N295WN
Service difficulty reports · 291
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 = 'N295WN' 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 = 'N295WN' 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 SWAA2023062955205Floor Panel · pulledAFT CABIN FLOOR PANEL 241VF HAS A PULLED THROUGH INSERT HOLE<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW FLOOR PANEL USING BMS4-23 TYPE II LOT 1525675-1 AND BMS5-107 LOT AK2KP8383K-1 RESIN; CURED RESIN WITH A HEAT LAMP USING THERMOMSDR SWAA2023062955231Floor Panel · brokenFWD CABIN FLOOR PANEL 221BF AFT O/B CORNER IS BROKEN (TANG)<[01] IDENTIFIED PANEL 221BF IAW SRM 53-00-50-0I-1 FIGURE 2. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.E.(2).(B) AND WILL BE REPAIRED IAW SRM 53-00-50-2R-6. REMOVED NUMEROUS ISDR SWAA2023062955233Floor Panel · brokenFWD CABIN FLOOR PANEL 221GF FWD O/B CORNER IS BROKEN (TANG)<[01] IDENTIFIED FLOOR PANEL 221GF IAW SRM 53-00-50-0I-1 FIGURE 2 TABLE 2 <BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR.4 B<BR><BR>DAMAGE TO BE REPAIRED IAW SRM 53-00-50-2R-1SDR SWAA2023062955204Floor Panel · pulledAFT CABIN FLOOR PANEL 241VF HAS A PULLED THROUGH INSERT HOLE<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW FLOOR PANEL USING BMS4-23 TYPE II LOT 1525675-1 AND BMS5-107 LOT AK2KP8383K-1 RESIN; CURED RESIN WITH A HEAT LAMP USING THERMOMSDR SWAA2023062954825Stringer · crackedSTRINGER S-24L IS CRACKED AT STA 540.<[01] CRACK FOUND OUT OF LIMITS ON STRINGER S-24L BS 535 SKIN ATTACHMENT FLANGE 100% OF MATERIAL THICKNESS L=0.5' IAW SRM 53-00-03-1A-1;[02] VERIFIED APPLICABILITY OF SRM 53-00-03-2R-1 REP.1. FOR STRINGER S-24L BS 535 SKIN SDR SWAA2023062954821Stringer · crackedSTRINGER S-25R IS CRACKED AT STA 540.<[01] REMOVED DAMAGED SECTION OF STRINGER S-25R BS 500D+10' - BS 535 IAW SRM 53-00-03-2R-1 REP.1 PAR 4 A-B AND EA 23-153-01768;[02] PERFORMED A GVI ON REPAIR AREA OF STRINGER S-25R BS 500D+10' - BS 535 AND NOT FOUND ADDITIOSDR SWAA2023062954823Stringer · crackedSTRINGER S-26L IS CRACKED AT STA 540.<[01] CRACK FOUND OUT OF LIMITS ON STRINGER S-26L BS 535 SKIN ATTACHMENT FLANGE 100% OF MATERIAL THICKNESS L=0.5' IAW SRM 53-00-03-1A-1;[02] VERIFIED APPLICABILITY OF SRM 53-00-03-2R-1 REP.1. FOR STRINGER S-26L BS 535 SKIN SDR SWAA2023062954819Stringer · corrodedCORROSION ON STRINGER S-23R FROM STA 520+18 TO STA 540.<[01] CORROSION FOUND OUT OF LIMITS ON STRINGER S-23R BS 535 SKIN ATTACHMENT FLANGE 100% OF MATERIAL THICKNESS LOSS L=1' X W=0.5' IAW SRM 53-00-03-1A-1;[09] RECEIVED PARTS NEW STRINGER SECTION OF STR-23R RSDR SWAA2023062955285Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 380-400; RBL 10; WL 208 IS CRACKED.<[01] NO ENTRIES FOUND ON SRM FOR PASSENGER CABIN FLOOR SUPPORT BS 380-400; RBL 10; WL 208 PART TO BE REMOVED AND REPLACED PER SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED PASSENGER CABIN FLOOR SUPPSDR SWAA2023062955287Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 380-400; LBL 15; WL 208 IS CRACKED.<[01] NO ENTRIES FOUND ON SRM FOR CRACKED INTERCOSTAL UPPER ATTACH ANGLE STA 380-400; LBL 15; WL 208 PART TO BE REMOVED AND REPLACED PER SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED CRACKED INTERCOSSDR SWAA2023062955283Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 380-400; RBL 1; WL 208 IS CRACKED.<[01] NO ENTRIES FOUND ON SRM FOR PASSENGER CABIN FLOOR SUPPORT BS 380-400; RBL 1; WL 208 PART TO BE REMOVED AND REPLACED PER SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED PASSENGER CABIN FLOOR SUPPORSDR SWAA2023062955277Girt Bar · out of adjustFWD ENTRY DOOR FWD GIRT BAR MOUNTING BRACKET INBOARD FASTENER IS LOOSE.<[01] DISCREPANCY TO BE ACCOMPLISHED ON COSTUMER CARD TTG8Q00LDPKH INSTALLATION OF MOPSILL I.A.W SRM 51-40-02-0G-0;[02] VERIFIEDSDR SWAA2023062955263Stub Frame · crackedPASSENGER CABIN STUB FRAME TO MOPSILL ATTACH ANGLE; OUTBOARD OF MOPSILL; BS 294.5; RBL 65; WL 208 IS CRACKED<[01] AFTER FURTHER INVESTIGATION CRACKED PASSENGER CABIN STUB FRAME TO MOPSILL ATTACH ANGLE; OUTBOARD OF MOPSILL; BS 294.5; RBL 65; WL 208 FOUND CRACK SDR SWAA2023062954829Shield · elongatedFORWARD CARGO BAY AFT SHIELD HAS AN ELONGATED FASTENER HOLE BS495 RBL22 WL 156<[01] ELONGATED HOLE ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION 1;[03] UPDATE TO CORRECTIVE ACTION STEP 1. ELONGATSDR SWAA2023062955255Bracket · brokenAFT CARGO BAY LAV TANK BULKHEAD LOWER BRACKET IS BROKEN BS867 LBL10 WL166<[01] REMOVED DAMAGED ACB LAV TANK BULKHEAD LOWER BRACKET BS 867; LBL10; WL166 PER SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED ACB LAV TANK BULKHEAD LOWER BRACKET BS 867; LBL10; WL166 PERSDR SWAA2023062655268Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 312-328; LBL 45; WL 208 IS CRACKED.<SDR SWAA2023062655262Stub Frame · crackedPASSENGER CABIN STUB FRAME TO MOPSILL ATTACH ANGLE; OUTBOARD OF MOPSILL; BS 294.5; RBL 65; WL 208 IS CRACKED<SDR SWAA2023062655258Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 277-294; RBL 1; WL 208 IS CRACKED.<SDR SWAA2023062655259Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 277-294; RBL 1; WL 208 IS CRACKED.<[01] VERIFIED APPLICABILITY PER SRM 53-10-51-1A-1 ALLOWABLE DAMAGE 1;[02] CRACKED PASSENGER CABIN FLOOR SUPPORT BS 277-294; RBL 1; WL 208 EXCEED ALLOWABLE LIMITS ON SRM 53-10-51-1A-1 ALLOWABLESDR SWAA2023062655269Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 312-328; LBL 45; WL 208 IS CRACKED.<[01] VERIFIED APPLICABILITY OF SRM 53-10-51-1A-1;[02] CRACKED PASSENGER CABIN FLOOR SUPPORT BS 312-328; LBL 45; WL 208 EXCEED ALLOWABLE LIMITS ON SRM 53-10-51-1A-1 ALLOWABLE DAMAGE 1 PAR 4.B SDR SWAA2023062655297Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 344-360; LBL 3; WL 208 IS CRACKED.<[01] VERIFIED APPLICABILITY OF SRM 53-10-51-1A-1;[02] CRACKED PASSENGER CABIN FLOOR SUPPORT BS 344-360; LBL 3; WL 208 EXCEED ALLOWABLE LIMITS ON SRM 53-10-51-1A-1 ALLOWABLE DAMAGE 1 PAR 4.E SRSDR SWAA2023062655296Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 344-360; LBL 3; WL 208 IS CRACKED.<SDR SWAA2023062655286Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 380-400; LBL 15; WL 208 IS CRACKED.<SDR SWAA2023062655284Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 380-400; RBL 10; WL 208 IS CRACKED.<SDR SWAA2023062655282Floor Support · crackedPASSENGER CABIN FLOOR SUPPORT BS 380-400; RBL 1; WL 208 IS CRACKED.<SDR SWAA2023062954801Vapor Barrier · debondedR/H VAPOR BARRIER HAS DISBONDED REPAIRS BS663 RBL 35 WL 178<[01] IDENTIFIED R/H VAPOR BARRIER IAW SRM 57-10-10-0I-2 TABLE 2; FIG 2; ITEM 4.<BR><BR>DAMAGE IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10-1A-2 PARA 4.D (1).<BR><BR>DAMAGE WILL BE REPAIRED IAW SSDR SWAA2023053052469Compensator · inoperativeLEFT FUEL IMBALANCE OF 1200 LB AFTER DEPARTING BUR WITH MORE THAN 1000 LB IN CENTER TANK WITH CTR; #1 & #2 FUEL PUMPS. PERFORMED TANK & COMPENSATOR UNIT RESISTANCE & CAPACITANCE CHECK IAW AMM 28-41-21-710-801. FOUND COMPENSATOR CAPACITANCE VALUE OUT OF LIMITSDR SWAA2023032720603Slide · looseFWD SERVICE DOOR SLIDE BAR RETAINER BRACKET LOOSE<[01] REPLACED RIVET ON FWD SERVICE DOOR SLIDE PER SRM 51-40-02SDR SWAA2023032017395Engine · failedAFTER TAKEOFF LARGE RPM FLUCTUATION NR 2 ENGINE, SPARKS WERE REPORTED BY PASSENGER. NO OVERWEIGHT LANDING. LOUD POPPING SOUNDS FROM NR 2 ENG. REMOVED AND REPLACED NR 2 ENGINE IAW AMM 71-00-02 & MT 771-00-01.SDR SWAA2023021300477Pump · stalledON CLIMB OUT; #2 ENGINE WAS UNRESPONSIVE TO THRUST LEVER MOVEMENT. TOPPED OUT ABOUT 86.4% N1 EGT 40-90 WARMER THEN #1. RAN ENGINE LIMIT SURGE STALL QRH AND RECOVERED NORMAL ENGINE OPERATIONS EGT REMAINS STABLE 40 DEG. WARMER THEN #1.<[01] REMOVED AND REPLACED SDR SWAA2023020698832Valve · faulty#2 ENG COMP STALL<[01] SEE FOUND FAULTS TTG8Q00HMT8Y TTG8Q00HMT1Q TTG8Q00FTQP7 TTG8Q00CYJR7 TTG8Q00HMYNQ TTG8Q00HN801 FOR CORRECTIVE ACTIONS ALSO PERFORMED FIM TASK 71-05 TASK 805 AND AMM 71-00-00-210-801-F00SDR SWAA2022040489212Hmu · faultedCLIMBING THROUGH 2;500- LOUD BANG FROM NUMBER 2 ENG FOLLOWED BY FLAMES FROM TAILPIPE- 30 SEC LATER ANOTHER BANG FOLLOWED BY FLAMES AND SPARKS FROM TAILPIPE. RETURNED TO MKE NORMAL LANDING. ALL ENGINE PARAMETERS WHERE NORMAL NO INDICATIONS OF FIRE / [01] R&R?D SDR SWAA2022020164877Bulb · inoperativeLH OVERWING EXIT EMERGENCY SIGN HAS ONE LIGHT INOP. ; / [01] RELAMPED LH OVERWING EXIT EMERGENCY SIGN AFT BULB IAW AMM 33-51-01.SDR SWAA2021072797424Skin · delaminatedR/H OUTBD AFT FLAP HAS DELAM INBD LOWER CORNER. REMOVED AND REPLACED R/H OUT/BD AFT FLAP AS PER AMM 27-51-22.SDR SWAA2021080591695Angle · elongatedFORWARD CARGO TRANSITION ANGLE RBL21 HAS NUMEROUS FASTENER HOLES ELONGATED AND DOUBLE DRILLED AT STA494 (MARKED) ; / [01] OVER SIZED THE HOLES TO .216 PER SRM 51-40-05 OK TO INSTALL TRANSITION ANGLE; [02] VERIFIED OVER SIZED THE HOLES TO .216 PER SRM 51-40-05 SDR SWAA2021080591696Angle · corrodedFORWARD CARGO TRANSITION ANGLE RBL21 HAS CORROSION AROUND NUMEROUS FASTENER HOLES STA500 TO STA500A (MARKED) ; / [01] REMOVED AND REPLACED TRANSITION ANGLE FROM STA 500-520 PER SRM 51-10-02;51-40-02; [02] VERIFIED INSTALLATIONSDR SWAA2021080591694Angle · corrodedFORWARD CARGO TRANSITION ANGLE LBL21 HAS CORROSION AROUND FASTENER HOLES STA500+10 TO 500B++10 (MARKED) ; / [01] BLENDED AREAS OF CORROSION AT FWD CARGO TRANSITION ANGLE; STA. 500+10 TO STA.500B+10 LBL 21. REMOVED 0.008; ALLOWED 0.004; BLENDS OUT OF LIMITS ALLSDR SWAA2021080591698Angle · corrodedFORWARD CARGO TRANSITION ANGLE LBL21 HAS CORROSION NUMEROUS FASTENER HOLES STA500B+10 TO 500D (MARKED) ; / [01] BLENDED AREAS OF CORROSION ON FWD CARGO TRANSITION ANGLE STA. 500B+10 TO STA.500D; REMOVED 0.005; ALLOWED 0.004; BLENDS OUT OF LIMITS ALL IAW SRM 53SDR SWAA2021080591705Angle · corrodedAFT CARGO LEFT SIDE TRANSITION ANGLE HAS CORROSION F.S. 727D TO 807. ; / [01] BLENDED/REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED DAMAGED TRANSITION ANGLE. ORIGINAL THICKNESS = .040'. REMAINING THSDR SWAA2021080591702Angle · corrodedAFT CARGO RIGHT SIDE TRANSITION ANGLE HAS CORROSION F.S. 727D TO 767. ; / [01] BLENDED/REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED DAMAGED TRANSITION ANGLE. ORIGINAL THICKNESS = .040'. REMAINING TSDR SWAA2021080591699Angle · corrodedAFT CARGO RIGHT SIDE TRANSITION ANGLE HAS CORROSION F.S.727A TO 727B. ; / [01] BLENDED/REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED DAMAGED TRANSITION ANGLE. ORIGINAL THICKNESS = .040'. REMAINING TSDR SWAA2021080591697Angle · corrodedAFT CARGO RIGHT SIDE TRANSITION ANGLE HAS CORROSION FORWARD OF CARGO DOOR CUTOUT AT BS 767 TO 787. BLENDED/REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED DAMAGED TRANSITION ANGLE. DRILLED UP REPLASDR SWAA2021080591704Angle · corrodedAFT CARGO LEFT SIDE TRANSITION ANGLE HAS CORROSION BS 727 TO 727D. BLENDED/REMOVED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED DAMAGED TRANSITION ANGLE. REMOVED AND REPLACED THE TRANSITION ANGLE IAW SRMSDR SWAA2021080591262Floor Panel · damagedFLOOR PANEL 241AF HAS AREAS OF DAMAGE TO UPPER SURFACE. REMOVED AND REPLACED FLOOR PANEL 241AF PER AMM 53-21-00.SDR SWAA2021080591263Floor Panel · damagedFLOOR PANEL 241BF HAS AREAS OF DAMAGE TO UPPER SURFACE. ; REMOVED AND REPLACED 241BF PER AMM 53-21-00.SDR SWAA2021080591265Floor Panel · damagedFLOOR PANEL 242AF HAS AREAS OF DAMAGE TO UPPER SURFACE. REMOVED AND REPLACED FLOOR PANEL PER AMM 53-21-00.SDR SWAA2021080591266Floor Panel · damagedFLOOR PANEL 242BF HAS AREAS OF DAMAGE TO UPPER SURFACE. ; / [01] R&R'D FLOOR PANEL PER MM 53-21-00 R&R FLOOR PANEL PER MM 53-21-00.SDR SWAA2021080990181Fitting · damaged#1 ENGINE AFT O/B PYLON FITTING HAS DAMAGE FROM MAKING CONTACT WITH AFT UPPER METAL FIRE SEAL ON O/B T/R.(MARKED) ; / [01] REMOVED DAMAGE ON #1 ENGINE AFT O/B GSE BOOTSTRAP FITTING.MEASURING 1INCH DOWN FROM TOP OF STRUT BOX TO FORWARD O/B FLANGE EDGE OF FITTINSDR SWAA2021080990173Skin · chafedRIGHT HAND WING INBOARD GROUND SPOILER #7 O/B LEADING EDGE LOWER SURFACE IS CHAFED.(MARKED) ; / [01] #7 GROUND SPOILER TO BE REPLACED ON CARD# TTG8Q005NZHO.; [02] CARD # SHOULD BE TTG8Q005NZH0; [03] C/W; [04] VERIFIED.SDR SWAA2021080990164Angle · bentLEFT WING PNL 551FB FWD ATTACH ANGLE IS BENT. ; / [01] REMOVED AND REPLACED FWD ATTACH ANGLE ON PANEL 551FB PER SRM 51-40-02
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