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 USAA040723Angle · corrodedZEE ANGLE, 8 AREAS, .2500 INCH SPOTS, CORROSION; LEVEL 1; TASK NR C53-202-01, RT ZEE ANGLE FROM STA 727B TO 767. DEFECTIVE PART REPLACED WITH ID PN, ZEE ANGLE SPLICE IAW SRM 53-60-53-201.SDR USAA040682Fitting · crackedPIT - FOUND STRINGER END FITTING CRACKED .25 INCH, STRINGER 15L AFT OF STATION 360. INSTALLED NEW PART PER BOEING DWG 65-17685 ND SRM 51-40-02, 51-10-02, 51-40-03. (M)SDR USAA040681Skin · crackedPIT - FOUND NR 2 SLAT WITH 4 CRACKS .125 INCH, TWO .375 INCH CRACKS AND .0625 INCH CRACK, 4 RIVET HOLES, LOWER SKIN UNDER ACTUATOR ATTACH AREA. INSTALLED FILLER AND DOUBLER PER SRM 57-43-01 FIG 206. (M)SDR USAA040836Angle · corrodedZEE ANGLE, 6 INCHES BY 4 INCHES AREA, CORROSION, LEVEL 1; TASK NR C53-107-01, RT AFT ZEE ANGLE FROM STA 940-990. DEFECTIVE PART REPLACED WITH IDENT PN.SDR USAA040683Floorbeam · corrodedPIT - FOUND FLOORBEAM T-CAP CORRODED, STATION 344, LBL 12 TO RBL 12, 10 PERCENT OF .080 INCH REMOVED, THREE AREAS .020 INCH DEEP. CORROSION LEVEL 1, TASK NR C53-107-01. INSTALLED NEW T-CAP PER SRM 53-10-51. (M)SDR USAA040600Skin · crackedPIT - FOUND SKIN CRACKED, 1.125 INCH, STATION 125.5 RT HORIZ STAB LOWER SURFACE AT AFT SPAR. REMOVED BLIND FASTENERS AND INSTALLED SOLID FASTENERS PER TYPICAL REPAIR 55-10-07B. (M)SDR USAA040722Mount · corrodedMOUNT, 1 INCH BY 1 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, AFT LAV MOUNT, STA 947, RBL25. REMOVED AND REPLACED LAV MOUNT IAW SRM 51-10-2, 51-40-00.SDR USAA040714Skin · delaminatedNR 2 SLAT, 3 INCH BY 3 INCH AREA, DELAMINATION, INBD AND OTBD ENDS LOWER SKIN. REPLACED CORE, INSTALLED DOUBLER IAW SRM 51-70-10.SDR USAA040713Tee Fitting · crackedTEE-CHORD, .2500 INCH LONG, AFT CARGO DOOR, 3RD LOCK FASTENER FROM AFT END OF LOWER TEE CHORD. REPLACED T-CORD ANGLE IAW SRM 52-30-02.SDR USAA040586Pylon · crackedFOUND NACELLE WITH .5 INCH CRACK, LT ENGINE PYLON, NR 1527L ACCESS, OUTBOARD EDGE LIP. DOUBLER INSTALLED PER TYPICAL REPAIR 54-30-07. (M)SDR USAASB04123Fuel Control · malfunctionedMIA - FLT 724 - FLIGHT DEPARTED MIA WITH THE NR 1 ENGINE CSD ON MEL FOR AN OIL LEAK. CON CLIMB-OUT, EN ROUTE TO CLT, THE APU GENERATOR DROPPED OFF LINE AT 700 FEET ABOVE GROUND LEVEL. CREW ATTEMPTED TO RESET THE GENERATOR WITH NO HELP. TWO MINUTES LATER, THSDR USAA040717Skin · chafedLOWER SKIN, 1 INCH LENGTH, CHAFE WEAR, NR 3 SLAT LOWER SURFACE TRAILING EDGE. REMOVED DAMAGED SKIN AND CORE, INSTALLED NEW DOUBLER, FILLER, NEW CORE, TOP DOUBLER, IAW SRM 51-70-10.SDR USAA040715Intercostal · crackedINTERCOSTAL, .5 INCH CRACK IN RADIUS, BETWEEN STA 500E AND 500F, UNDER LT AFT CARGO PIT FLOOR ZEE ANGLE. FABRICATED REPLACEMENT PART IAW SRM 53-30-04, 51-10-02.SDR USAA040710Frame · crackedFRAME, .5 INCH CRACK, BS907, S-8L-S-9L. CUT OUT CRACK, INSTALLED PLUG FILLER AND DOUBLER IAW SRM 53-00-07, FIG 202.SDR USAA040688Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH CRACK, FRAME BS 867 S8R, S9R. CUT OUT CRACK, INSTALLED PLUG FILLER AND DOUBLER PER SRM 53-00-07. (M)SDR USAA040684Web · corrodedPIT - FOUND WEB CORRODED NUMEROUS AREAS, 12 INCHES LONG, AFT CARGO THRESHOLD AND ADJACENT STRAP JUST INBOARD. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 51-10-02. (M)SDR USAA040693Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, FRAME BS 727F, S8L, S9L. CUT OUT CRACK, INSTALLED FILLER AND DOUBLER PER SRM 53-00-07, FIG 202. (M)SDR USAA040691Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, BS 727D, S8R, S9R. CUT OUT CRACK, INSTALLED FILLER PLUG AND DOUBLER PER SRM 53-00-07 FIG 202. (M)SDR USAA040690Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, FRAME FS 747, S8R S9R. CUT OUT CRACK, INSTALLED PLUG FILLER AND DOUBLER PER SRM 53-00-07 FIG 202. (M)SDR USAA040695Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, BS 867, S8L, S9L. CUT OUT CRACK, INSTALLED PLUG FILLER AND DOUBLER PER SRM 53-00-07 FIG 202. (M)SDR USAA040692Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, BS 727B, S8R, S9R. DOUBLER INSTALLED PER SRM 53-00-07 FIG 202. (M)SDR USAA040689Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, FRAME BS 827, S8R, S9R. CUT OUT CRACK, INSTALLED PLUG FILLER AND DOUBLER PER SRM 53-00-07 FIG 202. (M)SDR USAA040694Frame · crackedPIT - FOUND FRAME CRACKED .5 INCH, BS 747, S8L, S9L. CUT OUT CRACK, INSTALLED PLUG FILLER AND DOUBLER PER SRM 53-00-07, FIG 202. 9M)SDR USAASB04121Relay · failedPIT - FLT 1451 - ON CLIMB-OUT FROM PIT, EN ROUTE TO PBI, CREW REPORTED THE STABILIZER TRIM WAS INOPERATIVE IN BOTH ELECTRIC AND MANUAL. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND RSDR USAA040716Skin · delaminatedUPPER SKIN, 1.5 INCH SQ AREA DELAMINATED; NR 4 SLAT IB T/E. REMOVED DELAMINATED TOP SKIN AND CORE, INSTALLED NEW CORE, TOP DOUBLER AND REFINISHED IAW SRM 57-40-02 AND 51-70-10.SDR USAA040712Skin · delaminatedUPPER AND LOWER SKIN, 2 INCH SQUARE AREA, DELAMINATION, NR 4 SLAT CTR AREA NEAR AUX TRACK, TOP AND BOTTOM SKIN. REMOVED DELAMINATED TOP SKIN AND CORE MATERIAL. INSTALLED NEW CORE AND TOP DOUBLERS, REFINISHED IAW SRM 57-43-02.SDR USAA040687Skin · crackedPIT - FOUND FORWARD ENTRANCE DOOR CRACKED TWO PLACES .25 INCH EACH, INTERIOR DOOR SKIN AT 1ST AND 2ND DOOR STOPS. INSTALLED DOUBLER PER TR 52-10-16. (M)SDR USAA040686Splice · crackedPIT - FOUND STRINGER SPLICE CRACKED .25 INCH, STATION 908 AND STRINGER 4L. INSTALLED NEW SPLICE PER SRM 51-40-02 AND 51-40-03. (M)SDR USAA040629Cargo Track · corrodedPIT - FOUND TIEDOWN TRACK CORRODED .5 INCH BY 3 INCH AREA, STATION 727F AT LBBL 17.10. REPLACED SECTION OF TIE DOWN TRACK PER SRM 53-00-53 PAGE 205. (M)SDR USAA040718Skin · damagedTOP SKIN, CORE BOND, 1 INCH SQUARE AREA, NR 1 SLAT IB TE UPPER SURFACE. REMOVED TOP SKIN AND CORE, INSTALLED NEW CORE, TOP DOUBLER IAW SRM 51-70-10 AND 09.SDR USAA040624Skin · chafedPIT - FOUND SKIN CHAFED 1 INCH BY .250 INCH WIDE BY .006 INCH DEEP, STAITON 879 BETWEEN STRINGER 1L AND 2L. INSTALLED DOUBLER, TRIPLER PER SRM 53-00-01 FIG 231. (M)SDR USAA040630Support · corrodedPIT - FOUND SUPPORT ZEE ANGLE CORRODED .5 INCH BY 10 INCH AREA, STATION 727E PLUS 8 INCHES TO STATION 787, LEFT SIDE. REMOVED AND REPLACED ZEE ANGLE PER SRM 51-10-02. (M)SDR USAA040565Skin · crackedPIT - FOUND SKIN CRACKED 2 INCHES, FS 124-126 AFT SPAR LOWER SURFACE LEFT HORIZ STAB. REMOVED BLIND FASTENERS AND INSTALLED SOLID FASTENERS PER TR 55-10-07B. (M)SDR USAASB04118Charger · failedCLT - PILOT REPORTED THE EMERGENCY EXIT LIGHTS IN THE AFT GALLEY ARE BLINKING AND WON'T ILLUMINATE AND STAY ON WHEN SELECTED. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY PACK, P/N 2013-1A. OPS CHECK GOOD. (M)SDR USAA040584Channel · corrodedPIT - FOUND Z-CHANNEL APPROXIMATELY 3 INCHES LONG, NUMEROUS AREAS, RIGHT AFT SERVICE DOOR Z-CHANNEL STAITON 961-992. CORROSION LEVEL 1, TASK NR C53-107-02. REMOVED Z-CHANNEL, CLEANED AND TREATED FOR CORROSION, INSTALLED NEW CHANNEL PER SRM 51-10-02. (M)SDR USAA040626Floor Support · corrodedPIT - FOUND FLOOR SUPPORT WEB CORRODED .5 INCH BY .75 INCH AREA, STATION 847-867 RBL 21 AFT CARGO. INSTALLED NEW WEB PER SRM 53-60-53. (M)SDR USAA040627Support Angle · corrodedPIT - FOUND SUPPORT ANGLE CORRODED 1 INCH BY .5 INCH AREA, AFT CARGO RT TRACK SUPPORT ANGLE ABOVE STRINGER 26R. REMOVED AND REPLACED ANGLE PER SRM 51-40-02. CORROSION LEVEL 1, TASK NR C53-202-01. (M)SDR USAA040720Stringer Clip · crackedCLIP, 1 INCH CRACK, FRAME TO LONGERON CLIP INTERIOR FUSELAGE, STA 344, STR 11R. MFG AND INSTALLED REPLACEMENT CLIP IAW MFG DWG 69-38939.SDR USAA040816Strap · corrodedPIT, Q5, STRAP 1 INCH X 3 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, STA 1016 BL 0. REPLACED STRAP IAW MFG DRAWING 65-46812.SDR USAA040583Channel · corrodedPIT - FOUND RADIAL CHANNEL CORRODED 1 SQUARE INCH, AFT PRESSURE BULKHEAD. REMOVED CORROSION, MANUFACTURED AND INSTALLED RADIAL CHANNEL PER EO 5302V112. (M)SDR USAA040587Skin · crackedPIT - FOUND SKIN CRACKED 1 INCH, LOWER LEADING EDGE SKIN FORWARD OF OUTBOARD ALT SLAT TRACK. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PE SRM 57-43-01, FIG 206. (M)SDR USAA040585Clip · crackedPIT - FOUND SLIP CRACKED .5 INCH, STATION 685 LLT AND S12 SKIN CLIP CRACKED IN RADIUS. REPLACED CLIP PER SRM 51-40-03. (M)SDR USAA040597Tee Fitting · crackedPIT - FOUND LOWER T-CHORD CRACKED 1.25 INCH, AFT CARGO DOOR. REPLACED T-CHORD ANGLE AND LOWER INNER SKIN PER SRM 52-30-02 AND 52-30-01. (M)SDR USAA040592Floor Support · corrodedPIT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 1 INCH WIDE AREA, BETWEEN STATION 967 AND 986.5 AT RBL 18. REPLACED FLOOR SUPPORT PER SRM 51-40-03. (M)SDR USAA040593Floorbeam · corrodedPIT - FOUND FLOORBEAM CORRODED 1 INCH BY 1 INCH WIDE AREA, FS 947 FLOORBEAM TOP FLANGE RBL 0. CORROSION LEVEL 1, TASK NR C53-107-02. REPLACED/SPLICE UPPER FLANGE OF FLOORBEAM PER TYPICAL REPAIR 53-60-02 REV A. (M)SDR USAA040628Floor Support · corrodedPIT - FOUND FLOOR SUPPORT CORRODED 1 INCH WIDE, BETWEEN STATION 947 AND 967 RBL 18. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-10-02. (M)SDR USAA040680Frame · crackedPIT - FOUND FRAME CRACKED .125 INCH, RIVET FAR SIDE AIR RAIL SUPPORT STATION 727F LEFT SIDE. INSTALLED REPAIR ANGLES PER TYPICAL REPAIR 53-10-20A. (M)SDR USAA040596Angle · corrodedPIT - FOUND ZEE ANGLE CORRODED TWO AREAS 1 INCH, WEB SUPPORT AT STATION 992 RBL 24. FABRICATED AND REPLACED ZEE ANGLE PER BOEING DWG PL 69-77477. (M)SDR USAA040591Clip · chafedPIT - FOUND CLIP WITH CHAFE WEAR .75 INCH BY .1875 INCH BY .050 INCH DEEP, STATION 277 BETWEEN S2L AND S3L. REPLACED CLIP PER BOEING DWG 65-49806. (M)SDR USAA040594Mount · corrodedPIT - FOUND LAVATORY MOUNT CORRODED 2 SQUARE INCH AREA, LEFT OUTBOARD LAV MOUNT STATION 947. CORROSION LEVEL 1, TASK NR C53-107-02. REPLACED LAV MOUNT PER SRM 51-10-00. (M)
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