Boeing 737-522
Service difficulty reports · 1,682
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 = '737522' 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 = '737522' 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 2006UALA00666Frame · crackedCABIN BS 787 & 867 FRAME CRACKED BETWEEN STR 8L & 9L. REMOVED DAMAGE, FABRICATED AND INSTALLED ANGLE REPAIRS PER MM 53-10-84SDR 2006UALA00665Frame · crackedCABIN BS 400, BS 727B, BS 827, BS 867 AND 907 FRAME CRACKED BETWEEN STRINGER 8R & 9R. REMOVED CRACKS, FABRICATED AND INSTALLED TWO EACH ANGLE DOUBLER PER MM 53-10-84.SDR 2006UALA00664Frame · crackedFRAME CRACKED AT FASTENER AT STATION 400 8L & 9L BS 747 8L & 9L, BS 747 8R & 9R, BS 787 8L & 9L, BS 907 8L & 9L. DAMAGE RMVD, HFEC ACP REF MM53-10-84, NDT MAN PART 6 51-00-00 FIG. 23.SDR 2006UALA00652Frame · crackedFOUND BODY STATION 787 FRAME IS CRACKED BETWEEN STR 8R AND 9R BEHIND PSU RAIL. REMOVED DAMAGE & VERIFIED CRACK CONTAINMENT. FABRICATED & INSTALLED TWO EACH NESTED ANGLES REPAIR REF. MM53-10-84. REPAIR NR 3.SDR 2006UALA00651Skin · dentedRT HORIZ STAB LEADING EDGE DENTED APPROX 5 FT FROM FUSELAGE. DAMAGE REMOVED AND A FLUSH REPAIR WAS INSTALLED PER SRM 55-10-01 REPAIR NR 2.SDR 2006UALA00650Floorbeam · corrodedFOUND FLOORBEAM AT STA 947 CORRODED FROM RBL 29 TO RBL 39. BLENDED CORRODED AREA. ACP NDT FOR CRACKS BLEND OUT OF LIMITS. FABRICATED & INSTALLED NESTED ANGLE REPAIR ON AFT SIDE OF FRAME REF. MM 53-10-95.SDR 2006UALA00642Frame · crackedPASSENGER CABIN STA 827 BETWEEN STR 9L-8L FRAME CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED NESTED ANGLE AND REPAIR PER MM 53-10-84.SDR 2006UALA00641Frame · crackedSTA 400 BETWEEN STR 8R AND 9R FRAME CRACKED AT RIVET JUST BELOW STR 8R CLIP. REMOVED CRACK ACCOMPLISHED NESTED ANGLE AND FILER REPAIR PER MM 53-10-84.SDR 2006UALA00640Frame · crackedBS 400FRAME IS CRACKED AT STR 8L-9L. REMOVED CRACK, FABRICATED AND INSTALLED DOUBLER AND TRIPLER PER MM 53-10-84.SDR 2006UALA00624Lap Joint · damagedLH AFT FUSELAGE BS 921-945 STR 20L SKIN LAP IS DAMAGED. SUPPLEMENTAL DATA UPDATE REMOVED EXISTING REPAIR & PREPARED TO COMPLETE NEW REPAIR PER SRM 53-00-01 REPAIR 31 DETAI L XIII. FOUND 21 HOLES OVERSIZED PAST SRM LIMITS. REMOVED STR 20L SECTION & SPLICED IN NSDR 2006UALA00933Connector · burnedLEFT AFT BOOST PUMP CONNECTOR BURNED TO PUMP ASSEMBLY. THE LEAKAGE OBSERVED WAS VERIFIED AND CAUSED BY A LOCALIZED OVERHEATING OF THE CONNECTOR PINS THAT RESULTED IN DAMAGE TO THE SEAL AROUND PIN 2. THE CAUSE FOR THE EXCESSIVE OVERHEATING IN THE CONNECTOR SDR 2006UALA00622Bushing · damagedFOUND VERTICAL STAB LT PRIMARY FWD LUG BUSHING SPUN WHILE MACHINING. DAMAGE REMOVED AND A NEW REPAIR BUSHING WAS INSTALLED PER AAR EA I060151. RESULTING BORE SIZE WAS 1.6048 IN.SDR 2006UALA00620Frame · crackedFOUND CABIN BODY FRAME WEB IS CRACKED AT STRINGER CUT OUT BS 727 STR 14R. TRIMED OUT DAMAGE FABRICATED DOUBLER AND FILLER AND INSTALLED THE REPAIR PER AAR EAI060128 AND UNITED EVA-60171.SDR 2006UALA00613Frame · crackedFOUND FUSELAGE FRAME AT STA 440 CRACKED BETWEEN STR 8R AND 9R CRACK RADIATING FROM INBD RIVET OF FRAME. DAMAGE & CHECK FOR CRACK CONTAINMENT WITH NDT. FABRICATED & INSTALLED NESTED ANGLE DOUBLER REPAIR REF MM53-10-84. RPR 3.SDR 2006UALA00612Frame · crackedFOUND FUSELAGE FRAME AT STA 440 CRACKED BETWEEN STR 8L AND 9L PSU RAIL ATTACH BRACKET. REMOVED DAMAGE & CHECK FOR CRACK CONTAINMENT USING NDT. FABRICATED & INSTALLED NESTED ANGLE DOUBLER REPAIR REF MM53-10-84 RPR NR 3.SDR 2006UALA00611Frame · crackedFRAME STA 927 IS CRACKED BETWEEN STR 8L AND 9L AT THE INBD RIVET OF THE PSU RAIL SUPPORT BRACKET. REMOVED DAMAGE & CHECK FOR CRACK CONTAINMENT USING NDT. FABRICATED & INSTALLED NESTED ANGLE DOUBLER REPAIRS REF SRM 53-00-07-201.SDR 2006UALA00610Frame · crackedBS 727 BULKHEAD FRAME WAS FOUND CRACKED AT THE STR 15L CUT-OUT EMANATING UPWARD FROM THE STRINGER CUT-OUT. REMOVED DAMAGE & VERIFIED CRACK CONTAINMENT WITH NDT. FABRICATED & INSTALLED NESTED ANGLE REPAIR & STRUCTURAL FILLERS REF. AAR ENGINEERING AUTHORIZATIONSDR 2006UALA00606Intercostal · crackedCRACKS WERE FOUND IN THE INTERCOSTAL BETWEEN FRAME STATIONS 294.5 & 303 NEAR STRINGERS 7L, 11L & 16L. *S/D* REPLACEMENT INTERCOSTAL WEBS INSTALLED PER AAR EA'S-I060133, I060124, I060121 & UA EVA-60168.SDR 2006UALA00607Intercostal · crackedFOUND FWD CABIN BS 303 INTERCOSTAL ANGLE IS CRACKED AT STR 11R. MAJOR REPAIR ACP'D, INST'D TEE CHORD REPAIR PER BACO DRAWING 65-17684 & AAR EA-I060138 ON NR11079-2000-0047.SDR 2006UALA00605Web · crackedFOUND CABIN STR 7L WEB CRACKED STA 294.5 IN RADIUS, AFT SIDE OF FRAME. MAJOR REPAIR ACP'D, INSTALLED REPLACEMENT INTERCOSTAL PER AAR EA-I060121 & UA EVA-60168.SDR 2006UALA00584Door Frame · crackedFWD CARGO DOOR CUTOUT SURROUND AFT FRAME STA 452.4 HAS CRACK IN WEB AT UPPER IB CORNER OF LOWER STOP STR 24R. REMOVED AND REPLACED FRAME REF SRM 51-40-02 AND BACO DWG 65-20723.SDR 2006UALA00575Shear Tie · crackedA 1 INCH CRACK WAS FOUND IN THE FWD RADIUS OF THE SHEAR TIE TO INTERCOSTAL STR 11L AT BS 294.5. REMOVED & REPLACED CRACKED SHEAR TIE - REF UAL EVA UA-EVA-60168.SDR 2006UALA00578Stringer Clip · crackedSTATION 360 STR 8R STRINGER CLIP CRACKED. REMOVED & REPLACED STR CLI P REF SRM 51-40-02.SDR 2006UALA00577Stringer · crackedFUSELAGE UPPER LOBE STA 907 STRINGER 4L IS CRACKED AT FASTENER. REMOVED & REPLACED DAMAGED STRINGER SPLICE REF SRM 51-40-02.SDR 2006UALA00576Shear Tie · crackedCABIN INTERCOSTAL AND SHEAR TIE CRACKED AT BS 294.5 NEAR STRINGERS 7L, 11L, 16L. INSTALLED NEW INTERCOSTAL WEB PER UAL EVA-60172.SDR 2006UALA00561Attach Angle · corrodedVERTICAL STAB LEF ATTACH AT AFT SPAR FWD & AFT DRAG ANGLES ARE CORRODED AT PRIMARY (O/B) BOLT HOLES. VERTICAL STAB L-H AFT SPAR FWD AND AFT DRAGE ANGLE CORROSION WAS REPAIRED PER AAR EO I060139.SDR 2006UALA00560Intercostal · crackedFUSELAGE STA 277 STRINGER 14R INTERCOSTAL CRACKED. REMOVED & REPLACED INTERCOSTAL REF SRM 51-40-02.SDR 2006UALA00567Line · leakingRETURNED TO YYZ AND CANCELLED DUE TO SMOKE IN THE CABIN. UNITED DISCOVERED THE INTERNAL BOOSTER SPOOL CAVITY SURFACES BADLY BATTERED FROM WHAT APPEARS TO BE LIBERATED BOLT HEADS COMING OFF AFT BLADE RETAINER FASTENERS AND PUNCTURING 1-2 BEARING SUPPORT OIL TUSDR 2006UALA00559Shear Web · corrodedUPPER FUSELAGE AT STA 727C & STRINGER 17L AT RBL 65 SHEAR WEB AT FLOOR LEVEL CORRODED. REMOVED CORROSION & FOUND BLEND OUT OF LIMITS. REMOVED & REPLACED SHEAR WEB REF SRM 51-40-02.SDR 2006UALA00558Frame · crackedCABIN BODY FRAME WEB IS CRACKED AT 1 EACH STRINGER CUTOUTS BS 663 STR 3L. REMOVED DAMAGE, MANUFACTURED REPAIR ANGLE FILLERS AND STRINGER SPLICE AND INSTALLED REF SRM 53-00-07.SDR 2006UALA00550Stringer Clip · crackedSTATION 380 STRINGER 15R STRINGER CLIP IS CRACKED. SUPPLEMENTAL DATA UPDATE REMOVED DAMAGED STRINGER CLIP. FABRICATED & INSTALLED NEW STRINGER CLIP REF SRM 51-40-02.SDR 2006UALA00549Frame · crackedCABIN UPPER LOBE FRAME STA 927 IS CRACKED BETWEEN STRINGERS 8L & 9L. *S/D* REMOVED DAMAGE & ACP NDT FOR CRACKS. FABRICATED & INSTALLED NESTED ANGLE REPAIR REF SRM 53-00-07 & AMM 53-11-99 REPAIR IX.SDR 2006UALA00548Sill · crackedAFT PIT DOOR CUTOUT, LWR SILL BEAM UPPER FLANGE CRACKED BS 818 RBL 19" WL 159. INSTALLED DOUBLER REPAIR PER SRM 51-70-11 AND MM 51-21-21.SDR 2006UALA00547Attach Fitting · corrodedVERTICAL STAB RIGHT AFT FUSE ATTACH FITTING OUTBOARD CLEVIS AFT LUG HAS CORROSION IN BORE & ON FWD & AFT FACES. VERTICAL STAB RIGHT AFT FUSE ATTACH FITTING OUTBOARD CLEVIS AFT LUG WAS REPAIRED PER AAR EA I060130. CORROSION WAS REMOVED AND NEW BUSHINGS FABRICSDR 2006UALA00546Stringer Clip · crackedCABIN FRAME STA 277, STR 15R ATTACH CLIP IS CRACKED. INSTALLED REPLACEMENT STR CLIP REF SRM 51-40-02 AND DWG 69-32411.SDR 2006UALA00545Skin · dentedAFT CARGO DOOR OUTER SKIN HAS A DENT 10 INCHES FROM TOP EDGE, 9.5 INCHES FROM FWD EDGE. MAJOR REPAIR ACP'D, INSTALLED ENTIRE EXTERNAL SKIN RE-SKIN REPAIR PER SRM 52-30-01 FIG 201.SDR 2006UALA00520Skin · dentedFUSELAGE SKIN SCRATCHED AND DENTED FROM BS 807-947 BETWEEN STR 25R - 26R. *S/D* INSTALLED DOUBLER TRIPLER REPAIR PER SRM 53-00-01 DETAIL XII.SDR 2006UALA00519Attach Angle · crackedLEFT CABIN STA 294.5 AT STR 11, INTERCOSTAL FRAME ATTACH ANGLE IS CRACKED. *S/D* VERIFIED MATERIAL USED, VERIFIED HEAT TREATMENT TO T6, FABRICATED PART, TREATED & PRIMED AND INSTALLED PART REF SRM 51-40-02, SRM 51-40-03, & EA I060119.SDR CA060321002Brake · failed(CAN) UPON LANDING ( MONCTON ) WITH THE ANTI-SKID SYSTEM OPERATING UNDER MEL 32-2 (ANTI-SKID SYSTEM INOP), THE AC LANDED ON A BARE RUNWAY AND BLEW 3 MAIN WHEEL TIRES AND BADLY SCUFFED THE FOURTH. ALL FOUR MAIN TIRES REPLACED. AIRCRAFT FERRIED. UPON FURTHER INSDR 2006UALA00518Frame · damagedAFT PIT RIGHT FRAME NEEDS TO BE REPLACED. REMOVED AND REPLACED THE FRAME REF SRM 51-40-02.SDR 2006UALA00517Skin · dentedTHE UPPER FUSELAGE IS DENTED AT STA 1006 BETWEEN STR 14L & 15L. *S/D* REMOVED DAMAGE FROM SKIN & STRINGER. FABRICATED & INSTALLED REPAIR DOUBLER & STRUCTURAL FILLER TO SKIN & U-CHANNEL REPAIR TO STRINGER 14L. REF AAR ENGINEERING AUTHORIZATION I060113 REV ISDR 2006UALA00516Frame · crackedBS 727 BULKHEAD FRAME WAS FOUND CRACKED AT S14R CUTOUT, THE CRACK WAS IN THE TEE CHORD ONLY. FABRICATED AND INSTALLED ANGLE, 2 EACH FILLERS NEW STRINGER CLIP AND RADIUS FILLER PER AAR I060112 AND REF SB 737-53-1181 AND UAL-EVA-60151.SDR 2006UALA00514Skin · gougedLT HORIZ STAB LEADING EDGE 70" FROM THE I/B END IS DENTED WITH A GOUGE. DAMAGE WAS REMOVED AND LEADING EDGE REPAIRED PER MM 27-41-21, SRM 55-10-01, GNMM 5-0-4-011, SRM 51-70-01, 55-70-01 AND MM 51-31-00.SDR 2006UALA00513Skin · damagedRUDDER MR55225-133 LT SKIN 11.75 INCHES FROM T/E & 113.5 INCHES FROM BOTTOM SKIN HAS AREA APPROX 0.250 LONG DAMAGE DOWN TO TOP OF THIRD PLY. LT SPAR CAP FLANGE & RT EXTERNAL NOSE SKIN RUDDER STATION 3.0 ALSO DAMAGED. RUDDER SKIN, LH SPAR CAP FLANGE AND RT ESDR 2006UALA00508Frame · crackedCABIN UPPER LOBE, FRAME AT STA 827, IS CRACKED BETWEEN STR 8L AND STR 9L. REMOVED DAMAGED AREA. NDT CUT OUT AREA, FABRICATED AND INSTALLED REPAIR ANGLES REF MM 53-10-84.SDR 2006UALA00507Frame · crackedCABIN STA 440, FRAME IS CRACKED AT PSU RAIL ATTACH FASTENER, BETWEEN STR 8L & 9L. REMOVED DAMAGE FROM FRAME, NDT NO DEFECT NOTED, INSTALLED REPAIR, REF B737 MM 53-10-84.SDR 2006UALA00506Frame · crackedCABIN FRAME CRACKED AT STA 400 BETWEEN STR 8R & 9R AT PSU FRAME RAIL ATTACH. MAJOR REPAIR ACP'D, INSTALLED REPAIR ANGLE DOUBLERS PER MM 53-10-84 FIG 803.SDR 2006UALA00505Repair · gougedFWD CARGO PIT CUTOUT UPPER FRAME REPAIR DOUBLER HAS A GOUGE. REMOVED OLD REPAIR, CUT OUT DAMAGE AREA, FABRICATED NEW DOUBLER, TRIPLER, FILLER & INSTALLED REPAIR. REF SRM 53-00-01 REPAIR 32.SDR 2006UALA00504Skin · gougedLOWER RIGHT FUSELAGE, APPROX STA 209, AT STRINGER 18, JUST ABOVE AFT PIT DOOR HAS A DEEP GOUGE. CUT OUT DAMAGE REF 53 -00-01 MFG DOUBLER SRM 53-00-01 DETAIL III REPAIR 32.SDR 2006UALA00501Frame · crackedCABIN UPPER LOBE, STA 787 FRAME IS CRACKED BETWEEN STR 8L & STR 9L. REMOVED DAMAGE, NDT NO DEFECTS NOTED. INSTALLED REPAIR REF B737 MM 53-10-84.
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