# N322DL: 1984 Boeing 737-232, registration cancelled 2021-01-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 9, 2021
- Status when cancelled: Registration expired, pending cancellation
- 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: 23094
- Year built: 1984
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: August 3, 1984
- Certificate issued: June 5, 2006
- Last registry action: April 18, 2017
- Mode S code: A37614
- Owner when cancelled: [Northern Air Cargo Inc](https://openairdocs.org/faa-owner/NORTHERN%20AIR%20CARGO%20INC)
- Location: [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage)
- Owner type: Corporation
- Owner's area on the map: 61.1637° N, 149.9966° W: Placed by OpenAirDocs at the center of ZIP code 99502, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N322DL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=322DL
- Page: https://openairdocs.org/deregistered/N322DL-2021-01-09

From the FAA registry file of November 3, 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 (162, newest 50)

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

- [SDR NACA2017010300001](https://openairdocs.org/sdr/NACA2017010300001), Jan 1, 2017: SKIN. CRACKED. A SKIN CRACK WAS FOUND AT BS727B, S19R WHILE PERFORMING THE AD 2005-13-30 ZONE 1 INSPECTION. THERE WAS AN EXISTING REPAIR IN THE AREA THAT HAD TO BE INCORPORATE
- [SDR NACA20160711005](https://openairdocs.org/sdr/NACA20160711005), Jul 11, 2016: FRAME. CRACKED. THE BS 360 FRAME INSULATION BLANKET HOLE WAS DISCOVERED CRACKED AT S20R, DURING ACCOMPLISHMENT OF AD2015-28-03. FRAME REPAIR INSTALLED IAW MFG SERVICE REQUEST M
- [SDR NACA201607110004](https://openairdocs.org/sdr/NACA201607110004), Jul 11, 2016: FRAME. CRACKED. A PARTIALLY SEVERED FRAME WAS DISCOVERED AT BS 328, S20R-S21R, DURING THE ACCOMPLISHMENT OF AD2015-28-03. THE REPAIR/PREVENTIVE MODIFICATION ON THE BS 328 FRAME
- [SDR NACA201511160001](https://openairdocs.org/sdr/NACA201511160001), Nov 13, 2015: FRAME. DAMAGED. FRAME DAMAGED AT BS 500 BETWEEN STRINGERS 13-14R. INSTALLED REPAIR TO FRAME IAW SRM 51-40-3, FIG 1.
- [SDR NACA201505010059](https://openairdocs.org/sdr/NACA201505010059), May 1, 2015: FAILSAFE. MISINSTALLED. DURING REPAIR OF A CRACKED FRAME FAIL SAFE ANGLE IN THE AREA, IT WAS NOTED THAT THE FRAME SPLICES DID NOT CONFORM TO AEI DRAWINGS. AT REQUEST, NON-CONFORMING FR
- [SDR NACA201505010058](https://openairdocs.org/sdr/NACA201505010058), May 1, 2015: FLOOR SUPPORT. CRACKED. UPPER FUSELAGE MAIN CABIN BL0 BS719 LONGITUDINAL FLOOR BEAM WEB CRACKED 3 PLACES. REPLACED UPPER FUSELAGE MAIN CABIN BL0 BS719 LONGITUDINAL FLOOR BEAM WEB WITH 
- [SDR NACA201505010057](https://openairdocs.org/sdr/NACA201505010057), May 1, 2015: FAILSAFE. CRACKED. DURING REPAIR OF A CRACKED FRAME FAIL SAFE ANGLE IN THE AREA, IT WAS NOTED THAT THE FRAME SPLICES DID NOT CONFORM TO AEI DRAWINGS. NON-CONFORMING FRAMES IN THE 
- [SDR NACA201505010056](https://openairdocs.org/sdr/NACA201505010056), May 1, 2015: FAILSAFE. CRACKED. DURING REPAIR OF A CRACKED FRAME FAIL SAFE ANGLE IN THE AREA, IT WAS NOTED THAT THE FRAME SPLICES DID NOT CONFORM TO AEI DRAWINGS. NON-CONFORMING FRAMES IN THE 
- [SDR NACA201505010055](https://openairdocs.org/sdr/NACA201505010055), May 1, 2015: FAILSAFE. CRACKED. DURING REPAIR OF A CRACKED FRAME FAIL SAFE ANGLE IN THE AREA, IT WAS NOTED THAT THE FRAME SPLICES DID NOT CONFORM TO AEI DRAWINGS. NON-CONFORMING FRAMES IN THE 
- [SDR NACA201505010054](https://openairdocs.org/sdr/NACA201505010054), May 1, 2015: FAILSAFE. CRACKED. DURING REPAIR OF A CRACKED FRAME FAIL SAFE ANGLE IN THE AREA, IT WAS NOTED THAT THE FRAME SPLICES DID NOT CONFORM TO AEI DRAWINGS. NON-CONFORMING FRAMES IN THE 
- [SDR NACA201505010053](https://openairdocs.org/sdr/NACA201505010053), May 1, 2015: FAILSAFE. CRACKED. DURING REPAIR OF A CRACKED FRAME FAIL SAFE ANGLE IN THE AREA, IT WAS NOTED THAT THE FRAME SPLICES DID NOT CONFORM TO AEI DRAWINGS. NON-CONFORMING FRAMES IN THE 
- [SDR NACA201505010052](https://openairdocs.org/sdr/NACA201505010052), May 1, 2015: WEB. CRACKED. UPPER FUSELAGE AT BS 1016, LBL40 FLOOR WEB CRACKED. CRACK IN THE AFT CABIN STRESS WEB. FABRICATED AND INSTALLED REPLACEMENT WEB IAW DWG 65-46812 AND SRM R108.
- [SDR NACA201505010051](https://openairdocs.org/sdr/NACA201505010051), May 1, 2015: BELTFRAME. CRACKED. AFT CARGO PIT, BS 847 BELTFRAME CRACKED INBD OF STR 25L. CRACK FRAME AT BS 847 AT S25L +5, REPAIRED IAW SRM R108 53-10-4, FIG 7.
- [SDR NACA201505010050](https://openairdocs.org/sdr/NACA201505010050), May 1, 2015: FRAME. CRACKED. FRAME AT BS 277, S16L CRACKED IN UPPER FUSELAGE. REPAIRED FRAME AT BS 277, STR 16L IN UPPER FUSELAGE IAW SRM 53-10-04 FIG 7, REPAIR 2, R108. REF KFC MCO 3218, W
- [SDR NACA201505010049](https://openairdocs.org/sdr/NACA201505010049), May 1, 2015: FRAME. DAMAGED. DAMAGE ON FRAME, BS 380, S15-16R. DURING INSPECTION, DAMAGE WAS NOTED ON THE INNER CHORD OF THE FRAME AT THIS LOCATION. REPAIRED IAW DWG R23094.1-053-012-001, R
- [SDR NACA201505010048](https://openairdocs.org/sdr/NACA201505010048), May 1, 2015: INTERCOSTAL. CORRODED. AFT CARGO BAY BS 789, RBL 23 INTERCOSTAL CORRODED. BLENDED, MEASURED AND FOUND TO BE BEYOND THE LIMITS OF SRM R108, 53-10-1. FABRICATED AND INSTALLED REPLACEMEN
- [SDR NACA201505010047](https://openairdocs.org/sdr/NACA201505010047), May 1, 2015: SHEAR WEB. CORRODED. UPPER FUSELAGE FLOOR CORRODED SHEAR WEB BS 639 TO BS 663, LBL 65, STR 17R. DURING INSPECTION, CORROSION THAT WAS VISIBLY BEYOND LIMITS WAS NOTED ON THE CREASE B
- [SDR NACA201505010046](https://openairdocs.org/sdr/NACA201505010046), May 1, 2015: WEB. CORRODED. UPPER FUSELAGE FLOOR CORRODED SHEAR WEB BS 616 TO BS 639, RBL 65, STR 17R. DURING INSPECTION, OUT OF LIMITS, CORROSION WAS NOTED ON THE CREASEBEAM WEB BETWEEN B
- [SDR NACA201505010045](https://openairdocs.org/sdr/NACA201505010045), May 1, 2015: WEB. CORRODED. UPPER FUSELAGE FLOOR CORRODED SHEAR WEB BS 616 TO BS 639, LBL 65, STR 17L. FABRICATED AND INSTALLED REPLACEMENT WEB IAW SRM 53-10-02, FIG 1, ITEM 3, REV 108, RE
- [SDR NACA201505010044](https://openairdocs.org/sdr/NACA201505010044), May 1, 2015: FITTING. CORRODED. CORROSION ON VERTICAL STABILIZER ON RT AFT FITTING FWD SIDE. DURING THIS INSPECTION, CORROSION WAS NOTED IN THIS FITTING AND FOUND TO BE BEYOND LIMITS. FITTING 
- [SDR NACA201505010043](https://openairdocs.org/sdr/NACA201505010043), May 1, 2015: SUPPORT FITTING. CRACKED. OTBD MLG SUPPORT BEAM FITTING CRACKED. THE FITTING WAS REPLACED WITH THE NEWER STYLE AS SHOWN SB 57-1216R2, REF KFC MCO 3218, WO 1367210.
- [SDR NACA201505010042](https://openairdocs.org/sdr/NACA201505010042), May 1, 2015: ATTACH FITTING. CORRODED. CORROSION ON VERTICAL STABILIZER ATTACH FITTING LT AFT FWD FACE. DURING INSPECTION CORROSION WAS NOTED ON THE VERTICAL STABILIZER ATTACH FITTING, LT SIDE, AFT. 
- [SDR NACA201505010041](https://openairdocs.org/sdr/NACA201505010041), May 1, 2015: SKIN. CRACKED. CRACKED EXTERIOR FUSELAGE BETWEEN BS 747 & BS 767 AT STR 18L. REPAIRED CRACK WITH EXTERNAL DOUBLER AT BS 747-BS 767 IAW SB 737-53-1065, REV 2, APRIL 19, 2001, R
- [SDR NACA201505010040](https://openairdocs.org/sdr/NACA201505010040), May 1, 2015: STRINGER. CORRODED. AFT CARGO BAY BS 904, STRINGER 26R CORRODED OUT OF LIMITS. . FABRICATED AND INSTALLED REPLACEMENT STRINGER SECTION AND ASSOCIATED SPLICES.
- [SDR NACA2015105010039](https://openairdocs.org/sdr/NACA2015105010039), May 1, 2015: DOOR FRAME. CORRODED. AFT CARGO BAY BS 797, RBL 26, LWR CARGO ENTRY WAY SKIN CORRODED. OUT OF LIMITS CORROSION NOTED ON THE STRUCTURAL SILL WEB AND THE C2 THRESHOLD. REPLACED WITH NE
- [SDR NACA201505010038](https://openairdocs.org/sdr/NACA201505010038), May 1, 2015: SUPPORT. CRACKED. AFT CARGO BAY BS 775, RBL 2 ANTENNA SUPPORT STRUCTURE HAS 2 CRACKS. THE INTERIOR STRUCTURE WAS REPLACED AND AN EXTERNAL DOUBLER WAS INSTALLED. DOUBLER IS IN PRO
- [SDR NACA201505010037](https://openairdocs.org/sdr/NACA201505010037), May 1, 2015: SKIN. CRACKED. FWD CARGO BAY DOOR INNER SKIN LIGHTING HOLE CRACKED AT BS 480, RBL 44. REPAIRED CRACKED LIGHTNING HOLE WITH DOUBLER INSTALLED AT BS 480, RBL 44 WITH FABRICATED 
- [SDR NACA201505010036](https://openairdocs.org/sdr/NACA201505010036), May 1, 2015: FLOORBEAM. CRACKED. UPPER FUSELAGE FLOORBEAM SUPPORT ANGLE AT BS 328, RBL 34 HAS CRACK. REPLACED CRACKED ANGLE WITH FABRICATED NEW PART IAW 51-20-01, FIG 7, REV 108, SRM, REF KFC M
- [SDR NACA201505010035](https://openairdocs.org/sdr/NACA201505010035), May 1, 2015: INTERCOSTAL. CRACKED. UPPER FUSELAGE DOOR FRAME SUPPORT INTERCOSTAL AT BS 294 BETWEEN STR 12R AND STR 13R CRACKED. DURING INSPECTION OF THE SURROUND STRUCTURE OF THE R1 ORIFICE, A CR
- [SDR NACA201505010034](https://openairdocs.org/sdr/NACA201505010034), May 1, 2015: SKIN. DAMAGED. FWD AIR STAIR DOOR INNER SKIN DAMAGE IN UPPER FWD CORNER. DURING INSPECTION, SIGNIFICANT DAMAGE WAS NOTED ON THE INNER SKIN OF THE FORWARD AIRSTAIR DOOR. FABRIC
- [SDR NACA201505010033](https://openairdocs.org/sdr/NACA201505010033), May 1, 2015: ANGLE. CRACKED. AFT CARGO BAY BS 727, RBL 18, WL 200 CRACKED CLIP. DURING INSPECTION, A CRACKED CLIP WHICH SERVES TO SECURE THE UPPER END OF THE RBL 18 VERTICAL BEAM OF THE BS 
- [SDR NACA201505010032](https://openairdocs.org/sdr/NACA201505010032), May 1, 2015: FLOOR SUPPORT. CORRODED. FLOORBEAM CHORD AT RBL24 FROM BS 540 TO BS 727B HAS CORROSION AROUND CLIPNUT HOLES. OUT OF LIMITS CORROSION NOTED IN SEVERAL PLACES DURING INSPECTION NECESSITAT
- [SDR NACA201505010031](https://openairdocs.org/sdr/NACA201505010031), May 1, 2015: FLOOR SUPPORT. CORRODED. UPPER FLOOR BS 673 TO BS 639, LBL 65 HAS CORROSION ON TOP & BOTTOM OF SILL. DURING INSPECTION, CORROSION WHICH WAS VISUALLY BEYOND LIMITS WAS NOTED ON THE CREAS
- [SDR NACA201505010030](https://openairdocs.org/sdr/NACA201505010030), May 1, 2015: FLOOR SUPPORT. CORRODED. UPPER FUSELAGE FLOOR BS727B TO 540 LBL25 CORROSION ON FLOORBOARD FLANGE STRUCTURE. AWAITING PAPERWORK FROM C-CHECK.
- [SDR NACA201505010029](https://openairdocs.org/sdr/NACA201505010029), May 1, 2015: FLOOR SUPPORT. CRACKED. UPPER FUSELAGE FLOOR BS 616 & BS 639 AT RBL 65 SIDE RAIL CRACKED. DURING INSPECTION, CRACKS WERE NOTED AT THE CREASE BEAM INNER CHORD. THIS CHORD ALSO SUPPORTS 
- [SDR NACA2015105010028](https://openairdocs.org/sdr/NACA2015105010028), May 1, 2015: FLOOR SUPPORT. CORRODED. UPPER FUSELAGE FLOOR HAS CORROSION ON FLOORBEAM FLANGE STRUCTURE AT BS 727B TO BS 540, RBL45. OUT OF LIMITS CORROSION WAS NOTED ON THE UPPER CAP OF THE LONGITUD
- [SDR NACA201505010027](https://openairdocs.org/sdr/NACA201505010027), May 1, 2015: FLOORBEAM. CORRODED. UPPER FUSELAGE BS 807, LBL 65 TO RNL 65 HAS CORROSION ON LWR FLANGE OF FLOORBEAM & LWR STRAP. DURING INSPECTION, CORROSION WAS NOTED ON THE LOWER FLANGE OF THE 
- [SDR NACA201505010026](https://openairdocs.org/sdr/NACA201505010026), May 1, 2015: FLOORBEAM. CORRODED. UPPER FUSELAGE BS 867, LBL 25 TO LBL 45 CORRODED ON LWR FLANGE OF FLOORBEAM. CORROSION BEYOND LIMITS WAS NOTED ON THE LOWER FLANGE OF THE MAIN DECK FLOORBEAM AT
- [SDR NACA2015051100001](https://openairdocs.org/sdr/NACA2015051100001), May 1, 2015: FLOORBEAM. CORRODED. UPPER FUSELAGE BS 867, LBL 25 TO LBL 45 CORRODED ON LWR FLANGE OF FLOORBEAM. CORROSION BEYOND LIMITS WAS NOTED ON THE LOWER FLANGE OF THE MAIN DECK FLOORBEAM AT
- [SDR NACA201505010025](https://openairdocs.org/sdr/NACA201505010025), May 1, 2015: WEB. CORRODED. UPPER FUSELAGE BS 887 TO BS 907, RBL 65 CORRODED ON FLOOR STRESS WEB. CORROSION WAS NOTED ON THE CREASE BEAM WEB AT FLOOR LEVEL DURING INSPECTION. CORROSION WAS
- [SDR NACA201505010024](https://openairdocs.org/sdr/NACA201505010024), May 1, 2015: FLOORBEAM. CORRODED. UPPER FUSELAGE FLOOR BS 480, RBL 65-45 HAS CORROSION ON FLOORBEAM. UPPER FUSELAGE BS 480 RBL 65-45 HAD CORROSION ON FLOORBEAM BEYOND LIMITS. REPAIRED FLOORBEAM 
- [SDR NACA201505010023](https://openairdocs.org/sdr/NACA201505010023), May 1, 2015: FLOORBEAM. CORRODED. UPPER FUSELAGE FLOOR BS 887, RBL 25 TO LBL 12.5 HAS CORROSION ON LOWER FLANGE OF FLOORBEAM. REPAIRED FLOOR BEAM IAW SRM R108, 53010-9, FIG 7. REF KFC MCO 3218, 
- [SDR NACA201505010022](https://openairdocs.org/sdr/NACA201505010022), May 1, 2015: FRAME. DAMAGED. UPPER FUSELAGE FRAME BS 360 S16L DAMAGE ON FRAME.
- [SDR NACA201505010021](https://openairdocs.org/sdr/NACA201505010021), May 1, 2015: FAILSAFE. CRACKED. FORWARD CARGO PIT AT BS 520, LBL 30, FAILSAFE CRACKED.
- [SDR NACA201505010020](https://openairdocs.org/sdr/NACA201505010020), May 1, 2015: FRAME. DAMAGED. UPPER FUSELAGE, BS 787 BETWEEN S17R-16R DAMAGED FRAME. REPAIRED IAW KF DWG R23094.1-053-007-001, REV NC.
- [SDR NACA201505010019](https://openairdocs.org/sdr/NACA201505010019), May 1, 2015: WEB. CRACKED. CRACKED LIGHTNING HOLE AT BS 450, RBL 44. REPAIRED CRACKED LIGHTNING HOLE WITH DOUBLER INSTALLED AT BS450, RBL 44 WITH FABRICATED PART IAW 52-30-1, FIG 1, REV 1
- [SDR NACA201505010018](https://openairdocs.org/sdr/NACA201505010018), May 1, 2015: SKIN. CRACKED. FWD CARGO BAY DOOR INNER SKIN LIGHTING HOLE CRACKED AT BS 450 AND RBL 34. REPAIRED CRACKED LIGHTNING HOLE WITH DOUBLER INSTALLED IAW 52-30-1, FIG 1, REV 108, AN
- [SDR NACA201505010017](https://openairdocs.org/sdr/NACA201505010017), May 1, 2015: SUPPORT ANGLE. CRACKED. FWD CARGO BAY STRINGER SUPPORT ANGLE CRACKED AT BS 440 AT STR 24R. REPLACED WITH MADE PART IAW DWG 65-20722, REV K. FASTENERS INSTALLED IAW -200, SRM 51-30-2.
- [SDR NACA201505010016](https://openairdocs.org/sdr/NACA201505010016), May 1, 2015: WEB. CORRODED. AFT CARGO BAY WEB FROM BS 927 TO BS 947, RBL65 CORROSION FOUND. FABRICATED AND INSTALLED REPLACEMENT WEB IAW DWG 65-45855, REV CV.
- [SDR NACA201505010015](https://openairdocs.org/sdr/NACA201505010015), May 1, 2015: WEB. CORRODED. AFT CARGO BAY BS 907 STRINGER 17R WEB CORROSION FOUND AT RBL65. FABRICATED AND INSTALLED REPLACEMENT WEB IAW SRM 53-10-2, FIG 13, PG 97, REV 108, DWG 65-47976, 

All 162: https://openairdocs.org/deregistered/N322DL-2021-01-09/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB FTW92IA055](https://openairdocs.org/ntsb/FTW92IA055), Jan 7, 1992: Boeing 737-232 (N322DL), Dfw Airport, TX, incident, minor damage. Probable cause: THE FAILURE OF THE AFT CONE BOLT AS RESULT OF PREEXISTING FATIGUE CRACKING DUE TO IMPROPER MAINTENANCE, AND THE FAILURE OF THE SECONDARY SUPPORT STRUCTURE AS A RESULT OF LOADS THAT EXCEEDED THE…

## FAA accident and incident reports (5)

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 20110614011039I](https://openairdocs.org/incident/20110614011039I), Jun 14, 2011: Boeing 737-232 (N322DL), Anchorage, AK, No damage. 6/14/2011 At approximately 2145 hours AKDT, naca - a/c N322DL was on take off roll at anc runway 32. At approximately 100 knots a loud bang was heard and take…
- [Incident 20091020050479I](https://openairdocs.org/incident/20091020050479I), Oct 20, 2009: Boeing 737-232 (N322DL), Kotzebue, AK, No damage. At 1540Z #1 "a" system hydraulic low pressure light illuminated. #2 "a" system low pressue light on/off intermittently. Declared emergency due to hydraulic…
- [Incident 20080119000489I](https://openairdocs.org/incident/20080119000489I), Jan 19, 2008: Boeing 737232 (N322DL), Dillingham, AK, Minor damage. (-23) On January 19, 2008, at about 2024GMT, a Boeing 737-200 airplane, N322DL, sustained minor damage to its left engine lower cowling when it hit several…
- [Incident 20000102000169I](https://openairdocs.org/incident/20000102000169I), Jan 2, 2000: Boeing 737232 (N322DL), Kansas City, MO. (-23) On 1/3/2000, delta aircraft N322DL, flight #2588, a Boeing 737-200, was INB0UND to Kansas City, and declared an emergency. When they lowered their flaps,…
- [Incident 19920107000289I](https://openairdocs.org/incident/19920107000289I), Jan 7, 1992: Boeing 737232 (N322DL), Dallas-Ft Worth, TX, Minor damage. NR2 lengine separated from aircraft after departure. Aircraft returned and landed without incident.

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