Boeing 737-2B7
Service difficulty reports · 1,360
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 = '7372B7' 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 = '7372B7' 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 USAA951283Stringer · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 6 INCH BY 1 INCH S-27 L, BS 1004 TO BS 1010 ON STRINGER. SPLICED IN NEW STRINGER SECTION WEIGHT CHANGE LESS THAN 1 LB. REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (SDR USAA951282Angle · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 24 INCH FORWARD ENTRY DOOR TRANSITION ANGLE. INSTALLED FILLER AND DOUBLER, REPAIRED PER SRM 51-40-3. CORROSION TASK NR C53-107-01, CORROSION LEVEL 2. (M)SDR USAA951281Intercostal · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION, 1 INCH BY 3 INCHES, STA 312 TO STA 328, LBL 12 INCHES, ON INTERCOSTAL. REPLACED INTERCOSTAL, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-01. CORROSION LEVESDR USAA951280Floor Beam · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION, 2 INCHES BY 4 INCHES, STA 344, BL ZERO TO LBL 8 INCHES, ON FLOOR BEAM. CUT OUT FLOOR BEAM SECTION, FABRICATED NEW T-CAP, AND REPAIRED DOUBLERS AND INSTALLED PER TR 53-10-13. CORROSION TASK NR C53-1SDR USAA951279Seat Track · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND SPOT OF CORROSION ON SEAT TRACK, .75 INCH BY 6 INCHES, LBL 24, BS 943. INSTALLED NEW TRACK SECTION. REPAIRED PER SRM 53-10-5. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)SDR USAA951278Intercostal · corrodedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 6 INCH CORRODED AREA, BS 984, LBL 19, ON INTERCOSTAL. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)SDR USAA951277Intercostal · corrodedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH CORRODED AREA BETWEEN BS 967 AND BS 947 AT RBL 7 INCHES ON INTERCOSTAL. REPLACED INTERCOSTAL, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSISDR USAA951274Floor Beam · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK, RLB 25 LONGITUDINAL FLOOR BEAM LOWER WEB, STA 707, WL 203. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2 AND DWG 65C34537. (X)SDR USAA951273Keel Beam · wornINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND WORN AREAS AT SCREW HOLES, BS 719 TO BS 727, RIGHT WHEELWELL ON KEEL BEAM. INSTALLED STRAP, REPAIR PER EA 40457. (X)SDR USAA951272Chord · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1.5 INCH LONG CRACK IN UPPER COMPRESSION CHORD, BS 727 - RLB 24. INSTALLED ANGLE REPAIR, REPAIRED PER EA NR 40453. (X)SDR USAA951271Splice · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 1 INCH CORROSION, STA 907 - STR 26L, ON STRINGER SPLICE. REPLACED SPLICE, REPAIRED PER SRM 51-10-1. REPLACED SPLICE, REPAIRED PER SRM 51-10-1. (X)SDR USAA951270Stringer · gougedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 3 INCH BY .25 INCH HOLE GOUGED IN OUTBOARD J-SECTION OF STRINGER, STA 1050, STR 27L. FORMED AND INSTALLED DOUBLER FOR J-LEG OF STRINGER, REPAIRED PER SRM 53-10-3, FIGURE 1. (X)SDR USAA951269Intercostal · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH, STA 957, RBL 18 - RBL 45, ON INTERCOSTAL. REPLACED INTERCOSTAL, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)SDR USAA951268Intercostal · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH, STA 927 TO STA 947, RBL 7, ON INTERCOSTAL. REPLACED INTECOSTAL PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)SDR USAA951267Floor Beam · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORRODED AREA ROUND NUTPLATE HOLES, .50 INCH BY .50 INCH, FLOOR BEAM BS 947.6, RBL 34 TO RBL 52, AND LBL 35 TO LBL 41. INSTALLED T-CAP REPAIR ANGLES. REPAIRED PER TR 53-10-05. CORROSION TASK NR C53-107-02. SDR USAA951266Floor Beam · corrodedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORRODED AREAS AROUND NUTPLATE HOLES, .50 INCH BY .50 INCH, FLOOR BEAM BS 947.6, LBL 24 TO RBL 6 (6 PLACES). INSTALLED NEW T-CAP SECTION, RBL 37 INCHES TO LBL 60 INCHES, REPAIRED PER TR 53-10-05C, WEIGHT ADDEDSDR USAA951265Intercostal · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCHES, STA 312 TO STA 328, RBL 12 INCHES, ON INTERCOSTAL. REPLACED INTERCOSTAL. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)SDR USAA951264Intercostal · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCHES, STA 294 TO STA 312, RBL 12 INCHES ON INTERCOSTAL. REPLACED INTERCOSTAL, REPAIRED PER 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)SDR USAA951263Floor Beam · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 45 INCHES, STA 328, BL ZERO TO RBL 45 INCHES. CUT OFF T-CAP FROM LBL 28 TO RBL 45, FABRICATED NEW T-CAP AND SPLICES AND INSTALLED PER TR 53-10-13. CORROSION TASK NR C53-107-02. CORROSION SDR USAA951194Floor Beam · corrodedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 3 INCH BY 1.50 INCH CORRODED AREA, BS 967, RBL 45 ON FLOOR BEAM. INSTALLED NEW T-CAP AND REPAIR ANGLES, REPAIRED PER TR 53-10-05 C. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)SDR USAA91299Support · crackINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK, SEAT TRACK SUPPORT CHANNEL, STA 520, LBL 25, WL 207.5. INSTALLED FLOOR BEAM REPAIR, WEIGHT .8 POUNDS, AT BS 520, REPAIRED PER SB 737-53-1120 EA 40385. (X)SDR USAA951213Stringer · corrosionROA - DURING 'BX' CHECK VISUAL INSPECTION, FOUND 18.5 INCHES BY 2 INCHES CORROSION (STRINGER IS CORRODED), BS 967 STRINGER 27 LEFT. REMOVED DAMAGE AND INSTALLED STRINGER SPLICE. REPAIRED PER SRM 53-10-3, FIG 1. (M)SDR USAASB95006Oil Line · looseMSP - FLT NR 1090 - ON CLIMB-OUT, PASSING THROUGH 10,000 FEET, NR 2 ENGINE LOP LIGHT ILLUMINATED ALONG WITH OIL QUANTITY AND OIL PRESSURE DECREASE TO ZERO. FLIGHT CREW SHUT DOWN NR 2 ENGINE AND RETURNED TO MSP WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINSDR USAA951046Mode Cntl Pnl · failedPHL - FLT NR 0117 - CLIMBING OUT FROM LGA EN ROUTE TO MCO WITH ALT ALERTING AND 'A' CHANNEL AUTOPILOT ON MEL, AIRCRAFT WOULD NOT HOLD ALTITUDE OR RESPOND TO CHANGES WITHOUT USING ALT SEL. MAINTENANCE REPLACED THE AUTOPILOT MODE CONTROL PANEL. BITE CHECKED ANSDR USAA951002Stringer · corrodedROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 1 INCH CORRODED AREA STRINGER 27L BETWEEN STATION 986-1016. SPLICED NEW STRINGER, REPAIRED PER SRM 53-10-3. (M)SDR USAA951001Skin · corrodedROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND 6.5 INCH BY 8 INCH CORRODED SKIN, BS 747 S-27R. REMOVED CORROSION AND INSTALLED DOUBLER, REPAIRED PER SRM 53-10-4. (M)SDR USAA950965N2 Gear Box · oil lossLGA - FLT NR 0152 - NR 1 ENGINE LOSING OIL QUANTITY ON CLIMB-OUT FROM LGA. FLIGHT CREW SHUT DOWN NR 1 ENGINE AND RETURNED TO LGA. SET WAS APPROXIMATELY 10 MINUTES. MAINTENANCE REPLACED LEFT ENGINE N2 GEAR BOX ASSEMBLY. (M)SDR USAA950943Stringer · corrodedROA - DURING CD-3 CHECK VISUAL INSPECTION, FOUND STRINGER CORRODED AT BS 767, STRINGER 276 BS 767. REMOVED DAMAGED STRINGER AND SPLICED NEW STRINGER PER SRM 53-10-3. (M)SDR USAA950838Eel Batt Pack · dischargedCLE - THE CABIN CEILING EXIT SIGN, FOR THE OVERWING EMERGENCY EXIT, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M)SDR USAA950749Eel Batt Pack · dischargedCLE - INTERIOR OVERWING EMERGENCY EXIT LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED BATTERY PACK AND CHARGER ASSEMBLY. (M)SDR USAA950608Eel Wiring · failedBWI - FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. MAINTENANCE REPAIRED WIRING AT ROW 1C FLOOR LIGHTS. REPLACED FORWARD FLOOR EMERGENCY LIGHTS BATTERY CHARGER. REF 95ZZZW801.SDR 95ZZZW801Eel Charger · inoperativeBWI - FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. MAINTENANCE REPAIRED WIRING AT ROW 1C FLOOR LIGHTS. REPLACED FORWARD FLOOR EMERGENCY LIGHTS BATTERY CHARGER. REF USAA950608.SDR USAA950598Overheat Unit · failedCLT - FLT 955 - FLIGHT EN ROUTE BWI TO BHM WHEN LEFT WING BODY OVERHEAT LIGHT CAME ON. FLIGHT DIVERTED TO CLT WHERE LANDING WAS MADE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED OVERHEAT ACCESSORY UNIT. OPS CHECK NORMAL. (M)SDR USAA950597Rt Unit · failedPIT - FLT 1069 - AFTER DEPARTURE FROM PIT, CREW WAS UNABLE TO TURN RADAR ON. FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED R/T UNIT. RADAR WORKED NORMAL. (M)SDR USAA950605Eel Socket · corrodedCLE - THE RT FORWARD SLIDE LIGHT INOPERATIVE. MAINTENANCE FOUND SOCKET ASSEMBLY CORRODED. REPLACED SOCKET ASSEMBLY, OPS CHECKED GOOD. (W)SDR USAA950528Battery Pack · dischargedCLT - EXTERIOR AFT EMERGENCY LIGHTS AT BOTH AFT DOORS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS AND CHARGER. (M)SDR 95ZZZM72Charger · inoperativeCLT - EXTERIOR AFT EMERGENCY LIGHTS AT BOTH AFT DOORS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS AND CHARGER.SDR USAA950449Pin · not removedBDL - FLT 2074 - UNABLE TO RETRACT NOSE GEAR AFTER TAKEOFF. CREW RECYCLED GEAR AND NOSE GEAR STILL WOULD NOT RETRACT. FLIGHT RETURNED TO BDL WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NOSE GEAR RETRACT PIN INSTALLED. REMOVED AND INSTALLED SDR USAA950516Frame · corrodedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 2 INCH BY 2 ICH F/S 500 A RT S-26 R. REPAIRED PER SRM 51-40-3. CORROSION TASK NR C53-208-01. CORROSION LEVEL 2. (W)SDR USAA950514Frame · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORRODED AREA .5 INCH BY .5 INCH STATION 500 RT. REPAIRED PER SRM 51-40-3. CORROSION TASK NR C53-208-01. CORROSION LEVEL 2. (W)SDR USAA950403Circuit Breaker · trippedPIT - FLT 19 - UNABLE TO CONTROL PRESSURIZATION AFTER TAKEOFF. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND MANUAL DC CIRCUIT BREAKER POPPED, RESET C/B. REPLACED OVERHEAD CONTROL PANEL. ALL CHECKS NORMAL. REF 95ZZZZ232.SDR USAA950402Outflow Valve · failedPIT - FLT 19 - AFTER TAKEOFF, AC CABIN PRESSURIZATION BEGAN TO CLIMB. AUTO CABIN PRESSURE SYSTEM WAS ON MEL, ACFT WAS IN STANDBY MODE. UNABLE TO CONTROL PRESSURIZATION IN STANDBY AC AND DC MODE. FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDSDR 95ZZZZ232Control Panel · failedPIT - FLT 19 - UNABLE TO CONTROL PRESSURIZATION AFTER TAKEOFF. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND MANUAL DC CIRCUIT BREAKER POPPED, RESET C/B. REPLACED OVERHEAD CONTROL PANEL. ALL CHECKS NORMAL. REF USAA950403.SDR 95ZZZZ231Controller · failedPIT - FLT 19 - AFTER TAKEOFF, AC CABIN PRESSURIZATION BEGAN TO CLIMB. AUTO CABIN PRESSURE SYSTEM WAS ON MEL, ACFT WAS IN STANDBY MODE. UNABLE TO CONTROL PRESSURIZATION IN STANDBY AC AND DC MODE. FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDSDR USAA950517Angle · corrosionINT - DURING 'Q-1' CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH AREA OF CORROSION FORWARD SERVICE DOOR 'Z' ANGLE STATION 302 TO 322, WL 208. REPAIRED PER BOEING DRAWING NR 65-45875 SRM 51-10-1 PG 5. CORROSION TASK NR C53-107-01, CORROSION LEVEL 2. (W)SDR USAA950381Outflow · failedCLT 2234 - UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF. FLIGHT RETURNED TO CLT WHERE AN OVERWEIGHT LANDING WAS MADE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED INSULATION FROM OUTFLOW VALVE AND REPLACED OUTFLOW VALVE AND PRESSURE CONTROLLER. REFERENCE 95ZSDR 95ZZZW782Press Controller · failedCLT 2234 - UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF. FLIGHT RETURNED TO CLT WHERE AN OVERWEIGHT LANDING WAS MADE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED INSULATION FROM OUTFLOW VALVE AND REPLACED OUTFLOW VALVE AND PRESSURE CONTROLLER. REFERENCE USASDR USAA950378Uplock Sensor · out of adjustCLT - FLT 1263 - AFTER TAKEOFF GSP, LEFT LANDING GEAR RED LIGHT REMAINED ON. CREW RECYCLED NO HELP. LIGHT FLICKERED OFF AND ON THROUGHOUT FLIGHT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED LEFT GEAR UPLOCK SENSOR. SENSOR TEST PER MM 32-6SDR USAA950515Intercostal · corrodedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 1 INCH BY 15 INCH AREA OF SURFACE CORROSION, STATION 947 TO 967 AT RBL 46. REPAIRED PER SRM 51-10-9. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W)SDR USAA950377Eel Track · crackedCLT - FIRST CLASS LOW LEVEL LIGHTING STRIP CRACKED. MAINTENANCE REPLACED LIGHTING TRACK. (W)
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