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 IPXA2019060322732Skin · deformedINSPECTION TYPE:1CAPU COMPARTMENT. TAIL CONE, AFT EDGE OF APU CUTOUT DAMAGED / GOUGEDREPAIRED PER UPS EO NO: A300-5330-72788-ASDR SWAA2022030807993Panel · elongated193 B FAIRING PANEL ELONGATED FASTENER HOLES AT LOCATION 1 THRU 7; 15; 27 THRU 33; AND 34 THRU 38 / REMOVED AND REPLACED 193B PANEL PER ENGINEERING ORDER 14108 AND SIPSDR SWAA2022030951272Fairing · elongated193 PANEL HAS ELONGATED HOLES IN PANEL MOD / REMOVED AND REPLACED THE 193B PANEL PER AMM 53-51-21SDR SWAA2022030951236Fairing · delaminatedPANEL 193AL HAS DELAMINATION ON LEADING EDGE 7' FROM TOP OF PANEL 13' LONG 3/4' WIDE 5 PLYS DEEP.ACCOMPLISHED EA TASKS AS REQUIRED PER REPAIR-53EA-06466; SEE ALSO SA-M 943T V009237 FOR FURTHER ACTION.PERMANENT ACTION REQUIRED:PERFORM A PERMANENT REPAIR PER SRMSDR 2019F00205Fairing · crackedLT LOWER WING FAIRING TRIM CRACK REPAIR RFTS-103325 REV 0 DATED MAY 15, 2019.SDR SWAA2022030936460Fairing · elongatedPANEL 193B HAS 19 FASTENER HOLES THAT ARE ELONGATED. HOLE POSITIONS MARKED ON EO 14108 TABLE 1. / RREMOVED AND REPLACED 193B PANEL REF B737 AMM 53-51-21 AND B737 SRM 51-20-07SDR SWAA2022030981668Fairing · elongatedPANEL 195CR HAS AN ELONGATED FASTENER HOLE / PANEL 195CR WITH AN ELONGATED FASTNER HOLE WAS REPAIRED IAW SRM 51-70-04-2R-9 57545U 5-31-19SDR DALA2019051503019Radome · damagedFOUND SMALL DAMAGED AREA TO THE RADOME. R/R NOSE RADOME PER AMM 53-50. OPS CKS GOOD RADOME, NOSE, D OFF 88-5351-9-0002 00077 ON 88-5351-9-0002 01938. (LP5471157)SDR IPXA2019051041978Doubler · wornINSPECTION TYPE:4C TAILCONE RT UPPER INTERNAL PRODUCTION DOUBLER HAS DEEP WEAR IN SEVERAL PLACES. ACCOMPLISHED REPAIR ON TAILCONE RH SIDE INTERNAL DOUBLER REPAIR FILLER PER EO MD-11-5350-66790-A APPENDIX B.SDR SWAA2022030930539Fairing · crackedPANEL 193B HAS SMALL CRACK OUTER SKIN LEADING EDGE AREA. / APPLIED REPAIR PLIES AND BONDED PER SRM 51-70-05 REPAIR 2.SDR SWAA2022030959608Fairing · elongatedWING TO BODY FAIRING PANEL 193B HAS ENLONGATED & ENLARGED FASTENER HOLES AT LOCATIONS 1-6;10;12-17; 19;21;22;29-33 & 35-38 MOD / INSTALLED NEW PANEL 193B REF AMM 53-40-70 PERFORMED ELECTRICAL RESISTANCE CHECK REF AMM 53-51-01SDR SWAA2022030902334Fairing · delaminatedPANEL 193AL OUTER SKIN HAS LARGE DISBONDED DENT JUST BELOW 'WARNING'. (MARKED) / PANEL 193AL OUTER SKIN WITH LARGE DISBONDED DENT JUST BELOW 'WARNING' AS MARKED WAS REPAIRED PER SWA EA# 1-753-34858 REV#1 DATED 20-MAY-2019 AND ATS ER# 19-03107 REV A DATED 20-MASDR SWAA2019050932490Tail Cone · delaminatedRT OF AFT AUXILIARY POWER UNIT TAIL CONE LOWER FORWARD SURFACED DELAMINATED BY FORWARD LOWER CORNER ACCESS PANEL. REPAIRED TAIL CONE PER SRM.SDR SWAA2022030849713Fairing · delaminatedDURING PFC; FOUND LEADING EDGE OF PANEL 193AL DELAMINATED FROM 1 TO 3 PLYS. DAMAGE STARTS AT 7.5' FROM TOP OF PANEL AND IS 15.5' IN LENGTH; 1.0' AT ITS WIDEST WIDTH. ACCOMPLISHED REPAIR-53EA-06469PERMANENT ACTION REQUIRED:PERFORM A PERMANENT REPAIR PER SRM 51-SDR SWAA2022030998373Attach Angle · corrodedAFT AND LOWER ATTACH ANGLES FOR PANEL 193AL HAS FRETTING CORROSION ON THE LOWER ATTACH SURFACE. (AREA IS MARKED) / REMOVED AND REPLACED ATTACH ANGLE PER SRM 51-40-02 AND SRM 51-10-02. P/N 149A7214-15.SDR SWAA2019060533334Support Angle · crackedAFT R/H WING TO BODY FAIRING PANEL #194 CR-INBOARD VERTICAL SUPPORT ANGLE CRACKED (BS 727A). APPROX. 2.0" LONG. / R&R ANGLE PER SRM.SDR SWAA2022030948126Fairing · delaminatedPANEL 192JR HAS A DELAMINATED DENT IN THE EXTERNAL SURFACE / PANEL 192JR WITH A DELAMINATED DENT ON THE EXTERNAL SURFACE WAS REPAIRED IAW SRM 51-70-05-2R-2.SDR SWAA2022030977928Fairing · delaminatedPANEL 191D HAS A DELAMINATED DENT ON THE EXTERNAL SURFACE; IN THE CORE AREA. / DELAMINATED DENT ON THE EXTERNAL SURFACE HAS BEEN REPAIRED ON PANEL 191D IAW SRM 51-70-05-2R-2 59313U 05-09-19SDR SWAA2022030846213Fairing · delaminatedDISBONDED DENT ON OUTER SURFACE OF PANEL 193AR; 43' FROM IB END; 8' FROM AFT EDGE / REPAIRED DISBONDED DENT ON OUTER SURFACE OF PANEL 193AR; 43' FROM IB END; 8' FROM AFT EDGE IAW SRM 53-40-70; SRM 51-70-05-2R-2; SRM 51-70-05-2R-11; AMM 51-21-71SDR DALA2019071904350Structure · dentedDENT ON RT SIDE OF EMPENNAGE BETWEEN STR21 AND STR 20, FRAME 74 AND 75, PERFORMED PERMANENT REPAIR ON DENTED AREA ASPER ER/A 579558-14. REV ORIGINAL AND PRI 579558-14 REV 0 AND REV 1.SDR ASOA201905014013Strake · dentedHOB- DURING PREFLIGHT INSPECTION THE CREW REPORTED A DENT IN THE LEFT HAND REAR STRAKE BETWEEN FRAMES 9 & 10. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE PERFORMED A DOUBLER REPAIR ON THE AFFECTED AREA AND THE AIRCRAFT WAS SUBSEQUENTLY APPROVED FOR RETURSDR SWAA2022030878261Fairing · crackedWING TO BODY FAIRING 192BL HAS A CRACK ON OUTER SURFACE 1' LONG. 8-3 / REMOVED DAMAGE AREA ON WING TO BODY FAIRING 192 BL OUTERSURFACE CLEANED ;PREPARED AND INSTALLED REPAIR PLIES IAW B737-7 SRM 51-70-05-2R-1 TOTAL REPAIR SIZE 3' DIAMETERSDR SWAA2022030856145Panel · delaminated193B PANEL L/H TRAILING EDGE HAS DELAMINATION & MISSING MATERIAL BETWEEN FASTNER LOCATIONS 33 AND 32 MEASURING .6' X .4' GREATER THAN 1PLY DEEP. MOD / REMOVED AND REPLACED PNL 193B REF SRM 51-7 SRM 51-40-02SDR IPXA2019051242012Frame · gougedINSPECTION TYPE:4C FWD. TAIL CONE AFT BULKHEAD RT UPPER FRAME IS GOUGED. REPAIRED TAIL CONE FRAME IAW DWG. AKC7539 AND SRM 53-80-07 REPAIR 4. (MINOR)SDR LR7A2019042901519Strap · corrodedDURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5321, FOUND WING-TO-FUSELAGE FAIRING FS617-TO-FS667 STEEL STRAP CORRODED, RBL61, WL256. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2136.SDR SWAA2022030804196Panel · elongatedWING TO BODY PANEL 193CL INBD EDGE HAS HOLE THAT IS ELONGATED. / REPAIRED WING TO BODY PANEL 193CL I/B EDGE FASTNER HOLE AS MARKED IAW 737-700 SRM 51-70-04-2R-01 REV 67.SDR SWAA2022030857607Panel · delaminatedWING TO BODY FAIRING PANEL 193B; HAS A .80' DIAMETER AREA OF DELAMINATION ON THE LOWER SURFACE; NEXT TO A PREVIOS REPAIR; LOCATED 10.25' AFT OF FASTENER #15. / REPLACED PANEL 193B PER M/M 53-51-21.SDR SWAA2022030804077Panel · delaminatedAFT OUTBOARD WHEEL WELL PANEL 193CR IS DELAMINATED ON FWD EDGE. / REFERENCE DEFECT NO. T914544 PANEL 193CR ROBBED FROM N7723E AND INSTALLED ON DEFECT NO. T914544SDR SWAA2022030829768Panel · delaminatedPANEL 193AR HAS PUNCTURES & DELAMINATED AREA ON THE INNER SURFACE OF THE CORE AREA. / PANEL 193AR WITH PUNCTURES AND DELAMINATED AREA ON THE INNER SURFACE OF THE CORE AREA WAS REPAIRED IAW SRM 51-70-05 REPAIRS 2 AND 11. 59702U 05/06/19SDR IPXA2019050141645Doubler · chafedINSPECTION TYPE:4C TAILCONE RT UPPER INTERNAL DOUBLER WORN (CHAFED). REPAIRED TAILCONE RT UPPER INTERNAL DOUBLER CHAFE DAMAGE IAW EO MD11-5350-66790-A. (MINOR)SDR DALA2019042502630Release Mech · inoperativeMAINTENANCE FOUND THE TAILCONE RELEASE MECHANISM DOOR TAPED SHUT WITH THE DECAL. DURING REMOVAL, THE TAIL CONE WAS DEPLOYED, BUT THE SLIDE DID NOT DEPLOY. MAINTENANCE THEN FOUND THE LANYARD BROKEN ON THE DEPLOYED TAIL CONE AND REPLACED THE TAIL CONE WITH A NEWSDR SWAA2022030700331Panel · delaminated193 B. PANEL EROSION OF CORNER LOCATION (8) (MARKED). ALOO HAS HOLE IN PANEL SURFACE NOT CONTINUING THRU JUST FWD OF FASTENER 34. HOLE IS APPROX .125 IN DIAMETER AND HAS LOCALIZED DELAMINATION ASSOCIATED WITH HOLE APPROX .250 INDIAMETER / REMOVED AND REPLACED SDR SWAA2022030869260Panel · elongatedPANEL 193B ALL SCREW HOLES WORN AND ELONGATED. / COMPLIED WITH ON E.A. 1-753-34687SDR SWAA2022030729756Panel · crackedFAIRING PANEL #195CL HAS SMALL CRACK AT THE AFT LOWER RADIUS MARKED / FAIRING PANEL # 195CL SMALL CRACK AT THE AFT LOWER RADIUS WAS REPAIRED IAW SRM 51-70-04-2R-0 56114U 05/03/2019SDR SWAA2022030729757Panel · crackedFAIRING PANEL #195CR HAS SMALL CRACK AT THE AFT LOWER RADIUS MARKED / FAIRING PANEL #195CR SMALL CRACK AT THE AFT LOWER RAIDUS WAS REPAIRED IAW SRM 51-70-04-2R-6 56144U 05/03/2019SDR DXTA201904230182Fairing · damagedDURING CHECKLIST DAMAGE WAS FOUND TO COMPOSITE PANELS ON UNDERSIDE OF AFT FUSELAGE AREA. ACCOMPLISHED AQRD ENGINEERING REPAIR ORDER NO. ERO-103261 DATED APRIL 15, 2019; BELLY AND WHEEL BIN FAIRINGS - PERMANENT REPAIR.SDR UIEA2019042604008Skin · scratchedLH TAIL CONE FROM STA 2438-2445 BTW STR 20L FOUND 26 IN LONG SCRATCH MARK(<P>EMP-STA 2488-2448 STR 15L TO STR 20L SKIN SCRATCH MARK AREAS REPAIRED IAW RI-53-81-13521 REV A</P>)SDR CALA2019042200639Fastener · missingPDA 3 BELLY FAIRING PANEL 192AB HAS 1 EA MISSING FASTENER.RPL FASTENER. RPL FASTENER SEE LOG PAGE 3043667.SDR SWAA2022030705301Panel · elongated193B PANEL HOLES ARE ELONGATED AT THIS LOCATIONS 3 ;4; 5; 6; & 33 THUR 38 AND 14 THRU 22 MOD / R/R PNL 193B PER AMM 53-51-21. DRILLED; COUNTER SINK AND TRIMED TO FIT PNL 193B PR SRM 51-20-07-06-0; 51-040-08 86275SDR DALA2019042512637Support · corrodedSHIP 6708 CORROSION ON BODY FARING SUPPORT AT BS=900 BTW RBL40 TO LBL 40. CORRECTIVE ACTION: SUMMARY: NRC 00467, CORROSION LEVEL 2. (UT) MEASUREMENT THICKNESS WAS OUT OF LIMITS PER B757-200 SRM. REPLACED PER B757-200 SRM. (1039485)SDR SWAA2022030739750Panel · delaminatedWING TO BODY FAIRING PANEL 193B IS CRACKED AND HAS A 1' AREA OF DELAMINATION ON UPPER SURFACE; LOCATED 7.5' FORWARD OF FASTENER #1. AREA IS CONTAMINATED WITH HYDRALIC FLUID. / R&R'D PANEL ASSY PER SRM 51-40-02. AND M/M 53-51-21.SDR SIMA2019042919007Angle · crackedRIGHT UPPER WING TO FUSELAGE FAIRING AFT ATTACH ANGLE ON WING HAS 1/4" CRACK ON THE AFT END. -C/A-CUT OUT DAMAGED SECTION AND INSTALLED SERVICEABLE SECTION OF ATTACH ANGLE IAW ETN-EM-53-142.SDR SWAA2022030746205Panel · delaminatedPANEL 193AR HAS PUNCTURES & DELAMINATION ON INNER SURFACE CORE AREA / REPAIRED PUNCTURES ON DELAMMATIONS ON INNER SURFACE CORE AREA ON PANEL 193AR IAW SRM 53-40-70; SRM 51-40-02; SRM 51-70-05-2R-2; SRM 51-70-05-2R-11SDR SWAA2022030797761Panel · corrodedBODY ACCESS PANEL 192E HAS CORROSION AND WEAR ON MOUNTING SURFACE FOR MARKER BEACON ANTENNA AND DME ANTENNA. / REMOVED AND REPLACED BODY ACCESS PANEL 192E PER AMM 53-51-21.SDR SWAA2022030727321Frame · crackedRIGHT FORWARD WING TO BODY STRUCTURE STA 500D HALF MOON FRAME AT WING LEADING EDGE IS CRACKED / REMOVED CRACKED RIGHT FORWARD WING TO BODY FAIRING STRUCTURE AT STA 500D IAW 737 SRM 51-40-02-0G-0. RECEIVED AND VERIFIED NEW PART P/N 116A3118U10 IAW BOEING DWG 11SDR SWAA2022030730499Panel · delaminatedPANEL 193B HAS DELAMINATED CORNER; FWD RH. / REPAIRED IAW SRM 51-70-05 REPAIR 6. RESTORED FINISH IAW AMM 51-21-99. SEE INDIVIDUAL SIGN OFFS FOR ALL WORK ACCOMPLISHED.SDR SWAA2022030744589Panel · delaminatedAFT R/H CORNER OF 193B PANEL HAS SMALL DELAMINATION INNER AND OUTER / REPAIRED PER SRM 51-70-04-2R-13SDR SWAA2022030764104Panel · delaminatedWING TO BODY FAIRING PANEL 193B HAS DELAMINATION ON CORNERS BETWEEN FASTENER HOLES 8 & 9 AND 13 & 14 MOD / REMOVED AND REPLACED PNL 193B REF AMM 53-51-21SDR SWAA2022030893439Fairing · elongated193B WING TO BODY FAIRING PANEL HOLES ELONGATED/ WORN. / REMOVED AND REPLACED PANEL 193B IAW AMM 53-51-21.SDR SWIA2019051745895Drag Angle · damagedTAILCONE DRAG ANGLE HAS 5 ELONGATED FASTENER HOLES. (C-CHECK) RO: 05/16/2019 REPAIRED TAILCONE DRAG ANGLE 5 ELONGATED FASTENER HOLES IAW REO.
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