N447WN
Service difficulty reports · 396
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 = 'N447WN' 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 = 'N447WN' 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 SWAA2021091599397Web · corrodedCORROSION ON WEB AT AFT WET AREA BS1015 LBL38 WL208. ; / [01] REMOVED 1 EA FASTENER TO FOM PER SRM 51-40-02 AT DISCREPANCY AREA.; [02] REMOVED AND EVALUATED CORROSION REMOVAL AT DISCREPANCY AREA L= 1.3' W=0.8'. NO ALLOWABLE DAMAGE FOUND ON SRM. PART TO BE REPASDR SWAA2021091599416Web · corrodedCORROSION ON 1016 WEB AT AFT WET AREA BS 1026.5 LBL 16 WL 208 ; / [01] REMOVED 2 EA FASTENER TO FOM PER SRM 51-40-02 AT DISCREPANCY AREA.; [02] REMOVED AND EVALUATED CORROSION REMOVAL AT DISCREPANCY AREA L= 1.0' W=1.0'. NO ALLOWABLE DAMAGE FOUND ON SRM. PART TSDR SWAA2021091599393Channel · corrodedCORROSION ON MOP SILL AT AFT WET AREA BS 963 TO BS 994 RBL 46 WL 208 ; / [01] REMOVED AND EVALUATED CORROSION AT DISCREPANCY AREA. L=1' W=1.5. ORIGINAL THICKNESS 0.080' REMAINING 0.064' LOSS= 0.016' BLEND LOCATION FOUND TO BE OUT OF LIMITS PER SRM 53-70-15-1A-SDR SWAA2021091599413Web · corrodedCORROSION ON WEB AT AFT WET AREA BS987 RBL41.5 WL208. ; / [01] REMOVED 1EA FASTENER TO FOM PER SRM 51-40-02; [02] REMOVED AND EVALUATED CORROSION REMOVAL AT DISCREPANCY AREA L=1.0' W=1.0' . NO ALLOWABLE DAMAGE FOUND ON SRM. PART TO BE REPAIR BY REPLACEMENT PERSDR SWAA2021091599412Web · corrodedCORROSION ON WEB AT AFT WET AREA BS987 RBL39 WL208. ; / [01] REMOVED AND EVALUATED CORROSION REMOVAL AT DISCREPANCY AREA L= 1.3' W=1.0'. NO ALLOWABLE DAMAGE FOUND ON SRM. PART TO BE REPAIR BY REPLACEMENT PER SRM 51-10-02; [02] VERIFIED; DAMAGE NOT ALLOWED AT TSDR SWAA2021091599410Floorbeam · corrodedCORROSION ON FLOOR BEAM AT AFT WET AREA BS986.5 RBL32 WL208. ; / [01] ACCOMPLISHED PERMANENT REPAIR ON FLOOR BEAM AFT WET AREA BS986.5 RBL20-RBL51 WL208 IAW SRM 53-70-51-2R-4 REPAIR#4; IS DOCUMENTED ON TASK CARD# TTG8Q005Z33B; [02] REMOVED CORROSION ON FLOOR BSDR SWAA2021091599409Floor Support · corrodedCORROSION ON FLOORT SUPPORT AT AFT WET AREA BS991 LBL20 WL208. ; / [01] REMOVED AND EVALUATED CORROSION AT DISCREPANCY AREA. L=1.8' W=0.8' DEPTH= 0.030'. NO ALLOWABLE DAMAGE FOND ON SRM. PART TO BE REPAIR BY REPLACEMENT PER SRM 51-10-02; [02] VERIFIED; DAMAGE SDR SWAA2021091599407Floorbeam · corrodedCORROSION ON FLOOR BEAM AT AFT WET AREA BS 986.5 LBL 43 WL 208 ; / [20] INSTALLED REPAIR PARTS 4 EA ANGLES AND T FLOOR BEAM SECTION; INSTALLED NEW SHEAR TIE AT FLOOR BEAM BS 986.5 BETWEEN LBL 7.9 TO LBL 50 PER SRM 53-70-51-2R-4 REPAIR 4; [21] VERIFIED INSTALLESDR SWAA2021091599396Floorbeam · corrodedCORROSION ON FLOOR BEAM AT AFT WET AREA BS 986.5 LBL 35 WL 208 ; / [01] REMOVED CORROSION ON FLOOR BEAM AFT WET AREA BS 986.5 LBL 35 WL208 IAW SRM 51-10-02-0G-0 AND EVALUATED AREA AND FOUND TO BE OUT OF LIMITS IAW 53-70-51-1A-1 PART 4H MEASURES L=1.5'' X W=1.3SDR SWAA2021091599386Support Fitting · corrodedCORROSION ON FORWARD ENTRY DOOR FORWARD GIRT BAR FITTING SUPPORT AT B.S. 344; LBL 59; WL 208.1. ; / [01] REMOVED ON FWD ENTRY DOOR AFT GIRT BAR FITTING SUPPORT AT BS 344; LBL; 59; WL 208.1 IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9.C MUST BE REPAIRED BY REPLACEMSDR SWAA2021091599391Support Fitting · corrodedCORROSION ON FORWARD ENTRY DOOR FORWARD GIRT BAR FITTING SUPPORT AT B.S. 312; LBL 55; WL 208.1. ; / [01] REMOVED ON FWD ENTRY DOOR FWD GIRT BAR FITTING SUPPORT AT BS 312; LBL; 55; WL 208.1 IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9.C MUST BE REPAIRED BY REPLACEMSDR SWAA2021091599390Channel · corrodedCORROSION ON FORWARD ENTRY DOOR MOP SILL FROM B.S. 303.9 TO B.S. 348.2. LBL 58; WL 208.1 ; / [01] REMOVED CORROSION ON FWD ENTRY DOOR MOP SILL( INNER CHORD)LOCATED BTW BS.303 TO BS.348.2 LBL 58; WL 208.1 MEASUREMENTS L=7' X W= 1.5' X D=0.040 IAW SRM 51-10-02 PSDR SWAA2021091598742Former · crackedLT WING TO BODY FAIRING FORMER COMMON TO L/E SKIN. POSSIBLE CRACK EXTENDING OUT FROM FASTENER LOCATION. BS500D; WL190. ; / [01] FOR ACCESS REMOVED STRAP ASSY PN 149A7120-11. IAW SRM 51-40-02-0G-0; [02] REMOVED FAIRING FORMER PN 116A3118U9; COMMON TO L/E SKIN; SDR SWAA2021091598292Scuff Plate · corrodedCORROSION ON FORWARD ENTRY DOOR CENTER SCUFF PLATE INBOARD SUPPORT AT B.S. 314-338; L.B.L. 63; W.L. 208.1. ; / [01] REMOVED CORROSION ON FWD ENTRY DOOR CENTER SCUFF PLATE INBOARD SUPPORT BS 314-338 LBL 63; WL 208.1 IAW SRM 51-10-02-0G-0; BLENDED AREA IS L=18';SDR SWAA2021091598288Scuff Plate · corrodedCORROSION ON FORWARD ENTRY DOOR CENTER SCUFF PLATE OUTBOARD SUPPORT AT B.S. 320-336; L.B.L. 66; W.L. 208.1. ; / [01] REMOVED CORROSION ON FWD ENTRY DOOR CENTER SCUFF PLATE OUTBOARD SUPPORT BS 320-336 LBL 66; WL 208.1 IAW SRM 51-10-02-0G-0; BLENDED AREA IS L=22SDR SWAA2021091598297Stiffener · crackedLEFT HAND HORIZONTAL STABLILIZER INSPAR RIB; STATION 120.3; 3RD VERTICAL STIFFENER IS CRACKED. ; / [01] REMOVED THE DAMAGED PART AT LH HORIZONTAL STABILIZER STA 120.30 RIB 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4; [05] HFEC REQUEST ON THE CUT OUT EDGES; WESDR SWAA2021091598291Stiffener · crackedLEFT HAND HORIZONTAL STABLILIZER INSPAR RIB; STATION 120.3; 2ND VERTICAL STIFFENER IS CRACKED. ; / [01] REMOVED THE DAMAGED PART AT LH HORIZONTAL STABILIZER STA 120.30 RIB 2ND VERTICAL STIFFENER IAW SRM 55-10-09-2R-4; [02] UPDATED CHART MEASUREMENTS; [03] VERISDR SWAA2021091598001Panel · delaminatedPANEL 194CR OUTER SURFACE DELAMINATION; 7.75' FROM I/B END; 7.5' FROM FWD EDGE ; / [01] PART/MATERIAL IDENTIFIED IAW SRM 53-60-70-0I-1 FIG 2 TABLE 2 ITEM 6 .<BR>7/16 DIA DELAMINATION EXCEEDS THE ALLOWABLE LIMITS AS GIVEN IN SRM 53-60-70-1A-1 PARA 4 A (6) .<BR>SDR SWAA2021091598002Panel · delaminatedPANEL 194CR OUTER SURFACE DELAMINATION; 14' FROM I/B END; 8.25' FROM FWD EDGE ; / [01] PART/MATERIAL IDENTIFIED IAW SRM 53-60-70-0I-1 FIG 2 TABLE 2 ITEM 6 .<BR>7/16 DIA DELAMINATION EXCEEDS THE ALLOWABLE LIMITS AS GIVEN IN SRM 53-60-70-1A-1 PARA 4 A (6) .<BR>RSDR SWAA2021091505750Skin · debondedRIGHTI WING OUTBOARD AFT FLAP HAS AN AREA OF DISBOND ADJACENT TO THE INBOARD AFT CORNER OF THE TRAILING EDGE WEDGE. /SDR SWAA2021091597564Skin · chafedPANEL 194CR INNER SKIN MATING SURFACE IS CHAFED. / [01] IDENTIFIED PANEL 194CR / MATERIAL IAW SRM 53-60-70-0I-1 FIG. 2 TABLE 2 ITEM [6]. <BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-60-70-1A-1 PARA 4. B. (8). FIG. 105. <BR><BR>REPAIR TO BE ACCSDR SWAA2021091597565Panel · chafedPANEL 194CR OUTER SKIN IS CHAFED IN MIDDLE OF THE OUTBOARD EDGE. (MARKED) / [01] PART/MATERIAL IDENTIFIED IAW SRM 53-60-70-0I-1 FIG 2 TABLE 2 ITEM 6 .<BR>DAMAGE AT THE OUTER SKIN EDGE BAND EXCEEDS THE ALLOWABLE LIMITS AS GIVEN IN SRM 53-60-70-1A-1 PARA 4 B (3)SDR SWAA2021091597563Panel · chafedPANEL 194CL INNER SKIN MATING SURFACE IS CHAFED. / [01] IDENTIFIED PANEL 194CL / MATERIAL IAW SRM 53-60-70-0I-1 FIG. 2 TABLE 2 ITEM [6].<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-60-70-1A-1 PARA 4. B. (3) (A) NOTE: (5) (A).<BR>REPAIR TO BE ACCOMSDR SWAA2021091598005Support · crackedBULB SEAL RETAINER SUPPORT IS CRACKED AT LOWER FASTENER HOLE AT LEFT WING FIXED T/E PANEL JUST AFT OF THE PYLON. ; / [01] LOCATED AND DRILLED WEB ASSY IAW SRM 51-40-02. OK TO INSTALL.; [02] VERIFIED CORRECTIVE ACTION STEP 1. VERIFIED OK TO INSTALL.; [03] INSTASDR SWAA2021091597556Skin · debondedRIGHTI WING OUTBOARD AFT FLAP HAS AN AREA OF DISBOND ADJACENT TO THE INBOARD AFT CORNER OF THE TRAILING EDGE WEDGE. / [01] IDENTIFIED MATERIAL OF R/H O/B AFT FLAP IAW SRM 57-53-01-0I-4 FIGURE 1 AND 2; ITEM 2; 4 AND 5; TABLE 2.<BR><BR>DAMAGE IS OUT OF ALLOWABLESDR SWAA2021091597550Support · crackedRIGHT WING UPPER VERTICAL BULB SEAL RETAINER SUPPORT AFT OF #2 PYLON IS CRACKED. ; / [01] REMOVED AND REPLACED UPPER VERTICAL BULB SEAL RETAINER SUPPORT IAW SRM 51-40-02-0G-0; OK TO INSTALL.; [02] OK TO INSTALL; [03] INSTALLED UPPER VERTICAL BULB SEAL RETAINERSDR SWAA2021091597551Support · crackedRIGHT WING LOWER VERTICAL BULB SEAL RETAINER SUPPORT AFT OF #2 PYLON IS CRACKED. ; / [01] REMOVED AND REPLACED LOWER VERTICAL BULB SEAL RETAINER SUPPORT IAW SRM 51-40-02-0G-0; OK TO INSTALL.; [02] OK TO INSTALL; [03] INSTALLED LOWER VERTICAL BULB SEAL RETAINERSDR SWAA2021072797531Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK AT B.S. 767+15; L.B.L. 45; W.L. 208.1. REMOVED CORROSION, REWORKED AREA L=8' W=1' D=0.015' WAS FOUND WITHIN THE LIMITS IAW SRM 53-00-52-1A-1 STEP 4 A(2)A FIG.103. APPLIED A CHEMICAL CONVERSION COATING & ONE LAYER OF SDR SWAA2021091597509Bear Strap · crackedFORWARD GALLEY DOOR BEAR STRAP; BETWEEN S-8R AND 9R; BS291.- BS294.5 CRACKED APROX. 2.800' ; / [01] TRIMED OUT AND REMOVED THE DAMAGED AREA AT BEARSTRAP FWD GALLEY DOOR BETTWEEN S-8R AND S-9R BS 293 L=3.4; W=3 PER SRM 53-10-01-2R-6 REP. 6; [02] DO A HEFC EDDY SDR SWAA2021091597501Attach Angle · crackedB.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 9; W.L. 164. ; / [01] INSTALLED WIRE BUNDLE PROTECTION AROUND THE REPAIR AREA IAW AMM 20-60-07-913-801; [02] TRIMED OUT DAMEGE AREA AT UPPER ANGLE BAPPOR BARRIER BS663 LBL 13 PER SRM 57-SDR SWAA2021091597482Attach Angle · crackedB.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 9; W.L. 164. ; / [01] INSTALLED WIRE BUNDLE PROTECTION AROUND THE REPAIR AREA IAW AMM 20-60-07-913-801; [02] TRIMED OUT DAMAGED ANGEL AT RBL 13 BS 663 R/H SIDE UPPER ANGLE PER SRM 57-10-SDR SWAA2021091597149Pressure Deck · crackedCRACK AT LBL-32 BS-663+2 WL-201; CRACK APPROXIMATELY 1 INCH LONG; COMMON TO HORIZONTAL BEADED PRESSURE DECK. ; / [02] HORIZONTAL BEADED PRESSURE DECK AT LBL32 ; BS 663 + 2'; WL 201 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE IN SRM. IT WILL BE REPAIRESDR SWAA2021091597150Stub Frame · crackedCRACK FOUND ON FSD FWD INNER CUTOUT; BS 294.5+5; RBL 48; WL 266 (MARKED) ; / [01] REMOVED STOP FRAME SUPPORT AT FSD FWD INNER CUTOUT BS 294.5 PER SRM 51-40-02; [02] CORRECTING 'STOP FRAME' TO STUB FRAME.; [03] LOCATED AND DRILLED FSD UPPER STUB FRAME PN#141A83SDR SWAA2021052474962Seal · crackedRIGHT HORIZONTAL STABILIZER UPPER SLIDING SEAL CRACKED ; / REMOVED AND REPLACED RIGHT HAND UPPER SLIDING SEAL ON RIGHT HORIZONTAL PER MM 53-31-31SDR SWAA2021052474961Seal · crackedLEFT HORIZONTAL STABILIZER UPPER SLIDING SEAL CRACKED ; / R&R SLIDING SEAL PER MM REF 53-31-31SDR SWAA2021052474960Battery Pack · no testEMERGENCY LIGHT BATTERY PACK AT LOCATION M1673 FAILED CAPACITY CHECK ; / R&R EMERGENCY LIGHT BATTERY PACK AT LOCATION M1673 PER AMM 33-51-06SDR SWAA2021052474959Battery Pack · no testEMERGENCY LIGHT BATTERY PACK AT LOCATION M1670 FAILED CAPACITY CHECK ; / R&R EMERGENCY LIGHT BATTERY PACK AT LOCATION M1670 PER AMM 33-51-06SDR SWAA2021052474952Battery Pack · no testEMERGENCY LIGHT BATTERY PACK M1668 FAILED CAPACITY CHECK ; / R&R EMERGENCY BATTERY PACK AT LOCATION M1668 PER AMM 33-51-06SDR SWAA2020070898108Lens · unsecureEMERGENCY EXIT LENS CAME OFF. LOWER LENS AT RT OVERWING EXIT ON WALL. REINSTALLED LENS PER MM 33-51-11.SDR SWAA2019112539068Battery · no testEMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672 IN THE CABIN. / R&R BATTERY PER AMM.SDR SWAA2022032149819Angle · crackedAFT CARGO CENTER BULKHEAD SUPPORT ANGLE STA 947.5 LBL 23 CRACKED. / REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-40-02SDR SWAA2022032149813None · elongatedAFT CARGO B.S. 807 RBL 13 AFT CARGO FLOOR STRUCTURE CLIP HAS ELONGATED HOLES. / REMOVED AND REPLACED CLIP PER SRM 51-40-02SDR SWAA2022032149811Skin · crackedRIGHT WING ZONE #2 LEADING EDGE FASTENER; HOLE #8(NUMBERED FROM THE PYLON TO THE FUSELAGE) HAS A CRACK INDICATION IN THE SKIN ONLY. VERIFIED WITH NDT INSPECTION OF HOLE PER BOEING NDT MANUAL PART 6 51-00-00 PROC.23 AND PART6; 53-30-00 PROC.4. HOLE IS CURRENTLYSDR SWAA2022032149812Skin · crackedRIGHT WING ZONE #2 LEADING EDGE FASTENER; HOLE #9(NUMBERED FROM THE PYLON TO THE FUSELAGE) HAS A CRACK INDICATION IN THE SKIN ONLY. VERIFIED WITH NDT INSPECTION OF HOLE PER BOEING NDT MANUAL PART 6 51-00-00 PROC.23 AND PART6; 53-30-00 PROC.4. HOLE IS CURRENTLYSDR SWAA2019092537185Floorbeam · corrodedAFT CARGO FLOORBEAM CORRODED AT BS 767+5, RBL 13.84. REPAIRED FLOOR BEAM PER SRM AND EA.SDR SWAA2022032949800Strip · corroded6EA AFT CARGO FLOOR TO SIDE WALL PANEL CAP STRIPS CORRODED.(MARKED) / REMOVED AND REPLACED 6 EACH AFT CARGO FLOOR TO SIDEWALL PANEL CAP STRIPS PER AMM 25-52-10.SDR SWAA2022032949801Angle · corrodedAFT CARGO COMPARTMENT - R/H SIDE TRANSITION ANGLE BETWEEN FUSELAGE STATION 767 AND STATION 787 - UNDERLYING STRUCTURE. THE ANGLE THAT ATTACHES TO THE BOTTOM SIDE OF THE TRANSITION ANGLE AT THAT LOCATION HAS CORROSION ON THE BOTTOM SIDE AROUND THE NUTPLATES. / SDR SWAA2022032949773Door · corroded145AL HAS SURFACE CORROSION AT TOP OF PANEL / E56288-MARTIN; DUSTYN - 09/19/2019 09:58 COMPLETE: REMOVED AND REPLACED LAV DOOR ASSY (145AL) PN# 146A7410-7 PER AMM 52-49-07SDR SWAA2022032949774Angle · crackedFORWARD CARGO RH TRANSITION ANGLE CRACKED AT STA 500A; RBL 22. / REMOVED AND INSTALLED NEW SECTION RH TRANSITION ANGLE FROM STA.500A TO STA.500D ( P/N # 143A7501-4 ) PER SRM 51-40-02 .SDR SWAA2022032949794Angle · corrodedREPLACE AFT CARGO R/H TRANSITION ANGLE FROM STA. 727-767 TO COMPLY WITH MULTIPLE CORROSION N/R CARDS. / REMOVED AND REPLACED AFT. CARGO R/H TRANSITION ANGLE FROM STA. 727+5 TO 767 (PART REPLACED #146A7502-2 ) PER SRM. 51-10-02
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