Boeing 737-330
Service difficulty reports · 430
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 = '737330' 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 = '737330' 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 DU4R2021030100012Frame · dentedDURING SCHEDULED INSPECTION, FOUND MAIN CABIN R/H FRAME HAS A DENT 4-5" INCHES ABOVE FLOOR LEVEL AT STA. 500A. S/O 660004, N/R 44352SDR DU4R2021022500010Attach Angle · corrodedDURING SCHEDULED INSPECTION, FOUND FWD CARGO COMPARTMENT, BILGE AREA, LBL 21.8 FLOOR BEAM, FS 500D BULKHEAD ATTACH ANGLE HAS CORROSION. S/O 660004 N/R 44444.SDR DU4R2021022500009Skin · damagedDURING SCHEDULED INSPECTION, FOUND BLEND IN DOOR SKIN UPPER CORNER AT LT FWD CABIN DOOR. S/O 660004 N/R 44380.SDR DU4R2021022400008Angle · crackedDURING SCHEDULED INSPECTION, FOUND FWD ENTRY DOOR AFT EDGE OF DOOR CUTOUT HAD A CRACKED ANGLE AT STA. 348 BETWEEN S8L - S9L.SDR DU4R2021022200007Seat Track · gougedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MAIN CABIN SEAT TRACK OUTBOARD FLANGE SPLICE GOUGED AT STA 420 RBL 45.50.SDR DU4R2021021800005Skin · gougedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND RT HORIZONTAL STABILIZER, PANEL 92226R, STAINLESS ANGLE WAS GOUGED. S/O 6600004 N/R 44479.SDR DU4R2021021600004Cap · corrodedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MAIN CABIN FLOOR SUPPORT CAP HAS EVIDENCE OF CORROSION AND PUNCTURES AT STA. 540 RBL 24.50 - 45.50, LBL 24.50 - 45.50 AND LBL 70.53 - RBL 70.53. S/O 660004 N/R 44786SDR DU4R2021021200003Floor Panel · corrodedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND AFT CARGO FLOOR PANEL 1538, MIDDLE AREA, HAS PITTING CORROSION. S/O 660004 N/R 44977SDR NACA2020120900020Flap System · malfunctionedDISCREPANCY: MISSED APPROACH DUE TO FLAPS NOT DEPLOYING AND SPEED BRAKE NOT DEPLOYING. NO FLAP ASSYMETRY AND NO FLAP DISAGREE. CORRECTIVE ACTION: PERFORMED FLAP OPERATION CHECK & SPEED BRAKE OPERATIONAL CHECK WITH NO BINDING OR INABILITY TO MOVE HANDLES. INSDR NACA2020112700019Skin · crackedDISCREPANCY: CRACK ON LEFT SIDE FUSELAGE, 14 INCHES FWD OF BS 500, 2.75 INCHES ABOVE S26L, 1.5 INCHES LONG. CUT OUT DAMAGE, FABBED DOUBLER AND INSTALLED, PER REF B737-300 SRM 53-00-01 REPAIR 31 DETAIL XIX AND PEMCO EA NR PD37-53-3220.SDR NACA2020110600018Start Valve · inoperativeDISCREPANCY: DURING CLIMB NR 2 ENGINE EGT LIGHT ILLUMINATED A/T DISCONNECT MANUAL THRUST REDUCTION. LARGE THRUST LEVER SPLIT FOR EQUAL THRUST. A/P & AT ILS ENGINE PERFORMANCE NORMAL. CORRECTIVE ACTION: PERFORMED VISUAL CHECK OF INLET AND EXHAUST, NO DEFECTSSDR NACA2020080500015Skin · corrodedCORROSION ON WING LOWER SKIN AT STR7 WBL55R. REMOVED AND FOUND WITHIN LIMITS IAW DWG 5710D2830 REV IR, NO REMAINING DEFECTS FOUND.SDR NACA2020080500014Skin · corrodedCORROSION FOUND ON THE LOWER LEFT WING SKIN BETWEEN STRINGERS 5 & 6, WBL40L TO WBL60L. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW DWG 5710D2830, REV IR. REPAIRED IAW DWG R27905.1-057-013-001, REV NC.SDR TSAA20191003045Floorbeam · not reportedREPAIRED FLOOR BEAM UPPER CHORD AT STA 986.5 RBL 40-45. REPLACED UPPER CAP FROM LBL 50 TO RBL 50 AS PER AEI EO 9563 REV IR AND FAA FORM 8110-3.SDR TSAA20191003055Skin · damagedREPAIRED RH WING ROOT TO W STA 270, UPPER WING SKIN IN MULTIPLE LOCATIONS AS PER BOEING SR# 4-45466890303 DATED SEPT 23, 2019 AND FAA 8100-9.SDR TSAA20191003056Structure · crackedREPAIRED CRACKED FASTENER HOLE ON RH WING T/E WBL 136 IAW BOEING SR# 4-4546890303 DATED SEP 23, 2019.SDR TSAA20191003013Strap · crackedREPAIRED CRACKED STRAPS AT STA 312 BL 0 AND LBL 14 IAW BOEING 737-300 SRM 53-10-51 REPAIR 4 REV 119.SDR TSAA20191003007Frame · dentedREPAIRED DENT DAMAGE ON INNER FLANGE OF STA 500 FRAME AT STR 16R+4" IAW KF DWG# R27904.1-053-099-001 REV A AND AEI EO 09520 REV IR. SEE FORM 8110-3 FOR FAA APPROVAL.SDR TSAA20191003005Skin · dentedREPAIRED DENT DAMAGE ON FUSELAGE BELLY SKIN AT STA 1016-1088 STR 25L-25R IAW KF DRAWING NO. R27904.1-053-011-001 REV NC, SEE FAA FORM 8110-3 FOR APPROVAL.SDR NACA2019042900088Vortex Gen · corrodedDISCREPANCY: LT WING UPPER SURFACE VORTEX GENERATOR CORRODED AT WBL 369 #3 FROM OUTBOARD. CORRECTION: LT WING UPPER SURFACE VORTEX GENERATOR REPLACED AT WS 423, #3 FROM OB IAW AMM 57-32-00 REV 88.SDR NACA2019071600087Door Sill · corrodedDISCREPANCY: STA 500D CORROSION FOUND ON LOWER SILL IN FWD PIT. LBL 30 TO RBL 30. CORRECTION: STA 500D CORROSION FOUND ON LOWER SILL IN FWD PIT LBL 30 TO RBL 30 REPLACED WITH MADE REPAIR PART IAW SRM REV 119 CH 51-40-02 PARA 4. STRUCTURE IDENTIFIED IN SRM REV SDR NACA2019071600086Intercostal · corrodedDISCREPANCY:STA 500 - 500A INTERCOSTAL AT S-26L CORRODED AROUND NUT PLATES. CORRECTION: STA 500 - 500A INTERCOSTAL AT S-26L REPLACED WITH MADE REPAIR PART IAW DWG NR 69-41473 AND SRM 51- 40-02 REV 118. STRUCTURE IDENTIFIED IAW SRM REV 118 CH 53-30-04.SDR NACA2019071600085Intercostal · corrodedDISCREPANCY: STA 500C TO 500D INTERCOSTAL AT S-26L CORRODED AROUND NUT PLATES. CORRECTION: STA 500C TO 500D INTERCOSTAL AT S-26L REPLACED IAW DWG NR 69-41757 AND B737-300 SRM 51-40-02 REV 118 WITH MADE REPAIR PART IAW SRM REV 119 CH 51-30-01.SDR NACA2019071600084Plate · corrodedDISCREPANCY: STA 380 - 420 RT FLOOR SIDE PLATE IN FWD CARGO PIT CORRODED AROUND NUT PLATES. CORRECTION: STA 380-420 RT FLOOR SIDEPLATE IN FWD CARGO PIT REPLACED IAW SRM 51-40-02 REV 118. SERVICEABLE. PART IDENTIFIED AS PER SRM REV 118 CH 53-30-53.SDR NACA2019071600083Attach Angle · corrodedDISCREPANCY: 794 STR 25R CORROSION ON SCUFF PLATE ATTACH ANGLE AFT PIT. CORRECTION: 794 STR 25R CORROSION ON SCUFFPLATE ATTACH ANGLE AFT PIT FOUND TO BEYOND LIMITS. ATTACH ANGLE REPLACED WITH MADE REPAIR PART IAW SRM REV 118,CH 51-30-01 PARA 3,8. ANGLE IDENTIFSDR NACA2019071600082Angle · corrodedDISCREPANCY: STA320, BL48 R1 DOOR ENTER WAY BUST SILL ANGLE CORRODED AROUND ANCHOR NUTS. CORRECTION: STA 320. BL 48 R1 DOOR ENTER WAY DUST STILL ANGLE REPLACED IAW DOCUMENT # 65-45875 REV J.SDR NACA2019071600081Plate · corrodedDISCREPANCY: STA 430 S-26-R FLOOR SUPPORT CHANNEL SIDE PLATE CORRODED IN FWD PIT. CORRECTION: STA 430 526R FLOOR SUPPORT CHANNEL SIDE PLATE IN FWD PIT REPLACED WITH MADE REPAIR PART IAW DRAWING 65-20726 REV F AND SRM REV 119 CH 51-30-01.SDR NACA2019071600080Plate · corrodedDISCREPANCY: STA 500-500A S-26-R FLOOR SUPPORT CHANNEL SIDE PLATE HAS SURFACE CORROSION FWD PIT. CORRECTION: STA 500-500A 526R FLOOR SUPPORT CHANNEL SIDE PLATE REPLACED WITH MADE REPAIR PART IAW DRAWING 65-20726 REV F AND SRM REV 119 CH 51-30-01.SDR NACA2019071600079Intercostal · corrodedDISCREPANCY: STA 500C-500D INTERCOSTAL: FLANGE STA 500C-500D 5-26R HAS SURFACE CORROSION. CORRECTION:STA 500C-500D INTERCOSTAL AT S-26R REPLACED IAW DWG NR 69-41757 REV - AND SRM 51-40-02 REV 118 AND IAW SRM REV 119 CH 51-30-01.SDR NACA2019042900078Intercostal · corrodedDISCREPANCY: STA 500B - 500C S-26R HAD CORROSION ON INTERCOSTAL. CORRECTION: STA 500B - 500C S-26R INTERCOSTAL REPLACED WITH MADE REPAIR PART IAW DWG NR 69-41473 AND B737-300 SRM 51-40-02 REV 118. IDENTIFIED IAW SRM REV 118 53-30-04. SERVICEABLE.SDR NACA2019042900077Intercostal · corrodedDISCREPANCY: STA 500A- 500B S-26R CORROSION ON INTERCOSTAL. CORRECTION: STA 500A - 500B S-26R INTERCOSTAL REPLACED WITH MADE REPAIR PART IAW DRAWING NO 69-41473 AND SRM 51-40- 02 REV 118 AND 53-30-04 SERVICEABLE. DWG NO 69-41473 REV.SDR NACA2019042900076Plate · corrodedDISCREPANCY: STA 500A - 500D CORROSION ON FLOOR SUPPORT CHANNEL SIDE PLATE AND NUT PLATES. CORRECTION: STA 500A-500D FLOOR SUPPORT CHANNEL SIDE PLATE RT REPLACED IAW SRM 51-40-02 REV 118, CH 51-30-01 AND CH 53-30- 53.SDR NACA2019070800045Skin · corrodedUPPER RT WING SURFACE BETWEEN WBL 71-110 APPROX HAS MULTI CORROSION SPOTS. UPPER RT WING SURFACE BETWEEN WBL71-110 APPROX, MULTIPLE CORROSION SPOTS BLENDED IAW SRM 51-10-02 PARA 14 REV 119. AREAS MARKED A1-A20 REPAIRED IAW SR # 4- 4400528446.SDR NACA2019070800048Skin Panel · corrodedDISCREPANCY: LWR RT WING SURFACE @ WBL 72 APPROX HAS BLISTERING PAINT. CORRECTIVE ACTION: LWR RT WING SURFACE @ WBL 72 APPROX BLISTERING PAINT DETERMINED TO BE CORROSION. REPAIRED IAW SR #4- 4400286260 ISSUED 22 MAR 2019.SDR NACA2019070800049Skin Panel · corrodedDISCREPANCY: STA 500A & 10 BETWEEN STR 20R & 21R CORRODED FASTENERS X3 COMMON TO EXTERIOR SKIN REPAIR. CORRECTIVE ACTION: STA 500A + 10 BETWEEN STR 20R AND 21R CORRODED FASTENERS X3 COMMON TO EXTERIOR SKIN REPAIR REPAIRED IAW SRM REV 119 CH. 53-00-01 REPAIR 35SDR NACA2019070800051Skin Panel · crackedDISCREPANCY: STA.219.8 PILOT SIDE #1 WINDOW EXTERIOR SKIN CRACKED AT UPPER AFT CORNER. CORRECTIVE ACTION: REPAIRED STA219.8 PILOT SIDE #1 WINDOW, EXTERIOR SKIN CRACK AT AFT UPPER CORNER IAW SRM REV 119 53-10-01, REPAIR 10 FIGURE 201.SDR NACA2019070800052Floorbeam · corrodedDISCREPANCY: STA 986 MAIN CABIN RBL 24-45 FLOORBEAM HAS CORROSION. CORRECTIVE ACTION: STA 986 MAIN CABIN RBL 24-45 FLOORBEAM REPAIRED IAW AEI EO 8512 REV IR SEE FAA FORM 8110-3 FOR APPROVAL FOR THE REPAIR ACCOMPLISHED TO BS986 UPPER FLOORBEAM CAP.SDR NACA2019070800053Seat Track · corrodedDISCREPANCY: STA 887-986 MAIN CABIN LBL 45 SEAT TRACK HAS CORROSION ON BOTH FLOORBOARD FLANGES. CORRECTIVE ACTION: INSTALLED MADE REPAIR SEAT TRACK STA 887-986 MAIN CABIN LBL 45 SEAT TRACK IAW AEI DRAWING 5714 REV G.SDR NACA2019070800046Skin · corrodedUPPER RT WING SURFACE @ WBL 522 APPROX HAS CORROSION. UPPER RT WING SURFACE @ WBL 522,608,613 APPROX, CORROSION BLENDED IAW SRM 51-10-02 PARA 14 REV 119. AREAS MARKED D3,D4,D5,D6,D7 REPAIRED IAW KF DWG NR R27905.1-057- 008-001 REV NC.SDR NACA2019070800054Seat Track · corrodedDISCREPANCY: STA 947-1006 MAIN CABIN RBL 24 SEAT TRACK HAS CORROSION ON BOTH FLOORBOARD FLANGES. CORRECTIVE ACTION: STA 947-1006 MAIN CABIN INSTALLED MADE REPAIR PART RBL24 SEAT TRACK IAW AEI DRAWING # AE5714 REV G.SDR NACA2019070800055Seat Track · corrodedDISCREPANCY: STA 927-1006 MAIN CABIN BLO SEAT TRACK HAS CORROSION ON BOTH FLOORBOARD FLANGES. CORRECTIVE ACTION: STA 927-1006 MAIN CABIN INSTALLED MADE REPAIR PART BLO SEAT TRACK IAW AEI DRAWING # AE5714 REV.SDR NACA2019070800044Skin · corrodedUPPER RT WING SURFACE BETWEEN WBL 479-541 APPROX HAS MULTI PAINT BLISTERS. UPPER RT WING SURFACE BETWEEN WBL 479-541 APPROX MULTI PAINT BLISTERS DETERMINED TO BE CORRODED SKIN PANEL AT D1, D2 LOCATIONS. CORRODED SKIN PANEL AT D1, D2 LOCATIONS REPLACED WITH NEWSDR NACA2019070800056Seat Track · corrodedDISCREPANCY: STA 907-1006 MAIN CABIN LBL 24 SEAT TRACK HAS CORROSION ON BOTH FLOORBOARD FLANGES. CORRECTIVE ACTION: INSTALLED MADE REPAIR PART SEAT TRACK AT STA 907-1006 MAIN CABIN LBL 24 IAW AEI DRAWING # AE5714 REV G.SDR NACA2019070800043Skin · corrodedUPPER LT WING SURFACE BETWEEN WBL 71-200 HAS MULTI PAINT BLISTERS BETWEEN FWD & AFT SPAR. UPPER LT WING SURFACE BETWEEN WBL 71-200 BETWEEN FWD AND AFT SPAR PAINT BLISTERS BLENDED IAW SRM 51-10-2 REV 119. BLEND OUTS FOUND TO BE WITHIN LIMITS AND REPAIRED IAW SDR NACA2019070800057Web · corrodedDISCREPANCY: 986 MAIN CABIN RBL32 FLOOR WEB HAS LIGHT CORROSION. CORRECTIVE ACTION: MADE AND INSTALLED NEW MADE REPAIR PART OF FLOOR WEB @ SAT 986 MAIN CABIN RBL 32 IAW SRM 51-40-02 REV 119 AND CH 51-30-01.SDR NACA2019070800058Crease Beam · corrodedDISCREPANCY: 967-986 MAIN CABIN RBL 50 CORROSION ON DUST SILL INB R2 DOOR. CORRECTIVE ACTION: NEW CREASE BEAM INNER CHORD @ R2 DOOR STA 967-986 RBL 50 IN MAIN CABIN INSTALLED IAW DWG G5-52878 REV 5 AND SRM 51-40-02 REV 119.SDR NACA2019070800042Fitting · crackedLEFT HAND MAIN LANDING GEAR BEAM FITTING ON AFT SPAR WBL157, HAS A CRACK INDICATION ON THE FORWARD FITTING. LEFT HAND MAIN LANDING GEAR BEAM FITTING ON AFT SPAR WBL157 CRACK REMOVED IAW SB737-57A1334 REV IR SEPT 16 2017.SDR NACA2019070800060Skin Panel · dentedDISCREPANCY: STA 388 BETWEEN STR 26R + 25R EXTERNAL SKIN DENTS 2 LOCATIONS AS MARKED. CORRECTIVE ACTION STA 388, BETWEEN STR 24+25R, EXTERNAL DENTS IN 2 LOCATIONS REPAIRED IAW SRM 53-00-01 REPAIR 35 REV 119:SDR NACA2019070800041Skin · crackedBS 947 STR MAGER 17L CRACK ON FUSE SKIN AT L2 DOOR FOUND BY INSPECTION SB737-53A1350. BS967 STRINGER 17L CRACK, REMOVED & REPAIRED ON FUSE SKIN AT L2 DOOR IAW SERVICE REQUEST 3-4426422151, SEE FAA FORM 8100-9 FOR THE APPROVAL FOR THE REPAIR, ATTACHED.SDR NACA2019070800061Stringer Clip · crackedDISCREPANCY: STRINGER CLIP @FSTA 500D STR L27 CRACKED. CORRECTIVE ACTION: STR CLIP @ STA 500D STR 27 REPLACED WITH NEW STR CLIP AND INSTALLED IAW SRM REV 119 CH 51-40-02 PARA. 4.
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