# N815EA: Boeing 727-225, registration cancelled 2023-05-19

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 19, 2023
- Exported to: Panama
- Status when cancelled: Valid registration
- Airframe: [Boeing 727-225](https://openairdocs.org/model/boeing-727-225) (registry code 1384077)
- Engine: [Pratt & Whitney JT8D-5](https://openairdocs.org/engine/pratt-whitney-jt8d-5) (registry code 52046)
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 22552
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: October 1, 1981
- Certificate issued: July 28, 2022
- Last registry action: May 4, 2023
- Mode S code: AB1C54
- Owner when cancelled: [727 Air Leasing Corp Inc](https://openairdocs.org/faa-owner/727%20AIR%20LEASING%20CORP%20INC)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: Non-citizen corporation
- Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N815EA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=815EA
- Page: https://openairdocs.org/deregistered/N815EA-2023-05-19

From the FAA registry file of November 7, 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 727-225: https://openairdocs.org/model/boeing-727-225.md

## Service difficulty reports (70, newest 50)

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

- [SDR C8GA2012011800002](https://openairdocs.org/sdr/C8GA2012011800002), Jan 18, 2012: WINDOW. CRACKED. DURING CRUISE OPERATION THE R1 WINDOW BEGAN ARCING AND GLOWING RED. WHILE DESCENDING, THERE WAS A LOUD BANG AND NOTED THAT THE WINDOW HAD CRACKED. AN EMERGENCY 
- [SDR FOTR2101904252](https://openairdocs.org/sdr/FOTR2101904252), Feb 25, 2011: SKIN. DAMAGED. LIGHTNING STRIKE REPAIR AT FUSELAGE SKIN STATION 720B+13 BETWEEN STRINGER 17-18 LT. REMOVED BLIND FASTENER AT FUSELAGE SKIN STATION 720B+13 BETWEEN STR. 17-18 L
- [SDR FOTR2101904448](https://openairdocs.org/sdr/FOTR2101904448), Feb 25, 2011: SKIN. DENTED. EVALUATE EXISTING DENT AT FUSELAGE SKIN STATION 364 BETWEEN STRINGER 23-24 RT. REMOVED PREVIOUS REPAIR FROM BS364 STR. 23-24 RT IAW SRM 51-30-2. FABRICATED NEW 
- [SDR FOTR2101904238](https://openairdocs.org/sdr/FOTR2101904238), Feb 25, 2011: SKIN. DAMAGED. EVALUATE EXISTING LIGHTNING STRIKE REPAIR AT FUSELAGE SKIN STATION 506 BETWEEN STRINGER 24-25 LT. REMOVED BLIND FASTENER AT FUSELAGE SKIN STATION 506 IAW SRM 51
- [SDR FOTR2101904027](https://openairdocs.org/sdr/FOTR2101904027), Feb 25, 2011: SKIN. DAMAGED. EVALUATE EXISTING LIGHTNING STRIKE REPAIR AT FUSELAGE SKIN STATION 296 BETWEEN STRINGER 26-25 LT. REMOVED BLIND FASTENER AT FUSELAGE SKIN STATION 296 BETWEEN ST
- [SDR FOTR2101904249](https://openairdocs.org/sdr/FOTR2101904249), Feb 25, 2011: SKIN. DAMAGED. EVALUATE EXISTING LIGHTNING STRIKE REPAIR AT FUSELAGE SKIN STATION 720A BETWEEN STRINGER 18-19 LT. REMOVED BLIND FASTENER AT FUSELAGE SKIN STATION 720A BETWEEN 
- [SDR FOTR2101904250](https://openairdocs.org/sdr/FOTR2101904250), Feb 25, 2011: SKIN. DAMAGED. EVALUATE EXISTING LIGHTNING STRIKE REPAIR @ FUSELAGE SKIN STA. 720B+3 AND 702B+4 BETWEEN STR. 18-19 L/H.... REMOVED BLIND FASTENER @ FUSELAGE SKIN STA 720B+3 AN
- [SDR FOTR2101904396](https://openairdocs.org/sdr/FOTR2101904396), Feb 21, 2011: SEAT TRACK. CORRODED. STA 865, LBL 24 AND LBL 45, SEAT TRACK FLANGE CORRODED. REMOVED SEAT TRACK FLANGE AT STA 865, LBL24 AND LBL45 IAW SRM 51-30-2. FABRICATED 2 EA NEW PARTS FROM BA
- [SDR FOTR2101903914](https://openairdocs.org/sdr/FOTR2101903914), Feb 21, 2011: SKIN. BENT. PREVIOUS REPAIR ON RT WING INBD FLAP, INBD END BENT, WBL 70. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATED REPAIR PART FROM 2024T3 .063 DIM 2.5" X 2" PO 9
- [SDR FOTR2101904393](https://openairdocs.org/sdr/FOTR2101904393), Feb 21, 2011: FRAME. DENTED. AFT CARGO COMPARTMENT, FRAME DENTED BETWEEN 25R-26R, BS 1010. CUTOUT DAMAGED AREA DIM. 1" X 1.25" IAW SRM 51-40-3, FIG 1. FABRICATED REPAIR FRAME FROM 7075-0 .0
- [SDR FOTR2101904392](https://openairdocs.org/sdr/FOTR2101904392), Feb 21, 2011: FRAME. DENTED. AFT CARGO COMPARTMENT, FRAME DENTED BETWEEN STRINGER 25L-26L BS 1090 CUTOUT DAMAGED AREA 1" X 1.25" IAW SRM 51-40-3, FIG 1. FABRICATED REPAIR FRAME FROM 7075-0 
- [SDR FOTR2101903974](https://openairdocs.org/sdr/FOTR2101903974), Feb 21, 2011: COVER. CRACKED. LT WING L/E NR 2 SLAT TRACK COVER CRACKED. (OTBD TRACK) STOP DRILLED CRACK ON NR 2 SLAT IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM 7075T6 .080" PO 9007282 
- [SDR FOTR2101904218](https://openairdocs.org/sdr/FOTR2101904218), Feb 21, 2011: FRAME. GOUGED. FRAME AT STA 660 BETWEEN STR 6R AND STR 7R IS GOUGED. REMOVED DAMAGED AREA OF FRAME IAW SRM 51-10-1, DIM 1.5" X 1.5". FABRICATED 2 EA CHANNELS 12" X 3" FROM 707
- [SDR FOTR2101904217](https://openairdocs.org/sdr/FOTR2101904217), Feb 21, 2011: FRAME. GOUGED. FRAME AT STA 640 STR 6R IS GOUGED AND DENTED. REMOVED DAMAGED AREA OF FRAME 1.5" X 1.5" IAW SRM 51-10-1. FABRICATED CHANNEL 2 EA 12" X 3" FROM 7075-0 .063 PO 90
- [SDR FOTR2101903892](https://openairdocs.org/sdr/FOTR2101903892), Feb 21, 2011: SKIN. CHAFED. LWR T/E INTERIOR LIP OF NR 8 SLAT CHAFED ALONG LENGTH OF SLAT. BLENDED CHAFED AREA ORIG MAT .070 WITH .039 REMAINING AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10
- [SDR FOTR2101904400](https://openairdocs.org/sdr/FOTR2101904400), Feb 21, 2011: SKIN. DEBONDED. LT WING T/E NR 6 SPOILER UPPER SKIN IS DISBONDED. REMOVED DAMAGE APPROX 13" X 5.5" AND CLEANED AND PREPPED AREA IAW SRM 51-40-20, PG 12-14 PARA 7.FABRICATED REP
- [SDR FOTR2101904371](https://openairdocs.org/sdr/FOTR2101904371), Feb 21, 2011: STRINGER. DENTED. FWD PIT LT SIDE STR 25L HAS A DENT AT BS 508. CUTOUT DAMAGED STRINGER DIM. 2.1" LONG. FABRICATED HAT CHANNEL FROM BAC1498-140 7075T6 PO 2101970 DIM 2.1" LONG. F
- [SDR FOTR2101904166](https://openairdocs.org/sdr/FOTR2101904166), Feb 21, 2011: SEAT TRACK. CORRODED. CABIN SEAT TRACK AT BS 480-720B, LBL 24.5 HAS HEAVY CORROSION IN SEVERAL AREAS OVER ENTIRE LENGTH. REMOVED CORROSION ON SEAT TRACK LBL 24, BS 480-720B AND FOUND
- [SDR FOTR2101904399](https://openairdocs.org/sdr/FOTR2101904399), Feb 21, 2011: SKIN. DEBONDED. LT WING NR 1 SPOILER UPPER SKIN IS DEBONDED. REMOVED DAMAGE, CLEANED AND PREPPED AREA IAW SRM 51-40-20, PARA 7,11 AND 14. FABRICATED FILLER DIM 24" X 7" .025 AN
- [SDR FOTR2101904398](https://openairdocs.org/sdr/FOTR2101904398), Feb 21, 2011: SKIN. DEBONDED. RT WING T/E NR 10 SPOILER UPPER SKIN IS DEBONDED. REMOVED DAMAGE, SANDED, CLEANED AND PREPPED AREA IAW SRM 51-40-20, PARA 7, 11, 14, 15, AND 18. FABRICATED REPA
- [SDR C8GA2010000073](https://openairdocs.org/sdr/C8GA2010000073), Nov 10, 2010: INDICATOR. MALFUNCTIONED. ON TAKEOFF ROLL, THE NR1 EPR INDICATION PEGGED. THE TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO THE BLOCKS. HIGH ENERGY INSP WAS PERFORMED. R & R THE NR1 EPR I
- [SDR C8GA20090075](https://openairdocs.org/sdr/C8GA20090075), May 13, 2009: PUMP. FAULTY. FLT 720 FROM TOL TO ATL, DURING CLIMB-OUT THE NR 2 ENGINE FUEL FLOW BECAME ERRATIC, THE N1 AND N2 STARTED WINDING DOWN FOLLOWED BY COMPRESSOR STALL. THE NR 2 EN
- [SDR C8GA20070003](https://openairdocs.org/sdr/C8GA20070003), Feb 16, 2007: BLADES. DAMAGED. FLT 1723 FROM BOS TO TOL, DURING CLIMB-OUT, NR 2 ENGINE BEGAN TO VIBRATE AND WAS CONFIRMED WITH THE THROTTLE. ENGINE BEGAN TO COMPRESSOR STALL, ENGINE WAS SHUTD
- [SDR C8GA20060020](https://openairdocs.org/sdr/C8GA20060020), Nov 22, 2006: ROD. BROKEN. FLT 713 FROM BOS TO ROC, AFTER TAKEOFF AND CLIMBING, THE RIGHT MAIN GEAR DOOR LIGHT REMAINED ON. CYCLED THE GEAR AND THE LIGHT REMAINED ILLUMINATED. AN EMERGENC
- [SDR C8GA20060006](https://openairdocs.org/sdr/C8GA20060006), Mar 28, 2006: QUICK DISCONNECT. LOOSE. FLT 1719 FROM MCO TO ATL, DURING TAKEOFF ROLL, FOR’S AIRSPEED INDICATOR BEGAN TO LAG. AFTER TAKEOFF WHILE CLIMBING, GEAR RETRACTED AND FLAPS RETRACTING FOR’S AI
- [SDR C8GA20060004](https://openairdocs.org/sdr/C8GA20060004), Mar 2, 2006: OIL COOLER. FAILED. FLT 1707 FROM PHX TO MEM. DURING CLIMBOUT NR 2 ENGINE OIL TEMP BEGAN RISING. INITATED ENGINE SHUT DOWN AS PRECAUTIONARY. EMERGENCY WAS DECLARED, AIRCRAFT RETURN
- [SDR RYN2003F00000](https://openairdocs.org/sdr/RYN2003F00000), Jan 23, 2003: ACTUATOR. DEFECTIVE. DURING CLIMBOUT, NR 7 LEADING EDGE SLAT WOULD NOT RETRACT. EMERGENCY FLAP PROCEDURES FOLLOWED. AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT.
- [SDR 2002F00589](https://openairdocs.org/sdr/2002F00589), Apr 12, 2002: FLAP. DENTED. AT C-CHECK, FOUND DENT OUT OF LIMITS ON RIGHT WING INBOARD AFT FLAP. (M)
- [SDR 2002F00588](https://openairdocs.org/sdr/2002F00588), Apr 3, 2002: FRAME. CRACKED. AT C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME, UPPER CHORD, CRACKED AT STATION 580 RBL 3. (M)
- [SDR 2002F00586](https://openairdocs.org/sdr/2002F00586), Apr 2, 2002: FLOORBEAM. CRACKED. AT C-CHECK, FOUND FORWARD CABIN FLOORBEAM CRACKED IN RADIUS 1.5 INCHES LONG AT STATION 326 RBL 24. (M)
- [SDR 2002F00497](https://openairdocs.org/sdr/2002F00497), Apr 2, 2002: FLOOR SUPPORT. CRACKED. AT C-CHECK, FOUND AFT PIT FLOOR SUPPORT CRACKED AT STATION 950F LBL 4. (M)
- [SDR 2002F00496](https://openairdocs.org/sdr/2002F00496), Mar 28, 2002: FRAME. CORRODED. AT C-CHECK, FOUND CORROSION ON FRAME AT FORWARD ACCESS COMPARTMENT AFT OF DOOR AT STATION 227. (M)
- [SDR 2002F00495](https://openairdocs.org/sdr/2002F00495), Mar 28, 2002: FRAME. CRACKED. AT C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME CRACKED AT STATION 560 RBL 3. (M)
- [SDR 2002F00494](https://openairdocs.org/sdr/2002F00494), Mar 28, 2002: SHEAR TIE. CORRODED. AT C-CHECK, FOUND SHEAR TIE CORRODED AT COMPARTMENT FRAME STATION 720A LBL 10. (M)
- [SDR 2002F00477](https://openairdocs.org/sdr/2002F00477), Mar 28, 2002: WEB. TORN. AT C-CHECK, FOUND AFT CARGO DOOR CLOSE OUT WEB TORN AT STATION 620 ABOVE STRINGER 26R. (M)
- [SDR 2002F00476](https://openairdocs.org/sdr/2002F00476), Mar 28, 2002: ANGLE. CRACKED. AT C-CHECK, FOUND L-ANGLE CRACKED BELOW FORWARD CARGO DOOR CUTOUT, FORWARD WEB AT STATION 560 BETWEEN STRINGER 23 AND 24R. (M)
- [SDR 2002F00463](https://openairdocs.org/sdr/2002F00463), Mar 28, 2002: FRAME. CRACKED. AT C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME UPPER CHORD CRACKED AT STATION 600 RBL 3. (M)
- [SDR 2002F00462](https://openairdocs.org/sdr/2002F00462), Mar 28, 2002: PANEL. CORRODED. AT C-CHECK, FOUND CORROSION IN AFT PIT AT RIGHT TRANSITION PANEL TOP SIDE FROM STATION 950A TO 1066. (M)
- [SDR 2002F00461](https://openairdocs.org/sdr/2002F00461), Mar 28, 2002: SEAT TRACK. GOUGED. AT C-CHECK, FOUND SEAT TRACK GOUGED AT STATION 848 TO 870 RB 44. (M)
- [SDR 2002F00460](https://openairdocs.org/sdr/2002F00460), Mar 28, 2002: BULKHEAD. CRACKED. AT C-CHECK, FOUND THREE CRACKS AT FORWARD PIT AFT BULKHEAD CENTER PANEL. (M)
- [SDR 2002F00475](https://openairdocs.org/sdr/2002F00475), Mar 25, 2002: FLOOR SUPPORT. CORRODED. AT C-CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT STATION 644 RBL 9. (M)
- [SDR 2002F00474](https://openairdocs.org/sdr/2002F00474), Mar 23, 2002: BRACKET. DAMAGED. AT C-CHECK, FOUND NR 3 SPOILER INBOARD ATTACH BRACKET WITH TWO ELONGATED HOLES AT STATION 507 AND 515. (M)
- [SDR 2002F00457](https://openairdocs.org/sdr/2002F00457), Mar 22, 2002: SUPPORT. CORRODED. AT C-CHECK, FOUND CORROSION ON FORWARD CARGO SUPPORT AT STATION 644. (M)
- [SDR 2002F00455](https://openairdocs.org/sdr/2002F00455), Mar 22, 2002: SEAT TRACK. WORN. AT C-CHECK, FOUND SEAT TRACK WORN OUT OF LIMITS AT STATION 852-868. (M)
- [SDR 2002F00454](https://openairdocs.org/sdr/2002F00454), Mar 21, 2002: SUPPORT. CORRODED. AT C-CHECK, FOUND FORWARD CARGO SUPPORT CORROSION AT STATION 536. (M)
- [SDR 2002F00453](https://openairdocs.org/sdr/2002F00453), Mar 20, 2002: FRAME. CRACKED. AT C-CHECK, FOUND CRACK SIX INCHES LONG AT LOWER LEFT Z-FRAME IN FORWARD CARGO PIT STATION 480 LBL 32. (M)
- [SDR 2002F00452](https://openairdocs.org/sdr/2002F00452), Mar 20, 2002: PANEL. CORRODED. AT C-CHECK, FOUND CORROSION AND CRACK IN THE FORWARD PIT AT THE RIGHT TRANSITION PANEL TOP SIDE FROM STATION 480-560. (M)
- [SDR 2002F00451](https://openairdocs.org/sdr/2002F00451), Mar 19, 2002: SKIN. CHAFED. AT C-CHECK, FOUND L-1 DOOR INTERIOR SKIN CHAFED BETWEEN THE CENTER STOPS ON THE AFT EDGE. (M)
- [SDR 2002F00450](https://openairdocs.org/sdr/2002F00450), Mar 18, 2002: WEB. CORRODED. AT C-CHECK, FOUND AFT PIT SHEAR FLOOR WEB CORRODED AT STATION 1183 RBL 18. (M)
- [SDR 2002F00456](https://openairdocs.org/sdr/2002F00456), Feb 22, 2002: SEAT TRACK. WORN. AT C-CHECK, FOUND SEAT TRACK WORN OUT OF LIMITS AT STATION 700D TO STATION 720E LBL 44. (M)

All 70: https://openairdocs.org/deregistered/N815EA-2023-05-19/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 19870511019269I](https://openairdocs.org/incident/19870511019269I), May 11, 1987: Boeing 727225 (N815EA), Kansas City, MO. A panel fell from right wheelwell during final approach. No damage. Had gear warning light on unrelated to other.

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