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 TWAA0009401Support Bracket · puncturedDURING CHECK-C MAINT, THE RT WING T/E BUTE DOOR SUPPORT RAIL, INBOARD RIGHT T/E HAD HOLE PUNCTURED IN IT. MADE BEAM (P/N 5936844-7), CLIP (5936844-13), CLIP (5936814-15) AND HEAT TREATED AND PAINTED PER DOUGLAS DRAWING 5936844. MADE CLIP (P/N 5936824-7) PER Jun 9, 2000 · N9409F · Doug DC983SDR RRXA002707Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED NR 11 RIB ON THE RT WING NR 3 STUB LWR LT RIB ANGLE AT STA XS 246, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EO NR 00-Jun 7, 2000 · N8084U · Doug DC871FSDR UPS00433325Channel · corrodedINSPECTION TYPE:C, RT WING L/E CORROSION ON L/E FALSE WORK SUPPORT CHANNEL AT OLES 1373 4 AND OLES 1444. CORROSION REMOVED DEPTH 10, AREA RE-PROTECTED IAW SRM 51-10-02.Jun 7, 2000 · N521UP · Boeing 747200BSDR UPS00433301Strap · corrodedINSPECTION TYPE:C, RT WING L/E CORROSION ON L/E LOWER IN SPAR SKIN EXT AT OLES 1116 RT. REPAIR CARRIED OUT IAW Q/NOTE 8/2000 AND SRM 57-30-03 FIG 4. BLENDED OUT CORROSION / SPLICE REPAIR.Jun 7, 2000 · N521UP · Boeing 747200BSDR UPS00433300Channel · corrodedINSPECTION TYPE:C, RT WING L/E CORROSION ON L/E LOWER FALSE WORK PANEL FWD OF SUPP CHANNEL AT SEVERAL LOCATIONS AT OLES 1066 OUT TO NR 4 ENG. REPAIR CARRIED OUT IAW QUERY NOTE 4/2000 AND SRM 51-30-01 AND 51-30 -06. REMOVED CORRODED BEAM SECTION AND SPLICE INJun 7, 2000 · N521UP · Boeing 747200BSDR UPS00433302Panel · corrodedINSPECTION TYPE:C, RIGHT WING L/E LOWER FALSE WORK PANEL IS BULGING AT O/B WING JACK PAD LOCATION. REPAIR CARRIED OUT IAW QUERY NOTE 7/2000 AND SRM 57-30-01 AND 57-30-03. BLENDED OUT CORRODED AREA AND INSTALLED FILLER AND RETURNED AREA TO ORIGINAL DIMENSIOJun 6, 2000 · N521UP · Boeing 747200BSDR LR7A00144Angle · crackedDURING SCHEDULED C2 INSPECTION PER JOB CARD HST5713 FOUND RH CWS 220 FWD MINOR BOLT ATTACH ANGLE CRACKED IN LOWER RADIUS AT FWD SPAR.REPLACED ANGLE PER SRM SMP 583-57-30-23. NR 39028.Jun 3, 2000 · N402LC · Lkheed 382GSDR COMA0010157Angle · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5320-243/244-02I, THE WING TO FUSE FAIRING LOWER ATTACH ANGLES WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 1226-9.May 31, 2000 · N257CA · Emb EMB120RTSDR QXEA0001650Screw · incorrectYYC- RIGHT HAND WING LOWER JOINT STRIP AT STATION 11253 HAS DAMAGE FROM INCORRECT LENGTH SCREW. REPAIRED IAW HORIZON AIR EA 4-57-417 AND FOKKER SRM 57-01-01.May 30, 2000 · N480AU · Fokker F28MK4000SDR QXEA0001636Bracket · wornYYC- LEFT HAND NR 1 LIFTDUMPER SPIGOT HOLES ARE WORN IN MOUNTING BRACKET. REPAIRED IAW HORIZON AIR EA 4-57-423.May 30, 2000 · N480AU · Fokker F28MK4000SDR DHL2000801128Fitting · crackedRIGHT WING FITTING UPPER PART CRACKED 2 INCHES AT STA XRS 421.000. REMOVED CRACKED FITTING PER SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA PER SRM 51-1-8B. INSTALLED NEW FITTING PER SRM 51-1-20D.May 27, 2000 · N801DH · Doug DC873FSDR RRXA002706Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED RT SIDE ON THE RT WING NR 3 STUB WING NR 11 RIB LOWER ANGLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW ANGLE IAW DC-8 SRM 51-1-May 24, 2000 · N8084U · Doug DC871FSDR TSAA0057142Beam · gougedREPAIRED LT MLG BEAM AT THE OUTBOARD STABILIZER ATTACH POINT. REPAIR CONSISTS OF BLENDING OUT GOUGE AND REAMING OUT FASTENER HOLES AND INSTALLATIONS OF BUSHINGS IAW ECO 3146. AIRCRAFT RETURNED TO SERVICE. (M)May 22, 2000 · N807AL · Boeing 7372T4SDR UPS00832887Angle · crackedINSPECTION TYPE:C123, LEFT WING L/E VERTICAL ANGLE IS CRACKED AT XS 250.089. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9753293 AND SRM 51-1-20D, 51-1-21.May 21, 2000 · N730UP · Doug DC871FSDR UPS00832819Angle · crackedINSPECTION TYPE:C123, LEFT WING L/E ANGLE IS CRACKED AT XS 520. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5769589 AND SRM 51-1-20D.May 21, 2000 · N730UP · Doug DC871FSDR DHL200070720CDoubler · crackedCORRUGATED DOUBLER CRACKED AT T/E AREA L/W SPAR LOWER SECTION APPROX WS 546.5 (I/B SECTION OF STATION). STOP DRILLED CRACK AT CORRUGATED STRAP AT FT WING REAR SPAR AT WS 546.5 PER SRM 51-10-1. PERFORMED HFEC INSP PER NDT MAN PART 6-51-00-00 FIG 4. NO CRACK May 20, 2000 · N707DH · Boeing 72722SDR L1GA200000139Angle · misdrilledHOLE DRILLED IN ATTCH ANGLE RADIUS XRS460 FWD RT AILERON.May 18, 2000 · N17533 · Doug DC932SDR AALA2000819Stiffener · corrodedTUL - FOUND CORROSION ON VERTICAL STIFFENER AT GROUND WIRES JUST OUTBOARD OF NR 5 LEADING EDGE FLAP ACTUATOR. REMOVED AND REPLACED FRONT SPAR VERT STIFFENER SRM 51-30-2. (M)May 15, 2000 · N728AA · Boeing 727227SDR 20000601SH020Gusset · crackedRIGHT LOWER OUTBOARD WING HAD CRACK IN DOUBLER AT FORWARD ATTACH POINT AND GUSSET CRACKED AT APPROX BS 160.00 AND WS 110.11. TWO CRACKS IN WING SKIN RIGHT WING 4 INCHES BEHIND FORWARD SPAR JUST AFT OF FORWARD WING BOLT ON TOP SIDE OF WING. TWO CRACKS IN WINGMay 15, 2000 · N16 · Beech C90SDR DHL200070722CFairing · tornNR 7 FLAP JACKSCREW FAIRING TORN AT I/B EDGE, UPPER SURFACE. CUT OUT DAMAGED AREA AT NR 7 JACKSCREW FAIRING I/B EDGE PER SRM 51-40-2. MATRL LOSS .5 INCH. INSTALLED EXTERNAL DOUBLER PER SRM 51-4-02 FIG 1. ALODINED AND PRIMED AREA PER 51-10-2.May 13, 2000 · N707DH · Boeing 72722SDR RRXA002727Gusset · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LOWER RIB INTERCOSTAL GUSSET ON THE RT WING L/E MIDDLE SECTION AT STA XFS 350, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPMay 12, 2000 · N8084U · Doug DC871FSDR RRXA002712Stiffener · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING NR 4 STUB WING RT SIDE VERTICAL STIFFENER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-4 AND May 12, 2000 · N8084U · Doug DC871FSDR RRXA002709Baffle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LOWER SURFACE OF THE RT WING O/B LEADING EDGE DUCTED SKIN BAFFLE AT STA 678, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRMay 12, 2000 · N8084U · Doug DC871FSDR DL72S000946Attach Angle · crackedFOUND ON C1 LETTER CK, 1 INCH CRACK NR 11 SPOILER ACTUATOR I/B ATTACH ANGLE. REPAIRED PER MM 57-42-0.May 12, 2000 · N411DA · Boeing 727232SDR P2EA00166Angle · crackedSJO - DURING C-CHECK, FOUND LEFT WING EXTERNAL ANGLE AT WBL 70.85 STR 18A WITH CRACK. REPLACED LEFT WING EXTERNAL ANGLE AT WBL 70.85, STR 18A IAW BOEING SB 737-57-1087 REV 9 DATED JULY 6, 1987 FABRICATED ANGLE IAW BOEING DRAWING 65C16958 SHEETS 1 AND 2 AND BMay 11, 2000 · N912MP · Boeing 737247SDR COMA0010072Angle · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5320-244-02I, THE RT WING UPPER SKIN ATTACH ANGLE FOR FAIRING 194 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-13, REV IR, 2-May 11, 2000 · N258CA · Emb EMB120RTSDR COMA0010071Angle · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5320-243-02I, THE LT WING UPPER SKIN ATTACH ANGLE FOR FAIRING 193 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-13 REV IR, 2-7May 11, 2000 · N258CA · Emb EMB120RTSDR MWEA00417Angle · elongatedELONGATED HOLE ON AFT SPAR ATTACH ANGLE LEFT WING STATION XRS 161.7. FABRICATED AND INSTALLED REPAIR ANGLES. INSTALLED, FABRICATED REPAIR DOUBLER.May 9, 2000 · N900ME · Doug DC915SDR TWAA0007104Fitting · crackedDURING ROUTINE CHECK, FOUND RT WING SPAR TO TRAP FITTING WITH CRACK BETWEEN TRAP ATTACH BOLTS. REPLACED THE RT SPAR TO TRAP FITTING PER SRM 51-00, STANDARD PRACTICE AND EMLR 70740. CHECK-C 3-10-00 STL.May 7, 2000 · N926L · Doug DC932SDR CA000530008Attach Bolt · corroded(CAN) RT WING AFT UPPER ATTACH BOLY FOUND CORRODED, NEW BOLT INSTALLED.May 3, 2000 · Bag BAE146200ASDR MWEA00406Clip · damagedREMOVED ALL LOWER SHEAR TIES FROM STATION 23 TO STATION 11 AT RIGHT WING STATION XRS69. REMOVED TO FACILITATE OTHER MAINTENANCE AND FOUND THREE SHEAR TIE CLIPS OUT OF LIMITS. MAINTENANCE FABRICATED AND INSTALLED NEW SHEAR TIE CLIPS.May 3, 2000 · N900ME · Doug DC915SDR CA000511030Fitting · loose(CAN) DURING SCHEDULED INSPECTION, MOVEMENT WAS NOTICED AT THE AFT TIP TANK FITTING AS MAINTENANCE PERSONNEL APPLIED UP AND DOWN FORCES TO THE TIP TANK TRAILING EDGE. THE TWO MOST OUTBOARD RIVETS WHICH ATTACH THE FITTING TO THE OUTBOARD RIB (THROUGH THE REAR SMay 2, 2000 · Cessna 402BSDR MWEA00397Door · crackedRIGHT WING CENTER BUTE DOOR INBOARD AFT ATTACH HOLE CRACKED. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER.May 1, 2000 · N900ME · Doug DC915SDR UPS00832571Stiffener · crackedINSPECTION TYPE:C-2, LEFT WING NUMBER 2 STUB WING VERTICAL STIFFENER CRACKED APPROX STA XS256. REMOVED, FAB AND INSTALLED IAW DWG NR 9753294 AND SRM 51-1-8, 51-1-20D.Apr 25, 2000 · N700UP · Doug DC871FSDR UPS00832566Angle · crackedINSPECTION TYPE:C-2, RIGHT WING L/E STIFFENER ANGLE CRACKED STA XOLDI 6.225. STOP DRILLED CRACKED IAW SRM 57-2-0. FAB AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 & 51-1-20D.Apr 25, 2000 · N700UP · Doug DC871FSDR USAA000597Fitting · crackedCLT - FOUND FITTING CRACKED .5 INCH, RIGHT MIG BEAM OUTBOARD SUPPORT FITTING ABOVE BEAM CUTOUT. NDT PERFORMED BOLTS REINSTALLED PER TR 57-40-10. (M)Apr 24, 2000 · N279AU · Boeing 7372B7SDR CALA0000512Fitting · crackedLEFT WING MLG BEAM ATTACH BRACKET O/B OF GEAR TO REAR SPAR CRACKED AT EDGE (1) OF OPENING O/B UPPER EDGE. REMOVED AND REPLACED FITTING PER EC/RA 5740-01423.Apr 22, 2000 · N18350 · Boeing 7373T0SDR EIA2000160Pad · damagedHAECO-HKG - RIGHT MAIN JACK PAD ASSEMBLY FOUND DEFORMED AND DAMAGED. JACK PAD ASSEMBLY REPLACED PER HAECO RS R-57-11-34345. (M)Apr 21, 2000 · N482EV · Boeing 747212BSDR RRXA002199Plate · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED LWR FRONT SPAR CAP ON THE NR 4 STUB WING I/B MOUNT SHIM, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED EDGES SMOOTH AND RETURNED TO SERVICE IAW EO NR Apr 18, 2000 · N995CF · Doug DC862SDR AT0000240Cap · crackedFOUND RIGHT WING AT BS 58.5 HAS CORROSION AND CRACK ON T-CAP BETWEEN STRINGER 15 AND 16. REMOVED CORROSION, DRILLED, SEALED, AND INSTALLED 6 REPAIR CLIPS IAW RES 00-0442 AND REWORK DRAWING 5932267.Apr 17, 2000 · N825AT · Doug DC932SDR TWAA0006312Fitting · crackedDURING OP 16 MAINT CHECK ON RT WING FOUND CRACK IN FITTING 26 IN AFT OF FWD WALL OF WHEEL WELL, RBL 53 IN, APPROX 8 IN DOWN FROM UPPER SURFACE OF WHEEL WELL. REPLACED CASTING (P/N 9919618-2N). INSTALLED PER SB 53-131.Apr 17, 2000 · N984Z · Doug DC931SDR TWAA0006103Casting · crackedDURING OP 16 MAINT CHECK, ON RT WING A GAP BETWEEN CASTING BOLT HEAD AND WASHER. ALSO FOUND CRACK IN CASTING, STA 718. REPLACED CASTING, PN 9919618-2N. INSTALLED PER DOUGLAS SERVICE BULLETIN 53-131. ---CLOSED---Apr 17, 2000 · N984Z · Doug DC931SDR MWEA00344Fitting · crackedDURING UT TEST, CRACK INDICATION NOTED AT FORWARD SIDE OF THREE BOLT HOLES OF RT TRAPEZOIDAL PANEL LOWER SUPPORT FITTING. FABRICATED AND INSTALLED REPAIR ANGLES.Apr 14, 2000 · N900ME · Doug DC915SDR QXEA0001093Strap · chafedPDX - TWO CHAFED AREAS AT FORWARD END OF LT WING STRAP, LOCATED AT STATION 1700. REPAIRED IAW HORIZON AIR EA 4-57-400.Apr 11, 2000 · N494US · Fokker F28MK4000SDR 20000619SH003Fitting · crackedDURING C-CHECK, INSPECTION FOUND THE FOLLOWING: CRACKED FITTING ON RIGHT WING AT BS 983. (X)Apr 10, 2000 · N260FA · Lkheed 1011385114SDR RRXA002359Angle · crackedDURING A MAINTENANCE VISIT FOUND A 6 INCH CRACK TO THE LT WING I/B SLOT UPPER O/B CUTOUT ANGLE AT STA XFS 250.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED PART IAW DC-8 SRM 51-1-21.Apr 7, 2000 · N995CF · Doug DC862SDR RRXA001932Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AROUND THE SCREW HOLES AT THE LT WING I/B LEADING EDGE UPPER SURFACE SKIN AT STA XFS 113.750 TO XFS 10.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8Apr 5, 2000 · N961R · Doug DC873FSDR DHL200072628CAngle · crackedLOWER T/E PANEL WS 536 APPROX ANGLE SUPPORT CRACKED. REMOVED AND REPLACED LOWER OUTBOARD T/E ANGLE SUPPORT PER SRM 57-30-2. INSTALLED PHENOLIC BLOCK AT LOWER T/E PER SRM 51-30-2.Apr 5, 2000 · N726DH · Boeing 727228SDR UPS00832384Angle · crackedINSPECTION TYPE:C123 LEFT WING L/E UPPER ANGLE IS CRACKED AT XS195. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5769859 AND SRM 51-1-20D.Apr 4, 2000 · N709UP · Doug DC871FSDR CALA0000395Hinge · crackedINSPECTION FOUND A 0.2 INCH CRACK IN RT WING TRAILING EDGE HINGE AT STA XORS 714. THE HINGE WAS REPLACED IAW SRM 57-31-01.Apr 4, 2000 · N12061 · Doug DC1030
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