JASC 5710
Service difficulty reports · 4,462
Reports filed under 5710 · Wing Main, Frame Structure, newest first.
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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 = '5710' ORDER BY difficulty_date DESC"
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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 = '5710' ORDER BY difficulty_date DESC
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SDR VNAA0601015Structure · ground damageWHILE PARKED AT THE GATE THE RIGHT WING TIP LEADING EDGE TRANSITION FAIRING AND OUTBOARD SLAT WERE HIT BY A VEHICLE. THE FAIRING WAS DENTED AND THE SLAT WAS DENTED & CRACKED. MAINTENANCE REMOVED AND REPLACED THE RIGHT WING TRANSITION FAIRING AND OUTBOARD SLASDR QXEA200600316Fastener · brokenYYC - C3 RIGHT WING UPPER SKIN TRAILING EDGE (OUTBOARD OF MULTI FUNCTION SPOILER) HAS BROKE FASTENER. REPAIRED IAW CRJ700/900 SRM 51-42-06-001-001-A01.SDR 06FDEA0141Stop Fitting · crackedLEFT WING OUTBOARD FLAP SECONDARY UP STOP FITTING FOUND CRACKED. LEFT HAND WING OUTBOARD FLAP SECONDARY UP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA0097Structure · crackedLT WING L/E FOUND 1 CRACK 1" LONG ON CHORD FIXED PANEL AT STA XORS 798. REPAIRED STRINGER DOUBLER IAW SRM 57-10-00 FIG 49 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F160724-3 IAW SRM 57-10-00 FIG 49 VOL 1.SDR DHL2006746001Structure · ground damageRT WING TIP AND OUTBOARD AILERON TRAILING EDGE STRUCK BY UPS TRUCK. REMOVED RT WING TIP, PERFORMED HFEC INSPECTION IAW B727 AMM 5-51-61, HARD LANDING INSPECTION AND NDT MANUAL D6-48875. INSTALLED NEW WING TIP, P/N 65-24965-2 IAW B727 SRM 57-40-10 AND 51-10-3SDR 06FDEA00023Tape · crackedSNRM NO.: N00556 - CRACK FOUND DURING HFEC INSPECTION AT RT WING TANK AT THE END OF STRINGER 12 (UPPER STRINGER) ARB7512-2.SDR VNAA0512017Structure · bird strikeDURING CLIMBOUT FROM BDL THE CREW REPORTED A POSSIBLE BIRD STRIKE. THE FLIGHT CONTINUED TO PIT AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED IMPACT DAMAGE ON THE RT WING INBOARD LEADING EDGE. MAINTENANCE REMOVED AND REPLACED THE RT WING INBOARD LEADING ESDR 05FDEA04355Balance Weight · corrodedRIGHT WING OUTBOARD AILERON BALANCE WEIGHT CORRODED. REMOVED AND REPLACED BALANCE WEIGHT IAW DAC DC10 CMM 57-51-02. CALCULATED NEW BALANCE WEIGHT IAW DC10 SRM 57-50-00 VOL I, SEE FEDEX NONROUTINE NR N00245 OF WORK ORDER NR 00031297.SDR 05FDEA04331Repair · unknownFOUND REPAIR LOCATED ON RIGHT WING L/E WING ROOT REPAIR REQUIRES EVALUATION FOR COMPLIANCE WITH FAA APPROVED DATA. REPAIR WAS DETERMINED ACCOMPLISHED IAW SRM 57-30-4 FIG 2 BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED, CONSISTED OF LOCATION, SHSDR 05FDEA04258Track · wornRT WING L/E SECTION OB OF TRACK NR 3 HAS 5 WEAR MARKS IN L/E LARGEST .400 IN DIA AND THE DEEPEST .04. ALL WEAR MARKS ARE CIRCULAR AND ARE WITHIN FOUR IN OF EACH OTHER REF N00136. REPLACED SKIN IAW DRW A57244112 AND EA 6-5741-94835.SDR 05FDEA04066Structure · crackedHFEC INSPECTED CARRIED OUT AND CRACK FOUND ON LOWER LEFT HAND WING STRINGER S44. REPAIR CARRIED OUT ON CRACK FOUND AT LEFT HAND WING STRINGER 44 AS PER FEDEX EA 1-5720-90707, TITLE: "WINGS - STRINGER 44 LEFT HAND CRACK AT WING STATION XORS=508 - REPASDR 05FDEA03973Hinge · crackedLT WING LEADING EDGE AT STA XOS 906 FOUND ACCESS PANEL TEE/HINGE CRACK .5 INCH LONG. INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 FIG 49 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F163377/N00377 AND IAW SRM 57-10-00 FIG 49 VOL 1.SDR CA051129004Bracket · crackedDURING INSPECTION OF AD 80-11-04, BRACKET P/N 0432001-9 FOUND CRACKED AT THE SAME TIME, REAR SPAR P/N 0432001-56 AND REINFORCEMENT P/N 0432001-15 FOUND ALSO CRACKED. ALL THOSE 3 PARTS REPLACED WITH NEW. AVAILABLE FROM CESSNA.SDR 05FDEA03862Doubler · unknownLT WING LOWER SURFACE FOUND A DOUBLER 24.5 X 8 INCHES ON SKIN AT STA XORS 1070. REMOVED AND REPLACED FASTENERS IAW SRM 57-10-00 FIG 85 VOL 1.SDR 05FDEA03755Repair · undamagedFOUND REPAIR AT NR 4 L/E KRUGER FLAP, RT WING TOP SIDE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR AT NR 4 L/E KRUGER FLAP, RT WING TOP SIDE WAS DETERMINED SDR 05FDEA03397Retainer · looseSTATIC DISCHARGER RETAINER AT RT WING MOST OUTBOARD IS BAD/LOOSE. COMPLIED WITH EA6-5720-92943 REF N00232.SDR 05FDEA03316Hinge · crackedRT OB AILERON 2ND FROM I/B HINGE ASSY FLANGE SECTION MISSING. REMOVED AND REPLACED HINGE ASSY IAW SRM 51-30-2.SDR QXEA200501327Plate · corrodedPDX: RT WING STRESS PANEL LADDER PLATE AFT ROW HAS A SCREW HOLE WITH PITTING CORROSION THAT HAS BEEN BLENDED BEYOND LIMITS. LOCATED AT YW 157.825, APPROX DEPTH IS .017". MAINTENANCE HFEC INSPECTED BLENDED AREA FOR CRACKS IAW Q400 NDTM PART 6, TASK 51-00-02-2SDR IXXA05SMN193SSkin · crackedDURING ROUTINE C CHECK INSPECTION, LT WING. UPPER SKIN AROUND HILOK CRACKED, XRS 72.000 S.9PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 17, EO SEMAN NR 20051211 DATED 09-21-05. REMOVED FASTENERS IAW SRM . REMOVED DAMAGED SECTION IAW SRM 57-2-1 FIG 17. PERFORMSDR IXXA05SMN192SDoor · crackedDURING ROUTINE C CHECK INSPECTION, LT WING NR 2 ALT TANK 506B ACCESS DOOR CRACKED. REMOVED AND REPLACED CRACKED ACCESS DOOR NR 506 B (NR 2 ALT TANK) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE) REFER TO JC 99116 FOR LEAK CHECK.SDR 05FDEA02852Structure · corrodedDURING PASSENGER TO FRIEGHT CONVERSION, FOUND THE SEQUENT PUFFIN CORROSIONS ON THE UPPER LEFT WING SKIN IN THE FOLLOWING ZONES: FROM WING CROSS-SECTION STA XORS 97 TO XORS 1042. NOTE: THE UPPER MENTIONED CORROSIONS HAVE BEEN INDIVIDUALIZED IN 38 POINT. BLENDSDR 05FDEA02851Structure · corrodedDURING PASSENGER TO FRIEGHT CONVERSION, FOUND THE SEQUENT PUFFIN CORROSIONS ON THE UPPER RIGHT WING SKIN IN THE FOLLOWING ZONE: FROM WING CROSS-SECTION STA XORS 402 TO XORS 433. NOTE: THE UPPER MENTIONED CORROSIONS HAVE BEEN INDIVIDUALIZED IN 2 POINT. BLENDOSDR SIMA200525222Fitting · damagedABI - THE RIGHT AILERON PCA FITTING INBOARD BUSHING HOLE WAS FOUND DAMAGED. REMOVED AND THE EXISTING PCA FITTING. INSTALLED NEW PCA FITTING IAW EMB 145 SRM, SRM EMB-145/1142 REV 30, CHAPTERS 51-40-02 AND EMB REPAIR STATEMENT IC2005-145/4844 DATED SEPT 2, 200SDR DHL2005806525Cap · corrodedRT SLANT PANEL UPPER CAP CORRODED, STA XFS 95. PERFORMED MAJOR REPAIR. REMOVED FASTENERS, REMOVED CORROSION FROM RT SLANT PANEL UPPER CAP STA XFS 95 IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 37. PERFORMED DETAIL VISUAL INSP OF REWORKESDR UPS05245442Shear Tie · crackedINSPECTION TYPE:C SUSPECT CRACK IN CENTER TANK FRONT SPAR TO STIFFENER SHEAR TIE CLIP O/B AFT RADIUS LBL 25-08. SHEAR TIE CLIP REPLACED IAW 51-30-02.SDR DHL2005806507Strap · crackedRIGHT WING CTR L/E INTERNAL SPLICE STRAP CRACKED 12 INCHES XW 257.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-3-3 FIG 3 SHEET 3. REMOVED SPLICE STRAP DAMAGED IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. FABRICATED NEW SPLICE STRAP (ASDR 05FDEA02493Rivet · looseLEFT WING TOPSIDE FIXED TRAILING EDGE ISLAND FWD AREA BETWEEN O/B FLAP AND I/B AILERON FOUND WORKING RIVETS ON FORWARD I/B CORNER. LEFT WING TOPSIDE FIXED TRAILING EDGE ISLAND FWD AREA BETWEEN O/B FLAP AND I/B AILERON I/B AND O/B CORNER SKIN TRIMMED. REPAIR SDR 05FDEA02370Shear Tie · crackedRT WING XORS 130 ABOVE STR 36 BEHIND A LOWER PIPE SUPPORT BRACKET THE BULKHEAD WEB HAS A 1.250" CRACK LONG. REPAIR IAW SRM 57-00-01 FIG 12 SHT 4 VOL 1.SDR 05FDEA02365Cap · crackedLT WING XORS 402 BULKHEAD CAP CRACKED FWD OF STR 15. REPAIR IAW EA 8-5710-84859.SDR 05FDEA02355Bulkhead · damagedRIGHT WING XORS 372 FWD OF STR 12 BULKHEAD CAP CRACKED BETWEEN FASTENERS. REPAIR PER EA 8-5710-84863.SDR 05FDEA02275Structure · crackedON LEFT WING FOUND CRACK 1 INCH ON L/E AT STA XORS 455. REPAIR IAW SRM 57-10-00 FIG 18 VOL I.SDR 05FDEA02214Skin · corrodedRIGHT HAND WING UPPER SURFACE TRAILING EDGE FORWARD OF OUTBOARD AILERON SKIN BULGE FOUND AT XORS 979. RTW UPPER SURFACE T/E FWD OF O/B AILERON XORS 979 SKIN BULGE AREA CORROSION REMOVED. MAT'L REMOVED:0.031"; ORIGINAL THK: 0.150"; MAT'L REMAINED: 0119"; FSDR 05FDEA02213Skin · corrodedRIGHT HAND WING UPPER SURFACE TRAILING EDGE FORWARD OF OUTBOARD AILERON SKIN BULGE FOUND AT XORS 989. RTW UPPER SURFACE T/E FWD OF O/B AILERON XORS 989 SKIN BULGE AREA CORROSION REMOVED. MAT'L REMOVED:0.035"; ORIGINAL THK: 0.150"; MAT'L REMAINED: 0.115"SDR 05FDEA02202Structure · unknownRIGHT WING TIP AT STA YW=756 LOWER SURFACE FOUND DOUBLER REPAIR. REMOVED REPAIRED WING TIP IAW AMM 57-23-01-2 DWG ARB2208 ARB2209 AND SRM 51-30-00.SDR 05FDEA02201Structure · damagedWING LT LOWER SIDE AT XORS=391 TO XORS=433 OLD REPAIR QTY 3 EACH DOUBLER. ACCOMPLISH FEDEX EA 8-5710-84114.SDR VNAA0508001Structure · lightning strikeEVIDENCE OF LIGHTNING DAMAGE ON THE RIGHT WINGLET WAS FOUND DURING THE SERVICE CHECK. MAINTENANCE COMPLIED WITH LIGHTNING STRIKE INSPECTIONS IAW CRJ200 AMM 05-51-05-220-803. NO OTHER DEFECTS WERE FOUND. THE WINGLET WAS TEMP REPAIRED IAW BOMBARDIER REO 601R-SDR 05FDEA02052Skin · corrodedLEFT HAND WING UPPER SURFACE MOST INBOARD FOUND 1 EACH SKIN BULGE. LH WING UPPER SURFACE MOST INBD 01 EA. SKIN BULGE AREA CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL. II. MAT'L REMOVED 0.042"; ORIG. THICKNESS 0.241"; MAT'L REMAINED 0.199";SDR SIMA200520601Aileron · damagedLT AILERON AND WING WERE DAMAGED BY A CATERING TRUCK. MAINTENANCE REPLACED LT WING SPAR SEGMENT AND WING SKIN. REPLACED LT AILERON IAW EO. AC WAS RETURNED TO SERVICE. (K)SDR SIMA200520602Sill · corrodedTHE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED DAMAGED SILL AND CLEANED THE AREA. INSTALLED NEW SILL IAW SRM. (K)SDR USAA050897Support Angle · crackedCLT - C-6 - SUPPORT ANGLE, .75 INCH CRACK. SUPPORT ANGLE FOR UPPER FIXED T/E PANEL OB OF NACELLE, LT WING. FABRICATED AND INSTALLLED NEW ANGLE, SRM. (K)SDR IXXA05SMN143SPan · crackedDURING ROUTINE C CHECK INSPECTION, RT WING. CTR L/E ZEE PAN CRACKED 2 INCHES, XFS 520.168. REMOVED AND REPLACED ZEE PAN ON RT WING CTR. L/E XFS 520.168 IAW SRM 51-1-21, SRM 51-1-20 PAGE 9, 21.SDR 05FDEA01732Hinge · corrodedDURING ACCOMPLISHMENT OF EA 1-5750-87541. LT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) OUTBOARD AFT BOLT HOLE FOUND CORRODED. REMOVED AND REPLACED PER AMM 27-50-30-4. FLAP RIGGING CARRIED OUT PER AMM 27-50-30-5.SDR 05FDEA01621Structure · crackedLT WING NR 1 TANK STRUCTURE APPROX ALONG STA XORS 504 SUSPECTED CRACK. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II.SDR 05FDEA01610Stringer · crackedWHILE WORKING N00525, FOUND RT WING UPPER STRINGER NR 10 CRACKED AT WS 686.5 RIB BOLT. REPAIRED STRINGER PER FED EX EA 7-5710-86308.SDR AWXA200500763Fitting · damagedDURING C-10 CHECK, FOUND ELONGATED HOLE ON THE RT WING SIDE LOAD DRAG FITTING. MAINTENANCE OVERSIZED THE HOLE IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (ER) 19-5704-05175-ES3. FABRICATED BUSHING WITH AN INTERNAL HOLE DIAMETER OF .375 IAW SERVICE BULSDR 05FDEA01356Skin · damagedLT WING LOWER SKIN, XORS 455, WITH EXISTING BLEND OUT. BLEND OUT AT LT WING LOWER SKIN, XORS 455 EVALUATED AND FOUND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG 32 VOL I.SDR 05FDEA00615Stiffener · crackedRIGHT WING INTERIOR FUEL CELL UPPER STIFFENER NR 10 IS CRACKED AT WS 686.5. REPAIRED FUEL CELL UPPER STIFFNER NR 10 AT WS 686.5 PER EA 7-5710-86251.SDR 05FDEA00614Stiffener · crackedRIGHT WING INTERNAL FUEL CELL UPPER STIFFENER NR 9 IS CRACKED AT WS 656.5. REPAIRED PER E.A. 7-5710-86251.SDR ASOA05300Housing · corrodedDURING A C-CHECK, THE HOUSING ON FUEL PANEL 622CT BETWEEN RIBS 4 AND 5 ON THE RT WING WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED THE HOUSING ON FUEL PANEL 622CT BETWEEN RIBS 4 AND 5 ON THE RT WING IAW EO. (K)SDR IXXA0500147SRepair · improperDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD FLAP FORWARD UPPER PLATING INTERIM REPAIR AT STA XW 87.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING REPAIR AND THE DAMAGED AREA. FABRICATED NEW PLATING SEGMENT + INTERNAL SPLICE, EXTERNAL DOUBL
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