Boeing 737-201
Service difficulty reports · 2,471
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 = '737201' 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 = '737201' 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 F3LA96033Stringer · crackedFOUND CRACK IN STRINGER 14R AT BS 277. STOP DRILLED CRACK AND INSTALLED REPAIR PER SRM 53-10-3, FIG 1. WORK DOCUMENTED ON TRAMCO NRC INTERIOR 178. (M)SDR F3LA96032Frame · corrodedPAE - FOUND CORROSION ON FORWARD AND AFT SIDE OF FRAME AND CORRODED AND CRACKED SHEAR TIE BS 807, LBL 25 - RBL 25, WL 148-153. REMOVED CORROSION FROM FRAME AND FOUND WITHIN LIMITS OF SRM. CUTOUT DAMAGED SHEAR TIES BETWEEN STRINGER 26-27L AND STRINGER 27L-27RSDR F3LA96031Skin · crackedDURING SERVICE CEHCK, INSPECTION REPORTED A .5 INCH CRACK IN THE UPPER FORWARD CORNER OF THE FORWARD ENTRY DOOR CUTOUT. REPAIRED PER BOEING TELEX FRO-DEN-96-0085RR AND SRM 51-10-1. (M)SDR F3LA96030Stringer · crackedPAE - FOUND CRACK IN STRINGER 27 LEFT AT BS 380 PLUS 12. CUTOUT DAMAGED AREA OF STRINGER AND REPAIRED PER SRM 53-10-03. WORK DOCUMENTED ON NRC FUSELAGE 291. (M)SDR F3LA96076Control System · stiffUPON ARRIVAL, FLIGHT CREW REPORTED ELEVATOR STIFF, ESPECIALLY DURING FLARE. MAINTENANCE CHECKED ALL FLIGHT CONTROLS FOR MOVEMENT AND POSITION PER MM AND FOUND OK. PERFORMED TEST FLIGHT AND CHECK OK. (M)SDR F3LA96028Controls Systems · stiffDEN - UPON ARRIVAL, FLIGHT CREW REPORTED ELEVATOR STIFF, ESPECIALLY DURING FLARE. MAINTENANCE CHECKED ALL FLIGHT CONTROLS FOR MOVEMENT AND POSITION PER MM AND FUOND OK. PERFORMED TEST FLIGHT AND CHECKED OK. (M)SDR USAA960665Frame · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACKED FRAME .75 INCH LONG STATION 727 JUST BELOW STRINGER 13L. INSTALLED REPAIR DOUBLERS, REPAIRED PER EA 51489. (M)SDR USAA960664Stringer · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 4 INCH LONG 1 INCH WIDE BS 1003 TO BS 1014 STRINGER. REMOVED DAMAGE AND FABRICATED REPAIR, REPAIRED PER SRM 53-10-2. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)SDR USAA960663Keel Beam · damageINT - DURING Q-3 CHECK VISUAL INSPECTION FOUND THREE ACCESS PLATE MOUNTING FLANGE HOLES DAMAGED IN KEEL BEAM, RIGHT SIDE KEEL BEAM LOWER CHORD OUTBOARD FLANGE FORWARD OF BS 727. INSTALLED STRAP REPAIR PER EA, REPAIRED PER EA 41514. (M)SDR USAASB96205Controller · failedCLT - FL 8026 - CAPTAIN ADVISED HE LOST AUTO AND STANDBY PRESSURIZATION. MANUAL PRESSURIZATION WAS OK. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CABIN PRESSURE CONTROLLER. OPS CHECK GOOD. (M)SDR USAASB96204Sliding Window · crackedPIT - FLT 1111 - WHILE EN ROUTE TO IND, THE FLIGHT OFFICERS SLIDING WINDOW DEVELOPED A CRACK. AFTER CHECKING WITH MAINTENANCE, IT WAS DECIDED TO DIVERT TO PIT DUE TO POSSIBLE ICING CONDITIONS. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER ISDR F3LA96029Floor Beam · crackedDURING SERVICE CHECK, INSPECTION REPORTED A 1.25 INCH CRACK IN THE CABIN FLOOR BEAM WEB AT STATION 663, BBL 0. REPAIRED PER BOEING SERVICE BULLETIN 737-57-121D, FIG 4 AND BOEING TELEX M-7272-96-4639. (M)SDR USAA960659Beam · crackedROA - DURING BX CHECK VISUAL CONFIRMED WITH HFEC INSPECTION, FOUND .5 INCH CRACK BS 706 STRINGER 18A SHEAR BEAM WEB, LEFT. INSTALLED DOUBLER REPAIR, REPAIRED PER EO 5393G256 PART 3 SECTION IV PRIOR TO REV FLIGHT. (M)SDR USAA960658Floor Beam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FOUR .75 INCH CRACKS, LBL 25 INCHES LONG FLOOR BEAM WEB STATION 707 TO 712, WL 203.5. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M)SDR USAA960657Floor Beam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FOUR .5 INCH CRACKS BL 0 INCH LONG FLOOR BEAM WEB STATION 707 TO STATION 712, WL 203.5. INSTALLED REPAIR WEB, REPAIRED PER SRM 51-40-2. (M)SDR USAA960656Skin · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK EXTERNAL SKIN DOUBLER FORWARD SERVICE DOOR LOWER HINGE. INSTALLED NEW DOUBLER, REPAIRED PER TR 52-10-01A. (M)SDR USAA960655Skin · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK CORNER OF HINGE CUT OUT FORWARD SERVICE DOOR SKIN. INSTALLED DOUBLER, REPAIRED PER TR 52-40-03A. (M)SDR USAA960654Stub Beam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 597 STUB BEAM WEB RBL 60 TO RBL 62, WL 207.5. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M)SDR USAA960653Bulkhead · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 663 BULKHEAD UPPER CHORD ANGLE AT LBL 25, WL 202. INSTALLED DOUBLER, REPAIRED PER DRAWING 65C37732. (M)SDR USAA960652Bulkhead · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 663 BULKHEAD UPPER CHORD ANGLE AT LBL 25, WL 202. INSTALLED DOUBLERS, REPAIRED PER DRAWING 65C37732. (M)SDR USAA960651Frame · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK IN CIRCUFERENTIAL FRAME STATION 328 3 INCHES BELOW STRINGER STRINGER 20R. FABRICATED 707576 .040 MATERIAL, INSTALLED WEB REPAIR, REPAIRED PER SRM 51-40-2 FIG 1. (M)SDR USAA960650Floor Beam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACKS IN FOUR PLACES, RBL 25 INCHES LONG, FLOOR BEAM WEB STATION 707 TO 712, WL 203.5. INSTALLED WEB REPAIR, REPAIRED PER SRM 51-40-2. (M)SDR USAA960649Support Channel · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRCK RBL 45 SEAT TRACK SUPPORT CHANNEL ABOVE UPPER INBOARD BOLT. INSTALLED DOUBLERS, REPAIRED PER EA 41455 AND SB 737-53-1120. (M)SDR USAA960648Web · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND TWO CRACKS 1 INCH BY 3 INCH CREASE BEAM WEB 2 INCHES AFT OF STATION 639 PLUS 1 INCH FORWARD OF STATION 663 FRAME LBL 67, WL 208. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M)SDR USAA960647Support Channel · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK LBL BS 520, WL 207.5 SUPPORT CHANNEL. FABRICATED DOUBLER CHANNEL RADIUS FILLERS, INSTALLED CHANNEL AND FILLERS. REPAIRED PER EA 41455 SB 337-53-1120. (M)SDR USAA960646Stringer · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACKS EMITTING FROM FASTENER HOLES (2) STRINGER 15L BS 525. CHANNEL REPAIR INSTALLED ON STRINGER, REPAIRED PER SRM 53-10-3. (M)SDR USAA960645Stub Beam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 578 STUB BEAM WEB LBL 61.5 TO LBL 62.5, WL 207.5. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M)SDR USAA960644Frame · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 4 INCH LONG CRACK STATION 747 STRINGER 19 L CIRCUMFERENTIAL FRAME. INSTALLED DOUBLERS, REPAIRED PER SRM 53-10-4. (M)SDR USAA960643Stringer · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION ON STRINGER 1 INCH BY 3 INCH SECTION AROUND RIVETS, BS 363 TO BS 500 PLUS 13 INCHES. REPLACED STRINGER SECTION, REPAIRED PER SRM 53-10-3 FIG 3 SHEET 2 TABLE 1. CORROSION TASK NR C53-107-01, CORROSION SDR USAA960642Floor Beam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK BS 675 WL 202.5 LONGITUDINAL FLOOR BEAM LOWER CHORD. INSTALLED REINFORCING ANGLE/SPLICE, REPAIRED PER EA 41578. (M)SDR USAA960641Floor Beam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK RBL 45 LONG FLOOR BEAM LOWER CHORD STATION 695 WL 202.5. INSTALLED REPAIR ANGLE, REPAIRED PER EA 41557. (M)SDR USAASB96198Gear Light · no testCLT - FLT 2002 - AT FL270 CLIMBING OUT FROM IAD, A LOUD BANG WAS HEARD UNDER THE LT SIDE OF FWD ENTRY DOOR. ENG PARAMETERS AND HYD NORMAL. NOSE WHEEL GREEN LIGHT WOULD NOT TEST. CHECKED LIGHT BULBS, C/B AND SOCKETS. CAPTAIN MADE PRECAUTIONARY DIVERSION TO SDR USAA960625Skin · crackedROA - DURING CX-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND .0625 INCH CRACK FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNER FUSELAGE SKIN. STOP DRILLED CRACK AND INSTALLED DOUBLER. REPAIRED PER TYPICAL REPAIR 53-10-19 REV A. (M)SDR USAASB96200Battery Pack · dischargedPHL - MAINTENANCE FOUND THE OVERHEAD EMERGENCY EXIT IDENTIFIER LIGHT INOP AT ROW 2. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD. (M)SDR USAASB96194Engine · bird strikeBOS - FL 1153 - DURING TAKEOFF ROLL, THE AIRCRAFT INJESTED A LARGE SEAGULL INTO THE NR 2 ENGINE. CREW AND DISPATCH ELECTED TO DIVERT TO BOS AS A PRECAUTIONARY MEASURE. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE PERSDR USAA960609Skin · crackedROA - DURING 'CX-3' CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND .125 INCH CRACK FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNER FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER. REPAIRED PER TYPICAL REPAIR 53-10-19 REV A. (M)SDR USAA960608Skin · crackedCLT - INSPECTION VISUALLY FOUND 1 INCH AND 1.4 INCH SKIN CRACKS LOCATED AT STATION 727A, 2 INCH AND PLUS 7 INCH IN THE FUSELAGE SKIN, RIGHT BL 70 BETWEEN STRINGER 17 AND 18. INSTALLED DOUBLER AS PER BOEING SRM 53-10-1 AND 53-30-3. (M)SDR USAASB96186Engine · failedPIT - FLT 111 - AT 30,500 FEET, THE NR 1 ENGINE EXPERIENCED A FIRST AND SECOND COMPRESSOR STALL. CREW STARTED DESCENT AND GOT A THIRD STALL. CREW PULLED THROTTLE BACK AND COMPRESSOR STALLS CEASED. CREW CONTINUED DESCENT AND DIVERTED TO PIT WHERE THE FLIGHT SDR USAASB96181Air Distr · odorPIT - FL 553 - FLIGHT ATTENDANTS ADVISED COCKPIT CREW THAT THEY SMELLED SMOKE OR FUMES IN THE REAR OF THE AIRCRAFT. THEY DID NOT DETECT ANY SIGHT OF SMOKE. CAPTAIN COULD NOT ISOLATE PROBLEM AND ELECTED TO DECLARE AN EMERGENCY AS A PRECAUTIONARY MEASURE AND DSDR USAASB96180Socket · looseCLT - FL 1188 - CREW REPORTED EMERGENCY EXIT SIGN IN CENTER OF CABIN, ROW 9 OVERHEAD, IS LOOSE/INOP. MAINTENANCE REPAIRED WIRING AT EMERGENCY EXIT SIGN SOCKET AND RESECURED LIGHT ASSEMBLY. OPS CHECK GOOD. (M)SDR USAASB96175Battery Pack · failedCLT - MAINTENANCE FOUND BOTH OVERWING EMERGENCY EXIT LIGHTS FLASHING. MAINTENANCE REMOVED AND REPLACD THE BATTERY PACK FOR THE OVERWING EMERGENCY EXIT LIGHTS. OPS CHECK GOOD. (M)SDR USAASB96171Light Ballast · burnedIAH - FL 1183 - ON DESCENT INTO IAH, CREW DETECTED SMELL OF SMOKE IN THE COCKPIT. WHILE LOOKING FOR THE SOURCE, THE SMOKE ALARM IN THE FORWARD LAV WENT OFF. SHORTLY AFTER, SMOKE WAS SPOTTED ABOVE THE LEFT FORWARD JUMP SEAT. CREW WENT ON OXYGEN AND STARTED ESDR USAASB96167Door Tape · detachedCLT - FL 1024 - CREW AND PASSENGERS HEARD A LOUD THUMPING NOISE COMING FROM THE TOP OF THE AIRCRAFT DURING CLIMB. AT APPROX 5,000 FEET, CREW DECIDED TO RETURN TO FIELD AT CLT. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE DISCOVERED DUCT TAPE AT UPPERSDR USAA960579Skin · dentedROA - DURING 'CX-1' CHECK VISUAL INSPECTION, FOUND 2.5 INCH BY 1.75 INCH DENT STRINGER 22L BS 937 FUSELAGE SKIN. REMOVED DAMAGE AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (M)SDR USAA960568Floor Beam · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND ONE .25 INCH CRACK BS 520 AT RBL 45 INCH FLOOR BEAM. INSTALLED NEW CHANNEL AND DOUBLERS, REPAIRED PER EA 41421. (M)SDR USAA960567Floor Beam · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND ONE .25 INCH CRACK BS 520 AT RBL 25 CABIN FLOOR BEAM. INSTALLED NEW CHANNELS AND DOUBLERS PER EA 41421. (M)SDR USAA960565Floor Beam · brokenINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND UPPER 'T' OF FLOOR BEAM BROKEN INTO STATION 663 BL0. INSTALLED DOUBLER ON T-CAP AND WEB. REPAIRED PER BOEING DRAWING 65C34537. (M)SDR USAA960564Stringer · corrodedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 7 INCH CORRODED AREA STRINGER 27L, STATION 967. CUT OUT DAMAGE AND INSTALLED STRINGER SPLICE REPAIR. REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)SDR USAA960563Floor Beam · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH BY 6 INCH AT STATION 947.5 FLOOR BEAM. REPAIRED T-CAP, DOUBLERS AND REPAIR ANGLES. REPAIRED PER TR 53-10-05C. SUBMITTER STATES, CORROSION ATTRIBUTED TO CHEMICAL SPILL. CORROSION TASK NR C53-SDR USAA960562Stringer · crackedINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH CRACKS IN FASTENER HOLES FOR STRINGER 15R TO STATION 532. CUT OUT DAMAGED AREA AND FABRICATED AND REPLACED DAMAGED SECTION WITH STRINGER. REPAIRED SPLICE REPAIR PER SRM 53-10-3 FIG 1. (M)
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