Boeing 737-2Q8
Service difficulty reports · 133
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 = '7372Q8' 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 = '7372Q8' 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 P2EA00106Skin · wornYXD - DURING C-CHECK, FOUND RIGHT LE SKIN WITH WEAR OUT OF LIMITS WBL 275.4, LENGTH 1.1 INCH, WIDTH .550 INCH DEPTH .060 INCH. REPLACED SKIN ON RIGHT LE AT WBL 275.4 PER BOEING SRM 57-30-4 FIG 5, WORK COMPLETED ON VAM100-0098. (M)SDR P2EA00105Skin · dentedYXD - DURING C-CHECK, FOUND AFT CARGO DOOR WITH DENT OUT OF LIMITS BS 817.5 STRINGER 23-24R, LENGTH 3.250 INCH, WIDTH 1.675 INCH, DEPTH .054 INCH. REPAIRED AFT CARGO DOOR BS 817.5 STRINGER 23-24R PER BOEING SRM 52-00-3 FIG 6, WORK COMPLETED ON VAM100-0077. (SDR P2EA00085Skin · gougedYXD - DURING C-CHECK, FOUND PLATE AND WEB AT FORWARD CARGO AFT CUTOUT, BS 440, WL 168 GOUGED AND CORRODED, LENGTH 1.1 INCH, WIDTH 1.1 INCH, DEPTH .1 INCH. REPLACED PLATE AND WEB ON CARGO AFT CUTOUT BS 440, WL 168 IAW BOEING SRM 51-10-1 AND 51-10-3 ON BELL CRASDR P2EA00108Door Frame · crackedYXD - DURING C-CHECK, THE AFT CARGO FORWARD DOOR FRAME CRACKED AT BS 802, LENGTH 2 INCHES. REPLACED THE AFT CARGO FORWARD DOOR FRAME AT BS 802 PER BOEING SRM 53-40-1 AND BOEING PREVENTIVE MOD NR 65C35243, WORK COMPLETED ON VAM100-0021. (M)SDR P2EA00099Skin · crackedYXD - DURING C-CHECK, FOUND CREASE AND CRACK OUT OF LIMITS ON FUSELAGE SKIN BS 360-375 STRINGER 13-15L, WL 232, LENGTH 4.5 INCHES. REPAIRED AND INSTALLED DOUBLER AND FUSELAGE SKIN BS 360-375 STRINER 13-15L WL232 PER AAPROVED SPAR MPP NR VAN-2000-737-53-028 RESDR P2EA00096Intercostal · crackedYXD - DURING C-CHECK, FOUND INTERCOSTAL UPPER CHORD AT BS 344 LBL 12 WITH CRACK, LENGTH .750 INCH. REPAIRED INTERCOSTAL UPPER CHORD AT BS 344 LBL 12 WITH DOUBLER PER SRM 51-40-3 FIG 1, WORK ACCOMPLISHED ON NON-ROUTINE NR 0121. (M)SDR P2EA00095Skin · corrodedYXD - DURING C-CHECK, FOUND THE FUSELAGE WITH A BULGE (LENGTH 6 INCHES, WIDTH .750 INCH, DEEP .020 INCH) AT BS 1007 BL3R. REPLACED SHEAR TIE AND BLENDED CORROSION AT BS 1007 BL3R PER SRM 51-10-1, 51-10-6 AND 51-30-2 WORK ACCOMPLISHED ON NON=ROUTINE NR0021. (SDR P2EA00078Skin · crackedYXD - DURING C-CHECK, FOUND A CRACK ON AFT ENTRY DOOR SKIN AFT UPPER CORNER EXTENDING FROM RIVET, .375 INCH, BS 986, WL 280L. REPAIRED CRACK AT BS 986 WL 280L AFT ENTRY DOOR SKIN UPPER AFT CORNER WITH DOUBLER PER SRM 52-00-3 FIG 5. WORK ACCOMPLISHED ON NON-RSDR P2EA00077Skin · dentedYXD - DURING C-CHECK, FOUND A DENT BEYOND LIMITS, (LENGTH 5 INCHES, WIDTH 2 INCHES, DEPTH .071 INCHES)AT BS 882 STRINGER 15-16R PER SRM 53-30-1. REPAIRED DENT AT BS 882 STRINGER 15-16R WITH DOUBLER PER SRM 53-30-1. WORK ACCOMPLISHED ON NON-ROUTINE NR 0014. SDR P2EA00066Skin · crackedMCI - DURING WALKAROUND, MAINTENANCE FOUND TWO CRACKS IN FUSELAGE SKIN ABOVE THE RIGHT AFT WING TO BODY FAIRING, APPROXIMATE LOCATION FS 727B RT. (M)SDR P2EA00015Swivel · leakingMCI - FLT 327 - ON DESCENT, AIRCRAFT LOST SYSTEM-A HYDRAULIC PRESSURE AND INDICATION. AIRCRAFT LANDED AT MCI WITH NO INCIDENT. REMOVED AND REPLACED SWIVEL AT NR 3 SLAT ACTUATOR, OPERATIONAL CHECK IAW MM 27-81-0. REMOVED AND REPLACED SYSTEM-A HYDRAULIC PUMP SDR P2EA99236Module · unserviceableMSP - FLT 703 - NO EMERGENCY DECLARED, LANDING NORMAL. LANDING GEAR UNSAFE LIGHTS, 3 RED, REMAINED ON AFTER TAKEOFF. AIRCRAFT WAS INSPECTED THEN REPOSITIONED TO MCI ON SPECIAL FLIGHT PERMIT. REPLACED LANDIGN GEAR MODUEL, OPS CHECK NORMAL PER MM 32-09-100. SDR P2EA99225Control Handle · lack of lubeMCI - FLT 402 - AFTER TAKEOFF WHEN THE LANDING GEAR WAS PLACED IN THE UP POSITION, ALL 3 GEAR LIGHTS REMAINED ON (RED). THE SAME INDICATION WAS PRESENT IN THE LANDING GEAR HANDLE. DISCOVERED LANDING GEAR CONTROL HANDLE STICKING. CLEANED AND LUBED HANDLE. PSDR P2EA99224Tire · failedMDW - FLT 744 - ON TAKEOFF ROLL, PILOT HEARD A LOUD BANG. AIRCRAFT RETURNED TO GATE WITH NO INCIDENT. UPON INSPECTION, FOUND NOSE TAXI LIGHT LENS BROKEN, BOTH NLG TIRES WITH MANY CUTS AND NR 3 AND NR 4 MAIN TIRES OUT. REMOVED AND REPLACED NOSE TAXI LIGHT ASSDR P2EA99218Mechanical · out of ajdustMDW - FLT 738 - LEADING EDGE IN-TRANSIT LIGHT STAYS ON IN FLAP POSITIONS 1-10, SLAT NR 3 SLOWS IN TRANSIT. AIRCRAFT ISSUED A SPECIAL FLIGHT PERMIT TO MCI. RE-ADJUSTED LEADING EDGE NR 3 SLAT AND RE-RIGGED DETENT ARMS. AIRCRAFT FLAPS WERE FUNCTIONAL TESTED INSDR AWXA9500298Eel Connector · dirtyPHX - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT MOUNTED EMERGENCY EXIT LIGHTS IN AFT SECTION OF AIRCRAFT INOPERATIVE. REMOVED AND CLEANED BATTERY PACK CONNECTOR AT ROW 18. OPS CHECK GOOD. (M)SDR AWXA9500214Intercostal · corrodedDURING C12 INSPECTION, FOUND INTERCOSTAL STATION 294 TO 312 RBL 12 CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL PER SRM 51-30-2 AND 53-10-2, FIGURE 7.SDR AWXA9500213Plate · corrodedPHX - DURING C12 INSPECTION, FOUND L1 DOOR FORWARD GIRT BAR ATTACH PLATE CORRODED. FABRICATED AND INSTALLED NEW PLATE PER SRM 51-10-1. (W)SDR AWXA9500212Angle · crackedPHX - DURING C12 INSPECTION, FOUND INTERCOSTAL ANGLE BETWEEN STATION 294.5 AND 303.9 CRACKED AT STRINGER 12R, 13R AND 14R. FABRICATED NEW ANGLES AND INSTALLED PER SRM 51-30-02. (W)SDR AWXA9500211Intercostal · crackedPHX - DURING C12 INSPECTION, FOUND INTERCOSTAL BETWEEN STATION 540 BL0 TO LBL 24.75 CRACKED. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-2 AND 51-10-1. (W)SDR AWXA9500210Angle · corrodedDURING C12 INSPECTION, FOUND R1 DOOR THRESHOLD SUPPORT ANGLE CORRODED BEYOND CLEAN UP LIMITS. REMOVED, FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-30-2. (W)SDR AWXA9500209Intercostal · corrodedPHX - DURING C12 INSPECTION, FOUND INTERCOSTAL FORWARD OF STATION 294 LBL 12 CORRODED BEYOND CLEAN UP LIMITS. REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL PER SRM 53-10-2 AND 51-30-2. (W)SDR AWXA9500208Skin · crackedDURING C12 INSPECTION, FOUND SKIN CRACKED AT R1 DOOR CUT OUT LOWR AFT CORNER. REPAIRED DAMAGE PER SRM 53-30-3, FIGURE 26. (W)SDR AWXA9500207Skin · crackedPHX - DURING C12 INSPECTION, FOUND SKIN CRACKED AT STATION 370 BL 0. DAMAGE REPAIRED PER EO 53-30-13. (W)SDR AWXA9500206Skin · crackedPHX - DURING C12 INSPECTION, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUT OUT. DAMAGE REPAIRED PER SRM 53-30-3, FIGURE 35. (W)SDR AWXA9500201Floor Beam · corrodedPHX - DURING SCHEDULED INSPECTION OF TASK C53 107 02, FOUND TWO AREAS OF CORROSION THAT WERE BEYOND CLEAN UP LIMITS AROUND SCREW HOLES OF STATION 294 FLOOR BEAM, RBL 8 AND RBL 30. REMOVED DAMAGED AREAS OF FLOOR BEAM AND INSTALLED REPAIR TOP CAP AND ANGLES PERSDR AWXA9500200Floor Beam · corrodedPHX - DURING SCHEDULED INSPECTION OF TASK C53 107 02, FOUND CORROSION BEYOND CLEAN UP LIMITS AROUND SCREW HOLES ON FLOOR BEAM, STA 328 RBL 15 TO RBL 25. REPLACED TOP CAP AND SPLICE ANGLES PER SRM 53-10-9. (W)SDR AWXA9500199Floor Beam · corrodedDURING SCHEDULED INSPECTION OF TASK C53 107 02, FOUND CORROSION BEYOND CLEAN UP LIMITS AROUND SCREW HOLES ON FLOOR BEAM, STATION 328 RBL 30 TO RBL 50. REPLACED DAMAGED TOP CAP SECTION OF FLOOR BEAM PER SRM 53-10-9, FIGURE 5. (W)SDR AWXA9500198Chord · corrodedPHX - DURING SCHEDULED INSPECTION OF TASK C53-107-02, FOUND R1 DOOR INNER CHORD CORRODED BEYOND LIMITS, STATION 294 STR 17. REPLACED CHORD PER SRM 53-10-1 AND 51-30-2. (W)SDR AWXA9500197Chord · corrodedDURING SCHEDULED INSPECTION OF TASK C53 107 02, FOUND L1 DOOR INNER CHORD CORRODED BEYOND CLEAN UP LIMITS AROUND SCREW HOLES, STATION 312 TO 340. REMOVED AND REPLACED CHORD PER SRM 51-10-1 AND 51-30-02. (W)SDR AWXA9500171Fluid · leakingSLC - FLT 2808 - PHX-SLC - CREW DECLARED AN EMERGENCY DUE TO LOSS OF HYDRAULIC FLUID. 125 MILES FROM SLC THE HYDRAULIC FLUID QUANTITY DROPPED. AIRCRAFT LANDED WITHOUT INCIDENT. AFTER LANDING, THE INDICATOR CAME UP TO THE REFILL MARK ON GAUGE. CONTRACT MAINSDR AWXA9500106Eel Battery Pack · dischargedPHX - DURING ROUTINE MAINTENANCE CHECK, FOUND BOTH OVERWING INTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT OVERWING CEILING LOCATION, OPS CHECK NORMAL. (Z)SDR AWXA9500023Eel Battery Pack · dischargedPHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS WOULD NOT EXTINGUISH, ROWS 16-22. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (W)
Back to Boeing 737-2Q8