REPAIRED PER SRM 57-43-01 FIG 205.
- [SDR DL733950118](https://openairdocs.org/sdr/DL733950118.md): Floor Beam · corrosion · Jan 4, 1995 · N308WA · Boeing 737347 · Fuselage Main, Floor Beam
  > AT HMV, CORROSION WAS FOUND ON FLOOR BEAM CAPS SECTIONS AT STA 960 TO 975 RBL 30-40. REPAIRED PER SRM 53-00-51.
- [SDR DL733950101](https://openairdocs.org/sdr/DL733950101.md): Floor Support · corroded · Jan 4, 1995 · N308WA · Boeing 737347 · Fuselage Miscellaneous Structure
  > AT HMV, FOUND FLOOR SUPPORT CORRODED AT STA 960 LBL 10-30. REMOVED OLD, FABRICATED AND INSTALLED NEW SUPPORT PER SRM 51-00-00.
- [SDR DL733950097](https://openairdocs.org/sdr/DL733950097.md): Seat Track · corrosion · Jan 4, 1995 · N308WA · Boeing 737347 · Fuselage, Seat/Cargo Attach Fittings
  > AT HMV, CORROSION WAS FOUND ON SEAT TRACK UPPER SURFACES AT STA 960 ON THE OUTBOARD SIDE. REPAIRED PER SRM 53-00-52 FIG 204.
- [SDR DL733950068](https://openairdocs.org/sdr/DL733950068.md): Floor Beam · corroded · Jan 4, 1995 · N308WA · Boeing 737347 · Fuselage Main, Floor Beam
  > DURING HMV, CORROSION WAS FOUND ON FLOOR BEAM AT STA 986.5 AROUND FASTENER HOLES ON TOP FLANGE. REPAIRED PER SRM 53-00-51 PG 220.
- [SDR DL733950076](https://openairdocs.org/sdr/DL733950076.md): Floor Track · corrosion · Jan 3, 1995 · N308WA · Boeing 737347 · Fuselage, Seat/Cargo Attach Fittings
  > AT HMV, CORROSION WAS FOUND ON GALLEY FLOOR TRACK AT FLOOR BEAM 328 RT SIDE ON THE FWD END OF INBOARD TRACK. REPAIRED PER SRM 53-00-52 PG 202-205.
- [SDR DL733950075](https://openairdocs.org/sdr/DL733950075.md): Floor Track · corrosion · Jan 3, 1995 · N308WA · Boeing 737347 · Fuselage, Seat/Cargo Attach Fittings
  > AT HMV, CORROSION WAS FOUND ON GALLEY FLOOR TRACK AT FLOOR BEAM STA 328 ON OUTBOARD TRACK RIGHT HAND SIDE AT FWD END. REPLACED SEAT TRACK PER SRM 51-00-00.
- [SDR DL733950074](https://openairdocs.org/sdr/DL733950074.md): Floor Track · corrosion · Jan 3, 1995 · N308WA · Boeing 737347 · Fuselage, Seat/Cargo Attach Fittings
  > AT HMV, CORROSION WAS FOUND ON GALLEY FLOOR TRACK AT FLOOR BEAM 328 ON RT SIDE AT CENTER FWD END. REPAIRED PER SRM 53-00-52 PG 202-205.
- [SDR DL733950073](https://openairdocs.org/sdr/DL733950073.md): Seat Track · corroded · Jan 3, 1995 · N308WA · Boeing 737347 · Fuselage, Seat/Cargo Attach Fittings
  > AT HMV, FOUND CORROSION ON LEFT OUTBOARD SEAT TRACK AT FS 344. REPAIRED PER SRM 53-00-52 PG 202-205.
- [SDR DL733950072](https://openairdocs.org/sdr/DL733950072.md): Floor Beam · corrosion · Jan 3, 1995 · N308WA · Boeing 737347 · Fuselage Main, Floor Beam
  > AT HMV, CORROSION WAS FOUND ON FLOOR BEAM 'T' CAP SURFACE AT STA 294 BL0 TO OUTBOARD RBL AROUND FASTENER HOLES. REPAIRED PER ERA 300920-14.
- [SDR DL733950071](https://openairdocs.org/sdr/DL733950071.md): Floor Beam · corroded · Jan 3, 1995 · N308WA · Boeing 737347 · Fuselage Main, Floor Beam
  > DURING HMV, CORROSION WAS FOUND AT FS 312 FLOOR BEAM FASTENER HOLES AT LBL 6, CENTERLINE AND RBL 8. REPAIRED PER SRM 53-10-51 FIG 205.

## 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 = 'N308WA' AND deregistration_id = 'N308WA-2018-01-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N308WA-2018-01-03/reports

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