# N219US: Boeing 737-281, registration cancelled 2000-07-19 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 19, 2000 - Exported to: Peru - Status when cancelled: Triennial form not returned - Airframe: [Boeing 737-281](https://openairdocs.org/model/boeing-737-281) (registry code 138448P) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 20414 - Type of aircraft: Fixed wing multi engine - Certificate issued: May 14, 1997 - Last registry action: May 16, 2000 - Mode S code: A1DCC4 - Owner when cancelled: [First Security Bank Na Owner Trustee](https://openairdocs.org/faa-owner/FIRST%20SECURITY%20BANK%20NA%20OWNER%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N219US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=219US - Page: https://openairdocs.org/deregistered/N219US-2000-07-19 From the FAA registry file of October 28, 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 737-281: https://openairdocs.org/model/boeing-737-281.md ## Service difficulty reports (90, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR P2EA99354](https://openairdocs.org/sdr/P2EA99354), Dec 3, 1999: FLOORBEAM. CORRODED. SJO - C-CHECK, FLOORBEAM WEB CORRODED AT BS 259.5, FROM WL 208.5 TO WL 206, BETWEEN LBL 13 INCH TO RBL 13 INCH. DEFECT SIZE, LENGTH 16 INCHES, WIDTH 5 INCHES. R - [SDR P2EA99351](https://openairdocs.org/sdr/P2EA99351), Dec 3, 1999: FLOORBEAM. CORRODED. SJO - C-CHECK, FLOORBEAM CORROSION AT BS 259.5, WL 208.5, BETWEEN LBL 20 AND RBL 15 INCHES. DEFECT SIZE, LENGTH 14 INCHES, WIDTH 4 INCHES. REPAIRED FLOORBEAM AN - [SDR P2EA99350](https://openairdocs.org/sdr/P2EA99350), Dec 3, 1999: ANGLE. CORRODED. SJO - C-CHECK, FLOOR SUPPORT ANGLE CORRODED AT BS 270, WL 208.5, BETWEEN RBL 17 INCHE LBL 10 INCH. DEFECT SIZE, LENGTH 10 INCH, WIDTH 2 INCH. REPAIRED FLOOR SUP - [SDR P2EA99342](https://openairdocs.org/sdr/P2EA99342), Dec 3, 1999: SKIN. DELAMINATED. SJO - C-CHECK, LEFT AC BAY DOOR DELAMINATED. REPAIRED LEFT AC BAY DOOR PER EO COO-CMP-3-53-704-99 DATED DECEMBER 4, 1999. (M) - [SDR P2EA99335](https://openairdocs.org/sdr/P2EA99335), Dec 2, 1999: BULKHEAD. CRACKED. SJO - C-CHECK, WEB CRACKED AT BS 178, LBL 10 INCHES, WL 235. DEFECT SIZE, LENGTH .375 INCH. REPAIRED BULKHEAD WEB AT BS 178 FROM LBL 7 TO LBL 17.5, BETWEEN WL 2 - [SDR P2EA99352](https://openairdocs.org/sdr/P2EA99352), Dec 1, 1999: RIB. CRACKED. SJO - C-CHECK ITEM, SUPPORT RIB CRACKED AT RT WING SLAT STATION 25. DEFECT SIZE, LENGTH .75 INCH. REPLACED SLAT TRACK SUPPORT RIB AT SLAT STATION 25 PER SRM 51- - [SDR P2EA99345](https://openairdocs.org/sdr/P2EA99345), Dec 1, 1999: SKIN. DENTED. SJO - C-CHECK, E/E DOOR HAS A DENT OUT OF LIMITS, DEFECT SIZE, LENGTH 1.75 INCH, WIDTH 1.5 INCH, DEPTH .045 INCH. REPLACED DOOR SKIN PER SRM 51-10-1, PAGE 5 AND - [SDR P2EA99355](https://openairdocs.org/sdr/P2EA99355), Nov 30, 1999: SKIN. CRACKED. SJO - C-CHECK, FUSELAGE SKIN CRACKED FROM BS 727 TO BS 727A BETWEEN STRINGER 14 RT AND 16 RT. DEFECT SIZE LENGTH 1.75 INCH. REPAIRED FUSELAGE SKIN SECTION FROM - [SDR P2EA99336](https://openairdocs.org/sdr/P2EA99336), Nov 30, 1999: SKIN. CRACKED. SJO - C-CHECK, FUSELAGE SKIN CRACKED FROM BS 268 TO BS 277, BETWEEN STRINGER 15 RT AND 16 RT. DEFECT SIZE 1 INCH. REPAIRED FUSELAGE SKIN SECTION FROM BS 263.5 T - [SDR P2EA99311](https://openairdocs.org/sdr/P2EA99311), Nov 12, 1999: TRANSMITTER. INOPERATIVE. FLT 588 - MCI - ABORTED TAKEOFF, NO EMERGENCY DECLARED. DURING TAKEOFF ROLL, NR 2 EPR GAUGE READS ZERO. REPLACED NR 2 EPR TRANSMITTER AND NR 2 EPR INDICATOR PER - [SDR P2EA99253](https://openairdocs.org/sdr/P2EA99253), Oct 5, 1999: SKIN. CRACKED. SJO - C-CHECK, LEFT RAM DOOR INNER SKIN CRACKED, DEFECT SIZE, LENGTH 3 INCHES AND WIDTH 1 INCH. REPAIRED RAM DOOR INTERNAL SKIN PER COOPESA EO COO-3-52-708-99 D - [SDR P2EA99220](https://openairdocs.org/sdr/P2EA99220), Jul 20, 1999: DOOR. MISSING. NSP - FLT 707 - THIS IS A SUPPLEMENTAL/CLOSING ACTION FOR MRR 99220. ON WALK-AROUND INSPECTION AFTER FLIGHT MAINTENANCE, CREW DISCOVERED THE CENTER BOOST PUMP D - [SDR P2EA99195](https://openairdocs.org/sdr/P2EA99195), May 25, 1999: PUMP. LEAKING. PIT - FLT 588 - NO EMERGENCY DECLARED, LANDING UNEVENTFUL. TOTAL LOSS OF SYSTEM 'A' HYDRAULICS. FOUND NR 2 ENGINE SYSTEM 'A' HDYRAULIC PUMP SHAFT SEAL BLOWN. RE - [SDR P2EA99090](https://openairdocs.org/sdr/P2EA99090), Mar 12, 1999: MECHANISM. WORN. MCI - FLT 819 - RETRACTING FLAPS FROM 5 TO 1 DEGREE OUT OF MDW, FELT HEAVY FLUTTER. GOING FROM FLAPS 1 TO 5 ON LANDING AT MCI FELT MINOR FLUTTER. LANDING AT MCI - [SDR P2EA99001](https://openairdocs.org/sdr/P2EA99001), Jan 7, 1999: VALVE. FAILED. MSP - FLT 404 - DURAL BLEED INDICATION DURING TAKEOFF. ABORTED TAKEOFF AT 70 KNOTS, RETURNED TO GATE. DEFERRED PER MEL 36-6, CI M219725 ASSIGNED. FEF CI M219725 - [SDR P2EA98312](https://openairdocs.org/sdr/P2EA98312), Dec 26, 1998: WINDOW. CRACKED. MCI - FLT 586 - THE AIRCRAFT DEPARTED MCI AND 35 MINUTES INTO FLIGHT THE FIRST OFFICERS SLIDING WINDOW CRACKED. THE AIRCRAFT RETURNED TO MCI WITHOUT INCIDENT. M - [SDR P2EA98311](https://openairdocs.org/sdr/P2EA98311), Dec 15, 1998: SKIN. CRACKED. SJO - NR 1 THRUST REVERSER LOWER BUCKET EXTERNAL SKIN CRACKED, DEFECT SIZE LENGTH 2.75 INCH. REPAIRED THRUST REVERSER PER COOPESA EO COO-3-78-754-98 DATED DEC 1 - [SDR P2EA98305](https://openairdocs.org/sdr/P2EA98305), Dec 8, 1998: SKIN. DAMAGED. SJO - PROVISIONAL REPAIR AT FORWARD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED FUSELAGE SKIN SECTION FROM BS 299 TO BS 305 BETWEEN STRINGER 12 RT AND STRINGER 14 R - [SDR P2EA98296](https://openairdocs.org/sdr/P2EA98296), Dec 1, 1998: SLAT. DELAMINATED. SJO - NR 5 SLAT DELAMINATED, DEFECT SIZE TOTAL 400 SQ INCH. REPAIRED NR 5 SLAT PER COOPESA EO COO-3-57-719-98 DATED DEC 2, 1998. DOCUMENTED ON FAA FORM 8110-3. - [SDR P2EA98307](https://openairdocs.org/sdr/P2EA98307), Nov 27, 1998: SKIN. DELAMINATED. SJO - NR 5 SPOILER DELAMINATED, DEFECT SIZE TOTAL 234 SQUARE INCH. REPAIRED NR 5 SPOILER PER COOPESA EO C00-3-57-709-98 DATED NOV 30, 1998. (M) - [SDR P2EA98306](https://openairdocs.org/sdr/P2EA98306), Nov 27, 1998: SKIN. DELAMINATED. SJO - NR 2 SPOILER DELAMINATED, DEFECT SIZE TOTAL 6 SQUARE INCH. REPAIRED NR 2 SPOILER PER COOPESA EO COO-3-57-710-98 DATED NOV 30, 1998. (M) - [SDR P2EA98303](https://openairdocs.org/sdr/P2EA98303), Nov 27, 1998: SKIN. DELAMINATED. SJO - NR 7 SPOILER DELAMINATED, DEFECT SIZE TOTAL 325 SQUARE INCH. REPAIRED NR 7 SPOILER PER COOPESA EO COO-3-57-711-98 DATED NOV 30, 1998. (M) - [SDR P2EA98298](https://openairdocs.org/sdr/P2EA98298), Nov 27, 1998: SPOILER. DELAMINATED. SJO - NR 8 SPOILER DELAMINATED, DEFECT SIZE TOTAL 320 SQ IN. REPAIRED NR 8 SPOILER PER COOPESA EO C00-3-57-713-98 DATED NOV 30, 1998. DOCUMENTED ON FAA FORM 811 - [SDR P2EA98295](https://openairdocs.org/sdr/P2EA98295), Nov 27, 1998: SPOILER. DELAMINATED. SJO - NR 6 SPOILER DELAMINATED, DEFECT SIZE TOTAL 160 SQ INCH. REPAIRED NR 6 SPOILER PER COOPESA EO COO-3-57-712-98 DATED NOV 30, 1998. DOCUMENTED ON FAA FORM 8 - [SDR P2EA98294](https://openairdocs.org/sdr/P2EA98294), Nov 22, 1998: SKIN. DAMAGED. SJO - FUSELAGE SKIN DOUBLER MISSING MATERIAL AT BS 178, WL 243, BETWEEN LBL 2 INCH AND LBL 7 INCH. REPLACED WINDOW CENTER POST DOUBLER AT BS 178, SL 243, BETWEE - [SDR P2EA98267](https://openairdocs.org/sdr/P2EA98267), Nov 21, 1998: STRINGER. CRACKED. SJO - STRINGER 15 LEFT CRACKED AT BS 360, DEFECT SIZE LENGTH .5 INCH. REPLACED STRINGER 15 LEFT SECTION FROM BS 348 TO BS 367 PER SRM 51-10-1 PAGE 5 AND SRM 51- - [SDR P2EA98266](https://openairdocs.org/sdr/P2EA98266), Nov 21, 1998: STRINGER. CRACKED. SJO - STRINGER 14 LEFT CRACKED AT BS 360, DEFECT SIZE LENGTH .5 INCH. REPLACED FUSELAGE STRINGER 14 LT SECTION FROM BS 367 TO BS 348 PR SRM 51-10-1 PAGE 5 AND S - [SDR P2EA98265](https://openairdocs.org/sdr/P2EA98265), Nov 21, 1998: FRAME. CRACKED. SJO - FRAME WEB CRACKED AT BS 303.9, BETWEEN STRINGER 16L AND STRINGER 17L, DEFECT SIZE, LENGTH 1 INCH. REPAIRED FUSELAGE WEB SECTION AT BS 303.9, BETWEEN STRIN - [SDR P2EA98293](https://openairdocs.org/sdr/P2EA98293), Nov 20, 1998: STRINGER. CORRODED. SJO - FOUND CORROSION AT BS 727A, STRINGER 22 LEFT, LOWER CHORD, DEFECT SIZE LENGTH 2.5 INCH WIDTH 1 INCH. REPAIRED FUSELAGE SKIN SECTION FROM BS 727 PLUS 11 IN - [SDR P2EA98273](https://openairdocs.org/sdr/P2EA98273), Nov 20, 1998: SKIN. CORRODED. FUSELAGE SKIN CORRODED BETWEEN BS 907 AND BS 967, BETWEEN STRINGER 4 RT AND STRINER 5 RT. REPLACED FUSELAGE SKIN SECTION FROM BS 902.5 TO BS 914, BETWEEN STRING - [SDR P2EA98268](https://openairdocs.org/sdr/P2EA98268), Nov 20, 1998: BEAM. CRACKED. SJO - FORWARD SERVICE DOOR NR 7 BEAM CRACKED, DEFECT SIZE LENGTH .5 INCH. REPAIRED FUSELAGE SKIN FORWARD ENTRY DOOR BEAM NR 7 BETWEEN BS 302 AND BS 309 PER SRM - [SDR P2EA98264](https://openairdocs.org/sdr/P2EA98264), Nov 20, 1998: FRAME. CRACKED. SJO - FRAME CRACKED AT BS 344, BETWEEN STRINGER 23 RT AND STRINGER 24 RT, DEFECT SIZE LENGTH 6.75 INCH. REPLACED FRAME SECTION AT BS 344, BETWEEN STRINGER 21 RT - [SDR P2EA98301](https://openairdocs.org/sdr/P2EA98301), Nov 19, 1998: SEAT TRACK. CRACKED. SJO - SEAT TRACK CRACKED AT BS 709, RBL 25 INCHES, WL 203.1, DEFECT SIZE LENGTH .625 INCH. REPAIRED FLOORBEAM SECTION FROM BS 698 AND BS 717, RBL 25 INCHES PER - [SDR P2EA98299](https://openairdocs.org/sdr/P2EA98299), Nov 19, 1998: SEAT TRACK. CRACKED. SJO - SEAT TRACK LOWER CHORD CRACKED AT FROM BS 663.75 TO BS 690 AT RBL 24.5, DEFECT SIZE LENGTH .563. REPAIRED FLOORBEAM UPPER CHORD BETWEEN BS 660 AND BS 682, - [SDR P2EA98291](https://openairdocs.org/sdr/P2EA98291), Nov 19, 1998: ANGLE. CRACKED. SJO - ANGLE CRACKED AT BS 559, RBL 46, WL 205 DEFECT SIZE LENGTH .4375. REPLACED FUSELAGE LOWER CHORD AT BS 559, WL 204, BETWEEN RBL 46 INCHES AND RBL 70 INCHES - [SDR P2EA98290](https://openairdocs.org/sdr/P2EA98290), Nov 19, 1998: FLOORBEAM. CRACKED. SJO - FLOORBEAM CRACKED AT BS 578, RBL 50, WL 206, DEFECT SIZE .5 INCH. REPAIRED FLOORBEAM WEB AT BS 578, BETWEEN RBL 45 INCHES TO RBL 70 INCHES, FROM WL 208 TO - [SDR P2EA98280](https://openairdocs.org/sdr/P2EA98280), Nov 19, 1998: WEB. CRACKED. SJO - WEB CRACKED AT BS 663.75, RBL 0, WL 206. DEFECT SIZE LENGTH 1.5 INCH. REPAIRED CENTER WING BOX, FLOORBEAM UPPER CHORD BETWEEN BS 650 AND BS 675, BL 0 PER - [SDR P2EA98274](https://openairdocs.org/sdr/P2EA98274), Nov 19, 1998: RIB. CRACKED. SJO - RIB CRACKED AT RIGHT WING FUEL TANK WBL 135.5, DEFECT SIZE LENGTH 1.125 INCH. REPAIRED RIGHT WING RIB LOWER CHORD AT WBL 135.5, BETWEEN STRINGER 2 AND STR - [SDR P2EA98270](https://openairdocs.org/sdr/P2EA98270), Nov 19, 1998: SEAT TRACK. CRACKED. SJO - SEAT TRACK WEB CRACKED AT BS 639, RBL 45.5, WL 201, DEFECT SIZE LENGTH 1 INCH. REPAIRED FUSELAGE WEB SECTION FROM BS 636 TO BS 642, FROM WL 204 TO WL 199. - [SDR P2EA98269](https://openairdocs.org/sdr/P2EA98269), Nov 19, 1998: STRINGER. CRACKED. SJO - STRINGER 5 LEFT SPLICE CRACKED AT BS 360, DEFECT SIZE LENGTH .75 INCH. REPLACED FUSELAGE STRINGER 5 LEFT SPLICE FROM 348.2 TO BS 367 PER SRM 51-10-1 PAGE - [SDR P2EA98260](https://openairdocs.org/sdr/P2EA98260), Nov 19, 1998: ANGLE. CRACKED. SJO - RIGHT EMERGENCY EXIT DOOR FRAME ANGLE CRACKED AT FORWARD SECTION, DEFECT SIZE LENGTH .375 INCH. REPLACED RIGHT EMERGENCY EXIT DOOR FORWARD FRAME ANGLE AT - [SDR P2EA98258](https://openairdocs.org/sdr/P2EA98258), Nov 19, 1998: SKIN. DAMAGED. SJO - LEFT WING OUTBOARD FOREFLAP LEADING EDGE SKIN REPAIR DOUBLER WORN. REPAIRED FOREFLAP LEADING EDGE SKIN BETWEEN WSL 493 AND WSL 488 PER SRM 57-50-4 FIG 1. - [SDR SIMA98257](https://openairdocs.org/sdr/SIMA98257), Nov 18, 1998: SKIN. CRACKED. SJO - FORWARD RIGHT UPPER HINGE CUTOUT CRACKED AT BS 310, DEFECT SIZE LENGTH .50 INCH. REPAIRED FORWARD RIGHT SERVICE DOOR SKIN SECTION BETWEEN BS 308 AND BS 31 - [SDR P2EA98308](https://openairdocs.org/sdr/P2EA98308), Nov 18, 1998: SKIN. CRACKED. SJO - INTERNAL DOUBLER CRACKED FORWARD ENTRY DOORWAY UPPER HINGE CUTOUT, DEFECT SIZE LENGTH 1.937 INCH. REPAIRED FUSELAGE SKIN FROM BS 297 TO BS 305 BETWEEN STR - [SDR P2EA98302](https://openairdocs.org/sdr/P2EA98302), Nov 18, 1998: WEB. CRACKED. SJO - WEB CRACKED AT BS 253, LBL 8 INCHES DEFECT SIZE, LENGTH .375 INCH. REPAIRED FUSELAGE WEB SECTION BETWEEN BS 232 AND BS 257, WL 190 FROM BL 0 TO LBL 18 INC - [SDR P2EA98300](https://openairdocs.org/sdr/P2EA98300), Nov 18, 1998: FRAME. CRACKED. SJO - AFT ENTRY DOOR LOWER PAN SECTION CRACKED. DEFECT SIZE LENGTH 1.125 INCH. REPLACED AFT ENTRY DOOR FRAME AT BS 949 PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. ( - [SDR P2EA98297](https://openairdocs.org/sdr/P2EA98297), Nov 18, 1998: SKIN. CANNING. SJO - AFT CARGO DOOR DENTED AND OL CANNED, DEFECT SIZE WIDTH 2.125 INCH DEPTH .060. REPLACED AFT CARGO DOOR OUTER SKIN BETWEEN BS 839 AND BS 887 PER SRM 51-10-1 - [SDR P2EA98292](https://openairdocs.org/sdr/P2EA98292), Nov 18, 1998: STRINGER. CORRODED. SJO - STRINGER 22 LEFT CORRODED BETWEEN BS 727 AND BS 727A, DEFECT SIZE LENGTH 3 INCH WIDTH .75 INCH. REPAIRED STRINGER 22 LEFT BETWEEN BS 727 AND BS 727A PLUS - [SDR P2EA98288](https://openairdocs.org/sdr/P2EA98288), Nov 18, 1998: SKIN. CRACKED. SJO - INTERNAL DOUBLER CRACKED AT THE AFT SERVICE DOORWAY LOWER HINGE CUTOUT, DEFECT SIZE LENGTH .75 INCH. REPAIRED FUSELAGE SKIN SECTION FROM BS 939 TO BS 953, - [SDR P2EA98281](https://openairdocs.org/sdr/P2EA98281), Nov 18, 1998: FRAME. CRACKED. SJO - FRAME CRACKED AT BS 578, WL 207, LBL 65, DEFECT SIZE LENGTH 5 INCH. REPLACED FUSELAGE FRAME SECTION AT BS 578, BETWEEN STRINGER 12 LEFT AND STRINGER 18 LE All 90: https://openairdocs.org/deregistered/N219US-2000-07-19/reports.md ## FAA accident and incident reports (5) 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 19990107015539I](https://openairdocs.org/incident/19990107015539I), Jan 7, 1999: Boeing 737281 (N219US), Minneapolis, MN. (-5) Aircraft aborted takeoff at 70 KTS due to dual bleed indication. Maintenance personnel determined that APU bleed valve failed in open postion. Replaced… - [Incident 19981226042259I](https://openairdocs.org/incident/19981226042259I), Dec 26, 1998: Boeing 737281 (N219US), Kansas City, MO. (-5) December 26, 1998, vanguard airlines Boeing 737-281, N219US, departed Kansas City International Airport, and returned to mci due to a cracked sliding… - [Incident 19970124006839I](https://openairdocs.org/incident/19970124006839I), Jan 24, 1997: Boeing 737281 (N219US), Denver, CO. Narrative: vanguard flight 612 returned to the field (dia) after flying for approximately 20 minutes, enroute to (mci) Kansas city, MO. (PIC) pilot in command… - [Incident 19960415013459I](https://openairdocs.org/incident/19960415013459I), Apr 15, 1996: Boeing 737281 (N219US), Dallas-Ft Worth, TX. Narrative: vanguard airlines (vam) flt 126 departed dfw for ict on takeoff/rotation the stick shaker activated. The crew made a turn back and landed… - [Incident 19891220065419I](https://openairdocs.org/incident/19891220065419I), Dec 20, 1989: Boeing 737281 (N219US), Miami, FL, Minor damage. Blew a tire on takeoff roll. Pilot knew nothing about tire blowing out until he landed at destination. --- 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.