JASC 5350
Service difficulty reports · 6,124
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 SWAA2022020991149Panel · delaminatedPANEL 194CR HAS A DELAMINATION ON THE OUTER SKIN 3' FROM UPPER EDGE / REPAIR PANEL 194CR OUTER SKIN 3' FROM UPPER EDGE IAW 51-70-05-2R-2SDR SWAA2022020991595Fitting · broken(FUSELAGE BELLY) SUPPORT FITTING BROKEN AT STA.540 BL 0 FWD R/H / REMOVED BROKEN SUPPORT FITTING AT STA 540 BL 0 FWD R/H I.A.W. B737 SRM 51-40-02-0G-0. INSTALLED NEW SUPPORT FITTING AT STA 540 BL 0 R/H P/N 149A7712-22 LOT #506700F I.A.W. B737 SRM 51-40-02-0G-0SDR SWAA2018040320878Former · chafedFAIRING FORMER CHAFED BETWEEN BS 663 & 673, RBL 28. R & R THE FORMER IAW SRM & DWG.SDR SWAA2022021161548Fairing · delaminatedR/H UNDERWING FAIRING 192BR IS DELAMINATED ON THE LEADING EDGE. / REPAIRED DAMAGED AREA PER SRM 51-70-05-2R-6.SDR DALA2018030601438Fairing · crackedDURING INSPECTION, FOUND THE BODY FAIRING PANEL NR 191FR, A CRACK WAS FOUND IN THE PANEL. MAINTENANCE REPAIRED IAW SRM 51-70-05.SDR SWAA2022021006284Fairing · delaminatedFAIRING PANEL 192BR IS DELAMINATED ON LEADING EDGE / FAIRING PANEL 192BR DELAMINATION ON LEADING EDGE REPAIRED IAW SRM 51-70-05-2R-6 20549U 03/02/18SDR SIMA2018101028015Strap · crackedLT BODY TO BODY FAIRING STRAP CRACKED 6 INCH AFT OF FR 49. -C/A- LT WING TO BODY FAIRING STRAP 6 INCH AFT OF FR 49 REPAIRED IAW SRM 53-23-12 TYPE II. AFTER INVESTIGATION EXISTING DRILL RUN FOUND UNDER REPAIR STRAP, SKIN REPAIRED IAW SRM 53-23-01, TABLE 108 WITSDR SWAA2022020951424Panel · delaminatedPANEL 191HL LOCATED JUST AFT OF LH RAM AIR INLET HAS A DELAMINATED DENT ON OUTER SURFACE. / REPAIRED PER SRM 51-70-05-2R-1.SDR SWAA2022020910627Panel · crackedPANEL 195CL AFT LOWER CORNER CRACKED / PANEL 195CL AFT LOWER CORNER CRACK REPAIRED IAW SRM 51-70-05-2R-6 20549U 03/02/18SDR FDEA201802220468Support Bracket · crackedRADOME HOLD OPEN ROD STOWAGE SUPPORT BRACKET IS DAMAGED AND BENT. EVALUATED DAMAGED SUPPORT BRACKET ON RADOME HOLD OPEN ROD STOWAGE AREA, FOUND A CRACKED BRACKET. FOUND TO BE OUT LIMITS IAW SRM 53-10-08-1A, FIG 101, NOTE A, DETAIL XIII. REMOVED, FABRICATESDR SWAA2022020942878Panel · crackedSUPPLEMENTAL INFORMATION: FAIRING PANEL #195CL AFT BOTTOM CORNER CRACKED / FAIRING PANEL #195CL AFT BOTTOM CORNER CRACK REPAIRED IAW SRM 51-70-05-2R-6 20549U 02/22/18SDR CALA2018022100731Skin · chafedEXTERNAL SKIN AT BS 2108 - 2150, STRINGERS 1 - 3L CHAFED. THE SKIN WAS REPAIRED IAW SRM 53-70-01, REPAIR 2, AND ECRA 5330-06322.SDR DALA2018022001036Attach Bracket · corrodedLEFT WING UPPER WING ROOT, WING TO BODY FAIRING ATTACH BRACKET CORRODED. REMOVED AND REPLACED THE ATTACH FITTING IAW SRM 51-40-02, AND DWG 149N7550, REV- .SDR DALA2018022001034Support Bracket · corrodedRT WING TO BODY FAIRING SUPPORT BRACKET CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-71, DETAIL VII. FABRICATED, REMOVED AND REPLACED THE BRACKET IAW SRM 51-40-02, AND DWG 149N7210, REV C.SDR DALA2018022001033Bracket · corrodedLEFT WING TO BODY FAIRING ATTACH BRACKETS CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-71, DETAIL VII. REMOVED AND REPLACED THE BRACKET IAW SRM 51-40-02, AND DWG 140N7210, REV C.SDR ASOA201802175053Fairing · damagedFOUND A LARGE DENT AND CRACK ON THE RT WING AFT FAIRING. REPAIRED THE FAIRING IAW SRM 53-00-00-201-002-A01. REPLACED THE FAIRING SUPPORT FRAME AND ATTACH ANGLES IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. REPAIRED THE FUSESDR SWAA2022021032387None · delaminatedSUPPLEMENTAL INFORMATION: PANEL 193 B HAS DELAMINATED IN LEADING EDGE CORNERS / R/R'D PANEL 193B PER SRM 51-40-02SDR SWAA2022021006244Attach Bracket · crackedKEEL BEAM PANEL 192E;FWD LEFT ATTACH BRACKET BROKEN OFF / REMOVED AND REPLACED BRACKET PER SRM 51-40-02.SDR SWAA2022021022962Former · crackedR/H WING-TO-BODY FAIRING FORMER AT BS 500D COMMON TO PANEL 191AR AND L.E. CRACKED ON AFT SIDE (MARKED) / R/H WING TO BODY FAIRING FORMER WAS REMOVED & REPLACED ON NRC # T751602SDR SWAA2022021051146Access Panel · crackedSUPPLEMENTAL INFORMATION: NO.2 CANOE ACCESS PANEL 543CL CRACKED. / REPLACED NO.2 CANOE ACCESS PANEL 543CL PER SOPM 20-50-01SDR SWAA2022021031357Frame · crackedRH WING INBD LE BODY FAIRING SUPPORT STRUCTURE; INBD OF LANDING LILGHT ASSY; ANGLE CRACKED ON AFT SIDE. / REMOVED CRACKED FRAME IAW B737 SRM 51-40-02-0G-0. FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-30-71-1A-1; FIG 105. IDENTIFIED NEW PART AS FRAME P/N 116A3118SDR SWAA2022020912415Fairing · crackedBODY FAIRING PANEL 191FL CRACKED ON UPPER EDGE / REPAIRED CRACK AT UPPER EDGE OF BODY FAIRING PANEL 191FL PER SRM 53-30-70-2R-1 TABLE 202 AND SRM 51-70-05-2R-6SDR SWAA2018021919740Attach Bracket · crackedRIGHT WING TO BODY FAIRING PANEL 191AR AFT CENTER ATTACH BRACKET CRACKED. R & R THE ATTACH BRACKET IAW SRM.SDR SWAA2022020931286Fairing · crackedPANEL 191FL UPPER AFT CORNER CRACKED / BROKEN / REPAIRED PANEL 191FL UPPER AFT CORNER IAW 737-700 SRM 51-70-04-2R-6 REV 63: 737-700 SRM 51-70-04-2R-0 REV 63 PER 737-700 SRM 53-30-70-2R-1 TABLE 202 REV 63.SDR IPXA2018022026690Skin · chafedINSPECTION TYPE: 4C, TAIL CONE UPPER FWD LT INTERNAL SKIN DOUBLER CHAFED. REPAIRED IAW EA 011-5350-01-A7110, REV IR, AND EO MD11-5350-67365-A.SDR SWAA2022020936987Fairing · delaminatedL/H WTB PANEL 193CL HAS AREA OF DISBOND 4' AFT OF L/E TOOL SIDE OF PANEL / REPAIRED AREA OF DISBOND 4' AFT OF L/E TOOLSIDE OF L/H WTB PANEL 193CL PER SRM 53-40-70-2R-1 TABLE 201 AND SRM 51-70-05-2R-1SDR SWAA2022020811705Panel · crackedFAIRING PANEL # 194BL IS CRACKED ON UPPER EDGE OF PANEL / REPAIRED CRACK ON UPPER EDGE OF PANEL # 194BL. WORK ACCOMPLISHED IAW SRM 51-70-05-2R-10. 57252U 02/04/18SDR DALA2018013100585Tail Cone · out of rigREQUIRED TO RELEASE THE COMPLETELY RIGGED TAILCONE IS 30+/- 5LBS. THE TAIL CONE IS OUT OF RIG AND RELEASING TOO EARLY USING THE INSIDE TAIL CONE RELEASE HANDLE. CHECKED & ADJUSTED TAILCONE RIG REF AMM 53-52-01. CHECK IS NOW WITHIN LIMITS.SDR DALA2018013100584Tail Cone · out of rigTHE TAIL CONE IS OUT OF RIG AND RELEASING TOO EARLY DURING USE OF THE EXTERNAL TAIL CONE RELEASE HANDLE. CHECKED & ADJUSTED TAILCONE RIG REF AMM 53-52-01. CHECK WITHIN LIMITS.SDR DALA2018013000580Latch · wornTAIL CONE UPPER LATCH IS WORN. REPLACED UPPER LEFT HAND LATCH IAW MM. OPERATION CHECKS GOOD.SDR SWAA2022020812404Panel · crackedFAIRING PANEL #194DL / #149A7547-5; MULTI CRACKS AROUND FASTENING LOCATION. (MARKED) / FAIRING PANEL #194DL/ #149A7547-5; MULTI CRACKS AROUND FASTENING LOCATION (MARKED) REPAIRED IAW SRM 53-60-70-2R-1 TABLE 202 AND IAW SRM 51-70-05-2R-8.SDR YENA201801270899Rib · crackedON 01/27/2018, DCA MX REPORTED CRACK DAMAGE ON THE RIB IN THE LT WING FUSELAGE FAIRING (WFF) BULKHEAD AT FRAME 52. THE CRACK DAMAGE WAS MEASURED TO BE 1.06" (27MM) LONG. SEE REF. /3/ FOR ADDITIONAL DETAILS. THE PART (RIB) CANNOT CURRENTLY BE REPLACED OR REPAIRSDR JJBA20180127015Skin · damagedDAMAGE ON RIGHT SIDE OF AIRCRAFT AT TAIL CONE. DAMAGE LOCATED BELOW Z150 AND BETWEEN BS 753.949 AND 789.656. DAMAGE REMOVED. NDT HFEC CARRIED OUT ON HOLE CUTLINE. NO CRACK INDICATION.SDR UIEA2018012900131Frame · corrodedLEFT FWD WING TO BODY FAIRING FRAME CORRODED, BS 880, LBL18. REMOVE AND REPLACED THE FRAME IAW SRM 51-40-02, REV 101, EI T2017P53M-2984, REV 0, DWG 65B06749, REV 1.SDR IPXA2018020126099Skin · chafedINSPECTION TYPE: 4C, TAIL CONE INTERNAL UPPER RT SKIN HAS A DEEP CHAFE FROM CONTACT WITH RIVETS. REPAIRED IAW EA 011-5350-01-A7076, REV IR AND EO MD11-5350-67142-A.SDR SWAA2022020855485Attach Bracket · crackedKEEL BEAM BODY FAIRING 192E FWD 2 ATTACH FITTINGS ARE CRACKED . / REMOVED AND REPLACED FITTINGS REF SRM 51-40-02.SDR SIMA20180111006Angle · crackedLEFT WING UPPER WING TO FUSELAGE PANEL, LOWER ANGLE, FIRST FROM AFT END IS CRACKED AT FORWARD END. R & R THE ANGLE IAW SRM-51-20-02 AND ETN-EM-53-142.SDR SIMA20180111010Angle · crackedLEFT WING UPPER WING TO FUSELAGE PANEL, LOWER ANGLE, SECOND FROM AFT END IS CRACKED AT THE AFT END. R & R THE LT WING SECOND FROM AFT UPPER WING TO FUSELAGE PANEL ANGLE IAW SRM 51-20-02 AND ETN-EM-53-142.SDR SWAA2022020835117None · crackedSUPPLEMENTAL INFORMATION: BODY FAIRING PANEL 191FL CRACKED / REPAIRED CRACK ON BODY FAIRING PANEL 191FL PER SRM 53-30-70-2R-1 TABLE 202 AND SRM 51-70-05-2R-7SDR SWAA2022020892368Former · crackedL/H BOW TIE PANEL JUST FWD OF BS 727 FAIRING FORMER IS CRACKED AT LBL33 / REMOVED AND REPLACED L/H BOW TIE PANEL JUST FWD. OF B.S. 727 FAIRING FORMER LBL 33 IAW DWG 149A7602 AND SRM 51-40-02SDR SWAA2022020792361Fairing · delaminatedPANEL 193CR HAS A DELAMINATION ON THE OUTER SKIN MID SPAN. / PANEL 193 CR DELAMINATION ON THE OUTER SKIN MID SPAN REPAIRED IAW SRM 51-70-05-2R-2 20549U 12JAN18SDR SWAA2022020740534Fairing · crackedFAIRING PANEL 195CL IS CRACKED IN THE LOWER RADIUS / CRACK ON LOWER RADIUS OF PANEL 195CL REPAIRED IAW SRM 51-70-05-2R-06 57443U 13JAN18SDR SWAA2022020760870Support Bracket · crackedFUSELAGE WING TO BODY FAIRING SUPPORT BRACKET CRACKED BETWEEN FAIRINGS 191AR AND 195AR. / REMOVED AND REPLACED FUSELAGE WING TO BODY FAIRING SUPPORT BRACKET IAW SRM 51-10-02SDR SWAA2022020767759Fairing · cracked#6 CANOE FARING CRACKED INSIDE AFT BOTTOM / REMOVED DAMAGE AND ACCOMPLISHED REPAIR TO CANOE REF EA 1-A57-6168. CHANGED CANOE MPN TO 113A9350 REF EA 1-A57-6168 AND TSR#201800113. RESTORED FINISH TO CANOE REF AMM 51-21-99.SDR SWAA2022020722555Fairing · delaminatedPANEL 193AR HAS PUNCTURES & DELAMINATION ON INNER SURFACE CORE AREA / PANEL 193 AR PUNCTURES AND DELAMINATION ON INNER SURFACE CORE AREA REPAIRED IAW SRM 51-70-05-2R-2 20549U_10529C 1/13/18SDR SWAA2022020792257Bracket · cracked2 EA FAIRING FORMER BRACKETS BS 551 LH FWD AND RH FWD ARE CRACKED; UNDER PANEL #192E / REMOVED AND REPLACED 2EA FAIRING FORMER BRACKETS; BS 551 L/H & R/H UNDER PANEL #192E PER SRM 51-40-02-0G-0; IPC 53-12-11-25.SDR R61A20180110043Angle · corrodedANGLES ON PANEL 1441FR CORRODED. REMOVED AND REPLACED IAW SRM 51-40-08.SDR DALA2018010300029Control Arm · out of adjustTAILCONE DID NOT DEPLOY ON OPS CK. MADE ADJUSTMENT TO THE AFT FUSELAGE CONTROL ARM PER MD88 AMM 53-53.SDR DALA2018010300026Strap · brokenVELCRO STRIP ON INTERIOR TAILCONE BARRIER STRAP BROKEN. REATTACHED VELCRO STRIP FOR AFT STAIR DOOR BARRIER STRAP. OPN CKS GOOD. OK FOR SVC.SDR SWAA2022020767684Panel · delaminatedPANEL 194DL HAS DELAMINATION. / REMOVED DAMAGE AND REPAIRED REF SRM 51-70-05 REPAIR #1. RESTORED FINISH TO PANEL REF AMM 51-21-99.
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