# N144DA: 1999 Boeing 767-332, registration cancelled 2020-01-24

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 24, 2020
- Status when cancelled: First renewal notice
- 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: 27584
- Year built: 1999
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 13, 1999
- Certificate issued: May 14, 1999
- Last registry action: February 16, 2017
- Mode S code: A0B1D8
- Owner when cancelled: [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC)
- Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta)
- Owner type: Corporation
- 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/N144DA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=144DA
- Page: https://openairdocs.org/deregistered/N144DA-2020-01-24

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 767-332: https://openairdocs.org/model/boeing-767-332.md

## Service difficulty reports (54, newest 50)

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

- [SDR DALA2017021001128](https://openairdocs.org/sdr/DALA2017021001128), Feb 9, 2017: CONNECTOR. DETACHED. EMERGENCY LIGHTS AT 5FE ARE INOPERATIVE. MAINTENANCE RECONNECTED THE ELECTRICAL CONNECTOR. SYSTEM OPERATION IS NORMAL.
- [SDR DALA2016122810105](https://openairdocs.org/sdr/DALA2016122810105), Dec 16, 2016: SKIN. DELAMINATED. DURING WALK AROUND INSPECTION, FOUND AREA OF DELAMINATION ON RIGHT VERTICAL STABILIZER PANEL LOCATED AT FSS 220 AND BL 1750. DELAMINATION IS OUT OF SRM LIMITS. 
- [SDR DALA2016112309132](https://openairdocs.org/sdr/DALA2016112309132), Nov 22, 2016: SEAT TRACK. BROKEN. SEAT TRACK BROKEN. CUT OUT DAMAGED SECTION OF SEAT TRACK & FABRICATED A REPAIR IAW SRM 53-00-52 REPAIR 1 FIG.201 AND INSTALLED THE REPAIR IAW SRM 53-00-52, REPA
- [SDR DALA2015091205677](https://openairdocs.org/sdr/DALA2015091205677), Sep 12, 2015: STRUCTURE. CRACKED. LEFT HORIZONTAL INNER CHORD CRACKED OUT OF FASTENER, BS 1809, REPAIRED IAW SRM 53-80-08.
- [SDR DALA13056451404](https://openairdocs.org/sdr/DALA13056451404), Oct 22, 2013: WIRE. DISCONNECTED. EMERGENCY LIGHTS AT SEAT 5FE ARE INOPERATIVE. MX FOUND A WIRE DISCONNECTED. CONNECTED WIRE SYS OPS NORMAL.
- [SDR DALA13049581404](https://openairdocs.org/sdr/DALA13049581404), Oct 2, 2013: SKIN. CRACKED. NR 2 PYLON FWD UPPER PYLON DRAIN HOLE CRACKED. REPAIRED IAW ERA 519157-14.
- [SDR DALA13021221404](https://openairdocs.org/sdr/DALA13021221404), May 4, 2013: SQUIB. INOPERATIVE. DURING CHANGE OF LT WING SLIDE BOTTLE, FOUND RT WING SPOILER BLOW DOWN SQUIB BAD. REPLACED RT WING SPOILER OVERRIDE ACTUATOR SQUIB.
- [SDR DALA1230061404](https://openairdocs.org/sdr/DALA1230061404), May 8, 2012: FRAME. CRACKED. FS 903 LT BETWEEN STR 20L AND STR 21L FRAME CHORD CRACKED. CHORD CRACK REPAIR ACCOMPLISHED AS PER ERA 501545-14AD REV ORG SECTION 1.
- [SDR DALA1230051404](https://openairdocs.org/sdr/DALA1230051404), May 8, 2012: FRAME. CRACKED. FS 903 RT BETWEEN STR 20R AND STR 21L INNER CHORD CRACKED. TRIMMED OUT AND REPAIRED AS PER ERA 501546-14AD REV ORG SECTION 1.
- [SDR DALA1230041404](https://openairdocs.org/sdr/DALA1230041404), May 8, 2012: SPAR. CRACKED. NR 1 PYLON FWD UPPER SPAR WEB LT DRAIN HOLE FOUND CRACKED. REPAIRED AS PER ERA 502699-14AD, REV ORG NRC 52915.
- [SDR DALA1229051404](https://openairdocs.org/sdr/DALA1229051404), May 5, 2012: FAILSAFE. CORRODED. LT STA 955 REAR SPAR BULKHEAD FAIL SAFE STRAP FASTENER HOLE CORRODED. REPAIRED AS PER ERA 501535-14AD, REV ORG.
- [SDR DALA1229041404](https://openairdocs.org/sdr/DALA1229041404), May 5, 2012: TEE FITTING. CORRODED. RIGHT BS 955 REAR SPAR BULKHEAD FITTING FOUND CORRODED AT TEE FITTING. REPLACED TEE FITTING AS PER ERA 501536-14AD, REV ORG.
- [SDR DALA1229031404](https://openairdocs.org/sdr/DALA1229031404), May 5, 2012: TEE FITTING. CRACKED. LEFT BS 955 REAR SPAR BULKHEAD FITTING CRACKED AT TEE FITTING. TEE FITTING REPLACED AS PER ERA 501535-14AD, ORG.
- [SDR DALA1229021404](https://openairdocs.org/sdr/DALA1229021404), May 5, 2012: FAILSAFE. CRACKED. RIGHT BS 955 REAR SPAR BULKHEAD FAILSAFE STRAP CRACKED, AREA TRIMMED OUT AND REPAIRED AS PER ERA 501536-14AD REV. ORG
- [SDR DALA1224811404](https://openairdocs.org/sdr/DALA1224811404), Apr 19, 2012: FAIRING. DELAMINATED. RT I/B MAIN FLAP O/B L/E FAIRING IS DELAMINATED IN 3 PLACES. REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 TABLE 1 AND 51-70-05 PAR 5A(1) FIG 5.
- [SDR DALA1223701404](https://openairdocs.org/sdr/DALA1223701404), Apr 17, 2012: TEE FITTING. CRACKED. FS 955 LT REAR SPAR BLKHD "T" FITTING AT FAILSAFE IS CRACKED AT A HOLE, WORKING FROM A PRI.
- [SDR DALA1223681404](https://openairdocs.org/sdr/DALA1223681404), Apr 16, 2012: TEE FITTING. CORRODED. FS 955 RT REAR SPAR BLKHD "T" FITTING HAS A FASTENER HOLE CORRODED, WORKING ON PRI.
- [SDR DALA1223591404](https://openairdocs.org/sdr/DALA1223591404), Apr 16, 2012: FRAME. CRACKED. FS 903 LT BETWEEN STR 20L-21L FRAME INNER CHORD IS CRACKED, WORKING FROM PRI.
- [SDR DALA1223581404](https://openairdocs.org/sdr/DALA1223581404), Apr 16, 2012: FRAME. CRACKED. FS 903 BETWEEN STR 20R-21R FRAME INNER CHORD IS CRACKED, WORKING FROM PRI.
- [SDR DALA1223571404](https://openairdocs.org/sdr/DALA1223571404), Apr 16, 2012: FITTING. CRACKED. FS 927 AT STR 20R-21R FRAME TO WING CENTER SECTION FITTING IS CRACKED AND BEING REPLACED PER B767-300 SRM 51-10-02 PG 8 PARA 9 AND DWG 100T1410.
- [SDR DALA1223201404](https://openairdocs.org/sdr/DALA1223201404), Apr 16, 2012: FAIRING. GOUGED. LT HORIZONTAL STAB L/E FAIRING 332DL IS GOUGED AND REPAIRED PER B767-300 SRM 55-10-01 REPAIR 1 FIG 201 AND 51-70-10 REPAIR 4 FIG 201 SHT 2.
- [SDR DALA1223191404](https://openairdocs.org/sdr/DALA1223191404), Apr 16, 2012: WEDGE. DELAMINATED. NR 4 SLAT T/E WEDGE IS DELAMINATED IN 2 PLACES AND REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 FIG 201 AND 51-70-10 REPAIR 4 FIG 202 SHT 1.
- [SDR DALA1223181404](https://openairdocs.org/sdr/DALA1223181404), Apr 16, 2012: FAIRING. DELAMINATED. LT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING IS DELAMINATED IN 2 PLACES AND HAS BEEN REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 TABLE 1 AND SRM 51-70-05 PAR 
- [SDR DALA1221451404](https://openairdocs.org/sdr/DALA1221451404), Apr 10, 2012: FAILSAFE. CRACKED. RIGHT FUSELAGE STATION 955 REAR SPAR BULKHEAD FAILSAFE STRAP FASTENER HOLE CRACKED.
- [SDR DALA1221431404](https://openairdocs.org/sdr/DALA1221431404), Apr 10, 2012: FAILSAFE. CRACKED. LEFT FUSELAGE STATION 955 REAR SPAR BULKHEAD FAIL SAFE STRAP FASTENER HOLE FOUND CORROSION AND CRACKED.
- [SDR DALA1013110144](https://openairdocs.org/sdr/DALA1013110144), Jun 10, 2010: WIRE. BROKEN. FOUND ON PDC/DRC CHECK, EMERGENCY LIGHT IS INOPERATIVE AT THE BASE OF LAVATORY 215. MX REPAIRED A BROKEN WIRE FOUND AT BASE. SYS OPS IS NORMAL. (DL76P101504)
- [SDR DL76P100749](https://openairdocs.org/sdr/DL76P100749), Mar 22, 2010: CONNECTOR. DISCONNECTED. EMERGENCY PATH LIGHT AT 3AB IS INOPERATIVE. MX FOUND CONNECTORS DISCONNECTED AND RECONNECTED THEM. SYS OPS IS NORMAL.
- [SDR DL76P100623](https://openairdocs.org/sdr/DL76P100623), Mar 11, 2010: CONTROL PANEL. ODOR. ACRID ODOR IN COCKPIT DURING CRUISE AND IN DESCENT LASTING FOR APPROX. 10 SECONDS EACH TIME. FOUND GALLEY CONTROL PANEL AT 1R WITH ACRID ODOR. SUSPECT 5 AMP FRE
- [SDR DL76P092019](https://openairdocs.org/sdr/DL76P092019), Dec 18, 2009: TURBINE BLADES. DAMAGED. NR 2 ENGINE FAILED, OP 5067 BOROSCOPE 2ND STAGE. PERFORMED NR 2 OP 5067 ENG BOROSCOPE. FOUND ONE 2ND STG HPT BLADE DAMAGE. ALSO AP-9 DAMAGE EMP 221084. SEE ITEM
- [SDR DL76P091971](https://openairdocs.org/sdr/DL76P091971), Dec 13, 2009: INDICATOR. MALFUNCTIONED. RTB DUE TO INOPERATIVE SPEED FLAG ON ADIS RESET TMC C/BS. FLAGS CLEARED - NO ADC FAULTS. TMC TESTS GOOD. A/T SERVO TESTS GOOD.
- [SDR DL76P090752](https://openairdocs.org/sdr/DL76P090752), Apr 22, 2009: STARTER. INOPERATIVE. APU START 15-20 PSI RT ENG BEGAN TO START W/N2 AT LEAST 8 THEN ROLLED BACK. START VALVE LITE NORMAL. TRIED AIR FROM LT ENG NR N2 OR OIL PRESS. REMOVED AND REPLA
- [SDR DL76P090381](https://openairdocs.org/sdr/DL76P090381), Mar 7, 2009: GENERATOR. FAULTED. AFTER PUSHBACK LT GEN DID NOT AUTOMATICALLY PICK UP THE LOAD. MANUAL RESET BROUGHT GEN ONLINE. DUE TO MULTIPLE EICAS MSGS RE EECS ACFT RETURNED TO GATE. BIT BPC
- [SDR DL76P090292](https://openairdocs.org/sdr/DL76P090292), Feb 23, 2009: IDG. INOPERATIVE. ON NR 2 ENG START NR 1 GEN FELL OFF LINE. L ENG EEC C1 STATUS MSG BIT BPCU LEFT ENG FAULT LOW FREQ TRIP. BIT PIMU ON LT ENG HAD NUMEROUS FAULTS DUE TO POWER DRO
- [SDR DL76P090261](https://openairdocs.org/sdr/DL76P090261), Feb 21, 2009: GCU. FAILED. LT ENG GENERATOR FAILED ON TAXI OUT DURING X BLEED START. REPLACED LEFT GCU RAN ENG OPS CK OK.
- [SDR DL76P090192](https://openairdocs.org/sdr/DL76P090192), Feb 11, 2009: PROBE. UNKNOWN. RIGHT ENGINE CONTROL EICAS MESSAGE AFTER ENGINE START. REPLACED P2/T2 PROBE, OPS NORMAL.
- [SDR DL76P091576](https://openairdocs.org/sdr/DL76P091576), Jan 10, 2009: TRANSMITTER. FAILED. RTB - FLAPS WILL NOT LOWER AND FLAP DISAGREE EICAS MSG. T/S PER FIM 27-51-00 FIG 105. DIRECTED TO FIM 27-51-00 FIG 11, CHECKS OK UP TO STEP 5-SHEET 3 FIG 114C. 
- [SDR DL76P081154](https://openairdocs.org/sdr/DL76P081154), Sep 4, 2008: STARTER. FAILED. NR 1 ENG NO START NO ROTATION, FOUND STARTED AT FAULT. REPLACED STARTER.
- [SDR DL76P080378](https://openairdocs.org/sdr/DL76P080378), Mar 16, 2008: HYDRAULIC LINE. LEAKING. ON LANDING ROLLOUT, AFTER ACTUATING THRUST REVERSERS LOST RT HYDRAULIC QTY. FOUND REVERSER HYDRAULIC LINE WITH HOLE IN IT. PERFORMED TEMP REPAIR PER MM 20-10-09
- [SDR DL76P071602](https://openairdocs.org/sdr/DL76P071602), Dec 10, 2007: INDICATOR. ODOR. CAPTAINS VSI WENT BLANK. DETECTED FAINT ELECTRICAL ODOR. PULLED VSI CIRCUIT BREAKER. ODOR DISSIPATED. REPLACED CAPTS VSI, OPS TESTS GOOD.
- [SDR DL76P071007](https://openairdocs.org/sdr/DL76P071007), Aug 3, 2007: LOOP. UNKNOWN. PASSING 28000 FT T/O PLUS 15 MIN CLIMB PWR RT DUCT BLEED LIGHT AND EICAS MSG. COMPLETED WITH QRH PROCEDURE RT DUCT BLEED LEAK EXTINGUISHED PASSING 32500 FEET. V
- [SDR DL76P071029](https://openairdocs.org/sdr/DL76P071029), Aug 2, 2007: CONTROL MODULE. MALFUNCTIONED. SPOILERS CAUTION LIGHT ON TAXI OUT. RESET PCA3 FAULT ON 2L SPOILER CONTROL MODULE. OPERATED SPOILERS ALL MODES WITH DIFFERENT POWER SOURCES.
- [SDR DL76P070953](https://openairdocs.org/sdr/DL76P070953), Jul 24, 2007: CIRCUIT CARD. DEFECTIVE. RIGHT DUCT LEAK LIGHT INFLIGHT CLIMBING THRU FL210. CHECKED ALL DUCTS FROM RT ENGINE TO THE RT ISOL VALVE. REPLACED WHEEL WELL OVHT ECS DUCT LEAK DETECTION SYS 
- [SDR DL76P060811](https://openairdocs.org/sdr/DL76P060811), Oct 2, 2006: FAN. ODOR. EQUIPMENT COOLING OVHT LIGHT ON OVERHEAD PANEL ACCOMPANIED BY BURNING SMELL IN COCKPIT. FOUND EICAS MSG FWD EQUIP SUPPLY FAN 1 PULLED AND COLLARD C/B H-18 FWD T
- [SDR DL76P040974](https://openairdocs.org/sdr/DL76P040974), Oct 16, 2004: TURBINE. DAMAGED. ON T/O ROLL APPROX 130 KTS CREW EXPERIENCED LOUD BANG AND FLASH FOLLOWED BY YAW TO THE RIGHT. EGT REPORTED OFF SCALE ON RT ENG. PASSENGERS REPORTED SMOKE FROM E
- [SDR DL76P040882](https://openairdocs.org/sdr/DL76P040882), Sep 15, 2004: SMOKE DETECTOR. MALFUNCTIONED. MID CABIN SMOKE ALARM WENT OFF ON T/O. F/A NOTIFIED CREW SHORTLY AFTER T/O. THOROUGHLY INSPECTED AIRCRAFT, RAN ENGINES AND SYSTEMS, UNABLE TO DUPLICATE.
- [SDR DL76P040694](https://openairdocs.org/sdr/DL76P040694), Jul 25, 2004: BULB. INOPERATIVE. ON LAYOVER FOUND EMERGENCY LIGHTS INOPERATIVE AT FWD F/A OVERHEAD AND AFT OVERHEAD AT SEAT 47 C AN E. RELAMPED OPERATION OK.
- [SDR DL76P040250](https://openairdocs.org/sdr/DL76P040250), Mar 20, 2004: POWER SUPPLY. INOPERATIVE. EMERGENCY PATH LIGHTS INOP IN FIRST CLASS. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK.
- [SDR DL76P021416](https://openairdocs.org/sdr/DL76P021416), Dec 5, 2002: ODOR. DETECTED. AFTER TAKE OFF, FLT ATTENDANT REPORTED STRANGE FUMES & ODOR IN MIDSECTION GALLEY AREA. LT ENGINE BLEED AND PACK TURNED OFF AND ODOR SUBSIDED & DISSIPATED. BLEED
- [SDR DL76P020666](https://openairdocs.org/sdr/DL76P020666), Jun 13, 2002: SKIN. DENTED. FUSELAGE / SKIN / FS 374 / STRG. 17L / SKIN LAP JOINT : DENT REPAIR THE FUSELAGE SKIN AT FS 374 AT THE STRINGER 17L LAP JOINT WAS DENTED. THE DENT WAS REMOVED W
- [SDR DL76P020536](https://openairdocs.org/sdr/DL76P020536), May 10, 2002: BOLT. SHEARED. ON TAXI OUT, GOT L/E ASYMMETRY T/S AND FOUND PROX SENSOR TARGET AT S286 LEFT SLAT NR 5 EXTEND PLATE MISSING AND ATTACH SCREW SHEARED. INSTALLED NEW TARGET AND A

All 54: https://openairdocs.org/deregistered/N144DA-2020-01-24/reports.md

## Other aircraft with N144DA

- [Registered now](https://openairdocs.org/aircraft/N144DA): Xag P150, S/N 1863FPEG82235080XF45

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