# N586US: 1988 Boeing 737-301, registration cancelled 2007-08-13 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 13, 2007 - Exported to: Indonesia - Status when cancelled: Valid registration - Airframe: [Boeing 737-301](https://openairdocs.org/model/boeing-737-301) (registry code 138447R) - 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: 23931 - Year built: 1988 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 18, 1988 - Certificate issued: January 31, 2007 - Last registry action: January 31, 2007 - Mode S code: A78E05 - Owner when cancelled: [Cjet Inc](https://openairdocs.org/faa-owner/CJET%20INC) - Location: [Houston, TX](https://openairdocs.org/faa-place/TX/Houston) - Owner type: Corporation - Owner's area on the map: 29.7441° N, 95.4892° W: Placed by OpenAirDocs at the center of ZIP code 77057, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N586US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=586US - Page: https://openairdocs.org/deregistered/N586US-2007-08-13 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 737-301: https://openairdocs.org/model/boeing-737-301.md ## Service difficulty reports (98, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 2007FA0000135](https://openairdocs.org/sdr/2007FA0000135), Sep 27, 2006: FRAME. CRACKED. FRAME IS CRACKED AT BODY STATION 727, STRINGER 14L. (K) - [SDR 2007FA0000128](https://openairdocs.org/sdr/2007FA0000128), Sep 27, 2006: SKIN. DENTED. BODY STATION 915 ABOVE STRINGER 25L LAP JOINT FUSELAGE SKIN HAS DENT. (K) - [SDR 2007FA0000126](https://openairdocs.org/sdr/2007FA0000126), Sep 27, 2006: FRAME. CRACKED. FRAME IS CRACKED AT BODY STAION 727, STRINGER 14L. (K) - [SDR 2007FA0000125](https://openairdocs.org/sdr/2007FA0000125), Sep 26, 2006: FRAME. CRACKED. UPPER FUSELAGE, BS 500A, BETWEEN STR 8R AND STR 9R, FRAME IS CRACKED AT PSU MOUNT. (K) - [SDR 2007FA0000124](https://openairdocs.org/sdr/2007FA0000124), Sep 26, 2006: SKIN. GOUGED. UPPER FUSELAGE, STA 860 THRU 885, LBL 8 THRU RBL 8, UNDER DORSAL FIN BLADE SEAL, SKIN IS GOUGED. (K) - [SDR 2007FA0000136](https://openairdocs.org/sdr/2007FA0000136), Sep 24, 2006: FITTING. CORRODED. DOOR 1R, BS 306-312, WL 248-249, LBL 57-63, SERPENTINE PLATE CASTING CORRODED AROUND FASTENER HOLES. (K) - [SDR 2007FA0000134](https://openairdocs.org/sdr/2007FA0000134), Sep 24, 2006: PRESSURE PANEL. CRACKED. MID CABIN BS 663, LBL 31, WHEEL WELL PRESSURE DECK WEB, CRACKED. (K) - [SDR 2007FA0000133](https://openairdocs.org/sdr/2007FA0000133), Sep 24, 2006: FRAME. CRACKED. CABIN, BS 787, FRAME AT STR 8R, CRACKED AT STOW BIN ATTACH BRACKET. (K) - [SDR 2007FA0000129](https://openairdocs.org/sdr/2007FA0000129), Sep 24, 2006: FLOORBEAM. GOUGED. CABIN FLOORBEAM, STA 827, WL 203.6, RBL 10, LOWER T-CAP, AFT FLANGE, GOUGED. (K) - [SDR 2007FA0000140](https://openairdocs.org/sdr/2007FA0000140), Sep 18, 2006: SUPPORT. CRACKED. AT FWD CABIN STA 328+6, DOOR 2R AFT STOP FTG INTERCOSTAL TEE SUPPORT, CRACKED. (K) - [SDR 2007FA0000139](https://openairdocs.org/sdr/2007FA0000139), Sep 18, 2006: FRAME. CRACKED. MID CABIN, STATION 500A FRAME, BETWEEN STRINGER 8 AND 9L, CRACKED AT PSU MOUNT RAIL ATTACH POINT. (K) - [SDR 2007FA0000138](https://openairdocs.org/sdr/2007FA0000138), Sep 18, 2006: FRAME. CRACKED. MID CABIN, STATION 480 FRAME, AT STRINGER 8L, CRACKED AT PSU MOUNT RAIL ATTACH POINT. (K) - [SDR 2007FA0000137](https://openairdocs.org/sdr/2007FA0000137), Sep 18, 2006: STRINGER CLIP. CRACKED. PASSENGER CABIN, STATION 639 AT STRINGER 4L, STRINGER CLIP, CRACKED. (K) - [SDR 2007FA0000131](https://openairdocs.org/sdr/2007FA0000131), Sep 18, 2006: CREASE BEAM. CORRODED. AFT GALLEY DOOR CREASE BEAM INNER CHORD ANGLE, BS 947 TO 992, STRINGER 17R, WL 208, CORROSION OUT OF LIMITS. (K) - [SDR 2007FA0000130](https://openairdocs.org/sdr/2007FA0000130), Sep 18, 2006: FRAME. CRACKED. MID CABIN, STATION 400 FRAME AT STRINGER 8R, CRACKED AT PSU RAIL OUNT ATTACH POINT. (K) - [SDR 2007FA0000127](https://openairdocs.org/sdr/2007FA0000127), Sep 18, 2006: FRAME. CRACKED. MID CABIN, STA 500A FRAME, BETWEEN STRINGER 8 AND 9L, CRACKED AT PSU MOUNT RAIL ATTACH POINT. (K) - [SDR 2007FA0000123](https://openairdocs.org/sdr/2007FA0000123), Sep 18, 2006: INTERCOSTAL. CRACKED. CABIN STA 303.9 JUST ABOVE STRINGER 10L. INTERCOSTAL OUTER CHORD ANGLE, CRACKED. (K) - [SDR 2007FA0000132](https://openairdocs.org/sdr/2007FA0000132), Aug 17, 2006: FLOORBEAM. CORRODED. CABIN BS 312, FROM LBL 55 TO RBL 55 WL 208, FLOORBEAM HAS LIGHT CORROSION. (K) - [SDR SB05061](https://openairdocs.org/sdr/SB05061), May 14, 2005: WIRE. BROKEN. MAINTENANCE REPORTED THE EMERGENCY LIGHT ON SEAT 5A INOPERATIVE. MAINTENANCE REPAIRED WIRE ON LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. - [SDR SB05034](https://openairdocs.org/sdr/SB05034), Mar 2, 2005: SWITCH. FAULTY. SYR - MAINTENANCE REPORTED THAT WHEN THE BATTERY IS SELECTED OFF, THE EMERGENCY EXIT LIGHTS ILLUMINATE AND WILL NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED T - [SDR USAA040685](https://openairdocs.org/sdr/USAA040685), Sep 29, 2004: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 1 NCH, STATION 943 STRINGER 24L. INSTALLED DOUBLER IAW EA 95872A. (M) - [SDR USAA040364](https://openairdocs.org/sdr/USAA040364), Jul 20, 2004: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 1 INCH LONG, FS 727D AND STRINGER 23L. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M) - [SDR USAASB04081](https://openairdocs.org/sdr/USAASB04081), Jun 27, 2004: BATTERY PACK. INOPERATIVE. PIT - FOUND DURING WEEKLY CHECK, MAINTENANCE FOUND THE INTERIOR EMERGENCY LIGHTS AT SEAT ROWS 12 THROUGH 16 AND THE EXTERIOR LIGHTS AT RIGHT OVERWING EXIT AND L - [SDR USAA030322](https://openairdocs.org/sdr/USAA030322), Dec 28, 2003: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 2.250 INCH, 4 INCHES FORWARD OF FS 727E .500 INCH ABOVE S-24R ON SKIN. INSTALLED DOUBLER 24 INCHES BY 30 INCHES PER SRM 53-00-01 FIG 22 - [SDR USAASB03120](https://openairdocs.org/sdr/USAASB03120), Jul 23, 2003: CONTROL VALVE. FAILED. ON SLOW DESCENT TO PHL, FROM FL370 TO FL350, THE NR 1 ENGINE BLEED TRIPPED FOLLOWED BY A PACK TRIP. FLIGHT DESCENDED TO 10,000 FEET AND CONTINUED TO PHL UNPRESS - [SDR USAA030092](https://openairdocs.org/sdr/USAA030092), Jun 6, 2003: STRUCTURE. DAMAGED. PIT - BEARING BORE REPAIR, SINGLE LUGE MOUNT BEARING BORE OF CROSSBEAM. INSTALLED OVERSIZED BEARING. (M) - [SDR USAASB03022](https://openairdocs.org/sdr/USAASB03022), Feb 9, 2003: ACTUATOR. MALFUNCTIONED. PIT - FLT 865 - DURING APPROACH, CREW REPORTED THE NR 5 LEADING EDGE SLAT INTRANSIT LIGHT ILLUMINATED WHEN FLAPS/SLATS WERE SET TO 5 UNITS. CREW NOTED AIRCRAFT - [SDR USAASB02057](https://openairdocs.org/sdr/USAASB02057), Mar 19, 2002: PUMP. FAILED. CLT - FLT 9228 - DURING CLIMB-OUT FROM TPA, EN ROUTE TO CLT, CAPTAIN REPORTED THE HYDRAULIC MASTER CAUTION ILGHTS ILLUMINATING INTERMITTENTLY. CAPTAIN OBSERVED - [SDR USAASB01307](https://openairdocs.org/sdr/USAASB01307), Nov 5, 2001: BATTERY PACK. DISCHARGED. CLT - MAINTENANCE FOUND THREE SECTIONS OF CABIN EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THREE CABIN EMERGENCY LIGHT BATTERY PACKS. OPS - [SDR USAA010704](https://openairdocs.org/sdr/USAA010704), May 18, 2001: BELLCRANK. BROKEN. PIT - FOUND BELLCRANK HAD .75 INCH SECTION BROKEN OUT, RT INBOARD AILERON HINGE ASSY. NOTCHED OUT TOP OF FITTING, REMOVED LOWER FLANGE, INSTALLED TWO MACHINED D - [SDR USAA010733](https://openairdocs.org/sdr/USAA010733), May 17, 2001: WEB. CRACKED. PIT - FOUND ANGLE WEB CRACKED 1 INCH, UNDER AFT SERVICED DOOR SILL PLATE. MANUFACTURED AND INSTALLED NEW WEB PER BOEING DRAWING 65.45855. (M) - [SDR USAA010734](https://openairdocs.org/sdr/USAA010734), May 17, 2001: SKIN. CRACKED. PIT - FOUND PYLON SKIN CRACKED 1 INCH, UPPER RIGHT CORNER OF PANEL 5724L OPENING. STOP DRILLED CRACK, INSTALLED DOUBLER PER TYPICAL REPAIR 54-50-07. (M) - [SDR USAA010735](https://openairdocs.org/sdr/USAA010735), May 17, 2001: SKIN. CRACKED. PIT - FOUND SKIN CRACKED .25 INCH, BS 947 AT STRINGER 11R. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-60-01. (M) - [SDR USAA010736](https://openairdocs.org/sdr/USAA010736), May 17, 2001: FRAME. CRACKED. PIT - FOUND FRAME CRACKED .25 INCH, BS 663 AT S2L. CUT OUT DAMAGE, INSTALLED DOUBLER PER SRM 53-00-07 FIG 208, SRM 51-70-13, SRM 53-60-08, SRM 53-60-08. (M) - [SDR USAA010737](https://openairdocs.org/sdr/USAA010737), May 17, 2001: FRAME. CRACKED. PIT - FOUND FRAME CRACKED .25 INCH, BS 747 AT S8R. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-10-14. (M) - [SDR USAA010738](https://openairdocs.org/sdr/USAA010738), May 17, 2001: FRAME. CRACKED. PIT - FOUND FRAME CRACKED .25 INCH, BS 440 AT S8L. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-10-14. (M) - [SDR USAA010739](https://openairdocs.org/sdr/USAA010739), May 17, 2001: CLIP. CRACKED. PIT - FOUND CLIP CRACKED .25 INCH, BS 360 AT S13L. FABRICATED, HEAT TREATED AND INSTALLED PER SRM 53-00-07 FIG 205. (M) - [SDR USAA010740](https://openairdocs.org/sdr/USAA010740), May 17, 2001: FRAME. CRACKED. PIT - FOUND FRAME CRACKED .5 INCH, BS 440 AT STRINGER 8R. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-10-14. (M) - [SDR USAA010710](https://openairdocs.org/sdr/USAA010710), May 17, 2001: BULKHEAD. CRACKED. PIT - FOUND BULKHEAD CRACKED .125 INCH, STATION 178 BETWEEN LBL 5.7 AND 17. REPAIRED DOUBLER, FILLER PER SRM 53-10-08 PAGES 265-269. (M) - [SDR USAA010728](https://openairdocs.org/sdr/USAA010728), May 17, 2001: SKIN. CRACKED. PIT - FOUND SKIN CRACKED .095 INCH, LOWER HINGE CUTOUT. ROUTED OUT CRACK AND INSTALLED DOUBLER PER SRM 52-10-01 S/B 737-52-1096. (M) - [SDR USAA010708](https://openairdocs.org/sdr/USAA010708), May 17, 2001: WEB. CRACKED. PIT - FOUND WEB CRACKED .75 INCH, STATION 178 BULKHEAD WL 184. REPAIRED FILLERS, DOUBLERS AND SHIMS PER SRM 53-10-08 FIG 211. (M) - [SDR USAA010711](https://openairdocs.org/sdr/USAA010711), May 17, 2001: WEB. CRACKED. PIT - FOUND WEB CRACKED 5 INCHES, STATION 178 BULKHEAD RIGHT FLOOR WEB AT WL 207. REMOVED AND REPLACED FLOORWEB. (M) - [SDR USAA010712](https://openairdocs.org/sdr/USAA010712), May 17, 2001: ANGLE. CRACKED. PIT - FOUND ANGLE CRACKED .125 INCH, STATION 178 BULKHEAD RIGHT CHORD ANGLE AT WL 207. REPAIRED DOUBLER, CHORD, CLIPS, SPLICE ANGLE PER SRM 53-10-08. (M) - [SDR USAA010713](https://openairdocs.org/sdr/USAA010713), May 17, 2001: ANGLE. CRACKED. PIT - FOUND ANGLE CRACKED .125 INCH, STATION 178 BULKHEAD LEFT CHORD ANGLE AT WL 207. REPAIRED FILLER, DOUBLER AND SHIMS PER SRM 53-10-08 FIG 211. (M) - [SDR USAA010714](https://openairdocs.org/sdr/USAA010714), May 17, 2001: WEB. CRACKED. PIT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD LBL 5.7 WL 200, LOWER ANTENNA MOUNT. REPAIRED FILLER, DOUBLER AND SHIMS PER SRM 53-10-08 FIG 211. (M) - [SDR USAA010715](https://openairdocs.org/sdr/USAA010715), May 17, 2001: WEB. CRACKED. PIT - FOUND WEB CRACKED .25 INCHES IN LENGTH, STATION 178 BULKHEAD LBL 5.7 WL 210 UPPER ANTENNA MOUNT. REPAIRED FILLER, DOUBLER AND SHIMS PER SRM 53-10-08 FIG 2 - [SDR USAA010716](https://openairdocs.org/sdr/USAA010716), May 17, 2001: CLIP. CRACKED. PIT - FOUND CLIP CRACKED .25 INCH, BS 639 AT S11L. MANUFACTURED, HEAT TREATED, INSTALLED CLIP PER BOEING PRINT 66-2411241-1. (M) - [SDR USAA010718](https://openairdocs.org/sdr/USAA010718), May 17, 2001: FRAME. CRACKED. PIT - FOUND FRAME CRACKED 1 INCH, BS 787 BETWEEN 58L AND 59L. INSTALLED DOUBLER PER T/R 53-10-14. (M) - [SDR USAA010723](https://openairdocs.org/sdr/USAA010723), May 17, 2001: FRAME. CRACKED. PIT - FOUND FRAME CRACKED .25 INCH, BS 480 AT STRINGER 8R. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-10-14 AND EA 70650. (M) - [SDR USAA010724](https://openairdocs.org/sdr/USAA010724), May 17, 2001: FRAME. CRACKED. PIT - FOUND FRAME CRACKED .5 INCH, BS 500C AT STRINGER 8R. ROUTED OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-10-14 AND EA 70647. (M) All 98: https://openairdocs.org/deregistered/N586US-2007-08-13/reports.md ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB NYC93IA017](https://openairdocs.org/ntsb/NYC93IA017), Oct 12, 1992: Boeing 737-300 (N586US), Pittsburgh, PA, incident, no damage. Probable cause: THE HIGH CYCLE FATIGUE FAILURE OF BLADES ON THE STAGE 1 HIGH PRESSURE COMPRESSOR, WHICH RESULTED IN BLADE FRACTURE AND SUBSEQUENT INTERNAL ENGINE DAMAGE AND FIRE. ## FAA accident and incident reports (1) 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 19921012046589I](https://openairdocs.org/incident/19921012046589I), Oct 12, 1992: Boeing 737301 (N586US), Pittsburgh, PA. Smoke and flames from right engine on takeoff. Aborted. Appears to have stage one or two blade failure. ## Other aircraft with N586US - [Registered now](https://openairdocs.org/aircraft/N586US): DJI AGRAS T50, S/N 1581F6BUB24A60016J41 --- 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.