Boeing 737-3B7
Service difficulty reports · 4,722
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 = '7373B7' 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 = '7373B7' 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 USAASB02154Panel · illuminatedDURING CRUISE, ENROUTE, THE NR1 ENGINE DRIVEN HYDRAULIC PUMP (A) SYSTEM LOW PRESSURE LIGHT ILLUMINATED. FIVE MINUTES LATER, THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP (B) SYSTEM LOW PRESSURE LIGHT ILLUMINATED. HYDRAULIC SYSTEM QUANTITY WAS OK AND HYDRAULIC SYSTEMSDR USAA020334Fitting · crackedPIT - FOUND FITTING CRACKED .5 INCH, LEFT WING AT FASTENER HOLE MLG BEAM SUPPORT FITTING. FITTING REPLACED, MODIFIED PART INSTALLED PER EA 74450 AND EA 74371. (M)SDR AWXA200200856Attach Angle · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK 2 EACH CRACKS WERE FOUND ON ATTACH ANGLES OF #1 PYLON, JUST AFT OF LOWER HEATSHIELD BLANKET. MAINTENANCE REMOVED CRACKED ATTACH ANGLES JUST AFT OF LOWER HEATSHIELD BLANKET, FABRICATED 2 EACH REPLACEMENT ATTACH ANGLES, ANSDR USAA020327Skin · crackedPIT - FOUND SKIN CRACKED 3.5 INCH, S25R BETWEEN STATION 727E AND 747. INSTALLED DOUBLER PER SRM 53-00-01 FIG 2. (M)SDR USAA020326Skin · damagedPIT - FOUND RUDDER WITH SKIN DAMAGE, STATION 7.60, 17.70. REPAIRED PER SRM 51-70-17, 55-40-01. (M)SDR AWXA200200861Angle · corrodedMCN - MAJOR REPAIR - DURING C-16 CHECK CORROSION WAS FOUND ON THE LOWER TEE CHORD REPAIR SPLICE ANGLE AT BS 344 FORWARD SIDE, LBL 53, WL 207.5. MATERIAL LOSS OUT OF LIMITS PRIOR TO BLEND. MAINTENANCE REMOVED EXTRUDED ANGLE, WEB PANEL AND DAMAGED SPLICE ANGLESDR AWXA200200833Strap · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK A 1.25 INCH CRACK WAS FOUND ON LOWER FRAME TO FRAME STRAP BS 312, RBL 26. MAINTENANCE FABRICATED A REPAIR DOUBLER, AND INSTALLED REPAIR TO LOWER FRAME TO FRAME STRAP BS 312, RBL 26 IAW B737-300 SRM 53-10-51 PG 213-219 FISDR AWXA200200862Web · corrodedMCN - MAJOR REPAIR - DURING C-16 CHECK CORROSION WAS FOUND ON THE LOWER SURFACE OF HORIZONTAL WEB AT BS 988, RBL 45, WL 208 (AFT OF 986.5 FLOORBEAM AND INBOARD OF CREASE BEAM). MAINTENANCE REMOVED DAMAGED WEB, FABRICATED A NEW WEB, AND INSTALLED REPAIR IAW DWSDR AWXA200200830Channel · corrodedMCN - MAJOR REPAIR - DURING C-16 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF L-1 ENTRY WAY CHANNEL (LOWER SCUFF PLATE ATTACHMENT INBOARD SIDE) BS 312 - 344, LBL 61. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS PER B737-300 SRM 53-10-15SDR AWXA200200793Floor Support · corrodedMCN - MAJOR REPAIR - DURING C-16 CHECK CORROSION WAS FOUND ON THE UPPER SURFACE OF RT AFT LAV FLOOR SUPPORT BS 992, RBL 29.5, WL 208. MAINTENANCE CLEANED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; REMOVED FLOOR SUPPORT BS 992, RBL 29.5. FABRICATED A NESDR AWXA200200792Floor Support · corrodedMCN - MAJOR REPAIR - DURING C-16 CHECK CORROSION WAS FOUND ON THE UPPER SURFACE OF THE OUTBOARD FORWARD RT AFT LAV FLOOR SUPPORT BS 991, RBL 32, WL 208. MAINTENANCE CLEANED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS; REMOVED FLOOR SUPPORT BS 991, RBL 32.SDR AWXA200200855Frame · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK A 3/4" CRACK WAS FOUND ON AFT CARGO DOOR FORWARD LOWER FRAME BETWEEN THE 1ST AND 2ND STOP FITTINGS, BS 802, RBL 42. MAINTENANCE REMOVED AFT CARGO DOOR FORWARD LOWER FRAME, FABRICATED A NEW SECTION OF FRAME, AND INSTALLEDSDR USAA020356Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, STATION 867 AT S8L-S9L. INSTALLED DOUBLER PER TYPICAL REP 53-10-14A. (M)SDR USA2002F00078Warning Light · false indicationTHE NR 1 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. CAPTAIN FELT THE AIRCRAFT YAW, SO HE SHUT DOWN THE NR 1 ENGINE. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. TOTAL SINGLE ENGINE TIME WAS 20 MINUTESDR USA2002F00074Handle · lack of lubeON APPROACH, CREW RECEIVED A GEAR INDICATION OF 3 RED UNSAFE LIGHTS ALONG WITH 3 GREEN DOWN AND LOCKED LIGHTS WHEN FLAPS 30 WAS SELECTED. THE (TOO LOW, GEAR) WARNING SOUNDED SEVERAL TIMES UNTIL AFTER THE GEAR WAS RETRACTED DURING GO AROUND. CREW ACCOMPLISHEDSDR USAA020329Skin · crackedPIT - FOUND SKIN CRACKED 2.1 INCH, STATION 727E ABOVE STRINGER 24L IN AFT FUSELAGE SKIN. CRACKED AREA CUT OUT AND DOUBLER INSTALLED PER SRM 53-00-01 FIG 202. (M)SDR USAA020320Channel · crackedPIT - FOUND CHANNEL CRACKED 1 INCH, STATION 228, LBL 12 INCHES BELOW FLOOR. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M)SDR USAA020323Intercostal · crackedPIT - FOUND INTERCOSTAL CRACKED 1 INCH, STATION 344 BELOW FLOOR LBL 45 INCHES. REPLACED ASSEMBLY WITH IDENT PART NR PER SRM 51-10-02. (M)SDR USAA020317Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, FRAME ATTACH BRACKET HOLE AT STATION 887-S9L. MANUFACTURED REPAIR IAW TYPICAL REPAIR 53-10-14A. (M)SDR USAA020318Channel · crackedPIT - FOUND CHANNEL CRACKED .25 INCH, STATION 223 136-0 BELOW FLOOR. REPLACED ASSEMBLY WITH IDENT PART PER SRM 51-10-02. (M)SDR USAA020319Intercostal · crackedPIT - FOUND INTERCOSTAL CRACKED .25 INCH, STATION 340 BOTTOM OF VERTICL L. MANUFACTURED FROM BOEING DRAWING NR 65-45912-46. (M)SDR USAA020321Floor Support · crackedPIT - FOUND L-SUPPORT CRACKED .5 INCH, STATION 328 LBL 47 FLOORBEAM VERTICAL L. MANUFACTURED AND HEAT TREATED FROM PERFORMED STOCK PER SRM 51-10-02 AND 20-30-06. (M)SDR USAA020322Channel · crackedPIT - FOUND CHANNEL CRACKED .5 INCH, BELOW FLOOR STATION 328 LBL 4 INCHES. REPLACED ASSEMBLY PER SRM 51-10-02. (M)SDR USAA020316Tie Clip · crackedPIT - FOUND TIE CLIP CRACKED .125 INCH, STATION 908 S-4R. MANUFACTURED AND REPAIRED SPLICE PER DWG 65-45772 AND SRM 51-10-02. (M)SDR USAA020309Stringer · corrodedPIT - FOUND STRINGER CORRODED ON ENDS OF STRINGER STATION 323.7 AND BL 0 TO S28R. (M)SDR USAA020297Door Frame · crackedPIT - FOUND FRAME CRACKED TWO PLACES 1 INCH EACH, UPPER FORWARD CORNER OF INTERIOR DOOR STOP FRAME. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M)SDR USAA020298Door Frame · crackedPIT - FOUND FRAME CRACKED TWO PLACES 1 INCH EACH, UPPER AFT CORNER OF INTERIOR DOOR STOP FRAME. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M)SDR USAA020293Attach Angle · crackedPIT - FOUND ANGLE CRACKED .75 INCH, INT ATTACH ANGLE FORWARD STATION 291.5, S12R AND S13R. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-2. (M)SDR USAA020294Angle · crackedPIT - FOUND ANGLE CRACKED .5 INCH, INT ATTACH ANGLE FORWARD OF STATION 291.5, S11R AND S12R. DEFECTIVE PART REPLACED WITH IDENT PART NR PER BOEING DWG 65-45807-31. (M)SDR USAA020296Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, INT DOOR FRAME ON FUSELAGE AT FORWARD UPPER CORNER. FABRICATED NEW ANGLE PER EA. (M)SDR USAA020299Stringer · crackedPIT - FOUND STRINGER CRACKED .125 INCH, AT RIVET STATION 927 AT STRINGER 8R AND 9R. REMOVED CRACK AND INSTALLED OVERSIZED FASTENER PER 51-40-05. (M)SDR USAA020311Clip · corrodedPIT - FOUND CORROSION ON CLIP 1 INCH BY 4 INCH, AT STATION 500D S28L-S28R. CORROSION LEVEL 1. CORROSION REMOVED, TREATED, PRIMED PER SRM 53-00-07, 51-10-02, 51-20-01. (M)SDR USAA020300Stringer · crackedPIT - FOUND STRINGER CRACKED .25 INCH, STATION 907, STRINGER 8L-9L AT RIVET. REMOVED CRACKED AND INSTALLED A REPAIR ANGLE PER TYPICAL REPAIR 53-10-14A. (M)SDR USA2002F00072Module · faultyON DESCENT, THE FIRE WARNING ANNUNCIATOR ON THE GLARESHIELD ILLUMINATED. CREW COULD NOT CANCEL THE LIGHT. NO OTHER INDICATIONS OF FIRE WAS NOTED. FIRE DETECTION TESTS NORMAL OTHERWISE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACSDR USA2002F00076Light · failedPILOT REPORTED THE EMERGENCY LIGHTS AT SEAT ROW 10ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK NORMAL.SDR USAASB02144Battery Pack · inoperativeSYR - MAINTENANCE FOUND THE EVACUATION LIGHTS BY THE FORWARD ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR USAASB02142Wire · brokenSYR - MAINTENANCE FOUND THE EMERGENCY EVACUATION LIGHTS AT SEAT ROWS 8, 9 AND 10L LEFT SIDE, INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. OPERATIONAL CHECK OF EVACUATION LIGHTS GOOD. (M)SDR USAASB02141Charger · inoperativeIND - MAINTENANCE FOUND THE AFT LEFT ESCAPE SLIDE EMERGENCY LIGHT AT THE AFT RIGHT SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M1197 BATTERY CHARGER ASSEMBLY AT STATION 960L. OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD.SDR USA2002F00075Outflow Valve · leakingON CLIMB OUT, ENROUTE, CABIN ALT WARNING HORN SOUNDED. CREW REPORTED OUTFLOW VALVE WAS FULLY CLOSED IN AUTO, STANDBY, AND MANUAL PRESS MODES BUT THEY WERE NEVER ABLE TO GET CABIN PRESS. EMER DESCENT WAS ACCOMPLISHED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. SDR USAASB02140Wire · disconnectedORD - MAINTENANCE FOUND THE EMERGENCY EXIT AISLE LIGHT AT SEAT 6C INOPERATIVE. MAINTENANCE RESPLICED THE WIRE CONNECTION AT THE INBOARD ARMREST ASSEMBLY AT SEAT 6C. OPERATIONAL CHECK GOOD. (M)SDR USAA020339Skin · crackedCLT - FOUND SKIN CRACKED .4375 INCH STATION 380 STRINGER 00 BOTTOM FUSELAGE CENTER LINE. INSTALLED DOUBLER PER TR 53-30-07. (M)SDR USAA020284Skin · delaminatedPIT - FOUND LOWER SURFACE DELAMINATED 5 INCHES BY 5 INCHES, 74.5 INCHES FROM INBOARD END AND 10.5 INCHES FROM LEADING EDGE. REPAIRED PER SRM 55-20-01, 51-70-17 AND EA 74407. (M)SDR USAA020312Frame · corrodedPIT - FOUND FRAME CORRODED 4 INCHES BY 8 INCHES, STATION 500C BETWEEN STRINGER 28R AND 29L FORWARD SIDE OF FRAME. CORROSION REMOVED, TREATED, PRIMED, PAINTED PER SRM 51-20-04, 51-10-02. (M)SDR USA2002F00071Circuit Breaker · trippedON DESCENT, CREW DID NOT RECEIVE THREE GREEN LANDING GEAR LIGHTS WHEN LOWERING THE LANDING GEAR. CREW ACCOMPLISHED GO-AROUND, AND WHILE PERFORMING CHECKLIST, THEY FOUND THE SECTION 5 CIRCUIT BREAKER POPPED. CREW RESET CIRCUIT BREAKER AND RECEIVED NORMAL GEARSDR USAA020314Floor Support · corrodedPIT - FOUND FLOOR SUPPORT CORRODED 2 INCHES BY 6 INCHES, STATION 967-986 RBL 19 TOP BOTTOM. REMOVED FLOOR SUPPORT WITH IDENT PART NR PER SRM 51-40-02. (M)SDR USAA020315Attach Angle · crackedPIT - FOUND ATTACH ANGLE CRACKED 6 INCHES IN RADIUS, RIGHT THRUST BEAM UPPER INBOARD ATTACH ANGLE. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)SDR USAA020301Keelbeam · corrodedPIT - FOUND KEEL BEAM CORRODED, 3-4 INCHES, EXFOLIATION THROUGH BEAM S-28R AT STATION 540. CORROSION LEVEL 2, TASK NR C53-208-01. REPLACED KEEL BEAM SECTION PER EA 74111. (M)SDR USAA020291Intercostal · corrodedPIT - FOUND INTERCOSTAL/ANGLE CORRODED 1 INCH BY 1 INCH AND .5 INCH BY .33 INCH, STATION 219.8 BELOW CAPTAIN NR 2 WINDOW. REMOVED CORROSION FROM INTERCOSTAL AND RIB ANGLE PER BOEING DWG 65-16305. (M)SDR DL733020861Skin · gougedTHE BONDED SKIN AND UNDERLYING BEARSTRAP WERE FOUND DENTED AND GOUGED AT THE FWD EDGE OF THE C1 CARGO DOOR OPENING AT FS 440 NEAR STRINGER 23R. THE DAMAGE WAS REMOVED IN ALL LAYERS. THE CUTOUT WAS REPAIRED WITH 3 EXTERNAL DOUBLERS PER ER/A 383504-14, REV A.SDR USAA020285Skin · crackedPIT - FOUND SKIN CRACKED 3 INCHES, LOWER AFT CORNER OF FORWARD SERVICE DOOR CUT OUT AT BS 328. INSTALLED DOUBLERS PER SRM 53-10-01. (M)
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