Boeing 737-222
Service difficulty reports · 657
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 = '737222' 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 = '737222' 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 CALA9701651Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 1016, LBL 1.5 AND LBL 9. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03623.SDR CALA9701650Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER CAP CORRODED AT STA 312, RT OUTBOARD END. THE CORRODED SECTION WAS REMOVED IAW SRM 51-30-2, REPAIR FILLER AND ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-9, 51-10-2, AND 51-30-2.SDR CALA9701649Web · corrodedINSPECTION FOUND WEB CORRODED AT BS 330 TO 340, RT CUSP. THE CORROSION WAS REMOVED IAW SRM 51-10-6, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, AND 51-30-2.SDR CALA9701648Angle · corrodedINSPECTION FOUND CORROSION IN ANGLE AT BS 797, S26L. THE CORRODED AREA WAS CUT OUT IAW SRM 53-10-3, FIGURE NR 1, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-3, 51-10-2, AND 51-30-0.SDR CALA9701647Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER T-CAP CORRODED AT STA 344 FROM LBL 24 TO RBL 24. THE CORRODED FLOORBEAM CAP WAS REMOVED, A REPLACEMENT CAP AND SPLICES WERE FABRICATED AND INSTALLED IAW SRM 53-10-9 AND 53-30-2.SDR CALA9701646Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 328 TO 344, LBL 10. THE FLOOR SUPPORT WAS REMOVED IAW SRM 53-10-2. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-10-2.SDR CALA9701645Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 294.5 TO 312, RBL 10. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-10-2.SDR CALA9701644Frame · corrodedINSPECTION FOUND CABIN FLOOR FRAME CORRODED AT STA 987 FROM BL 55L TO BL 55R. THE CORRODED UPPER CAP WAS REMOVED IAW SRM 51-30-2. A NEW UPPER CAP WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2.SDR CALA9701643Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER CAP AND WEB CORRODED INSIDE E AND E COMPARTMENT AT BS 328. THE CORRODED SECTION OF BEAM CAP WAS REMOVED AND A NEW SECTION AND SPLICE ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-2. THE CORRODED SECTION OF FLOORBEAM WEB SDR CALA9701642Support · corrodedINSPECTION FOUND FLOOR SUPPORT UPPER PLATE CORRODED AT STA 328 TO 344, RBL 10. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-10-2.SDR 97UAL900824Actuator · crackedFLIGHT CREW NOTED THAT THE HYDRAULIC SYSTEM 'A' QUANTITY AND PRESSURE WAS ZERO AFTER LANDING. *S/D* THE RIGHT INBOARD GROUND SPOILER HOUSING WAS FOUND TO BE CRACKED. THE ACTUATOR WAS REPLACED. SINCE THE REPLACEMENT, THERE HAVE NOT BEEN ANY HYDRAULIC PROBLESDR P2EA97072Slide · failedMCI - REPLACE L2 DOOR EMERGENCY ESCAPE SLIDE DUE TO TIME. PERFORMED OPERATIONAL CHECK OF ESCAPE SLIDE REF JOB CARD J225-60-10. SLIDE MOUNTED LIGHTS DID NOT ILLUMINATE. REPLACED L2 EMERGENCY ESCAPE SLIDE. (M)SDR 97UAL900813So Valve · failedNUMBER ONE ENGINE HYDRAULIC SHUTOFF VALVE CIRCUIT BREAKER TRIPPED AND WOULD NOT RESET. *S/D* REPLACED NR 1 ENGINE HYDRAULIC SHUTOFF VALVE. NO LEAKS WERE NOTED, OPS CHECK GOOD.SDR 97UAL900804Vhf Comm · inoperativeNUMBER 1 VHF COM WAS INOPERATIVE. NUMBER 2 VHF COM WAS INTERMITTENT.SDR 97UAL900781Acm · failedRIGHT PACK OVERTEMP, NO PACK TRIP OFF. SMOKE INSIDE AND OUTSIDE OF AIRCRAFT. *S/D* FOUND METAL SHAVINGS COMING FROM WATER SEPARATOR DRAIN. REPLACED THE RIGHT-HAND AIR CYCLE MACHINE AND COALESCER BAGS, OPS CHECK GOOD.SDR P2EA97069Lens Cover · missingFLT 8129 - MCI - LEFT OVERWING INSPECTION LIGHT LENS COVER MISSING (WING FLOOD LIGHT), FOUND AFTER BLOCK IN, MCI, BY MAINTENANCE. ITEM DEFERRED PER CDL 33-40-3 PER CONTROLLER. NO DAMAGE NOTED TO AIRCRAFT. (M)SDR P2EA97068Battery Pack · dischargedPHX - FOUND DURING SCHEDULED MAINTENANCE CHECK, EMERGENCY PATH LIGHTING INOP, ROWS 1-8. REPLACED BATTERY CHARGER AND BATTERY PACK ASSEMBLY AT ROW 7. OPS CHECK OK PR MM 33-51-11A. (M)SDR CALA9701376Hyd Line · crackedTHE AIRCRAFT LOST A-HYDRAULIC SYSTEM WHILE EN ROUTE. THE HYDRAULIC LOSS CHECKLIST WAS COMPLETED AND THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND NR 1 ENGINE A-SYSTEM HYDRAULIC PRESSURE LINE CRACKED. THE HYDRAULIC PRESSURE LINE WAS REMOVED SDR 97UAL900715Oil Syst · lostNUMBER ONE ENGINE SHUT DOWN DUE TO LOSS OF OIL.SDR 97UAL900730Torque Tube · wornFLAP DRIVE TORQUE TUBE WORN ON LEFT REAR TRUNNION BEAM HANGER, LEFT INBOARD FLAP WELL, INBOARD END. *S/D* PROVIDED CLEARANCE BY REPOSITIONING HYDRAULIC LINES AND RESECURING. REPLACED THE LEFT-HAND, INBOARD FLAP DRIVE TORQUE TUBE.SDR 97UAL900649Uplock Actuator · failedON CLIMB-OUT, GEAR RETRACTED NORMALLY AND GEAR HANDLE MOVED TO THE OFF POSITION. LEFT GEAR RED LIGHT ILLUMINATED FOLLOWED BY THE LEFT GEAR GREEN LIGHT. HANDLE RAISED AND HEARD A THUMP FOLLOWED BY A YAW. ALL LIGHTS WENT OUT. HANDLE RETURNED TO OFF AND ALL LSDR ZZDA5328297Skin · crackedDURING C-CHECK AT AERO CORP, FOUND 1 INCH CRACK AT EDGE OF FRAME ANGLED STRAP TO FASTENER HOLE AT BS 1104 LWL 290. FABRICATED DOUBLER FROM 301 1/2 HARD .040 INCH, 8 INCHES BY 2.5 INCHES BY 1.25 INCHES. FABRICATED FILLER FROM 2024T3 .083 INCH, 3.2 INCHES BY 1SDR CALA9701232Connector · shortedTHE AIRCRAFT HAD A BRIEF HISTORY OF THE APU FIRE WARNING ACTIVATING DURING FLIGHT. NO EVIDENCE OF FIRE WAS FOUND. TROUBLESHOOTING FOUND APU TAILPIPE DETECTOR CONNECTORS SHORTING TO GROUND. THE CONNECTORS WERE REPLACED. IN ADDITION, THE FIRE DETECTION MODULSDR P2EA97066Oil Press Ind · malfunctionedDEN - FLT 229 - NR 2 ENGINE OIL PRESSURE 37 PSI JUST PRIOR TO TAKEOFF. RETURNED TO GATE. REMOVED AND REPLACED OIL PRESSURE INDICATOR. SYSTEM CHECKS NORMAL PER MM 79-32-01. (X)SDR ZZDA5316697Floor Beam · corrodedDURING C-CHECK, FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 967 LBL 28. FABRICATED FLOOR BEAM CAP FROM 1505-100617-7075 T3 16 INCHES BY 2 INCHES IAW B 737 SRM 53-10-9. FABRICATED ANGLE REPAIR FROM 7075.0 .071 INCH 22.50 INCHES BY 1.50 INCHES BY 1 INCH. FABRSDR ZZDA5316397Skin · damagedDURING C-CHECK INSPECTION, FOUND IMPROPER REPAIR DOUBLER LT BS 360 STR 16L. FABRICATED DOUBLER AND FILLER FROM 2024 T3 .090 INCH BY 9.5 INCHES BY 3.75 INCHES. INSTALLED IAW B 737 SRM 53-30-3. (X)SDR ZZDA5316797Floor Beam · corrodedDURING C-CHECK, FOUND FLOOR BEAM UPPER CAP CORRODED AT BS 344 LBL 60 OUT OF LIMITS. FABRICATED CHORD FROM 7075 T6 2 INCHES BY 30.75 INCHES BY 1.25 INCHES. FABRICATED WEB SPLICE FROM 7075 T6 .032 INCH 4 INCHES BY 7.2 INCHES. FABRICATED 2 WEBS FROM 7075 T6 .0SDR 97ZZZM952Stringer · corrodedDURING C-CHECK, FOUND STRINGER 25L WITH HEAVY CORROSION WITH A HOLE THROUGH THE STRINGER. TRIMMED THE AREA (HOLE STRINGER 25) IAW B737 SRM 53-10-3. FABRICATED ANGLE AND FILLER FOR REPAIR. MATERIAL .46 BAC 1498-156 (7075-T60) 7.125 INCH BY 1.875 INCH, .625 ISDR ZZDA5516597Bushing · corrodedDURING C-CHECK SURVEILLANCE INSPECTION, RT HORIZONTAL STABILIZER REMOVAL FOUND CENTER STABILIZER RT AFT ATTACH LUGS, 6 EACH, BUSHING HAVE PITTING CORROSION. REMOVED HINGE FITTING FOR REPLACEMENT. DRILLED NEW FITTING. REMOVED BUSHING FROM OLD FITTING. INSPESDR ZZDA9714997Chord · crackedDURING C/W AD 95-12-17 IAW SB 737-53A 1166, NOTED CRACK INDICATIONS BETWEEN FASTENERS IN BS 727 RT SIDE FRAME FORWARD FLANGE OF OUTER CHORD COMMON WITH LOWER FLANGE OF STR 18A. REPLACED RT STA 727 CHORD IAW B 737 SB 737-53-1088. (X)SDR ZZDA5315597Seat Track · corrodedDURING C-CHECK, FOUND CABIN SEAT TRACKS CHIPPED AND CORRODED OUT OF LIMITS IAW SRM 53-10-1 FIG 4 AT BS 847 - BS 960. FABRICATED NEW SEAT TRACK FROM BAC 1520-792 113 INCHES IAW B 737 SRM 53-10-5. INSTALLED IAW B 737 SRM 53-10-5 FIG 3 AND SRM 51-30-2. (X)SDR ZZDA5315297Skin · crackedDURING C-CHECK, FOUND BS 360 BELOW STR 16L HAS REPAIR DOUBLER NOT IAW B 737 SRM 53-30-3 FIG 8. CUT OUT CRACKED AREA OF SKIN IAW 737 SRM 53-30-3. FABRICATED 1 EACH FILLER AND DOUBLER IAW 53-30-3. ALODINED AND PRIMED IAW SRM 52-10-2 AND MM 51-21-0. INSTALLEDSDR ZZDA5315197Skin · damagedDURING C-CHECK, FOUND BS 460 RT IMPROPER REPAIR FORWARD LOWER SIDE OF PASSENGER WINDOW NOT IAW 737 SRM 53-30-3 FIG 38. FABRICATED DOUBLER FROM 2024 T3 .083, 15.75 INCHES BY 12.25 INCHES IAW B 737 SRM 53-30-3. INSTALLED IAW B 737 SRM 53-30-3. (X)SDR ZZDA5315097Frame · crackedDURING C-CHECK AT AERO CORP, FOUND LT BS 578 FRAME WL 205 LBL 58 CRACKED APPROXIMATELY .50 INCH LOWER INBOARD CORNER. FABRICATED FRAME FROM 7075 0.050 33.50 INCHES BY 7.25 INCHES IAW B 737 SRM 51-20-1 FIG 7. INSTALLED IAW B 737 SRM 51-20-1 FIG 7 AND 51-30-1.SDR ZZDA5314897Floor Beam · corrodedDURING C-CHECK INSPECTION, FOUND AFT CABIN FLOOR BEAM CORRODED TOP CHORD BS 1006 LBL 3 - RBL 3 OUT OF LIMITS IAW B 737 SRM 53-10-1. FABRICATED FLOOR BEAM FROM BAC 1505-100617 29.750 INCHES BY 2.25 INCHES IAW B 737 SRM 53-10-9. INSTALLED IAW B 737 SRM 53-10-9SDR P2EA97064Control Cable · failedATL - FLT 352 - NO EMERGENCY DECLARED. FLAPS INOP, STUCK AT 1 DEGREE TRAILING EDGE, SLATS AT EXTEND, GAUGE READS R-1. NO INDICATION. REPLACED FLAP CABLE FAC-1, PER MM 27-09-111A, 27-58-21A AND CHAPT 20. (M)SDR 97ZZZM924Floorbeam · corrodedDURING C-CHECK INSPECTION, FOUND AFT CABIN FLOORBEAM CORRODED TOP CHORD BS 1008 LBL 3 - RBL 3 OUT OF LIMITS IAW B737 SRM 53-10-1.SDR 97ZZZM923Chord · crackedDURING COMPLIANCE OF AD 95-12-17 IAW SB 737-53A 1166, NOTED CRACK INDICATIONS BETWEEN FASTENERS IN BS 727 RT SIDE FRAME FWD FLANGE OF OUTER CHORD COMMON WITH LOWER FLANGE OF STRINGER 18A.SDR 97ZZZM922Frame · crackedDURING C-CHECK AT AERO CORP, FOUND LEFT BS 578 FRAME WL 205 LBL 58 CRACKED APPROX .5 INCH LOWER INBOARD CORNER.SDR 97ZZZM921Skin · misrepairedDURING C-CHECK, FOUND BS 480 RT IMPROPER REPAIR FORWARD LOWER SIDE OF PASSENGER WINDOW NOT IAW 737 SRM 53-30-3 FIG 38. (M)SDR 97ZZZM920Skin · misrepairedDURING C-CHECK, FOUND BS 360 BELOW STRINGER 16L HAS REPAIR DOUBLER NOT IAW B737 SRM 53-30-3 FIG 8. (M)SDR 97ZZZM919Seat Track · corrodedDURING C-CHECK, FOUND CABIN SEAT TRACKS CHIPPED AND CORRODED OUT OF LIMITS IAW SRM 53-10-1 FIG 4 AT BS 847-960. (M)SDR 97ZZZM918Frame · crackedDURING C-CHECK, RIGHT VS 706 FRAME CRACKED FWD AND AFT SIDES AT WL 202, C/W SB 737-53-1055.SDR 97ZZZM917Frame · crackedDURING C-CHECK, FOUND BS 685 LT FRAME CRACKED ON FWD AND AFT SIDES AT WL 202.SDR 97ZZZM916Frame · crackedDURING C-CHECK, FOUND BS 685 RT FRAME CRACKED ON FWD AND AFT SIDES AT WL 202. (M)SDR 97ZZZM915Frame · crackedDURING C-CHECK, FOUND LT BS 685 FRAME RBL 58 WL 208 CRACKED 1.5 INCH AT INTERCOSTAL FLOORBEAM ATTACH POINT TO FRAME.SDR ZZDA5328397Skin · disbondedDURING C-CHECK AT AERO CORP, FOUND DISBOND AT BONDED DOUBLER AROUND AFT ENTRY DOOR. NOTED DURING C/W SB 53-1076 APPROX BS 940 TO BS 943 WL 225 TO WL 228 APPROX BS 972 TO BS 980 WL 196 TO WL 199. AREAS MARKED IN RED. REPAIRED DISBONDED AREAS PER B 737 SRM 53SDR ZZDA5316497Skin · corrodedDURING C-CHECK, FOUND REPAIR NOT IAW SRM 53-30-3 AT BS 460 STR 14L. REMOVED EXISITNG REPAIR, FABRICATED DOUBLERS FROM 2024 T3 .050 44.50 INCHES BY 3.75 INCHES AND 44.50 INCHES BY 9.50 INCHES IAW B737 SRM 53-30-3, FIG 9. INSTALLED IAW B737 SRM 53-30-3, FIG 9 SDR ZZDA5316197Skin · corrodedDURING C-CHECK, FOUND RT INLET DUCT, FUSELAGE SKIN HAS EXFOLIATION AT STA 639.0 AROUND RIVETS (WING BOX). REMOVED CORROSION WITH A REMAINING THICKNESS OF .116 ORG. .250 INCH IAW B 737 SRM 51-10-6 AND SRM 51-30-2. SPOT-FACED, REAMED, COLD-WORKED, AND SHOT-PEESDR 97ZZZM912Fitting · crackedDURING C-CHECK INSPECTION, FOUND RIGHT MLG SUPPORT BEAM OUTBOARD ATTACH FITTING CASTING CRACKED AT REAR SPAR RWBL 160.
Back to Boeing 737-222