Boeing 737-4B7
Service difficulty reports · 5,757
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 = '7374B7' 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 = '7374B7' 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 USAA070345Support · crackedSTA 727D + 12 INCHES AT RBL 2, ANTENNA BRACKET SUPPORT MOUNT CRACKED. DRILLED & INSTALLED NEW PART PER SRM 51-10-02, DEFECT SIZE: 1 INCH.SDR USAA070354Tie Clip · crackedSTA 807 STR 4, STRINGER TIE CLIP CRACKED. REPLACED TIE CLIP PER SRM 51-10-02, DEFECT SIZE: .5 INCH.SDR USAA070343Frame · crackedSTUB FRAME ATTACH POINT BS 616 & LBL 64 CRACKED. INSTALLED REPAIR ANGLE PER TYP REP 53-62-05, DEFECT SIZE: .250 INCH.SDR USAA070341Frame · crackedSTA 500C BETWEEN STR 8 & 9, RT AT ATTACH BRACKET AT INBD RIVET HOLE. INSTALLED REPAIR ANGLES PER TR 53-10-20E. DEFECT SIZE: 1/4"SDR USAA070340Frame · crackedSTA 480 BETWEEN STR 8 & 9 RT AT ATTACH BRACKET ON FRAME, INBD RIVET. INSTALLED REPAIR ANGLES PER TR 53-10-20E. DEFECT SIZE: 1/4"SDR USAA070339Floor Support · crackedBETWEEN BL0 TO LBL -24 AT STA 540. REMOVED & REPLACED SUPPORT ANGLE PER SRM 51-10-02. DEFECT SIZE: 1"SDR USAA070344Mount · crackedSTA 727D+12 AT RBL 2, ANTENNA MOUNT Z SUPPORT. DRILLED & INSTALLED NEW PART PER SRM 51-10-02. DEFECT SIZE: 1 INCHSDR USAA200705002Skin · cracked2" CRACK FOUND AT RT HORIZ STAB LOWER SKIN CENTER OF 3" PANEL. (CLT) INSTALLED TEMPORARY DOUBLER PER TR 55-10-07 REV B.SDR USAA200705001Skin · cracked1" CRACK FOUND AT STA 727D STR 23L ON SKIN. (CLT) INSTALLED DOUBLER PER TR 53-60-03ASDR SB07035Iru · failedMCO FLT 1672 - CLIMBING THROUGH 3,000 FEET OUT OF MCO, EN ROUTE TO BWI, CREW REPORTED BOTH ADI'S AND HSI'S FAILED. FLIGHT RETURNED TO FIELD AT MCO AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 2 IRU.SDR USAA200704004Skin · cracked1.5" CRACK FOUND AT L2 DOOR LOWER HINGE CUT OUT. INSTALLED DOUBLER/TRIPLER PER EA 84451.SDR SB07030Battery Pack · dischargedCLT - MAINTENANCE FOUND THE FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT POWER SUPPLY M01132. OPERATIONAL CHECK GOOD.SDR SB07029Module · faultyIAD FLT1724, ON DESCENT, CREW REPORTED THERE WAS NO INDICATION OF GEAR EXTENSION (RED OR GREEN LIGHTS) WHEN LANDING GEAR HANDLE WAS PUT IN THE DOWN POSITION. CREW PERFORMED QUICK REFERENCE HANDBOOK PROCEDURES AND EXTENDED THE GEAR MANUALLY. STILL NO LIGHTS. FLSDR SB07028Charger · inoperativeDCA - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 24 AND 25 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD.SDR USAA200704002Skin · cracked1.25 INCH CRACK FOUND ON SKIN AT STA 944 AND S-24L. REPAIR: INSTALLED DOUBLER IAW EA 98606.SDR USAA200704003Skin · cracked2.5 INCH CRACK FOUND AT LOWER SKIN AT STAB ST. 98-100 (TE). INSTALLED DOUBLER IAW EA 98607 AND TR 55-10-07B.SDR USAA200704001Skin · crackedA 3 INCH CRACK FOUND ON SKIN, RIGHT SIDE AT STA 727E + 3 INCHES. REMOVED DAMAGED AREA & INSTALLED REPAIR DOUBLER PER SRM 53-00-01 REP 31.SDR SB07024Battery Pack · dischargedBDL - MAINTENANCE REPORTED THE FORWARD LEFT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD.SDR USAA200703005Skin · crackedA .75 INCH CRACK FOUND AT LEFT PYLON AT ACCESS PANEL 5727L OPENING. STOP DRILLED & INSTALLED DOUBLER PER TYPICAL REPAIR 54-30-07.SDR USAA070227Frame · crackedBS 492 S-24R HAS CRACK. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER EA 98545, DEFECT SIZE: .5 INCH.SDR USAA070228Skin · puncturedRIGHT AILERON, UPPER SURFACE, 10.5 INCHES INBOARD OF OUTBOARD EDGE PUNCTURED. REMOVED DAMAGE, LAYED UP PLIES PER EA 98560, DEFECT SIZE: .5 INCH.SDR USAA070222Frame · crackedSTA 440 STR 24R O/B RADIUS OF FRAME CRACKED. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER EA 98545, DEFECT SIZE: 1 INCH.SDR USAA200703001Skin · crackedA 2.25 INCH CRACK FOUND AT LT HORIZONTAL STAB LWR SKIN STA 115. INSTALLED DOUBLER PER SRM 55-10-01.SDR SB07019Battery Pack · dischargedPHL MAINTENANCE REPORTED THE FORWARD SERVICE DOOR LOWER EMERGENCY EXIT SIGN ALONG WITH THE ONE ABOVE THE DOOR WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD.SDR SB07018Battery Pack · dischargedPIT MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT FOR THE LEFT FORWARD OVERWING EMERGENCY ESCAPE DOOR, BETWEEN SEAT ROWS 10 AND 11, WAS INOPERATIVE. MAINTENANCE CHARGED THE EMERGENCY EXIT LIGHTS. OPERATIONAL CHECK GOOD.SDR USAA200702001Rib · crackedCRACK FOUND AT RIB 135.5 SKIN CLIP CRACKED BETWEEN STR 2 & 3. REPAIRED PER EA 84116.SDR SB07017Battery Pack · dischargedDCA - MAINTENANCE REPORTED THE EMERGENCY EXIT SIGN AT THE FORWARD ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK PER MM 33-51-00. OPERATIONAL CHECK GOOD.SDR SB07016Flap · out of rigCLT FLT750 ON DESCENT INTO CLT FROM GCM, WHEN FLAPS WERE SELECTED TO 30 UNITS, THE AIRCRAFT ROLLS TO THE LEFT. WINGS CAN BE KEPT LEVEL WITH 3 DEGREES OF RIGHT AILERON. FUEL WAS BALANCED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE CABLE DSDR USAA070108Door Frame · crackedFWD CARGO DOOR, AFT FUSELAGE FRAME, O/B OF UPPER I/B STOP BOLT HOLE CRACKED. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER EA 98497, DEFECT SIZE: .075 INCH.SDR USAA070109Door Frame · crackedSTA 440 S-21R CARGO DOOR FUSELAGE FRAME, UPPER I/B STOP BOLT HOLE CRACKED. REMOVED DAMAGE & INSTALLED PARTS PER EA 98496, DEFECT SIZE: .5 INCHES.SDR USAA070110Door Frame · crackedRADIATING FROM UPPER I/B STOP BOLT HOLE, STA 492.4, S-24R, FWD CARGO DOOR CRACKED. INSTALLED DOUBLER PER EA 98497, DEFECT SIZE: .5 INCHES.SDR USAA070111Door Frame · damagedRADIATING FROM LOWER O/B STOP BOLT HOLE, STA 492.4, S24R, FWD CARGO DOOR DAMAGE. INSTALLED DOUBLER PER EA 98497, DEFECT SIZE: .375 INCH.SDR USAA070105Frame · crackedBS 440 S-24R WL 160 CRACKED. TRIMMED OUT CRACK, HEAT TREATED, INSTALLED REPAIR DOUBLERS PER EA 98453, DEFECT SIZE: 1 INCH.SDR USAA070106Frame · crackedBS 492, S-24R, WL 160 CRACKED. REPLACED FRAME PER DWG 65-20723, DEFECT SIZE: .5 INCH.SDR USAA070094Skin · crackedLT ENG PYLON PANEL OPENING 5727L AT O/B AFT CORNER OF OPENING. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER TYP REP 54-30-07, DEFECT SIZE: .5".SDR SB07012Hydraulic Line · leakingCLT FLT1786 EN ROUTE FROM JAX TO CLT, DURING CRUISE, CREW REPORTED LOSS OF B-HYDRAULIC SYSTEM AS HYDRAULIC QUANTITY RAPIDLY WENT DOWN TO 1/4. THE FIRST INDICATION WAS NR 2 ENGINE BELOW PRESSURE LIGHT, FOLLOWED BY LOSS OF B-HYDRAULIC FLUID AND THEN B-SYSTEM LOSDR USAA070090Angle · crackedBS 348 S-15L CRACKED. REPLACED WITH IDENTICAL PART PER BOEING DWG 64-17685-37, DEFECT SIZE: .250 INCH.SDR USAASB07011Indicator · faultyBDL FLT 1067 - AFTER TAKEOFF AND FLAP SELECTION TO 1, CREW REPORTED A FLAP ASYMMETRY LOCKOUT. POINTERS ON FLAP POSITION INDICATOR WERE LEFT AT 2 AND RIGHT AT 5. AIRCRAFT CIRCLED BDL TO BURN OFF FUEL TO AVOID AN OVERWEIGHT LANDING. FLIGHT RETURNED TO FIELD ASDR USAA070082Angle · crackedINTERCOSTAL ANGLE STA 360 AND S-8L CRACKED. MANUFACTURED PART PER DWG 69-48985, DEFECT SIZE: .75 INCH.SDR USAA070083Angle · crackedBS 360 S-13L CRACKED. REMOVED & REPLACED WITH FABRICATED PART PER BOEING DWG 65-17685, DEFECT SIZE: .250 INCH.SDR USAA070084Intercostal · crackedSTA 360 & S-11L CRACKED. REMOVED DAMAGE & INSTALLED FABRICATED REPAIR PARTS PER BOEING DWG 65-17685, DEFECT SIZE: 1 INCH.SDR USAA070085Skin · crackedLEFT ENGINE PYLON PANEL OPENING 572L AT O/B AFT CORNER OF OPENING CRACKED. STOP DRILLED CRACK & INSTALLED REPAIR DOUBLER PER TYP REP 54-30-07, DEFECT SIZE: .5 INCH.SDR USAA070080Skin · chafedOUTBOARD END OF LEFT WING OUTBOARD MID FLAP CHAFED. REMOVED DAMAGED AREA, INSTALLED DOUBLER PER SRM 57-53-03, DEFECT SIZE: 1 X 2 INCHES.SDR USAASB07010Speed Switch · faultyCLT FLT 1081 FLIGHT DEPARTED PIT EN ROUTE TO FLL WITH THE NR 2 GENERATOR/CSD INOPERATIVE. DURING CRUISE, AT FL340, THE APU OVERSPEED LIGHT ILLUMINATED AND THE APU AUTO SHUTDOWN. WITH ONLY ONE GENERATOR REMAINING, CREW DIVERTED FLIGHT TO CLT WITHOUT INCIDENT.SDR SB07007Windshield · crackedDCA FLT 1781 EN ROUTE FROM MHT TO DCA, THE FIRST OFFICER'S WINDSHIELD ARCED, THEN CRACKED. APPEARS TO BE THE OUTER PANE THAT CRACKED. FLIGHT LANDED WITHOUT FURTHER INCIDENT AT DCA. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICER'S WINDSHIELD PER MM 56-11SDR USAA070059Skin · crackedE&E AREA EXHAUST PORT FOR EQUIPMENT COOLING HAS CRACK. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER EA 98416, DEFECT SIZE: 1 INCH.SDR USAA070060Skin · crackedBS 379 BL 0 HAS CRACK. REMOVED DAMAGE, INSTALLED REPAIR PARTS, INSTALLED DOUBLER PER EA 98415, DEFECT SIZE: 1 INCH.SDR USAA070061Door Frame · crackedFWD CARGO DOOR/FWD FRAME AT 1F FOOTPRINT HAS CRACK. REMOVED DAMAGE & INSTALLED FABRICATED REPAIR PARTS PER EA 98414, DEFECT SIZE: 2 INCHES.SDR USAA070062Door Frame · crackedFWD CARGO/AFT DOOR FRAME AT 1A STOP FOOTPRINT HAS CRACK. REMOVED DAMAGE & INSTALLED REPAIR DOUBLER & TRIPLER PER EA 98413, DEFECT SIZE: .100 INCH.SDR USAA070063Door Frame · crackedFWD CARGO DOOR/FWD FRAME AT 1F FOOTPRINT HAS CRACK. REMOVED DAMAGE & INSTALLED FABRICATED REPAIR PARTS FROM EA 98414, DEFECT SIZE: 2 INCHES.
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