Boeing 737-2L9
Service difficulty reports · 593
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 = '7372L9' 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 = '7372L9' 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 2003F00564Skin · crackedDURING C-CHECK INSPECTION, THE FUSELAGE WAS FOUND TO BE CRACKED AT THE R1 DOOR LOWER AFT CORNER. THE CRACK WAS 2.5 TO 3 INCHES AND VERIFIED BY NDT. ALL REPAIRS HAVE BEEN ACCOMPLISHED ON NON ROUTINE 031033. TOTAL AIRCRAFT TIME 46985.2, TOTAL CYCLES 41351. (SDR 2003F00569Stringer · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION WAS FOUND AT STRINGER 24L BETWEEN BS 330.7 AND BS 334 IN THE E/E COMPARTMENT. THE DAMAGE WAS REPAIRED ON NON-ROUTINE 031078 IAW WITH SRM 53-10-3 FIGURE 1. TOTAL AIRCRAFT TIME 46985.2, TOTAL CYCLES 41351. (M)SDR 2003F00568Rib · crackedDURING C-CHECK INSPECTION, A CRACKED RIB WAS FOUND AT BS 400 ABOVE STRINGER 20L. THE REPAIRS HAVE BEEN ACCOMPLISHED ON NON ROUTINE 031072. AIRCRAFT TOTAL TIME 46985.2. TOTAL CYCLES 41351. (M)SDR CA021129003Servo · malfunctioned(CAN) CRUISING FL310, AURAL WARNING FOR PRESSURIZATION SOUNDED, OVERHEAD MASTER CAUTION ILLUMINATED.INITIATED EMERG. DESCENT, PRESSURIZATION CONTROLLED MANUALLY BUT NOT BEFORE MASKS IN CABIN DROPPED. EMERG. DESCENT & RAPID DEPRESSURIZATION CHECKLIST COMPLETED.SDR F3LA200200362Door Frame · crackedDURING C 2 CHECK, A CRACK WAS FOUND IN THE LOWER, FORWARD AND AFT CORNERS OF THE DOOR FRAME ON THE FORWARD BAGGAGE COMPARTMENT DOOR. THE LOWER, FORWARD AND AFT FRAMES OF THE FORWARD BAGGAGE COMPARTMENT DOOR WERE REPLACED IAW SB 737-52A1100, FIGURE 2, AND COMPSDR F3LA200200357Cargo Track · corrodedDURING A C 2 CHECK, CORROSION WAS FOUND IN THE CARGO TIE DOWN TRACK AT LBL 17, WL 157, BS 813. TIE DOWN TRACK WAS REPLACED IAW SRM 53-10-05 AND SRM 51-10-02.SDR F3LA200200353Structure · crackedDURING C 2 CHECK, THE FORWARD CARGO DOOR, LOWER CORNER, WAS FOUND TO HAVE A CRACK. THE CRACK WAS REPAIRED USING SB 737-52A1100 AND COMPLIED WITH THE REQUIREMENTS OF AD 2000-07-06 UNDER ENGINEERING REQUEST 02-1333SDR F3LA200200346Skin · crackedDURING C-2 CHECK, INSPECTION REPORTED LT WING FIXED LE CRACKED ON INBD SIDE OF NR 2 SLAT, INBD AUX TRACK CUTOUT. REPAIRED CRACK PER SRM 57-20-L1 AND MM 51-21-021.SDR F3LA200200345Floorbeam · corrodedDURING C-2 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOORBEAM, BS 813, RBL 8, WL 157. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-5 AND 51-30-02.SDR F3LA200200344Skin · crackedDURING C-2 CHECK, INSPECTION REPORTED FWD GALLEY DOOR INNER DOOR SKIN CRACKED AT ATTACH RIVET, FWD EDGE, CENTER SPAN. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-30-02, 51-10-02 AND 51-21-0.SDR F3LA200200343Floorbeam · corrodedDURING C-2 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOOR BEAM, BS 813, LBL 8, WL 157. REPAIRED DAMAGED AREA PER SRM 53-10-1 AND 53-10-5.SDR F3LA200200342Floorbeam · corrodedDURING C-2 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOORBEAM, BS 813, LBL 12, WL 157. FABRICATED AND INSTALLED REPLACEMENT PARTS PER SRM 53-10-5 AND 51-30-02.SDR F3LA200200341Strap · corrodedDURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOORBOARD SPLICE STRAP, BS 772, WL 157. REPLACED STRAP PER SRM 51-30-2.SDR F3LA200200340Strap · corrodedDURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR SPLICE, BS 504, WL 155. REPLACED STRAP PER SRM 51-30-02.SDR F3LA200200339Clip · damagedDURING C-2 CHECK, INSPECTION REPORTED SHEARED RIVETS ON SUB THRESHOLD "T" CLIP, BS 440, RBL 16. REPLACED "T" CLIP PER SRM 51-30-02.SDR F3LA200200337Support · corrodedDURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 786, RBL 21, WL 157. REPLACED SIDEWALL SUPPORT PER SRM 51-30-02, FIG. 1, AND SRM 51-30-02, FIG. 9.SDR F3LA200200338Support · corrodedDURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FLOOR TO SIDEWALL SUPPORT, BS 500A - BS 520, RBL 25, WL 156. FABRICATED AND INSTALLED REPLACEMENT SIDEWALL SUPPORT PER SRM 53-10-1, 53-10-2. 51-21-21 AND 51-30-2.SDR F3LA200200336Frame · corrodedDURING C-2 CHECK, INSPECTION REPORTED CORROSION ON FRAME AT BS 747, RBL 6, WL 148. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-4, 53-10-1 AND 51-30-02.SDR F3LA200200335Structure · crackedDURING C-2 CHECK, INSPECTION REPORTED FWD ENTRY DOOR AFT LOWER THRESHOLD CRACKED AT FWD EDGE. REPAIRED PER SRM 52-30-3 AND BOEING DRAWING 65-02938.SDR F3LA200200333Skin · crackedDURING C-2 CHECK, INSPECTION REPORTED CRACKED SKIN AT AFT ENTRY DOOR CUTOUT FWD LOWER CORNER, APPROX .25 INCH IN LENGTH. REPAIRED PER SRM 53-30-3, FIGURE 24.SDR F3LA200200334Skin · crackedDURING C-2 CHECK, INSPECTION REPORTED FWD SERVICE DOOR CUTOUT SKIN CRACKED AT AFT LOWER CORNER. REPAIRED SKIN PER SRM 53-30-3.SDR F3LA200200332Angle · crackedDURING C-2 CHECK, INSPECTION REPORTED RT AFT WING TO BODY FAIRING SUPPORT ANGLE CRACKED AT STRINGER 20, BS 727-727B. FABRICATED AND INSTALLED REPLACEMENT SUPPORT ANGLE PER SRM 51-10-02, SRM 51-30-00 AND BOEING DRAWING 65-48657.SDR F3LA200200331Skin · gougedDURING C-2 CHECK, INSPECTION REPORTED RT. WING OTBD FOREFLAP UPPER SURFACE GOUGED AT WBL 314. REMOVED EXISTING REPAIR DOUBLER, FABRICATED AND INSTALLED REPLACEMENT DOUBLER PER SRM 51-40-20.SDR F3LA200200330Skin · gougedDURING C-2 CHECK, INSPECTION REPORTED RT. WING INBD FOREFLAP, INBD UPPER SURFACE, GOUGED IN 2 AREAS. FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-20.SDR F3LA200200364Stringer · corrodedDURING C 2 CHECK, CORROSION WAS FOUND ON THE STRINGER AT STA 520, STR 26L.THE STRINGER WAS REPAIRED BY REMOVING THE DAMAGED SECTION BETWEEN STA 510 AND 540 AT STR 26L. NEW PARTS WERE FABRICATED AND INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-10-3,SDR F3LA200200349Skin · corrodedDURING C 2 CHECK, CORROSION WAS FOUND ON THE SKIN AT BS 470, ON THE EXTERIOR, UNDER THE DME ANTENNAE. REPAIR WAS PERFORMED IN ACCORDANCE WITH SRM 53-30-3, FIGURE 2SDR F3LA200200348Floor Support · corrodedDURING C 2 CHECK, CORROSION FOUND IN AFT CARGO BAY FLOOR SUPPORT AT LBL 8. REMOVED DAMAGED SECTION OF FLOOR SUPPORT, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-5, FIGURE 6SDR F3LA200200256Sensing Element · faultyAIR TURNBACK. FLIGHT CREW REPORTED NR 2 FIRE WARNING BELL SOUNDED AND LIGHT ILLUMINATED. LIGHT EXTINGUISHED WITH THRUST REDUCED TO IDLE. ALL ENGINE INDICATIONS APPEARED NORMAL. REPLACED NR 2 ENGINE UPPER FIRE SENSING ELEMENT. REMOVED PLACARD.SDR F3LA200200255Connector · dirtyAIR TURNBACK. FLIGHT CREW REPORTED NR 2 FIRE WARNING HANDLE ILLUMINATED MOMENTARILY ON THREE OCCASIONS DURING DEPARTURE. CLEANED CONNECTORS A AND B ON LOWER FIRE DETECTOR ELEMENT AND CHECKED OKAY.SDR F3LA200200254Module · malfunctionedAIR TURNBACK. FLIGHT CREW REPORTED NR 2 ENGINE FIRE WARNING ILLUMINATED APPROXIMATELY 5 MINUTES AFTER TAKEOFF. FIRE WARNING WENT OUT WHEN THRUST REDUCED, ALL INDICATIONS NORMAL. WHEN MORE THRUST ADDED, FIRE WARNING ILLUMINATED AGAIN. REDUCED THRUST TO IDLESDR F3LA200200171Battery Pack · dischargedMAINTENANCE REPORTED SECTION OF EMERGENCY AISLE PATH LIGHTING IN FWD CABIN INOPERATIVE. FERRIED AIRCRAFT TO DEN FOR REPAIR. UPON ARRIVAL, REPLACED THE FWD BATTERY AND POWER SUPPLY ASSY. PERFORMED OPERATIONAL TEST AND CHECKED OKAY.SDR F3LA200200107Door Frame · crackedDURING AN OUTFLOW VALVE TEST WITH THE AIRCRAFT PRESSURIZED, MAINTENANCE REPORTED A LOUD POP IN THE AREA OF THE AFT CARGO DOOR AND FOUND A 5-INCH CRACK IN THE RADIUS OF THE DOOR FRAME OTBD OF THE LOWER FWD STOP FITTING AND CRACKS IN THE LOWER DOOR BEAM OTBD CHOSDR F3LA200200106Cartridge · defectiveUPON ARRIVAL, FLIGHT CREW REPORTED AILERONS BECAME EXTREMELY TIGHT AND FELT AS IF IN MANUAL REVERSION. HYDRAULIC SYSTEM PRESSURES WERE BOTH NORMAL. RUDDER AND ELEVATOR FELT NORMAL. ACCOMPLISHED NORMAL LANDING. REPLACED AILERON SPRING CARTRIDGE PER MM 27-11SDR F3LA200100151Skin · gougedDURING C-1 CHECK, INSPECTION REPORTED FUSELAGE SKIN LAP AT STR 19-R, STA 386 TO STA 410 SCRATCHED AND GOUGED. A 14.5 INCH AREA ON SKIN LAP AT STR 19-R, STA 386 TO STA 410 FOUND TO BE OUT OF LIMITS PER SRM 53-30-01. DAMAGE WAS REMOVED BETWEEN STA 390 AND STA SDR F3LA200100138Bushing · corrodedDURING C-1 CHECK, INSPECTION REPORTED ALL BUSHINGS CORRODED ON RT WING SWING LINK ASSY. REPLACED RT WING SWING LINK ASSY PER BOEING DRAWING 65-82770 AND MM 57-15-0, STEP 5E.SDR F3LA200100137Collar · corrodedDURING C-1 CHECK, INSPECTION REPORTED LT. MLG BELLCRANK RETAINING COLLAR CORRODED. REPLACED RETAINING COLLAR PER MM 32-32-31.SDR F3LA200100132Odor · detectedUPON DEPARTURE FROM ABQ, FLIGHT CREW REPORTED STRONG PULL TO THE RIGHT JUST AFTER TAKEOFF THRUST WAS SET. FULL LEFT RUDDER WITH A LITTLE TILLER STRAIGHTENED THE AIRCRAFT OUT AND CONTINUED TAKEOFF ROLL, WHICH APPEARED NORMAL. ALSO REPORTED A STRONG BURNING RUSDR F3LA200100Odor · detectedUPON DEPARTURE FROM ABQ, FLIGHT CREW REPORTED A STRONG PULL TO THE RIGHT JUST AFTER TAKEOFF THRUST WAS SET. FULL LEFT RUDDER WITH A LITTLE TILLER STRAIGHTENED THE AIRCRAFT OUT. CONTINUED TAKEOFF ROLL WHICH APPEARED NORMAL. AT GEAR RETRACTION, A STRONG BURNISDR F3LA200100122Pylon · gougedDURING C-1 CHECK, INSPECTION REPORTED GOUGE IN NR 1 ENGINE PYLON, AFT OTBD LOWER CORNER. REMOVED GOUGE PER SRM 51-10-2. FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-2.SDR F3LA200100126Skin · damagedDURING C-1 CHECK, INSPECTION REPORTED A 14.5 INCH AREA ON FUSELAGE SKIN LAP AT STR 19R, BS 386-410, SCRATCHED AND GOUGED. REMOVED DAMAGE AT BS 390-404, STR 19R PER SRM 53-30-3, FABRICATED FILLER AND DOUBLER AND INSTALLED PER SRM 53-30-3, 51-20-4, 20-10-18 ANDSDR F3LA200100125Doubler · tornDURING C-1 CHECK, INSPECTION REPORTED NR 2 ENGINE OTBD ENGINE COWL DOUBLER METAL TORN AT LATCH CUTOUT, 5TH LATCH FROM AFT. FABRICATED AND INSTALLED DOUBLER AND STRIKER PLATE PER SRM 51-40-2.SDR F3LA200100121Skin · dentedDURING C-1 CHECK, INSPECTION REPORTED SEVERAL DENTS IN SKIN OF DORSAL FIN FWD OF VERTICAL STABILIZER. FABRICATED AND INSTALLED EXTERNAL REPAIR PER SRM 55-30-6 AND 51-20-1.SDR F3LA200100120Skin · gougedDURING C-1 CHECK, INSPECTION REPORTED GOUGES IN SKIN AND SCRATCHES ON OTBD SIDE OF RT ENGINE PYLON, AFT END AREA ABOVE THRUST REVERSER FAIRING. PERFORMED TYPICAL WEB REPAIR PER SRM 51-40-01 AND 51-30-02.SDR F3LA200100118Door · crackedDURING C-1 CHECK, INSPECTION REPORTED CRACK IN OUTER SKIN OF NR 2 ENGINE TOP OUTBOARD THRUST REVERSER FAIRING DOOR. INSTALLED SCAB PATCH PER SRM 51-40-02.SDR F3LA200100119Nose Cowl · wornDURING C-1 CHECK, INSPECTION REPORTED NR 1 ENGINE NOSE COWL AT 2 O'CLOCK POSITION MATING SURFACE WORN. CUT AWAY DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 54-10-03, 51-20-1 AND MM 51-21-99.SDR F3LA200100124Controller · failedAIR TURN BACK. FLIGHT CREW REPORTED LOUD RUMBLE NOISE NEAR RT. PACK, ASSOCIATED WITH STRONG SMELL. TURNED PACK AND RT. BLEED OFF AND SMELL AND NOISE WENT AWAY. LOW VIBRATION CONTINUED. MAINTENANCE RAN RT. PACK AND COULD NOT DUPLICATE DISCREPANCY. OPENED PASDR F3LA200100114Actuator · failedUPON ARRIVAL, FLIGHT CREW REPORTED "A" SYSTEM HYDRAULIC QUANTITY AND PRESSURE FELL TO ZERO AFTER LANDING. REPLACED NO. 8 GROUND SPOILER ACTUATOR PER MM 27-62-101. PERFORMED OPERATIONAL CHECK, LEAK CHECK AND RIG CHECK. REPLACED NO. 1 AND NO. 2 ENGINE DRIVEN SDR 2001F00470Shield · faultyDURING TAKEOFF OF FLIGHT, THE NOSE GEAR DIDN'T RETRACT, THE AIRCRAFT RETURNED TO SJO STATION. AFTER LANDING, TECHNICIANS PERFORMED INSPECTION OF THE AIRCRAFT AND FOUND THE NOSE GEAR LOCK ACTUATOR DAMAGED, IT WAS REPLACED IAW AMM 32-33-21 AND 32-33-00. ALSO, SDR 2001F00469Actuator · damagedDURING TAKEOFF OF FLIGHT, THE NOSE GEAR DIDN'T RETRACT, THE AIRCRAFT RETURNED TO SJO STATION. AFTER LANDING, TECHNICIANS PERFORMED INSPECTION OF THE AIRCRAFT AND FOUND THE NOSE GEAR LOCK ACTUATOR DAMAGED, IT WAS REPLACED IAW AMM 32-33-21 AND 32-33-00. ALSO, SDR F3LA200100108Coupling · disconnectedAIR TURN BACK. FLIGHT CREW REPORTED FLAPS DID NOT RETRACT AFTER TAKEOFF. LT. TORQUE TUBE COUPLING AT NO. 4 FLAP TRANSMISSION WAS DISCONNECTED. RECONNECTED COUPLING PER MM 27-51-251. ADJUSTED TRAILING EDGE FLAPS PER MM 27-51-01 AND PERFORMED OPERATIONAL TES
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