Boeing 737-2B7
Service difficulty reports · 1,360
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 = '7372B7' 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 = '7372B7' 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 USAA951388Floor Beam · corrodedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .25 INCH BY 48 INCH CORRODED CABIN FLOOR BEAM, BS 328 AT RBL 10 INCHES - RBL 58 INCHES. REMOVED CORRODED SECTION OF T-CAP AND SPLICED IN NEW SECTION. REPAIRED PER TR 53-10-13. CORRISION TASK NR C53-107-02. SDR USAA951387Tee Cap · corrosionINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 3 INCH BY 8 FEET CORROSION FS 328, RBL 10 INCHES, RBL 58 INCHES, TEE CAP. INSTALLED LOCAL MANUFACTURED TEE CAP AND SPLICED ANGLES. REPAIRED PER T.R. 53-10-13, EA 40349. CORROSION LEVEL 1. (X)SDR USAA951386Angle · corrodedINT - DURING 'Q-2' CHECK VISUAL INSPECTION FOUND CORROSION .50 INCH BY 1 INCH FORWARD SERVICE DOOR SILL PLATE SUPPORT ANGLE. REPLACED ANGLE, REPAIRED PER SRM 51-10-01. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)SDR USAA951385Intercostal · corrodedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORROSION ON INTERCOSTAL, LBL 10, STA 296. INSTALLED NEW INTERCOSTAL. REPAIRED PER SRM 51-10-1, RESTORED TO ORIGINAL. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)SDR USAA951384Intercostal · corrodedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORROSION ON TOP FLANGE OF INTERCOSTAL, RBL 11, STA 328 TO STA 344. INSTALLED NEW PART ON AIRCRAFT. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)SDR USAA951383Intercostal · corrodedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORRODED INTERCOSTAL RBL 11, STA 316. INSTALLED NEW INTERCOSTAL. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C52-107-02. CORROSION LEVEL 2. (X)SDR USAA951382Intercostal · corrodedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORRODED INTERCOSTAL RBL 12, STA 294 - STA 312. INTERCOSTAL REPLACED. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)SDR USAA951381Angle · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH BY 3 INCH AT ATTACH ANGLE STATION 947.5 BETWEEN STRINGER 26L AND 27L. REPLACED ANGLE WITH NEW ONE FROM STOCK. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-202-01. CORROSION LEVEL 2. (M)SDR USAA951380Stringer · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 6 INCH CORRODED AREA ON STRINGER S-27L AT STATION 947.5. REMOVED CORRODED SECTION OF STRINGER AND REPLACED. REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01. CORROSION LEVEL 2. (M)SDR USAA951379Frame · corrosionINT - DURING 'Q-2' CHECK VISUAL INSPECTION FOUND 1.50 INCH BY 1 INCH CORROSION AT FRAME BS 992. MANUFACTURED FRAME REPAIR, HEAT TREATED, AND INSTALLED. REPAIRED PER SRM 51-40-3, SPM 20-30-06. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)SDR USAA951378Intercostal · corrosionINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORROSION ON INTERCOSTAL CLIP NUT HOLES, STA 957. MANUFACTURED NEW INTERCOSTAL. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)SDR USAA951377Floor Web · corrodedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 1 INCH ROUND AREA AT NUTPLATE CORRODED, FLOOR WEB 10 INCHES AFT OF FLOOR BEAM, BS 1016, BL ZERO. CUT OUT CORROSION, INSTALLED DOUBLER. REPAIRED PER SRM 51-40-2. CORROSION TASK NR C53-107-02. CORROSION LEVELSDR USAA951376Floor Beam · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 SQUARE INCHES OF CORROSION AT T-CAP FLOOR BEAM STATION 947 RBL 9. REMOVED CORRODED SECTION OF T-CAP. SPLICED IN NEW SECTION OF T-CAP. REPAIRED PER SRM 53-10-9. CORROSION TASK NR C53-107-02. CORROSION LEVELSDR USAA951375Seat Tracks · corrosionINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORROSION AT SEAT TRACKS 1 INCH BY 1 INCH, RBL 8, RBL 24, AND RBL 36 AT STA 986 - STA 1016. REPLACED THREE SEAT TRACKS. REPAIRED PER SRM 51-10-01. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)SDR USAA951374Floor Beam · corrosionINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .50 INCH BY .50 INCH HOLE AT WEB OF FLOOR BEAM, STA 1016 PLUS 6 INCHES, RBL 6. INSTALLED DOUBLER. REPAIRED PER SRM 51-40-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)SDR USAA951373Angle · corrosionINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORROSION .50 INCH BY 66 INCHES AT Z-ANGLE AT FORWARD SERVICE DOOR AREA STA 294 TO STA 360. REPLACED Z-ANGLE. REPAIRED PER SRM 51-10-01. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)SDR USAA951353Skin · crackedCLT - CLT INSPECTION FOUND A FUSELAGE SKIN CRACK 2 INCHES LONG, LOCATED AT STATION 727, STRINGER 17L. INSTALLED DOUBLER AS PER BOEING SRM 53-30-3 FIG 6. (M)SDR USAA951251Skin · crackedCLT - CLT INSPECTION VISUALLY FOUND A 2 INCH SKIN CRACK AT BS 727, STR 17L. INSTALLED DOUBLER PER SRM 53-30-3. (X)SDR USAA951372Intercostal · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1.5 INCH BY 1 INCH, BY STATION 947 TO STATION 967, RBL 45 INTERCOSTAL. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)SDR USAA951317Seat Track · corrodedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 3 INCH CORRODED AREA BS 986.5 RBL 24. REPLACED SEAT TRACK, WT CHANGE LESS THAN 1 LB. REPAIRED PER SRM 51-10-1 AND SRM 53-10-5. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M)SDR USAA951316Floor Beam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK LBL 25 LONGITUDINAL FLOOR BEAM WEB (LOWER) STATION 707, WL 203. INSTALLED WEB REPAIR (WT .3 LBS), REPAIRED PER SRM 51-40-2. (M)SDR USAA951315Floor Beam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BL 0 STATION 708 AND BS 710. INSTALLED WEB REPAIR, REPAIRED PER DWG 65C34537. (M)SDR USAA951314Skin · gougedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH GOUGE IN OUTER SKIN OF AFT CARGO DOOR TOP AFT CORNER OF DOOR (6 INCH BY 6 INCH DOUBLER). INSTALLED EXT SKIN DOUBLER, REPAIRED PER SRM 52-00-3. (M)SDR USAA951313Fitting · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK, BL 0 LONGITUDINAL FLOOR BEAM SUPPORT FITTING FORWARD RADIUS, STATION 727, WL 202.5. INSTALLED REINFORCING ANGLES, RADIUS FILLERS, SHIMS AND SEALED. REPAIRED PER EO 5394G176. (M)SDR USAA951312Angle · crackINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK RIGHT WING TO BODY SUPPORT ANGLE BS 540-522. REPLACED ANGLE, LESS THAN 1 LB WEIGHT CHANGE, REPAIR PER EA 25375 AND SRM 51-40-3. (M)SDR USAA951311Stringer · crackINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK S-16R, BETWEEN STATION 500B AND 520, ON STRINGER. INSTALLED STRINGER REPAIR, REPAIRED PER EO 5393X228. (M)SDR USAA951310Stringer · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STRINGER 16 L, BETWEEN STATION 500B AND STATION 520, ON STRINGER. INSTALLED STRINGER REPAIR, REPAIRED PER EO 5393X228. (M)SDR USAA951309Hinge · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AT AFT END OF HINGE, FRONT CABIN SERVICE DOOR LOWER GATE HINGE. REPLACED HINGE, REPAIR PER EA 40350. (M)SDR USAA951308Stringer · gougedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH GOUGE IN STRINGER OUTBOARD 'J' SECTION, STATION 1044 STRINGER 27L. INSTALLED REPAIR DOUBLER UNDER 'J' LEG OF STRINGER, AFTER SMOOTHING GOUGE. REPAIRED PER SRM 53-10-3 FIG 1. (M)SDR USAA951307Skin · damagedINT - DURING 'Q-3' CHECK VISUAL INSPECTION (PREVIOUS REPAIR NOT PER SRM), FOUND UNKNOWN DAMAGED DOUBLER, 8 INCHES BY 9.50 INCHES, BS 227 TO BS 235, S19R TO S20R. INSTALLED DOUBLER PER SRM, REPAIRED PER SRM 53-30-3. (X)SDR USAA951306Floor Beam · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH LONG CRACK IN UPPER RADIUS OF BEAM CAP, STA 520, FLOOR BEAM RBL 25. INSTALLED FLOOR BEAM REPAIR, .8 POUNDS AT BS 520, REPAIRED PER SB 737-53-1120, EA 40385. (X)SDR USAA951305Stringer · gougedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND DEEP GOUGE .25 INCH BY 2 INCHES IN UPPER INBOARD LEG OF S26L, BS 1044. INSTALLED STR REPAIR, LESS THAN 1 POUND ADDED, REPAIRED PER SRM 53-10-3, FIGURE 1. (X)SDR USAA951304Angle · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 1.50 INCH CRACK, BS 727, RBL 24.5 ON ANGLE. INSTALLED REPAIR ANGLE, REPAIRED PER EA 40453. (X)SDR USAA951303Attach Angle · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK, STA 639, STUB BEAM ATTACH ANGLE, RBL 45, WL 207. REPLACED ATTACH ANGLE, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER SRM 51-10-1. (X)SDR USAA951302Frame · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK, STA 616, RIGHT FRAME INBOARD CHORD, FIRST FASTENER ABOVE CENTER WING SKIN. INSTALLED FILLER ANGLE, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER EA 40391. (X)SDR USAA951301Frame · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK, STA 616, LT FRAME INBOARD CHORD, FIRST FASTENER ABOVE CENTER WING SKIN. INSTALLED FILLER AND ANGLE, WEIGHT CHANGE LESS THAN 1 POUND. REPAIRED PER EA 40391. (X)SDR USAA951300Support · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK, SEAT TRACK SUPPORT CHANNEL, STA 520, LBL 45, WL 207.5. INSTALLED FLOOR BEAM REPAIR, REPAIRED PER SB 737-53-1120, EA 40385, .8 POUNDS AT BS 520. (X)SDR USAA951298Floor Beam · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK, RBL 24.5, STA 675, IN FLOOR BEAM. CRACK CONTAINED AT AILERON QUADRANT CUT-OUT. INSTALLED REPAIR CHANNEL AMD DOUBLERS, AND RADIUS FILLERS AS REQUIRED PER CO 5791G632 AND EA 40396. (X)SDR USAA951297Floor Beam · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK, LBL 24.5, STA 675, IN FLOOR BEAM. CRACK CONTAINED BY FASTENER HOLE AND CUT-OUT INSTALL REPAIR CHANNEL, DOUBLERS, AND RADIUS FILLER AS REQUIRED BY EO 5791G632 AND EA 40396. (X)SDR USAA951296Skin · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .25 INCH LONG CRACK IN OUTER SKIN AT UPPER HINGE CUT-OUT AT ENTRY DOOR. INSTALLED EXTERIOR SKIN REPAIR. REPAIRED PER EA 40360. (X)SDR USAA951295Doubler · damagedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 5 INCH SLOT IN BEAR STRAP - DOUBLER PREVIOUSLY INSTALLED, BUT NOT PER SRM BS 794 AT S23R. REMOVED PREVIOUSLY INSTALLED DOUBLER AND INSTALLED REPAIR PER EA. (X)SDR USAA951293Seat Track · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 3.50 INCH BY 1 INCH AND 2 INCHES BY 1 INCH, BS 990 AND BS 1015 AT RBL 8 INCHES ON SEAT TRACK. REPLACED TRACK, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSIOSDR USAA951292Intercostal · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCHES, STA 328 TO 340, LBL 12 INCHES ON INTERCOSTAL. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-10. CORROSION LEVEL 2. (X)SDR USAA951290Floor Beam · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 2 INCHES, STA 312 RBL 35 INCHES ON FLOOR BEAM. REPLACED T-CAP FROM LBL 6 TO RBL 36, REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)SDR USAA951289Floor Beam · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .75 INCH BY .50 INCH CORRODED AREA FLOOR BEAM BS 1016, LBL 15. REMOVED CORROSION AND INSTALLED REPAIR STRAP, REPAIRED PER TR 53-10-01A. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)SDR USAA951288Intercostal · corrosionINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 1 INCH, STA 986.5 TO 1006 BL ZERO ON INTERCOSTAL. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)SDR USAA951287Intercostal · corrosionINT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND CORROSION 1.50 INCHES BY 1 INCH, STA 947 TO STA 967, RBL 45 ON INTERCOSTAL. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X)SDR USAA951286Floor Beam · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA AROUND NUTPLATE HOLES .25 INCH BY .25 INCH, BS 967 LBL 4, RBL 5, RBL 18 RBL 26, RBL 47, ON FLOOR BEAM. INSTALLED TEE SECTION ANGLES AND STRAPS. REPAIRED PER TR 53-10-05 C. CORROSION TASK NR C53-1SDR USAA951285Stringer · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 12 INCH BY 1 INCH AT S-26 R, BS 974 TO BS 986 ON STRINGER. SPLICED NEW STRINGER SECTION IN, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)SDR USAA951284Stringer · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 5 INCH BY 1 INCH S-25 L BS 968 ON STRINGER. INSTALLED DOUBLER WEIGHT CHANGE LESS THAN 1 LB. REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M)
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