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 USAA2008112492116Skin · crackedCLT - C1 - MAJOR REPAIR - CRACK ON FUSELAGE SKIN AT BS 484.5, S1R. REPAIRED FUSELAGE SKIN AT BS 484.5, S1R IAW B737 SRM 53-00-01.SDR USAA2008112492114Skin · crackedCLT - RON - MAJOR REPAIR - CRACK FUSELAGE SKIN AT BS 727E +9 INCHES, S26R. REPAIRED FUSELAGE SKIN IAW B737 SRM 53-00-01 REPAIR 31.SDR USAA2008112492118Flap · delaminatedCLT - C1 - MAJOR REPAIR - LEFT FOREFLAP DELAMINATED ALONG TRAILING EDGE APPROX 85.5 INCHES FROM INBOARD END AND 25 INCHES FROM INBOARD END. REPLACED LEFT FOREFLAP IAW B737 AMM 27-51-37.SDR USAA2008112492117Tab · debondedCLT - C1 - MAJOR REPAIR - LEFT AILERON TAB DISBONDED ON LOWER SIDE 1.5 INCHES FROM OUTBOARD END AND 1 INCH FROM TRAILING EDGE. REPLACED LEFT AILERON TAB IAW US AIRWAYS TASK CARD 03I30627002L.SDR USAA920082084Beam · crackedPIT FPBH MAJOR REPAIR LOG NR 4335081 4 CRACKS IN BEAM WEB AT BS178 BULKHEAD, LBL17, BETWEEN WL225 AND WL234. REPAIRED BEAM WEB AT BS178 BULKHEAD, LBL17, BETWEEN WL225 AND WL234 IAW B737 SRM 53-10-08.SDR USAA2008112492115Door · crackedCLT - Q2 - MAJOR REPAIR - FORWARD ENTRANCE DOOR CRACKED AT INTERIOR SKIN AT NR 7 STOP PIN HOLE ON AFT SIDE OF DOOR. REPAIRED FORWARD ENTRANCE DOOR INTERIOR SKIN AT NR 7 STOP PIN HOLE IAW US AIRWAYS TYPICAL REPAIR 52-10-16.SDR USAASB08113Indicator · defectiveDCA - FLT 1282 EN ROUTE PBI TO DCA. DURING PREPARATION FOR LANDING, THE TRAILING EDGE FLAPS ONLY DEPLOYED TO TWO DEGREES AND INDICATED UNEVENLY SPLIT. THE CREW EXECUTED A MISSED APPROACH. THE CREW RECYCLED THE FLAPS AND MADE A SECOND APPROACH. THE FLAPS DSDR USAA920082085Bulkhead · crackedPIT FPBH MAJOR REPAIR LOG NR 4335079 CRACK ON FORWARD SIDE OF FORWARD PRESSURE BULKHEAD SKIN AT BS 178, RBL10, WL234. REPAIRED FORWARD SIDE OF FORWARD PRESSURE BULKHEAD SKIN AT BS 178, RBL10, WL 234 IAW SRM 53-10-08.SDR USAA920082088Frame · crackedCLT Q2 MAJOR REPAIR NR 03C10753039/005 FRAME CRACKED AT PSU RAIL ATTACH POINT BS 500C, BETWEEN S8L AND S9L. REPAIRED FRAME AT PSU RAIL ATTACH POINT BS 500C, BETWEEN S8L AND S9L IAW TYPICAL REPAIR NR 53-10-20E.SDR USAA920082087Frame · crackedCLT Q2 MAJOR REPAIR NR 03C10753039/006 FRAME CRACKED AT PSU RAIL ATTACH POINT BS 727B, BETWEEN S8R AND S9R. REPAIRED FRAME AT PSU RAIL ATTACH POINT BS 727B, BETWEEN S8R AND S9R IAW TYPICAL REPAIR NR 53-10-20E..SDR USAA920082086Frame · crackedCLT Q2 MAJOR REPAIR NR 03C10753039/007 FRAME CRACKED AT PSU RAIL ATTACH POINT BS727D, BETWEEN S8R AND S9R. REPAIRED FRAME AT PSU RAIL ATTACH POINT BS727D, BETWEEN S8R AND S9R IAW TYPICAL REPAIR NR 53-10-20E.SDR USAASB08112Unknown · odorFLT 1868. ON TAKEOFF & LANDING, CREW NOTICED AN ODOR COMING FROM A/C PACKS. MX PLACED ACFT ON MEL. ODOR DISSIPATED DURING CLIMB. CLT MX PLACED LT PACK ON MEL 21-01A. WHILE ON MEL, ANOTHER REPORT OF ODOR COMING FROM A/C PACKS DURING HIGH POWER ON TAKEOFF OSDR USAA920082082Bulkhead · crackedPIT FPBH MAJOR REPAIR NR 4335082 5 CRACKS IN BEAM WEB AT BS178, BETWEEN WL225 TO 234 RBL17. CRACKS MEASURE 0.125, 0.250, 0.50, 0.750 AND 0.250 INCHES IN LENGTH. REPAIRED BEAM WEB AT BS178, BETWEEN WL225 TO 234 RBL17 IAW B737 SRM 53-10-08.SDR USAA920082079Frame · crackedCLT Q2 MAJOR REPAIR NR 03C10753039/004 FRAME CRACKED AT PSU RAIL ATTACH POINT AT BS727D, BETWEEN S8L AND S9L. REPAIRED FRAME AT PSU RAIL ATTACH POINT AT BS727D, BETWEEN S8L AND S9L IAW US AIRWAYS TYPICAL REPAIR NR 53-10-20E.SDR USAASB08110Fan · noisyMIA - FLT 741 - EN ROUTE PHL TO MIA. ON TAXI-OUT, THE FLIGHT CREW NOTICED THAT THE LEFT RECIRCULATION FAN WAS NOISY. THE FAN WAS TURNED OFF AND THE FLIGHT PROCEEDED. DURING THE FLIGHT, THE FLIGHT CREW NOTICED AN OILY ODOR COMING FROM THE COCKPIT GASPER VENTSDR USAA2008111992090Trim Tab · crackedCLT - RON - MAJOR REPAIR - LEFT ELEVATOR TRIM TAB DELAMINATED AT NR 2 HINGE CUTOUT AREA AND HAS CRACKS AT THE NR 1 HINGE CUTOUT. REPLACED LEFT ELEVATOR TRIM TAB IAW US AIRWAYS TASK CARD 03C71127007.SDR USAA2008111992089Trim Tab · crackedCLT - RON - MAJOR REPAIR - RIGHT ELEVATOR TRIM TAB HAS CRACKS COMING FROM HINGE CUTOUTS (2 PLACES). REPLACED RIGHT ELEVATOR TRIM TAB IAW US AIRWAYS TASK CARD 03C71227004.SDR USAASB08108Battery · dischargedDCA - MAINTENANCE REPORTED THE AFT EMERGENCY FLASHLIGHT HAS A DEAD BATTERY. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE AFT EMERGENCY FLASHLIGHT. OPERATIONAL CHECK GOOD.SDR USAAB08107Battery · dischargedDCA - MAINTENANCE REPORTED THE AFT EMERGENCY FLASHLIGHT HAS A DEAD BATTERY. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE AFT EMERGENCY FLASHLIGHT. OPERATIONAL CHECK GOOD.SDR USAASB08107Acm · overservicedDURING CLIMBOUT FROM PHL, EN ROUTE TO MCO, CREW REPORTED A SOUR ODOR HAD FILLED THE CABIN ATMOSPHERE CAUSING THE FORWARD LAVATORY SMOKE DETECTOR TO SOUND. SMELL DISSIPATED EN ROUTE BUT RETURNED ON FINAL APPROACH TO MCO. FLIGHT LANDED WITHOUT FURTHER INCIDENTSDR USAA920082002Skin · crackedCLT RON MAJOR REPAIR LOG NR 8218827 CRACK IN FUSELAGE SKIN AT BS727E, S22L. REPAIRED FUSELAGE SKIN AT BS727E, S22L IAW B737 SRM 53-00-01.SDR USAA920081998Frame · crackedCLT Q5 MAJOR REPAIR NR 03C20853011/010 FUSELAGE FRAME CRACKED AT BS 520 BETWEEN S20L AND S21L. REPAIRED FUSELAGE FRAME AT BS 520 BETWEEN S20L AND S21L IAW SRM 53-00-07 REPAIR 13.SDR USAASB08104Charger · inoperativeFLL - MAINTENANCE REPORTED THE LOW LEVEL EMERGENCY LIGHTING, FROM SEAT ROWS 12 THRU 17, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD.SDR USAA920081986Frame · crackedCLT MAJOR REPAIR Q5 CHECK NR 03C20853011/018, CRACKED FRAME AT BS 500C, S20R - S21R. REPAIRED FRAME AT BS 500C, S20R - S21R. IAW EA 100716.SDR USAA920081985Skin · crackedCLT MAJOR REPAIR Q5 CHECK NR 03C21952009/002, AFT CARGO DOOR SKIN CRACKED, AFT OF HANDLE. REPLACED AFT CARGO DOOR IAW TASK CARD 03C21952008.SDR USAA920081981Skin · crackedCLT RON MAJOR REPAIR LOG NR 4371367 RT HORIZONTAL STABILIZER LOWER SURFACE HAS A CRACK FORWARD OF CENTER ELEVATOR BALANCE PANEL AT AFT SPAR. REPAIRED RT HORIZONTAL STABILIZER LOWER SURFACE IAW US AIRWAYS TYPICAL REPAIR NR 55-10-07 REV D.SDR USAA920081980Skin · crackedCLT RON MAJOR REPAIR NR 8213467 AND 4371386 LT FUSELAGE SKIN CRACKED AT BS 967, 24L. REPAIRED LT FUSELAGE SKIN AT BS967, 24L IAW US AIRWAYS EA NR 100715.SDR USAASB08102Fuel Control · faultyEN ROUTE FROM ORD TO PHL, DURING CRUISE, THE APU GENERATOR FELL OFF LINE. CREW WAS UNABLE TO GET IT BACK ON LINE. SINCE THE NR 1 ENGINE GENERATOR WAS ALREADY ON MEL, THE FLIGHT DIVERTED TO PIT WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WSDR USAA920081972Frame · crackedCLT Q5 MAJOR REPAIR NR 03C20853011/008 CRACK IN FRAME STIFFENER AT LIGHTNING HOLE AT BS500B BETWEEN S20L AND S21L. REPAIRED FRAME STIFFENER AT LIGHTNING HOLE AT BS500B BETWEEN S20L AND S21L. IAW SRM 53-00-07, EA NR 100705.SDR USAA920081971Frame · crackedCLT Q5 MAJOR REPAIR NR 03C20853011/012 CRACK AT FRAME 500E BETWEEN S20L AND S21L. REPAIRED FRAME 500E BETWEEN S20L AND S21L IAW SRM 53-00-07, REPAIR 13.SDR USAA920081962Attach Angle · crackedCLT Q5 MAJOR REPAIR NR 03052980086/002 CRACK ON LT WING LOWER SKIN ATTACH ANGLE AT WBL 135.5, 6 INCHES FORWARD OF REAP SPAR. REPAIRED LT WING LOWER SKIN ATTACH ANGLE AT WBL 135.5, 6 INCHES FORWARD OF REAR SPAR IAW US AIRWAYS EA NR 100682.SDR USAASB08100Csd · malfunctionedSHORTLY AFTER TAKEOFF FROM PIT, EN ROUTE TO FLL, THE NR 2 ENGINE GENERATOR CSD HIGH OIL TEMPERATURE LIGHT ILLUMINATED AND THE LOW OIL PRESSURE LIGHT WAS FLASHING. CREW DISCONNECTED CSD PER QUICK REFERENCE HANDBOOK PROCEDURES AND BROUGHT APU ON LINE. APU THEN SDR USAA920081973Web · crackedCLT Q5 MAJOR REPAIR NR 03C20353004/003 WEB CRACKED AT BS 243.7, WL 208, LBL 18 AT LIGHTNING HOLE. REPLACED WEB AT BS 243.7, WL 208, LBL 18 IAW DRAWING NR 69-1338.SDR USAA920082003Frame · crackedCLT Q5 MAJOR REPAIR NR 03C20853011/014 AND 4262806 FRAME CRACKED AT 500B BETWEEN S20L AND S21L. REPAIRED FRAME AT 500B BETWEEN S20L AND S21L IAW US AIRWAYS EA NR 100705.SDR USAA920081935Channel · crackedCLT Q5 MAJOR REPAIR NR 03C21853024/005 HAT CHANNEL CRACKED AT BS 727D, BLO IN AFT CARGO COMPARTMENT. REPLACED HAT CHANNEL AT BS 727D, BLO IN AFT CARGO COMPARTMENT IAW B737 SRM 51-40-02.SDR USAA920081977Frame · crackedCLT Q5 MAJOR REPAIR NR 03C20853011/019 CRACK AT FRAME BS500B, BETWEEN S20L AND S21L. REPAIRED FRAME AT BS500B, BETWEEN S20L AND S21L IAW B737 SRM 53-00-07 REPAIR 13.SDR USAA920081978Frame · crackedCLT Q5 MAJOR REPAIR NR 03C20853011/017 AND 03C20853011/016 FRAME STIFFENER CRACKED AT BS 500E BETWEEN S20L - S21L AND S20R - S21R. REPAIRED FRAME STIFFENER AT BS 500E BETWEEN S20L - S21L AND S20R - S21R IAW B737 SRM 53-00-07 REPAIR 13.SDR USAA920081970Frame · crackedCLT Q5 MAJOR REPAIR NR 03C20853011/005 CRACK IN FRAME AT LIGHTNING HOLE AT BS 500D BETWEEN S20R TO S21R. REPAIRED FRAME AT LIGHTNING HOLE AT BS 500D BETWEEN S20R TO S21R IAW SRM 53-00-07.SDR USAA920081955Frame · crackedCLT MAJOR REPAIR Q5 CHECK NR 03C20853011/007, CRACKED FRAME AT BS 500C, S20L - S21L. REPAIRED FRAME AT BS 500C, S20L - S21L IAW B737 SRM 53-00-07.SDR USAA920081953Skin · crackedCLT MAJOR REPAIR Q5 CHECK NR 03C50754003/011 LT PYLON STRUT SKIN CRACKED AT ACCESS PANEL OPENING 5724. REPAIRED THE LT PYLON STRUT SKIN AT ACCESS PANEL OPENING 5724 IAW US AIRWAYS TYPICAL REPAIR 54-50-07 PART 2 FIGURE 3.SDR USAA920081936Skin · crackedCLT Q5 MAJOR REPAIR NR 03C00053006/001 FUSELAGE SKIN AT EXTERNAL POWER RECEPTICAL LOWER LATCH IS CRACKED ON INSIDE AT BS219, S23R. REPAIRED FUSELAGE SKIN AT EXTERNAL POWER RECEPTICAL LOWER LATCH ON INSIDE AT BS219, S23R IAW US AIRWAYS EA NR 100686.SDR USAASB08099Battery · dischargedPIT - MAINTENANCE REPORTED THE FORWARD CABIN EMERGENCY FLASHLIGHT RED INDICATOR WAS NOT BLINKING. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN FLASHLIGHT. OPERATIONAL CHECK GOOD.SDR USAA920081900Frame · crackedCLT Q5 MAJOR REPAIR NR 03C20053004/004 FRAME CRACKED AT BS 639, S17L, WL 200. REPAIRED FRAME AT BS 639, S17L, WL 200 IAW TYPICAL REPAIR NR 53-62-01 AND EA NR 100695.SDR USAA920081892Spindle · crackedPIT FPBH MAJOR REPAIR LOG NR 4352180 AND 03T30757001 OTBD LT SPINDLE SHOWS CRACK 60% AT 35 THRU GATE VERTICALLY TO 40% AT 50 HORIZONTALLY. REPLACED SPINDLE IAW B737 MM 27-51-44-404-006.SDR USAASB08096Indicator · faultyON APPROACH TO FLL, CREW REPORTED A SPLIT FLAP INDICATION ON INDICATOR WHEN SELECTING FLAPS 25. NO ROLL PROBLEMS WERE ENCOUNTERED. CREW SELECTED FLAPS 15 AND ACCOMPLISHED A GO-AROUND. INDICATOR WENT TO NORMAL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. PER FSDR USAA920081869Stringer Clip · crackedCLT Q5 MAJOR REPAIR NR 03C20053004/003 STRINGER CLIP CRACKED AT BS 663, 10R. REPLACED STRINGER CLIP AT BS663, 10R IAW SRM 51-10-02.SDR USAA920081889Angle · crackedCLT Q5 MAJOR REPAIR NR 03C10853029/001. SHEAR WEB ANGLE CRACKED BETWEEN BS 927 AND BS 947, BL 0. REPLACED SHEAR WEB ANGLE BETWEEN BS 927 AND BS 947, BLO IAW SRM 53-60-51.SDR USAA920081871Frame · crackedCLT Q5 MAJOR REPAIR NR 03C10753038/006 FUSELAGE FRAME CRACKED ON INNER CHORD AT BS 601, S17R, WL 202, RBL 66. REPAIRED FUSELAGE FRAME INNER CHORD AT BS 601, S17R, WL 202, RBL 66 IAW EA NR 100688.SDR USAA920081954Web · crackedCLT MAJOR REPAIR Q5 CHECK NR 03C10652003/007. CRACKED WEB ON THE AFT SERVICE DOOR AT THE 4TH STOP CUT OUT FROM THE BOTTOM. REPAIRED AFT SERVICE DOOR WEB AT THE 4TH STOP CUT OUT FROM THE BOTTOM IAW TYPICAL REPAIR 52-10-11.SDR USAA920081851Floorbeam · corrodedCLT Q5 MAJOR REPAIR NR 03C10853029/005 LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM T-CAP AT BS208 LBL29 THRU RBL29. REPAIRED FLOORBEAM T-CAP AT BS208 LBL29 THRU RBL29 REPAIR NR 53-10-05B.
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