# N152DL: 1990 Boeing 767-3P6, registration cancelled 2022-10-26

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 26, 2022
- Exported to: Denmark
- Status when cancelled: Valid registration
- Airframe: [Boeing 767-3P6](https://openairdocs.org/model/boeing-767-3p6) (registry code 1385105)
- Engine: [GE CF6-80 series](https://openairdocs.org/engine/ge-cf6-80-series) (registry code 30025)
- Data sheets: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs)
- Serial number: 24984
- Year built: 1990
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 27, 1997
- Certificate issued: August 14, 2021
- Last registry action: August 14, 2021
- Mode S code: A0D1F3
- 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/N152DL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=152DL
- Page: https://openairdocs.org/deregistered/N152DL-2022-10-26

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 767-3P6: https://openairdocs.org/model/boeing-767-3p6.md

## Service difficulty reports (169, newest 50)

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

- [SDR 2022FA0000544](https://openairdocs.org/sdr/2022FA0000544), Sep 19, 2022: PANEL. DENTED. DURING MAINTENENCE INSPECTION FOUND FILLING REPAIR ADJACENT TO A DENT ON ENGINE #2, CF6-80C2, INLET COWL LOWER ACOUSTIC PANEL BETWEEN 6 AND 7 O'CLOCK.
- [SDR 2022FA0000543](https://openairdocs.org/sdr/2022FA0000543), Sep 19, 2022: SKIN. PUNCTURED. DURING MAINTENENCE INSPECTION FOUND ON L/H HORIZONTAL STABILIZER UPPER SURFACE SKIN PUNCTURE DAMAGE BY 1.0" WICH PENETRATED THE HONEYCOMB STRUCTURE BETWEEN AUXI
- [SDR 2022FA0000542](https://openairdocs.org/sdr/2022FA0000542), Sep 19, 2022: SKIN. DAMAGED. DURING MAINTENENCE INSPECTION FOUND SEVERAL BLEND OUTS ON FUSELAGE SKIN BETWEEN STA 172 AND STA 196, AROUND STR 21R.
- [SDR 2022FA0000541](https://openairdocs.org/sdr/2022FA0000541), Sep 19, 2022: FAILSAFE. CRACKED. DURING MAINTENENCE INSPECTION FOUND CRACKED HOLE ON FAIL SAFE CHORD, STA 1540, BETWEEN STR 35L AND STR 36L.
- [SDR 2022FA0000540](https://openairdocs.org/sdr/2022FA0000540), Sep 19, 2022: SKIN. CORRODED. DURING MAINTENENCE INSPECTION FOUND CORROSION ON FUSELAGE SKIN BETWEEN STA 1219 AND STA 1307, STR 36L UNDER LAP JOINT.
- [SDR 2022FA0000538](https://openairdocs.org/sdr/2022FA0000538), Sep 19, 2022: SKIN. DAMAGED. DURING MAINTENENCE INSPECTION FOUND BLEND OUTS AND NICKS ON BULK CARGO DOOR CUTOUT BETWEEN STA 1461 AND STA 1480, BETWEEN STR 27L AND STR 32L.
- [SDR 2022FA0000537](https://openairdocs.org/sdr/2022FA0000537), Sep 19, 2022: SKIN. DAMAGED. DURING MAINTENENCE INSPECTION FOUND BLENDED AREA AND ONE (1) DENT ON FUSELAGE SKIN BETWEEN STA 148.75 AND STA 157, 8" BELOW STR 30R.
- [SDR 2022FA0000531](https://openairdocs.org/sdr/2022FA0000531), Sep 19, 2022: SKIN. DAMAGED. DURING MAINTENENCE INSPECTION FOUND SEVERAL GOUGES AND DENT ON FUSELAGE SKIN BETWEEN STA 256.25 AND STA 266.5 AND BETWEEN STR 11L AND STR 20L.
- [SDR 2022FA0000530](https://openairdocs.org/sdr/2022FA0000530), Sep 19, 2022: SKIN. DAMAGED. DURING MAINTENENCE INSPECTION FOUND DENT AND SHARP NICK ON BULK CARGO DOOR OUTER SKIN.
- [SDR 2022FA0000529](https://openairdocs.org/sdr/2022FA0000529), Sep 19, 2022: SKIN. DAMAGED. DURING MAINTENENCE INSPECTION FOUND DENT ON FUSELAGE SKIN AND BUILT UP FRAME, STA 1654.5 BETWEENSTR 32R AND STR 34R.
- [SDR 2022FA0000528](https://openairdocs.org/sdr/2022FA0000528), Sep 19, 2022: SKIN. DAMAGED. DURING MAINTENENCE INSPECTION FOUND SEVERAL ADJACENT BLEND OUTS BETWEEN STA 588 AND STA 654+88 AND BETWEEN STR 33R AND STR 34R.
- [SDR 2022FA0000527](https://openairdocs.org/sdr/2022FA0000527), Sep 19, 2022: SKIN. DAMAGED. DURING MAINTENENCE INSPECTION FOUND SEVERAL ADJACENT BLEND OUTS ON FUSELAGE SKIN, SEC 41, BETWEEN STA 246 AND STA 434 AND BETWEEN STR 29R AND STR 34R.
- [SDR 2022FA0000526](https://openairdocs.org/sdr/2022FA0000526), Sep 19, 2022: SKIN. DAMAGED. DURING MAINTENENCE INSPECTION FOUND BLEND OUTS ON RH FUSELAGE SKIN BETWEEN STA 1219 AND STA 1270 AND BETWEEN STR 26R AND STR 36R.
- [SDR DALA2020052902429](https://openairdocs.org/sdr/DALA2020052902429), May 25, 2020: SLIDE. BLOWN. RETURN TO GATE FOR REMOVING NO REVS, R1 SLIDE BLEW. REPLACED DOOR SLIDE. SYSTEM OPERATION IS NORMAL
- [SDR DALA2020012300520](https://openairdocs.org/sdr/DALA2020012300520), Jan 22, 2020: SKIN. DAMAGED. NR 7 SLAT T/E WEDGE INBD EDGE AFT, HAD BENT SKIN AND SEPARATED FORM COMPOSITE. REPAIRED IAW SRM 51-70-10.
- [SDR DALA2020011700368](https://openairdocs.org/sdr/DALA2020011700368), Jan 15, 2020: STRUCTURE. CORRODED. CORROSION LEVEL: 2 "J" CHORD AT STA 566 IN FLC IS CORRODED. REPLACED J CHORD.
- [SDR DALA2020011400257](https://openairdocs.org/sdr/DALA2020011400257), Jan 13, 2020: KEELBEAM. CORRODED. CORROSION LEVEL: 2 CORROSION ON KEEL BEAM WEB AT STA 965. REPAIRED PER ERA 584052-00.
- [SDR DALA2020011400256](https://openairdocs.org/sdr/DALA2020011400256), Jan 13, 2020: STRUCTURE. CORRODED. CORROSION LEVEL: 2 AT FLC MAIN CARGO DOOR AT STA 524 AND STA 569 HAS CORROSION ON LOWER CHORD. REMOVED CORROSION AT FLC STA 569. FOUND TO BE OUT OF LIMITS. REPA
- [SDR DALA2020011400255](https://openairdocs.org/sdr/DALA2020011400255), Jan 10, 2020: SEAT TRACK. CORRODED. CORROSION LEVEL: 2 UPPER CABIN SEAT TRACK RBL 88 STA 1097-1200 IS CORRODED ALONG ENTIRE LENGTH. REPLACED SEAT TRACK.
- [SDR DALA2020011400254](https://openairdocs.org/sdr/DALA2020011400254), Jan 9, 2020: SEAT TRACK. CORRODED. CORROSION LEVEL: 2 UPPER CABIN SEAT TRACK RBL 88 STA 965-987 CORRODED. REPLACED SEAT TRACK.
- [SDR DALA2020011400253](https://openairdocs.org/sdr/DALA2020011400253), Jan 9, 2020: SEAT TRACK. CORRODED. CORROSION LEVEL: 2 UPPER CABIN SEAT TRACK RBL 88 STA 762 CORRODED. REPLACED SEAT TRACK.
- [SDR DALA2020011400252](https://openairdocs.org/sdr/DALA2020011400252), Jan 8, 2020: BUSHING. CORRODED. CORROSION LEVEL: 2 NR 1 PYLON UPPER LINK I/B BUSHING ON PYLON SIDE SHOWS SIGNS OF PITTING. REPLACED BUSHING.
- [SDR DALA2020010900170](https://openairdocs.org/sdr/DALA2020010900170), Jan 8, 2020: STRINGER. CORRODED. CORROSION LEVELCORROSION ON S34L STA 453 REPAIRED STRINGER S34L STA 453 PER SRM 53-00-03 (LP 1436930)
- [SDR DALA2020010900168](https://openairdocs.org/sdr/DALA2020010900168), Jan 8, 2020: BUSHING. CORRODED. CORROSION LEVEL: 2 NO.1 PYLON UPPER LINK I/B BUSHING ON PYLON SIDE SHOWS SIGNS OF PITTING. REPLACED BUSHING. (LP 1436667)
- [SDR DALA2020010900166](https://openairdocs.org/sdr/DALA2020010900166), Jan 8, 2020: SKIN. CRACKED. AFT EXTERIOR FUSELAGE SKIN IS CRACKED EXTENDING FROM RIVET HEAD STATION 1725 STRINGER 7R (VERIFIED WITH HFEC SURFACE SCAN). REPAIRED PER SRM 53-80-01 (LP 143658
- [SDR DALA2020010900162](https://openairdocs.org/sdr/DALA2020010900162), Jan 6, 2020: PANEL. WORN. # 6 SLAT SPRING LOADED PANEL AT OUTBOARD END OF SLAT WORN THRU ON LEADING EDGE REPAIRED PANEL PER SRM 57-10-17 (LP 1434234)
- [SDR DALA2020010900157](https://openairdocs.org/sdr/DALA2020010900157), Jan 4, 2020: SEAT TRACK. CORRODED. CORROSION LEVEL: 2 UPPER CABIN SEAT TRACK LBL 88 STA 1097 CORRODED. REPLACED SEAT TRACK (LP 1433563)
- [SDR DALA2020010900156](https://openairdocs.org/sdr/DALA2020010900156), Jan 4, 2020: SEAT TRACK. CORRODED. CORROSION LEVEL: 2 UPPER CABIN SEAT TRACK LBL 88 STA 920 CORRODED. REPLACED SEAT TRACK (LP 1433561)
- [SDR DALA2020010710077](https://openairdocs.org/sdr/DALA2020010710077), Dec 31, 2019: STRINGER. CORRODED. STRINGER 36L BETWEEN BS 1351 AND 1373 HAD CORROSION IN CENTER SECTION, FOUND OUT OF LIMITS. REPLACED THE STRINGER.
- [SDR DALA2020010407689](https://openairdocs.org/sdr/DALA2020010407689), Dec 28, 2019: SHEAR TIE. CORRODED. CORROSION LEVEL: 2 SHEAR TIE CORRODED AT STA.1307 BETWEEN S39L AND 39R. FOUND OUT OF LIMITS. REPLACED SHEAR TIE. (LP 1420767)
- [SDR DALA2020010407685](https://openairdocs.org/sdr/DALA2020010407685), Dec 28, 2019: SHEAR TIE. CORRODED. CORROSION LEVEL: 2SHEAR TIE CORRODED AT STA 1241 BETWEEN S35R AND 36R BLEND AND CHECK LIMITS. REPLACED SHEAR TIE. (LP 1421261)
- [SDR DALA2020010407684](https://openairdocs.org/sdr/DALA2020010407684), Dec 28, 2019: SHEAR TIE. CORRODED. CORROSION LEVEL: 2 SHEAR TIE AT STA 1540 BEWEEN S39L 38L CORRODED, BLEND AND CHECK LIMITS. REPLACED SHEAR TIE. (LP 1421250)
- [SDR DALA2020010407692](https://openairdocs.org/sdr/DALA2020010407692), Dec 27, 2019: BUSHING. CORRODED. CORROSION LEVEL: 2 NO 1 PYLON UPPER LINK, O/B BUSHING ON UPPER MOUNT ON WING SIDE SHOW SIGNS OF PITTING. REPLACED BUSHING ON CWO 115958-0003. (LP 1420528)
- [SDR DALA2020010407691](https://openairdocs.org/sdr/DALA2020010407691), Dec 27, 2019: BUSHING. CORRODED. CORROSION LEVEL: 2 NO 1 PYLON, UPPER LINK I/B BUSHING ON WING SIDE SHOWS SIGNS OF PITTING. REPLACE BUSHINGS ON CWO 115958-0003. (LP1420523)
- [SDR DALA2020010407690](https://openairdocs.org/sdr/DALA2020010407690), Dec 27, 2019: BUSHING. CORRODED. CORROSION LEVEL: 2 NO.1 PYLON UPPER LINK O/B BUSHING ON PYLON SIDE SHOWS SIGNS OF PITTING REMOVED AND REPLACED BUSHING ON CWO 115959-0005. (LP 1420526)
- [SDR DALA2020010407688](https://openairdocs.org/sdr/DALA2020010407688), Dec 27, 2019: SHEAR TIE. CORRODED. CORROSION LEVEL: 2 SHEAR TIE STA 1540 39R-39L CORRODEDREMOVED AND REPLACED SHEAR TIE. (LP 1420435)
- [SDR DALA2020010407683](https://openairdocs.org/sdr/DALA2020010407683), Dec 27, 2019: STRINGER. CORRODED. CORROSION LEVEL: 2 STR 39R BETWEEN STA 412-434 CORRODEDREMOVED CORROSION ON STR 39R 100% MATERIAL LOSS. REMOVED DAMAGED STRINGER AND REPLACE WITH NEW STRINGER
- [SDR DALA2020010407682](https://openairdocs.org/sdr/DALA2020010407682), Dec 27, 2019: SHEAR TIE. CORRODED. SHEAR TIE @STA 434 BETWEEN STR 36R-37R CRACKED REMOVED AND REPLACED SHEAR TIE AT STA 434 BETWEEN STR 3612-37R (LP 1419810)
- [SDR DALA2020010407681](https://openairdocs.org/sdr/DALA2020010407681), Dec 27, 2019: STRINGER. CORRODED. CORROSION LEVEL: 2 CORROSION ON S37R STA 434 REMOVED COROSION 100% MATERIAL LOSS FOUND TO BE OUT OF LIMITS REMOVED DAMAGED STR AREA AND INSTALLED STR REPAIR AND
- [SDR DALA2020010407680](https://openairdocs.org/sdr/DALA2020010407680), Dec 27, 2019: STRINGER. CORRODED. CORROSION LEVEL: 2 CORROSION ON S36R STA 430 REMOVED CORROSION, FOUND TO BE OUT OF LIMITS REPLACED WITH NE STRINGER AND INSTALLED NEW STRINGER (LP 1419804)
- [SDR DALA2020010710078](https://openairdocs.org/sdr/DALA2020010710078), Dec 26, 2019: SHEAR TIE. CORRODED. SHEAR TIE CORRODED AT BS 1417 BETWEEN STRINGERS 39L AND 39R, FOUND OUT OF LIMITS. THE SHEAR TIE WAS REPLACED.
- [SDR DALA2020010407679](https://openairdocs.org/sdr/DALA2020010407679), Dec 26, 2019: BUSHING. CORRODED. CORROSION LEVEL: 2 NO.1 PYLON FWD BUSHING ON UPPER LINK SHOWS SIGNS OF PITTING. REPLACED (LP1418700)
- [SDR DALA2020010407678](https://openairdocs.org/sdr/DALA2020010407678), Dec 26, 2019: SHEAR TIE. CORRODED. CORROSION LEVEL: 2 SHEAR TIE @ STA 412 BETWEEN STR 36R-37R CORRODED OUT OF LIMITS. REPLACED SHEAR TIE. (LP1418076)
- [SDR DALA2020010407687](https://openairdocs.org/sdr/DALA2020010407687), Dec 23, 2019: SEAT TRACK. CORRODED. CORROSION LEVEL: 2 UPPER CABIN SEAT TRACK RBL 88 STA 1201-1439 IS CORRODED ALONG THE ENTIRE LENGTH. REPLACED SEAT TRACK. (LP1415508)
- [SDR DALA2020010407677](https://openairdocs.org/sdr/DALA2020010407677), Dec 23, 2019: STRINGER CLIP. CORRODED. CORROSION LEVEL: 2 STRINGER CLIP @ STA 1540 STR 39R.REPLACED STRINGER CLIP (LP 1416198)
- [SDR DALA2020010700079](https://openairdocs.org/sdr/DALA2020010700079), Dec 21, 2019: WEDGE. DAMAGED. #10 SLAT T/E EDGE WEDGE, I/B T/E HAS DAMAGE & COMPOSITE EXPOSED C/W SRM 51-70-10. (LP 1425960)
- [SDR DALA2019092305493](https://openairdocs.org/sdr/DALA2019092305493), Sep 21, 2019: LIGHT. INOPERATIVE. CREW REST EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED ALL BULBS. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2019062503853](https://openairdocs.org/sdr/DALA2019062503853), Jun 19, 2019: PUMP. MAKING METAL. LT HYDARULIC LOW PRESSURE LIGHT FOLLOWED LT HYD QUANTITY LIGHT FOUND DP INDICATOR BLOWN OUT OF FILTER MODULE. CHECK EDP CASE DRAIN FILTER AND PRESSURE FILTER. C
- [SDR DALA2018121747243](https://openairdocs.org/sdr/DALA2018121747243), Dec 13, 2018: FRAME. DAMAGED. FRAME AT STA 148.5 WL 210 DAMAGED REWORKED INNER AND OUTER FRAME CHORDS TO ORIGINAL CONTOUR @ STA 148.5 WL 210. REPAIRED PER ERA 568021-14. (LP 0863239)
- [SDR DALA2018121747242](https://openairdocs.org/sdr/DALA2018121747242), Dec 13, 2018: FRAME. DAMAGED. BULKHEAD FRAME AT STA 132.5 BETWEEN WL 207-220 DAMAGED. REPAIRED PER ER/A 568021-14. (LP 0863234)

All 169: https://openairdocs.org/deregistered/N152DL-2022-10-26/reports.md

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