# N797AS: 1998 Boeing 737-490, registration cancelled 2018-10-26 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 26, 2018 - Exported to: Austria - Status when cancelled: Valid registration - Airframe: [Boeing 737-490](https://openairdocs.org/model/boeing-737-490) (registry code 138449M) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs) - Serial number: 28892 - Year built: 1998 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 8, 1998 - Certificate issued: December 27, 2017 - Last registry action: December 27, 2017 - Mode S code: AAD217 - 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/N797AS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=797AS - Page: https://openairdocs.org/deregistered/N797AS-2018-10-26 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 737-490: https://openairdocs.org/model/boeing-737-490.md ## Service difficulty reports (193, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASAA2016060917002](https://openairdocs.org/sdr/ASAA2016060917002), Jun 9, 2016: LENS. DETACHED. F/A REPORTS EXIT SIGN AT OVERHEAD ROW 3 FWD SIDE COVER COMES OFF ON RT SIDE. ACFT GROUNDED. SECURED EXIT SIGN OVERHEAD AT ROW 3 AS REQUIRED. - [SDR ASAA2016041316390](https://openairdocs.org/sdr/ASAA2016041316390), Apr 13, 2016: LENS. BROKEN. EMERGENCY LIGHT EXIT LOCATOR SIGN LENS BROKEN AT L2 DOOR. ACFT GROUNDED. R & R LENS AND TESTED LIGHT ASSY IAW AMM 33-51-81-962-011. OPS NORMAL. - [SDR ASAA2016032716109](https://openairdocs.org/sdr/ASAA2016032716109), Mar 27, 2016: LENS. DETACHED. F/A REPORTS R2 DOOR EXIT SIGN FELL OFF. ACFT GROUNDED. REINSTALLED R2 DOOR EXIT SIGN IAW AMM 33-50-00. - [SDR ASAA2016031015879](https://openairdocs.org/sdr/ASAA2016031015879), Mar 10, 2016: LENS. MISSING. L2 DOOR SMALL EXIT LIGHT COVER MISSING. ACFT GROUNDED. REPLACED MISSING LENS COVER. - [SDR ASAA2016010614668](https://openairdocs.org/sdr/ASAA2016010614668), Jan 6, 2016: LENS. MISSING. EMERGENCY LIGHT EXIT LOCATOR SIGN LENS MISSING AT NR 4 GALLEY ADJACENT TO L-2 DOOR. ACFT GROUNDED. REPLACED LENS AND TESTED EXIT LOCATOR SIGN IAW AMM 33-51-81-9 - [SDR ASAA2015110313884](https://openairdocs.org/sdr/ASAA2015110313884), Nov 3, 2015: SHEAR TIE. CORRODED. FWD CARGO BAY, BS 500 BETWEEN STRINGERS 27 - 28R AFT SIDE OF FRAME HAS CORROSION. ACFT GROUNDED. R & R FRAME ANGLE IAW SRM 51-40-02-0G-0. - [SDR ASAA2015103013870](https://openairdocs.org/sdr/ASAA2015103013870), Oct 30, 2015: WEB. CRACKED. FWD CABIN AT BS 303 ON WEB ON 4L AREA IS CRACKED. ACFT GROUNDED. R & R WEB IAW SRM - [SDR ASAA2015103013819](https://openairdocs.org/sdr/ASAA2015103013819), Oct 30, 2015: STRINGER. CRACKED. AFTER REMOVING STRINGER CLIP AT BS 380 S-8R STR WAS FOUND TO BE CRACKED. ACFT GROUNDED. REPAIRED STRINGER IAW ASA EA 400 53EA 16105, THIS IS A CATEGORY B REPAIR - [SDR ASAA2015102813577](https://openairdocs.org/sdr/ASAA2015102813577), Oct 28, 2015: STRAP. CRACKED. INTERCOSTAL STRAP AT BS 294, STRINGER 4L IS CRACKED. ACFT GROUNDED. FAB, LOCATED AND DRILLED NEW STRAP IAW SRM 51-40-05-0G-0. - [SDR ASAA2015102713868](https://openairdocs.org/sdr/ASAA2015102713868), Oct 27, 2015: INTERCOSTAL. CRACKED. FWD WET AREA INTERCOSTAL CRACKED AROUND 2 FASTENER HOLES ON UPPER FLANGE BETWEEN BS 312-328 AT LBL44. ACFT GROUNDED. R & R INTERCOSTAL IAW SRM 51-40-02-0G-0. - [SDR ASAA2015102213832](https://openairdocs.org/sdr/ASAA2015102213832), Oct 22, 2015: FITTING. CRACKED. LEFT AFT LOWER HORIZONTAL THRUST BEAM FITTING IS CRACKED, REF TASK SB737-55-1091-400-1 STEP 17, REQUIRES ISSUANCE OF EC SB737-55-1091-400-2. ACFT GROUNDED. R & - [SDR ASAA2015102213598](https://openairdocs.org/sdr/ASAA2015102213598), Oct 22, 2015: ANGLE. CRACKED. PASSENGER CABIN FUSELAGE STIFFENER ANGLE CRACKED FWD OF R1 DOOR AT WL 240. ACFT GROUNDED. R & R ANGLE BETWEEN 12R AND 13R IAW SRM 51-40-02-0G-0. - [SDR ASAA2015102113837](https://openairdocs.org/sdr/ASAA2015102113837), Oct 21, 2015: FRAME. CRACKED. FRAME AT BS IS CRACKED BETWEEN S-8L AND S-9L. ACFT GROUNDED. REPAIRED FRAME IAW T/C AD20062609-400-53-107, REV 00, DATED 11SEP15. - [SDR ASAA2015102113834](https://openairdocs.org/sdr/ASAA2015102113834), Oct 21, 2015: FRAME. CRACKED. FRAME AT BS 907 IS CRACKED BETWEEN S-8R AND S-9R. ACFT GROUNDED. REPAIRED FRAME IAW T/C AD20062609 400-53-107, REV 00, DATED 11SEP15, FIG 2. - [SDR ASAA2015102113831](https://openairdocs.org/sdr/ASAA2015102113831), Oct 21, 2015: FRAME. CRACKED. FRAME AT BS 907 IS CRACKED BETWEEN S-8L AND S-9L. ACFT GROUNDED. REPAIRED FRAME IAW T/C AD20062609-400-53-107, REV 00, DATED 11SEP15. - [SDR ASAA2015102113830](https://openairdocs.org/sdr/ASAA2015102113830), Oct 21, 2015: FRAME. CRACKED. FRAME AT BS 380 IS CRACKED BETWEEN S-8R AND S-9R. ACFT GROUNDED. REPAIRED FRAME IAW T/C AD20062609 S400-53-107, REV 00, DATED 11SEP15, FIG 2. - [SDR ASAA2015102113829](https://openairdocs.org/sdr/ASAA2015102113829), Oct 21, 2015: FRAME. CRACKED. FRAME AT BS 480 IS CRACKED BETWEEN S-8R AND S-9R. ACFT GROUNDED. REPAIRED FRAME IAW T/C AD20061609-400-53-107, REV 00, DATED 11SEP15, FIG 2. - [SDR ASAA2015102113828](https://openairdocs.org/sdr/ASAA2015102113828), Oct 21, 2015: FRAME. CRACKED. FRAME AT BS 727F IS CRACKED BETWEEN S-8R AND S-9R. ACFT GROUNDED. REPAIRED FRAME IAW T/C AD20062609-400 -3-107, REV 00, DATED 11SEP15, FIG 2. - [SDR ASAA2015101713867](https://openairdocs.org/sdr/ASAA2015101713867), Oct 17, 2015: SKIN. DELAMINATED. RT WING NR 4 L/E SLAT INBD T/E WEDGE HAS POSSIBLE AREA OF DELAMINATION AT EDGE, MARKED. ACFT GROUNDED. REPAIRED RT WING NR 4 SLAT L/E IB T/E WEDGE AT EDGE IAW S - [SDR ASAA2015011910295](https://openairdocs.org/sdr/ASAA2015011910295), Jan 19, 2015: LENS. DETACHED. EMERGENCY EXIT SIGN BESIDE RT OVERWING EXIT FELL OFF. ACFT GROUNDED. REPLACED EMERGENCY EXIT SIGN FLOOR PROXIMITY LIGHT FOR RT AFT OVERWING EXIT REF AMM 33-51-8 - [SDR ASAA2014072608801](https://openairdocs.org/sdr/ASAA2014072608801), Jul 26, 2014: FRAME. DAMAGED. STUB FRAME HAS FIVE DAMAGED FASTENER HOLES AT BS 351 BETWEEN STRINGERS 16 - 17L. ACFT GROUNDED. REPAIRED FRAME IAW EA AD20121205-400-53-107. - [SDR ASAA2014072508799](https://openairdocs.org/sdr/ASAA2014072508799), Jul 25, 2014: SKIN. CHAFED. LEFT INBD MID FLAP UPPER SKIN IS CHAFED ON INBD EDGE. ACFT GROUNDED. CHAFE ON LT INBD MID FLAP UPPER SKIN WAS ON EXISTING REPAIR. REPAIRED UPPER SKIN IAW SRM 57 - [SDR ASAA2014072308800](https://openairdocs.org/sdr/ASAA2014072308800), Jul 23, 2014: SKIN. CHAFED. RIGHT INBD MID FLAP IS CHAFED AT THE VERY INBD TOP SIDE, JUST AFT OF INBD SIDE SEAL. ACFT GROUNDED. CHAFE ON RT INBD MID FLAP UPPER SKIN WAS ON A EXISTING REPAI - [SDR ASAA2014071008533](https://openairdocs.org/sdr/ASAA2014071008533), Jul 10, 2014: FLOORBEAM. CORRODED. CORROSION FOUND FLOOR PANEL FLOORBEAM SPLICE AT BS 772.6, AFT CARGO BAY. ACFT GROUNDED. REPLACED TEE SPLICE AND REINSTALLED FLOOR PANELS. - [SDR ASAA2014012112450](https://openairdocs.org/sdr/ASAA2014012112450), Jan 21, 2014: LENS. BROKEN. EMERGENCY LIGHT LOCATOR SIGNS ADJACENT TO L1 AND R1 DOORS HAVE BROKEN LENSES. ACFT GROUNDED. R & R LENS AND TESTED IAW MM 33-51-81-962-011. OPS NORMAL. - [SDR ASAA2013062095234](https://openairdocs.org/sdr/ASAA2013062095234), Jun 20, 2013: SCREW. SHEARED. FORWARD ENTRY DOOR (L-1) WILL NOT FULLY OPEN. DOOR HANDLE OPENS ABOUR 2/3 OF FULL AND DOOR ITSELF OPENS ABOUT 3-5. (NO PRESSURIZATION ISSUES NOTED) (NO COMMUICA - [SDR ASAA2013040794484](https://openairdocs.org/sdr/ASAA2013040794484), Apr 7, 2013: STIFFENER. CORRODED. APU COMPARTMENT RT SIDE APU AIR INLET FLANGE HAS CORROSION ON OTBD SIDE. REMOVED STIFFENER AT RT SIDE APU AIR INLET FLANGE AND REPLACED WITH NEW STIFFENER IAW S - [SDR ASAA2013040794467](https://openairdocs.org/sdr/ASAA2013040794467), Apr 7, 2013: FLANGE. CORRODED. APU COMPT. RT SIDE APU AIR INLET FLANGE FASTENER HOLES HAVE CORROSION. REMOVED CORRODED AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-80-13 1A 2, FIG - [SDR ASAA2013040594514](https://openairdocs.org/sdr/ASAA2013040594514), Apr 5, 2013: SKIN. CHAFED. LT WING INBD FOREFLAP UPPER SURFACE REPAIR DOUBLER IS CHAFED AT MID SECTION. REPLACED DOUBLER IAW SRM 51-70-10-2R-4 ON LT WING INBD FOREFLAP. - [SDR ASAA2013040494614](https://openairdocs.org/sdr/ASAA2013040494614), Apr 4, 2013: FLANGE. CORRODED. AFTER REMOVAL OF LT LOWER BLADE SEAL RETAINER, FOUND UPPER FLANGE CORRODED, LT WHEEL WELL MANIFOLD UPPER FLANGE. ACFT GROUNDED. R & R UPPER FLANGE IAW SRM 51-40 - [SDR ASAA2013040494536](https://openairdocs.org/sdr/ASAA2013040494536), Apr 4, 2013: SKIN. CHAFED. LT WING OTBD FOREFLAP L/E SKIN IS CHAFED AT INBD CORNER. REPAIRED LT WING OTBD FOREFLAP L/E SKIN IAW SRM 57 53 01 2R 1, FIG 201. - [SDR ASAA2013040494534](https://openairdocs.org/sdr/ASAA2013040494534), Apr 4, 2013: SKIN. CHAFED. LT WING INBD MIDFLAP L/E SKIN IS CHAFED AT MID SECTION. REPAIRED LT WING INBD MIDFLAP L/E IAW SRM 57 53 01 2R 2. - [SDR ASAA2013040494483](https://openairdocs.org/sdr/ASAA2013040494483), Apr 4, 2013: SKIN. CHAFED. RT WING OTBD FOREFLAP UPPER SURFACE IS CHAFED TWO PLACES. REPAIRED RT WING OTBD FOREFLAP UPPER SURFACE IAW SRM 51 70 10 2R 4, REPAIR 4. - [SDR ASAA2013040494408](https://openairdocs.org/sdr/ASAA2013040494408), Apr 4, 2013: SKIN. DENTED. LT FUSELAGE AT STA 422.2 5IN BELOW 14L IS A DENT WITHIN 3IN OF LAP SEAM C. REPAIRED DENT AT FUSELAGE STA 4202 BETWEEN STR 14L AND STR15L IAW ASA EA 400-53EA-101 - [SDR ASAA2013040394962](https://openairdocs.org/sdr/ASAA2013040394962), Apr 3, 2013: WEB. CORRODED. FWD CARGO BAY AFT CUTOUT FRAME AT BS 492 AT STR 23R UPPER STRAP ON REVEAL WEB IS CORRODED. ACFT GROUNDED. REMOVED, FABRICATED AND INSTALLED STRAP IAW DWG NR 65- - [SDR ASAA2013040394554](https://openairdocs.org/sdr/ASAA2013040394554), Apr 3, 2013: SKIN. CHAFED. NR 2 SLAT INBD LOWER SURFACE IS CHAFED. REPAIRED CHAFE ON NR 2 SLAT INBD LOWER SURFACE IAW SRM 51 70 10 2R 4, REPAIR 4, PARA 20, PG 48. - [SDR ASAA2013040394553](https://openairdocs.org/sdr/ASAA2013040394553), Apr 3, 2013: SKIN. CHAFED. RT WING INBD GROUND SPOILER LOWER SURFACE IS CHAFED MULTIPLE PLACES. ACFT GROUNDED. REMOVED AND REINSTALLED REPAIRED RT INBD GROUND SPOILER IAW SRM 51 70 10, PG - [SDR ASAA2013040394537](https://openairdocs.org/sdr/ASAA2013040394537), Apr 3, 2013: WEDGE. CHAFED. RT WING NR 5 SLAT T/E WEDGE LOWER SURFACE IS CHAFED AT INBD CORNER REPAIRED NR 5 SLAT LOWER INBD CORNER T/E WEDGE IAW SRM 51 70 10 2R 4, PERMANENT REPAIR. - [SDR ASAA2013040394535](https://openairdocs.org/sdr/ASAA2013040394535), Apr 3, 2013: SKIN. CHAFED. NR 2 SLAT INBD LWR SURFACE IS CHAFED. REPAIRED CHAFE ON NR 2 SLAT INBD LOWER SURFACE IAW SRM 51-70-10-2R-4. REPAIR 4, PARA 20 PG 48. - [SDR ASAA2013040394422](https://openairdocs.org/sdr/ASAA2013040394422), Apr 3, 2013: SKIN. CHAFED. RT WING INBD FOREFLAP UPPER SURFACE INBD REPAIR DOUBLER IS CHAFED AT INBD AFT CORNER. ACFT GROUNDED. REPAIRED CHAFE DAMAGE IAW SRM 51 70 10, REPAIR 4, PG 1. - [SDR ASAA2013040394407](https://openairdocs.org/sdr/ASAA2013040394407), Apr 3, 2013: SKIN. CHAFED. RT WING INBD FORFLAP UPPER SURFACE REPAIR DOUBLER IS CHAFED. ACFT GROUNDED. BONDED REPAIR OF RT WING INBD FOREFLAP UPPER SURFACE REPAIR DOUBLER IAW SRM 51 70 10 - [SDR ASAA2013040294486](https://openairdocs.org/sdr/ASAA2013040294486), Apr 2, 2013: FLOOR PANEL. CRACKED. AFT CARGO BAY FLOOR PANEL CRACKED. REMOVED, FABRICATED AND INSTALLED FLOOR PANEL IAW SRM 51-40-05-0G-0 AND AMM 25-52-51-004-001 AND AMM 25-52-51-404-011. - [SDR ASAA2012080892684](https://openairdocs.org/sdr/ASAA2012080892684), Aug 8, 2012: UNKNOWN. MULTIPLE FAIL. DURING CLIMBOUT, AUTOTHROTTLE FAILED, TRANSPONDER FAILED, GROUND PROXIMITY FAILED, ACARS REPORTED INCORRECTLY, ENGINE LOW IDLE ILLUMINATED ON THROTTLE REDUCTION - [SDR ASAA12410925](https://openairdocs.org/sdr/ASAA12410925), Jan 11, 2012: MECHANISM. LACK OF LUBE. F/A REPORTS L1 DOOR STIFF AND HARD TO OPEN AND CLOSE. VERIFIED THAT THE L1 DOOR IS TOO HARD TO SWING OPENED PER AMM 52 11 00 755 051 STEP D(5)(C) J. LUBED L1 DO - [SDR ASAA12410907](https://openairdocs.org/sdr/ASAA12410907), Jan 6, 2012: GUIDE ARM. OUT OF ADJUST. 1ST CLASS F/A REPORTED, SHE GOT THE L1 DOOR HALF WAY OPEN AND IT WAS VERY DIFFICULT TO OPEN ALL THE WAY. F/O WAS REQUIRED TO OPEN IT ALL THE WAY. EXCESSIVE DRAG - [SDR ASAA1149347](https://openairdocs.org/sdr/ASAA1149347), Mar 27, 2011: SIGN. BROKEN. EMERGENCY LIGHT EXIT LOCATOR SIGN AT L1 DOOR IS BROKEN. REMOVED AND REPLACED EXIT LOCATOR SIGN AND PERFORMED TEST PER B737 400 AMM 33 51 81 962 011. OPS NORMAL. - [SDR ASAA1149130](https://openairdocs.org/sdr/ASAA1149130), Mar 3, 2011: FLOORBEAM. CORRODED. CORROSION ON FUSELAGE FLOORBEAM BS 986.5 LBL 20 AND RBL 45. REPAIRED FLOORBEAM IAW ASA EA 400 53EA 04881. - [SDR ASAA1149128](https://openairdocs.org/sdr/ASAA1149128), Mar 3, 2011: CREASE BEAM. CORRODED. AFTER REMOVAL OF PARTS TO ACCESS FLOORBEAM REPAIR AT BS 986 FOUND CORROSION ON CREASE BEAM WEB AT BS 1008 RBL 42. REMOVED CORRODED WEB FABRICATED REPLACEMENT PA - [SDR ASAA1149127](https://openairdocs.org/sdr/ASAA1149127), Mar 3, 2011: FLOOR SUPPORT. CRACKED. FLOOR STRUCTURE SUPPORT AT BS 986 TO BS 1006 RBL 32 CRACKED. REMOVED AND REPLACED FLOOR STRUCTURE SUPPORT IAW B737 400 SRM 51 40 02. - [SDR ASAA1149126](https://openairdocs.org/sdr/ASAA1149126), Mar 3, 2011: SHEAR WEB. CORRODED. AFTER REMOVAL OF PARTS TO ACCESS FLOORBEAM REPAIR AT BS 986 FOUND CORROSION ON LOWER SURFACE OF SHEAR WEB AT BS 986 LBL 42. FABRICATED NEW SHEAR WEB AND INSTALL All 193: https://openairdocs.org/deregistered/N797AS-2018-10-26/reports.md ## Other aircraft with N797AS - [Cancelled 1986-01-03](https://openairdocs.org/deregistered/N797AS-1986-01-03): Boeing 727-90C, S/N 19169, built 1966. Exported to Canada. Owner: [Alaska Airlines Inc](https://openairdocs.org/faa-owner/ALASKA%20AIRLINES%20INC), [Seattle, WA](https://openairdocs.org/faa-place/WA/Seattle) --- 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.