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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DHL9980174CStrip · crackedAT C-CHECK, RIGHT WING LEADING EDGE I/B EXT LOWER AREA AT STA 69 METAL RUB STRIP CRACKED. REMOVED DAMAGED STRIP, FABRICATED NEW STRIP AND INSTALLED PER SRM 51-1-1.SDR CALA9801976Angle · crackedINSPECTION FOUND A .625 INCH CRACK IN LT WING AFT FALSE SPAR LOWER CHORD ANGLE AT BOLT HOLE (FWD OF NR 7 SPOILER ACTUATOR CASTING, WBL 135). THE ANGLE WAS CUT OUT AND A NEW ANGLE, SPLICE AND STRAPS WERE INSTALLED IAW SRM 51-30-2.SDR DHL9980153CBracket · crackedAT C-CHECK, RT WING O/B LEADING EDGE INTERIOR AT STA 603 FOUND PNEUMATIC SUPPORT CRACKED. FABRICATED REPAIR DOUBLER PER SRM 51-1-21, 2 X 6.SDR DHL99801107Angle · crackedAT C-CHECK, RIGHT WING T/E INBOARD LOWER STA 5.00 AT I/B FLAP I/B HINGE SUPPORT FWD AREA FOUND CRACK ON ANGLE REINFORCEMENT. REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE 12 X 2.5 PER SRM 51-1-21.SDR DHL99801106Angle · crackedAT C-CHECK, RT WING T/E AREA AT STA XW 5 CRACKED ON ANGLE NEXT TO WEB PANEL. STOP DRILLED, FABRICATED ANGLE REPAIR PER DC-8 SRM 51-1-4, 6 X 2.SDR UPS98828056Tripler · crackedINSPECTION TYPE-C, 3 RT WING L/E INTERNAL TRIPLER ABOVE THE NR 3 PYLON AT THE L/E OF THE PYLON CUT OUT IS CRACKED. REPAIRED L/E SKIN IAW EO DC8-5720-4087.SDR UPS98827991Chord · corrodedINSPECTION TYPE-D, RT WING I/B LEADING EDGE UPPER CHORD XFS 10.0 TO 26.25 HAS HEAVY EXFOLIATION CORROSION. REPAIRED IAW SRM 57-2-1.SDR UPS98828027Doubler · crackedINSPECTION TYPE-C, LT WING L/E INNER DOUBLER AROUND SMALL LWR SWING DOWN PANEL UNDER I/B FIRE BOTTLE CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21 AND DWG 5641252.SDR CALA9801952Fitting · wornRIGHT WING FORWARD SIDE OF MLG BEAM WING T/E PANEL TO BEAM ATTACH LINK FITTING HAS ELONGATED BOLT HOLES. REMOVED AND REPLACED FITTING PER SRM 51-30-1.SDR UPS98827966Angle · crackedINSPECTION TYPE-C, LT WING L/E VERTICAL FWD ANGLE CRACKED AT O/B END OF THE I/B SLOT. REMOVED, FABRICATED AND REPLACED VERTICAL ANGLE IAW DWG 9753293 AND SRM 51-1-20D AND 51-3-0.SDR DHL9871523CBracket · crackedAT C-CHECK, RIGHT WING TIP FWD NAV LIGHT BRACKET CRACKED AT I/B UPPER CORNER. REMOVED AND REPLACED BRACKET PER SRM 57-20-1, 8 X 3.1. N/R 2123SDR ABXA9801071Doubler · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND RIGHT WING REAR SPAR DOUBLER CRACKED OUTBOARD OF TRAPEZOIDAL PANEL. REPAIRED IAW ABX REA D957-25132MR.SDR UPS98828051Fitting · crackedINSPECTION TYPE-C, THE RT LWR AUX SPAR TO REAR SPAR STA 98 TIE FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DHC SK- 729-846 AND SRM 51-3-0.SDR UPS98827962Angle · crackedINSPECTION TYPE-C, RT WING L/E VERTICAL ANGE JUST I/B OF XS 250.089 AND AFT OF THE SLOT IS CRACKED AT THE LWR END. REMOVED, FABRICATED AND REPLACED VERTICAL ANGLE IAW DWG 9753293 AND SRM 51-1-20D AND 51-3-0.SDR UPS98227987Fitting · corrodedINSPECTION TYPE-C, CORROSION FOUND ON RT LANDING GEAR SUPPPORT FITTING ON WING REAR SPAR STA 224.5. FITTING REPLACED IAW DRAWING 65-84405.SDR DL72L982107Stiffener · crackedSPAR STIFFENER CRACKED NR 3 SLAT IB TRACK. REPAIRED PER MM 57-20-21.SDR AALA981896Angle · crackedTUL - FOUND LEFT WING ROOT ANGLE CRACKED. REPLACED LEFT PICK UP ANGLE PER ESO 3095, DATED 10-7-98. (M)SDR CALA9801905Beam · crackedINSPECTION FOUND A .375 INCH CRACK IN LT WING J-BEAM ABOVE NR 7 SPOILER ACTUATOR. A REPAIR WAS INSTALLED IAW ECRA 5750-02914.SDR AALA981905Slat Track · gougedTUL - NR 4 SLAT TRACK CAN GOUGED FROM SLAT TRACK ON OUTBOARD SIDE. REPAIRED IAW AARD 57-20-00-6. (M)SDR P2EA98216Beam · wornSJO - RIGHT WING TRUNNION SUPPORT BEAM WORN AT RSS 222. REPAIRED RIGHT WING MAIN LANDING GEAR BEAM UPPER FORWARD FLANGE SECTION PER BOEING FAX COO-SJO-98-0761RR DATED OCT 12, 1998. DOCUMENTED ON FAA FORM 8110-3. (M)SDR P2EA98211Stiffener · wornSJO - RIGHT WING REAR STIFFENER WORN AT RSS 155. REPLACED RIGHT WING REAR SPAR STIFFENER AT RSS 155 PER SRM 51-10-1 PAGE 5, AND SRM 51-30-2. (M)SDR DHL9871512CSupport · crackedAT C-CHECK, RT WING FIXED INTERIOR VERTICAL SUPPORT WEB AT WBL 92.8 IS CRACKED AT THE 11TH BOLT FROM THE BOTOM JUST FWD OF FRONT SPAR. HFEC, INSTALLED DOUBLER REPAIR PER SRM. N/R 2036SDR AALA981840Stiffener · corrodedTUL - FOUND CORROSION ON TOP OF VERTICAL STIFFENER ON FORWARD SPAR AT APPROX WS 248. INSTALLED NEW VERTICAL STIFFENER ON FORWARD SPAR AT APPROX WS 248. (M)SDR DHL9871511CStrip · crackedAT C-CHECK, RT WING O/B SUPPORT ANGLE FOR RT WING LOWER SURFACE PANEL 8506 IS LOOSE AND CORROGATED STRIP IS CRACKED AT FWD END OF SUPPORT. REMOVED AND REPLACED CORROGATED STRIP PER SRM 51-30-2. N/R 2014SDR DHL9871509CAngle · crackedAT C-CHECK, LT WING I/B AND O/B ANGLE CRACKED BELOW NR 7 SPOILER ACTUATOR. REPLACED ANGLES PER SRM 51-30-2. N/R 1043SDR DL72S982015Angle · crackedREF TPA LETTER CHECK D-1, SUPPORT ANGLE CRACKED AT LWR FWD SIDE OF NR 8 SPOILER ACTUATOR SUPPORT FITTING. INSTALLED DOUBLER PER M/M 57-20-22.SDR AU981234Web · cracked(AUS) WING CENTER SPAR WEB CRACKED. PART TC: 26,549.SDR ABXA9800848Trap Panel · crackedDURING C-CHECK, FOUND LEFT FORWARD UPPER HORIZONTAL TRAPEZOIDAL PANEL CRACKED PAST 4TH HOLE. REPAIRED HORIZONTAL TRAPEZOIDAL PANEL IAW DC9 SRM 57-09.SDR AALA981800Casting · corrodedTUL - NR 5 L/E FLAP CENTER HINGE CASTING CORRODED, RT WING. REPLACED NR 5 L/E FLAP CENTER HINGE CASTING. (M)SDR AALA981798Casting · corrodedTUL - NR 4 L/E FLAP CENTER HINGE CASTING CORRODED INBOARD AND OUTBOARD SIDES AND UPPER OUTBOARD END. REMOVED AND REPLACED NR 4 L/E FLAP CENTER HINGE CASTING WITH NEW CASTING, P/N 65-18531-8. (M)SDR ABXA9801025Angle · crackedLEFT WING AT STATION XW 3.00, THE DRIVE LINK STIFFENER ANGLE IS CRACKED. REPAIRED IAW DC8 SRM.SDR ABXA9801019Angle · crackedLEFT WING TRAILING EDGE CAVITY AT STATION XW 3.00, THE DRIVE LINK FITTING STIFFENER ANGLE IS CRACKED. REPAIRED IAW DC8 SRM 51-1-20D.SDR C2XA98IA376Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT NACELLE FLAP CENTER SKIN SUPPORT CRACKED ON UPPER SIDE. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA375Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER SKIN SUPPORT FORWARD OF ACCESS 522EB CUTOUT ON RIB 8 CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA374Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING RIB 8 TO STRINGER 11 SUPPORT ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ANGLE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA98IA373Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING UPPER SKIN SUPPORT AT RIB 8, SECOND FROM FORWARD, CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR UPS98827863Angle · crackedINSPECTION TYPE-C, LT WING L/E VERTICAL ANGLE CRACKED AT LWR END AT STA XS 250.089. REMOVED, FABRICATED AND INSTALLED ANGLE IAW DWG 9753293 AND SRM 51-3-0, 51-1-20D.SDR UPS98827860Doubler · crackedINSPECTION TYPE-C, LT WING L/E LWR ACCESS PANEL DOUBLER CRACKED BETWEEN STA'S XFS 303 AND XFS 310.25. REMOVED, FABRICATED AND INSTALLED DOUBLER IAW DWG 5641252 AND SRM 51-1-20D AND 51-1-21.SDR DL72S981967Angle · crackedNR 6 L/E FLAP ACT ATTACH ANGLE CRACKED O/B LOWER RADIUS. REPAIRED PER MM 57-20-21 PG 811.SDR ABXA9800976Stiffener · crackedRIGHT WING TRAILING EDGE AT STATION XW98, VERTICAL STIFFENER IS CRACKED AT THE BOTTOM. REPAIRED IAW DC8 SRM 51-1-20D AND 51-3-0.SDR CALA9801815Chord · crackedINSPECTION FOUND A .5 INCH CRACK IN LT WING LOWER CHORD AT NR 7 SPOILER ACTUATOR. THE CRACKED AREA WAS CUT OUT, STRAPS AND CHORD ANGLE WERE INSTALLED IAW ECRA 5720-01680 AND SRM 51-10-2.SDR CALA9801814Stiffener · corrodedINSPECTION FOUND LT WING FRONT SPAR STIFFENER CORRODED ON INBOARD SIDE CENTER AT STA 224. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-2 AND 51-20-4.SDR CALA9801804Angle · crackedINSPECTION FOUND A 1.6 INCH CRACK ON RT AND LT WING INBOARD ISLAND LOWER AFT INBOARD SPLICE ANGLE OF RIB. THE SPLICE ANGLE WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 57-22-01, FIGURE 2, 51-21-01, AND 51-33-01.SDR DL72S981942Stiffener · damagedWING UPPER SURFACE J STIFFENER REPAIR (STR 17 RT AT WS 300). REPAIR PER ER/A 332215-14 REV A.SDR CALA9801798Angle · corrodedINSPECTION FOUND LT WING NR 3 SPOILER L-ANGLE CORRODED AT INBOARD SIDE OF TRANSMISSION, WS 491. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-2 AND 51-10-3.SDR CALA9801787Beam · crackedINSPECTION FOUND A .375 INCH CRACK IN LT WING TRAILING EDGE J-BEAM ABOVE NR 7 SPOILER ACTUATOR. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW ECRA 5750-02914 AND SRM 51-10-6.SDR CALA9801783Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN OUTBOARD ANGLE BRACKET UNDER J-BEAM AT RT WING NR 8 SPOILER. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2.SDR UPS98227681Doubler · crackedINSPECTION TYPE-N/A, RIGHT WING AFT SPAR LOWER EDGE CORRIGATED DOUBLER CRACKED APROX 2 INCHES AT APROX WS 340 WBL 220. STOP DRILLED CRACK PER SRM 51-10-1 PG 6B.SDR 98ZZZX4260Strut Fitting · crackedDURING ANNUAL INSPECTION, FOUND THE AFT LEFT UPPER DIAGONAL STRUT FITTING CRACKED IN FIVE SEPARATE AREAS ON BOTH THE UPPER AND LOWER SURFACES ALONG THE LONGITUDINAL GRAIN. IT WAS ALSO NOTED THAT TWO CRACKS WERE LOCATED ALONG AN ORIGINAL MACHINING MARK. THE MSDR 98ZZZX4580Strut Fitting · corrodedDURING THE RECEIVING INSPECTION OF A WIPLINE 3730 FRONT STRUT JOINING FITTING, PITTING CORROSION WAS FOUND ON THE FRONT FACE SURFACE. THE PART WAS RED TAGGED AND RETURNED TO WIPAIRE, INC.
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