# Service difficulty reports: N319DL, cancelled May 13, 2009

A list on [N319DL, cancelled May 13, 2009](https://openairdocs.org/deregistered/N319DL-2009-05-13.md).

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

- [SDR DL73S060132](https://openairdocs.org/sdr/DL73S060132.md): Gasper Fan · failed · Feb 15, 2006 · N319DL · Boeing 737232 · Air Distribution Fan
  > BURNT ELECT SMELL WITH GASPER FAN ON. REPLACED FAN.
- [SDR DL73S060092](https://openairdocs.org/sdr/DL73S060092.md): Stiffener · corroded · Jan 30, 2006 · N319DL · Boeing 737232 · Fuselage Main, Bulkhead
  > CORROSION FOUND ON THE BS 1016 AFT PRESSURE BULKHEAD Z-STIFFENER AT STR 26R. REMOVED CORROSION, DAMAGE WITHIN ALLOWABLE LIMITS WITHOUT REINFORCEMENT. REF AD 2002-10-11, SB 737-53A-1075.
- [SDR DL73S060090](https://openairdocs.org/sdr/DL73S060090.md): Floorbeam · cracked · Jan 29, 2006 · N319DL · Boeing 737232 · Fuselage Main, Floor Beam
  > THE LBL & RBL 24 LONGITUDINAL OVERWING FLOORBEAMS WERE PREVIOUSLY MODIFIED PER REV B OF 3-56673-12AD, HOWEVER THIS INSTALLATION DOES NOT MEET THE REQUIREMENTS OF AD 2001-17-18. FLOORBEAM WEBS WERE FOUND CRACKED. FLOORBEAM C-CHANNELS WERE REPLACED WITH AD COM
- [SDR DL73S050226](https://openairdocs.org/sdr/DL73S050226.md): Indicator · failed · Apr 20, 2005 · N319DL · Boeing 737232 · Flight Environment Data
  > DURING PUSHBACK A ELECTRICAL SPARKING ARCING LIKE SOUND A VERY SLIGHT SMELL OF ELECTRICAL FUMES WHICH STOPPED VERY QUICKLY F/O`S VSI WENT INOP. REPLACED VSI.
- [SDR DL73S050091](https://openairdocs.org/sdr/DL73S050091.md): Engine · malfunctioned · Feb 8, 2005 · N319DL · Boeing 737232 · Engine (Turbine/Turboprop)
  > FLT 7000 FT CLIMB EPR 250 - CLIMBING CLEAN HEARD LOUD BOOM WITH A/C SHUDDER ONCE. ALL ENG IND NORM AND STEADY. PNEU NORM. NO VISIBLE DAMAGE FROM CABIN F/A'S. ATB CVG UNEVENTFUL. DECLARED EMERGENCY WITH CVG DEPT CONTROL. BORO BOTH ENGINES, OK. FOUND LEFT
- [SDR DL73S050026](https://openairdocs.org/sdr/DL73S050026.md): Ballast · inoperative · Jan 13, 2005 · N319DL · Boeing 737232 · Passenger Compartment Lighting
  > CREW REPORTED ACRID SMELL THROUGHTOUT CABIN. INSP E/E COMP, CARGO BAYS, CABIN BALLAST. FOUND BALLAST OF SEAT 2CD BAD. REPLACED BALLAST. A/C OK FOR SERVICE.
- [SDR DL73S040999](https://openairdocs.org/sdr/DL73S040999.md): Skin · cracked · Oct 28, 2004 · N319DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH A 4 INCH CRACK RUNNING ALONG THE BONDED DOUBLER EDGE JUST BELOW STRINGER 23R BETWEEN FS 927 & 947. AN EXISTING SKIN DOUBLER WAS IN AN ADJACENT FRAME BAY. THE EXISTING REPAIR WAS REMOVED, THE CRACK WAS CUT OUT OF THE SKIN, AND
- [SDR DL73S040193](https://openairdocs.org/sdr/DL73S040193.md): Accessory Unit · failed · Feb 26, 2004 · N319DL · Boeing 737232 · Landing Gear Retraction/Extension System
  > ON T/O WHEN GEAR HANDLE RAISED LEFT MAIN GEAR RED UNSAFE LIGHT REMAINED ON. NO OTHER ABNORMAL INDICATIONS. REPLACED LANDING GEAR ACCESSORY UNIT.
- [SDR DL73S040172](https://openairdocs.org/sdr/DL73S040172.md): Clevis · corroded · Feb 18, 2004 · N319DL · Boeing 737232 · Fuselage Main, Attach Fittings
  > CORROSION DAMAGE WAS NOTED ON THE NR 5, NR 6 AND NR 11 BODY CLEVIS LUGS. CORROSION WAS REMOVED AND FITTINGS REWORKED IAW 386170-14.
- [SDR DL73S040170](https://openairdocs.org/sdr/DL73S040170.md): Skin · dented · Feb 18, 2004 · N319DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > THE UPPER SKIN OF THE S19R WAS FOUND DENTED. DENTED WAS REMOVED AND REPAIR INSTALLED IAW 386089-14.
- [SDR DL73S040169](https://openairdocs.org/sdr/DL73S040169.md): Support Fitting · corroded · Feb 18, 2004 · N319DL · Boeing 737232 · Fuselage Main, Attach Fittings
  > CORROSION WAS NOTED ON BOTH THE LT AND RT BS 685 MLG SUPPORT FITTINGS IN THE LUG BORES AND FACES. CORROSION WAS REMOVED AND FITTINGS REWORKED IAW ERA 386114-14.
- [SDR DL73S040152](https://openairdocs.org/sdr/DL73S040152.md): Bulkhead · corroded · Feb 12, 2004 · N319DL · Boeing 737232 · Fuselage Main, Bulkhead
  > CORROSION WAS NOTED AT BS 1016 PRESSURE BLKHD, AT BL 0 AND AFFECTED THE WEB/GORE AND CHANNEL STIFFENERS. REPAIRED PER ERA 386069-14AD.
- [SDR DL73S040149](https://openairdocs.org/sdr/DL73S040149.md): Frame · cracked · Feb 11, 2004 · N319DL · Boeing 737232 · Fuselage Main, Frame
  > DURING INSPECTION OF THE BS 663 FRAME CRACKS WERE NOTED IN THE FRAME AT S3L, S2L AND S1. DURING INSTALLATION OF THE SRM FRAME REPAIR IT WAS NECESSARY TO CUT THE FUSELAGE SKIN TO ACCOMMODATE FRAME REPAIR FASTENERS. FRAME WAS REPAIRED PER SRM, SKIN REPAIRED PE
- [SDR DL73S040144](https://openairdocs.org/sdr/DL73S040144.md): Flap Track · corroded · Feb 9, 2004 · N319DL · Boeing 737232 · Trailing Edge Flaps
  > THE REAR ENGINE MOUNT ATTACH HOLES, LOCATED AT THE NR 2 AND NR 3 T/E FLAPS, OUTBOARD TRACKS WERE NOTED WITH CORROSION IN THE BORES. CORROSION WAS REMOVED AND TRACKS WERE REWORKED PER ERA 386130-14.
- [SDR DL73S040115](https://openairdocs.org/sdr/DL73S040115.md): Attach Fitting · corroded · Jan 28, 2004 · N319DL · Boeing 737232 · Horizontal Stabilizer, Attach Fittings
  > THE STABILZER ATTACHMENT LUGS WERE FOUND WITH DAMAGE EXCEEDING THE LIMITS OF SB 737-55-1033. DAMAGE WAS REMOVED BY BLENDING AND OVERSIZING BORES PER ER/A 386108-14AD.
- [SDR DL73S040104](https://openairdocs.org/sdr/DL73S040104.md): Attach Fitting · corroded · Jan 28, 2004 · N319DL · Boeing 737232 · Empennage Flight Control Surfaces, Attach Fittings
  > NUMEROUS ATTACHMENT FITTING LUGS ON THE HORIZ STAB TO FUSELAGE JOINT REQUIRED MACHINING BEYOND PUBLISHED LIMITS IN ORDER TO REMOVE CORROSION. CORROSION WAS REMOVED AND LUGS REWORKED IAW ERA 386108-14AD.
- [SDR DL73S040102](https://openairdocs.org/sdr/DL73S040102.md): Floorbeam · cracked · Jan 28, 2004 · N319DL · Boeing 737232 · Fuselage Main, Floor Beam
  > DURING INSPECTION THE BS 520 FLOORBEAM WAS NOTED WITH CRACKS IN THE RADIUS, ALONG THE UPPER CHORD TO WEB RADIUS AT LBL 24.75, LBL 45.5 AND RBL 24.75. UPPER CAP WAS REMOVED AND A NEW SECTION SPLICED IN PER ERA 386080-14.
- [SDR DL73K002017](https://openairdocs.org/sdr/DL73K002017.md): Actuator · intermittent · Oct 15, 2000 · N319DL · Boeing 737232 · Engine Fuel Distribution
  > AFTER STARTING NR 1ENG (NORMAL START) DURING TAXI OUT NR 1 ENG FLAMED OUT. ON RESTART ATTEMPT AT GATE, NO FUEL FLOW INDICATION AFTER START LEVER RAISED TO IDLE. REPLACED BAD FUEL SOV ACTUATOR AND GATE ASSY PER MM. RAN NR 1 ENG, ALL PARAMETERS GOOD.
- [SDR DL73K001081](https://openairdocs.org/sdr/DL73K001081.md): Antenna · inoperative · Jun 2, 2000 · N319DL · Boeing 737232 · Weather Radar System
  > WEATHER RADAR INOP, CON/IND FAULT. REPLACED R/T AND ANT PER MM, PUSHED OUT INTO RAMP AND PAINTED ACTUAL WEATHER, OPS NORMAL IN ALL MODES.
- [SDR DL73K000625](https://openairdocs.org/sdr/DL73K000625.md): Controller · malfunctioned · Apr 2, 2000 · N319DL · Boeing 737232 · Overheat Detection
  > ON DESCENT INTO TPA PASSING THROUGH 15000 FT, RECEIVED A WHEEL WELL FIRE INDICATION. AFTER PERFORMING APPROPRIATE PROCEDURE WHEEL WELL FIRE LIGHT BECAME INTERMITTENT. T/S PER MM. UNABLE TO DUPLICATE DISCREPANCY. REPLACED COMP OVHT CONTROLLER MODUEL AS P
- [SDR DL73K000529](https://openairdocs.org/sdr/DL73K000529.md): Valve · malfunctioned · Mar 17, 2000 · N319DL · Boeing 737232 · Cabin Pressure Control System
  > AIRCRAFT FAILED TO PRESSURIZE AFTER T/O FROM PBI. OUTFLOW VLVS INDICATED FULL CLOSED. F/A REPORTED THERE WAS LOUD WIND NOISE AROUND L1 DOOR. DOOR INDICATED CLOSED AND LOCKED. DIVERTED TO MCO. PRESSURIZED AC TO 7 PSID. CHECKED ALL DOOR SEALS- CABIN, CARGO
- [SDR DL73K991715](https://openairdocs.org/sdr/DL73K991715.md): Wire · failed · Jul 31, 1999 · N319DL · Boeing 737232 · Stabilizer Control System
  > STAB TRIM CONTROL WHEEL SWITCHES INOP. POPS ACTUATOR C/B. AUTOPILOT TRIM IS OK. FOUND WIRES SHORTED TO GROUND AT BULKKHEAD 1088. REPAIRED WIRE WITH SPLICES. WIRE NRS W326-313, W326-312, W326-311 PER BOEING STANDARD WIRING PRACTICES MANUAL.
- [SDR DL73K982229](https://openairdocs.org/sdr/DL73K982229.md): O-Ring · failed · Oct 29, 1998 · N319DL · Boeing 737232 · Drag Control Actuator
  > LOSS OF HYD SYS A QTY IN FLT. REPL NO3 FLT SPOILER ACTUATOR. O-RING RUPTURED ON ACTUATOR. ALL LEAK AND OPN TEST NML.
- [SDR DL73K980223](https://openairdocs.org/sdr/DL73K980223.md): Bulkhead Web · cracked · Jan 26, 1998 · N319DL · Boeing 737232 · Fuselage Main, Bulkhead
  > SEVERAL CRACKS FOUND IN THE FS 178 BULKHEAD. REPAIRED PER ERA 331261-14.
- [SDR DL73K980222](https://openairdocs.org/sdr/DL73K980222.md): Fitting · cracked · Jan 26, 1998 · N319DL · Boeing 737232 · Wing, Landing Gear Attach Fittings
  > DURING INSPECTION PER SB 737-57-1216 TWO CRACKS WERE FOUND IN THE MLG BEAM AFT SUPPORT FITTING ON THE RS OF THE RT WING. THE INBD CRACK LOCATION IS TYP PER SB. THE OUTBOARD FASTENER LOCATION WAS OS TO 0.438 DIAM AND THE CRACK WAS REMOVED. REPAIRED PER ERA 3
- [SDR DL73K980221](https://openairdocs.org/sdr/DL73K980221.md): Spar Chord · corroded · Jan 26, 1998 · N319DL · Boeing 737232 · Horizontal Stabilizer, Spar/Rib
  > CORROSION FOUND ON THE UPPER SURFACE OF THE AFT FLANGE OF THE HORIZ STAB REAR SPAR UPPER CHORD. REPAIRED PER ERA 331272-14.
- [SDR DL73K980184](https://openairdocs.org/sdr/DL73K980184.md): Skin · cracked · Jan 22, 1998 · N319DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > SKIN AT THE COOLING DUCT CUTOUT AT BS 379, APPROXIMATELY BL0 WAS FOUND CRACKED AT THE AFT EDGE OF THE CUTOUT. CRACK IS APPROXIMATELY 1.5 IN LENGTH AND IS TYPICAL OF CRACKS DESCRIBED BY SB 737-53-1117. REPAIRED PER ERA 331270-14 (SB 737-53-1117).
- [SDR DL73K980066](https://openairdocs.org/sdr/DL73K980066.md): Apu · odor · Jan 9, 1998 · N319DL · Boeing 737232 · APU Bleed Air System
  > SMOKE ALARM WENT OFF IN FWD LAV CREW COULD SMELL ACRID SMELL. FOUND APU PUTTING OIL INTO PNEUMATIC DUCTS. FWD APU TO MCO REPLD DETECTOR BATTERY, REPLD LT AND RT COALESCER BAGS RAN BOTH ENGS AT 1.80 EPR FOR APPROX 15 MINS TO BURN OIL SMELL OUT.
- [SDR DL73K972197](https://openairdocs.org/sdr/DL73K972197.md): Skin · cracked · Oct 17, 1997 · N319DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AND BEAR STRAP AFT GALLEY DOOR SURROUND. REPAIR FOR CRACK AT LWR HINGE CUT OUT. A.25 INCH CRACK WAS FOUND IN THE SKIN AND A 1.0 INCH CRACK IN THE BEAR STRAP OF THE AFT GALLEY DOOR SURROUND LOWER HINGE CUT OUT. A TIME-LIMITED REPAIR DOUBLER W
- [SDR DL73K971141](https://openairdocs.org/sdr/DL73K971141.md): Power Supply · inoperative · Jun 15, 1997 · N319DL · Boeing 737232 · Emergency Lighting
  > FWD CABIN EMERGENCY LIGHTS STUCK ON AFTER TEST. REPLACED POWER SUPPLY.
- [SDR DL73K962792](https://openairdocs.org/sdr/DL73K962792.md): P6 Panel · tripped · Dec 31, 1996 · N319DL · Boeing 737232 · AC Generation System
  > BOTH GENRATORS WERE LOST AT FL310. ACCOMPLISHED LOSS OF BOTH GENERATORS CHECKLIST PER AOM. DIVERTED TO JFK, STIMATED LANDING WT 103,500 AND LANDING NORMAL. REPLACED G7 BUS PROTECTION PANEL AND R3 RELAY. RUN UP AND FUNCTIONAL CHECK GOOD.
- [SDR DL73K962355](https://openairdocs.org/sdr/DL73K962355.md): Charger · inoperative · Oct 18, 1996 · N319DL · Boeing 737232 · Emergency Lighting
  > FOUND ON L/O CHECK, EMERGENCY FLOOR TRACK LIGHTING HAS A SECTION INOP. REPLACED CHARGER ASSY, OPS CHECK NORMAL.
- [SDR DL73S953413](https://openairdocs.org/sdr/DL73S953413.md): Skin · damaged · Aug 15, 1995 · N319DL · Boeing 737232 · Rudder, Plate/Skin
  > RUDDER HAS TEMPORARY REPAIR ON UPPER RT SIDE SKIN. REPAIRED DAMAGE AS PER SRM 55-40-5 WITH REF TO 51-40-15.
- [SDR DL73S953409](https://openairdocs.org/sdr/DL73S953409.md): Skin · damaged · Aug 14, 1995 · N319DL · Boeing 737232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT FS 935 BETWEEN STR 21 AND 22, SUSTAINED PUNCTURE DAMAGE FROM GROUND EQUIPMENT. REPAIRED PER DL ERA 302319-14 AND SRM 53-10-3 FIG 1 FOR DAMAGE TO FS 935 FRAME.
- [SDR DL73S953056](https://openairdocs.org/sdr/DL73S953056.md): Anti-Ice Duct · cracked · Jul 11, 1995 · N319DL · Boeing 737232 · Engine Anti-Icing System
  > AFTER TAKEOFF, NR 2 OIL TEMP CLIMBED THROUGH YELLOW ZONE, ENGINE WAS SHUTDOWN WHEN TEMP WENT TO RED. RETURNED TO ATL. FOUND ENGINE ANTI-ICE DUCT CRACKED AND BLOWING HOT AIR ON FUEL HEAT VALVE. THE DUCT AND FUEL HEAT VALVE WERE REPLACED, OPERATION NORMAL.
- [SDR DL73S952862](https://openairdocs.org/sdr/DL73S952862.md): Gcu · failed · Jun 28, 1995 · N319DL · Boeing 737232 · AC Power Distribution System
  > DURING CRUISE, LOST NR 1 GENERATOR, GCU BREAKER TRIPPED. STARTED APU, UNABLE TO TRANSFER POWER, DIVERTED BOS. REPLACED NR 1 GCU AND NR 1 GEN BREAKER. OP CHECK NORMAL.
- [SDR DL73S952692](https://openairdocs.org/sdr/DL73S952692.md): Relay · failed · Jun 19, 1995 · N319DL · Boeing 737232 · Dependent Position Determining System
  > ON CLIMBOUT, LOST ALL FLT INSTRUMENTS ON LEFT SIDE, RETURNED TO CVG. FOUND NORMAL TRANSFER C/B TRIPPED. REPLACED R3 TRANSFER RELAY, OPERATION NORMAL.
- [SDR DL73S950481](https://openairdocs.org/sdr/DL73S950481.md): Floor Beam · cracked · Feb 1, 1995 · N319DL · Boeing 737232 · Fuselage Main, Floor Beam
  > DURING ROUTINE INSPECTION, THE BL 0.07 FLOORBEAM OF THE WING CENTER SECTION WAS FOUND CRACKED AT STA 657. THE UPPER CAP WAS COMPLETELY CRACKED, BUT NO CRACKS WERE FOUND IN THE WEB. PER B737 S/B 737-57-1210, THE CAP WILL BE REPAIRED.

## 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 = 'N319DL' AND deregistration_id = 'N319DL-2009-05-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N319DL-2009-05-13/reports

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