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 2006UALA02194Floorbeam · damagedFLOORBEAM AT BS 294.5 HAS TOOLING DAMAGE & GOUGES RBL 29-52 AT WL 208. MAJOR REPAIR: FABRICATED AND INSTALLED ENSTED ANGLE AND STRAP REPAIR. REFERENCE MM 53-10-95 REPAIR NR 8.SDR 2006UALA02193Skin · crackedRT HORIZ STAB HAS LOWER EXTERNAL SKIN CRACK AT REAR SPAR, 68" OB OF IB END. MAJOR REPAIR: INSTALLED ACCESS HOLE DOUBLER REPAIR PER SRM 55-10-01 REPAIR 6. INSTALLED LOWER SKIN DOUBLER PER MM 55-10-94 PG 801.SDR 2006UALA02192Frame · crackedBS 695 FRAME CRACKED IN LOWER RADIUS ABOVE & AFT OF LT MLG UPLOCK MECHANISM IN LT MLG WW. MAJOR REPAIR: REMOVED AND REPLACED ANGLE. REFERENCE SRM 51-40-02 AND MM 53-10-98.SDR AMTA200600669Post · corrodedAFT LAV POST HAS CORROSION AT LWR END. REPLACED AFT LAV FWD POST IAW EA, STA 1000, LBL 12. (K)SDR 2006UALA02182Skin · damagedRH HORZ STAB LOWER SPAR SKIN BETWEEN STA. 207.7 AND 234.5 IS DAMAGED. MAJOR REPAIR: REMOVED DAMAGE. REPAIRED PER BOEING MESSAGE 1-243907360-3.SDR 2006UALA02189Wire Harness · chafedWIRE RUN STAND OFF MELTED AT SEAT ROW 1A, LOCATED ABOVE CABIN WINDOW STRUCTURE STA 370. LOCATION IS THE CAUSE CHAFING OF WIRE HARNESS. COA 93020 HAS BEEN DEVELOPED TO REROUTE THE HARNESS PERMANENTLY TO PREVENT SIMILAR CHAFING FROM OCCURING.SDR 2006UALA02171Stiffener · crackedRH MLG WW FWD BULKHEAD VERTICAL "Z" ANGLE STIFFENER AT RBL 7 CRACKED HORIZONTALLY APPROX. 30" FROM WHEEL WELL. MAJOR REPAIR: FABRICATED AND INSTALLED U CHANNEL AND STRAP REPAIR. REFERENCE MM 57-12-96 REPAIR NR 3.SDR 2006UALA02169Frame · crackedFWD CARGO DOOR CUT-OUT AFT FRAME HAS 3 EACH CRACKS AT BS 492 NEAR STR S24R. MAJOR REPAIR: TRIMMED OUT DAMAGE. FABRICATED AND INSTALLED NESTED ANGLE REPAIR. REFERENCE AAR EA I060503 AND UA-EVA-60687.SDR 2006UALA02168Web · wornKEELBEAM VERTICAL WEB AT BS 583 & LBL 6 HAS WEAR DAMAGE APPROX 4" FROM UPPER CHORD ACCESS FROM LT A/C BAY. MAJOR REPAIR: REMOVED DAMAGE. ACCOMPLISHED NDT AND PROVIDED INSURANCE CUT. FABRICATED AND INSTALLED EXTERNAL DOUBLER REPAIR.SDR AMTA200600655Floor Panel · corrodedAFT CARGO FLOOR PANEL 1538X HAS CORROSION ALONG EDGE OF PART AS MARKED F/S 946 TO 948, LBL 22 TO RBL 22, UPPER SURFACE. BLENDED AREA, MATERIAL THICKNESS 080, MAX MATERIAL LOSS IS 003 WITHIN LIMITS IAW SRM, FIG 101. TREATED AND PRIMED ARA IAW SRM. (K)SDR AMTA200600654Strap · corrodedAFT CARGO RT SIDE NR 2 FLOOR STRAP IS CORRODED THROUGHOUT F/S 727D TO 767, RBL 22. REMOVED CORROSION FROM RT NR 2 FLOOR STRAP IN AFT CARGO FROM F/S 727D TO 767, RL 22 IAW B737-300, MM 51-21-31. ORIGINAL THICKNESS IS 071, MATERIAL LOSS IS 016. MAX ALLOWABLE SDR AMTA200600653Floor Panel · corrodedFWD CARGO BAY, THE FWD PORTION OF THE LT TRAP FOR THE FLOOR PANEL IS CORRODED. F/S 472-500, LBL 22. REMOVED CORROSION IAW 53-30-53, ORIGINAL THICKNESS IS 063, REMAINING MATERIAL THICKNESS IS .060 AND FOUND TO BE WITHIN LIMITS IAW SRM 53-30-53, FIG 101. (K)SDR AMTA200600652Strap · corrodedAFT CARGO BAY, LT NR 2 FLOOR STRAP IS CORRODED ON LOWER SIDE THROUGHOUT ITS LENGTH. F/S 727D TO 767 LBL 22. REMOVED CORROSION ON AFT CARGO BAY LT NR 2 FLOOR STRAP F/S 727D TO 767, LBL22 IAW MM. ORIGINAL THICKNESS IS 071, MATERIAL LOSS 014, MAX ALLOWABLE LOSSDR AMTA200600651Strap · corrodedAFT CARGO BAY, LT NR 3 FLOOR STRAP IS CORRODED AS MARKED. F/S 814, LBL 22 (UNDERSIDE). REMOVED CORROSION ON AFT CARGO BAY LT NR 3 FLOOR STRAP F/S 814, LBL 22, IAW MM 51-21-31. ORIGINAL MATERIAL THICKNESS IS 071, MATERIAL LOSS IS .004 AREA FOUND TO BE WITHISDR AMTA200600650Seat Track · corrodedCORROSION ON SEAT TRACK IN AFT GALLEY FLOOR BETWEEN COMP 411 ON TOP OF LUGS AND INSIDE TRACK STA 986 TO STA 1016, RBL 16. REMOVED CORROSION .006 MATERIAL LOSS WITHIN LIMITS IAW SRM. TREATED PRIMED AREAS IAW SRM. (K)SDR AMTA200600649Strap · corrodedAFT CARGO COMP BETWEEN STA 772, WL 155.5 AND BL 13R STRAP CORROSION. REMOVED CORROSION ORIGINAL MATERIAL THICKNESS 063, MATERIAL LOSS 005, WITHIN LIMITS IAW SRM. TREATED AND PRIMED AREA.SDR AMTA200600648Floor Panel · corrodedAFT CARGO FLOOR PANEL 1534X HAS CORROSION AROUND FASTENER HOLES ON FORWARD F/S 727 TO 732, LBL 20 TO RBL 20 ON ITS UPPER SURFACE. BLENDED AREA AT AFT CARGO FLOOR PANEL 1534X AROUND FASTENER HOLES ON FORWARD END UPPER SURFACE. ORIGINAL THICKNESS IS 080, BLENDSDR AMTA200600647Floor Panel · corrodedAFT CARGO FLOOR PANEL 1535X HAS CORROSION ON EDGES OF THE UPPER SURFACE AS MARKED. REMOVED CORROSION ON FLOOR PANEL 1535X IAW SRM 53-30-53 FIG 101. ORIGINAL THICKNESS IS 080 ENDING THICKNESS IS 076 MATERIAL LOSS IS 004 AND FOUND TO BE WITHIN LIMITS. (K)SDR AMTA200600646Floor Panel · corrodedAFT CARGO FLOOR PANEL 1536X IS CORRODED ESPECIALLY AT DOOR THRESHOLD AREA F/S 767 TO 789 RBL 17 TO 22.0 UPPER SURFACE. BLENDED OUT CORROSION ON UPPER SURFACE OF FLOOR PANEL IAW 53-30-53 WITHIN LIMITS. ORIGINAL MATERIAL .071 MATERIAL LOSS .005. (K)SDR AMTA200600645Strap · corrodedFORWARD CARGO BAY, RT STRAP HAS VISIBLE CORROSION THROUGHOUT F/S 472.5 TO 500 RBL 22. REMOVED CORROSION FROM RT STRAP AT F/S 472.5 TO 500 RBL 22.0 IAW SRM 53-30-53 ORIG MATERIAL THK .063, MATERIAL LOSS .003 WITHIN LIMITS IAW SRM. (K)SDR 2006UALA02166Skin · crackedKEELBEAM LOWER SKIN PANEL HAS A CRACK RBL 5 BS 699. MAJOR REPAIR: REPAIRED LOWER KEELBEAM PANEL. REFERENCE SRM 53-60-12 REPAIR 2.SDR 2006UALA02165Wire Harness · shortedNUMEROUS CB POPPING AND ELEC ODOR IN AFT CABIN. WIRE HARNESS SHORTED AND BURNED IN SIDEWALL NEXT TO SEAT 1AB. FOUND CHAFED WIRE HARNESS. ALL CURRENT UAL A/C WITH SIMILAR WIRE HARNESS CONFIGURATION BEING INSPECTED FOR CHAFING. COA 93020 IS IN PROGRESS TO PERMSDR 2006UALA02156Door Frame · crackedFWD CARGO DOOR CUT-OUT AFT FRAME CRACKED AT 2 EA LOCATION AT BS 492 NEAR STR S-24R. REMOVED DAMAGE. FABRICATED AND INSTALLED NESTED ANGLES REPAIR. REFERENCE AAR EA I060500 AND UA-EVA-60678.SDR AMTA200600635Filter · unserviceableRT FUEL FILTER BYPASS LIGHT COME ON AT TAKEOFF. REMOVED AND REPLACED NR 2 ENGINE FUEL FILTER IAW MM 71-00-46 AND 73-11-02. OPERATIONAL CHECK NORMAL. (K)SDR AMTA200600634Electrical Sys · out of adjustNR 1 ENGINE SPOOLED UP FROM IDLE THEN SHUTDOWN WHEN GROUND POWER WAS PLUGGED IN AND THE GROUND POWER DROPPED OFF. INSPECTED, PREFORMED ADJUSTMENT AND TEST OF EXTERNAL POWER IAW 24-41-00. TASK 24-41-00715-004. NO FAULTS NOTED. NR 1 OK FOR SERVICE. (K)SDR 2006UALA02154Skin · dentedFOUND FUSELAGE EXTERNAL SKIN DENTED AT AFT JACK PAD AREA. REPAIR ACCOMPLISHED.SDR 2006UALA02134Angle · corrodedFWD GALLEY DOOR Z ANGLE CORRODED BS 294.5 - BS 328 RBL 54 -RBL 55 STR 17R TO STR 17R. REMOVED AND REPLACED Z ANGLE, REFERENCE SRM 51-40-02.SDR 2006UALA02133Skin · crackedFWD GALLEY DOOR CUTOUT FUSELAGE SKIN HAS A CRACK RUNNING FROM CUTOUT THROUGH AND PASSED RIVET HOLE AT LOWER AFT CORNER STA 328 STR 17R. REMOVED CRACK. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND STRUCTURAL FILLER REPAIR PER SRM 53-10-01 REPAIR 2.SDR 2006UALA02132Skin · crackedEXTERNAL FUSELAGE SKIN ELECTRONICS BAY COOLING DUCT CUT OUT AFT SIDE IS CRACKED. REMOVED CRACKED. FABRICATED AND INSTALLED DOUBLER REPAIR PER MM 53-30-99.SDR 2006UALA02128Line · severedNR 2 ENGINE FIREX SUPRESSION LINE FOUND SEVERED IN THE NR 6 FLAP TRACK FAIRING JUST IB OF THE NR 6 FLAP TRANSMISSION. FOUND THAT THE LINE WAS NOT PROPERLY CLAMPED IN PLACE. REPLACED LINE. ENSURED LINE WAS PROPERLY CLAMPED.SDR 2006UALA02126Strap · damagedAFT PIT STA. 907 REPLACEMENT STRAP HAS DRILL MARK, PARTIAL HOLE BELOW STR 23L UPPER FLANGE AND STR 21L SPLICE IS MISSING FASTENERS AND AFT END. REMOVED DAMAGE. INSTALLED REPAIR DOUBLER AND TRIPLER IAW EA I060496 REV IR.SDR 2006UALA02125Frame · crackedFWD CABIN STA 294 STR 17R LOWER FRAME CRACKED. REMOVED DAMAGE. FABRICATED AND INSTALLED FILLER AND REPAIR ANGLE. REFERENCE SRM 51-70-11 TABLE III.SDR 2006UALA02124Skin · crackedLT HORIZONTAL STAB TE LOWER SKIN APPROX 64 INCHES FROM FUSELAGE AND 2 INCHES FWD OF REAR SPAR CRACKED. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLER SHIM AND ACCESS PLATES. REFERENCE SRM 5-10-01 REPAIR 6 FIGURE 803.SDR 2006UALA02118Skin · dentedAFT CARGO COMPARTMENT SKIN DENTED AT BODY STA 834 TO 830 RBL 21 TO RBL 28 MARKED. FABRICATED AND INSTALLED REPAIR DOUBLER, TRIPLER, QUADRUPLER AND STRUCTURAL FILLER IAW EAI-6490 AND SRM 53-00-01 REPAIR 32.SDR 2006UALA02117Bushing · corrodedRT STAB AFT UPPER LUG, FWD BUSHING FACE PITTED, MATERIAL LOSS OUT OF LIMITS. MAJOR REPAIR: REWORKED LUG IAW EA-1060488.SDR 2006UALA02107Door Frame · crackedFWD CARGO DOOR FWD AND AFT FRAMES CRACKED AT LOWER STOP FITTINGS. INSTALLED NEW FRAME SECTIONS. REFERENCE SRM 51-40-02.SDR 2006UALA02106Skin · gougedEXTERNAL FUSELAGE SKIN HAS 2 EA GOUGES APPROX 4 INCHES LONG BTWN BS 887-907 STR 20L. INSTALLED EXTERNAL FUSELAGE SKIN DOUBLER TRIPLER REPAIR.SDR 2006UALA02105Skin · wornEXTERNAL CROWN FUSELAGE SKIN WORN UNDER DORSAL FIN LANDING. INSTALLED EXTERNAL SKIN TRIPLER REPAIR IAW SRM 53-60-01 REPAIR 9 PAGES 201-206 DETAIL 1.SDR 2006UALA02099Frame · damagedFRAME TO FLOOR Z ANGLE HAS DRILL START IN FRAME BS 747 LT SIDE. MAJOR REPAIR: INSTALLED NESTED ANGLE FILLER DOUBLER FRAME REPAIR PER MM 53-11-99 REPAIR VIII PAGE 812-813 AND 828 AND REINSTLALED Z ANGLE. REFERENCE SRM 51-40-02.SDR 2006UALA02095Filter · bypassingABORTED TAKEOFF AT 70 KTS FOR NR 1 ENGINE FUEL FILTER BY PASS LIGHT. SUPPLEMENTAL DATA UPDATE CAUSE: CONTAMINATED FUEL FILTER. REPLACED NR 1 ENGINE FUEL FILTER.SDR 2006UALA02089Skin · damagedUPPER SKIN HAS 12 EACH LIGHTING STRIKES AT BS 393 TO BS 412 STR 2R. REMOVED DAMAGE. INSTALLED REPAIR DOUBLER, TRIPLER, FILLER, AND TEAR STRAP DOUBLERS PER AAR EAI060494 REV IR. MAJOR REPAIRSDR 2006UALA02088Skin · dentedLOWER EXTERIOR FUSELAGE SKIN IS DENTED AT BS 972.5 STR S25R + 4 A=2.0 AND Y=.072 A OVER Y IS 27 OUT OF LIMITS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED DOUBLER AND STRUCTURAL FILLER PER AAR EAI060495 REV IR.SDR 2006UALA02087Door Frame · crackedFWD PIT DOOR WAY AFT SIDE FRAME IS CRACKED AT LOWER STOP FITTING IB SIDE OF FITTING. REMOVED DAMAGE. INSTALLED REPAIR ANGLES AND FILLER PER AAR EAI060493 AND UA-EVA-60653. MAJOR REPAIRSDR 2006UALA02078Stringer Clip · damagedAFT CARGO COMPARTMENT BS 887 RT SIDE STRINGER 20R CLIP ATTACHED FRAME TO STRINGER HAS TOOL MARKS AND HOLE IS ELONGATED. INSTALLED NEW STRINGER CLIP PER SRM 51-40-02.SDR 2006UALA02077Frame · corrodedAFT CARGO COMPARTMENT FRAME INBOARD FLANGE HAS 2 AND 1 MISDRILLED HOLES WITH LIGHT CORROSION AROUND THE HOLES AT THE FOLLOWING LOCATIONS, BS 727E AND BS 727D BETWEEN STR 25R AND 26R. REMOVED CORROSION AND INSTALLED STRAP REPAIR PER MM 53-11-99.SDR 2006UALA02076Angle · damagedAFT PIT Z ANGLES AT THE FOLLOWING STA ATTACHED HOLES DAMAGED, STA 727A STR 25R, STA 727B STR 25R, STA 727C STR 25R, STA 747 STR 25R, AND STA 767 STR 25R. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR STRAP PER MM 53-11-99.SDR AMTA200600628Actuator · unserviceableNR 2 FUEL VALVE CLOSED LIGHT ILLUMINATES WITH ENGINE START LEVER AT IDLE. REMOVED AND REPLACED NR 2 ENGINE FUEL SHUTOFF VALVE ACTUATOR. (M)SDR 2006UALA02063Door Frame · crackedFWD GALLEY DOOR LOWER FWD FRAME CRACKED AT LWR FITTING ATTACH HOLE. REMOVED AND REPLACED DAMAGED FRAME SECTION. REFERENCE SRM 51-40-02.SDR 2006UALA02062Strap · damagedAFT PIT STA 907 SKIN LAP STRAP BETWEEN STR S20L AND S21L HAS AN ENLARGED HOLE. REMOVED DAMAGE. FABRICATED AND INSTALLED REPLACEMENT STRAP. REFERENCE DRW 65-46880 AND SRM 51-40-02 PAGE 2.SDR 2006UALA02061Skin · crackedRT HORIZ STAB LWR SKIN CRACKED APPROX 56 INCHES OUTBOARD FROM INBOARD END AND 2 INCHES FWD OF REAR SPAR. REMOVED DAMAGE. FABRICATED AND INSTALLED EXTERNAL DOUBLER REPAIR. REFERENCE MM 55-10-94/801.
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