N733PA
Service difficulty reports not matched to an aircraft · 176
They name N733PA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N733PA' AND registry_match IS NULL 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 = 'N733PA' AND registry_match IS NULL 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 SROM2012032000019Duct Clamp · wornON CLIMBOUT, RIGHT WING TO BODY OVERHEAT LIGHT ILLUMINATED. REDUCED POWER ON RIGHT ENGINE LIGHT EXTINGUISHED. RETURNED TO AIRPORT FOR UNEVENTFUL LANDING. REPLACED BLEED AIR CLAMP ON RIGHT BLEED AIR DUCT ON RIGHT ENGINE. SUBSEQUENT LEAK CHECK OF DUCT WAS SASDR SROM201203200018Sill · corrodedLEVEL 1 CORROSION FOUND ON L1 DOOR INNER SILL. SECOND BLEND ON THIS PART'S HISTORY.SDR SROM201203200017Sill · corrodedLEVEL 1 CORROSION FOUND ON FORWARD SERVICE DOOR SILL CHORD. SECOND BLEND IN THIS PART'S HISTORY.SDR SROM2012032000016Bear Strap · crackedDURING INSPECTION, CRACKS WERE FOUND IN THE BEAR STRAP RE-INFORCEMENT OF THE L1 DOOR, BS 304 S10-13L.SDR SROM201203160002Stringer · corrodedLEVEL 1 CORROSION FOUND ON STRINGER.SDR SROM201203200014Spar · corrodedCORROSION FOUND ON LOWER SPAR CHORD.SDR SROM201203200013Shear Tie · damagedDAMAGED SHEAR TIE FRAME.SDR SROM20120320013Strap · damagedSTRAP DAMAGED.SDR SROM201203200012Frame · damagedDAMAGED FRAME AT BS 867 S26R.SDR SROM201203160001Frame · damagedDAMAGE /DRILL START ON FRAME.SDR SROM201203200011Frame · crackedFRAME CRACKED AT AIR CONDITIONING BRACKET.SDR SROM201203200010Frame · crackedCRACKED FRAME AT AIR CONDITIONING SUPPORT BRACKET.SDR SROM201203200009Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 360 S5L.SDR SROM201203200008Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 400 S18R.SDR SROM201203200007Stringer Clip · crackedCRACKED STRINGER CLIP AT BS 500A S19R.SDR SROM201203200006Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 908 S4R.SDR SROM201203200005Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 767 S22L.SDR SROM201203200004Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 907 S21R.SDR SROM201203200003Stringer Clip · crackedCRACKED STRINGER CLIP AT BS 706 S13R.SDR SROM201203200002Stringer Clip · crackedSTRINGER CLIP AT BS 663 S9R IS CRACKED.SDR SROM201203200001Stringer Clip · crackedSTRINGER CLIP AT BS 663 S10L CRACKED.SDR SROM2012001Contactor · burnedEXPERIENCED SMOKE IN THE COCKPIT AT THE GATE PRIOR TO DEPARTURE. THE FLIGHT CREW QUICKLY POWERED DOWN THE AIRCRAFT; NO PASSENGERS WERE ON BOARD. MAINTENANCE FOUND THE GROUND SERVICE CONTACTOR TO BE THE PROBLEM AND ONE PHASE OF THE THREE PHASE GROUND POWER CISDR SROM2010009Skin · damagedREPAIRED FUSELAGE SKIN BLEND OUT BELOW STRINGER S-25R, STA BS 885.25 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL, REV 101, DATED MAR 10, 2010, SECTION 53-30-3, PAGES 254, 257 TO 263 AND 286 AND 51-30-1, PAGE 3. REFERENCE NON-ROUTINE TASK CARD 6SDR SROM2010015Shear Tie · crackedREPAIRED SHEAR TIE BETWEEN STRINGERS 20L AND S-21L, STA: BS 907 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL (SRM), REV 101, DATED MARCH 10, 2010, SECTION 53-10-4, FIGURE 8. REFERENCE NON-ROUTINE TASK CARD 813, DATED APRIL 01, 2010.SDR SROM2010014Skin · damagedREPAIRED FUSELAGE SKIN BLEND OUT 0.4 INCHES BELOW STRINGER S-20L, STA: BS 896 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL (SRM), REV 101, DATED MARCH 10, 2010, SECTION 53-30-3, FIGURE 48. REFERENCE NON-ROUTINE TASK CARD 799, DATED MARCH 25, 2SDR SROM2010013Skin · damagedREPAIRED FUSELAGE SKIN SCRIBE LINES LEFT WING TO BODY FAIRING AT STRINGERS S-16L TO 3 INCHES BELOW S-17L, STA: BS 500B - 516 IN ACCORDANCE WITH MESSAGE KFC-ATR-10-0001-01C, DATED MARCH 30, 2010, KFC-ATR-10-0001-05B, DATED MARCH 31, 2010, KFC-ATR-10-0001-06B, SDR SROM2010012Skin · damagedREPAIRED FUSELAGE SKIN BLEND OUT AT STRINGER S-20L, STA: BS 974 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL, REV 101, DATED MARCH 10, 2010, SECTION 53-30-3, FIGURE 48, DETAIL XV. REFERENCE NON-ROUTINE TASK CARD 743, 742 AND 744, DATED MARCH 18SDR SROM2010011Skin · damagedREPAIRED FUSELAGE SKIN BLEND OUT 1.6 INCHES ABOVE STRINGER S-23L, STA: BS 926.5 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL, REV 101, DATED MARCH 10, 2010, SECTION 53-30-3, FIGURE 48, PAGES 256 TO 260 AND 264, DETAIL VII, PAGES 261 AND 281 ANDSDR SROM2010010Skin · damagedREPAIRED FUSELAGE SKIN BLEND OUT ABOVE STRINGER S-26R, STA: BS 838.5 IN ACCORDANCE WITH MESSAGE KFC-ATR-10-0001-01C, DATED MARCH 31, 2010, KFC-ATR-10-0001-05B, DATED APRIL 05, 2010, KFC-ATR-10-0001-06C, DATED APRIL 19, 2010, BOEING REPAIR DRAWING 65-45775, SHSDR SROM2010008Skin · nickedREPAIRED FUSELAGE NICK 3 INCHES ABOVE STRINGER S-20R, STA: BS 914 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL (SRM), REV 101, DATED MARCH 10, 2010, SECTION 53-30-3, FIGURE 48. REFERENCE NON-ROUTINE TASK CARD 617, DATED MARCH 18, 2010.SDR SROM2010007Intercostal · damagedREPAIRED STRINGER INTERCOSTAL AT STRINGER S-4L, STA: BS 305 BY REPLACEMENT WITH NEW PART 50-8261-62 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL (SRM), REV 101, DATED MARCH 10, 2010, SECTION 53-30-3 AND BOEING DRAWING 50-8261, REV H. REFERENCE NSDR SROM2010006Skin · damagedREPAIRED FUSELAGE SKIN BLEND OUT 1.75 INCHES ABOVE STRINGER S-23R, STA: BS 904.8 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL, REV 101, DATED MARCH 10, 2010, SECTION 53-30-3, FIGURE 48. REFERENCE NON-ROUTINE TASK CARD 380, 374, 375, AND 383, DASDR SROM2010005Skin · damagedREPAIRED FUSELAGE SKIN BLEND OUT THREE INCHES BELOW STRINGER S-25R, STA: BS 775 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL, REV 101, DATED MARCH 10, 2010, SECTION 53-30-3, FIGURE 48, DETAIL XII. REFERENCE NON-ROUTINE TASK CARD 334, 316 AND 66SDR SROM2010004Bearing · looseREPLACED NLG UPPER ATTACH BEARING IN ACCORDANCE WITH FAA DER APPROVED FORM 8110-3 NO. 091-1236-10-848, DATED APRIL 01, 2010, ASI ENGINEERING REPORT 5310848-ER, REV IR, DATED MARCH 25, 2010 AND ASI DRAWING 5310848-1, SHTS 1 THRU 3, REV IR, DATED MARCH 25, 2010.SDR SROM2010003Skin · damagedREPAIRED FUSELAGE SKIN BLEND OUT AT STRINGER S-23L, STA: BS 897 IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL, REV 101, DATED MAR 10, 2010, SECTION 53-30-1, FIGURE 1 AND 53-30-3, FIGURE 48. REFERENCE NON-ROUTINE TASK CARD 206, DATED MAR 08, 2010SDR SROM2010002Fairing · delaminatedREPAIRED LEFT AND RIGHT GRAVEL EQUIPPED NOSE LANDING GEAR FILLET FAIRINGS AND DOOR FAIRINGS IN ACCORDANCE WITH FAA DER APPROVED FORM 8110-3, REV IR, DATED JANUARY 22, 2010 AND ENGINEERING STRESS REPORT SCS-3220-001, REV IR, DATED OCTOBER 05, 2009 AND SCS-3220-SDR SROM20090017Actuator · inoperativeNLG WOULD NOT RETRACT AFTER TAKE-OFF. SELECTED GEAR DOWN AND RETURNED TO DEPARTURE AIRPORT. FOUND NOSE GEAR GRAVEL DEFLECTOR ACTUATOR FUNCTIONING IMPROPERLY.SDR SROM20080024Slide · inoperativeDURING MINI EVACUATION DEMONSTRATION TRAINING SLIDE DEPLOYED BUT DID NOT INFLATE. WAITING ON TEAR DOWN REPORT FOR FINAL DISPOSITION. 11/20/08 FINAL DISPOSITION. TEARDOWN REPORT INDICATED NO FINDINGS.SDR SRO2008F00000Slide · inoperativeDURING MINI EVACUATION DEMONSTRATION TRAINING SLIDE DEPLOYED BUT DID NOT INFLATE. WAITING ON TEAR DOWN REPORT FOR FINAL DISPOSITION.SDR SROM2008021Torque Box · crackedCRACKED APU TORQUE BOX WEB AT STA BS 1115 RBL 2. HFEC CARRIED OUT IN ACCORDANCE WITH BOEING 737 NDT MANUAL 51-00-00, FIGURE 23, PART 6 ON A CUT-OUT ON THE APU TORQUE BOX, STA BS 1115. NO DEFECTS EVIDENT (NDT08-0461). APU TORQUE BOX WEB AT STA BS 1115 RBL 2 SDR SROM2008020Floorbeam · crackedCORROSION ON FLOOR I-BEAM AT STA BS 344 LBL 18 THRU RBL 39. REPAIRED FLOOR I-BEAM AT STA BS 344 LBL 18 THRU RBL 39 IN ACCORDANCE WITH BOEING 737 STRUCTURAL REPAIR MANUAL (SRM), 53-10-9, FIGURE 5. REFERENCE NON-ROUTINE CARD 858, DATED 03/25/08.SDR SROM2008008Keelbeam · corrodedLOWER CHORDS OF KEEL BEAM IN MAIN LANDING GEAR HAS CORROSION AT LOWER FLANGE IN SEVERAL AREAS UPPER & LOWER SURFACES FROM STA BS 663-727 RBL 6.5 & LBL 6.5. REPAIRED LOWER CHORD OF KEEL BEAM IN MLG WHEEL WELL AT LOWER FLANGE IN ACCORDANCE WITH BOEING MESSAGE 1SDR SROM2008003Floorbeam · corrodedCORROSION ON UPPER CAP OF FLOORBEAM AT STA BS 294.5 BETWEEN LBL 12 AND RBL 50. CORROSION ON UPPER CAP OF FLOORBEAM AT STA BS 294.5 BETWEEN LBL 12 AND RBL 50 BLENDED BEYOND LIMITS IN ACCORDANCE WITH BOEING 737 STRUCTURAL REPAIR MANUAL (SRM), 53-10-1. REPAIREDSDR SROM2008019Floorbeam · crackedLOWER LONGITUDINAL FLOORBEAM CHORD CRACKED AT RBL 24.5 STA BS 663. REPLACED LOWER LONGITUDINAL FLOORBEAM CHORD AT RBL 24.5 STA BS 663 IN ACCORDANCE WITH BOEING 737 STRUCTURAL REPAIR MANUAL (SRM), 51-30-01 AND BOEING DRAWING 65-45410. REFERENCE NON-ROUTINE CASDR SROM2008012Skin · damagedLIGHTNING STRIKE AT STA BS 933 STR 25.5R. REPAIRED IN ACCORDANCE WITH BOEING 737 STRUCTURAL REPAIR MANUAL (SRM), 53-30-03, FIGURE 23 (PERMANENT REPAIR), SECTION 1, PARAGRAPH 3., (NDT08-0509). REFERENCE NON-ROUTINE CARD 602, DATED 03/04/08.SDR SROM2008006Skin · crackedCRACK IN FUSELAGE SKIN AT STA BS 760 STR 19L, (NDT CONFIRMED CRACK). REPAIRED FUSELAGE SKIN AT STA BS 760 STR 19L IN ACCORDANCE WITH BOEING 737 STRUCTURAL REPAIR MANUAL (SRM), 53-30-03, FIGURE 48, FASTENERS INSTALLED IN ACCORDANCE WITH SRM 51-30-02. REFERENCSDR SROM2008007Bar · crackedREPAIR CRACKED SPREADER BARS ON PASSENGER SEATS. REPAIRED CRACKED SPREADER BARS ON PASSENGER SEATS IN ACCORDANCE WITH CPAI EO C007-2525-B737-01 AND FAA DER APPROVED 8110-3, 080-1226-08-471 AND ASI DRAWING 2520471-1, REV IR, DATED MARCH 19, 2008. REFERENCE KESDR SROM2008002Floorbeam · corrodedCORROSION ON AFT GALLEY FLOORBEAM AT STA BS 980 RBL 4. BLENDED AND FOUND CORROSION ON AFT GALLEY FLOORBEAM AT STA BS 980 RBL 4 TO BE BEYOND LIMITS. REPAIRED AFT GALLEY FLOORBEAM AT STA BS 980 RBL 4 IN ACCORDANCE WITH BOEING 737 STRUCTURAL REPAIR MANUAL (SRM)SDR SROM2008018Floorbeam · crackedLOWER LONGITUDINAL FLOORBEAM CHORD CRACKED AT LBL 24.5 STA BS 663. REPLACED LOWER LONGITUDINAL FLOORBEAM CHORD AT LBL 24.5 STA BS 663 IN ACCORDANCE WITH BOEING 737 STRUCTURAL REPAIR MANUAL (SRM), 51-30-01 AND BOEING DRAWING 65-45410. REFERENCE NON-ROUTINE CASDR SROM2008017Bracket · crackedLEFT HAND ENGINE TAILPIPE CRACKED AT BRACKET MOUNT (3 O'CLOCK POSITION). REPAIRED LEFT HAND ENGINE TAILPIPE BRACKET MOUNT (3 O'CLOCK POSITION) IN ACCORDANCE WITH FAA DER APPROVED FORM 8110-3, 073-1236-08-477 AND ASI SOLUTIONS DRAWING 7830477-1, REV IR, DATED
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