N912WN
Service difficulty reports · 270
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 = 'N912WN' 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 = 'N912WN' 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 SWAA2025040922144Floor Panel · cracked12 INCH CRACK FOUND IN FLOOR AFT CARGO.<[01] REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR PANEL 140BF PER AMM 25-52-10.SDR SWAA2024111859650Seal · crackedRIGHT HORIZONTAL STABILIZER UPPER FORWARD SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER UPPER FORWARD SLIDING SEAL PER AMM 53-31-31.SDR SWAA2024090332379Lamp · inoperativeROW 8 RH EMER LIGHT INOP<[01] RELAMPED PER AMM 33-51-03. OPS CHECK GOOD.SDR SWAA2024080924346Fairing · delaminatedR/H I/B (#6) AFT FLAP FAIRING TAIL CONE IS DELAMINATED R/H I/B (#5) AFT FLAP FAIRING TAIL CONE IS DELAMINATED<[01] REMOVED AND REPLACED PER [AMM 27-51-18-400-802-NG (INBOARD FLAP SUPPORT AFT FAIRING INSTALLATION - PERMANENT)]SDR SWAA2024080520046Sign · detachedFORWARD ENTRY EXIT SIGN FELL OFF<[01] RESECURED FWD ENTRY EMERGENCY EXIT SIGN COVER IN REF. TO AMM 33-51-01.SDR SWAA2024050783117Guide Arm · shearedFWD ENTRY DOOR GUIDE ARM SHEARED<[01] FWD ENTRY (L!) DOOR GUIDE ARM AND ROLLER PER AMM 52-11-21 & ADJUSTED FWD ENTRY (L!) DOOR PER AMM 52-11-00.;[02] R&R?D FWD ENTRY (L1) DOOR GUIDE ARM & ROLLER PER AMM 52-11-21 & ADJUSTED FWD ENTRY (L1) DOOR PER AMM 52-11-00.SDR SWAA2024050783342Roller · shearedFWD ENTRY DOOR GUIDE ARM SHEARED<[01] FWD ENTRY (L!) DOOR GUIDE ARM AND ROLLER PER AMM 52-11-21 & ADJUSTED FWD ENTRY (L!) DOOR PER AMM 52-11-00.;[02] R&R?D FWD ENTRY (L1) DOOR GUIDE ARM & ROLLER PER AMM 52-11-21 & ADJUSTED FWD ENTRY (L1) DOOR PER AMM 52-11-00.SDR SWAA2024050783343Guide Arm · shearedFWD ENTRY DOOR GUIDE ARM SHEARED<[01] FWD ENTRY (L!) DOOR GUIDE ARM AND ROLLER PER AMM 52-11-21 & ADJUSTED FWD ENTRY (L!) DOOR PER AMM 52-11-00.;[02] R&R?D FWD ENTRY (L1) DOOR GUIDE ARM & ROLLER PER AMM 52-11-21 & ADJUSTED FWD ENTRY (L1) DOOR PER AMM 52-11-00.SDR SWAA2023112223290Seat · faultyEMERGENCY EXIT ROW 11 SEATS RECLINE WITHOUT PUSHING THE BUTTON<[01] REPLACED HARDWARE REF CMM 25-21-42 OPS CHECK NORMALSDR SWAA2023092503084Switch · faultyFO FIRE WARN WILL NOT CUTOUT<[01] R&R'D F/O GLARESHIELD FIRE WARNING SWITCH & OPS CKS OK PER AMM 33-18-00SDR SWAA2023091198280Light · burned outMAIN PASSENGER CABIN L/H OVER WING EXIT DOOR SIDE EXIT SIGN HAS A BURNED-OUT BULB.<[01] RELAMPED L/H OVERWING EXIT DOOR PROXIMITY LIGHT AND TESTED PER AMM 33-51-01-960-801; NO DEFECTS NOTED.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2023091198281Light · burned outMAIN PASSENGER CABIN R/H OVER WING EXIT DOOR SIDE EXIT SIGN HAS A BURNED-OUT BULB.<[01] RELAMPED R/H OVERWING EXIT DOOR PROXIMITY LIGHT AND TESTED PER AMM 33-51-01-960-801; NO DEFECTS NOTED.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2023091198279Light · burned outMAIN PASSENGER CABIN FWD ENTRY DOOR EMERGENCY EXIT LIGHT HAS A BURNED-OUT BULB.<[01] RELAMPED MAIN CABIN FORWARD ENTRY DOOR PROXIMITY LIGHT AND TESTED PER AMM 33-51-01-960-801; NO DEFECTS NOTED.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2023091197925Bulb · inoperativeFOUND OUTSIDE LH OVW EXIT LIGHT AND RH FWD SERVICE DOOR EMERGENCY LIGHT INOP.<[01] REPLACED BULBS AND PERFORMED GOOD TEST OF OUTSIDE LH OVW EXIT LIGHT AND RH FWD SERVICE DOOR EMERGENCY LIGHT PER AMM 33-51-04-960-801.;[02] VERIFIED ACTION 1 IS COMPLETE;[03] VERSDR SWAA2023091197082Light · inoperativeL/H OVER WING EXIT LIGHT INOP.<[01] REPLACED L/H OVER WING EXIT LIGHT AND PERFORMED GOOD OPERATIONAL TEST PER AMM 33-51-01-960-801.;[02] CERTIFIED ACTION 1.;[03] VERIFIED CORRECTIVE ACTION #1SDR SWAA2023091293208Collar · damagedFWD ENTRY DOOR SURROUND AFT ASSIST HANDLE MOUNTING COLLARS DAMAGED.<[01] REMOVED FWD ENTRY DOOR SURROUND AFT ASSIST HANDLE MOUNTING COLLARS IAW AMM 25-21-31-420-801 STEP 2. B. (2); INSTALLED FWD ENTRY DOOR SURROUND AFT ASSIST HANDLE MOUNTING COLLARS IAW AMM 25SDR SWAA2023091392976Lens · damagedFWD SERVICE DOOR HEADER PANEL EXIT LIGHT LENS IS DAMAGED.<[01] REMOVED AND REPLACED FWD SERVICE DOOR HEADER PANEL EXIT LIGHT LENS IAW SOPM 20-50-01 #3.;[02] JOB COMPLETE.SDR SWAA2023091390394Panel · crackedPANEL 661BB INTERIOR SURFACE CRACKED.<[01] REPAIRED CRACK DAMAGE ON INTERIOR SURFACE OF PANEL 661BB IAW SRM 51-70-05-2R-2.;[02] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2023091190385Stringer Clip · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727E S-5L. MARKED<[01] REMOVED AND REPLACED NEW STRINGER CLIP AT PASSENGER CABIN BS727E S-5L IAW SRW 51-40-02-0G-0 AND DWG 146A1112;[02] VERIFIED MEASUREMENTS TABLE.<BR>VERIFIED CORRECTIVE ACTION 1; CARD COMPLETE.SDR SWAA2023091190386Stringer Clip · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727D S-4L. MARKED<[01] REMOVED AND REPLACED NEW STRINGER CLIP AT PASSENGER CABIN BS727D S-4L IAW SRW 51-40-02-0G-0 AND DWG 146A1111;[02] VERIFIED MEASUREMENTS TABLE.<BR>VERIFIED CORRECTIVE ACTION 1; CARD COMPLETE.SDR SWAA2023091190388Stringer Clip · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727C S-6L. MARKED<[01] REMOVED AND REPLACED NEW STRINGER CLIP AT PASSENGER CABIN BS727C S-6L IAW SRW 51-40-02-0G-0 AND DWG 146A1103;[02] VERIFIED MEASUREMENTS TABLE.<BR>VERIFIED CORRECTIVE ACTION 1; CARD COMPLETE.SDR SWAA2023091190387Stringer Clip · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727C S-5L. MARKED<[01] REMOVED AND REPLACED NEW STRINGER CLIP AT PASSENGER CABIN BS727C S-5R IAW SRW 51-40-02-0G-0 AND DWG 146A1103;[02] VERIFIED MEASUREMENTS TABLE.<BR>VERIFIED CORRECTIVE ACTION 1; CARD COMPLETE.SDR SWAA2023091190389Stringer Clip · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727B S-6L. MARKED<[01] REMOVED AND REPLACED NEW STRINGER CLIP AT PASSENGER CABIN BS727B S-6L IAW SRW 51-40-05-0G-0 AND DWG 146A1102;[02] CORRECTION: REMOVED AND REPLACED NEW STRINGER CLIP AT PASSENGER CABIN BS727B S-6SDR SWAA2023091190390Stringer Clip · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727B S-7L. MARKED<[01] REMOVED AND REPLACED NEW STRINGER CLIP AT PASSENGER CABIN BS727B S-7L IAW SRW 51-40-05-0G-0 AND DWG 146A1102;[02] CORRECTION: REMOVED AND REPLACED NEW STRINGER CLIP AT PASSENGER CABIN BS727B S-7SDR SWAA2023091190392Stringer Clip · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727A S-5L. MARKED<[01] REMOVED AND REPLACED NEW STRINGER CLIP AT PASSENGER CABIN BS727A S-5L IAW SRW 51-40-05-0G-0 AND DWG 146A1101;[02] CORRECTION: REMOVED AND REPLACED NEW STRINGER CLIP AT PASSENGER CABIN BS727A S-5SDR SWAA2023091190391Stringer Clip · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727A S-7L. MARKED<[01] REMOVED AND REPLACED NEW STRINGER CLIP AT PASSENGER CABIN BS727A S-7L IAW SRW 51-40-05-0G-0 AND DWG 146A1101;[02] CORRECTION: REMOVED AND REPLACED NEW STRINGER CLIP AT PASSENGER CABIN BS727A S-7SDR SWAA2023091190384Stringer Clip · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727C S-5R. MARKED<[01] REMOVED AND REPLACED NEW STRINGER CLIP AT PASSENGER CABIN BS727C S-5R IAW SRW 51-40-02-0G-0 AND DWG 146A1103;[02] VERIFIED MEASUREMENTS TABLE.<BR>VERIFIED CORRECTIVE ACTION 1; CARD COMPLETE.SDR SWAA2023091190393Stringer Clip · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS727B S-6R. MARKED<[01] REMOVED AND REPLACED NEW STRINGER CLIP AT PASSENGER CABIN BS727B S-6R IAW SRW 51-40-05-0G-0 AND DWG 146A1102;[02] CORRECTION: REMOVED AND REPLACED NEW STRINGER CLIP AT PASSENGER CABIN BS727B S-6SDR SWAA2023091390382Vapor Barrier · debondedRH VAPOR BARRIER BS 663 - DURING INSPECTION OF REMOVED VAPOR BARRIER; FOUND DISBOND TO BE 27' FROM O/B EDGE AND 9' FROM UPR EDGE. MARKED AREA.<[01] R/H VAPOR BARRIER BS 663 WITH DISBOND AT 27' FROM O/B EDGE AND 9' FROM UPR EDGE WAS REPAIRED IAW SRM 51-70-04-2RSDR SWAA2023091289905Shield · corrodedAFT CARGO BAY SHIELD HAS CORROSION BS 767+7 RBL 23 WL 156<[01] REMOVED AND REPLACED AFT CARGO BAY SHIELD; BS 767-794 RBL 23 WL 156 PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 146A0081.;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2023091289907Sidewall Support · corrodedAFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT HAS CORROSION BS 727C+7 TO BS 767+14 LBL 21 WL 156<[01] PARTIAL UPDATES TO STEP 3 & 4;[02] COMPLETED STEP 4;[03] COMPLETED STEP 5;[04] PARTIAL UPDATE TO STEP 3;[05] COMPLETED STEP 3SDR SWAA2023091289909Sidewall Support · corrodedAFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT HAS CORROSION BS 727A+10 TO BS 747+6 RBL 21 WL 156<[01] PARTIAL UPDATES ON STEP 3 & 4;[02] ADDED REFERENCES TO STEP 4;[03] COMPLETED STEP 5;[04] PARTIAL UPDATE TO STEP 3;[05] COMPLETED STEP 3SDR SWAA2023091289908Strap · corrodedAFT CARGO BAY FLOOR T STRAP HAS CORROSION BS 767+5 LBL 3 TO BL 0 WL 156<[01] RECEIVED NEW FLOOR T STRAP ON PO # 910723 APPLIED TOP COAT AS PER PREVIOUSLY ACCOMPLISHED ON ACO 5360-E-16462-NG AND MM 51-21-23-370-804 NEW T STRAP WILL BE INSTALL ON CARD # TTG8Q00LSDR SWAA2023091289910Strap · corrodedAFT CARGO BAY FLOOR T STRAP HAS CORROSION BS 727D+5 BL 0 TO RBL 13 WL 156<[01] RECEIVED NEW FLOOR T STRAP ON PO # 933979 APPLIED TOP COAT AS PER PREVIOUSLY ACCOMPLISHED ON ACO 5360-E-16462-NG AND MM 51-21-23-370-804 NEW T STRAP WILL BE INSTALL ON CARD # TTG8Q0SDR SWAA2023091290374Floorbeam · corrodedCORROSION ON FLOOR BEAM AT BS 986; LBL 43; WL 208 AT NUTPLATE HOLE.<[01] REMOVED CORROSION AT BS 986; LBL 43; WL 208 AT NUTPLATE HOLE PER SRM 51-10-02. DIMENSION OF BLEND IS 0.30'X 0.20' X 0.045' WITH REMAINING THICKNESS OF 0.105'. FOUND TO BE OUT OF LIMITS PESDR SWAA2023091290377Channel · corrodedCORROSION ON FWD ENTRY DOOR MOPSILL BS 294-310; LBL 65; WL 208.<[01] UPDATED STEP 1.;[02] UPDATED STEP 2.;[03] UPDATED MEASUREMENT TABLE.;[04] UPDATED STEP NUMBER 3.;[05] INSTALLED NEW FED MOPSILL BAS 294-3`0; LBL 65; WL 208 IAW SRM 51-40-02-0G-0; BOEING DOCUMSDR SWAA2023091190378Intercostal · crackedCRACKED INTERCOSTAL BS 277-294; RBL 1; WL 208.<[01] UPDATED MEASUREMENTS. UPON FURTHER INVESTIGATION; THERE'S NO ALLOWABLE DAMAGE AND PART WILL BE REPLACE IAW SRM 51-10-02 STEP 9. UPDATED STEPS 1 & 2.;[02] REMOVED AND REPLACED CRACK DAMAGED INTERCOSTAL AT BS27SDR SWAA2023091190379Intercostal · crackedCRACKED INTERCOSTAL BS 344-360; LBL 12; WL 208.<[01] COMPLETED MEASUREMENT TABLE.;[02] UPDATED STEP 1.;[03] COMPLETED STEP 2.;[04] COMPLETED STEP 1.SDR SWAA2023091190375Intercostal · crackedCRACKED INTERCOSTAL BS 380-400; LBL 13; WL 208.<[01] UPDATED STEP 1.;[02] STEP 2 COMPLETE; STEP 3 IN PARTIAL.;[03] COMPLETED MEASUREMENT TABLE.;[04] COMPLETED STEP 1.;[05] TASK CARD COMPLETE.SDR SWAA2023091189912Scuff Plate · crackedFORWARD CARGO BAY FORWARD CORNER SCUFF PLATE IS CRACKED<[01] APPLIED A CHEMICAL CONVERSION COATING TO BARE ALUMINUM SURFACES OF CORNER SCUFF PLATE PER SRM 53-30-15-2R-1 PARAGRAPH 4.B. (6) AND SOPM 20-43-03 TYPE 2; CLASS A OR C APPLIED 2 LAYERS OF BMS 10-11; TYSDR SWAA2023091189906Angle · corrodedAFT CARGO BAY INTERCOSTAL ANGLE BELOW SHIELD HAS CORROSION BS 767+12 RBL 23 WL 156<[01] REMOVE AND REPLACED INTERCOSTAL ANGLE BELOW SHIELD BS 767-787 RBL 23 WL 156 PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 146A 8123.;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2023091289427Floor Panel · brokenFWD FLOOR PANEL 221GF FWD O/B TANG IS BROKEN.<[01] REPAIRED FWD FLOOR PANEL 221GF FWD O/B TANG IAW SRM 53-00-50-2R-6.<BR><BR>ATTACHED CURE SHEETS TO FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEMS AND MEASUREMENT FIELDS; CARD COMPLETE.SDR SWAA2023091189756Intercostal · crackedCRACKED INTERCOSTAL; BS312; WL208; RBL20.5<[01] STEP 1 COMPLETE.;[02] TASK CARD COMPLETE.SDR SWAA2023091189428Floor Panel · pulledFWD FLOOR PANEL 221GF UPPER SKIN HAS AREAS OF PULLED STRANDS<[01] REPAIRED FWD FLOOR PANEL 221GF UPPER SKIN IAW SRM 53-00-50-2R-1 AND BOEING DWG 141A5810<BR><BR>ATTACHED CURE SHEETS TO FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEMS AND MEASUREMENT FIELDS; CARD CSDR SWAA2023091189429Floor Panel · pulledFWD FLOOR PANEL 222AF UPPER SKIN HAS AREA OF PULLED STRANDS<[01] REPAIRED UPPER SURFACE SKIN ON FWD FLOOR PANEL 222AF IAW SRM 53-00-50-2R-1 AND BOEING DWG 141A7810.<BR><BR>ATTACHED CURE SHEETS TO FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEM AND MEASUREMENT FIELSDR SWAA2023091189421Floor Panel · pulledFLOOR PANEL 242PF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL THE DAMAGE; DECIDED TO FABRICATE A NEW FLOOR PANEL WITH BMS4-23 TYPE II LOT 1531001-1 AND BMS5-107 LOT AK2KP8383K-1 RESIN; CURED THE RESIN; UNDER A HEAT LAMP; USING THERMOMSDR SWAA2023091189422Floor Panel · delaminatedFLOOR PANEL 242QF FWD O/B CORNER IS DELAMINATED.<[01] DELAMINATED BOARD WAS REPLACED WITH BOARD FABRICATED FROM RAW STOCK IAW SRM 53-00-50-2R-0 AND DRAWING 146A5810 SHEET 468.<BR><BR>UPLOADED CURE SHEET.<BR><BR>JOB COMPLETE.;[02] VERIFIED JOB COMPLETE; VERIFIESDR SWAA2023091189430Floor Panel · pulledAFT FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED THE PANEL IAW SRM 53-00-50-0I-1 FIGURE 6 AND TABLE 6. THE DAMAGE TO THE PANEL IS BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F AND WILL BE REPAIRED IAW SRM 53-00-50-2R-SDR SWAA2023091189431Floor Panel · pulledAFT FLOOR PANEL 241YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241YF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2023091189432Floor Panel · pulledAFT FLOOR PANEL 241ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ZF UPPER SKIN WITH AREAS OF PULLED STRAND WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[02] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUR
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