# N620PC: 1968 Boeing 737-244, registration cancelled 2002-02-26

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 26, 2002
- Exported to: Nigeria
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 737-244](https://openairdocs.org/model/boeing-737-244) (registry code 138448U)
- Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Serial number: 19708
- Year built: 1968
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: February 3, 1984
- Certificate issued: June 5, 1997
- Last registry action: August 15, 2000
- Mode S code: A81785
- Owner when cancelled: [Interlease Aviation Investors III (Taca) LLC](https://openairdocs.org/faa-owner/INTERLEASE%20AVIATION%20INVESTORS%20III%20(TACA)%20LLC)
- Location: [Northfield, IL](https://openairdocs.org/faa-place/IL/Northfield)
- Owner type: Corporation
- Owner's area on the map: 42.1041° N, 87.7539° W: Placed by OpenAirDocs at the center of ZIP code 60093, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N620PC
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=620PC
- Page: https://openairdocs.org/deregistered/N620PC-2002-02-26

From the FAA registry file of October 27, 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 737-244: https://openairdocs.org/model/boeing-737-244.md

## Service difficulty reports (173, newest 50)

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

- [SDR P2EA01081](https://openairdocs.org/sdr/P2EA01081), May 29, 2001: RIB. CHAFED. OKC - DURING C-CHECK, FOUND LEFT HORIZONTAL STABILIZER BALANCE BAY RIB WEB CHAFED AT ES 66.54 ES 94.07, ES 121.59 AND 149.12. REPAIRED IAW DRAWING 55-01204-1 AN
- [SDR P2EA01043](https://openairdocs.org/sdr/P2EA01043), May 1, 2001: ANGLE. CRACKED. OKC - DURING C-CHECK, L-ANGLE CRACKED AT BS 1150 WL 238, RIGHT SIDE. REPAIRED L-ANGLE IAW SRM 51-40-3. (M)
- [SDR P2EA01067](https://openairdocs.org/sdr/P2EA01067), Apr 28, 2001: STRAP. CRACKED. OKC - DURING C-CHECK, INNER TEAR STRAP AT BS 1136 TO BS 1156 WL 240 ON RIGHT SIDE OF APU TORQUE BOX CRACKED 5 INCHES. FABRICATED TEAR STRAP AND REPLACED IAW SRM
- [SDR P2EA01038](https://openairdocs.org/sdr/P2EA01038), Apr 28, 2001: STRAP. CRACKED. DURING C-CHECK, INNER TEAR STRAP AT BS 1136 TO BS 1156, WL 240 ON RIGHT SIDE IS CRACKED. (M)
- [SDR P2EA001088](https://openairdocs.org/sdr/P2EA001088), Apr 26, 2001: ANGLE. CORRODED. OKC - DURING C-CHECK, FOUND CORROSION ON EXTRUDED ANGLES IN RIGHT SIDE OF TORQUE BOX AT BS 1088 TO BS 1156. FOUND TO BE OUT OF LIMITS, LEVEL 2. REPAIRED EXTRUDE
- [SDR P2EA01041](https://openairdocs.org/sdr/P2EA01041), Apr 26, 2001: ANGLE. CORRODED. OKC - DURING C-CHECK, FOUND CORROSION ON EXTRUDED ANGLES IN RIGHT SIDE OF TORQUE BOX AT BS 1088 TO BS 1156. FOUND TO BE OUT OF LIMITS 5/1/2001. (M)
- [SDR P2EA01065](https://openairdocs.org/sdr/P2EA01065), Apr 17, 2001: FRAME. DENTED. OKC - DURING C-CHECK, FRAME AT BS 827 DENTED BETWEEN 24L AND 25L, LENGTH 2 INCHES, WIDTH 1 INCH, DEPTH .080 INCH. REPAIRED IAW SRM 53-10-4. (M)
- [SDR P2EA01064](https://openairdocs.org/sdr/P2EA01064), Apr 13, 2001: FRAME. CRACKED. OKC - DURING C-CHECK, FLOOR UPPER CHORD AFT FLANGE AT BS 328 BL 0 CRACKED .400 INCHES. REPAIRED FLOORBEAM PER SRM 53-10-9. (M)
- [SDR P2EA001082](https://openairdocs.org/sdr/P2EA001082), Apr 5, 2001: BEAM. GOUGED. OKC - DURING C-CHECK, FOUND THE RIGHT MLG SUPPORT BEAM GOUGED 10 INCHES INBOARD FROM THE LOWER OUTBOARD END, AFTER BLENDING IT WAS FOUND TO BE OUT OF LIMITS. RE
- [SDR P2EA001085](https://openairdocs.org/sdr/P2EA001085), Apr 5, 2001: SKIN. CORRODED. OKC - DURING C-CHECK, FOUND THE INTERNAL FUSELAGE SKIN WITH CORROSION OUT OF LIMITS AT STATION 322 BETWEEN STRINGERS 28R AND 29R, LEVEL 2. REPAIRED THE INTERNAL
- [SDR P2EA001017](https://openairdocs.org/sdr/P2EA001017), Apr 5, 2001: BEAM. GOUGED. OKC - DURING C-CHECK, FOUND THE RIGHT MAIN LANDING GEAR SUPPORT BEAM GOUGED 10 INCHES INBAORD FROM THE LOWER OUTBOARD END. AFTER BLENDING IT WAS FOUND TO BOUT O
- [SDR P2EA001018](https://openairdocs.org/sdr/P2EA001018), Apr 5, 2001: SKIN. CORRODED. OKC - DURING C-CHECK, FOUND THE INTERNAL FUSELAGE SKIN WITH CORROSION OUT OF LIMITS AT STATION 322 BETWEEN STRINGERS 28R AND 29R. (M)
- [SDR P2EA001032](https://openairdocs.org/sdr/P2EA001032), Apr 4, 2001: SKIN. CRACKED. OKC - DURING C-CHECK, FOUND THE FORWARD FUSELAGE SKIN T STATION 196.5 AT LBL 3 WITH CRACK, .75 INCH IN LENGTH. REPAIRED THE FORWARD FUSELAGE SKIN AT STATION 196
- [SDR P2EA001015](https://openairdocs.org/sdr/P2EA001015), Apr 4, 2001: SKIN. CRACKED. OKC - FOUND DURING C-CHECK, FORWARD FUSELAGE SKIN AT STATION 196.5 TO 203.5 AT LBL 3 WITH CRACK .75 INCH IN LENGTH. (M)
- [SDR P2EA001016](https://openairdocs.org/sdr/P2EA001016), Apr 4, 2001: SKIN. CORRODED. OKC - DURING C-CHECK, FOUND THE INTERNAL SKIN AT FUSELAGE STATION 322 BETWEEN STRINGERS 28-29 RIGHT HAS CORROSION. (M)
- [SDR P2EA001083](https://openairdocs.org/sdr/P2EA001083), Mar 30, 2001: LANDING GEAR. WORN. OKC - DURING C-CHECK, FOUND THE RIGHT MAIN LANDING GEAR TRUNNION RACE WITH WEAR OUT OF LIMITS. REPAIRED THE RIGHT MLG TRUNNION RACE IAW BOEING OVERHAUL MANUAL, 
- [SDR P2EA001084](https://openairdocs.org/sdr/P2EA001084), Mar 30, 2001: SKIN. CRACKED. OKC - DURING C-CHECK, FOUND THE RIGHT WING LEADING EDGE AT NR 6 LEADING EDGE SLAT ANTI-ICE TUB CUTOUT WITH CRACK, .25 INCH. REPAIRED THE RIGHT WING LEADING EDGE
- [SDR P2EA001014](https://openairdocs.org/sdr/P2EA001014), Mar 30, 2001: SKIN. CRACKED. OKC - DURING C-CHECK, FOUND THE RIGHT WING LEADING EDGE AT NR 6 LEADING EDGE SLAT ANTI-ICE TUB CUTOUT WITH CRACK, LENGTH .25 INCH. (M)
- [SDR P2EA01080](https://openairdocs.org/sdr/P2EA01080), Mar 29, 2001: RIB. CHAFED. OKC - DURING C-CHECK, FOUND RIGHT HORIZONTAL STABILIZER BALANCE BAY RIB WEBS CHAFED AT ES 66.54, ES 94.07 ES 121.59 AND ES 149.12. REPAIRED IAW DRAWING 55-01204
- [SDR P2EA001031](https://openairdocs.org/sdr/P2EA001031), Mar 29, 2001: SKIN. CORRODED. OKC - DURING C-CHECK, FOUND THE LEFT WING CENTER SECTION LOWER SKIN SURFACE ABOVE THE LEFT RAM AIR DUCT WITH CORROSION OUT OF LIMITS AT LBL 41, STRINGER 5C. REM
- [SDR P2EA001030](https://openairdocs.org/sdr/P2EA001030), Mar 29, 2001: SKIN. CORRODED. OKC - DURING C-CHECK, FOUND THE RIGHT WING CENTER SECTION LOWER SKIN SURFACE ABOVE THE RIGHT RAM AIR DUCT WITH CORROSION OUT OF LIMITS AT RBL 40.5 THROUGH 43.5,
- [SDR P2EA001013](https://openairdocs.org/sdr/P2EA001013), Mar 29, 2001: SKIN. CORRODED. OKC - DURING C-CHECK, FOUND THE LEFT WING CENTER SECTION LOWER SKIN SURFACE ABOVE THE LEFT RAM AIR DUCT WITH CORROSION OUT OF LIMITS. (M)
- [SDR P2EA01053](https://openairdocs.org/sdr/P2EA01053), Mar 28, 2001: FLAP. DELAMINATED. OKC - DURING C-CHECK, RIGHT WING INBOARD MID-FLAP OUTBOARD EDGE DELAMINATED 6.5 INCHES, WIDTH 1 INCH. REPAIRED IAW SRM 51-40-20. (M)
- [SDR AALA01037](https://openairdocs.org/sdr/AALA01037), Mar 28, 2001: FLAP. DELAMINATED. OKC - DURING C-CHECK, LEFT WING OUTBOARD MID-FLAP INBOARD EDGE DELAMINATED, LENGTH 2 INCHES, WIDTH 1 INCH. REPAIRED IAW SRM 57-50-2 AND SRM 51-40-2. (M)
- [SDR P2EA001009](https://openairdocs.org/sdr/P2EA001009), Mar 28, 2001: SKIN. DELAMINATED. OKC - DURING C-CHECK, FOUND THE LEFT WING OUTBOARD MID-FLAP INBAORD EDGE WITH DELAMINATION, LENGTH 2 INCHES, WIDTH 1 INCH. (M)
- [SDR P2EA001068](https://openairdocs.org/sdr/P2EA001068), Mar 28, 2001: SKIN. DELAMINATED. DURING C-CHECK, FOUND THE RIGHT WING INBOARD MID-FLAP OUTBOARD EDGE WITH DELAMINATION, LENGTH 6.5 INCH, WIDTH 1 INCH. (M)
- [SDR P2EA01049](https://openairdocs.org/sdr/P2EA01049), Mar 27, 2001: FLOORBEAM. CORRODED. OKC - DURING C-CHECK, FOUND CORROSION ON FLOORBEAM AT BS 312, BOTTOM AFT SIDE OF UPPER CHORD AT BL 0, LBL 8 AND RBL 8. REPAIRED PER DRAWING 53-01181-1 AND 8110-
- [SDR P2EA001012](https://openairdocs.org/sdr/P2EA001012), Mar 25, 2001: SKIN. CORRODED. OKC - DURING C-CHECK, FOUND THE RIGHT WING CENTER SECTION LOWER SKIN SURFACE ABOVE THE RIGHT RAM AIR DUCT WITH CORROSION OUT OF LIMITS. (M)
- [SDR P2EA01004](https://openairdocs.org/sdr/P2EA01004), Feb 22, 2001: SEAL. FAILED. MCI - FLT 350 - WHILE IN CLIMB-OUT OF MCI, AIRCRAFT WOULD NOT PRESSURIZE, RETURN TO MCI. INSPECTION FOUND AIRCRAFT L1 DOOR SEAL NOT PROPERLY SEATED. RESECURED D
- [SDR P2EA00463](https://openairdocs.org/sdr/P2EA00463), Dec 11, 2000: LEVER. MALFUNCTIONED. MSY - AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO MSY WITH NO INCIDENT. RESET LANDING GEAR LEVER AND PRESSURE WARNING CIRCUIT BREAKERS, S
- [SDR P2EA00274](https://openairdocs.org/sdr/P2EA00274), Sep 30, 2000: FLOORBEAM. CORRODED. SJO - FOUND DURING C-CHECK, CORROSION ON FLOORBEAM LOWER CHORD AT BS 867, RBL 25 AND WL 202. REPAIRED FLOORBEAM LOWER CHORD AT BS 867 WL 202 BETWEEN RBL 16 AND 
- [SDR P2EA00273](https://openairdocs.org/sdr/P2EA00273), Sep 28, 2000: BULKHEAD. DAMAGED. SJO - DURING C-CHECK, TEMPORARY REPAIR AT BS 178 FROM LBL 8 TO LBL 15 AND FROM WL 233 AND WL 238. INSTALLED PERMANENT REPAIR AT BS 178 FROM LBL 8 TO LBL 15 AND 
- [SDR P2EA00272](https://openairdocs.org/sdr/P2EA00272), Sep 28, 2000: SKIN. DAMAGED. SJO - DURING C-CHECK, RIGHT FORWARD AND AFT CORNERS WORN ON E/E DOOR. REPAIRED RIGHT SKIN SECTIONS AT FORWARD AND AFT CORNERS IAW SRM 52-00-3 FIG 5. (M)
- [SDR P2EA00263](https://openairdocs.org/sdr/P2EA00263), Sep 28, 2000: BULKHEAD. CRACKED. SJO - DURING C-CHECK, TEMPORARY REPAIR AT BS 178 FROM RBL 8 TO RBL 15 AND BETWEEN WL 233 TO WL 238. INSTALLED PERMANENT REPAIR AT BS 178 FROM RBL TO RBL 15 AND 
- [SDR P2EA00285](https://openairdocs.org/sdr/P2EA00285), Sep 28, 2000: RUDDER. DELAMINATED. SJO - DURING C-CHECK, RUDDER DELAMINATION BETWEEN STA 17.25 AND STA 35.25. REPAIRED RUDDER IAW SRM 51-40-9, PARAGRAPH 3 AND PARAGRAPH 5, FIG 3. (X)
- [SDR P2EA00282](https://openairdocs.org/sdr/P2EA00282), Sep 28, 2000: WEB. CORRODED. DURING C-CHECK, CORROSION (LEVEL 2) ON WEB SECTION AT BS 178 FROM LBL 16 TO LBL 29 AND BETWEEN WL 180 AND WL 240. REPAIRED WEB SECTION AT BS 178 FROM LBL 16 TO 
- [SDR P2EA00281](https://openairdocs.org/sdr/P2EA00281), Sep 28, 2000: SKIN. DELAMINATED. SJO - DURING C-CHECK, LEFT WING NR 1 SPOILER UPPER SKIN WITH DELAMINATION. REPAIRED NR 1 SPOILER IAW COOPESA EO COO-CMP-3-57-609-00, DATED OCT 2, 2000. (M)
- [SDR P2EA00280](https://openairdocs.org/sdr/P2EA00280), Sep 28, 2000: SKIN. DELAMINATED. SJO - FOUND DURING C-CHECK, LEFT OUTBOARD FLIPPER FLAP UPPER AND LOWER SKIN WITH DELAMINATION. REPAIRED FLIPPER FLAP SKIN IAW COOPESA EO COO-CMP-3-57-607-00 DAT
- [SDR P2EA00276](https://openairdocs.org/sdr/P2EA00276), Sep 28, 2000: SKIN. DELAMINATED. SJO - FOUND DURING C-CHECK, LEFT WING SPAR LOWER ACCESS PANEL INNER SKIN DELAMINTATED FROM RSS 339 TO 380. REPAIRED PANEL IAW COOPESA EO COO-CMP-3-57-608-00, DA
- [SDR P2EA00260](https://openairdocs.org/sdr/P2EA00260), Sep 27, 2000: SKIN. CRACKED. SJO - DURING C-CHECK, LFEC SKIN CRACK INDICATION BETWEEN BS 755 AND BS 760 AT STRINGER 25R. REPAIRED SKIN FROM BS 755 TO BS 769 BETWEEN STRINGERS 24R AND 26R IA
- [SDR P2EA00259](https://openairdocs.org/sdr/P2EA00259), Sep 27, 2000: SKIN. CRACKED. SJO - DURING C-CHECK, MFEC SKIN CRACK INDICATION AT BS 366 STRINGER 19R. REPAIRED SKIN FROM BS 306 TO BS 371 BETWEEN STRINGERS 18R AND 20R IAW SRM 53-30-3 FIG 1
- [SDR P2EA00258](https://openairdocs.org/sdr/P2EA00258), Sep 27, 2000: SKIN. CRACKED. SJO - DURING C-CHECK, MFEC SKIN CRACK INDICATION AT BS 778 STRINGER 25L. REPAIRED SKIN FROM BS 751 TO BS 795 AND BETWEEN STRINGERS 24L AND 26L IAW SRM 53-30-3 F
- [SDR P2EA00271](https://openairdocs.org/sdr/P2EA00271), Sep 27, 2000: SKIN. CRACKED. SJO - DURING C-CHECK, MFEC SKIN CRACK ON LOWER ROW OF FASTENERS AT BS 877 STRINGER 25R. REPAIRED SKIN FROM BS 870 TO BS 883 AND FROM STRINGERS 25R TO 27R IAW SR
- [SDR P2EA00270](https://openairdocs.org/sdr/P2EA00270), Sep 27, 2000: SKIN. CRACKED. SJO - DURING C-CHECK, MFEC SKIN CRACK INDICATION ON LOWER ROW OF FASTENERS AT BS 1006 STRINGER 4L. REPAIRED SKIN FROM BS 1000 TO BS 1012 AND BETWEEN STRINGER 3L
- [SDR P2EA00269](https://openairdocs.org/sdr/P2EA00269), Sep 27, 2000: SKIN. CRACKED. SJO - DURING C-CHECK, MFEC SKIN CRACK INDICATION, 2 INCHES LONG, ON UPPER ROW OF FASTENERS AT STRINGER 26L BETWEEN FROM BS 460 TO BS 464. REPAIRED SKIN FROM BS 
- [SDR P2EA00279](https://openairdocs.org/sdr/P2EA00279), Sep 27, 2000: SKIN. CRACKED. SJO - DURING C-CHECK, FOUND MFEC SKIN CRACKED INDICATIONS 3 INCHES LONG FROM BS 515 TO 518 AT STRINGER 10R. REPAIRED SKIN FROM BS 510 TO BS 500A PLUS 1 AND BETW
- [SDR P2EA00284](https://openairdocs.org/sdr/P2EA00284), Sep 25, 2000: BULKHEAD. CRACKED. SJO - DURING C-CHECK, VERTICAL CHORD CRACKED AT BS 178. LBL 5.7 AND WL 184. FABRICATED AND REPLACED VERTICAL CHORD AT BS 178, LBL 5.7 AND FROM WL 177 AND WL 197
- [SDR P2EA00262](https://openairdocs.org/sdr/P2EA00262), Sep 24, 2000: SKIN. CRACKED. SJO - DURING C-CHECK, SIX SKIN CRACKS, AVERAGE LENGTH .25 INCH, AT BS 188, WL 214, TWO BS 188 WL 216, ONE AT BS 203, WL 216, ONE AT BS 211, WL 217 AND TWO AT BS
- [SDR P2EA00278](https://openairdocs.org/sdr/P2EA00278), Sep 24, 2000: SKIN. DEBONDED. SJO - DURING C-CHECK, UPPER WINDOW BELT DISBONDING FROM BS 360 TO BS 380 AND BETWEEN STRINGER 11R AND 13R. REPAIRED WINDOW BELT FROM BS 360 TO BS 380 AND FROM S
- [SDR P2EA00277](https://openairdocs.org/sdr/P2EA00277), Sep 24, 2000: SKIN. DEBONDED. SJO - DURING C-CHECK, UPPER WINDOW BELT DISBONDING FROM BS 887 TO BS 907 AND BETWEEN STRINGER 11L AND 13L. REPAIRED WINDOW BELT FROM BS 887 TO BS 907 AND BETWEE

All 173: https://openairdocs.org/deregistered/N620PC-2002-02-26/reports.md

## 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 20000621022119I](https://openairdocs.org/incident/20000621022119I), Jun 21, 2000: Boeing 737244 (N620PC), Kansas City, MO. (-23) On June 21, 2000, vanguard airlines, flight 590, was scheduled to enroute from mci to mdw. At start of take off, number one engine would not spool-up and…
- [Incident 19991210037459I](https://openairdocs.org/incident/19991210037459I), Dec 10, 1999: Boeing 737244 (N620PC), Minneapolis, MN. (-23) During flight at cruise #1 engine overheat light illuminated, power was reduced and the light extinguished, an emergency was declared and the aircraft…
- [Incident 19981122040829I](https://openairdocs.org/incident/19981122040829I), Nov 22, 1998: Boeing 737244 (N620PC), Kansas City, MO. (-5)Air carrier P2EA, flight number 819, 737-244, mci-dfw, while enroute to dfw both airspeed indicators had false indictions on climbout, first officer…
- [Incident 19980121003019I](https://openairdocs.org/incident/19980121003019I), Jan 21, 1998: Boeing 737244 (N620PC), Chicago, IL, Minor damage. De-ice truck backed into left wing of 620PC. Due no help in backing. Change in operator policy help remedy.

## Other aircraft with N620PC

- [Registered now](https://openairdocs.org/aircraft/N620PC): Diamond Aircraft Ind DA20-C1, S/N C0464, built 2007

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