Boeing 737-301

Service difficulty reports · 4,797

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "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 aircraft_model_key = '737301'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR F3LA200200326Floor Support · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT, BS 328 TO 344, LBL 12. REPLACED FLOOR SUPPORT PER SRM 53-10-51, 51-40-02 AND EA 53-737-181.Oct 6, 2002 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR F3LA200200325Floor Support · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT, BS 294.5 TO 312, LBL 12. REPLACED FLOOR SUPPORT PER SRM 53-10-51, 51-40-02 AND EA 53-737-181.Oct 6, 2002 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA020384Skin · crackedPIT - FOUND SKIN WITH THREE CRACKS, ONE AT .075 INCH, TWO AT .250 INCH, STATION 380 BL 0. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER TYPICAL REPAIR 53-30-07. (M)Oct 5, 2002 · N573US · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA200201002Support · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 3" CRACK WAS FOUND ON THE INTERCOASTAL FOR AFT CARGO COMPARTMENT DOOR LATCH SUPPORT, BS 787. MAINTENANCE REMOVED THE CRACKED AFT CARGO COMPARTMENT DOOR LATCH SUPPORT AT BS 787, FABRICATED A NEW REPLACEMENT SUPPORT, AND Oct 5, 2002 · N324AW · Boeing 737301 · Wing Miscellaneous StructureSDR USAA020431Skin · crackedPIT - FOUND SKIN CRACKED .25 INCH LONG, BETWEEN AT 1 AND NR 2 CAPTAINS WINDOW. INSTALLED BOEING DOUBLER PER SRM 53-10-01. (M)Oct 4, 2002 · N558AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA020388Angle · crackedPIT - FOUND VERT Z-ANGLE CRACKED IN HALF, FORWARD BULKHEAD LEFT SIDE W/W STATION 663 LBBL 6.15. INSTALLED TEMP SUPPORT ANGLE AND STRAPS PER EA 74968A. (M)Oct 4, 2002 · N590US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA020390Stiffener · crackedIT - FOUND STIFFENER ANGLE CRACKED 1 INCH LONG, VERTICAL STIFFENER MLG W/W FORWARD BULKHEAD CENTER LINE STATION 663. FABRICATED AND INSTALLED 2 REPAIR STRAPS AND ATTACH ANGLE IAW EA 75025. (M)Oct 4, 2002 · N355US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA020381Skin · delaminatedPIT - RUDDER SKIN DELAMINATED, BOTTOM L/E CORNERS RT AND LT SIDE. REMOVED DAMAGE, REPAIRED AND RESTORED PER EA 75009, AND SRM 51-70-03. (M)Oct 4, 2002 · N588US · Boeing 737301 · Rudder, Plate/SkinSDR AWXA200201037Beam · crackedDURING C-17 CHECK A 1/2 INCH CRACK WAS FOUND ON AFT CARGO DOOR LOWER CROSS BEAM AT FASTENER HOLE AFT END OF DOOR BS 801.5, STR 23 RT. MAINTENANCE CUTOUT DAMAGED AREA OF CROSS BEAM AT BS 801.5, STR 23 RT; FABRICATED A REPLACEMENT SECTION OF TEE CHORD, 2 EACH REOct 4, 2002 · N324AW · Boeing 737301 · Cargo/Baggage DoorsSDR F3LA200200355Floor Support · corrodedDURING C 4 CHECK, USING INSPECTION CRITERIA IN SRM 53-60-53, CORROSION WAS FOUND AROUND THE NUT PLATE ON THE FLOOR SUPPORT CHANNEL AT RBL 3 AT BS 887. REMOVED AND REPLACED A SECTION OF THE FLOOR SUPPORT CHANNEL, FROM BS 887 TO BS 947 AT RBL 3, IAW SRM 53-00-5Oct 4, 2002 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200201021Clip · crackedDURING C-17 CHECK A 1/2 INCH CRACK WAS FOUND ON RIB BRACKET (SPRING CLIP) AT THE OUTBOARD SIDE OF THE RT PYLON NAC STA 282.67, NAC WL 117. MAINTENANCE REMOVED THE DAMAGED SPRING CLIP AT THE OUTBOARD SIDE OF RT PYLON NAC STA 282.67, NAC WL 117; FABRICATED A NEWOct 4, 2002 · N324AW · Boeing 737301 · Nacelle/Pylon, Main FrameSDR AWXA200201020Clip · crackedDURING C-17 CHECK 2 EACH 3/4 INCH CRACKS WERE FOUND ON RIB BRACKETS (SPRING CLIPS) AT THE INBOARD SIDE OF THE LT PYLON NAC STA 282.67, NAC WL 117. MAINTENANCE REMOVED 2 EACH DAMAGED SPRING CLIPS AT INBOARD SIDE OF THE LT PYLON NAC STA 282.67, NAC WL 117; FABRIOct 4, 2002 · N324AW · Boeing 737301 · Nacelle/Pylon, Main FrameSDR AWXA200201012Channel · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 2 1/2" CRACK WAS FOUND ON THE LOWER WEB OF R/H PYLON STRUT FAIRING BETWEEN NAC STA. 345 TO 363, WL 117. MAINTENANCE REMOVED 1 EACH CHANNEL AND FRAME AT R/H PYLON STRUT FAIRING BETWEEN NAC STA. 345 TO 363, WL 117; FABRICOct 4, 2002 · N324AW · Boeing 737301 · Nacelle/Pylon, Frame/Spar/RibSDR AWXA200201004Web · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK MULTIPLE CRACKS (8 EACH) WERE FOUND ON BULKHEAD BS 178 AT LBL 1.25 AND RBL 1.5 WL 206, LBL 11 AND RBL 11 WL 213, LBL 4.7 WL 198 & 201, RBL 4.7 WL 198 & 210. MAINTENANCE CUTOUT DAMAGE ON WEB BS 178 AT LBL 1.25 AND RBL 1.5 Oct 4, 2002 · N324AW · Boeing 737301 · Fuselage Main, BulkheadSDR F3LA200200351Floor Support · corrodedDURING C 4 CHECK, CORROSION WAS FOUND ON THE FLOOR SUPPORT CHANNEL AT BS 897 AROUND THE NUT PLATE HOLE. REMOVED AND REPLACED SECTION OF FLOOR SUPPORT CHANNEL FROM BS 887 TO BS 947, RBL 3, IAW SRM 53-00-53Oct 4, 2002 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR F3LA200200350Cargo Track · corrodedDURING C 4 CHECK, CORROSION WAS FOUND ON CARGO TRACK AT BS 947, RBL 14 AT THE TIE DOWN SOCKET. CARGO TRACK SECTION WAS REPLACED IN ACCORDANCE WITH SRM 53-00-53, FROM BS 867 TO BS 947.Oct 4, 2002 · N578US · Boeing 737301 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200201001Angle · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK 3 EACH 1 1/2" CRACKS WERE FOUND ON FLOOR SUPPORT ANGLE FROM BS 500D TO BS 520, BL 0. MAINTENANCE REMOVED CRACKED FLOOR SUPPORT UPPER ATTACH ANGLE FROM BS 500D TO BS 520, FABRICATED A NEW REPLACEMENT UPPER ATTACH ANGLE, ANOct 4, 2002 · N324AW · Boeing 737301 · Fuselage Main, Floor BeamSDR F3LA200200317Channel · corrodedDURING C-4 CHECK, INSPECTION REPORTED FLOOR SUPPORT CHANNEL CORRODED AT BBL 8.1 BETWEEN BS 867 AND 847. FABRICATED AND INSTALLED REPAIR PER SRM 53-00-53, 55-00-53, 51-40-02 AND SOPM 20-41-02.Oct 4, 2002 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR F3LA200200316Frame · crackedDURING C-4 CHECK, INSPECTION REPORTED LT FUSELAGE FORMER AT FWD OTBD CORNER OF OUTER AIR CONDITIONING DUCT BAY DOOR CRACKED APPROXIMATELY 4 INCHES. DRILLED AND INSTALLED REPLACEMENT TEE CHORD PER SRM 51-40-02 AND 51-10-2.Oct 4, 2002 · N578US · Boeing 737301 · Fuselage Main, FrameSDR F3LA200200315Threshold · corrodedDURING C-4 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR SILL PLATE IN FRONT OF C2 DOOR CORRODED. REPLACED THRESHOLD WEB PER SRM 51-40-02 AND 51-30-01.Oct 4, 2002 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR F3LA200200314Skin · dentedDURING C-4 CHECK, INSPECTION REPORTED L/E OF LT OTBD MID T/E FLAP DENTED AND GOUGED AT OTBD ACTUATOR. FABRICATED AND INSTALLED DOUBLER PER SRM 57-53-01, SOPM 20-41-02 AND SOPM 20-42-01.Oct 4, 2002 · N578US · Boeing 737301 · Trailing Edge FlapsSDR F3LA200200313Angle · looseDURING C-4 CHECK, INSPECTION REPORTED RT WING INBD TE PLATE LOOSE FASTENERS ON MID FLAP. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-30-01, FIGURE 7 AND 51-40-02.Oct 4, 2002 · N578US · Boeing 737301 · Trailing Edge FlapsSDR F3LA200200312Doubler · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON RADIO ALTIMETER ANTENNA INTERNAL DOUBLER BETWEEN BS 440 AND 460. REPLACED RADIO ALTIMETER ANTENNA INTERNAL DOUBLER PER SRM 51-10-2 AND BOEING DRAWING 69-27827.Oct 4, 2002 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA020383Angle · crackedPIT - FOUND Z-ANGLE CRACKED 2 INCHES, W/W FORWARD BULKHEAD LEFT CENTER VERTICAL Z-ANGLE. MANUFACTURED IAW EA 75003. (M)Oct 3, 2002 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB02185Wire · brokenEWR - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT 1C INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE UNDER SEATS 2A AND C. OPERATIONAL CHECK GOOD. (M)Oct 3, 2002 · N585US · Boeing 737301 · Light System WiringSDR AWXA200201045Skin · wornMCN - MAJOR REPAIR - DURING C-17 CHECK A WORN AREA WAS FOUND ON THE L/H WING MID FLAP AT THE TOP INBOARD END, WBL 73. MAINTENANCE CUTOUT DAMAGED AREA OF L/H WING MID FLAP AT THE TOP INBOARD END WBL 73; FABRICATED A PLATE, 2 EACH DOUBLERS, AND A FILLER; BONDED Oct 3, 2002 · N324AW · Boeing 737301 · Trailing Edge FlapsSDR AWXA200201042Bulkhead · canningMCN - MAJOR REPAIR - DURING C-17 CHECK OIL CANNING WAS DISCOVERED ON THE AFT PRESSURE BULKHEAD BS 1016, RBL 54, BETWEEN STR 11 R/H AND STR 13 R/H, CANNING CONCAVED FORWARD. MAINTENANCE REMOVED BOLTS FROM STR 11 R/H TO STR 14 R/H, FABRICATED AND INSTALLED SHIMSOct 3, 2002 · N324AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA200201000Angle · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1 1/2" CRACK WAS FOUND ON THE L/H UPPER WING PANEL ATTACH ANGLE OUTBOARD OF THE PYLON, WS 204.40. MAINTENANCE REMOVED CRACKED L/H UPPER WING PANEL ATTACH ANGLE AT WS 204.40, FABRICATED A NEW REPLACEMENT ATTACH ANGLE, ANOct 3, 2002 · N324AW · Boeing 737301 · Wing Miscellaneous StructureSDR USAA020416Support · corrodedPIT - FOUND SUPPORT CORRODED SEVERAL AREAS, BS 960 Z-ANGLE SUPPORT, AFT ENTRY THRESHOLD DOOR JAM. CORROSION, LEVEL 2, TASK NR C53-107-01. REPLACED Z-ANGLE PER BOEING DWG 65-52878. (M)Oct 2, 2002 · N300AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR F3LA200200311Bear Strap · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON C-1 DOOR BEAR STRAP AT BS 441, RBL 7.5. FABRICATED AND INSTALLED REPAIR PER PER EA 53-737-180.Oct 2, 2002 · N578US · Boeing 737301 · Fuselage Main, StructureSDR F3LA200200310Floorbeam · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON 312 FLOOR BEAM UPPER CHORD. FABRICATED AND INSTALLED REPLACEMENT UPPER CHORD PER SRM 51-40-02, 51-40-06 AND SOPM 20-41-01.Oct 2, 2002 · N578US · Boeing 737301 · Fuselage Main, Floor BeamSDR F3LA200200308Floor Support · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON DIAGONAL FLOOR SUPPORT BETWEEN BS 1006 AND 1016, RT. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER SRM 53-60-51 AND 51-40-02.Oct 2, 2002 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR F3LA200200309Floor Support · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON DIAGONAL FLOOR SUPPORT BETWEEN BS 1006 AND 1016, L/H. FABRICATED AND INSTALLED REPLACEMENT FLOOR SUPPORT PER SRM 53-60-51 ANDD 51-40-02.Oct 2, 2002 · N578US · Boeing 737301 · Fuselage Main, Floor BeamSDR F3LA200200307Floorbeam · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR BEAM UPPER CHORD AT BS 294.5. FABRICATED REPLACEMENT PARTS AND INSTALLED REPAIR PER SRM 53-10-51, SRM 51-40-02 AND SOPM 20-41-02.Oct 2, 2002 · N578US · Boeing 737301 · Fuselage Main, Floor BeamSDR F3LA200200306Channel · corrodedDURING C-4 CHECK, INSPECTION REPORTED FLOOR CHANNEL CORRODED AT BS 727D ABOVE STRINGER 28L. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-60-53. FABRICATED AND INSTALLED REPLACEMENT CHANNEL PER SRM 53-60-53, SRM 51-40-02 AND SOPM 20-41-02.Oct 2, 2002 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR F3LA200200305Angle · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR TO BULKHEAD ANGLE AT BS 947. REPLACED BULKHEAD ANGLE PER SRM 53-30-53 AND 51-40-03.Oct 2, 2002 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR F3LA200200304Strap · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR STRAP BETWEEN BS 1006 AND BS 1016, RBL 18. FABRICATED AND INSTALLED REPLACEMENT FLOOR STRAP PER BOEING DRAWING 65-46812 AND SRM 51-30-01.Oct 2, 2002 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR F3LA200200303Strap · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR STRAP AT BS 1016. FABRICATED AND INSTALLED REPLACEMENT FLOOR STRAP PER SRM 53-30-01 AND BOEING DRAWING 65-46812.Oct 2, 2002 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR F3LA200200302Web · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR WEB AT BS 1016. FABRICATED AN INSTALLED REPLACEMENT WEB PER BOEING DRAWING 65-46812-109 AND SRM 53-30-01.Oct 2, 2002 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR F3LA200200301Intercostal · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL IN FWD CARGO COMPARTMENT BETWEEN BS 500B AND 500C, ABOVE STR 25L. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 53-30-04 AND 51-40-02.Oct 2, 2002 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR F3LA200200300Intercostal · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL BETWEEN BS 294.5 AND BS 312, RBL 1 AND CRACKED ON AFT END. REMOVED DAMAGED INTERCOSTAL PER SRM 51-40-02. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-40-06, SRM 51-40-02 AND SOPM 2Oct 2, 2002 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR F3LA200200299Intercostal · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL IN FWD CARGO COMPARTMENT BETWEEN BS 500 AND 500A, ABOVE STR 25L. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 53-30-04 AND 51-40-02.Oct 2, 2002 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR F3LA200200298Stringer · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON STR 25L AT BS 500B+6. REPAIRED PER SRM 53-00-03, DETAIL VII.Oct 2, 2002 · N578US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR F3LA200200297Stringer · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON STR 26R AT BS 380. REMOVED CORRODED SECTION OF STRINGER PER SRM 51-40-02. FABRICATED AND INSTALLED REPAIR PER SRM 53-30-03 AND 53-00-03.Oct 2, 2002 · N578US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR F3LA200200296Sill · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON R2 MOP SILL. REPLACED MOP SILL PER SRM 51-40-02.Oct 2, 2002 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR F3LA200200295Sill · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON L2 DOOR MOP SILL. REPLACED MOP SILL PER SRM 51-40-02.Oct 2, 2002 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR F3LA200200294Intercostal · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT BS 947-967, LBL 45. REMOVED INTERCOSTAL PER SRM 51-40-02. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 53-60-51, 51-40-02, MM 51-21-99 AND EA 53-737-181.Oct 2, 2002 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR F3LA200200293Attach Angle · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON CLOSET ATTACH ANGLES AT BS 1015. FABRICATED AND INSTALLED REPLACEMENT ANGLES PER BOEING DRAWING 65-48812 AND SRM 51-40-02.Oct 2, 2002 · N578US · Boeing 737301 · Fuselage, Equipment Attach FittingsSDR F3LA200200292Intercostal · corrodedDURING C-4 CHECK, INSPECTION REPORTED ON CORROSION ON FLOOR INTERCOSTAL AT STA 986.5 - 1006, RBL 37. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-40-02 AND 53-60-51.Oct 2, 2002 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR F3LA200200291Intercostal · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION STA 947-967 LBL 17 INTERCOSTAL. FABRICATED NEW INTERCOSTAL PART SRM 53-60-51 & MM 51-21-99. INSTALLED PART PER SRM 51-40-02 & EA 53-737-181.Oct 2, 2002 · N578US · Boeing 737301 · Fuselage Miscellaneous Structure
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