N438US
Service difficulty reports · 235
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N438US' AND registry_match = 'registration' 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 n_number = 'N438US' AND registry_match = 'registration' 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 USAA2012091000020Tie Clip · crackedQ6 CHECK - CRACK ON STRINGER TIE CLIP AT BS 663, S10R. REPLACED STRINGER TIE CLIP AT B663, S10R IAW B737 SRM 51-40-02.SDR USAA2012091000019Tie Clip · crackedQ6 CHECK - CRACK ON STRINGER TIE CLIP AT BS 727E, S10R. REPLACED STRINGER TIE CLIP AT BS 727E, S10R IAW B737 SRM 51-40-02.SDR USAA2012091300024Seat Track · crackedQ6 CHECK - CRACK IN UPPER FLOOR CAP OF SEAT TRACK AT BS 727B +1 INCH, RBL 48. REPAIRED UPPER FLOOR CAP OF SEAT TRACK AT BS 727B +1 INCH, RBL 48 IAW B737 SRM 53-60-52-01-1 & 53-00-52-2R-3.SDR USAA2012091000025Frame · crackedQ6 CHECK - CRACK ON FUSELAGE FRAME AT BS 747 BETWEEN S8R TO S9R. REPAIRED FUSELAGE FRAME AT BS 747 BETWEEN S8R TO S9R IAW TYPICAL REPAIR TR737-5310-10-0287.SDR USAA2012091000023Tie Clip · crackedQ6 CHECK - CRACK ON STRINGER TIE CLIP AT BS 663, S10L. REPLACED STRINGER CLIP AT BS 663, S10L IAW B737 SRM 51-40-02.SDR USAA2012091000018Tie Clip · crackedQ6 CHECK - CRACK ON STRINGER TIE CLIP AT BS 639, S8L. REPLACED STRINGER TIE CLIP AT BS 639, S8L IAW B737 SRM 51-40-02 & BOEING DRAWING # 65-46540.SDR USAA2012092600035Tie Clip · crackedQ6 CHECK - CRACK ON STRINGER TIE CLIP AT BS 707, S11R. REPLACED STRINGER TIE CLIP AT BS 707, S11R IAW B737-400 SRM 51-40-02.SDR USAA2012091300025Crease Beam · corrodedQ6 CHECK - LEVEL 2 EXFOLIATION CORROSION ON CREASE BEAM BETWEEN BS 616 TO BS 639, S17R. REPAIRED CREASE BEAM BETWEEN BS 616 TO BS 639, S17R IAW B737 SRM 51-70-13.SDR USAA2012091000029Skin · crackedQ6 CHECK - CRACK IN FUSELAGE SKIN AT BS 800, S19L. REPAIRED FUSELAGE SKIN AT BS 800, S19L IAW B737 SRM 53-00-01-2R-31.SDR USAA2012091000021Tie Clip · crackedQ6 CHECK - CRACK ON STRINGER TIE CLIP AT BS 706, S11L. REPLACED STRINGER TIE CLIP AT BS 706, S11L IAW B737 SRM 51-10-02.SDR USAA2012091000028Skin · crackedQ6 CHECK - CRACK ON FUSELAGE SKIN AT BS 727D+19 INCHES & 0.5 INCHES ABOVE S24L. REPAIRED FUSELAGE SKIN AT BS 727D+19 INCHES & 0.5 INCHES ABOVE S24L IAW B737 SRM 53-00-01-2R-31.SDR USAA2012091000022Tie Clip · crackedQ6 CHECK - CRACK ON STRINGER TIE CLIP AT BS 727B, S10R. REPLACED STRINGER TIE CLIP AT BS 727B, S10R IAW B737 SRM 51-10-02.SDR USAA2012100400007Flap · corrodedQ6 CHECK - PITTING CORROSION ON LEFT INBOARD FLAP AT LEADING EDGE AND OUTBOUND END OF CARRIAGE TORQUE SHAFT. REPLACED LEFT INBOARD FLAP IAW JOB CARD 03C30727030.SDR USAA2012092600032Skin · debondedQ2 CHECK - DEBONDING ON NR 2 SLAT UPPER SKIN TRAILING EDGE WEDGE 8 INCHES FROM INBOARD END. REPLACED NR 2 SLAT IAW JOB CARD 03C30227005.SDR USAA2012091300028Skin · delaminatedQ6 CHECK - DELAMINATION ON LEFT INBOARD AFT FLAP SKIN UPPER & LOWER SURFACE AT BUTT END APPROX 5 INCHES INBOARD OF THE OUTBOARD END EXTENDING TO THE END. REPAIRED LEFT INBOARD AFT FLAP SKIN IAW BOEING DRAWING 65-46434.SDR USAA2012091000027Frame · crackedQ6 CHECK - CRACK ON FUSELAGE FRAME AT BS 500D, S8L. REPAIRED FUSELAGE FRAME AT BS 500D, S8L IAW TYPICAL REPAIR TR737-5310-10-0287.SDR USAA2012091000026Frame · crackedQ6 CHECK - CRACK ON FUSELAGE FRAME AT BS 500A, S8R. REPAIRED FUSELAGE FRAME AT BS 500A, S8R IAW TYPICAL REPAIR TR737-5310-10-0287.SDR USAA2012091000024Frame · crackedQ6 CHECK - CRACK ON FUSELAGE FRAME AT BS 440 BETWEEN S8R TO S9R. REPAIRED FUSELAGE FRAME AT BS 440 BETWEEN S8R TO S9R IAW TYPICAL REPAIR TR737-5310-10-0287.SDR USAA2012092600034Balance Weight · corrodedQ6 CHECK - EXFOLIATON CORROSION ON TUNGSTEN WEIGHT ON RUDDER MID BALLAST AT RS121.64. REPLACED TUNGSTEN WEIGHT ON RUDDER MID BALLAST AT RS121.64 IAW CMM 55-40-12 PAGE 704.SDR USAA2012091300027Skin · delaminatedQ6 CHECK - DELAMINATION ON LEFT OUTBOARD FOREFLAP SKIN UPPER AT TRAILING EDGE SURFACE 12 INCHES OUTBOARD OF INBOARD END. REPAIRED LEFT OUTBOARD FOREFLAP SKIN UPPER AT TRAILING EDGE IAW B737 SRM 51-70-10.SDR USAA2012091000017Tie Clip · crackedQ6 CHECK - CRACK ON STRINGER TIE CLIP AT BS 500C, S11R. REPLACED STRINGER TIE CLIP AT BS 500C, S11R IAW B737 SRM 51-40-02.SDR USAA2012091000016Tie Clip · crackedQ6 CHECK - CRACK ON STRINGER TIE CLIP AT BS 360, S5L. REPLACED STRINGER TIE CLIP AT BS 360, S5L IAW B737 SRM 51-40-02.SDR USAA2012091000015Tie Clip · crackedQ6 CHECK - CRACK ON STRINGER TIE CLIP AT BS 500G, S8R. REPLACED STRINGER TIE CLIP AT BS 500G, S8R IAW B737 SRM 51-40-02.SDR USAA2012091000014Tie Clip · crackedQ6 CHECK - CRACK ON STRINGER TIE CLIP AT BS 380, S8R. REPLACED STRINGER TIE CLIP AT BS 380, S8R IAW B737 SRM 51-40-02.SDR USAA2012091000013Tie Clip · crackedQ6 CHECK - CRACK ON FRAME TIE CLIP AT BS 380, S6R. REPLACED FRAME TIE CLIP AT BS 380, S6R IAW B737 SRM 51-40-02.SDR USAA2012091300026Wedge · delaminatedQ6 CHECK - DELAMINATION ON NR 5 SLAT TRAILING EDGE WEDGE LOWER SURFACE 5 INCHES FORWARD OF LOWER TRAILING EDGE & 7 INCHES FROM OUTBOARD CORNER. REPAIRED NR 5 SLAT TRAILING EDGE WEDGE LOWER SURFACE IAW B737 SRM 51-70-10.SDR USAA2012060700009Light · inoperativeMAINTENANCE REPORTED THE EMERGENCY AISLE LIGHT WAS OUT AT ROW 9A. MAINTENANCE REMOVED AND REPLACED EMERGENCY AISLE LIGHT AT ROW 9A PER AMM 33-51-21-962-001.SDR USAA2012060700007Sign · damagedCREW REPORTED THE EMERGENCY EXIT SIGN AT SEAT 11C NEEDS REPAIR. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN AT SEAT 11C. OPS CHECK GOOD PER AMM 33-51-501-715-001.SDR USAA2012041100002Door · out of rigCREW REPORTED THE MAIN ENTRY DOOR IS DIFFICULT TO CLOSE AND IS NOT AIR TIGHT IN FLIGHT. MAINTENANCE CHECKED AND RIGGED DOOR HANDLE TORQUE PER AMM 52-11-00-755-051 AND CHECKED RIG ON DOOR STOPS PER AMM 52-10-00-501. PRESSURIZED AIRCRAFT TO 6 PSI.SDR USAA2012040300006Nut Clip · not seatedCREW REPORTED THE L1 DOOR WAS VERY DIFFICULT TO CLOSE AND THE DOOR SQUEALS VERY LOUDLY WHEN PRESSURIZED. MAINTENANCE TROUBLESHOT AND FOUND THE L1 DOOR FRAME TRIM PANEL CLIP NUT NOT ENGAGED CORRECTLY CAUSING A RAISED AREA FOR SEAL TO SEAT. RESEATED CLIP NUT ASDR USAA2012031200022Slide · tornDURING FORWARD SERVICE DOOR (R1) ESCAPE SLIDE OPERATIONAL CHECK PER J/C 03L10025002, THE ESCAPE SLIDE INFLATED PROPERLY BUT DEFLATED IMMEDIATELY DUE TO A TEAR IN THE UPPER FORWARD CORNER. MAINTENANCE REMOVED AND REPLACED THE FORWARD SERVICE DOOR (R1) ESCAPE SSDR USAA2012012400006Lens · detachedCREW REPORTED THE EMERGENCY EXIT SIGN LENS OVER COCKPIT DOOR FELL OFF. MAINTENANCE RE-INSTALLED EMERGENCY EXIT LIGHT COVER OVER COCKPIT DOOR.SDR USAA2012011100011Trim Panel · out of adjustMAINTENANCE REPORTED THAT DURING O2 ACTUATION TEST, THE FORWARD FLIGHT ATTENDANT MASK DID NOT DROP. MAINTENANCE FOUND DOOR HANGING ON CEILING PANEL TRIM AT O2 DOOR. ADJUSTED CEILING PANEL TRIM AND FLIGHT ATTENDANT O2 DOOR DROPPED PER ACTUATION TEST.SDR USAA2012011100010Engine · malfunctionedDURING DESCENT, ALL THREE FLIGHT ATTENDANTS REPORTED A "DIRTY SOCKS" SMELL TO BE VERY STRONG IN CABIN. UPON THEIR REQUEST, PASSENGER O2 MASKS WERE DROPPED. FLIGHT ATTENDANTS ALSO WENT ON O2. APU BLEED AIR SWITCH WAS OFF. FLIGHT LANDED AT CLT WITHOUT FURTHESDR USAA2012010600029Retainer · out of adjustCREW REPORTED THAT WHEN THE ESCAPE SLIDE BAR IS STOWED FOR DEPLANING IN THE THE HOLDER ON THE L1 DOOR, BRACKET IS LOOSE, ALLOWING GIRT BAR TO HANG. MAINTENANCE ADJUSTED GIRT BAR RETAINER AS REQUIRED.SDR USAA2012010600026Filter · dirtyON APPROACH, FLIGHT ATTENDANT REPORTED A STRONG SMELL LIKE DIRTY SOCKS IN CABIN, PROGRESSIVELY STRONGER WHEN MOVING FROM AFT OF AIRCRAFT TO FORWARD CABIN. SMELL NOT NOTICEABLE IN COCKPIT. SMELL DISSIPATED/COMPLETED ONCE AIRCRAFT LANDED. MAINTENANCE ACCOMPLISDR USAA2012010300038Gasket · missingFLIGHT ATTENDANT REPORTED A DIRTY SOCK SMELL THROUGHOUT CABIN ON APPROACH TO LANDING. APU WAS OFF AND BOTH PACKS WERE ON. SMELL WAS WORSE FROM MID TO REAR OF CABIN. NO SMELL IN FLIGHT DECK. MAINTENANCE ACCOMPLISHED J/C 03L00021001 - 737 T/S CABIN ODOR. FOSDR USAA2012010300037Wire · brokenCREW REPORTED THE RIGHT SIDE WINDOW HEAT ARCING AT CONNECTION BY TIE WRAP, WITH SMOKE. MAINTENANCE REPAIRED BROKEN WIRING TO CONNECTOR PER WDM 30-41-11, PAGE 5A, SHEET 1. WINDOW HEAT OPERATES NORMALLY. OK FOR SERVICE.SDR USAA2011121600012Acm · faultyFLIGHT ATTENDANT'S REPORTED AN ODOR IN THE MAIN CABIN - MUSTY/DIRTY SOCK SMELL. MAINTENANCE ACCOMPLISHED T/S CABIN ODOR JOBCARD AND FOUND THE RIGHT ACM BAD. REMOVED AND REPLACED RIGHT ACM PER AMM 21-51-11-401. LEAK CHECK GOOD. ACCOMPLISHED DECONTAMINATION PSDR USAA2011120500015Coffeemaker · odorON DESCENT INTO MCO, A VERY STRONG ODOR WAS REPORTED IN CABIN BY FLIGHT ATTENDANT. OCCURRED DURING LAST FIVE MINUTES OF FLIGHT. MAINTENANCE ACCOMPLISHED 737 T/S CABIN ODOR JOB CARD 03L00021001. INSPECTED AND OPS CHECKED ENGINE, APU AND PACKS. REPLACED HEPA SDR USAA2011112900002Window · leakingPASSING 5500 ON DEPARTURE GOT VERY LOUD BUZZING SOUND ON LEFT COCKPIT SIDE EYEBROWS WINDOWS. SO LOUD COULD NOT COMMUNICATE WITH F/O WITHOUT YELLING. COULD NOT COMMUNICATE WITH ATC. REPAIRED BOTH NR 4 AND NR 5 EYEBROW WINDOWS PER EO 5611-01005. ACCOMPLISHEDSDR USAA2011112800026Skin · wornC4 CHECK, THE RIGHT OUTBOARD MIDFLAP LEADING EDGE HAS WORN AND GOUGED AREA 21 INCHES FROM THE INBOARD END AT THE FOREFLAP INBOARD TRACK CUTOUT. REPAIRED THE RIGHT OUTBOARD MIDFLAP LEADING EDGE 21 INCHES FROM THE INBOARD END AT THE FOREFLAP INBOARD TRACK CUTOUSDR USAA2011112500007Skin · crackedC4 CHECK, FORWARD ENTRY DOOR INNER SKIN IS CRACKED 1 INCH FROM THE AFT EDGE AND 20 INCHES FROM THE BOTTOM OF THE DOOR. REPAIRED THE FORWARD ENTRY DOOR INNER SKIN AT 1 INCH FROM THE AFT EDGE AND 20 INCHES FROM THE BOTTOM OF THE DOOR IAW EA 103516.SDR USAA2011112800025Skin · crackedC4 CHECK, CRACKED FUSELAGE SKIN AT BS 380 AND BL 0 AT THE E&E COOILING DUCT OUTLET AREA. REPAIRED FUSELAGE SKIN AT BS 380 AND BL 0 AT THE E&E COOLING DUCT OUTLET AREA IAW EA 201324A.SDR USAA2011112800024Skin · debondedC4 CHECK, THE LEFT INBOARD AFT TRAILING EDGE FLAP UPPER SURFACE HAS AREA OF DISBOND 12.5 INCHES FROM INBOARD EDGE. REPAIRED THE LEFT INBOARD AFT TRAILING EDGE FLAP UPPER SURFACE IAW B737 SRM 51-70-10.SDR USAA2011111800032Window · leakingON CLIMBOUT FROM FLL, EN ROUTE TO CLT, CREW REPORTED AN EXTREMELY LOUD NOISE COMING FROM COCKPIT OVERHEAD WINDOW L5 WHICH DID NOT ALLOW CREW TO COMMUNICATE WITH EACH OTHER. FLIGHT RETURNED TO FIELD AT FLL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WASSDR USAA2011111600006Bypass Valve · faultyAFTER TAKEOFF, FLAPS WOULD NOT RETRACT TO THE UP POSITION WITH THE FLAP LEVER SELECTED IN THE UP POSITION. FLAPS REMAINED AT 5 UNITS. FLIGHT RETURNED TO FIELD AT BOS WITHOUT INCIDENT AND TAXIED TO THE GATE. FLAPS WERE LOWERED TO 15 UNITS ELECTRICALLY FOR LASDR USAA2011103100005Light · brokenCREW REPORTED THE IN-THE-SEAT EXIT LIGHT AT ROW 12, AIRCRAFT LEFT, IS BROKEN. MAINTENANCE SECURED THE EMERGENCY EXIT LIGHT AT ROW 12, AIRCRAFT LEFT. OK FOR SERVICE.SDR USAA2011101100022Shear Tie · corrodedRON CHECK - CORROSION ON FRAME SHEAR TIE AT BS 847 BETWEEN S26R TO S27R. REPAIRED FRAME SHEAR TIE AT BS 847 BETWEEN S26R TO S27R IAW EA 103419.SDR USAA2011101000032Intercostal · corrodedRON CHECK - CORROSION ON INTERCOSTAL BETWEEN BS 928 TO BS 948, S21R. REPLACED INTERCOSTAL BETWEEN BS 928 TO BS 948, S21R IAW BOEING DRAWING 65-45856.
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