Boeing 737-832
Service difficulty reports · 9,893
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 = '737832' 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 = '737832' 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 DALA2025082806367Seat Track · corrodedAIRCRAFT 3767, CORROSION LEVEL 2- SEAT TRACK SECTION LBL 24.75 BTW STA 500H TO 520 AT PAX CABIN FLOOR STRUCTURE. CORRECVTIVE ACTION: REPLACED SEAT TRACK SECTION LBL 24.75 BTW STA 500H TO 520 PER B737-800 SRM 51-40-02-0G PAR. 7. (LP 1165303)SDR DALA2025082806365Seat Track · corrodedAIRCRAFT 3769, CORROSION OUT OF LIMITS ON SEAT TRACK LBL 45 BTW STA 500H+10 TO 520. CORRECTIVE ACTION: CORROSION LEVEL 2. SEAT TRACK LBL 45 BTW STA 500H+10 TO 520 WAS FABRICATED PER BAC 1520-2789 REV. (B) AND B737-800 SRM 53-00-52-2R PROCEDURE 4, REPAIR 4 AND SDR DALA2025082806364Seat Track · corrodedAIRCRAFT 3769, CORROSION OUT OF LIMITS ON SEAT TRACK RBL 45 BTW STA 500H+10 TO 520. CORRECTIVE ACTION: CORROSION LEVEL 2 - SEAT TRACK RBL 45 BTW STA 500H+10 TO 520 WAS FABRICATED PER BAC1520-2789 REV. (B) AND B737-800 SRM 53-00-52-2R PROCEDURE 4, REPAIR 4, ANDSDR DALA2025082806363Seat Track · corrodedAIRCRAFT 3767, CORROSION LEVEL 2- SEAT TRACK SECTION LBL 24.75 BTW STA 500H TO 520 AT PAX CABIN FLOOR STRUCTURE. CORRECTIVE ACTION: REPLACED SEAT TRACK SECTION LBL 24.75 BTW STA 500H TO 520 PER B737-800 SRM 51-40-02-0G PAR. 7. (LP 1163766)SDR DALA2025082806362Receptacle · crackedAIRCRAFT 3769, CRACK ON INNER STRAP ON GROUND POWER RECEPTACLE AT LOWER FUSELAGE. CORRECTIVE ACTION: GROUND POWER RECEPTACLE AT LOWER FUSELAGE WAS REPAIRED PER B737-800 SRM 53-10-15-2R PROCEDURE 5 REPAIR 5. (LP 1163677)SDR DALA2025082806361Receptacle · crackedAIRCRAFT 3769, CRACK ON INNER STRAP ON GROUND POWER RECEPTACLE AT LOWER FUSELAGE. CORRECTTIVE ACTION: GROUND POWER RECEPTACLE AT LOWER FUSELAGE WAS REPAIRED PER B737-800 SRM 53-10-15-2R PROCEDURE 5 REPAIR 5. (LP 1163662)SDR DALA2025082806359Skin · crackedAIRCRAFT 3766, CRACK ON LOWER SKIN APROX STAB STA 101.90 AT RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: CRACK ON LOWER SKIN APROX STAB STA 101.90 AT RH HORIZONTAL STABILIZER WAS REPAIRED PER B737-800 SRM 55-10-01-2R PROCEDURE 11. (LP 1163553)SDR DALA2025082806358Skin · crackedAIRCRAFT 3766, CRACK ON LOWER SKIN APROX STAB STA 101.90 AT RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: CRACK ON LOWER SKIN APROX STAB STA 101.90 AT RH HORIZONTAL STABILIZER WAS REPAIRED PER B737-800 SRM 55-10-01-2R PROCEDURE 11 CATEGORY B REPAIR. (LP 1163546SDR DALA2025082806356Floorbeam · corrodedAIRCRAFT 3769, CORROSION OUT OF LIMITS ON FLOOR BEAM STA 986.5 BTW LBL 45 TO LBL 46. CORRECTIVE ACTION: PREVIOUS REPAIR ON BEAM STA 986 BTW LBL 25/50 WAS REPLACED PER B737-800 SRM 51-40-02-0G. (LP 1163445)SDR DALA2025082806354Frame · crackedAIRCRAFT 3767, INITIAL INSPECTION: CRACK ON FRAME STA 400 BTW STR 9 AND 8 RH SIDE AT PAX CABIN. CORRECTIVE ACTION: FRAME STA 400 BTW STR 9 AND 8 RH SIDE AT PAX CABIN WAS REPAIRED PER B737-800 SRM 53-00-07-2R-1 REPAIR 1. (LP 1162366)SDR DALA2025082806353Seat Track · corrodedAIRCRAFT 3767, CORROSION ON SEAT TRACK RBL 24.75 BTW STA 520 THICKNESS CROWN IS 0.188" AND MINIMUM REMAINING THICKNESS CROWN IS 0.050" THEREFORE AREA OUT OF LIMITS PER B737-800 SRM 53-00-52-1A PROCEDURE 1 ALLOWABLE DAMAGE 1, PAR. 4. A (2) (A) FIG.103 DETAIL A.SDR DALA2025082606336Battery Pack · no test(LOG 7385044) DURING SERVICE CHECK FOUND CABIN EMERGENCY LIGHTS ON R1 DOOR AND RIGHT SIDE 1-4 ROWS INOP. R/R BATTERY PACK PER B737 AMM 33-51. EMERGENCY LIGHTS OPS CHECK GOOD.SDR DALA2025082506283Flap · missingFCNT- AIRCRAFT ARRIVED AUS WITH THE LEFT WING OUTBOARD TRAILING EDGE AFT FLAP MISSING. MAINTENANCE REPLACED LEFT OUTBOARD FLAP, BOTH BELLCRANKS ASSYS, 4 CONTROL RODS AND THE #1 AND 2 FLAP CANOES PER B 737 AMM 27-51. REFER TO LOG PAGES 7056569, 7056570 AND 705SDR DALA2025082506292Skin · damaged(LOG 7056570) FOUND LT O/B FLAP DAMAGED. R/R LT OB FLAP IAW A/C 2750-4569-01.SDR DALA2025082506290Seat Track · corroded(LOG 1158690) CORROSION ON SEAT TRACK LBL 45.50, STA 520 AT PAX CABIN FLOOR STRUCTURE. SEAT TRACK LBL 45.50 BTW STA 500H TO 520 AT PAX CABIN FLOOR STRUCTURE WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025082606333Pressure Deck · cracked(LOG 1155124) A.A AD 5714-01004-02 STEP 8 AND 9 2 CRACKS ON PRESSURE DECK WEB (1CRACK BTW STA 663 AND RBL 35 .593 IN AND 2 CRACK RBL 42 .656. PRESSURE DECK WEB WAS REPAIRED PER B737-800 SRM 57-10-10-2R PROCEDURE 3 AND A.A AD 5714-01004-02.SDR DALA2025082506287Floor Support · corroded(LOG 1156122) CORROSION ON FLOOR SUPPORT UPPER AND LOWER SIDE STA 951 TO 967 BTW LBL 48 AT PAX CABIN. .FLOOR SUPPORT UPPER AND LOWER SIDE STA 951 TO 967 BTW LBL 48 AT PAX CABIN WAS REPLACED AND INSTALLED PER B737-800 SRM 51-40-02-0G.SDR DALA2025082506286Attach Angle · cracked(LOG 1155116) CRACK OF: 0.156 IN LENGTH ON RH VERTICAL PRESSURE DECK WEB ATTACH ANGLE AT THE DRAIN SLOT. VERTICAL PRESSURE DECK WEB ATTACH ANGLE WAS REPAIRED PER B737-800 SRM 57-10-10-2R PROCEDURE 6 AND A.A./ A.D. 5714-01004-02.SDR DALA2025082206273Window Frame · cracked(LOG 1155742) FUSELAGE RH NO. 3 FLIGHT COMPARTMENT WINDOW FRAME E-F POST LOWER CORNER CRACKED. REPAIRED PER ERA 628209-14.SDR DALA2025082206272Window Frame · cracked(LOG 1156206) CRACK OF 0.062 IN LENGTH ON NO. 1 RH WINDOW FRAME RADIUS AREA. NO. 1 RH WINDOW FRAME UPPER CORNER WAS REPAIRED PER ERA 619132-14 AD TR REV. A.SDR DALA2025082206270Floorbeam · corroded(LOG 1154417) CORROSION ON FLOORBEAM AT STA 947 BTW RBL 40-RBL 55. AT PAX CABIN. FLOORBEAM BTW RBL 38.5 TO RBL 59 AND STA 947 WAS REPAIRED PER B737-800 SRM 53-70-51-2R REP. 5.SDR DALA2025082206269Floor Support · corroded(LOG 1154285) CORROSION ON FLOOR SUPPORTS (02 EAS) BTW STA 947- 967 AT RBL 24, & LBL 47 AT PAX CABIN. FLOOR SUPPORTS (2 EA'S) BTW STA 947-967 AT RBL 24 AND LBL 47 AT PAX CABIN WERE REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025082206274Floorbeam · corrodedCORROSION ON FLOORBEAM AT STA 986 BTW RBL 20-RBL 50, AT PAX CABIN. T-CHORD BTW LBL 9 TO RBL 50 WAS REPLACED PER B737-800 SRM 53-70-51-2R PROCEDURE 4, REPAIR 4.SDR DALA2025082506288Window Frame · cracked(LOG 1150740) CRACK ON WINDOW FRAME NO. 3 RH FDW LOWER CORNER AT FLIGHT COMPARTMENT. WINDOW FRAME NO. 3 RH FDW LOWER CORNER WAS REPAIRED PER PRI 628209-14 REV. 0 TO REV. 3 AND ERA 628209-14AD REV. ORIGINAL, SECTION I: PERMANENT REPAIR.SDR DALA2025081906189Skin · damagedFUSELAGE SKIN DAMAGE FS 887 BTWN S-26L AND S-27L. C/W ERA 628536-14 REV ORIG FUSELAGE SKIN DAMAGE FS 887 BTWN S-26L AND S-27L. ENSURED PRI 628536-14 REV 0,1,2,3 MATCHES ERA 628536-14 REV ORIG.SDR DALA2025081906187Skin · cracked(LOG 1151052) A.A 5750-01127-0201 REFERENCE STEP 3. CRACK ON OUTBD LE FLAP RIB WS 182 APROX, AT RH WING. LEADING EDGE FLAP (KRUEGER FLAP NO.4) WAS REPLACED SERVICEABLE PER B737-800 AMM 27-81-11.SDR DALA2025081906185Pressure Deck · crackedCRACK OF 2.000IN (LENGTH) PRESSURE DECK WEB ON LH SIDE STA 663.0 BTW LBL35.0/LBL45.0. PRESSURE DECK WEB ON LH SIDE STA 663.0 BTW LBL35.0 TO LBL45.0 WAS REPAIRED PER B737-800 SRM 57-10-10-2R REPAIR 3. PRESSURE DECK WEB ON LH SIDE STA 663.0 BTW LBL 35.0/LBL45.0 SDR DALA2025081806146Flap System · lockedSHIP 3714 -UFC/DE- DECLARED EMERGENCY DUE TO FLAP LOCKOUT ON APPROACH TO LAND. CORRECTIVE ACTION: REPLACED FSEU. LUBRICATED #1 FLAP ROLLER. AHM REPORT SHOWS #4 SKEW SENSOR INVALID. REPLACED #4 AND #7 SKEW SENSORS. OPS CHECK GOOD.SDR DALA2025081906184Skin · dentedDENT DAMAGE TO THE FUSELAGE SKIN SUSTAINED IN BOS. THE DENTED AREA EXISTS BETWEEN STA 891-902 AND BETWEEN STRINGERS 26L TO 27L. MAINTENANCE REPAIRED DAMAGE PER ERA 628536-14.SDR DALA2025081906183Battery Pack · no testMULTIPLE EMERGENCY LIGHTS INOP NEAR FWD GALLEY LH SIDE. REMOVED AND REPLACED BATTERY PACK EQUIP NUMBER M1675 PER B737 AMM 33-51 AND WDM 33-51-12.SDR DALA2025081906182Floor Support · corrodedCORROSION ON FLOOR ANGLES BTW STA 294-360 RBL 60 AT PAX CABIN. ANGLE LOWER SILL RH STA 257 TO STA 360 WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025081806150Skin · damagedFUSELAGE STA 500F - 500G & STR 9L LIGHTING STRIKE. C/W 628552-14.SDR DALA2025081806147Skin · damagedFUSELAGE STA 500E- 500F & STR 10L LIGHTING STRIKE. C/W RI 628552-14.SDR DALA2025081806144Floor Support · corrodedCORROSION OUT LIMITS MEASUREMENT THICKNESS WAS ACCOMPLISHED FLOOR SUPPORTS (1 EAS) BTW STA 328-344 LBL 12. FLOOR SUPPORT (1 EAS) BTW STA 328-344 LBL 12 PAX CABIN WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025081806143Angle · corrodedCORROSION ON ANGLE BTW STA 980 TO 960 LBL 54 AT PAX CABIN. ANGLE BTW STA 980 TO 960 LBL 54 AT PAX CABIN WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025081506107Angle · corrodedCORROSION ON LONGITUDINAL ANGLE FROM STA 312 TO STA 323.7 AND STRG S-23L AT E/E COMPARTMENT. LONGITUDINAL ANGLE FROM STA 312 TO STA 323.7 AND STRG S-23L AT E/E COMPARTMENT WAS REPAIRED PER ERA 628115-14 REV. ORIGINALSDR DALA2025081406096Plate · corroded(LOG 1138154) CORROSION ON SIDE PLATE LH STA 450 TO 500I AT FWD CARGO COMPARTMENT. SIDE PLATE LH STA 450 TO 500I AT FWD CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025081406095Skin · cracked(LOG 1138000) CRACK ON LOWER SKIN AT STAB STA 157.10 AT RH HORIZONTAL STAB. LOWER SKIN AT STAB STA 157.10 AT RH HORIZONTAL STAB WAS REPAIRED PER B737-800 SRM 55-10-01-2R REPAIR 11.SDR DALA2025081406093Floorbeam · corroded(LOG 1137870) CORROSION ON FLOOR BEAM UPPER CHORT AT STA 344 BTW RBL 1-LBL 5. FLOOR BEAM UPPER CHORT AT STA 344 BTW RBL 3 TO LBL 5 WAS REPAIRED PER B737-800 SRM 53-10-51-2R REPAIR 8.SDR DALA2025081406092Frame · damaged(LOG 1136820) FRAME 203.8, LOWER LOBE DAMAGED. PROCURED LOWER CHORD AND WEB. POSITIONED PER BOEING DRAWING 141A1503. MATCH DRILLED PER BOEING B737 DRAWING 141A1503 (RJD 471692). INSTALLED LOWER LOBE FRAME 203.8 PER BOEING DRAWING 141A1503.SDR DALA2025081406091Frame · cracked(LOG 1136833) BHEC CRACK INDICATION IN STA 196.5 L/H FRAME SPLICE WEB. COMPLETED DRILLING SPLICE PLATE PER BOEING DRAWING 141A1502 (RJD 471692) OKAY TO TREAT AND PRIME (QC 5332). TREATED AND PRIMED (RJD 471692). INSTALLED SPLICE PLATE PER BOEING DRAWING 141A15SDR DALA2025081406090Frame · damaged(LOG 1136825) FRAME 196.5, LOWER LOBE DAMAGED. COMPLETED INSTALLATION OF LOWER LOBE FRAME 196.5 PER BOEING DRAWING 141A1502.SDR DALA2025081306053Actuator · looseSEAT ROW 30 D + E LOOSE. FOUND SEAT ACTUATORS LOOSE.TIGHTENED HARDWARE. BOTH SEATS 30 D AND E SECURED.SDR DALA2025081306052Intercostal · corrodedCORROSION ON SEVERAL INTERCOSTALS (9 EAS) BTW STA 450 TO STA 500I WAS FOUND AFTER REMOVAL OF LH SIDE PLATE AT FWD CARGO COMPARTMENT. INTERCOSTALS (9 EAS) BTW STA 500 TO STA 500I OF LH SIDE PLATE AT FWD CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0SDR DALA2025081105974Floor Support · corroded(LOG 1132978) CORROSION ON INTERCOSTAL (1 E/A) STA 460 TO 480 LH SIDE. INTERCOSTAL (1 E/A) STA 460 TO 480 LH SIDE WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025081105971Elec Connector · damaged(LOG 7056962) SEAT 32 EXIT AISLE LIGHT INOP. REPLACED CONNECTOR ON PSU END IAW B737 SWPM 20-42-01 OP'S CHECKED GOOD.SDR DALA2025081105969Frame · ground damage(LOG 1131559) REMOVED FRAME 188; LOWER LOBE, DUE TO IMPACT DAMAGE. INSTALLED FOR ALIGNMENT REF B737 DRAWING 141A1501 (RJD 471692). REMOVED WEB AND LOWER CHORD, DEBURRED AND PRIMED ALL BARE METAL . COMPLETED INSTALLATION OF FRAME 188 LOWER LOBE PER BOEING 737 DSDR DALA2025081105970Seat · loose(LOG 7717042) SEATS LOOSE IN TRACK 3AB, 3CD, 12DEF, 13DEF, 14DEF, 19DEF, 20DEF, 21DEF, 22DEF, 23DEF, 24DEF, 25DEF, 26DEF, 27DEF, 29DEF, 32DEF. SECURED SEATS REF B737 AMM 25-22.SDR DALA2025081105964Seat Track · corroded(LOG 1130647) CORROSION ON FLOOR SUPPORT STA 500I BTW LBL 17. FLOOR SUPPORT (TRACK) ON STA 500 G +24 TO STA 500 I LBL 17 WAS REPAIRED PER B737-800 SRM 53-00-53-2R PROCEDURE 3.SDR DALA2025080705913Brake · fireFIRE/BRAKE- #1 BRAKE FIRE ON GATE ARRIVAL. PERFORMED AXLE INSPECTION. NO DAMAGE NOTED. REPLACED NR 1 & 2 BRAKE AND WHEEL ASSEMBLIES. REPLACED NR 1 WHEEL SPEED TRANSDUCER. OPS CHECKS GOOD.
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