JASC 5730
Service difficulty reports · 27,269
Reports filed under 5730 · Wing, Plate/Skin, 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 = '5730' 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 = '5730' 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 VTZA200500206Skin · crackedLEFT WING PLANK AT FS 148.019 IS CRACKED AT 1 INCH IN LENGTH.SDR CA051012005Skin · debondedFOUND LT AND RT WING DISBONDING OF THE UPPER WING SKIN, INBOARD AND OUTBOARD OF NACELLES FROM YW 60 TP YW 150. BOMBARDIER IS IN THE PROCESS OF ISSUING A SB TO COVER INSPECTION OF THE UPPER WING SKINS. DARK AREAS ON THE SKETCHES INDICATE DISBONDING. MODEL P/SDR 05FDEA03231Access Panel · crackedACCESS PANEL LT WING 516ET FOUND 2 CRACK ON ANGLE INTERNAL SKIN. REMOVED EXISTING REPAIR AND REPAIR STIFFENERS IAW SRM 51-35-01 PAG 1-13 AND 51-33- 01 PAGE 34-47 AND SRM 57-10-00 FIG 23 VOL I.SDR CA051003001Screw · damaged(CAN) AFTER LANDING, AFTER THE AIRCRAFT WAS REFUELED, FUEL WAS OBSERVED COMING FROM THE RIGHT WING FORWARD OF THE IB FLAP TRACK. THE FUEL ACCESS PANEL DIRECTLY AFT OF THE RT WING NACELLE WAS FOUND LEAKING. ON INVESTIGATION SEVERAL SCREWS WERE FOUND TO BE STRSDR 2005FA0001447Skin · wrinkledDURING ANNUAL INSPECTION NOTED WING ROOTS, BOTH LT AND RT WRINKLED. AREA OF DEFECT IS FORWARD OF MAIN CARRY THRU SPAR. A SERIES OF 3 WAVES EXTENDING APPROXIMATELY 6-8 INCHES LONG. PROBABLE CAUSE: SEVERE TURBULENCE OR OVER CONTROL OF AIRCRAFT EXCEEDING (G) LSDR 05FDEA03169Panel · damagedRIGHT WING LOWER LEADING EDGE PANEL NR 6212 REQUIRES FABRICATION FOR REPLACEMENT ON-N00505. FABRICATED NEW PANEL IAW BAC DRAWING 65-21661. ALODINED, PRIMED AND PAINTED NEW PANEL IAW FED-EX SRDM SR-57-005B.SDR 05FDEA03168Panel · erodedRIGHT WING LEADING EDGE PANEL NR 6541 ERRODED. FABRICATED NEW PANEL IAW BAC DRAWING 65-21675. ALODINED, PRIMED AND PAINTED IAW B727 SRM 51-10-2.SDR 05FDEA03167Panel · damagedRIGHT WING LOWER LEADING EDGE PANEL NR 6539 REQUIRES FABRICATION FOR REPLACEMENT ON N00158. FABRICATED NEW PANEL IAW BAC DRAWING 65-21674. ALODINED, PRIMED, AND PAINTED IAW B727 SRM 51-10-2.SDR 05FDEA03166Panel · wornRIGHT WING LEADING EDGE FIBERGLASS PANEL NR 6212, BADLY WORN AROUND EDGE. FABRICATED NEW PANEL IAW BAC DRAWING 65-21674. ALODINED, PRIMED AND PAINTED IAW B727 SRM 51-10-2.SDR IXXA05SMN222SSkin · crackedDURING C CHECK INSPECTION, NR 3 RT STUB WING LWR SKIN CRACK 2 AT STA XW 255.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 37, EO SEMAN NR 20051284 DATED 09-27-05. REMOVED FASTENERS IAW DC8 SRM 51-1-20D. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FSDR IXXA05SMN221SSkin · crackedDURING C CHECK INSPECT, LT WING LWR SKIN CRACK AT STA XRS 172.000 BETWEEN S-56 AND S-57. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 1, EO SEMAN # 20051287 DATED 09-29-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. STOP DRILLED CRACK END IAW SDR IXXA05SMN220SSkin · scratchedDURING ROUTINE C CHECK INSPECTION, EXTERNAL FUS. (C) BELLY PIT DOOR SKIN SCRATCHES OUT OF LIMITS. PERFORMED MAJOR REPAIR, REMOVED FASTENERS IAW SRM 51-1-20D. REMOVED DAMAGED SECTION IAW DWG NR ED-4075. NDT INSPECTED IAW NDT SPM PART 06-10-01-001. NEITHERSDR IXXA05SMN210SSkin · corrodedDURING C CHECK INSPECTION, RT OUTER WING INBD L/E UPPER SKIN CORRODED, STA XFS 710.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05461 DATED 10-10-05, SEMAN DWG # ED-4070 DATED 10-07-05, EO SEMAN # 20051276 DATED 10-10-05. REMOVED FASTENERS IAW DC8 SRM SDR IXXA05SMN209SSkin · crackedDURING ROUTINE C CHECK INSPECTION, RT OUTER WING IB L/E LOWER SKIN, .2500 IN CRACK, STA XFS 597.500. PERFORMED MAJOR REPAIR DATED 10-07-05, DWG NR ED-4069 DATED 10-06-05, EO NR 20051275 DATED 10-07-05. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. PERFORMESDR IXXA05SMN206SSkin · corrodedDURING C CHECK INSPECT, LT WING CTR UPPER L/E CORRODED, STA XFS 304 310.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 44, EO SEMAN # 20051213 DATED 09-22-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OSDR IXXA05SMN205SSkin · crackedDURING C CHECK INSPECT, LT WING CTR L/E SKIN CRACKED ½, STA XFS 285.250. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05451 DATED 10-07-05, SEMAN DWG # ED-4066 DATED 10-03-05, EO SEMAN # 20051212 DATED 10-07-05. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRMSDR IXXA05SMN200SVane · elongatedDURING C CHECK INSPECT, LT WING OTBD SLOT VANE HOLES ELONGATED, STA XS 520.168. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05447 DATED 10-05-05, SEMAN DWG # ED-4064 DATED 09-30-05, EO SEMAN # 20051206. REMOVED FASTENERS IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0SDR A6WA200540310Access Door · corrodedRT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT PANEL 650 GB WING STA 274.319 HAS MINOR CORROSION .006 INCH DEEP AND 2 INCH LONG. MAINTENANCE REMOVED MINOR CORROSION IAW REO. MATERIAL REMOVED WAS LESS THAN .010 INCH IAW REINSPECT IS DUE OF HOLE NR 14 AT 386SDR 05FDEA03139Panel · damagedLEFT WING LOWER PANEL NR 6249 REQUIRES FABRICATION FOR REPLACEMENT ON FED, EX NON-ROUTINE N00517. FABRICATED NEW PANEL IAW BAC DRAWING 65-21675-5, ALODINED, PRIMED AND PAINTED IAW B727 SRM 51-10-2.SDR IXXA05RNG117SSkin · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION AND BONDED DOUBLERS IN LT OB AILERON UPPER INNER SKIN, STA XA 621 TO XA 724. UPPER SKIN IN LT OB AILERON WAS FABRICATED AND INSTALLED IAW MFG DRAWING 5763133, AND RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7.SDR USAA051149Skin · crackedLT WING SKIN FWD OF FRONT SPAR O/B SIDE OF PYLON. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR PIECES, DEFECT SIZE: 1".SDR QXEA200501322Panel · chafedPDX: LEADING EDGE PANEL 512AL HAS CHAFE ON INBOARD WEB. MAINTENANCE BLENDED CHAFE MARK ON WEB IAW Q400 SRM 51-14-00 TO REMOVE DAMAGE. HFEC INSPECTED BLENDED AREA FOR CRACKS IAW Q400 PART 6, 51-00-01. NO CRACKS NOTED. COMPLIED WITH STEPS 4-6 OF EA 6-57-378.SDR 05FDEA03111Skin · damagedRIGHT WING UPPER SURFACE AFT OF NR 7 SLAT, 2 EACH LOCKBOLT HEAD FOUND FUEL LEAK, SKIN PLANK FOUND TO HAVE AN ELONGATED BORE. CARRIED OUT REPAIR AS PER FEDEX EA 1-5710-90018.SDR 05FDEA03110Access Panel · damagedRIGHT WING, LOWER FUEL TANK PANEL 638CB CUTOUT FASTENER HOLE FOUND ELONGATED. REPAIRED AS PER FEDEX EA 1-5710-90029.SDR 05FDEA03109Access Panel · damagedLEFT WING, UPPER FUEL TANK ACCESS PANEL 534BT CUTOUT FASTENER HOLE FOUND ELONGATED. REPAIRED AS PER FEDEX E.A. 1-5710-90037.SDR IXXA05RNG110SSkin · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION AND BONDED DOUBLER DELAMINATED ON LT WING INTERIOR UPPER SURFACE T/E, STA XW 700 - XW 736.500.SKIN WAS REPLACED IAW MFG DRAWING 5644654, RIVETS WERE INSTALLED IAW SRM 51-1-21 PAGE 1-7 AND ANTI-CORROSIVE TREATMENT WSDR 05FDEA03088Skin · dentedRT WING L/E HAS DENT ABOVE NR 3 FLAP TRACK. REMOVED DAMAGE, FABED REPAIR PARTS, TREATED AND PRIMED, INSTALLED REPAIR PARTS IAW SRM 57-53-12, 51-21-10, AND 51-40-2.SDR IXXA05SMN199SSkin · crackedDURING C CHECK INSPECTION, RT WING OTBD L/E LOWER SKIN CRACKED 1” APPROX, BETWEEN STA XFS 710.000 AND XFS 716.250. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05461 DATED 10-05-05, SEMAN DWG # ED-4071 DATED 10-06-05, EO SEMAN # 20051277 DATED 10-05-05. REMOSDR IXXA05SMN198SSkin · crackedDURING C CHECK INSPECT, RT WING CTR L/E LOWER SKIN CRACKED 1” APPROX, BETWEEN STA XFS 335.250 AND XFS 340.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05463 DATED 10-11-05, SEMAN DWG NR ED-4067 DATED 10-11-05, EO SEMAN NR 20051227 DATED 10-11-05. REMOVSDR IXXA05SMN197SSkin · crackedDURING C CHECK INSPECTION, RT WING OTBD L/E LOWER SKIN CRACKED 1” APPROX, BETWEEN STA XFS 566.250 AND XFS 572.500. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 # 05446 DATED 10-05-05, SEMAN DWG # ED-4068 DATED 09-27-05, EO SEMAN # 20051231 DATED 10-05-05. REMOSDR USAA051143Skin · crackedFOUND LT WING SKIN CRACKED, FWD OF FRONT SPAR O/B SIDE OF PYLON. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR PIECES IAW TR 57-41-023.SDR 2005FA0001405Skin · crackedWING WALK STIFFENER PANEL CRACKED UNDER UPPER WING SKIN, YEARS OF WALKING ON PANEL. STIFFENER PANEL SHOULD BE HEAVER GAUGE METAL. (K)SDR 0509020Door · delaminatedLT WING, TRAILING EDGE, BUTE DOOR P/N 5919572-1, UPPER SKIN DELAMINATED AT STATION XRS 260 AND SKIN WORN OUT AT STATION XRS 153.SDR 0509005Panel · delaminatedRT WING FIXED PANEL P/N: 65-50818-316, DELAMINATED AT WS 465.SDR QXEA200501314Skin · chafedYYC - RIGHT WING LEADING EDGE SKIN AT WING STATION 108 CHAFED. REMOVED DAMAGE IAW CRJ-700 SRM 51-12-00-001-001-A01, MATERIAL REMOVED .004". RESTORED FINISH.SDR QXEA200501308Skin · damagedYYC - RIGHT WING UPPER SKIN TRAILING EDGE INBOARD OF MULTI FUNCTION SPOILERS HAS A LOOSE FASTENER. INSTALLED RIVETS IAW CRJ-700 SRM 51-42-06-001-001-A01.SDR QXEA200501301Skin · damagedYYC - LEFT WING UPPER SKIN TRAILING EDGE JUST INBOARD OF THE MULTI-FUNCTION SPOILERS HAS LOOSE FASTENERS. REPLACED RIVETS IAW CRJ-700 SRM 51-42-06-001-001-A01.SDR IXXA05RNG065SSkin · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION ON UPPER SKIN AT LEADING EDGE STA XW 408 TO 454, LT.CORROSION ON UPPER SKIN AT LEADING EDGE STA XW 408 TO 454-LT WAS REPAIRED IAW SRM 57-2-1 FIGURE 38 AND EWO ATI 57-043.SDR IXXA05RNG106SSkin · corrodedDURING INSPECTION CHECK, FOUND TWO IMPROPER PATCHES AND CORROSION ON RT WING INBOARD FLAP TOP SURFACE, STA XW 31 - XW 92. SKIN ON RT WING INBOARD FLAP WAS REPLACED IAW DOUGLAS DRAWING 5642960 AND RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGE 1-7.SDR IXXA05RNG104SSkin · corrodedDURING INSPECTION CHECK, FOUND A CORROSION ON LT WING OUTBOARD AILERON LWD SKIN, STA XW 565 TO XA 638. SKIN IN LT WING OUTBOARD AILERON WAS REMOVED AND REPLACED IAW DRAWING 5763133 AND RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGE 1-7.SDR 09122005ESkin · bird strikeBIRD STRIKE ON LEFT INBOARD LEADING EDGE. REMOVED AND REPLACED LEADING EDGE, ONLY WAITING ON A BOOT.SDR IXXA05RNG073SSkin · misrepairedDURING INSPECTION CHECK WAS FOUND A IMPROPER REPAIR ON WING LEADING EDGE, STA XW 257.50, RT. PERMANENT REPAIR WAS PERFORMED IAW EWO ATI 57-044 AND EO ATI-090905. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.SDR IXXA05RNG101SSkin · unbondedDURING INSPECTION CHECK, FOUND LT WING UPPER SKIN PANEL AT STA XW 761.695 DISBONDED. SKIN WAS REMOVED AND REPLACED ON LT WING UPPER PANEL IAW DOUGLAS DRAWING 5644654, RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGE 1-7 AND PROTECTIVE TREATMENT WAS APPLIED IAW SDR DL757050525Skin · wornWEAR DAMAGE WAS FOUND ON THE LEFT HAND SIDE LOWER WING SKIN CAUSED BY CONTACT WITH THE WING-TO-BODY FAIRING SKIN. THE DAMAGE WAS REPAIRED BY ACTS IN VANCOUVER PER ACTS PP B757-57-21136.SDR IXXA05RNG103SSkin · corrodedDURING INSPECTION CHECK, FOUND A CORROSION ON LT WING EXTERIOR LWD SURFACE, REAR SPAR BETWEEN STA XW 736.500 - XW 761.0 AND STA XRS 700.000 - XW 736.000. SKIN WAS REMOVED AND REPLACED IAW DOUGLAS DRAWING 5644654, RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGESDR IXXA05RNG054SSkin · crackedDURING INSPECTION CHECK, FOUND A CRACK (1.5 INCHES) ON TOP PANEL PLATING OUTBOARD OF STA XCW 69.5 AND STRINGER 1 RT. DAMAGE WILL BE REPAIRED IAW EWO ATI 57-039 AND SRM 57-2-1 FIG 18A.SDR IXXA05RNG068SSkin · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION ON WING UPPER SKIN STA XRS 40.869 REAR SPAR TO AUX SPAR - LT. REPORTED AREA WAS BLENDED OUT AND REINFORCEMENT DOUBLER WAS FABRICATED AND INSTALLED IAW EO ATI-091005 AND EWO ATI 57-045. FAA FORM 8110-3 WAS ISSUED ASDR IXXA05RNG057SSkin · crackedDURING INSPECTION CHECK, FOUND A CRACK ON TOP PANEL PLATING AT CENTER SPAR AND STA XRS 74.869 LT. DAMAGE WILL BE REPAIRED IAW EWO ATI 57-040 AND SRM 57-2-1 FIG 17.SDR IXXA05RNG052SSkin · corrodedDURING INSPECTION CHECK, FOUND STRESS CORROSION CRACK ON RT WING UPPER EXTERIOR SURFACE STA XRS74 STRINGERS 9 TO 15. DAMAGE WILL BE REPAIRED IAW EWO ATI 57-038 AND FAA FORM 8110-3 MUST BE ISSUED APPROVING THIS REPAIR.SDR 05FDEA02751Skin · crackedCRACK INDICATIONS ON NR 5 BORE HOLES FOUND DURING HFEC INSPECTION AT LEFT HAND WING LOWER SKIN DOOR CUTOUT OF PANEL 536AB. FOUND HOLES CRACK LENGTH APPROXIMATELY 0.100", 1 HOLE CRACK LENGTH APPROXIMATELY 0.187" ON BORE SURFACE. REPAIR CARRIED OUT AS PER FEDE
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