Boeing 737-301
Service difficulty reports · 4,797
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 = '737301' 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 = '737301' 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 USAA010528Tie Clip · crackedCLT - FOUND STRINGER TIE CLIP CRACKED, .1875 INCH, BS 827, STRINGER 16R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-2. (M)SDR USAA010527Tie Clip · crackedCLT - FOUND STRINGER TIE CLIP CRACKED, BS 727A, STRINGER 6R. REMOVED AND REPLACED TIE CLIP P ER SRM 51-10-2. (M)SDR USAA010526Tie Clip · crackedCLT - FOUND STRINGER TIE CLIP CRACKED .25 INCH, BS 663, STRINGER 10R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-2. (M)SDR USAASB01134Light · inoperativePIT - PILOT REPORTED THAT THE FORWARD FLOOR LEVEL EMERGENCY EXIT LIGHT, IN THE AISLE, IS DEFECTIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AND THE BATTERY PACK (P/N 2013-1A). OPS CHECK GOOD. (M)SDR USAASB01132Switch · failedCLT - MAINTENANCE FOUND THE EMERGENCY LIGHTS (NOT ARMED)INOPERATIVE/WON''T TEST. MAINTENANCE REMOVED AND REPLACED THE SOCKET/SWITCH ASSEMBLY ON THE P5 OVERHEAD PANEL. OPERATIONAL CHECK GOOD. (M)SDR AWXA0001717Tee Chord · corrodedREMOVE FASTENERS AND STRIP AREA AT BS 500D-510 STR 28R TO FACILITATE INSPECTION. REMOVED LOWER T-CHORD AND SKIN. REPAIRED LOWER T-CHORD AND SKIN IAW ER 03-5315-01120-DL1.SDR USAASB01129Proximity Sensor · failedCLT - FLT 1670 - AFTER TAKEOFF FROM SAV, EN ROUTE TO CLT, CREW ATTEMPTED TO RAISE THE LANDING GEAR HANDLE BUT THE HANDLE WOULD NOT MOVE MORE THAN HALFWAY UP. AFTER FLAPS WERE UP, GEAR WARNING HORN STOPPED SOUNDING. CREW DID NOT ATTEMPT OVER-RIDE BUT ELECTED SDR USAA010729Beam · crackedPIT - FOUND BEAM CRACKED .5 INCH, BL0 FLOORBEAM AT BS 712. MANUFACTURED AND INSTALLED FILLERS AND DOUBLER PER EA 71067 AND SRM 51-70-13. (M)SDR USAA010694Web · corrodedPIT - FOUND WEB PANEL CORRODED 1 INCH BY 10 INCHES, STATION 956.5 TO 967. CORRODED LEVEL 1, TASK NR C53-202-01. MFG WEB PANEL FROM STATION 947.5 TO 967 PER SRM 51-20-01/51-40-01/51-30-01/51-20-05. (M)SDR USAA010699Clip · corrodedPIT - FOUND SKIN CLIP CORRODED 1 INCH BY 4 INCH AREA EXFOLIATED, SKIN CLIP AFT SIDE STATION 967 STRINGER 25L AND 26L. CORROSION LEVEL 2, TASK NR C53-208-01. REMOVED AND REPLACED WITH SECTION OF NEW SKIN CLIP PER SRM 53-00-03. (M)SDR USAA010688Floorbeam · corrodedPIT - FOUND TOP FLANGE ENTIRE LENGTH OF FLOORBEAM CORRODED 1 INCH BY 2 INCHES, FLOORBEAM STATION 986.5. CORROSION LEVEL 1, TASK C53-107-02. TOP SECTION OF FLOORBEAM REPLACED ENTIRE LENGTH WITH BOEING KIT NR 6132505 PER TYPICAL REPAIR 53-60-01. (M)SDR USAA010700Angle · corrodedPIT - FOUND Z-ANGLE CORRODED 1 INCH BY 6 INCHES, AT DOOR SILL OF AFT ENTRANCE DOOR. CORROSION LEVEL 1, TASK NR C53-107-01. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M)SDR USAA010730Beltframe · crackedPIT - FOUND BELTFRAME CRACKED .25 INCH, STATION 633 S2L. INSTALLED DOUBLER PER 53-00-7 FIG 209. (M)SDR USAA010731Beam · crackedPIT - FOUND BEAM CRACKED 1 INCH, BS 867 BETWEEN S8L AND S9L. REMOVED DAMAGE, INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14. (M)SDR USAA010732Frame · crackedPIT - FOUND FRAME CRACKED .75 INCH, BS 867 BETWEEN S8R AND S9R. CUT OUT DAMAGE AND INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-14. (M)SDR AWXA0001678Bushing · out of positionNR 2 ENGINE PYLON O/B MID SPAR BUSHING HAS MIGRATED .095 INCHES. REPLACED BUSHINGS IAW SB 54-1037 PARAGRAPH 1D, AWA ER 03-5410-0111D-JS1. P/N: 311A1151-12, 311A1151-13.SDR AWXA0001677Floor Support · corrodedSTA 1015 LBL 8 FLOOR SUPPORT UPPER CAP CORRODED. REMOVED AND INSTALLED FLOOR SUPPORT IAW B737 SRM 51-40-02 PG 16-17.SDR AWXA0001676Skin · dentedSEVERAL DENTS IN LT HORIZ STAB STA 95.66 - 104.66. INSTALLED REPAIR IAW ER 03-5515-01117-TB1.SDR USAA010547Skin · delaminatedPIT - FOUND RUDDER DELAMINATED AND GOUGED IN SEVERAL AREAS, LT AND RT RUDDER SKIN AND ONE LEADING EDGE GOUGE. COMPOSITE WET LAYUP REPAIR 230. (M)SDR USAA010686Web · corrodedPIT - FOUND WEB PANEL CORRODED 12 INCHES BY 48 INCHES AT NUT PLATE, AFT CARGO DOOR WEB PLATE. CORROSION LEVEL 1, TASK C53-202-01. REMOVED CORRODED WEB PANEL AND REPLACED WITH NEW PANEL PER DRWG NR 65-47957. (M)SDR AWXA0001648Web · crackedFWD CARGO DOOR - CRACK IN LWR WEB INSIDE LWR AFT ACCESS HOLE. CUT OUT DAMAGED AREA; INSTALLED FILLER AND DOUBLER IAW AWA ER 03-5231-01106-TB2.SDR AWXA0001647Web · crackedLT CUSP WEB HAS CRACK APPROX 2 INCHES LONG AT FS 638 STR 17L. CUT OUT DAMAGED AREA; INSTALLED FILLER AND DOUBLER IAW B737-300 SRM 51-70-13 PG 1-3.SDR AWXA0001642Web · crackedCOCKPIT FLOOR CRACKED AT FS 180 WL 207 LBL 23. REMOVED AND REPLACED WEB IAW B737-300 SRM 51-40-02 PG 2-4, 6-8, 10-11, 16-17.SDR AWXA0001641Web · crackedCOCKPIT FLOOR CRACKED AT FS 180 WL 207 RBL 23. REMOVED AND REPLACED WEB IAW B737-300 SRM 51-40-02 PG 2-4, 6-8, 10-11, 16-17.SDR AWXA0001640Bulkhead · crackedFS 178 BLKHD CRACKED AT WL 200 RBL 5. REPAIRED AREA IAW B737-300 SRM 53-10-08 FIG 211 PG 1-11 AND 51-21-41 PG 701-702 AND 51-40-02 PG 2-4, 6-8, 10-11.SDR AWXA0001639Bulkhead · crackedFS 178 BLKHD CRACKED AT WL 201.5 LBL 6.5. REPAIRED AREA IAW B737-300 SRM 53-10-08 FIG 211 PG 1-11 AND 51-21-41 PG 701-702 AND 51-40-02 PG 2-4, 6-8, 10-11.SDR AWXA0001638Bulkhead · crackedFS 178 BLKHD CRACKED AT WL 201.5 LBL 5. REPAIRED AREA IAW B737-300 SRM 53-10-08 FIG 211 PG 1-11 AND 51-21-41 PG 701-702 AND 51-40-02 PG 2-4, 6-8, 10-11.SDR AWXA0001637Bulkhead · crackedFS 178 BLKHD CRACKED AT WL 200 LBL 5. REPAIRED AREA IAW B737-300 SRM 53-10-08 FIG 211 PG 1-11 AND 51-21-41 PG 701-702 AND 51-40-02 PG 2-4, 6-8, 10-11.SDR AWXA0001636Bulkhead · crackedFS 178 BLKHD CRACKED AT WL 234 RBL 8 - 11.5. REPAIRED AREA IAW B737-300 SRM 53-10-08 PG 265-269 AND 51-40-02 PG 3-4 & 9-11 AND 51-20-01 PG 1-10.SDR AWXA0001635Bulkhead · crackedFS 178 BLKHD CRACKED AT WL 234 LBL 8 - 11.5. REPAIRED AREA IAW B737-300 SRM 53-10-08 PG 265-269 AND 51-40-02 PG 3-4 & 9-11 AND 51-20-01 PG 1-10.SDR AWXA0001634Bulkhead · gougedFS 178 BLKHD GOUGED AT WL 205 RBL 24. REPAIRED AREA IAW B737-300 SRM 51-40-02 PG 6-8, 10, 11 AND 51-20-01 PG 1-11 AND 53-40-08 FIG 209 PG 266-267 AND 53-10-08 FIG 101 PG 102-103.SDR AWXA0001633Pressure Panel · crackedLEFT WHEEL WELL PRESSURE WEB CRACKED AT FS 663 LBL 32. INSTALLED REPAIR CHANNEL IAW AWA ER 03-5716-0110-552.SDR AWXA0001632Flap · puncturedLEFT O/B KRUEGER FLAP PUNCTURED AT ACTUATOR MOUNT. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER IAW AWA EO 03-5743-01106-TB1.SDR AWXA0001631Floor Support · corrodedFS 993 RBL 17 FLOOR SUPPORT UPPER CAP CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW B737-300 SRM 53-60-51 PG 108-114 AND 51-40-08 PG 1-6.SDR AWXA0001630Floorbeam · corrodedFS 1016 LBL 7 FLOORBEAM UPPER CAP CORRODED. REMOVED CORROSION; TREATED AND INSTALLED REPAIR IAW B737-300 SRM 53-00-51 FIG 203 PG 211-215 AND 53-60-51 FIG 101 PG 109.SDR USAA010549Aileron · crackedPIT - FOUND RIGHT AILERON CRACKED .5 INCH BY .5 INCH, AILERON FRONT SPAR UPPER FLANGE AT NR 1 HINGE ACCESS. INSTALLED WET LAYUP WITH A 230 CURE WITH ONE EXTRA PLY PER SRM 51-70-17, EA 70844. (M)SDR USAA010391Frame · crackedCLT - FOUND SIDE CHORD CRACKED, .5 INCH, BS 178, LBL 24, WL 207. CUT OUT DAMAGE, SPLICED IN NEW SIDECHORD, SRM 51-10-02, EO 5300V157. (M)SDR USAA010390Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED 3 INCHES, WL 195, STATION 178, RBL 24. REMOVED AND REPLACED SRM 51-10-02, EO 5300V153. (M)SDR USAA010389Bulkhead · crackedCLT - FOUND WEB CRACKED 2 INCHES, BS 178, RBL 6, BETWEEN WL 197 AND 205. INSTALLED DOUBLER SRM 53-10-08, EO 5300V153. (M)SDR USAA010388Web · crackedCLT - FOUND WEB CRACKED .5 INCH, FLOORWEBS STATION 179, LBL 28, WL 207. REMOVED AND REPLACED WEB, EO 5300V157. (M)SDR USAA010387Web · crackedCLT - FOUND WEB CRACKED .5 INCH, BS 179, RBL 28, WL 207. REMOVED AND REPLACED WEB EO 5300V157. (M)SDR USAA010386Skin · crackedCLT - FOUND SKIN CRACKED 2 INCHES, STATION 947 AT STRINGER 34L, FORWARD OF POTABLE WATER SERVICE PANEL. INSTALLED DOUBLER PER SRM 53-00-01, FIG 201. (M)SDR USAASB01101Engine · malfunctionedTPA - FLT 1580 - EN ROUTE FROM PHL TO TPA, A BURNING OIL SMELL WAS REPORTED COMING FROM THE LEFT PACK DURING FLIGHT. FLIGHT CONTINUED AND LANDED AT TPA WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE AS THE SOURCE OF THE ODOR. REMOVED AND REPLACSDR SWAA011156Container · looseAFT SERVICE DOOR EMERGENCY EVAC SLIDE CONTAINER CAME LOOSE. INSPECTED SLIDE & RESECURED CONTAINER.SDR USAA010376Frame · crackedCLT - FOUND FRAME CRACKED .0500 INCH, STATION 7270, BETWEEN STRINGER 8R-9R. INSTALLED DOUBLER PER TR 53-10-14. (M)SDR USAA010418Door Frame · crackedPIT - FOUND FORWARD CORNER FRAME CRACKED 1 INCH AND .25 INCH, FORWARD CARGO DOOR LOWER FWD CORNER TOP FLANGE. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER EO 5290X045. (M)SDR USAASB01093Battery Pack · dischargedLGA - MAINTENANCE FOUND THE FORWARD ENTRY DOOR EMERGENCY EXIT LIGHTS WEAK. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)SDR USAA010417Floor Support · corrodedPIT - FOUND BEAM SUPPORT CORRODED .5 INCH TO 6 INCHES AT NUTPLATES, BS 727D-827 ON ALL LEFT SIDE FLOOR SUPPORT. CORROSION LEVEL 1, TASK NR C53-208-01. REPLACED DEFECTIVE PARTS WITH IDENTICAL BEAM SUPPORT PER TYPICAL REPAIR 53-10-06B. (M)SDR USAASB01091Coffeemaker · shortedMIA - FLT 1191 - EN ROUTE FROM CLT-MIA, FLIGHT ATTENDANT REPORTED A SCORCHING SMELL IN THE FORWARD GALLEY APPROXIMATELY TEN MINUTES BEFORE LANDING AT MIA. OVENS WERE NOT IN USE AT THE TIME. COFFEE MAKER CIRCUIT BREAKERS WERE ALL PULLED AND GALLEY POWER WAS TSDR USAASB01087Battery Pack · dischargedCLT - PILOT REPORTED THAT NUMEROUS EMERGENCY EVACUATION LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE ASSOCITED BATTERY PACK. OPS CHECK GOOD. (M)
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