JASC 5414
Service difficulty reports · 4,357
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 IPXA2026082679985Skin · crackedPANEL 485AL HAS A CRACK ON THE FWD SIDE. INSTALLED SKIN PANEL ON PANEL 485AL FWD SIDE IAW SRM-51-40-21.SDR HNAA2026082700798Hinge · brokenNR 1 ENG START VALVE ACCESS PANEL HINGE BROKEN. R & R HINGE IAW SRM 51-40-02SDR IPXA2026091160874Skin · crackedNR 1 PYLON, PRECOOLER AREA, INTERNAL LT SKIN, AT RIB 4, WITH CRACK. INSTALLED RIVETS (7EA) STEP 10 AND (1EA) STEP 1 AT NR 1 PYLON, PRECOOLER AREA, INTERNAL LT SKIN, AT RIB 4 IAW SRM 51-40-21-001.SDR IPXA2026091160860Skin · crackedNR 1 PYLON, PRECOOLER AREA, INTERNAL RT SKIN, AT RIB 4, WITH CRACK. INSTALLED RIVETS (8EA) AT NR 1 PYLON, PRECOOLER AREA, INTERNAL LT SKIN, AT RIB 4 IAW SRM 51-40-21-001.SDR IPXA2026081160860Skin · crackedNR 1 PYLON, PRECOOLER AREA, INTERNAL RT SKIN, AT RIB 4, WITH CRACK. EWIS, NR 1 PYLON PRECOOLER CAVITY IAW ESPM 20-54-50-02.SDR IPXA2026091125996Skin · crackedNR 2 PYLON, TOP SKIN RT SIDE AT RIB 8 IS CRACKED. WELD REPAIRED ON TRAVELER T26/1874956SDR IPXA2026082662254Skin · crackedNR 2 PYLON, FR 8, RT SIDE, EXTERNAL SKIN PANEL CRACKED. ACCOMPLISHED WELD REPAIR IAW SRM 54-50-00-101-C1, FIGURE 105.SDR JR2R20260708611Panel · chafedPYLON PANEL 429NR HAS MULTIPLE CHAFED OUT OF LIMITS. REPAIREDSDR JR2R20260708615Panel · chafedPYLON PANEL 419ML HAS MULTIPLE CHAFES ON INSIDE OF PANEL. REPAIREDSDR SWAA2026070718666Skin · cracked#2 ENGINE PYLON STRUT AFT LOWER SKIN IS CRACK; AROUND 7 INCHES LENGTH.<[01] C/W EA 26-154-01802.SDR IPXA2026071560216Skin · crackedCRACKED SKIN, NR 4 PYLON R/H FAIRING DOOR L/E AREA. I.A.W.AMM 54-62-03-404-005 REV117 INSTALLED NO.4 PYLON R/H FAIRING DOOR.SDR DALA2026062903828Skin · crackedAREA OF FASTENERS NEAR UPPER EDGE OF THE EXTERNAL SURFACE OF THE LEFT PYLON AT RIB 8 LEVEL 01 EA FASTENER FOUND 2 CRACKS. PERFORMED REPAIR PER A330 SRM 54-51-00-300-016. (1672546) AIRCRAFT WAS GROUNDED.SDR IPXA202606290225Skin · crackedNR 1 ENG INLET COWL LIP CRACKED BETWEEN 11 AND 1 O'CLOCK POSITIONS REMOVED #1 ENGINE INLET IAW AMM 71-11-01SDR IPXA2026070343513Fan Cowl · crackedCRACKED SKIN, NR 1 ENG RT FAN COWL INNER FWD LWR CORNER AREA. IAW AMM 71-11-02-024-001-H00 REV.148 AND AMM 71-11-02-424-005-H00, REV 148 TRANSFERRED THE CHINE TO THE SERVICEABLE FAN COWL. INSTALLED THE LEADING EDGE PROTECTIVE TAPE PER SREO-22247-REQ002. IAW ASDR JR2R20260624815Panel · chafedLEFT PYLON PANEL 419ML HAS CHAFING IN MULTIPLE PLACES. REPAIRED PER ETD.SDR JR2R20260624814Panel · chafedRT PYLON PANEL 429ML HAS CHAFING IN MULTIPLE PLACES. REPAIRED PER ETD.SDR JR2R20260624813Panel · chafedLEFT PYLON PANEL 419NR HAS CHAFING IN MULTIPLE PLACES. REPAIRED PER ETD.SDR JR2R20260624842Skin · chafedLEFT OVER PYLON FIXED LEADING EDGE PANEL CHAFED. REPAIRED.SDR IPXA2026063061139Panel · erodedEROSION, L/E, NR 3 PYLON 471B PANEL. REMOVE THE ERODED MATERIALS AND CLEAN. MEASURE THE DAMAGE AREA ( L : 3.5", W : 0.2", D : 1 PLY, AT L/E, 22" FROM INBD EDGE ). APPLY ADHESIVE TO THE REPAIR AREA, CURED AT 80 F FOR 10 HOURS. I.A.W AMM 51-24-11-477-083 REV.11SDR IPXA2026063061135Panel · erodedEROSION, L/E, NR 4 PYLON 481B PANEL. IAW SRM 54-51-70-1A-1 REV. 107 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR AS BELOW STEP: REMOVE THE ERODED MATERIALS AND CLEAN. APPLY ADHESIVE TO THE REPAIR AREA, CURED AT 80°F FOR 10 HOURS. CONDITION CHECK IS SATISFASDR CALA2026062217260Panel · missingPANEL 433HR ON THE NR 1 ENG PYLON RIGHT SIDE MISSING. INSTALLED PANEL 433HR ON NR 1 PYLON, REF IPC 54-53-01-05. IN REF TO GMM 02-30-95. NO DAMAGE TO VICINITY AREA. AIRCRAFT IS OK TO CONTINUE IN REF TO GMM 02-30-95. NOTICED NO DAMAGE TO VI LP 9325265: PANELSDR JR2R20260617886Fan Cowl · not reportedREPAIR FAN COWL PN 15D1100009 S/N RMAFE904. REPAIREDSDR IPXA2026062286352Skin · dentedDENTED SKIN, NR 2 ENG INLET COWL INNER BARREL NEAR 6:00 POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.5", 14.25" FROM FWD EDGE AND 38.5" FROM INBD EDGE, AT 6 O'CLOCK ON THE INNER BARREL OF NR 2 ENG INLET COWL ). BOND THE SPACER WITH FISDR DALA2026061503562Access Panel · corrodedLEVEL 2 CORROSION, NR 2 ENGINE, RT UPPER PYLON, ACCESS PANEL 424CR WITH CORROSION. REPAIRED EXTERNAL SKIN IN ACCESS PANEL 424CR, ENGINE NR 2 RT UPPER PYLON AREA IAW SRM 54-52-11-300-003 PARAG 2.A FIG 001, REV 158. THIS REPAIR IS CATEGORY A WITH NO ADDITIONAL SDR IXXA20260609002Web · crackedNUMBER 2 PYLON AFT FAIRING 447DB (STINGER) INTERNAL SUPPORT WEB IS CRACKED REFERENCE AMES WO N503AZ-28 NR 193266-0400-0075SDR 4VAA202605270028Skin · corrodedDURING INSPECTION, THE LEFT NACELLE INSIDE SKIN WAS FOUND CHAFED AND CORRODED. THE SKIN WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060709.SDR IPXA2026060258511Nose Cowl · dentedDENT - SKIN, NO. 1 ENG NOSE COWL INNER BARREL 11:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUTOUT ( DIA : 0.7", 22" FROM FWD EDGE AND AT 11 O'CLOCK ON THE INNER BARREL OF NR 1 ENF INLET COWL) FILL THE CUTOUT WITH ADHESIVE CURED AT 200°F FOR 1 HOUR IASDR CALA2026052816597Skin · corrodedNR 1 ENGINE INBD (R/H) FAN COWL, LOWER INNER SKIN HAS SIGNS OF SURFACE CORROSION. REMOVED AND REPLACED NR 1 ENG INBD RT FAN COWL DOOR 2ND FROM FWD ZEE FRAME AND LOWER END TEE CLIP IAW SRM 51-40-02-0G-0 AND CMM 71-13-30. BLENDED LOWER EMD OF ZEE FRAME, FOUND SDR FDEA202605230629Skin · corrodedPYLON NR 1 AROUND THE CUT OUT FOR ACCESS PANEL 433JR INTERNAL SKIN SHOWS CORROSION. REMOVED AND REPLACED INBD PYLON SKIN PANEL IAW B DWG 012N8774 REV A AND SRM 51-40-02-0G.SDR UIEA2026042200236Skin · cracked2L CORE COWL EXTERIOR SURFACE T/E AT 12 O'CLOCK POSITION FOUND CRACKED(<P>SKIN CRACK AREA REPAIRED AS PER ATLAS AIR EA-1971A268 REV 1. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050100281Skin · damagedSKIN REPAIR FOR RHW LE D-BEAM FOR O/B UPPER CHORD REPAIR (3 PYLON OB)(<P>L/E SKIN REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2 AND RI-57-41-18181 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050100283Skin · damagedL/E SKIN REPAIRED AT #4 PYLON I/B D-BEAM FOR UPPER CHORD REPAIR(<P>L/E SKIN REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2 AND RI-57-41-18200 REV A. NO FURTHER DEFECTS NOTED</P>)SDR 1Q2R2026061100001Latch · nickedRIGHT HAND TRANS COWL NICKED/DENTED ON THE LATCH DOOR BELOW THE FORWARD LATCH. DAMAGE MEASURED 3/8"L X 1.0"W. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH MHI RJ REO 670-54-21-1816 REV. --, DATED MAY 5TH, 2026, AND REPLACED LATCH.SDR CALA2026060116718Skin · damagedAIR INTAKE COWL SHOWS SIGN OF LIGHTNING STRIKE. PICT AND DIMENSION. 6 O'CLOCK POSITION. DIMENSIONS PER ATTACHED IMAGE: 3/16 INCH WIDE, 1/4 INCH WIDE, 0.024 INCH DEEP. AFT EDGE OF DAMAGE IS 9/16 INCH FORWARD OF AFT EDGE OF INLET COWL. REMOVED AIR INTAKE COWL SDR FDEA202605180619Access Panel · crackedNR 3 PYLON COMPARTMENT THROUGH ACCESS PANEL 617BT OUTBOARD LOWER AFT WEB FOUND CRACK APPROXIMATELY 0.75" AT XFS 427 #3 PYLON COMPARTMENT ACCESS PANEL 617BT OUTBOARD LOWER AFT CRACKED WEB AT XFS 427 REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-31-01-0G. WSDR FDEA202605180618Access Panel · crackedNR 1 PYLON COMPARTMENT THROUGH ACCESS PANEL 517BT OUTBOARD LOWER AFT WEB FOUND CRACK APPROXIMATELY 0.5" AT XFS 427. #1 PYLON COMPARTMENT ACCESS PANEL 517BT OUTBOARD LOWER AFT CRACKED WEB AT XFS 427 REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-31-01-0G. WSDR IXXA2026051601Skin · chafedCHAFE DAMAGE ON THE NR 2 ENGINE, FWD NACELLE STRUT UPPER SKIN AT NSTA 150.9SDR 4VAA202605140027Skin · corrodedDURING INSPECTION, CORROSION AND CHAFING WAS FOUND ON THE RIGHT NACELLE INSIDE SKIN. THE SKIN WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060709.SDR SWAA2026061503106Fairing · crackedNR 1 ENGINE AFT FAIRING AFT END IS CRACKED. REMOVED; AND REPLACED NR 1 ENGINE AFT FAIRING AFT END TRAILING EDGE ASSY IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 313A2400 REV:A; DWG 313A2700 REV-.SDR IPXA2026061072557Skin · damagedMAJOR REPAIR, NR 1 PYLON RT SIDE BEHIND PANEL ATTACHMENT BRACKET HAS A HOLE IN SIDE SKIN RII REQUIRMENTS COMPLETED IAW UPS GMM 04-02 MAJOR REPAIRS REQUIREMENT 5SDR SWAA2026061097913Access Panel · crackedCRACKED SEAL BLADE ACCESS PANEL 431AL AT LT PYLON. REPLACED SEAL BLADE ACCESS PANEL 431AL AT LT PYLON IAW SRM 51-10-02-0G-0, ITEM 9, & SRM 51-40-02-0G-0.SDR VNAA20260512038Skin · crackedCRACK WAS FOUND ON EXTERNAL SKIN LH UPPER ENGINE TRANSCOWL. CRACK WAS FOUND ON EXTERNAL SKIN LH UPPER ENGINE TRANSCOWL WAS REPAIRED PER REO 670-54-21-1818 REV. -A.SDR JR2R20260512738Skin · chafedRIGHT ENGINE CORE COWL 427AL EXTERIOR SKIN HAS CHAFE MARKS. REPAIRSDR IPXA2026060226363Skin · crackedNR 2 PYLON UPPER SKIN 12 HOLE HAS CRACK AT 12 O'CLOCK POSITION AT LOWER LAYER. ACCOMPLISHED REPAIR PER EO-97524-REQ1 AND VT-SAA EA 757-5700-01-B0750, REV I/R.SDR IPXA2026062915824Fan Cowl · dentedRIGHT ENGINE OTBD FAN COWL OUTER SKIN TWO DENTS AT 1 O'CLOCK POSITION IAW AMM 71-11-04-714-002-H00, REV 148, INSTALLED THE FAN COWL OF NR 2 ENGINE. CONDITION CHECKED IS SATISFACTORY.SDR IPXA2026060205494Skin · crackedNR 2 ENG FIRE LOOP ACCESS PANEL L/E SKIN CRACKED . INSTALLED EXTERNAL REPAIR DOUBLER AT #2 ENG FIRE LOOP ACCESS PANEL IAW E.A.# 757-5741-01-B0742 REV P1 STEP 7. ACCOMPLISHED PERMANENT REPAIR PER EO-97550-REQ1 AND VT-SAA EA 757-5741-01-B0742, REV. I/R.SDR FDEA202605050556Skin · pulledNR 1 ENG PYLON HAS 3 PULLED FASTENERS ON SKIN O/B SIDE ABOVE AFT ENG MOUNT POINT.SDR SWAA2026060194857Access Panel · crackedCRACK SEAL BLADE ACCESS PANEL 441AL AT RT PYLON. REPLACED SEAL BLADE LOCATED ON ACCESS PANEL 441AL AT RT PYLON IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02.SDR CALA2026050115912Access Panel · missingRIGHT PYLON OTBD SIDE CIRCULAR ACCESS PANEL MISSING. COMPLIED WITH A NEW PANEL FITTED IAW AMM 54-53-01.SDR DALA2026043002738Access Door · crackedL/H PYLON I/B SKIN ACCESS DOOR 436AR CUT-OUT FOUND CRACK AT 12 O'CLOCK. REPAIRED AS PER ER/A 633786-14 (1570034) (AIRCRAFT GROUNDED)
Back to JASC 5414