Boeing 737-3B7
Service difficulty reports · 4,722
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 = '7373B7' 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 = '7373B7' 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 USAA050233Web · tornPIT - FOUND WEB WITH .5 INCH SQUARE SECTION TORN OUT, BS 847 AT S24R. CUT OUT DAMAGE AND INSTALLED DOUBLER SPLICE AND NEW WEB PER SRM 51-70-13. (M)SDR USAA050232Frame · crackedPIT - FOUND FRAME CRACKED .25, BS 440 BETWEEN S8R AND S9R. CUT OUT DAMAGE AND INSTALLED REPAIR ANGLES PER TYPICAL REPAIR 53-10-20A. (M)SDR USAA050312Hinge Bracket · wornPIT - FOUND HINGE PLATES WITH THREE WORN HOLES .25 INCH DIAMETER, RUDDER HINGE NR 7 PLATES ON VERTICAL STABILIZER. DEFECTIVE PART REPLACED WITH IDENT PART PER AMM 55-00-00. (M)SDR USAA050300Skin · dentedPIT - FOUND SKIN DENTED AND PUNCTURED, 1 INCH BY 1 INCH BY .125 INCH, BETWEEN S-26R AND S27R AND STA 500D PLUS 10 INCHES. REPAIR DOUBLER INSTALLED PER SRM 53-00-01 FIG 229 DETAIL XII. (M)SDR USAA050234Angle · chafedPIT - FOUND SKATE ANGLE CHAFED, VERT STAB RT AND LT LOWER SKATE ANGLE. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-40-00 AND DWG 65-54842. (M)SDR USAA050231Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, FS 887 S-9R. DOUBLER REPAIR INSTALLED PER 53-10-20A. (M)SDR USAA050236Stringer Splice · crackedPIT - FOUND STRINGER SPLICE CRACKED 1 INCH IN TWO LOCATIONS, BS 908 S4L AND S4R. REMOVED TWO SPLICES, MANUFACTURED NEW AND INSTALLED PER SRM 51-40-02 AND DWG NR 65-51698. (M)SDR AWXA200500186Charger · failedDURING OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM THE L-2 DOOR EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO HAVE VERY WEAK ILLUMINATION. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER M1197, OPERATIONAL CHECK WAS GOOD.SDR USAA050299Skin · crackedPIT - FOUND NR 5 SLAT SKIN CRACKED 1 INCH, OUTBOARD FORWARD EDGE ABOVE UPSTOP. INSTALLED DOUBLER PER SRM 57-43-01. (M)SDR USAA050230Frame · crackedPIT - FOUND FRAME CRACKED .75 INCH, FS 616 S17R. INSTALLED DOUBLER PER TYPICAL REPAIR 53-62-01. (M)SDR USAA050224Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH, AFT LEFT SERVICE DOOR CUTOUT LOWER HINGE AREA. INSTALLED DOUBLER PER TR 53-60-10. (M)SDR USAA050201Stringer Clip · crackedCLT - FOUND CLIP CRACKED .5 INCH, STATION 344 STRINGER 11R. REPLACED TIE CLIP IAW SRM. REPLACED TIE CLIP IAW SRM 51-10-02. (M)SDR USAA050227Frame · crackedPIT - FOUND FRAME CRACKED .125 INCH, BETWEEN 4TH DOOR STOP FORWARD SIDE. INSTALLED DOUBLER PER TYPICAL REPAIR 52-10-11. (M)SDR USAA050228Door Frame · crackedPIT - FOUND FRAME CRACKED .125 INCH, FRAME FORWARD SIDE NR 3 DOOR STOP CUTOUT. INSTALLED DOUBLER PER TYPICAL REPAIR 52-10-11. (M)SDR SB05023Bracket · out of adjustCLT - THE L1 DOOR GIRT BAR WOULD NOT STAY ATTACHED. MAINTENANCE ADJUSTED THE GIRT BAR ATTACH BRACKETS.SDR USAA050229Door Frame · crackedPIT - FOUND FORWARD ENTRY DOOR CRACKED .3750, FRAME AND INNER WEB AT STOPS NR 5 AND NR 6 CUTOUTS. REMOVED DAMAGE, INSTALLED DOUBLER PER TYPICAL REPAIR 51-10-16. (M)SDR SB05022Starter · faultyAT THE BEGINNING OF DESCENT INTO CLT, AN APU OVERSPEED OCCURRED RESULTING IN AN APU SHUTDOWN. THIS RESULTED IN A SINGLE GENERATOR OPERATION SINCE THE NR 1 ENGINE GENERATOR WAS ALREADY ON MEL. CREW COMPLIED WITH QUICK REFERENCE HANDBOOK PROCEDURES AND LANDED ASDR USAA050220Reveal · crackedPIT - FOUND REVEAL 2 INCH CRACK, UPPER FORWARD CORNER REVEAL AT FORWARD SVC DOOR CUTOUT. INSTALLED CORNER REVEAL, STRIP AND SHIM PER EA 79829B. (M)SDR SB05018O-Ring · damagedCLT - FLT556 - DURING CRUISE, ENROUTE FROM TPA TO DCA, CREW REPORTED LOSING SYSTEM B HYDRAULIC FLUID. FLIGHT DIVERTED TO CLT AND LANDED WITH A HYDRAULIC QUANTITY READING OF 1/4. THE B SYSTEM ENGINE DRIVEN PUMP LIGHT ALSO ILLUMINATED ON LANDING AND WAS ON FORSDR USAA050177Skin · crackedCLT - FOUND SKIN CRACKED, STATION 727D STRINGER S24L. INSTALLED DOUBLER IAW SRM 53-00-01. (M)SDR SB05014Pmc · faultyIAD - FLT1187 - ON CLIMB-OUT FROM IAD, EN ROUTE TO CLT, THE NR 2 ENGINE SURGED AS N1 ROLLED BACK 10 PERCENT AND BEGAN TO FLUCTUATE 4-5 PERCENT THEREAFTER. AIRCRAFT BEGAN TO YAW AND ROLL. AT 11,000 FEET, CREW DISENGAGED AUTOPILOT BUT PROBLEM CONTINUED. FLIGHSDR SB05011Apu · malfunctionedBDL - FLT902 - EN ROUTE FROM PHL TO BDL, THE NR 1 ENG CSD LOW OIL PRESSURE LIGHT ILLUMINATED. CREW DISCONNECTED THE CSD PER QUICK REF HANDBOOK PROCEDURES AND STARTED THE APU. AFTER APPROX TEN MINUTES OF USE, THE APU OVERSPEED LIGHT ILLUMINATED AND THE APU SHSDR SB05012Holder · failedPHL - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT 13C INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE HOLDER AT SEAT 13C. OPERATIONAL CHECK NORMAL.SDR USAA050085Threshold · corrodedPIT - Q3 - WEB PLATE, .2500 INCH AROUND, CORROSION; LEVEL 1; TASK NR C53-202-01; AFT CARGO DOOR THRESHOLD AROUND NUT PLATE HOLES. DEFECTIVE PART REPLACED WITH IDENT PART IAW DWG 65-47957 AND SRM 51-40-03. (K)SDR USAA050062Skin · crackedPIT - FOUND SKIN CRACKED 2.5 INCHES, 1 INCH ABOVE S23L AT BS 745. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229. (M)SDR USAA050151Skin · crackedPIT - Q6 - PYLON STRUT SKIN, .7500 INCH CRACK; PYLON STRUT SKIN FOR LT ENGINE, ACCESS PANEL CUTOUT. STOP DRILL OF CRACK AND INSTALLATION AT DOUBLER IAW TYP REP 54-30-07. (K)SDR USAA050222Floor Support · corrodedPIT - FOUND FLOOR SUPPORT CORRODED APPROX 3 INCHES BY .5 INCH, STATION 797 TO 817. FABRICATED AND INSTALLED NEW FLOOR SUPPORT PER SRM 53-00-53. (M)SDR USAA050189Bracket · crackedPIT - FOUND DOUBLER BRACKET CRACKED, FS 500-500A, VHF NR 2 ANTENNA MOUNT BRACKET. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 51-40-02. (M)SDR USAA050167Skin · chafedPIT - FOUND SKIN CHAFFING AND FRETTING WEAR 25.5 BY 30 INCH, BS 860 BETWEEN STRINGER 3L AND 3R. DAMAGE REMOVED, DOUBLER INSTALLED PER SRM 53-60-01 FIG 209. (M)SDR USAA050064Skin · delaminatedPIT - FOUND TOP SKIN CORE BOND DELAMINATED 2.5 INCH BY 2.5 INCH AREA, NR 3 SLAT INBOARD TRAILING EDGE. REMOVED DAMAGED SKIN AND CORE, INSTALLED NEW CORE, DOUBLERS PER SRM 51-70-10. (M)SDR SB05003Battery Pack · dischargedPIT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 17 THRU 22 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT STATION 975 FOR SEAT ROWS 17 THRU 22. ALSO, REPAIRED A PIN IN CANNON PLUG WHICH WAS FOUND BAD. OPERATIONAL CHECK GOOD.SDR USAA050162Bracket · crackedPIT - Q6 - BRACKET, 10 INCHES LONG CRACK; VHF COMM ANT BRACKET, STA 500-500A FWD BAGGAGE PIT; REMOVED AND REPLACED CRACKED BRACKET, BLENDED CORROSION IAW SRM. (K)SDR USAA050161Skin · crackedPIT - Q6 - INNER SKIN, APPROX .5 INCH LONG; MAIN ENTRANCE DOOR AFT SIDE AT NR 7 STOP; INSTALLED DOUBLER IAW TYP REP. (K)SDR USAA050063Skin · delaminatedPIT - FOUND TOP SKIN CORE BOND DELAMINATED 3 INCHES BY 3 INCHES, NR 5 SLAT OUTBOARD TRAILING EDGE. REMOVED DAMAGE, INSTALLED NEW CORE, FILLERS, DOUBLERS PER SRM 51-70-10. (M)SDR USAA050003Skin · crackedCLT - FOUND SKIN CRACKED 1.750 INCH, STATION 74-2 AT STRINGER 19R. INSTALLED DOUBLER IAW 53-00-01. (M)SDR USAA050046Rivet · loosePIT - FOUND LT WING FOREFLAP 42 LOOSE RIVETS, LT WING OUTBOARD FOREFLAP APPROX 42 INCHES. DEFECTIVE PART REPLACED WITH IDENT PART. (M)SDR USAA050045Skin · crackedPIT - FOUND SKIN CRACKED, AFT ENTRY DOOR LOWER HINGE CUTOUT. DOUBLER INSTALLED PER TYPICAL REPAIR 53-60-10 AND EA 79782. (M)SDR USAA050163Keelbeam · crackedPIT - Q6 - KEELBEAM, 1 INCH CRACK; STA540 39R; REPLACED SECTION OF FWD KEELBEAM, SPLICES MFGD IAW TYP REP 53-60-09. (K)SDR USAA050083Stringer · crackedPIT - FOUND STRINGER CRACKED .3750 INCH AT S-8 UPPER STRINGER AT WBL 355 AT ATTACH BOLT ON, RT WING. INSTALLED REPAIR ANGLES PER EA 79684. (M)SDR USAA050071Skin · tornPIT - FOUND SKIN WITH .5 INCH TEAR, STATION 1025 LBBL 33. PART REPLACED PR JOB CARD J3-58-53500-C-010. (M)SDR USAA050090Frame · crackedPIT - Q6 - FRAME, .0625 INCH CRACK, CRACK RADIATING FROM RIVET AT STA 827S-9R. INSTALLED DOUBLER IAW SRM 53-10-20A. (K)SDR USAA050078Intercostal · crackedPIT - FOUND INTERCOSTAL CRACKED .5 INCH, AT KEEL BEAM BETWEEN STATION 500 AND 520 IN DISTRIBUTION BAY. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-40-02. (M)SDR USAA050164Intercostal · crackedPIT - Q6 - BAFFLE, 1 INCH CRACK; AFT CARGO BIN STA 927 S-25L; FABRICATED AND INSTALLED NEW BAFFLE IAW SRM. (K)SDR USAA050108Skin · crackedPIT - Q6 - SKIN, 2.2500 INCH CRACK; FUSELAGE SKIN AT FWD SVC DOOR CUT OUT AFT; CUT OUT CRACKED AREAS AND INSTALLED REPAIR DOUBLERS IAW SRM 53-10-01 AND EA 79657. (K)SDR USAA050092Plate · fatiguedPIT - Q6 - MAIN LANDING GEAR FG; INSTALLATION OF REAR SPAR FATIGUE PLATE; INSTALLATION OF REAR SPAR FATIGUE PLATE; LT REAR SPAR UPPER CHORD BETWEEN WBL 150 AND 126. FABRICATED DOUBLER AND INSTALLED IAW EA 79629. (K)SDR USAA050079Stringer · crackedPIT - FOUND STRINGER CRACKED .5 INCH, RT WING WBL 479 AT S-8. REPAIR ANGLES PER EA 79684. (M)SDR USAA050080Stringer · crackedPIT - FOUND STRINGER CRACKED .5 INCH, RT WING WBL 355 AT S-8. REPAIR ANGLES PER EA 79684. (M)SDR USAA050077Stringer · crackedPIT - FOUND UPPER STRINGER 2 INCH CRACK, WBL 505 RT WING. INSTALLED REPAIR ANGLES WITH MINOR DEVIATION PER EA 79684 AND SRM 57-00-03. (M)SDR USAA050075Stiffener · crackedPIT - FOUND STIFFENER CRACKED .75 INCH, MAIN LANDING GEAR WHEEL WELL BS 663.75 AT LBL 6.15. REPLACED STIFFENER PER EA 75002 AND BOEING DWG 65-45402. (M)SDR USAA050076Support Bracket · crackedPIT - FOUND ANTENNA CHANNEL, SUPPORT BRACKETS WITH THREE .5 INCH CRACKS, BETWEEN STATION 500/500A, STRINGER 28L-28R, VHF-2 ANTENNA CHANNEL. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)
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