# N326DL: 1984 Boeing 737-232, registration cancelled 2008-11-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 18, 2008 - Exported to: Uganda - Status when cancelled: Valid registration - Airframe: [Boeing 737-232](https://openairdocs.org/model/boeing-737-232) (registry code 1384475) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 23098 - Year built: 1984 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: October 6, 1984 - Certificate issued: May 17, 2007 - Last registry action: May 17, 2007 - Mode S code: A384F0 - 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/N326DL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=326DL - Page: https://openairdocs.org/deregistered/N326DL-2008-11-18 From the FAA registry file of October 29, 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 737-232: https://openairdocs.org/model/boeing-737-232.md ## Service difficulty reports (46) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR KNN2008F00000](https://openairdocs.org/sdr/KNN2008F00000), Aug 22, 2008: BOLT. WORN. IN FLIGHT AGGRESSIVE VIBRATION FELT AT VARIOUS AIRSPEEDS 190 KTS-290 KTS, ALTITUDE STARTING AT 10,300 FT NOT RELENTING UNTIL WELL BELOW 190 KTS. (K) - [SDR KNNA20080003](https://openairdocs.org/sdr/KNNA20080003), Mar 8, 2008: ENGINE. FAILED. ACCORDING TO THE PILOT IN COMMAND’S REPORT, THEY HAD TO DEICE THE PLANE BEFORE TAKEOFF. THEN, ON TAKEOFF ROLL, DURING ROTATION, THERE WAS A LOUD BANG AND VIBRAT - [SDR KNNA200700068](https://openairdocs.org/sdr/KNNA200700068), Dec 10, 2007: SKIN. DAMAGED. WHILE PERFORMING AN A-7 CHECK, A LIGHTNING STRIKE WAS FOUND ON THE LT ELEVATOR AT THE OUTBOARD TRAILING EDGE LOWER SIDE, UNDER I/B STATIC WICK, SPECIAL INSPECTI - [SDR KNNA200700043](https://openairdocs.org/sdr/KNNA200700043), Nov 13, 2007: SLAT TRACK. JAMMED. AFTER TAKEOFF, LT LEADING EDGE SLAT DID NOT RETRACT, AIRCRAFT DIVERTED FROM KGNV TO KJAX. PILOT DECLARED IN FLIGHT EMERGENCY FOR FLAPS UP LANDING. AFTER REMOVAL - [SDR KNNA200700061](https://openairdocs.org/sdr/KNNA200700061), Nov 13, 2007: SLAT TRACK. JAMMED. AFTER TAKEOFF, LT LEADING EDGE SLAT DID NOT RETRACT, AIRCRAFT DIVERTED FROM KGNV TO KJAX. PILOT DECLARED IN FLIGHT EMERGENCY FOR FLAPS UP LANDING. AFTER REMOVAL - [SDR KNNA200700030](https://openairdocs.org/sdr/KNNA200700030), Apr 28, 2007: LEVER. BINDING. IN FLIGHT DURING DESCENT INTERMITTENTLY AT FIRST THEN STEADY PROCEDURES WERE FOLLOWED WITH THRUST LEVERS BINDING (RESTRICTED) ENGINE 1 WAS SHUTDOWN IAW CHECK LI - [SDR KNNA200700022](https://openairdocs.org/sdr/KNNA200700022), Mar 14, 2007: FLOORBEAM. CORRODED. FLOOR PANEL ATTACH POINT STA 344, LBL 12 IS CORRODED. PROVIDE INSTRUCTIONS ON REPAIR OF STA 344, LBL 12 FLOOR PANEL ATTACH POINT. REMOVED AND REPLACED FLOORBEAM - [SDR KNNA200700026](https://openairdocs.org/sdr/KNNA200700026), Mar 11, 2007: FRAME. DAMAGED. AFT CARGO PIT, INTERIOR BILGE B-STA 867 BETWEEN STR 27 R AND STR 28 L FRAME BOTTOM SIDE, CORRODED. PROVIDE INSTRUCTIONS ON REPAIR OF CORROSION AFT CARGO PIT, IN - [SDR KNNA200700025](https://openairdocs.org/sdr/KNNA200700025), Mar 11, 2007: SKIN. CORRODED. AFT CARGO PIT INTERIOR BILGE, BS 927 BETWEEN STR-27L STR AND 27R, FRAME BOTTOM SIDE CORRODED. PROVIDE INSTRUCTIONS ON REPAIR OF CORROSION AFT CARGO PIT, INTERIO - [SDR KNNA200700024](https://openairdocs.org/sdr/KNNA200700024), Mar 9, 2007: SKIN. CORRODED. CORRODED SKIN AT BS 500A+ 10' BETWEEN STR 27L/28L. PROVIDE INSTRUCTION ON REPAIR OF CORRODED EXTERIOR SKIN STA 500A + 10' STR 27L/28L. - [SDR KNNA200700021](https://openairdocs.org/sdr/KNNA200700021), Mar 9, 2007: FLOORBEAM. CRACKED. CARGO FLOORBEAM CRACKED AT BS 460, RBBL 14.5 FWD CARGO COMPARTMENT. PROVIDE INSTRUCTIONS ON REPAIR OF CARGO FLOORBEAM BS 460 RBL 14.5. REMOVED AND REPLACED CARG - [SDR KNNA200700020](https://openairdocs.org/sdr/KNNA200700020), Mar 4, 2007: SKIN. DAMAGED. MAIN ENTRY DOOR L-2 EXTERIOR SURFACE, UPPER AFT CORNER, SKIN BEND. PROVIDE INSTRUCTIONS ON REPAIR OF DOOR SKIN. CUT OUT BEND CORNER AND REPAIR PER SRM 52-00-3 F - [SDR KNNA200700023](https://openairdocs.org/sdr/KNNA200700023), Mar 1, 2007: SKIN. CORRODED. FUSELAGE, EXTERNAL SURFACE LOWER LOBE, B-STA 968, STR 27 L CORRODED. PROVIDE INSTRUCTIONS ON REPAIR OF FUSELAGE EXTERNAL SURFACE LOWER LOBE BS 968 STR 27 L. BOE - [SDR DL73S060329](https://openairdocs.org/sdr/DL73S060329), Dec 20, 2005: SKIN. CRACKED. THE FUSELAGE SKIN AT THE AFT ENTRY DOOR UPPER HINGE CUTOUT HAS A .7500 IN. CRACK AT THE UPPER CORNER. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INST - [SDR DL73S050728](https://openairdocs.org/sdr/DL73S050728), Nov 18, 2005: SKIN. DEFORMED. THE FUSELAGE SKIN WAS FOUND WITH AN OIL CAN CONDITION FROM BS 747-767 BELOW S-18R. INSTALLED DOUBLER PER ER/A 451596-14AD. REF AD 2005-13-30 & 2004-18-06. - [SDR DL73S050718](https://openairdocs.org/sdr/DL73S050718), Nov 16, 2005: SKIN. CRACKED. FUSELAGE SKIN WAS FOUND CRACKED AT BS 932, S-21R, CRACK IS 3 INCHES LONG. DOUBLER INSTALLED, REF AD 2004-18-06 & 2005-13-30. - [SDR DL73S050712](https://openairdocs.org/sdr/DL73S050712), Nov 14, 2005: FLOORBEAM. CRACKED. THE OVERWING FLOORBEAM AT LBL 24.8 WAS FOUND CRACKED. INSPECTED PER ER/A 451613-14AD. REF AD 2001-17-18, SI 03-056673-12AD, ER/A 369397-14. - [SDR DL73S050711](https://openairdocs.org/sdr/DL73S050711), Nov 14, 2005: FLOORBEAM. CRACKED. CRACKS WERE FOUND IN THE OVERWING FLOORBEAMS AT RBL 24.8. INSTALLED REPAIR DOUBLERS AND CHANNEL PER ER/A 451614-14AD. REF AD 2001-17-18, AD 93-17-08, AD 90-06-0 - [SDR DL73S050710](https://openairdocs.org/sdr/DL73S050710), Nov 14, 2005: SKIN. CRACKED. CRACK WAS FOUND IN THE FUSELAGE SKIN AT BS 540 AND JUST BELOW LAP SPLICE AT S-14L. INSTALLED DOUBLER PER ER/A 451595-14AD AND SRM 53-30-3. REF AD 2004-18-06. - [SDR DL73S041055](https://openairdocs.org/sdr/DL73S041055), Nov 20, 2004: SKIN. CRACKED. A 1.5 INCH CRACK WAS FOUND IN THE SKIN RUNNING ALONG THE BONDED DOUBLER MILL LINE JUST BELOW STRINGER 18L AT FS 727B. THE CRACK WAS REMOVED WITH A CUTOUT AND RE - [SDR DL73S040902](https://openairdocs.org/sdr/DL73S040902), Sep 19, 2004: SHUTOFF VALVE. MALFUNCTIONED. AFTER PUSHBACK ENGINE START, NR 2 ENGINE HAD A FLAME OUT OCCUR. DISCOVERED THAT THE NR 2 ENGINE FUEL SHUTOFF VALVE WAS AT FAULT. PART REPLACED BY TPA MTC AND EN - [SDR DL73S031131](https://openairdocs.org/sdr/DL73S031131), Dec 24, 2003: ATTACH FITTING. CORRODED. CORROSION WAS NOTED DURING INSPECTION OF THE HORIZ STAB ATTACH LUGS PER 03-069697-03 AND 03-053025-03AD. THE RIGHT SIDE OUTBOARD HORIZ STAB REAR SPAR UPPER ATTA - [SDR DL73S031129](https://openairdocs.org/sdr/DL73S031129), Dec 23, 2003: SKIN. DAMAGED. DAMAGED FASTENER HOLES WERE REPORTED DURING PERMANENT REPAIR ACCOMPLISHMENT TO THE R2 DOOR UPPER HINGE CUTOUT. AREA WAS REWORKED/REPAIRED PER ERA 360517-14, REV - [SDR DL73S031128](https://openairdocs.org/sdr/DL73S031128), Dec 23, 2003: SKIN. DENTED. A DENT WAS FOUND ABOVE S19L NEAR THE LWR AFT CORNER OF THE DOOR LOCATED NEAR BS 985. DAMAGE WAS REMOVED AND REPAIRED PER ERA 385887-14. - [SDR DL73S031127](https://openairdocs.org/sdr/DL73S031127), Dec 23, 2003: FRAME. DENTED. A DENT WAS FOUND IN THE INNER CHORD OF THE BS 767 FRAME JUST ABOVE S24L. DENT WAS REMOVED AND REPAIRED PER ERA 385960-14. - [SDR DL73S031126](https://openairdocs.org/sdr/DL73S031126), Dec 23, 2003: CLEVIS. CORRODED. CORROSION DAMAGE FOUND WHICH EXCEEDED LIMITS COVERED IN 03-085220-03. CORROSION WAS FOUND IN THE NR 6 AND NR 12 BODY CLEVIS LUGS. CORROSION WAS REMOVED AND REWO - [SDR DL73S031123](https://openairdocs.org/sdr/DL73S031123), Dec 22, 2003: SKIN. CRACKED. CRACK DAMAGE WAS NOTED ON THE KEEL BEAM LOWER SKIN PANEL. SKIN PANEL WAS REPLACED PER ERA 385927-14. - [SDR DL73S031099](https://openairdocs.org/sdr/DL73S031099), Dec 16, 2003: SKIN. CORRODED. THE FUSELAGE SKIN WAS FOUND CORRODED AT THE FWD INBD CORNER OF THE AFT LAV SERVICE DOOR CUTOUT NEAR FS 987 AND STRINGER 27R. THE DAMAGE WAS REMOVED WITH A 4 X 4 - [SDR DL73S031089](https://openairdocs.org/sdr/DL73S031089), Dec 15, 2003: BULKHEAD. CORRODED. CORROSION WAS FOUND ON THE AFT PRESSURE BULKHEAD AT BS 1016 AND BL 0, BETWEEN S26L AND 26R. CORROSION WAS REMOVED THEN REPAIRED PER ERA 385921-14AD. - [SDR DL73S031078](https://openairdocs.org/sdr/DL73S031078), Dec 12, 2003: SKIN. DENTED. DENTS WERE NOTED IN THE SKIN PANEL AT APPROXIMATELY BS 380 AND BETWEEN S15L AND S18L. DENTS WERE CUTOUT AND REPAIRED PER ERA 385947-14. - [SDR DL73K010217](https://openairdocs.org/sdr/DL73K010217), Feb 6, 2001: SKIN. CRACKED. THE SKIN AND UNDERLYING BEARSTRAP OF THE L2 DOOR CUTOUT WERE FOUND CRACK AT THE LOWER HINGE CUTOUT. CRACK REMOVAL RESULTED IN A 2 INCH X 2 INCH CUTOUT IN SKIN A - [SDR DL73K010216](https://openairdocs.org/sdr/DL73K010216), Feb 6, 2001: SKIN. CRACKED. A 3 INCH LONG CRACK WAS FOUND IN THE SKIN JUST BELOW STRINGER 18R AT FS 749. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN ALUMINUM EXTERNAL DOUBLER - [SDR DL73K010200](https://openairdocs.org/sdr/DL73K010200), Feb 5, 2001: SKIN. CRACKED. FOUND ON T1 LETTER CK, COCKPIT WINDOW POST IS CRACKED AT THE UPPER OUTBD CORNER OF THE CAPTS WINDSHIELD. REPAIRED PER SRM 53-30-3. - [SDR DL73K002013](https://openairdocs.org/sdr/DL73K002013), Oct 13, 2000: ENGINE. INOPERATIVE. OIL FILTER BYPASS LIGHT ON AFTER TAKEOFF. NR 1 ENG SHUT DOWN. RETURNED TO MCI. OIL PRESSURE WAS NORMAL WHILE ENGINE RUNNING. ENGINE WINDMILLED ABOUT 30 MIN. MET - [SDR DL73K001848](https://openairdocs.org/sdr/DL73K001848), Sep 23, 2000: WINDOW. SHORTED. AIRTURN BACK DUE TO UNIDENTIFIED ODOR IN COCKPIT. FOUND TERMINAL AND WIRE ON R2 SLIDING WINDOW OVERHEATED. REPLACED TERMINALS, WINDOW AND CONTROLLER. LEAKS CHEC - [SDR DL73K001847](https://openairdocs.org/sdr/DL73K001847), Sep 22, 2000: VALVE. STUCK. ACRID ODOR IN COCKPIT DURING DESCENT, COULD NOT IDENTIFY SOURCE BUT VERIFIED BY ALL CREW MEMBERS DID NOT AFFECT CABIN AIR. ON GROUND AT GATE F/A REPORTS ODOR IN - [SDR DL73K001489](https://openairdocs.org/sdr/DL73K001489), Aug 6, 2000: LIGHT. DAMAGED. SEAT 01D EMERGENCY LIGHT RIPPED OFF. REPLACED SAME, OPS NORMAL. - [SDR DL73K992301](https://openairdocs.org/sdr/DL73K992301), Oct 19, 1999: BATTERY. DISCHARGED. ON L/O, FOUND AFT SECTION EMERGENCY LIGHTS INOP ROWS 17 TO 20 INCLUDING RT SIDE GALLEY. FOUND BATTERY AT MODULE M9222 INOP. REPLACED BATTERY, EMERGENCY LIGHTS O - [SDR DL73K991176](https://openairdocs.org/sdr/DL73K991176), May 25, 1999: CONNECTOR. CHAFED. DURING CLIMBOUT HAD RAPID FLICKERING OF LT WING BODY OVERHEAT LIGHT. TURNED OFF LEFT BLEED, LIGHT STILL ON. PULLED BACK THROTTLE LIGHT EXTINGUISHED. RETURNED TO - [SDR DL73K980450](https://openairdocs.org/sdr/DL73K980450), Feb 23, 1998: INTERCOSTAL. CRACKED. DURING INSPECTION PER SI3-55852-12AD, THE R1 DOOR AFT FRAME INTERCOSTALS BETWEEN FS 332 AND 344 WERE FOUND CRACKED AT TWO LOCATIONS, AT STG 8A AND 11. REPAIRED - [SDR DL73K971714](https://openairdocs.org/sdr/DL73K971714), Aug 31, 1997: BATTERY. DISCHARGED. ON INSPECTION, FOUND EMERGENCY TRACK LIGHTING INOP SEATS 5 TO 9. REPLACED BATTERY AND RACK ASSY, CKS NORMAL. - [SDR DL73S961074](https://openairdocs.org/sdr/DL73S961074), May 4, 1996: OVEN. FAILED. AIRCRAFT RETURNED WITH LOG BOOK IRREG STRONG ODOR BEHIND PILOT SEATS BETWEEN C/B PANEL. THEN SMOKE FROM FORWARD GALLEY VENT AND OVENS. CORRECTIVE ACTION: FOUND - [SDR DL73S960510](https://openairdocs.org/sdr/DL73S960510), Mar 3, 1996: BLKHD WEB. CRACKED. DURING ACCOMPLISHMENT OF S.I. 3-69482-12, A 1 INCH CRACK WAS FOUND IN THE RADIUS OF THE VERTICAL CHORD OF THE LBL 5.7 VERTICAL STIFFENER AT BS 178. THE BULKHEAD - [SDR DL73S954360](https://openairdocs.org/sdr/DL73S954360), Nov 12, 1995: MEGAPHONE. FAILED. ON 7802L, FOUND F/C GALLEY MEGAPHONE WOULD NOT PROJECT VOICE WHEN THE BUTTON ON THE HANDLE WAS PUSHED. TRIED CHANGING THE BATTERIES, NO HELP. REPLACED MEGAPHONE - [SDR DL73S953678](https://openairdocs.org/sdr/DL73S953678), Sep 6, 1995: ACTUATOR. CRACKED. DURING APPROACH, LOST A-SYSTEM HYDRAULIC QTY AND PRESS. FOUND NR 1 SPOILER ACTUATOR CRACKED. REPLACED ACTUATOR, AS PRECAUTION REPLACED PUMP AND FILTER AND OPERA - [SDR DL73S952588](https://openairdocs.org/sdr/DL73S952588), Jun 1, 1995: FLOORBEAM. CRACKED. DURING LAY OVER, INSPECTION FOUND THE FLOORBEAM AT BL 0.07 OF THE WING CENTER SECTION CRACKED AT STA 661. IN ACCORDANCE WITH BAC S/B 737-57-1210, THE CRACKS ARE ## 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 20080308011619I](https://openairdocs.org/incident/20080308011619I), Mar 8, 2008: Boeing 737232 (N326DL), Pittsburgh, PA, Minor damage. (-23) During rotation, the number 1 engine developed a vibration. The engine was shut down eventually. The aircraft returned and landed at pit runway 28L and… - [Incident 20001013029239I](https://openairdocs.org/incident/20001013029239I), Oct 13, 2000: Boeing 737232 (N326DL), Kansas City, MO. (-23)On October 13, 2000, at approximately 0700 CDT, delta airlines flight 2589, a Boeing 737, N326DL, left Kansas City International Airport, Kansas City, MO… --- 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.