# N762AS: 1992 Boeing 737-4Q8, registration cancelled 2019-08-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 28, 2019 - Exported to: Malaysia - Status when cancelled: Valid registration - Airframe: [Boeing 737-4Q8](https://openairdocs.org/model/boeing-737-4q8) (registry code 138447Q) - Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802) - Serial number: 25099 - Year built: 1992 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 25, 2002 - Certificate issued: June 22, 2017 - Last registry action: May 8, 2018 - Mode S code: AA4907 - Owner when cancelled: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%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/N762AS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=762AS - Page: https://openairdocs.org/deregistered/N762AS-2019-08-28 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 737-4Q8: https://openairdocs.org/model/boeing-737-4q8.md ## Service difficulty reports (326, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASAA2017051220744](https://openairdocs.org/sdr/ASAA2017051220744), May 12, 2017: GUIDE ARM. LACK OF LUBE. FLIGHT ATT. REPORTS R2 DOOR HARD TO OPEN AND GUST LOCK WONT ENGAGE. GROUNDED - YES. VERIFIED GVI OF RII DOOR. LUBED GUST LOCK & GUIDE ARMS OPS NORMAL. - [SDR ASAA2016051816795](https://openairdocs.org/sdr/ASAA2016051816795), May 18, 2016: LENS. DETACHED. AFT ACFT RT OVERWING EXIT LIGHT SIGN FELL OFF. ACFT GROUNDED. REPLACED AFT ACFT RT OVERWING EXIT LIGHT ASSY IAW AMM 33-51-11, OPS CHECK GOOD. - [SDR ASAA2016022415691](https://openairdocs.org/sdr/ASAA2016022415691), Feb 24, 2016: INTERCOSTAL. CRACKED. INTERCOSTAL AT BS 277 AND STR 14R CRACKED IN RADIUS. ACFT GROUNDED. R & R DAMAGED INTERCOSTAL IAW SRM 51-40-02-0G-0. - [SDR ASAA2016022215857](https://openairdocs.org/sdr/ASAA2016022215857), Feb 22, 2016: SKIN. CRACKED. ACFT SKIN APPEARS TO BE CRACKED FWD AND AFT OF NR 2 VHF COMM ANTENNA. ACFT GROUNDED. REPAIRED SKIN FWD, AND AFT OF NR 2 VHF ANTENNA BS 5000 TO 500A IAW EA 400-5 - [SDR ASAA2016022115853](https://openairdocs.org/sdr/ASAA2016022115853), Feb 21, 2016: SUPPORT FITTING. CRACKED. R/W REAR SPAR MLG BEAM AFT SUPPORT FITTING CRACK IN RADIUS 2ND FASN OTBD. ACFT GROUNDED. ACCOMPLISHED INSPECTIONS TO RT MLG BEAM AFT SUPPORT FITTING IAW EA 400- - [SDR ASAA2016022115852](https://openairdocs.org/sdr/ASAA2016022115852), Feb 21, 2016: SUPPORT FITTING. CRACKED. LT WING REAR SPAR MLG SUPPORT BEAM AFT SUPPORT FITTING CRACKED IN RADIUS 4 FAST OTBD. ACFT GROUNDED. ACCOMPLISHED INSPECTIONS TO LT MLG BEAM AFT SUPPORT FITTING - [SDR ASAA2016021915887](https://openairdocs.org/sdr/ASAA2016021915887), Feb 19, 2016: FRAME. GOUGED. TAILCOMP TOP SIDE OF FRAME 1061 GOUGED ON AFT RADIUS AT LBL 18, ABOVE LIGHT SWITCH. ACFT GROUNDED. REPAIRED TOP SIDE OF FRAME 1064 IAW EA 400 53EA 16732 REPAIR - [SDR ASAA2016021715851](https://openairdocs.org/sdr/ASAA2016021715851), Feb 17, 2016: SKIN. DENTED. LT AFT FUSELAGE PANEL OTBD OF TAILSKID FAIRING HAS SEVERAL PROTRUSIONS AND DENTS. ACFT GROUNDED. REPAIRED LT AFT FUSELAGE SKIN IAW EA 400-53EA-16728. THIS REPAI - [SDR ASAA2015100413334](https://openairdocs.org/sdr/ASAA2015100413334), Oct 4, 2015: SKIN. CRACKED. CRACK IN FUSELAGE, RT SIDE .8750 LONG, 1.5 FWD 727E, TOP SIDE OF S-24R TRANSFERRED FROM N/R 00001 DEFECT NR 11426711. ACFT GROUNDED. REPAIRED SKIN CRACK DAMAGE - [SDR ASAA2015060312033](https://openairdocs.org/sdr/ASAA2015060312033), Jun 3, 2015: LOCK. BROKEN. FLOOR PALLET LOCK BROKEN , NR 1 POSITION FAR RT INBD SIDE, FWD. ACFT GROUNDED. REMOVED DAMAGED TRACK MATERIAL IN POSITION NR 1, REF SRM 53-00-52, REPAIR OPTION - [SDR ASAA2015022310790](https://openairdocs.org/sdr/ASAA2015022310790), Feb 23, 2015: SKIN. DAMAGED. LIGHTING STRIKE DAMAGE AT FRONT LT SIDE OF ACFT FS 291, STRINGER 21L REF LP 11338892. ACFT GROUNDED. REPAIRED LIGHTNING STRIKE DAMAGE AT LT SIDE FS 291, STR 21L - [SDR ASAA2015022310774](https://openairdocs.org/sdr/ASAA2015022310774), Feb 23, 2015: SKIN. DAMAGED. LIGHTING STRIKE DAMAGE AT FRONT LT SIDE OF ACFT FS 291, STRINGER 21L, REF LP 11338892. ACFT GROUNDED. REPAIRED LIGHTNING STRIKE DAMAGE AT LT SIDE FS 291, STR 21 - [SDR ASAA2014102909534](https://openairdocs.org/sdr/ASAA2014102909534), Oct 29, 2014: LAMP. INOPERATIVE. L2 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMP, OPS NORMAL. - [SDR ASAA2014020806805](https://openairdocs.org/sdr/ASAA2014020806805), Feb 8, 2014: DOOR. OUT OF RIG. F/A REPORTS L2 DOOR DIFFICULT TO CLOSE. ACFT GROUNDED. FOUND L-2 DOOR OUT OF RIG. ACCOMPLISHED RIG ON L-2 DOOR HORIZONTAL ROD, GUIDE ARM & STOP PINS IAW AMM 52- - [SDR ASAA2014010812355](https://openairdocs.org/sdr/ASAA2014010812355), Jan 8, 2014: SKIN. CRACKED. CRACK FOUND ON FUSELAGE SKIN STA 941 TO 944.2, BETWEEN STR 24R AND 25R. ACFT GROUNDED. REPAIRED SKIN IAW SRM 53-00-01-2R-31, CAT B REPAIR INSPECTION THRESHOLD 6 - [SDR ASAA2014010712464](https://openairdocs.org/sdr/ASAA2014010712464), Jan 7, 2014: SKIN. CRACKED. FOUND A CRACK AT BS 941 TO 944, 2.75 INCHES LONG BETWEEN STRINGERS 24 & 25R. ACFT GROUNDED. REPAIRED SKIN IAW SRM 53-00-01-2R-31, CAT B REPAIR. - [SDR ASAA2014010212316](https://openairdocs.org/sdr/ASAA2014010212316), Jan 2, 2014: COVER. LOOSE. AFT EXIT LIGHT COVER LOOSE. ACFT GROUNDED. REPLACED AFT L2 DOOR EXIT LIGHT ASSY. OPTS CHECKED GOOD IAW AMM 33-51-11. - [SDR ASAA2013100396150](https://openairdocs.org/sdr/ASAA2013100396150), Oct 3, 2013: ANGLE. CRACKED. AFTER REMOVAL OF FWD PIT VHF DOUBLER FOUND DOUBLER SUPPORT ANGLE CRACKED. FABRICATED NEW ANGLE, TREAT, PRIMED AND TOPCOATED IAW SWRM 51-20-01-0G-0. AND INSTALLE - [SDR ASAA2013100296148](https://openairdocs.org/sdr/ASAA2013100296148), Oct 2, 2013: DOUBLER. CRACKED. FWD CARGO VHF ANTENNA DOUBLER FOUND CRACKED AFTER CLEANING FOR PEELING PAINT NR MIG5 SN 5413337. R & R CRACKED ANTENNA DOUBLER IAW SRM 51-40-02-0G-0. - [SDR ASAA2013091896082](https://openairdocs.org/sdr/ASAA2013091896082), Sep 18, 2013: ATTACH BRACKET. CRACKED. ATTACH BRACKET CRACKED BS 291 AND RBL 60, BELOW STR 18 FOUND AFT REMOVING SHEAR WEB. ACFT GROUNDED. FABRICATED NEW ATTACH BRACKET ALODINED PRIMED AND TOPCOATED - [SDR ASAA2013091796121](https://openairdocs.org/sdr/ASAA2013091796121), Sep 17, 2013: SKIN. CRACKED. RT HORIZONTAL LOWER SKIN IS CRACKED AT APPROX STAB STA 113 JUST FWD OF REAR SPAR. ACFT GROUNDED. REPAIRED SKIN IAW SRM 55-10-01-2R-13 - [SDR ASAA2013091596215](https://openairdocs.org/sdr/ASAA2013091596215), Sep 15, 2013: SHEAR WEB. CRACKED. AFTER REMOVAL OF UPPER TEE ANGLE OF FRAME AT BS 328, FOUND SHEAR WEB GOUGED AND CRACKED RBL 60 ON LOWER SURFACE. ACFT GROUNDED. REMOVED SHEAR WEB FABRICATED NEW - [SDR ASAA2013090507269](https://openairdocs.org/sdr/ASAA2013090507269), Sep 5, 2013: WEB. CORRODED. AFTER REMOVAL OF LT AFT MOP SEAL LOWER SURFACE OF WEB IS CORRODED, STA 967-986 AT STR 18 LT. ACFT GROUNDED. REMOVED CORRODED ON LT AFT MOP SEAL WEB AND FOUND TO - [SDR ASAA2013090496007](https://openairdocs.org/sdr/ASAA2013090496007), Sep 4, 2013: FRAME. CRACKED. RT FUSELAGE FRAME, BS 480 CRACKED ABOVE SHEAR WEB. R & R FRAME ASSY IAW SRM 51-40-05 AND 51-40-02. - [SDR ASAA2013090195962](https://openairdocs.org/sdr/ASAA2013090195962), Sep 1, 2013: FLOOR SUPPORT. CRACKED. FLOOR SUPPORT CRACKED AT FS 344 AND LBL 47, ACFT GROUNDED. R & R FLOOR SUPPORT IAW SRM 51-40 02. - [SDR ASAA2013083096090](https://openairdocs.org/sdr/ASAA2013083096090), Aug 30, 2013: STRINGER CLIP. CRACKED. STRINGER CLIP 6R ON AFT SIDE OF FRAME AT BS 500 HAS EVIDENCE OF A CRACK AT FASTENER HOLE. R & R STRINGER CLIP IAW SRM 51-40-02. - [SDR ASAA2013082595963](https://openairdocs.org/sdr/ASAA2013082595963), Aug 25, 2013: ANGLE. CRACKED. FORWARD GALLEY SERVICE DOOR BS 194.5 S9R EVIDENCE OF A CRACK FIN RADIUS OF FRAME SUPPORT. ACFT GROUNDED. R & R FRAME SUPPORT IAW SRM 51-40-05-0G-0. - [SDR ASAA2013082396097](https://openairdocs.org/sdr/ASAA2013082396097), Aug 23, 2013: DOOR FRAME. CRACKED. DOOR FRAME IS CRACKED APPROX 1.25 AT LOWER DOORSTOP FITTING MOUNTING AREA EXTENDING FROM LOWER OTBD CORNER INWARD. REMOVED OLD FRAME, DRILLED AND INSTALLED NEW - [SDR ASAA2013082395925](https://openairdocs.org/sdr/ASAA2013082395925), Aug 23, 2013: SKIN. DELAMINATED. LEFT INBD AFT FLAP OTBD UPPER AND LOWER SURFACES DELAMINATED. REPAIRED LT INBD AFT FLAP OTBD UPPER AND LWR SURFACES IAW SRM 51-70-10-2R-4, REPAIR 4. PERMANENT R - [SDR ASAA2013071295554](https://openairdocs.org/sdr/ASAA2013071295554), Jul 12, 2013: BEAR STRAP. CRACKED. SUSPECT CRACK FWD OF L2 DOOR SILL APPROX BS 957. ACFT GROUNDED. REPAIRED FUSELAGE SKIN AND BEAR STRAP IAW SRM 53-00-01-2R-32 REPAIR 32. - [SDR ASAA2012092492795](https://openairdocs.org/sdr/ASAA2012092492795), Sep 2, 2012: FRAME. CRACKED. FRAME BS 500C HAS A CRACK .25 LONG EXTENDING I/B FROM EDGE OF THE 1.04 WIRE PENETRATION HOLE. FRAME REPAIRED IAW SRM 53-00-07. - [SDR ASAA2012091392871](https://openairdocs.org/sdr/ASAA2012091392871), Sep 1, 2012: FRAME. CRACKED. FRAME 520, RT SIDE HAS 2 CRACKS, 1 INBD BRACKET HOLE BETWEEN STR 8R AND 9R, AND 1 OTBD BRACKET HOLE ABOVE STR 8. ACFT GROUNDED. REPAIRED FRAME 520 RT IAW ASA EA - [SDR ASAA2012082593078](https://openairdocs.org/sdr/ASAA2012082593078), Aug 25, 2012: SKIN. CHAFED. LT WING L/E NR 3 SLAT LOWER INBD T/E CHAFED THRU REPAIR DOUBLER. ACFT GROUNDED. REPAIRED NR 3 SLAT LWR INBD CORNER DAMAGE IAW SRM 51 70 10 PAR 20, PG 254, REP 4 - [SDR ASAA2012082592876](https://openairdocs.org/sdr/ASAA2012082592876), Aug 2, 2012: FLOOR SUPPORT. CRACKED. LONGITUDINAL FLOOR SUPPORT RBL 24.5 UPPER CHORD CRACKED AT FS 664. REPAIRED LONGITUDINAL BEAM AT FS 664, RBL 24.5 IAW EA NR AD20080506-400-57-1-101. - [SDR ASAA2012082492794](https://openairdocs.org/sdr/ASAA2012082492794), Aug 2, 2012: FRAME. CRACKED. FRAME AT BS 500B RT SIDE HAS A CRACK .375 LONG EXTENDING INBD FROM EDGE OF THE 1.04 WIRE PENETRATION HOLE. ACFT GROUNDED. FRAME REPAIRED IAW SRM 53 00 07, REPAI - [SDR ASAA2012082592790](https://openairdocs.org/sdr/ASAA2012082592790), Aug 2, 2012: SKIN. CHAFED. LT WING L/E NR 3 SLAT LOWER INBD T/E CHAFED. REPAIRED IAW SRM 51-70-10, PARA 20, PG 254, REP 4, PG 201. - [SDR ASAA2012082492786](https://openairdocs.org/sdr/ASAA2012082492786), Aug 2, 2012: SKIN. CRACKED. LT FUSELAGE SKIN BS 727D HAS A CRACK .75 LONG BELOW STR 23L IN CHEM MILLED AREA. ACFT GROUNDED. REPAIRED SKIN IAW SRM 53-00-01, FIG 201. - [SDR ASAA12410952](https://openairdocs.org/sdr/ASAA12410952), Jan 13, 2012: GUIDE ARM. WORN. L2 DOOR IS DIFFICULT TO OPEN. FOUND AFT ENTRY DOOR SNUBBER INOP. REPLACED SNUBBER REF AMM 52 13 71. FOUND GUIDE ARM AND DOWL PIN WORN. REPLACED GUIDE ARM REF AM - [SDR ASAA11410722](https://openairdocs.org/sdr/ASAA11410722), Nov 28, 2011: DOOR. LACK OF LUBE. AFT ENTRY DOOR (L2) REPORTED "SQUEAKY" AND DIFFICULT TO OPERATE BY FLIGHT ATTENDANT CREW. INSPECTED AND LUBRICATED AFT ENTRY (L2) DOOR. OPS CHECK NORMAL. OK FOR - [SDR ASAA11410653](https://openairdocs.org/sdr/ASAA11410653), Nov 11, 2011: SIGN. CRACKED. L1 DOOR LOWER EMERGENCY EXIT SIGN CRACKED AND WILL NOT STAY IN PLACE. REPLACED L1 DOOR EMERGENCY EXIT SIGN. - [SDR ASAA11410641](https://openairdocs.org/sdr/ASAA11410641), Nov 6, 2011: SKIN. DENTED. DURING PREFLT W/A DAMAGED NOTED ON UNDERSIDE OF RT HORIZ STAB ABOUT 8" FROM ROOT. 2" AFT OF LEADING EDGE. DAMAGED AREA EST TO BE APPROX 6" LONG 3" WIDE & 1/2 TO - [SDR ASAA11410348](https://openairdocs.org/sdr/ASAA11410348), Sep 7, 2011: SKIN. CRACKED. CRACK FOUND DURING MFEC RT STA 727D BELOW STR 23R. CUT OUT DAMAGED SECTION. REPAIRED CRACKED SKIN IAW B737 400 SRM 53 00 01 FIG 201 REPAIR 31. - [SDR ASAA11410385](https://openairdocs.org/sdr/ASAA11410385), Sep 3, 2011: SKIN. CRACKED. R2 DOOR CUTOUT LOWER FWD CORNER EXTERNAL SKIN CRACKED. REPAIRED R2 DOOR CUTOUT LOWER EXTERNAL SKIN & BEAR STRAP IAW B737 400 SRM 53 00 01 FIG 201 REPAIR 32 DETA - [SDR ASAA11410400](https://openairdocs.org/sdr/ASAA11410400), Sep 2, 2011: FRAME. CRACKED. BS 500G RT WIRE PENETRATION HOLE FOUND CRACKED AT INBD 9 O'CLOCK POSITION BETWEEN S 20R AND S 21 R GROUNDED YES. TRIMMED OUT DAMAGE FABRICATED REPAIR DOUBLERS A - [SDR ASAA11410214](https://openairdocs.org/sdr/ASAA11410214), Aug 8, 2011: GLOWSTRIP. LOOSE. PHOTOLUMINESCENT TRACK LIGHT AT ROW 19C LOOSE. REPLACED APPROX 5 FT OF PHOTOLUMINESCENT FLOOR TRACK LIGHT FROM 17C, 19C. - [SDR ASAA1149963](https://openairdocs.org/sdr/ASAA1149963), Jun 25, 2011: DOUBLER. CRACKED. LT WING I/B FOREFLAP HAS CRACKED REPAIR DOULBER ON UPPER SURFACE JUST O/B OF MIDSPAN. REPAIRED DAMAGE TO UPPER SURFACE AND CORE OF LT WING I/B FOREFLAP IAW B737 - [SDR ASAA1149572](https://openairdocs.org/sdr/ASAA1149572), May 3, 2011: BATTERY. DISCHARGED. RT INTERIOR OVERWING EXIT EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY IN CHARGER M1468 CHECKS GOOD REF MM 33 51 02. - [SDR ASAA1048515](https://openairdocs.org/sdr/ASAA1048515), Nov 17, 2010: DOOR. DIRTY. F/A REPORTS L2 DOOR HARD TO OPEN AND MAKES LOUD SQEAKING SOUND WHEN OPENING. CLEANED AND LUBRICATED DOOR, OPS CHECK GOOD. - [SDR ASAA1048064](https://openairdocs.org/sdr/ASAA1048064), Jul 14, 2010: SLAT. DELAMINATED. NR 1 SLAT L/E DELAMINATED I/B AFT CORNER. REMOVED DAMAGE, INSTALLED AND BONDED REPAIR DOUBLER. - [SDR ASAA1048096](https://openairdocs.org/sdr/ASAA1048096), Jul 9, 2010: SKIN. DENTED. DENT AFT OF L2 DOOR BETWEEN STR 12L AND 13L IS WITHIN 3 INCHES OF SKIN BUTT SPLICE. REMOVED DAMAGED AREA, INSTALLED REPAIR. All 326: https://openairdocs.org/deregistered/N762AS-2019-08-28/reports.md ## Other aircraft with N762AS - [Registered now](https://openairdocs.org/aircraft/N762AS): Ea Vision EA J100, S/N EAVUAV502585790 --- 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.