# Service difficulty reports: N382DL, cancelled Feb 17, 2006

A list on [N382DL, cancelled Feb 17, 2006](https://openairdocs.org/deregistered/N382DL-2006-02-17.md).

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

- [SDR DL73S050211](https://openairdocs.org/sdr/DL73S050211.md): Bulkhead · cracked · Apr 8, 2005 · N382DL · Boeing 737247 · Fuselage Main, Bulkhead
  > THE AFT PRESSURE P-DOME WEB WAS FOUND WITH CRACKS AS FASTENER HOLES COMMON TO THE Y-CHORD AT STRINGER 6L. THE CRACKS ARE TYPICAL OF AD 99-08-23. THE CRACKS WERE REMOVED WITH A CUTOUT AND REPAIRED WITH ALUMINUM DOUBLERS PER B737 SRM AND PER ER/A 097892-14AD.
- [SDR DL73S040909](https://openairdocs.org/sdr/DL73S040909.md): Ballast · odor · Sep 23, 2004 · N382DL · Boeing 737247 · Passenger Compartment Lighting
  > FLT ATTENDANT IN AFT GALLEY REPORTED ELECTRIC SMELL JUST PRIOR TO PUSHBACK. FOUND BALLAST IN AFT CABIN HOT. REPLACED SAME.
- [SDR DL73S040605](https://openairdocs.org/sdr/DL73S040605.md): Skin · cracked · Jun 26, 2004 · N382DL · Boeing 737247 · Fuselage Main, Plate/Skin
  > ER/A 091431-14, CRACK FOUND IN FUSELAGE SKIN AT APPROX FS 520 JUST ABOVE STRINGER 16L. CRACK IS APPROX.5 INCH LONG.
- [SDR DL73S040033](https://openairdocs.org/sdr/DL73S040033.md): Spar · damaged · Jan 13, 2004 · N382DL · Boeing 737247 · Elevator, Spar/Rib
  > RIGHT ELEVATOR REAR SPAR FOUND DAMAGED AT OUTBOARD END. REPAIR ACCOMPLISHED FROM ELEV STA 88 TO OUTBOARD END PER ER/A 426886-14.
- [SDR DL73S030794](https://openairdocs.org/sdr/DL73S030794.md): Adc · failed · Aug 29, 2003 · N382DL · Boeing 737247 · Air Data Computer
  > ON T/O LOST BOTH CAPT AND F/O AIRSPEED AND ALTIMETER. CAPTS FROZE, NO FLAGS. F/O HAD FLAGS IN VIEW. FOUND HOSES OFF NR 1 ADC. RECONNECTED HOSES, BOTH WERE SECURE. PERFORMED TEST ON ADC CHECKS OK. F/O ADC HAD FAILED. REPLACED SAME, TEST OK.
- [SDR DL73K030501](https://openairdocs.org/sdr/DL73K030501.md): Tube · cracked · Jun 1, 2003 · N382DL · Boeing 737247 · Hydraulic System, Main
  > SLOW LEAK IN FLT RESULTED IN A-SYSTEM RESERVOIR GOING TO ZERO AND SUBSEQUENT LOW PRESSURE LIGHTS ILLUMINATED. FOUND NR 1 ENG TO PYLON PRESSURE LINE CRACKED AT BEND. REPLACED HYD LINE. RAN ENGINES/FLIGHT CONTROLS, NO FURTHER LEAKS NOTED.
- [SDR DL73K030310](https://openairdocs.org/sdr/DL73K030310.md): Door Frame · cracked · Mar 29, 2003 · N382DL · Boeing 737247 · Fuselage Main, Structure
  > THE UPPER STUB SECTION OF THE R1 DOOR OPENING FWD FRAME WAS FOUND WITH A 1.1 INCH CRACK IN THE BEND RADIUS EMANATING FROM THE FRAME CUTOUT FOR THE UPPER DOOR STOP FITTING. THE CRACK WAS REMOVED WITH A TRIM OUT AND REPAIRED WITH AN ALUMINUM REPAIR ANGLE PER ER
- [SDR DL73K021229](https://openairdocs.org/sdr/DL73K021229.md): Wire · broken · Oct 24, 2002 · N382DL · Boeing 737247 · Light System Wiring
  > RED TRACK LIGHTING INOP AT FWD COAT CLOSET, REPAIRED WIRE.
- [SDR DL73K020636](https://openairdocs.org/sdr/DL73K020636.md): Garlock Seal · leaking · Jun 7, 2002 · N382DL · Boeing 737247 · Turbine Engine Oil System
  > NR 1 ENG OIL QTY SHOWED A STEADY DECREASE AS FLIGHT PROGRESSED. ULTIMATELY QUANTITY WENT TO ZERO INDICATION. OIL TEMP AND PRESSURE REMAINED STEADY IN THE NORMAL RANGE AT ALL TIMES. FOUND NR 1 ENG GARLOCK SEAL AT STARTER LEAKING. REPLACED STARTER GARLOCK S
- [SDR DL73K020598](https://openairdocs.org/sdr/DL73K020598.md): Ballast · failed · May 28, 2002 · N382DL · Boeing 737247 · Flight Compartment Lighting
  > COCKPIT CENTER FLORESCENT LIGHTS INOP CA RPLD BALLAST, OP CKS GOOD.
- [SDR DL73K011708](https://openairdocs.org/sdr/DL73K011708.md): Strut · overserviced · Oct 23, 2001 · N382DL · Boeing 737247 · Nose/Tail Landing Gear Attach Section
  > ON TAXI IN, THE MASTER CAUTION LIGHT AND THE STALL WARNING AND ISOLATION LIGHTS ON THE OVERHEAD PANEL WERE FLICKERING ON AND OFF. HEARD CIRCUITS POPPING ON AND OFF ON THE C/B PANEL. SMELLED OZONE/BURNING SMELL ON THE TAXI IN. FOUND NOSE STRUT OVERSERVICED.
- [SDR DL73K011082](https://openairdocs.org/sdr/DL73K011082.md): Skin · corroded · Jun 27, 2001 · N382DL · Boeing 737247 · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN / FS 837 / STRG. 27R / ANTENNA CUTOUT: CORROSION REPAIR THE FUSELAGE SKIN WAS FOUND CORRODED AT AN EXISTING ANTENNA CUTOUT AT FS 837 BETWEEN STRINGERS 26R & 27R. THE CUTOUT REINFORCING DOUBLER
- [SDR DL73K011081](https://openairdocs.org/sdr/DL73K011081.md): Skin · cracked · Jun 27, 2001 · N382DL · Boeing 737247 · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN ASSY / C1 DOOR CUTOUT / FS 492 / STRG. 25R:CRACK REPAIR THE FUSELAGE SKIN AND UNDERLYING BEARSTRAP WERE FOUND CRACKED AT AN EXISTING FASTENER LOCATION COMMON TO THE FS 492 FRAME BELOW STRI
- [SDR DL73K010812](https://openairdocs.org/sdr/DL73K010812.md): Unknown · odor · May 21, 2001 · N382DL · Boeing 737247 · Air Distribution System
  > AFTER NR 2 ENG GEN PUT ON LINE XFER BUSS NR 1 DID NOT TAKE POWER. RECYCLED BUSS XFER SWITCH, OPS NORMAL. NR 2 FUEL HEAT LIGHT WOULD BLINK PERIODICALLY. AT V1 SMELLED ELECTRICAL BURNING ODOR. THE FLIGHT ATTENDANTS CONFIRMED THE ODOR. RAN BOTH ENGS, ALL POW
- [SDR DL73K001752](https://openairdocs.org/sdr/DL73K001752.md): Power Supply · inoperative · Sep 11, 2000 · N382DL · Boeing 737247 · Engine Fuel Indicating System
  > CLIMBING OUT BOTH F/F GAUGES WENT TO ZERO. LT STAYED AT -0- RT FLUX BETWEEN -0- AND 1000. ON DESCENT BOTH WORKED NORMAL THEN LT FAILED AGAIN AFTER LANDING. REPLACED F/F POWER SUPPLY, OPN CKS NORMAL.
- [SDR DL73K001481](https://openairdocs.org/sdr/DL73K001481.md): Line · ruptured · Aug 4, 2000 · N382DL · Boeing 737247 · Hydraulic System, Main
  > AFTER GEAR RETRACTION EXPERIENCED SYSTEM A HYDRAULIC QTY LOSS. RAN PUMPS A SYSTEM FOR 5 MINUTES BEFORE TURNING OFF PER CHECKLIST. FOUND RT FLEX HYD LINE HOSE TO THE RETRACT LANDING GEAR ACT LEAKING. REPLACED PRESS AND RETURN LINE. SIMULATED GEAR RETRACTION
- [SDR DL73K001170](https://openairdocs.org/sdr/DL73K001170.md): Coalescer Bag · dirty · Jun 17, 2000 · N382DL · Boeing 737247 · Humidity Control System
  > CREW REPORTED ODOR IN CABIN. REPLACED LT AND RT WATER BAGS. RAN BOTH PACKS ON APU AND ENG BLDAIR. INSP PACK INTAKES, NO TROUBLE FOUND.
- [SDR DL73E991888](https://openairdocs.org/sdr/DL73E991888.md): Epr Indicator · inop · Aug 23, 1999 · N382DL · Boeing 737247 · Engine Pressure Ratio (EPR)
  > NR 1 EPR IND DID NOT INDICATE ON TAKEOFF ROLL. EPR GAUGE DID INDICATE ON ENG RUN AFTER ABORTED TAKEOFF. REPLACED NR 1 EPR INDICATOR.
- [SDR DL73E990526](https://openairdocs.org/sdr/DL73E990526.md): Controls · malfunctioned · Mar 12, 1999 · N382DL · Boeing 737247 · Rudder Control System
  > ACFT EXPERIENCED RT RUDDER DISPLACEMENT FOR APPROX 2 SEC. RUDDER PEDALS DID NOT MOVE FROM NEUTRAL, A A/P ENGAGED. REMOVED MAIN PCU, STANDBY PCU, AND YAW DAMP COUPLER FOR TEST AND INSPECTION.
- [SDR DL73E990370](https://openairdocs.org/sdr/DL73E990370.md): Skin · cracked · Feb 22, 1999 · N382DL · Boeing 737247 · Fuselage Main, Plate/Skin
  > THE UPPER HINGE CUTOUT OF THE AFT GALLEY DOOR CUTOUT (R2) WAS FOUND WITH A.26 CRACK IN THE SKIN AND BONDED DOUBLER. THE UNDERLYING BEAR STRAP WAS NOT DAMAGED. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXTERNAL DOUBLER PER B737 SRM 53-30-3, FIG 21A. E
- [SDR DL73E990369](https://openairdocs.org/sdr/DL73E990369.md): Skin · cracked · Feb 22, 1999 · N382DL · Boeing 737247 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN AND BONDED DOUBLER WERE FOUND WITH A.68 CRACK AT THE LOWER FWD CORNER OF THE AFT GALLEY DOOR CUTOUT. THE CRACK DID NOT EXTEND INTO THE UNDERLYING BEAR STRAP. THE CRACK WAS ROUTED OUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL DOUBLER AND TR
- [SDR DL73E971308](https://openairdocs.org/sdr/DL73E971308.md): Prox Sensor · out of adjust · Jul 6, 1997 · N382DL · Boeing 737247 · Landing Gear Position and Warning
  > UPON GEAR EXT, THE NOSE GEAR DOWN GREEN LIGHT FAILED TO ILLUMINATE. RED LIGHTS NML DURING EXT AND REMAINED OUT AFTER GEAR EXT. REQUIRED MISSED APPROACH. RECYCLED GEAR AND GOT NML INDICATIONS ON EXT. CHECKED NOSE GEAR THROUGH VIEWER APPROACH AND LANDING NML
- [SDR DL73E971226](https://openairdocs.org/sdr/DL73E971226.md): Skin · gouged · Jun 20, 1997 · N382DL · Boeing 737247 · Fuselage Main, Plate/Skin
  > A GOUGE WAS FOUND IN THE SKIN AT STA 1088 BETWEEN STR 8 AND 9R. THE DAMAGE WAS TRIMMED OUT AND REPAIRED WITH AN INTERNAL DOUBLER. THIS REPAIR WAS APPROVED BY FAA/DER FORM 8110-3, DER DESIGNATION SO-889, DATED 06-19-97.
- [SDR DL73E971225](https://openairdocs.org/sdr/DL73E971225.md): Skin · dented · Jun 20, 1997 · N382DL · Boeing 737247 · Fuselage Main, Plate/Skin
  > A 4 BY 9 BY.173 DENT AT STA 1006 BETWEEN STR 13R AND 14R. THE DENT IS LOCATED AT A LAP SPLICE. THE DENT WAS REPAIRED PER B737 SRM 53-30-3, FIGURE 9. IT IS NOTED THAT THE UPPER ROW OF FASTENERS IN THE UPPER ROW OF THE LAP SPLICE WOULD NOT MAINTAIN 2D EDGE M
- [SDR DL73E971120](https://openairdocs.org/sdr/DL73E971120.md): Tee Cap · corrosion · Jun 3, 1997 · N382DL · Boeing 737247 · Fuselage Miscellaneous Structure
  > CORROSION ON UPPER SURFACE OF FS 312 FLOOR. REMOVED LIGHT SURFACE CORROSION PER SRM 51-10-6. REMOVED DAMAGED SECTION OF TEE CAP. FABRICATED REPLACEMENT SECTION PER M/M 53-21-0. INSTALLED REPAIR FROM LBL 25 TO RBL53 PER M/M 53-21-0 COMPLETED INSTALLATION OF
- [SDR DL73E962197](https://openairdocs.org/sdr/DL73E962197.md): Charger · failed · Sep 27, 1996 · N382DL · Boeing 737247 · Emergency Lighting
  > DURING L/O CHECK, FOUND EMERGENCY TRACK LIGHTING SECTION INOP FROM ROWS 10 TO 16. REPLACED AFT EMERGENCY LIGHT BATTERY CHARGER POWER SUPPLY, OPERATION CHECKS GOOD.
- [SDR DL73E962132](https://openairdocs.org/sdr/DL73E962132.md): Bulkhead Web · cracked · Sep 13, 1996 · N382DL · Boeing 737247 · Fuselage Main, Bulkhead
  > DURING ACCOMPLISHMENT OF SI 3-69482-12, TWO CRACKS WERE DISCOVERED ON THE FORWARD FACE OF THE FS 178 BULKHEAD WEB. THE FIRST CRACK IS LOCATED NEAR THE RBL 5.7 VERTICAL STRAP AT APPROXIMATELY WL 202. THE SECOND IS LOCATED NEAR THE LBL 5.7 VERTICAL STRAP AT AP
- [SDR DL73E960145](https://openairdocs.org/sdr/DL73E960145.md): Socket · broken · Jan 21, 1996 · N382DL · Boeing 737247 · Emergency Lighting
  > EMERGENCY FLOOR LIGHT AT ROW 2 IS INOP. REPLACED SOCKET, DL (P/N 337201959), (MFG 08169-1), OPS GOOD.
- [SDR DL73E951125](https://openairdocs.org/sdr/DL73E951125.md): Nose Cowl · worn · Feb 28, 1995 · N382DL · Boeing 737247 · Engine Cowling System
  > AFT BULKHEAD DOOR FRAME LIP WORN AT 7 O'CLOCK POSITION. REPAIRED PER SRM 54-10-3. FOR NR 2 ENGINE INTAKE COWL, DAMAGE FOUND AT SHOP INSPECTION.

## 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 = 'N382DL' AND deregistration_id = 'N382DL-2006-02-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N382DL-2006-02-17/reports

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