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 NWAA081855642Skin · crackedDURING ENGINE CHANGE, FOUND CRACK IN NR 2 PYLON SKIN AT ACCESS HOLE OUTBOARD SIDE NEAR THRUST REVERSER CENTER HINGE POINT. REPAIRED PER EA 55-212947.SDR 08FDEA01464Panel · corrodedPYLON NR 1 SKIN CUTOUT AT ACCESS PANEL 433AL FOUND CORROSION. TO EVALUATE AND RECTIFY, REPLACED SKIN CUTOUT OF ACCESS PANEL IAW SRM 51-10-02 AND DRAWING 311N5002. REPAIRED CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.SDR NWAA081845532Skin · crackedDURING "M" CHECK, FOUND CRACK IN NR 2 PYLON SKIN AT NAC STA 132 RT. REPAIRED PER EA 56-212921.SDR 2010FA0000378Skin · cracked(KADY) CRACK WAS FOUND ON THE NR 2 ENG RT SIDE COWL UPPER SKIN AT NAC STA 226.95-236.85.SDR 2010FA0000376Skin · debonded(KADY) DISBONDED INNER DOUBLER WAS FOUND ON THE NR 1 LT SIDE COWL SKIN AT NAC STA 192.05-204.55, NAC WL 100-110.SDR 2010FA0000375Skin · damaged(KADY) A BENT DAMAGE WAS FOUND ON THE NR 1 RT SIDE COWL SKIN AT NAS STA 155.61, NAC WL100.SDR 2008UALA02039Skin · crackedNR 2 PYLON UPPER WEB FUEL LINE CUTOUT SKIN CRACKED AT NAC STA 178. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR, ACCOMPLISHED REMOVED EXISTING REPAIR DOUBLER FROM NAC STA 172 TO 178. STOP DRILLED CRACK AND ACCMP'D HFEC TO VERIFY DAMAGE REMOVED. FABRICATED AND INSTSDR 08FDEA01325Skin · crackedCRACKS FOUND ON PYLON NR 2 AFT FAIRING FWD SKIN PANEL REPAIR PERFORMED BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER IAW, RAS/ROHR/0162/2008 , APPROVED BY EA 6-5455-115264.SDR 2008UALA01955Skin · crackedRT WING TO NR 4 PYLON ATTACH AREA "D" L/E NOSE INTERNAL SKIN CRACKED (5") AND UPPER AND LOWER CHORD CRACKED.SDR 2010FA0000374Skin · worn(KADY) WORN DAMAGE WAS FOUND ON THE CAP SKIN OF THE NR 1 PYLON. THE DAMAGED CAP SKIN IS REPAIRED IAW SRM.SDR 08FDEA01175Panel · chafedNR 3 PYLON LT TOP PANELS 487CL & 487 BL INTERIOR IS CHAFED. BLENDED DISCREPANT AREAS ON THE NR 3 PYLON PANEL 487 CL WHERE CHAFING WAS PRESENT IAW SRM 54-00-01. CHECKED LIMITS IN DISCREPANT AREA IAW THE FOLLOWING SRMS 54-00-01 VOL I & 54-31-02 VOL III. ORIGSDR 08FDEA01150Panel · corrodedNR 2 PYLON PANEL NR 424 ER IS CORRODED ON THE INNER AND OUTER SURFACES. REMOVED CORROSION & CHECKED LIMITS IAW SRM 54-52-21 PG 104. FOUND TO BE OUT OF LIMITS IAW SRM 54-52-51 PG 104. INSTALLED REPAIR IAW SRM 51-52-51 PGS 219-220. ALODINED PARTS IAW SRM 51-2SDR 08FDEA01119Panel · chafedNR 1 PYLON PANEL NR 439 AL IS CHAFED. REMOVED WEB IAW SRM 51-31-01 VOL II. LOCATED, DRILLED & DEBURRED NEW WEB IAW SRM 51-35-01 VOL II. INSTALLED WEB IAW DWG AUG 7107; REV P.SDR QXEA200800324Skin · crackedPDX -C4- NR 1 NACELLE SKIN FWD MLG DOOR APERTURE INBD FWD CORNER HAS A 1/4" CRACK. REPAIRED IAW RD8-54-873. HFEC INSPECTED BLEND AREA FOR CRACKS IAW NDTM, PART 6, 51-00-01, NO CRACKS NOTED.SDR QXEA200800323Skin · crackedPDX - C4- NR 1 NACELLE SKIN FWD MLG DOOR APERATURE, O/B FWD CORNER, HAS A 1/2" CRACK. CUTOUT DAMAGE REF RD8-54-873. PERFORMED HFEC AROUND CUT OUT IAW NDTM PART 6, 51-00-01, NO CRACKS NOTED. COMPLETED REPAIR IAW RD8-54-873 NOTES 2-5.SDR QXEA200800325Skin · crackedPDX -C4- NR 1 NACELLE SKIN INBD SIDE HAS 3/4" CRACK, AFT UPPER CORNER OF PANEL 416AR APERATURE. REPAIRED DAMAGE REFERENCING RD8-54-1193. HFEC INSPECTED AREA FOR CRACKS IAW D 8/200 NDTM, PART 6, 51-00-01, NO CRACKS NOTED.SDR HNAA0800136Access Panel · damagedDURING INSPECTION AFTER INFLIGHT FIRE, ACCESS PANEL 419AT WAS FOUND TO HAVE FIRE DAMAGE. MAINTENANCE REPLACED THE PANEL.SDR 08FDEA01004Skin · delaminatedNR 2 ENGINE OUTBD FAN COWL IS DELAMINATED AT THE EXTERIOR CENTER SECTION, 18 INCHES FROM THE T/E. ABRADED SURFACE & REPAIRED IAW SRM 54-10-00 FIG 1 & RDN 54-20-00 REPAIR 1 & 2.SDR 08FDEA00969Panel · chafedNR 2 PYLON PANEL NR 423 BL IS CHAFED ON THE MATING SURFACES. BLENDED CHAFED AREAS IAW SRM 54-52-51; ITEM 4; PG 102. ORIGINAL MATERIAL THICKNESS IS .079 IAW SRM 54-52-51; FIG 4; SHEET 2. REMOVED .031; REMAINING MATERIAL THICKNESS IS .048. FOUND TO BE OUT SDR 08FDEA00919Access Panel · crackedNR 1 PYLON, LEFT SIDE THRU ACCESS PANEL 413EL THE INTERNAL WEBBING IS CRACKED AT A PREVIOUS WELD. REMOVED INTERNAL DOUBLER IAW SRM 51-40-21; PG 7. PART MARKED IAW GMM 7-0-1001. INSTALLED IAW SRM 51-40-21; PG 7. MINOR REPAIRSDR 08FDEA00916Panel · corrodedNR 1 PYLON PANEL NR 414 GR IS CORRODED AROUND THE SCREW HOLES. REMOVED THE CORROSION IAW SRM 51-74-10. ORIGINAL MAT THICKNESS .079 IAW SRM 54-52-51; PG 12. REMOVED .059; .020 MAT REMAINING. OUT OF LIMITS IAW SRM 54-52-51; FIG 101. FABBED FILLER/DOUBLER ANDSDR 08FDEA00903Panel · chafedNR 1 PYLON PANEL NR 414BR HAS 2 CORNERS CHAFED. BLENDED CHAFED AREA IAW SRM 54-52-51; FIG 101. FOUND TO BE OUT OF LIMITS IAW SRM 54-52-51; FIG 101. FABBED DOUBLER IAW SRM 54-52-51; FIG 202. ALODINED IAW SRM 51-21-10 AND PRIMED IAW 54-52-51; FIG 51-23-10. INSSDR A6WA200840189Ground Stud · corrodedLT PYLON UPPER TRAILING EDGE GROUNDING PLATES CORRODED. LT PYLON UPPER TRAILING EDGE GROUNDING PLATES REPLACED IAW SRM 51-24-16 AND SRM 51-42-13. (M)SDR 08FDEA00896Skin · crackedNR 2 ENGINE AFT PYLON FAIRING; INBD MID SKIN IS CRACKED AT THREE PLACES. REMOVED DAMAGED SKIN AND DOUBLER. FABRICATED DOUBLER FROM .063 2024-0, PO 597274.1 IAW A310-300 SRM 51-26-10 AND 51-26-20; LOCATED HOLES IAW A310-300 SRM 51-40-40. ALODINED AND PRIMED SDR 08FDEA00820Fairing · crackedNR 1 PYLON PANEL 438CL IS CRACKED. REPAIRED CRACKS IAW DRAWING AIB7120-501.SDR 08FDEA00822Panel · crackedNR 3 PYLON PANEL 488CL IS CRACKED AT THE CUTOUT. WELD REPAIRED CRACKS IAW DWG AUB 7120 AND DPS 4.801 AND DPS 10.225.SDR 08FDEA00821Panel · crackedNR 3 PYLON PANEL 488CL IS CRACKED AT THE CUTOUT. WELD REPAIRED CRACKS IAW DWG AUB 7120 & DPS 4.801 & DPS 10.225.SDR FDKA200803102Panel · damagedPANEL 412CL HAS ONE FASTENER HOLE ELONGATED. THE DAMAGE HAS BEEN REPAIRED AND A DIMPLED WASHER INSTALLED.SDR 08FDEA00776Panel · crackedPYLON NR 1 LEFT SIDE LOWER SHIRT CLOSE OUT AT RIB 9 AND JUST FWD OF RIB 8, SHIRT IS CRACKED. REMOVED RUB STRIP, COVER PLATE, SHIRT PANEL AND ATTACH ANGLE IAW FEDEX A310-300 SRM 51-40-21, PG 6. LOCATED, DRILLED AND DEBURRED CLOSE OUT PANEL P/N A54610811600SDR 08FDEA00765Panel · chafedNR 2 PYLON PANEL NR 424 BR; CHAFED ON THE MATING SURFACES. CUT OUT DAMAGED AREA OF PANEL 424BR IAW SRM 54-52-51 FIG 203.; SHEETS 1-3. FABBED REPAIR DOUBLER & SHIM. INSTALLED BOTH IAW SRM 54-51-51; FIG 203; SHEETS 1-3. MINOR REPAIR.SDR 08FDEA00762Access Panel · dentedNR 2 ENGINE PYLON ACCESS PANEL NR 362 DR HAS A DENT. REPAIRED PANEL BY FABRICATING SKINS, CORE, LAYED UP & BONDED IAW TPS 1001 REV E & EA 8-5530-116967 "RT VERTICAL STABILIZER PICKLE BARREL PANEL". PANEL REMOVED & REINSTALLED TO FACILITATE MAINTENANCE IAW SSDR 08FDEA00757Panel · dentedNR 2 PYLON PANEL NR 423 DL IS DENTED. DRESSED OUT DENT REF SRM 51-73-10 PAGE 214. ACCOMPLISHED HFEC INSPECTION IF THE DENT AREA IAW NTM 51-10-20. NO DEFECTS NOTED. MINOR REPAIR.SDR 08FDEA00751Fairing · crackedNR 2 PYLON SKIN ABOVE THE INBD T/R IS CRACKED AT APPROX STA 704 RIB 7. CLEANED AREA & REMOVED SCRATCHES IAW SRM 51-73-10 PG 203. NO CRACKS NOTED. REPLACED SEAL SECTION IAW SRM 51-40-21. ORIGINAL MATERIAL THICKNESS 0.024. MATERIAL REMAINING 0.021. WITSDR 08FDEA00749Panel · chafedL/E NR 1 PYLON TOP PANEL P/N A572-44103-000 BACK SIDE HAS CHAFING MARKS IN NUMEROUS PLACES. BLENDED CHAFE MARKS IAW SRM 57-41-12 PG 102. MAT THICKNESS IS .035 IAW SRM 57-41-12, ITEM 60. MAT LOSS .006; MAT REMAINING .024, CHECKS TO BE OUT OF LIMITS IAW SRMSDR KCSA081133Skin · damagedNR 4 PYLON I/B SKIN DAMAGED ALONG LOWER EDGE BETWEEN NAC STA 220 AND 239.SDR DHL2008805510Skin · wornNR 2 ENG NACELLE INLET COWL UPPER SKIN WORN, STA YN 147.334 AT 12 O'CLOCK POS. (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED SKIN (AL2024T3 0.080") AND SPLICSDR DHL2008805509Skin · wornNR 1 ENG NACELLE INLET COWL UPPER EXTERNAL SKIN WORN, STA YN 147.534 AT 12 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED SKIN (AL2024T3 0.080") ASDR 08FDEA00649Skin · crackedON THE NR 1 ENG AFT PYLON FAIRING, O/B MID SKIN PANEL ASSY IS CRACKED AT THE MID FRAME. REMOVED MID FRAME IAW SRM 51-40-21; PGS 22 & 23; PARA 6. MATERIAL ID 2024- O .063 FOR THE PATCH & 2024-0 .071 FOR THE DOUBLER IAW SRM 54-55-51; PG 202. HEAT TREATEDSDR 2008UALA01055Retainer · wornWEAR WAS FOUND AT SEAL RETAINER OF NR 2 STRUT AFT FAIRING AT SAF STA 362, FAIRING OUTBOARD FRAME.SDR A6WA200840127Panel · damagedRIGHT PYLON PANEL 422DB, SEPARATORS ABRADED. RIGHT PYLON PANEL 422DB, SEPARATORS REPLACED IAW CRJ200 SRM 51-42-06. (M)SDR KCSA081118Skin · chafedNR 4 PYLON OUTBOARD SIDE EXTERNAL SKIN IS CHAFED AT FIREWALL AREA FROM NAC STA 180 TO 220.SDR HALA0800339Skin · corrodedLEVEL 1 CORROSION AND PAINT PEELING ON LT ENG UPPER COWL EXTERIOR SURFACE. REPAIR IN WORK.SDR HALA0800338Skin · corrodedLEVEL 1 CORROSION, ON LT ENGINE PYLON T/E ASSY LOWER SURFACE. REPAIR IN WORK.SDR HLA0800340Skin · corrodedLEVEL 1 CORROSION ON LT ENG, LOWER COWLING FWD NR 1RIB, I/B REPAIR DOUBLER. REPAIR IN WORK.SDR HALA0800318Skin · corrodedLEVEL 1 CORROSION AND PAINT PEEL NR 1 ENGINE, LOWER COWL, EXTERIOR. REPAIR IN WORK.SDR HALA0800317Skin · corrodedLEVEL 1 CORROSION AND PAINT PEEL, NR 1 ENGINE, TOP COWL EXTERIOR AT FAN AIR VALVE EXIT AND 1 PLACE AT COWL HALF. REPAIR IN WORK.SDR HALA0800316Skin · corrodedLEVEL 1 CORROSION ON TOP COWL NR 1 ENGINE, ALONG L/E AND HINGE EDGE. REPAIR IN WORK.SDR 08FDEA00495Panel · chafedNR 3 PYLON AFT "V" PANEL NR 488 GL, ATTACHMENT HOLES CHAFFED. BLENDED DAMAGED AREAS, MAXIMUM DEPTH .055 IAW SRM 54-00-01, FIG 1A VOL I. FABRICATION PER EA NR 8-5480-118437. ALODINED AND PRIMED IAW SRM 51-21-01, VOL II, PG 21-24. INSTALLED DOUBLER AND FILLSDR 08FDEA00467Panel · corrodedNR 2 PYLON PANEL 444BL IS GOUGED IN 2 PLACES AND HAS SURFACE CORROSION. REMOVED CORROSION IAW SRM 54-50-71. ORIGINAL MATERIAL THICKNESS .063. L=1.0", W=.50", D=.011". FOUND TO BE OUT OF SRM 54-50-71, FIG 101 LIMITS, 10 PERCENT MATERIAL LOSS. FABRICATED NESDR S9BA20080004Skin · corrodedCPCP INSPECTION, LT WING, LT AND RT NACELLE SKINS CORRODED. REMOVED AND REPLACED NACELLE SKINS AND SPLICED SKINS IAW RD6-54-004 AND AC 43-13, PARA 4-57.
Back to JASC 5414