Boeing 737-824
Service difficulty reports · 9,839
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 = '737824' 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 = '737824' 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 CALA2026010712735Skin · crackedRIGHT STAB LOWER SKIN NR 2, CRACK INDICATION FOUND, HSS 184.70 INBD OF INBD ROW OF FASTENERS, AFT OF FWD SPAR. REMOVED THE DAMAGE & ACCOMPLISHED A REPAIR OF THE DAMAGE AT THE RT STAB LOWER SKIN NR 2 HAS CRACKED AT BS 184.70 INBD OF INBD ROW OF FASTENERS AFT OSDR CALA2025122912476Floorbeam · crackedMAIN CABIN BS 540 LBL 1 FLOORBEAM CRACKED. R & R THE FLOORBEAM IAW SRM 51-40-02-0G-0.SDR CALA2025122412393Skin · crackedBROKEN DOUBLER AT PREVIOUS REPAIR OF POWER RECEPTACLE SURROUND SKIN. INSTALLED REPAIR PARTS AT POWER RECEPTACLE AREA IAW SRM 53-10-15-2R-4, REPAIR 4.SDR CALA2025122412391Balance Weight · corrodedRIGHT WING AILERON BALANCE BAY MOST INBD WEIGHTS (5EA) HAVE SIGNS OF CORROSION. R & R RT WING AILERON BALANCE BAY MOST INBD WEIGHTS (5EA) IAW SRM 51-40-02-0G-0, AMM 27-11-31-400-801, PAR 3, G. (M), STEPS 1 TO 3, OPS TESTED OK.SDR CALA2026090119152Floorbeam · corrodedAFTER FURTHER EVALUATION FOUND CORROSION OUT OF LIMITS ON FWD WET AREA FLOORBEAM BS 344 AND LBL 56, REQ REPAIR. PERFORMED THE REPAIR TO THE BS 344 FLOORBEAM IAW ECRA 531 0-08749 .SDR CALA2026011312915Stub Frame · crackedCRACK FOUND AT FWD GALLEY DOOR STUB FRAME INTERNAL ABOVE SEAL DEPRESSOR. CRACK LENGTH ; 1". (REF AAR 99981339) REMOVED AND REPLACED R1 GALLEY DOOR CUTOUT FWD UPPER CORNER STUB FRAME REF. USED B737-800 SRM 51-40-02-0G-0 AND DRW 141A8370. REMOVED AND REPLACED SDR CALA2026010712734Floorbeam · corrodedMAIN CABIN STA 328, FLOORBEAM UPPER SURFACE CORRODED AT APPROX RBL 54. REMOVED DAMAGE, ORIG THICKNESS .130, REMOVED .038, REMAINING .092 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51-1A-1. REPAIRED DAMAGED SECTION OF FLOORBEAM IAW SRM 53-10-51-2R-7.SDR CALA2026010212592Pressure Panel · deformedFLIGHT DECK FLOOR HAS DENTS BETWEEN BS 260 AND BS 270 AND BETWEEN LBL 15 AND RBL 15. REPAIRED FLIGHT DECK FLOOR WEB IAW AAR REO-G25697 REV IR AND UAL ECRA 5310-08753. REPAIR COMPLETED PER ECRA 5310-08753. PER ECRA NOT MAJOR REPAIR.SDR CALA2025122912474Angle · crackedLOWER FUSELAGE BS 663 VAPOR BARRIER UPPER ANGLE CRACKED AT RBL 7". REPAIRED THE ANGLE IAW SRM 57-10-10-2R-5.SDR CALA2025122912470Angle · crackedLOWER FUSELAGE STA 663 VAPOR BARRIER UPPER ANGLE CRACKED AT LBL 7". ACCOMPLISHED REPAIR AT BS 663 LT VAPOR BARRIER UPPER ANGLE FROM LBL 5 TO LBL 30 PER SRM 57-10-10-2R-5.SDR CALA2025122912468Skin · corrodedFUSELAGE SKIN CUTOUT AROUND LAVATORY EXHAUST VENT HAS CORROSION. REPAIR ACCOMPLISHED IAW SRM 53-70-01-2R-3, REPAIR 3 FIGURE 201-203.SDR CALA2025122412426Sensor · out of adjustON DESCENT, FWD SERVICE DOOR OPEN LIGHT ILLUMINATED. CONFIRMED DOOR IS LATCHED & SECURED CLOSED. PLACING DOOR WARNING LIGHT SYS ON DEFERRAL IAW MEL 5203F. ITEM HAS HISTORY. DOOR RIGGING, PERFORMED PSEU BITE TEST OF SENSOR S194 FWD SERVICE DOOR FOUND GAP SDR CALA2025122412419Door · missingOPS REPORTED ON ARRIVAL TO LIR EXTERIOR LAV SERVICE DOOR MISSING. MISSING LAV SERVICE DOOR ASSY ON ARRIVAL TO LIR. SERVICE DOOR PLACED ON CDL 52D AND PDA CONDITIONAL INSPECTION COMPLETED REF AMM TASK 05-51-59-200-801 SDR SELECTED AS REQUIRED PER GMM 02-30-95.SDR CALA2025122312363Fitting · wornNLG RETRACT ACTUATOR UPPER FITTING BEARING HAS SIDE TO SIDE PLAY IN HOUSING. R & R THE NLG ACTUATOR UPPER FITTING IAW SRM 51-40-02-0G-0, AND SRM 51-40-05-0G-0.SDR CALA2025122312354Skin · corrodedFOUND BULGING CORROSION ON RT WING INBD FRONT SPAR FUEL BOOST PUMP TANK NR 2 FWD AT LOWER CUTOUT SKIN BONDING STRAP ATTACHMENT POINT. REPAIR ACCOMPLISHED IAW ESR-WI 4-13335 AND ECRA 5720-03597.SDR CALA2025122312314Battery Pack · inoperativeRIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE. ATTEMPTED TO REMOVE COVER BUT 2 NUT PLATES WERE BROKEN IN THE BACK. COMPLETED UP TO STEP 5 OF THE RH AFT EMERGENCY WING LIGHT ASSEMBLY REF AMM 33-51-04-960-802. COMPLETED LIGHT ASSY INSTALL UP TO STEP G12 AMM 33SDR CALA2025122112280Light · no testSEAT 36C EMERGENCY LIGHT IS OUT. EMERGENCY LIGHTS - OPS CHECKED EMERGENCY LIGHTS, REMOVED AND REPLACED EMERGENCY LIGHT ASSY. AT SEAT 36C IAW AMM 33-51-15.SDR CALA2026012213134Rib · crackedRIGHT HORIZONTAL STAB INBD SIDE OF RIB AT HSS 101.90 IS CRACKED AT THE LOWER TRANSITION RADIUS OF THE NR 1 VERTICAL STIFFENER. REPAIRED THE NR 1 VERTICAL STIFFENER INBD SIDE OF RIB IAW SRM 55-10-09-2R-4, TABLE 201, REPAIR 4.SDR CALA2026012213132Rib · crackedRIGHT HORIZONTAL STAB INBD SIDE OF RIB AT HSS 92.70 CRACKED AT THE LOWER TRANSITION RADIUS OF THE NR 4 VERTICAL STIFFENER. REPAIRED NR 4 VERTICAL STIFFENER INBD SIDE OF RIB IAW SRM 55-10-09-2R-4, TABLE 201, REPAIR 4.SDR CALA2026012213130Rib · crackedRIGHT HORIZIZONAL STAB INBD SIDE OF RIB AT HSS 92.70 IS CRACKED AT THE LOWER TRANSITION RADIUS OF THE NR 3 VERTICAL STIFFENER. REPAIRED THE NR 3 VERTICAL STIFFENER INBD SIDE OF RIB AT HSS 92.70 IAW SRM 55-10-09-2R-4, TABLE 201, REPAIR 4.SDR CALA2025122912463Beam · crackedAFT CARGO DOOR, INTERNAL BEAM ASSEMBLY 146A6117-8 IS CRACKED AT FASTENER HOLE. REMOVED AND REPLACED BEAM IAW DWG 146A6110 REV C, BAC DWG 146A6117 REV A, AND SRM 51-40-02 REF AAR GSO.SDR CALA2025122412389Rib · crackedRIGHT HORIZONTAL STAB INBD SIDE OF RIB AT HSS 101.90 WAS CRACKED AT THE LOWER TRANSITION RADIUS OF THE NR 2 VERTICAL STIFFENER. REPAIRED NR 2 VERTICAL STIFFENER AND INBD SIDE OF RIB AT STA 101.90 R/H HORIZ STAB IAW B737-800 SRM 55-10-09-2R-4 TABLE 201 REPAIR SDR CALA2025122312348Battery Pack · no testEMERGENCY LIGHT BATTERY M1676 FAILED A CAPACITY CHECK. REMOVED AND REPLACED THE BATTERY PACK FROM EMERGENCY POWER SUPPLY M1676 IAW AMM 33-51-06-960-805, OPS TESTED GOOD.SDR CALA2025122312342Battery Pack · no testEMERGENCY LIGHT BATTERY M1675 FAILED A CAPACITY CHECK. REMOVED AND REPLACED EMERGENCY BATTERY PACK M1675 IAW AMM 33-51-06-960-805. OPS TESTED GOOD.SDR CALA2025122312340Battery Pack · no testEMERGENCY LIGHT BATTERY M1671 FAILED A CAPACITY CHECK. REMOVED AND REPLACED THE BATTERY PACK M1671 IAW AMM 33-51-06-960-805. OPS TESTED GOOD.SDR CALA2025122312338Battery Pack · no testEMERGENCY LIGHT BATTERY M1670 FAILS CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK M1670 IAW AMM 33-51-06-960-805. OPS TESTED GOOD.SDR CALA2025122312336Web · corrodedCORROSION AT AFT WET AREA BS 986+6, LBL 45 UPPER WEB PLATE REMOVED AND REPLACED THE WEB IAW SRM 51-40-02-0G-0, AND DWG 147A5700.SDR CALA2025122312334Battery Pack · no testEMERGENCY LIGHT BATTERY M1694 FAILED A CAPACITY CHECK. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-06-960-805. TESTED GOOD.SDR CALA2025122312332Battery Pack · inoperativeRIGHT FWD OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE RT FWD OVERWING EMERGENCY LIGHT LAMP & BATTERY PACK IAW AMM 33-51-04-960-801, AND AMM 33-51-06-960-805. TESTED GOOD.SDR CALA2025122312330Web · corrodedFOUND TWO DENTS IN AFT CABIN WET AREA GALLEY SUPPORT FLOOR WEB, LBL 7 & 12, BS 1016. REMOVED AND REPLACED THE WEB BS 1016 & LBL 3.59 - 27.95 IAW SRM 51-40-02-0G-0 & DWG 147A5700.SDR CALA2025122312328Support Angle · corrodedCORROSION ON AFT WET AREA BS 1016+2, RBL2 BETWEEN RBL 2 - 20, SUPPORT ANGLE INSTALLED A NEW SUPPORT ANGLE IAW SRM 51-40-02-0G-0 & DWG 147A5700.SDR CALA2025122312313Elec Connector · damagedSEAT 35C EMERGENCY EXIT LIGHT INOPERATIVE. FOUND CONECTOR ON ACFT SIDE BROKEN. CAPPED WIRES WITH TAPE RECRIMPED TERMINALS AND CONNECTOR SEAT 35C EMERGENCY LIGHT, R&R EMERGENCY LIGHT BATTERY PACK FUSE. SWPM 20-61-11, WDM 33-51-22. OPS CK GOOD.SDR CALA2025122212285Warning Light · false activationFWD SERVICE DOOR LIGHT CAME ON DURING LANDING STAYED ON DURING TAXI IN. PERFORMED OPS CHECK OF WARNING SYSTEM OF SERVICE DOOR IAW AMM 52-41-00-700-801, OPS NORMAL, OPS CHECKED GOOD.SDR CALA2025122112283Transmitter · faultedFLAPS STOPED AT 2, NO TRAILING EDGE FLAPS UNTIL ALT FLAPS. SHOWS LEFT TE FLAP POSITION TRANSMITTER LAGGING BAD. REMOVED & REPLACED THE LT FLAP TRANSMITTER & PERFORMED ALL TESTS IAW AMM 27-58-01. NO FAULT NOTED.SDR CALA2025122412433Skin · crackedCRACK FOUND AT RIGHT HORIZONTAL STABILIZER LOWER SKIN AT HSS 157.10, - 8 INCHES FROM REAR SPAR, INBD ROW. CRACK LENGTH: 1 INCH. CRACK FOUND AT RT HORIZONTAL STAB LOWER SKIN, FABRICATED REPAIR PARTS, DOUBLER, 2 FILLERS AND INSTALLED IAW SRM 55-10-01-2R-11, FISDR CALA2025122412431Pressure Web · crackedCRACK FOUND AT VERTICAL PRESSURE WEB BETWEEN LBL 31.83 AND LBL 24.92 BETWEEN WL 200.6 & WL 192.0. CRACK LENGTH: 1 INCH. FABRICATED AND INSTALLED VERTICAL PRESSURE WEB REPAIR PARTS AT BS 663, LBL 14 TO LBL 47 IAW SRM 57-10-10-2R-3, STEP 6.F, TABLE 203, FIGURE SDR CALA2025122212307Door Frame · crackedCRACKED MAIN CABIN R1 DOOR CUTOUT FWD LOWER FRAME CRACKED. INSTALLED A NEW LOWER FRAME AND SEAL DEPRESOR IAW SRM 51-40-02, IPC 53-11-00-80, & DWG 141A8370.SDR CALA2025122212305Floorbeam · corrodedMAIN CABIN AFT WET AREA CORROSION AT FLOORBEAM UPPER SURFACE, BS 947.5, LBL 52. ACCOMPLISHED REPAIR AT FLOORBEAM REPAIR AT BS 947, LBL 24, LBL 30, AND LBL 50 IAW SRM 53-70-51-2R-5,.SRM 51-40-02-0G-0, AND ECRA 5370-01190.SDR CALA2025122212303Structure · corrodedCORROSION AT AFT WET AREA, BS 986 - 947, LBL 50, UPPER AND LOWER INNER CHORD AT FASTENERS HOLES. INSTALLED 100% OF FASTENERS ON LEFT INNER CHORD AT MAIN CABIN FLOOR STRUCTURE AFT WET AREA IAW SRM 51-40-02-0G-0, AND DWG 147A8501.SDR CALA2025122212301Skin · deformedNUMBER 7 SPOILER HAS A PUNCTURE ON LWR SURFACE. CLEANED, PREPPED, AND PERFORMED A PERMANENT REPAIR AND APPLIED PAINT ON NR 7 SPOILER ON LOWER SURFACE IAW SRM-57-70-01-1A-1, SRM-57 -70-01-2R-2, SRM 57-10-01-2R-2, AMM-51-21-99-300-802, AMM-51-21-41-370-803, ANSDR CALA2025122212299Beam · crackedR1 SERVICE DOOR HANDLE TORQUE BOX UPPER SUPPORT BEAM CRACKED NEAR TORQUE BOX FWD ATTACH BOLT. INSTALLED UPPER BEAM AND STOP FITTING NR 3 AT R1 DOOR PENDING SKIN IAW SRM 51-40-02-0G-0, DRAWING 141A6516 AND DRAWING 141A6535.SDR CALA2025121912263Beam · crackedR1 SERVICE DOOR HANDLE TORQUE BOX LOWER SUPPORT BEAM CRACKED NEAR TORQUE BOX FWD ATTACH BOLT. R & R LOWER INNER SKIN & LOWER BEAM IAW SRM 51-40-02-0G-0 & DWG 141A6516 AND DWG 141A6535.SDR CALA2026010712733Floorbeam · corrodedMAIN CABIN BS 986, RBL 38 - 41 HAS CORROSION ON UPPER SURFACE. REPAIRED CORRODED T-FITTING WITH ANGLES STRAPS AND NEW T-FITTING FROM RBL 50 TO LBL 50 IAW SRM 53-70-51-2R REPAIR 4.SDR CALA2025123012519Floorbeam · corrodedFOUND CORROSION FWD WET AREA FLOORBEAM UNDER SEAT TRACK END, BS 344, LBL 57. ACCOMPLISHED REPAIR, INSTALLED 100% OF FASTENERS ON FLOORBEAM REPAIR, BS 344, LBL 15 - 66 IAW SRM 53-10-51-2R-10, STEP 4.SDR CALA2025121912253Floorbeam · crackedCABIN FLOOR BEAM CRACKED AT BS 540, RBL 1. R & R THE FLOORBEAM IAW SRM 51-40-02-0G-0.SDR CALA2025121812210Shear Web · damagedMAIN CABIN SHEAR WEB AFT OF L2 DOORWAY AT BS 986 - 1016, LBL 32 HAD MULTIPLE ELONGATED FASTENER HOLES. THE SHEAR WEB TO BE INSTALLED ON GSO NRC 9288447 LOCATED AND DRILLED IAW SRM 51-40-05-0G-0.SDR CALA2025121812208Crease Beam · corrodedMAIN CABIN CREASE BEAM INNER CHORD UPPER SURFACE IS CORRODED FROM BS 940 - 947, RBL 56. R & R THE CREASE BEAM IAW DWG 147A8501, REV T, AND SRM 51-40-02.SDR CALA2025121812206Fitting · chafedR2 DOOR CUT FWD INTERNAL FITTING HAS A DEEP CHAFE BY LWR AREA OF BODY TORQUE. R & R THE R2 DOOR FWD INTERNAL FITTING IAW SRM 51-40-02-0G-0, DWG 147A8901, DWG 147A8101, AND DWG 147A0010.SDR CALA2025121812204Floor Support · corrodedMAIN CABIN FLOOR SUPPORT, LBL 44 BETWEEN BS 328 - 344 WAS CORRODED ON UPPER SURFACE JUST IN FRONT OF SEAT TRACK. R & R THE FLOOR SUPPORT IAW DWG 141A5730, REV A.SDR CALA2025122412435Bulkhead · corrodedAPU AIR INLET PLENUM TRANSITION DUCT MATING SURFACE AT APU BAY BULKHEAD WAS CORRODED. ACCOMPLISHED A REPAIR AT APU AIR INLET PLENUM DUCT BULKHEAD AT BS 1088 IAW SRM 51-40-02-0G-0, ESR 29-13201, REV P1, DWG 148A0924, DWG 148A1684, AND DWG 148A3800.
Back to Boeing 737-824