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 UPS97223041Rib · wornINSPECTION TYPE:D, LT WING NR 7 SPOILER I/B DOWNSTOP RIB FWD LWR ATTACH POINT LOOSE. REPAIRED IAW SRS EO 97-09-006, UPS FILE NUMBER B727-57-1826.SDR SCNA97108Rib · crackedDURING HEAVY MAINTENANCE VISIT, CRACKS WERE FOUND ON THE RIB CHORD LOCATED AT STATION 760, LBL 70.5 AND RBL 70.5. REPAIRED CRACKS IAW B727 SERVICE BULLETIN 57-112, ENGINEERING ORDER 57-5127-1, AND DRAWING 65C21524, 65C33202, AND 65C37221.SDR ABXA9700922Rib · crackedDURING C-CHECK, FOUND THE RIGHT WING LEADING EDGE RIB AT STA 172 CRACKED. CUTOUT CRACKED SECTION OF RIB, AND REPAIRED IAW ABX REA D957-19252.SDR ABXA9700921Bulkhead Fitting · crackedDURING C-CHECK, FOUND THE RIGHT WING BULKHEAD FITTING AT W/STA XRS 69 BETWEEN STRINGERS 12 AND 13 INSIDE LT WING FUEL TANK CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-05.SDR SCNA97176Rib · crackedDURING HEAVY MAINTENANCE VISIT, A LEADING EDGE RIB WAS FOUND TO HAVE A 1.5 INCH CRACK IN THE RADIUS AT RIGHT WING STATION 385. FABRICATED AND INSTALLED NEW PART IAW B727 SRM 51-40-3 AND 51-30-2.SDR DHL9770162CRib · crackedAT C-CHECK, C/W WITH LEFT WING RIB CHORD INSP BL 70.5. REMOVED FASTENERS, NDT FASTENERS HOLES CRACK INDICATION NOTED, STOP DRILLED, HFEC STOP DRILL. ACCOMPLISHED S/B 57-112, INSTALLED FASTENERS.SDR SCNA97159Rib · crackedDURING HEAVY MAINTENANCE VISIT, THE NUMBER 4 SLAT ACTUATOR ATTACHMENT RIB WAS FOUND CRACKED IN LOWER RADIUS. STOPPED DRILLED CRACK, INSTALLED REPAIR ANGLE IAW B727 SRM 51-10-1, 57-50-3, 51-40-2 AND MAINTENANCE MANUAL 51-20-2.SDR RAAA97B2026Rib · crackedDURING AD 94-07-08 INSPECTION, FOUND RBL 70.5 WING RIB UPPER CHORD CRACKED VERTICALLY BETWEEN FORWARD HOLES (REF S/B 727-57-0112) AT BS 760.95. REPAIRED PER S/B 727-57-0112, REV 4 SECTION III, PART V.SDR RAAA97B2025Rib · crackedDURING AD 94-07-08 INSPECTION, FOUND LBL 70.5 WING RIB UPPER CHORD CRACKED VERTICALLY BETWEEN FORWARD HOLES (REF S/B 727-57-0112) AT BS 760.95. REPAIRED PER S/B 727-57-0112, REV 4, SECTION III, PART V.SDR UPS97822906Rib · crackedINSPECTION TYPE-D, LT WING L/E BETWEEN NR 1 AND NR 2 PYLONS, 10TH RIB FROM INBD END IS CRACKED. FABRICATED AND INSTALLED REPAIR IAW SRM 55-2-0.SDR DHL9770522CRib · crackedAT C CHECK, RIGHT WING RIB UPPER CHORD AT BL 70.5 INSPECT PER S/B 57-0112. NDT INSPECTED, TWO CRACKS NOTED, STOP DRILLED CRACKS, HFEC, ACCOMPLISHED S/B 57-112. INSTALLED KIT COMMON TO RT WING JUST OUTBD AND COMMON TO CENTER TANK. INSTALLED REMAINDER OF REPSDR 97ZZZX2070Rib · crackedUPON INSPECTION FOR RECOVER PROCESS, FOUND BRACKET P/N 2-1992 AND RIB P/N 3-446 CRACKED AT SPAR ATTACH. SL 404 COVERS THIS SUBJECT FOR '7' SERIES AIRCRAFT WITH 1,000 'PLUS' HOURS, BUT DOES NOT INCLUDE '8' SERIES AIRCRAFT, THIS CONDITION FOUND ON BOTH AILERONSSDR TWAA9804001Rib · crackedMCI - DURING C-CHECK MAINTENANCE, THE LEFT WING EDDY CURRENT SHOWED CRACK INDICATION AT 6 AND 12 O'CLOCK POSITION IN RIB CHORD TOP FORWARD HOLE. LEFT BOTTOM FWD HOLE HAD 2 CRACKS IN VERTICAL LEG 2 AND 7 'CLOCK. STOP DRILLED CRACKS PER SRM 51-10-01 FIG 6A. ISDR DHL9770501CRib · crackedDURING C CHECK, A CRACK WAS FOUND IN THE RIB ON THE L/W AT WS 656 AT LOWER STR NR 2. STOP DRILLED CRACK AT BOTH ENDS AND INSTALLED RIB REPAIR AT LOWER SECTION OF RIB, STR NR 2, AS PER S/B 727- 57-127. NON ROUTINE NR 1226.SDR 97UAL900331Rib · crackedUPPER CHORD ON LEFT WING RIB AT WS 1516.6 CRACKED. CRACK DISCOVERED DURING HEAVY MAINTENANCE VISIT. REPLACED CRACKED CHORD PER STRUCTURAL REPAIR MANUAL.SDR TWAA9807907Rib · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LEFT WING LE WING LE RIB CRACKED AT XRS 486. REPLACED RIB PER SRM 51-00, PAGE 27 ITEM 1B. (M)SDR TWAA9803804Rib · crackedMCI - DURING C-CHECK MAINTENANCE, A CRACK INDICATION WAS FOUND IN THE RT WING RIB UPPER CHORD AT RBL 70.5 STATION 760, THE UPPER FORWARD HOLE AT 6 O'CLOCK AND 12 O'CLOCK. REPAIRED PER ARA 11719 AND TWA STANDARD PRACTICES. (M)SDR DHL9770505CRib · crackedDURING C CHECK, R/W INTERIOR WS 629.0 WING RIB LOWER FLANGE CRACKED AT STR 6. STOP DRILLED CRACK. PERFORMED HFEC CHECK. INSTALLED REPAIR PER SRM 57-10-5 PAGE 4 AT R/W WS 629, STR 6 PER S/B 727-57-127. REPAIR SIZE 3X8. NON ROUTINE 2476.SDR DHL9770502CRib · crackedDURING C CHECK, A CRACK WAS FOUND AT LEFT WS 686.5 LOWER FLANGE OF RIB AT STR 6 ATTACH POINT. STOP DRILLED CRACK AT BOTH ENDS. INSTALLED WING RIB REPAIR AT LT WING STA 686.5 PER SRM 57-10-5 PAGE 5. REPAIR SIZE 1X8X3. NON ROUTINE 1228.SDR UPS97822783Rib · crackedINSPECTION TYPE:D, LEFT WING L/E SECTION OVER NR 3 PYLON, L/E RIB IS CRACKED, AT LWR END JUST OB OF STA XS 250.089. FABRICATED AND INSTALLED REPAIR IAW SRM 57-2-0.SDR UPS97822782Rib · crackedINSPECTION TYPE:D, RT WING L/E SECTION BETWEEN PYLONS STA XFS 341.5 THE LOWER L/E RIB IS CRACKED IN CENTER. FABRICATED AND INSTALLED REPAIR IAW SRM 57-2-0 AND 51-1-20D.SDR ABXA9700650Rib · crackedDURING C-CHECK, FOUND THE LEFT WING LEADING EDGE RIB JUST INBD OF STA XRS 531 IS CRACKED INSIDE RADIATING FROM HI-LOCK. REPLACED RIB IAW DC9 SRM 51-30-2 AND 51-30-5.SDR 97ZZZX3057Rib · damagedATW - RT WING JO-BOLT RIB NR 2 USED 3 OVERSIZED FASTENERS DUE TO TOOLING MARKS REAMING OUTBOARD. RT WING RIB NR 2 STRINGERS 2A, 7A; RT INBOARD RIB NR 2, STRINGERS 7F: HC571H9003, PC/RJ0652-95, DJR/RJ0634. REAMED HOLES TO OVERSIZE, SPOT FACED, COUNTERSUNK, DSDR AU970298Rib · corroded(AUS) RH WING ROOT RIB LOWER FLANGE CORRODED IN AREA OF RIB TO LOWER WING SKIN ATTACHMENT RIVETS - AIRCRAFT OPERATES IN A SALT LADENENVIRONMENT AND IS NOT HANGAREDSDR C2XA97IA118Rib · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING NOSE RIB AT RIB 20 WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA97IA117Rib · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT WING NOSE RIB AT RIB 21 WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR 97ZZZX3466Rib · defectiveATW - PERFORMED BAE AVRO RIL HC571H9033 TO RIGHT WING AND RIB NR 2 AND FAXES PC/RJ0652-95 AND DJR/RJ0634-96. INSTALLED JO-BOLTS TO RIB NR 2 PER INSTRUCTIONS STATED ABOVE.SDR 97ZZZX3465Rib · defectiveATW - PERFORMED BAE AVRO RIL HC571H9033 TO LEFT WING RIB NR 2 AND FAX ES PC/RJ0652-95 AND DJR/RJ0634-96. PERFORMED BAE AVRO RIL HC571H9033 INSTALLATION OF MRL FASTENERS TO RIB NR 2 CROWN FITTINGS IN LEFT WING INBD AND OTBD. REF: FAXES PC/RJO 652-95 AND DJR/SDR 97ZZZX3463Rib · defectiveATW - PERFORMED BAE AVRO RIL HC571H9033 TO LEFT WING RIB ZERO AND FAXES PC/RJ0652-95 AND DJR/RJ0634-96. C/W RIL HC571H9033 AND FAXES PC/RJ0652-95 AND DJR/RJ0634-9.SDR 97ZZZX3056Rib · damagedATW - LT WING RIB NR 2, 4 OVERSIZED J-BOLT FASTENERS DUE TOOLING MARKS REAMING AT POS'S . OUTBOARD STRINGERS 1A, 6A, 7A AND INBOARD STRINGERS B4A.1A A 70, 12 DIA.ALTOTNRS800, 12 DIA.HC571H9003, PC/RJ0652-95, DJR/RJ0634. REAMED HOLES TO OVERSIZE SPOT FACED, SDR UPS97822585Rib · crackedINSPECTION TYPE-D, LT NR 2 ENG L/E STUB WING L/E RIB UPPER AFT END CRACKED, THIRD RIB FROM I/B END. FABRICATED AND INSTALLED ANGLE PER SRM 57-2-0 FIG 2.SDR UPS97822535Rib · crackedINSPECTION TYPE-D, RT WING L/E SECTION BETWEEN PYLONS HAS ONE UPPER RIB CRACKED AT THE AFT END 48 O/B OF SLOT ACTUATORS. REPAIRED IAW SRM 57-2-0 AND 51-1-21.SDR UPS97822666Rib · crackedINSPECTION TYPE:D, LT WING L/E RIB CRACKED AT PNEUMATIC DUCT ATTACH POINT JUST OB OF NR 2 ENGINE. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW SRM 52-2-0, 51-1-8, 57-2-0 FIG 2, 51-1-20D.SDR UPS97822536Rib · crackedINSPECTION TYPE-D, RT WING L/E AT STA XFS 804.00 TO THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.SDR UPS97822530Rib · crackedINSPECTION TYPE: D. RIGHT WING L/E AT STA XFS 747, THE UPPER L/E RIB IS CRACKED AT AFT END. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 57-2-0 FIG 2 SHT 2.SDR CALA9700513Rib · crackedINSPECTION FOUND A 1 INCH CRACK BETWEEN TWO AFT UPPER BOLTS OF LT WING LEADING EDGE RIB AT SLAT STA 0. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.SDR CKSA97150Rib · crackedDURING C-1 CHECK INSPECTION, FOUND RIGHT HAND WING TRAILING EDGE (FLAPWELL) HAS A CRACKED RIB FRAME AT XRS303. REPAIRED FRAME AT XRS303 TRAILING EDGE RIGHT HAND WING AS PER AIA SKETCH AIA/E/2501 EA 97-013. C-1 CHECK INSPECTION WORK CARD NUMBER 2002. NON-ROUSDR CKSA97101Rib · crackedDURING CPCP CHECK INSPECTION, FOUND RIGHT HAND UPPER WING OUTBOARD LEADING EDGE SLOT HAS THREE RIB FRAMES CRACKED BEHIND CENTER SLOT PANEL. REPAIRED RIBS FRAME CRACK IAW SRM 57-2-0 AIA EER D8-05184. TREATED AND PRIMED AS PER SRM 51-1-8. CORROSION TASK CARD NSDR ABXA9700163Rib · crackedRIGHT WING LEADING EDGE AT STATION XFS 591.25 IS CRACKED AT AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8.SDR DHL9771296DRib · crackedDURING D-CHECK, A CRACK WAS LOCATED AT THE RIGHT WING LEADING EDGE RIB AT SLAT STA AT 260 ORIGINATING AT PREVIOUS REPAIR. REMOVED AND REPLACED DAMAGED REPAIR ON RIGHT WING LEADING EDGE RIB AT SLAT STA 260 PER BOEING SRM 57-30-3. REPAIR SIZE 2 X 16.SDR HALA97101Rib · corrodedRIGHT WING TE XRS 350, TRAILING EDGE SUPPORT RIB FOR UPPER TE PANEL HAS LEVEL 11 CORROSION. REMOVED AND REPLACED 9957465-8 TEE AND -6 ANGLE DUE TO CORROSION AND REPLACED SPOILER WEAR PLATE PER SRM 51-10-2, 51-10-3, 51-30-2, 51-30-0. (M)SDR ABXA9700350Rib · crackedDURING C INSPECTION, FOUND THE RIGHT WING TRAILING RIB AT XRS 167, CRACKED AT AFT END. REPLACED TRAILING EDGE RIB IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.SDR ABXA9700344Rib · crackedDURING C INSPECTION, FOUND A RIGHT WING LEADING EDGE RIB CRACKED, INBOARD OF NR 7 SLAT TRACK. REPAIRED RIB IAW ABX REA D957-18711 AND DC-9 SRM CHAPTER 57-06A FIGURE 5 SHEET 1.SDR UPS97822364Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB CRACKED AT LOWER AFT END XFS 424.5. REPAIRED IAW SRM 57-2-0 FIG 2.SDR CALA9700427Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN UPPER RIB CAP OF RT WING LEADING EDGE FS 340. THE ANGLE WAS REMOVED, A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-2.SDR AU970255Rib · corroded(AUS) LH AND RH WINGS CORRODED IN AREA BETWEEN RIBS AND SKIN - SEE MDR97/0252 FOR ADDITIONAL INFORMATIONSDR ABXA9700351Rib · crackedDURING C INSPECTION, FOUND THE RIGHT WING TRAILING EDGE RIB AT OUTBOARD END OF OUTBOARD SPOILER, CRACKED AT AFT END. REPLACED TRAILING EDGE RIB IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.SDR DHL9771258DRib · crackedAT D-CHECK, RIGHT WING UPPER RIB CHORD CRACKED AT FWD LOWER HOLE. STOP DRILLED CRACK, HFEC, INSTALLED REPAIR KIT PER S/B 57-0112, INSTALLED PRESSURE BOX PER SRM 51-30-2.SDR C2XA97IA079Rib · crackedIAH - DURING C-CHECK INSPECTION, RIB 30 ON THE RIGHT WING WAS FOUND TO BE CRACKED AT ATTACHMENT FOR PANELS 615 AND 616AR. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A DOUBLER REPAIR PER ATR SRM 51-70-00 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICSDR ABXA9700511Rib · crackedDURING C-CHECK, THE LEFT WING NR 2 SLAT TRACK INBOARD RIB WAS FOUND CRACKED. THE RIB WAS REPLACED IAW DC9 SRM 51-30-1.
Back to JASC 5712