# N2807W: Boeing 727-247, registration cancelled 2000-02-29

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 29, 2000
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 727-247](https://openairdocs.org/model/boeing-727-247) (registry code 138408F)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE) (OpenAirDocs)
- Serial number: 20579
- Type of aircraft: Fixed wing multi engine
- Certificate issued: April 14, 1987
- Last registry action: June 15, 1999
- Mode S code: A2D15D
- 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: 33.7490° N, 84.3880° W: Placed by OpenAirDocs: center of Atlanta, GA, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N2807W
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=2807W
- Page: https://openairdocs.org/deregistered/N2807W-2000-02-29

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 727-247: https://openairdocs.org/model/boeing-727-247.md

## Service difficulty reports (42)

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

- [SDR DL72W991926](https://openairdocs.org/sdr/DL72W991926), Aug 29, 1999: SKIN. CORRODED. THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION BETWEEN FS 720 & 720A AND BETWEEN S-28L & 28R. THE DAMAGE WAS ADJACENT TO AN EXISTING REPAIR CUTOUT. THE E
- [SDR DL72W991196](https://openairdocs.org/sdr/DL72W991196), May 27, 1999: LINE. CHAFED. CLIMBING THROUGH 13,000 FEET B-HYD SYSTEM FLUID QTY DECREASE TO ZERO AND BOTH B-SYSTEM PUMP LIGHTS ILLUMINATED. CHECKLIST PERFORMED SAFETY WIRE CUT ON GPWS AND 
- [SDR DL72W990276](https://openairdocs.org/sdr/DL72W990276), Feb 10, 1999: SKIN. CRACKED. FUSELAGE SKIN FS 548, STRG 4R SKIN LAP SPLICE, CRACK REPAIR. EXTERNAL LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SHOWED A CRACK INDICATION AT FS 548. INTERNAL 
- [SDR DL72W990068](https://openairdocs.org/sdr/DL72W990068), Dec 16, 1998: ANGLE. CORRODED. CORROSION ON SECONDARY HEAT EXCHANGER CLOSE OUT PANEL ATTACH ANGLE LT SIDE I/B ANGLE. INSTALLED REPAIR PER MM 53-30-1.
- [SDR DL72W990042](https://openairdocs.org/sdr/DL72W990042), Dec 15, 1998: ANGLE. CRACKED. A 2 INCH VISIBLE CRACK RT LOWER TORQUE BOX SUPPORT ANGLE BELOW AIRSTAIR ACTUATOR ATTACH FITTING STA 1263 RT (MARKED). REPLACED PART PER SRM 53-10-10.
- [SDR DL72W982645](https://openairdocs.org/sdr/DL72W982645), Dec 15, 1998: RIB. CRACKED. FOUND DURING MV2/F-1 LETTER CHECK, .75 INCH CRACK AT NR 2 SLAT NOSE RIB O/B SIDE OF ACTUATOR AT AFT LWR CORNER. REPAIRED PER M/M 57-54-0.
- [SDR DL72W982589](https://openairdocs.org/sdr/DL72W982589), Dec 15, 1998: RIB. CRACKED. FOUND DURING MV2/F 1 LETTER CHECK, .75 INCH CRACK AT NR 3 SLAT NOSE RIB O/B SIDE OF ACTUATOR AFT LWR CORNER. REPAIRED PER M/M 57-54-0.
- [SDR DL72W982656](https://openairdocs.org/sdr/DL72W982656), Dec 13, 1998: BULKHEAD ANGLE. CRACKED. REF NR 214, 215, 216, 217, 218 AND 219 REPAIRED STA 178 BLKHD AND REPLACED UPPER AND LWR ANGLES PER SRM 53-10-9 FIG 14. COMPLETED AND FORWARDED DATA RETRIEVAL.
- [SDR DL72W982556](https://openairdocs.org/sdr/DL72W982556), Dec 12, 1998: BATTERY PACK. DISCHARGED. EMERG EXIT LIGHT ABOVE L1 DOOR WEAK DURING TEST. REPLACED BATTERY PACK.
- [SDR DL72W981123](https://openairdocs.org/sdr/DL72W981123), May 26, 1998: WEB. CRACKED. A .5 INCH CRACK LIGHTENING HOLE STA 1248 ON AIRSTAIR CUTOUT VERTICAL WEB LT SIDE. A .25 INCH CRACK LIGHTENING HOLE STA 1228 ON AIRSTAIR CUTOUT VERTICAL WEB RT S
- [SDR DL72W981122](https://openairdocs.org/sdr/DL72W981122), May 26, 1998: SKIN. CRACKED. A .5 INCH CRACK ON A/C SKIN FROM RT SIDE OF AIRSTAIR CUTOUT FWD SIDE. REPAIRED PER MM 53-30-0 P 803.
- [SDR DL72W981121](https://openairdocs.org/sdr/DL72W981121), May 26, 1998: SKIN. DELAMINATED. T/E OF LT AND RT ELEV DELAMINATED FROM I/B EDGE TO 15 INCHES O/B OF ELEV TAB. REPAIRED PER MM 55-20-0 P 801.
- [SDR DL72W972518](https://openairdocs.org/sdr/DL72W972518), Dec 1, 1997: BEAR STRAP. CORRODED. THE R2 DOOR SURROUND BEAR STRAP WAS FOUND CORRODED APPROX 5 ABOVE THE SKIN LAP SPLICE. THE CORROSION WAS REMOVED WITH A 2.25 X 2.25 CUTOUT IN THE BEARSTRAP. THE
- [SDR DL72W972323](https://openairdocs.org/sdr/DL72W972323), Nov 10, 1997: PUMP. LEAKING. ON CLIMBOUT WITH B-SYS PUMP NR 2 B PRESSURE STARTED TO DROP TOWARD ZERO. SWAPPED B-PUMPS THEM B-SYS HYD QTY DROPPED TO ZERO. REPLACED HYD PUMP.
- [SDR DL72W972219](https://openairdocs.org/sdr/DL72W972219), Oct 31, 1997: WIRE. CROSSED. RT AFT EXTERIOR EMERGENCY LIGHT INOP. FOUND WIRES SWAPPED AT PLUG D5024. REPAIRED SAME AND REPLACED M957 FOR FUSES BLOWN, SYS CHKS GOOD.
- [SDR DL72W972134](https://openairdocs.org/sdr/DL72W972134), Oct 22, 1997: BRACKET. CRACKED. 1.5 INCH VISIBLE CRACK IN NR 1 SLAT ACTUATOR ATTACH BRACKET I/B SIDE, FOUND AT E1 LTR CK. REPAIR PER M/M 57-20-21.
- [SDR DL72W971352](https://openairdocs.org/sdr/DL72W971352), Jul 10, 1997: CLAMP. FAILED. ON CLIMBOUT, GOT NUMBER 1 ENGINE FIRE WARNING, BOTH LOOPS AND BELL. RETARDED THE THROTTLE AND FIRE WARNING LIGHTS AND BELL WENT OUT. DID NOT SHUT DOWN ENGINE, D
- [SDR DL72W970793](https://openairdocs.org/sdr/DL72W970793), Apr 28, 1997: ACTUATOR. DESTROYED. ON CLIMBOUT THROUGH 7,000 FEET, THE A-SYSTEM HYDRAULIC QUANTITY WENT TO ZERO AND THE PRESSURE WENT TO ZERO, FOLLOWED POM. FOUND THE NR 4 SLAT ACTUATOR CASTING E
- [SDR DL72W970633](https://openairdocs.org/sdr/DL72W970633), Apr 1, 1997: BULKHEAD WEB. CRACKED. BS 1183 BULKHEAD FOUND CRACKED IN THE WEB. STOPPED DRILLED AND REPAIRED TO SRM 53-10-9, FIG. 4.
- [SDR DL72W970436](https://openairdocs.org/sdr/DL72W970436), Mar 8, 1997: HYD MODULE. CRACKED. SYS-A HYD QTY LEAKED BELOW 2.5 GALS COMPLETED POM PROCEDURES LEAK STOPPED WITH PRESSURE OFF. FOUND A-SYS MODULE LEAKING. BORROWED PART FROM FEDX (S/N 260SA), IN
- [SDR DL72W962735](https://openairdocs.org/sdr/DL72W962735), Dec 18, 1996: SKIN. CRACKED. INNER SKIN CRACKED BETWEEN RIBS 10/11. REPAIRED PER M/M 57-54-0.
- [SDR DL72W961520](https://openairdocs.org/sdr/DL72W961520), Jun 24, 1996: DOOR. CRACKED. THE R-1 DOOR WAS FOUND CRACKED AT THE UPPER FWD CORNER. REPAIRED PER 52-12-0, FIG 805.
- [SDR DL72W961509](https://openairdocs.org/sdr/DL72W961509), Jun 22, 1996: LIGHT. INOPERATIVE. R2 ABOVE DOOR EXIT EMERGENCY LIGHT INOP. REPLACED EXIT LIGHT AND BATTERIES, CKS NORMAL.
- [SDR DL72W961411](https://openairdocs.org/sdr/DL72W961411), May 19, 1996: SKIN. CRACKED. DURING INSPECTION, FOUND 1 INCH CRACK IN THE UPPER FWD CORNER OF THE L-1 DOOR CUTOUT. REPAIRED PER ER/A 303614-14AD.
- [SDR DL72W961290](https://openairdocs.org/sdr/DL72W961290), May 19, 1996: SKIN. FATIGUE. THE FUSELAGE SKIN AND UNDERLYING DOUBLER WAS FOUND TO HAVE A ONE INCH CRACK IN THE UPPER FWD CORNER OF THE L-1 DOOR CUTOUT. REPAIRED PER DAL ER/A 303614-14AD.
- [SDR DL72W960318](https://openairdocs.org/sdr/DL72W960318), Feb 6, 1996: WEB. CRACKED. DURING INSPECTION, THE LT SIDEWALL WEB OF THE NOSE WHEEL WELL HAS A 1.25 INCH CRACK BETWEEN STA 294.5 AND 285.5, APPROXIMATELY AT WL 170. THE REPAIR IS ACCOMPLI
- [SDR DL72W960270](https://openairdocs.org/sdr/DL72W960270), Feb 5, 1996: ANGLE. CRACKED. FOUND ON C-2 LETTER CHECK, COVE SKIN SUPPORT ANGLE CRACKED .0625 INCH BELOW NR 7 SLAT ANTI-ICE DUCT. REPAIRED PER MM 57-54-0.
- [SDR DL72W960109](https://openairdocs.org/sdr/DL72W960109), Jan 13, 1996: BUSHING. WORN. ON CLIMBOUT FROM RIC AT 360 KTS, THE NOSE WHEEL DOORS WERE SLAMMING OPEN AND SHUT REPEATEDLY. FOUND NLG DOOR OUT OF RIG AND BUSHINGS WORN IN ROD ON FWD QUAD. RE
- [SDR DL72W962734](https://openairdocs.org/sdr/DL72W962734), Dec 18, 1995: SKIN. CRACKED. AFT LOWER SKIN CRACKED I/B END. REPAIRED PER M/M 57-54-0.
- [SDR DL72W954568](https://openairdocs.org/sdr/DL72W954568), Nov 29, 1995: BATTERY. DISCHARGED. DURING LAYOVER, MTC FOUND EMERGENCY LIGHT ABOVE AFT RIGHT SERVICE DOOR WOULD NOT TEST. REPLACED BATTERIES, NOW OPERATION IS NORMAL.
- [SDR DL72W954269](https://openairdocs.org/sdr/DL72W954269), Oct 30, 1995: SKIN. CORROSION. ADDITIONAL CORROSION WAS CUT OUT JUST AFT OF FS 720A. THE NEW CUT OUT AND THE PREVIOUS CUT OUT ARE SEPARATED BY APPROXIMATELY 5.5 INCHES. THE ORIGINAL DOUBLER W
- [SDR DL72W954263](https://openairdocs.org/sdr/DL72W954263), Oct 30, 1995: SKIN. CORROSION. AT CV2 IN TPA, CORROSION WAS DISCOVERED ON THE FUSELAGE SKIN BETWEEN STA 1010 AND 1030 STR 23R AND 24R. A SECTION OF THE BONDED DOUBLER AT STR 24R AND TWO AREAS
- [SDR DL72W954041](https://openairdocs.org/sdr/DL72W954041), Oct 16, 1995: BATTERY. DISCHARGED. AFT RIGHT SERVICE DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES, CHECKS NORMAL.
- [SDR DL72W954040](https://openairdocs.org/sdr/DL72W954040), Oct 15, 1995: BATTERY PACK. DISCHARGED. FWD RT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED RACK AND BATTERIES, OPERATION NORMAL.
- [SDR DL72W953151](https://openairdocs.org/sdr/DL72W953151), Jul 4, 1995: ANGLE. CRACKED. CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM OF THE RT TORQUE BOX AT STA 1263. REPAIRED PER DL ERA 302068-14AD.
- [SDR DL72W952916](https://openairdocs.org/sdr/DL72W952916), Jul 3, 1995: SKIN. CRACKED. RT ELEVATOR LWR SKIN CRACKED 1 INCH AT L/E AFT OF NR 4 BALANCE BOARD. FOUND AT C-1 LTR CK. REPAIRED PER SRM 55-20-3 FIG 4.
- [SDR DL72W952915](https://openairdocs.org/sdr/DL72W952915), Jul 3, 1995: SKIN. CRACKED. A .5 INCH CRACK RT ELEVATOR LWR SKIN AFT OF NR 4 BALANCE BOARD. FOUND DURING C-1 LTR CK TPAMM. REPAIRED PER SRM 55-20-3 FIG 4.
- [SDR DL72W952914](https://openairdocs.org/sdr/DL72W952914), Jul 3, 1995: SKIN. CORRODED. SKIN CORRODED AT STA 720C STR 10 RT. FOUND DURING C-1 LTR CK TPAMM. REPAIRED PER SRM 53-30-3 FIG 5, TIME LIMITED DOUBLER.
- [SDR DL72W952913](https://openairdocs.org/sdr/DL72W952913), Jul 3, 1995: SKIN. CORRODED. FOUND A LINE OF SMALL NICKS 6 INCHES LONG COMING DOWN FROM AFT LAV SERVICE PAN ON THE FUSELAGE SKIN WITH CORROSION. FOUND DURING C-1 LTR CK TPAMM. REPAIRED PER 
- [SDR DL72W952574](https://openairdocs.org/sdr/DL72W952574), Jun 5, 1995: BULKHEAD. DAMAGED. PERFORM BODY STA 178 BULKHEAD ACCESS HOLE INSTALLATION PER SRM 53-10-9 PG 8 TO FOM. INSTALLED REPAIR PER SRM 53-10-9 PG 8 AND 9.
- [SDR DL72W950406](https://openairdocs.org/sdr/DL72W950406), Jan 29, 1995: RIB. CRACKED. DURING SHOP INSPECTION, FOUND NR 6 RIB FOR NR 3 SLAT CRACKED. REPAIRED PER SRM 57-54-0.
- [SDR DL72W950079](https://openairdocs.org/sdr/DL72W950079), Jan 7, 1995: BALLAST. SHORTED. DURING CRUISE, CABIN CEILING LIGHTS CIRCUIT BRAKER TRIPPED. HAD BURNING ODOR AT SEAT ROW 13. FOUND BALLAST FOR CEILING LIGHTS SHORTED. REPLACED BALLAST OPERATIO

## 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 19880317029699I](https://openairdocs.org/incident/19880317029699I), Mar 17, 1988: Boeing 727247 (N2807W), Los Angeles, CA. Departed las vegas with the e and e compartment open and continued to Los Angeles. No violation indicated.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.