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 UPS99830848Rib · crackedINSPECTION TYPE:C123 LT WING L/E STUB WING RIB AT XS 520.168 IS CRACKED ABOVE THE ELECT CONDUIT. STOP DRILL THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.SDR UPS99830831Rib · crackedINSPECTION TYPE:C123 LT WING L/E RIB AT STA XFS347.75 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS99830802Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT FS 461.372 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.SDR UPS99830801Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT FS 466.651 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.SDR UPS99830776Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT FS 227.335 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.SDR UPS99830775Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT FS 195.0 WAS CRACKED AT THE AFT LWR END. REPAIRED THE RIB IAW SRM 57-2-0.SDR UPS99830768Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 435.789 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS99830767Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS442.185 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS99830764Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 476.897 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS99830763Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT STA XOLDI6.225 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR UPS99830759Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT STA XFS 448.501 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.SDR 20001031SH002Rib · crackedDURING A 100-HOUR INSPECTION INTERVAL, CRACKS WERE FOUND IN THE WING RIBS ADJACENT TO THE LEFT INBOARD AND OUTBOARD AILERON HINGE BEARING ATTACHMENT BRACKETS P/N 105-100011-51. BOTH CRACKS BEGAN AT THE AFT EDGE OF EACH RIB AND PROCEEDED FORWARD TO THE BOTTOM SDR 20001031SH001Rib · crackedDURING A 100-HOUR INSPECTION INTERVAL, CRACKS WERE FOUND IN THE WING RIBS ADJACENT TO THE LEFT INBOARD AND OUTBOARD AILERON HINGE BEARING ATTACHMENT BRACKETS P/N 105-100011-51. BOTH CRACKS BEGAN AT THE AFT EDGE OF EACH RIB AND PROCEEDED FORWARD TO THE BOTTOM SDR UPS99830800Rib · crackedINSPECTION TYPE:C123, RT WING L/E RIBS AT FS 735.0 & 738.75 WERE CRACKED AT THE AFT UPPER ENDS. STOP DRILLED CRACKS AND REPAIRED THE RIBS IAW SRM 57-2-0 FIG 2.SDR UPS99830790Rib · crackedINSPECTION TYPE:C123, RT WING L/E RIBS AT FS 616.25 AND FS 622.5 ARE CRACKED AT THE AFT LWR END. STOP DRILLED THE CRACKS AND REPAIRED THE RIBS IAW SRM 57-2-0 FIG 2.SDR AT9900768Rib · gougedFOUND RIGHT WING 5TH SLAT TRACK WAS CHAFING INTO XRS 241 LEADING EDGE RIB. BLENDED GOUGED AREA, TREATED AND PRIMED. REMOVED AND REPLACED ROLLER BEARING IAW TIMCO EO 99-1294 REV DATED 10/05/99.SDR AT9900762Rib · crackedFOUND RIGHT WING LEADING EDGE HAD TWO CRACKED REPAIR FRAMES/RIBS AT BS 383. FABRICATED AND INSTALLED REPAIR ANGLES/FRAMES/RIBS IAW DC9 SRM 51-30-1, 51-30-2, 51-10-4, 57-22-1, 57-01 FIGURE 3.SDR A6WA9900105Stiffener · crackedLEFT WING UPPER TRAILING EDGE STIFFENER INBOARD OF RIB 9 IS CRACKED AT FORWARD END. REPAIRED LEFT WING UPPER TRAILING EDGE STIFFENER INBOARD OF RIB 9 IAW BAE FAX DJR/RJ0630-98. (M)SDR LR7A9998Rib · crackedDURING SCHEDULED C1 INSPECTION PER SB 382-57-75, FOUND RT RIB FORMER CRACKED AT OWS 293R. REPLACED RIB FORMER IAW SRM 583-57-50-02. DRC 2173.SDR QXEA9901801Rib · crackedPDX - CRACK AT Z STRINGER CUTOUT AT BL 225R AT STRINGER 2.04. REPAIRED IAW HORIZON AIR EA 4-57-303, STEPS 3-6.SDR QXEA9901800Rib · crackedPDX - CRACK AT Z STRINGER CUTOUT AT BL 225R AT STRINGER 2.05. REPAIRED IAW HORIZON AIR EA 4-57-303, STEPS 3-6.SDR RRXA991662Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, WING, LT CENTER L/E UPPER RIB CRACKED AT FASTENER END AT STA XFS 347.75, 354, AND 372.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DCSDR RRXA991463Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LT CENTER L/E UPPER RIB AT FASTENER END, AT STA XFS 347.75, XFS 354, AND XFS 372.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR LT, L/E RIBSDR RRXA991664Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIB AT STA XFS 163.75, CRACKED AT THE AFT LWR END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-0 FIGSDR RRXA991647Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E RIB AT STA XFS 385.25, 17 FWD OF THE SPAR. 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 RRXA991641Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, WING, RIGHT L/E RIB AT STA XFS 163.75, CRACKED AT THE AFT LOWER 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 RRXA991470Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E EDGE RIB AT STA XFS 163.75 AT THE AFT LOWER END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACKED, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DCSDR RRXA991466Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIB, AT STA XFS 163.75, AT THE AFT LOWER 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 RRXA991448Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E RIB AT STA XFS 385.25, 17 FWD OF THE SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57SDR RRXA991447Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING LE RIB AT STA XFS 354 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, FABRICATED AND INSTALLED REPAIR DOUBLER PER DC8 SRM 57-2-SDR RRXA991659Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LT L/E LOWER RIB CRACKED AT FASTENER END AT STA XFS 622.5 AND STA XFS 628.750 FWD OF ACCESS PANEL 519C OPENING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACSDR RRXA991658Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING L/E UPPER RIB AT STA XFS 521.168, CRACKED 6 FWD OF THE SPAR. THE CRACK IS APPROX 2.5 INCHES LONG. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED RIB ANSDR RRXA991655Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LT O/B L/E UPPER RIB CRACKED AT FASTNER END OF STA XFS 585. 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 RRXA991653Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, WING, LEFT, LOWER L/E RIB, CRACKED AT FASTENER END AT STA XFS 653.75 FWD OF ACCESS PANEL 519C OPENING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND RESDR RRXA991652Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIB AT STA XFS 616.25, CRACKED AT THE LWR FASTENER. 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 FIB 2.SDR RRXA991650Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIB AT STA XFS 735.00, CRACKED AT THE AFT LOWER 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 RRXA991649Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIB AT STA XFS 772.5, CRACKED AT THE AFT LOWER 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 RRXA991460Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LT L/E LOWER RIB AT FASTENER END, BETWEEN STA XFS 622.5 AND XFS 628.75 FWD OF ACCESS PANEL 519C OPENING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK AND RSDR RRXA991459Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING L/E UPPER RIB AT STA XFS 521.168, 6 FWD OF THE SPAR. THE CRACK APPROXIMATELY 25 INCHES LONG. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED RIB AND REPAIRSDR RRXA991456Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LT OBD L/E UPPER RIB AT FASTENER END AT STA XFS 585. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2SDR RRXA991454Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LT WING LOWER L/E RIB AT FASTENER END AT STA XFS 653.75, FWD OF ACCESS PANEL 519C OPENING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSSDR RRXA991453Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E RIB AT STA XFS 616.25 AT THE LWR FASTENER. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 5SDR RRXA991451Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E RIB AT STA XFS 735.0 AT THE AFT LWR END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-SDR RRXA991450Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RT WING, L/E RIB AT STA XFS 772.5 AT THE AFT LWR END. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACKED, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM SDR UPS99830409Rib · crackedINSPECTION TYPE:C234, RT WING L/E RIB AT XFS 640 WAS CRACKED AT THE AFT LWR FASTENER. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.SDR UPS99830393Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XFS 316.5 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.SDR UPS99830391Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XFS 366.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0.SDR DLL19991828Rib · crackedLT AND RT WING UPPER RIB CAP AT IWS 555 FOUND CRACKED DURING ROUTINE INSPECTION ERA 333431-14 REV B.SDR AT9900761Rib · crackedFOUND RIGHT WING LEADING EDGE HAD THREE CRACKED REPAIR FRAMES/RIBS AT BS 445. REMOVED, FABRICATED AND INSTALLED REPAIR ANGLES IAW DC9 SRM 51-30-5, 57-01 FIGURE 3.SDR UPS99830385Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XS 478.897 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.
Back to JASC 5712