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 USAA960027Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACKED STRINGER TIE CLIP BS 787 STRINGER 4R. REPLACED CLIP, REPAIRED PER EO 5393G227. (M)SDR USAA960026Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACKED STRINGER TIE CLIP BS 767 STRINGER 10R. REPLACED TIE CLIP, REPAIRED PER EO 5393G227. (M)SDR USAA960025Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STRINGER TIE CLIP BS 787 STRINGER 10R. REPLACED CLIP, REPAIRED PER EO 5393G227. (M)SDR USAA960024Support · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 1 INCH AT FLOOR SUPPORT 10 PERCENT DEEP AT STRINGER 28L STATION 947. REPAIRED AND REPLACED STR SECTION AND REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)SDR USAA960023Stringer · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AT STRINGER 27R STATION 1006, 2 INCH BY 1 INCH. REPAIRED AND REPLACED SHORT STRINGER SECTION WITH NEW COMPLETE STRINGER. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (MSDR USAA960021Doubler · damagedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND DAMAGE ON UNKNOWN DOUBLER 12 INCHES BY 18 INCHES STATION 500B BETWEEN STRINGER 27R AND 26R. PREVIOUS INSTALLED EXT DOUBLER. REPAIRED PER SRM 53-30-3. (M)SDR USAA960020Fitting · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT STATION 727 BULKHEAD STIFFENER FITTING IN LOWER FORWARD RADIUS, BL 0 WL 202.5. REPAIRED PER EO 5394G176. (M)SDR USAA960019Intercostal · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK IN INTERCOSTAL BS 328 TO 344 LBL 17 INCHES. INSTALLED NEW INTERCOSTAL. (M)SDR USAA960018Clip · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK IN STRINGER CLIP, BS 597 S-9 R. REPLACED CLIP, REPAIRED PER EO 5393G227. (M)SDR USAA960017Floor Beam · corrosionINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 12 CORRODED AREAS APPROX 1 INCH BY 1 INCH EACH AT FLOOR BEAM, BS 328 RBL 48 AND LBL 48. SPLICED IN NEW T-CAP. REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-01, CORROSION LEVEL 2. (M)SDR USAA960015Floor Beam · crackedINT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 CRACKS IN UPPER RADIUS OF FLOOR BEAM AND .5 INCH LONGITUDINAL CRACK BS 520 2 INCH CRACK AT LBL 24 AND RBL 24, AND .5 INCH CRACK AT LBL 45. INSTALLED REPAIRS AND PREVENTIVE MODIFICATION ON BS 520 FLOOR BEAM PERSDR USAASB96001Element · shortedFLT NR 1244 - CLT - LEFT WING BODY OVERHEAT ILLUMINATED IN FLT. ISOLATED LEFT BLEED AIR DUCT BUT OVERHEAT LIGHT REMAINED ON. MAINTENANCE FOUND OVERHEAT ELEMENT SHORTED. REPLACED ELEMENT. OPS CHECKS SAT. (M)SDR USAA951426Skin · crackedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND TWO CRACKS (LIGHTNING STRIKE) ON SKIN S-19R FS 328. INSTALLED DOUBLER AND FILLER. REPAIRED PER EO 40393 EA 40393. (M)SDR USAA951425Channel · crackedINT - DURING Q-2 CHECK VISUAL INSPECTION, FouND .75 INCH CRACK LBL 45 SEAT TRACK SUPPORT CHANNEL STATION 520, WL 207.5. REPLACED SUPPORT CHANNEL, REPAIRED PER SRM 51-10-01. (M)SDR USAA951424Channel · crackedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK LBL 25 SEAT TRACK SUPPORT CHANNEL STATION 520, WL 207.5. REPLACED SUPPORT CHANNEL, REPAIRED PER SRM 51-10-1. (M)SDR USAA951423Frame · crackedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CRACK 1.25 INCH LONG STATION 597 ABOVE WING CENTER FRAME SECTION RIGHT SIDE. REPLACED FRAME SECTION. REPAIRED PER SRM 51-10-01. (M)SDR USAA951422Frame · crackedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CRACK 1.5 INCHES LONG STATION 597 ABOVE WING CENTER SECTION LEFT FRAME. REPLACED FRAME SECTION. REPAIRED PER SRM 51-10-01. (M)SDR USAA951421Frame · crackedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK STATION 616 RIGHT FRAME INBOARD CHORD AT FIRST FASTENER ABOVE CENTER WING. INSTALLED DOUBLER, REPAIRED EPR EA 40390. (M)SDR USAA951420Frame · crackedINT - DURING Q-2 VISUAL INSPECTION, FOUND 1 INCH CRACK STATION 616 LEFT FRAME INBOARD CHORD FIRST FASTENER ABOVE CENTER WING. INSTALLED DOUBLER, REPAIRED PER EO 40390. (M)SDR USAA951419Floor Beam · crackedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK RBL 25 LONGITUDINAL FLOOR BEAM AT AILERON QUADRANT STATION 676, WL 206.5. INSTALLED DOUBLER, REPAIRED PER EA 40395 AND EO 5791G632. (M)SDR USAA951418Floor Beam · crackedINT - DURING 'Q-2' CHECK VISUAL INSPECTION FOUND 1.25 INCH CRACK LBL 25 LONGITUDINAL FLOOR BEAM AT AILERON QUADRANT STA 676. WL 206.5. INSTALLED DOUBLER, REPAIRED PER EA 40395, EO 5791G632. (X)SDR USAA951417Blkhd Stiffener · crackedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK STA 727 BULKHEAD STIFFENER FITTING LBL 25, WL 202.5. REPLACED FITTING. REPAIRED PER SRM 5-10-1. (X)SDR USAA951416T-Splice · crackedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .3750 INCH CRACK S27L (KEEL BEAM) TO BS 727 BULKHEAD ATTACH ANGLE 1 INCH AFT OF BULKHEAD PLUS 5 INCHES ABOVE LOWER SKIN T-SPLICE. INSTALLED PREFABRICATED T-SPLICE, REPAIRED PER BOEING DRAWING 69-41460. (X)SDR USAA951415Stringer · crackedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CRACK .25 INCH LONG IN STRINGER 18A LEFT, STA 727. INSTALLED DOUBLERS, REPAIRED PER EA 40452. (X)SDR USAA951414Gate Hinge · crackedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 15 INCH CRACK IN HINGE AT LOWER GATE, LOWER GATE HINGE OF FORWARD GALLEY DOOR. INSTALLED IMPROVED PART, REPAIRED PER EA 40349. (X)SDR USAA951413Floor Beam · corrosionINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 1 INCH CORROSION ON FLOOR BEAM BS 344, LBBL 15. INSTALLED NEW T-CAP REPAIRED PER TR 53-10-13. (X)SDR USAA951412Web · crackedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CRACK .25 INCH LONG AT WEB, STRINGER 18A RIGHT, STA 727. INSTALLED DOUBLER, REPAIRED PER EA 40452. (X)SDR USAA951411Bulkhead · dentedINIT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH DENTED AREA PRESSURE BULKHEAD, STA 727, BULKHEAD RBL 40. REPAIRED OVERSIZED FASTENER HOLES AND INSTALLED REPAIR PER EO. WEIGHT CHANGE LESS THAN 1 POUND. REPAIRED PER EO 5394G068 AND BOEING DSDR USAA951410Chord · crackedINT - DURNG 'Q-2' CHECK EDDY CURRENT INSPECTION, FOUND 2 CRACKS IN AFT OPEN FASTENER HOLE BS 727, OUTBOARD CHORD, BS 727, STRINGER 18L, IN OUTBOARD CHORD. INSTALLED LEFT 727 OUTBOARD CHORD, REPAIRED PER EO 5394G068 AND 262-21-93828. (X)SDR USAA951409Clip · crackedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CRACK .25 INCH LONG AT TIE CLIP, STA 727, STRINGER 5 RIGHT. REPLACED TIE CLIP, REPAIRED PER EO 5393G227. (X)SDR USAA951408Clip · crackedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CRACK .25 INCH LONG STA 747 AT STRINGER 6 RIGHT, TIE CLIP. REPLACED TIE CLIP, REPAIRED PER EO 5393G227. (X)SDR USAA951407Clip · crackedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .25 INCH LONG CRACK STA 767 AT STRINGER 10 RIGHT, TIE CLIP. REPLACED TIE CLIP PER EO 5393G227. (X)SDR USAA951406Clip · crackedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STRINGER 3L TIE CLIP STATION 707. REPLACED TIE CLIP, REPAIRED PER EO 5393G227. (M)SDR USAA951405Fitting · crackINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STATION 727 BULKHEAD STIFFENER ATTACH FITTING BL 0, WL 202.5. REPLACED FITTING. REPAIRED PER EO 5394G176. (M)SDR USAA951404Clip · crackedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK S-10 L TIE CLIP STATION 747. REPLACED TIE CLIP, REPAIRED PER EO 5393G227. (M)SDR USAA951403Clip · crackedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .3750 INCH CRACK S4R TIE CLIP STA 707. REPLACED TIE CLIP, REPAIRED PER EO 5393G227. (X)SDR USAA951402Stringer · crackedIINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CRACK APPROXIMATELY .1850 INCH, BS 727, S18A, LEFT SIDE. INSTALLED SPLICE STRAPS, REPAIRED PER EA 40542. (X)SDR USAA951401Frame · crackedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND SEVERAL CRACKS IN HOLES BETWEEN S20L AND S21L, ONE, .50 INCH CRACK AT ATTACH HOLE FOR TRANSITION ANGLE FRAME, BS 460, LEFT SIDE. CUT OUT CRACK AT TRANSITION AREA OF FRAME AND BETWEEN S20L AND S21L. MANUFACTURSDR USAA951400Skin · dentedINT - DURING 'Q-2' CHECK VISUAL INSPECTION FOUND 1 INCH BY 1 INCH DENT STA 907, S17L, SKIN. INSTALLED 1.50 INCH BY 1.50 INCH FILLER 2024-T3 .080, AND 7 INCH BY 8 INCH DOUBLER 2024-T3 .090. REPAIRED PER SRM 53-30-3, FIGURE 28. (X)SDR USAA951399Floor Beam · crackedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND SIX, .25 INCH CRACKS, BL ZERO, LONGITUDINAL FLOOR BEAM WEB BETWEEN STA 707 - STA 713, WL 203. INSTALLED REPAIR DOUBLER, REPAIRED PER BOEING DRAWING NR 65C34537. (X)SDR USAA951398Intercostal · crackedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT LBL 25 INTERCOSTAL 1 INCH FORWARD OF BS 520, FLOOR BEAM WL 206 (UPPER CHORD). REPLACED INTERCOSTAL PER SRM 51-10-2. (X)SDR USAA951397Frame · crackedINT - DURING 'Q-2' CHECK EDDY CURRENT, FOUND CRACKED FRAME .5 INCH LONG AT STA 727, S18R. REPLACED FRAME SECTION, EO 5394G068. (X)SDR USAA951396Skin · damagedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 9 INCH BY 5.50 INCH DOUBLER PREVIOUSLY INSTALLED FUSELAGE SKIN, BS 847, S22R. REPAIR IS PER SRM, DOUBLER INSTALLED, REPAIRED PER SRM 737-200, SRM 53-30-3, FIGURE 1. (X)SDR USAA951395Skin · damagedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 36 INCH BY 22 INCH DOUBLER PREVIOUSLY INSTALLED EXTERNAL SKIN OF AFT CARGO DOOR FUSELAGE SKIN. DOUBLER INSTALLED, REPAIRED PER 737-200, SRM 52-00-3, FIGURE 5. (X)SDR USAA951394Floor Beam · corrosionINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CLIP-NUT HOLES CORRODED ENTIRE LENGTH OF FLOOR BEAM STA 986.5, RBL 70 - LBL 70 FLOOR BEAM WL 208.1. REPLACED T-CAP OF BEAM. REPAIRED PER TR 53-10-05 C. CORROSION LEVEL 1. (X)SDR USAA951393Skin · corrosionINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 4.5 INCH BY 6.5 INCH CORROSION, BS 550A PLUS 10 INCHES, STRINGER 28 RIGHT, FUSELAGE SKIN. INSTALLED DOUBLER, REPAIRED PER EA 40449. CORROSION LEVEL 1. (X)SDR USAA951392Angle · corrosionINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 36 INCH AREA OF SURFACE CORROSION, 1 INCH CIRCLE OF EXFOLIATION AT RIGHT REAR CABIN DOOR Z-ANGLE, STA 947 - STA 1006, RBL 50, WL 208.1. REPLACED Z-ANGLE. REPAIRED PER SM 51-10-01. CORROSION LEVEL 1SDR USAA951391Angle · corrosionINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 40 INCH CORRODED Z-ANGLE AT LEFT REAR CABIN ENTRY DOOR, STA 947 - STA 986, LBL 50, WL 208.1. INSTALL NEW PREFABRICATED Z-ANGLE. WEIGHT CHANGE LESS THAN 1 POUND. REPAIRED PER SRM 510-10-1, PAGE 5, ISDR USAA951390Seat Track · corrosionINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORROSION AT CLIP NUT HOLES, STA 986 - STA 1016, RBL 24 AND RBL 26, WL 208.1 SEAT TRACK. REPLACED SEAT TRACKS, REPAIRED PER SRM 51-10-01. CORROSION LEVEL 1. (X)SDR USAA951389Angle · corrosionINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 30 INCH FLOOR SUPPORT ANGLE CORRODED AT CLIP NUT HOLES, STA 947 - STA 986, BL ZERO, WL 208.1. INSTALLED NEW PRE-FAB ANGLE. WEIGHT CHANGE LESS THAN 1 POUND. REPAIRED SRM 51-10-1, PAGE 5. CORROSION
Back to Boeing 737-2B7