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 DL764020082Plate · damagedFOUND BY MTC, RT WING LOWER CLOSE OUT PANEL FOR T/E FLAP DAMAGED BETWEEN NR 7 AND 8 TRACK HOUSINGS. REPLACED 4 WIGGLER PLATES AND C-CHANNEL BETWEEN NR 7 AND NR 8 FLAP TRACK HOUSING AND INSTALLED CLOSURE PANEL.Jan 16, 2002 · N838MH · Boeing 767432ERSDR DL764020081Plate · damagedFOUND ON PDC CHECK, LT WING CLOSURE PANEL FWD OF T/E FLAP HAS DAMAGED ATTACH POINTS AND FITTINGS. REPLACED DAMAGE C-CHANNEL 1 EA TIED ROD AND 3 EA WIGGLE PLATES.Jan 16, 2002 · N833MH · Boeing 767432ERSDR QXEA0200105Support Bracket · crackedPDX - LT WING FORWARD SPAR UPPER LEADING EDGE SUPPORT BRACKET IS CRACKED AT STATION YW139.00. REPAIRED IAW DHC-8-200 SRM 51-40-00.Jan 16, 2002 · N356PH · Dhav DHC8202SDR QXEA0200104Bracket · crackedPDX - BRACKET CRACKED OUTBOARD TOP END OF INBOARD LEADING EDGE FLANGE AT STATION YW138.00. REPAIRED IAW DHC-8-200 SRM 51-40-00.Jan 16, 2002 · N356PH · Dhav DHC8202SDR UPS02237553Channel · crackedINSPECTION TYPE:C+SI CHANNEL ON LT WING REAR SPAR O/B OF NR 1 SPOILER CRACKED.Jan 15, 2002 · N940UP · Boeing 727185CSDR DL72L020032Stiffener · crackedL/E SPAR STIFFENER CRACKED AT NR 7 SLAT I/B TRACK I/B SIDE. REPLACED STIFFENER PER M/M.Jan 9, 2002 · N508DA · Boeing 727232SDR 0200149946Skin · corrodedDuring HCK in ATL, corrosion was found on the R/H wing upper skin doubler flange attachment holes for the fuel access door. Repaired per EA 99-185451.Jan 8, 2002 · N8926E · Doug DC931SDR QXEA0200015Bracket · crackedPDX - OUTBOARD BRACKET FOR LEADING EDGE 611AR AT NACELLE END, LOWER SIDE IS CRACKED. REPAIRED IAW DHC-8 SRM 51-40-00.Jan 3, 2002 · N355PH · Dhav DHC8202SDR UPS02237540Support Bracket · corrodedINSPECTION TYPE:C+SI SUPPORT BRACKET FOR LT FWD END OF NR 4 FLAP TRACK HAS PITTING CORROSION IN BORE OF HOLE.Jan 2, 2002 · N940UP · Boeing 727185CSDR UPS02237462Fitting · corrodedINSPECTION TYPE:C+SI RT WING NR 8 FLAP TRACK SUPPORT FITTING (WING FITTING) HAS PITTING CORROSION ON INBOARD FACE. CORROSION REMOVED BY MACHINING, NDT COMPLIED WITH AND NDF. FLAP PEENED AND CADPLATED IAW OHM.Jan 2, 2002 · N940UP · Boeing 727185CSDR UPS02237510Bushing · corrodedINSPECTION TYPE:C+SI, RT WING REAR TERMINAL FORGING FWD BUSHING IS CORRODED. RETAINER REPLACED IAW MM 57-41-11, BUSHING REPLACED IAW OHM20-50-03.Dec 19, 2001 · N940UP · Boeing 727185CSDR BTH2001F00002Fitting · frettedDISCOVERED DURING 100 HOUR INSPECTION NOTED MOVEMENT OF WING AT FORWARD WING ATTACH FITTING WHEN WING WAS PUSHED FROM BOTTOM OR TOP.Nov 29, 2001 · N75387 · Piper PA32R300SDR QXEA0102012Shim · damagedPDX - LT WING FUEL ACCESS APERTURE 71A, SHIM HAS BEEN BLENDED COMPLETELY THROUGH AT SEVERAL SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-568.Nov 27, 2001 · N482US · Fokker F28MK4000SDR CALA0101009Bracket · crackedINSPECTION FOUND A 1/4" CRACK IN R/H WING #6 FLAP TRACK FAIRING I/B SUPPORT BRACKET. A NEW BRACKET WAS INSTALLED IAW MM 51-10-02.Nov 23, 2001 · N17309 · Boeing 7373T0SDR SIMA200132406Bracket · crackedDURING INSPECTION, FOUND RIGHT WING TIP LOWER ATTACHMENT BRACKET CRACKED. REMOVED CRACK BY CUT OUT. FABRICATED A DOUBLER ANGLE AND A FILLER. REPAIR DONE IAW EMB GST 3691/01 AND STANDARD SRM PRACTICES. (M)Nov 20, 2001 · N602AE · Emb EMB145LRSDR QXEA0101924Support · chafedPDX - LT WING SKIN LOWER SURFACE SUPPORT STRUCTURE CHAFED. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 5 AND SRM 51-30-00, PAGE 701-706.Nov 13, 2001 · N482US · Fokker F28MK4000SDR C2XA01TY175Rod End · corrodedTYS DURING A SCHEDULED 1-C INSPECTION THE LEFT FUSELAGE TO SPAR 3 ROD END ASSEMBLY HAD CORRODED ON THE LOWER ROD END. MAINTENANCE REMOVED AND REPLACED THE LEFT ROD ASSEMBLY IAW GST-3655A-01 WHICH WAS ACCOMPLISHED. THE AIRCRAFT WILL BE RELEASED TO SERVICE UPONov 11, 2001 · N15509 · Emb EMB135ERSDR C2XA01TY174Rod End · corrodedTYS DURING A 1-C INSPECTION THE RIGHT FUSELAGE TO SPAR 3 ROD ASSEMBLY HAD CORROSION ON THE LOWER ROD ENDS. MAINTENANCE REMOVED AND REPLACED RIGHT ROD ASSEMBLIES IAW EMB GST-3655A/01 WHICH WAS ACCOMPLISHED. THE AIRCRAFT WILL BE RELEASED TO SERVICE UPON COMPLENov 11, 2001 · N15509 · Emb EMB135ERSDR QXEA0101794Bolt · strippedPDX - INSIDE FUEL PANEL 72A, 5TH VENT STRUT FROM FORWARD SPAR TOP AND BOTTOM OUTBOARD MOUNTING BOLTS WILL NOT TIGHTEN UP. REPAIRED IAW FOKKER SRM 51-31-01.Nov 7, 2001 · N482US · Fokker F28MK4000SDR AUS20011258Fitting · cracked(AUS) LANDING GEAR ACTUATOR SUPPORT FITTING CRACKED.Oct 30, 2001 · Beech 58SDR CA011108008Angle · cracked(CAN) WHILE CARRYING OUT INSP CALLED UP IN "B" CHECK TECHNICIAN NOTICED CRACK IN RADIUS OF RT FWD DRAG ANGLE P/N 215-30031-59. INSPECTION OF OTHER DRAG ANGLES ON SAME A/C REVEALED FWD LT DRAG ANGLE WAS CRACKED IN SAME AREA. CRACK LENGTH ON BOTH LT & RT DRAG ANOct 29, 2001 · Cndair CL2151A10SDR NXT2001F00000Bolt · wornINSPECTION FOUND THE STUB WING TO HAVE SLIGHT UP AND DOWN MOVEMENT. REMOVAL OF THE STAB WING FROM THE AIRFRAME REVEALED BOTH UPPER AND LOWER STUB WING ATTACHMENT BOLTS PN 222031830101(UPPER) & PN 222031831101(LOWER). TO HAVE THE LINING MATERIAL WORN OFF, ALMOOct 26, 2001 · N144CF · Bell 222USDR 01FDEA00957Bracket · crackedCRACK AT TOP OF CORNER ANGLE BRACKET. REMOVED AND REPLACED BRACKET PER EA 8-5710-56175 & S/B 57-88.Oct 24, 2001 · N377FE · Doug DC1010SDR HNAA0100070Angle · crackedCRACK IN CLOSING ANGLE BETWEEN OUTBOARD SIDE OF NR 1 NACELLE AND WING FRONT SPAR. REPAIRED IAW EO8-57-01-509.Oct 23, 2001 · N914HA · Dhav DHC8102SDR 0103989998Cap · crackedDuring H ck in Atl, The rear spar, lower cap aft flange at approx. at approximately sta xrs 80 was found to be corroded and cracked. The damage was blended out and protected against corrosion. Material 2024-t3511 EA 99-185232Oct 22, 2001 · N8934E · Doug DC931SDR 01FDEA00906Channel · crackedN 345 CHANNEL CRACKED ON LEFT WING BS 425, WL 357. R&R CHANNEL PER SRM 51-30-2Oct 21, 2001 · N282FE · Boeing 727233SDR QXEA0101723Support Bracket · crackedPDX - RIGHT WING UPPER AND LOWER LEADING EDGE FRONT SPAR SUPPORT BRACKETS ARE CRACKED AT STATION YW137.00. REPAIRED IAW DHC-8-200 MM 51-40-00, PAGE 1.Oct 17, 2001 · N354PH · Dhav DHC8202SDR QXEA0101722Support Bracket · crackedPDX - LEFT WING UPPER AND LOWER LEADING EDGE FRONT SPAR SUPPORT BRACKETS ARE CRACKED AT STATION YW137.00. REPAIRED IAW DHC-8-200 MM 51-40-00, PAGE 1.Oct 17, 2001 · N354PH · Dhav DHC8202SDR DL72S011722Slat · crackedMULTIPLE RIBS CRACKED,REPAIRED PER AMM 57-54-000-8 FIG 814Oct 16, 2001 · N543DA · Boeing 727232SDR QXEA0101673Angle · crackedPDX - RIGHT-HAND WING AT FORWARD SPAR A Z-ANGLE SUPPORT IS CRACKED AT TOP AND DOWN TWO RIVETS. REPLACED Z-ANGLE IAW SRM 51-40-11.Oct 11, 2001 · N353PH · Dhav DHC8202SDR UPS01837108Fitting · crackedINSPECTION TYPE:C23 RIGHT WING STRINGER 64 SPLICE FITTING IS CRACKED AT APPROX XRS 510. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3644046 AND SRM 51-1-20D.Oct 10, 2001 · N836UP · Doug DC873FSDR UPS01837140Angle · crackedINSPECTION TYPE:C23 LEFT WING L/E UPPER RIB ANGLE IS CRACKED AT XS 472.099. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 5770170, AND SRM 51-1-20D, 51-1-21.Oct 4, 2001 · N836UP · Doug DC873FSDR UPS01837119Clip · crackedINSPECTION TYPE:C23 RIGHT WING L/E INTERCOSTAL ATTACH CLIP IS CRACKED AT XOLDI 6.225. REMOVED, FABRICATED, AND REPLACED CLIP IAW DWG 5769589, AND SRM 51-1-21.Oct 4, 2001 · N836UP · Doug DC873FSDR UPS01837111Rib · crackedINSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 834. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Oct 4, 2001 · N836UP · Doug DC873FSDR UPS01837026Angle · crackedINSPECTION TYPE:C23 NR 2 STUB WING VERTICAL ATTACH ANGLE IS CRACKED AT XS 250. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 9753293, AND SRM 51-1-20D, 51-3-0.Oct 4, 2001 · N836UP · Doug DC873FSDR UPS01837013Clip · crackedINSPECTION TYPE: C23, LEFT WING L/E. INTERCOSTAL ATTACH CLIP IS CRACKED AT XOLDI 6.225. REMOVED,FABRICATED,AND REPLACED CLIP I.A.W.DWG. 5769589,AND SRM. 51- 1-20DOct 4, 2001 · N836UP · Doug DC873FSDR DHL2001742504Angle · crackedAT C-CHECK, RT WING L/E INTERIOR AT WS 130, FOUND CRACK DAMAGE TO UPPER ANGLE BETWEEN UPPER SKIN AND STA 130 RIB. REMOVED UPPER ANGLE AT RT WING L/E INTERIOR AT WS 130 BETWEEN UPPER SKIN AND STA 130 RIB IAW B727 SRM 51-30-2. INSTALLED UPPER ANGLE AT RT WING Oct 3, 2001 · N742DH · Boeing 727225SDR DHL2001742503Channel · crackedAT C-CHECK, LEFT WING T/E AREA, UPPER FIXED PANEL TOP OF I/B FLAP O/B JACKSREW HAS SUPPORT ANGLE CRACKED ALONG RIVET. REMOVED AND REPLACED U-CHANEL SUPPORT ON LEFT WING T/E FIXED PANEL TOP OF I/B FLAP O/B JACKSCREW, IAW B727-SRM 51-10-1.Oct 3, 2001 · N742DH · Boeing 727225SDR QXEA0101638Bracket · crackedPDX - BRACKET CRACKED, FRONT SPAR, LEFT WING UPPER SPAR CAP AT STATION YW138. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 1 (2) AND PAGE 2.Oct 3, 2001 · N353PH · Dhav DHC8202SDR QXEA0101637Bracket · crackedPDX - BRACKET CRACKED, FRONT SPAR LEFT WING LOWER SPAR CAP AT YW138. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 1 (2) AND PAGE 2.Oct 3, 2001 · N353PH · Dhav DHC8202SDR QXEA0101636Bracket · crackedPDX - BRACKET CRACKED, FRONT SPAR, RIGHT WING LOWER SPAR CAP AT YW138. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 1 (2) AND PAGE 2.Oct 3, 2001 · N353PH · Dhav DHC8202SDR QXEA0101635Bracket · crackedPDX - BRACKET CRACKED, FRONT WING SPAR UPPER SPAR CAP AT YW138. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 1 (2) AND PAGE 2.Oct 3, 2001 · N353PH · Dhav DHC8202SDR DHL2001742541Angle · crackedAT C-CHECK, LEFT WING HAS A CRACK AT LEFT EDGE FRONT SPAR VERTICAL ANGLE LOWER END AT WBL 92.8 MARKED. CUT OFF LOWER SECTION OF ANGLE AT WBL 92.8 LEFT WING L/E AS PER B-727 SRM 51-40-4 FIGURE 2. FABRICATE NEW ANGLE AS PER B-727 SRM 51-40-4. ALODINED AND PRIOct 1, 2001 · N742DH · Boeing 727225SDR DHL2001742544Angle · crackedAT C-CHECK, LT WING HAS A CRACK AT LEADING EDGE FRONT VERTICAL ANGLE LOWER END AT WBL 92.8.Oct 1, 2001 · N742DH · Boeing 727225SDR CALA0100914Stiffener · crackedINSPECTION FOUND AN 8" CRACK IN STIFFENER LOCATED JUST FORWARD OF HORSE COLLAR IN #6 FLAP TRACK FAIRING. THE STIFFENER WAS REPLACED IAW SRM 51-10-02.Oct 1, 2001 · N14335 · Boeing 7373T0SDR CALA0100912Stiffener · crackedINSPECTION FOUND A 5" CRACK IN ANGLE STIFFENER INSIDE #3 FLAP TRACK FAIRING. THE ANGLE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-10-2.Oct 1, 2001 · N14335 · Boeing 7373T0SDR CALA0100911Splice · crackedINSPECTION FOUND A 5" CRACK IN #3 FLAP TRACK FAIRING SPLICE. THE #3 FAIRING SPLICE WAS REMOVED AND REPLACED IAW SRM 51-10-02.Oct 1, 2001 · N14335 · Boeing 7373T0SDR COMA0160761Skin · corrodedR/H LOWER WING FUEL TANK ACCESS HOLE (640DB) HAS CORROSION ON FORWARD AND AFT CUT-OUT AREAS.REPAIRED R/H LOWER WING FUEL TANK ACCESS HOLE (640DB) I/A/W CANADAIR R.E.O. 601R-57-21-148 AND 601R-57-21-030 REV A.Oct 1, 2001 · N979CA · Cndair CL6002B19SDR DHL2001801524Channel · crackedNR 1 MAIN TANK-CHANNEL ASSY CRACKED (REF ACCESS DOOR NR 505 C). REMOVED AND REPLACED CHANNEL ASSY PER S/B57-65 PG 1-5, LEAK CHECKED.Sep 30, 2001 · N801DH · Doug DC873FSDR DHL2001801523Channel · crackedNR 4 MAIN TANK-CHANNEL ASSY CRACKED (REF ACCESS DOOR 505C). REMOVED AND REPLACED CHANNEL ASSY PER S/B 57-65 PG 1-5. LEAK CHECK ACCOMPLISHED.Sep 29, 2001 · N801DH · Doug DC873F
Back to JASC 5720