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 SWAA2022020238080Former · crackedL/H FAIRING FORMER AT BS 500D BETWEEN STR18L AND 19L IS CRACKED / REMOVED AND REPLACED L/H FAIRING FORMER BS 500D B/W STR 18L + 19L IAW SRM 51-40-02;51-40-05; DWG #116A3010 + DWG #116A3118; DWG #116A3310SDR SWAA2021102138075Fairing · damagedSUPPLEMENTAL INFORMATION: FAIRING # 193B HAS OVERSIZED HOLES AND CHAFFING ON THE INTERNAL SIDE OF PANEL / OVERSIZED HOLES & CHAFTING DAMAGE TO INNER SURFACE OF FAIRING 193 B WERE REPAIRED IAW SRM 53-40-70; SRM 51-70-05-2R-G; & SRM 51-40-05SDR SWAA2022020105313Panel · crackedKEEL BEAM PANEL 192E FWD L/H MOUNTING BRACKET CRACKED. / R&R'D FWD L/H BRACKET FOR KEEL BEAM PANEL 192E PER SRM 51-40-02SDR IPXA2017092321967Support · corrodedINSPECTION TYPE: C-18, RIGHT AFT LOWER WING TO BODY SUPPORT, FIVE INCHES ABOVE RAT DOOR HAS CORROSION AT INTERSECTION OF BS 1220. REMOVED AND REPLACED THE SUPPORT.SDR FDEA201709192613Panel · missingON ARRIVAL, FOUND A PANEL MISSING AT THE RT OVERWING BODY BS 1147 - 1180. REPLACED THE PANEL IAW SRM 51-40-02.SDR SWAA2022020151346Panel · delaminatedPANEL 193AL DELAMED ON FWD EDGEPERMANENT ACTION REQUIRED:REMOVE AND REPLACE THE DISCREPANT PANEL OR ACCOMPLISH PERMANENT REPAIRS / ACCOMPLISHED PERMANENT REPAIR OF PANEL EDGE PER SRM 51-70-05-2R-0SDR SCNA20170918182Support · wornSUPPORT STRUCTURE FOR RT WTB PANEL (193AR) IS WORN IN SEVERAL SPOTS. BLENDED WEAR SPOTS ON RT PANEL 193AR SUPPORT STRUCTURE. FOUND TO BE 100% AND LOSS. REMOVED AND REPLACED FRAME PART NUMBER 149A7214-20.SDR SWAA2022020166845Panel · brokenPANEL 194BR AFT CORNER BROKEN. / REPAIRED PANEL 194 BR IAW B737-700 SRM 51-70-05-2R-10 REV 62 RESTORED FINISH IAW B737 AMM 51-21-99-300-801 PARA E (6) TABLE 701SDR SWAA2022020151422Fairing · delaminatedPANEL 193AL DELAMED ON FWD EDGE / APPLIED TWO LAYERS OF SPEEED TAPE IAW WI. REPAIR-53EA-04251PERMANENT ACTION REQUIRED: REMOVED AND REPLACE THEDISCREPANT PANEL OR ACCOMPLISH PERMANENT REPAIRSSDR SWAA2022011985049Panel · delaminatedMAIN WHEEL WELL PANEL 193B HAS A DENT WITH DELAM ON EXTERIOR SURFACE 7.5' FROM FORWARD EDGE AND 20.5' FROM RIGHT EDGE / REPAIRED MAIN WHEEL WELL PANEL 193 EXTERIOR SURFACE 7.5 ' FROM FORWARD EDGE AND 20.5 ' FROM RIGHT SIDE EDGE IAW SRM 51-70-04-2R-1 REV 62 PERSDR 2018091200001Skin · corrodedCORROSION ON THE FORWARD TAILCONE SKIN AND GOUGES ON FUSELAGE SPLICE STRAP.SDR DALA2017091106779Cam · out of adjustDURING TAIL ESCAPE SLIDE CHANGE. FOUND THE TAILCONE RELEASE CAM CLOCKED INCORRECTLY. ADJUSTED THE TAIL CONE RELEASE CAM IAW AMM 53-53-02.SDR SWAA2022013112428Tail Cone · delaminatedRH SIDE OF TAIL CONE HAS A 1/4' X 1/4' HOLE WITH DELAMINATION SURROUNDING IT. LOCATED 9 1/4' FROM FWD EDGE OF CONE AND 7' DOWN FROM ACCESS PANEL 318BR. DELAMINATION AREA MEASURES 1 1/2' X 3'. MOD / REPAIRED DAMAGED AREA PER SRM 51-70-04-2R-2.SDR AALA201709299023Structure · crackedCRACK ON SECTION CONNECTION, RIGHT AFT POSITION ON BELLY FAIRING AT STRINGER 42R, BETWEEN FRAME 40 AND 42. REPLACED SECTION CONNECTION IAW SRM 51-72-11.SDR SIMA20170906003Attach Angle · crackedRIGHT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE HAS A 1/2 INCH CRACK JUST FWD OF SPAR 2. REPAIRED THE ATTACH ANGLE IAW ETN-EM-53-142.SDR SIMA20170906004Attach Angle · crackedRIGHT UPPER WING TO FUSELAGE FAIRING UPPER ATTACH ANGLE ON FUSELAGE HAS 1/8 INCH CRACK BETWEEN FRAMES 48-49. REPAIRED THE ATTACH ANGLE IAW SRM 53-23-12.SDR SIMA20170906005Attach Angle · crackedLEFT UPPER WING TO FUSELAGE LOWER ATTACH ANGLE ON WING HAS 1/8 INCH CRACK JUST AFT OF SPAR 2. R & R THE ATTACH ANGLE IAW SRM 51-40-02.SDR DALA2017090706713Cam · wornTAIL CONE RELEASE CAM IS WORN. HAS A GROOVE IN THE RAMP AREA. REPLACED THE CAM ASSY.SDR DALA2017090706705Cam · wornTAIL CONE RELEASE CAM IS WORN. HAS A GROOVE IN THE RAMP AREA. REPLACED CAM ASSY.SDR SWAA2022013174800Fairing · cracked#3 FLAP FAIRING CRACKED; CRACK UNDER FAIRING ADJUSTMENT LINK / REPAIRED # 3 FLAP FAIRING PER SRM 51-70-04-2R. SEE WIPS AND SUB TASKS FOR INDIVIDUAL SIGN OFFSSDR SWAA2022013127615Bracket · crackedFUSELAGE 192E ACCESS PANEL FWD OUTBOARD MOUNTING PAD CRACKED. / REMOVED AND REPLACED FUSELAGE 192E ACCESS PANEL FWD OUTBOARD MOUNTING BRACKET REFERENCE SRM 51-10-02 AND SRM 51-40-02.SDR SIMA20170905005Attach Angle · crackedLEFT FUSELAGE TO WING FAIRING LATERAL PANEL. LOWER ATTACH ANGLE CRACKED AT THE AFT END. R & R THE ATTACH ANGLE IAW ETN-EM-53-142.SDR DXTR2017090401Strake · corrodedFOUND CORROSION ON THE LT AND RT STRAKE, REPAIRED IAW ERO-905194.SDR SWAA2022013112600Fairing · brokenPANEL 192E FWD L/H ATTACH POINT ON KEEL BEAM BROKEN BS 540+10 LBL 5 / REMOVED PNL192E IAW AMM 53-51-21-000-802. REMOVED BROKEN FITTING AT L/H FWD ATTACH POINT ON KEEL BEAM IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED PART #149A7712-41 P.O. 645835 AND INSTALLED FSDR DALA2017090206532Barrel · damagedTHE AFT DEPLOYED SWITCH FOR THE TAILCONE HAS A DAMAGED SET OF TURN BARRELS AND CABLE ENDS. WITH A SECOND CORRODED CABLE FROM THE EXTERNAL HANDLE SWITCH. REPLACED CABLES PER MD88 SRM 53-10-00 ON NR 3. (LP3444131)SDR DALA2017090106519Cable · corrodedTHE AFT DEPLOYED SWITCH FOR THE TAILCONE HAS A DAMAGED SET OF TURN BARRELS AND CABLE ENDS. WITH A SECOND CORRODED CABLE FROM THE EXTERNAL HANDLE SWITCH. REPLACED THE CABLES IAW SRM 53-10-00.SDR DALA2017083106478Retainer · brokenNR 2 THE INTERNAL TAIL CONE HANDLE, RETAINER IS BROKEN. REPLACED BOTH RETAINERS IAW AMM 53-53-00.SDR SWAA2017082915959Support Bracket · crackedLT SIDE OUTER FUSELAGE SUPPORT STRUCTURE FOR WING TO BODY ACCESS PANEL FAIRINGS 191AL AND 195AL SUPPORT BRACKET CRACKED AT BS 500D, BETWEEN STR 18L TO STR 19L. R&R BRACKET IAW SRM & DWG.SDR SWAA2022020137919Panel · elongatedSUPPLEMENTAL INFORMATION: LOWER FUSELAGE EXTERIOR PANEL 193D; AFT EDGE #6 HOLE IS ENLARGED / OUT OF ROUND / REPAIRED LOWER FUSELAGE EXTERIOR PANEL 193D AFT EDGE #6 HOLE I/A/W SRM 51-70-04-2R-9 PAR 4 REV 62 PER SRM 53-40-70-2R-1 PAR 2. B (1) REV 62.SDR SWAA2022020134451Panel · crackedSUPPLEMENTAL INFORMATION: R/H WING TO BODY PNL 196CR AFT TRAILING EDGE RADIUS HAVE A APPROX. 3 IN. CRACK. / REPAIRED DAMAGE PER SRM 53-40-70-2R-1.SDR SWAA2022020141352Panel · corrodedSUPPLEMENTAL INFORMATION: KEEL BEAM PANEL 192F SHOWS CORROSION ON FLAME SPRAY AT ANTENNA LOCATIONS. / IDENTIFIED PART MATERIAL PER SRM 51-70-14-0G-0; FIG 1; TABLE 2. DETERMINED DAMAGE TO BE BEYOND LIMITS PER SRM 51-70-14-1A-0; PARA; 4C. APPLICABLITY OF SRM 51-SDR SWAA2022020137895Fairing · crackedSUPPLEMENTAL INFORMATION: LEFT SIDE OVER WING FAIRING 195CL IS CRACKED IN AFT LOWER RADIUS / PREPPED CLEANED AND REPAIRED CRACK AT AFT LOWER RADIUS UPPER AND LOWER SURFACE ON PANEL 195 CL IAW B737 SRM 51-70-04-2R-0 REPAIR GENERAL PER SRM 51-70-04-2R-8 PAR 4 ( SDR SWAA2022020112571Fitting · brokenPANEL 192E FWD R/H ATTACH POINT ON KEEL BEAM BROKEN / PANEL 192E FWD R/H ATTACH POINT ON KEEL BEAM BROKEN. REMOVED DAMAGE SUPPORT FITTING IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW SUPPORT FITTING IAW SRM 51-40-05-0G-0 AND BOEING DWG 149A7712. INSTALLED NEWSDR IPXA2017090621417Support Angle · corrodedINSPECTION TYPE: C10, RT AFT WING TO BODY FAIRING HAS CORROSION ON OUTER SUPPORT ANGLE AT BS 1180. REPLACED THE SUPPORT ANGLE.SDR SWAA2022020113309Panel · delaminatedUPPER LH PAC PANEL FWD EDGE DELAM / R&R L/H PAC PANEL 192BL ROBBED FROM A/C 7834 ER M/M 21-51-24SDR IPXA2017091421715Frame · crackedINSPECTION TYPE: 3C, TAILCONE AFT END, RT FRAME IS CRACKED AT THE UPPER LATCH. REPAIRED THE TAILCONE FRAME IAW SRM 53-80-07, REPAIR 4.SDR IPXA2017091121600Support · corrodedINSPECTION TYPE: C-10, RT AFT WING TO BODY FAIRING SUPPORT HAS CORROSION, BS 1240. REPAIRED THE SUPPORT IAW SRM 51-70-12.SDR IPXA2017091321682Fitting · crackedINSPECTION TYPE: 3C, TAILCONE RT UPPER HORIZONTAL BEAM END FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED THE BEAM END FITTING IAW DWG AKC7520, AND SRM 51-35-01.SDR SWAA2022011949239None · delaminatedSUPPLEMENTAL INFORMATION: WING TO BODY FAIRING PANEL 194GR HAS DENT WITH DELAMINATION AT FORWARD LOWER CORNER. MARKED. / REPAIRED PER SRM 51-70-05-2R-2.SDR SWAA2022020133657Bracket · crackedSUPPLEMENTAL INFORMATION: L/H SIDE OUTER FUSELAGE SUPPORT STRUCTURE FOR WING T O BODY ACCESS PNL FAIRINGS 191AL AND 195AL STA 500D BETWEEN STR 18L AND 19L SUPPORT BRACKET IS CRACKED A S MARKED / REMOVED 2 EA WING TO BODY FAIRING SUPPORT BRACKETS @ STA 500D FROSDR SWAA2022020149233Fairing · delaminatedSUPPLEMENTAL INFORMATION: RIGHT WING TO BODY FAIRING 194GR HAS DELAMINATION. / REPAIRED DAMAGED AREA PER SRM 51-70-05SDR SWAA2022020108375Frame · crackedR/H SIDE OUTER FUSELAGE SUPPORT STRUCTURE FOR WING TO BODY ACCESS PNL FAIRINGS 191AR AND 195AR STA 500D BETWEEN STR 18R AND 19R SUPPORT BRACKET IS CRACKED AS MARKED / REMOVED RH OUTER FUSELAGE SUPPORT STRUCTURE (FROME) IAW B737-700 SRM 51-40-02; VERIFIED FRAMESDR SWAA2022020108376Bracket · crackedFUSELAGE LOWER LOBE KEEL BEAM STA 546 RBL 5 SUPPORT BRACKET FOR LOWER LOBE ACCESS PNL# 192 E IS BROKEN AS MARKED / REMOVED AND REPLACED SUPPORT BRACKET AT STA 546 5 IAW SRM 51-40-05; SRM 51-40-02-0G-0; AND SRM 51-40-0G-0SDR DALA2017081606279Release Cable · wornTAILCONE RELEASE CABLE ASSEMBLY ON THE LT SIDE HAS WORN AND BROKEN STRANDS. REPLACED THE CABLE ASSEMBLY IAW AMM 53-52-01.SDR SWAA2022013009324Fairing · elongatedWTB PANEL # 194E HAS CHAFFING AND OVERSIZED HOLES ALONG AFT AFT EDGE OF PANEL ON INTERNAL SIDE / CHAFFING AND OVERSIZED HOLES ALONG AFT EDGE ON INTERNAL SIDE OF WTB PANEL # 194E WAS REPAIRED IAW SRM 51-70-05-2R-6 56563USDR SWIA201743696Skin · dentedAFT STRUCTURE OF THE TAILCONE ON LOWER RIGHT SIDE DENTED AND GOUGED 14.75 INCHES L X .002 INCH DEEP AND DENT IS 8.125 INCH L X .250 INCH W X .025 INCH D. REPAIRED IAW REO.SDR WX0A201708113285Retainer · disconnectedTAILCONE UNSAFE LIGHT ILLUMINATED. EMERGENCY DECLARED. RECONNECTED RETAINING BALL ON CABLE & RETURNED EXTERNAL HANDLE TO STOWED POSITION.SDR SWAA2022012738816Fairing · delaminatedPANEL 193D HAS AN AREA OF DELAMINATION ON THE OUTER SKIN / PANEL 193D WITH AN AREA OF DELAMINATION ON THE OUTER SKIN WAS REPAIRED PER SRM 51-20-05-2R-2SDR SWAA2022012709681Fairing · delaminatedWING TO BODY PANEL 193AL HAS COMPOSITE DELAMINATION AT PANEL EDGE / REPAIRED FWD EDGE OF PANEL 193AL AS REQ IAW B737 SRM 53-40-70-2R-1 TABLE 202 REV 62; SRM 51-70-04-2R-0 PARA 4 (L-N) REV 62 & SRM 51-70-14-2R-4 PARA 4 REV 62. RESTORED FINISH IAW AMM 51-21-99-3SDR 2017FA0000344Strake · dentedRIGHT STRAKE TRAILING EDGE DENT. CESSNA ENGINEERING MEMO REF: DQ8718M1 DATED JULY 10, 2017.
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