# N708AS: 1999 Boeing 737-490, registration cancelled 2018-10-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 9, 2018
- Exported to: Ireland
- 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: 28895
- Year built: 1999
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 22, 1999
- Certificate issued: November 1, 2017
- Last registry action: November 1, 2017
- Mode S code: A97257
- Owner when cancelled: [Classic 490 LLC](https://openairdocs.org/faa-owner/CLASSIC%20490%20LLC)
- Location: [Lake Mary, FL](https://openairdocs.org/faa-place/FL/Lake%20Mary)
- Owner type: Corporation
- Owner's area on the map: 28.7714° N, 81.3530° W: Placed by OpenAirDocs at the center of ZIP code 32746, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N708AS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=708AS
- Page: https://openairdocs.org/deregistered/N708AS-2018-10-09

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 (151, newest 50)

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

- [SDR ASAA2017053020919](https://openairdocs.org/sdr/ASAA2017053020919), May 30, 2017: BATTERY PACK. FAILED. EMERGENCY EXIT LIGHTS ABOVE SEAT ROWS 1 - 11ABC FOUND INOPERATIVE. ACFT GROUNDED. REMOVED AND REPLACED THE BATTERY PACK, OPS NORMAL IAW AMM 33-51-06-960-805.
- [SDR ASAA2016110718677](https://openairdocs.org/sdr/ASAA2016110718677), Nov 7, 2016: FITTING. CORRODED. AFTER REMOVAL OF OTBD FOREFLAP OTBD TORQUE TUBE, FOUND ATTACH FITTING FOR TORQUE TUBE CORRODED. ACFT GROUNDED. REMOVED & REPLACED THE FITTING IAW AMM 20-80-11-9
- [SDR ASAA2016110718675](https://openairdocs.org/sdr/ASAA2016110718675), Nov 7, 2016: FITTING. CORRODED. AFTER REMOVAL OF INBD FOREFLAP INBD TORQUE TUBE, FOUND ATTACH FITTING FOR TORQUE TUBE CORRODED. ACFT GROUNDED. REMOVED AND REPLACED THE FITTING IAW AMM 20-50-11
- [SDR ASAA2016103118688](https://openairdocs.org/sdr/ASAA2016103118688), Oct 31, 2016: FRAME. CRACKED. PAX CABIN FRAME CRACKED BS 827 BETWEEN STRINGERS 8 AND 9R. ACFT GROUNDED. REPAIRED THE FRAME IAW T/C AD20062609-400-53-107 REV 00.
- [SDR ASAA2016103018772](https://openairdocs.org/sdr/ASAA2016103018772), Oct 30, 2016: FLOORBEAM. CRACKED. CABIN FLOORBEAM CRACKED AT BS 538 LBL 1 - 22. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-05-0G-0.
- [SDR ASAA2016103018674](https://openairdocs.org/sdr/ASAA2016103018674), Oct 30, 2016: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT RBL 22 CORRODED AT BS 952. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51-01-1, REMOVED AND REPLACED THE FLOOR SU
- [SDR ASAA2016103018673](https://openairdocs.org/sdr/ASAA2016103018673), Oct 30, 2016: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT LBL 42 BS 947 TO 967 CORRODED MULTIPLE AREAS. ACFT GROUNDED. REMOVED AND REPLACED DAMAGED FLOOR SUPPORT IAW SRM 51-40-02-0G-0.
- [SDR ASAA2016103018672](https://openairdocs.org/sdr/ASAA2016103018672), Oct 30, 2016: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT LBL 22 CORRODED AT BS 952. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0W.
- [SDR ASAA2016102918676](https://openairdocs.org/sdr/ASAA2016102918676), Oct 29, 2016: SKIN. CHAFED. LT WING I/B EXHAUST GATE O/B UPPER CORNER SKIN IS CHAFED. GROUNDED - YES. REMOVED DAMAGE FROM UPPER SKIN REMAINING MAT. FOUND TO BE .0605, RESTORED FINISH IAW S
- [SDR ASAA2016102818755](https://openairdocs.org/sdr/ASAA2016102818755), Oct 28, 2016: CARGO TRACK. CRACKED. AFT CARGO RT CARGO TRACK IS CRACKED IN RADIUS OF VERTICAL LEG AT BS 747. ACFT GROUNDEDS. REPAIRED THE CARGO TRACK IAW SRM 53-00-53-2R-2 AND EA 400-53EA-18029.
- [SDR ASAA2016102818708](https://openairdocs.org/sdr/ASAA2016102818708), Oct 28, 2016: CARGO TRACK. CRACKED. AFT CARGO BAY RT CARGO TRACK IS CRACKED IN THE RADIUS OF VERTICAL LEG AT BS 727C. ACFT GROUNDED. REPAIRED THE CARGO TRACK IAW SRM 53-00-53-2R-2.
- [SDR ASAA2016102818678](https://openairdocs.org/sdr/ASAA2016102818678), Oct 28, 2016: FLOORBEAM. CORRODED. FLOORBEAM BS 312 HAS SPOT OF CORROSION AT LBL 14. ACFT GROUNDED. REPAIRED DMGE TO FLOOR BEAM UPPER CHORD IAW SRM 53-10-51-2R-5.
- [SDR ASAA2016102818557](https://openairdocs.org/sdr/ASAA2016102818557), Oct 28, 2016: TRANSITION PANEL. CRACKED. AFT CARGO RIGHT TRANSITION IS CRACKED AT BS 727F. ACFT GROUNDED. REMOVED CRACKED TRANSITION PANEL AND REPLACED WITH NEW IAW SRM 51 40 02 0G 0.
- [SDR ASAA2016081217684](https://openairdocs.org/sdr/ASAA2016081217684), Aug 12, 2016: ARM. OUT OF ADJUST. L1 DOOR WILL NOT CLOSE. THERE WERE NO PRESSURIZATION ISSUES ON PREVIOUS FLIGHT SEGMENT. ACFT GROUNDED. ADJUSTED L1 DOOR GUIDE ARM, IAW AMM 52-11-00-705. ACCOMPL
- [SDR ASAA2016051716786](https://openairdocs.org/sdr/ASAA2016051716786), May 17, 2016: LATCH. GOUGED. AFT CARGO DOOR HANDLE RECESS IS GOUGED FROM MISSING HANDLE BUMPER. ACFT GROUNDED. REMOVED RIVETS FROM HOUSING, REF SRM 51-40-02. ALL HOLES PREVIOUSLY OVERSIZED 
- [SDR ASAA2016041316391](https://openairdocs.org/sdr/ASAA2016041316391), Apr 13, 2016: CONTROLLER. FAILED. PROMPTLY AFTER LEVEL OFF AT FL 310 HEARD CABIN ALTITUDE WARNING HORN ACCOMPANIED BY VISUAL CABIN RED ANNUNCIATER LIGHT PERFORMED QRH CHECKLIST PROCEDURES & EXEC
- [SDR ASAA2015100513347](https://openairdocs.org/sdr/ASAA2015100513347), Oct 5, 2015: LAMP. FAILED. EMERGENCY LIGHT EXIT LOCATOR SIGNS AT LT FORWARD, LT AFT, AND RT AFT OVERWING EXITS HAVE MULTIPLE LAMPS INOPERATIVE. ACFT GROUNDED. RELAMPED AND TESTED IAW MM 3
- [SDR ASAA2015082012954](https://openairdocs.org/sdr/ASAA2015082012954), Aug 20, 2015: FLOOR SUPPORT. BENT. AFT CARGO COMPARTMENT, LT FLOOR SUPPORT INTERCOSTAL BS 727A-727B IS BENT. ACFT GROUNDED. R & R FLOOR SUPPORT INTERCOSTAL AT BS 727A-727B IAW SRM 51-10-02, PARA 
- [SDR ASAA2015072912676](https://openairdocs.org/sdr/ASAA2015072912676), Jul 29, 2015: STIFFENER. CRACKED. LEFT HORIZONTAL STABILIZER AT STABILIZER 129.5 RIB, STIFFENER CRACKED. ACFT GROUNDED. R & R STIFFENER IAW SRM 51-10-02, PARA 8 AND 51-40-02, AND DWG 65-47508, R
- [SDR ASAA2015072912675](https://openairdocs.org/sdr/ASAA2015072912675), Jul 29, 2015: STIFFENER. CRACKED. LEFT HORIZONTAL STABILIZER AT STAB STA 129.5 RIB, STIFFENER, PN 65-47508-50 IS CRACKED. ACFT GROUNDED. R & R STIFFENER IAW SRM 51-10-02, PARA 8 AND 51-40-02, AN
- [SDR ASAA2015072812940](https://openairdocs.org/sdr/ASAA2015072812940), Jul 28, 2015: FRAME. DAMAGED. FUSELAGE FRAME BS 727D HAS AN ENLONGATED HOLE AT LT LOWER Z ANGLE ATTACHMENT. ACFT GROUNDED. REPAIRED IAW EA 400-53EA-15683, REV NEW.
- [SDR ASAA2015072812939](https://openairdocs.org/sdr/ASAA2015072812939), Jul 28, 2015: FRAME. DAMAGED. FUSELAGE FRAME 727F HAS AN ENLONGATED HOLE AT LT LOWER Z-ANGLE ATTACHMENT. ACFT GROUNDED. REPAIRED FRAME IAW EA 400-53EA-15684, REV NEW, STA 727F.
- [SDR ASAA2015072312757](https://openairdocs.org/sdr/ASAA2015072312757), Jul 23, 2015: WEB. CORRODED. AFT CARGO DOOR SILL WEB IS CORRODED. ACFT GROUNDED. REMOVED CORRODED ORIG .045", REMAIN .040" LOSS OF .005", FOUND OUT OF LIMITS IAW SRM 53-60-16, NEW WEB IAW D
- [SDR ASAA2015072212933](https://openairdocs.org/sdr/ASAA2015072212933), Jul 22, 2015: FLOOR SUPPORT. CORRODED. AFT CARGO BAY LT FLOOR SUPPORT ANGLE IS CORRODED APPROXIMATELY BS 727+4 TO BS 760. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53
- [SDR ASAA2015072212920](https://openairdocs.org/sdr/ASAA2015072212920), Jul 22, 2015: STRIP. CORRODED. AFT CARGO COMPARTMENT, RT CAP STRIP NR 4, AFT OF DOORWAY IS CORRODED. ACFT GROUNDED. REMOVED CORROSION, MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS -.063. R
- [SDR ASAA2015072212756](https://openairdocs.org/sdr/ASAA2015072212756), Jul 22, 2015: STRIP. CORRODED. AFT CARGO COMPARTMENT, RT CAPSTRIP NR 3, FWD OF DOORWAY IS CORRODED. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL USING TOOL T82254 CAL DATE 11/
- [SDR ASAA2015072112937](https://openairdocs.org/sdr/ASAA2015072112937), Jul 21, 2015: FRAME. CRACKED. CRACK INDICATIONS FOUND BS 520 ABOVE S-21L IN .500" HOLE, MARKED AT 7 & 9 O'CLOCK POSITION IN FWD PIT. ACFT GROUNDED. REPAIRED FRAME IAW EA 400-53EA-15603.
- [SDR ASAA2015072112936](https://openairdocs.org/sdr/ASAA2015072112936), Jul 21, 2015: FRAME. CRACKED. RIGHT BS 500B, .500" WIRE PENETRATION HOLE, ABOVE S-21R HAS CRACK INDICATION DUE TO NOISE. IN FWD PIT, MARKED. ACFT GROUNDED. CLEANED HOLE RT BS 500B, 500" WIRE
- [SDR ASAA2015072112934](https://openairdocs.org/sdr/ASAA2015072112934), Jul 21, 2015: STRIP. CORRODED. PARTS RACK, AFT CARGO FLOOR/SIDEWALL CAPSTRIP IS CORRODED. LT NR 2. ACFT GROUNDED. REMOVED CORROSION, MEASURED THICKNESS OF METAL. ORIGINAL THICKNESS .063, REMO
- [SDR ASAA2015072112933](https://openairdocs.org/sdr/ASAA2015072112933), Jul 21, 2015: STRIP. CORRODED. PARTS RACK, AFT CARGO FLOOR/SIDEWALL CAPSTRIP IS CORRODED, RT NR 3. ACFT GROUNDED. REMOVED CORROSION FROM PANEL, ORIGINAL THICKNESS .063. REMAINING THICKNESS .0
- [SDR ASAA2015072112694](https://openairdocs.org/sdr/ASAA2015072112694), Jul 21, 2015: SUPPORT. CORRODED. AFT CARGO SIDEWALL CAPSTRIP IS CORROSION LT NR 1. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL. ORIGINAL THICKNESS .063, REMOVED .022, REMAINING
- [SDR ASAA2015072112691](https://openairdocs.org/sdr/ASAA2015072112691), Jul 21, 2015: SUPPORT. CORRODED. AFT CARGO SIDEWALL CAPSTRIP SPLICE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS .063, REMOVED .031, REMAINING T
- [SDR ASAA2015072112690](https://openairdocs.org/sdr/ASAA2015072112690), Jul 21, 2015: SUPPORT. CORRODED. AFT CARGO SIDEWALL CAPSTRIP SPLICE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS 0.63, REMOVED .012, REMAINING T
- [SDR ASAA2015072112689](https://openairdocs.org/sdr/ASAA2015072112689), Jul 21, 2015: SUPPORT. CORRODED. AFT CARGO SIDEWALL CAPSTRIP IS CORRODED RT NR 1. ACFT GROUNDED. REMOVED CORROSION MEASURED THICKNESS OF METAL, ORIGINAL THICKESS .063, REMOVED .013, REMAINING T
- [SDR ASAA2015072112688](https://openairdocs.org/sdr/ASAA2015072112688), Jul 21, 2015: SUPPORT. CORRODED. AFT CARGO SIDEWALL CAPSTRIP IS CORRODED LT NR 4. ACFT GROUNDED. REMOVED CORROSION, MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS .063 REMOVED .018. REMAINING 
- [SDR ASAA2015072112674](https://openairdocs.org/sdr/ASAA2015072112674), Jul 21, 2015: SUPPORT. CORRODED. AFT CARGO SIDEWALL CAPSTRIP SPLICE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION. MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS .063. REMOVED .037, REMAINING 
- [SDR ASAA2015072112673](https://openairdocs.org/sdr/ASAA2015072112673), Jul 21, 2015: SUPPORT. CORRODED. AFT CARGO SIDEWALL CAPSTRIP SPLICE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION. MEASURED THICKNESS OF METAL. ORIGINAL THICKNESS .063, REMOVED .011. REMAINING 
- [SDR ASAA2015072112672](https://openairdocs.org/sdr/ASAA2015072112672), Jul 21, 2015: SUPPORT. CORRODED. AFT CARGO SIDEWALL CAPSTRIP IS CORRODED. ACFT GROUNDED. REMOVED CORROISON. MEASURED THICKNESS OF METAL. ORIGINAL THICKNESS .063, REMOVED .031. REMAINING THICKNE
- [SDR ASAA2015072112671](https://openairdocs.org/sdr/ASAA2015072112671), Jul 21, 2015: SUPPORT. CORRODED. AFT CARGO SIDEWALL CAPSTRIP IS CORRODED. ACFT GROUNDED. REMOVED CORROISON. MEASURED THICKNESS OF METAL, ORIGINAL THICKNESS .063, REMOVED .024. REMAINING THICKNE
- [SDR ASAA2015072012938](https://openairdocs.org/sdr/ASAA2015072012938), Jul 20, 2015: DOOR FRAME. GOUGED. AFT CARGO DOOR, FWD DOOR FRAME, 2ND FROM UPPER DOOR STOP PIN FITTING GOUGED. APPROXIMATELY S-21R MARKED IN RED. DOT ATTACHED. ACT GROUNDED. R & R AFT CARGO DOOR
- [SDR ASAA2015072012913](https://openairdocs.org/sdr/ASAA2015072012913), Jul 20, 2015: STOP FITTING. GOUGED. FORWARD CARGO DOOR, FWD DOOR FRAME, UPPER DOOR STOP PIN FITTING GOUGED DEEP. APPROXIMATELY S-20R, MARKED IN RED, DOT ATTACHED. ACFT GROUNDED. R & R CARGO DOOR F
- [SDR ASAA2015071812938](https://openairdocs.org/sdr/ASAA2015071812938), Jul 18, 2015: FRAME. CRACKED. BS 500F RT FRAME IN FWD PIT, .500" HOLE HAS CRACK INDICATION NOTED IN FRAME AT 6 O'CLOCK POSITION, REF OPS 7318, FIG 11, CIRCLE NOTE 1, STR 20L-STR 21L. ACFT GR
- [SDR ASAA2015071812919](https://openairdocs.org/sdr/ASAA2015071812919), Jul 18, 2015: FRAME. CRACKED. BS 500B, LT FRAME IN FWD PIT, .500" HOLE HAS CRACK INDICATION NOTED IN FRAME AT 1 O'CLOCK POSITION, REF OPS 7318, FIG 11, CIRCLE NOTE 1, STR 20L-STR 21L. ACFT G
- [SDR ASAA2015071812918](https://openairdocs.org/sdr/ASAA2015071812918), Jul 18, 2015: FRAME. CRACKED. BS 500G, LT FRAME IN FWD CARGO BAY, A .500 INCH HOLE HAS CRACK INDICATION NOTED IN FRAME AT 10 O'CLOCK POSITION. REF OPS 7318, FIG 11, CIRCLE NOTE 1, STR 20L-ST
- [SDR ASAA2015071812871](https://openairdocs.org/sdr/ASAA2015071812871), Jul 18, 2015: ATTACH BRACKET. GOUGED. FWD CARGO DOORWAY FWD FRAME INTERNAL ATTACH BRACKET GOUGED, STREAMER ATTACHED, STR 24R. ACFT GROUNDED. R & R FWD CARGO DOORWAY, FW FRAME BACKUP FITTING IAW SRM 
- [SDR ASAA2015071812868](https://openairdocs.org/sdr/ASAA2015071812868), Jul 18, 2015: FRAME. CRACKED. BS 500F STRINGERS 20 - 21L FRAME IN FWD CARGO BAY, A .500 HOLE HAS CRACK INDICATION NOTED IN FRAME AT 5 O'CLOCK POSITION. ACFT GROUNDED. REPAIRED THE FRAME IAW 
- [SDR ASAA2015071812843](https://openairdocs.org/sdr/ASAA2015071812843), Jul 18, 2015: FRAME. CRACKED. BS 500D LT FRAME IN FWD PIT, .500" HOLE HAS CRACK INDICATION NOTED IN FRAME AT 1 O'CLOCK POSITION, REF OPS 7318, FIG 11, CIRCLE NOTE 1, STR 20L-STR 21L. ACFT GR
- [SDR ASAA2015071812833](https://openairdocs.org/sdr/ASAA2015071812833), Jul 18, 2015: SKIN. CRACKED. CRACK INDICATION ON LT HORIZONTAL STABILIZER LOWER SKIN, APPROXIMATELY STABILIZER BS 123, APPROXIMATELY 1" IN LENGTH, MARKED IN RED. ACFT GROUNDED. REPAIRED LT 
- [SDR ASAA2015071712915](https://openairdocs.org/sdr/ASAA2015071712915), Jul 17, 2015: HINGE. CRACKED. FORWARD SERVICE DOOR, LOWER HINGE HAS ONE FASTENER HOLE WITH A CRACK INDICATION. UNABLE TO DETERMINE LAYER. INDICATION POSITIONED AT 11 O'CLOCK IN HOLE, MARKED.
- [SDR ASAA2015071712869](https://openairdocs.org/sdr/ASAA2015071712869), Jul 17, 2015: FITTING. CRACKED. CRACK INDICATION ON LT UPPER, OTBD HORIZONTAL STABILIZER THRUST BEAM CORNER FITTING, APPROX 2" IN LENGTH. ACFT GROUNDED. ACCOMPLISHED REPLACEMENT OF LT SIDE HOR

All 151: https://openairdocs.org/deregistered/N708AS-2018-10-09/reports.md

## FAA accident and incident reports (2)

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 20060201002279I](https://openairdocs.org/incident/20060201002279I), Feb 1, 2006: Boeing 737490 (N708AS), Yakutat, AK, Minor damage. (-23) Upon landing, flight 66 veered to the right and the right main gear hit runway edge lights. The PIC stated that the #1 engine had failed upon landing,…
- [Incident 19990502017529I](https://openairdocs.org/incident/19990502017529I), May 2, 1999: Boeing 737490 (N708AS), Palm Springs, CA. Alaska airlines flight 592, a B-737-490, N708AS, was dispatched from koak to kpsp on may 2, 1999. Due to delays out of koak, the aircraft was not expected to…

## Other aircraft with N708AS

- [Registered now](https://openairdocs.org/aircraft/N708AS): Ea Vision EA J100, S/N EAVUAV502585781

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