# N703AS: 1998 Boeing 737-490, registration cancelled 2018-11-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 28, 2018 - Exported to: Austria - Status when cancelled: Valid registration - Airframe: [Boeing 737-490](https://openairdocs.org/model/boeing-737-490) (registry code 138449M) - Engine: [GE CFM56 series](https://openairdocs.org/engine/ge-cfm56-series) (registry code 30016) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 28893 - Year built: 1998 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 10, 1998 - Certificate issued: December 27, 2017 - Last registry action: December 27, 2017 - Mode S code: A95FC4 - Owner when cancelled: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%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/N703AS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=703AS - Page: https://openairdocs.org/deregistered/N703AS-2018-11-28 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 737-490: https://openairdocs.org/model/boeing-737-490.md ## Service difficulty reports (183, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASAA2016050416624](https://openairdocs.org/sdr/ASAA2016050416624), May 4, 2016: LAMP. FAILED. DOOR EMERGENCY EXIT SIGN LAMPS INOPERATIVE, ACFT GROUNDED. REPLACED THE LAMPS. OPS CHECKED NORMAL. - [SDR ASAA2015100113552](https://openairdocs.org/sdr/ASAA2015100113552), Oct 1, 2015: DOUBLER. CRACKED. L2 DOOR CUTOUT BEARSTRAP IS CRACKED AT THE FWD LOWER RADIUS. ACFT GROUNDED. REPAIRED L2 DOORWAY CUTOUT FWD, LOWER BEAR STRAP IAW SRM 53-00-01-2R-32, DETAIL IV. - [SDR ASAA2015100113536](https://openairdocs.org/sdr/ASAA2015100113536), Oct 1, 2015: STIFFENER. CORRODED. APU TORQUE BOX CUTOUT AT 10888 BULKHEAD INBD STIFFENER FLANGE CORRODED. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS, FOUND TO BE OUT OF LIMITS IAW SRM 5 - [SDR ASAA2015100113438](https://openairdocs.org/sdr/ASAA2015100113438), Oct 1, 2015: INTERCOSTAL. CORRODED. FLOOR SUPPORT STRUCTURE AT APPROXIMATELY BS 360 JUST AFT OF G2 INBD GALLEY MOUNT IS CORRODED. ACFT GROUNDED. REAMED HOLE FOR NUTPLATE ON FLOOR SUPPORT STRUCTURE - [SDR ASAA2015100113525](https://openairdocs.org/sdr/ASAA2015100113525), Oct 1, 2015: DOOR SILL. CORRODED. L1 MOPSILL HAS AREAS OF CORROSION ON UPPER SURFACE. ACFT GROUNDED. BLENDED CORRODED AREAS ON L1 MOPSILL, INNER CHORD OUT OF LIMITS, REMOVED AND INSTALLED NEW MO - [SDR ASAA2015093013594](https://openairdocs.org/sdr/ASAA2015093013594), Sep 30, 2015: FLOORBEAM. CORRODED. BS 986 FLOORBEAM UPPER HORIZONTAL FLANGE HAS AREAS OF CORROSION. ACFT GROUNDED. REPAIRED FLOORBEAM IAW EA 400, 53EA 15973. - [SDR ASAA2015093013593](https://openairdocs.org/sdr/ASAA2015093013593), Sep 30, 2015: STRINGER. CORRODED. STRINGER 21R AT BS 986 HAS LARGE AREA OF CORROSION. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-A-1. REMOVED, - [SDR ASAA2015093013533](https://openairdocs.org/sdr/ASAA2015093013533), Sep 30, 2015: FRAME. CORRODED. FRAME AT BS 992 HAS AREAS OF CORRODED JUST ABOVE L2 MOPSILL. ACFT GROUNDED. REPAIRED FRAME IAW EA 400 53EA, 15969. THIS IS A CAT B REPAIR WITH TRACKING IAW 400, - [SDR ASAA2015093013493](https://openairdocs.org/sdr/ASAA2015093013493), Sep 30, 2015: DOOR SILL. CORRODED. L2 MOPSILL HAS AREAS OF CORROSION ON UPPER SURFACE. ACFT GROUNDED. R & R MOPSILL IAW SRM 51-40-02-0G-0 AND DWG NR 65-52878, W 5", O .071", R .060, L 1", D .011" - [SDR ASAA2015093013439](https://openairdocs.org/sdr/ASAA2015093013439), Sep 30, 2015: STRINGER CLIP. CRACKED. STRINGER CLIP AT BS 947 AT 25R IS CRACKED. ACFT GROUNDED. REMOVED, LOCATED AND DRILLED NEW CLIP AND INSTALLED IAW SRM 51-40-02-0G-0, 51-40-05-0G-0. - [SDR ASAA2015093013453](https://openairdocs.org/sdr/ASAA2015093013453), Sep 30, 2015: FRAME. CRACKED. FRAME AT BS 400 BETWEEN STRINGERS 8-9L IS CRACKED. ACFT GROUNDED. REPAIRED THE FRAME IAW TC QAD20062609 400-53-107, FIG 2. - [SDR ASAA2015093013451](https://openairdocs.org/sdr/ASAA2015093013451), Sep 30, 2015: ANGLE. CRACKED. INTERCOSTAL AT BS 727A AT 25R HAS A CRACKED ATTACH ANGLE. ACFT GROUNDED. REMOVED ANGLE IAW SRM 51-40-02-0G-0, FIG 8 INSTALLED NEW ANGLE IAW SRM 51-40-02-0G-0, P - [SDR ASAA2015092913578](https://openairdocs.org/sdr/ASAA2015092913578), Sep 29, 2015: SPAR. CORRODED. RIGHT HORIZONTAL STABILIZER AFT UPPER ATTACH LUG, STABILIZER SIDE, HAS CORROSION ON AFT FACE. ACFT GROUNDED. REPAIRED RT HORIZONTAL STABILIZER AFT UPPER ATTACH - [SDR ASAA2015092913472](https://openairdocs.org/sdr/ASAA2015092913472), Sep 29, 2015: STRINGER. CORRODED. STRINGER AT BS 500G AT 27R IS CORRODED AROUND DOMENUT. ACFT GROUNDED. REMOVED CORRODED FROM STR 27R AT BS 500G FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03-1A-1, - [SDR ASAA2015092913454](https://openairdocs.org/sdr/ASAA2015092913454), Sep 29, 2015: ATTACH ANGLE. CRACKED. INTERCOSTAL AT BS 500E AT 26R HAS A CRACKED ATTACHED ANGLE. ACFT GROUNDED. R & R ATTACH ANGLE IAW SRM 51-40-02-0G-0, PARA 4 AND 7D. - [SDR ASAA2015092913452](https://openairdocs.org/sdr/ASAA2015092913452), Sep 29, 2015: ANGLE. CRACKED. INTERCOSTAL AT BS 500E AT 26L HAS A CRACKED ANGLE. ACFT GROUNDED. R & R ANGLE IAW SRM 51-40-02-0G-0, PARA 4 AND 7D. - [SDR ASAA2015092913362](https://openairdocs.org/sdr/ASAA2015092913362), Sep 29, 2015: ANGLE. CRACKED. INTERCOSTAL AT BS 500F 26L HAS A CRACKED ANGLE. ACFT GROUNDED. R & R ANGLE IAW SRM 51-40-02-0G-0, PARA 4 AND 7D. - [SDR ASAA2015092913361](https://openairdocs.org/sdr/ASAA2015092913361), Sep 29, 2015: ANGLE. CRACKED. INTERCOSTAL AT BS 500F AT 26R HAS A CRACKED ANGLE. ACFT GROUNDED. R & R ANGLE IAW SRM 51-40-02-0G-0, PAR 4 AND 7D. - [SDR ASAA2014081308932](https://openairdocs.org/sdr/ASAA2014081308932), Aug 13, 2014: FLOOR SUPPORT. CRACKED. FLOOR SUPPORT, LBL 24.82 BETWEEN BS 660 - 666 IS CRACKED. ACFT GROUNDED. REPAIRED IAW EA NR AD20080506-400-57-119. - [SDR ASAA2014081208909](https://openairdocs.org/sdr/ASAA2014081208909), Aug 12, 2014: SKIN. CHAFED. LEFT WING INBD EXHAUST GATE UPPER OTBD CORNER IS CHAFED. ACFT GROUNDED. REPAIRED EXHAUST GATE IAW SRM 57-53-01-2R-10 ADJUSTMENT CK GOOD IAW MM 27-51-05-404-016 - [SDR ASAA2014081208908](https://openairdocs.org/sdr/ASAA2014081208908), Aug 12, 2014: FRAME. CRACKED. FRAME BS 360 CRACKED BY A SCREW THAT WAS TOO LONG IN NUT PLATE BETWEEN STRINGERS 12 AND 13L. ACFT GROUNDED. REPAIRED FRAME IAW EA 400, 53EA, 13259. - [SDR ASAA2014081208899](https://openairdocs.org/sdr/ASAA2014081208899), Aug 12, 2014: SKIN. CHAFED. RT WING INDB EXHAUST GATE UPPER SKIN IS CHAFED. ACFT GROUNDED. REMOVED EXISTING REPAIR AND INSTALLED NEW REPAIR DOUBLER ON RT WING INBD EXHAUST GATE UPPER SKIN - [SDR ASAA2014081208898](https://openairdocs.org/sdr/ASAA2014081208898), Aug 12, 2014: SKIN. CHAFED. LEFT INBD MID FLAP IS CHAFED AT INBD UPPER EDGE. ACFT GROUNDED. REPAIRED LT INBD MID FLAP INBD UPPER SKIN IAW SRM 57-53-01-2R-3. - [SDR ASAA2014050907753](https://openairdocs.org/sdr/ASAA2014050907753), May 9, 2014: LIGHT. BROKEN. AFT OVERWING EXIT DOOR LT SIDE EMERGENCY LIGHT ASSY BROKEN. ACFT GROUNDED. REPLACED AFT LT OVERWING EMERGENCY LIGHT ASSY OPS CHECK GOOD IAW AMM 33-31-01. - [SDR ASAA2014031007134](https://openairdocs.org/sdr/ASAA2014031007134), Mar 10, 2014: LENS. DISLODGED. EXIT LAMP COVER FELL OFF AT RT FORWARD OVERWING EXIT. ACFT GROUNDED. RE-INSTALLED EXIT LENSE COVER RT FWD OVERWING EXIT. - [SDR ASAA2013061295080](https://openairdocs.org/sdr/ASAA2013061295080), Jun 12, 2013: SUPPORT. CRACKED. NR 6 SLAT ACTUATOR DOOR LANDING ON WING BENT. R & R 36 SLAT ACT DOOR LANDING (SUPPORT) IAW SRM 51-40-02-0G-0. - [SDR ASAA2013060795016](https://openairdocs.org/sdr/ASAA2013060795016), Jun 7, 2013: RETAINER. CRACKED. SEAL RETAINER CRACKED FOR SEAL ON LWR SHELF PANEL AFT OF RT MLG FOUND DURING SEAL REPLACEMENT. ACFT GROUNDED. FABRICATED, LOCATED AND DRILLED NEW RETAINER IAW B - [SDR ASAA2013060795015](https://openairdocs.org/sdr/ASAA2013060795015), Jun 7, 2013: HINGE. CHAFED. RT MLG OUTER DOOR AFT HINGE ARM CHAFED. ACFTGROUNDED. R & R RT MLG OUTER DOOR AFT HINGE ARM IAW SRM 51-40-02. - [SDR ASAA2013060795012](https://openairdocs.org/sdr/ASAA2013060795012), Jun 7, 2013: RETAINER. CORRODED. LEFT NR 3 UPPER BLADE SEAL RETAINER IS CORRODED ON BOTTOM SIDE. ACFT GROUNDED. REMOVED CORROSION ON LT NR 3 UPPER BLADE SEAL RETAINER. MATERIAL LOSS FOUND TO BE - [SDR ASAA2013060795011](https://openairdocs.org/sdr/ASAA2013060795011), Jun 7, 2013: RETAINER. CORRODED. LT MLG NR 4 LWR BLADE SEAL RETAINER HAS MULTIPLE SPOTS OF CORROSION. ACFT GROUNDED. R & R RETAINER IAW SRM 51-40-05-0G-0, FIG 2, PAGE 5, W .50, O .063, R .056, - [SDR ASAA2013060795010](https://openairdocs.org/sdr/ASAA2013060795010), Jun 7, 2013: FAIRING. CHAFED. RIGHT AFT NR 5 MLG SKI JUMP FAIRING IS CHAFED. ACFT GROUNDED. - [SDR ASAA2013060795009](https://openairdocs.org/sdr/ASAA2013060795009), Jun 7, 2013: SUPPORT BRACKET. CRACKED. NR 2 ENG PYLON AFT RT PANEL SUPPORT BRACKET CRACKED ON UPPER END (AFT OF RT MID SPAR ATTACH PIN LUG) ACFT GROUNDED. REMOVED NR 2 OTBD SUPPORT ASSY, FABRICATED N - [SDR ASAA2013060795008](https://openairdocs.org/sdr/ASAA2013060795008), Jun 7, 2013: WEB. GOUGED. AFT CARGO DOOR CUTOUT LWR FWD REVEAL WEB IS DAMAGED ALONG AFT EDGE. ACFT GROUNDED. FABRICATED NEW REVEAL IAW SRM 51-70-13, OG 0 AND DWG NO 65-56655-2. - [SDR ASAA2013060695022](https://openairdocs.org/sdr/ASAA2013060695022), Jun 6, 2013: SKIN. DENTED. RT INBD FOREFLAP FOUND DENT CLUSTER ON LWR SURFACE STARTING AT 43" FROM INBD END TO 53" AND 2 TO 12" FROM T/E. ACFT GROUNDED. REPAIRED IAW SRM 51-70-10-2R-4, RE - [SDR ASAA2013060395052](https://openairdocs.org/sdr/ASAA2013060395052), Jun 3, 2013: TAB. DAMAGED. LEFT ELEVATOR TAB INBD EDGE IS DAMAGED. BONDED REPAIR ON LT ELEVATOR TAB, INBD CORNER EDGE IAW SRM 51-70-17, REPAIR 11. - [SDR ASAA2013053194994](https://openairdocs.org/sdr/ASAA2013053194994), May 31, 2013: SEAT. CRACKED. L1 DOOR FWD UPPER DOOR SEAL LOCATOR IS CRACKED. R & R L1 DOOR FWD SEAL LOCATOR IAW BAC5065, PG 24-27. - [SDR ASAA2013053194968](https://openairdocs.org/sdr/ASAA2013053194968), May 31, 2013: SKIN. DENTED. NR 3 SPOILER UPPER SURFACE DENTED WITH A CREASE LOCATION 4.5 FROM T/E AND 12 FROM INBD END. REPAIRED NR 3 SPOILER UPPER AFT INBD SKIN IAW SRM 51-70-10-2R-4, REP - [SDR ASAA2013052895002](https://openairdocs.org/sdr/ASAA2013052895002), May 28, 2013: STRUCTURE. CORRODED. RIGHT WHEEL WELL MANIFOLD ASSY LOWER FWD STRUCTURE HAS BARE METAL AND SURFACE CORRODED, FWD AND AFT SIDES. ACFT GROUNDED. BLENDED CORROSION, FOUND TO BE 100 MAT - [SDR ASAA2013052894883](https://openairdocs.org/sdr/ASAA2013052894883), May 28, 2013: SKIN. DENTED. FUSELAGE DAMAGE AFT OF L2 DOOR BOTTOM CORNER. ACFT GROUNDED. REPAIRED FUSELAGE SKIN AFT OF L2 DOOR BOTTOM CORNER STA 1010, STR 15L IAW SRM 53-00-01-2R-35. - [SDR ASAA2013052694983](https://openairdocs.org/sdr/ASAA2013052694983), May 26, 2013: STRAP. CRACKED. AFT CARGO COMPARTMENT UNDER STRAP, FS 847-867 IS CRACKED. ACFT GROUNDED. FABRICATED NEW STRAP STA 847-867, STR 25R IAW SRM 51-40-05-0G-0 STRAP TO BE INSTALLED O - [SDR ASAA2013052694885](https://openairdocs.org/sdr/ASAA2013052694885), May 26, 2013: FLOORBEAM. CORRODED. ON REMOVAL OF NR 2 AFT CARGO FLOORBOARD, FOUND FLOOR SPLICE AT BS 727D CORRODED. ACFT GROUNDED. BLENDED AND FOUND TO BE OUT OF LIMITS. FABRICATED, ALODINED, PRI - [SDR ASAA2013052495004](https://openairdocs.org/sdr/ASAA2013052495004), May 24, 2013: DOOR FRAME. CORRODED. AFT CARGO DOOR CUTOUT FWD FRAME REPAIR DOUBLER IS CORRODED. FOUND ON REMOVAL OF TRANSITION PANEL. ACFT GROUNDED. R & R AFT CARGO DOOR CUTOUT FWD FRAME AND FACTO - [SDR ASAA2013052295048](https://openairdocs.org/sdr/ASAA2013052295048), May 22, 2013: STIFFENER. CORRODED. APU BAY RT TORQUE BOX INLET CUTOUT LOWER STIFFENER IS CORRODED, BS 1118-1127. R & R RT TORQUE BOX INLET CUTOUT LOWER STIFFENER IAW SRM 51-40-05-0G-0 AND 51-40-0 - [SDR ASAA2013052295013](https://openairdocs.org/sdr/ASAA2013052295013), May 22, 2013: RETAINER. CORRODED. LEFT MLG NR 3 LOWER BLADE SEAL RETAINER HAS BARE METAL. ACFT GROUNDED. R & R LEFT MLG NR 3 LWR BLADE SEAL RETAINER IAW SRM 51-40-05-0G-0, FIG 2, PAGE 5, W 0.50, - [SDR ASAA2013052294880](https://openairdocs.org/sdr/ASAA2013052294880), May 22, 2013: STIFFENER. CORRODED. APU COMPARTMENT RT TORQUE BOX INLET CUTOUT UPPER STIFFENER IS CORRODED STA 1112 TO 1127. ACFT GROUNDED. R & R TORQUE BOX CUT OUT UPPER STIFFENER IAW SRM 51-40-0 - [SDR ASAA2013052195014](https://openairdocs.org/sdr/ASAA2013052195014), May 21, 2013: WEB. CORRODED. UPON REMOVAL OF AFT RT LWR MANIFOLD STRUCTURE FOUND WEB TO BE CORRODED. ACFT GROUNDED. REPAIRED RT MLG MANIFOLD WEB IAW EA 400 53, EA 10436, REV NEW DATED 30MAY - [SDR ASAA2013052095001](https://openairdocs.org/sdr/ASAA2013052095001), May 20, 2013: SUPPORT ANGLE. CRACKED. NR 1 PYLON INBD AFT SUPPORT ANGLE AFT OF FUSE PIN IS CRACKED. ACFT GROUNDED. REMOVED AND INSTALLED NR 1 PYLON INBD SUPPORT ANGLE IAW SRM 51-40-02. - [SDR ASAA2013052094916](https://openairdocs.org/sdr/ASAA2013052094916), May 20, 2013: WEB. CRACKED. L1 AFT REVEAL WEB IS CRACKED. FABRICATED NEW WEB L1 AFT REVEAL IAW BAC DWG 65-17685. - [SDR ASAA2013051915373](https://openairdocs.org/sdr/ASAA2013051915373), May 19, 2013: FLOOR PANEL. CORRODED. UPON REMOVAL OF PIT SIDEWALL PANEL FOUND NR 1 FLOOR PANEL RT EDGE TO HAVE LIGHT SURFACE CORROSION. ACFT GROUNDED. REMOVED CORROSION ON NR 1 FLOOR PANEL MATERIAL - [SDR ASAA2013051995018](https://openairdocs.org/sdr/ASAA2013051995018), May 19, 2013: ANGLE. CHAFED. LT WING INBD UPPER T/E SHELF PANEL ATTACH ANGLE CHAFED ON LWR SIDE. ACFT GROUNDED. DAMAGE AREA FOUND TO BE OUT OF LIMITS IAW SRM 57-51-02-1A-1. R & R ANGLE IAW All 183: https://openairdocs.org/deregistered/N703AS-2018-11-28/reports.md ## FAA accident and incident reports (3) 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 20081205851849I](https://openairdocs.org/incident/20081205851849I), Dec 5, 2008: Boeing 737490 (N703AS), Palm Springs, CA, No damage. (-23) Alaska 387 sfo to psp encountered a split flap indication. Emergency declared. Crew exercised manual extension per operational procedures. Aircraft… - [Incident 20080417014229I](https://openairdocs.org/incident/20080417014229I), Apr 17, 2008: Boeing 737490 (N703AS), Seattle, WA, No damage. (-23) Asa flight 529, inbound to sea initially reported an unsafe gear indication while on approach. When extended, the nose gear indicated a red light and… - [Incident 20070413005789I](https://openairdocs.org/incident/20070413005789I), Apr 13, 2007: Boeing 737490 (N703AS), Juneau, AK. (-23) Acft in cruise over sitka (sit) FL310 experienced electrical failure, DC fail lights, master caution illuminated, avionics pwr failure, loss of… --- 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.