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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR F3LA200200290Channel · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO BIN LT FLOOR SUPPORT ZEE CHANNEL. FOUND TO BE OUT OF LIMITS PER SRM 53-60-53. FABRICATED PARTS PER SRM 53-60-53 & SOPM 20-41-02. INSTALLED PART PER SRM 51-40-02.SDR F3LA200200289Intercostal · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION STA 947-967 LBL 30-45 ON INTERCOSTAL. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 53-60-51, 51-40-02, EA 53-737-181 AND MM 51-21-99.SDR F3LA200200284Intercostal · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT BS 947 - BS 967, LBL 8. REMOVED DAMAGED INTERCOSTAL PER SRM 51-40-02. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-40-02, SRM 53-60-51 AND EA 53-737-181.SDR F3LA200200283Intercostal · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT BS 947-BS 967, RBL 41. REMOVED INTERCOSTAL PER SRM 51-40-02. FABRICATED AND INSTALLED INTERCOSTAL PER SRM 51-60-02, MM 51-21-99 AND EA 53-737-181.SDR F3LA200200288Floor Support · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT BS 1006 - 1016 RBL32.FABRICATED FLOOR SUPPORT ANDINSTALLED FLOOR SUPPORT BS 1006 - 1016 RBL 32 PER SRM 51-40-02 & SRM 53-60-51.SDR F3LA200200287Floor Support · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION FLOOR SUPPORT BS 986 TO 1006 LT. FABRICATED FLOOR SUPPORT AND INSTALLED AT BS 986-1006 LT PER SRM 53-60-51, SRM 51-40-2 MM 51-21-99 AND EA 53-737-181.SDR F3LA200200286Floor Support · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION CARGO FLOOR SUPPORT BS727C(-4) LBL8. DETERMINED SUPPORT TO BE OUT OF LIMITS PER SRM 53-60-53. FABRICATED PARTS PER SRM 53-00-53 / SOPM 20-41-02. INSTALLED PER 737-300 SRM 51-40-02.SDR F3LA200200285Torque Tube · corrodedDURING C-4 CHECK, INSPECTION REPORTED AFT ENTRY DOOR TORQUE TUBE CORROSION LENGTH OF TUBE. REPLACED TORQUE TUBE ASSEMBLY PER OHM 52-16-01.SDR F3LA200200282Intercostal · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON INTERCOSTAL AT BS 947 - BS 967, LBL 17. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 53-60-51, 51-40-02 AND EA 53-737-181.SDR F3LA200200273Skin · gougedDURING C-4 CHECK, INSPECTION REPORTED RT WING LEADING EDGE AT INBD END OF NR 5 SLAT GOUGED. REPAIRED DAMAGE PER SRM 51-70-17, FIGURE 19.SDR DL733021152Oven · malfunctionedFLT ATTENDANT REPORTED SMOKE/ELECTRICAL SMELL COMING FROM F/C GALLEY OVEN AND CONTROL PANEL. FIRE EXTINGUISHER USED. NO FIRE NOTICED. GALLEY POWER SECURED. ELECTED TO DIVERT TO LBB. REMOVED AND REPLACED OVEN, OP CKS NORMAL.SDR F3LA200200272Door · corrodedDURING C-4 CHECK, INSPECTION REPORTED FWD LAVATORY SERVICE PANEL CORRODED. REPLACED LAVATORY SERVICE DOOR.SDR F3LA200200271Channel · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON RT LAVATORY HAT CHANNEL FOR WALL ATTACH ANGLE, RBL 20. FABRICATED AND INSTALLED HAT SECTION PER BOEING DRAWING 65-73223 AND SRM 51-40-02.SDR F3LA200200270Attach Angle · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON RT. AFT LAV WALL ATTACH ANGLE. FABRICATED AND INSTALLED REPLACEMENT ATTACH ANGLE PER BOEING DRAWING 65-73223 AND SRM 51-40-02.SDR F3LA200200268Attach Angle · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON LT. LAVATORY WALL ATTACH ANGLE, BS 994. REPLACED ATTACH ANGLE PER SRM 51-10-02 AND 51-40-02.SDR F3LA200200267Floor Support · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOOR SUPPORT AT BS 727C (-4), LBL 8, AT NUTPLATE. REMOVED DAMAGED FLOOR SUPPORT CHANNEL. FABRICATED AND INSTALLED REPLACEMENT PARTS PER SRM 53-00-53, 51-40-02, AND SOPM 20-41-02.SDR F3LA200200266Panel · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON TRANSITION PANEL AT BS 787 TO BS 707. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-60-53, SRM 51-40-02 AND SOPM 20-41-02.SDR F3LA200200269Channel · corrodedDURING C-4 CHECK, INSPECTION REPORTED LT. AFT LAVATORY WALL HAT CHANNEL, BS 992, CORRODED BEYOND LIMITS PER SRM 53-60-51. FABRICATED AND INSTALLED REPLACEMENT PARTS PER SRM 51-40-02, 51-4-05 AND SOPM 20-44-04.SDR USAA020372Skin · crackedPIT - FOUND PYLON BONDED SKIN CRACKED 1.687, LEFT ENGINE PYLON STATION 196, PANEL NR 572 LEFT OPENING. REPAIRED PER TYPICAL REPAIR 54-30-07. (M)SDR USAA020369Structure · chafedPIT - FOUND TRAILING EDGE HAS CHAFE, 59 INCHES INBOARD FROM INBOARD END. BURNISHED/BLENDED AND INSTALLED WEAR PAD PER TYPICAL REPAIR 57-50-17. (M)SDR USAA020370Skin · crackedPIT - FOUND SKIN WITH TWO CRACKED .25 INCH LONG, STATION 380 BODYLINE 0 AT RIVET FASTENER. INSTALLED DOUBLER, ROUTED OUT CRACK PER TYPICAL REPAIR 53-30-07 AND EA 74918. (M)SDR USAA020374Frame · corrodedPIT - FOUND FRAME CORRODED, BALANCE ASSEMBLY END FRAME ON RUDDER. CORRODED LEVEL 2. REPLACED DEFECTIVE PART WITH IDENTICAL PART PER OM-26 AND JPC J3-65-27500-005. (M)SDR USAA020371Mount · wornPIT - FOUND ENGINE MOUNT CROSSBEAM WORN LUG, LUG BORE ON ENGINE MOUNT. MACHINE INSIDE DIAMETER OF LUG BORE TO OVERSIZE BEARING PER TYPICAL REPAIR 550-19 REV B. (M)SDR SWAA022252Lens · crackedDURING SCHEDULED BC3 CHECK, FOUND FWD ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.SDR AWXA200200946Former · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1" CRACK WAS FOUND ON R/H WING TO BODY FAIRING FORMER, AFT OF R/H RAM AIR SCOOP, BS 535. MAINTENANCE REMOVED DAMAGED WING TO BODY FAIRING FORMER BS 535; FABRICATED A -2 REPAIR ANGLE; INSTALLED REPAIR PART IAW AWA E.R. 0SDR USAASB02176Handle · lack of lubeIN PREPARATION FOR LANDING, CREW REPORTED THEY RECEIVED THREE GREEN AND THREE RED GEAR LIGHTS UPON GEAR EXTENSION. CREW RECYCLED GEAR WITH SAME SIX LIGHTS ILLUMINATING. GEAR HANDLE WAS THEN PULLED OUT AND PUSHED IN AND THE THREE RED GEAR LIGHTS EXTINGUISHED SDR USAA020414Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH LONG, STATION 616 RIGHT SIDE FRAME LOWER INBOARD END. INSTALLED DOUBLER ANGLE PER TYPICAL REPAIR 53-61-01 AND EA 74856. (M)SDR USAA020365Frame · crackedPIT - FOUND FRAME CRACKED 1 INCH, STATION 616 RIGHT SIDE, FRAME LOWER INBOARD END CABIN FLOOR. INSTALLED DOUBLER ANGLE PER TYPICAL REPAIR 53-61-01 AND EA 74256. (M)SDR USAA020364Skin · delaminatedPIT - FOUND RUDDER DELAMINATED, LEFT SIDE, BOTTOM EDGE 19 INCHES AFT OF LEADING EDGE. RESIN AND OVERLAYED WITH TWO PLIES OF GRAPHITE FABRIC PER EA 74841, SRM 55-40-01, 51-70-17. (M)SDR USAASB02175Csd · failedTPA - FLT 1883 - FLIGHT DEPARTED CLT, EN ROUTE TO SRQ, WITH MEL 49-1 APPLIED TO APU FOR NOT STARTING. DURING DESCENT INTO SRQ, AT 8,000 FEET, THE NR 2 ENGINE GENERATOR TRIPPED AND THE CSD LOW OIL PRESSURE LIGHT ILLUMINATED. CREW DISCONNECTED THE NR 2 CSD ANDSDR USAA020367Skin · crackedRIGHT AILERON, CRACKED 2 LOCATIONS. LOWER SKIN FLANGE AT NR 3 HINGE AND NR 2 HINGE. REMOVED ALL DAMAGE PLUS COMPLETED WET LAYUP REPAIR IAW SRM AND EA.SDR USAASB02172Sensor · out of adjustCLT - FLT 565 - IN PREPARATION FOR LANDING AT CLT, CREW ADVISED THEY DID NOT RECEIVE A NOSE LANDING GEAR GREEN SAFE LIGHT AFTER GEAR EXTENSION. CREW RECYCLED GEAR WITH NO HELP. QUICK REF HANDBOOK PROCEDURES WERE THEN FOLLOWED AND NORMAL GEAR INDICATIONS WERESDR F3LA200200261Frame · crackedDURING C-4 CHECK, INSPECTION REPORTED FRAME CRACKED AT BS 460 BETWEEN STR 26R AND 27R. REPAIRED CRACKED FRAME PER SRM 53-00-07.SDR F3LA200200262Intercostal · damagedDURING C4 CHECK, INSPECTION REPORTED ELONGATED HOLE ON INTERCOSTAL AT BS 500A-500B, STR 26. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-10-02, 51-50-02 AND SOPM 20-41-01.SDR F3LA200200259Floorbeam · corrodedDURING C-4 CHECK, INSPECTION REPORTED VARIOUS STAGES OF CORROSION ON AFT GALLEY/LAVATORY FLOOR BEAMS. REMOVED CORROSION ON FLOOR BEAM AT BS 986.5 PER SRM 53-60-51. CORROSION REMOVAL AT LBL 28 TO LBL 44 WAS OUT OF LIMITS AND REPAIRED PER SRM 53-00-51, FIG. 20SDR USAASB02170Socket · defectiveIND - MAINTENANCE FOUND THE EMERGENCY LIGHT AT THE AFT LEFT ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE REFLECTOR SOCKET ASSEMBLY. OPERATIONAL CHECK GOOD. (M)SDR AWXA200200945Skin · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK 1/16" AND 1/32" CRACKS WERE FOUND ON THE FUSELAGE SKIN AT THE LOWER AFT CUTOUT OF THE R-1 DOOR, BS 326.5 AND BS 327.5. MAINTENANCE CUTOUT 2 EACH CRACKS AT THE LOWER AFT CUTOUT OF THE R-1 DOOR, BS 326.5 AND BS 327.5; FABRISDR AWXA200200922Web · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 2" CRACK WAS FOUND ON WEB AT RIVET HOLE BS 178, WL 234, LBL 9. MAINTENANCE BLENDED OUT DAMAGE AT BS 178, WL 234, LBL 9, AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER AND FILLER, SDR AWXA200200921Web · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 5/8" CRACK WAS FOUND ON WEB AT BS 178, WL 213, RBL 5.7. MAINTENANCE STOP DRILLED CRACK AT BOTH ENDS, AND REPAIRED DAMAGED AREA IAW B 737-300 SRM 53-10-08, PG. 275-279, & 286, FIG. 210.SDR AWXA200200920Web · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 2" CRACK WAS FOUND ON WEB AT RIVET HOLE BS 178, WL 234, RBL 8. MAINTENANCE BLENDED OUT DAMAGE AT BS 178, WL 234, RBL 8, AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER AND FILLER, SDR AWXA200200919Web · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 3/8" CRACK WAS FOUND ON WEB AT BS 178, WL 213, LBL 5.7. MAINTENANCE STOP DRILLED CRACK AT BOTH ENDS, AND REPAIRED DAMAGED AREA IAW B 737-300 SRM 53-10-08, PG. 275-279, & 286, FIG. 210.SDR AWXA200200926Angle · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1" CRACK WAS FOUND ON THE #2 PYLON AFT PANEL ATTACH ANGLE RADIATING FROM THE LOWER AFT NUTPLATE HOLE. MAINTENANCE REMOVED AND REPLACED THE 32 PYLON AFT PANEL ATTACH ANGLE IAW B737-300 SRM 51-40-02, PG. 38, 44-45, & 63, SDR F3LA200200264Intercostal · crackedDURING C-4 CHECK, INSPECTION REPORTED INTERCOSTAL CRACKED AT BS 500B - 500C AT STR 26. FABRICATED AND REPLACED INTERCOSTAL PER SRM 51-10-02, 51-40-02, AND SOPM 20-41-01.SDR F3LA200200263Panel · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION AND PUNCTURE IN TRANSITION PANEL AT BS 500A TO 500D. FABRICATED AND INSTALLED REPLACEMENT PANEL PER SRM 51-40-02 AND SOPM 20-41-01.SDR USAASB02168Battery Pack · dischargedGSO - MAINTENANCE FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT THE LEFT ESCAPE HATCH FLOOR LEVEL, SEAT ROW 10 LEFT SIDE AND THE BULLNOSE LIGHT AT SEAT ROW 15 RIGHT SIDE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR AWXA200200925Doubler · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1 1/8" CRACK WAS FOUND ON FLANGE OF #1 NACELLE ACCESS PANEL 5727L. MAINTENANCE STOP DRILLED HOLES AND PERFORMED A HFEC INSPECTION TO VERIFY CRACKS WERE CONTAINED; REMOVED NECESSARY FASTENERS; FABRICATED A REPAIR DOUBLERSDR USAA020360Skin · crackedCLT - FOUND SKIN CRACKED 2.5 INCHES, BELOW RIGHT LIGHT AFT OF FLAP TO FUSELAGE FAIRING. INSTALLED DOUBLER AND TRIPLER PER EA 86586. (M)SDR AWXA200200957Angle · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 5/16" CRACK WAS FOUND ON R/H RAM AIR SCOOP SUPPORT ANGLE BS 539. MAINTENANCE CUTOUT DAMAGE ON SUPPORT ANGLE AT BS 539, FABRICATED 1 EACH REPAIR AND SPLICE ANGLE, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-11, PG.SDR AWXA200200944Stringer · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON BOTH SIDES OF STRINGER 26 R/H, BS 1006-1012, AFT SIDE OF WASTE SERVICE COMPARTMENT. MAINTENANCE FOUND MATERIAL LOSS OUT OF LIMITS; REMOVED CORRODED STRINGER 26 R/H, BS 1006-1012; FABRICASDR AWXA200200930Stiffener · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1.75 INCH CRACK WAS FOUND ON THE RT WING INTERNAL STRAP AT THE INBOARD SIDE AFT END OF NR 6 FLAP TRACK FAIRING, WS 259 RT. MAINTENANCE REMOVED DOUBLER AND DAMAGED STIFFENER, FABRICATED A NEW DOUBLER AND STIFFENER, AND
Back to Boeing 737-301