Boeing 737-436
Service difficulty reports · 390
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 = '737436' 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 = '737436' 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 EE4Y2022051715611None · crackedDURING HFEC INSPECTION OF FRAMES, IAW AD2016-11-04 AND SB737-53A1279 INSTRUCTIONS, IT WAS FOUND AT FWD CARGO COMPT. BS 500E BETWEEN STR 20R-22R THE FRAME WEB WITH WIRE PENETRATION HOLE AND STANDOFF/TOOLING HOLES WITH CRACK. THE REPAIR WAS CARRIED OUT UNDER AESDR EE4Y2022051715612None · crackedDURING AN OPEN-HOLE HFEC INSPECTION OF FRAME WEB TOOLING HOLES, AND INSULATION ATTACHMENT HOLES ON THE LEFT AND RIGHT SIDE IAW BOEING SB 737-53A1362 IR (SEPT 20, 2018), PART 12, FIGURES 73, 74, 79 AND 80. (REF:AD 2019-15-07 (H): TABLE 11) IT WAS FOUND AT BS 96SDR EE4Y20225241510Keelbeam · corrodedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND ON FWD CARGO COMPT. BETWEEN BS 500G AND BS 520, (S-28L LEVEL) THE KEEL BEAM LOWER FLANGES CORRODED. THE REPAIR WAS CARRIED OUT UNDER ASAP E.O. #5322-020 REV-IR A INSTRUCTIONS WITH FAA FORM 8110-3 APPROVAL.SDR K11A2021110900083Transceiver · inoperativePROBLEM DESCRIPTION: NUMBER 1 VHF COM NOT TRANSMITTING. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: SWAPPED #1 AND #2 VHF COM R/T IAW KCII GMM CHAPTER 1, TRANSFERRED TO DMI # 73400055 IAW KCII B737 MEL 23-3A CAT C DUE 11-19-2021 PLACARDS INSTALLED. REF CSDR K11A2021100100080Door · out of adjustUNABLE TO PRESSURIZE IN AUTO OR STANDBY. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: FOUND AFT CARGO DOOR SLIGHTLY OPEN, ADJUSTED AFT CARGO DOOR IAW B737 AMM 53-11-00. CARGO DOOR CHECK GOOD, PERFORMED OPS CHECK AND LEAK CHECK OF PRESSURIZATION SYSTEM IAW SDR K11A2021090800069Wire · brokenON APPROACH FLAPS WOULD NOT EXTEND PAST 25 WITH FLAPS SELECTED 30, UPON LANDING FLAPS EXTENDED TO 30. R & R RELAY R123 IAW BSWPM 20-81-22 & ADJUSTED LT & RT FLAP TRANSMITTERS IAW AMM 27-51-00. PERFORMED FLAP POSITION INDICATING TEST IAW AMM 27-58-01. OPS CHSDR K11A2021021100043Handle · out of positionREJECTED TAKEOFF CONFIGURATION WARNING ON TAKEOFF. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: FOUND SPEED BRAKE HANDLE NOT STOWED, STOWED SPEED BRAKE HANDLE IAW B737 AMM 27-62-22, PERFORMED TAKEOFF WARNING TEST IAW B737 AMM 31-26-00
OPS CHECK GOOD.SDR K11A2021010600035Transponder · malfunctionedCO PILOT STATIC INSTRUMENT AS WELL AS TRANSPONDER FAILED ON TAKEOFF. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: PERFORMED OPERATIONS CHECK OF THE NR 2 EFIS SYSTEM, IRU SYSTEM, DADC AND ATC SYSTEM, IAW B737 AMM 34-22-00, 34-28-01, 34-12-01 AND 34-53-02. SDR K11A2020120700033Indicator · failedFLAPS FAILED TO EXTEND PAST 15 DEGREES ON LANDING APPROACH. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: R & R TRAILING EDGE FLAP POSITION INDICATOR, IAW B737 AMM 27-58-41. ALL OPERATIONS CHECKS GOOD NO DEFECTS NOTED.SDR K11A2020101800022Warning Light · false activationPROBLEM DESCRIPTION: ABORTED TAKEOFF DUE TO CARGO DOOR LIGHT ILLUMINATING. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: INSPECTED AND PERFORMED OPERATIONS CHECK OF CARGO DOOR, IAW B737 AEI SUPPLEMENTAL AMM 52-33-02, NO DEFECTS NOTED.SDR K11A2020092400020Indicator · failedON TAKEOFF FLAPS SELECTED UP, THE FLAP INDICATOR SPLIT WITH ONE FLAP AT 5 AND THE OTHER AT 1, FLAP STOPPED MOVING. CORRECTIVE ACTION & OTHER PERTINENT INFORMATION: R&R FLAP POSITION INDICATOR, OPS CHECK GOOD IAW B737 AMM 20-50-11 AND 27-58-01 REMOVED E1-1 RASDR K11A202008031006Skin · corrodedDRAIN MAST MATING SKIN SURFACE HAS CORROSION @ #2 & #4 MOUNTING HOLES LOCATED @ STA 986 - 1006 BETWEEN STR 26L & 25LSDR K11A2020080300005Skin · corrodedCORROSION ON INTERNAL SKIN BY #1 FASTENER HOLE OF REMOVED DRAIN MAST LOCATED @ STA 986-1006 BETWEEN STR 24L & 25LSDR DU4R2020070900050Bracket · corrodedBONDING BRACKET LT SIDE OF VERT STAB JUST BELOW UPPER RUDDER HINGE HAS EXFOLIATED CORROSION REQUIRING REPLACEMENT.SDR K11A202007028002Mec · failedDURING TAKEOFF, NR 1 ENGINE HIT 965 DEG. FOR 3 SECONDS UNTIL PULLED BACK. ENGINE WAS REMOVED AND SENT FOR A SHOP VISIT DURING SHOP VISIT, R & R THE EGT HARNESS, RERIGGED THE VSV, AND R & R THE MEC, ENGINE WAS REINSTALLED AND PAST ALL TESTSSDR K11A2020070600002Engine · overtempDURING TAKEOFF NR 1 ENGINE HIT 965 DEG. FOR 3 SECONDS UNTIL PULLED BACK. PERFORMED VISUAL INSPECTION OF NR 1 ENGINE INLET AND EXHAUST, NO DEFECTS NOTED AND PERFORMED BORESCOPE INSPECTION OF THE HTP BLADES AND THE 1ST STAGE LPT BLADES IAW AMM 72-00-00, NO DEFESDR DU4R2020061800049Frame · crackedAD 2019-08-02(H): TABLE 2 / PART 2 AND BOEING SB 737-53A1360,IR,PART 2 INSPECTION FIGURE 7,8,13 AND 14, FORWARD SIDE OF FRAME WEB HAS A CRACK RUNNING OUTBOARD FROM FASTENER HOLE 1/4" LONG BS 500E JUST BELOW STR10LSDR DU4R2020061600047Skin · crackedAIR STAIR DOOR CUTOUT AROUND FWD UPPER HOLE NR 8 WAS CRACKED.SDR DU4R2020061500046Frame · crackedBS360 BETWEEN STR25L AND STR27 6 EACH FASTENER HOLES PRODUCED REJECTABLE INDICATIONS DURING ABHEC INSPECTION. ALL APPLICABLE DISCREPANT HOLES MARKEDSDR DU4R2020061500045Attach Fitting · crackedLEFT MLG BEAM FORWARD SUPPORT FITTING FASTENER HOLE MARKED AS #16 CRACKED AT 1:00. THOUGHT TO BE IN THE WEB LAYER. BOEING SERVICE BULLETIN 737-57A1334,IR, PARAGRAPH 3.B PART 2SDR DU4R20200615045Floor Support · corrodedFORWARD LOWER CARGO COMPARTMENT R/H SIDE STR 26R FLOOR SUPPORT PROFILE HAS CORROSION BETWEEN BS 520-540SDR DU4R2020061500044Floor Support · corrodedFORWARD LOWER CARGO COMPARTMENT LT SIDE STR 26L FLOOR SUPPORT PROFILE HAS CORROSION BETWEEN BS 500D-520.SDR DU4R2020061500043Support · corrodedFORWARD LOWER CARGO COMPARTMENT LH SIDE SIDEWALL SUPPORT HAS CORROSION AT BS 500CSDR DU4R2020061400042Structure · crackedAD2016-13-11 RELATED, UPON FASTENER REMOVAL TO ACCOMPLISH PREVENTIVE MOD AT BS727 FOUND CRACKS GOUGES AND OUT OF ROUND HOLES AT LBL 24.82, LBL 45.57,RBL 24.82 AND RBL 45.57 TOTALING 10 EA HOLESSDR DU4R2020061000041Fitting · crackedAD 2018-09-13(H): TABLE 8/OPTION 1: SERVICE BULLETIN 737-57A1318, R1, PARA 3B PART 3A1, LEFT MLG FORWARD SUPPORT FITTING, AFT SUPPORT FITTING, REAR SPAR UPPER CHORD AND REAR SPAR WEB HOLE 5 IS CRACKED IN THE AFT FITTING AT 600 AND IN THE WEN AT 1:00.SDR DU4R2020061000040Attach Fitting · crackedAD 2018-09-13(H): TABLE 8 / OPTION 1: RT MLG FORWARD FITTING, AFT SUPPORT FITTING, REAR SPAR UPPER CHORD AND REAR WEB, IAW SB 737-57A1318,R1 PARA 3B PART 3 STEP 3A1, HOLE 4 AND 5 ARE CRACKED IN THE AFT FTG AND IN THE UPPER SPAR CHORD.SDR DU4R2020061000039Skin · crackedAFT GALLEY DOOR, FWD LWR CORNER HAS CRACK, EMANATES FROM EDGE, TRAVELS DOWN TO 5TH FASTENER HOLE IN NDT INSPECTION AREA ( SEE SB 737-53A1350 FIG 8) THEN COMES OUT OF THAT HOLE AND TRAVELS DOWN/FWD S INSIDE HOLE,AS MARKED IN BLACKSDR 2020FA0000273Frame · corrodedNON-ROUTINE DISCREPANCY. STA 380, STR 28L-28R, FRAME CORRODED FWD AND AFT SIDES. CORRECTIVE ACTION COMPLIED WITH EA -PD37-53-3139 WITH NO DEVIATIONS PER APPROVED 8110-3.SDR DU4R2020052800038Frame · crackedMAIN CARGO, RT FR360 FOUND CRACK AT STR 13R.SDR DU4R2020052800037Shear Tie · crackedAD 2019-08-02(H): TABLE 3/:PART 3: SB 737-53A1360, IR, PART 3, CABIN BS 360 FRAME TO BODY SHEAR TIE OUTBOARD FLANGE IS CRACKED AT STRINGER 15.SDR DU4R2020052000036Upper Sheet · corrodedAFT CARGO BS 847 STR 25R FLOOR SUPPORT SHEET UPPER SURFACE HAS CORROSIONSDR DU4R2020052000035Frame Angle · corrodedAD 2019-15-07 AFT CARGO COMPARTMENT L/H FRAME AT BS727D UPPER SURFACE ON ANGLE ASSY CORRODED AT SEVERAL LOCATIONS FROMSDR DU4R2020052000034Flap · chafedCHAFING AT RT WING OB FLAP INBD OF MID FLAP LOWER L/E.SDR DU4R2020052000033Floorbeam · corrodedFORWARD LOWER CARGO COMPARTMENT FLOOR BEAM BETWEEN STR 26L-27L HAS CORROSION JUST FWD OF AFT BULKHEADSDR DU4R2020051900032Baffle · crackedLH BAFFLE BETWEEN 400D AND 500E CRACKED AT STRINGER 26LSDR DU4R2020051900031Support Web · crackedLH TRANSITION PANEL SUPPORT WEB AT STR 26L BETWEEN BS 400-420 CRACKEDSDR DU4R2020051900030Baffle · crackedBAFFLE CRACKED BETWEEN FR STATION 500E AND 500F AT STRINGER 26L FWD CARGO PITSDR DU4R2020051900029Stringer Clip · crackedAD 2019-08-02(H): TABLE 2/PART 2 AND BOEING SB 737-53A1360,IR PART 2 INSPECTION FIGURE 7,8,13 AND 14. STRINGER CLIP IS CRACKED AFT SIDE OF FRAME BS727B S10LSDR DU4R2020051900028Stringer Clip · crackedAD 2019-08-02(H):TABLE 2 /PART 2 AND BOEING SB 737-53A1360,IR, PART 2 INSPECTION FIGURE 7,8,13 AND 14, STRINGER CLIP IS CRACKED UPPER AND LOWER FLANGES AFT SIDE OF FRAME BS 500D S10LSDR DU4R2020051900027Channel · corrodedFORWARD LOWER CARGO COMPARTMENT L/H SIDE STR 26L FLOOR SUPPORT SIDE PLATE HAS CORROSION BETWEEN B.S 500B-500CSDR DU4R2020051900026Baffle · crackedCRACKED BAFFLE IN FWD PIT COMP BETWEEN BS 460-480 STR 26LSDR DU4R2020051900025Intercostal · crackedFUSELAGE FWD OF R1 DOOR AT STR 14R ADJACENT TO FRAME BS 277 HAS CRACK IN ITS FWD RADIUS TRIM OUT. REPAIR IN CONJUNCTION WITH SB 737-53A1241.SDR DU4R2020051900024Gusset · gougedAPU DOOR INNER SURFACE GUSSET AND CENTER HINGE SUPPORT GOUGEDSDR DU4R2020051900023Stringer Clip · crackedAD 2019-08-02(H): TABLE 3 /PART3: BOEING SB 737-53A1360,IR, PART 3. CABIN B>S. 420 FORWARD SIDE OF FRAME STRINGER CLIP UPR HORIZ FLANGE AFT FASTENER HOLE IS CRACKED AT STRINGER 16RSDR DU4R2020051900022Stringer Clip · crackedAD 2019-08-02(H): TABLE 3/ PART 3: BOEING SB 737-53A1360,IR,PART 3. CABIN B.S 380 FORWARD SIDE OF FRAME STRINGER CLIP UPR HORIZ. FLANGE AFT FASTENER HOLE IS CRACKED AT STRINGER 15RSDR DU4R2020051900021Stringer Clip · crackedAD 2019-08-02(H)TABLE 3/PART 3: SB 737-53A1360 IR PART 3. CABIN BS 440 FORWARD SIDE OF FRAME STRINGER CLIP LWR HORIZ FLANGE AFT FASTENER HOLE IS CRACKED AT STRINGER 16R.SDR DU4R202005190020Stringer Clip · crackedAD 2019-08-02(H): TABLE 2 / PART 2 AND SB 737-53A1360 IR PART 2 INSPECTION FIGURE 7,8,13 AND 14. STRINGER CLIP IS CRACKED HORIZONTAL FLANGE AFT HOLE S16L FORWARD SIDE OF FRAME BS767.SDR DU4R2020051900019Stringer Clip · crackedFUSELAGE FWD OF R1 DOOR, STRINGER CLIP AT STR 10R, FWD SIDE OF FRAME BS 277 HAS CRACK REPAIR IN CONJUNCTION WITH SB 737-53A1241.SDR DU4R2020051900018Support Plate · corrodedFORWARD LOWER CARGO COMPARTMENT RT SIDE STR26R FLOOR SIDE PLATE HAS CORROSION APPROX 6" FWD BS 500D.SDR DU4R2020051900017Floorbeam · corrodedFORWARD LOWER CARGO COMPARTMENT FLOORBEAM BETWEEN STR 27L-28L HAS CORROSION JUST FWD OF AFT BULKHEAD.
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