# Service difficulty reports: N313DL, cancelled Jul 20, 2017

A list on [N313DL, cancelled Jul 20, 2017](https://openairdocs.org/deregistered/N313DL-2017-07-20.md).

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

- [SDR DL73S041091](https://openairdocs.org/sdr/DL73S041091.md): Shuttle Valve · leaking · Dec 9, 2004 · N313DL · Boeing 737232 · Master Cylinder/Brake Valve
  > B-SYSTEM HYD LEAK FOUND AT PUSHBACK. REPLACED BRAKE SHUTTLE VLV IAW M/M.
- [SDR DL73S030925](https://openairdocs.org/sdr/DL73S030925.md): Stiffener · corroded · Oct 10, 2003 · N313DL · Boeing 737232 · Fuselage Main, Bulkhead
  > INSPECTION OF THE FS 1016 AFT PRESSURE BULKHEAD PER AD 2002-10-11 REVEALED CORROSION ON THE RT BL 0 STIFFENER. NO OTHER DAMAGE WAS FOUND. THE DAMAGED AREA OF STIFFENER WAS TRIMMED AWAY AND REPAIRED PER BAC S/B 737-53A1075 AND ER/A 087493-14AD.
- [SDR DL73K020379](https://openairdocs.org/sdr/DL73K020379.md): Skin · cracked · Mar 28, 2002 · N313DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > FUSELAGE / AFT GALLEY DOOR CUTOUT / LOWER HINGE CUTOUT: CRACK REPAIR THE LOWER HINGE CUTOUT OF THE AFT GALLEY DOOR CUTOUT (R2) WAS FOUND WITH A.5 INCH CRACK IN THE SKIN ASSY AND UNDERLYING BEARSTRAP. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WI
- [SDR DL73K020376](https://openairdocs.org/sdr/DL73K020376.md): Wedge · delaminated · Mar 27, 2002 · N313DL · Boeing 737232 · Wing Structure
  > FOUND ON V1 LETTER CK AFT WEDGE DALAMINATED O/B END NUMBER 5 SLAT.__C/A REPLACED WEDGE ASSEMBLY
- [SDR DL73K011922](https://openairdocs.org/sdr/DL73K011922.md): Floorbeam · cracked · Dec 10, 2001 · N313DL · Boeing 737232 · Fuselage Main, Floor Beam
  > INSPECTION OF THE RBL 24 FLOORBEAM UPPER CAP PER AD 2001-17-18 REVEALED A TYPICAL CRACK AT FS 680 AT THE AILERON QUADRANT CUTOUT IN THE FLOORBEAM. A PREVIOUS ALUMINUM DOUBLER REPAIR WAS INSTALLED FOR THE WEB. THE CRACKED UPPER CHORD WAS REMOVED, THE WEB INSP
- [SDR DL73K011675](https://openairdocs.org/sdr/DL73K011675.md): Battery · unserviceable · Oct 16, 2001 · N313DL · Boeing 737232 · Emergency Lighting
  > FWD CABIN EMEGENCY EXIT LIGHTS INOP RPLD BATTERY PACK NOW OPS NML
- [SDR DL73K011065](https://openairdocs.org/sdr/DL73K011065.md): Skin · cracked · Jun 23, 2001 · N313DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN AND BONDED DOUBLER ARE CRACKED AT THE R-2 DOOR UPPER HINGE CUTOUT. THE UNDERLYING BEARSTRAP IS NOT DAMAGED. THE CRACK MEASURES.375 INCH. REPAIRED PER ER/A 381177-14.
- [SDR DL73K010303](https://openairdocs.org/sdr/DL73K010303.md): Skin · cracked · Feb 21, 2001 · N313DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH A 3 INCH CRACK AT FS 520 NEAR STRINGER 16L. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B737 SRM 53-30-3 AND ER/A 380104-14.
- [SDR DL73K010134](https://openairdocs.org/sdr/DL73K010134.md): Skin · cracked · Jan 25, 2001 · N313DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > A.75 INCH CRACK WAS FOUND AT THE L2 DOOR CUTOUT UPPER HINGE. THE CRACK WAS TRIMMED OUT AND DOUBLERS INSTALLED PER ERA 259485-14 AT HMV.
- [SDR DL73K010131](https://openairdocs.org/sdr/DL73K010131.md): Clip · tool damage · Jan 25, 2001 · N313DL · Boeing 737232 · Fuselage Miscellaneous Structure
  > THE STRINGER TO FRAME CLIPS AT FS 380 AND STR 5L AND 5R WERE FOUND DAMAGED AND IN NEED OF REPLACEMENT. THE EXTRUDED CLIPS COULD NOT BE PURCHASED SO THEY WERE MANUFACTURED PER ERA 396674-14 AT HMV. THIS EFFECTS SSI F-36.
- [SDR DL73K010110](https://openairdocs.org/sdr/DL73K010110.md): Fitting · corroded · Jan 22, 2001 · N313DL · Boeing 737232 · Fuselage, Stabilizer Attach Fittings
  > CORROSION WAS FOUND ON THE LT AND RT FUSELAGE CLEVIS LUGS THAT ATTACH THE HORIZONTAL STABILIZER. CORROSION WAS REMOVED FROM THE LUG BORES AND FACES PER ERA 396637-14 AT HMV.
- [SDR DL73K010109](https://openairdocs.org/sdr/DL73K010109.md): Fitting · corroded · Jan 22, 2001 · N313DL · Boeing 737232 · Vertical Stabilizer, Attach Fittings
  > CORROSION WAS FOUND ON THE VERTICAL STABILIZER ATTACHMENT LUGS AT THE FRONT SPAR. THE DAMAGE WAS REMOVED AND REPAIRED BY ERA 396636-14 AT HMV.
- [SDR DL73K010108](https://openairdocs.org/sdr/DL73K010108.md): Fitting · corroded · Jan 22, 2001 · N313DL · Boeing 737232 · Horizontal Stabilizer, Attach Fittings
  > CORROSION WAS FOUND ON THE LT AND RT HORIZONTAL STABILIZER ATTACH FITTINGS. THE CORROSION WAS REMOVED AND REPAIRED PER ERA 396651-14 AT HMV.
- [SDR DL73K010092](https://openairdocs.org/sdr/DL73K010092.md): Fitting · corroded · Jan 19, 2001 · N313DL · Boeing 737232 · Fuselage, Landing Gear Attach Fittings
  > CORROSION WAS FOUND IN THE BORES OF THE LT SIDE STRUT SUPPORT FITTING LOCATED AT FS 685. THE BORE DIAMETER WAS INCREASED TO 2.325 INCHES AND REPAIRED PER ERA 396650-14 AT HMV.
- [SDR DL73K010018](https://openairdocs.org/sdr/DL73K010018.md): Frame · cracked · Jan 5, 2001 · N313DL · Boeing 737232 · Fuselage Main, Frame
  > A CRACK WAS FOUND AT THE LOWER FASTENER ON THE INNER CHORD OF THE LEFT AND RIGHT SIDE FS 616 FRAMES AT THE OVERWING FRAME TO STUB JOINT. THIS IS THE TYPICAL CRACK OF S/B 737-53-1182. THE CRACK WAS CUT OUT AND THE AREA REPAIRED PER THE REFERENCED S/B AT MV.
- [SDR DL73K010012](https://openairdocs.org/sdr/DL73K010012.md): Skin · cracked · Jan 2, 2001 · N313DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > A 1 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN JUST FORWARD OF THE LOWER AFT CORNER OF THE L1 DOOR. THE DAMAGE WAS REPAIRED PER BACO DWG 65C27257 AND BACO S/B 737-53-1083. THE DAMAGE WAS FOUND AT HMV.
- [SDR DL73K000515](https://openairdocs.org/sdr/DL73K000515.md): Duct · failed · Mar 14, 2000 · N313DL · Boeing 737232 · Air Distribution System
  > AFTER TAKEOFF PVD WITH BLEEDS OFF, RE-CONFIGURED PNEU PANEL. FELT SURGE OF AIR IN A/C AND MUFFLED NOISE HEARD. FLT ATTN INFORMED CREW OF SMOKE AND FUMES IN CABIN. DECLARED EMERGENCY AND DIVERTED INTO BOS. FOUND BLOWN DUCTS IN AIR CONDITIONING DISTRIBUTION
- [SDR DL73K992427](https://openairdocs.org/sdr/DL73K992427.md): Compressor · bird srtike · Nov 2, 1999 · N313DL · Boeing 737232 · Turbine Engine Compressor Section
  > ON APPROACH BOS CREW REPORTED POSSIBLE BIRD STRIKE. INSPECTION FOUND DAMAGE TO NR 2 ENGINE FAN BLADES. DRESSED BLADES TO LIMITS OF 5 FLIGHTS FLY BACK LIMITS. RAN ENGINE TO TAKEOFF POWER. ALL PARAMETERS AND OPERATION NORMAL.
- [SDR DL73K990771](https://openairdocs.org/sdr/DL73K990771.md): Light · damaged · Apr 9, 1999 · N313DL · Boeing 737232 · Passenger Compartment Lighting
  > LIGHT IN GALLEY SMOKED AND C/B POPPED. PULLED AND COLLARD GALLEY LIGHT C/B ON P18 PANEL. FOUND AFT LEFT GALLEY LIGHT ASSY TO BE THE PROBLEM. REPLACED SAME.
- [SDR DL73K982266](https://openairdocs.org/sdr/DL73K982266.md): Skin · cracked · Oct 31, 1998 · N313DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN AND DOUBLER WERE FOUND TO HAVE A 1.5 INCH TYPICAL CRACK AT THE LOWER AFT CORNER OF THE R1 DOOR CUTOUT. THE CRACK WAS REPAIRED PER THE B737-200 SRM 53-30-3 FIG 26, EXCEPT BLIND BOLTS WERE AUTHORIZED ON A TIME LIMITED BASIS. THE REPAIR WAS AC
- [SDR DL73K972292](https://openairdocs.org/sdr/DL73K972292.md): Mask · unsafe · Nov 8, 1997 · N313DL · Boeing 737232 · Crew Oxygen System
  > COCKPIT PBE INDICATOR BEYOND LIMITS. REPLACED COCKPIT PBE.
- [SDR DL73K971885](https://openairdocs.org/sdr/DL73K971885.md): Skin · cracked · Sep 10, 1997 · N313DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE R2 DOORWAY HAS A CRACK AT THE FWD LOWER CORNER APPROX 3.5 IN LENGTH. THE CRACK IS IN THE EXTERIOR SKIN AS WELL AS THE BONDED DOUBLER AND THE BEAR STRAP. THE SKIN AND DOUBLER ARE BOTH MADE OUT OF CLAD 2024-T3 WITH A THICKNESS OF.036. THE BEAR STRAP IS.
- [SDR DL73K962708](https://openairdocs.org/sdr/DL73K962708.md): Bulkhead Web · cracked · Dec 11, 1996 · N313DL · Boeing 737232 · Fuselage Main, Bulkhead
  > SIX CRACKS WERE FOUND ON THE FWD FACE OF THE FS 178 BULKHEAD WEB. THREE INDEPENDENT CUTOUTS WERE REQUIRED TO REMOVE THE CRACKS. TWO CUTOUTS MEASURE 5.O VERTICALLY BY 1.0 INBOARD-OUTBOARD AT WL 197 TO WL 202 AND ARE AT THE LBL 5.7 AND RBL 5.7 VERTICAL STRAP P
- [SDR DL73S953418](https://openairdocs.org/sdr/DL73S953418.md): Skin · damaged · Aug 17, 1995 · N313DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > GROUND SERVICE EQUIPMENT CAUSED 2 X 4 INCH TEAR IN FUSELAGE SKIN FROM FS 360 - 380, STRINGER 19R TO 20R. SKIN WAS TRIMMED OUT AND REPAIRED PER DL ERA 302313-14.
- [SDR DL73S951035](https://openairdocs.org/sdr/DL73S951035.md): Coffee Maker · failed · Mar 9, 1995 · N313DL · Boeing 737232 · Buffet/Galleys
  > DURING CLIMB-OUT, HAD SMOKE AND FUMES COMING FROM FORWARD GALLEY. ALSO, WATER LEAKING AT COFFEE MAKER. DEACTIVATED POWER AND RETURNED ICT. FOUND COFFEE MAKER DRAIN VALVE STUCK OPEN. REPLACED MAKER 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 = 'N313DL' AND deregistration_id = 'N313DL-2017-07-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N313DL-2017-07-20/reports

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