JASC 5414
Service difficulty reports · 4,361
Reports filed under 5414 · Nacelle/Pylon, 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 = '5414' 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 = '5414' 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 EIAA20120402028Skin · damagedNR 3 PYLON SKIN CAP DOUBLER MOST AFT I/B FASTENER HOLE HAS DEFECT. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-54-023-2.SDR EIAA20120330027Skin · damagedNR 2 PYLON SKIN CAP DOUBLER AFT I/B FASTENER HOLE HAS DEFECT. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-54-024-2.SDR EIAA20120327024Skin · crackedNR 4 PYLON I/B SIDE CRACK IN SKIN OF ACCESS CUT OUT, FWD UPPER CORNER NAC273. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-54-019-2.SDR EIAA20120326016Skin · chafedNR 4 PYLON CAP SKIN O/B SIDE NAC STA 258 HAS CHAFE. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 54-31-03 FIG 2 SHEET 1-4 AND ENG DISPOSITION 17.SDR EIAA20120326015Skin · chafedNR 4 PYLON CAP SKIN I/B SIDE NAC STA 258 HAS CHAFE. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 54-31-03 FIG 2 SHEET 1-4 AND ENG DISPOSITION NR 16.SDR FDEA201203251095Panel · missingDURING WALKAROUND, FOUND NR 3 PYLON MISSING PIE SHAPED PANEL AFT OF ENGINE PYLON. REPLACED SUPPORT ANGLE AUB7036-4 USING SRM. FINAL CLOSED.SDR FDEA201203140946Skin · corrodedLT PYLON ACCESS THRU PANEL 433AL HAS CORROSION IN BETWEEN CUT-OUT AND SKIN. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMIT OF REMOVAL, REMOVED .017, ORIGINAL .090, REMAINING .063, OUT OF LIMITS IAW SRM 54-50-01, FIG 101, DETAIL V. LOCATED, DRILLED ANSDR FDEA201203140945Skin · corrodedLEFT PYLON CORROSION ON PANEL 433GR CUT-OUT. REMOVED CORROSION IAW SRM 51-10-02. MATERIAL LOSS OUT OF LIMITS IAW SRM 54-50-01, FIG 101, DETAIL 5. INSTALLED NEW FWD RT SKIN IAW SRM 51-40-02 AND BAC DWG 311N5002. MAJOR REPAIRSDR FDEA201203140944Skin · corrodedNR 2 PYLON LT DOOR 443GL CUT-OUT HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01, PG 103, FIG 101. REMOVED INBD FWD SKIN IAW SRM 51-40-02. LOCATED,DRILLED AND COUNTERSUNK NEW SKIN IAW SRM 51-40-02 AND DWG 311N5002. INSTALLEDSDR FDEA201203140943Skin · corrodedNR 2 PYLON RT PANEL 443 AR CUT OUT HAS CORROSION SPOTS.SDR FDEA201203130928Skin · corrodedLEFT PYLON, LT SIDE THRU ACCESS PANEL, NR 433BL, CORROSION ON INTERNAL SKIN. REMOVED CORROSION IAW SRM 51-10-02. MATERIAL LOSS .023, ORIGINAL .090, REMAINING .067, OUT OF LIMITS OF SRM 54-50-01, FIG 101, DETAIL V. LOCATED, DRILLED AND COUNTERSUNK NEW SKINSDR FDEA201203130927Skin · corrodedNR 2 PYLON LT SKIN HAS CORROSION SPOTS ON P-STA 128-136. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 54-50-01, FIG 101, DETAIL V. INSTALLED NEW SKIN IAW SRM 51-40-02 AND DWG 311N5002. MAJOR REPAIR.SDR FDEA201203130925Panel · damagedNR 1 PYLON DOOR CUTOUT FOR DOOR PANEL 433LR HAS MISSING MATERIAL IN UPPER AFT CORNER. REPAIRED IAW EA F-5450-157272.SDR FDEA201203130919Panel · corrodedNR 2 PYLON CUTOUT FOR PANEL 443LL HAS CORROSION IN UPPER AFT CORNER. COMPLIED WITH EA F-5450-159901, CAT."A" MAJOR REPAIR.SDR FDEA201203130918Skin · misrepairedNR 2 PYLON OTBD SKIN HAS AN EXISTING REPAIR THAT EXCEEDS LIMITS OF SB 757-54-0022. R & R NR 2 PYLON OTBD SKIN IAW EA F-5450-159905. MAJOR REPAIR.SDR DALA1214880180Skin · damagedNR 1 & 2 PYLON UNDERWING SKIRT BEAM HAS COUNTERSUNK FASTENER HOLES THAT ARE OVERSIZE. WORKING FROM A PRI (NRC 52506).SDR FDEA201203100874Skin · corrodedNR 2 PYLON RT INTERNAL SKIN, PP STA144-153, CORRODED. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS AND FOUND OUT OF LIMITS IAW SRM 54-50-01, FIG 101, DETAIL IV. REMOVED AND INSTALLED NEW RT SIDE SKIN IAW SRM 51-40-02 AND DWG 311N5002.SDR KCSA201203091029Skin · crackedNR 3 PYLON CAP SKIN HAS A CRACK INDICATION IN THE AFT CENTER HOLE OF THE SPAR CHORD AT NAC STA 221.9.SDR KCSA201203091028Skin · crackedNR 2 PYLON CAP SKIN HAS A CRACK INDICATION IN THE AFT CENTER O/B HOLE OF THE SPAR CHORD AT NAC STA 221.9SDR KCSA201203091027Skin · crackedNR 1 PYLON CAP SKIN HAS CRACK INDICATIONS IN THE TWO CENTER AFT HOLES OF THE SPAR CHORD AT NAC STA 221.9SDR V0XR201203090005Skin · damagedLEFT NACELLE FWD/OTBD CORNER CUT OUT FOR MLG DOOR DAMAGED. REPAIRED DAMAGE ON FWD/OTBD CORNER MLG DOOR CUT OUT ON LT NACELLE IAW RD 8-54-874, PERMANENT REPAIR FOR CRACK DAMAGE AT FWD UPPER CORNERS OF MLG DOOR OPENING.SDR HNAA2012030700663Skin · crackedUPPER INBD SIDE SKIN IS CRACKED 1 INCH FORWARD OF NR1 NACELLE FRONT WING SPAR, LOWER FLANGE. REMOVED RIVETS AT CRACK LOCATION, FOR FURTHER INSPECTION. COMPLIED WITH DYE PEN INSPECTION IAW RD8-54-1557. NO CRACKS FOUND. REPAIRED DAMAGE IAW EO8-54-12-0077 ANDSDR EIAA20120306012Skin · chafedNR 4 PLYON CAP SKIN I/B SIDE AT NAC 258 HAS CHAFING. REMOVED DAMAGED SECTION OF CAP SKIN, FABBED REPAIR PARTS AND INSTALLED PER EMC ENGINEERING DISPOSITION 3823 AND B747 SRM 54-31-03 PG 2 SHEET 1-4.SDR EE4Y201203050104Skin · corrodedENGINE, PYLON AFT LOWER SECTION INBD AND OTBD SKIN WITH CORROSION. REPLACED NR 2 ENGINE PYLON AFT LOWER OUTBD SKIN PANEL IAW SRM 54-54-11 PB 101 PARAG 4B DIAGRAM 101 TABLE A.SDR HNAA2012030200642Skin · corrodedON FINGERNAIL OF LT NACELLE, AFT SKINS ON BOTH SIDE HAS SURFACE CORROSION. BLENDED CORROSION ON BOTH SIDES OF LT NACELLE TO WITHIN LIMITS IAW SRM 54-00-16.SDR UIEA2012042000151Skin · damagedNR 1 CORE COWL SCRATCH. REPAIRED IAW SRM 54-45-01-2R-1, REPAIR 1.)SDR KCSA201202271022Skin · crackedNR 3 PYLON I/B SIDE LOWER SKIN HAS 2 INCH CRACK AT NAC STA 230.SDR USAA2012022900008Skin Panel · crackedC4 CHECK - .250 INCH CRACK IN RIGHT PYLON ACCESS DOOR 5828R FRAME WORK FLANGE AT NAC STA 213.0 APPROX 1.25 INCHES FROM OUTBOARD EDGE. REPAIRED RIGHT PYLON ACCESS DOOR 5828R FRAME WORK FLANGE IAW EA # 103647 & TR737-5430-10-0054.SDR A6WA201240363Skin · damagedRT UPPER CORE COWL HAS SCRATCHES ON OUTER SKIN. REPAIRED RT UPPER CORE COWL OUTER SKIN ON OTBD SIDE IAW CMM 71-12-01, REPAIR SRS 021.SDR KCSA201202141005Skin · crackedNR 2 PYLON SKIN HAS A POSSIBLE CRACK ON O/B SIDE APPROX NAC STA 182 NEAR PYLON SKIRT.SDR ERAA201200027Skin · crackedLT NACELLE OUTBD NACELLE SKIN CRACKED AT STA ZN 0-00 AND ZN 130.00. REPLACED SKIN.SDR FDEA201202130568Skin · gougedDEEP GOUGE MARK ON LT UPPER SKIN OF NR 2 PYLON FAN COWL BEAM. REMOVED TOP SKIN IAW SRM 51-40-02. FABRICATED NEW SKIN IAW SRM 54-51-01 FIG 101. TREATED AND PRIMED IAW SRM 51-21-01. LOCATED AND DRILLED IAW SRM 51-40-05 AND INSTALLED IAW SRM 51-40-02. MAJOR RESDR A6WA201240364Skin · chafedRT LOWER CORE COWL OUTER SKIN CHAFED FROM BLOCKER DOOR. COMPLIED WITH CMM REPAIR SRS 104C.SDR A6WA201240365Skin · chafedLT LOWER CORE COWL OUTER SKIN CHAFED FROM LOCKER DOOR COMPLIED WITH CMM. REPAIR SRS 104428.SDR DALA1207415642Skin · crackedDURING HEAVY CHECK MAINTENANCE FOUND NR 1 PYLON RIGHT SKIN AT 433AR ACCESS PANEL CRACKED BEYOND LIMITS. ENGINEERING CURRENTLY DRAFT ERA FOR REPAIR. PERMANENT REPAIR CARRIED OUT IAW DELTA ROUTINE CARD 5451-01010-02B.SDR FDEA201202080517Panel · corrodedRT PYLON NOSE COWL FAIRING PANEL 421AL BOTTOM SURFACE CORROSION AROUND SCREW HOLE APP. L=2",W=1.5". REMOVED CORROSION ON ARCH PANEL 421AL NR 2 ENGINE PYLON IAW SRM 51-74-10, PG. 205 PAR.3, CHECKED LIMITS FOUND TO BE BEYOND LIMITS IAW SRM 54-50-00, PG 111 PSDR EE4Y201202060025Skin · corrodedNR 2 ENGINE PYLON AFT LOWER SECTION, INBD AND OTBD SKIN FAIRING WITH CORROSION. THE DAMAGED PARTS WERE REPLACED IAW SRM 51-72-11, PARA 4 AND 6.SDR EE4Y201202060024Skin · corrodedNR 1 ENGINE PYLON AFT LOWER SECTION, INBD AND OTBD SKINS FAIRING WITH CORROSION. THE DAMAGED SKIN WAS REPLACED IAW SRM 51-72-11, PARA 4 AND 6.SDR EE4Y201202060022Skin · corrodedDURING INSPECTION, FOUND CORROSION AT THE ENGINE NR 2 PYLON AFT FAIRING INBD SKIN PANEL. REPLACED SKIN PANEL IAW SRM 51-72-11.SDR ABXR2012020400025Skin · crackedDURING INSPECTION, FOUND NR2 PYLON ACCESS PANEL 446AL FLANGE CRACKED AT NUTPLATE HOLE. REPAIRED PANEL ATTACH FLANGE IAW REA B654-59629.SDR UALA2012020300681Panel · wornLEFT ENGINE, OUTBOARD PYLON PANEL 436AL HAS FASTENER HOLE WORN OUT FASTENER JUST FALLS THROUGH. ROUND SMALL PANEL WITH 4 FASTENERS. REMOVED PANEL AND PLACED IN LOB. PARTS: 160-8839 311T3065-159 (DOOR ASSY) REPLACED OLD PANEL WITH NEW PANEL. SECURED ON PYSDR KCSA121011Skin · crackedSKIN CRACKED IN AREA OF CAP SKIN DOUBLER NR 2 PYLON.SDR A6WA201240302Skin · crackedA CRACK IN RT (FWD) CORE COWL DOOR OUTER SKIN. REMOVED DAMAGE FROM OUTER SKIN. FABRICATED DOUBLER AND SPIGOT IAW REO 601R-71-12-4095 AND CMM 71-12-01. REPAIR SRS118.SDR AALA20120128AFW01Skin · crackedPYLON HAS VISUAL CRACK INDICATIONS IN THE UPPER PYLON SKIN AT THE GENERATOR CABLE FEED THRU LOCATION. INSTALLED DOUBLER REPAIR PER AARD 54-52-01-1.SDR GLBA20120124GSkin · damagedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND THE RT INBD NACELLE SKIN, JUST ABOVE FWD EDGE OF GEAR DOOR CUTOUT, FASTENERS PULLED THROUGH SKIN.SDR GLBA20120124FSkin · damagedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND THE RT OTBD NACELLE SKIN FASTENERS AT FRAME 10, FS 1744 BETWEEN STRINGER 3 AND 6 PULLING THROUGH SKIN.SDR UALA2012011800375Latch · faultyINBD LATCH ON FWD STRUT PANEL 441BT ON NR 2 ENG BROKEN. REPLACED INBD LATCH, PANEL CLOSE AND SECURE, SUGGEST REPLACING CLEVIS ASSY 160-8050, AND LUG ASS 313T3100-56 IPC 54-52-01-005 ITEM 300. PANEL SPEED TAPED PRECAUTIONARY CONT OF AMIS ITEM 1262005 CLOSED ANSDR UALA2012011600311Doubler · crackedNR 1 PYLON, PREVIOUS REPAIR ANGLE DOUBLER IS CRACKED AT INBOARD SIDE. REMOVED NR 1 PYLON MIDSPAR CLOSEOUT ANGLE PREVIOUS REPAIR ANGLE DOUBLER-TRIPLER. FABRICATED A REPAIR SPLICE AND STRUCTURAL FILLER AND INSTALLED PER REO G13357, REV A AND UAL EVA 73769 ON NSDR FDEA201201060029Skin · crackedPANEL RACK NR 2 PYLON BULL NOSE PANEL CRACKED AT AFT END, BY RUB SEAL. REMOVED SKIN IAW SRM 51-40-02. FABRICATED NEW SKIN IAW EA F-5710-156984. INSTALLED NEW SKIN IAW SRM 51-40-02 AND DWG 114N1802. MAJOR REPAIR.SDR 2012FA0000059Angle · crackedDURING A SCHEDULED INSPECTION, A CRACK WAS FOUND IN THE NACELLE ANGLE. UPON FURTHER INVESTIGATION, IT WAS FOUND THAT THE CRACK WAS BETWEEN THE 2 RIVETS THAT EXTENDED THRU THE WING SKIN INTO CAP (P/N 67097-002 OR -003 DEPENDENT ON SIDE) WHICH IS ATTACHED TO A
Back to JASC 5414