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 SWAA2022012530967Bracket · brokenPANEL 192E HAS RIGHT FORWARD BRACKET BROKEN / REMOVED AND REPLACED FORWARD R/H BRACKET FOR PANEL 192E PER SRM 51-40-02.SDR SWAA2017061314320Bracket · crackedRT WING TO BODY FAIRING FORWARD BRACKET RT WHEEL WELL CRACKED. R&R BRACKET PER SRM.SDR DALA2017060704556Shaft · brokenDURING A CHECK OF TAILCONE RELEASE MECHANISM, MAINTENANCE FOUND THAT THE RELEASE SHAFT WAS BROKEN. MAINTENANCE REPLACED THE CAM LATCH/LOCK ASSEMBLY. THE TAILCONE WAS ADJUSTED AND RIGGED AFTER INSTALLATION AND FOUND OPERATIONAL. THE RII WAS COMPLETED FOLLOWING SDR MASA2017060712359Seal · cutFOUND LT MLG FWD FAIRING SEAL CUT ON INSPECTING IT PER EO CRJ7/9-32-4018.SDR DALA2017060404473Ball · not seated"TAIL CONE UNSAFE" ILLUM ON OAP. FOUND BALL UNSEATED AT OUTSIDE HANDLE RELEASED INSERTED BALL BACK INTO OUTSIDE MECHANISM. LIGHT OUTS ALL RUN IN GOOD CONDITION PER MM 25-62-01. INSPECTED CABLES ON INTERNAL AND EXTERNAL HANDLES. OK FOR SERVICE RII.SDR SWAA2022012609849Fitting · brokenFWD KEEL BEAM CNTR ACCESS PANEL FWD LH ATTACH POINT ANGLE IS BROKEN OFF / REMOVED AND REPLACED FWD KEEL BEAM CNTR ACCESS PANEL FWD L/H ATTACH FITTING IAW SRM 51-40-02 A55686SDR SWAA2022012609856Fairing · delaminatedLEFT SIDE LOWER BODY FAIRING #192AL; HAS 1' DELAM ON EXTERIOR SKIN. 9.5' FORWARD OF AFT EDGE AND 3.25' OUTBOARD OF INBOARD EDGE. / REPAIRED LEFT SIDE LOWER BODY FAIRING # 192AL EXTERIOR AFT INBOARD SKIN AS REQ IAW B737-700 SRM 51-70-04-2R-1 REPAIR 1 PAR 4 (A-GSDR DALA2017053004518Support · corrodedFAIRING SUPPORT STRUCTURE FOR PANEL 191AL 29" AFT OF L/E AND LBL 5 HAS CORROSION. REMOVED CORROSION FROM PANEL 191AL FAIRING SUPPORT STRUCTURE 29" AFT OF L/E AT LBL 5 ORIGINAL MATERIAL THICKNESS .063", LOSS OF .009", WITH .054" REMAINING IS OUT OF LIMITS IAW SSDR DALA2017060604504Skin · corrodedCORROSION WAS FOUND ON THE EXTERNAL SKIN SURFACE UNDER THE WING TO-BODY FAIRING BETWEEN BS 750 AND 780 FROM S-18R TO S-21R. SEVERAL AREAS WERE FOUND TO BE OUT OF SRM LIMITS. REPAIRED PER ER/A 558393-14.SDR AALA201705309059Mechanism · puncturedTHE AIRCRAFT WAS GROUNDED. TAILCONE EMERGENCY HANDLE RELEASE MECHANISM DECAL OVER DOOR SLOT HAS BEEN PUNCTURED. ACCOMPLISHED ADJ & TEST OF TAIL CONE RELEASE MECHANISM PER AMM 53-53-02 AND REPLACED AFT ENTRY DOOR WARNING DECAL AND EMERGENCY HANDLE COPPER WIRE &SDR DALA2017052904420Support · corrodedFAIRING SUPPORT STRUCTURE FOR PANEL 192AR HAS CORROSION 13" AFT OF L/E AND RBL21 CORROSION. CORROSION FOUND TO BE OUT OF LIMITS REF SRM. REPAIR DAMAGED AREA IAW SRM AND RESTORE FINISHES AMM 51-21, AMM.SDR SWAA2022012683289Panel · delaminatedPANEL 193AR HAS DELAMINATION ON INNER SURFACE. / REPAIRED PANEL 193AR WITH DELAMINATION ON INNER SURFACE IAW SRM 51-70-05-2R-2. 92420U 13JUN17SDR DALA2017060504554Cable · frayedTAIL CONE LATCH RELEASE CABLE RUN 547 HAS SEVERAL BROKEN STRANDS . REMOVED & REPLACED, OPS CHECKED GOOD.SDR DALA2017060504485Cylinder · emptyTAIL CONE DISPLACEMENT CYLINDER EMPTY. SERVICED, OPERATION CHECKS GOOD.SDR SWAA2022012683222Fairing · crackedFAIRING PANEL 191FL IS CRACKED AT A FASTENER HOLE. / REPAIRED FAIRING PANEL 191FL WITH CRACK AT A FASTENER HOLE IAW SRM 57-70-05-2R-6; 92420U 13JUN17SDR SWAA2022012606360Fairing · crackedFAIRING PANEL 191FL IS CRACKED AT A FASTENER HOLE. / REPAIRED FAIRING PANEL 191FL WITH CRACK AT A FASTENER HOLE IAW SRM 57-70-05-2R-6; 92420U 13JUN17SDR SWAA2022012582545Panel · corrodedFWD KEEL BEAM PANEL 192E; FWD PANEL SUPPORT STRUCTURE; HAS MULTIPLE WEAR MARKS AND CORROSION. / REMOVED CORROSION AND WEAR MARKS ON FWD KEEL BEAM SUPPORT STRUCTURE FOR PANEL 192E. VERIFIED MATERIAL LOSS. ORIGINAL THICKNESS .110; REMAINING .094 LOSS OF .016. OUSDR DXTR2017051702Stinger · corrodedTAIL STINGER ASSY HAS SEVERAL AREAS OF MINOR LEVEL 1 CORROSION ON THE LH SIDE AT FS 718-725 ZONE 331. AQRD ERO-895673 PROVIDED ENGINEERING FOR A PERMANENT REPAIR.SDR DALA2017051603928Radome · damagedRADOME HAD TWO AREAS SHOWING FIBER. REPAIRED THE RADOME IAW SRM 53-10-72, REPAIR GENERAL, STEP B.SDR DALA2017051003735Cable · tornTORN TAILCONE CABLE ASSEMBLY. REPLACED THE CABLE IAW AMM 53-53 AND COMPLETED REQUIRED INSPECTION.SDR SWAA2022012476605Retainer Seal · crackedCRACK ON RETAINER SEAL ON FLAP TRACK 3 ON ACCESS PANEL # 542BB AT LT WING / REPLACED RETAINER SEAL ON FLAP TRACK 3 ON ACCESS PANEL #542BB AT LT WING IAW B737-700 SRM 51-10-02SDR SWAA2022012476583Angle · crackedCRACK ON ANGLE - SUPPORT LOCATED ON BS 500D WING TO BODY FAIRING AREA AT LT WING / REPLACED SUPPORT ANGLE LOCATED ON BS 500D WING TO BODY FAIRING AREA AT LT WING IAW B737-700 SRM 51-10 -02 ITEM 9 PAGE 7 AND DRAWING # 116A3010 REV BSDR SWAA2022012466295Fairing · cracked#6 CANOE HAS A SMALL CRACK ON THE INSIDE SURFACE / REPAIRED PER E/A 1-A57-6168.SDR SWAA2022012402470Support · corrodedWING TO BODY SUPPORT STRUCTURE STA. 727C RBL 0 TO RBL 10 HAS CORROSION / REMOVED CORROSION @ STA 727C RBL 0 - RBL 10 IAW SRM 53-60-71-1A-1 STEP 2 (2); VERIFIED MATERIAL LOSS ORIG 'T' = .100. REMAINING + .085 LOSS OF .015 AREA FOUND TO BE OUT OF LIMITS IAW 53-6SDR SWAA2022012402469Support · corrodedWING TO BODY SUPPORT STRUCTURE STA. 727C HAS CORROSION LBL 0 TO LBL 10 / REMOVED CORROSION @ STA 727C LBL 0 - LBL 10 IAW SRM 53-60-71-1A-1 STEP 2 (2); VERIFIED MATERIAL LOSS ORIG 'T' = .100 REMAINING 'T' .082 LOSS OF .018 AREA FOUND TO BE OUT OF LIMITS IAW 53-SDR SWAA2022012425549Support Bracket · crackedSUPPORT BRACKET CRACKED FWD LEFT; PANEL 192F. / REMOVED AND REPLACED PER SRM 51-40-02.SDR SWAA2022012425548Support Bracket · crackedSUPPORT BRACKET CRACKED FWD RIGHT PANEL 192F. / REMOVED AND REPLACED PER SRM 51-40-02.SDR DALA2017050803677Pin · wornTAILCONE LOCK PIN SPADE WORN AR 10:00 POSITION. REPLACED WORN SPADE PIN.SDR DALA2017050803675Lanyard · frayedTAILCONE RELEASE CAM LANYARD FRAYED. REPLACED TAILCONE CAM LANYARD.SDR SWAA2017051613741Skin · delaminatedRIGHT TAIL CONE SKIN DELAMINATED AT BS 1156 +9. REPAIRED SKIN IAW SRM.SDR DALA2017050803717Fitting · brokenDURING OPERATIONAL CHECK OF THE INTERNAL EMERGENCY TAIL CONE RELEASE MECHANISM, HANDLE CLIPS WERE BROKEN. REPLACED IAW SRM 51-30-02.SDR DALA2017050803632Receptacle · looseTAILCONE ACCESS DOOR CAMLOCK RECEPTICALS LOOSE AND MISSING ON TAILCONE. DOOR CONTAMINATED WITH HYDRAULIC FLUID. REPLACED THE RECEPTICALS. OK FOR SERVICE. FOUND HYD LEAK AND REPAIRED.SDR SWAA2022012117688Angle · brokenATTACH ANGLES (2 EA) AT BS 546; LBL 4 AND RBL 4 UNDER FAIRING PANEL 192E ARE BROKEN / ATTACH ANGLES (2 EA) BS 546. LBL 4 AND RBL 4 UNDER FAIRING PANEL 192E REMOVED PER SRM 51-40-02. LOCATED AND DRILLED NEW ANGLES P/N 149A7712-1 & -22 P.O# 629499 IAW SRM 51-40-SDR JJBA20170502019Fairing · puncturedRIGHT FWD WING TO FUSELAGE FAIRING PUNCTURED. REPAIRED IAW SRM 51-70-00, 53-70-28, 51-20-26, AND 51-20-36.SDR SWIA201743293Fairing · dentedFUSELAGE FAIRING DENTED OUT OF LIMITS. REPAIRED IAW SRM.SDR DALA2017050103525Lock · wornTAIL CONE RELEASE MECHANISM UPPER LOCK FOUND WORN. REMOVED AND REPLACED UPPER LEFT LOCK PIN ASSEMBLY IAW TASK 53-52-01-211-802.SDR DXTR2017042701Stinger · corrodedTHE STINGER ASSY HAS CORROSION ON THE OUTER SKIN AT THE 6 O’CLOCK POSITION.SDR SWAA2022012407238Fairing · crackedWTB FAIRING # 195CR IS CRACKED IN RADIUS OF AFT END OF PANEL / WTB FAIRING #195CR WITH CRACK IN RADIUS OF AFT END OF PANEL WAS REPAIRED PER SRM 51-70-05-2R-6 57276U 13MAY17SDR DALA2017042803446Clamp · wornLEFT & RIGHT TAIL CONE RELEASE CABLE CLAMPS WORN. REPLACED THE CABLE CLAMPS. OPS CHECKED GOOD.SDR DALA2017050103510Tail Cone · no testTAILCONE FAILED TEST DROP DUE TO EXCESSIVE FORCE REQUIRED. MAINTENANCE COMPLETED.SDR DALA2017050103509Lanyard · damagedTAIL CONE LANYARD WITH BOX IN POOR CONDITION. MAINTENANCE COMPLETE.SDR DALA2017042503376Cable · frayedDURING TAILCONE INSPECTION FOUND CABLE FRAYED. R & R TAILCONE CABLE IAW AMM 53-53-0.SDR SWAA2022012467862Fairing · elongatedBODY FAIRING PANEL 193D HAS SEVERAL HOLES BLOWN OUT AT AFT END OF PANEL ALSO REQUIRES ONE HOLE TO BE FILLED. / REPAIRED DAMAGE HOLES PER SRM 51-70-06-2R-9SDR DALA2017042503377Handle · unknownDURING TAIL CONE RELEASE SYSTEM FUNCTIONAL CHECK, UNABLE TO ROTATE EMERGENCY HANDLE TO THE UNLOCKED POSITION ON AFT ENTRANCE DOOR. INSPECTION COMPLETE.. ER/A 557676-14 REV 0 ISSUED AND COMPLETE.SDR DALA2017042403324Switch · failedDURING FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM USING AFT PASSENGER ENTRANCE DOOR EMERGENCY HANDLE, AFTER TAILCONE RELEASED FROM ACFT A TAILCONE UNSAFE MESSAGE ON EOAP PANEL IN FLIGHT COMPARTMENT FAILED TO COME ON. REPLACED THE SWITCH S1-538 IAW WDM 52-73-SDR SWAA2022012181580Panel · delaminatedDELAMINATED INNER SKIN OF ACCESS PANEL 193AR WING TO BODY FAIRING ON LOWER FUSELAGE / REPAIRED INNER SKIN OF ACCESS PANEL 193AR WING TO BODY FAIRING ON LOWER FUSELAGE IAW B737-700 SRM 51-70-05-2R-2 REP.2 PAR 4SDR SWAA2022012167929Angle · crackedR/H FWD WING TO BODY CENTER SUPPORT ANGLE IS CRACKED / REMOVED AND REPLACED R/H FWD WING TO BODY CENTER SUPPORT ANGLE PER SRM 51-40-02.SDR DALA2017042003285Panel · gougedGROOVE FOUND AT AFT FUSELAGE LEFT SIDE APPROXIMATELY BS 1862, BELOW HORIZONTAL STABILIZER. REMOVED DAMAGE AND EVALUATED, ORIGINGAL .080, LOSS .036, REMAINING .044, OUT OF ALLOWABLE LIMITS IAW SRM 53-80-01. REMOVED, FABRICATED, AND INSTALLED A NEW FAIRING PASDR DALA2017042003259Cable · frayedRT TAILCONE RELEASE CABLE HAD BROKEN STRANDS, LT CABLE CLAMP WORN. REPLACED THE LEFT CABLE CLAMP. REPLACED THE RT RELEASE CABLE IAW 5350-01077-0101.SDR SWAA2022012029865Fairing · brokenLEFT LOWER FUSELAGE WING TO BODY FAIRING 191FL LOWER AFT CORNER IS BROKEN OFF AS MARKED. / REPAIRED LEFT LOWER FUSELAGE WING TO BODY FAIRING 191FL LOWER AFT CORNER IAW SRM 51-70-04-2R-6 PAR 4 REV 61 PER SRM 53-30-70-2R-1 TABLE 202 REV 61.
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