JASC 5710

Service difficulty reports · 4,462

Reports filed under 5710 · Wing Main, Frame Structure, 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 = '5710'
  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.

SDR COMA0060745Structure · damagedWHILE IN TALLAHASSEE, A BAGGAGE CART STRUCK THE LEFT WINGLET CAUSING DAMAGE TO THE WINGLET TRAILING EDGE (P/N 600-15109-33) AND LOWER OUTBOARD FAIRING (P/N 600-10388-410). THE WINGLET TRAILING EDGE WAS REMOVED AND THE PLANE FERRIED TO ORLANDO UNDER REO 601R-5Sep 16, 2000 · N959CA · Cndair CL6002B19SDR UPS00833758Structure · crackedINSPECTION TYPE:N/A, LT WING SLOT I/B OF NR 1 ENGINE CRACKED.Sep 15, 2000 · N867UP · Doug DC873FSDR ASOA00101Rivet · missingFLT 4815 - DURING FLIGHT TUL-DFW - PASSENGER NOTICED FUEL SPILLING OUT OF THE TOP PORTION OF THE LEFT WING. CAPTAIN CONFIRMED FUEL LEAKAGE AND DECLARED AN EMERGENCY. FLIGHT DIVERTED TO OKC AND LANDED SAFELY. MAINTENANCE INSPECTED SKIN TO RIB ATTACHMENT BRACSep 12, 2000 · N283AS · Emb EMB120RTSDR AWXA0000563Structure · gougedC-CHECK, LT WING BBL 70.85 RTB UPPER CHORD HAS LENGTH WISE GOUGE IN RADIUS FS 663 - 653.Aug 18, 2000 · N184AW · Boeing 737277SDR 20001212AP011Rivet · missingFLT 165 - BOS-MDW - DIVERTED TO SYR AFTER FIVE RIVETS WERE NOTICED MISSING ON THE LEFT WING. THE AIRCRAFT LANDED AT SYR WITHOUT FURTHER INCIDENT. MAINTENANCE CONFIRMED THAT 5 RIVETS WERE MISSING ON THE LEFT WING. THE RIVETS WERE INSTALLED AND THE AIRCRAFT WJul 24, 2000 · N767AT · Boeing 727227SDR QXEA0002024Fastener · loosePDX- RIGHT HAND WING TOP INBOARD AT TRAILING EDGE OF WHITE WALKWAY HAS LOOSE SMOKING RIVETS AT CORNER. REPAIRED IAW FOKKER SRM 57-34-01, SRM 51-10-01, AND SRM 51-31-01, AND HORIZON AIR EA 4-57-439.Jul 7, 2000 · N491US · Fokker F28MK4000SDR UPS00833361Fitting · crackedINSPECTION TYPE:C123, WING CENTER SECTION LONGERON 34R AFT ATTACH FITTING HAS 4 INCH LONG CRACK AT STA 776.0. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-0 AND 51-3-2.Jun 20, 2000 · N708UP · Doug DC871FSDR CA000824021Bolt · cracked(CAN) UPPER FORWARD WING - BOLT FOUND CRACKED DURING ROUTINE INSPECTION.Jun 4, 2000 · Beech B100SDR COMA0010159Clip · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5720-522-0II, THE RIB NR 5 SKIN CLIP WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RTSDR UPS00832811Doubler · crackedINSPECTION TYPE:C123, LEFT WING LOWER INTERNAL DOUBLER IS CRACKED AT XFS 250. REMOVED, FABRICATED AND REPLACED DOUBLER IAW 5769699 AND SRM 51-1- 21.May 20, 2000 · N730UP · Doug DC871FSDR L1GA200000072Structure · corrodedCORROSION FOUND ON LEFT LEADING EDGE INBOARD SIDE TO OUTBOARD SIDE OF WING.May 10, 2000 · N27509 · Doug DC932SDR MALA000319Structure · crackedRIGHT OUTBOARD NACA SCOOP CRACKED AT BOTH AFT CORNERS. SAAB STATEMENT 72SDS1747 DATED 9/2/99. REFER CELSIUS TASK CARD 4542.May 9, 2000 · N407XJ · Saab 340BSDR MALA000318Structure · crackedFOUND DURING C-CHECK, LT OUTBOARD NACA SCOOP CRACKED AT AFT CORNER. SAAB STATEMENT 72SDS1747, REFER TO CELSIUS TASK CARD 4541.May 9, 2000 · N407XJ · Saab 340BSDR MWEA00411Access Panel · puncturedPUNCTURE IN UPPER FORWARD BUTE DOOR, LEFT WING APPROXIMATELY XTE 293. FABRICATED AND INSTALLED A DOUBLER.May 5, 2000 · N900ME · Doug DC915SDR EIAA2000104Shear Tie · crackedHAECO-HKG - C6/D-CHECK - RIGHT WING WS 669.5 RIB UPPER CHORD MOST FORWARD SHEAR TIE FOUND CRACKED. STOP HOLE DRILLED PER BSB 747-54-2273 REV 2 FIG 7, EDDY CURRENT INSP. CUT OUT PER NTM PT 6 51-00-00 FIG 4. NO CRACK BEYOND STOP DRILL HOLE. UPPER CHORD REPAIApr 21, 2000 · N482EV · Boeing 747212BSDR 20000516SH007Bolt · shearedDURING MAINTENANCE TO REPAIR FUEL LEAKS, FIVE STRUCTURAL BOLTS THAT ATTACH THE UPPER WING SKIN TO BEAMS NR 1 AND NR 3 WERE FOUND SHEARED. TWO RT WING BEAM NR 1 BOLTS ALSO SHEARED. THIRTY-TWO WING PLANK TO LT AND RT WING BEAM BOLTS WERE REPLACED A PRECAUTIOApr 17, 2000 · N404CE · Raythn HAWKER800XPSDR MWEA00304Clip · crackedRIGHT WING STATION XRS 111.5 SHEAR CLIP HAS A CRACK AT AFT FLANGE. FABRICATED AND INSTALLED CLIP.Apr 6, 2000 · N900ME · Doug DC915SDR EIAA2000091Spar · crackedEAC-MZJ - C6/D CHECK - NR 3 MAIN TANK CRACKED MID-SPAR WEB APPROX WS 569 AFT SIDE OF UPPER CHORD. REPAIRED PER ECRA 479-57-134-2. TRIMMED WEB OUT AND INSTALLED FILLER, DOUBLERS, AND STIFFENER. (X)Mar 30, 2000 · N479EV · Boeing 747132SDR EIAA2000090Fitting · damagedEAC-MZJ - C6/D-CHECK - DSB AND BACKUP FITTING HOLE LOCATIONS - NR 4 WING POSITION. REPAIRED PER ECRA 479-57-130-2. NR 1 HOLE - REAMED USING EXISTING HOLE LOCATION, NR 2 HOLE - PULLED OUTBOARD 0.063 INCH, NR 3 HOLE - PULLED 0.063 INCH, NR 4 HOLE - PULLED FORWMar 30, 2000 · N479EV · Boeing 747132SDR EIAA2000089Fitting · damagedEAC-MZJ - C6/D-CHECK - DSB AND BACKUP FITTING HOLE LOCATIONS - NR 2 WING POSITION. REPAIRED PER ECRA 479-57-129-2, NR 1 HOLE - REAMED AND PULLED DIRECTLY INBOARD 0.130 INCH, NR 2 HOLE - PULLED DIRECTLY OUTBOARD 0.100 INCH, NR 3 HOLE AND NR 4 HOLE - USED EXISTMar 30, 2000 · N479EV · Boeing 747132SDR EIAA2000088Fitting · damagedEAC-MZJ - C6/D-CHECK - DSB AND BACKUP FITTING HOLE LOCATIONS - NR 1 WING POSITION. REPAIRED PER ECRA 479-57-128-2, NR 2 HOLE - REAMED UP AND PULLED OUTBOARD 0.063 INCH. NR 3 HOLE - REAMED AND PULLED AFT 0.063 INCH, NR 4 HOLE - REAMED AND PULLED FORWARD 0.044Mar 30, 2000 · N479EV · Boeing 747132SDR EIAA2000086Structure · damagedEAC-MZJ - C6/D-CHECK - DSB AND BACKUP FITTING HOLE LOCATIONS - NR 3 WING POSITION. REPAIRED PER ECRA 479-57-121-2, NR 1 HOLE. INSTALLED FREEZE PLUG, NR 2 HOLE - REAMED UP AND PULLED OUTBOARD 100 PERCENT (-0.14 INCH), NR 3 HOLE - INSTALLED 0.56 INCH DIA BOLT Mar 30, 2000 · N479EV · Boeing 747132SDR EIAA2000085Structure · crackedEAC-MZJ - C6/D-CHECK - LEADING EDGE WING CRACKED IN SEVERAL PLACES, CONTINUES PAST FIELD REPAIR AND INTO WEB STRUCTURE AT WING AT APPROXIMATELY STA 557. REPAIRED BY PART 1 OF ECRA 479-57-116-2. INSTALLED REPAIR DOUBLER AND FILLER. (X)Mar 30, 2000 · N479EV · Boeing 747132SDR UPS00831611Stiffner · crackedINSPECTION TYPE:C123 RIGHT WING L/E AT STA XS250.089 VERTICLE STIFFENER IS CRACKED. REMOVED, FABRICATED, AND REPLACED STIFFENER IAW DWG 9753293, AND SRM 51-1-20D.Jan 24, 2000 · N707UP · Doug DC871FSDR 2000ZZZX622Strut · corrodedDURING ANNUAL INSPECTION, FOUND RT WING FORWARD LIFT STRUT, LOWER MOUNT AREA (ON STRUT) SEVERELY CORRODED (EXFOLIATION) AND CRACKED APPROXIMATELY 3 INCHES LONG FROM MOUNT BOLT HOLE UPWARD. AREA IS HIDDEN UNDER FAIRING. SPECIFIC CAUSE IS UNKNOWN. REPLACED PAJan 19, 2000 · N2962Z · Bbavia 8KCABSDR UPS00831427Rib · crackedINSPECTION TYPE:C123, LEFT WING LEADING EDGE SECTION, LOWER RIB PREVIOUS REPAIR CRACKED STA XW 300 DOT D973 PARTS RACK. FABBED REPAIR ANGLE FROM 7075-T6511, FILLERS FROM 7075-T6 IAW DC8 SRM 57-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SJan 9, 2000 · N752UP · Doug DC871FSDR RRXA000703Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AT THE RT WING L/E RIB AFT UPPER END AT STA XFS 741.25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIRED PARTS IAW DC-8 Jan 7, 2000 · N831AL · Doug DC873FSDR 99UAL900651Structure · damagedWHILE TAXIING THE AIRCRAFT FOR MAINTENANCE, THE LEFT-HAND WING HIT A BLAST FENCE, SHEARING OFF THE WING TIP ASSEMBLY AND DAMAGING THE FRONT SPAR LOWER CHORD, LOWER WING SKIN AND THE OUTBOARD FIXED LEADING EDGE SKIN. *S/D* REPLACED THE WING TIP ASSEMBLY AND FDec 14, 1999 · N344UA · Boeing 737322SDR CA991208044Fasteners · undertorqued(CAN) FUEL LEAK FOUND IN RIGHT REAR WING ROOT AREA. SEVERAL SUSPECT FASTENERS TIGHTENED IAW HC536H9043 AND THE LEAK SUBSIDED.Dec 1, 1999 · Bag BAE146200ASDR CA991208046Fasteners · loose(CAN) FUEL LEAK FOUND IN RIGHT REAR WING ROOT AREA. SEVERAL SUSPECT FASTENERS TIGHTENED IAW HC536H9043 AND THE LEAK SUBSIDED.Nov 15, 1999 · Bag BAE146200ASDR 20000505AP011Frame · crackedWING TRAILING EDGE CHORD ANGLE CRACKED BELOW NR 8 SPOILER (WBL 125.0). REPAIRED CRACK PER BOEING SERVICE BULLETIN 727-57-158 R1. (M)Oct 27, 1999 · N887MA · Boeing 727225SDR QXEA9901516Structure · chafedPDX - LEFT LOWER WING MAIN LANDING GEAR OUTBOARD DOOR CUTOUT HAS TWO DEEP CHAFFED AREAS AT AFT SIDE APPROXIMATELY STATION 1800. REPAIRED IAW HORIZON AIR EA 4-57-296.Jul 13, 1999 · N490US · Fokker F28MK4000SDR 99ZZZX2636Bulkhead · damagedMLG ACTUATING STRUT SUPPORT. THIS PIVOT SHAFT IS HELD IN PLACE BY 2 COTTER KEYS AT EACH END. A NAVION B OWNER STATED THE LT MAIN GEAR WOULD NOT RETRACT. UPON PLACING ACFT ON JACKS AND USING AUX HAND PUMP, A GRINDING SOUND WAS HEARD FROM LT HAND GEAR WELL. Jul 4, 1999 · Tmpson NAVIONBSDR ABXA9900639Skin · corrodedCORROSION AT RIGHT WING UPPER SKIN AT FORWARD SPAR, STATION XRS 250. INSTALLED REPAIR DOUBLER IAW ABX REA D857-27330MR.Jun 28, 1999 · N822AX · Doug DC863SDR 99ZZZX2476Structure · damagedAIRCRAFT ENCOUNTERED CLEAR AIR TURBULENCE AT 17,500 FEET WHICH CAUSED THE LEFT AND RIGHT INBOARD WING STRUCTURE TO BUCKLE.Jun 16, 1999 · N9255B · Piper PA46350PSDR QXEA9900569Structure · crackedPDX - TAILBOX STRUCTURE AT STATION 4790 CRACKED BETWEEN RIVETS ATTACHING SHROUD DOOR BELL CRANK PIVOT BRACKET TO TAILBOX. REPAIRED IAW HORIZON AIR EA 4-57-244.Apr 5, 1999 · N475AU · Fokker F28MK4000SDR 99ZZZX950Bolt · corrodedMAIN WING SPAR BOLTS REMOVED IN ORDER TO REMOVE WING FOR REPAIRS. FOUND BOLTS BADLY CORRODED. BOLTS HAVE TO BE REMOVED TO SEE CORROSION. SUBMITTER STATED THIS IS THE THIRD AIRCRAFT IN SIX MONTHS THAT HAS BEEN FOUND IN THIS SHOP.Jan 6, 1999 · N2073M · Piper PA28R201SDR COMA9960006Structure · damagedDURING TAXI, THE RIGHT HAND WING STRUCT A POWER CART. REPAIRED WING.Jan 3, 1999 · N963CA · Cndair CL6002B19SDR DHL99801109Structure · crackedAT C-CHECK, RT CENTER LOWER INT AREA AT STA 337 CRACKED. REMOVED CENTER L/E, FABRICATED REPAIR DOUBLER PER SRM 57-3-3, 25 X 16. INSTALLED PER SRM 51-1-8, INSTALLED CENTER L/E PER 57-20-2.Oct 17, 1998 · N801DH · Doug DC873FSDR CA981013002Structure · damaged(CAN) ON LANDING ROLL OUT, AIRCRAFT STRUCK A DEER AND DAMAGED THE INBOARD LEADING EDGE AND LEFT INBOARD FLAP. THE FLAP WAS REMOVED AND INSPECTED FOR INTERNAL DAMAGE ALONG WITH THE LEADING EDGE. THE FLAP WAS INSTALLED AND SECURED IN THE RAISED POSITION. A LISep 30, 1998 · Beech 1900DSDR 98ZZZX3134Frame · crackedNOTED CRACKS EXTENDING FROM 2 END RIVET ATTACHING HAT CHANNNEL P/N 45-110014-647 TO SKIN, P/N 58-100022-5. FURTHER INVESTIGATION FOUND TOP SKIN CRACKED 6 INCHES LONG, APPROXIMATELY 3 INCHES EACH SIDE OF HAT CHANNEL, PARALLEL TO RIVETS ATTACHING SKIN TO BUTT RAug 14, 1998 · N9446Q · Beech 58SDR 98ZZZX2657Wing · corrodedWHILE DOING ANNUAL INSPECTION REPLACING VERY STIFF TANK HOSE IN THE WING - THE LEFT TANK ON BEING PULLED EXPOSED MOUSE NEST. THE NEST WAS FORWARD OF SPAR AND INBOARD OF TANK ALMOST FILLING 2 SPACES BETWEEEN RIBS. THERE WAS CONNSIDERABLE CORROSION.Jun 23, 1998 · N4345P · Piper PA28180SDR DHL9870635CCenter Section · crackedAT C-CHECK, RT UPPER AT 70.5 WING CENTER SECTION HAS 2 CRACKS AT FWD LOWER HOLE. INSTALLED REPAIR AT RT WING LOWER I/B AND CENTER SECT PER S/B 57-0112. N/R 213.May 20, 1998 · N706DH · Boeing 72722CSDR CA980602057Wing · bird strike(CAN) IN CRUISE, PILOT CAUGHT A FLASH OF MOTION AND HEARD A BIRD IMPACT WITH HIS LEFT WING. DAMAGE WAS VISIBLE FROM THE COCKPIT. WIRES WERE VISIBLE SO ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO BASE. DAMAGE WAS FOUND TO EXTEND FROM STN 204 TO 222. LEADINMay 15, 1998 · Cessna 337GSDR 98ZZZX1917Wing · twistedCUSTOMER REPORTED ACFT HAS A LT WING HEAVY CONDITION IN-FLIGHT. ATTEMPTS TO CORRECT THE CONDITION BY ADJUSTING THE LT WING ECCENTRIC IAW CESSNA 182 SM DID NOT CORRECT THE CONDITION. THE LT WING FLAP HAD TO BE LOWERED ABOUT .3750 INCH TO GET THE AIRCRAFT TO FApr 24, 1998 · N25HP · Cessna 182PSDR COMA9860058Wing Extension · damagedDURING AIRCRAFT DE-ICING, GROUND EQUIPMENT STRUCK THE LEFT HAND OUTBOARD WING. REPLACED THE LEFT HAND WING EXTENSION ASSY FROM WS 353 OUTBOARD.Mar 9, 1998 · N937CA · Cndair CL6002B19SDR AU980107Frame · cracked(AUS) LT AND RT WING ARCH FRAMES CONTAIN NUMEROUS CRACKS. LONGEST CRACK IS MORE THAN 127MM (5IN) IN LENGTH. CAUSED BY CONTACT WITH BRAKE CYLINDERS.Feb 5, 1998 · Piper PA31350SDR 98ZZZX1051Wing Assy · damagedAIRCRAFT OPENED FOR ANNUAL AND FOUND SEVERAL RAT NESTS AND URINE DAMAGE IN BOTH WINGS (NORMALLY SEALED). LARGE RAT NEST AND URINE DAMAGE IN RT WING TRAILING EDGE. WASP/MUD DAUBER NEST IN RT LEADING EDGE ATTACHED TO SPAR CABLES. BIRD NEST IN LT WING. LUSCOMFeb 1, 1998 · N2227K · Luscom 8ASDR CA971223004Wing · bird strike(CAN) ON APPROACH BIRD STRIKE, DUCK, ON LT WING LEADING EDGE STA 276L. LARGE DENT AND RIB DAMAGE, REPAIRED.Dec 10, 1997 · Cessna 208BSDR B4MR97029Structure · corrodedDURING ROUTINE CPCP CHECK INSPECTION, FOUND LT WING L/E AREA, NR 2 L/E FLAP STA 212 HAS SUPPORT ANGLE WEB CORRODED AND CORROSION AROUND ANCHOR NUTS. FOUND CORROSION TO BE OUT OF LIMITS IAW B727 SRM 57-20-1. REMOVED AND REPLACED ACCESS WEBBING PANEL, TOP COVESep 26, 1997 · N284KH · Boeing 7272J0
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