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 RRXA991644Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E RIB AT STA XFS 354, CRACKED AT THE AFT UPPER END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND REPAIRED IAW DC8 SRM 57-2-0 FIG 2.SDR RRXA991643Intercostal · crackedDURING A MAINTENANCE VISIT FOUND CRACK, WING, RIGHT, L/E RIB AT STA XFS 335.25, 17 FWD OF THE SPAR, AT THE INTERCOSTAL GUSSET AFT FASTENERS IS CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACSDR RRXA991458Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E AT STA XW 0.00, THE UPPER AFT L/E ATTACH ANGLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW DAC DWG NR 5613646 AND DC8 SDR RRXA991446Intercostal · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E RIB AT STA XFS 335.25, 17 FWD OF THE SPAR, AT THE INTERCOSTAL GUSSET AFT FASTENERS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED ANSDR MALA976557Angle · crackedDURING HEAVY CHECK, RIGHT FLAP ASSEMBLY HI-LOCKS BROKEN, RIB SUPPORT ANGLE AT WS 142 IS CRACKED. MAINTENANCE COMPLETED AD 99-04-17.SDR C2XA99IA426Gussett · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT WING OUTBOARD LEADING EDGE OUTBOARD ATTACH GUSSETT WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED GUSSETT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 3,939.5 HOURS. CYCLES: 2,7SDR UPS99230534Beam · corrodedINSPECTION TYPE:SI, SPOILER BEAM MOUNT PAD FOR NR 6 FLAP TRACK IS CORRODED (ON WING SIDE). REMOVED AND REPLACED SPOILER BEAM MOUNT PAD PER SRM 51-20-151, 51-30-2.SDR COMA9960444Scupper · damagedCENTER TANK GRAVITY FILL SCUPPER ASSY HAS SEVERAL DAMAGED HI-LOC PIN HOLES. REPAIRED IN ACCORDANCE WITH REO 601R-57-21-077.SDR CALA9901054Angle · crackedINSPECTION FOUND FOUR CRACKS IN RT WING FIXED LEADING EDGE RIB TO SKIN INBOARD SIDE CURVED ATTACH ANGLE AT WBL 92, ACCESS CUTOUT 6401. THE CRACKS MEASURED FROM .5 TO FIVE INCHES IN LENGTH. THE CRACKS WERE STOP DRILLED, A REPAIR DOUBLER, ANGLE AND STIFFENER WSDR UPS99830392Rib · crackedINSPECTION TYPE:C1 LT WING L/E RIB AT XS 454.976 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.SDR MWEA99489Splice · misinstalledLEFT WING UPPER REAR SPAR SPLICE PLATE REMOVED FOR INCORRECT BUSHING ALIGNMENT. MTC FABRICATED AND INSTALLED NEW SPAR SPLICE.SDR UPS99830388Doubler · crackedINSPECTION TYPE:C1 RT WING L/E LWR SKIN INTERNAL DOUBLER AT XFS 570 IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-21.SDR UPS99830387Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XS 497.491 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.SDR AALA991161Angle · damagedTUL - ACCOMPLISH PERMANENT REPAIR TO RIGHT WING ROOT PICK UP ANGLE. MADE REPAIR TO RT WING ROOT PER ESO 3095, DATED 7-6-99. (M)SDR UPS99830381Doubler · crackedINSPECTION TYPE:C1 RT WING L/E LWR SKIN INTERNAL DOUBLER AT XFS 597.5 IS CRACKED IN TWO PLACES. REMOVED, FABRICATED AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-21.SDR 99ZZZX3192Fitting · crackedFOUND CRACK IN LOWEST (AS INSTALLED) RIVET HOLE. INSPECTING SIMILAR (1963-1974) 182'S, SUBMITTER HAS FOUND 3 CRACKS IN A MONTH.SDR MWEA99474Clip · crackedFOUND CRACKS IN RIGHT WING LEADING EDGE RIB ATTACH CLIPS AT FRONT SPAR UPPER CAP STATION XRS 330 AND 338. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIR.SDR MWEA99473Fixed Vane · chafedTHE LEFT WING INBOARD NR 3 FLAP FIXED VANE IS CHAFED. MAINTENANCE INSTALLED REPAIR DOUBLER.SDR DL767991774Fitting · crackedA CRACK WAS FOUND IN THE LHS KICKLOAD FITTING IN THE INBD HOLE ON THE OUTER WING SIDE. THE HOLE WAS REAMED TO REMOVED THE CRACK INDICATION. FINAL REWORKED HOLE DIAMETER IS 0.947. REF NPRM 98-NM-278-AD. REWORKED PER ERA 333356-14AD.SDR COMA9960427Leading Edge · dentedRIGHT WING OUTBOARD LEADING EDGE HAS A DENT. REPAIRED RIGHT WING OUTBOARD LEADING EDGE AT FS 279.699 AND 288.641 IAW WVAC EO NR 601R-57-0211.SDR UPS99830406Doubler · crackedINSPECTION TYPE:C123, RT WING L/E SKIN UPPER DOUBLER AT XFS 418 WAS CRACKED. REMOVED, FABRICATED AND REPLACED THE DOUBLER IAW DWG 5769891 AND SRM 51-1-20D AND 51-1-21.SDR UPS99830362Fitting · crackedINSPECTION TYPE:C123, STA XRS 74 BULKHEAD, O/B SIDE, THE STR 51 END FITTING IS CRACKED. REMOVED AND REPLACED FITTING SRM 51-1-20D AND 51-3-0.SDR UPS99830346Doubler · crackedINSPECTION TYPE:C1, RT WING L/E LWR SKIN INTERNAL DOUBLER AT XFS 572.5 IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-20D & 51-1-21.SDR UPS99830411Doubler · crackedINSPECTION TYPE:C123, LT WING L/E UPPER SKIN INTERNAL DOUBLER AT XFS 540 IS CRACKED. REMOVED, FABRICATED AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-21.SDR CALA9901004Angle · crackedINSPECTION FOUND TWO .5 INCH CRACKS THROUGH BOLT HOLES AT O/B LOWER ANGLE INSIDE RT WING FIXED LEADING EDGE RIB, WBL 92.0 (AFT OF NR 4 L/E FLAP I/B END). THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, PAGE 2, 51-40-3, PAGE 1, AND 51-20-2SDR CALA9901002Angle · crackedINSPECTION FOUND A 4.5INCH CRACK IN UPPER T-ANGLE ABOVE WHERE RT O/B AILERON I/B HINGE BRACKET ATTACHES AT RT WING T/E RIB. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-01, PAGE 401 AND 51-30-2.SDR UPS99830340Doubler · crackedINSPECTION TYPE:C1, RT WING L/E LWR INTERNAL SKIN DOUBLER AT XFS 597.5 IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-20D & 51-1-21.SDR CALA9900962Chord · chafedINSPECTION FOUND LT WING/FUSELAGE CHORD CHAFED BY UNDER CARRIAGE BEAM REAR SPAR AT STA 720, WBL 70.5. THE CHORD WAS REPLACED IAW BOEING DRAWING 149N7222.SDR CALA9900960Chord · chafedINSPECTION FOUND RT WING/FUSELAGE CHORD CHAFED AT STA 730, WBL 70.5 BY U/C BEAM REAR SPAR. THE CHORD SECTION WAS REPLACED IAW BOEING DRAWING 149N7222 AND SRM 51-50-02.SDR AWXA9900256Web · crackedIN MAINTENANCE, FOUND NR 3 WEB RIGHT WING HAS 9 CRACK OUTBD FROM END OF AILERON. REMOVED CRACKED WEB. FABRICATED WEB 2024-T3 .032. TREATED, PRIMED, AND INSTALLED WEB IAW SRM 51-10-2 AND 51-30-2.SDR CALA9900985Angle · crackedINSPECTION FOUND A .25 INCH CRACK IN ANGLE AT LT WING DROOPED LEADING EDGE. REPAIRED IAW SRM 57-00-01.SDR CALA9900937Angle · crackedINSPECTION FOUND A 2 CRACK IN RT WING TRAILING EDGE ANGLE AT XORS 486. THE ANGLE WAS REPLACED IAW SRM 51-30-00.SDR AALA991191Stiffener · corrodedTUL - FRONT SPAR VERT STIFFENER CORRODED AT TOP JUST OUTBOARD OF FUEL PRESS SWITCHES. REMOVED AND REPLACED STIFFENER WITH 6 EACH , STEEL HI-LOCKS HL62, 7 EACH STEEL HI-LOCKS HL62 PER SRM 51-10-1 AND SAME PART NR STIFFENER. (M)SDR AT9900564Fixed Vane · corrodedDURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND SPOTS OF CORROSION ON UNDERSIDE OF RT WING FLAP FIXED VANE. REMOVED CORROSION. FABRICATED FILLERS AND DOUBLER. BONDED REPAIR. ALODINED AND SEALED IAW DC9 SRM 57-50-9 IG 2, 51-50-2.SDR CALA9900979Channel · crackedINSPECTION FOUND A 1 INCH CRACK IN LEFT WING UPPER FUEL ACCESS DOOR NR 534CT CHANNEL. THE CHANNEL WAS REPLACED IAW SRM 51-30-00.SDR UPS99230755Bracket · corrodedINSPECTION TYPE:C, ANGLE BRACKET CORRODED ON R/W UPPER AFT SPAR CHORD AT NR 14 SPOILER I/B SIDE HINGE. REMOVED SPOILER I/B ANGLE SUPPORT BRACKET. FABRICATED NEW SUPPORT ANGLE PER SRM 51-20-1 AND 51-30-05. INSTALLED NEW BRACKET PER SRM 51-30-02. LEAK CHECKEDSDR AT9900562Fixed Vane · corrodedDURING SCHEDULED CHECK AT TIMCO LAKE CITY FL, FOUND OUTBOARD FIXED VANE ON RT WING CORRODED. FABRICATED FILLER AND DOUBLER. INSTALLED IAW DC9 SRM 57-50-1, 51-70-2, 51-10-3, 51-30-2.SDR CALA9900864Stiffener · crackedINSPECTION FOUND A 1 INCH CRACK IN STIFFENER ON I/B SIDE OF FIXED L/E RIB O/B OF RT WING FORWARD BOTTLE PIN (AFT OF ANTI-ICE DUCT, ACCESS CUTOUT 6402). THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, PAGE 2. A FORMER ANGLE WAS INSTALLED IAW SRM 51-40-3, FIGURE 1SDR C2XA99IA413Bracket · holes elongatedDURING CONTINENTAL EXPRESS CHECK, FOUND TIE ANGLE BRACKET HOLES ELONGATED FOR INTERNAL WING STRINGER AFT OF ACCESS PANEL 622EB. REPLACED BRACKET IAW SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 18,416.5 HOURS. TAC: 24,388. (X)SDR 99ZZZX3329Panel · disbondedFERRY FLIGHT FROM MARANA, AZ, TO HONG KONG, PILOT REPORTED. CLIMB THROUGH 34,000 FEET AT .84 MACH, A SUDDEN ONSET AIRFRAME SHUDDER OCCURRED. ALL DOORS CLOSED, BUT HAD LEFT INBORD FLAP VIBRATING VISIBLY GETTING WORSE AS IT WENT INBOARD. SLOW TO .60 MACH AND SDR 9903659912Doubler · corrodedDURING PERIODIC CHECK, CORROSION WAS FOUND ON LOWER SECTION OF FUSELAGE SKIN BETWEEN FS 935 AND 996 AT AFT CARGO DOOR JAMB DOUBLER. REPAIRED PER EA 99-164498.SDR QXEA9901585Angle · crackedPDX - LEFT FORWARD WING SPAR TO FUSELAGE CLOSING ANGLE IS CRACKED. REPAIRED IAW DHC8 SRM 51-40-00, PAGE 4, TABLE 4.SDR UIEA99057Beam · crackedDURING ROUTINE INSPECTION OF THE WING TRAILING EDGE AREA, FOUND THE UPPER CHORD SUPPORT BEAM CRACKED IN THE VICINITY OF THE LINK ASSEMBLY. MADE PERMANENT REPAIR BY SPLICING IN A REPLACEMENT SECTION IAW KLM ENGINEERING AND MAINTENANCE REPORT NR 1H105453 AND BOSDR USAA990741Doubler · crackedPIT - DURING Q5/C2 CHECK FOUND 2 INCH CRACK AT LEFT WING PRODUCTIONS SPLICE DOUBLER STATION XFS 196.236. REPLACED DOUBLER (SPLICE) AND ADDED STRAPS PER SRM 57-06B (FIGURE 9). (M)SDR UPS99230258Angle · crackedINSPECTION TYPE:C, RT WING TE PANEL OUTBOARD OF NR 7 FLAP TRACK, ATTACH ANGLE CRACKED. ANGLES REPLACED IAW SRM 51-30-2.SDR UPS99230154Beam · corrodedINSPECTION TYPE:C, CORROSION ON LOWER SURFACE OF LT WING LANDING GEAR BEAM AT NR 4 FLAP TRACK MOUNT. REPAIRED LANDING GEAR BEAM AT NR 4 FLAP TRACK IAW ER 99-5716 (UPS FILE 727-57-2091).SDR DHL9970305CFairing · corrodedAT C CHECK, LEFT WING NR 1 MOVABLE FAIRING SKIN CORRODED AT FWD I/B SIDE AT FAIRING ATTACH POINT. REMOVED PAINT FROM SKIN CORRODED AREA PER MM 51-20-0, CUT 6 INCH BY 5 INCH SECTION OF SKIN AWAY AND INSTALLED REPAIR SKIN AND SPLICE PLATE PER SRM 53-50-1 FIG 1 SDR DHL9970339CAngle · crackedAT C-CHECK, LEFT WING LEADING EDGE CAVITY AREA FSS 115.0 VERTICAL ANGLE CRACKED LOSER SECTION. CUTOUT DAMAGED SECTION 3 BY 2 PER SRM 51-40-3. FABRICATED NEW VERTICAL ANGLE PER SRM 51-40-3 FIGURE 1, MATERIAL USED 7075-0 .071 3 BY 8, .375 INCH, HEAT TREATED 7SDR DHL9970326CStiffener · crackedAT C CHECK, LW VERT STIFFENER IS CRACKED AT LOWER END AT FALSE SPAR BELOW NR 5 SPOILER O/B SIDE. STOP DRILLED 1 CRACK PER SRM 57-50-6. REMOVED APPROX 6 OF FASTENERS PER SRM 57-50-6, MADE NEW L ANGLE DOUBLER PER SRM 57-50-6. PICKED UP EXISTING FASTENER HOLESDR DHL9970307CAngle · crackedAT C CHECK, RT WING TRAILING EDGE COVER PANEL INBOARD SUPPORT ANGLE IS CRACKED AT WS 447.90 JUST INBOARD OF NR 11 SPOILER ACTUATOR. REMOVED AND REPLACED SUPPORT ANGLE AT RT WING AT WS 447.90 PER SRM 51-10-1 PAR 4 AND 51-30-2, N/R 2044.
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