Boeing 737-832
Service difficulty reports · 9,903
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 DALA2025060504291Plate · corroded(LOG 1003178) CORROSION ON SIDEPLATE BTW STA 500A TO STA 500I AND RBL=23 AT FWD CARGO. SIDE PLATE BTW STA 500A TO STA 500I AND RBL=23 AT FWD CARGO WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025060504290Plate · corroded(LOG 1003164) CORROSION ON UPPER AN LOWER SURFACE OF SIDE PLATE LH BTW STA 727G TO 847 AT AFT CARGO COMPARMENT. SIDE PLATE LH BTW STA 727G TO 847 AT AFT CARGO COMPARMENT WAS REPLACED PER B737-800 SRM 51-40-02-0GSDR DALA2025060504289Plate · corroded(LOG 1003151) CORROSION ON UPPER AN LOWER SURFACE OF SIDE PLATE LH BTW STA 727 TO 727G AT AFT CARGO COMPARMENT. SIDE PLATE LH BTW STA 727 TO 727G AT AFT CARGO COMPARMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025060304245Bulkhead Web · gouged(LOG 1001891) WING CENTER SECTION REAR SPAR VERTICAL PRESSURE DECK, BS 663 RBL 25-45 HAS HOLES WITH GOUGE. ASSOCIATED ER/A 14-626327 ADDED FOR AC 3752.SDR DALA2025060304244Bulkhead Web · gouged(LOG 1002166) GOUGES WERE FOUND ON HOLES (5EAS) VERTICAL PRESSURE DECK WEB, VERTICAL STIFFENERS AND ATTACH ANGLE AT RH SIDE AS FOLLOW: HOLE # 1 GOUGE AT 6 O CLOCK POSITION ON ATTACH ANGLE AND PRESSURE DECK WEB, HOLE #2 GOUGE AT 5 O CLOCK POSITION ON ATTACH ANGSDR DALA2025060304243Box Beam · corroded(LOG 1001651) CORROSION ON BOX BEAM STA 948 LBL 24 AND RBL 24 AND 45 AT CPAX. BOX BEAM STA 948 LBL 24 AND RBL 24 AND 45 AT CPAX WERE REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025060304242Floorbeam · corroded(LOG 1001625) CORROSION ON FLOOR BEAM (PREVIOUS REPAIR) STA 986.5 , BTW LBL 55 AND RBL 55 AT CABIN PAX. FLOOR BEAM (PREVIOUS REPAIR) ON STA 986.5 BTW LBL 55 AND RBL 55 AT CABIN PAX WAS REPLACED PER B737-800 SRM 53-70-51-2R PROCEDURE 4. REPAIR 4.SDR DALA2025060304241Window Frame · cracked(LOG 1001259) CRACK OF 0.180IN ON INNER CORNER RADIUS OF NO. 1 RH WINDOW FRAME. FRAME WAS REPAIRED PER ERA 619132-14ADTR REV. A. SECTION II: PERMANENT REPAIR.SDR DALA2025060304240Window Frame · cracked(LOG 1001254) CRACK OF 1.200IN ON INNER CORNER RADIUS OF NO. 1 LH WINDOW FRAME. INNER CORNER RADIUS OF NO. 1 LH WINDOW FRAME WAS REPAIRED PER ERA 619132-14ADTR, REV A, SECTION I: PERMANENT REPAIR.SDR DALA2025060304239Window Frame · cracked(LOG 1001217) CRACK OF 0.180IN ON INNER CORNER RADIUS OF NO. 1 RH WINDOW FRAME. FRAME WAS REPAIRED PER ERA 619132-14ADTR REV. A.SDR DALA2025060204215Stringer · corroded(LOG 1000515) CORROSION ON STRINGER (TERMINAL) S-24LH IN FRONT STA 540 AT FWD CARGO COMPARTMENT. STRINGER (TERMINAL) S-24LH IN FRONT STA 540 AT FWD CARGO COMPARTMENT WAS REPAIRED PER B737-800 SRM 53-00-03-2R.SDR DALA2025060204216Skin · corroded(LOG 0998694) DURING CURRENT H CHECK AT TECHOPS (QRO) WHILE ACCOMPLISHING ZONAL INSPECTIONS PER 2550-2418/009, THE FUSELAGE EXTERNAL SKIN WAS FOUND CORRODED BETWEEN BSTA 787 AND BSTA 807 AND BETWEEN S-27L AND S-27R. DAMAGE REPAIRED PER ERA 626303-14 REV A.SDR DALA2025060204214Stringer · corroded(LOG 1000189) CORROSION ON STRINGER S-25LH IN FRONT STA 540 AT FWD CARGO COMPARTMENT. SECTION OF LONGERON 25 LH FROM STA 500I +10 TO STA 540 AND REPAIR SPLICE WERE REPLACED PER B737-800 SRM 53-00-03-2R REPAIR 1.SDR DALA2025060204213Stringer · corroded(LOG 0999979) CORROSION ON STRINGER (TERMINAL) S-26RH IN FRONT STA 540 AT FWD CARGO COMPARTMENT. STRINGER S-26RH IN FRONT STA 540 AT FWD CARGO COMPARTMENT WAS REPAIRED PER B737-800 SRM 53-00-03-2R REPAIR 1.SDR DALA2025060204212Doubler · corroded(LOG 0999418) CORROSION ON DOUBLER AND FUSELAGE SKIN BTW S27L AND S27R STA 800 AT AFT CARGO COMPARTMENT. FUSELAGE SKIN BTW S27L AND S27R STA 800 AT AFT CARGO COMPARTMENT WAS REPAIRED PER PRI: 626303-14, REV:0 TO REV: 3 AND ERA 626303-14 REV. ORIGINAL.SDR DALA2025060204211Stringer Splice · corroded(LOG 0998309) CORROSION ON LOGITUDINAL LAP SPLICE BTW BS= 28 TO 312 STRINGER 30 AND 29LH AT E/E COMPARTMENT. LOGITUDINAL LAP SPLICE (INTERCOSTAL) BTW BS=328 TO 312 STRINGER 30 AND 29LH AT E/E COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025060204210Access Panel · corroded(LOG 0998144) AFTER CLEANING FUEL TANK ACCESS DOORS, SEVERAL CORROSION WAS FOUND ON ACCESS #632HB, RH WING. FUEL TANK ACCESS DOORS #632HB ON RH WING WAS REPLACED PER B-737-800 IPC: 28-11-11-02 ITEM: -140 AND WILL BE INSTALL PER AMDS: 2820-0599.SDR DALA2025060204209Plate · corroded(LOG 0998075) CORROSION ON RH SIDEPLATE FROM STA 500 TO STA 500I FWD CARGO. RH SIDEPLATE FROM STA 500 TO STA 500I FWD CARGO WAS REPLACED PER DGW 143A8126 REV. B AND B737-800 SRM 51-40-02-0G.SDR DALA2025060204208Fitting · corroded(LOG 0996026) CORROSIONS ON UPPER INNER CHORD (FITTING) ON S-27RH BTW STA 520 AND STA 540 AT FWD CARGO COMPARTMENT. UPPER INNER CHROD FITTING ON S-27RH BTW STA 520 AND STA 540 AT FWD CARGO COMPARTMENT WAS REPAIRED PER ERA 626316-14 REV. ORIGINAL SECTION I PERMSDR DALA2025060204207Floor Support · corroded(LOG 0995823) CORROSION ON FLOOR SUPPORT (SHIELD) BTW STA 767 TO 794.3 BTW STRG 25R/26R AT AFT CARGO COMPARMENT. FLOOR SUPPORT (SHIELD) BTW STA 767 TO 794.3 BTW STRG 25R/26R AT AFT CARGO COMPARMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025053004157Attach Angle · cracked(LOG 0995067) CRACK OF: 0.220 IN LENGTH ON RH VERTICAL PRESSURE DECK WEB ATTACH ANGLE AT THE DRAIN SLOT. RH VERTICAL PRESSURE DECK WEB ATTACH ANGLE AT THE DRAIN SLOT WAS REPAIRED PER B737-800 SRM 57-10-10-2R-6 PROCEDURE 6 REPAIR 6. ASSOCIATED AA 5714-01004 ADDSDR DALA2025053004161Metering Valve · failedSHIP 3713 -DIV/GEAR- DIVERTED TO JFK DUE TO LOUD NOISE FROM NOSE WHEEL AFTER TAKEOFF. CORRECTIVE ACTION: MAINTENANCE REPLACED BOTH NOSE WHEELS AND THE NOSE STEERING METERING VALVE. ALL RTS TEST NORMAL.SDR DALA2025053004156Intercostal · corroded(LOG 0994513) CORROSION WAS FOUND INTERCOSTAL BELOW SIDE PLATE BETWEEN STA 500F AND 500G. INTERCOSTAL BELOW SIDE PLATE BETWEEN STA 500F AND 500G WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025053004155Skin · worn(LOG 0994349) WORN AROUND CUT OUT OF EXTERNAL POWER DOOR. CUT OUT OF EXTERNAL POWER DOOR WAS REPAIRED PER ER/A 566156-14 REV. C SECTION III PERMANENT REPAIR AND PRI 566156-14 REV. 1.SDR DALA2025053004154Gust Lock · malfunctioned(LOG 0994320) R-2 PASSENGER DOOR PUSH BUTTON RELEASE ( GUST LOCK ) WILL NOT LOCK WHEN DOOR IN FULLY OPEN POSITION. REMOVED AND REPLACED IAW B737 AMM 52-41-21-400-801. PERFORMED SATISFACTORY, R-2 PASSENGER DOOR PUSH BUTTON RELEASE ( GUST LOCK ) TEST IAW B737 AMSDR DALA2025053004153Web · corroded(LOG 0993663) CORROSION ON WEB STA 987 RBL 39 ALSO ON STA 1017 RBL 37 AT CPAX. WEB STA 987 RBL 39 ALSO ON STA 1017 RBL 37 AT CPAX WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025053004152Seat Track · corroded(LOG 0991762) SEAT TRACK OUTBOARD LH SIDE IN STA 500 I + 18 TO 500 I +20 AT CAB. PAX. HAS CORROSION. ORIGINAL THICKNESS AND CROWN IS 0.530IN MINIMUM REMAINING THICKNESS IS 0.502 IN THEREFORE AREA REWORKED IS OUT OF LIMITS AT CPAX. SEAT TRACK OUTBOARD LBL 24.75SDR DALA2025053004151Pin · missing(LOG 0991308) L-2 DOOR, SCAPE SLIDE MISSING BOTTLE LOCKOUT PIN. INSTALLED MISSING SAFETY PIN ON THE ESCAPE SLIDE IAW B737 AMM 25-66-01. REMOVAL AND ACTIVATION OF PIN TO BE ACOMPLISHED ON AMDS T/C 2560-4426SDR DALA2025052904134Fitting · corroded(LOG 0990074) CORROSION ON FLOOR FITTING (4EAS) AT CLOSET. FLOOR FITTING (4EAS) AT CLOSET WERE REPLACED PER ER/A NO. 626423-14 REV. ORIGINAL.SDR DALA2025052904133Intercostal · corroded(LOG 0990214) INTERCOSTAL; STA 291 RBL 41; INTERCOSTAL STA 307 LBL ,STABILIZER STRAPS STA 318 TO STA 328 LBL/RBL 11; STABILIZER STRAP STA 331 AND STA 340 LBL 12 CORROSION.SDR DALA2025052904132Doubler · corroded(LOG 0989278) CRACKS SEVERAL SECTIONS ON INNER DOUBLER AT EXTERNAL POWER PANEL. SECTIONS ON INNER DOUBLER AT EXTERNAL POWER PANEL WAS REPAIRED PER B737-800 SRM 53-10-15-2R REP. 5.SDR DALA2025052904131Floorbeam · corroded(LOG 0988528) CORROSION ON BEAM W2 STA 947 LBL 50 TO LBL 54 AT CPAX. BEAM W2 STA 947 LBL 50 TO LBL 54 WAS ALTERNATIVE 2 REPAIRED PER B737-800 SRM 53-70-51-2R PROCEDURE 5 REPAIR 5.SDR DALA2025053004150Window Frame · cracked(LOG 0987923) CRACK ON UPPER AFT CORNER FRAME OF NO.1 RH WINDOW AT COCKPIT. WINDOW AT COCKPIT WAS REPAIRED PER ER/A 619132-14ADTR REV A.SDR DALA2025052904130Intercostal · corroded(LOG 0988039) CORROSION ON INTERCOSTAL W2 STA 950 LBL 50 AT CPAX. INTERCOSTAL W2 STA 950 LBL 50 AT CPAX WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025052904129Plate · corroded(LOG 0987969) CORROSION ON RH SIDEPLATE FROM STA 727E+8 TO STA 767 AT AFT CARGO COMPARTMENT. RH SIDEPLATE FROM STA 727E+8 TO STA 767 AT AFT CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2025052904128Frame · damaged(LOG 0987724) ACCOMPLISH AMDS 5311-01251-02B - RIGHT HAND STA 727 FRAME INNER CHORD, 737 REPAIR; RII; SECTION 02. COMPLIED WITH AMDS CARD 5311-01251-02B. INSTALL A NEW SHIM R/H SIDE STA 727 FRAME INNER CHORD S-18A. (AD 2023-06-15) (BOEING SERVICE BULLETIN 737-SDR DALA2025052904127Frame · damaged(LOG 0987719) ACCOMPLISH AMDS 5311-01251-02A - LEFT HAND STA 727 FRAME INNER CHORD, 737 REPAIR; RII; SECTION 02. COMPLIED WITH AMDS CARD 5311-01251-02A. INSTALL A NEW SHIM L/H SIDE STA 727 FRAME INNER CHORD S-18A. (AD 2023-06-15) (BOEING SERVICE BULLETIN 737-5SDR DALA2025052904126Floorbeam · corroded(LOG 0987657) CORROSION ON FLOORBEAM W2 STA 986 LBL 37 TO LBL 39 AT PAX CABIN. FLOORBEAM W2 STA 986 LBL 37 TO LBL 39 AT PAX CABIN WAS REPAIRED PER ER/A 464736-14MA REV.ASDR DALA2025052804121Elec Connector · disconnected(LOG 7146958) ROW 15D EEPL LIGHT INOP. FOUND EEPL LIGHT HARNESS CONNECTOR UNPLUGGED. REINSTALLED OLD EEPL LIGHT ASSY. PER B737 AMM 33-51. ROW 15D EEPL LIGHT OPS CHECK GOOD.SDR DALA2025052804120Door · lack of lube(LOG 7093557) MAIN CABIN DOOR COULD NOT BE OPERATED FROM OUTSIDE BY GATE AGENT. LUBED L1 DOOR PER B737-800 AMM 51-11, PERFORMED OPEN/CLOSE OPS CHECK PER B737-800 AMM 52-11. L1 DOOR OPERATES NORMAL.SDR DALA2025052804119Floor Support · corroded(LOG 0983775) CORROSION UNDER NUTPLATES IN AFT CARGO FLOOR STRUCTURE SUPPORT STRINGER APPROX' BS.773 RBL.7.5. REMOVED AND REPLACED ANGLE IAW B 737 SRM 51-40-02.SDR DALA2025052804117Frame · corroded(LOG 0988241) SEVERAL CORROSION ON FRAME STA. 907 BTW S- 24L AND S-25L AT AFT CARGO COMPARTMENT. FRAME STA. 907 BTW S-24L AND S-25L AT AFT CARGO COMPARTMENT WAS REPAIRED PER ER/A 626212-14 REV. ORIGINAL.SDR DALA2025052704089Frame · corroded(LOG 0981758) DURING HCK AT QRO, WHILE PERFORMING AFT CARGO COMPARTMENT INSPECTIONS PER WC 5300-2190, CORROSION WAS FOUND AFFECTING THE FUSELAGE FRAME AT STA 907 BETWEEN S-23L AND S-24L. REPAIRED DAMAGE PER ERA 626212-14.SDR DALA2025052704087Bulkhead Web · cracked(LOG 0982606) CRACKED LEFT VERTICAL PRESSURE DECK WEB AT BSTA 663 LBL 36 AT WING BOX AREA. VERTICAL PRESSURE DECK WEB AT BSTA 663 LBL 36 AT WING BOX AREA WAS REPAIRED PER B737-800 SRM 57-10-10-2R-3 REPAIR 3.SDR DALA2025052704086Button · intermittent(LOG 0981775) R-1 PASSENGER DOOR RELEASE BUTTON INTERMITTENT. REMOVED R-1 PASSENGER DOOR RELEASE BUTTON IAW B737 AMM 52-41-21. CLEANED EXCESS SEALANT AND DEBRIS FROM R-1 PASSENGER DOOR RELEASE BUTTON IAW DELTA PROCESS STANDARD 900-1 NO.07. REINSTALLED AND PERFSDR DALA2025052704085Skin · damaged(LOG 0981754) POSSIBLE ELECTRICAL ARCING IN MAIN CABIN FUSELAGE SKIN APPROX BS.282 BETWEEN STR.2L AND 3L. INSTALLATION OF DOUBLER,TRIPLER AND FILLER IAW B737 SRM 51-40-02, IAW B 737 SRM 53-00-01-2R-35.SDR DALA2025052704084Pressure Deck · damaged(LOG 0981068) GOUGES WERE FOUND ON TWO FASTENER HOLES AT THE RH VERTICAL PRESSURE DECK WEB COMMON TO THE UPPER COMPRESSION CHORD. HOLES AT RH PRESSURE DECK WEB WAS REPAIRED PER PRI: 626166-14, REV: 3 AND ER/A 626166-14 REV. ORIG.SDR DALA2025052704083Attach Angle · damaged(LOG 0981065) GOUGES WERE FOUND ON THREE FASTENER HOLES AT THE RH ATTACH ANGLE AND ON THREE FASTENER HOLES AT RH VERTICAL PRESSURE DECK WEB. HOLES AT RH PRESSURE DECK WEB WAS REPAIRED PER PRI: 626166-14, REV: 3 AND ER/A 626166-14 REV. ORIG.SDR DALA2025052704090Pressure Blkhd · damaged(LOG 0980586) VERTICAL PRESSURE DECK AT STA 662 AND BTW RBL 22 & RBL 44 WEB & ANGLE HOLES GOUGES. ASSOCIATED AA 5714-01004 ADDED FOR AC 3751, ASSOCIATED ER/A 14-626166 ADDED FOR AC 3751.SDR DALA2025052704082Doubler · damaged(LOG 0980649) MISSING SECTION ON INNER DOUBLER AT EXTERNAL POWER PANEL. REPAIRED PER REPAIR PER B737-800 SRM 53-10-15-2R-5 PROCEDURE 5 REPAIR 5.
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