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 TWAA0010009Frame · crackedDURING CHECK-C MAINT, THE FAIRING SUPPORT FRAME WAS CRACKED AT STA 946, RBL 7 AND LBL 7. REPAIRED BOTH PER SRM 53-05, FIG 81, PAGE 267.SDR DHL200080163CAngle · crackedAT C CK; LT WING TO FUSELAGE UPPER FAIRING SUPPORT ANGLE CRACKED 1/4 INCH AT STA. 920. PERFORMED STOP DRILL IAW SRM 53-2-0, FABRICATED AND INSTALLED ANGLE IAW SRM 53-2-0. REF: N/R 1437.SDR UPS00433333Flange · corrodedINSPECTION TYPE:C, FUSELAGE CORROSION ON WING TO BODY FAIRING SUPPORT FWD FLANGE AT BS 1000 RBL 10. FAIRING SUPPORT FLANGE REPAIRED IAW SRM 51-40-04 FIG 2.SDR DHL2000740003Radome · lightning strikeIP RADAR TILT INOP, 2P TOOK LIGHTNING STRIKE ON RADOME AREA DURING CLIMBOUT. 1P REMOVED AND REPLACED RADAR TRANCEIVER AND RADAR INDR. OPS CHKD OK PER M/M 5-51-171 PG 201. NO DAMAGE FOUND.SDR DHL200080183CFairing · crackedAT C CK; LT HORIZONTAL STABILIZER, ELEVATOR SUPPORT (2ND) FAIRING SHOWS 2 EA. CRACKS (0.05 INCHES) AT XE 272.0. REMOVED DAMAGED AREA IAW SRM 55-2-0, FIG. 2, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B, FIG 2, FABRICATED AND INSTALLED FAIRING. REF: N/R 10SDR DHL200080147CAngle · crackedAT C CK; LT WING TO FUSELAGE UPPER FAIRING SUPPORT ANGLE SHOWS CRACKS 1/4 INCH & 1/2 INCH AT STA. 660. REMOVED DAMAGED ANGLE IAW SRM 51-1-21 PAGE 1, FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-1-21 PAGE 1. REF: N/R 1431.SDR RRXA002775Fairing · crackedDURING A MAINTENANCE VISIT FOUND A CRACK ABOUT 2 INCHES LONG ON THE O/B REV TOP FAIRING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-107 WITH APPROVED 8110-3 DATED 6-7SDR UPS00433323Support Bracket · crackedINSPECTION TYPE:C, FUSELAGE WING TO BODY FAIRING SUPPORT CRACKED AT BS 1265 BELOW REAR SPAR SPLICE LT. DAMAGE REMOVED AND REPAIR CARRIED OUT IAW SRM 51-40-03 FIG 1.SDR UPS00433322Support Bracket · crackedINSPECTION TYPE:C, FUSELAGE WING TO BODY FAIRING SUPPORT CRACKED AT BS 1265 BELOW LOWER REAR SPAR SPLICE. DAMAGE REMOVED AND REPAIR CARRIED OUT IAW SRM 51-40-03 FIG 1.SDR DHL200070728CSkin · delaminatedAT C CK; AFT CARGO DOOR MOVABLE FAIRING EXTERNAL SKIN HAS DELAMINATION ON DIFFERENT PLACES. INSTALLED FIBERGLASS OVERLAY REPAIR AFT CARGO DOOR FAIRING EXTERNAL SKIN PER B727 SRM 51-40-8 FIG. 1, PAINTED AS REQUIRED IAW B727 M/M 51-20-0. REF: N/R 3347.SDR TWAA0009605Stiffener · crackedDURING CHECK-C MAINT AT STA 996 BODY FAIRING STIFFENER BOTTOM CORD HAD A 6.5 INCH CRACK AND THE REPAIR ANGLE HAD 1.5 INCH CRACK. STOP DRILLED CRACKS PER SRM 53-00. ACCOMP NDT HIGH FREQ EDDY CURRENT ON STIFFENER PER 51-00-03 PART 6. FABRICATED NEW ANGLE AND SDR QXEA0001649Structure · crackedYYC- RIGHT HAND WING TO FUSELAGE LOWER SIDE ''2'' PROFILE UNDER PANEL 92L IS CRACKED. REPAIRED IAW FOKKER SRM 51-31-01.SDR DHL200070710CRib · crackedTAIL CONE INTERIOR RIB CROSS SUPPORT ANGLE CRACKED. REMOVED FIBERGLASS RIB CROSS SUPPORT ANGLE AT TAIL CONE PER SRM 51-30-2. APPLIED FIBERGLASS CLOTH OVERLAY REPIAR TO INTERIOR RIB CROSS SUPPORT ANGLE PER SRM 51-40-8 FIG 1. INSTALLED RIB SUPPORT ANGLE PER SSDR 20000601SH021Seal · tornSHORTLY AFTER TAKEOFF, CREW FELT A VIBRATION IN THE AIRCRAFT. UNABLE TO DETERMINE SOURCE OF THE VIBRATION, CREW DECLARED AN EMERGENCY AND RETURNED TO THE AIRPORT. MAINTENANCE FOUND APPROXIMATELY 4-5 INCH PIECE OF THE WING TO FAIRING SEAL HAD TORN AWAY. ENGISDR TWAA0007506Skin · damagedDURING OP 16 MAINT CHECK, THE TAIL CONE MATING FRAME AND EXTERIOR SKIN HAD HOLE WORN THROUGH ON RT SIDE AT DRAIN CHANNEL, APPROXIMATELY 5 O''CLOCK POSITION. REPAIRED FRAME AND SKIN BY INSTALLING DOUBLERS PER SRM 53-01, PAGE 10, AND SRM 53-01 PAGE 18.SDR QXEA0001172Fairing · delaminatedYYC- AREAS OF DELAMINATION ON LEFT HAND WING TO BODY AERODYNAMIC FAIRING STATION X333.0. REPAIRED IAW HORIZON AIR EA 9-53-557.SDR P2EA00191Angle · crackedSJO - DURING C-CHECK, FOUND THE LEFT WING TO BODY FAIRING SUPPORT AT BS 540 STRINGER 22L WITH CRACK 2 INCHES LONG, .001 INCH WIDE. REPLACED THE LEFT WING TO BODY FAIRING SUPPORT AT BS 540 STRINGER 22 IAW BOEING SB 737-53-1098 SECTION III FIG 3 REV 3 DATED JANSDR P2EA00190Angle · crackedSJO - DURING C-CHECK, FOUND THE RIGHT WING TO BODY FAIRING SUPPORT AT BS 540 STRINGER 22R WITH CRACK 2 INCHES IN LENGTH, .001 INCHES WIDE. REPLACED THE RIGHT WING TO BODY FAIRING SUPPORT AT BS 540 STRINGER 22R IAW BOEING SB 737-53-1098 SECTION III FIG 3 REV 3SDR 20000516SH026Fairing · corrodedDURING ROUTINE MAINTENANCE TO REPAIR FUEL LEAK FROM OVERWING FAIRING ASSY, REMOVED LEFT OVERWING FAIRING AND DISCOVERED EXTREME CASE OF EXFOLIATION CORROSION THAT CAUSED A HOLE THROUGH UPPER WING SKIN. AFTER FINDING CORROSION ON LEFT SIDE, DECIDED TO PULL OFFSDR 20000516SH025Fairing · corrodedDURING ROUTINE MAINTENANCE TO REPAIR FUEL LEAK FROM OVERWING FAIRING ASSY, REMOVED LEFT OVERWING FAIRING AND DISCOVERED EXTREME CASE OF EXFOLIATION CORROSION THAT CAUSED A HOLE THROUGH UPPER WING SKIN. AFTER FINDING CORROSION ON LEFT SIDE, DECIDED TO PULL OFFSDR 20000516SH024Fairing · corrodedDURING ROUTINE MAINTENANCE TO REPAIR FUEL LEAK FROM OVERWING FAIRING ASSY, REMOVED LEFT OVERWING FAIRING AND DISCOVERED EXTREME CASE OF EXFOLIATION CORROSION THAT CAUSED A HOLE THROUGH UPPER WING SKIN. AFTER FINDING CORROSION ON LEFT SIDE, DECIDED TO PULL OFFSDR 20000516SH023Fairing · corrodedDURING ROUTINE MAINTENANCE TO REPAIR FUEL LEAK FROM OVERWING FAIRING ASSY, REMOVED LEFT OVERWING FAIRING AND DISCOVERED EXTREME CASE OF EXFOLIATION CORROSION THAT CAUSED A HOLE THROUGH UPPER WING SKIN. AFTER FINDING CORROSION ON LEFT SIDE, DECIDED TO PULL OFFSDR 20000515SH033Cowling · departedRIGHT HAND MAIN GEARBOX COWLING CAME OFF OF AIRCRAFT DURING FLIGHT. NO DAMAGE TO AIRCRAFT OTHER THAN MGB COWL ITSELF. NO PERSONAL OR PROPERY DAMAGE OCCURRED. (X)SDR DLM88000787Fairing · missingAILERON TRIM WILL NOT MOVE LEFT OR RIGHT IN CRUISE. WORKED IN CLIMB BUT JAMMED IN CRUISE WITH A/P OFF AND ON. FOUND LT AILERON TRAILING EDGE TRIM TAB ROD COVER FAIRING (UPPER PORTION) MISSING. REPLACED COVER. OPERATION NOW CHECKS NORMAL.SDR CALA0000510Clip · out of adjTHE FORCE REQUIRED TO PULL EXTERIOR AND INTERIOR TAIL CONE RELEASE HANDLES FROM THEIR RETAINING CLIPS EXCEEDED LIMITS. THE CLIPS WERE ADJUSTED AND TESTED IAW MM 53-53-00.SDR CALA0000509Cable · frayedTHE FORCE REQUIRED TO DROP TAIL CONE USING AFT PASSENGER ENTRANCE DOOR AND INTERIOR TAIL COMPARTMENT RELEASE HANDLE EXCEEDED LIMITS. MAINTENANCE FOUND TAIL CONE CABLE WORN AND FRAYED WHERE IT PASSES OVER UPPER PULLEY. THE CABLE ASSEMBLY WAS REPLACED IAW MM 5SDR MALA000265Fairing · damagedPLANNING ITEM TO INSPECT LT AND RT WING LEADING EDGE TO NACELLE SKIN FAIRING SEAL SECTION CHAFED. MX REPAIRED PER REPAIR ORDER 72SDS2412.SDR RRXA001905Frame · damagedDURING A MAINTENANCE VISIT FOUND A HOLE TO THE RT SIDE OF THE TAIL CONE INSIDE STA 1940, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-4 AND 51-1-21.SDR RRXA001769Frame · damagedDURING A MAINTENANCE VISIT, FOUND A HOLE TO THE RT. SIDE TAIL CONE INSIDE STA 1940, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-21 AND 51-1-4.SDR UPS00232257Stiffener · corrodedINSPECTION TYPE:C, WING TO BODY FAIRING NR 3334 HAS CORRODED STIFFENER AROUND GROUND FAN DOOR CUTOUT (RT). ALSO, CORROSION ON DOOR CUTOUT CORRODED STIFFENER REPAIRED IAW SRM 51-40-3, FIGURE 1. CORROSION FOUND ON CORNER OF DOOR CUTOUT. CORROSION REMOVED, SKSDR CALA0000413Cable · out of rigTHE FORCE REQUIRED TO DROP THE TAIL CONE USING INTERIOR AND EXTERIOR RELEASE HANDLES EXCEEDED 35 POUNDS. THE TAIL CONE RELEASE SYSTEM CABLES WERE ADJUSTED IAW MM 53-53-00.SDR RRXA001904Frame · damagedDURING A MAINTENANCE VISIT FOUND A HOLE IN THE RT SIDE OF THE TAIL CONE INSIDE AT STA 1953, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-4 AND 51-1-2SDR RRXA001768Frame · damagedDURING A MAINTENANCE VISIT, FOUND A HOLE TO THE RT. SIDE OF THE TAIL CONE INSIDE AT STA 1953, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8 FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-21.SDR RRXA001903Frame · damagedDURING A MAINTENANCE VISIT FOUND A HOLE IN THE RT SIDE OF THE TAIL CONE INSIDE AT STA 1961, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-21 AND 51-1-SDR RRXA001767Frame · damagedDURING A MAINTENANCE VISIT FOUND A HOLE IN THE RT SIDE TAIL CONE INSIDE AT STA 1961, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-21 AND 51-1-4.SDR DHL2000804133Radome · crackedRADOME INNER SKIN CRACKED 1 INCH AT 3 O''CLOCK LT. REMOVED FASTENERS PER SRM 51-1-21. STOP DRILLED PER SRM 53-2-5. FABRICATED DOUBLER PER SRM 53-2-5. CLEANED TREATED AND PRIMED PER 51-1-8. INSTALLED DOUBLER PER SRM 53-2-5. INSTALLED NEW FASTENERS PER SRMSDR DHL2000804128Radome · crackedRADOME INTERNAL ZONE CRACKED 1 INCH AT 8 O''CLOCK POSITION RT. REMOVED FASTNERS PER SRM 51-1-21. STOP DRILLED PER SRM 53-2-5. FABRICATED DOUBLER PER SRM 53-2-5. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED DOUBLER PER SRM 53-2-5. INSTALLED NEW FSDR DHL200080485CAngle · crackedRT WING TO FUSELAGE FAIRING LOWER PART SUPPORT ANGLE CRACKED 1 INCH AT STA 760.00. REMOVED FASTENERS PER SRM 51-1-21. STOP DRILLED PER SRM 53-2-5. FABRICATED DOUBLER PER SRM 53-2-5. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED DOUBLER WITH NEW FASDR DHL200080439CAngle · crackedRT WING TO FUSELAGE FAIRING ANGLE CRACKED .5 INCH AT STA 630. STOP DRILLED PER SRM 53-2-5. FABRICATED DOUBLER PER SRM 53-2-5. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED DOUBLER PER SRM 53-2-5.SDR ASAA0080226Support Bracket · crackedSEA - DURING INSPECTION, THE RIGHT HORIZONTAL FAIRING SUPPORT WAS FOUND WITH A SMALL CRACK EMANATING FROM AN ELONGATED NUTPLATE HOLE ON THE UPPER SECTION OF THE SUPPORT. REPAIRED PER EA 5510-01094. (M)SDR ASAA0080225Plate · looseSEA - DURING INSPECTION, THE SHEAR PIN PLATE ATTAHED TO THE RADIAL FRAME OF THE TAILCONE WAS FOUND LOOSE AT THE 10 O''CLOCK POSITION. UPON REMOVAL OF THE PLATE, MAINTENANCE FOUND THE TWO ATTACHING HOLES ON BOTH SIDES OF THE MAIN ALIGNMENT PIN HOLE WERE ELONGASDR QXEA0000983Fairing · chafedPDX - WING FAIRING 92J CHAFING ON WING RIB AT 1700 LOWER ATTACH PLATE. REPAIRED IAW FOKKER SRM 57-01-01, PAGE 5, PARAGRAPH 3F.SDR 2000UALA00119Radome · bird strikeRETURNED TO EWR DUE TO A BIRD STRIKE. *S/D* ACP BIRD STRIKE AND OVERWEIGHT LANDING INSPECTIONS. REMOVED AND REPLACED NOSE RADOME DUE TO DAMAGE. ALL ELSE CHECKED OK.SDR DHL200072406CTail Cone · puncturedAT C-CHECK, FOUND VERTICAL FIN TAIL CONE ASSY PUNCTURED IN SEVERAL PLACES ON LOWER HALF. REMOVED TAIL CONE IAW B72755-30-41. INSTALLED FIBERGLASS OVERLAY REPAIR AS PER BOEING M/M 51-40-8 FIG 1. USED FIBERGLASS CLOTH STYLE 7781 P/O 931150556 EPOCAST RESIN 5SDR DHL200072434CFairing · crackedAT C CHECK, FOUND LOWER FUSELAGE FAIRING CRACKED AT BS 740 AND ACCESS PANEL 3448R. RENOVED AND REPLACED DAMAGED SECTION OF FAIRING FRAME AT STA 740. ALODINE AND PRIMED AREA.SDR DHL200080368CSupport Bracket · crackedAT C-CHECK, WING UPPER PLATING FAIRING SUPPORT ANGLE CRACKED 1.5 INCH CLOSE TO FRONT SPAR. FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0 PG 9 & SRM 51-1-8 PG 12. N/R 1246SDR TWAA0003734Angle · crackedDURING CHECK-C MAINT, THE LOWER FAIRING ATTACH STRUCTURE CRACKED FWD INBD CORNER OF RT MLG WHEEL WELL, STA 943 RBL 8. REPLACED ATTACHMENT CHANNEL PER SPM 6-70-01 PAGE 3, PARA 4B AND DOUGLAS DRAWING 5930584.SDR TWAA0003733Angle · crackedDURING CHECK-C MAINT, FWD FAIRING ATTACH STRUCTURE WAS CRACKED, FWD INBD CORNER, LT MLG WHEEL WELL STA 943, LBL 8. REPLACED ATTACHMENT CHANNEL PER SPM 6-70-01, PAGE 3 PARA 4B AND DOUGLAS DRAWING 5930584.SDR CALA0000181Cable · out of rigTHE FORCE REQUIRED TO DROP TAILCONE USING EXTERIOR AND INTERIOR RELEASE HANDLES EXCEEDED 35 POUNDS. THE TAILCONE CABLES WERE RIGGED AND DROP CHECK WAS GOOD IAW MM 53-53-00.SDR QXEA0000562Radome · damagedYYC - PAINT FINISH CHIPPED, WIRE MESH IS DAMAGED OR MISSING AND CONDUCTIVE COAT IS PEELED, AT SEVERAL LOCATIONS ON NOSE COMPARTMENT, EXTERIOR SURFACE, RIGHT UPPER QUARTER, STATION X66.0 - X97.0. REPAIRED IAW HORIZON AIR EA 2-53-135.
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