# N396AN: 1999 Boeing 767-323, registration cancelled 2022-03-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 23, 2022
- Exported to: United Kingdom
- Status when cancelled: Valid registration
- Airframe: [Boeing 767-323](https://openairdocs.org/model/boeing-767-323) (registry code 1385205)
- Engine: [GE CF6-80C2B6](https://openairdocs.org/engine/ge-cf6-80c2b6) (registry code 30103)
- Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM), [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs)
- Serial number: 29603
- Year built: 1999
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 23, 1999
- Certificate issued: April 22, 2021
- Last registry action: March 23, 2022
- Mode S code: A49920
- Owner when cancelled: [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC)
- Location: [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.4607° N, 83.8443° W: Placed by OpenAirDocs at the center of ZIP code 45177, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N396AN
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=396AN
- Page: https://openairdocs.org/deregistered/N396AN-2022-03-23

From the FAA registry file of November 5, 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 767-323: https://openairdocs.org/model/boeing-767-323.md

## Service difficulty reports (137, newest 50)

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

- [SDR MK1Y202201025](https://openairdocs.org/sdr/MK1Y202201025), Jan 2, 2022: NONE. NONE. THE ENGINEERING ORDER PROVIDES DETAILED INSTRUCTIONS FOR THE REPAIR OF THE FUSELAGE MAIN FRAME INNER CHORD TRANSITION RADII LOCATED ON THE RIGHT SIDE OF B767-30
- [SDR MK1Y202201024](https://openairdocs.org/sdr/MK1Y202201024), Jan 2, 2022: NONE. NONE. THE ENGINEERING ORDER PROVIDES DETAILED INSTRUCTIONS FOR THE REPAIR OF THE FUSELAGE MAIN FRAME INNER CHORD TRANSITION RADII LOCATED ON THE LEFT SIDE OF B767-300
- [SDR MK1Y202201023](https://openairdocs.org/sdr/MK1Y202201023), Jan 2, 2022: NONE. NONE. DENT DAMAGE AND AN EXISTING BLEND-OUT WAS FOUND ON THE LOWER WING SKIN PANEL (P/N 112T4702-1) COMMON TO THE OUTBOARD STRINGER L-9.5 (P/N 767-3421-7) BETWEEN WS 
- [SDR MK1Y202201022](https://openairdocs.org/sdr/MK1Y202201022), Jan 2, 2022: NONE. NONE. PROBLEM DESCRIPTION: ENGINE #2, THRUST REVERSER TRANSLATING COWL, INNER SKIN, P/N CF6-F23G019, S/N R647-129: DURING MAINTENANCE INSPECTION AT IAI A CRACKED DENT
- [SDR MK1Y202201021](https://openairdocs.org/sdr/MK1Y202201021), Jan 2, 2022: NONE. NONE. R/H WING, UNDERSIDE, MAIN FUEL TANK, FUEL BOOST PUMP HOUSING, WS 226.3 – WS 255.4, P/N 50060050: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WAS FOUND ON TH
- [SDR MK1Y202201020](https://openairdocs.org/sdr/MK1Y202201020), Jan 2, 2022: NONE. NONE. L/H WING, UNDERSIDE, MAIN FUEL TANK, FUEL BOOST PUMP HOUSING, WS 226.3 – WS 255.4, P/N 50060050: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WAS FOUND ON TH
- [SDR MK1Y202201019](https://openairdocs.org/sdr/MK1Y202201019), Jan 2, 2022: NONE. NONE. PROBLEM DESCRIPTION: SLAT NO. 4, OSS 579.05: SHOP FOUND A DENT ADJACENT TO A BULGE IN UPPER LE SKIN OF SLAT NO. 4. THE DAMAGED AREA LOCATED ON A RIB AND STIFFEN
- [SDR MK1Y202201018](https://openairdocs.org/sdr/MK1Y202201018), Jan 2, 2022: NONE. NONE. FUSELAGE SKIN (SEC 45), STA 999 AND STA 1043, STR-2L AND STR-2R: DURING CONVERSION PROCESS, AIRCRAFT MAINTENANCE WAS REQUIRED TO DEACTIVATE AND REMOVE THE HIGH 
- [SDR MK1Y202201017](https://openairdocs.org/sdr/MK1Y202201017), Jan 2, 2022: NONE. NONE. PROBLEM DESCRIPTION: SLAT NO 5 AT OSS 389.71: SHOP FOUND DENT AMONG FASTENERS AT THE EDGE OF SLAT LE SKIN ATTACHMENT COMMON TO A RIB. THE REPORTED DAMAGE WAS FO
- [SDR MK1Y202201016](https://openairdocs.org/sdr/MK1Y202201016), Jan 2, 2022: NONE. NONE. HORIZONTAL STABILIZER, CENTER SECTION, UPPER SKIN, REAR SPAR – AT RBL10.33 STR U3 TO REAR SPAR: DURING MAINTENANCE INSPECTION AT IAI, CORROSION WERE FOUND.THE C
- [SDR MK1Y202201015](https://openairdocs.org/sdr/MK1Y202201015), Jan 2, 2022: NONE. NONE. HORIZONTAL STABILIZER, CENTER SECTION, UPPER SKIN, REAR SPAR – AT LBL10.83 STR U3 TO U2 AND LBL 11.83 STR U2 TO U1: DURING MAINTENANCE INSPECTION AT IAI, CORROS
- [SDR MK1Y202201013](https://openairdocs.org/sdr/MK1Y202201013), Jan 2, 2022: NONE. NONE. PROBLEM DESCRIPTION: #2 ENGINE OUTBOARD THRUST REVERSER DAGMAR FAIRING DAMAGE, ASSY IDENT: 683L136613, MODEL NO. TR-CF6-F23G019, S/N R647-129: DURING MAINTENANC
- [SDR MK1Y202201012](https://openairdocs.org/sdr/MK1Y202201012), Jan 2, 2022: NONE. NONE. ENGINE #1 OUTBD CORE COWL HAT FRAME NAC STA 303.75, LOWER AREA: DURING THE MAINTENANCE INSPECTION AT IAI, CRACK WAS FOUND AT DATUM LOCATION WITH 1.5 INCH LENGTH
- [SDR MK1Y202201011](https://openairdocs.org/sdr/MK1Y202201011), Jan 2, 2022: TEAR STRAP. CORRODED. TEAR STRAP, INNER SKIN, STA 544, S-1R AND S-4R, DOOR SURROUND ZONE: SHOP DISCOVERED DEEP CORROSION ON TEAR STRAP EDGE COMMON TO S-2R (LAP SPLICE). THE DAMAGED A
- [SDR MK1Y202201010](https://openairdocs.org/sdr/MK1Y202201010), Jan 2, 2022: NONE. NONE. PROBLEM DESCRIPTION: R/H WING LOWER SKIN SURFACE BETWEEN WS.994.7 AND WS.1001.7: SHOP FOUND TOOL MARK AMONG FASTENERS, PAINT STRIPPED AND PERFORMED NDT THICKNES
- [SDR MK1Y202201009](https://openairdocs.org/sdr/MK1Y202201009), Jan 2, 2022: NONE. NONE. WORN CORE COWL ALUMINUM HAT FRAME – ENGINE# 1, R/H CORE COWL, HAT FRAME, NAC STA 303.75, UPPER AREA DURING THE MAINTENANCE INSPECTION AT IAI, MAINTENANCE DISCOV
- [SDR MK1Y202201008](https://openairdocs.org/sdr/MK1Y202201008), Jan 2, 2022: NONE. NONE. . DURING A/C SURVEY AT TLV, MAINTENANCE DISCOVERED EXISTING BLENDOUT AT THE EDGE OF AN EXISTING FLUSH REPAIR CUTOUT LOCATED ON THE FUSELAGE SKIN AT STA 616 BETW
- [SDR MK1Y202201007](https://openairdocs.org/sdr/MK1Y202201007), Jan 2, 2022: NONE. NONE. ENGINE # 2, LH CORE COWL, HAT FRAME, NAC STA 303.75, MID LOWER AREA: DURING MAINTENANCE INSOECTION AT IAI, MAINTENANCE DISCOVERED ON #2 ENGINE, LH CORE COWL HAT
- [SDR MK1Y202201006](https://openairdocs.org/sdr/MK1Y202201006), Jan 2, 2022: NONE. NONE. NLG SUPPORT STRUCTURE, AFT VERTICAL STIFFENERS, UPPER EDGES, STA 287, L/RBL 13.10 DURING THE MAINTENANCE INSPECTION AT IAI, TWO CRACKS WERE FOUND AT DATUM LOCAT
- [SDR MK1Y202201005](https://openairdocs.org/sdr/MK1Y202201005), Jan 2, 2022: NONE. NONE. EXTERNAL FUSELAGE SKIN, STA 1487, STR-21L & STA 1460, STR-29L-STR-30L: DURING THE MAINTENANCE INSPECTION AT IAI, SCRATCHES WERE FOUND AND BLENDED OUT PER SRM 51
- [SDR MK1Y202201004](https://openairdocs.org/sdr/MK1Y202201004), Jan 2, 2022: NONE. NONE. EXTERNAL FUSELAGE SKIN, STA 308, STR-33L: DURING THE MAINTENANCE INSPECTION AT IAI, A SCRATCH WAS FOUND AND BLENDED OUT PER SRM 51-10-02. THE BLEND OUT EXCEEDS 
- [SDR MK1Y202201003](https://openairdocs.org/sdr/MK1Y202201003), Jan 2, 2022: NONE. NONE. EXTERNAL FUSELAGE SKIN, STA 588, STR-33R: DURING THE MAINTENANCE INSPECTION AT IAI, A SCRATCH WAS FOUND AND BLENDED OUT PER SRM 51-10-02. THE BLEND OUT EXCEEDS 
- [SDR MK1Y202201002](https://openairdocs.org/sdr/MK1Y202201002), Jan 2, 2022: NONE. NONE. FAN COWL SUPPORT BEAM LINK, #2 PYLON, P/N 31112522-1 DURING THE MAINTENANCE INSPECTION AT IAI, THE BORES IN THE #2 PYLON FAN COWL SUPPORT BEAM LINK PIN 311T2522
- [SDR MK1Y202201001](https://openairdocs.org/sdr/MK1Y202201001), Jan 2, 2022: NONE. NONE. PROBLEM DESCRIPTION: DURING THE MAINTENANCE INSPECTION FOUND SCRATCHES ON EXTERNAL FUSELAGE SKIN AMONG FASTENERS AREA. - SHOP CLEANED DAMAGED AREA IAW SRM 51-10
- [SDR AALA2020022089025](https://openairdocs.org/sdr/AALA2020022089025), Feb 17, 2020: CLUTCH. STICKING. AIRCRAFT WAS NOT GROUNDED: LEFT THROTTLE STICKING AUTO AND MANUAL OPERATION DOES NOT KEEP UP WITH RIGHT THROTTLE IN AUTO MODE. REPLACED AUTO THROTTLE CLUTCH PAC
- [SDR 2019FA0000383](https://openairdocs.org/sdr/2019FA0000383), Nov 23, 2019: LIGHT. INOPERATIVE. 7A SEAT EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY IAW AMM 33-51-10. OPS CHECK GOOD.
- [SDR AALA201910039007](https://openairdocs.org/sdr/AALA201910039007), Oct 2, 2019: ACCESS PANEL. DAMAGED. AIRCRAFT WAS GROUNDED: CABIN FLOOR ACCESS PANEL FOR E&E COMPARTMENT BOARD SOFT. REPLACED ACCESS PANEL PER AMM 52-48-05.
- [SDR AALA201906189013](https://openairdocs.org/sdr/AALA201906189013), Jun 16, 2019: SLIDE. LOW PRESSURE. AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS L1 DOOR SLIDE DOES NOT SHOW NEEDLE SHADOW IN GREEN BAND AND IS OUT OF LIMITS FOR PRESSURE GAUGE ON LOW SIDE. REMOVED 
- [SDR AALA20190512004](https://openairdocs.org/sdr/AALA20190512004), May 12, 2019: SUPPORT FITTING. CORRODED. AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT SUPPORT FITTING AT BS 1570 ON THE LAVATORY DUMP CRANK TOWER. REPLACED SUPPORT FITTING PER SRM 5
- [SDR AALA20190512002](https://openairdocs.org/sdr/AALA20190512002), May 12, 2019: SHEAR TIE. CORRODED. AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT SHEAR TIE AT BS 1562 AND BL 0. REPLACED SHEAR TIE PER SRM 51-10-02-0G
- [SDR AALA201902264001](https://openairdocs.org/sdr/AALA201902264001), Feb 23, 2019: FUEL FILTER. DIRTY. DURING CLIMB, THE RIGHT ENGINE FUEL FILTER LIGHT ILLUMINATED. REFERRED TO THE QRH, ADVISED TO LAND AS SOON AS POSSIBLE. DECLARED AN EMERGENCY AND RETURNED TO DE
- [SDR AALA2018102979001](https://openairdocs.org/sdr/AALA2018102979001), Oct 25, 2018: FLASHLIGHT. NO TEST. EMERGENCY FLASHLIGHTS AT THE FLIGHT ATTENDANTS JUMPSEAT, DID NOT TEST. REPLACED THE FLASHLIGHT AND TESTED GOOD IAW FIM 25-60-05.
- [SDR AALA2018101529023](https://openairdocs.org/sdr/AALA2018101529023), Oct 10, 2018: BATTERY PACK. INOPERATIVE. MID CABIN, LEFT SIDE ,AFT FLIGHT ATTENDANT SEAT FLASHLIGHT WAS INOPERATIVE. THE AIRCRAFT WAS GROUNDED. REPLACED THE FLASHLIGHT BATTERY IAW GPM 05-01-07. OPS CHE
- [SDR AALA2018091879012](https://openairdocs.org/sdr/AALA2018091879012), Sep 16, 2018: ANTENNA. FAULTED. WEATHER RADAR FAILED DURING FLIGHT. ACCOMPLISHED TROUBLESHOOTING IAW FIM 34-43-00, FOUND WEATHER RADAR PANEL AND ANTENNA AT FAULT. AN EMERGENCY WAS DECLARED, RE
- [SDR AALA2018091879004](https://openairdocs.org/sdr/AALA2018091879004), Sep 16, 2018: CONTROL PANEL. FAILED. WEATHER RADAR FAILED DURING FLIGHT. AN EMERGENCY WAS DECLARED, RETURNED TO DEPARTURE, AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED TROUB
- [SDR AALA201807129024](https://openairdocs.org/sdr/AALA201807129024), Jul 10, 2018: BATTERY. INOPERATIVE. MID GALLEY LEFT SIDE LOWER ACCESS DOOR DETACHABLE FLASHLIGHT BATTERY INOPERATIVE. REPLACED THE BATTERY. CHECKED NPRMAL.
- [SDR AALA20180327007](https://openairdocs.org/sdr/AALA20180327007), Mar 26, 2018: LIGHT. INOPERATIVE. SEAT 3J MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED 3J SEAT MOUNTED EMERGENCY LIGHT ASSY IAW AMM 33-51-10. OPS CHECKED NORMAL. AIRCRAFT WAS GROUNDED.
- [SDR AALA201801199005](https://openairdocs.org/sdr/AALA201801199005), Jan 16, 2018: BATTERY. NO TEST. FLASHLIGHT AT THE JUMPSEAT REAR LEFT FLIGHT COMPARTMENT BATTERY WILL NOT TEST. REPLACED THE BATTERY IAW AMM 25-64-00.
- [SDR AALA201712279032](https://openairdocs.org/sdr/AALA201712279032), Dec 25, 2017: THRESHOLD. LOOSE. FIRST CLASS FORWARD LAVATORY DOOR STICKING AT THRESHOLD BASE. TIGHTENED THRESHOLD SCREWS. CHECKED NORMAL.
- [SDR AALA20171205003](https://openairdocs.org/sdr/AALA20171205003), Dec 5, 2017: STIFFENER. CRACKED. AIRCRAFT IN BASE MAINTENANCE. CRACKED STIFFENER ON FORWARD SIDE OF FRAME 246 AT LBL26. INSTALLED ANGLE STIFFENER PER SRM 53-10-51-2R3.
- [SDR AALA20171204002](https://openairdocs.org/sdr/AALA20171204002), Dec 4, 2017: STIFFENER. CRACKED. AIRCRAFT IN BASE MAINTENANCE. CRACKED STIFFENER AT STA. 246 LEFT BUTTLINE 2 AND LEFT BUTTLINE 6. REPLACED STIFFENER AT STA. 246 LEFT BUTTLINE 2 AND LEFT BUTTLIN
- [SDR AALA20171204001](https://openairdocs.org/sdr/AALA20171204001), Dec 4, 2017: STIFFENER. CRACKED. AIRCRAFT IN BASE MAINTENANCE. CRACKED STIFFENERS ON STA. 246 AT LEFT BUTTLINE 0 TO LEFT BUTTLINE 4. REPLACED STIFFENERS ON STA. 246 AT LEFT BUTTLINE 0 TO LEFT B
- [SDR AALA201709059036](https://openairdocs.org/sdr/AALA201709059036), Sep 1, 2017: SMOKE DETECTOR. NO TEST. THE AIRCRAFT WAS NOT GROUNDED. PASSENGER SMOKING IN LAV A5. SMOKE DETECTION SYSTEM DID NOT INDICATE ANY SMOKE. LAV A5 SMOKE DETECTOR OPS CHECK PERF IAW AMM 26-1
- [SDR AALA201707249032](https://openairdocs.org/sdr/AALA201707249032), Jul 21, 2017: PUMP. FAILED. DURING FLIGHT LEFT FWD BOOST PUMP WOULD NOT WORK AFTER BALANCING FUEL. CIRCUIT BREAKER DISCOVERED TRIPPED. REMOVED AND REPLACED LEFT FWD BOOST PUMP IAW AMM 28-2
- [SDR AALA201706279041](https://openairdocs.org/sdr/AALA201706279041), Jun 26, 2017: LENS. DETACHED. AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT AT THE L1 DOOR HAS A DETACHED LENS COVER. REINSTALLED LENS COVER IAW AMM 33-51-03. OPERATIONAL CHECK GOOD.
- [SDR AALA20170622006](https://openairdocs.org/sdr/AALA20170622006), Jun 22, 2017: LENS. MISSING. EMERGENCY EXIT CEILING LIGHT NEAR SEATS 26G AND 25H HAS A MISSING LENS. REPLACED THE LENS IAW AMM 33-51-04. OPS CHECKED GOOD.
- [SDR AALA201706019034](https://openairdocs.org/sdr/AALA201706019034), May 30, 2017: ATTACH ANGLE. CORRODED. LEFT ENGINE FAN CASE NOSE COWL ATTACH ANGLE HAS EVIDENCE OF CORROSION AT THE 4 O'CLOCK AND 5'OCLOCK POSITIONS. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED LEFT 
- [SDR AALA201704259001](https://openairdocs.org/sdr/AALA201704259001), Apr 21, 2017: BATTERY PACK. NO TEST. SEAT MOUNTED EMERGENCY LIGHTS ON SEATS 22 TO 28HJ FAILED TEST. REMOVED AND REPLACED CHARGER ASSEMBLY AND BATTERY AT M732 IAW AMM 33-60-98. OPERATIONAL CHECKED G
- [SDR AALA201704249031](https://openairdocs.org/sdr/AALA201704249031), Apr 21, 2017: CHARGER. NO TEST. SEAT MOUNTED EMERGENCY LIGHTS ON SEATS 22 TO 28HJ FAILED TO TEST. REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY AT M732 IAW AMM 33-60-98. OPERATIONAL CH
- [SDR AALA20170413002](https://openairdocs.org/sdr/AALA20170413002), Apr 13, 2017: CONNECTOR. BROKEN. AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT SEAT 39H HAS A BROKEN CONNECTOR. REMOVED AND REPLACED CONNECTOR IAW SWPM 20-64-17. OPERAT

All 137: https://openairdocs.org/deregistered/N396AN-2022-03-23/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 DCA18WA173](https://openairdocs.org/ntsb/DCA18WA173), May 3, 2018: Boeing 767 323 (N396AN), Guayaquil, Ecuador, incident, no damage

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