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 CALA9601621Chord · crackedINSPECTION FOUND A 3.5 INCH CRACK ON LOWER LEADING EDGE CHORD JUST INBOARD OF INBOARD TRACK FOR NR 2 LEADING EDGE SLAT. THE CRACK WAS STOP DRILLED, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4.SDR CALA9601620Chord · crackedINSPECTION FOUND A 3 INCH CRACK ON LOWER LEADING EDGE CHORD JUST OUTBOARD OF OUTBOARD TRACK FOR NR 2 LEADING EDGE SLAT. THE CRACK WAS STOP DRILLED, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4.SDR ZIAA961136Hoist Point · corrodedMCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED WING STRUCTURE LE HOIST POINT LT WS 672-720-803 CORRODED. REPAIRED IAW DWG A74-R06. (X)SDR ZIAA961127Flange · corrodedMCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED WING STRUCTURE LT FLANGE, LT XFS 525-560 CORRODED. REPAIRED IAW DWG A74-R24. (X)SDR ZIAA961124Angle · corrodedMCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED WING STRUCTURE L-ANGLE XW428 CORRODED. REPAIRED IAW DWG A74-R23. (X)SDR HAL960095Doubler · corrodedUNDERSIDE OF LEFT WING JUST OUTBOARD OF MLG STRUT DOOR TAPER LOCK FASTENER HEAD CORRODED. INSTALLED DOUBLER (ESO 7349) CORROSION PROTECT THE RE-WORKED AREA PER SRM VOL 2 CHAPTER 51-21-01. (M)SDR CA961112028Latch Receiver · bent(CAN) AT 11,000 FEET, PILOT NOTICED A LARGE VIBRATION AND A PITCH DOWN ATTITUDE. CREW DETERMINED THAT THE RIGHT WING LOCKER WAS OPENED. EMERGENCY DECLARED AND AIRCRAFT LANDED OK. BOTH LATCH RECEIVER ASSEMBLIES WERE BENT NOT ALLOWING THE LATCH ASSEMBLY PIN TO ESDR DHL9672015CStiffener · crackedAT C-CHECK, WING CENTER SECTION INTERIOR STIFFENER, RBL 51 FS 740 CRACKED AT LOWER AREA. REPLACED STIFFENER PER SRM 51-30-2, 34 INCHES LONG.SDR 96FDEA01675Chord · corrosionCENTER WING AFT WEB UPPER CHORD BULGED AND CORROSION EMANTING FROM BETWEEN WEB AND CHORD AT STA 870 W/L 190 LBL 30. REMOVED CORRODED WEB AND UPPER CHORD STA 870 LBL 70 RBL 70. INSTALLED REPAIR PER ESO 11697 DATED 9-10-96, PER SRM 57-10-00.SDR ARWA9610052Pan Assy · crackedARROW AIR SICR 7185 PROVED PERMANENT REPAIR OF PAN CRACK AT XS 526 LT WING USING DOUGLAS SKETCH. FORMED PAN PER DAC AUTHORIZATION DATED 9-24-96, DAC DRWAING 5769857. TREATED AND INSTALLED REPAIR PARTS AT XS 526 IAW DC-8 SRM 51-1-21, 51-1-8 AND 51-1-17.SDR DHL9672035CStiffener · crackedAT C-CHECK, WING CENTER SECTION INTERIOR UPPER STIFFENER ATTACH ANGLE CRACKED LBL 24, BS 740. REMOVED AND REPLACED ANGLE PER SRM 51-30-2, 3 BY 3.5.SDR 96FDEA01681Vert Stiffener · crackedVERTICAL STIFFINER ON CENTER WING AFT WEB AFT SIDED CRACKED APPROX 4 INCHES AT UPPER END STA 868 RBL 40 WL 190. REMOVED STIFFENER AND INSTALLED NEW STIFFENER PER SRM 51-10-1.SDR SCNA96350Brace · crackedDURING HEAVY MAINTENANCE FOUND SUPPORT BRACE CRACKED AT LEFT WING FRONT SPAR, STA XORS 130, INBOARD OF NR 1 SLAT, NR 3 TRACK. REMOVED SUPPORT BRACE, FABRICATED AND INSTALLED A NEW BRACE IN ACCORDANCE WITH SRM 53-00-01.SDR CKSA96170Shear Tie · crackedKOSC - DURING C-2 CHECK INSPECTION FOUND: NR 2 MAIN TANK INTERIOR SHEAR TIE CRACKED WS 670 (FORWARD PYLON INBOARD STRUT SUPPORT APPROXIMATELY 11 INCHES AFT OF FORWARD SPAR) 1.50 INCH CRACK. REPAIRED SHEAR TIE IAW SB 747-57-2273 REV 2 FIGURE 10 AND 11. AD 94-SDR CKSA96169Fitting · crackedKOSC - DURING C-2 CHECK INSPECTION FOUND: CRACK IN RIB SUPPORT FITTING 65B01020-1137 WING STATION 669.5. REPLACED RIB SUPPORT FITTING IAW BOEING 747 SRM 51-10-1 AND 53-30-2. C-CHECK CARD NR 7GK0542. TASK CARD NR 85710.SDR ABXA9700389Bolt · corrodedDURING C-CHECK INSPECTION, FOUND CORRODED BOLT AT LEFT WING UPPER FUSELAGE TO WING ATTACH FITTING. REPLACED BOLT IAW YS-11 M.M. 57-41-1.SDR ABXA9700388Bolt · corrodedDURING C-CHECK INSPECTION, FOUND CORRODED BOLT AT RIGHT WING UPPER FUSELAGE TO WING ATTACH FITTING. REPLACED BOLT IAW YS-11 M.M. 57-41-1.SDR DL72W962332Stiffener · crackedA 1 INCH CRACK IN WING L/E VERTICAL STIFFENER AT NR 5 SLAT I/B TRACK O/B POSITION. REPLACED STIFFENER PER M/M.SDR MWEA96578Fitting · crackedDURING D-CHECK, FOUND RT WING UPPER OUTBD SKIN FITTINGS AT STA XRS 164 NEAR REAR SPAR ARE CRACKED. MAINTENANCE FABRICATED AND INSTALLED NEW FITTINGS IAW DAC DRAWING 4913298, 4911461, AND SRM 57-01.SDR MWEA96564Trap Panel · crackedDURING D-CK, FOUND RT TRAPEZOIDAL PANEL FWD FLANGE HAS A CRACK THAT EXTENDS AFT THROUGH THE FOURTH FASTENER APPROX .125 INCH. INSTALLED DOUBLER REPAIR IAW SRM 57-09, FIG 6 AND DAC TELEX SVC-MSP-0789.SDR MWEA96540Frame · dentedDURING D-CK, FOUND LT WING TIP FRAME DENTED LOWER EDGE OF NAV LIGHT CAVITY. REPLACED WING TIP FRAME.SDR 96ZZZM1525Splice · crackedMCI - DURING OP-16, FOUND A 1 INCH CRACK IN RIGHT WING LE SPLICE PLATE, STATION 164. REPAIRED PER SSRM 57-40-103.SDR DL757962335Te Wedge · delaminatedT/E WEDGE DELAMINATED ALONG FORWARD SPAR. REPLACED WEDGE PER SRM 57-43-02 FIG 202.SDR P5CA9600770Bracket · brokenLEFT WING FUEL PANEL HOLD OPEN BRACKET BROKEN. REPAIRED PER SRM 51-10-01.SDR 96FDEA01569Strap · crackedSNRM 00182, RIGHT O/B FLAP I/B HINGE O/B SIDE AT REAR TENSION STRAP IS CRACKED AT BOTTOM FLANGE. *S/D* COMPLIED WITH EA 8-5710-31702, INSTALLED NEW PART PER SRM 53-00-01.SDR 96FDEA01568Strap · crackedSNRM 00181, LEFT O/B T/E FLAP I/B HINGE O/B SIDE AT REAR SPAR TENSION STRAP IS CRACKED AT BOTTOM FLANGE. *S/D* COMPLIED WITH EA 8-5710-31702, INSTALLED NEW PART PER SRM 53-00-01.SDR 96FDEA01567Stiffener · crackedNR0510 AND 017, TOP OF THE VERTICAL STIFFENER IS CRACKED IN THE WING CENTER SECTION AT BS 740 RBL 45. *S/D* REMOVED AND REPLACED VERTICAL STIFFENER IN THE WING CENTER SECTION AT BS 740 RBL 45 IAW FEDEX SRM 51-30-2.SDR HAL960087False Spar Cap · corrodedDURING C-CHECK, FOUND CORROSION ON LEFT WING FUSELAGE SPAR UPPER CAP AT STATION XW=320 TO XW=224. REMOVED AND REPLACED EIGHT FOOT SECTION OF FALSE SPAR PER AARD 51-01-00-05, 51-35-01 VOL 2 AND ESO 7349 DATED 10-4-96. (M)SDR SRAA961004Wing Tip · damagedWHILE ON GROUND AT SIN, AIRCRAFT'S RIGHT WING TIP GOT STRUCK BY GROUND EQUIPMENT. REMOVED AND REPLACED RIGHT WING TIP PER DOUGLAS M.M. CH 57-24.SDR HALA960084False Spar · corrodedCORROSION ON AFT SIDE OF FALSE SPAR JUST OUTBOARD OF NR 1 SPOILER ACT. REMOVED AND REPLACED 8 FOOT SECTION OF FALSE SPAR PER AARD 51-01-00-05 AND ESO 7349 DATED 10-4-96. (M)SDR CALA9601386Clearance Door · out of positionTHE FLAPS WOULD NOT EXTEND BEYOND 8 DEGREES DURING FLAP EXTENSION FOR LANDING. THE FLAPS WOULD NOT MOVE USING ALTERNATE FLAP SYSTEM. THE LEADING EDGE DEVICES WENT TO FULL EXTENSION. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT INBOARD FLASDR P5CA9600752Support Rod · brokenBROKEN ANGLED SUPPORT ROD LEFT WING NR 7 LEADING EDGE FLAP WELL. FABRICATED AND INSTALLED NEW SUPPORT ROD PER BOEING SRM 51-10-01 AND 51-30-02.SDR 97ZZZX1420Cap · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON LT WING LOWER CAP AT WS 437. REF: SI 104SDR CALA9601499Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN ANGLE OF LT WING LEADING EDGE CAVITY AT STA 333. THE ANGLE WAS REMOVED, A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-20-2.SDR CALA9601494Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK AT AFT END OF UPPER RIB CAP INSIDE OF RT WING LEADING EDGE, FS 333. THE CRACKED ANGLE WAS REMOVED AND A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-20-2.SDR UPS96221250Shear Tie · corrodedINSPECTION TYPE: C. CORROSION ON SHEAR TIE STA 500 RBL 17-22 WL 150. MECH REMOVED CORROSION FROM SHEAR TIE AT STA 500 RBL 17-22 WL 150. REWORKED DEEMED OUT OF LIMITS IAW SRM 53-10-1. REPAIRED SHEAR TIE IAW SRM 53-10-4.SDR DU4R9600018Fitting · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND THE LT FORWARD SPAR TO TRAP FITTING SUPPORT (SKI FITTING) HAS CORROSION AROUND FASTENERS.SDR DU4R9600007Doubler · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND THE LT WING UPPER BEAVER TAIL DOUBLER PANEL HAS CORROSION THROUGHOUT PANEL. STRIPPING REQUIRED FOR FURTHER INSPECTION.SDR ABXA9700683Splice · crackedDURING C-CHECK, THE LEFT WING LEADING EDGE SPLICE WAS FOUND CRACKED AT STA 111. REPLACED SPLICE IAW DC-9 SRM.SDR ABXA9700682Splice · crackedDURING C-CHECK, THE LEFT WING LEADING EDGE SPLICE WAS FOUND CRACKED AT STA 267. REPLACED SPLICE IAW DC-9 SRM.SDR UPS96821336Web · crackedINSPECTION TYPE-C/CK, RIGHT CENTER WING STA XCW23 WEB HAS CRACKED LOWER ATTACH ANGLE AT ST RINGER 58. REMOVED CRACKED ATTACH ANGLE, LOCATED, DRILLED AND REAMED NEW ATTACHED ANGLE IAW DC8 SRM 51-1-24, ALODINED AND PRIMED NEW ATTACH ANGLE IAW DC8 SRM 51-1-8, INSDR 9621289872Fitting · crackedDURING H-CHECK, FOUND A 4 INCH CRACK IN THE CENTER WING FRONT SPAR UPPER LEFT SUPPORT FITTING AT FS 693. REPLACED FITTING (P/N 5913055-507).SDR AALA961423Splice Plate · crackedTUL - SPLICE PLATE CRACKED ABOVE NR 5 LEFT FLAP ACT. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 51-40-02 R8-12. (M)SDR 9621249910Doubler · crackedDURING H-CHECK, FOUND A CRACK IN THE RIGHT WING FRONT SPAR DOUBLER AT XOS 530. REPAIRED DOUBLER (P/N 9919343-2) PER EA 99-110333.SDR USAA960624Doubler · crackedPIT - DURING Q-3/C-2 CHECK, FOUND .5 INCH CRACK LOWER WING SKIN PLATE DOUBLER AT LOWER WING ACCESS PLATE 1456A DOUBLER. INSTALLED DOUBLERS PER SRM 57-03 FIG 29A AND EA 33614. (M)SDR CALA9601450Bracket · crackedRIGHT WING BRACKET HAS CORROSION INSIDE FIXED L/E AT OUTBOARD SIDE OF NR 5 L/E FLAP OUTBOARD HINGE. REMOVED FABRICATED AND INSTALLED REPLACEMENT BRACKET PER SRM 51-10-1 AND 51-10-2.SDR 96FDEA01492Chord · corrodedNR 0674 AND 035, CORROSION (C53-224-05) ON BS 740 LOWER CHORD FOR CENTER WING SECTION FROM LBL 7 TO LBL 27. *S/D* REMOVED DAMAGED LOWER CHORD AT BS 740 AND INSTALLED NEW CHORD PER FEDEX EA NR 7-5710-31187.SDR 9620129960Fitting · corrodedDURING M-CHECK, FOUND CORROSION ON THE CENTER WING TANK FORWARD RIGHT ATTACH FITTING FS 610. REPLACED FITTING PER SRM 51-30-5, 51-30-1.SDR EISA96216Angle · crackedFOUND RIGHT WING LE RIB LOWER ANGLE CRACKED AT WS 130.7. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-30-02. (M)SDR EISA96214Angle · crackedFOUND RIGHT WING LE ANGLE CRACKED AT AFT END JUST INBOARD OF WS 330. FABRICATED AND INSTALLED DOUBLER PER SRM 51-20-2 AND 51-30-2. (M)
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