Boeing 737-322
Service difficulty reports · 4,751
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 = '737322' 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 = '737322' 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 2006UALA00687Skin · damagedUPPER FUSELAGE STA 727D + 10, STR 1 HAS ONE EACH EXTRA HOLE AS MARKED. FABRICATED REPAIR ANGLES, INSTALLED REPAIR ANGLES, ALODINED, PRIMED AND PAINTED PER SRM 53-00-03 FIG201.SDR 2006UALA00686Skin · damagedUPPER FUSELAGE STA 727D + 10, STR 2R HAS ONE EACH EXTRA FASTENER HOLE AS MARKED. FABRICATED REPAIR ANGLES, INSTALLED REPAIR ANGLES, ALODINED, PRIMED AND PAINTED PER SRM 53-00-03 FIG201.SDR 2006UALA00685Skin · damagedUPPER FUSELAGE STA 727B STR 1 HAS ONE EACH EXTRA HOLE AS MARKED. FABRICATED REPAIR ANGLES, INSTALLED REPAIR, ALODINED, PRIMED AND PAINTED PER SRM 53-00-03 FIG 201SDR 2006UALA00682Stiffener · crackedFOUND STIFFENERS AT RBL 6.15 CRACKED ON THE WING REAR SPAR CENTER SECTION APPROX 17 INCHES UP FROM LOWER END OF LT & RT STIFFENER. STIFFENERS AT LBL & RBL REPLACED PER SB 737-57A1269. THIS IS TERMINATING ACTION FOR AD 2005-20-01.SDR 2006UALA00672Light · inoperativeEEL LIGHTS OUT FROM ROW 15A BACK.SDR 2006UALA00671Light · inoperativeALL EEL LIGHTS AFT OF ROW 15 INOPERATIVE.SDR 2006UALA00660Stringer Clip · crackedDURING BELLY SKIN REPLACEMENT 4 EA STRINGER CLIPS WERE FOUND CRACKED AT STA 787 STR 21R, STA 787 STR 22R, STA 867 STR 20R & STA 887 STR 20R. REPLACED STRINGER CLIPS REF SRM 51-40-02.SDR 2006UALA00659Skin · crackedFWD GALLEY DOOR LOWER AFT CORNER SKIN CRACKED. DAMAGE RMVD FROM SKIN, BONDED DOUBLER AND BEAR STRAP PER EVA UA 60210 AND EA I060175.SDR 2006UALA00655Skin · crackedFOUND STA 296.5 STR 10L UPPER FLANGE CUTOUTS CRACKED. REMOVED CRACK, INSTALLED STRAP INSTALLED STRINGER CLIP PER AAR EA I060145 AND UAL UA-EVA-60211.SDR 2006UALA00644Crease Beam · corrodedCREASE BEAM AT FWD GALLEY DOOR CORRODED STA 339 TO 374 RBL 59. REMOVED & REPLACED CREASE BEAM REF SRM 51-40-02.SDR 2006UALA00657Frame · crackedROUND OVERWING FRAME STA 616 RT SIDE IS CRACKED. INSTALLED STIFFENING ANGLE PER MM53-11-89.SDR 2006UALA00656Skin · crackedFOUND HORIZONTAL STAB LOWER SURFACE AFT SPAR SKIN CRACKED AT THIRD BAY FROM I-B END. REMOVED DAMAGE AND ACP NDT FOR CRACKS. FABRICATED AND INSTALLED REPAIR DOUBLER WITH TWO EACH CUT-OUT ACCESS HOLES REF SRM 55-10-01.SDR 2006UALA00654Bulkhead · damagedFOUND LT AC BAY OB SIDE OF DOOR CUTOUT 22" FROM AFT END. BULKHEAD WEB DAMAGED FROM CONTACT WITH DOOR LATCH. DAMAGE AREA TRIMMED OUT REF MM51-20-01 & EA I060153.SDR 2006UALA00653Web · damagedFOUND FWD GALLEY DOOR FLOOR WEB AT STA 328 HAS ELONGATED HOLES. REMOVED DAMAGED WEB, FABRICATED NEW WEB AND INSTALLED REF SRM 51-40-02.SDR 2006UALA00648Wire Harness · damagedNR 2 ENG WINDMILLED IN FLIGHT AT 0 PSI OIL PRESS FOR APPROXIMATELY 7 MINUTES. ENG SHUT DOWN DUE TO SUSPECTED FUEL LEAK. ACCOMPLISHED ENGINE WINDMILLING INSPECTION REF JRH2-95-63. ACCOMPLISHED ENGINE IDLE RUN AND LEAK CHECK NO LEAKS NOTED. CHECKED CHIP DETECTOSDR 2006UALA00645Frame · crackedLT WW BS 695 FRAME AT STR 18A IS CRACKED IN THE RADIUS. REPLACED ANGLE PER SRM51-4 0-02.SDR 2006UALA00643Skin · dentedRAMP REPORTED NUMEROUS DENTS IN THE OUTSIDE OF THE AFT CARGO PIT DOOR. DOOR HAS BEEN RESTORED TO SERVICEABLE CONDITION BY REPLACING DOOR SKIN AT HMV VISIT. NO FURTHER FINDINGS, O.K. FOR SERVICE.SDR 2006UALA00630Web · crackedSTRINGER 7L ATTACH WEB AT STA 294.5 IS CRACKED AT INBD CORNER. REPLACED WEB PER SRM51-40- 02.SDR 2006UALA00629Clip · crackedSTA 294.5 AFT SIDE OF FRAME INTERCOSTAL CLIP IS CRACKED IN RADIUS AT STR 11L. REPLACED CLIP WITH A NEW CLIP FABRICATED REF AAR ENGINEERING AUTHORIZATION I 060154 & UA EVA 60197.SDR 2006UALA00628Clip · crackedSTA 360 FWD SIDE OF FRAME INTERCOSTAL CLIP AT STR 11L WAS FOUND CRACKED. REPLACED CLIP WITH NEW ONE SUPPLIED BY BOEING REF. AAR ENGINEERING EA I060152 & UA EVA 60197.SDR 2006UALA00626Frame · crackedFWD GALLEY DOOR AFT FRAME IS CRACKED AT 4TH FRAME TOP STOP FITTING CUTOUT. REMOVED DAMAE, FABRICATED AND INSTALLED DOUBLER REPAIR PER SM-90-52-40-14-JD. NO OTHER FINDINGS, O.K. FOR SERVICE.SDR 2006UALA00625Skin · dentedAFT CARGO DOOR EXT. SKIN HAS 3 EACH DENTS APROX.14" TO AFT 24"LWR, 18"TO AFT, 24"TO TOP, 16"TO FWD, 12" TO TOP EDGE. 3 EA. DENTS ON AFT CARGO DOOR OUT OF ALLOWABLE LIMITS. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIRS PER SRM 52-30-01 AND SRM 51-40-02. NO OTSDR 2006UALA00636Window · crackedR2 WINDOW CRACKED DUE TO ARCING. NR 2 RT SLIDING WINDOW CRACKED DUE TO ARCING. REMOVED AND REPLACED WITH SERVICEABLE WINDOW. THIS WINDOW WAS INSTALLED ON A/C 2 YEARS AGO. NO FURTHER FINDINGS, OK FOR SERVICE.SDR 2006UALA00634Light · inoperativeAFT CABIN EEL LIGHTS INOP FROM ROW 15 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT.SDR 2006UALA00596Wire · damagedEEL LIGHTS INOP FROM ROW 15 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT.SDR 2006UALA00595Power Supply · inoperativeEMERGENCY EXIT SIGNS ABOVE LT OVERWING HATCH AND LOWER FWD CORNER OF LT OVERWING HATCH INOP.SDR 2006UALA00594Power Supply · inoperativeFOUND EEL LIGHTS FROM ROW 3-9 INOP.SDR 2006UALA00563Skin · dentedACFT DENTED 11 INCHES FWD OF RADAR COMPT DOOR IN 2 AREAS, 5 X 1.25 X .187 INCH & 7 X 9 X .25 INCH. DENTS IN PRESSURIZED AREA AND ON A BUTT JOINT. REMOVED DAMAGE. MANUFACTURED REPAIR DOUBLERS, TEAR STRAP, AND FILLER PER EVA.SDR 2006UALA00562Stringer · crackedAFT PIT STA 800 STRINGER 22L IS CRACKED. STOP DRILLED CRACK & CHECK FOR CONTAINMENT USING NDT. FABRICATED & INSTALLED NESTED ANGLE REPAIR REF SRM 53-00-53 REPAIR 2.SDR 2006UALA00552Frame · crackedCABIN FRAME INBOARD CHORD CRACKED BS 616 RBL 64", WL 201. INSTALLED REPAIR ANGLE DOUBLER PER MM 53-11-89.SDR 2006UALA00551Frame · crackedCABIN FRAME BS 616 INBOARD CHORD IS CRACKED LBL 64", WL 201. INSTALLED REPAIR ANGLE DOUBLER PER MM 53-11-89.SDR 2006UALA00524Warning Light · illuminatedFLAP DISAGREE ILLUMINATED ON APPROACH. ON APPROACH, THE FLAP DISAGREE LIGHT ILLUMUNATED. THE TRAILING EDGE FLAP POSITION INDICATOR SHOWED RIGHT FLAP AT 2, LEFT FLAP BETWEEN 2-5. AFTER LANDING, THE TRAILING EDGE FLAP POSITION INDICATOR (MR27583) WAS REPLACEDSDR 2006UALA00540Skin · dentedFUSELAGE DENT IS A CRACK 3 - 8 INCHES IN CENTER OF DENT. *S/D* RE-CHECKED DENT WITH HFEC. NO CRACKS FOUND. ACP HFEC INSPECTION EVERY A CHK UNTIL PERMANENT REPAIR INSTALLED NO LATER THEN 05NOV06. ENSURE THAT THERE ARE NO LOOSE FASTENERS IN & ADJACENT TO THSDR 2006UALA00523Trim System · failedELEVATOR TRIM FAILED. THE MANUAL HORIZONTAL STABILIZER TRIM SYSTEM WAS INNOPERATIVE DUE A BROKEN LINK IN THE STABILIZER TRIM MECHANISM CHAIN ASSEMBLY. THIS ALLOWED THE CHAIN TO COME APPART AND PREVENT CREW MANUAL INPUTS FROM THE FLIGHT DECK. THE CHAIN ASSEMSDR 2006UALA00511Light · inoperativeAFT CABIN EEL LIGHTS INOP FROM ROW 15 AFT TO AND INCLUDING AFT EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT.SDR 2006UALA00502Indication Sys · malfunctionedON APPROACH NOSE GEAR RED LIGHT ON AND MAINS GREEN, GEAR HANDLE DOWN. M983,NOSE GEAR RED LIGHT & TO. WARNING CIRCUIT CCARD FAILED. REPLACED CARD PER MM 32-09-20 PGS 410- 411. PERFORMED NOSE GEAR SAFETY SENSOR ADJ TEST PER MM 32-09-02. .501. NOSE GEAR EXTENSIOSDR 2006UALA00494Warning Light · illuminatedFLIGHT HAD UNSAFE GEAR INDICATION WITH NO GEAR LIGHTS AND ONE RED NOSE GEAR LIGHT ON. FOUND THE P6-3 C18 FOR THE AIR-GROUND RELAY AND LIGHTS IN ADDITION TO AURAL WARNING BREAKER P6-3 D18 TRIPPED.RESET BREAKERS AND NO FURTHER INCIDENT REPORTED.SDR 2006UALA00473Skin · damagedDAMAGE TO AREA BELOW FWD LAV SERVICE POINT. REMOVED FASTENERS AND PREPARED AREA FOR SHEET METAL REPAIR. MANUFACTURED FILLER, DOUBLER AND TRIPLER AND LOCATED HOLES REF SRM 53-10-01 REPAIR 11. PRIMERED, SEALED & STARTED INSTALLATION, REF SRM 53-10-01 (DETAILSDR 2006UALA00451Skin · dentedLH HORIZONTAL STAB UPPER SKIN DENTED 6 FEET FROM INBD. NEW REPAIR SKIN SPLICED IN PER AAR EA 1060102.SDR 2006UALA00447Floorbeam · crackedCABIN LONGITUDINAL FLOOR SUPPORT AT LBL45.5 WAS FOUND CRACKED AT THE OUTBOARD FLANGE FASTENER HOLE OF THE UPPER CHORD WHERE THE ASSY IS ATTACHED TO THE BS 727B FLOORBEAM. REMOVED DAMAGED AREA. ACP NDT FOR CRACKS. FABRICATED & INSTALLED TWO STRAPS, FILLER & SSDR 2006UALA00446Stringer · crackedCABIN BS 296 S10L IS CRACKED AT UPPER FLANGE. REMOVED DAMAGE, MANUFACTURED AND INSTALLED STRINGER REPAIR, STRINGER CLIP AND INTERCOSTAL.SDR 2006UALA00432Bushing · migratedLT HORIZ STAB FWD SPAR UPPER LUG FWD & AFT BUSHINGS MIGRATED. REMOVED BUSHINGS, FOUIND CORROSION, REMOVED CORROSION, FABRICATED ADN INSTALLED NEW BUSHINGS PER BOEING DRAWINGS 65-72039-29, 30, AND 31. WORK ACCOMPLISHED PER AAR EA I060104 AND SUPPORTED WITH 810SDR 2006UALA00445Skin · damagedRUDDER AT NR 4 HINGE CUTOUT RIGHT UPPER EDGE DAMAGED. DAMAGE TO RUDDER AT NR 4 HINGE CUTOUT WAS REPAIR PER AAR EO I060062.SDR 2006UALA00402Cable · faultyEEL LIGHTS INOP AFT OF ROW 15. REPLACED RIBBON CABLE.SDR 2006UALA00401Battery · inoperativeFOLLOWING EEL INOP, ROW 10-15, ROW 10, 11, 15, 17, EXIT MARKER DOOR 2L, RIGHT OVERWING EXTERIOR LIGHT.SDR 2006UALA00399Skin · puncturedNR 1 KRUGER FLAP DAMAGED, PUNCTURED APPROXIMATELY 1.2 BY 100 PERCENT THRU. PERMANENT REPAIR DOUBLER WAS INSTALLED PER AAR EA I060103 SUPPORTED WITH 8100-9 FORM.SDR 2006UALA00394Skin · erodedAFT UPPER EXTERNAL FUSELAGE BS 860 TO 887 BTWN STR 2L & 2R DORSAL FIN FWD FRG. PHENOLIC WEAR STRIP UNDER BLADE SEAL IS ERRODED TO THE EDGE OF BLADE IN SEVERAL SPOTS, BLADE SEAL SHOULD BE CENTERED ON WEAR STRIP. REMOVED DAMAGE AND INSTALLED A DOUBLER, TRIPLERSDR 2006UALA00382Stiffener · crackedMAIN WHEEL WELL FWD BULKHEAD STIFFENER IS CRACKED WL 170 LBL 6.5. STIFFENER WAS REMOVED AND REPLACED AT MAIN WHEEL WELL STA. 663, LBL 6.15 PER MM57-12-96 PAGE 401 REPAIR 2. PER ADVANCE MM 57-12-96 PAGE 404 ITEM 6. B. CREATED A CF ITEM TO REPLACE BOTH STIFFENERSDR 2006UALA00403Slide · no testDURING DEPLOYMENT OF FWD GALLEY DOOR SLIDE, SLIDE TWISTED AND DEPLOYED VERTICALLY AT DOOR THRESHOLD AREA.SDR 2006UALA00566Wire · inoperativeFLOOR EEL LIGHTS ARE INOP FROM ROW 15 TO THE AFT GALLEY.
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