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 SWAA2024010323804Access Panel · crackedCRACK SEAL PLATE ACCESS PANEL 441AT AT RT PYLON (2 EA) 2023-719810<[01] REPLACED SEAL PLATE ACCESS PANEL 441AT AT RT PYLON (2 EA IAW B737-800 SRM-51-40-02 AND SRM-51-10-02 ITEM 9;[02] REPLACED SEAL PLATE ACCESS PANEL 441AT AT RT PYLON (2 EA IAW B737-800 SRM-51SDR IPXA2023112740899Skin · corroded*MAJOR REPAIR* FAULT: EVIDENCE OF CORROSION INSIDE #2 PYLON SKIN FWD OF PANEL 443CR. DOT 140-13. ACCOMPLISH EO-88765-REQ1 AND EA 757-5450-27-A3442. SUBTASK UP TO REP REVIEW, JOB COMPLETE, AUDIT COMPLETE. REVIEWED.SDR IPXA2023112486155Skin · corroded*MAJOR REPAIR* FAULT: #1 ENGINE PYLON I/B AFT. SKIN HAS CORROSION AT INNER SKIN APP. STA 154 . DOT 07308-005 (PLACED AT EXTERNAL SKIN) VERIFIED COMPLIED WITH EO 88741-REQ1 AND EA 757-5450-27-A3437 REV. -. JOB COMPLETESDR IPXA2023112732706Skin Panel · dented*MAJOR REPAIR* FAULT:#2 PYLON I/B HAS DENT AT OUTTER SKIN BETWEEN NAC STA 105.66 AND NAC STA 169.8. DOT119-009. ACCOMPLISH EO-88785-REQ1 AND EA 757-5450-27-A3452. JOB COMPLETED. REVIEWEDSDR SWAA2023112116215Panel · damagedINLET ACCESS #2 ENGINE LOWER NOSE COWL PANEL #422AB HAS ELONGATED FASTENER HOLES<[01] RECEIVED NEW LOWER NOSE COWL PANEL #422AB P# 314-2163-1 PO# 2028887 BN 406123. PANEL WILL BE INSTALLED ON TASK CARD # TTG8Q00P88YN;[02] VERIFIED STEP 1SDR SWAA2023112814930Skin · corrodedCORROSION INLET COWL LIP-SKIN INBOARD AREA ON ENGINE 1 2023-661449<[01] ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N: 130063701 AND DUE DATE: 24-JUL-24.;[02] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[03] REPAIRED INLET COWL LIP-SKISDR SWAA2023112814931Skin · corrodedCORROSION INLET COWL LIP-SKIN INBOARD AREA ON ENGINE 2 2023-661450<[01] TOOL USED: ULTRASONIC THICKNESS GAGE. PN: 45MG; SN: 232019809; DUE DATE: 22-SEP-24;[02] TOOL USED ULTRASONIC THICKNESS GAUGE P/N: 45MG; S/N: 130063701; CAL DUE DATE: 24-JUL-24;[03] REPAIRESDR DALA2023102508778Unknown · unknownSHIP 1703 NO.2 PYLON I/B ACCESS DOOR 442AL CUTOUT UPPER EDGE CRACK. CORRECTIVE ACTION: THE CRACK SKIN AT NO.2 PYLON I/B ACCESS HOLE 442AL AFT UPPER EDGE REMOVED AND APPLY DOUBLER REPAIR WITH MATERIAL:15-5PH-0.090 " AS PER PRI 612706-14 REV 0. (0026135)SDR FDEA202310031695Skin · cracked#2 PYLON AFT LOWER HEAT SHIELD SKIN IS CRACKED @ APPROX. PPS 295 REMOVED #2 PYLON AFT LOWER HEAT SHIELD AND INSTALLED NEW HEAT SHIELD P/N 313N5042-11 PER BAC DWG 313N5042 REV FSDR JJBA20231004001Access Panel · damagedE1 2 ACCESS PANELS OPEN UPON LANDING. PERFORMED GVI OF E1. NO DEFECTS FOUND. INSPECTED E1 COWLING (INTERNALLY AND EXTERNALLY) AND SURROUNDING AREA. FOUND THE AIR START VALVE ACCESS PANEL AND THE OIL SERVICE PANEL WERE LEFT OPEN IN FLIGHT. NO DAMAGE WAS OBSERVESDR DALA2023100308107Unknown · unknownSHIP 3166 FOUND NBR 1 ENGINE PYLON PANEL HAS EROSION & SMALL HOLE. # 414FR. CORRECTIVE ACTION: REPAIRED PER ERA 612551-14. (4575918)SDR IPXA202312070001Skin · cracked#2 PYLON LH SIDE AT RIB11 UPPER SKIN PANEL HAS WELDED REPAIRED CRACK [T3F18E002SNR7]SDR DALA2023101808591Unknown · unknownSHIP 179 FOUND #2 ENG OUTBOARD NACELLE ACCESS PANEL MISSING. CORRECTIVE CATION: INSTALLED NACELLE STRUT ACCESS DOOR PER B767 AMM 54-33. DEFERRAL + PLACARD REMOVED (4191823)SDR IPXA2023092294229Panel · brokenINSPECTION TYPE:CPANEL 423BL INSIDE BROKENREPAIRED PANEL IAW SRM 54-52-51SDR 2023FA0000549Cover · missingDURING INCOMING INSPECTION OF THE SUBJECT AIRCRAFT, 1 COVER ON ENGINE NR 1 UPPER COWL FOUND MISSING, APPARENTLY FLEW AWAY DURING FLIGHT. SAME COVER ON ENGINE NR 2 UPPER COWL HAS BEEN FOUND DAMAGED.
ON BOTH COVERS, ONLY ONE FASTENER FOUND INSTALLED. LE UPON SDR FDEA202309131593Skin · corroded#1 PYLON PANEL 433HR HAS CORROSION ON AFT SURFACE OF THE PANEL FABRICATED NEW PANEL PER BAC DWG 311N5049 REV C AND FEDEX EA # F-5430-T0376029 TITLE: NACELLS/PYLONS - SKIN/PLATES/PANELS - #1 PYLON, STRUT ACCESS PANEL ASSY (443HR), FABRICATIONSDR CALA2023091402780Skin · crackedB767-54-3-7005 #1 PYLON STRUT EXTERNAL SKIN IS CRACKED AT AFT UPPER CORNER OF PANEL 416BR CUTOUT.SDR IPXA2023092094204Doubler · brokenINSPECTION TYPE:1CRH PYLON ON ACCESS PANEL 423BL BROKEN.FABRICATED REPAIR DOUBLER IAW SRM 54-52-51.SDR IPXA2023082494012Skin · crackedINSPECTION TYPE:CD809754: NO 1 PYLON FAIRING OB SIDE LOWER ATTACHMENT FASTENER CRACK EO 87447 "PERMANENT REPAIR"REPLACED CRACKED SKIN IAW SRM 51-40-21.SDR DALA2023081806737Unknown · unknownSHIP 171 NBR 1 ENGINE INBD NACELLE STRUT ROUND ACCESS DOOR MISSING. MEL NUMBER ADDED FOR DISPATCH RELEASE, LOG REDEFERRAL REQUIRED. CORRECTIVE ACTION: MCC NOTIFIED. FWD 54-53-02 CDLA/C OK FOR SVC. (4535898)SDR SWAA2023091389099Panel · delaminatedPANEL 434AL PANEL ASSEMBLY - AFT FAIRING - #1 ENGINE OUTBOARD STRUT WITH DELAMINATED CORNER.<[01] PREPARED REPAIR ON PANEL 434AL PANEL ASSEMBLY - AFT FAIRING - #1 ENGINE OUTBOARD; AS PERSRM 51-70-04-2R-6; AND REPAIRED PANEL 434AL PANEL ASSEMBLY - AFT FAIRING -SDR IPXA2023083100462Skin · corrodedFAULT- #2 ENGINE OUTBD PYLON INNER SKIN FWD OF PANEL 443CR OPENING HAS CORROSION. DOT 8-005. MAJOR REPAIR. REVIEWED.WORK ACCOMPLISHED PER UPS EO: EO-87945-REQ1 AND VTMAE EA 757-5450-27-A3326 REV1SDR IPXA2023082599526Skin · corroded#1 ENGINE PYLON INNER SKIN HAS EXFOLITATION CORROSION FWD OF THE VENT PANEL OPENING. DOT 8-001. AUDIT COMPLETE.ALL WORK ACCOMPLISHED PER EO-87960-REQ1 AND VT-MAE EA 757-5450-27-A3329SDR IPXA2023082500462Skin · corroded**SDR FILED OPEN**FAULT- #2 ENGINE OUTBD PYLON INNER SKIN FWD OF PANEL 443CR OPENING HAS CORROSION. DOT 8-005. AUDIT COMPLETE.SDR IPXA2023082500262Skin · corroded#1 ENGINE INBD PYLON INNER SKIN AFT OF THE SQUARE PANEL OPENING HAS EXFOLIATION CORROSION. DOT 8-004. MAJOR REPAIR. REVIEWED.VERIFIED WORK ACCOMPLISHED PER UPS EO-87954-REQ1 AND VTMAE 757-5450-27-A3328SDR IXXA2023080102Skin Panel · bulged#1 PYLON I/B STRUT FAIRING SKIN/ ARROWHEAD PANEL BULGEDSDR SWAA2023082483507Skin · corrodedL/H AFT STRUT FAIRING I/B SIDE AFT LOWER SKIN SURFACE HAS CORROSION.<[01] REMOVED AND REPLACED #1 PYLON STRUT AFT LOWER EDGE SKIN IN REF B737-700 SRM 51-40-02-0G-0 AND BOEING DRAWING #313A2750.;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2023082483506Skin · corrodedR/H AFT STRUT FAIRING I/B SIDE AFT LOWER SKIN SURFACE HAS CORROSION.<[01] REMOVED AND REPLACED R/H LOWER STRUT FAIRING EDGE IN REF B737-700 SRM 51-40-02-0G-0 AND BOEING DRAWING # 313A2750.;[02] VERIFIED STEP 1 COMPLETE.SDR ABXA20230814164Skin Panel · wornDURING C1 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE DISCOVERED WEAR DAMAGE TO AN EXISTING REPAIR AND THE STRUT SKIN ON THE OUTBOARD SIDE OF THE NO. 1 PYLON. SEE FIGURE 1 FOR DETAILS. THE EXISTING REPAIR WAS PERFORMED PER DAL SUPPLEMENTAL SRM 54-51-01. TSDR DALA2023071005572Unknown · unknownSHIP 3123 CRACK ACCESS PANEL 483AL ON RH PYLON. CORRECTIVE ACTION: COMPLIED WITH ER/A # 609699-14. (2858004)SDR ABXA20230814165Doubler · gougedDURING C1 MAINTENANCE CHECK AT HAECO AMERICAS, DURING C1 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED WORN AND GOUGE DAMAGE ON #1 PYLON INBD. CUT OUT (INTERNAL DOUBLER 311T1540-10) AT PANEL 436AR. DAMAGE WAS BLENDED WITH MINIMUM REMAINING MATERIALSDR CALA2023070302148Access Panel · missingENG NBR 1 OUTBOARD NACELLE STRUT ACCESS DOOR FOUND MISSING DURING WALK AROUND ENG 1 OUTBOARD NACELLE STRUT ACCESS DOOR DEFERRED IAW CDL 54D DEFERRED IAW CDL 54D MAINT PROCEDURE ACCOMPLISHED DISPATCH DESK: 64 NAME: DS, DATE: 02-JUL-23- PANEL 436AL MISSING. APPRSDR SWAA2023072559479Access Panel · crackedCRACK WEB LEADING EDGE ACCESS PANEL 341B LOC. STA 114.55 AT RT HORIZONTAL STABILIZER (1 EA) 2023-394553<[01] REPLACED WEB (RIB) LEADING EDGE ACCESS PANEL 341B LOC. STA 114.55 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 18SDR DALA2023061404860Unknown · unknownAIRCRAFT 682, AD RELATED DURING ROTO TEST OF ENGINE 1 UPPER SKIN, DRAG FITTINGS HOLE #8 WAS FOUND TO HAVE A CRACK IN THE FITTING LAYER, CRACK IN THE FITTING LAYER NOTED AT THE 8:00 POSITION. CORRECTIVE ACTION: ACCOMPLISHED EA #609176-14 AD ON L/H WING DRAG-FITSDR IXXA2023060105Skin · crackedINBOARD FWD CORNER OF #2 STRUT CRACKED.SDR SWAA2023070563553Panel · elongated#2 ENG INLET COWL LOWER ANTI ICE VENT ACCESS PANEL HAS ELONGATED HOLES AT FASTENER LOCATIONS<[01] LOCATED ; DRILLED AND PERFORMED COUNTERINK ON FASTENER HOLES REF. SRM 51-40-08-0G-0 ; REF. SRM 51-40-05-0G-0. APPLIED TOP COAT PAINT TO PANEL 422 AB REF. AMM 51-2SDR SWAA2023060254934Skin · cracked#2 ENG INLET COWLING LOWER SKIN IS CRACKED.<[01] R&R #2 ENG NOSE COWL PER AMM 71-11-01SDR IPXA2023053193341Skin · crackedINSPECTION TYPE:C#2 ENGINE AFT FAIRING 6 HOLES FROM AFT END IS CRACKEDREPAIRED WITH A DOUBLER IAW 54-50-00SDR IPXA2023053193340Skin · crackedINSPECTION TYPE:C#2 ENGINE AFT LOWER FAIRING HAS A CRACKREPAIRED WITH A DOUBLER IAW 54-50-00SDR IPXA2023053193339Skin · crackedINSPECTION TYPE:CD807756 #1 ENG OB LWR AFT FAIRING .500" L CRACK 9TH FASTENER FWD FROM AFT EDGE, CRACK IS FASTENER TO SKIN EDGEREPAIRED WITH A DOUBLER IAW 54-50-00SDR DALA2023062605123Unknown · unknownPYLON INBD NACELLE STRUT DOOR MISSING. CORRECTIVE ACTION: INSTALLED RT ENG PANEL 446AL PER B767 AMM 54-53 OK FOR SVC. CDL & PLAC RMVDSDR IXXA2023052201Skin Panel · cracked#1 PYLON O/B SKIN IS CRACKED AT THE 442AL SKIN CUTOUT.SDR CALA2023042801282Panel · missingENGINE NR 1, INBOARD NACELLE STRUT PANEL 436BR IS MISSING ONE LATCH. INSTALLED NEW PANEL 436BR ON I/B NACELLE STRUT REF AMM 54-53-00.SDR V0XD20230503001Doubler · dentedDENT UPPER LEFT INSIDE COWLING DAMAGED ON EXISTING DOUBLER FORWARD HINGE. CORRECTIVE ACTION REMOVED AND REPLACED EXISTING DOUBLER IAW EMB 145 SRM 51-40-02, EDT 2023 145-010-409-REV A.SDR COEA2023051608913Panel · chafedWO 242864 NR 400035 HEAVY CHECK COE/MAJOR REPAIR: L/H ENGINE NACELLE OUTBOARD REBATE PANEL FOR 475AL HAS CHAFE DAMAGE. CORRECTIVE ACTION: REPAIRED PER SRAS ES_00215296_01...20656 ISSUE A, DATED 5/5/2023.SDR VNAA202304270020Skin · corrodedCORROSION ON LEADING EDGE (LIP SKIN) OF RH ENGINE INLET COWL.SDR SWAA2023050125002Skin · cracked#1 I/B FAN COWL UPPER AFT SKIN IS CRACKED AT FASTENER HOLE; RIVET CRACKED AT HALF MISSING. MRKD PHOTO ATTACHED.<[01] REMOVED FAN COWL FOR REPLACEMENT.<BR>TRANSFERRED VCD IAW AMM 71-11-08;[02] FAN COWL REQUIRES INSTALLATION.;[03] VERIFIED CORRECTIVE ACTION STEPSDR SWAA2023042022957Skin · crackedREFERENCE FAULT TTG8Q00JXCVW; ON THE #2 LIP SKIN; THE FASTENER HOLE LOCATED AT THE 6 O'CLOCK POSITION HAS A CRACK INDICATION DURING HFEC HOLE PROBE INSPECTION.<[01] REAMED HOLE TO SECOND OVERSIZE (.199) PER SRM 54-10-01-1A-2;[02] C/W HOLE PROBE INSP. PER NDT MSDR VNAA202302040005Skin · corrodedCORROSION ON LEADING EDGE (LIP SKIN) OF RH ENGINE INLET COWL
LEADING EDGE (LIP SKIN) OF RH ENGINE INLET COWL WAS REPAIRED PER EA 23-C9-55-0324 REV. IR.SECTION III-PERMANENT REPAIRSDR COEA2023051604913Skin · corrodedNTERNAL FUSELAGE SKIN BETWEEN FRAMES 23-24 AND STRINGERS 2AR-3R HAS LEVEL 2 CORROSION. REPAIRED PER SRAS ES_00214692_01...20657 ISSUE A, DATED 5/9/2023.
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