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 UPS99828469Rib · crackedINSPECTION TYPE:C3, RT WING L/E RIB AT STA XOLDI6.225 IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.SDR UPS99828465Rib · crackedINSPECTION TYPE:C3, LT WING L/E RIB AT STA XILD7.095 IS CRACKED AT THE AFT UPPER END. REPAIRED AREA IAW SRM 57-2-2 FIG 2.SDR P2EA99047Rib · crackedSJO - Q-CHECK ITEM. RIB CRACKED IN FRONT SPAR CAVITY FSS 390 (SLAT STATION 144.96). DEFECT SIZE: LENGTH 0.500 INCH. REPLACED LEADING EDGE RIB AT SS 144.96 PER SRM 51-10-1, PAGE 5, AND SRM 51-30-2. SEE COOPESA W.O. M1-0003-5-69, VAM 100 NR 313 FOR TECHNICALSDR P2EA99043Rib · crackedSJO - Q-CHECK ITEM. RIGHT WING, RIB CRACKED AT FRONT SPAR CAVITY AT FSS 479 (SLAT STA 231.84). DEFECT SIZE: LENGTH 0.0250 INCH. SEE COOPESA W.O. M1-0003-6-3, VAM 100 NR 148. (X)SDR P2EA99040Rib · crackedSJO - Q-CHECK ITEM. RIGHT WING, FRONT SPAR RIB CRACKED AT FSS 595 (SLAT STA 387) DEFECT SIZE: LENGTH 0.0375 INCH. REPLACED RIB PER SRM 51-10-1, PAGE 5 AND SRM 51-30-2. SEE COOPESA W.O. M1-0003-6-6, VAM 100 NR 151 FOR TECHNICAL AND PART FABRICATION INFORMATSDR AU990005Rib · cracked(AUS) SMALL CRACKS WERE FOUND IN LEFT WHEELWELL RIB MODIFICATION PLATES. ON CLOSER INSPECTION, BOTH INBOARD AND OUTBOARD PLATES WERE FOUND TO HAVE MORE SERIOUS CRACKS. THE OUTBOARD PLATE HAD ALMOST COMPLETELY LOST STRENGTH. THE INBOARD PLATE HAD TWO MINOR CSDR UPS99828411Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB AT XFS 385.25 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS99828428Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB AT XFS 630 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS99828342Rib · crackedINSPECTION TYPE:C LT WING L/E UPPER RIB CRACKED AT XFS660. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR COMA9810289Rib · bentDURING THE E5 PART A INSPECTION OF ZONE 600, FOUND RIB NR 27 OF THE RIGHT WING TO BE BENT AT THE TRAILING EDGE. RIB WAS STRAIGHTENED AND AREA WAS DYE PENETRANT INSPECTED AND FOUND TO HAVE NO CRACKS. A DOUBLER WAS MADE AND INSTALLED AT THE TRAILING EDGE FOR SSDR 98FDEA00754Rib · crackedBS 760 AT RBL 70.5 RIB UPPER CHORD IS CRACKED. FOUND AT COOL CHECK BY VISUAL INSP. LARGE REPAIR INSTALL IAW SB 727-57-0112.SDR DL72W982589Rib · crackedFOUND DURING MV2/F 1 LETTER CHECK, .75 INCH CRACK AT NR 3 SLAT NOSE RIB O/B SIDE OF ACTUATOR AFT LWR CORNER. REPAIRED PER M/M 57-54-0.SDR VJ9800666Rib · crackedSCHEDULED INSPECTION, LEFT WING LEADING EDGE RIB IS CRACKED AT STA 543 (NR 5 SLAT). REMOVED LEFT WING LEADING EDGE CRACKED RIB, DRILLED, DEBURRED, TREATED, PRIME AND INSTALLED NEW RIB IAW DC9 SRM 51-10-4, 51-10-3, AND 51-30-3.SDR CALA9802147Rib · crackedINSPECTION FOUND A 1.25 INCH CRACK AROUND BOLT HEADS AT UPPER AFT END OF LT WING FIXED LE RIB, WS 330. THE RIB WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-2, PAGE 3, 51-40-3, 51-10-6, PAGE 1, AND 51-10-1, PAGE 1.SDR DL72L982509Rib · crackedREF SHIP 512 TPA LTR CHK D-1 12-07-98, NR 5 L/E SLAT I/B ACTUATOR ATTACH RIB CRACKED. REPAIRED PER MM 57-54-0 AND ERA 366246-14.SDR CALA9802139Rib · crackedINSPECTION FOUND A 1 INCH CRACK ON RIB OF RT WING FIXED LEADING EDGE JUST IN FRONT OF L/E DEVICE NR 5. THE CRACKED AREA OF RIB WAS TRIMMED OUT. THE AREA WAS REINFORCED WITH A DOUBLER IAW SRM 57-00-01, FIGURE 4, 51-21-01, AND 51-33-01.SDR CALA9802138Rib · crackedINSPECTION FOUND A 1 INCH CRACK ON RIB OF FIXED LEADING EDGE RT WING BETWEEN STA XORS 455 AND 506. THE CRACKED AREA OF RIB WAS TRIMMED. THE AREA WAS REINFORCED WITH A DOUBLER IAW SRM 57-00-01, FIGURE 4 AND 51-31-01.SDR 98ZZZX4774Rib · crackedDURING AN ANNUAL INSPECTION, THE TRAILING EDGE RIBS P/N 2522101-1 AND 2522101-2 WERE FOUND CRACKED. THE CRACKS WERE LOCATED IN THE WEB TO FLANGE RADIUS EMANATING FROM THE CUT-OUT FOR THE STRINGER PROGRESSING APPROXIMATELY .50 INCH ALONG THE RADIUS. SUBMITTERSDR 98ZZZX4773Rib · crackedDURING AN ANNUAL INSPECTION, THE TRAILING EDGE RIBS P/N 2522101-1 AND 2522101-2 WERE FOUND CRACKED. THE CRACKS WERE LOCATED IN THE WEB TO FLANGE RADIUS EMANATING FROM THE CUT-OUT FOR THE STRINGER PROGRESSING APPROXIMATELY .50 INCH ALONG THE RADIUS. SUBMITTERSDR 98ZZZX4772Rib · crackedDURING AN ANNUAL INSPECTION, THE TRAILING EDGE RIBS, P/N 2522140-3, AND 2522140-4 WERE FOUND CRACKED. THE CRACKS WERE LOCATED IN THE WEB TO FLANGE RADIUS EMANATING FROM THE CUT-OUT FOR THE STRINGER PROGRESSING APPROXIMATELY .50 INCH ALONG THE RADIUS. SUBMITTSDR 98ZZZX4771Rib · crackedDURING AN ANNUAL INSPECTION, THE TRAILING EDGE RIBS, P/N 2522140-3, AND 2522140-4 WERE FOUND CRACKED. THE CRACKS WERE LOCATED IN THE WEB TO FLANGE RADIUS EMANATING FROM THE CUT-OUT FOR THE STRINGER PROGRESSING APPROXIMATELY .50 INCH ALONG THE RADIUS. SUBMITTSDR AU981572Rib · cracked(AUS) RIGHT WING NOSE RIB LOCATED AT WS 84.00 CRACKED.SDR AU981571Rib · cracked(AUS) LT WING NOSE RIBS LOCATED AT WS 84.00 CRACKED.SDR RRXA98582Rib · misdrilledDURING MAINTENANCE VISIT, FOUND LT WING LEADING EDGE RIB WITH MISDRILLED HOLE AT WS XFS 540. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05589, AREA TREATED IAW DC-8 SRM 51-1-8.SDR P2EA98274Rib · crackedSJO - RIB CRACKED AT RIGHT WING FUEL TANK WBL 135.5, DEFECT SIZE LENGTH 1.125 INCH. REPAIRED RIGHT WING RIB LOWER CHORD AT WBL 135.5, BETWEEN STRINGER 2 AND STRINGER 3 PER BOEING SERVICE BULLETIN 737-57-1186 DATED 4-13-98, SECTION III, PART 3 FIG 3. (M)SDR ARWA981111Rib · crackedC-CHECK, 3.5 INCH CRACK IN RT WING L/E RIB STA XFS 422. STOP DRILLED CRACK, INSTALLED DOUBLER PER SRM 57-2-0 UNDER WORK ORDER NR 1299.SDR ABXA9801124Rib · crackedRIGHT WING OUTBOARD STUB WING LEADING EDGE RIB CRACKED, 7 INCHES FORWARD OF FRONT SPAR AT STATION XS 520.168. REPAIRED IAW DC8 SRM.SDR ABXA9801125Rib · crackedRIGHT WING LEADING EDGE RIB AT STATION XFS 610 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW ABX DWG K05056, DC8 SRM 51-1-8 AND 51-1-20D.SDR ABXA9801122Rib · crackedLEFT WING LEADING EDGE RIB CRACKED AT STATION XS520.168. REPAIRED IAW DC8 51-1-21, 51-1-20D AND DWG 5769523.SDR UPS98828221Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB AT FS 672.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.SDR DL72S982282Rib · crackedDURING SHOP INSPECTION, A REPAIR DOUBLER AT THE I/B AFT RIB WAS FOUND TO BE CRACKED. THE DOUBLER WAS REMOVED AND THE RIB WAS REPAIRED PER MM 57-52-0 FIG 808.SDR UPS98828153Rib · crackedINSPECTION TYPE:C LT WING L/E RIB CRACKED XFS 635.00. REPAIRED IAW SRM 57-2-0.SDR UPS98828152Rib · crackedINSPECTION TYPE:C LT WING L/E RIB CRACKED XFS 722.500. REPAIRED IAW SRM 57-2-0.SDR UPS98828150Rib · crackedINSPECTION TYPE:C LT WING L/E RIB CRACKED XFS 728.750. REPAIRED IAW SRM 57-2-0.SDR UPS98828149Rib · crackedINSPECTION TYPE:C LT WING UPPER L/E RIB CRACKED XFS 610.00. REPAIRED IAW SRM 57-2-0.SDR UPS98828148Rib · crackedINSPECTION TYPE:C LT WING L/E UPPER RIB CRACKED AT XFS 628.75. REPAIRED IAW SRM 57-2-0.SDR UPS98828147Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB CRACKED UPPER XFS 835. REPAIRED IAW SRM 57-2-0.SDR UPS98828145Rib · crackedINSPECTION TYPE-C, L/E RIB CRACKED XFS 772.5 LT WING. REPAIRED IAW SRM 57-2-0.SDR UPS98828141Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB CRACKED XFS 803.750 UPPER. REPAIRED IAW SRM 57-2-0.SDR UPS98828140Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB CRACKED XFS 810 UPPER. REPAIRED IAW SRM 57-2-0.SDR UPS98828139Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB CRACKED XFS 816.250 UPPER. REPAIRED IAW SRM 57-2-0.SDR UPS98828138Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB AT XFS 778.75 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-2-0.SDR UPS98828135Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB AT XFS 616.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS98828134Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB AT XFS 616.25 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED RIB IAW SRM 57-2-0 FIG.SDR UPS98828133Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB AT XFS 622.5 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACKED AND REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR UPS98828132Rib · crackedINSPECTION TYPE-C3, RT WING L/E RIB AT XFS 660.0 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED RIB IAW SRM 57-2-0 FIG 2.SDR ABXA9801152Rib · crackedLEFT WING LEADING EDGE RIB UPPER ARM CRACKED BY AFT FASTENER AT STATION XFS 778.750. REPAIRED IAW ABX DWG K05056.SDR ABXA9801151Rib · crackedLEFT WING LEADING RIB UPPER ARM CRACKED BY AFT FASTENER AT STATION XFS 766.250. REPAIRED IAW ABX DWG K05056.SDR ABXA9801150Rib · crackedRIGHT WING LEADING EDGE RIB STATION 628.75 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-20D.SDR ABXA9801149Rib · crackedRIGHT WING LEADING EDGE RIB STATION XFS 622.5 IS CRACKED AT THE AFT LOWER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-20D.
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