# N630DL: 1987 Boeing 757-232, registration cancelled 2017-05-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 16, 2017
- Status when cancelled: First renewal notice
- 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: 22920
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 19, 1987
- Certificate issued: June 18, 2010
- Last registry action: May 8, 2014
- Mode S code: A83E12
- 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/N630DL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=630DL
- Page: https://openairdocs.org/deregistered/N630DL-2017-05-16

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 (43)

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

- [SDR DALA1130440630](https://openairdocs.org/sdr/DALA1130440630), May 2, 2011: CONNECTOR. DAMAGED. DURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY PATH LIGHTS AT SEATS 19 - 22 INOPERATIVE. MAINTENANCE REPAIRED THE CONNECTOR AT SEAT 22. OPERATIONAL CHE
- [SDR DALA1127980630](https://openairdocs.org/sdr/DALA1127980630), Apr 20, 2011: CONNECTOR. DAMAGED. DURING A LAYOVER CHECK, MX FOUND THE EMERGENCY PATHLIGHTS AT SEATS 19DEF THROUGH 22DEF INOPERATIVE. MX REPAIRED A CONNECTOR. OPS CHECK WAS GOOD.
- [SDR DALA1030140630](https://openairdocs.org/sdr/DALA1030140630), Oct 28, 2010: LIGHT. INOPERATIVE. DURING LAYOVER CHECK MAINTENANCE FOUND SEAT 4CD EMERGENCY LIGHT ON THE SIDE PANEL TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND FOLLOW UP CHECK
- [SDR DL757092025](https://openairdocs.org/sdr/DL757092025), Dec 21, 2009: BULB. INOPERATIVE. EXTERIOR EMERGENCY LIGHTS INOP AT R2 DOOR. BOTH LT AND RT OVERWING AFT LOCATIONS. AND BOTH L3 AND R3 DOORS AND INTERIOR AT ROW 45. RELAMPED ALL LOCATIONS. LIGHT
- [SDR DL757091010](https://openairdocs.org/sdr/DL757091010), Jun 8, 2009: TEE FITTING. CRACKED. WHILE WORKING EA06-465922-03AD REV B ME-02 OPN0201, FOUND L4 DOOR NR 3 STOP FITTING SUPPORT TEE CRACKED AT RADIUS.
- [SDR DL757090866](https://openairdocs.org/sdr/DL757090866), May 15, 2009: ACOUSTIC PANEL. DELAMINATED. DURING SHOP VISIT, LARGE DELAMINATIONS WERE FOUND ON (PN 314N3011-4)ENGINE INLET ACOUSTIC PANEL, REQUIRING REPLACEMENT OF THE DELAMINATED SKINS. REPAIRED IAW ER
- [SDR DL757060821](https://openairdocs.org/sdr/DL757060821), Oct 4, 2006: CONTROLLER. MALFUNCTIONED. AC DID AN EMERGENCY DECENT DO TO LOSS OF CONTROL OF CABIN IN AUTO .5. NO FAULTS ON CABIN PRESS CONT 1 OR 2. ALL DOOR SEALS GOOD OVER PRESS VLVS NORMAL. REPLACED
- [SDR DL757060587](https://openairdocs.org/sdr/DL757060587), Jul 15, 2006: WARNING LIGHT. UNKNOWN. INTERMITTENT WHEEL WELL FIRE WARNING. PNEUMATIC DUCT REPLACED. FIRE CONTROL CARD REPLACED. ILSN VALVE REPLACED.
- [SDR DL757060571](https://openairdocs.org/sdr/DL757060571), Jul 10, 2006: CIRCUIT BOARD. FAULTY. FOUND READING LIGHT AT 28B BURNED OUT, HAD SMOKE AND ELECTRICAL SMELL. REPLACED CARD AND SWITCH. CHECKS GOOD. MCO AND PLACARD REMOVED.
- [SDR DU4R2006528](https://openairdocs.org/sdr/DU4R2006528), Jun 27, 2006: FRAME. CORRODED. CORROSION LEFT LOWER WING TO BODY FAIRING STRUCTURE BS 1037 BL 7 TO BL 30L. REMOVED CORRODED SECTION BL 7L TO BL 29L BS 1037. FABRICATED AND INSTALLED REPAIR PL
- [SDR DU4R2006530](https://openairdocs.org/sdr/DU4R2006530), Jun 25, 2006: FITTING. CORRODED. TWO CHORD FITTINGS CORRODED IN CABIN FRAME BS 1720, RBL 56 S-17R. REMOVED AND REPLACED 2 EA CHORD FITTINGS P/N 146N8722-16 AND 146N8726U2 IAW B757 SRM 51-10-2, 
- [SDR DU4R2006529](https://openairdocs.org/sdr/DU4R2006529), Jun 25, 2006: FITTING. CORRODED. TWO CORRODED AND ELONGATED HOLES IN TEE CHORD AT AFT PRESSURE BULKHEAD P/N 146N8726U2 AND 146N8722-16 BS 1720 RBL 57. OVERSIZED 2 EA HOLES AND INSTALLED FREEZE 
- [SDR DU4R2006501](https://openairdocs.org/sdr/DU4R2006501), Jun 23, 2006: TRANSITION PANEL. CORRODED. S/O 292018 NR 23829 CORROSION AFT PIT RT TRANSITION PANEL 1460 - 1530. REMOVED CORRODED PANEL. DRILLED ATTACHMENT HOLES AND INSTALLED NEW PANEL P/N 146N5391-51 
- [SDR DU4R2006498](https://openairdocs.org/sdr/DU4R2006498), Jun 21, 2006: TRANSITION PANEL. CORRODED. CORROSION ON AFT PIT TRANSITION PANEL BS 1310 - 1380 RT. FABRICATED AND INSTALLED TRANSITION PANEL SPLICE 10 X 10 INCHES FROM 7075-T6 .071" IAW SRM 53-60-53D.
- [SDR DU4R2006506](https://openairdocs.org/sdr/DU4R2006506), Jun 20, 2006: FLOOR SUPPORT. CORRODED. S/O 291018 NR 23848 CORROSION AROUND FASTENER HOLES ON FLOOR SUPPORT AFT PIT BS 1490 TO 1520, RBL 3. FABRICATED AND INSTALLED REPAIR CHANNEL 211/2 INCHES FROM B
- [SDR DU4R2006505](https://openairdocs.org/sdr/DU4R2006505), Jun 20, 2006: FLOOR SUPPORT. CORRODED. S/O 291018 NR 23847 CORROSION AROUND FASTENER HOLES ON FLOOR SUPPORT AFT PIT BS 1500 TO 1523, LBL 3. FABRICATED AND INSTALLED REPAIR CHANNEL 31 INCHES FROM BAC1
- [SDR DU4R2006504](https://openairdocs.org/sdr/DU4R2006504), Jun 20, 2006: FLOOR SUPPORT. CORRODED. S/O 291018 NR 23846 CORROSION AROUND FASTENER HOLES ON FLOOR SUPPORT AFT PIT BS 1500 TO 1520, LBL 7. FABRICATED AND INSTALLED REPAIR CHANNEL 19 INCHES FROM BAC1
- [SDR DU4R2006500](https://openairdocs.org/sdr/DU4R2006500), Jun 18, 2006: TRANSITION PANEL. CORRODED. CORROSION ON RT TRANSITION PANEL IN AFT PIT BS 1530 TO BS 1640. ROUTED OUT CORRODED AREAS IAW B757 MM 53-88-01-801. FABRICATED AND INSTALLED 2 EACH REPAIR DOUBL
- [SDR DU4R2006509](https://openairdocs.org/sdr/DU4R2006509), Jun 16, 2006: SEAT TRACK. CORRODED. S/O 291018 NR 23985 CORROSION ON CABIN SEAT TRACK AT OUTBD SIDE FLOOR PANEL ATTACH FLANGE BS 1117 RBL 47. FABRICATED AND INSTALLED SEAT TRACK REPAIR 106 X 3-1/2
- [SDR DU4R2006503](https://openairdocs.org/sdr/DU4R2006503), Jun 15, 2006: ANGLE. CORRODED. S/O 291018 NR 23842 CORROSION IN AFT PIT BS 1470 TO 1475, RBL 12 AROUND NUTPLATE HOLES, ANGLE. REMOVED CORRODED ANGLE. DRILLED, DEBURRED, ALODINED, PRIMED AND I
- [SDR DU4R2006502](https://openairdocs.org/sdr/DU4R2006502), Jun 15, 2006: INTERCOSTAL. CORRODED. S/O 291018 NR 23839 CORROSION IN AFT PIT BS 1478 INTERCOSTAL WEB RBL-11. FABRICATED AND INSTALLED INTERCOSTAL WEB 20.5" X 8.5" FROM 7075-T6 .040 IAW B757 SRM 51
- [SDR DU4R2006510](https://openairdocs.org/sdr/DU4R2006510), Jun 14, 2006: FITTING. CORRODED. S/O 291018 NR 24021 CORROSION ON CABIN CREASE BEAM UPPER FITTING AT BS 1720 BULKHEAD. REMOVED AND REPLACED FITTING P/N 146N8726U2 IAW B757 SRM 51-40-02.
- [SDR DU4R2006499](https://openairdocs.org/sdr/DU4R2006499), Jun 14, 2006: STRAP. CHAFED. CABIN FRAME STA 1640 S-10R CHORD/STRAP CHAFED. FABRICATED AND INSTALLED REPAIR STRAP FROM 7075-T6 IAW BOEING DWG 146N8738 REV V DATED 2-12-02 IAW B757 SRM 51-40
- [SDR DU4R2006490](https://openairdocs.org/sdr/DU4R2006490), Jun 13, 2006: TRANSITION PANEL. CORRODED. CORROSION FWD PIT LT TRANSITION PANEL BS 510 - 644. INSTALLED NEW TRANSITION PANEL P/N 143N366Y83 IAW B757 SRM 53-30-53 FIG 1, 53-00-53 FIG 101, 51-40-05 FIG 2,
- [SDR DU4R2006496](https://openairdocs.org/sdr/DU4R2006496), Jun 12, 2006: SHIM. CORRODED. CORROSION AT CABIN FLOOR SUPPORT BS 1676 BL 0. REMOVED CORROSION. SHIM OUT OF LIMITS. FABRICATED AND INSTALLED SHIM 2 X 15.75 INCHES FROM 7075-T6 .125" IAW B757
- [SDR DU4R2006489](https://openairdocs.org/sdr/DU4R2006489), Jun 12, 2006: SKIN. CORRODED. CORROSION LOWER FUSELAGE EXT SKIN AROUND FWD FASTENER HOLES OF PANEL 191AL BL 0 - LBL 17. FABRICATED AND INSTALLED REPAIR DOUBLER 10.4 X 8.3 INCHES FROM 20-24-T
- [SDR DU4R2006492](https://openairdocs.org/sdr/DU4R2006492), Jun 10, 2006: SKIN. CORRODED. CORROSION FWD CARGO FUSELAGE INTERNAL SKIN SURFACE B/O 0 BS 660. FABRICATED AND INSTALLED FUSELAGE SKIN REPAIR 8.3 X 7.75 INCHES FROM 2024-T3 .063 IAW B757 SRM 
- [SDR DU4R2006497](https://openairdocs.org/sdr/DU4R2006497), Jun 8, 2006: SUPPORT ANGLE. CORRODED. CORROSION ON CABIN L-4 DOOR SILL SUPPORT ANGLE BS 1681.8. REMOVED DOOR SILL SUPPORT ANGLE. FABRICATED AND INSTALLED ANGLE REPAIR 5 X 1 X 1 INCH FROM 7075-T6 .06
- [SDR DU4R2006495](https://openairdocs.org/sdr/DU4R2006495), Jun 7, 2006: TRANSITION PANEL. CORRODED. CORROSION ON AFT PIT LT TRANSITION PANEL BS 1200 TO 1310. REMOVED CORRODED TRANSITION. DRILLED FASTENER HOLES AND INSTALLED P/N 146N539U171 AND INSTALLED NUT PL
- [SDR DU4R2006494](https://openairdocs.org/sdr/DU4R2006494), Jun 7, 2006: SHEAR PLATE. CORRODED. CORROSION AT CABIN SUB-FLOOR B/O 0 TO RBL 50 BS 1716 (MAIN DECK FLOOR) SHEAR DECK PLATE RBL 25 CORRODED. REMOVED CORROSION RBL 28 TO RBL 50 WITHIN LIMITS. FABRI
- [SDR DU4R2006493](https://openairdocs.org/sdr/DU4R2006493), Jun 7, 2006: SKIN. CORRODED. CORROSION FWD CARGO PIT IN BILGE AT BS 850 B/O 0 WL 148.5 ON UPPER SURFACE OF THE LOWER SKIN. FABRICATED AND INSTALLED EXTERNAL DOUBLER 10.5 X 8.5 INCHES FROM 2
- [SDR DU4R2006507](https://openairdocs.org/sdr/DU4R2006507), Jun 6, 2006: CREASE BEAM. CORRODED. S/O 291018 NR 23878 CORROSION ON CABIN CREASE BEAM BS 660 TO 760 LT. REMOVED AND REPLACED L/H BS 660 - 760 CABIN CREASE BEAM P/N 143N8328U53 IAW B757 SRM 51-40-
- [SDR DU4R2006491](https://openairdocs.org/sdr/DU4R2006491), Jun 4, 2006: TRANSITION PANEL. CORRODED. CORROSION FWD PIT RT TRANSITION PANEL BS 560 - 644. INSTALLED NEW TRANSITION PANEL P/N 143N366U126 IAW B757 SRM 53-30-53 FIG 1, 53-00-53 FIG 101, 51-40-05 FIG 2
- [SDR DL757040316](https://openairdocs.org/sdr/DL757040316), Apr 8, 2004: ENGINE. FAILED. ENGINE FAILURE ON LEFT ENGINE WITH T/O POWER SET, BOTH FIRE BOTTLES DISCHARGED INTO ENGINE MAX EGT 762 DEG FOR 3.06 MINUTES. REPLACED ENGINE.
- [SDR DL757040317](https://openairdocs.org/sdr/DL757040317), Apr 5, 2004: SKIN. DENTED. THE FUSELAGE SKIN WAS FOUND DENTED BETWEEN STRINGERS 18L & 19L, JUST FWD OF THE FS 1618 SKIN BUTT SPLICE. THE DENTED AREA WAS REMOVED WITH A CUT OUT AND REPAIRE
- [SDR DL757021151](https://openairdocs.org/sdr/DL757021151), Sep 29, 2002: COFFEEMAKER. SHORTED. A/C 630 ON FLT 1107 HAD ATB TO SAV DUE TO F/C GALLEY COFFEE MAKER HAD AN ELECTRICAL SHORT AND CAUSED HAZE/SMELL IN FWD GALLEY/CABIN AREAS. CREW REPORTED NO SMOK
- [SDR DL757020071](https://openairdocs.org/sdr/DL757020071), Jan 20, 2002: WIRE. DAMAGED. LEFT ENGINE HYD MESSAGE AND OVERHEAD LIGHT CAME ON PRIOR TO T/O. REPAIRED SHIELDED WIRE 18 INCHES FROM CANNON PLUG IN LEFT ENGINE PYLON. INDICATION NOW NORMAL.
- [SDR DL757011928](https://openairdocs.org/sdr/DL757011928), Dec 11, 2001: LINE. FAILED. CENTER HYDRAULIC SYST QUANTITY LOSS WITH 'C HYD QTY' EICAS MSG. REPLACED FLEX LINE AT CENTER HYD BAY. LEAK CHECKS GOODSERVICED SYSTEM TO FULL.
- [SDR DL757001102](https://openairdocs.org/sdr/DL757001102), Jun 6, 2000: KEELBEAM. CORRODED. THE STRINGER 29R KEEL CHORD WAS FOUND BADLY CORRODED AT FS 1405. THE CHORD WAS CUT AT FS 1390 AND THE AFT SECTION OF CHORD REMOVED TO ELIMINATE THE CORROSION. A
- [SDR DL757001100](https://openairdocs.org/sdr/DL757001100), Jun 6, 2000: SKIN. LIGHTNING STRIKE. THE FUSELAGE CROWN SKIN BETWEEN FS 514 & 520 WAS DAMAGED IN TWO SPOTS BY LIGHTNING. THE DAMAGE WAS REMOVED WITH A 3.5 X 2.9 CUTOUT AND A 1.1 X 1.9 CUTOUT. BOTH 
- [SDR DL757990055](https://openairdocs.org/sdr/DL757990055), Jan 10, 1999: FIRE LIGHT. CONTAMINATED. AT FLIGHT LEVEL 350 EXPERIENCED MODERATE UNEXPECTED TURBULANCE, BOTTLED WATER SPILLED ON CENTER CONSOLE. DURING DESCENT TO FL 260 AFT CARGO FIRE LIGHT ILLUMINAT
- [SDR DL757961871](https://openairdocs.org/sdr/DL757961871), Aug 11, 1996: BATTERY PACK. DISCHARGED. ON L/O, FOUND 1ST CLASS EMERGENCY PATH LIGHTS INOP. REPLACED BATT PACK, CHECKS GOOD.
- [SDR DL757954061](https://openairdocs.org/sdr/DL757954061), Oct 19, 1995: BULB. FAILED. R2 EMERGENCY ESCAPE LIGHT IS INOP. RELAMPED, OPS CKS GOOD.

## FAA accident and incident reports (4)

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 19980607026489I](https://openairdocs.org/incident/19980607026489I), Jun 7, 1998: Boeing 757232 (N630DL), Albuquerque, NM, No damage. On June 7, 1998, at 2009 MDT, a delta flight 491, a Boeing 757, diverted to Albuquerque International Airport on a flight from kennedy airport, new york city,…
- [Incident 19921013044759I](https://openairdocs.org/incident/19921013044759I), Oct 13, 1992: Boeing 757232 (N630DL), Covington - Cin, OH. Pilot had flap lock-out after takeoff. Returned. Landed safely. Found a faulty left wing inboard flap-loss switch.
- [Incident 19891016060369I](https://openairdocs.org/incident/19891016060369I), Oct 16, 1989: Boeing 757232 (N630DL), Portland, OR. Unable to lower flaps. Did a go around and used alternate method. Landed without incident. Unable to dupicate.
- [Incident 19890628039019I](https://openairdocs.org/incident/19890628039019I), Jun 28, 1989: Boeing 757232 (N630DL), Portland, ME. Failure of left engine. Returned. Engine was replaced. Cause not stated.

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