# N1402A: 1993 Boeing 767-332, registration cancelled 2020-10-17

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 17, 2020
- Status when cancelled: Sale reported
- Airframe: [Boeing 767-332](https://openairdocs.org/model/boeing-767-332) (registry code 1385101)
- Engine: [Pratt & Whitney PW4000 series](https://openairdocs.org/engine/pratt-whitney-pw4000-series) (registry code 52119)
- Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM) (OpenAirDocs)
- Serial number: 25989
- Year built: 1993
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 19, 1993
- Last registry action: August 25, 2020
- Mode S code: A0A54F
- Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta)
- Owner type: Individual
- Owner's area on the map: 33.6604° N, 84.3865° W: Placed by OpenAirDocs at the center of ZIP code 30354, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N1402A
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=1402A
- Page: https://openairdocs.org/deregistered/N1402A-2020-10-17

From the FAA registry file of October 31, 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 767-332: https://openairdocs.org/model/boeing-767-332.md

## Service difficulty reports (103, newest 50)

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

- [SDR DALA2019051503063](https://openairdocs.org/sdr/DALA2019051503063), May 13, 2019: SLIDE. OUT OF LIMITS. FOUND L1 ESCAPE SLIDE INSPECTION OUT OF LIMITS. REPLACED L1 DOOR SLIDE. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2018110206417](https://openairdocs.org/sdr/DALA2018110206417), Nov 1, 2018: STRUCTURE. CRACKED. BHEC INSPECTION OF BS 1809 RT OUTER STRUCTURE, SHOWS CRACK INDICATIONS AT 3 HOLE LOCATIONS. COMPLIED WITH E/RA 572634-14.
- [SDR DALA2018110206415](https://openairdocs.org/sdr/DALA2018110206415), Nov 1, 2018: HINGE FITTING. GOUGED. NR 2 ENGINE, OTBD CORE COWL, CENTER HINGE FITTING WAS GOUGED ON THE FORWARD SIDE. FOUND TO BE OUT OF LIMITS IAW SRM 54-53-90, COMPLIED WITH ER/A 572646-14.
- [SDR DALA2018033002037](https://openairdocs.org/sdr/DALA2018033002037), Mar 29, 2018: SKIN. CRACKED. DURING SERVICE CHECK, FUSELAGE SKIN AT BS 1654.5, STRINGER 13L FOUND CRACKED. REMOVED THE DAMAGED AREA, PERFORMED EDDY CURRENT, AND INSTALLED A REPAIR DOUBLER A
- [SDR DALA2018030401433](https://openairdocs.org/sdr/DALA2018030401433), Mar 4, 2018: ANGLE. CRACKED. FUSELAGE BULKHEAD BS 1809.5 LEFT HALF AFT OUTER ANGLE CRACKED. COMPLIED WITH ERA 566145-14AD.
- [SDR DALA2018030501428](https://openairdocs.org/sdr/DALA2018030501428), Mar 2, 2018: FITTING. CRACKED. REMOVED AND REPLACED THE LT INNER TENSION FITTING AT BS 1809 DUE TO CRACKING. COMPLIED WITH ERA 566145-14AD.
- [SDR DALA2018030201426](https://openairdocs.org/sdr/DALA2018030201426), Mar 2, 2018: STRINGER. CRACKED. LOWER AFT HOLE HAS CRACK INDICATIONS. REPAIRED IAW ERA 566145-14.
- [SDR DALA2018030201425](https://openairdocs.org/sdr/DALA2018030201425), Mar 1, 2018: SKIN. CRACKED. FUSELAGE SKIN CRACKED AFT OF BS 1654.50, STRINGER 13R. REPAIRED IAW ERA 566160-14.
- [SDR DALA2018022601298](https://openairdocs.org/sdr/DALA2018022601298), Feb 24, 2018: SLIDE. UNWANTED DEPLOY. RIGHT SIDE OVER WING SLIDE DEPLOYED. REPLACED SLIDE. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2017062705032](https://openairdocs.org/sdr/DALA2017062705032), Jun 25, 2017: COOLING FAN. FAILED. SMOKE IN COCKPIT, FOLLOWED BY FORWARD EQUIPMENT EXHAUST FAN STATUS MESSAGE. FOUND EQUIPMENT COOLING FAN INOPERATIVE AND REPLACED.
- [SDR DALA2017060904596](https://openairdocs.org/sdr/DALA2017060904596), May 12, 2017: SEAT TRACK. CORRODED. FOUND CORROSION ON SEAT TRACK, RBL 54.75, BS 852, REPLACED.
- [SDR DALA2017051503966](https://openairdocs.org/sdr/DALA2017051503966), May 12, 2017: SEAT TRACK. CORRODED. CORROSION ON RBL 33 SEAT TRACK, BS 852. REPLACED THE SEAT TRACK.
- [SDR DALA2017051503965](https://openairdocs.org/sdr/DALA2017051503965), May 12, 2017: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK, RBL 88.5, BS 852. REPLACED THE SEAT TRACK.
- [SDR DALA2017051503964](https://openairdocs.org/sdr/DALA2017051503964), May 12, 2017: SEAT TRACK. CORRODED. CORROSION ON RBL 74.75 SEAT TRACK AT BS 852. REPLACED THE SEAT TRACK.
- [SDR DALA2017051303963](https://openairdocs.org/sdr/DALA2017051303963), May 12, 2017: SKIN. CORRODED. FUSELAGE SKIN BULGING WITH FASTENERS PULLING, BS 1219, STRINGER 32L, APPROXIMATLEY 8 INCH AREA, 12 INCHES AFT OF PREVIOUS REPAIR. REPAIRED IAW ERA 558384-14.
- [SDR DALA2017051503959](https://openairdocs.org/sdr/DALA2017051503959), May 6, 2017: STRINGER SPLICE. CORRODED. STRINGER SPLICE 34L, BS 1219 - 1241 CORRODED. REPAIRED IAW ERA 558384-14.
- [SDR DALA2016120809816](https://openairdocs.org/sdr/DALA2016120809816), Dec 7, 2016: WIRE. OPEN. RED EMERGENCY LIGHT AT DOOR 1R CLOSET WALL INOPERATIVE. FOUND OPEN WIRES AT FLOOR SPLICED IN LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2016110208197](https://openairdocs.org/sdr/DALA2016110208197), Oct 30, 2016: LIGHT. INOPERATIVE. R1 DOOR SLIDE LIGHT INOPERATIVE. MAINTENANCE REPLACED SLIDE LIGHT ASSEMBLY AND ADJUSTED TO SECURE LENS WITHIN LIGHT. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2016102507642](https://openairdocs.org/sdr/DALA2016102507642), Oct 24, 2016: LENS. WRONG PART. EMERGENCY ESCAPE LIGHTS AT SEAT 26B LENS INCORRECT COLOR. REPLACED CLEAR LENS WITH RED LENS. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2016110208218](https://openairdocs.org/sdr/DALA2016110208218), Oct 19, 2016: FLOOR PANEL. CRACKED. DURING SERVICE CHECK FOUND A FLOOR PANEL CRACKED IN AFT CARGO AT STA 1200 BETWEEN RBL 20.5 AND 44.0 RT SIDE. C/W ERA 552002-14.
- [SDR DALA2016021601132](https://openairdocs.org/sdr/DALA2016021601132), Feb 11, 2016: CONNECTOR. DISCONNECTED. EMERGENCY EXIT LIGHT AT 29AB ARE INOPERATIVE. MAINTENANCE RECONNECTED WIRE AT CONNECTOR. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2015082305237](https://openairdocs.org/sdr/DALA2015082305237), Aug 21, 2015: ELECTRICAL BOX. CONTAMINATED. F/A REPORTED ELECTRICAL ODOR IN FIRST CLASS NEAR SEAT 4AB. TROUBLESHOT ENTIRE FIRST CLASS SECTION FOR ELECTRICAL ODOR, NONE FOUND. SUSPECT PASSENGER CHARGING UN
- [SDR DALA2015051903358](https://openairdocs.org/sdr/DALA2015051903358), May 9, 2015: FLOOR SUPPORT. CORRODED. CABIN FLOOR SUPPORT UPPER CHORD CORRODED AT RBL 33.06, BS 852-915. REPAIRED IAW SRM 53-00-51.
- [SDR DALA2015051903357](https://openairdocs.org/sdr/DALA2015051903357), May 8, 2015: FLOOR SUPPORT. CORRODED. CABIN FLOOR SUPPORT UPPER CHORD CORRODED AT RBL 74.18 AND BS 852. REPAIRED IAW SRM 53-00-51.
- [SDR DALA2015051903356](https://openairdocs.org/sdr/DALA2015051903356), May 7, 2015: FLOOR SUPPORT. CORRODED. CABIN FLOORBEAM UPPER TEE CORRODED AT RBL 54.81, BS 852-903. REPAIRED IAW SRM 53-00-51.
- [SDR DALA2015031202220](https://openairdocs.org/sdr/DALA2015031202220), Mar 11, 2015: FUSE. FAILED. FOUND EMERGENCY LIGHTS ROWS 1 AB - 12 FG INOPERATIVE. MAINTENANCE REPLACED BLOWN FUSE. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2014071404134](https://openairdocs.org/sdr/DALA2014071404134), Jul 11, 2014: POWER SUPPLY. INOPERATIVE. LEFT EXTERIOR EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENENACE REPLACED THE POWER SUPPLY M738.
- [SDR DALA13068361402](https://openairdocs.org/sdr/DALA13068361402), Dec 6, 2013: LIGHT. INOPERATIVE. EMERGENCY ESCAPE PATH LIGHT AT MID LAV AREA UNDER F/A SEAT INOPERATIVE. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT ASSY. CHECKED NORMAL.
- [SDR DALA13034071402](https://openairdocs.org/sdr/DALA13034071402), Jul 10, 2013: CONNECTOR. DISCONNECTED. EMERGENCY EXIT LIGHT AT SEAT 20G INOPERATIVE. MX RECONNECTED MATE-N-LOCK CONNECTOR AT LAMP ASSY. SYS OPS IS NORMAL.
- [SDR DALA13028331402](https://openairdocs.org/sdr/DALA13028331402), Jun 5, 2013: FITTING. CRACKED. NR 2 PYLON CRACK INDICATION FOUND ON RT UPPER LINK PITCH LOAD FITTING AT MOST OTBD AFT FASTENER HOLE REPAIRED IAW PRI 514654-14AD, REV 0, REV 1, REV 2 AND REV 3
- [SDR DALA13028321402](https://openairdocs.org/sdr/DALA13028321402), Jun 5, 2013: SKIN. CRACKED. NR 2 PYLON, CRACK INDICATION FOUND ON RT UPPER WING SKIN LOAD FITTING AT MOST OTBD AFT FASTENER HOLE. WORK CARRIED OUT IAW PRI 514654-14AD, REV 0, REV 1 AND REV
- [SDR DALA13028251402](https://openairdocs.org/sdr/DALA13028251402), Jun 5, 2013: FITTING. DAMAGED. DURING HFEC OPEN HOLE INSPECTION ON RT WING NR 2 PYLON AFT DIAGONAL BRACE FITTING, FOUND OTBD FASTENER HOLE (01 EA) WITH HOLE EDGE DAMAGE ON LOWER WING SURFACE 
- [SDR DALA13028241402](https://openairdocs.org/sdr/DALA13028241402), Jun 5, 2013: SPAR WEB. CANNING. NR 2 PYLON MID SPAR WEB FOUND OIL CANNING AND DEEP CHAFING AT LT SIDE, REPAIR CARRIED OUT IAW ERA 514639-14.
- [SDR DALA13027261402](https://openairdocs.org/sdr/DALA13027261402), Jun 5, 2013: LONGERON FITTING. CRACKED. CRACK INDICATION FOUND APPROX 0.3" IN LENGTH DURING HFEC ON RT SIDE UNDERWING LONGERON FITTING. FITTING REPAIRED IAW ER/A 514635-14AD.
- [SDR DALA13027241402](https://openairdocs.org/sdr/DALA13027241402), Jun 5, 2013: FAILSAFE. CRACKED. ULTRASONIC INSPECTION, FOUND CRACK INDICATION AT RT BS 955, FAILSAFE STRAP AT LOWER OF THE THE 3 FASTENER HOLES REPAIR COMPARED AND COMPLIED WITH ER/A 514032-14
- [SDR DALA13027231402](https://openairdocs.org/sdr/DALA13027231402), Jun 5, 2013: FAILSAFE. CRACKED. ULTRASONIC INSPECTION FOUND CRACK INDICATION AT LT BS 955, FAILSAFE STRAP AT LOWER OF THE 3 FASTENER HOLES. 3 FASTENER HOLES REPAIRED IAW PRI 514031-14AD, REV 0
- [SDR DALA13027221402](https://openairdocs.org/sdr/DALA13027221402), Jun 5, 2013: SKIN. CORRODED. FOUND ON RT WING UPPER SURFACE, WITHIN FILLET AREA AT WBL 102 TO WBL 106 AND 11" FWD OF RT WING REAR SPAR. REPAIR COMPARED AND COMPLIED WITH FINAL ER/A 514645-1
- [SDR DALA13027211402](https://openairdocs.org/sdr/DALA13027211402), Jun 5, 2013: SKIN. CORRODED. RT WING UPPER FILLET AREA-CORROSION FOUND ON WING UPPER SURFACE BELOW BRACKET, WITHIN FILLET AREA AT WBL 101 TO WBL 102.5 AND FWD OF RT WING REAR SPAR 22.5" TO 
- [SDR DALA13028231402](https://openairdocs.org/sdr/DALA13028231402), Jun 4, 2013: SKIN. CORRODED. LEFT WING UPPER FILLET AREA-CORROSION FOUND ON LT WING UPPER SURFACE AT WBL 101 TO WBL 104.5 AND FWD OF LT WING REAR SPAR 14" TO 18.5" AS MARKED. REPAIR CARRIED
- [SDR DALA13028221402](https://openairdocs.org/sdr/DALA13028221402), Jun 4, 2013: SKIN. CORRODED. CORROSION FOUND LT WING UPPER SURFACE AT WBL 101.5 TO WBL 104.5 AND 8.5 INCHES TO 12 INCHES FWD OF LT WING REAR SPAR CORRODED AREA. REPAIR CARRIED OUT IAW PRI 5
- [SDR DALA13027201402](https://openairdocs.org/sdr/DALA13027201402), Jun 4, 2013: SKIN. CORRODED. LT WING UPPER FILLET AREA-CORROSION FOUND ON LT WING UPPER SURFACE BELOW BRACKET, AT WBL 101 TO WBL 103.5 AND FWD OF LT WING REAR SPAR 22" TO 24". REPAIR CARRIE
- [SDR DALA13027191402](https://openairdocs.org/sdr/DALA13027191402), Jun 4, 2013: FRAME. CORRODED. CORROSION ON CABIN FRAME BS 1197+132 INBD FACE BETWEEN STRINGER 12-13L, CARRIED OUT REPAIR IAW ER/A514973-14.
- [SDR DALA13027181402](https://openairdocs.org/sdr/DALA13027181402), Jun 4, 2013: FRAME. CRACKED. CRACK INDICATION FOUND ON FRAME DURING HFEC INSPECTION ON LT BS 859.5, LBL 89, WL 200 FRAME INNER CHORD TRANSITION RADIUS APPROX 0.5". FRAME REPAIRED.
- [SDR DALA13027171402](https://openairdocs.org/sdr/DALA13027171402), Jun 4, 2013: FRAME. CRACKED. CRACK INDICATION FOUND DURING HFEC INSPECTION ON RT BS 883.5, RBL 89, WL 200 FRAME INNER CHORD TRANSITION RADIUS APPROX. 0.5" IN LENGTH AS MARKED. FRAME INNER C
- [SDR DALA13027031402](https://openairdocs.org/sdr/DALA13027031402), Jun 4, 2013: FRAME. CRACKED. CRACK INDICATION FOUND DURING HFEC INSPECTION ON RT BS 903.5, RBL 89, WL 200 FRAME INNER CHORD TRANSITION RADIUS APPROX 1.0" IN LENGTH. RT BS 903.5, RBL 89, WL 
- [SDR DALA13026321402](https://openairdocs.org/sdr/DALA13026321402), May 30, 2013: LONGERON. CORRODED. LONGERON 38R FOUND CORRODED AT BS 1540. BULK CARGO IAW SRM 53-00-03, FIG 201, REPAIR 2, REV 92. NEW STRINGER ANGLE AND CHANNEL FABRICATED USING MATERIAL 7075-0-
- [SDR DALA13026061402](https://openairdocs.org/sdr/DALA13026061402), May 28, 2013: FRAME. CRACKED. BS 1809, BULKHEAD RT FWD OUTER CHORD CRACKED AT STR 7-8R, REPAIRED IAW SRM 53-80-08, REPAIR 9.
- [SDR DALA13026051402](https://openairdocs.org/sdr/DALA13026051402), May 28, 2013: FRAME. CRACKED. DURING HFEC INSPECTION ON BS 1809 BULKHEAD LT FWD OUTER CHORD AT STR 6L TO 7L FOUND CRACKED. REPAIRED SRM 53-80-08, REPAIR 9, REV 92.00.
- [SDR DALA13026331402](https://openairdocs.org/sdr/DALA13026331402), May 22, 2013: FLOORBEAM. CORRODED. AFT CARGO FLOORBEAM SEVEN AREAS FOUND CORRODED BS 1153, RBL 20-42. REMOVED AND INSTALLED WITH NEW SPLICE IAW SRM 51-40-02.
- [SDR DALA13023441402](https://openairdocs.org/sdr/DALA13023441402), May 19, 2013: FLOORBEAM. CORRODED. CABIN FLOORBEAM AT BS 325 BETWEEN RBL 20 - 54.75 FOUND CORRODED. REPAIRED FROM LBL 45 TO RBL 60.

All 103: https://openairdocs.org/deregistered/N1402A-2020-10-17/reports.md

## 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 19941121044349I](https://openairdocs.org/incident/19941121044349I), Nov 21, 1994: Boeing 767332 (N1402A), Portland, OR. Compressor stall on NR1 engine en route. Returned to pdx. Remooved and replaced engine assembly.

## Other aircraft with N1402A

- [Cancelled 1989-03-24](https://openairdocs.org/deregistered/N1402A-1989-03-24): Piper PA-22, S/N 22314. N-number assigned, not yet registered

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