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 SWAA2018120427314Support · corrodedLOWER FAIRING SUPPORT STRUCTURE CORRODED AT BS 727+2.7, BETWEEN RBL 0 TO RBL 60. REPAIRED SUPPORT IAW SRM AND DWG.SDR SWAA2018120427313Support · corrodedLOWER FAIRING SUPPORT STRUCTURE CORRODED AT BS 727+2.7, BETWEEN LBL 0 TO LBL 60. REPAIRED SUPPORT IAW SRM AND DWG.SDR DALA2018111406630Bottle · low pressureLOW PRESSURE ON TAILCONE JETTISON BOTTLE. SERVICING OF THE TAILCONE NITROGEN CYLINDER - (20011201) WAS PERFORMED PER MD-90 AMM 12-18-01-612-801 STAYING IN TEMPERATURE: 58F, PRESSURE: 2200 PSI. (LP# 0823822)SDR DXTA2018F00145Access Panel · chippedTAILCONE STINGER DAMAGE (CORNER CHIPPED) ENGINEERING MEMO NUMBER DQ16422M1 REV A.SDR JJBA201811098004Rib · crackedCRACKED RIB END ON AFT WING-TO-FUSELAGE FAIRING SUPPORT IN LH MLG WELL. FOUND ADDITIONAL CRACK IN FAIRING SUPPORT WEB STOP-DRILLED CRACK ENDS OF FAIRING SUPPORT WEB. PERFORMED NDI USING 30X MAGNIFIER AND FOUND NO FURTHER CRACKING. RIB END REPLACEMENT AND DEFERSDR SWAA2022022589459Fairing · delaminatedWING TO BODY FAIRING PANEL 193B HAS WEAR AND DELAMINATION ON THE FWD L/H CORNER. / REMOVED AND REPLACED PANEL PER 53-51-21 AMM.SDR SWAA2022022597866Fairing · crackedFOUND CRACK RADIATING FROM SCREW HOLE 20 ON PANEL 193B. CRACK MEASURES 1' IN EACH DIRECTION. MOD / FAIRING 193B WAS REPAIRED IAW SRM 51-70-05-2R-6 ON DEFECT #T908709. 80570U 20MAR19SDR SWAA2022022542708Fairing · crackedFOUND CRACK ON PANEL 193B L=11.5' W=.1'; .9' FWD OF AFT EDGE; 7.5' FROM LEFT EDGE AND 16' FROM RH EDGE; ALSO TOTAL AREA OF DELAMINATION IN WIDTH IS .5'. ( MX NOTE ) / R/R'D PANEL PER SRM 51-40-02 (AMT 89674)SDR SWAA2022022525215Fairing · delaminatedFAIRING PANEL 193B-FASTENER HOLE #33; #38 AND #28 DAMAGE AND DELAMINATION / PERMANENT REPAIR PERFORMED PER SRM 51-70-05-2R-10; REPAIR 10.SDR SWAA2022022525337Panel · crackedWING TO BODY PNL 193B HAS A CRACK IN THE LEADING EDGE OF THE PNL .380' LONG CRACKED THROUGH ALL LAYERS 9' FROM THE LEFT SIDE OF PNL. MOD / REMOVED & REPLACED AMM 53-51-21SDR SWAA2022022470633Panel · delaminatedSUPPLEMENTAL INFORMATION: FUSELAGE PANEL 193 AR HAS PUNCTURE AND DELAM ON INBOARD SKIN (MARKED) / REPAIRED AREA AS MARKED WITH PUNCTURE & DELAM ON (TOOLSIDE) OF PANEL 193AR IAW B737-700 SRM 53-40-70-2R-1 REPAIR 1; SRM 51-70-05-2R-1 REPAIR 1 SRM 51-70-05-2R-0 RSDR SWAA2022022464450Fairing · damagedSUPPLEMENTAL INFORMATION: FAIRING 193AL I/B EDGE IS CHAFED AND MULTIPLE OVERSIZED HOLES. (MARKED) / FAIRING 193AL I/B EDGE WITH CHAFING AND MULTIPLE; OVERSIZED HOLES AS MARKED WAS REPAIRED PER SWA EA# 1-753-33559 REV IR DATED 07NOV2018 AND ATS ER# 18-05109 REVSDR SWAA2022022489176Bracket · crackedKEEL BEAM PANEL 192E FORWARD RIGHT FUSELAGE ATTACH BRACKET CRACKED / REMOVED AND REPLACED ATTACH BRACKET PER SRM 51-40-02SDR SWAA2022022444180Panel · elongatedFASTENER HOLE IS ELONGATED ON WING TO BODY PANEL 194HR (MARKED). / REPAIRED ELONGATED FASTENER HOLE ON WING TO BODY PANEL 194HR IAW SRM 51-70-05-2R-9SDR SWAA2022022427482Former · crackedBS500D FAIRING FORMER JUST ABOVE STR19L IS CRACKED / REMOVED AND REPLACED FRAME (FAIRING FORMER) AT BS 500D STA 19L PER SRM 51-40-02 & DWGS 116A3010; 116A3110SDR SWIA201811045165Bracket · wornAT 12000 THE AIRCRAFT STARTED TO PRODUCE HEAVY UNUSUAL VIBRATION IN THE HULL THE AND A VERY LOUD VIBRATING NOISE. WE DECLARED EMERGENCY AND RETURNED TO FIELD. NO MASTER WARNING AND NO MASTER CAUTIONS MESSAGES AND ALL ENG VIBRATIONS WERE WITHIN NORMAL RANGE. (FSDR DALA2018102306241Tail Cone · unwanted deployWHILE PERFORMING MEET & GREET WALK AROUND AFT TAIL CONE DEPLOYED. TAIL CONE DROPPED DUE TO AFT ENTRY DOOR ACTIVATON PLACARD PUNCTURED, ARM OVER AFT DOOR DEPLOYED. SLIDE DID NOT DEPLOY DUE TO IT BEING PINED. INSTALLED TAIL CONE PER CARD 5350-9645 JOB #000-001: SDR SWAA2022022443113Panel · elongatedWING TO BODY FAIRING PANEL 193B HAS 7 FASTNER HOLES THAT ARE ELONGATED. MOD / R&R PANEL 193B. INSTALLED FASTENERS COMMON TO PANEL 183B PER SRM 51-40-02.SDR DALA2018102306242Pin · missingCANT. FRAME FOR TAILCONE ALL ALIGNMENT PINS FOR TAILCONE HAVE WASHERS ON AFT SIDE OF FRAME. ALIGNMT PIN MISSING AT 3:00 POSITION. FOUND SHIM WASHER ARRANGEMENT ON ALIGNMENT PINS TO BE DEPENDENT ON TAILCONE CLEARANCE CHECK AT EACH ALIGNMENT PIN LOCATION PER AMMSDR 2020FA0000146Radome · damagedIN SERVICE COLLAPSING OF THE NOSE SECTION OF THE RADOME OCCURRED. DURING INCOMING INSPECTION IT WAS NOTICED THAT THE AREA OF COLLAPSE CORRESPONDED WITH THE AREA OF A PREVIOUS REPAIR. THE ACCOMPLISHED REPAIR AND THE MATERIAL USED APPEARS NOT TO BE IN COMPLIANSDR SWAA2022022369526Panel · delaminatedPANEL 194AR HAS DELAMINATION ON OUTER SURFACE (MARKED). / REMOVED DAMAGE; ACCOMPLISHED CORE REPAIR AND ACCOMPLISHED REPAIR TO PANEL REF SRM 51-70-05-2R-2. RESTORED FINISH TO REPAIR REF AMM 51-21-99.SDR SWAA2022022305606Bracket · crackedFUSELAGE L/H FWD WING TO BODY FARING AFT SUPPORT BRACKET CRACKED. / REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-40-02SDR AALA201810299011Angle · crackedAIRCRAFT WAS IN BASE MAINTENANCE. CRACK FOUND ON TITANIUM ANGLE ON BELLY FAIRING AREA FR 42 RIGHT HAND SIDE AT LEVEL OF -Y254 ON LOWER FUSELAGE. REPLACED ANGLE PER SRM 51-72-11.SDR SWAA2022022320392Panel · delaminatedPANEL 193D HAS 2 SMALL AREAS OF DELAMINATION ON OUTER SURFACE.(MARKED) / REPAIRED PER SRM 51-70-05-2R-11.SDR IPXA2018110213554Intercostal · crackedTAILCONE LT UPPER BOX FITTING INTERCOSTAL WAS CRACKED. REMOVED, FABRICATED, AND REPLACED THE INTERCOSTAL IAW DWG AKC7520, AND SRM 51-31-01.SDR IPXA2018102635377Beam · chafedTAIL CONE HORIZONTAL BEAM HAD DEEP CHAFE DAMAGE ON THE RT SIDE. REPAIRED THE HORIZONTAL BEAM IAW DWG AKC7520, AND SRM 51-35-01. MINOR.SDR CALA2018101902134Seal · damagedHUMMING NOISE AND VIBRATION IN CABIN AT ROW 21. NO SPECIFIC LOCATION NOTED. REPLACED WING TO BODY FAIRING SEALS PANEL 192DT REF AMM 53-35-11. VERIFIED SAFETY AND SECURITY OF PANEL INSTALLATION. OP CK OF EEL LIGHTING NORMAL. WING ROOT PANEL HAS EMERGENCY LIGHTISDR SWAA2022022414981Fairing · delaminatedWING TO BODY FAIRING #194AL HAS DELAMINATION; MARKED. / WING TO BODY FAIRING #194AL. DELAMINATION WAS REAPIRED IAW SRM 51-70-05-2R-1 56144U. 10/25/2018.SDR IPXA2018110213559Web · tornTAILCONE RT PATIO DOOR PLATFORM STRUCTURE WAS TORN. REMOVED, FABRICATED, AND REPLACED R/H PATIO DOOR WEB IAW DWG AKC7861 AND SRM 51-35-01.SDR IPXA2018110235595Tail Cone · chafedLEFT SIDE EXTENDED TAILCONE REPAIR FILLER WAS CHAFED BS 2165, BETWEEN Z=35 AND Z=61.5. REPAIRED THE TAIL CONE REPAIR FILLER IAW EO MD11-5350-70353-A.SDR DALA2018101606074Release Cable · wornDURING TAILCONE EMERGENCY RELEASE FOUND COATED CABLE WORN THRU PROTECTIVE COATING. REQUIRES OPERATIONAL CHECK AFTER CABLE REPLACEMENT. REMOVED AND REPLACED WORN CABLE PERFORMED EXTERNAL EMERGENCY TAIL CONE RELEASE PER 5352-7116 C/W RII. (LP 0782148)SDR SWAA2022022403365Frame · crackedFWD L/H WING TO BODY FAIRING SUPPORT FRAME CRACKED. / R&R SUPPORT FRAME PER SRM 51-10-02 AND SRM 51-40-02SDR SWAA2022022422398Attach Bracket · crackedFWD L/H ATTACH BRACKET OF FWD KEEL BEAM PANEL 192E IS CRACKED. / REMOVED AND REPLACED BRACKET PER SRM 51-40-02.SDR IPXA2018101835122Doubler · tornTAIL CONE RT PATIO DOOR WORK PLATFORM SUPPORT STRUCTURE/BEAM HAS TORN REPAIR DOUBLER. REMOVED, FABRICATED AND REPLACED REPAIR DOUBLER IAW SRM 53-80-02 REPAIR 5 .(MINOR)SDR IPXA2018101835115Intercostal · crackedTAIL CONE RT CENTER GUIDE PIN ATTACH INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG AKC7520 AND SRM 51-35-01. (MINOR)SDR DALA2018101005961Cable · brokenCABLE FOR TAILCONE NITROGEN CYLINDER BROKEN. REMOVED AND INSTALLED NEW CABLE FOR TAILCONE NITROGEN CYLINDER PER AMM 20-30. (LP# 0777925)SDR RAIA201810090005Angle · crackedRT WW FWD O/B CORNER WING TO BODY FAIRING L ANGLE NUTPLATE SUPPORT BRACKET IS CRACKED. REMOVED AND FABRICATED L ANGLE.SDR IPXA2018101935166Support · crackedEXTERNAL FUSELAGE FAIRING 144FR AFT SUPPORT CRACK BETWEEN FR 45 AND FR 46. REMOVED AND REPLACED SUPPORT PER SRM 51-40-21.SDR IPXA2018101935164Support · crackedEXTERNAL FUSELAGE FAIRING 143FL AFT SUPPORT CRACK BETWEEN FR 45 AND FR 46. REMOVED AND REPLACED SUPPORT PER SRM 51-40-21.SDR FDEA2018102643013Skin · wornTAIL CONE FOREWARD UPPER LEFT SKIN EDGE HAS WEAR MARKS MARKED NR 5 REPAIRED THE DAMAGE AREA AS REQUIRED REF SRM 53-00-01 FIG. 4 SHEET. 2 VOL. 1.SDR DALA2018100505896Spring · brokenAWR, HIDDEN CRACK: IN REF AMDS 5350-01077-0101 STEP 2. BROKEN SPRING OF TAILCONE EMERGENCY RELEASE MECHANISM AT AFT PASSENGER DOOR UPPER DOOR JAMB. SPRING OF TAILCONE EMERGENCY RELEASE MECHANISM AT AFT PASSENGER DOOR UPPER DOOR JAMB WAS REPLACED PER MD-88 AMM SDR SWAA2022022320930Fairing · delaminatedWING TO BODY FAIRING #193AL HAS AREAS OF DELAMINATION ON OUTER SURFACE / WING TO BODY FAIRING #193AL WITH AREAS OF DELAMINATION ON OUTER SURFACE WAS REPAIRED PER SWA EA# 1-753-33475 REV IR DATED 27-OCT-2018 AND ATS ER# 18-04498 REV IR DATED 27-OCT-2018SDR SWAA2018110426417Support Angle · crackedLT WING LEADING EDGE WING-TO-BODY FAIRING SUPPORT ANGLE CRACKED AT BS 500D, STR 19L. R&R ANGLE PER DWG AND SRM.SDR SWAA2022022315815Fairing · delaminatedPANEL 195CR HAS A DELAMINATION ON THE OUTER SKIN 12' FWD OF THE AFT EDGE / PANEL 195CR DELAMINATION ON THE OUTER SKIN 12IN. FWD OF THE AFT EDGE REPAIRED IAW SRM 51-70-05-2R-2 PER SRM 53-40-70-2R-1 59198U 10/06/18SDR DALA2018100205816Cable · corrodedCORROSION ON TAILCONE INTERNAL PULL CABLE NR 28 AT FITTING. REPLACED AND ADJUSTED CABLE PER AMM 53-53-00. (LP0766216)SDR SWAA2022022319471Panel · elongatedSUPPLEMENTAL INFORMATION: PANEL 194BR HAS AN ELONGATED HOLE / PANEL 194BR ELONGATED HOLE REPAIRED IAW SRM 51-70-05-2R-8 PER SRM 53-60-70-2R-1 59298U 10/04/18SDR SWAA2022022319451Former · crackedSUPPLEMENTAL INFORMATION: FAIRING FORMER UNDER L/H ACCESS PANEL 191AL; BS 500D; WL 191 CRACKED AT FASTENER HOLE (MARKED) / REMOVED & REPLACED NEW FAIRING FORMER P/N 116A3118U9 IAW DRW 116A3010 & SRM 51-40-02-0G-0 88924U 10OCT18SDR SWAA2022022324806Fairing · crackedBELLY BODY FAIRING PNL # 193B HAS CRACKING AROUND 10 EA FASTENER HOLES AS MARKED IN COMPOSITE SKIN / BELLY BODY FAIRING PNL 3 193 B REQUIRED 10 EA FASTENER HOLES IAW B737 SRM 53-040-70-2R-1 REPAIR 1 PARA 4.SDR AALA201809249026Panel · crackedCRACKED RIGHT LEADING EDGE WING TO BODY PANEL 192AR. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED A REPAIR TO THE WING - BODY PANEL IAW EA 285262.SDR VNAA2018092199901Drag Angle · crackedRT TAIL CONE AFT DRAG ANGLE IS CRACKED ON FWD END. INSTALLED RT AFT TAIL CONE AFT DRAG ANGLE IAW SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01.
Back to JASC 5350