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 YENA2024041600609Skin · damagedDURING HEAVY MAINTENANCE: PYLONS / LH PYLON (#1 ENGINE) / CANTILEVER STRUCTURE SKIN / RIBS 3-4 / CRACK DAMAGE - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)SDR COEA2024041214757Skin · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, A CRACK WAS FOUND ON THE L/H ENGINE LOWER FWD COWL INBOARD UNDER EXHAUST. A TEMPORARY REPAIR WAS PERFORMED ON THE L/H ENGINE LOWER FWD COWL PER DOCUMENT REF: DQ428170M2. A NEW TEMPORARY REPAIR WAS PERFORMED PER DQ438SDR SWAA2024041071925Skin · corrodedPITTING FOUND ON #1 ENGINE COWL LIP SKIN AT 11 OCLOCK POSITION LOCATED ON #1 ENG COWL LIP SKIN LOCATED AROUND 10:30-12 POSITION. MULTIPLE PITTING AND DISCOLORATION SPOTS. DEEPEST OF THE PITTING IS 0.0045. TSR TRACKING# 2024002349<[01] PERFORMED E/A# 24-154-009SDR IPXA2024041978080Skin · corrodedFAULT-STRUC-400-#2 PYLON OUTBD INNER SKIN FWD OF VENT PANEL OPENING HAS EXFOLATION CORROSION. DOT 8-010. WORK ACCOMPLISHED PER UPS EO:EO90099-REQ1 AND VTMAE 757-5450-27-A3572 REV-,FAA 8100-9.SDR DALA2024040204019Panel · detachedSHIP 3405 -ATB- DUE TO PYLON PANEL FOUND ON RUNWAY AFTER TAKEOFF. CORRECTIVE ACTION: FOUND NUMBER 1 ENGINE PYLON AFT OUTBOARD PANEL MISSING. REPAIRED FRAME AND FASTENER MOUNTS AND REPLACED PANEL PER ERA 616876-14. OK FOR SERVICE. (4824266)SDR DALA2024040203989Latch · failedSHIP 1702 - ATB - FOR RT ENG PYLON PNL (PRESSURE RELIEF) OPEN IN FLIGHT. CORRECTIVE ACTION: C/W OVERWEIGHT LANDING AND REPLACED BOTH PRESSURE RELIEF PANEL LATCHES. (5031869)SDR CALA2024040300943Skin · cracked1 1/2 INCH CRACK IN THE UPPER AFT CORNER OF THE CUTOUT, FOR THE FWD ACCESS PANEL, ON THE O/B SIDE OF THE RIGHT ENGINE PYLON.#6204 REF AMES NR 167037-0400-0184. CRACK IN UPPER AFT CORNER OF CUTOUT REPAIRED IAW B767 SRM 54-53- 01-2R-G REPAIR 6 SEE PARTIAL WORK ASDR CALA2024032700883Access Panel · missingOIL FILLER DOOR MISSING UPON ARRIVAL. #1 ENGINE L/H OIL FILLER ACCESS PANEL. REPLACED MISSING OIL FILLER DOOR IN REFERENCE TO AMM 71-11-04-308-075-R00. AIPC REF 71-11-04-03.SDR DALA2024032603768Panel · detachedSHIP 3405 ATB DUE TO PYLON PANEL FALLING OFF ON LEFT ENGINE. CORRECTIVE ACTION: MTC IN PROGRESS.SDR DALA2024032603806Access Panel · missingSHIP 1813 LEFT ENNG INBOARD NCAELLE ACCESS PANEL MISSING. CORRECTIVE ACTION: INSTALLED LEFT ENG. INBOARD NACELLE ACCESS DOOR IAW B767-400 AMM 54-53. (5407760)SDR COEA2024032610767Skin · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, A CRACK WAS DISCOVERED IN THE #2 ENGINE R/H OUTBOARD ACCESSORY PANEL SKIN AROUND 1/4 TURN FASTENER. #2 R/H OUTBOARD ACCESSORY PANEL SKIN REPAIRED VIA REPLACEMENT AS NEEDED IAW C408 SPM 20-50-00 AND C408 IPC 54-10-00 SDR IXXA20240504003Access Panel · gouged#1 ENGINE NACELLE ACCESS PANEL 431AT FORWARD INBOARD MATING AREA IS GOUGED. REF HAECO WO 320005 NON ROUTINE 34693SDR IXXA2024041402Access Panel · worn#1 ENGINE, INBOARD ACCESS PANEL 437AR, AFT ATTACHMENT FLANGE FOUND WORN WITH A MATERIAL LOSS OF 0.026SDR CALA2024032000795Skin · crackedNR 2 PYLON PNL NR 446BL CUTOUT FOUND CRACKED. NR 2 PYLON PANEL #446BL CUTOUT SKIN REPAIRED AS PER ECRA 5450-02920 REV- ATTACH MAINTENANCE WORKSHEET FORM 44-0008 ITEM 1 TO ITEM 28 ACCOMPLISHED.SDR CALA2024032000793Skin · crackedNR 1 PYLON PNL NO.436BR CUTOUT SKIN FOUND CRACKED TRANSFER REFER NON-ROUTINE WO.2982368. NR 1 PYLON PANEL NR 436BR CUTOUT SKIN REPAIRED AS PER ECRA 5450-02919 REV- ATTACH MAINTENANCE WORKSHEET FORM ITEM 1 TO ITEM 35 ACCOMPLISHED.SDR CALA2024031900782Skin · crackedGEN ITEM: 63-54-1-2805// INNER SKIN CRACK AT AFT UPPER CORNER ON NO1 PYLON AT ACCESS PANEL 436BR CUTOUT (M) 2328. STOPPED DRILL CRACK FABRICATED AND INSTALLED REPAIR DOUBLER INST ALLED RUB STRIP IAW B767 SRM 54-53-01-2R-7 REPAIR 7. SEE PARTIAL WORK ACCOMPLISHSDR DALA2024031903481Skin · damagedSHIP 3115 ENGINE #1 PYLON EXPOSED MESH ON SKIN. CORRECTIVE ACTION: REPAIRED PER ERA 616686-14. (9134828)SDR DALA2024032003529Plate · corrodedSHIP 3252 DISC: CORROSION RIB 8 REFORCIN PLATE ON RH PYLON. C/A: OMPLIED WITH ER/A 616311-14AD REV. ORIGINAL MATCHES WITH ALL STEPS ON PRI 616311-14AD REV.0 AND PRI 616311-14AD REV.1 IT HASBEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON RH WING RIB 8 AND STRISDR IXXA20240505002Panel · worn#1 PYLON PANEL 437CL IS WORN ON INNER SURFACE. REF HAECO WO 320005 NON ROUTINE 34046SDR IXXA20240505001Panel · worn#1 PYLON PANEL 437CR IS WORN ON INNER SURFACE. REF HAECO WO 320005 NON ROUTINE 34047SDR IXXA20240504002Panel · worn#2 PYLON PANEL 447CR IS WORN ON INNER SURFACE. REF HAECO WO 320005 NR 34049SDR IXXA20240504001Panel · worn#2 PYLON PANEL 447CL IS WORN ON INNER SURFACE. REF HAECO WO 320005 NON ROUTINE 34048SDR SWAA2024041062212Skin · cracked#2 ENGINE O/B FAN COWL FWD LOWER END CRACK<[01] ACCOMPLISHED REPAIR- REPAIRED PER [SRM 54-20-01-2R-12-A01474 (REPAIR 12 - FAN COWL DOOR SKIN REPAIR AT FWD LATCH AREA - PERMANENT)];[02] VERIFIED FINAL STEP 1SDR SWAA2024031462046Skin · cracked#2 ENGINE I/B FAN COWL IS CRACKED 17' LONG AT FWD LOWER FWD END.<[01] REMOVED AND REPLACED #2 ENGINE INBOARD FAN COWL REF. AMM 71-11-02. INSTALLED VORTEX CONTROL DEVICE REF. AMM 71-11-08.SDR SWIA2024050800310Skin · chafedLEFT ENGINE UPPER FAN COWL INNER SKIN IS CHAFED AT THE OUTBOARD SIDE. (C-CHECK RO 5/6/2024) REMOVED DAMAGED OUTBOARD GUSSET P/N CN622-0333-203 FROM L/H UPPER FAN COWL, REF. CRJ700 SRM 51-42-13-001-001-A01 AND INSTALLED NEW OUTBOARD GUSSET P/N CN622-0333-20SDR SWAA2024041766895Fastener · loose#1 INLET COWL OUTER LIP SKIN HAS SEVERAL LOOSE FASTENERS AT THE 6 O'CLOCK POSITION (MKD)<[01] REMOVED DISCREPANT FASTENERS I.A.W SRM 51-40-02.;[02] C/W NDT PER PART 6 51-00-00 PROCEDURE 23 AND PART 6 53-30-00 PROCEDURE 3. NO DEFECTS NOTED.;[03] INSTALLED FIRSTSDR JR2R20240308330Panel · chafed429NR HAS CHAFING ON FWD IB SIDESDR DALA2024030402957Skin · puncturedSHIP 1707 NUMBER 1 ENGINE AFT PYLON PANEL MFG P/N 313T3391-299 PUNCTURED. CORRECTIVE ACTION: INSTALLED PERMANENT REPAIR PER B767-300 SRM 51-70-10-2R REF SRM 54-52-70-2R (0228874)SDR UIEA2024022300117Skin · punctured#2 ENG R/H CORE UPPER SECTION 10" (COUNT FROM AFT) EXT SURFACE FOUND PUNCH HOLE(<P>#2 ENG R/H CORE COWL UPPER SECTION TITANIUM FAIRING EXTERNAL DOUBLER REPAIRED AS PER SRM 54-45-01-2R-7 REPAIR 7. NO FURTHER DEFECTS NOTED</P>)SDR DALA2024030503045Skin · corrodedSHIP 698 AD - DAMAGES WERE FOUND ON RH ENG DRAG FTG HOLES AS FOLLOW: HOLE #5 CORROSION ON SKIN BETWEEN 4 AND 6 CLOCK POSITIONS, HOLE #8 CORROSION ON FITTING BETWEEN 7 AND 9 CLOCK POSITIONS, IN REFERENCE TO JOB 013-0001 CARD 5720-01100-04B, STEP 4.C. CORRECTIVESDR VNAA202404080007Access Panel · damagedPERM REPAIR - LH PYLON ACCESS PANELS 412EB AND 412GB REF REO 690-54-51-050 WHITHIN 800 FH, REPAIR THE AFFECTED PARTS ACCORDING TO APPROVED PROCEDURES. LH PYLON ACCESS PANELS 412EB AND 412GB WERE REPAIRED PER REO 690-54-51-052 REV. - -SDR IPXA2024032260994Skin Panel · corroded*SUPPLEMENTAL SDR* *MAJOR REPAIR* FAULT: EVIDENCE OF CORRISON ON INSIDE SURFACE OF #2 PYLON FWD OF PANEL 443CR. DOT 142-17. ACCOMPLISH EO-89829-REQ1 AND EA 757-5450-27-A3546. AUDIT COMPLETE.SDR SWIA202404250314Transcowl · crackedR/H UPPER TRANSCOWL PERFORATED SKIN UNDER Z STIFFENER IS CRACKED (C-CHECK RO 4/24/2024) CUT AWAY DAMAGED SECTION, FABRICATED AND INSTALLED ALL REPAIR PARTS, REF. REO670-54-21-1617, REV. --, 2024-03-06.COMPLIED WITH MAJOR REPAIR M-337 AND /SKY CARD 51-900-SDR SWAA2024031454154Cowl Door · cracked#1 ENGINE I/B FAN COWL OIL ACCESS DOOR CLOSE OUT FRAME IS CRACKED.<[01] REMOVE AND REPLACE #1 ENGINE I/B FAN COWL OIL ACCESS DOOR CLOSE OUT FRAME PER. SRM 51-40-02-0G-0 AND CMM 71-13-30;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLESDR SWAA2024030853374Access Door · cracked#1 ENGINE I/B FAN COWL OIL SERVICE DOOR OPENING INNER SUPPORT PANEL IS CRACKED. MRKD<[01] REPLACED SUPPORT PANEL PER SRM 51-40-02& SRM 51-10-02.;[02] INSPECTION C/WSDR IXX2024021600000Skin · cracked#1 PYLON UNDER TR HAS CRACKED SKIN.SDR IXX20240216000001Skin · cracked#1 PYLON UNDER TR HAS CRACKED SKIN.SDR SWAA2024031451950Inlet · cracked#2 ENGINE INLET COWL OUTER LIP SKIN HAS A CRACKED RIVET HEAD AT THE 10:00 POSITION SPLICE SECOND ONE IN FROM THE AFT SIDE OF LIP SKIN.<[01] UPDATED PARTS;[02] REMOVED AND REPLACED #2 ENGINE INLET COWL IAW 71-11-01-000-802-F00 AND 71-11-01-400-802-F00 STEP 5.H.SDR CALA2024022700551Skin · damagedLH PYLON IB SAIL TAIL PNL, HAS HEAT DAMAGE.SDR NACA2024020800003Skin · tornLEFT ENGINE INBOARD SIDE TOP NEAR PYLON, SHEET METAL APPEARS TO BE TEARING OFF. BROKEN RIVETS, RIPPED METAL. REMOVED AND REPLACED LEFT ENG INBD CORE COWL AS PER AMM 71-11-06/201. PART UNKNOWN TO TRAX.SDR IXXA2024020803Skin · crackedIB CORE COWL CRACKED AT AFT LATCHSDR IXXA2024020802Skin · crackedIB CORE COWL SKIN CRACKEDSDR CALA2024021300410Skin · corrodedDOT 86-58 #1 PYLON IB SAIL TAIL PANEL HAS CORROSION &HEAT DAMAGE AROUOND LOWER RIVETS ()SDR IPXA2024022092776Skin · corrodedNR 1 ENGINE OUTBD PYLON INNER SKIN, FWD OF VENT PANEL HAS EXFOLIATION CORROSION. ALL WORK ACCOMPLISHED PER EO EO-89461-REQ AND VT MAE 757-5450-27-A3512 REV.SDR IPXA2024022292675Skin · corroded*SUPPLEMENTAL SDR* *MAJOR REPAIR* FAULT- #2 ENGINE OUTBD PYLON, INNER SKIN FWD OF VENT PANEL HAS EXFOLIATION CORROSION. DOT 8-017. WORK ACCOMPLISHED PER UPS EO: EO-89467-REQ 1 AND VTMAE EA 757-5450-27-A3518 REV-SDR IPXA2024022192899Doubler · corrodedMAJOR REPAIR. #2 ENGINE INBD PYLON INNER SKIN UNDER THE CIRCLE PANEL OPENING HAS CORROSION. DOT 8-021. ACCOMPLISHED WORKED PER UPS EO-89493-REQ 1 AND VT MAE EA 757-5450-27-A3519 REV. FAA 8100-9 APPROVAL ATTACHED.SDR IPXA2024021992798Skin · corrodedMAJOR REPAIR, NR 1 ENGINE INBD PYLON INNER SKIN, AFT OF THE SQUARE PANEL HAS EXFOLIATION CORROSION. DOT 8-014. VERIFIED WORKED PER UPS EO: EO 89460-REQ 1 AND VT MAE 757-5450-27-A3511 REV.SDR IPXA2024021992675Skin · corrodedMAJOR REPAIR, NR 2 ENGINE OUTBD PYLON, INNER SKIN FWD OF VENT PANEL HAS EXFOLIATION CORROSION. DOT 8-017. OK TO APPLY TOP-COAT APPROVED. OPENSDR IPXA2024021792899Skin · corrodedMAJOR REPAIR, NR 2 ENGINE INBD PYLON INNER SKIN UNDER THE CIRCLE PANEL OPENING HAS CORROSION. DOT 8-021. ACCOMPLISH EO-89493-REQ1 AND EA 757-5450-27-A3519. OPENSDR IPXA2024021592776Skin · corrodedFAULT- #1 ENGINE OUTBD PYLON INNER SKIN, FWD OF VENT PANEL HAS EXFOLIATION CORROSION. OK TO INSTALL DOUBLER"INSP ONLY"
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