# Service difficulty reports: N586US, cancelled Aug 13, 2007 A list on [N586US, cancelled Aug 13, 2007](https://openairdocs.org/deregistered/N586US-2007-08-13.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 98 reports - [SDR 2007FA0000135](https://openairdocs.org/sdr/2007FA0000135.md): Frame · cracked · Sep 27, 2006 · N586US · Boeing 737301 · Fuselage Main, Frame > FRAME IS CRACKED AT BODY STATION 727, STRINGER 14L. (K) - [SDR 2007FA0000128](https://openairdocs.org/sdr/2007FA0000128.md): Skin · dented · Sep 27, 2006 · N586US · Boeing 737301 · Fuselage Main, Plate/Skin > BODY STATION 915 ABOVE STRINGER 25L LAP JOINT FUSELAGE SKIN HAS DENT. (K) - [SDR 2007FA0000126](https://openairdocs.org/sdr/2007FA0000126.md): Frame · cracked · Sep 27, 2006 · N586US · Boeing 737301 · Fuselage Main, Frame > FRAME IS CRACKED AT BODY STAION 727, STRINGER 14L. (K) - [SDR 2007FA0000125](https://openairdocs.org/sdr/2007FA0000125.md): Frame · cracked · Sep 26, 2006 · N586US · Boeing 737301 · Fuselage Main, Frame > UPPER FUSELAGE, BS 500A, BETWEEN STR 8R AND STR 9R, FRAME IS CRACKED AT PSU MOUNT. (K) - [SDR 2007FA0000124](https://openairdocs.org/sdr/2007FA0000124.md): Skin · gouged · Sep 26, 2006 · N586US · Boeing 737301 · Fuselage Main, Plate/Skin > 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.md): Fitting · corroded · Sep 24, 2006 · N586US · Boeing 737301 · Fuselage Miscellaneous Structure > 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.md): Pressure Panel · cracked · Sep 24, 2006 · N586US · Boeing 737301 · Fuselage Main, Bulkhead > MID CABIN BS 663, LBL 31, WHEEL WELL PRESSURE DECK WEB, CRACKED. (K) - [SDR 2007FA0000133](https://openairdocs.org/sdr/2007FA0000133.md): Frame · cracked · Sep 24, 2006 · N586US · Boeing 737301 · Fuselage Main, Frame > CABIN, BS 787, FRAME AT STR 8R, CRACKED AT STOW BIN ATTACH BRACKET. (K) - [SDR 2007FA0000129](https://openairdocs.org/sdr/2007FA0000129.md): Floorbeam · gouged · Sep 24, 2006 · N586US · Boeing 737301 · Fuselage Main, Floor Beam > CABIN FLOORBEAM, STA 827, WL 203.6, RBL 10, LOWER T-CAP, AFT FLANGE, GOUGED. (K) - [SDR 2007FA0000140](https://openairdocs.org/sdr/2007FA0000140.md): Support · cracked · Sep 18, 2006 · N586US · Boeing 737300 · Passenger/Crew Doors > AT FWD CABIN STA 328+6, DOOR 2R AFT STOP FTG INTERCOSTAL TEE SUPPORT, CRACKED. (K) - [SDR 2007FA0000139](https://openairdocs.org/sdr/2007FA0000139.md): Frame · cracked · Sep 18, 2006 · N586US · Boeing 737300 · Fuselage Main, Frame > 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.md): Frame · cracked · Sep 18, 2006 · N586US · Boeing 737300 · Fuselage Main, Frame > MID CABIN, STATION 480 FRAME, AT STRINGER 8L, CRACKED AT PSU MOUNT RAIL ATTACH POINT. (K) - [SDR 2007FA0000137](https://openairdocs.org/sdr/2007FA0000137.md): Stringer Clip · cracked · Sep 18, 2006 · N586US · Boeing 737300 · Fuselage Main, Attach Fittings > PASSENGER CABIN, STATION 639 AT STRINGER 4L, STRINGER CLIP, CRACKED. (K) - [SDR 2007FA0000131](https://openairdocs.org/sdr/2007FA0000131.md): Crease Beam · corroded · Sep 18, 2006 · N586US · Boeing 737300 · Fuselage Main, Structure > 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.md): Frame · cracked · Sep 18, 2006 · N586US · Boeing 737300 · Fuselage Main, Frame > MID CABIN, STATION 400 FRAME AT STRINGER 8R, CRACKED AT PSU RAIL OUNT ATTACH POINT. (K) - [SDR 2007FA0000127](https://openairdocs.org/sdr/2007FA0000127.md): Frame · cracked · Sep 18, 2006 · N586US · Boeing 737301 · Fuselage Main, Frame > 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.md): Intercostal · cracked · Sep 18, 2006 · N586US · Boeing 737300 · Fuselage Miscellaneous Structure > CABIN STA 303.9 JUST ABOVE STRINGER 10L. INTERCOSTAL OUTER CHORD ANGLE, CRACKED. (K) - [SDR 2007FA0000132](https://openairdocs.org/sdr/2007FA0000132.md): Floorbeam · corroded · Aug 17, 2006 · N586US · Boeing 737301 · Fuselage Main, Floor Beam > CABIN BS 312, FROM LBL 55 TO RBL 55 WL 208, FLOORBEAM HAS LIGHT CORROSION. (K) - [SDR SB05061](https://openairdocs.org/sdr/SB05061.md): Wire · broken · May 14, 2005 · N586US · Boeing 737301 · Light System Wiring > 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.md): Switch · faulty · Mar 2, 2005 · N586US · Boeing 737301 · Emergency Lighting > SYR - MAINTENANCE REPORTED THAT WHEN THE BATTERY IS SELECTED OFF, THE EMERGENCY EXIT LIGHTS ILLUMINATE AND WILL NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT SWITCH. OPERATIONAL CHECK GOOD. - [SDR USAA040685](https://openairdocs.org/sdr/USAA040685.md): Skin · cracked · Sep 29, 2004 · N586US · Boeing 737301 · Fuselage Main, Plate/Skin > CLT - FOUND SKIN CRACKED 1 NCH, STATION 943 STRINGER 24L. INSTALLED DOUBLER IAW EA 95872A. (M) - [SDR USAA040364](https://openairdocs.org/sdr/USAA040364.md): Skin · cracked · Jul 20, 2004 · N586US · Boeing 737301 · Fuselage Main, Plate/Skin > 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.md): Battery Pack · inoperative · Jun 27, 2004 · N586US · Boeing 737301 · Emergency Lighting > 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 LEFT AFT FUSELAGE, EXTINGUISH AFTER 10 SECONDS OF OPERATION. MAINTENANCE REMOVED AND REPLACED THE BA - [SDR USAA030322](https://openairdocs.org/sdr/USAA030322.md): Skin · cracked · Dec 28, 2003 · N586US · Boeing 737301 · Fuselage Main, Plate/Skin > 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 229. (M) - [SDR USAASB03120](https://openairdocs.org/sdr/USAASB03120.md): Control Valve · failed · Jul 23, 2003 · N586US · Boeing 737301 · Pneumatic Distribution System > 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 UNPRESSURIZED. BLEED RESET AFTER COOLING PERIOD PER QUICK REF HANDBOOK PROCEDURES. FLIGHT LANDED WITHOUT - [SDR USAA030092](https://openairdocs.org/sdr/USAA030092.md): Structure · damaged · Jun 6, 2003 · N586US · Boeing 737301 · Nacelle/Pylon Miscellaneous Structure > PIT - BEARING BORE REPAIR, SINGLE LUGE MOUNT BEARING BORE OF CROSSBEAM. INSTALLED OVERSIZED BEARING. (M) - [SDR USAASB03022](https://openairdocs.org/sdr/USAASB03022.md): Actuator · malfunctioned · Feb 9, 2003 · N586US · Boeing 737301 · Leading Edge Slat Actuator > 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 WANTED TO ROLL RT DURING FLAP/SLAT SET. NR 5 LEADING EDGE SLAT DID NOT RETRACT UNTIL APPROXIMATELY - [SDR USAASB02057](https://openairdocs.org/sdr/USAASB02057.md): Pump · failed · Mar 19, 2002 · N586US · Boeing 737301 · Hydraulic Pump (Electric/Engine), Main > CLT - FLT 9228 - DURING CLIMB-OUT FROM TPA, EN ROUTE TO CLT, CAPTAIN REPORTED THE HYDRAULIC MASTER CAUTION ILGHTS ILLUMINATING INTERMITTENTLY. CAPTAIN OBSERVED 'A' SYSTEM HYDRAULIC QUANTITY AT REFILL. A SHORT TIEM LATER, 'A' SYSTEM HYDRAULIC PRESSURE FLUCTUA - [SDR USAASB01307](https://openairdocs.org/sdr/USAASB01307.md): Battery Pack · discharged · Nov 5, 2001 · N586US · Boeing 737301 · Emergency Lighting > CLT - MAINTENANCE FOUND THREE SECTIONS OF CABIN EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THREE CABIN EMERGENCY LIGHT BATTERY PACKS. OPS CHECK OF EMERGENCY LIGHTS GOOD. (M) - [SDR USAA010704](https://openairdocs.org/sdr/USAA010704.md): Bellcrank · broken · May 18, 2001 · N586US · Boeing 737301 · Aileron Control System > 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 DOUBLERS PER EA 71077. (M) - [SDR USAA010733](https://openairdocs.org/sdr/USAA010733.md): Web · cracked · May 17, 2001 · N586US · Boeing 737301 · Fuselage Miscellaneous Structure > 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.md): Skin · cracked · May 17, 2001 · N586US · Boeing 737301 · Nacelle/Pylon, Plate/Skin > 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.md): Skin · cracked · May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General) > 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.md): Frame · cracked · May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General) > 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.md): Frame · cracked · May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General) > 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.md): Frame · cracked · May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General) > 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.md): Clip · cracked · May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General) > 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.md): Frame · cracked · May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General) > 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.md): Bulkhead · cracked · May 17, 2001 · N586US · Boeing 737301 · Fuselage Main, Structure > 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.md): Skin · cracked · May 17, 2001 · N586US · Boeing 737301 · Doors > 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.md): Web · cracked · May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General) > 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.md): Web · cracked · May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General) > 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.md): Angle · cracked · May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General) > 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.md): Angle · cracked · May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General) > 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.md): Web · cracked · May 17, 2001 · N586US · Boeing 737301 · Fuselage Main, Structure > 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.md): Web · cracked · May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General) > 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 211. (M) - [SDR USAA010716](https://openairdocs.org/sdr/USAA010716.md): Clip · cracked · May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General) > 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.md): Frame · cracked · May 17, 2001 · N586US · Boeing 737301 · Fuselage Main, Structure > 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.md): Frame · cracked · May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General) > 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.md): Frame · cracked · May 17, 2001 · N586US · Boeing 737301 · Fuselage Structure (General) > 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) Next page: https://openairdocs.org/deregistered/N586US-2007-08-13/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N586US' AND deregistration_id = 'N586US-2007-08-13' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N586US-2007-08-13/reports --- 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.