Boeing 737-201

Service difficulty reports · 2,471

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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.

SDR USAA980100Stringer · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STRINGER 15 LT AT STATION 1138, STRINGER. REPLACED SECTION OF STRINGER AND SPLICED TOGETHER, REPAIRED PER SRM 53-10-7. (M)Feb 23, 1998 · N259AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980099Skin · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FUOND CRACK 2 INCHES LONG STATION 727A PLUS 4 INCH STRINGER 18R SKIN. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 53-30-3. (M)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980098Spar Web · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION FOUND CRACK .25 INCH LONG LT HORIZONTAL STABILIZER AT STATION 200.5 FRONT SPAR WEB. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 55-10-5. (M)Feb 23, 1998 · N254AU · Boeing 737201 · Wing SparSDR USAA980097Skin · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK 2 INCH LONG STATION 727 A STRINGER 18R SKIN. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 53-30-3. (M)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980096Stringer · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK 1 INCH AT STATION 747 STRINGER REPAIR, REPAIRED PER 53-10-3. (M)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980095Bulkhead · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 178 BULKHEAD UNDER RADAR DISH MOUNT, INBOARD SIDE OF RT LOWER HAT SECTION LEG. INSTALLED DOUBLER, REPAIRED PER SRM 53-10-11-1, SRM 53-10-11. (M)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA980094Frame · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION FOUND, .75 INCH CRACK STATION 616 FRAME INBOARD CHORD, LBL 62.5 WL 202 FRAME. FABRICATED AND INSTALLED REPAIR ANGLE, REPAIRED PER EA 43552. (M)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, FrameSDR USAA980093Frame · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 616 FRAME INBOARD CHORD RBL 62.5, WL 202 FRAME. FABRICATED AND INSTALLED DOUBLER, REPAIRED PER EA 43551. (M)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, FrameSDR USAA980092Floorbeam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK 3 INCHES STATION 664 BL 0 WL 207.5 TO WL 204 FLOORBEAM WEB. REMOVED DAMAGED AREA INSTALLED WEB REPAIR, REPAIRED PER BOEING DRAWING 65-C34537. (M)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA980091Floorbeam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK .5 INCH LONG STATION 727 LBL 25 INCH FLOORBEAM LOWER CHORD. REPLACED SECTION OF LOWER CHORD, REPAIRED PER SRM 51-40-4. (M)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA980090Floorbeam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION FOUND SEVERAL .25 INCH CRACK LBL 25 LONGITUDINAL FLOORBEAM LOWER WEB STATION 707 TO STATION 714, WL 203.5. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-2, REPAIRED PER SRM 51-40-2. (M)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA980089Floorbeam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK .5 INCH LONG STATION 707 TO STATION 714 RBL 25 LONG FLOORBEAM WEB. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 51-40-2. (M)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA980088Skin · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK AFT ENTRY GALLEY DOOR UPPER HINGE CUT OUT SKIN EXTERIOR. CUT OUT CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980087Skin · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION FOUND .5 INCH CRACK FORWARD ENTRY DOORWAY UPPER HINGE CUTOUT SKIN. CUTOUT CRACK AND INSTALLED FILLER AND DOUBLER, REPAIRED PER SRM 51-10-1, SRM 53-30-3, AND EA 43555. (M)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980086Frame · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK .5 INCH AT STATION 328 STRINGER 20R FRAME. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 51-40-3. (M)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, FrameSDR USAA980085Frame · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK 1.25 INCH LONG AFT ENTRANCE DOOR FRAME STATION 947 STRINGER 11L WEB (FRAME). INSTALLED DOUBLER ON EXISTING WEB, REPAIRED PR TR 53-30-07. (M)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, FrameSDR USAA980084Blkhd Stiffener · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK BS 178 LBL 5.75 AT WL 183.5 STIFFENER, BULKHEAD. DOUBLER AND STIFFENERS INSTALLED, REPAIRED PER TR 53-10-17. (M)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA980083Bulkhead · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 178 BULKHEAD LBL 5, WL 199. INSTALLED DOUBLER REPAIRED PER SRM 53-10-11. (M)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, BulkheadSDR USAA980082Keel Beam · wornINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND WORN HOLES, HOLES ELONGATED IN CHORD .09375 INCH STATION 695 TO STATION 727 LOWER CHORD (KEEL BEAM). SPOT FACED SCREW HOLES, HFEC INSPECTION INSTALLED STRAP, REPAIRED PER EA 43618 SRM 51-30-6. (M)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, KeelSDR USAA980081Stringer · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK AND .75 INCH CRACK BS 727 LEFT OUTBOARD CHORD STRINGER 18A L/S. CUTOUT AND SPLICED IN NEW SECTION OF STRINGER, REPAIRED EO 5394G068. (M)Feb 23, 1998 · N254AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980078Floorbeam · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK BS 660 LBL 24 FLOORBEAM. INSTALLED DOUBLER, REPAIRED PER EO 5791G632. (M)Feb 19, 1998 · N223US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA980077Bulkhead Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2.5 INCH CRACK BS 178 BULKHEAD AT UPPER LEFT RADAR MOUNT BULKHEAD SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-10-11, FIG 1. (M)Feb 19, 1998 · N223US · Boeing 737201 · Fuselage Main, BulkheadSDR USAA980076Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK BS 963, STRINGER 17R SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 AND BOEING DRAWING 65C27287. (M)Feb 19, 1998 · N223US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980075Frame · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION FOUND 1.7 INCH CRACK IN WEB OF FRAME BS 328 BETWEEN S20R AND S21R WEB AREAS OF FRAME. INSTALLED DOUBLER OVER STOP DRILLED CRACKED AREA IN WEB, REPAIRED PER AIW SRM 51-40-2 AND BOEING PRING NR 65-45812. (M)Feb 19, 1998 · N223US · Boeing 737201 · Fuselage Main, FrameSDR USAA980074Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK LOWER AFT CORNER FORWARD SERVICE DOOR CUTOUT STATION 328 STRINGER 17 SKIN AND BARE STRAP. INSTALLED DOUBLERS PER SRM 53-30-3. (M)Feb 19, 1998 · N223US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980073Drag Angle · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 1090 BETWEEN S2R AND S3L DRAG ANGLE. INSTALLED REPAIR STRAP AND REPAIRED PER EA 43571. (M)Feb 19, 1998 · N223US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA980072Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK IN SKIN AT WINDOW FORWARD SERVICE DOOR. INSTALLED DOUBLER, REPAIRED PER T/R 52-10-01 A. (M)Feb 19, 1998 · N223US · Boeing 737201 · Service DoorsSDR USAA980071Skin · crackedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 764 AT STRINGER 19L SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (M)Feb 19, 1998 · N223US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980070Flange · crackedINT - DURING Q-4 CHECK NDT INSPECTION, FOUND .25 INCH CRACK BS 727 STRINGER 18A LEFT OUTBOARD FORWARD FLANGE. INSTALLED REPAIR ANGLES, REPAIRED PER EO 5394G068. (M)Feb 19, 1998 · N223US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAASB98043Battery · dischargedALB - MAINTENANCE FOUND THE COCKPIT EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERIES. OPS CHECK GOOD. (M)Feb 17, 1998 · N227AU · Boeing 737201 · Emergency LightingSDR USAASB98037Press Switch · failedCLT - FLT 764 - WHILE EN ROUTE TO CLT, THE NR 1 ENGINE CSD LOW OIL PRESSURE LIGHT ILLUMINATED. CREW DISCONNECTED CSD PER CHECKLIST AND DECLARED AN EMERGENCY. THE APU WAS ALREADY ON MEL, SO THE AIRCRAFT OPERATED ON ONE GENERATOR THE REMAINDER OF THE FLIGHT TOFeb 11, 1998 · N252AU · Boeing 737201 · Engine Oil PressureSDR USAASB98035Anti-Ice Duct · leakingTPA - FLT 1874 - THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED DURING CLIMB-OUT APPROXIMATELY 25 MILES NORTH OF TPA. CREW FOLLOWED EMERGENCY PROCEDURES FOR OVERHEAT PROBLEM. WHEN THRUST LEVER WAS BROUGHT TO IDLE, THE LIGHT WENT OUT. FLIGHT RETURNED TO FIELD ATFeb 10, 1998 · N236US · Boeing 737201 · Air Intake Anti/De-Ice SystemSDR USAA980053Skin · corrodedINT - DURING 1/2C-CHECK, FOUND 2 INCH BY 4 INCH BULGE AT BS 800 AND 2 INCH BY 3 INCH BULGE AT BS 810 SKIN BETWEEN STRINGER 26R AND STRINGER 27R. REMOVED CORROSION AND INSTALLED REPAIRS PER SRM 51-40-3 AND BAC DWG 65-46551. (M)Jan 31, 1998 · N229US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980052Skin · corrodedINT - DURING 1/2C-CHECK, FOUND 4 INCH BY 20 INCH SKIN BULGES AT RIGHT KEEL BEAM SPLICE AT BS 727 THROUGH BS 727A. CUT OUT FUSELAGE SKIN TO GAIN ACCESS TO KEEL BEAM, BLENDED OUT CORROSION, VERIFIED NO CRACKS AND INSTALLED REPAIR PER EA 43596. (M)Jan 31, 1998 · N229US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980045Skin · crackedROA - DURING CX-6 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND .625 INCH CRACK BS 945 STRINGER 24L FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 3. (M)Jan 31, 1998 · N229US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB98025Windshield · defectiveORF - FLT 1279 - CAPT REPORTED VIA ACARS THAT FLIGHT WAS RETURNING TO FIELD AT ORF DUE TO A LOUD AIRLEAK COMING FROM THE F/O'S WINDSHIELD. NOISE WAS TOO LOUD TO COMMUNICATE IN COCKPIT. CLIMBED TO 5,000 FEET TO SEE IF THERE WOULD BE ANY CHANGE, BUT NOISE GOT Jan 30, 1998 · N236US · Boeing 737201 · Flight Compartment WindowsSDR USAA980047Skin · crackedCLT - DURING VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1.1 INCH CRACK AT A PREVIOUS REPAIRED AREA FWD ADN AFT BS 767 STRINGER 18L ON THE SKIN. FWD AREA CUTOUT 6 INCH BY 6 INCH AFT AREA 4 INCH BY 2 INCH CUTOUT. INSTALLED DOUBLER PER REPAIR DOCUMENT SRM 53-3Jan 28, 1998 · N248US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980043Skin · crackedROA - DURING CX-3 CHECK, FOUND .75 INCH CRACK ON FUSELAGE SKIN AT BS 750 STRINGER 18 LEFT. DETECTED BY VISUAL/EDDY CURRENT. INSTALLED DOUBLER PER SRM 53-30-3 FIGURE 1. (M)Jan 26, 1998 · N249US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980042Skin · crackedROA - DURING CX-3 CHECK, FOUND 1 INCH CRACK ON FUSELAGE SKIN AT BS 727 PLUS B PLUS 10 STRINGER 17 RIGHT. DETECTED BY VISUAL/EDDY CURRENT. INSTALLED DOUBLER PER SRM 53-30-3 FIGURE 1. (M)Jan 26, 1998 · N249US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980041Skin · crackedROA - DURING CX-3 CHECK, FOUND .375 INCH CRACK ON FUSELAGE SKIN AT BS 727 A PLUS 12 STRINGER 18 RT. INSTALLED DOUBLER PER SRM 53-30-3 FIGURE 1. (M)Jan 26, 1998 · N249US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980018Skin · crackedROA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND .3125 INCH CRACK BS 750 STRINGER 19R FUSELAGE SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M)Jan 26, 1998 · N249US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980040Floorbeam · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK FLOORBEAM BS 520, RBL 24. INSTALLED DOUBLER AND MOD REPAIRED PER EA 43461. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA980039Stringer · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 20 INCHES BS 907-927 STRINGER 25L. INSTALLED STRINGER REPAIR SPLICE, REPAIRED PER SRM 53-10-3 FIG 1. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980038Skin · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 10 INCH BY 5 INCH SKIN BULGED FUSELAGE SKIN BS 727, STRINGER 27L, STRINGER 27R BELLY. INSTALLED DOUBLER AND FILLERS, REPAIRED PER SRM 53-30-3 FIG 1. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980037Chord · crackedINT - DURING Q-6 CHECK EDDY CURRENT INSPECTION, FOUND .25 INCH CRACK BS 727 RT STRINGER 18A FORWARD FASTENER HOLE CRACKED FORWARD FLANGE OF OUTBOARD CHORD. INSTALLED CHORD KIT, REPAIRED PER EA 5394GO68 CARD NR 2-21-93834. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA980036Floorbeam · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 CRACKS, .5 INCH AND 1.5 INCHES LONG AT BS 520 RBL 45 FLOORBEAM. INSTALLED KIT, REPAIRED PER EA 43461. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA980035Bulkhead Web · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 178 LBL 4.5 AT LOWER LEFT ANT MOUNT BULKHEAD WEB. STOP DRILLED, NDT INSPECTION AND INSTALLED FILLERS AND DOUBLER PER TR 53-10-11. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Main, BulkheadSDR USAA980034Frame · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK FORWARD DOOR FRAME AT UPPER HINGE CUTOUT. STOP DRILLED CRACK, NDT INSPECTION, INSTALLED REPAIR DOUBLER, REPIRED PER SRM 51-40-3 FIG 1. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA980033Floorbeam · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 520, LBL 24 FLOORBEAM. INSTALLED DOUBLER, REPAIRED PER EA 43461. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA980032Frame · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA BS 990 WL 208 STRINGER 17R FRAME. INSTALLED FILLER AND DOUBLER, REPAIRED PER SRM 51-40-3. CORROSION TASK NR C53-107-07, CORROSION LEVEL 2. (M)Jan 23, 1998 · N234US · Boeing 737201 · Fuselage Main, Frame
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