# N628DL: 1987 Boeing 757-232, registration cancelled 2018-08-21

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 21, 2018
- Status when cancelled: Valid registration
- Airframe: [Boeing 757-232](https://openairdocs.org/model/boeing-757-232) (registry code 1384965)
- Engine: [Pratt & Whitney PW2037](https://openairdocs.org/engine/pratt-whitney-pw2037) (registry code 52117)
- Data sheets: [TCDS A2NM](https://openairdocs.org/tcds/A2NM), [TCDS E17NE](https://openairdocs.org/tcds/E17NE) (OpenAirDocs)
- Serial number: 22918
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 28, 1987
- Certificate issued: November 14, 2017
- Last registry action: November 14, 2017
- Mode S code: A8344B
- 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/N628DL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=628DL
- Page: https://openairdocs.org/deregistered/N628DL-2018-08-21

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 757-232: https://openairdocs.org/model/boeing-757-232.md

## Service difficulty reports (73, newest 50)

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

- [SDR DALA1122080628](https://openairdocs.org/sdr/DALA1122080628), Mar 28, 2011: WIRE. SHORTED. FLIGHT RETURNED TO ATL AFTER CABIN CREW REPORTED SPARKS AND A STRONG ELECTRICAL SMELL COMING FROM AN OVERHEAD LIGHT ASSEMBLY. CABIN LIGHTING WAS TURNED OFF. MAI
- [SDR DALA1108340628](https://openairdocs.org/sdr/DALA1108340628), Feb 2, 2011: LIGHT. DEFECTIVE. CREW REPORTED AN ELECTRICAL ODOR IN THE AFT CABIN. TURNED OFF UTILITY BUSSES AND RECYCLED PACK BLEEDS PER MCC. ODOR IMPROVED WITH CABIN LIGHTS TURNED OFF. MAINT
- [SDR DALA1026610628](https://openairdocs.org/sdr/DALA1026610628), Oct 9, 2010: SOCKET. INOPERATIVE. DURING LAYOVER CHECK FOUND DOOR 3L EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED SOCKET.
- [SDR DALA1021040628](https://openairdocs.org/sdr/DALA1021040628), Aug 29, 2010: WIRE. DAMAGED. DURING LAYOVER CHECK, MX FOUND THE MID LAVATORY AREA EMERGENCY PATH LIGHTS INOPERATIVE. MX REPAIRED THE PATH LIGHT WIRING. OPS CHECK WAS GOOD.
- [SDR DL757100067](https://openairdocs.org/sdr/DL757100067), Jan 11, 2010: BULB. BURNED OUT. ELECTRICAL ODOR 1L LAV. NO ELECTRICAL ODOR. FOUND HOT PLASTIC ODOR COMING FROM OVERHEAD BULB. REPLACED BULB, CKS OK.
- [SDR DL757090679](https://openairdocs.org/sdr/DL757090679), Apr 16, 2009: WARNING SYSTEM. INTERMITTENT. ON TAKEOFF R2 DOOR HANDLE RAISED UP FROM LOCKED POSITION DOOR WARNING INTERMITTENT IN COCKPIT. R2 DOOR MTC IN PROGRESS.
- [SDR DALA1165610628](https://openairdocs.org/sdr/DALA1165610628), Apr 5, 2009: GEARBOX. DAMAGED. T/E FLAP TRANSMISSION GEARBOX REPAIRED IAW EA 06-097281-03, ME04.
- [SDR DL757090007](https://openairdocs.org/sdr/DL757090007), Jan 2, 2009: FAN. OVERHEATED. GOT AN ELECTRICAL ODOR FOLLOWED BY "EQPT OVHT" MESSAGE. RAN EQUIP OVHT CKLIST AND ODOR DISSIPATED. FOUND NR 1 EQUIP COOL FAN INOP. REPLACED NR 1 EQUIP COOLING F
- [SDR DALA1165710628](https://openairdocs.org/sdr/DALA1165710628), Nov 28, 2007: PLENUM. UNKNOWN. AIRBORNE AUX POWER AIR INTAKE PLENUM REPLACED IAW ERA 465354-14.
- [SDR DL757071568](https://openairdocs.org/sdr/DL757071568), Nov 28, 2007: BELLMOUTH. CRACKED. APU AIR INTAKE PLENUM BELLMOUTH CRACKED. MODIFED BELLMOUTH PER SERVICE BULLETIN 757-49-0011.
- [SDR DU4R2006445](https://openairdocs.org/sdr/DU4R2006445), May 16, 2006: FITTING. WORN. NR 2 PYLON FOUND LWR FWD OUTBOARD LUG TO BE 2.008, OVERSIZED SHOULD BE > 2.009. REPAIRED BY FABRICATING AND INSTALLING BUSHING 1.748 ID FROM 15-5 PH IAW DELTA E
- [SDR DU4R2006444](https://openairdocs.org/sdr/DU4R2006444), May 16, 2006: FRAME. MISDRILLED. NR 2 PYLON INBOARD LOWER CHORD FROM PPS 128 TO PPS 138 HAS 8 EACH DRILL MARKS BESIDE FASTENER HOLES. REPAIRED FASTENER HOLES BY FABRICATING AND INSTALLING FREEZ
- [SDR DU4R2006426](https://openairdocs.org/sdr/DU4R2006426), May 11, 2006: TRIPLER. CORRODED. CORROSION ON FUSELAGE SKIN TRIPLER BS 1466 TO 1478 WL 138.5 BL 0. REMOVED TRIPLER, FABRICATED AND INSTALLED REPAIR TRIPLER 23 X 12.5 INCHES FROM 2024-T3 .063 IA
- [SDR DU4R2006443](https://openairdocs.org/sdr/DU4R2006443), May 10, 2006: ATTACH ANGLE. CORRODED. CORROSION ON INTERCOSTAL ATTACH ANGLE IN AFT PIT BS 1320 RBL 6. FABRICATED AND INSTALLED INTERCOSTAL ATTACH ANGLE 6.75 X 1.25 X 1.25 INCHES FROM 7075-T6 .063 IA
- [SDR DU4R2006442](https://openairdocs.org/sdr/DU4R2006442), May 10, 2006: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL LWR LEG IN AFT PIT BS 1480 - 1500 LBL 24. REMOVED INTERCOSTAL, FABRICATED AND INSTALLED INTERCOSTAL ANGLE 16.25 X 2.25 INCHES FROM 7075
- [SDR DU4R2006440](https://openairdocs.org/sdr/DU4R2006440), May 6, 2006: SHEAR TIE. CORRODED. CORROSION ON BS 1400 FRAME SHEAR TIE S-26R. REMOVED SHEAR TIE, FABRICATED AND INSTALLED SHEAR TIE 6.25 X 2.0 INCHES FROM L-ANGLE EXTRUSION 7075-T6 .100" IAW B75
- [SDR DU4R2006435](https://openairdocs.org/sdr/DU4R2006435), May 5, 2006: SHEAR TIE. CORRODED. CORROSION AFT PIT ON FRAME AND FRAME SHEAR TIE BS 1500 S-29L TO S-27L. REMOVED CORROSION ON FRAME, FOUND TO BE WITHIN LIMITS. REMOVED CORRODED SHEAR TIES, FABRI
- [SDR DU4R2006434](https://openairdocs.org/sdr/DU4R2006434), May 5, 2006: INTERCOSTAL. CORRODED. CORROSION NOTED ON AFT PIT FLOOR STRUCTURE INTERCOSTAL WEB BS 1460 - 1480 RT. REMOVED CORRODED INTERCOSTAL. FABRICATED AND INSTALLED INTERCOSTAL 19.375 X 7.5 IN
- [SDR DU4R2006433](https://openairdocs.org/sdr/DU4R2006433), May 5, 2006: PANEL. CORRODED. CORROSION NOTED ON AFT PIT PANEL BS 1440 - 1530 RT. REMOVED CORRODED PANEL AND INSTALLED P/N 146N5391-30 IAW B757 SRM 51-10-01 AND 51-40-02.
- [SDR DU4R2006427](https://openairdocs.org/sdr/DU4R2006427), May 5, 2006: ANGLE. CORRODED. CORROSION ON TRANSITION ANGLE, FROM BS 1310 TO 1380 RT SIDE (ENTIRE LENGTH). REMOVED CORROSION. FABRICATED AND INSTALLED REPAIR DOUBLER 40.75 INCHES FROM 2024-T
- [SDR DU4R2006437](https://openairdocs.org/sdr/DU4R2006437), May 4, 2006: INTERCOSTAL. CORRODED. CORROSION AFT PIT INTERCOSTAL BS 1540 - BS 1560 LT. FABRICATED AND INSTALLED INTERCOSTAL 19.50 X 3.75 INCHES FROM 7075-T6 .032" IAW BOEING DWG 146N5461-15 AND 5
- [SDR DU4R2006431](https://openairdocs.org/sdr/DU4R2006431), May 3, 2006: TRANSITION PANEL. CORRODED. LEFT TRANSITION PANEL BS 1410 - 1530 CORRODED BA 1410 TO BS 1530 LT. REMOVED CORRODED PANEL. INSTALLED FABRICATED AND INSTALLED REPLACEMENT WEB 20.875 X 2.75 IN
- [SDR DU4R2006436](https://openairdocs.org/sdr/DU4R2006436), May 1, 2006: TRANSITION PANEL. CORRODED. CORROSION AFT PIT ON RT TRANSITION PANEL BETWEEN BS 1530 TO 1640. FABRICATED AND INSTALLED TRANSITION PANEL REPAIRS 63 X 1.5 INCHES FROM 2024-T3 .063 AND 64 X 3
- [SDR DU4R2006430](https://openairdocs.org/sdr/DU4R2006430), May 1, 2006: TRANSITION PANEL. CORRODED. CORROSION AFT PIT ON LT TRANSITION PANEL NUMEROUS AREAS FROM BS 1530 TO 1640. REMOVED CORRODED TRANSITION PANEL AND INSTALLED NEW PANEL P/N 146N5431-41 IAW B757
- [SDR DU4R2006432](https://openairdocs.org/sdr/DU4R2006432), May 1, 2006: DOOR FRAME. CORRODED. CORROSION LT AC BAY DOOR HINGE FRAME FROM BS 900 TO 1040. FABRICATED AND INSTALLED REPLACEMENT BEAM 38 X 1.625 X 2.875 X 1.5 INCHES FROM BAC1505-10047 IAW B757 
- [SDR DU4R2006428](https://openairdocs.org/sdr/DU4R2006428), May 1, 2006: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT STRUCTURE UPPER WEB FROM BS 1320 - 1340 ABOVE S-30, RBL 9. REMOVED CORRODED WEB. FABRICATED AND INSTALLED REPLACEMENT WEB 20.875 X 2.
- [SDR DL757060356](https://openairdocs.org/sdr/DL757060356), May 1, 2006: SPAR. DAMAGED. THE NR 2 PYLON INBOARD MID SPAR CHORD HAS 3 ELONGATED HOLES. HOLES WERE OVERSIZED TO CLEAN UP THE DAMAGE AND BUSHED TO ORIGINAL SIZE AND LOCATION.
- [SDR DU4R2006429](https://openairdocs.org/sdr/DU4R2006429), Apr 30, 2006: WEB. CORRODED. CORROSION ON AFT PIT FLOOR STRUCTURE WEB FROM BS 1320 - 1340 LT LBL 9. REMOVED CORRODED WEB. FABRICATED AND INSTALLED REPLACEMENT WEB 20.875 X 2.75 INCHES FROM 
- [SDR DU4R2006424](https://openairdocs.org/sdr/DU4R2006424), Apr 28, 2006: FLOORBEAM. CORRODED. FOUND CORROSION, AFT PIT, ON FLOOR SUPPORT ANGLE LWR SIDE BS 1510 LBL 7. FABRICATED AND INSTALLED REPAIR ANGLE 10 X .75 X .75 INCH FROM 7075-T6 .080 IAW B757 SR
- [SDR DU4R2006423](https://openairdocs.org/sdr/DU4R2006423), Apr 28, 2006: FLOORBEAM. CORRODED. FOUND CORROSION AFT PIT ON FLOOR SUPPORT ANGLE LWR SIDE BS 1510, LBL 3. FABRICATED AND INSTALLED REPAIR ANGLE 10 INCHES LONG FROM 7075-T6 .080 IAW B757 SRM 53-6
- [SDR DU4R2006422](https://openairdocs.org/sdr/DU4R2006422), Apr 28, 2006: FLOORBEAM. CORRODED. FOUND CORROSION AFT PIT ON FLOOR SUPPORT ANGLE LWR SIDE BS 1510, RBL 7. FABRICATED AND INSTALLED REPAIR ANGLE 8.75 INCHES LONG FROM 7075-T6 .080 IAW B757 SRM 53
- [SDR DUR42006417](https://openairdocs.org/sdr/DUR42006417), Apr 27, 2006: SKIN. DENTED. FOUND CREASE 28" AFT OF L-4 DOOR AT SILL LEVEL. CUT OUT CREASED AREA IAW B757 SRM 53-00-01 FIG 201. HFEC FOR CRACKS IAW D6-34N301-6-51-00P6. FABRICATED AND INST
- [SDR DUR42006416](https://openairdocs.org/sdr/DUR42006416), Apr 27, 2006: FRAME. DENTED. FOUND FRAME DENTED AT S-25L IN AFT PIT BS 1480. CUT OUT DENTED AREA IAW B757 SRM 51-70-11. FABRICATED AND INSTALLED FORMED SECTION REPAIR 210.50" BY 4.75" FROM 
- [SDR DUR42006413](https://openairdocs.org/sdr/DUR42006413), Apr 26, 2006: FLOOR SUPPORT. CORRODED. FOUND CORROSION AROUND NUTPLATES ON FLOOR SUPPORT RBL NR 10, NR 45 SEVERAL AREAS FROM BS 1400 TO BS 1440. FABRICATED AND INSTALLED REPAIR SUPPORT 102-1/8" FROM 
- [SDR DU4R2006403](https://openairdocs.org/sdr/DU4R2006403), Apr 26, 2006: PANEL. CORRODED. FOUND CORROSION ON RT TRANSITION STRIP BETWEEN BS 645 AND 765 (FWD CARGO). FABRICATED AND INSTALLED REPAIR DOUBLER 6-1/4" BY 2.5" BY 1-1/4" BY 3/4" FROM 7075 T6
- [SDR DU4R2006401](https://openairdocs.org/sdr/DU4R2006401), Apr 26, 2006: FLOOR SUPPORT. CORRODED. FOUND CORROSION ON FLOOR SUPPORT AT BS 1340 LBL 16 ABOVE S-29L (AFT PIT). FABRICATED AND INSTALLED DOUBLER REPAIR 5-3/4" FROM 301 .032 HD AND REPAIR SUPPORT 17"
- [SDR DU4R2006408](https://openairdocs.org/sdr/DU4R2006408), Apr 25, 2006: SKIN. PUNCTURED. FOUND PUNCTURED HOLE IN EXTERNAL FUSELAGE SKIN BS 1927 LBL 5.5, ABOVE APU. CUT OUT AND REMOVED PUNCTURED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER 4.25" IN 
- [SDR DU4R2006402](https://openairdocs.org/sdr/DU4R2006402), Apr 25, 2006: FRAME. CORRODED. FOUND CORROSION ON FRAME ANGLE BS 1360 BETWEEN S-27L AND S-25L (AFT PIT). FABRICATED AND INSTALLED CHANNEL REPAIR 31" BY 3" FROM 2024-T3 .050" IAW B757 SRM 51-2
- [SDR DU4R2006438](https://openairdocs.org/sdr/DU4R2006438), Apr 24, 2006: INTERCOSTAL. CORRODED. CORROSION ON FLOOR STRUCTURE AT L4 DOOR BETWEEN BS 1640 TO 1681. FABRICATED AND INSTALLED 2 EACH INTERCOSTAL WEBS 21.75 X 3.5 X 1.8 INCHES FROM 7075-T6 .071" IA
- [SDR DU4R2006411](https://openairdocs.org/sdr/DU4R2006411), Apr 24, 2006: CUSP WEB. CORRODED. FOUND CORROSION AT CABIN FLOOR STRUCTURE RBL 65 BS 996. FABRICATED AND INSTALLED REPAIR STIFFENER 3-3/4" BY 3-7/8" FROM 7075-T6 .090" IAW B757 SRM 53-40-13, 51-
- [SDR DU4R2006410](https://openairdocs.org/sdr/DU4R2006410), Apr 24, 2006: INTERCOSTAL. CORRODED. FOUND CORROSION IN AFT PIT ON FRAME UPPER ANGLE BS 1560, S-26R TO S-23R (UPPER SURFACE). CUT OUT CORRODED "C" CHANNEL. FABRICATED AND INSTALLED REPAIR "C" CHANN
- [SDR DU4R2006407](https://openairdocs.org/sdr/DU4R2006407), Apr 24, 2006: FLOOR SUPPORT. CORRODED. FOUND CORROSION ON FLOOR STRUCTURE AT R-4 DOOR BETWEEN BS 1640 AND BS 1681. REMOVED CORRODED FLOOR SUPPORT. FABRICATED AND INSTALLED FORMED SECTION REPAIRS 3.5"
- [SDR DU4R2006404](https://openairdocs.org/sdr/DU4R2006404), Apr 24, 2006: INTERCOSTAL. CORRODED. FOUND CORROSION ON WEB AT FWD END AT SKIN BELOW FLOOR SUPPORT RBL 2.90 FROM BS 1400 TO 1420 (AFT CARGO). REMOVED CORRODED INTERCOSTAL. FABRICATED AND INSTALLED 
- [SDR DU4R2006400](https://openairdocs.org/sdr/DU4R2006400), Apr 24, 2006: PANEL. CORRODED. FOUND CORROSION ON NUMEROUS AREAS OF TRANSITION ANGLE FROM BS 1200 TO 1310 RT. DRILLED AND INSTALLED NEW TRANSITION PANEL IAW B757 SRM 53-00-53 FIG 101.
- [SDR DU4R2006425](https://openairdocs.org/sdr/DU4R2006425), Apr 21, 2006: FRAME. CORRODED. FOUND CORROSION, AFT PIT, ON ATTACH ANGLE FOR FLOOR AND SIDEWALL PANELS (ALSO MISDRILLED HOLES, LOOSE FASTENERS) BS 1640 S-22R TO S-22L. FABRICATED AND INSTALLE
- [SDR DUR42006415](https://openairdocs.org/sdr/DUR42006415), Apr 19, 2006: FLOORBEAM. CORRODED. FOUND CORROSION ON FLOORBEAM BETWEEN R-1 AND L-1 DOORS BS 345. FABRICATED AND INSTALLED REPLACEMENT UPPER CAP 11 FEET BY 2" FROM BAC1505-100617 7075-T73 IAW B75
- [SDR DUR42006414](https://openairdocs.org/sdr/DUR42006414), Apr 19, 2006: INTERCOSTAL. CORRODED. FOUND CORROSION IN AFT PIT ON WEB BS 1600 TO 1620 INBD OF S-28L. FABRICATED AND INSTALLED INTERCOSTAL 19-5/8" BY 7-1/2" FROM 7075-T6 .040 IAW B757 SRM 51-20-01 
- [SDR DU4R2006409](https://openairdocs.org/sdr/DU4R2006409), Apr 19, 2006: FLOORBEAM. CORRODED. FOUND CORROSION ON FLOOR FRAME UPPER SURFACE, BS 700 INBD OF L2 DOOR AND UNDER CENTER FLOOR PANEL. CUT OUT CORRODED AREA. FABRICATED AND INSTALLED REPAIR DOUBLE
- [SDR DU4R2006439](https://openairdocs.org/sdr/DU4R2006439), Apr 17, 2006: SEAT TRACK. CORRODED. CORROSION ON LEFT O/B SEAT TRACK BS 1027. FABRICATED AND INSTALLED SEAT TRACK BS 898 TO BS 1075 177 INCHES FROM BAC1520-541 IAW B757 SRM 51-40-02 AND 53-00-52.
- [SDR DU4R2006418](https://openairdocs.org/sdr/DU4R2006418), Apr 17, 2006: FLOORBEAM. CORRODED. FOUND CORROSION ON UPPER SURFACE OF FLOORBEAM AT BS 720 INBD OF L2 DOOR AND UNDER CENTER FLOOR PANEL. FABRICATED AND INSTALLED FLOORBEAM REPAIR 12.25" BY 1.75" 

All 73: https://openairdocs.org/deregistered/N628DL-2018-08-21/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 NYC88IA112](https://openairdocs.org/ntsb/NYC88IA112), Mar 22, 1988: Boeing 757 (N628DL), Providence, RI, incident, no damage

## 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 19930624028669I](https://openairdocs.org/incident/19930624028669I), Jun 24, 1993: Boeing 757232 (N628DL), Lagrange, GA. Encountered severe clear air turbulance starting descent. Seat belt sign on. Cabin crew in process of securing cabin

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