# N382DL: 1987 Boeing 737-247, registration cancelled 2006-02-17 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 17, 2006 - Exported to: Jordan - Status when cancelled: Valid registration - Airframe: [Boeing 737-247](https://openairdocs.org/model/boeing-737-247) (registry code 138448D) - Engine: [Pratt & Whitney JT8D-15](https://openairdocs.org/engine/pratt-whitney-jt8d-15) (registry code 52051) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 23609 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 18, 1987 - Certificate issued: October 6, 2005 - Last registry action: October 6, 2005 - Mode S code: A4630E - Owner when cancelled: [Jetglobal LLC](https://openairdocs.org/faa-owner/JETGLOBAL%20LLC) - Location: [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago) - Owner type: Corporation - Owner's area on the map: 41.8947° N, 87.6151° W: Placed by OpenAirDocs at the center of ZIP code 60611, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N382DL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=382DL - Page: https://openairdocs.org/deregistered/N382DL-2006-02-17 From the FAA registry file of October 31, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Boeing 737-247: https://openairdocs.org/model/boeing-737-247.md ## Service difficulty reports (29) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL73S050211](https://openairdocs.org/sdr/DL73S050211), Apr 8, 2005: BULKHEAD. CRACKED. 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 - [SDR DL73S040909](https://openairdocs.org/sdr/DL73S040909), Sep 23, 2004: BALLAST. ODOR. 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), Jun 26, 2004: SKIN. CRACKED. 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), Jan 13, 2004: SPAR. DAMAGED. 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), Aug 29, 2003: ADC. FAILED. 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 SECUR - [SDR DL73K030501](https://openairdocs.org/sdr/DL73K030501), Jun 1, 2003: TUBE. CRACKED. 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 B - [SDR DL73K030310](https://openairdocs.org/sdr/DL73K030310), Mar 29, 2003: DOOR FRAME. CRACKED. 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 ST - [SDR DL73K021229](https://openairdocs.org/sdr/DL73K021229), Oct 24, 2002: WIRE. BROKEN. RED TRACK LIGHTING INOP AT FWD COAT CLOSET, REPAIRED WIRE. - [SDR DL73K020636](https://openairdocs.org/sdr/DL73K020636), Jun 7, 2002: GARLOCK SEAL. LEAKING. 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 - [SDR DL73K020598](https://openairdocs.org/sdr/DL73K020598), May 28, 2002: BALLAST. FAILED. COCKPIT CENTER FLORESCENT LIGHTS INOP CA RPLD BALLAST, OP CKS GOOD. - [SDR DL73K011708](https://openairdocs.org/sdr/DL73K011708), Oct 23, 2001: STRUT. OVERSERVICED. 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 - [SDR DL73K011082](https://openairdocs.org/sdr/DL73K011082), Jun 27, 2001: SKIN. CORRODED. 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 ST - [SDR DL73K011081](https://openairdocs.org/sdr/DL73K011081), Jun 27, 2001: SKIN. CRACKED. 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 L - [SDR DL73K010812](https://openairdocs.org/sdr/DL73K010812), May 21, 2001: UNKNOWN. ODOR. 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 SM - [SDR DL73K001752](https://openairdocs.org/sdr/DL73K001752), Sep 11, 2000: POWER SUPPLY. INOPERATIVE. 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. REPL - [SDR DL73K001481](https://openairdocs.org/sdr/DL73K001481), Aug 4, 2000: LINE. RUPTURED. 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 - [SDR DL73K001170](https://openairdocs.org/sdr/DL73K001170), Jun 17, 2000: COALESCER BAG. DIRTY. 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), Aug 23, 1999: EPR INDICATOR. INOP. 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), Mar 12, 1999: CONTROLS. MALFUNCTIONED. 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 CO - [SDR DL73E990370](https://openairdocs.org/sdr/DL73E990370), Feb 22, 1999: SKIN. CRACKED. 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. - [SDR DL73E990369](https://openairdocs.org/sdr/DL73E990369), Feb 22, 1999: SKIN. CRACKED. 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 UNDERL - [SDR DL73E971308](https://openairdocs.org/sdr/DL73E971308), Jul 6, 1997: PROX SENSOR. OUT OF ADJUST. 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. RECYCLE - [SDR DL73E971226](https://openairdocs.org/sdr/DL73E971226), Jun 20, 1997: SKIN. GOUGED. 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 FA - [SDR DL73E971225](https://openairdocs.org/sdr/DL73E971225), Jun 20, 1997: SKIN. DENTED. 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 NOTE - [SDR DL73E971120](https://openairdocs.org/sdr/DL73E971120), Jun 3, 1997: TEE CAP. CORROSION. 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 - [SDR DL73E962197](https://openairdocs.org/sdr/DL73E962197), Sep 27, 1996: CHARGER. FAILED. 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 GO - [SDR DL73E962132](https://openairdocs.org/sdr/DL73E962132), Sep 13, 1996: BULKHEAD WEB. CRACKED. 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 V - [SDR DL73E960145](https://openairdocs.org/sdr/DL73E960145), Jan 21, 1996: SOCKET. BROKEN. 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), Feb 28, 1995: NOSE COWL. WORN. 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. ## FAA accident and incident reports (2) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20000617021739I](https://openairdocs.org/incident/20000617021739I), Jun 17, 2000: Boeing 737247 (N382DL), Kansas City, MO. (-23) On June 17, 2000, at approximately 0726 CDT, delta airlines express flight 2589, a Boeing 737-247, N382DL, departed Kansas City International Airport,… - [Incident 19890206017099I](https://openairdocs.org/incident/19890206017099I), Feb 6, 1989: Boeing 737247 (N382DL), Jacksonville, FL. Aircraft may have struck approach lights when it made a takeoff during a touch and go. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.