N952WN
Service difficulty reports · 222
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 = 'N952WN' 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 = 'N952WN' 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 SWAA2022100649132Support Fitting · crackedACB SUPPORT FITTING CRACKED AT BS947 LBL11. MARKED. / [01] VERIFIED SRM 51-10-02-0G-0 STEP 9.IS APPLICABLE FOR REPAIR.<BR><BR>PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT PER SRM 51-10-02 STEP 9.<BR><BR>REMOVED SUPSDR SWAA2022100649131Sidewall Support · crackedAFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CRACK BS927+13 RBL20. / [01] VERIFIED SRM 53-00-53-1A-2 IS APPLICABLE FOR REPAIR.<BR><BR>SIDEWALL SUPPORT AT BS887 TO BS947 RH;FOUND TO BE OUT LIMITS FOR CRACK;IAW SRM 53-00-53-1A-2;PARAG. 4(1) DETAIL C;D FIG.103.IDESDR SWAA2022100649096Attach Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS400 LBL25 WL154. MARKED. / [01] AFTER FURTHER INVESTIGATION FOUND NO CRACK IN THE FCB INTERCOSTAL ATTACH ANGLE BS 400 LBL 25 WL 154 PER SRM 51-10-02;[02] CORRECTION:PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS ANDSDR SWAA2022100649098Shield · corrodedCORROSION ON AFT SHIELD AT AFT CARGO BAY BS493 - BS500 RBL24. DAMAGE FOUND TO BE AT FWD CARGO BAY. / [01] PRIOR TO REMOVAL; FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BNY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP;[02] VERIFIED APLICABILITY SRM 53-SDR SWAA2022100649130Sidewall Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS887+5; BS887+9; BS927+17 RBL20. / [01] VERIFIED APPLICABILITY SRM 53-70-53-01-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE.<BR><BR>REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFSDR SWAA2022100649081Shield · corrodedCORROSION ON FWD SHIELD AT FCB BS420 - BS440 RBL23. / [01] PRIOR TO REMOVAL; FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9;[02] LOCATED AND DRILLED NEW SHIELD AT BS420-BS440 RBL 23<BR> P/N 143A8126U21ATSSDR SWAA2022100649082Sidewall Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS500 - BS500D RBL23 . / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT CARGO BAY BS 500 -500D LBL23 AT DISCREPANCY AREA BS.500 L=1.700' W=0.800' D=0.020 ORIGINAL THICKNESS 0.040 REMAINING MAT 0.020 MAT LOSSDR SWAA2022100645316None · corrodedCORROSION AT AFT CARGO BAY ON TRACK TIEDOWN LBL 17 BS787+3. / [01] REMOVED CORROSION ON TRACK TIEDOWN AT FCB BS 500 RBL 13 WL 156 REWORKED AREA L=2XW=1 MAX MATERIAL LOSS 0.026 WAS FOUND IN THE LIMITS IAW SRM 53-00-53-1A-2 STEP 4(B)2 A FIGURE 103.- <BR>TOOL USESDR SWAA2022100649125Sidewall Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727 - BS767 RBL20. / [01] VERIFIED APPLICABILITY SRM 53-60-53-01-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE.<BR><BR>REMOVED CORROSION ON AFT CARGO BAY TO SIDEWALL SUPPORT AT RBL20 BSDR SWAA2022100649127Shield · corrodedCORROSION ON FWD SHIELD AT AFT CARGO BAY BS767 - BS787 RBL21. / [01] PRIOR TO REMOVAL; FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT; IAW SRM 51-10-02-0G-0 STEP 9.;[02] LOCATED AND DRILLED AFT NEW SHIELD AT AFT CARGO BAY BS767-BS787SDR SWAA2022100649118Web · corrodedCORROSION ON WEB AT AFT CARGO BAY BS787+2 RBL19. / [01] REMOVED WEB DAMAGED AT AFT CARGO BAY BS787 TO BS 795;IAW SRM 51-40-02.;[02] REMOVED CORROSION AT WEB BS787+2 RBL19;MEASURES:L=.9;W=.8;D=.024';REMAINING TICKNESS .021'.FOUND TO BE OUT LIMITS ;IAW SRM 53-60SDR SWAA2022100649129Shield · corrodedCORROSION ON AFT SHIELD AT AFT CARGO BAY BS855; BS858; RBL22. / [01] PRIOR TO REMOVAL; FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT; IAW SRM 51-10-02-0G-0 STEP 9.;[02] LOCATED AND DRILLED AFT NEW SHIELD AT AFT CARGO BAY BS847-BS867SDR SWAA2022100649121Support Angle · corrodedCORROSION AT ACB ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE BS947 LBL9 TO RBL17. / [01] REMOVED ON AFT CARGO BAY BULKHEAD SUPPORT (BRACKET) LOCATED BETWEEN RBL. 21 - LBL. 8 BS. 947.5 IAW SRM 51-40-02. PART NO HAVE ENTRIES IN SRM BY ALLOWABLE DAMAGE WILL BE REPAIR SDR SWAA2022100645329Shear Tie · corrodedCORROSION ON SHEAR TIE AT AREA AFT OF ACB BS967 BL0. / [01] DAMANGE FOUND ON SHEAR TIE AT AREA AFT OF ACB BS967 BL0 WL190 P/N 147A1120-71 FOUND TO BE OUT OF LIMIT IAW SRM PART WILL BE REPAIRED BY REMPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9C;[02] REMOVED SHEAR TISDR SWAA2022100649113None · corrodedCORROSION AT AFT CARGO BAY ON TRACK TIEDOWN LBL 17 BS787+3. / [01] REMOVED CORROSION ON TRACK TIEDOWN AT FCB BS 500 RBL 13 WL 156 REWORKED AREA L=2XW=1 MAX MATERIAL LOSS 0.026 WAS FOUND IN THE LIMITS IAW SRM 53-00-53-1A-2 STEP 4(B)2 A FIGURE 103.- <BR>TOOL USESDR SWAA2022100649135Shear Tie · corrodedCORROSION ON SHEAR TIE AT AREA AFT OF ACB BS967 BL0. / [01] DAMANGE FOUND ON SHEAR TIE AT AREA AFT OF ACB BS967 BL0 WL190 P/N 147A1120-71 FOUND TO BE OUT OF LIMIT IAW SRM PART WILL BE REPAIRED BY REMPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9C;[02] REMOVED SHEAR TISDR SWAA2022100545309Floor Support · crackedCRACK ON FWD PASSENGER CABIN INTERCOSTAL AT BL 0 BS 277+7; BS 277+14. / [01] REMOVED FWD PASSENGER CABIN INTERCOSTAL AT BL 0 BS 277+7 PER SRM 51-40-02;[02] LOCATED AND DRILLED FWD PASSENGER CABIN INTERCOSTAL AT BL 0 BS 277+7 PER SRM 51-40-05 AND DWG NBR 141A54SDR SWAA2022100549106Floor Support · crackedCRACK ON FWD PASSENGER CABIN INTERCOSTAL AT RBL 32 BS 344+5. / [01] REQUIRE NDI TO VERIFY FOR CRACK;[02] HFEC INSPECTED SUSPECTED CRACKED AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>CRACK NOTED TO BE .6' IN AREA MARKED.<BR>EQUIP USED:<BR>-NORTEC 600 ID:SDR SWAA2022100549104Floor Support · crackedCRACK ON FWD PASSENGER CABIN INTERCOSTAL AT BL 0 BS 344+9. / [01] REQUIRE NDI TO VERIFY FOR CRACK;[02] HFEC INSPECTED SUSPECTED CRACKED AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>CRACKS NOTED TO BE .3' AT MARKED AREA.<BR>EQUIP USED:<BR>-NORTEC 600 ID: SDR SWAA2022100549105Floor Support · crackedCRACK ON FWD PASSENGER CABIN INTERCOSTAL AT BL 0 BS 277+7; BS 277+14. / [01] REMOVED FWD PASSENGER CABIN INTERCOSTAL AT BL 0 BS 277+7 PER SRM 51-40-02;[02] LOCATED AND DRILLED FWD PASSENGER CABIN INTERCOSTAL AT BL 0 BS 277+7 PER SRM 51-40-05 AND DWG NBR 141A54SDR SWAA2022100545321Floor Support · crackedCRACK ON MID PASSENGER CABIN FLOOR SUPPORT AT BS 540 LBL 2. / [01] REMOVED MID PASSENGER CABIN FLOOR SUPPORT BS 540 BETWEEN LBL 25 AND BL 0 IAW SRM 51-40-02 ; LOCATED AND DRILLED NEW MID PASSENGER CABIN FLOOR SUPPORT IAW SRM 51-40-05 ; OK TO INSTALL;[02] VERIFSDR SWAA2022100545327Floor Support · crackedCRACK ON MID PASSENGER CABIN FLOOR SUPPORT AT BS 540 RBL 2. / [01] REMOVED MID PASSENGER CABIN FLOOR SUPPORT BS 540 BETWEEN RBL 25 AND BL 0 IAW SRM 51-40-02 ; LOCATED AND DRILLED NEW MID PASSENGER CABIN FLOOR SUPPORT IAW SRM 51-40-05 ; OK TO INSTALL;[02] VERIFSDR SWAA2022100545322Floor Support · crackedCRACK ON MID PASSENGER CABIN FLOOR SUPPORT AT BS 540 RBL 27. AFT SIDE OF I/B FASTENER. / [01] REMOVED MID PASSENGER CABIN FLOOR SUPPORT BS 540 BETWEEN RBL 25 AND RBL 45 IAW SRM 51-40-02 ; LOCATED AND DRILLED NEW MID PASSENGER CABIN FLOOR SUPPORT IAW SRM 51-40-SDR SWAA2022100549122Floor Support · crackedCRACK ON MID PASSENGER CABIN FLOOR SUPPORT AT BS 540 LBL 2. / [01] REMOVED MID PASSENGER CABIN FLOOR SUPPORT BS 540 BETWEEN LBL 25 AND BL 0 IAW SRM 51-40-02 ; LOCATED AND DRILLED NEW MID PASSENGER CABIN FLOOR SUPPORT IAW SRM 51-40-05 ; OK TO INSTALL;[02] VERIFSDR SWAA2022100549123Support · crackedCRACK ON MID PASSENGER CABIN FLOOR SUPPORT AT BS 540 RBL 27. AFT SIDE OF I/B FASTENER. / [01] REMOVED MID PASSENGER CABIN FLOOR SUPPORT BS 540 BETWEEN RBL 25 AND RBL 45 IAW SRM 51-40-02 ; LOCATED AND DRILLED NEW MID PASSENGER CABIN FLOOR SUPPORT IAW SRM 51-40-SDR SWAA2022100549133Floor Support · crackedCRACK ON MID PASSENGER CABIN FLOOR SUPPORT AT BS 540 RBL 2. / [01] REMOVED MID PASSENGER CABIN FLOOR SUPPORT BS 540 BETWEEN RBL 25 AND BL 0 IAW SRM 51-40-02 ; LOCATED AND DRILLED NEW MID PASSENGER CABIN FLOOR SUPPORT IAW SRM 51-40-05 ; OK TO INSTALL;[02] VERIFSDR SWAA2022100645277None · corrodedCORROSION ON AFT PASSENGER CABIN FLOOR BEAM AT BS 986 LBL 42; RBL 42. / [01] AFTER FURTHER INVESTIGATION FOUND NO CORROSION DAMAGE AT RBL 42 ( BARE METAL ONLY);[02] VERIFIED CORRECTIVE ACTION 1.;[03] APPLIED A CHEMICAL CONVERSION COATING AND TWO LAYERS OF BMS SDR SWAA2022100648706None · corrodedCORROSION ON AFT PASSENGER CABIN FLOOR BEAM AT BS 986 LBL 42; RBL 42. / [01] AFTER FURTHER INVESTIGATION FOUND NO CORROSION DAMAGE AT RBL 42 ( BARE METAL ONLY);[02] VERIFIED CORRECTIVE ACTION 1.;[03] APPLIED A CHEMICAL CONVERSION COATING AND TWO LAYERS OF BMS SDR SWAA2022101045258None · crackedBS 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT LBL 31 WL 157. / [01] IDENTIFIED PART AND MATERIAL IAW SRM 57-10-10-0I-2 FIGURES 1-2; TABLE 2; ITEM [4]. FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10-1A-2 PAR 4.D (1) (A) 1). PERMANENT REPAIR SDR SWAA2022101045259None · crackedBS 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT RBL 33 WL 155. / [01] IDENTIFIED PART AND MATERIAL IAW SRM 57-10-10-0I-2 FIGURES 1-2; TABLE 2; ITEM [4]. FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10-1A-2 PAR 4.D (1) (A) 1). PERMANENT REPAIR SDR SWAA2022101047673Angle · crackedBS 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT RBL 10; WL 164. / [01] VERIFY APLICABILITY PER REF SRM 57-10-10-2R-5<BR><BR>REMOVED FASTENERS AT DISCREPANCY AREA PER REF SRM 57-10-10-2R-5<BR><BR>REMOVED DAMAGED SECTION AT DISCREPANCY AREA PER SDR SWAA2022101047684Bulkhead · crackedBS 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT LBL 31 WL 157. / [01] IDENTIFIED PART AND MATERIAL IAW SRM 57-10-10-0I-2 FIGURES 1-2; TABLE 2; ITEM [4]. FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10-1A-2 PAR 4.D (1) (A) 1). PERMANENT REPAIR SDR SWAA2022101047685None · crackedBS 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT RBL 33 WL 155. / [01] IDENTIFIED PART AND MATERIAL IAW SRM 57-10-10-0I-2 FIGURES 1-2; TABLE 2; ITEM [4]. FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10-1A-2 PAR 4.D (1) (A) 1). PERMANENT REPAIR SDR SWAA2022100645251Attach Angle · crackedBS 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT RBL 10; WL 164. / REMOVED DAMAGED SECTION AT DISCREPANCY AREA PER REF SRM 57-10-10-2R-5;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.;[03] REQUIRE NDI TO PERFORM AN OPEN HOLE HIGH FREQSDR SWAA2022100545250Floor Panel · damagedFWD CABIN FLOOR PANEL 222DF HAS A PULLED THROUGH INSERT ON O/B EDGE / [01] DUE TO THE EXTENT OF DAMAGE; REPLACED FWD CABIN FLOOR PANEL 222DF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-21L ITEM 235.;[02] INSPECTION COMPLETESDR SWAA2022100547678Floor Panel · damagedFWD CABIN FLOOR PANEL 222DF HAS A PULLED THROUGH INSERT ON O/B EDGE / [01] DUE TO THE EXTENT OF DAMAGE; REPLACED FWD CABIN FLOOR PANEL 222DF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-21L ITEM 235.;[02] INSPECTION COMPLETESDR SWAA2022080437940Lens · missingAFT ENTRY DOOR EMER. EXIT LIGHT LENSE MISSING. / [01] RE-SECURED AFT RH EMER. EXT. LT LENSE PER AMM 33-51-01.SDR SWAA2022041892599Panel · delaminatedPANEL 551BB LOCATED L/H WING LOWER SURFACE FORWARD OF GEAR CUT OUT HAS A DENT WITH SAME AREA OF DELAMINATION. / [01] PANEL 551BB REMOVED FROM A/C. REQUIRES PANEL P/N 115A2711-7. IPC 24-51-00-12 ITEM 1;[02] P/N CHANGED TO 654A0004-1261.;[03] LOCATED; DRILLED; ASDR SWAA000092292Tire · blew outWE BLEW THE INSIDE TIRE ON THE CAPTAINS SIDE ON TAKEOFF. WE DID NOT KNOW THIS UNTIL LANDING IN PHX. WE DID A FLY BY OF THE TOWER. THEY TOLD US A WHEEL WAS BLOWN. WE DECLARED AN EMERGENCY. AFTER....... LANDING THE FIRE DEPARTMENT CHECKED THE TIRE AND THEN WE TASDR SWAA2022041292598Skin · delaminatedL/H INBOARD TRAILING EDGE SHELF PANEL HAS LARGE PUNCTURE IN LOWER SKIN WITH DELAMINATED AREA AROUND THE PUNCTURE / [01] REMOVED PANEL 193CL REF 737 SRM 51-40-02;[02] REMOVED LH MLG DOOR TOP SEAL RETAINER REF 737 SRM 51-40-02;[03] REMOVED LH WING TE SHELF PANELSDR SWAA2022011761184Slide · looseL1 DOOR SLIDE CAME OUT OF SHELL ; / [01] REINSTALLED SLIDE INTO SHELL PER AMM 25-66-01SDR SWAA000043717Panel · elongated193D PANEL HAS 2 HOLES ELONGATED. ; / [01] COMPLIED WITH EA-21-153-03375SDR SWAA2021111743716Panel · elongated194E PANEL 4 HOLES ELONGATED. ; / [01] ISSUED EA 21-153-03375.; [02] COMPLIED WITH EA-21-153-03375SDR SWAA2021082308881Lens · missingEXIT SIGN COVER MISSING ; / [01] INSTALLED EXIT SIGN COVER REF AMM 33-25-00SDR SWAA2020110428267Battery · inoperativeFWD LT WINDSREEN STOWAGE COMPARTMENT FLASH LIGHTS (2 EACH) BATTERY LIFE EXPIRED. REMOVED AND REPLACED 2 EACH FLASHLIGHT BATTERY, PER AMM 25-64-00.SDR SWAA2020110428259Lens · missingFWD RT DOOR HEADER PANEL EXIT SIGN LENS MISSING. REMOVED AND REPLACED DOOR EXIT LIGHT ASSEMBLY AND OPERATIONS CHECK OK, PER AMM 33-51-01.SDR SWAA2020110428230Floor Panel · damagedMAIN CABIN FLOOR PANEL 241AF HAS FIBER DAMAGE. REMOVED AND REPLACED CABIN FLOOR PANEL, PER AMM 53-21-00.SDR SWAA2020110428231Floor Panel · damagedMAIN CABIN FLOOR PANEL 241DF HAS FIBER DAMAGE. REMOVED AND REPLACED CABIN FLOOR PANEL, PER AMM 53-21-00.SDR SWAA2020110428226Structure · crackedFWD SERVICE DOOR 141A6536-15 CRACKED IN RADIUS. INSTALLED NEW SERVICEABLE DOOR, PER AMM 52-41-00. LEAK CHECKED GOOD, PER AMM 05-51-91. TAG NO: 651744 PN ON: 141A6516-20M SN ON: 002501 PN OFF: SN OFF: CYC0150.SDR SWAA2020110428225Floorboard · damagedCABIN FLOORBOARD 231DF BOWING AND POPPING WHEN WALKED ON. REMOVED AND REPLACED CABIN FLOOR BOARD 231DF, PER AMM 53-21-00.
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