# N328DL: 1984 Boeing 737-232, registration cancelled 2006-10-17 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 17, 2006 - Exported to: Russia - Status when cancelled: Valid registration - Airframe: [Boeing 737-232](https://openairdocs.org/model/boeing-737-232) (registry code 1384475) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 23100 - Year built: 1984 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: September 7, 1984 - Certificate issued: February 7, 2006 - Last registry action: February 7, 2006 - Mode S code: A38C5E - 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/N328DL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=328DL - Page: https://openairdocs.org/deregistered/N328DL-2006-10-17 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 (36) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DL73K011534](https://openairdocs.org/sdr/DL73K011534), Sep 15, 2001: BALLAST. DEFECTIVE. WHILE AT GATE WAITING FOR MTC ON A/C BLACK/GRAY SMOKE POURED OUT OF P18-1 PANEL. FLT CREW SHUT DOWN A/C POWER. FOUND BALLAST FOR FWD LAV MIRROR TO BE SOURCE OF - [SDR DL73K011385](https://openairdocs.org/sdr/DL73K011385), Aug 22, 2001: COOLER. UNSERVICEABLE. ENGINE OIL SYSTEM CONTAMINATED WITH FUEL. REPLACED FUEL OIL COOLER DL P/N 794001307 S/N 398 - [SDR DL73K010979](https://openairdocs.org/sdr/DL73K010979), Jun 15, 2001: KEELBEAM. CRACKED. THE RT STRINGER 18A SHEAR BEAM AT FS 727 WAS FOUND WITH A 2 INCH CRACK. THE CRACK IS SIMILAR TO BAC S/B 737-53-1170, EXCEPT THE SB IS NOT EFFECTIVE FOR THIS AIR - [SDR DL73K000962](https://openairdocs.org/sdr/DL73K000962), May 15, 2000: BATTERY. FAILED. AFT UPPER EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY. - [SDR DL73K000333](https://openairdocs.org/sdr/DL73K000333), Feb 18, 2000: SKIN. CRACKED. A 2 INCH LONG CRACK WAS FOUND IN THE SKIN, BONDED DOUBLER, AND BEAR STRAP OF THE AFT ENTRY DOOR (L2) CUTOUT AT THE UPPER AFT CORNER. THE CRACK WAS ROUTED OUT OF - [SDR DL73K000328](https://openairdocs.org/sdr/DL73K000328), Feb 17, 2000: SKIN. CRACKED. A CRACK WAS FOUND IN THE SKIN, BONDED DOUBLER, AND BEAR STRAP OF THE AFT ENTRY DOOR (L2) CUTOUT AT THE UPPER FWD CORNER. THE CRACK WAS ROUTED OUT OF ALL THREE M - [SDR DL73K000217](https://openairdocs.org/sdr/DL73K000217), Jan 29, 2000: WIRE. CHAFED. REPAIRED SHORTED WIRE W448-001-20 PER WD 26-12-01. REPLACED LOOP CONNECTOR D858. ALL OPERATIONAL CHECKS NORMAL. LEFT WING BODY OVERHEAT. - [SDR DL73K991234](https://openairdocs.org/sdr/DL73K991234), Jun 1, 1999: SKIN. CHAFED. NR 3 FOREFLAP CHAFING AND WORN THROUGH AT UPPER SURFACE I/B END. REPAIRED PER SRM 51-40-6, OPS CHECK OK. - [SDR DL73S981844](https://openairdocs.org/sdr/DL73S981844), Sep 6, 1998: BOLT. MISSING. APU FIRE WARNING WHILE ON APPROACH. FOLLOWED CHECKLIST. FIRED BOTTLE, FIRE WARNING EXTINGUISHED. FOUND BOLT MISSING FROM FUEL ATOMIZER CAUSING HEAT TO REACH FIR - [SDR DL73S981252](https://openairdocs.org/sdr/DL73S981252), Jun 13, 1998: TIRE. FAILED. AT 120 KT ON TAKEOFF, SEVERE NOSEWHEEL SHIMMY AND LOUD THUMP UNDER COCKPIT. AIRSPEED STAGNATED THROTTLES FIREWALLED; EGT RED LINED AT 635 BOTH ENGINES FOR ABOUT - [SDR DL73S981176](https://openairdocs.org/sdr/DL73S981176), Jun 1, 1998: TRANSMITTER. FAILED. HYD QTY GAUGE F/O INST PANEL A-SYS QTY GAUGE INDICATES DECREASING FLUID LEVEL BEGAN AT 3.5 NOW AT 1.75. PERFORMED WALKAROUND OF A/C CKED ALL FLT. CONTROLS AND L - [SDR DL73S980856](https://openairdocs.org/sdr/DL73S980856), Apr 20, 1998: BATTERY PACK. DISCHARGED. ON TEST L2 DOOR EXTERIOR EMERGENCY LIGHT WOULD NOT TEST. REPLACED BATTERY PACK POWER SUPPLY. - [SDR DL73S980340](https://openairdocs.org/sdr/DL73S980340), Feb 9, 1998: FITTING. CRACKED. DURING INSPECTION PER SI3-66022-12, THE RT MLG BEAM AFT SUPPORT FITTING ON THE REAR SPAR WAS FOUND WITH CRACKS. THE CRACKS WERE IN THE FITTING AND THE SPAR CAP - [SDR DL73S980339](https://openairdocs.org/sdr/DL73S980339), Feb 9, 1998: BULKHEAD WEB. CRACKED. DURING INSPECTION, SERVERAL CRACKS WERE FOUND IN THE BLKHD WEB AT FS 178. THE CRACKS WERE LOCATED AT WL 192 TO 202 AND LBL 5 AND RBL 5. REPAIRED PER ERA 331313- - [SDR DL73S980337](https://openairdocs.org/sdr/DL73S980337), Feb 9, 1998: SKIN. DENTED. DURING INSPECTION, A DENT WAS FOUND IN THE FUSELAGE SKIN AT APPROX STA 380 AND S18L. REPAIRED PER ERA 331346-14. - [SDR DL73S980336](https://openairdocs.org/sdr/DL73S980336), Feb 9, 1998: INTERCOSTAL. CRACKED. DURING INSPECTION, THE R1 DOOR INTERCOSTALS WERE FOUND CRACKED AT 3 LOCATIONS BETWEEN BS 332 AND 344. THE DAMAGED INTERCOASTALS WERE LOCATED AT S8A, 10A AND 11. - [SDR DL73S980280](https://openairdocs.org/sdr/DL73S980280), Feb 2, 1998: SKIN. CRACKED. FUSELAGE SKIN AT COOLING DUCT CUTOUT AT BS 379, BL 0 WAS FOUND CRACKED AT THE AFT EDGE OF THE CUTOUT. CRACK IS APPROX. 1.5 INCH LENGTH AND IS TYP PER SB 737-53- - [SDR DL73S961621](https://openairdocs.org/sdr/DL73S961621), Feb 9, 1996: FLOOR BEAM. CRACKED. THE BL 0 FLOOR BEAM OF THE WING CENTER SECTION IS CRACKED AT FS 664. NO CRACKS WERE FOUND ON THE WEB. THE CRACK IS TYPICAL PER BOEING SERVICE BULLETIN 737-57-12 - [SDR DL73S952021](https://openairdocs.org/sdr/DL73S952021), May 10, 1995: SKIN. GOUGE. FOUND SMALL .25 INCH BY .125 INCH GOUGE IN LOWER SKIN OF LEFT ELEV APPROX 6 INCHS FWD OF TAB. INSTALLED REPAIR PER SRM 55-20-03 FIG 01. - [SDR DL73S952116](https://openairdocs.org/sdr/DL73S952116), May 9, 1995: SKIN. CRACKED. LT ELEV TAB O/B HINGE UPPER AND LOWER SKIN CRACKED, COMPLIED WITH SRM 55-20-3. - [SDR DL73S952115](https://openairdocs.org/sdr/DL73S952115), May 8, 1995: SKIN. CRACKED. LT ELEV TAB CRACKED AT BOTH ENDS. BAL AFTER REPAIR. REPAIRED TAB PER ARM 55-20-01. - [SDR DL73S952455](https://openairdocs.org/sdr/DL73S952455), May 2, 1995: SKIN. DAMAGED. DURING INITIAL SHOP INSPECTION, MAINTENANCE FOUND A ONE INCH HOLE IN UPPER IB SKIN, 10 INCHES FROM THE INBOARD END AND 2 INCHES FROM THE TRAILING EDGE. REPAIR W - [SDR DL73S951950](https://openairdocs.org/sdr/DL73S951950), Apr 30, 1995: SKIN. DAMAGE. FOUND DURING INSP DFW, RT ELEVATOR DAMAGED JUST OUTBD OF TRIM TAB APPROXIMATE STATION 121.59, APPROX 3.0 INCHES FROM TRAILING EDGE 1.5 INCHES IN DIAMETER. REPAI - [SDR DL73S951949](https://openairdocs.org/sdr/DL73S951949), Apr 30, 1995: SKIN. DAMAGED. FOUND DURING INSP DFW, RT ELEVATOR DAMAGED INBD OF STA 149.12, 15.0 INCHES FROM TRAILING EDGE 3.0 INCHES IN DIAMETER. REPAIRED ELEV PER SRM 55-20-3, INSTALLED N - [SDR DL73S951948](https://openairdocs.org/sdr/DL73S951948), Apr 30, 1995: ELEVATOR. DAMAGED. FOUND DURING INSP DFW, RT ELEVATOR DAMAGED OUTBD OF STA 39.02 APPROXIMATELY 20.0 INCHES FROM TRAILING EDGE 3.0 INCHES IN DIAMETER. REPAIRED ELEV PER SRM 55-20-3 - [SDR DL73S951947](https://openairdocs.org/sdr/DL73S951947), Apr 30, 1995: SKIN. DAMAGED. FOUND DURING INSP DFW, RT ELEVATOR DAMAGED OUTBD OF STA 66.54 APPROX 15.0 INCHES FROM TRAILING EDGE 3.0 INCHES IN DIAMETER. REPAIRED ELEV PER SRM 55-20-3, INSTA - [SDR DL73S951946](https://openairdocs.org/sdr/DL73S951946), Apr 30, 1995: SKIN. DAMAGED. FOUND DURING INSP DFW, RT ELEVATOR DAMAGED INDB OF STA 66.54 APPROX 10.0 INCHES FROM TRAILING EDGE 3.0 INCHES IN DIAMETER. REPAIRED ELEV PER SRM 55-20-3, INSTAL - [SDR DL73S951945](https://openairdocs.org/sdr/DL73S951945), Apr 30, 1995: SKIN. DAMAGED. FOUND DURING INSP DFW, LT ELEVATOR DAMAGE OUTBOARD OF STA 176.64, 6 INCHES FROM TRAILING EDGE 1.25 INCH DAMAGE. REPAIRED ELEV PER SRM 55-20-3, INSTALLED NEW BAL - [SDR DL73S951944](https://openairdocs.org/sdr/DL73S951944), Apr 30, 1995: SKIN. DAMAGED. FOUND DURING INSP DFW, LT ELEVATOR DAMAGE BETWEEN STA 176.64 AND 149.12, 13 INCHES FROM TRAILING EDGE 2 INCH DAMAGE. REPAIRED ELEV PER SRM 55-20-3, INSTALLED NE - [SDR DL73S951943](https://openairdocs.org/sdr/DL73S951943), Apr 30, 1995: SKIN. DAMAGED. FOUND DURING INSP DFW, LT ELEVATOR DAMAGE BETWEEN STA 149.12 AND 121.59, 12 INCHES FROM TRAILING EDGE 2.5 INCH DAMAGE. REPAIRED ELEV PER SRM 55-20-3, INSTALLED - [SDR DL73S951942](https://openairdocs.org/sdr/DL73S951942), Apr 30, 1995: SKIN. DAMAGED. FOUND DURING INSP DFW, LT ELEVATOR DAMAGED BETWEEN STA 94.27 AND 66.54, 15 INCHES FROM TRAILING EDGE 2.5 INCH DAMAGE STARTED REPAIR PER SRM 55-20-3. REPAIRED EL - [SDR DL73S951941](https://openairdocs.org/sdr/DL73S951941), Apr 30, 1995: SKIN. DAMAGED. FOUND ON INSP DFW, LT ELEVATOR DAMAGE JUST OUTBOARD OF STA 3902, 4 INCHES FROM TRAILING EDGE 1 INCH DAMAGE. REPAIRED ELEV PER SRM 55-20-3, INSTALLED NEW BALANCE - [SDR DL73S950555](https://openairdocs.org/sdr/DL73S950555), Feb 8, 1995: COWL. DENTED. DURING A ROUTINE INSPECTION A 3 INCH BY 4 INCH DENT WAS FOUND ON THE NR 1 ENGINE SIDE COWL NEXT TO THE OIL ACCESS DOOR. THE DENT WAS CUT OUT AND AN EXTERNAL DOU - [SDR DL73S950386](https://openairdocs.org/sdr/DL73S950386), Jan 26, 1995: SKIN. LIGHTNING STRIKE. FOUND DURING LETTER CHECK, L2 LIGHTNING STRIKES ON LEFT FWD FUSELAGE BETWEEN STA 211 TO 259. BLENDED AREAS PER SRM 53-30-3. DYE CHECK OK, TREATED AREA PER SRM 5 - [SDR DL73S950385](https://openairdocs.org/sdr/DL73S950385), Jan 26, 1995: DOOR. CRACKED. FOUND DURING LETTER CHECK, L2 MLG INNER DOOR CRACKED AT T/E. REPAIRED PER SRM 51-40-13. - [SDR DL73S950384](https://openairdocs.org/sdr/DL73S950384), Jan 26, 1995: SKIN. PUNCTURED. FOUND DURING LETTER CHECK, L2 SMALL HOLE IN RUDDER. APPROXIMATELY .5 INCHES DIAMETER, 7 FEET FROM TOP OF RUDDER, AND APPROXIMATELY 7 INCHES AFT OF HINGE LINE. R ## FAA accident and incident reports (1) 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 19881215070469I](https://openairdocs.org/incident/19881215070469I), Dec 15, 1988: Boeing 737232 (N328DL), Covington - Cin, OH. Intermittent airframe vibration after departure. Returned. Precautionary shut down of nr 1 engine. --- 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.