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 USAA010836Frame · crackedCLT - FOUND FRAME CRACKED ON VHF ANTENNA .25 INCH AND 2.5 INCH, BS 727D, LBL 1.5 AND RBL 1.5. REMOVED DAMAGE, INSTALLED REPAIR DOUBLER PER SRM 51-70-11. (M)SDR USAA010837Beam · crackedCLT - FOUND BEAM CRACKED .5 INCH, BS 707 TO 711, BBL 0, LOWER ROW OF FASTENERS. INSTALLED REPAIR DOUBLER PER EA 69679 AND SB 737-57-1210 FIG 5. (M)SDR USAA010838Web · crackedCLT - FOUND WEB CRACKED INTERIOR CABIN 1 INCH, BS 947.8, AFT ENTRY DOOR, UPPER HINGE CUTOUT. INSTALLED RE-INFORCING STRAP PER EA 69847. (M)SDR USAA010839Frame · crackedCLT - FOUND FRAME STIFFENER CRACKED .5 INCH, RESULTING IN MISSING MATERIAL, BS 360, LEFT SIDE OF A/C AT FRAME, WL 215. INSTALLED STRAP AND FILLER PER EA 85025. (M)SDR USAA010840Bear Strap · gougedCLT - FOUND SKIN/BARE STRAP GOUGED AND DEFORMATION, 1 INCH BY 2.9 INCHES, BS 440, LOWER FORWARD CORNER OF CARGO DOOR CUTOUT. INSTALLED DOUBLER AND TRIPLER PER EA 69856. (M)SDR USAA010841Fitting · gougedCLT - FOUND BULKHEAD FITTING .75 INCH GOUGE, NACELLE STATION 254.525, NR 2 PYLON. BLENDOUT AND ROTO-PEEN. (M)SDR USAA010842FrameCLT - FOUND FRAME WITH TWO HOLES .1875 INCH, BS 500A, RIGHT SIDE TRANSITION ANGLE, FORWARD CARGO HOLD. DAMAGE REMOVED, INSTALLED FRAME SPLICE PER EA 85041. (M)SDR USAA010843Frame · dentedCLT - FOUND FRAME DENTED 1 INCH DIAMETER, BS 1064, 2 INCHES OUTBOARD OF STRINGER 2R. DAMAGED REMOVED, INSTALLED DOUBLER PER EA 69827. (M)SDR USAA010844FrameCLT - FOUND FRAME WITH HOLE .375 INCH, BS 807, AT TIE CLIP FOR STRINGER 27R. INSTALLED DOUBLER PER SRM 51-70-11. (M)SDR USAA010845Floorbeam · damagedCLT - FOUND FLOORBEAM WITH ELONGATED CLIPNUT HOLES .125 INCH AND .25 INCH, BS 328, LBL 28. INSTALLED REPAIR ANGLES PER SRM 53-10-51, FIG 206. (M)SDR USAA010846Skin · gougedCLT - FOUND FUSELAGE SKIN DENTED WITH GOUGE 2 INCHES IN DIAMETER, BS 500B BETWEEN STRINGERS 25 AND 26R. DAMAGE REMOVED, INSTALLED REPAIR PER SRM 53-00-01, FIG 210. (M)SDR USAA010847SkinCLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY INSTALLED DOUBLER 41 INCHES BY 23 INCHES, BS 380, STRINGER 26 TO 27R. INSTALLED NEW DOUBLER PER EO 5300V258 AND TR 53-30-07. (M)SDR USAA010869Skin · crackedTPA - FOUND DOOR EXTERIOR SKIN CRACKED .25 INCH, AFT ENTRY DOOR, UPPER HINGE CUTOUT. INSTALLED DOUBLER PER SRM 52-10-01 AND SERVICE BULLETIN 737-52-1096. (M)SDR USAA010870Skin · crackedTPA - FOUND DOOR EXTERIOR SKIN CRACKED .25 INCH, FORWARD SERVICE DOOR, LOWER HINGE CUTOUT. INSTALLED REPAIR DOUBLER PER SRM 52-10-01 PAGE 201 AND SB 737-52-1096. (M)SDR USAASB01198Socket · corrodedEWR - MAINTENANCE FOUND THE FORWARD MAIN ENTRY DOOR EXTERIOR EMERGENCY EVACUATION LIGHT INOPERATIVE. MAINTENANCE CLEANED CORROSION FROM THE LIGHT SOCKET. OPERATIONAL CHECK GOOD. (M)SDR USAASB01199Light · inoperativeEWR - FOUND AFT GALLEY DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M)SDR USAASB01190Battery Pack · dischargedPIT - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT ROWS 9 AND 11 THROUGH 16 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)SDR USAA010801Skin · crackedPIT - FOUND SKIN CRACKED 1.125 INCH, RIGHT SIDE STATION 727E STRINGER 24 RIGHT. CUT OUT DAMAGE, INSTALLED EXT DOUBLER PER SRM 53-00-01 FIG 201. (M)SDR USAASB01185Circuit Breaker · faultyEWR - FLT 432 - IN PREPARATION FOR LANDING AT EWR, FROM PIT, CREW RECEIVED A RED NOSE GEAR UNSAFE LIGHT WITHOUT ANY GEAR INDICATIONS. CREW CHECKED CIRCUIT BREAKERS AND ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES. CREW RECYCLED GEAR BUT STILL ONLY THE RED NOSESDR USAASB01184Battery Pack · dischargedGSO - MAINTENANCE FOUND THE EMERGENCY LIGHTS ON THE SEATS IN AFT CABIN DIM. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)SDR DL733011064Light · inoperativeFOUND DURING SVC CK - EMERGENCY AISLE ILLUMINATION LIGHT LOCATED 2 INCHES BELOW LATCH FOR OVERHEAD BIN 17/18FED INOP. REBULBED, OPN NORMAL.SDR DL733011063Light · inoperativeFOUND DURING SVC CK - IN-SEAT ESCAPE PATH LIGHT AT SEAT ROW 10FED INOP. REBULBED, NO HELP. REPLACED LIGHT ASSY, OPS NORMAL.SDR USAASB01177Light · inoperativeBWI - MAINTENANCE FOUND THE FLOOR LEVEL OVERWING EMERGENCY EXIT LIGHT BROKEN/INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)SDR USAASB01175Fuel Cell · leakingCLT - FLT 1290 - AFTER TAKEOFF, FUEL WAS REPORTED STREAMING OUT OF THE LEFT WING BY AN AMERICAN FLIGHT BEHIND AND WAS ALSO CONFIRMED BY THE CLT TOWER. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO FIELD AT CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. SDR USAA010804Frame · crackedPIT - FOUND FRAME CRACKED 2 INCHES, FS 663.75 AT ST-1C1-26-3R-2R AND 3L. REPAIRED PER EA 71500 AND SRM 53-00-07. (M)SDR USAA010743Skin · crackedPIT - FOUND SKIN CRACKED 5 INCHES BY 7 INCHES, FRAME STATION 580, S5L. REPAIR PCW, 5 INCHES BY 7 INCH DOUBLER INSTALLED PER SRM 53-00-01 FIG 202. (M)SDR USAA010744Skin · crackedPIT - FOUND SKIN CRACKED 6 INCHES BY 7 INCHES, FRAME STATION 556, STRINGER 5L. REPAIRED PCW, 6 INCHES BY 7 INCH DOUBLER INSTALLED PER SRM 53-00-01 FIG 202. (M)SDR USAA010745Skin · crackedPIT - FOUND SKIN CRACKED 8 INCHES BY 6 INCH AREA, BETWEEN FRAME STATION 500C AND 500D, S5L, 6 INCHES AFT 500C. REPAIR PCW, 8 INCHES BY 6 INCH DOUBLER INSTALLED PER SRM 53-00-01 FIG 201. (M)SDR USAA010746Skin · crackedPIT - FOUND SKIN CRACKED 4.75 INCHES BY 4.75 INCH AREA, BETWEEN FRAME 500B AND 500C, S5L, 4 INCHES AFT OF 500C. REPAIRED PCW, 4.75 INCHES CIRCULAR DOUBLER INSTALLED PER SRM 53-00-01 FIG 208. (M)SDR USAA010741Skin · delaminatedPIT - FOUND RUDDER DELAMINATION .75 INCH BY .375 INCH AREA, FORWARD LOWER SKIN CORNER. REPAIRED PER EA 71466 PER SRM 5160-07, 51-70-17 FIG 18 OF BOEING MM. (M)SDR USAA010625Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED APPROX .25 INCH, BS 379, BELLY, E/E COOLING OUTLET. INSTALLED DOUBLER PER TYPICAL REPAIR 53-30-07. (M)SDR USAA010624Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED 1.5 INCH, BS 727D, STRINGER 23L. DAMAGE REMOVED, DOUBLER INSTALLED PER TYPICAL REPAIR 53-60-03. (M)SDR USAASB01159Battery Pack · overheatedCLT - FLT 461 - PILOT REPORTED THAT THE AIRCRAFT ARRIVED AT THE GATE WITH AN ELECTRICAL/BURNING ODOR IN THE CABIN. MAINTENANCE FOUND TWO FORWARD EMERGENCY LIGHT BATTERY PACKS EXCESSIVELY HOT/OVERHEATED. REMOVED AND REPLACED BOTH UNITS. RAN ENGINES AND PACKSSDR 2001F00022Hydraulic Line · chafedDCA - FLT 2299 - AFTER TAKEOFF FROM \, AS CREW RETRACTED THE LANDING GEAR, THEY RECEIVED A RED LIGHT FOR THE RT MLG. SHORTLY AFTER, THEY RECEIVED A RED LIGHT FOR THE 'A' SYSTEM HYDRAULIC. CREW CONTINUED THEIR CLIMB TO FL190 AND THEN PERFORMED PROCEDURES FOR SDR USAASB01156Hydraulic Line · leakingDCA - FLT 2299 - AFTER T/O , AS THE LANDING GEAR RETRACTED, RECEIVED A RED LIGHT FOR THE RT MLG. THEN RECEIVED A RED LIGHT FOR THE A SYS HYDRAULIC. CONTINUED TO CLIMB TO FL190 THEN PERFORMED PROCEDURES FOR A SYS HYDRAULIC FAILURE. DECLARED AN EMERGENCY AND RETSDR DL733010886Skin · corrodedTHE FUSELAGE SKIN WAS FOUND CORRODED AT FS 525 AND STRINGER 28R ADJACENT TO THE GROUND AC ACCESS DOOR. THE CORROSION WAS REMOVED WITH A 5 X 2.2 CUTOUT. THE DAMAGE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PERER/A 380935-14, REV A.SDR USAA010582Skin · corrodedPIT - FOUND SKIN CORRODED 1 INCH BY 2 INCHES, STATION 969 BETWEEN RIGHT STRINGER 27 AND 28. INSTALLED DOUBLER PER EA NR 70922. CORROSION LEVEL 1, TASK NR C53-208-01. (M)SDR USAA010583Stringer · corrodedPIT - FOUND STRINGER CORRODED 1 INCH BY .500 INCH, STRINGER 28 AT STATION 948. CORROSION LEVEL 1, TASK NR C53-208-01. INSTALLED REPAIR SPLICES PER SRM 53-00-01 FIG 201. (M)SDR USAA010584Stringer · corrodedPIT - FOUND STRINGER CORRODED 1 INCH BY .500 INCH, STRINGER 28 AT STATION 948. CORROSION LEVEL 1 TASK NR C53-208-01. INSTALLED REPAIR SPLICES PER SRM 53-00-01 FIG 201. (M)SDR USAA010585Skin · corrodedPIT - FOUND SKIN CORRODED 1 INCH BY 2 INCHES, STATION 969 BETWEEN RIGHT STRINGER 27 AND 28. CORROSION LEVEL 1, TASK NR C53-208-01. INSTALLED DOUBLER PER EA NR 70922. (M)SDR USAASB01138Charger · failedCLE - MAINTENANCE FOUND THE EMERGENCY LIGHTS IN NR 2 AND NR 3 BULL NOSE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD. (M)SDR USAASB01127Flap · malfunctionedROC - FLT 582 - ON DESCENT INTO ROC FROM LGA, AT APPROXIMATELY 3,000 FEET, THE FLAP POSITION INDICATOR SHOWED A FLAP DISAGREEMENT AND THE TRAILING EDGE FLAP INDICATOR CIRCUIT BREAKER WAS POPPED. CREW ACCOMPLISHED A ZERO FLAPS LANDING AT ROC WHERE THE FLIGHT LSDR USAASB01125Servo · failedCLT - FLT 1549 - ON CLIMB-OUT FROM CLT, EN ROUTE TO DFW, CREW RECEIVED A STABILIZER OUT OF TRIM LIGHT THAT WOULD FLICKER OFF AND ON. AT APPROXIMATELY FL270, THE AUTOPILOT BEGAN TO GIVE THE AIRCRAFT INCORRECT TRIM INPUTS AND THE AIRCRAFT WOULD START TO NOSE OVSDR USAASB01124Uplock Sensor · faultyIAH - FLT 1620 - AFTER TAKEOFF FROM IAH, WHEN THE LANDING GEAR WAS RAISED, CREW RECEIVED TWO GREEN LIGHTS AND A LEFT MLG RED LIGHT. AN UNUSUAL RUMBLE WAS ALSO NOTICED WHILE GEAR WAS BEING RETRACTED. CREW RECYCLED GEAR AND GOT THREE GREEN LIGHTS WHEN GEAR WAS SDR USAASB01121Outflow Valve · malfunctionedPIT - FLT 1107 - EN ROUTE FROM YYZ TO CLT, AT FL350, THE CABIN ALTITUDE ALERT SOUNDED AS CABIN WAS AT 10,000 FEET AND CLIMBING AT APPROXIMATELY 600 FEET PER MINUTES. CREW INITIATED DESCENT TO FL115 AND COMPLIED WITH QUICK REFERENCE HANDBOOK PROCEDURES BUT OUTSDR USAASB01119Battery Pack · dischargedPIT - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 20 AND 22 AND ABOVE THE L2 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT AFT RIGHT SIDE CEILING PANEL. OPS CHECK GOOD. (M)SDR USAA010470Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .5 INCH B.25 INCH, BS 1006, LBL 10. REPLACED T-CAP SECTION PER EA 69149A. (M)SDR USAASB01116Charger · failedPHL - MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHTS AT ROWS 1 THROUGH 4 INOPERATIVE AND THE EMERGENCY LIGHTS AT THE FORWARD ENTRY AND SERVICE DOORS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK (P/N 2013-1A) AND CHAGER ASSEMBLY AT STATION SDR USAASB01115Fuse · blownTPA - MAINTENANCE FOUND THE FORWARD EMERGENCY EGRESS LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TWO 5 AMPS FUSES. OPS CHECK GOOD. (M)SDR USAASB01114Light · inoperativeTPA - MAINTENANCE FOUND SEAT 5C EMERGENCY SEAT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED SPLICE. OPS CHECK GOOD. (M)
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