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 USAA050988Support · corrodedBFM, Q2, ZEE SUPPORT, 100 INCHES, CORROSION; LEVEL 1 TASK C53-202-01, AFT CARGO COMPT RT SUPPORT ZEE STA 727C-747. FABRICATED AND INSTALLLED NEW ZEE SUPPORT IAW SRM. (K)SDR USAA050989Floor Support · crackedBFM - Q2 - CHANNEL, 1 INCH AND 1.25 INCH, CRACKS (2), PAX CABIN FLOOR SUPPORT (CHANNEL) AT STA 540 LBL 1. DEFECTIVE PART REPLACED WITH IDENT PART. (K)SDR USAA050987Floorbeam · crackedBFM, Q2, TEE CHORD, .5 INCH CRACK, CABIN FLOORBEAM AT STA 312 RBL 35. FABRICATED NEW UPPER CHORD, LOCATED DRILLED AND INSTALLED ALL REPAIR PARTS IAW SRM. (K)SDR USAA050970Skin · crackedCLT - Q1 - SKIN, 1 INCH CRACK, STA 727D, BELOW S-23L (NEAR LIGHT). CUT OUT CRACK, FABRICATED DOUBLER AND FILLER, INST 12 INCH X 12 INCH DOUBLER IAW SRM. (K)SDR SB05087Wire · brokenPHL - MAINTENANCE REPORTED, THE EMERGENCY EXIT SIGN, AT SEAT ROW 5, INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. OPERATIONAL CHECK GOOD.SDR SB05086Light · inoperativeMAINTENANCE REPORTED THE EMERGENCY LIGHT ASSEMBLY AT THE LEFT OVERWING EXIT ROW INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.SDR SB05085Wire · shortedCLT MAINTENANCE REPORTED THREE OVERWING EXIT HATCH HANDLE LIGHTS INOPERATIVE ON RIGHT-HAND SIDE. MAINTENANCE REPAIRED SHORTED HATCH HANDLE LIGHT L751 WIRE BEHIND EXIT LIGHT ASSEMBLY. ALSO, REPLACED FUSE IN M1497 POWER SUPPLY. OPERATIONAL CHECK GOOD.SDR SB05084Power Supply · inoperativeMAINTENANCE REPORTED THE AFT LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY. OPERATIONAL CHECK GOOD.SDR USAA050901Support Fitting · crackedCLT - Q5 - AFT SUPPORT FITTING, 1 INCH, CRACKED, FASTENER HOLE AT MLG BEAM ATTACH PT TO AFT SPAR ON AFT SUPPORT FITTING UP CHRD. REPAIR OF FITTING INCLUDED REAMING OF DISCREP HOLE, SHIMMING IAW EA. (K)SDR USAA050899Skin · wornCLT - Q - SKIN, 12 INCHES X .250 INCH X .015 INCH, SKIN WEAR, BS870, WL306.5, LBL3. INSTALLED REPAIR DOUBLER AND INSTALLED NEW RUB STRIPS IAW EA, WEIGHT CHANGE OF 1.5 LBS. (K)SDR USAA050882Angle · crackedCLT - Q5 - ANGLE, .375 INCH, CRACKED AT STA 601LT SIDE BODY WING TERMINAL FORGING ANGLE CRACKED ON AFT SIDE. REMOVED DAMAGED AND INSTALLED REPAIR ANGLE IAW SRM. (K)SDR USAA050881Balance Arm · wornCLT - Q5 - RUDDER BALANCE ARM, 1.6 INCH WEAR, RUDDER BALANCE ARM. BLENDED AREAS OF WEAR ON RUDDER BALANCE ARM SRM. (K)SDR USAA050853Pressure Panel · crackedCLT - FOUND PRESSURE DECK CRACKED .750 INCH, STATION 664 LBL 32.5. REMOVED DAMAGED DAMAGED AREA, INSTALLED REPAIR IAW SRM 53-60-04. (M)SDR USAA050850Splice · corrodedCLT - FOUND SPLICE STRAP CORRODED .5 INCH, AFT CARGO FLOOR PANEL SPLICE STRAP. FABRICATED NEW STRAP AND INSTALLED IAW SRM 51-10-02. (M)SDR USAA050851Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, CENTER AISLE FRAME BETWEEN STATION 380 AND 400. FABRICATED AND INSTALLED NEW PART IAW SRM 51-10-02. (M)SDR USAA050826Angle · crackedCLT - FOUND ANGLE CRACKED .750 INCH, STATION 616 LT SIDE BODY WING TERMINAL FORGING ANGLE, CRACKED ON FORWARD SIDE. REMOVED DAMAGE AND INSTALLED REPAIR ANGLES IAW RT 53-62-01. (M)SDR USAA050828Skin · lightning strikeCLT - FOUND SKIN WITH LIGHTNING STRIKE .125 INCH BY .125 INCH, STATION 500B, 2 INCHES BELOW STRINGER 18L AND 12 AFT. FASTENER INSTALLED IN SKIN IAW 53-00-01 FIG 219. (M)SDR USAA050829Skin · lightning strikeCLT - FOUND SKIN WITH LIGHTNING STRIKE, STATION 469, 4 INCHES ABOVE STRINGER 21L. FASTENER INSTALLED IN SKIN IAW 737 SRM 53-00-01 FIG 219. (M)SDR USAA050830Splice · crackedFOUND SPLICE CRACKED .5 INCH, BS 907, STRINGER S4R. REPLACED SPLICE WITH NEW PART IAW SRM 51-10-02. (M)SDR USAA050831Splice · crackedCLT - FOUND SPLICE CRACKED .5 INCH, BS 907, STRINGER S4L. REPLACED SPLICE WITH NEW PART IAW SRM 51-10-02. (M)SDR USAA050836Floor Support · corrodedCLT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 1 INCH, FORWARD CABIN FLOOR STRUCTURE STATION 310 RBL 13 TOP OF SUPPORT INBOARD SCREW HOLE. REMOVED DAMAGED STIFFENER, FRILLED UP AND INSTALLED PART IAW SRM 53-10-51 FIG 101, PAGE 105. (M)SDR USAA050837Fitting · corrodedFOUND FITTING CORRODED .25 BY .25, HORIZONTAL STAB CTR SECTION, RT SIDE, FORWARD SPAR. SPOT FACED FORWARD FACE OF FORWARD LUG IAW 55-10-10. (M)SDR USAA050824Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1.5 INCH BY 1.5 INCH, STATION 312 RBL 10. NEW TEE CAP INSTALLED IAW SRM 53-10-01, AND SRM 53-00-51. (M)SDR USAA050825Intercostal · corrodedCLT - FOUND INTERCOSTAL CORRODED 1 INCH BY 1 INCH, BS 306 LBL 11 FORWARD CABIN FLOOR SUPPORT. INSTALLED NEW INTERCOSTAL IAW SRM 53-10-51, 51-10-02, 51-40-02. (M)SDR USAA050818Door Frame · crackedCLT - C3 - FWD SERVICE DOOR, .6 INCH CRACK, FWD SERVICE DOOR FRAME LOWER AFT CORNER AFT LIGHTING HOLE. INSTALLED DOUBLER IAW EA. (K)SDR USAA050817Skin · crackedCLT - C3 - SKIN, .75 INCH CRACK, RT PYLON AT CORNER OF CUTOUT FOR PANEL NR 5828R, NAC, STA 166.5. INSTALLED DOUBLER IAW TYPICAL REPAIR SRM. (K)SDR USAA050816Floor Support · corrodedCLT - Q5 - FLOOR SUPPORT, 2 INCH X 2 INCH CORROSION, STA 312-328, RBL 13. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STIFFENER SUPPORT IAW SRM. (K)SDR USAA050815Stiffener · corrodedCLT - Q5 - FLOOR STIFFENER, 2 INCH X 16 INCH CORROSION, STA 312-328, LBL12. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STIFFENER IAW SRM. (K)SDR USAA050814Floor Support · corrodedCLT - Q5 - STA 328-344, LBL9, 2 INCH X 2 INCH, CORROSION, FLOOR SUPPORT. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STIFFENER IAW SRM. (K)SDR USAA050801Skin · gougedCLT - Q5 - FLAP SKIN, .500 X 3 INCH GOUGE, I/H OB MID FLAP BOTTOM SKIN 53 INCHES FROM IB END. REPAIRED DAMAGED SKIN IAW SRM. (K)SDR USAA050800Skin · wornMID FLAP SKIN, .500 WIDE X 4 INCHES LONG, WORN AREA, LT OB MID FLAP BOTTOM SIDE 68 INCH FROM IB END. REMOVED DAMAGE AND INSTALLED NEW TRIPLER DOUBLER IAW SRM. (K)SDR USAA050786Bulkhead · crackedFOUND BULKHEAD WEB WITH TWO CRACKS .125 INCH, WL 234, RBL 10.0 BS 178. INSTALLED DOUBLER PER EO 5300V153 AND SRM 53-10-08. (M)SDR USAA050784Skin · damagedCLT - FOUND SKIN WITH HOLE 10 INCH BY 2 INCH, STATION 887 TO STATION 908 BETWEEN STRINGER 21R AND STRINGER 22R. DOUBLER AND TRIPLER INSTALLED IAW SRM 53-00-01 FIG 231 DETAIL VIII. (M)SDR USAA050776Skin · crackedFOUND SKIN CRACKED 1 INCH, BS 727D. INSTALLED DOUBLER IAW SRM 53-00-01, FIG 231 DETAIL XI. (M)SDR USAA050766Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .5 INCH BY .5 INCH, BS 986.5, WL 208, RBL 24.75 TO SIDE OF BODY. CLEANED CORROSION, BLENDED, TREATED, PRIMED AND PAINTED PER SRM 53-60-51 AND IN-59-81613-2. (M)SDR USAA050765Skin · damagedCLT - FOUND SKIN AND TEAR STRAP 2 INCHES, BS 344 BETWEEN STRINGER S22 AND S23R. FABRICATED FROM 2024T3 DOUBLER .032, TRIPLER .050, STRUCTURAL FILLER .071 IAW SRM 53-00-01 FIG 231. (M)SDR USAA050751Skin · wornCLT - FOUND FUSELAGE SKIN WITH WORN .300 INCH LONG BY L.004 INCH WIDE BY .0135 INCH DEEP, AT BASE OF VERTICAL FIN, AFT END BODY CLOSURE ANGLE BODY STATION 1088. BLEND AREA OUT PER EA 96634 AND TREAT AREA. (M)SDR USAA050744Wedge · delaminatedCLT - FOUND NR 1 LE SLAT WEDGE DELAMINATED 5 INCHES BY 3 INCHES, OUTBOARD END OF SLAT TRAILING EDGE WEDGE. COMPOSITE REPAIR IAW EA NR 96573. (M)SDR USAA050746Support · damagedCLT - FOUND SUPPORT WITH 6 INCHES VARIOUS DAMAGE, BS 685. REPAIR DOUBLER INSTALLED IAW SRM 51-70-11. (M)SDR USAA050737Skin · crackedCLT - Q3/QX4 - WING L/E SKIN, .2500 INCH CRACK AND DENT; L/E SKIN ABOVE IB KREUGER FLAP. REMOVED DAMAGE AND INSTALLED DOUBLER IAW SRM. (K)SDR USAA050736Angle · corrodedCLT - Q3/QX4 - Z ANGLE, .25 INCH X .25 INCH CORROSION; LEVEL 1; TASK C53-107-01, LBL 60, STA 951-986. REMOVED AND REPLACED REPAIR PARTS IAW EA. (K)SDR USAA200506001Skin · cracked3.2 INCH CRACK FOUND AT BS 727E S23R. REPAIR DOUBLER PER SRM 53-00-01.SDR SB05066Circuit Breaker · trippedUPON LOWERING LANDING GEAR, CAPTAIN REPORTED THE NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED. CREW ACCOMPLISHED A FLYBY OF THE TOWER WHEREAS THE GEAR WAS CONFIRMED DOWN. CREW THEN NOTICED THE AIR/GROUND RELAY AND LIGHTS CIRCUIT BREAKER WAS POPPED. CREW RESETSDR USAA050718Wedge · crackedCLT - FOUND SKIN CRACKED, RT INBOARD MID FLAP WEDGE. INSTALLED DOUBLR IAW RM 51-70-10. (M)SDR USAA050717Angle · corrodedCLT - FOUND TRANSITION ANGLE CORRODED 1 INCH, RT TRANSITION ANGLE IN AFT CARGO COMPARTMENT STATION 727B-947. FABRICATED AND INSTALLED REPAIR PIECES IAW 737-400 SRM 56-60-53 AND 51-10-02. (M)SDR USAA050713Beam · crackedCLT - FOUND STUB BEAM CRACKED .375 INCH, UPPER CHORD LT 578 ATTACH POINT TO CREASE BEAM, INNER CHORD LBL 64 FROM RIVET. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-20=05 AND EA 96603. (M)SDR USAA050712Angle · corrodedCLT - FOUND TRANSITIONAL ANGLE CORRODED .3125 INCH, FS 727B-847. FABRICATED AND INSTALLED TRANSITION ANGLE AND COVE PANEL IAW 737 SRM 57-43-01, 53-60-53. (M)SDR USAA050708Stringer Clip · crackedCLT - FOUND TIE CLIP CRACKED .6 INCH, STRINGER TIE CLIP STATION 294.5 STRINGER 13L. FABRICATED AND INSTALLED NEW TIE CLIP IAW BOEING DRAWING 62-01633. (M)SDR USAA050710Clip · crackedCLT - FOUND SUPPORT CLIP CRACKED, AFT CARGO COMPARTMENT SUPPORT CLIP AT STATION 771 STRINGER 26R. FABRICATED AND INSTALLED A NEW CLIP IAW BOEING DRAWING 69-43445. (M)SDR USAA050711Beam · crackedCLT - FOUND STUB BEAM CRACKED .375 INCH, STATION 578 LBL 64. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-20-05. (M)
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