JASC 5750

Service difficulty reports · 1,158

Reports filed under 5750 · Wing, Control Surfaces, 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 = '5750'
  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 03FDEA00160Hinge Bracket · corrodedLT WING OUTBOARD FLAP, OUTBOARD AFT HINGE, OUTBOARD BORE FITTING, FOUND CORROSION. TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP, OUTBOARD HINGE BRACKET REPAIR CARRIED-OUT IAW EA 1-5750-67572.Feb 20, 2003 · N613FE · Doug MD11FSDR 03FDEA00164Hinge Bracket · corrodedLT WING OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END, OUTBOARD FITTING FOUND CORROSION . WING TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD. FLAP OUTBOARD HINGE BRACKET REPAIR CARRIED OUT IAW E.A. 1-5750-67572.Feb 20, 2003 · N613FE · Doug MD11FSDR QXEA0201925Attach Fitting · damagedPDX - RIGHT HAND OUTBOARD ROLL SPOILER CENTER ATTACH FITTING ON WING HAS DAMAGE. REPAIRED IAW DHC-8 SRM 51-40-00 AND SRM 51-40-11.Nov 8, 2002 · N369PH · Dhav DHC8202SDR USAA020369Structure · chafedPIT - FOUND TRAILING EDGE HAS CHAFE, 59 INCHES INBOARD FROM INBOARD END. BURNISHED/BLENDED AND INSTALLED WEAR PAD PER TYPICAL REPAIR 57-50-17. (M)Sep 27, 2002 · N300AU · Boeing 737301SDR CA020905007Slat Track · worn(CAN) DURING A 'C' CHECK, PREMATURE WEAR OF THE SLAT TRACK PLATING WAS DISCOVERED (PLATING WORN). IT APPEARS THE WORN SURFACE PLATING PROCESS WAS USED. TRACK AFFECTED RAIL : LT SLAT NR 1, RAIL NR 2, RT SLAT NR 1, RAIL NR 2, RT SLAT NR 3, RAIL NR 3Aug 23, 2002 · Bombdr BD7001A10SDR 2002FA0000955Stop · crackedDURING FLAP HANDLE REPLACEMENT, THE FLAP SETTING STOP ASSY WAS REMOVED AND A CRACK WAS FOUND IN THE FULL FLAP NOTCH AND FAILURE OF THE ASSY WAS FORTHCOMING. THIS SAME STOP ASSY HAD BEEN REMOVED 128.7 HOURS EARLIER FOR FLAP SYSTEM INSPECTION AND NO CRACK WASJul 24, 2002 · N96186 · Aviat A1ASDR UPS02238766Flap Track · corrodedINSPECTION TYPE:C+SI PITTING CORROSION IN BORE OF HOLES F+G ON NO3 FLAP TRACK TRACK REPLACED REF NRC 541795 FOR REPLACMENT DETAILS.Jun 13, 2002 · N942UP · Boeing 72722CSDR UIE2002F00000Flap Track · corrodedDURING CURRENT (D) CHECK AT SIAEC, THE NR 5 FLAP TRACK O/B LOWER FLANGE IN THE MID SECTION WAS FOUND WITH LEVEL 1 CORROSION FOR APPROX 10 INCHES. CORROSION MACHINED OUT AND BLENDED MAINTAINING A 100 TO 1 BLEND RATIO TO ENSURE A SMOOTH FLAT SURFACE. AREA MAGNJun 7, 2002 · N355MC · Boeing 747341SDR 2002UALA00929Fitting · crackedRIGHT HAND WING FRONT SPAR OUTBOARD PITCHLOAD FITTING CRACKED AT THE FORWARD UPPER RADIUS ABOVE FITTING LUG, CRACK FOUND AND CONFIRMED. MAJOR REPAIR ACCOMPLISHED. REPLACED OUTBOARD PITCHLOAD FITTING.May 27, 2002 · N604UA · Boeing 767222SDR 0200929970Rib · crackedDuring Overnight CK. in MSP the #5 leading edge rib was found cracked common to the lower most aft fastener hole . The crack was .5" long. Repaired per EA 99-189349.Mar 26, 2002 · N9334 · Doug DC931SDR MWEA020172Angle · brokenLEFT WING OUTBOARD FLAP HINGE FITTING INBOARD ATTACH ANGLE IS BROKEN. -- LOCATED, DRILLED & DEBURRED INBOARD ATTACH ANGLE AND INBOARD RIB ANGLE AND INSTALLED.Mar 19, 2002 · N205ME · Doug DC932SDR MWEA020163FormerINBOARD FIXED VANE OUTBOARD STRUT L/E NOSE FORMER CRACKED. -- REMOVED AND REPLACED DOUBLER.Mar 6, 2002 · N205ME · Doug DC932SDR MWEA020162Angle · crackedLEFT WING OUTBOARD FLAP HINGE FITTING OUTBOARD ATTACH ANGLE IS CRACKED. -- LOCATED, DRILLED AND DEBURRED RIB ANGLE.Mar 6, 2002 · N205ME · Doug DC932SDR MWEA020052Skin · corrodedLEFT HAND OUTBOARD FLAP UPPER SURFACE HAS LIGHT CORROSION AROUND STEEL FASTENERS AND AN AREA OF EXFOLIATION, STATION XFLS 149 TO 155 AT FRONT OF SPAR -- FABRICATED, LOCATED AND INSTALLED REPAIR DOUBLER.Jan 11, 2002 · N803ME · Doug DC981SDR MWEA020039Angle · corrodedLEFT HAND FLAP INTERNAL AT STATION 47 HAS RIB ANGLE ON THE INBOARD SIDE WITH EXFOLIATION CORROSION -- REMOVED, FABRICATED AND INSTALLED RIB ANGLE.Jan 7, 2002 · N803ME · Doug DC981SDR MWEA020005Skin · corrodedRIGHT HAND FLAP STATION 47 RIB TO UPPER SKIN, ATTACH TEE HAS EXFOLIATION CORROSION -- REMOVED, FABRICATED AND INSTALLED RUB STRIPS AND TEE.Jan 4, 2002 · N803ME · Doug DC981SDR CA020110014Aileron · failed(CAN) DURING AILERON DEFLECTION TEST ON GROUND, THE PILOT FOUND THAT THERE WAS ONLY 15 DEG DEFLECTION. MAINTENANCE FOUND THAT THE SEAL RETAINER ON THE WING TRAILING EDGE HAD CAUGHT WITH THE AILERONS LEADING EDGE AND INHIBITED AILERON FUNCTION. THIS CAUSED STJan 1, 2002 · Cndair CL6002B19SDR MWEA011483Spar Cap · crackedRIGHT HAND FLAP LOWER AFT FLAP SPAR CUP IS CRACKED JUST OUTBOARD OF FLEX JOINT -- REMOVED CRACKED SPAR CAP, LOCATED, DRILLED AND INSTALLED NEW SPAR CAP.Dec 12, 2001 · N804ME · Doug DC981SDR AALA20014070Fitting · corrodedAFW - FLAP ATTACH HOLES WERE REAMED TO REMOVE CORROSION. FABRICATE FREEZE FIT PLUGS IN ORDER TO ACHIEVE A MIN 0.001 INCH INTERFERENCE FIT. (M)Dec 4, 2001 · N39367 · Boeing 767323SDR MWEA011473Angle · corrodedRIGHT HAND FLAP HAS EXFOLIATION CORROSION PRESENT ON AN ANGLE THAT CONNECTS A FLAP RIB TO THE LEADING EDGE FLAP SPAR. ANGLE IS LOCATED APPROXIMATELY 24 INCHES INBOARD OF FLAP MIDDLE SUPPORT FITTING -- REMOVED LEADING EDGE RIB TO FACILIATATE OTHER MAINTENANCEDec 4, 2001 · N804ME · Doug DC981SDR DL72S011869Angle · crackedNBR 3 SLAT AFT ANGLE CRACKED AT ACTUATOR ROD END ATTACH REPAIR PER MM 57-54-000-8 FIG 807Nov 27, 2001 · N529DA · Boeing 727232SDR 2001FA0000615Control Cable · corrodedNEW FLAP CABLE (62701-14) ORDERED TO REPLACE EXISTING FLAP CABLE THAT CORRODED ON MS21260 END FITTING WAS ALSO FOUND TO BE PITTED AND CORRODED.Nov 27, 2001 · Piper PA28140SDR DHL2001806015FairingOn take off from Mexico City aborted----discrepancy R/H T/E Inboard flap, inboard actuator fairing FWD section is damaged on inboard side at mating edge, also not flush with wing surface when flaps in up position.1) Removed previous repair at actuator fairing Sep 29, 2001 · N806DH · Doug DC873FSDR RRXA11459Wedge · dentedDURING A MAINTENANCE VISIT FOUND LT WING O/B FLAP I/B TRAILING EDGE WEDGE DENTED AND HOLE, STA XRS 351 TO 380. REMOVED WEDGE, FABRICATED AND INSTALLED IAW SRM 51-1-21,51-1-21D AND DWG 56429704Aug 8, 2001 · N873SJ · Doug DC873FSDR RRXA11285Hinge · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H O/B FLAP SPRING PANEL I/B HINGE AT STA.219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM Jun 14, 2001 · N606AL · Doug DC873FSDR RRXA11197Skin · gougedDURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO L/H O/B FLAP BELOW FLAP HINGE AT STA. XRS340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRMMay 30, 2001 · N606AL · Doug DC873FSDR RRXA11138Fitting · wornDURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO L/H WING EXHAUST GATE OUTBOARD FITTING, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, May 4, 2001 · N996CF · Doug DC862FSDR RRXA11097Skin · gougedDURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO R/H OUTBOARD FLAP UPPER SKIN AT FLAP HINGE 219, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRApr 24, 2001 · N996CF · Doug DC862FSDR RRXA10959Panel · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H WING LOWER T/E PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-9A.Apr 12, 2001 · N602AL · Doug DC873FSDR RRXA10956Exhaust Gate · wornDURING A MAINTENANCE VISIT FOUND A WORN EXHAUST GATE LT FLAP L/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAAW DC-8 SRM 51-1-21A, 51-1-21 AND DWG 56414111.Apr 12, 2001 · N602AL · Doug DC873FSDR RRXA10905Skin · gougedDURING A MAINTENANCE VISIT FOUND A GOUGE AT FLAP HINGE 98 L/H I/B FLAP UPPER SKIN, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1, FIG 2Q.Mar 28, 2001 · N602AL · Doug DC873FSDR RRXA10904Skin · gougedDURING A MAINTENANCE VISIT FOUND A GOUGE TO THE L/H O/B FLAP UPPER SKIN O/B OF FLAP HINGE 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1, FIG 2Q.Mar 28, 2001 · N602AL · Doug DC873FSDR COMA0061011Vane Cap · chafedRIGHT HAND WING INBOARD FLAP INBOARD LEADING EDGE VANE CAP IS CHAFED .020. REMOVED CHAFED VANE CAP AND INSTALLED NEW SERVICEABLE VANE CAP IAW WVAC EO 601R-57-2009.Dec 11, 2000 · N965CA · Cndair CL6002B19SDR QXEA0002365Skin · unbondedYXX- RIGHT HAND AILERON TIP TRAILING EDGE IS DISBONDING. REPAIRED IAW DHC-8 SRM 57-60-63.Aug 2, 2000 · N822PH · Dhav DHC8102SDR UPS00233128Carriage · corrodedINSPECTION TYPE:C+SI NR 3 FLAPTRACK CARRIAGE SPINDLE BORE CORRODED (INTERNALLY) CARRAGE REPLACED. ***CPCP***Jun 7, 2000 · N954UP · Boeing 727185CSDR MALA000403Rib · crackedFOUND DURING C-CHECK, RT LEADING EDGE 611BR HAS SEVERAL CRACKED RIBS. REMOVED CRACKED AREA IAW SRM 57-10-30. NO CRACKS NOTED IAW FFVNDFOB6. INSTALLED REPAIR IAW SRM 57-10-30.May 24, 2000 · N442XJ · Saab 340BSDR UPS00232476Carriage · corrodedINSPECTION TYPE:C+SI, NR 4 FLAP CARRIAGE SPINDLE INNER BORE CORRODED. PART REPLACED IAW TC C57-581-04-3D.Apr 21, 2000 · N938UP · Boeing 727173CSDR RRXA000704Tip Cap · crackedDURING A MAINTENANCE VISIT FOUND A BARE STATIC WICK AND A DOUBLER MISSING AT THE T/E AT STA XW 773, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED, FABRICATED AND INSTALLED DOUBLER AND REPLACED STATIC WICMar 10, 2000 · N831AL · Doug DC873FSDR UPS00231931Carriage · corrodedINSPECTION TYPE:C&SI, FLAP CARRIAGE NR 2 PITTING CORROSION IN BORE OF SPINDLE. CARRIAGE REPLACED IAW OHM 57-52-11..Feb 11, 2000 · N908UP · Boeing 72727CSDR RRXA003395Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON INBD 2 DOORS AT THE LT OTBD UPPER SLOT DOORS 12-30 INCHES FWD OF SPAR BETWEEN STA'S XS448 TO 497 , DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART Jan 11, 2000 · N831AL · Doug DC873FSDR MWEA99832Rib · crackedRIGHT WING TRAILING EDGE RIB IS CRACKED BETWEEN INBOARD AND OUTBOARD SPOILER PANELS. MAINTENANCE FABRICATED AND INSTALLED NEW RIB.Nov 19, 1999 · N300ME · Doug DC915SDR MWEA99830Fitting · crackedRIGHT WING TRAILING EDGE RIB AT STATION XTE 251 HAS A CRACKED FITTING. MAINTENANCE FABRICATED AND INSTALLED NEW FITTING.Nov 19, 1999 · N300ME · Doug DC915SDR MWEA99828Flap · dentedRIGHT FLAP OUTBOARD EDGE HAS A DEEP DENT. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER.Nov 19, 1999 · N300ME · Doug DC915SDR CA990804037Spar · cracked(CAN) 2 LENGTHWISE CRACKS ON UPPER RADIUS OF THE REAR SPAR AT THE OUTBOARD FLAP ATTACHMENT BRACKET ON THE LEFT WING. REPAIR SCHEME REQUESTED.Aug 3, 1999 · Dhav DHC2MK1SDR DHL9980156CFairing · crackedAT C-CHECK, LT WING I/B UPPER AREA WING TO FUS FAIRING SUPPORT BRACKET AT FUSE 910 SUPPORT CRACKED. INSTALLED REPAIR PER SM 51-1-21, 2 X 6.5.Oct 16, 1998 · N801DH · Doug DC873FSDR DHL9872622DFillet · missingAT D CHECK, LEFT WING FILLET PANEL NR 3505 BOTTOM EDGE HAS MISSING FILLER IN SEVERAL AREAS. INSTALLED REPAIR PER SRM 51-40-1 .75 BY 36, N/R 1442.Mar 3, 1998 · N726DH · Boeing 727228SDR CA971125008Winglet · broke off(CAN) AIRCRAFT HIT BY LIGHTNING AND RIGHT WINGLET BROKE OFF. UPPER PORTION OF WINGLET REPLACED. NO OTHER DAMAGE OR FAULTS FOUND. PART TC: 3,858.Oct 31, 1997 · Cndair CL6002B19SDR CALA9701202Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN LT AND RT WING NR 4 FLAP HINGE BRACKETS. THE BRACKETS WERE REMOVED AND REPLACED IAW SRM 51-30-0.Jul 21, 1997 · N541NY · Doug DC932SDR CA970806010Cover Panel · cracked(CAN) LOOSE MATERIAL REPORTED ON UPPER RIGHT WING OUTBOARD OF SPOILER. FOUND MID FLAP COVER PANEL DAMAGED ON RIGHT HAND WING. REFERENCE BOEING SERVICE LETTER 747-SL-57-56 COVER PANEL CRACKS. REPLACED OUTBOARD MID FLAP RIGHT HAND TIE SECTION AS PER MAINTENANCE Jul 14, 1997 · Boeing 747433SDR UPS97223094Casting · corrodedINSPECTION TYPE-D, NR 6 FLAP TRANSMISSION SUPPORT CASTING HAS CORROSION IN HOLES. REPLACED CASTING IAW 51-30-2.Apr 25, 1997 · N913UP · Boeing 72762C
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