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 96FDEA01490Tension Strap · crackedSMRM NR 00506, RT WING, O/B FLAP I/B HINGE O/B SIDE TENSION STRAP IS CRACKED AT THE LOWER BOLT HOLE LOWER FLANGE. *S/D* REMOVED AND REPLACED TENSION STRAP BRACKET AS PER SRM 51-00-01 VOL NR I.Sep 14, 1996 · N322FE · Doug DC1030FSDR UPS96821309Fitting · crackedINSPECTION TYPE: CS2. FLAP ACTUATOR ATTACH FITTING CRACKED AND CORRODED ON RT WING REAR SPAR STA 98. REPLACED FITTING PER MM 20-16-00.Sep 13, 1996 · N813UP · Doug DC873FSDR UPS96821308Fitting · crackedINSPECTION TYPE: CS2. FLAP SUPPORT FITTING CRACKED AND CORRODED ON RT WING REAR SPAR STA 97. REPAIRED PER UPS EO DC8-57-0720.Sep 13, 1996 · N813UP · Doug DC873FSDR MWEA96504Access Panel · corrodedDURING INSP, RT WING LARGE LEADING EDGE LOWER ACCESS PANEL WAS FOUND TO HAVE CORROSION AT STA XRS 140. FABRICATED A REPAIR AND INSTALLED IAW SRM 57-01.Sep 12, 1996 · N209ME · Doug DC932SDR UPS96821306Doubler · crackedINSPECTION TYPE: CS2. LT WING LEADING EDGE SKIN DOUBLER CRACKED AT DRAIN HOLE STA XFS597 **(MRR FILED OPEN)** REPAIRED PER UPS EO.Sep 11, 1996 · N813UP · Doug DC873FSDR UPS96221094Stiffener · corrodedINSPECTION TYPE: C. CORROSION, RIGHT WING STATION 257.85. FRONT SPAR STIFFENER IS CORRODED ON I/B UPPER END. REMOVED CORRODED STIFFENER AND INSTALLED NEW STIFFENER. ALL WORK DONE IAW SRM 51-30-2, SRM 57-10-1, AND MM 28-11-00.Sep 9, 1996 · N214UP · Boeing 7272A1SDR UPS96221084Stiffener · corrodedINSPECTION TYPE: C. CORROSION ON RIGHT WING STATION 257.85. FRONT SPAR STIFFENER IS CORRODED ON I/B UPPER END. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 57-10-1, REMOVED STIFFENER AND INSTALLED NEW STIFFENER PER SRM 51-30-2.Sep 9, 1996 · N214UP · Boeing 7272A1SDR HAL960059Angle · crackedFOUND CORROSION AND METAL SPLIT AT TOP OF VERTICAL SUPPORT ON FALSE REAR SPAR 3 FEET FROM WHEEL WELL ON THE RIGHT TRAILING EDGE. REMOVED CORROSION AND INSTALLED REPAIR ANGLE PER ESO 7349 DATED 9-4-96. (M)Sep 9, 1996 · N153AA · Doug DC1010SDR CALA9601434Angle · crackedINSPECTION FOUND A .50 INCH CRACK BETWEEN BOLTS OF UPPER RIB CAP ANGLE AT RT WING LEADING EDGE, STA 332. A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM'S 51-40-3, 51-8-0, AND 51-30-2.Sep 9, 1996 · N69736 · Boeing 727224SDR CALA9601419Web · crackedINSPECTION FOUND LATERAL WEB CRACKED AT UPPER AND LOWER RADIUS INSIDE LEFT WING TIP, FORWARD OF FLUX VALVE COMPARTMENT. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-40-5.Sep 9, 1996 · N69736 · Boeing 727224SDR ABXA9700475Vortilon · dentedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LEFT WING VORTILON LEADING EDGE WITH PIN HOLES AND DENTS. REPAIRED IAW ABX REA 953-16330.Sep 9, 1996 · N902AX · Doug DC932SDR UPS96221156Stiffener · crackedINSPECTION TYPE-C, RT WING NR 5 SLAT AT ACTUATOR ROD MOUNT STIFFENER IS CRACKED IN RADIUS. REPAIRED IAW SRM 51-40-03 AND SRM 51-30-02.Sep 8, 1996 · N925UP · Boeing 72731CSDR UPS96221153Vert Stiffener · crackedINSPECTION TYPE-C, LT WING L/E, NR 3 SLAT I/B TRACK, O/B MOUNT VERTICAL STIFFENER ANGLE IS CRACKED AT BOTTOM. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW 65-16200 AND SRM 51-30-02.Sep 7, 1996 · N925UP · Boeing 72731CSDR UPS96221152Vert Stiffener · crackedINSPECTION TYPE-C, LT WING NR 3 SLAT O/B TRACK, O/B MOUNT VERTICAL STIFFENER ANGLE IS CRACKED AT BOTTOM. REMOVED DAMAGED STIFFENER, FAB AND INSTALLED REPLACEMENT STIFFENER SEALED DOME FASTENERS.Sep 7, 1996 · N925UP · Boeing 72731CSDR UPS96221151Vert Stiffener · crackedINSPECTION TYPE-C, LT WINGS L/E NR 2 SLAT I/B TRACK O/B MOUNT VERTICAL STIFFENER ANGLE IS CRACKED AT THE BOTTOM. REMOVED, FABRICATED AND INSTALLED STIFFENER ANGLE PER DWG 65-16200 SHT 1 AND 8 AND SRM 51-30-2.Sep 7, 1996 · N925UP · Boeing 72731CSDR CALA9601418Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK IN UPPER ANGLE JUST FORWARD OF FRONT SPAR AT LT WING LEADING EDGE RIB, STA 338. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.Sep 7, 1996 · N69736 · Boeing 727224SDR HALA960053Web · crackedDURING CHECK, FOUND CRACK ON WEB 46 RIGHT INBOARD OF ACCESS DOOR 142AZ ON THE INBOARD SIDE OF WEB APPROX 18 INCHES AFT THE FORWARD BULKHEAD. INSTALLED DOUBLER PER SRM 51-00-01. (M)Sep 3, 1996 · N153AA · Doug DC1010SDR HAL960051Doubler · corrodedDURING CHECK, FOUND THE LOWER LEFT LEADING EDGE SACRIFICIAL DOUBLER CORRODED WHERE THE INBOARD LATCH FOR ACCESS PANEL 517AB CONTACTS IT. INSTALLED DOUBLER AFTER CORROSION REMOVAL PER SRM 57-10-00, FIGURE 19. (M)Sep 3, 1996 · N153AA · Doug DC1010SDR MALA965114Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT INBOARD LOWER WING TO NACELLE ATTACH ANGLE CRACKED. COMPLETED REPAIR TO ATTACH ANGLE BY FABRICATING AND INSTALLING REPAIR ANGLE IAW FAIRCHILD ARP 54-20-9101 REV B. (M)Aug 31, 1996 · N421MA · Swrngn SA227ACSDR MALA965111Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT OUTBOARD UPPER WING TO NACELLE ATTACH ANGLE CRACKED IN TWO LOCATIONS. FABRICATED NEW ANGLE USING LIKE MATERIAL AND THICKNESS. INSTALLED ANGLE IAW FAIRCHILD SRM 51-00-00 PAGE 4 'PART FOR PART RAug 31, 1996 · N421MA · Swrngn SA227ACSDR ABXA9600644Fitting · crackedDURING 'C' CHECK, FOUND RIGHT WING SUPPORT FITTING CRACKED AT XW 340. REPAIRED RIGHT WING SUPPORT FITTING IAW REA NR D827-16054.Aug 26, 1996 · N805AX · Doug DC862SDR 9619069756Doubler · corrodedDURING H-CHECK, FOUND CORROSION ON THE RIGHT MAIN LANDING GEAR SUPPORT UPPER DIAMOND DOUBLER. REPLACED DOUBLER (P/N 5912438-2) PER DWG 9910010, 5910464.Aug 26, 1996 · N756NW · Doug DC941SDR UPS96821001Fitting · crackedRIGHT WING STA ZERO FLAP COVE FWD OF NR 1 FLAP DRIVE FWD PIVOT FITTING CRACKED ABOVE 90 DEGREE SPOILER CABLE BEND PULLEYS. REPLACED FITTING PER SRM 51-1-20D AND EO DC8-5310-8226D.Aug 24, 1996 · N812UP · Doug DC873FSDR ARWA9608005Fillet · crackedA 2 INCH CRACK IN RIGHT HAND WING INBOARD FLAP WELL LOWER EDGE FILLET XRS 217. REMOVED LOWER FILLET, FORMED FILLET PER DC-8 SRM 51-1-7, 57-2-0. INSTALLED PER DC-8 SRM 51-1-21.Aug 21, 1996 · N345JW · Doug DC863SDR ABXA9700113Splice · drilledDURING C-CHECK, FOUND 2 HOLES DRILLED IN RADIUS OF SPLICE ANGLES ON STRINGER NR 17. REPAIRED IAW ABX REA D957-15944-MR.Aug 21, 1996 · N923AX · Doug DC931SDR 96ZZZX6115Stiffener · crackedINSP FOUND STIFFENERS LOCATED ON REAR FALSE SPAR CRACKED. REFERENCE CASA COM LETTER 212-224.Aug 19, 1996 · N349TA · Casa C212CCSDR 96ZZZX6114Stiffener · crackedINSP FOUND STIFFENERS LOCATED ON REAR FALSE SPAR CRACKED. REFERENCE CASA COM LETTER 212-224.Aug 19, 1996 · N349TA · Casa C212CCSDR 96ZZZX6113Stiffener · crackedINSP FOUND STIFFENERS LOCATED ON REAR FALSE SPAR CRACKED. REFERENCE CASA COM LETTER 212-224.Aug 19, 1996 · N349TA · Casa C212CCSDR 96ZZZX6112Stiffener · crackedINSP FOUND STIFFENERS LOCATED ON REAR FALSE SPAR CRACKED. REFERENCE CASA COM LETTER 212-224.Aug 19, 1996 · N349TA · Casa C212CCSDR 96ZZZX6111Stiffener · crackedINSP FOUND STIFFENERS LOCATED ON REAR FALSE SPAR CRACKED. REFERENCE CASA COM LETTER 212-224.Aug 19, 1996 · N349TA · Casa C212CCSDR 96ZZZX6110Stiffener · crackedINSP FOUND STIFFENERS LOCATED ON REAR FALSE SPAR CRACKED. REFERENCE CASA COM LETTER 212-224.Aug 19, 1996 · N349TA · Casa C212CCSDR ARWA9608014Fitting · crackedRIGHT WING NR 4 ALT BOOSTER PUMP FITTING IS CRACKED (BOTH SIDES). REMOVED AND REPLACED FITTINGS PER DC-8 SRM 51-1-20D. DAC AUTHORIZATION.Aug 17, 1996 · N345JW · Doug DC863SDR ARWA9608013Fitting · crackedLT WING NR 1 ALT TANK 9 INCH CRACK SPLICE FITTING XRS 554 AND XRS 589, NR 5 STRINGER ACCESS DOOR 514H. REMOVED CRACKED SPLICE FITTING AND REPLACED PER DC-8 SRM 51-1-20D. MANUFACTURED FITTING PER DC-8 SRM'S 51-2-0, 57-403 AND DACO AUTHORIZATION.Aug 17, 1996 · N345JW · Doug DC863SDR ARWA9608009Angle · crackedONE INCH CRACK RT WING EXHAUST GATE INBOARD LOWER ANGLE XRS 255. REPAIRED EXHAUST GATE PER DC-8 SRM 57-2-1. FORMED DOUBLER AND INSTALLED PER DC-8 SRM'S 57-7-1, 51-1-4, 51-1-8 AND 51-1-21.Aug 17, 1996 · N345JW · Doug DC863SDR UPS96820926Doubler · crackedINSPECTION TYPE-SPEC, LT WING UPPER ACCESS PANEL DOUBLER HAS A 1.5 INCH LONG CRACK WS XRS 22.750 STRINGER NR 6. REPAIRED PER UPS EO.Aug 16, 1996 · N812UP · Doug DC873FSDR 96FDEA01358Casting · crackedNR 5002, LT WING O/B FLAP I/B HINGE TENSION TIE SUPPORT STRAP CRACKED AT LOWER ATTACH BOLT HOLE AS SEEN FROM LWR EXTERNAL SURFACE STA XORS562, VERIFIED BY HFEC.Aug 13, 1996 · N608FE · Doug MD11FSDR P5CA9601238Rivets · failedSHEAR RIVETS ON UPPER WING SKIN RT AT STA 380 FRONT SPAR AREA. INSTALLED NEW RIVETS PER SRM 51-30-02.Aug 12, 1996 · N832FT · Boeing 747121SDR P5CA9601178Bracket · brokenBROKEN SUPPORT BRACKET OF ENG NR 2 FAIRING NEAR FRONT SPAR LEADING EDGE AT STA 669.50 AREA. FAB NEW SUPPORT BRACKET PER OLD BRACKET, RIVETED PER SRM 51-30-02.Aug 12, 1996 · N832FT · Boeing 747121SDR P5CA9601177Fitting · crackingRT WING CRACKED UNDERWING FITTING OF FWD SKIRT ROD ATT, AFT OF DUAL SIDE STRUT FITTING OF NR 3 PYLON. MUST BE REPAIRED BEFORE INST NEW FITTING (P/N 69B12302-6) AND RIVETED PER SRM 51-30-02.Aug 12, 1996 · N832FT · Boeing 747121SDR P5CA9601036Rivets · shearedSHEARED RIVETS ON UPPER WING SKIN RT AT STA WS 990 IN FRONT SPAR AREA. INSTALLED NEW RIVET .1875 PER SRM 51-30-02.Aug 12, 1996 · N832FT · Boeing 747121SDR P5CA9601035Rivets · shearedSHEARED RIVETS ON UPPER WING SKIN RT AT STA 600 IN FRONT SPAR AREA. INSTALLED NEW RIVETS OBTAINED FROM STA STOCK BN 91662-25.Aug 12, 1996 · N832FT · Boeing 747121SDR P5CA9601034Rivets · shearedSHEARED RIVETS ON UPPER WING SKIN RT AT STA 565 FRONT SPAR. NEW RIVETS PER SRM 51-30-02.Aug 12, 1996 · N832FT · Boeing 747121SDR P5CA9601033Rivets · shearedSHEARED RIVETS ON UPPER WING SKIN RT AT STA 480 IN FRONT SPAR AREA. INSTALLED NEW RIVETS .1875 PER SRM 51-30-02.Aug 12, 1996 · N832FT · Boeing 747121SDR CALA9601247Tip · crackedINSPECTION FOUND A .25 INCH CRACK IN RT WING TIP UPPER SURFACE, JUST FORWARD OF PANEL 6641. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.Aug 7, 1996 · N14788 · Boeing 727232SDR CALA9601244Tip · crackedINSPECTION FOUND A .50 INCH CRACK IN LOWER OUTBOARD EDGE OF LT WING TIP. THE CRACKED AREA WAS CUT OUT. A DOUBLER AND FILLER REPAIR WERE FABRICATED AND INSTALLED IAW SRM 57-20-5.Aug 7, 1996 · N14788 · Boeing 727232SDR P5CA9600643Bracket · chafedFOUND LEFTHAND FORWARD MOUNTING BRACKET CHAFED AND ONE ANCHOR NUT MISSING NEAR NR 4 PYLON. FABRICATED NEW BRACKET AND INSTALLED BRACKET AND ANCHOR NUT IAW SRM 51-30-02.Aug 5, 1996 · N832FT · Boeing 747121SDR P5CA9600642Bracket · crackedLEFT WING NR 2 DIAGONAL FITTING BRACKET AT RIGHT SIDE IS CRACKED. FABRICATED NEW BRACKET AND INSTALLED AS PER SRM 51-20-01 AND 51-30-02.Aug 5, 1996 · N832FT · Boeing 747121SDR P5CA9600631Angle · crackedFOUND CRACK ON SUPPORT ANGLE AT WS 670 AT ATTACHMENT OF FRONT SPAR. NEW ANGLE INSTALLED PER SB 57-2159.Aug 5, 1996 · N832FT · Boeing 747121SDR P5CA9600628Rod · corrodedFOUND CORRODED ROD BEHIND HYDRAULIC TANK IN WING NEAR ATTACH TO NR 3 PYLON. LEVEL ONE CORROSION REMOVED AND TREATED AS PER MM 51-21-03.Aug 5, 1996 · N832FT · Boeing 747121SDR P5CA9600626Bracket · brokenFOUND BROKEN BRACKET AT BAY CUTOUT ABOVE PYLON NR 2. NEW BRACKET AND FASTENERS INSTALLED AS PER SRM 51-30-02.Aug 5, 1996 · N832FT · Boeing 747121
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