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 USAA040369Bulkhead · crackedPIT - FOUND BULKHEAD SKIN CRACKED .25 INCH, AT RIVET OUTBOARD OF RBL 57 AT WL 234 STATION 178 BULKHEAD. INSTALLED DOUBLER PER EO 5300V153. (M)SDR AWXA200400828Skin · corrodedDURING 4-DAY CHECK CORROSION WAS FOUND ON SKIN AT AFT AIR PHONE ANTENNA UNDER AFT CARGO DOOR AT BS 794.6, BETWEEN STR 27 LT AND STR 27 RT. MAINTENANCE CUTOUT DAMAGED SKIN AT AFT AIR PHONE ANTENNA BS 794.6, BETWEEN STR 27 LT AND STR 27 RT AND PERFORMED A HFEC ISDR USAA040344Skin · crackedCLT - FOUND SKIN CRACKED 2 INCHES, TWO 4.5 INCHES AFT OF 867, 1 INCH BELOW STRINGER 15R. INSTALLED DOUBLER PER SRM 53-00-01 DETAIL XI. (M)SDR USAASB04091Coalescer Bag · contaminatedCLT - FLT 983 - EN ROUTE FROM MCI-CLT, CREW REPORTED ANODOR OF JET FUEL PRESENT IN THE CABIN WITH APU AIR ON. THEN ON DESCENT INTO CLT, THE JET FUEL ODOR BECAME PRESENT IN THE COCKPIT WITHOUT THE APU RUNNING. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENASDR USAA040368Skin · delaminatedPIT - FOUND TOP SKIN AND CORE MATERIAL DELAMINATED 3 INCH BY 4 INCH AREA, NR 3 SLAT INBOARD T/E CORNER. INSTALLED NEW CORE, INSTALLED FILLER AND UPPER DOUBLER PER BOEING SRM 51-70-10. (M)SDR USAA040367Skin · chafedPIT - FOUND LOWER SKIN SURFACE CHAFED 2 INCH BY 1 INCH, NR 4 SLAT INBOARD TRAILING EDGE. REMOVED CHAFED AREA, BONDED, SEALED EDGE AND REFINISHED PER BOEING SRM 51-70-10. (M)SDR USAASB04090Sensor · malfunctionedPIT - FLT 1058 - AFTER TAKEOFF FROM PIT, EN ROUTE TO PVD, CREW REPORTED THE NR 4 LEADING EDGE FLAP WOULD NOT RETRACT AND THE LEADING EDGE FLAP TRANSIT AMBER LIGHT WAS ILLUMINATED. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGESDR USAA040437Skin · corrodedPIT - FOUND SKIN CORRODED .25 INCH BY .5 INCH SPOT, AFT PRESS BULKHEAD, AFT SIDE, STATION 1016 BL 0 . CLEANED LIGHT CORROSION PER SRM 51-21-31. (M)SDR USAA040341Web · crackedPIT FOUND WEB CRACKED 2 INCHES, STATION 1040, BL 0, 9 RIVETS UP FROM CENTER OF AFT PRESSURE DOME. CUT OUT DAMAGED AREA, INSTALLED FILLER AND DOUBLER REPAIR PER SRM 53-80-08. (M)SDR USAASB04088Charger · inoperativeCLT - MAINTENANCE REPORTED THE LOWER EMERGENCY EXIT SIGNS AT THE L1 AND R1 DOORS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY. OPERATIONAL CHECK GOOD. (M)SDR USAASB04085Relay · stuckON CLIMB-OUT FROM CLT, EN ROUTE TO DCA, CREW RECEIVED A RED NOSE GEAR LIGHT THA WOULD NOT EXTINGUISH WHEN THE GEAR WAS RETRACTED. AFTER SEVERAL ATTEMPTS TO EXTINGUISH THE RED LIGHT, CREW FOLLOWED PROCEDURES AND LOWERED THE GEAR, RECEIVING NORMAL GEAR INDICATISDR USAASB04084Circuit Card · failedCLT - FLT 194 - ON CLIMB-OUT FROM CLT, EN ROUTE TO ALB, CREW RECEIVED A RED NOSE GEAR LIGHT THAT WOULD NOT EXTINGUISH WHEN THE GEAR WAS RAISED. WHEN GEAR WAS LOWERED, ALL GEAR INDICATOINS WERE NORMAL. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHESDR USA2004F00094Charger · inoperativeFOUND SEVERAL AFT CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANE REPLACED THE AFT BATTERY AND CHARGER.SDR USAA040388Skin · delaminatedPIT - FOUND SKIN AND CORE BOND WITH DELAMINATION 2 INCH AREA, LEFT WING NR 3 SLAT INBOARD AFT CORNER TOP SURFACE. REMOVED DAMGAED SKIN AND CORE, INSTALLED INTERNAL AND TOP DOUBLER AND NEW CORE MATERIAL PER BOEING SRM 51-70-10. (M)SDR USAASB04082Reservoir · dischargedMCO - FOUND THE AFT RIGHT SLIDE BOTTLE PRESSURE READING 'ZERO'. MAINTENANCE REPLACED THE SLIDE. (M)SDR USA2004F00093Circuit Breaker · trippedON APPROACH, CREW DID NOT RECEIVE ANY LANDING GEAR INDICATION LIGHTS AFTER GEAR EXTENSION. A MISSED APPROACH WAS EXECUTED. CREW TESTED THE LIGHTS BUT HAD NO ILLUMINATION OF THE GEAR LIGHTS. BULBS CHECKED OK ALONG WITH CIRCUIT BREAKERS. MAINTENANCE FOUND THSDR USAASB04077Uplock Sensor · malfunctionedAFTER TAKEOFF FROM GSO, CREW RECEIVED A RIGHT MLG RED UNSAFE LIGHT AFTER GEAR RETRACTION. CREW LOWERED GEAR PER QUICK REF HANDBOOK PROCEDURES AND RECEIVED A NORMAL GEAR INDICATION OF THREE GREEN LIGHTS AND NO RED LIGHTS. FLIGHT LANDED WITHOUT INCIDENT AT CLTSDR USAASB04073Fuse · inoperativePHL - PILOT REPORTED THE SEAT ROW EMERGENCY LIGHTS, FROM ROWS 17 THROUGH 22, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE 5 AMP FUSE IN THE POWER SUPPLY. OPS CHECK GOOD. (M)SDR USAA040291Frame · corrodedPIT - FOUND LOWER LEG OF CHORD CORRODED .5 INCH BY 1 INCH AREA, AFT SIDE OF PRESSURE BULKHEAD FROM STRINGER 27L TO 26L. CLEANED CORROSION, TREATED AND PRIMED PER SRM 51-10-02 AND 51-20-01. (M)SDR USA2004F00092Gcu · failedENROUTE, CREW REPORTED THE G-3 PANEL CIRCUIT BREAKER OPENED IN FLIGHT. AN ELECTRICAL ODOR WAS PRESENT IN THE COCKPIT PRIOR TO THE OPENING OF THE CIRCUIT BREAKER. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE GENERASDR USA2004F00076Battery Pack · dischargedMAINTENANCE REPORTED THE EMERGENCY LIGHT BATTERY PACK, IN THE AFT POSITION, TO BE WEAK. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD.SDR USAA040243Skin · crackedSKIN CRACKED (1 INCH X Q.22 INCH) LOWER AFT CORNER FORWARD SERV CUTOUT STA 322, 4 INCH/ 14 INCH. INSTALLED DOUBLERS IAW SRM.SDR USA2004F00054Wire · chafedMAINTENANCE REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS AT SEAT ROWS 5 THROUGH 10 AND THE OVERWING EXIT IDENTIFIERS INOPERATIVE. MAINTENANCE FOUND POWER WIRE L7012A20 CHAFED TO STRUCTURE IN CEILING AREA. REMOVED DAMAGED WIRE SEGMENT AND RETERMINATED. ALSO,SDR USA2004F00050Flap · malfunctionedON APPROACH, CREW RECEIVED A LEADING EDGE FLAPS TRANSIT LIGHT ASSOCIATED WITH A YELLOW TRANSIT LIGHT ON THE NR 3 LEADING EDGE SLAT. CAPTAIN REPORTED THE FLAPS WOULD NOT EXTEND PAST 15 UNITS. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. AN SDR USA2004F00049Panel · loose(2) SECONDS PRIOR TO TOUCHDOWN, A PASSENGER REPORTED THAT TWO PANELS DEPARTED THE NR 1 ENGINE PYLON. ONE PANEL WAS REPORTED THO HAVE STRUCK THE LT HORIZONTAL STABILIZER LEADING EDGE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 1 ENGINE PSDR USA2004F00038Power Supply · faultyPILOT REPORTED THE EMERGENCY EXIT LIGHTS FLASH ON AND OFF INDEPENDENT OF SWITCH POSITION. MAINTENANCE REMOVED AND REPLACED THE M1136 POWER SUPPLY AND BATTERY PACK IAW MM. OPERATIONAL CHECK GOOD.SDR USA2004F00052Shutoff Valve · failedRT PACK TRIP OFF LIGHT ILLUMINATED, WOULD NOT RESET. LT PACK TRIP OFF LIGHT ILLUMINATED DURING TEMP ADJMT. IMMEDIATE DESCENT WAS INITIATED TO 10,000 FT BUT CABIN ALTITUDE CLIMBED ABOVE 14,000 FT DEPLOYING OXYGEN MASKS. LT PACK RESET, PRESS WAS REGAINED. FSDR DL733040406Control Unit · malfunctionedON LANDING ROLLOUT WITH AFT CARGO B SYSTEM LOOP INOPERATIVE, GOT FALSE AFT CARGO FIRE INDICATION AND BOTTLE WAS DISCHARGED. AFTER CONFIRMATION THAT NO FIRE EXISITED AIRCRAFT TAXIED TO GATE. REPLACED CARGO FIRE DETECTOR CONTROL UNITSDR USAA040206Skin · crackedSERVICE DOOR CUTOUT (.2500 INCH CRACK) AFT CORNER AT STA 332.101 FWD TO DOOR CUTOUT. REPAIRED IAW 53-10-01 FIG 202, PAGE 207.SDR USA2004F00051Outflow Valve · failedENROUTE, CREW REPORTED CABIN ALTITUDE WARNING HORN SOUNDED AS THEY ENCOUNTERED A SLOW LOSS OF CABIN PRESSURIZATION. PRESSURE LOSS WAS NOT EXPLOSIVE BUT CREW COULD NOT CNTRL PRESS. FLIGHT DESCENDED TO 10,000 FT AND CONTINUED. NO OXYGEN MASKS WERE DEPLOYED. SDR USA2004F00046Controller · malfunctionedENROUTE, CREW REPORTED VIA ACARS THEY ENCOUNTERED A SLOW LOSS OF CABIN PRESSURIZATION. PRESSURE LOSS WAS NOT EXPLOSIVE BUT CREW COULD NOT CONTROL PRESSURIZATION. FLIGHT DESCENDED TO 10,000 FEET AND CONTINUED. NO OXYGEN MASKS WERE DEPLOYED. FLIGHT LANDED WISDR USAA040201Intercostal · corrodedBULKHEAD, INTERCOSTAL (5 INCH WIDE X 7 INCHES TALL) CORROSION; NO LEVEL OR TASK NR STA 1016 AFT PRESS BULKHEAD AT LOWER AREA, BL 0 . REPAIRED IAW EO5302V112A, DOUBLER INSTALLATION.SDR USAA040190Skin · crackedCLT - FOUND SKIN CRACKED 1.5 INCHES, BS 727 0 PLUS 12 STRINGER 24R. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M)SDR USAASB04049Wire Harness · faultyPIT - FLT 991 - EN ROUTE FROM PHL TO DFW, SOUTH OF PIT, CREW REPORTED THE NR 2 ENGINE EGT SPIKED TO 1,000 DEGREES WITH THE RED OVERHEAT LIGHT ILLUMINATING. ALL OTHER ENGINE INDICATIONS WERE NORMAL. CREW REDUCED POWER ON THE NR 2 ENGINE AND THE LIGHT EXTINGUISDR USAASB04048Fan Blade · erodedIAH - FLT 775 - EN ROUTE FROM PHL-IAH, AT FL310, THE CABIN ALTITUDE CLIMBED VERY SLOWLY TO 9,500 FEET. AT THIS TIME, THE CABIN ALTITUDE WARNING HORN SOUNDED. CREW ACCOMPLISHED AN IMMEDIATE DESCENT OT FL240. CABIN ALTITUDE BEGAN TO DESCEND AND STABILIZE AT 3SDR USAA040187Skin · crackedCLT - FOUND SKIN CRACKED 1.35 INCHES, STATION 760 AT STRINGER 19R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M)SDR USAA040199Vertical Support · crackedSUPPORT (1.5 INCH CRACKED) CRACKED. VERTICAL SUPPORT AT LBL 5.7.SDR USAASB04045Bulb · inoperativeBUF - FLT 962 - ON FINAL APPROACH INTO BUF, CREW LOWERED GEAR AND DID NOT RECEIVE ANY INDICATION FOR THE RIGHT MLG. A TOWER FLY-BY WAS ACCOMPLISHED WITH THE TOWER CONFIRMING THE GEAR WAS DOWN. CREW REPLACED LIGHT BULBS AND RECEIVED GREEN LIGHTS. THE EMERGENSDR USAA040202Fairing · crackedPIT, ENGINE STRUT FAIRING, 1 INCH CRACK, FWD LT MOUNT HOLE NAC STA 279.50. REMOVED DEFECTIVE PART, WELDED AND REINSTALLED.SDR USAA040188Skin · crackedCLT - FOUND SKIN CRACKED 2.5 INCHES, LOWER AFT CORNER OF FORWARD SERVICE DOOR CUTOUT STATION 344.47 WL, 207.5. INSTALLED DOUBLER EPR SRM 53-00-01. (M)SDR USAASB04044Charger · failedPIT - MAINTENANCE REPORTED THE AFT SECTION OF SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY FOR THE AFT SECTION OF SEAT MOUNTED EMERGENCY LIGHTS. OPERATIONAL CHECK NORMAL. (M)SDR USAA040118Skin · crackedCLT - FOUND SKIN CRACKED 1.5 INCH, STATION 933 STRINGER 24R. INSTALLED REPAIR DOUBLER PER SRM 53-00-01. (M)SDR USAA040119Skin · crackedCLT - FOUND SKIN WITH TWO CRACKS .5 INCH AND 2 INCHES LONG, STATION 727E +4 AT STRINGER 22R, RIGHT FUSELAGE. INSTALLED REPAIR DOUBLER PER SRM 53-00-01. (M)SDR USAA040117Skin · crackedFOUND SKIN CRACKED 2.5 INCHES, STATION 727E AT STRINGER 18R, RT FUSELAGE. INSTALLED REPAIR DOUBLER PER SRM 53-00-01. (M)SDR USAA040112Skin · crackedFOUND SKIN CRACKED .600 INCH LONG, S-23L AT FS 744. REPAIR DOUBLER INSTALLED PER SRM 53-00-01, FIG 229. (M)SDR USAA040113Skin · crackedFOUND SKIN CRACKED 1.250 INCH LONG, 3 INCHES FORWARD OF FS 727E ADJACENT TO S-24L. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M)SDR USAA040107Skin · crackedFOUND SKIN CRACKED 1.250 INCH LONG, INSTALLED DOUBLER PER SRM. 53-00-01, FIG 229. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M)SDR USAA040111Skin · crackedCLT - FOUND SKIN CRACKED .600 INCH LONG, S22R 12 INCHES AFT OF FS 727D. INSTALLED DOUBLER PER SRM 53-00-01. (M)SDR USAA040110Skin · crackedFOUND SKIN CRACKED 1.450 INCH LONG, FS 891 ADJACENT OT S23R. INSTALLED DOUBLER PER SRM 53-00-01. (M)SDR USAA040066Bulkhead · crackedFOUND BULKHEAD SKIN CRACKED .25 INCH, BS 178 BULKHEAD LBL 5.7 WL 234. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER EO 5300V152C AND SRM 53-10-08 FIG 209 SHT 5. (M)
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