JASC 5712
Service difficulty reports · 6,970
Reports filed under 5712 · Wing, Rib/Bulkhead, 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 = '5712' 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 = '5712' 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 CALA9600663Rib · crackedINSPECTION FOUND A .50 INCH CRACK AT LOWER RADIUS OF LEADING EDGE RIB OF LT WING AT STA XRS 276. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5720-01521.SDR CA960524022Rib · rivets sheared(CAN) LEFT WING OUTBOARD END RIB JOINT TO REAR WING SPAR ATTACH POINT SHEARED BOTH RIVETS. THIS PERMITTED TIP TANK VERTICAL MOVEMENT WHICH LED TO CRACK IN WING SKIN. THIS IDENTICAL PROBLEM IS REPORTED TO HAVE ALSO HAPPENED IN A 414 AND THE SUBMITTER SUGGESTS TSDR AU960652Rib · cracked(AUS) LH AND RH MAIN LANDING GEAR WHEEL WELL WING RIBS AND SKINS CRACKEDSDR 96ZZZX3031Rib · crackedMCI - DURING SPECIAL CHECK FOUND CRACK IN RIB CASTELLATION AT FORWARD SIDE OF STR 9, BOTTOM IWS 555. REPAIRED PER SRM 51-10-01. AIRCRAFT TOTAL TIME: 60,229 HOURS; 22,908 CYCLES.SDR 96ZZZX3030Rib · crackedMCI - DURING SPECIAL CHECK FOUND CRACKS IN TOP WING RIB CASTELLATION OF RT WING, IWS 503, STRINGERS 18, 19, AND 21. REPAIRED PER SB 093-57-207 AND LOCKHEED DWG NR 1647070, SHEET 3. AIRCRAFT TOTAL TIME: 60,229 HOURS; 22,908 CYCLES.SDR 96ZZZX3029Rib · crackedMCI - DURING SPECIAL CHECK, FOUND CRACK IN RIB CASTELLATION AT FORWARD SIDE OF STR 13 AND STR 19, TOP IWS 555. REPAIRED PER SB 093-57-207 AND SRM 51-10-01. AIRCRAFT TOTAL TIME: 60,229 HOURS; 22,908 CYCLES.SDR EISA96044Rib · crackedLEFT WING TRAILING EDGE COVE STIFFENER RIB CRACKED, JUST OUTBOARD OF NR 4 FLAP TRACK. FABRICATED AND INSTALLED NEW RIB PER SRM 51-40-03. (M)SDR UPS96220085Rib · crackedINSPECTION TYPE 'D', RIGHT WING INTERNAL RIB STA 519 AT STR 6 IS CRACKED IN RADIUS ON LWR SIDE. STOP DRILLED CRACK, FAB AND INSTALLED REPAIR IAW SRM 57-10-5, 51-10-1 AND 57-10-5.SDR AU960716Rib · incorrect mod(AUS) RH WING RIB LOCATED IN ENGINE BAY ILLEGALLY MODIFIED - A HOLE HAD BEEN DRILLED THROUGH THE RIB STAINLESS STEEL FIRE BARRIER TO FACILITATE PUSHROD REMOVAL - THE HOLE WAS LEFT UNCOVERED ALLOWINGA POSSIBLE ENGINE FIRE TO PENETRATE TO THE FIBREGLASS LEADINGESDR AWXA960313Rib · crackedPAE - FLT 3819 - DURING ROUTINE SCHEDULED C-15 MAINTENANCE CHECK, FOUND LEFT L/E RIB CRCKED AT WBL 183.4. REPAIRED RIB IAW 51-40-4, 51-10-12 AND 51-30-2. (M)SDR AU960553Rib · corroded(AUS) LH AND RH WING RIBS AND STIFFENERS CONTAINED SEVERE EXFOLIATION CORROSION AND CRACKING OF INBOARD TRAILING EDGE ASSEMBLIES PNO 61217-000 AND PNO 61217-001 - CORROSION ALSO FOUND IN NUMEROUS WING WALK RIBS PNO 61224-000 - WING SKINS PNO 61158-010, PNO 61SDR DLL10961139Rib Caps · crackedTHE RT WING IWS 503 RIB UPPER AND LOWER CAPS HAVE CRACKS IN THE TYPICAL LOCATION AT THE ATTACH TABS. THE CAPS ARE TO BE REPLACED PER EO 7-59208-3AD, BUT THE COMPLETE REMOVAL OF THE UPPER CAP PROVIDES SUFFICIENT ACCESS TO ALLOW ONE SPLICE LOCATION IN EACH CAP SDR UPS96820059Rib · crackedINSPECTION TYPE 'C', 4 RIBS CRACKED LT WING L/E ABOVE I/B FUELING PORT. REPAIRED RIBS PER SRM 57-2-0.SDR CALA9600759Rib Attach Lug · crackedINSPECTION FOUND A .50 INCH CRACK IN RIB ATTACH LUG ON AFT SIDE OF UPPER VENT STRINGER 12, OUTBOARD SIDE OF W.S. 686 RIB, NR 3 TANK. REPAIR ANGLES, RADIUS BLOCKS, AND VENT PATCHES WERE FABRICATED AND INSTALLED IAW SRM 51-30-2.SDR 96ZZZM896Rib · crackedMCI - DURING SPECIAL CHECK, FOUND SEVEN CRACKS IN LEFT WING TOP RIB CASTELLATION, STATION 555. REPAIRED PER SERVICE BULLETIN 093-57-207, PARA 2B. (M)SDR 96ZZZM895Rib · crackedMCI - DURING SPECIAL CHECK, FOUND 1.25 INCH CRACK IN LEFT WING RIB CASTELLATION FORWARD SIDE OF STRINGER 19, TOP CHORD, WS 503. REPAIRED PER SERVICE BULLETIN 093-57-207, PARA 2B.SDR 96FDEA00798Rib · crackedRT WING L/E RIB HAS A VISUAL CRACK INDICATION AT THE LOWER RADIUS APPROX 1.5 INCH LONG ON XORSS562.SDR GTIA96NK164Rib Cap · corrodedDURING C-CHECK, FOUND CORRODED RIB CAP IN AFT CARGO COMPARTMENT STATION 930 LEFT. FABRICATED, TREATED AND INSTALLED NEW RIB CAP IAW SRM 51-10-3, 51-10-1 AND 51-10-4. (M)SDR 96ZZZM894Rib · crackedMCI - DURING SPECIAL CHECK, FOUND 1.5 INCH CRACK IN UPPER FORWARD CHORD OF LEFT WING RIB, STATION 503.76. STOP DRILLED AND REPAIRED PER EMLR 66589.SDR 96ZZZX3273Rib · crackedDURING CHECK C-4D, FOUND A 1.50 INCH CRACK IN LEFT WING LOWER AFT END OF RIB, WS 656.5. REPAIRED PER SRM 57-10-05, FIGURE 2, SHEET 3. AIRCRAFT TOTAL TIME: 63,700 HOURS; 42,677 CYCLES.SDR 96ZZZX3272Rib · crackedDURING CHECK C-4D, FOUND RIB CRACKED AT SECOND HOLE ON BOTTOM, STA 656.5. REPAIRED PER SRM 57-10-05, PAGE 6, FIGURE 2. AIRCRAFT TOTAL TIME: 63,700 HOURS; 42,677 CYCLES.SDR 96ZZZX3271Rib · crackedDURING CHECK C-4D, FOUND A 1 INCH CRACK IN RIGHT WING LOWER FORWARD END OF RIB AT RADIUS, WS 738.5. REPAIRED PER SRM 57-10-05. AIRCRAFT TOTAL TIME: 63,700 HOURS; 42,677 CYCLES.SDR 96ZZZX3269Rib · crackedDURING CHECK C-4D, FOUND A .75 INCH CRACK IN RT WING LOWER AFT END OF RIB, WS 629. INSTALLED AND SECURED RIB REPAIR PER SRM 57-10-05, PAGES 6, 7, AND 8. AIRCRAFT TOTAL TIME: 63,700 HOURS; 42,677 CYCLES.SDR 96ZZZM905Rib · crackedJFK - DURING C-4D CHECK, FOUND RIB CRACKED AT RADIUS AREA AT ATTACH POINT TO FIRST STRINGER AFT OF ACCESS HOLE, WL 601.5. REPAIRED BY STOP DRILLING, FABRICATING AND INSTALLING DOUBLER PER SRM 57-10-05, PAGES 6, 7 AND 8. (M)SDR 96ZZZM904Rib · crackedJFK- DURING C-4D CHECK, FOUND A 1.25 INCH CRACK BETWEEN HOLE AND RADIUS OF RIB LOWER FLANGE AT STRINGER 6, RIB WS 546.5. REPAIRED EPR SERVICE BULLETIN 727-57A159, PAGES 6, 7 AND 8. (M)SDR UPS96805980Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT CENTER L/E RIB CRACKED AT APPROX STA XFS 353 UPPER SIDE. STOP DRILLED CRACKS, FAB REPAIR ANGLES AND INSTALLED IAW DC8-SRM 57-3-0 AND 57-2-0.SDR AU960876Rib · cracked(AUS) WING RIBS AND SKINS CRACKED IN AREA OF WHEEL WELLSSDR 96ZZZX3114Rib · looseATW - LEFT WING, CENTER LIFT SPOILER INBOARD JACK RIBS, HAS LOOSE ATTACH BOLTS (UPPER AFT). SECURED AND SAFTIED BOLTS AT CENTER LIFT SUPPLIER INBOARD JACK-RIB UPPER AFT END.SDR 96FDEA00759Rib · crackedHFEC INSP EXHIBITS CRACKS EMANATING AT 12 AND 6 O'CLOCK FROM THE FWD MOST UPPER HOLE AT THE LT WING RIB CHORD BL 70.5 BS 760. REMOVED CRACK BY STOP DRILLING AND INSTALLED SMALL REPAIR AT STA 760 LBL 70.5 WL 209 TO 208 IAW FEDEX EA 7-5710-28232.SDR 96FDEA00746Rib · crackedNR 0137, -001, HFEC INSP EXHIBITS A CRACK IN THE FWD MOST UPPER HOLE AT APPROX 12 O'CLOCK AT RT WING RIB CHORD BL 70.5 BS 760. CUT OUT DAMAGE AT 630 JUST BELOW STR 22R AND REPAIRED PER FEDEX SRM 53-30-3 AND EA 7-5710-28223.SDR 96ZZZX2081Rib Assy · crackedDURING C/W PIPER AD 95-20-7, THE RIB ASSYS ON BOTH SIDES WERE FOUND CRACKED UNDERNEATH THE DRAG BRACE STUD BRACKETS. CRACKS WERE APPROXIMATELY 2 TO 3 INCHES LONG. REPLACEMENT OF THE RIB ASSYS ARE REQUIRED. SUBMITTER STATED THE NEW RIBS ARE MADE OF THICKER MSDR 96ZZZX2080Rib Assy · crackedDURING C/W PIPER AD 95-20-7, THE RIB ASSYS ON BOTH SIDES WERE FOUND CRACKED UNDERNEATH THE DRAG BRACE STUD BRACKETS. CRACKS WERE APPROXIMATELY 2 TO 3 INCHES LONG. REPLACEMENT OF THE RIB ASSYS ARE REQUIRED. SUBMITTER STATED THE NEW RIBS ARE MADE OF THICKER MSDR 9608331226Rib · crackedDURING M-CHECK, FOUND A CRACK IN THE LEFT WING LEADING EDGE FORMER AT XORS 644. REPAIRED FORMER (P/N ARB2917-11) PER EA 12-103929.SDR CAL960455Nose Rib · crackedHOU - INSPECTION FOUND A .75 INCH CRACK IN BEND RADIUS AT UPPER AFT END OF NOSE RIB AND A .75 INCH CRACK IN NOSE RIB ANGLE CLIP OUTBOARD OF NR 10 SLAT TRACK. THE CLIP WAS REPLACED AND THE RIB WAS REPAIRED PER ECRA 5720-01260. (X)SDR 96ZZZX2470Rib · crackedDISMANTLED BOTH LT AND RT WINGS FOR THE PURPOSE OF RECOVERING. IN THE PROCESS OF REMOVING OLD COVER, DETERMINED THAT ALL THE SCREWS THAT SECURE THE FABRIC TO THE RIBS FOR THE NR 2 AND NR 3 INBOARD RIBS OF EACH WING, HAD ELONGATED THE HOLES IN THE RIBS AND WASSDR 96ZZZX2469Rib · crackedDISMANTLED BOTH LT AND RT WINGS FOR THE PURPOSE OF RECOVERING. IN THE PROCESS OF REMOVING OLD COVER, DETERMINED THAT ALL THE SCREWS THAT SECURE THE FABRIC TO THE RIBS FOR THE NR 2 AND NR 3 INBOARD RIBS OF EACH WING, HAD ELONGATED THE HOLES IN THE RIBS AND WASSDR UPS96205850Wing Rib · crackedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED FINDING WING RIB REPAIR AT WS 601.5 LT STR 7 LOWER HAS 1 INCH CRACK. REMOVED CRACK IAW B727-5710-1325 APP A, REPLACED RIB, AND INSTALLED IAW B727-5710-1325 APP C.SDR PLG32596DG2Rib · crackedPSM - DURING ROUTINE C-CHECK INSPECTION, CRACKS WERE FOUND ON RIBS ON LEFT AND RIGHT INBOARD MOST WING LEADING EDGES AND RIGHT WING LEADING EDGE JUST OUTBOARD NACELLE. ALL CRACKS WERE REPAIRED IAW SAAB SRM CHAPTERS 51-57. (M)SDR 96ZZZX1940Rib · crackedTWO CRACKS IN WING RIB AT MLG SIDE BRACE ATTACHMENT AREA WHERE UPLOCK PUSH/PULL TUBE GOES THROUGH RIB. CESSNA SB ME76-2 ADDRESSES THIS PROBLEM.SDR UPS96406051Rib · crackedWHILE IN FOR "C" CHECK AT AMS, MAINTENANCE REPORTED LT L/E INTERIOR INBOARD OF PYLON NR 1 RIB CRACKED UPPER CHORD AT ILES 1094.25. REPLACED RIB IAW SRM 51-30-02.SDR CAL960567Former · crackedKUL - INSPECTION FOUND A 0.75 INCH CRACK AT XOS 1019 AND A 1 INCH CRACK AT XOS 1013 IN LEADING EDGE FORMER. THE FORMER WAS REPAIRED IAW SRM 57-20-00, FIGURE 1. (X)SDR DL72S960666Rib · crackedMTC DISCOVERED CRACKS IN THE LT AND RT WING RIB CHORD DURING MV-2 IN ATL. THE CRACK WAS REMOVED BY OVERSIZING THE HOLES TO .628 INCH IN THE LT RIB CHORD. IN THE RT RIB CHORD THE CRACK WAS REMOVED BY OVERSIZING THE UPPER HOLE TO .6435 INCH AND THE LOWER HOLE SDR CA960509202Ribs · bent(CAN) RIGHT WING RIBS AT W.S. 94.864, 108.281 AND 122.500 FOUND BENT AND BUCKLED UNDER THE UPPER WING SKIN. POSSIBLY CAUSED BY OVERPRESSURE OF FUEL IN AUXILIARY TANK (THERMAL EXPANSION ).SDR 96ZZZX2435Rib · crackedFOUND BOTH RIBS CRACKED WHERE FLANGE RIVETS AND BOLTS TO MAIN SPAR. CRACK IS APPROXIMATELY 1 INCH LONG AND ORIGINATES BY EDGE OF WASHER/NUT FOR TOP BOLT OF GEAR FITTING PN 95643-06 AND PN 95643-07.SDR 96ZZZX2434Rib · crackedFOUND BOTH RIBS CRACKED WHERE FLANGE RIVETS AND BOLTS TO MAIN SPAR. CRACK IS APPROXIMATELY 1 INCH LONG AND ORIGINATES BY EDGE OF WASHER/NUT FOR TOP BOLT OF GEAR FITTING PN 95643-06 AND PN 95643-07.SDR 96FDEA00486Rib · gougedSNRM (0109), FIXED LEADING EDGE LEFT WING HAS GOUGES JUST O/B OF NR 1 SLAT ON VERTICAL RIB. REMOVED AND REPLACED VERTICAL RIB.SDR 96FDEA00641Rib Chord · crackedLEFT 760 RIB CHORD AT BL 70.5, TOP FWD HOLE IND CRACK. ENLARGED TOP FWD HOLE. INSTALLED REPAIR PER DRAWING 65-68492-17, ESO 11782, DATED 2-24-96 AND EA.SDR EISA96034Rib · crackedRIGHT WING INTERNAL RIB CRACKED WS 738 FIRST LOWER STRINGER AFT OF REAR SPAR. INSTALLED RIB KIT PER SB 727-57-0127. (M)SDR 9607446601Rib · crackedDURING P-CHECK, FOUND A CRACK IN THE LEFT WING LEADING EDGE RIB AT FSSI 1453. REPAIRED RIB (P/N 65B07848-5) PER EA 66-99441.SDR EISA96025Rib · crackedLEFT WING INTERNAL RIB CRACKED AT WS 629 SECOND LOWER STRINGER FWD OF REAR SPAR. FABRICATED AND INSTALLED DOUBLER PER SRM 57-10-05. (M)
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