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 USAA051098Bracket · crackedFOUND CRACK STA 500G, S28R. FAB`D NEW ANGLE FROM 2024-T3 .040 PER DWG 69-73527 IAW SRM 51-10-02, DEFECT SIZE: .250" CRACK IN RADIUS.SDR USAA051092Skin · damagedSTA 200-210, S-22R - S-23R, 10 BY 8 DOUBLER INSTALLED IAW SRM 53-10-01, DEFECT SIZE: AT STA 200-210, S22R THRU S-23R, MEASURES 10 BY 8.SDR USAA051122Door Frame · crackedFOUND CRACK FWD SVC DOOR, FWD FRAME AT UPPER DOOR STOP FTG LWR O/B CRNR, STA 296 S-8R-10. REMOVED DAMAGED FRAME AND INSTALLED FRAME PIN PER BOEING DWG 65-45807 AND 65C34778, SRM 51-10-02, 51-40-DEFECT SIZE: 1.25".SDR SB05117Power Supply · inoperativeMCO - MAINTENANCE REPORTED THE EMERGENCY EXIT SIGNS FOR THE AFT GALLEY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT GALLEY POWER SUPPLY ALONG WITH THE BATTERY PACK. OPERATIONAL CHECK GOOD.SDR USAA051087Floor Support · crackedFLOOR SUPPORT CRACKED BETWEEN STATION 380 AND 400, BL0. FABRICATED AND INSTALLED NEW ANGLE, DEFECT SIZE: .125".SDR USAA051089Fitting · corrodedLT HORIZONTAL STAB LUG 3 FWD CLEVIS. REMOVED CORROSION FABRICATED AND INSTALLED NEW BUCHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 3".SDR USAA051088Fitting · corrodedLT HORIZONTAL STAB FWD SPAR FWD CLEVIS L1 LUG. REMOVED CORROSION FABRICATED AND INSTALLED NEW BUCHING IAW SRM 55-10-10, DEFECT SIZE: 1"X3".SDR USAA051085Skin · crackedLOWER SKIN, OUTBOARD END CRACKED. INSTALLED DOUBLER, IAW BOEING 737-400, SRM 57-43-01 DEFECT SIZE: 1.5 INCH.SDR USAA051086Spar · delaminatedINBOARD END OF RT AILERON FRONT SPAR. TRIMMED AND SEALED IAW 57-50-22 DEFECT SIZE: 1 X 3 INCH.SDR SB05113Indicator · faultyCLT FLT440 ON CLIMBOUT FROM CLT, AIRCRAFT EXPERIENCED AN ASYMMETRICAL FLAP INDICATION. ONE FLAP INDICATED ZERO UNITS WHILE THE OTHER FLAP INDICATED ONE UNIT. AIRCRAFT DID NOT EXPERIENCE ANY ROLL OR ADVERSE CONDITION ASSOCIATED WITH THE INDICATION. CREW SDR USAA051083Stringer · crackedFS 380-400 AT STR 4L CRACKED. FABBED PARTS, INSTALLED REPAIR PER SRM 51-40-02, DEFECT SIZE: 1 INCH CRACK.SDR USAA051082Plate · corrodedCORROSION LT DECK PLATE AT STA 1016 FWD OF PRESS BULKHEAD. REMOVED DAMAGED AREA PER SRM 52-70-13, FABBED REPAIR DOUBLER, FILLER, INSTALLED REPAIR, DEFECT SIZE: 2' APPROX EXFOLIATION CORROSION.SDR USAA051081Channel · corrodedCORROSION BETWEEN BS 957-993 LBL 48. REMOVED & REPLACED CHANNEL PER SRM 51-40-02, 51-40-05, DEFECT SIZE: 26"L X 2"W X .030"D.SDR USAA051080Support Angle · crackedRT WING T/E SUPPORT ANGLE, JUST INBOARD OF NR 6 SPOILER CRACKED. NEW PART SUPPORT ANGLE INSTALLED PER SRM 57-53-71 & 51-40-02, DEFECT SIZE: 0.050 INCH.SDR USAA051079Intercostal · bentSTA 787-807, STR 24L BENT. FABBED PART, INSTALLED INTERCOSTAL PER SRM 51-40-02, DEFECT SIZE: 1.5 INCH BENT.SDR USAA051078Channel · corrodedCORROSION BS 285 - BS 344 AT SUPPORT CHANNEL. INSTALLED SUPPORT CHANNEL PER SRM 5T1-40-00, DEFECT SIZE: 1 X 0.050 INCH.SDR USAA051084Support · corrodedCORROSION STA 993 AT LEFT SIDE. FABBED PART AND INSTALLED PER SRM 51-40-25, DEFECT SIZE: 4.6 INCH.SDR USAA051069Bushing · corrodedUNIVERSAL ASSY AND LWR DRAG STRUT BUSHINGS IN RT MAIN GEAR CORRODED. REMOVED CORROSION AND INSTALLED NEW BUSHINGS IAW EA 96880, DEFECT SIZE: 1 X 3 INCH.SDR USAA051068Skin · delaminatedUPPER SKIN OF FLAP T/E WEDGE DELAMINATED. REMOVED PREVIOUS REPAIR AND FABRICATED AND INSTALLED NEW REPAIR IAW SRM 51-70-10. DEFECT SIZE: 2 INCH DIAMETER DELAMINATION.SDR USAA051064Skin · gougedAFT CARGO DOOR AT UPPER FWD CORNER AREA. REMOVED DAMAGE AND INSTALLED REPLACEMENT STIFFENER AND REPAIR DOUBLER PER EA 96812 AND DWG 65-47952. DEFECT SIZE: .250 GOUGE INTO THE SKIN DOUBLER AND TEE STIFFENER AND PULLEY BRACKET STICKER NR 1888.SDR USAA051065Angle · damagedFUESLAGE STATION 344 RIGHT HAS GAP. FABRICATED SHIMS AND FILLERS AND INSTALLED PER EA 96820. DEFECT SIZE: .275 INCH GAP BETWEEN THE RIGHT CREASE BEAM INNER CHORD ANGLE AND FLOORBEAM.SDR SB05111Uplock Sensor · faultyCLT - FLT415 - ON CLIMB-OUT FROM CLT, CREW REPORTED THE RIGHT MAIN LANDING GEAR RED AND GREEN LIGHT ILLUMINATED WHEN GEAR HANDLE WAS PLACED IN THE UP AND/OR OFF POSITION. CREW MOVED GEAR HANDLE TO DOWN POSITION AND RECEIVED A NORMAL GEAR INDICATION OF THREE SDR SB05110Battery Pack · dischargedCLT - MAINTENANCE REPORTED THE FORWARD ENTRY AREA EMERGENCY LIGHTS WERE DIM. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD.SDR SB05107Battery Pack · dischargedPIT - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHTS FROM ROWS 12 THROUGH 19 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND FUSE. OPERATIONAL CHECK GOOD.SDR SB05105Cable · out of adjustAFTER TAKEOFF FROM CLT, CREW REPORTED MLG HANDLE WOULD NOT MOVE UP TO RETRACT THE GEAR. CREW LOWERED MLG HANDLE TO DOWN POSITION & RECEIVED A NORMAL GEAR INDICATION OF 3 GREEN LIGHTS. FLT RETURNED TO FIELD. DURING APPROACH, CREW REPORTED FLAPS WOULD NOT EXTSDR SB05104Relay · failedCLT - FLT102 - AFTER TAKEOFF FROM CLT, THE LANDING GEAR HANDLE WOULD NOT MOVE PAST THE OFF POSITION. THE WARNING HORN WAS SOUNDING OFF ALSO. CREW DID NOT ATTEMPT THE OVER-RIDE TRIGGER BUT LOWERED THE LANDING GEAR AND RECEIVED A NORMAL GEAR INDICATION OF THRESDR SB05100Wire · brokenPIT - MAINTENANCE REPORTED THE AFT LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT AND THE AISLE EMERGENCY EXIT SIGNS AT ROWS 10 ABC AND 11 ABC WERE INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT CEILING EMERGENCY EXIT SIGN AT EXIT WINDOWS AND REPLACED FUSES INSDR USAAA051049Floor Support · corrodedCLT - FOUND FLOOR SUPPORT STRINGER CORRODED, RBL 13.80 BETWEEN STATION 794 AND 847. CORROSION LEVEL 1. FABRICATED NEW FLOOR SUPPORT STRINGER AND INSTALLED PER TR 53-10-08 AND 51-10-02. (M)SDR USAA051050Web · damagedRIGHT CREASE BEAM WEB AT ATTACHMENT TO FRAME 344 HAS HOLE. COMPLIED WITH EA 9682 AND BOEING DWG 65-45875, DEFECT SIZE .1875 INCH.SDR USAA051049Floor Support · corrodedRBL 13.80 BETWEEN STA 794.0 AND 847.0 CORRODED. FABRICATED NEW FLOOR SUPPORT STRINGER AND INSTALLED PER TR 53-10-08 AND 51-10-02, DEFECT SIZE: LEVEL 1.SDR USAA051051Skin · delaminatedRUDDER LT SIDE MID SECTION AREA HAS DELAMINATION. COMPOSITE REPAIR IAW SRM 51-70-05, DEFECT SIZE: 2 INCHES.SDR USAA051038Structure · crackedINTERNAL FUEL TANK AT BOTTOM SKIN AT WBL 13550 CRACKED. FABRICATED NEW T-SECTION & INSTALLED REPAIR T-SECTION IAW EA 96796, DEFECT SIZE: 2.250 INCH.SDR SB05096Wire · brokenMAINTENANCE REPORTED THE LAST 2 ROWS OF FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE RE-SPLICED POWER WIRE IAW WPM 20-10-13. OPS CHECK GOOD.SDR USAA051029Splice · crackedBFM - Q2 - STRINGER SPLICE, .250 INCH, STA 907, STR; CRACK ON FASTENER HEAD, STA 907, STRINGER CRACK ON FASTENER HEAD. INSTALLED REPAIR/ FAB SPLICE ON STRINGER IAW SRM. (K)SDR USAA051028Shear Tie · crackedBFM - Q2 - SHEAR TIE CLIP, .050 INCH CRACKED, STA 277, STR 8L TO 9L SHEAR TIE CLIP. INSTALLED REPAIR PART, SHEAR CLIP, STA 277 IAW SRM. (K)SDR USAA051027Gate · corrodedBFM - Q2 - DOOR GATE SKIN, 29 INCH L X .250 INCH W, CORROSION; LEVEL 2; TASK C53-100-01, AFT ENTRY DOOR BOTTOM GATE LOWER EDGE OF SKIN. REMOVED AND REPLACED AFT ENTRY DOOR BOTTOM GATE IAW MM, SRM. (K)SDR USAA051026Shear Tie · crackedBFM - Q2 - SHEAR TIE CLIP, .250 INCH CRACK, STA 277, SHEAR TIE CLIP, STR 9L TO 10L. INSTALLED SHEAR CLIP ON STR STA 277 IAW SRM. (K)SDR USAA051025Stringer Clip · crackedBFM - Q2 - STRINGER CLIP, .250 INCH CRACK, STA 277; STR 9 L STR CLIP. INSTALLED REPAIR STRINGER CLIP STA 907 IAW SRM. (K)SDR USAA051024Floorbeam · corrodedBFM - Q2 - FLOORBEAM UPPER CHORD, 50 INCH CORROSION; NO LEVEL OR TASK; FS 986.5, LBL 0 TO LBL 50 INCH. FABED PART FLOORBEAM UPPER CHORD, INSTALLED IAW SRM. (K)SDR USAA051023Intercostal · crackedBFM - Q2 - FLOORBEAM INTERCOSTAL, .250 INCH CRACK, BET STA 328, 344 CABIN FLOORBEAM. INSTALLED REPAIR DOUBLER, TREATED AND PRIMED IAW SRM. (K)SDR USAA051022Frame · crackedBFM - Q2 - FLAME, 2.45 INCH LT, CRACKED FWD CARGO FRAME BS 500 BL 0. TRIM OUT CRACK, FAB REPAIR, INSTALLED DOUBLER IAW EA. (K)SDR SB05094Light · inoperativeMAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT ROW 11 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD.SDR USAA051003Wedge · delaminatedCLT - FOUND WEDGE SKIN AND CORE DELAMINATED 2 INCHES BY 3 INCHES, RT L/B T/E FLAP WEDGE AT LB END. REMOVED AND REPLACED SKIN AND CORE AS REQUIRED IAW SRM 51-70-10. (M)SDR USAA051007Splice · crackedCLT - FOUND SPLICE CHANNEL 1 INCH, BS 360 S15L STRINGER. REMOVED DAMAGED SPLICE AND INSTALLED NEW SPLICE P/N 65-61777-5 IAW SRM 51-40-02. (M)SDR USAA0514007Channel · crackedCLT - Q1 - SPLICE CHANNEL, 1 INCH CRACK, BS 360, S-15L STRINGER SPLICE CHANNEL. REMOVED DAMAGED SLICE AND INSTALLED NEW SLICE IAW SRM. (K)SDR USAA051004Bracket · crackedCLT - Q1 - BRACKET, 1 INCH, CRACK, STA 360, STR 7L BRACKET. REMOVED DAMAGED BRAKET, FRABRICATED NEW BRACKET AND INSTALLED, ISW SRM AND DWG. (K)SDR USAA050997Intercostal · crackedCLT - FOUND CHORD CRACKED .4 INCHES, UPPER CHORD ON INTERCOSTAL BETWEEN BS 380 AND 400, RBL 11. FABRICATED AND INSTALLED NEW CHORD IAW BOEING DRAWING 65C33655 AND SRM 51-40-02. (M)SDR USAA050998Intercostal · crackedCLT - FOUND CHORD CRACKED .3 INCH, UPPER CHORD ON INTERCOSTAL BETWEEN BS 380 AND BS 400 AT BL 0. FABRICATED AND INSTALLED NEW CHORD IAW BOEING DRAWING 69-35365 AND SRM 51-40-02. (M)SDR USAA050999Angle · corrodedCLT - FOUND ZEE ANGLE CORRODED 3.5 INCHES, SCREW HOLES ON THE SURFACE OF THE LEFT SUPPORT ZEE ANGLE AT LBL 20.20. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW 53-40-01. (M)SDR SB05089Charger · inoperativePIT - MAINTENANCE REPORTED FOUR EMERGENCY LIGHTS AT SEAT ROWS 7 THROUGH 10 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED CHARGER ASSEMBLY M1134 AND THE BATTERY PACK. OPERATIONAL CHECK GOOD.
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