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 SWAA2022032936463Panel · delaminated193B PANEL HAS DELAMINATION ON FWD LH EDGE. / REMOVED AND REPLACED 193B PANEL. REF EO DCR#39874SDR SWAA2022032942786Panel · delaminatedPNL 193B DELAMINATED / REMOVED AND REPLACED PNL 193B PER SRM 51-20-07 AND 51-40-07SDR SWAA2022032985793Fairing · delaminatedL/H WING TO BODY FAIRING 192BL HAS DELAM AT L/H TOP CORNER / APPLIED RESIN SWEEP TO SMALL AREA ON CORNER TO L/H WING TO BODY FAIRING PANEL (192BL) I/A/W B737-700 SRM 51-70-08-0G-0 & TOUCHED UP FINISH I/A/W B737-700 AMM 51-21-99-300-801.SDR SWAA2022032928593Panel · damagedPANEL 193AL HAS DELAMINATIONS & PUNCTURE ON THE INNER SURFACE OF THE CORE AREA. / REPAIRED DELAMINATION AND PUNCTURE ON PANEL 193AL ON THE INNER SURFACE OF THE CORE AREA PER SRM 51-70-05-2R-2 AND SRM 51-70-05-2R-0 AND ER 19-04879 REV IR & EA 1-753-35703 REV IRSDR IPXA2019092647264Intercostal · damagedINSPECTION TYPE:4CEXTENDED TAIL CONE FWD FRAME UPPER INTERCOSTAL IS DAMAGED.REMOVED AND REPLACED DAMAGED EXTENDED TAIL CONE FWD FRAME UPPER INTERCOSTAL IAW MD-11 SRM 51-33-01 & 51-35-01. (MINOR)SDR IPXA2019091746902Doubler · gougedINSPECTION TYPE:4C TAILCONE RT SIDE PRODUCTION DOUBLER IS GOUGED. REPAIRED GOUGED TAILCONE RT PRODUCTION DOUBLER AT STA Y=2165 & X=-36.5 IAW EO MD11-5350-66790-A APPENDIX B. (MINOR)SDR SWAA2022032906907Fairing · corrodedEXTERNAL LOWER FUSELAGE; MID FORWARD FAIRING 191D; DOUBLER AROUND OPENING FOR ATTACHED PANEL 191E IS CORRODED AT 2 EA HINGE LOCATIONS. / BLENDED CORROSION AT LOWER FUSELAGE FAIRING 191D DOUBLER AROUND OPENING FOR ATTACHED PANEL 181E. ORIGINAL .100; REMAINING .SDR DALA2019090905216Rub Strip · corrodedCORROSION AT SEVERAL FILLET FAIRING RUBSTRIPS BTW STA Y=560 TO STA Y=848 AND STA Y=858 TO STA Y=917 BOTH SIDES (FUS). NRC 00520: CORROSION LEVEL 2, RUBSTRIPS (8 EA) BTW STA Y=560 TO STA Y=848 AND STA Y=858 TO STA Y=917 BOTH SIDES WERE REPLACED PER SRM 51-20-05SDR SWAA2022031649754Fairing · elongatedACCESS PANEL 193D HAS SEVERAL FASTENER HOLES OVERSIZED AND ELONGATED (AREAS MARKED) / REPAIRED DAMAGED FASTENER HOLES ON 193D ACCESS PANEL IAW SRM 51-40-06-2R-9; RESTORED FINISH PER AMM 51-21-99.SDR SWAA2022031685786Fairing · delaminatedWING TO BODY PANEL 193AR; AFTER SMALL COMPOSITE REPAIR WAS PERFORMED FOUND 2 FOOT DIAMETER AREA OF DELAMINATION CENTERED IN PANEL / RECEIVED AND VERIFIED PNL PART 149A7655-14; PANEL NUMBER 193AR; PREPARED PNL FOR PAINT AND PAINTED HEART BLUE IAW SWA DRAWING 11SDR SWAA2022031638991Former · crackedFAIRING FORMER IS CRACKED BS 663 LBL 26 WL 150 / REPAIRED PER: EA 1-757-16571 REV IR AND ATS ER 19-04701 REV IRSDR SWAA2022031657418Fairing · elongatedWING TO BODY FAIRING PANEL 193B HAS ENLARGED FASTNER HOLES AT LOCATIONS 1-7;10;12;14-24;28-38 / REMOVED AND REPLACED PANEL 193B PER AMM 53-51-21SDR SWAA2022031502717Fairing · delaminatedPNL 193B EXTERIOR SURFACE HAS A SMALL DELAMINATION 4' FROM THE AFT EDGE; CENTER OF THE PANEL. DELAMINATION IS .25' X .25' (MARKED) / REMOVED AND REPLACED 193B PANEL REF AMM 53-51-21SDR SWAA2022031538984Former · crackedFAIRING FORMER IS CRACKED BS 663 RBL 26 WL 150 / REPAIRED PER: EA 1-757-16550 REV IR AND ATS ER 19-04678 REV IRSDR DALA2019090405135Cable · frayedAFT TAILCONE DISPLACEMENT NITROGEN CYLINDER PULL CABLE FRAYED THROUGH. REMOVED AND REPLACED CABLE PER AS REQUIRED PER AMM 53-52. SERVICED NITROGEN CYL PER AMM 12-16. LEAK CHECK GOOD. (LP# 4623321)SDR SWAA2022031503632Fairing · elongated193B PANEL HOLES ENLARGED OUT OF LIMITS / REMOVED AND REPLACED 193B PANEL REF B737 AMM 53-51-21 & SRM 51-20-07; TASK 14108SDR SWAA2022031838909Panel · delaminatedPANEL 193AR HAS DELAMINATION ON THE INNER SURFACE IN THE CORE AREA / DAMAGE PANEL 193AR WAS REPLACED WITH A SERVICABLE PART M NRC T975336SDR SWAA2022031638893Panel · elongatedFAIRING PANEL 195CL HAS ELONGATED HOLE / FAIRING PANEL 195CL WITH ELONGATED HOLE WAS REPAIRED IAW SRM 51-70-05-2R-9 57545U 9-9-19SDR SWAA2022031638897Panel · crackedFAIRING PANEL 195CR IS CRACKED / FAIRING PANEL 195CR CRACK WAS REPAIRED IAW SRM 51-70-05-2R-6SDR SWAA2022031884092Panel · debondedPANEL 193D OUTER SKIN IS DISBONDED ALONG AFT EDGE. (MARKED) / PANEL 193D OUTER SKIN DISBONDED ALONG THE AFT EDGE WAS REPAIRED. IAW SRM 51-70-05-212-1SDR SWAA2022031642083Panel · elongatedPANEL 193B HAS SEVERAL FASTNER HOLES WORN AND ELONGATED. / REMOVED AND REPLACED WING TO BODY FAIRING PANEL 193B IAW AMM 53-51-21.SDR SWIA2019091846331Strap · corrodedEXTERNAL FUSELAGE FS559 ATTACHMENT FLANGE FOR FAIRING 163AB FUSELAGE SIDE HAS DETERIORATED SEALANT PAD AND CORROSION ALL THE WAY ACROSS. (C-CHECK) RO: 09/14/19 REMOVED CORROSION ON EXTERNAL FUSELAGE ATTACHMENT FLANGE FOR FAIRING. REMOVED AND REPLACED 2 EA STRSDR SWAA2022031561929Panel · out of tolerance193B PANEL PER DRAWING 179A7652 HOLES OUT OF LIMITS / DRILLED UP NEW PANEL REF B737 SRM 51-20-07 & BOEING DWG 149A7652SDR DALA2019082805009Cable · frayedFOUND KEVLAR CABLE IN TAIL CONE FRAYED WHILE WORKING 88-0553-8-0066. REPLACED TAILCONE KEVLAR CABLE REF MD88 AMM 53-53 AND DRAWING LONG BEACH 5913350.SDR SWAA2022031553530Radome · delaminatedNOSE RADOME WORN AND DELAMINATED THROUGH BOOT. LARGE AREAS OF PAINT MISSING OVER BOOT. / REMOVED & REPLACED RADOME IAW B737 MM 53-52-00 TRANSACTION #2644984POS:ONLY P/N OFF:1001002-7 P/N ON:1001002-2 S/N OFF:NRD-0529 S/N ON:WN0020/5311CSDR SWAA2022031874562Fairing · crackedLEFT WING TO BODY FAIRING 195CL AFT CORNER RADIUS IS CRACKED / REPAIRED AND RESTORED DECORATIVE TEFLON FINISH TO LEFT WING TO BODY FAIRING 195CL AFT CORNER; IAW B737-700 SRM 51-70-04-2R-6 RREV 68; 53-40-70-2R-1 REV 68; 51-70-04-2R-0 REV 68 GENERAL AND B737-AMMSDR SWAA2022031531938Panel · corroded***CORROSION*** PANEL 192F CORRODED AT MARKER BEACON ANTENNA LOCATION. / CORROSION DAMAGE TO PANEL 192F IS BEYOND ECONOMICAL REPAIR; REQUIRES REPLACEMENT IAW SRM 51-10-02-0G-0 PARA 9. RECEIVED NEW PANEL 192F 149A7752-2; PANEL TO BE INSTALLED ON CARD JPANEL-130SDR DALA2019082654961Cable · misroutedTAIL CONE LOCK IS CABLE ROUTED INCORRECTLY TO THE EXTERIOR RELEASE HANDLE. MAINTENANCE REROUTED THE LOCKING CABLE CORRECTLY TO EXTERIOR HANDLE ASSEMBLY IAW B717 AMM 53-52-01 830-802. RII COMPLETED BY QC2045. (LP #1236960 )SDR SWAA2022031528659Panel · out of tolerance193B PANEL HOLES OUT OF LIMITS / REMOVED AND REPLACED PANEL 193B PER SRM 51-20-07; 51-40-08 AND 51-40-02SDR SWAA2022031537632Panel · out of tolerance193 B WING TO BODY FAIRING PANEL HOLES COUNTER SINKS ARE OUT OF LIMITS. ALL HOLES SHOW SIGNS OF UNSATISFACTORY WEAR. MOD / 193B WING TO BODY FAIRING PANEL HOLES WERE REPAIRED IAW SRM 51-70-05-2R-6 57545U 9-24-19SDR SWAA2022031569921Support · elongatedPANEL 193B PANEL SUPPORT STRUCTURE HAS HAS ELONGATED FASTENER HOLE AT LOCATION 9 / R & R'D NUTPLATE AND OVERSIZED FASTER AT ELONGATED HOLE PER SRM 51-40-02SDR SWAA2022031569922Support · elongatedPANEL 193B PANEL SUPPORT STRUCTURE HAS HAS ELONGATED FASTENER HOLE AT LOCATION 26 / R&R 193AL PANEL I/B SUPPORT STRUCTURE PER SRM 51-40-02; COMMON TO 193B FASTENER HOLE #26SDR DALA2019082835037Fairing · missing(LOG 5564488) CREW REPORTED NOISE AT @7000. FOUND WING BODY FAIRING PANEL 192AL MISSING AND 192BL DAMAGED AS WELL AS SUPPORT FITTING 149A7272-7 DAMAGED. INSTALLED BELLY FAIRING PANELS 192AL AND 192BL, INSTALLED SUPPORT FITTING IAW B737 AMM 53-51.SDR SWAA2022031555581Panel · out of tolerance193B PANEL HOLES OUT OF LIMITS / REMOVED AND REPLACED 193B PANEL REF AMM 53-51-21.SDR SWAA2022031581414Panel · corrodedPANEL 193 B HAS EDGE CORROSION ON CORNERS AT FASTENER LOCATIONS 1;26; AND 33. MEASURMENTS AT LOCATION 1 IS 1.0'; LOCATION 26 (CORNER) .75'X.5' AND LOCATION 33 IS .75'. / REMOVED AND REPLACED 193B PANEL PER 53-51-21SDR SWAA2022031581415Panel · delaminatedPANEL 193B HAS DELAMINATION ON THE LOCATE AT FASTENER CORNER AT FASTENER LOCATION 20 MEASURING 1'X 1' / REMOVED AND REPLACED 193B PANEL PER AMM 53-51-21.SDR SWAA2022031581416Panel · delaminatedPANEL 193 B HAS DELAMINATION ON THE CORNER AT FASTENER LOCATION 7 MEASURING 1.5'X1.25'. / REMOVED AND REPLACED 193B PANEL PER AMM 53-81-21.SDR QMLA201908219071Frame · crackedDURING A 2060 RT AAIP INSPECTION TWO (2) CRACKS WERE FOUND IN THE FRAME 5A WEBBING IN THE TAIL CONE AREA.SDR V0XD201908626001Strap · crackedAFT WING TO FUSELAGE FAIRING PANEL 195DL ATTACHMENT POINT STRAP CRACKED. REMOVED AND INSTALLED STRAP ON PANEL 195DL IAW SRM 51-42-13, 53-00-01, AND 51-40-11.SDR SWAA2022031552051Bracket · crackedRIGHT WING TO BODY FAIRING PNL 191AR AFT SIDE VERTICAL SUPPORT BRACKET AT LEADING EDGE SKIN CRACKED. / REMOVED AND REPLACED RIGHT WING TO BODY VERTICAL SUPPORT BRACKET AT LEADING EDGE SKIN PER SRM 51-40-02.SDR SWAA2022031538233Support · crackedSTRAP CRACKED AT RIGHT WING FWD WTB FAIRING SUPPORT I/B END OF FIXED LEADING EDGE / REMOVED AND REPLACED STRAP AT R/W FWD WTB FAIRING SUPPORT I/B END OF FIXED L/E IN REF B737-700 SRM 51-40-02-0G-0 JS 5083SDR SWAA2022031584015Former · crackedFAIRING FORMER IS CRACKED ON INBOARD END OF LEFT WING LEADING EDGE AT B.S. 500D. / FAIRING FORMER AT INBD L/W FIXED LE REMOVED AND REPLACED IAW B737 SRM 51-40-02 AND DWG 116A3010 AND 116A3110SDR SWAA2022031509609Fairing · cracked3 CANOE CRACKED ON THE INSIDE / REPAIRED PER E/A 1-A57-6168.SDR SWAA2022031585627Support Bracket · brokenLOWER FUSELAGE STA 550 LBL5; FAIRING SUPPORT BRACKET IS BROKEN. / REMOVED AND REPLACED FAIRING SUPPORT BRACKET LOWER FUSELAGE STA 550 LBL 5 IAW B737 SRM 51-40-02; IPC 53-12-11-25SDR SWAA2022031509236Fairing · delaminatedPANEL 193D HAS A DISBOND ON OUTER SURFACE 15 1/2' FROM AFT EDGE AND 12' FROM R/H EDGE / PANEL 193D WITH A DISBOND ON OUTER SURFACE 15 1/2 FROM AFT EDGE AND 12' FROM R/H EDGE WAS REPAIRED IAW SRM 51-70-05-2R-2 59313U 08-19-19SDR SWAA2022031551108Fairing · delaminatedCREW REPORTS WING TO BODY PANEL ABOVE THE RIGHT PACK INLET DOOR SHOWING SIGNS OF DELAMANATION PANEL # 191FRAPPLIED 2 LAYERS OF SPEED TAPE. REF REPAIR EA 53EA-07009ACTION REQUIRED: PERFORM A GVI OF THE SPEED TAPE SECURITY AND DEGRADATION. IF RE-APPLICATION OF TSDR SWAA2022031584009Panel · delaminatedPANEL 194FL HAS TOOL MARKS WITH POSSIBLE DELAMINATION AT FASTENER HOLE (MARKED) / REPAIRED DELAMINATION DAMAGE AT FASTENER HOLE ON PANEL 194FL IAW SRM 51-70-05-2R-1.SDR SWAA2022031584010Panel · delaminatedPANEL 194FR HAS POSSIBLE DELAMINATION ON OUTER SKIN (MARKED) / PANEL 194FR WITH DELAMINATION ON OUTER SKIN WAS REPAIRED IAW SRM'S 51-70-05-2R-2 AND 51-70-05-2R-11. 59702U 08/29/19SDR SWAA2022031451447Support Frame · crackedRT.WING FWD BODY FAIRING STRAKELET SUPPORT FRAME CRACKED AT UPPER END. / REMOVED AND REPLACED RT.WING FWD BODY FAIRING STRAKELET SUPPORT FRAME PER SRM 51-40-02.SDR SWAA2022031456088Fairing · delaminated193 B PANEL DELAMINATED FWD RT I/B CORNER / R&R 193B PANEL IAW AMM 53-51-21 REF SA-M 326 A1073930
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