JASC 5350
Service difficulty reports · 6,123
Reports filed under 5350 · Aerodynamic Fairings, 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 jasc_code = '5350' 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 jasc_code = '5350' 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 SWAA2022041221393Panel · crackedPANEL 194E ONE FASTENER HOLE HAS CRACKS IN THE COMPOSITE FROM THE BACKSIDE; AS MARKED. / REPAIRED AND RESTORED TEFLON DECORATIVE FINISH TO PANEL 194E FASTENER HOLE IAW B737-700-SRM 53-60-70-1A-1 REV 69; 51-70-08-0G-0 GENERAL REV 69 51-30-10-0G-0 GENERAL REV 69SDR SWAA2022041227862Panel · delaminatedPANEL 193AR HAS 2 DELAMINATED DENTS ON THE EXTERNAL SKIN / REPAIRED 2 DELAMINATED DENTS ON THE EXTERNAL SKIN OF PANEL 193AR PER SRM 51-70-05-2R-2 PARA 4A-K 59654U 12-17-19. 20021C 17DEC19SDR DALA2019121007199Longeron · crackedFOUND CRACK WING TO BODY LONGERON CRACKING ON L/H SIDE JUST AFT OF AFT E/E ACCESS DOOR. REMOVED PANEL 195HB PER A220 AMP BD500-A-J53-82-85-01AAA-520A-A AND PANEL 195JB PER TASK BD500-A-J53-82-85-04AAA-502A-A. REMOVED LONGERON ASSY P/N C02383111-001, REMOVED FRSDR SWAA2022041251180Access Panel · delaminatedACCESS PANEL 521ZB DELAMINATED. DOT 221-02 / CLEANED AND REQUIIRED AT ACCESS PANEL 521ZB PER B737-700 SRM 51-70-0G-2R-6 MATERIAL USED P.O. 1190381; P.O. 1624260 AND P.O. 614988SDR SWAA2022041251174Access Panel · brokenACCESS PANEL 194BR ; CORNER BROKEN. DOT 221-01 / CLEANED AND REPAIRED DAMAGE AREA ON CORNER OF ACCESS PANEL 194BR SIZE 2' DIAMETER WITH A PERMANENT WET LAY UP REPAIR AS PER B737 SRM 51-70-04-2R-10 REPAIR #10 MATERIAL USED PO # 1624260 AND PO # 1129190. PRIME ASDR SWAA2022041143727Panel · pulledPANEL 193B HAS SEVERAL COUNTERSINKS PULLED THRU. / REMOVED AND REPLACED PANEL PER AMM 20-50-11.SDR SWAA2022041100026Panel · elongatedPANEL 193B HAS ELONGATED FASTENER HOLES. / REPLACED PANEL 193B PER EO# 14108 AND SRM 51-40-02SDR SWAA2022041106046Panel · elongatedWING TO BODY FAIRING PANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES. / REMOVED AND REPLACED 193B PANEL REF AMM 53-51-21 .SDR SWAA2022040733416Panel · delaminated193B PANEL HAS DELAMATION ON THE TRAILING EDGE / REPLACED PNL 193B REF SRM 51-40-02; AND AMM 53-51-21 ASDR SWAA2022041107161Panel · delaminatedDELAMINATION ON PANEL # 195LR / REMOVED DAMAGE PANEL AND REPLACED WITH SERVICEABLE PANEL PER AMM 53-51-21SDR SWAA2022041107160Panel · delaminatedDELAMINATION ON PANEL # 194AR / REMOVED DAMAGED PANEL AND REPLACED WITH SERVICEABLE PANEL PER AMM 53-51-21SDR SWIA2020012147838Fairing · chafed* RIGHT WING TO BODY INBOARD AT STUB FAIRING, MULTIPLE CHAFE MARKS. (C-CHECK) RO:1/17/2020REPLACED CHAFED R/H STUB FAING ASSY. WITH NEW FAIRING ASSY AND HARDWARE. REF CRJ-200 SRM CRJ-200 SRM, CRJ-200 SRM REF CRJ-200 SRM AND DRW, PERFORMED CLEARANCE CHECSDR SWAA2022041126012Tail Cone · delaminatedEMPENAGE TAIL CONE LEFT HAND SIDE WHERE ELEVATOR SEAL RUBS HAS AN AREA OF DELAMINATION / REPAIRED EMPENAGE TAIL CONE 4H SIDE AREA OF DECLAMINATION I/A/W B737-700 SRM'S 53-80-70-2R-1 REV 69+51-70-04-2R-1 REV 69+ 51-70-04-2R-0 REV 69 AND B737-700 AMM 51-21-99-30SDR DALA2019120407040Longeron · crackedWHILE WORKING WRITE UP RT WING TO BODY LONGERON CRACK FOUND. REMOVED LONGERON 846371 COMPLETED WITH STEP ONE OF RI 583549-14 WIP329603 COMPLETED HFEC PER A220 ANDTP BD5000-A-J51-10-05-00AAA -353A-A ALL CRACKS MARKED QC2047 786880 COMPLETED STEP 4 AND 5 OF RI58SDR SWAA2022040748261Panel · delaminatedBELLY PANEL 192K (149A7753-3) IS DELAMINATED (OUTER LAYER OF FIBERGLASS PEELED OFF).INSTALLED PANEL 149A7753-2 PER EA OTHER-53EA-07525 PANEL MUST BE REMOVED AND INSTALL SERVICEABLE 149A7753-3 PANEL WITHIN 7 DAYSPERMANENT ACTION REQUIRED:REMOVE THE 149A7753-2 PSDR SWAA2022041122735Panel · delaminatedPANEL 191FL HAS DELAMINATION ON THE LOWER AFT EDGE / REPAIRED DELAMINATION ON THE LOWER AFT EDGE OF PANEL 191FL IAW SRM 51-70-05-2R-6 7062U 12-8-19SDR SWAA2022032548342Panel · delaminatedBELLY PANEL 192K (149A7753-3) IS DELAMINATED (OUTER LAYER OF FIBERGLASS PEELED OFF). / INSTALLED PANEL 149A7753-2 PER EA OTHER-53EA-07525 PANEL MUST BE REMOVED AND INSTALL SERVICEABLE 149A7753-3 PANEL WITHIN 7 DAYSSDR SWAA2022032477047Panel · elongatedPANEL 193B FASTNER HOLES ARE ENLARGED AND ELONGATED. / REMOVED AND REPLACED PER AMM.53-51-21SDR DALA2019120407052Release Mech · out of positionTAILCONE RELEASE CAM MECHANISM IS CLOCKED INCORRECTLY. NRC 001-0310:5300-2004/015 00218: RECLOCKED CAM REF AMDS CARD 5352-4002 TAILCONE INSTALL. (LP #1377133)SDR SWAA2022032422233Panel · crackedFAIRING PANEL #195CL HAS A CRACK IN THE RADIUS OF THE PANEL / REPAIRED FAIRING 195CL CRACK IN RADIUS OF PANEL IAW SRM 51-70-04-2R-6SDR SWAA2022032461130Panel · delaminatedLEADING EDGE OF PANEL 193AL DELAMINATED 6'L X 1' W MOD / REMOVED & REPLACED PANEL 193AL REF AMM 53-51-21SDR SWAA2022032457225Frame · crackedRIGHT WING TO BODY PANEL 191AR AFT VERTICAL SUPPORT FRAME CRACKED. / REMOVED AND REPLACED AFT VERTICAL SUPPORT PER SRM 51-10-02 AND SRM 51-40-02SDR SWAA2022032452359Panel · corrodedPANEL 192F HAS CORROSION UNDER ALL 3 ANTENNAS. / REMOVED AND REPLACED PANEL 192F P/N 149A7755-1 PER AMM.53-51-21 MARKER BEACON ANTENNA AND DME ANTENNAS WERE REPLACED ON N/R G697619SDR C77A2020020530036Fairing · corrodedDURING BASIC CHECK AT EAMS, CORROSION DAMAGE WAS FOUND TO THE WING-TO-FUSELAGE FAIRING LOWER FWD FLANGES, P/N 170-67752-003 AND P/N 170-67822-003 (LH & RH). REFERENCE ETD2019-170-157172 FIGURE 1 FOR DETAILS, FOR THE DAMAGE LOCATION AND DIMENSION. EAMS REQUESTESDR SWAA2022032413564Panel · delaminatedPANEL 192AR HAS DELAMINATION ON THE EXTERNAL SURFACE IN CORE AREA / REPAIRED DELAMINATION ON THE EXTERNAL SURFACE IN CORE AREA ON PANEL 192AR IAW SRM 53-40-70; SRM 51-70-05-2R-2; SRM 51-40-02.SDR SWAA2022032452634Angle · crackedWTB FAIRING SUPPORT ANGLE COMMON TO LT WING STRAKELET IS CRACKED. / REMOVED WTB FAIRING SUPPORT ANGLE COMMON TO L/H WING STAKELET. LOCATED DRILLED & INSTALLED PER SRM 51-40-02-0G-0; SRM 51-40-03-0G-0; DWG 116A3010 REMOVED & REINSTALLED FAIRINGS PANELS 191FL; 1SDR DALA201911256888Fairing · crackedRH BODY FAIRING PANEL 198CR LOWER EDGE FOUND CRACK. REPAIRED CRACK ON RH BODY FAIRING PANEL 198CR LOWER EDGE PER 51-70-05. (LP 136849)SDR SWAA2022032411446Panel · elongatedALL HOLES IN LOWER FUSELAGE PANEL 193B ENLARGED. / REMOVED AND REPLACED PANEL 193B PER SRM 51-10-01; SRM 51-40-02 AND INSTALLED NEW PANEL PER AMM 53-51-21SDR SWIA2019122747133Support · crackedRIGHT FUSELAGE WING TO FUSELAGE AFT FAIRING SUPPORT AT BS 909, RBL 17.63 WAS CRACKED. COMPLIED WITH ALL THE STEPS OF REO STEPS 1 TO 13. INSTALLED ALL REPAIR PARTS AND WET INSTALLED ALL REPAIR FASTENERS ON RT FUSELAGE WING TO FUSELAGE AFT FAIRING SUPPORT.SDR SWIA2019412277135Tee Fitting · corrodedUNDER FWD WING TO FUSELAGE FAIRING CENTER TEE HAS CORROSION AROUND (4) EA. FASTENER LOCATIONS PN SH670-39063-1 MACHINED ATTACHMENT. REMOVED OUT OF LIMITS TEE AND INSTALLED NEW UNDER FWD WING FUSELAGE FAIRING CENTER TEE IAW SRM.SDR SWIA2020010947564Attach Fitting · corroded* ATTACH FITTING FOR FORWARD LOWER FUSELAGE FAIRING 193AB HAS CORRODED HARDWARE. (C-CHECK) RO 01/07/2020 REMOVED AND INSTALLED NEW, P/N NAS428-3A12, BOLT, MS21042-3, NUT & NAS73-3E015, BUSHING ON THE L/H O/B ATTACH FITTING FOR FORWARD LOWER FUSELAGE FAIRING SDR DALA2019111506702Attach Bracket · crackedTAIL CONE ATTACH BRACKET CRACKED ON TAIL CONE @2:00 POSITION. REMOVED AND REPLACED TAIL CONE ASSY PER MD88 AMM 53-53 TAILCONE, AFT U OFF 88-5353-9-0002 S/N 00036. (LP1360531)SDR SWAA2022040547405Floor Panel · delaminatedCABIN FLOOR PANEL 221GF IS DAMAGED AT FWD OUTBOARD CORNER / REPAIRED CABIN FLOOR PANEL 221GF WAS DAMAGED AT FWD OUTBOARD CORNER IAW 800 SRM 53-00-50-2R-7; DAMAGE IS BEYOND ALLOWABLE LIMITS OF SRM 53-00-50-3A-1; PARA 4F. DELAMINATIONS ARE NOT PREMITTED AND REQUSDR DALA2019111506703Latch · looseLH UPPER LATCH ARM LOOSE/WORN. REPLACED LH UPPER LATCH ARM PER MD88 AMM 53-53, OPS CHECK GOOD, (LP1359437)SDR SWIA2019122747134Support · corrodedAFT FUSELAGE SUPPORT STRUCTURE FOR BODY FAIRINGS 195DL/196DR, SPLICE ANGLE CORRODED LOCATED AT BS 939. AFT FUSELAGE SUPPORT STRUCTURE FOR BODY FAIRINGS 195DL/196DR, SPLICE ANGLE REMOVED AND REPLACED WITH NEW ANGLE REF SRM.SDR EBVR20191112002Skin · corrodedCORROSION ON THE L/H AND R/H FUSELAGE AT THE EDGE OF THE AFT FAIRING.PERFORMED TAILCONE SECTION SKIN CORROSION REPAIR ON AFT FUSELAGE LH AND RH SKIN UNDER AFT FUSELAGE FAIRING. FABRICATED AND INSTALLED 4 DOUBLERS TO BLENDED AREAS USING .032" 2024T3 ALUMINUM ALSDR SWIA2019122747440Fairing · corrodedFWD FUSELAGE UNDER FAIRINGS 191AB AND 192BB BETWEEN STRINGERS 24 LT AND RT AT BS 409+96 MOUNT HOLES WERE CORRODED. REMOVED CORROSION FROM FWD FUSELAGE UNDER FAIRINGS MOUNT HOLES, BLENDED AREAS FOUND TO BE OUT OF LIMITS, APPLICABLE REO FOR THIS AREA STATES THSDR SWAA2022040734760Fairing · crackedWING TO BODY FAIRING 195CR IS CRACKED AT EDGE. MARKED. / REPAIRED WING-TO-BODY FAIRING 195CR AS MARKED IN AFT CORNER AT RADIUS IAW SRM 737-800 51-70-04-2R-6 REV 69; SRM 737-800 51-70-04-2R-0 GENERAL PER 737-800 SRM 53-40-70-2R-1 TABLE 201 REV 69.SDR SWAA2022040552275Panel · delaminatedTAIL CONE HAS AREA OF DELAMINATION ON R/H SIDE AT LOWER FWD. CORNER OF CUT OUT FOR ACCESS PANEL / REPAIRED PER SRM 51-70-04-2R-2. SEE SUBTASKS FOR INDIVIDUAL SIGNOFFS.SDR SWAA2022040510486Panel · elongatedFASTNER HOLES ELONGATED AT #1;#2;#3;#4;#5;#6;#7;#10 #13;#22 ON 193B PANEL / REMOVED AND REPLACED NUTPLATES PER SRM 51-40-02SDR IPXA2019111148861Doubler · wornINSPECTION TYPE:2CTAIL CONE R/H SIDE UPPER LATCH SPOOL FITTING/DOUBLER IS WORN THRU.REMOVED, FABRICATED AND REPLACED FITTING/DOUBLER IAW DWG. AKC7546 AND SRM 51-35-01. (MINOR)SDR SWAA2022040513478Panel · debondedPANEL 194CR OUTER SURFACE HAS A DISBOND 14' FROM THE L/E AND 21.5' FROM THE I/B EDGE / REPAIRED DAMAGE TO OUTER SURFACE OF PANEL 194CR IAW SRM 51-70-05-2R-2. 57885U 11-15-19SDR SWAA2022040513403Panel · delaminatedPANEL 193D OUTER SKIN HAS A DELAMINATION (MARKED) / PANEL 193D OUTER SKIN DELAMINATION REPAIRED IAW SRM 51-70-05-2R-2 PER SRM 53-40-70-2R-1SDR DALA2019110506386Release Cable · wornKEVLAR RELEASE CABLE IS WORN IN THE TAILCONE. REMOVED WORN KEVLAR RELEASE CABLE, INSTALLED NEW KEVLAR RELEASE CABLE, WITH COMPLETION OF KEVLAR CABLE ON AMDS CARD #5352-2001. (LP #1343143)SDR DALA2019110506385Bracket · wornTHE TAILCONE KEVLAR CABLE SPRING BRACKET ON THE RIGHT SIDE IS WORN. MAINTENANCE REPLACED THE TAIL CONE KEVLAR CABLE SPRING BRACKET WITH A NEW BRACKET. (LP #1343012)SDR IPXA2019103148512Skin · dentedINSPECTION TYPE:SEG2BARE METAL DENT IN TAIL CONE SKIN UPPER 18 INCHES BEHIND RUDDER APPROX FS 1900 DOT 30/020 DAMAGE BETWEEN STA 1918.9 AND STA 1941.0REPAIRED AREA IAW B757 SRM 51-70-10-2R REPAIR 4 310 DEGREE CURE IAW PRELIMINARY 1SDR SWAA2022032303722Panel · delaminatedWING TO BODY PANEL 193B HAS LARGE AREA OF DELAMINATION AND SEVERAL MOUNT HOLES ARE ELONGATED PAST LIMITS. FABRICATE NEW 193B PANEL / REMOVED AND REPLACED PANEL 193B IAW AMM 53-51-21 AND SRM 51-40-02SDR SWIA2019121746932Bracket · crackedFS 449 LBL 47 OVERWING FAIRING BRACKET IS CRACKED (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED BRACKET IAW CRJ200 SRM.SDR SWIA2019121746930Bracket · crackedFS 461 LBL OVERWING FAIRING BRACKET IS CRACKED (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED BRACKET IAW CRJ200 SRM.SDR SWIA2019121746928Bracket · crackedFS 469RBL 47 OVERWING FAIRING BRACKET IS CRACKED (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED BRACKET IAW CRJ200 SRM.
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