JASC 5720

Service difficulty reports · 13,638

Reports filed under 5720 · Wing Miscellaneous 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 = '5720'
  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 99FDEA00457Bracket · crackedRT WING O/B TRAILING EDGE FLAP, AFT REMOVAL OF FWD FAIRING 635AL FOUND I/B HINGE BRACKET FWD O/B END CRACKED. *S/D* REMOVED AND REPLACED PER MM 57-53-01 AND O/B FLAP ASSY REMOVED AND REPLACED PER MM 27-50-30-4.Nov 1, 1999 · N582FE · Doug MD11FSDR C2XA99IA576Angle · corrodedDURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON LEFT WING FORWARD SPAR, LOWER SPAR CAP AT RIB 19. REMOVED CORROSION, FABRICATED REPAIR ANGLE AND INSTALLED IAW DER REPORT NR 99-209 DER SO423, STRUCTURES. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)Oct 30, 1999 · N14819 · Aerosp ATR42320SDR 20000505AP020Bracket · crackedFOUND 3 INCH CRACK IN NR 8 JACKSCREW FARING AT AFT MOUNT. REMOVED DAMAGED BRACKET AND FABRICATED REPLACEMENT PART. (M)Oct 27, 1999 · N887MA · Boeing 727225SDR 20000505AP015Angle · crackedFOUND 1.25 INCH CRACK AT ANGLE INSIDE LEFT WING TRAILING EDGE AT OUTBOARD END OF AFT FALSE SPAR ACCESS THROUGH PANEL 8407. REMOVED ANGLE AND FABRICATED REPLACEMENT ANGLE AND INSTALLED IAW 51-10-1. (M)Oct 27, 1999 · N887MA · Boeing 727225SDR 20000502AP012Bracket · crackedFOUND BRACKET CRACKED AT RIGHT WING LOWER TRAILING EDGE SUPPORT, OUTBOARD OF NR 6 FLAP TRACK. REMOVED DOUBLER FABRICATED NEW DOUBLER PER SRM 51-40-2 FIG 1. (M)Oct 27, 1999 · N887MA · Boeing 727225SDR UIEA9992Bolt · crackedLEFT WING REAR SPAR STATION 1241, LOWER SPLICE PLATE AND KICK FITTING INBOARD BOLT AND BOLT HOLE HAS CRACK INDICATIONS, VERIFIED WITH HFEC INSPECTION. OVERSIZED KICK FITTING AND REAR SPAR LOWER CHORD BOLT HOLE TO .975 INCH. VERIFIED HOLE IS CRACK FREE WITH HOct 19, 1999 · N505MC · Boeing 7472D3BSDR DL72S992398Stiffener · crackedFOUND DURING MV2 CORROSION VISIT NRC 8 SPAR STIFFENER CRACKED APPROX 1.25 INCH AT NR 2 SLAT O/B TRACK I/B STIFFENER. REPLACED STIFFENER PER M/M 57-20-21 PG 813.Oct 19, 1999 · N539DA · Boeing 727232SDR DL72S992397Bracket · crackedFOUND DURING MV2 CORROSION VISIT NRC 9 I/B AND O/B SLAT ACTUATOR ATTACH BRACKETS CRACKED AT NR 1 SLAT ACTUATOR. REPAIRED PER M/M 57-20-21 PG 812.Oct 19, 1999 · N539DA · Boeing 727232SDR 20000424AP021Angle · crackedFOUND DURING D-CHECK, NR 3 RT STUB WING HAS CRACK INSIDE L/E DOUBLER. REMOVED CRACKED ANGLE. FABRICTED NEW ANGLE, TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-4 AND 51-1-20D. (M)Oct 17, 1999 · N605AL · Doug DC873FSDR QXEA9902240Skin · corrodedPDX - FRETTING CORROSION ON SURFACE THAT THE ANTI-FRET RING CONTACTS. REPAIRED IAW HORIZON AIR EA 9-57-457.Oct 14, 1999 · N827PH · Dhav DHC8102SDR MWEA99692Support · crackedLEFT WING SUPPORT AT STATION XTE 292 HAS A CRACK. MAINTENANCE REMOVED AND REPLACED SUPPORT.Oct 14, 1999 · N806ME · Doug DC981SDR CALA9901379Former · crackedLEFT WING TIP CRACKED IN THREE PLACES (3) INSIDE PANEL. REMOVED FORMER. FABRICATED AND INSTALLED NEW FORMER PER SRM 51-31-01, 57-23-01 AND 51-10-04.Oct 14, 1999 · N68047 · Doug DC1010SDR QXEA9902238Angle · gougedPDX - LOWER FORWARD SPAR LEADING EDGE ATTACH ANGLE IS GOUGED IN THE AREA FOR LEADING EDGE 613AR. REPAIRED IAW DHC-8-102 M/M 20-32-02.Oct 13, 1999 · N827PH · Dhav DHC8102SDR QXEA9902237Angle · gougedPDX - UPPER FORWARD SPAR LEADING EDGE ATTACH ANGLE IS GOUGED IN THE AREA FOR LEADING EDGE 613AR. REPAIRED IAW DHC-8-100 M/M 20-32-02.Oct 13, 1999 · N827PH · Dhav DHC8102SDR QXEA9902236Angle · gougedPDX - LOWER FORWARD SPAR LEADING EDGE ATTACH ANGLE IS GOUGED IN AREA FOR LEADING EDGE 613CR ATTACHMENT. REPAIRED IAW DHC-8-100 M/M 20-32-02.Oct 13, 1999 · N827PH · Dhav DHC8102SDR CALA9901368Beam · crackedTWO CRACKS AT STATION 253 ON TRAILING EDGE MID SPAN BEAM (.75 EACH). INSTALLED DOUBLERS ON RIGHT WING MID SPAN BEAM AND FITTING PER EC/RA 5750-03303.Oct 13, 1999 · N12216 · Boeing 737824SDR CALA9901362Angle · crackedRIGHT WING OUTBOARD FLAP OUTBOARD FAIRING RIGHT SIDE ANGLE IS CRACKED (0.5). REPLACED ANGLE PER SRM 51-33-01.Oct 8, 1999 · N19072 · Doug DC1030SDR WXOA99004Bracket · crackedMHV - DURING AIRCRAFT SCHEDULED INSPECTION AT REPAIR STATION, LEFT WING SLAT TRACK NR 2 FORWARD LOWER PANEL BRACKET CRACKED AND OUTBOARD BRACKET HOLE ELONGATED. REMOVED TWO DAMAGED BRACKETS, FABRICATED REPAIR BRACKETS AND INSTALLED REPAIR BRACKETS IAW DC-9 SROct 6, 1999 · N127NK · Doug DC921SDR 9904689963Doubler · corrodedDURING M CHECK, FOUND CORROSION ON LOWER FLANGE OF THE RIGHT WING FRONT SPAR LOWER TEE BETWEEN XFS=244 AND XFS=257. CORROSION WAS ALSO FOUND ON THE RIGHT WING LEADING EDGE DOUBLER BETWEEN XFS =225 AND XFS=274. THE PRESENT REPAIR WAS DEVELOPED AS AN ALTERNATIOct 6, 1999 · N913RW · Doug DC931SDR UPS99830915Angle · crackedINSPECTION TYPE:C1 RT WING L/E OTBD VERTICAL ANGLE AT XS 522.168 IS CRACKED PAST THE STOP DRILL. REMOVED, FABRICATED, AND REPLACED THE ANGLE IAW DWG 9753297 AND SRM 51-3-0.Oct 5, 1999 · N814UP · Doug DC873FSDR UPS99830912Tee Chord · crackedINSPECTION TYPE:C1 RT WING L/E AT XS 520.168, THE OTBD SLOT, UPPER TEE CHORD IS CRACKED AT THE OTBD END. STOP DRILLED THE CRACK AND REPAIRED THE TEE CHORD IAW SRM 57-2-0 FIG 2.Oct 5, 1999 · N814UP · Doug DC873FSDR GAIA99150Beam · corrodedPHX - DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED DURING FUEL CELL REPAIR THAT THE LOWER TRAILING EDGE PANEL ATTACHMENT TO THE LEFT MLG BEAM HAD CORROSION DAMAGE. REPAIRS WERE COMPLETED IAW FVI DRAWING NUMBER 57-99515-1 AND 8110 DATED OCTOBER 4, 1999. THE Oct 5, 1999 · N858AA · Boeing 727223SDR DL72S992221Casting · crackedFOUND ON D1 LETTER CK, NR 4 SLAT ACTUATOR I/B MOUNT CASTING CRACKED. REPLACED CASTING.Oct 5, 1999 · N544DA · Boeing 727232SDR DL72S992220Stiffner · crackedFOUND ON D1 LETTER CK, NR 4 SLAT I/B TRACK I/B SPAR STIFFENER CRACKED. REPAIRED PER MM 57-20-21.Oct 5, 1999 · N544DA · Boeing 727232SDR UPS99830919Fitting · crackedINSPECTION TYPE:C123, FITTING (P/N 5804007T6013) AT XRS 508, LT WING FOUND TO BE CRACKED. REMOVED, FABRICATED AND REPLACED THE FITTING IAW DWG 5804007 AND SRM 51-1-20D.Oct 4, 1999 · N718UP · Doug DC871FSDR 99ZZZX3947Angle · crackedLOWER TRAILING EDGE PANEL BELOW NR 8 SPOILER ACTUATOR (FALSE SPAR) LOWER CHORD ANGLE CRACKED. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. SUBMITTER SUGGESTED POSSIBLE CAUSE AS WING FLEXING LOADS.Sep 29, 1999 · N887MA · Boeing 727225SDR 99ZZZX3946Beam · crackedRIGHT WING TRAILING EDGE J-BEAM CRACKED (.3750 INCH) ABOVE NR 8 SPOILER ACTUATOR. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. SUBMITTER SUGGESTED POSSIBLE CAUSE AS DESIGN FLAW OR WING FLEXING LOADS.Sep 29, 1999 · N887MA · Boeing 727225SDR MZZA99219Fitting · crackedTNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CRACK WAS FOUND ON LEFT WING BOTTLE PIN. THE CORRODED FITTING WAS REMOVED AND REPLACED WITH A NEW ONE POWER SRM 53-30-02. (M)Sep 28, 1999 · N15781 · Boeing 727232SDR LR7A9960Stiffener · crackedDURING FUEL LEAK INVESTIGATION, FOUND OWS 28 LT WING FLAP TRACK RIB STIFFENER FITTING CRACKED APPROX 3 INCHES THROUGH THREE LOWER INBD ATTACH HOLES. REPLACED STIFFENER IAW SMP 583-57-60 PG 7 AND SMP 583-51-130 PG 47.Sep 28, 1999 · N403LC · Lkheed 382GSDR DHL9974220CAngle · crackedAT C CHECK, LEFT WING L/E CAVITY AT WS 130 RIB ATTACH ANGLE IS CRACKED BEYOND OLD DOUBLER. STOP DRILLED BOTH ENDS OF CRACK ON ANGLE, BEYOND LIMITS. REMOVED AND REPLACED ANGLE PER SRM 51-30-2. N/R 1033.Sep 24, 1999 · N742DH · Boeing 727225SDR 9904669963Press Panel · corrodedDURING M CHECK, CORROSION REMOVED EXCEEDS LIMITS AT 5 FASTENER LOCATIONS ON THE FITH SLAT PRESSURE PANEL LOWER ATTACH ANGLE CAP. REPAIRED PER EA 99-169178.Sep 22, 1999 · N913RW · Doug DC931SDR UF6A990913Stiffener · damagedSBN - LEFT WING RIB STATION 368.366 HAS A CRACKED STIFFENER AT THE LOWER ATTACHMENT POINT. MAINTENANCE FABRICATED AND INSTALLED STIFFENER. ALL WORK WAS DONE IAW BAE ATP SRM 57-40-01. (M)Sep 21, 1999 · N858AW · Bag ATPSDR 99ZZZM709Channel · crackedDURING FIRST ROUTINE 72 MONTH INSPECTION ON THIS AIRCRAFT, WHEN RIGHT WING WEDGE WAS REMOVED, INSPECTION FOUND THE INBOARD SUPPORT CHANNEL, P/N 1159W20194-1XD, S/N 860100 WAS CRACKED. THIS WAS CAUSED BY IMPROPER INSTALLATION DURING AIRCRAFT PRODUCTION. THE WSep 21, 1999 · N232K · Gulstm GIVSDR 99FDEA00477Cover · corrodedNR 782 - RT WING RT STUB TANK PLATE LAND NEEDS RESIDUE REMOVED FWD SPAR ACCESS. CORROSION REMOVED AND REPLACED AREA PER EA NR 75710-45413 DATED 9-29-99 SEEN NR 782 AND JPF AREA ON REVERSE SIDE.Sep 21, 1999 · N190FE · Boeing 72722SDR UF6A990908Bracket · crackedSBN - THE LEFT WING TIP FLUX VALVE MOUNTING BRACKET IS CRACKED. MAINTENANCE REPAIRED BRACKET. ALL WORK WAS DONE IAW BAE ATP SRM 57-30-00, FIGURE 1. (M)Sep 20, 1999 · N858AW · Bag ATPSDR CALA9901270Fitting · corrodedINSPECTION FOUND RT MLG BEAM H FITTING ATTACH HOLE AND UPPER FORWARD LUG CORRODED. THE ATTACH HOLE WAS REPAIRED IAW ECRA 5740-01903, PAGE 2 AND THE FITTING WAS REPLACED.Sep 20, 1999 · N79748 · Boeing 727224SDR CALA9901269Fitting · crackedINSPECTION FOUND A .75 INCH CRACK IN RT WING REAR SPAR O/B ATTACH FITTING FOR MLG. THE FITTING WAS REMOVED AND REPLACED IAW ECRA 5740-01901.Sep 20, 1999 · N79748 · Boeing 727224SDR CALA9901264Vane · gougedINSPECTION FOUND RT WING O/B NR 2 FIXED VANE GOUGED. THE FIXED VANE WAS REMOVED AND REPAIRED IAW DRAWING NR SR09570025. THE VANE WAS REINSTALLED IAW MM 27-51-03.Sep 19, 1999 · N14810 · Doug DC982SDR CALA9901262Vane · puncturedINSPECTION FOUND LT WING I/B FIXED VANE PUNCTURED ON TOP CENTER. THE VANE WAS REMOVED, REPAIRED, AND REINSTALLED IAW MM 27-51-03.Sep 19, 1999 · N14810 · Doug DC982SDR UPS99830795Fitting · crackedINSPECTION TYPE:C123, RT WING O/B SIDE OF THE STA XRS 74.9, THE STR 51 AFT END FITTING WAS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D & 51-3-0.Sep 17, 1999 · N718UP · Doug DC871FSDR EIA990280Chord · crackedTLV - FOUND CRACK IN THE RADIUS OF THE UPPER CHORD OF LEFT WING STATION 669.5 INTERIOR FUEL TANK. CRACKED UPPER CHORD REMOVED. INSTALLED NEW UPPER CHORD IAW SB 57-2273-R2. (M)Sep 17, 1999 · N3203Y · Boeing 747128SDR UPS99830856Doubler · crackedINSPECTION TYPE:C123 RT WING LWR L/E SKIN DOUBLER AT XFS 305 IS CRACKED AT ACCESS PANEL 524B. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5641252 AND SRM 51-1-20D AND 51-1-21.Sep 16, 1999 · N718UP · Doug DC871FSDR UPS99830789Clip · crackedINSPECTION TYPE:C123, RT WING L/E ABOVE AND FWD OF THE NR 3 PYLON CUTOUT STA FS 254.25, THE RIB FWD ATTACH CLIP WAS CRACKED. REMOVED, FABRICATED AND REPLACED THE CLIP IAW DWG 9753294 AND SRM 51-1-20D.Sep 16, 1999 · N718UP · Doug DC871FSDR UPS99830787Doubler · crackedINSPECTION TYPE:C123, RT WING LWR L/E SKIN INTERNAL DOUBLER AT XS 520.168 WAS CRACKED AND A PIECE WAS BROKEN OFF. REMOVED, FABRICATED AND REPLACED THE DOUBLER IAW SRM 57-3-1 FIG 5 AND 51-3-0.Sep 16, 1999 · N718UP · Doug DC871FSDR UPS99830783Angle · crackedINSPECTION TYPE:C123, RT WING L/E, INBOARD SIDE OF THE XS 520.168 RIB, THE SLOT AFT BLKHD VERTICAL ATTACH ANGLE WAS CRACKED AT THE BOTTOM. REMOVED, FABRICATED AND REPLACED THE ANGLE IAW DWG 9753297 AND SRM 51-1-20D.Sep 16, 1999 · N718UP · Doug DC871FSDR UPS99830778Doubler · crackedINSPECTION TYPE:C123, LT WING L/E LWR SKIN DOUBLER AT FS 570.5 WAS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-20D & 51-1-21.Sep 16, 1999 · N718UP · Doug DC871FSDR UPS99830854Ingercostal · crackedINSPECTION TYPE:C123 LT WING L/E AT XFS 115.0, JUST AFT OF THE ACCESS PANEL, THE INTERCOSTAL IS CRACKED AT THE 2ND FROM THE INBOARD FASTENER. REMOVED, FABRICATED, AND REPLACED THE INTERCOSTAL IAW DWG 3653679 AND SRM 51-1-20D.Sep 15, 1999 · N718UP · Doug DC871FSDR UPS99830850Angle · crackedINSPECTION TYPE:C123 LT WING L/E, INBD SIDE OF THE XS 250.089 RIB, THE INBD SLOT AFT BULKHEAD OTBD VERTICAL ANGLE IS CRACKED AT THE LWR END. REMOVED, FABRICATED, AND REPLACED THE ANGLE IAW DWG 9753293 AND SRM 51-1-20D AND 51-3-0.Sep 15, 1999 · N718UP · Doug DC871FSDR UPS99830849Angle · crackedINSPECTION TYPE:C123 LT INBD L/E UPPER AFT ATTACH ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED THE ANGLE IAW DWG 5769646 AND SRM 51-3-0.Sep 15, 1999 · N718UP · Doug DC871FSDR UPS99830798Angle · crackedINSPECTION TYPE:C123, LT WING L/E, FWD OF THE NR 2 PYLON CUTOUT THE L/E RIB FWD ATTACH CLIP WAS CRACKED AT THE LWR END. REMOVED, FABRICATED AND REPLACED THE CLIP IAW DWG 9753294 AND SRM 51-1-20D.Sep 15, 1999 · N718UP · Doug DC871F
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