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 USAA051159Flange · crackedFOUND FUSELAGE CRACKED STATION 559 STRINGER 13L. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE IAW EA 96912, DEFECT SIZE: .7".SDR USAA051158Stiffener · corrodedFOUND STIFFENER CORRODED FUSELAGE STATION 336 RBL 51 TO 59. REMOVED AND REPLACED STIFFENER IAW SRM 51-40-0, DEFECT SIZE: .75 BY 5".SDR USAA051157Skin · wornFOUND FLAP SKIN WORN OUTBOARD MID FLAP LEADING EDGE SKIN AT WING STATION 196.8461. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-53-1, REPAIR 8 DEFECT SIZE: 3.5X.75".SDR USAA051156Angle · corrodedLEFT TRANSITION ANGLE BS 727 - 835 FOUND CORRODED. REPLACED ANGLE IAW SRM 53-60-53, DEFECT SIZE: CORROSION IN AREA'S FROM BS 727E TO 835.SDR USAA051155Skin · delaminatedINBD END OF FLAP DELAMINATED. REMOVED DAMAGE AND REPAIRED IAW SRM 51-70-10, DEFECT SIZE: 6" BY 2".SDR USAA051152Angle · crackedANGLE CRACKED STA 360 AND STR 9L. FABRICATED NEW ATTACH ANGLE AND INSTALLED IAW DWG 69-48985, SRM 1-10-02, DEFECT SIZE: .50".SDR USAA051153Clip · crackedCLIP CRACKED BS 772, RBL 20, AFT CARGO COMPARTMENT. REPLACED CLIP WITH NEW PART IAW SRM 51-10-02, DEFECT SIZE: .5".SDR USAA051144Stringer · crackedSTRINGER CRACKED STA 303.9, S10L. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED PER EA 96914, DEFECT SIZE: .25".SDR USAA051145Skin · wornWORN AREA OB FLAP LEADING EDGE AT IB END. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW SRM 57-53-01 REPAIR 8 PG 204, DEFECT SIZE: 1".SDR USAA051146Attach Angle · crackedFOUND ANGLE CRACKED, STA 967 ABOVE AFT ENTRY DOOR. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW SRM 53-00-07, DEFECT SIZE: .250".SDR USAA051147Sill · corrodedZEE ANGLE AT AFT ENTRANCE DOOR SILL AROUND NUTPLATES BETWEEN STA 967 AND 986. REMOVED DAMAGE AND REINSTALLED FABRICATED REPAIR PARTS IAW SRM 51-70-11, DEFECT SIZE: 20".SDR USAA051148Skin · crackedFOUND SKIN CRACKED IL I/B MID FLAP 39" FROM O/B END. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 57-53-01, DEFECT SIZE: .25".SDR USAA051149Skin · crackedLT WING SKIN FWD OF FRONT SPAR O/B SIDE OF PYLON. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR PIECES, DEFECT SIZE: 1".SDR USAA051150Skin · crackedNR 1 ENG PYLON, ACCESS PNL OPENING NR 5727L. REPAIR DOUBLER INSTALLED IAW TYP REP 54-30-07, DEFECT SIZE: .400".SDR USAA051151Skate Angle · wornRIGHT SIDE BS 1016 L/E STATION 0.0. FABRICATED AND INSTALLED A NEW SKATE ANGLE IAW TYP REP 53-20-05A, DEFECT SIZE: .5" X 1.3".SDR SB05122Seal · missingCLT - FLT 1169 DURING CRUISE, AT FL240, THE AIRCRAFT BEGAN LOSING CABIN PRESSURIZATION WHILE OPERATING ON ONE PACK. CABIN PRESSURE COULD NOT BE STABILIZED. FLIGHT DESCENDED TO 10,000 FEET WHERE CABIN PRESSURE DROPPED TO 7,000 FEET. FLIGHT CONTINUED ONTO CSDR SB05121Battery Pack · dischargedCLT - DURING EMERGENCY LIGHT OPERATIONAL TEST, MAINTENANCE REPORTED THE LEFT AFT OVERWING EXIT LIGHT ON THE SIDEWALL EXTINGUISHED AND WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK FOR CHARGER ASSEMBLY M1435 PER MM 33-51-51. OPERATIONAL TSDR USAA051143Skin · crackedFOUND LT WING SKIN CRACKED, FWD OF FRONT SPAR O/B SIDE OF PYLON. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR PIECES IAW TR 57-41-023.SDR USAA051140Intercostal · crackedINTERCOSTAL CRACKED LBL 45 BETWEEN STA 312 AND 328. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02, DEFECT SIZE: .250" CRACK.SDR USAA051141Intercostal · crackedINTERCOSTAL CRACKED, LBL 45 BETWEEN STA 328 AND 344. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02, DEFECT SIZE: .375" CRACK.SDR USAA051142Frame · crackedFRAME CRACKED BS 380 JUST BELOW STR 8L. CUT OUT CRACKED AREA, INSTALLED REPAIR PER T/R 53-10-20B, DEFECT SIZE: APPROX 1 INCH CRACK.SDR USAA051133Skin · crackedFOUND FUSELAGE CRACKED, BS 380 JUST BELOW S-8L. CUTOUT CRACKED AREA INSTALLED REPAIR PER T/R 53-10-20B, DEFECT SIZE: 1".SDR USAA051134Intercostal · corrodedFOUND INTERCOSTAL CORRODED BETWEEN STATION 312 AND 328. MAJOR REPAIR IAW SRM 51-40-02, DEFECT SIZE: 3/16".SDR USAA051135Floorbeam · corrodedFOUND FLOORBEAM T-CAP CORRODED STATION 312 LBL 10 TO RBL 36. T-CAP REPLACED IAW SRM 53-10-51-2R-5, DEFECT SIZE: 2" X 6".SDR USAA051136Stringer Clip · crackedFOUND TIE CLIP CRACKED STA 500 G STRINGER 8R. DEFECTIVE PART REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STRINGER TIE CLIP IAW SRM 51-40-02, DEFECT SIZE: .250".SDR USAA051137Splice · crackedFOUND STRINGER CRACKED BS 360 STRINGER 15L. REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STRINGER SPLICE IAW SRM 51-40-02, DEFECT SIZE: .250".SDR USAA051138Stringer Clip · crackedFOUND TIE CLIP CRACKED, BS 500F S-8R. REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STRINGER TIE CLIP IAW SRM 51-40-02, DEFECT SIZE: .250".SDR USAA051139Stringer Clip · crackedTIE CLIP CRACKED, STA 787L STRINGER 4L. REPLACED WITH IDENTICAL PART, REMOVED AND REPLACED STRINGER TIE CLIP IAW SRM 51-40-02, DEFECT SIZE: .025.SDR SB05118Connector · burnedBOS - FLT822 - ON FINAL APPROACH TO BOS, THE TR2 AND TR3 CIRCUIT BREAKERS POPPED. CREW INITIATED A GO-AROUND THE FIELD AND POWERED UP THE APU. EVERYTHING WAS NORMAL FOR LANDING. UPON SECOND FINAL APPROACH, THE SAME THING HAPPENED AS WITH THE FIRST APPROACH.SDR USAA051094Splice · damagedFOUND SPLICE BS907, STRINGER S4R. REMOVED DAMAGED PARTS, AND INSTALLED NEW PARTS IAW SRM 51-10-02, DEFECT SIZE: 1/2" CRACK.SDR USAA051108Attach Fitting · corrodedFOUND CORROSION LT HORIZ STAB L5 BUSHING LUG FACE. REMOVE CORROSION AND BUSHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 2" AREA OF CORROSION.SDR USAA051132Pressure Panel · crackedFOUND CRACK STA 665, LBL 30. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW TR 53-60-04, DEFECT SIZE: 1.0" CRACK.SDR USAA051099Attach Bracket · crackedFOUND CRACK STA 500G, S28L. FAB NEW ANGLE FROM 2024-T3 .040 PER DWG 65C33472 IAW BOEING DWG 69-73527, SRM 51-10-02, DEFECT SIZE: .250" CRACK IN RADIUS.SDR USAA051100Stringer · crackedFOUND CRACK PRODUCTION SEAM AT STA 907 IN STR 4L. REMOVED CRACKED STRINGER SPLICE, INST NEW P/N 1122424 STR SPLICE, CLIP AND LADDER IAW SRM 51-10-02, DEFECT SIZE: PRODUCTION SEAM AT STA 907 IN STR 4L. (MARKED)SDR USAA051101Web · crackedFOUND CRACK 500G, S-27R. FAB FILLER AND DOUBLER PER SRM 51-70-11, DEFECT SIZE: 0.25" CRACK IN WEB.SDR USAA051103Attach Fitting · corrodedFOUND FWD FACE OF L4 LUG FWD CLEVIS OF LT HOR STAB. REMOVED CORROSION AND INSTALLED BUSHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 2" AREA OF CORROSION.SDR USAA051104Attach Fitting · corrodedFOUND CORROSION RT HORIZ STAB FORWARD LWR CLEVIS AFT BUSHING AFT FACE. REMOVED CORROSION AND INSTALLED BUSHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 2" AREA OF CORROSION.SDR USAA051105Attach Fitting · corrodedFOUND CORROSION FWD FACE OF L13 HOR STAB LUG. REMOVED CORROSION AND INSTALLED BUSHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 2" AREA OF CORROSION.SDR USAA051127Stringer · crackedFOUND FUSELAGE STR SPLICE AT STA 907 STR 4L. INSTALLED STRINGER SPLICE IAW SRM 51-40-02, DEFECT SIZE: .75" CRACK.SDR USAA051107Bushing · corrodedFOUND CORROSION LT HORIZ STAB, FWD L2 LUG BUSHING. REMOVED CORROSION AND INSTALLED BUSHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 2" AREA OF CORROSION.SDR USAA051109Bushing · corrodedFOUND CORROSION LT HORIZ STAB L14 AFT BUSHING. REWORKED AREA AND INSTALLED BUSHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 2" AREA OF CORROSION.SDR USAA051128Skin · chafedFOUND CHAFING UPPER FUSELAGE EXT SKIN DBLR UNDER DORSAL FIN STA 864 BL=0. REMOVED DBLR, FILLER, SKIN AND TEAR STRIP, FABBED AND INSTALLED NEW PER EA 96859, DEFECT SIZE: 5-3/4" X 7".SDR USAA051129Frame · crackedFOUND CRACK STA 907 STR 1. INSTALLED FRAME ANGLE REPAIR PER SRM 53-00-07, DEFECT SIZE: 1".SDR USAA051130Splice · crackedFOUND CRACK FUSELAGE STRINGER SPLICE AT STA 907 STR 4R. INSTALLED STRINGER SPLICE IAW SRM 51-40-02, DEFECT SIZE: .25".SDR USAA051131Frame · damagedBS 294.5, S-17R, CUT OUT DAMAGE, FABRICATED NEW ATTACH ANGLE AND INSTALLED IAW SRM 51-70-11 TABLE 5 OF FIG NR 1, DEFECT SIZE: .5" CRACKED DOOR FRAME.SDR USAA051106Attach Fitting · corrodedFOUND CORROSION AFT FACE OF L6 HORIZ STAB LUG. REMOVED CORROSION AND INSTALLED BUSHING IAW SRM 55-10-10, DEFECT SIZE: 1" X 2" AREA OF CORROSION.SDR USAA051093Stringer Clip · crackedFOUND CRACK STA 827, S4L. REMOVED DAMAGED PART, INSTALLED NEW IAW SRM 51-10-02 3.C (3), DEFECT SIZE: .125" CRACK.SDR USAA051095Stringer Clip · crackedFOUND TIE CLIP CRACKED AT STA 767, STR 2L. REPLACED TIE CLIP IAW SRM 51-10-02.SDR USAA051096Attach Bracket · crackedFOUND CRACK O/H DUCT ATTACH BRACKET AT STA 767 STR 1. FABRICATED AND INSTALLED IAW SRM 51-10-02 AND BOEING DWG 69-47869, DEFECT SIZE: 1/4" CRACK AT BRACKET.SDR USAA051097Frame · damagedSTA 294, S-16L AFT OF FRAME, NEW PART, INSTALLED WITH LOCK FASTENERS IAW SRM 51-10-02, DEFECT SIZE: SHEETMETAL NR 4365, WEB CRACKED (APPROX 1.5 INCHES LONG) S-161, AFT OF BS 294 FRAME.
Back to Boeing 737-4B7