JASC 5414
Service difficulty reports · 4,360
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 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.SDR DALA2023030801733None · noneSHIP 1707 #2 ENG - I/B PYLON SKIN CRACKED AT PANEL CUTOUT. CORRECITVE ACTION: C/W ERA 606707-14 REV ORIG. SECT. 1 PERM. REPAIR. ASSOCIATED ER/A 14-606707 ADDED FOR AC 1707 (2658722)SDR DALA2023030801730None · noneSHIP 1707 DUE PRI 03-03-2023, 1945 EST. (606707-14). CORRECITVE ACTION: RECEIVED FINAL ER/A 606707-14, REV. ORIG., COMPARED PRI 03-03- 2023, 1945 EST. TO ER/A 606707-14, REV. ORIG. AND FOUND TO MATCH (2658725)SDR IPXA2023032192094Skin · damagedINSPECTION TYPE:C3*MAJOR REPAIR* #2 ENGINE PYLON LEFT SIDE ENGINE MOUNT BULK HEAD ACCESS PANEL OVERSIZED HOLES, REPAIR AT STA YID 546.559 REF EO MD-11 5430-83790-AREPAIRED #2 PYLON SKIN OVERSIZED HOLES AT STA YID 546.559 IAW EA 011-5430-01-A9834 REV I/R DATED SDR DALA2023022401377None · noneSHIP 191 #1 ENG PYLON IS CRACKED ON INBD SIDE AT FWD ACCESS HOLE. CRACK IS APPROX 1.75 INCHES- MARKED. CORRECTIVE ACTION: DAMAGE AREA REPAIRED PER B767 SRM 54-53-01. (2634216)SDR DALA2023021601218None · noneSHIP 5812 CORROSION ON EXTERNAL SKIN BTW NAC STA 215- 272 AT RH PYLON (OUTBOARD/INBOARD FACES). CORRECTIVE ACTION: SUMMARY OF NRC:00160 EXTERNAL SKIN BTW NAC STA 215-272 AT RH PYLON (OUTBOARD/INBOARD FACES) WERE REPAIRED PER ER/A 605995-14 REV. ORIGINAL AND PRSDR SWAA2023021395228Cowling · elongated# 2 ENGINE NOSE COWL INLET SKIN HAS ELONGATED FASTENER HOLE AT 9 O'CLOCK POSITION AND 7.5' AFT OF FORWARD EDGE OF SKIN.(51-021)<[01] #2 ENG INLET COWL TO BE REPLACED ON TASK CARD NUMBER TTG8Q00HG69C.;[02] VERIFIED STEP 1SDR SWAA2023021395227Cowling · elongated# 2 ENGINE NOSE COWL INLET SKIN ATTACH STRAP HAS ELONGATED FASTENER HOLE AT 9 O'CLOCK POSITION AND 6' AFT OF FORWARD EDGE OF STRAP. (51-022)<[01] #2 ENG INLET COWL TO BE REPLACED ON TASK CARD NUMBER TTG8Q00HG69C.;[02] VERIFIED STEP 1SDR IXXA20230506001Skin Panel · corrodedENG #1 NACELLE STRUT - INBOARD PRESSURE RELIEF DOORS INTERNAL STRUCTURE, FOUND CORROSION. REFERENCE XTREME AVIATION NON - ROUTINE 432. WORK ORDER # 009657.SDR UIEA2023011200025Skin · crackedCRACK ON LH STRUT OUTBD SKIN PANEL BETWEEN NAC STA 221.25 / NAC / STA 237.5 (CUTOUT FOR ACCESS PANEL 432AL).(<P>REPAIR WAS ACCOMPLISHED PER BOEING SR# 3-5510858364.</P>)SDR HNAA2023013000028Skin · chafedLEFT PYLON SKIN CHAFED INSIDE 414DB. REPAIRED L/H PYLON SKIN CHAFE INSIDE 414DB IAW EO1-53-23-0006.SDR HNAA2023013000027Skin · chafedLT PYLON SKIN CHAFED INSIDE 414DB. REPAIRED LT PYLON SKIN CHAFE INSIDE 414DB IAW EO1-53-23-0006.SDR IPXA2023012090085Skin · corrodedINSPECTION TYPE:SEG1#1 ENGINE INSIDE O/B FWD PYLON DOOR 433BL BOTTOM RIM IS BULGINGREMOVED SKIN PANEL PER SRM 51-40-02-0G, REMOVED CORROSION AT SKIN PANEL PER SRM 54-50-01-1A DETAIL V ORIG THICKNESS 0.188 AFTER BLENDED THICKNESS IS 0.169 FOUND IN LIMITS PER SRSDR IPXA2023011990059Skin · corrodedINSPECTION TYPE:SEG1#1 ENGINE INSIDE O/B PYLON (PPS 124.76) IS SHOWING SIGNS OF CORROSION. REPAIRED PER RCD 264950 AND EA 757-5450-27-A3114 REV-SDR FDEA202301030012Skin · corrodedNR 1 PYLON AFT LT SIDE EXTERNAL SKIN FASTENERS ARE CORRODED. REMOVED AND REPLACED FASTENERS IAW DWG 313N3021 REV E.SDR SWAA2023021387201Cowling · pulledRH INLET COWL OUTER LIP SKIN AT 5 O'CLOCK TO 7 O'CLOCK HAS SEVERAL FASTENERS PULLED IN (14 EA)<[01] #2 ENG INLET COWL TO BE REPLACED ON TASK CARD NUMBER TTG8Q00HG69C.;[02] VERIFIED STEP 1SDR SWAA2023021387200Cowling · pulledRH INLET COWL OUTER LIP SKIN AT 11 O'CLOCK HAS TWO FASTENERS PULLED IN.<[01] #2 ENG INLET COWL TO BE REPLACED ON TASK CARD NUMBER TTG8Q00HG69C.;[02] VERIFIED STEP 1SDR SWAA2023021387202Cowling · pulledRH INLET COWL OUTER LIP SKIN AT 2 O'CLOCK HAS THREE FASTENERS PULLED IN.<[01] #2 ENG INLET COWL TO BE REPLACED ON TASK CARD NUMBER TTG8Q00HG69C.;[02] VERIFIED STEP 1SDR SWAA2023021387203Cowling · pulledRH INLET COWL OUTER LIP SKIN AT 4 O'CLOCK HAS TWO FASTENERS PULLED IN.<[01] #2 ENG INLET COWL WILL BE REPLACED ON TASK CARD NUMBER TTG8Q00HG69C.;[02] VERIFIED STEP 1SDR DALA2022122708382Drag Fitting · damagedDAMAGE FOUND ON OPEN HOLES AT RT ENG DRAG FITTING CLAMP-UP & DIAG BRACE, HOLE 4 CRACK ON SKIN BTW 8 O CLOCK POSITION AND HOLE 8 CORROSION ON SKIN BTW 7 TO 8 O CLOCK POSITION IAW CARD. OPEN HOLES AT RT ENGINE DRAG FITTING HOLE 4, HOLE 5 AND HOLE 8 WERE REPAIRSDR DALA2022122008242Access Door · missingSHIP 177 RT ENG OUTBOARD NACELLE STRUT ACCESS DOOR MISSING. CORRECTIVE ACTION: DEFERRED & PLACARDED THE THE RT ENG OUTBOARD NACELLE ACCESS DOOR AS PER CDL 54-53-02. DISPATCH APPROVED. (9925200)SDR MK1Y20221211005Skin · scratchedFOUND MULTIPLE SCRATCHES (28 TOTAL) ON EXTERIOR CORE COWL SKIN ENG.1 OUTBD SIDE BETWEEN 9 TO 11 CLOCKWISE. SCRATCHES AREA SMOOTHED OUT IAW SRM 51-10-02. FASTENERS REMOVED FROM THE BLENDED AREAS IAW SRM 51-40-02. HFEC INSP PERFORMED AND NO CRACK OR CORROSION WESDR MK1Y20221211004Skin · scratchedFOUND MULTIPLE SCRATCHES (9 TOTAL) ON EXTERIOR CORE COWL SKIN ENG.1 INBD SIDE BETWEEN 2 TO 3 CLOCKWISE. SCRATCHES AREA SMOOTHED OUT IAW SRM 51-10-02. FASTENERS REMOVED FROM THE BLENDED AREAS IAW SRM 51-40-02. HFEC INSP PERFORMED AND NO CRACK OR CORROSION WERE SDR MK1Y20221211003Skin · scratchedFOUND MULTIPLE SCRATCHES (27 TOTAL) ON EXTERIOR CORE COWL SKIN ENG.2 OUTBD SIDE BETWEEN 2 TO 6 CLOCKWISE. SCRATCHES AREA SMOOTHED OUT IAW SRM 51-10-02. FASTENERS REMOVED FROM THE BLENDED AREAS IAW SRM 51-40-02. HFEC INSP PERFORMED AND NO CRACK OR CORROSION WERSDR FDEA202212090131Skin · crackedNR 2 ENG INLET DUCT, L/H LWR FAN COWL DOOR LAND WORN AND CRACKED. (MARK) 0003749939 : EGASHIRA, JUN - 18-JAN-2023 14:20 REMOVED SKIN PANEL AJC7415-157 FROM ASSEMBLY AJC7415-159 IAW MD11 SRM 51-31-01-0G/ MD11 SRM 51-35-01-0G. FABRICATED SKIN PANEL AJC7415-SDR DALA2022121508136Access Door · missingSHIP 1814 LH INBD NACELLE STRUT ACCESS DOOR MISSING. CORRECTIVE ACTION: INSTALLED LH INB NACELLE STRUT ACCESS DOOR PER B767-400 AMM 54- 53. CDL AND PLACARD REMOVED (9185730)SDR DALA2022120607797Access Panel · missingSHIP 1200 RT PYLON OUTBD SIDE ROUND ACCESS PNL MISSING, INSTALLED NEW COVER RT PYLON CDL AND PLACARD REMOVED.SDR DALA2022120507786Panel · corrodedCORROSION ON FWD EDGE OF INB COWL PANEL ENGINE #1. INBOARD FAN COWL PANEL WAS REMOVED IAW AMM 71-11-04 AND SERVICEABLE INBOARD FAN COWL PANEL WAS REPLACED IAW AMM 71-11.SDR DALA2022120607795Access Door · missingSHIP 181 RT PYLON INBOARD SIDE NACELLE STRUT ACCESS DOOR MISSING. CORRECTIVE ACTION: REPLACED ACCESS DOOR ASSY REF B767-300 IPC 54-53-01-01 (9164456)SDR DALA2022112907596Access Panel · crackedSHIP 198 FOUND RH PYLON RH SIDE ACCESS PANEL 426BR CUT OUT CRACK. CORRECTIVE ACTION: CARRIED OUT THE REPAIR TO THE CRACK SKIN AT RH PYLON RH SIDE ACCESS PNL 426BR CUT OUT AREA AS PER B767-300 SRM54-53 (2511306)SDR 2022F00469Access Panel · corroded#2 PYLON ACCESS PANEL 5843 CORRODEDSDR JJBA20221122020Skin · corrodedRH PYLON, FUSELAGE SKIN WORN BY FRETTING FROM LANYARD BETWEEN FR67 AND FR68 AND STGR 07R. REPAIR DOUBLER ON RH REAR FUSE 1 SKIN, BTW FR 67-68 AND BTW STR 7R-8RSDR IPXA2022111188045Panel · crackedINSPECTION TYPE:SEGENG #2 PTLON PANEL 485AL OB SIDE AFT ATTATCHMENT AREA HAS A CRACK.REPAIRED PANEL 485AL PER EO NO A300-5450-21297-L.SDR IXXA2022110800010Skin · corroded#2 PYLON LEADING EDGE PANEL CORRODED SEVERAL SPOTS ON REPAIR RACK.SDR IXXA2022110800009Skin · corroded#2 PYLON THRU ACCESS PANEL 443CR INTERNAL SKIN HAS CORROSION FWD AND BELOW CUTOUT.SDR IXXA2022110800008Skin · corroded#2 PYLON ACCESS THRU PANEL 443HL LOWER FORWARD CORNER STRUCTURE INTERNALLY HAS CORROSION.SDR IXXA2022110800003Skin · corrodedPREVIOUS REPAIR ON LEFT WING UPPER SKIN AT WS 150.5 THRU WS 204.5 NEEDS REACCOMPLISHED PER AMES REA 47508REA41 AND FVCI ENGINEERING ORDER 22082-22 REV C.SDR IXXA2022110800001Skin · corrodedNUMBER 2 PYLON THRU ACCESS PANEL 443AR INTERNAL SKIN LWR SECTION AROUND OPENING HAS CORROSION.SDR FDEA202211022712Panel · cracked#1 PYLON PANEL 434DR HAS A CORNER CRACKED REPAIRED #1 PYLON PANEL 434DR CRACKED CORNER WITH 350 DEGREE REPAIR IAW B757 SRM 54-50-70-2R FIG 201 REPAIR 1 SHEET 3, 51-40-02,51-70-04,54-50-70-0IAND AMM 51-24-02-7, 51-21-00/701, B757NDTM PART 1 51-01-01.SDR FDEA202211012702Skin · damagedWHILE WORKING #1 O/B T/R C DUCT CHANGE FOUND DAMAGE ON UPPER PORTION OF INBOARD #1 ENG FAN COWL REPAIRED IAW EA F-7110-T0371402 THIS IS A MAJOR REPAIRSDR SWAA2022111666585Access Panel · crackedCRACK AFT STRUT FAIRING IB ACCESS PANEL AFT UPPER FASTENER HOLE AT LT PYLON. REPAIRED AFT STRUT FAIRING I/B ACCESS PANEL AT LT PYLON IAW SRM 51-70-04-2R-10 REPAIR 10.SDR JR2R20221029732Skin · chafedWING LE PANEL ABOVE #1 PYLON CHAFEDSDR IPXA2022110387788Skin · crackedINSPECTION TYPE:C13, CRACK DAMAGE WAS FOUND ON NR 1 PYLON OUTBD SKIN ASSEMBLY (P/N:311T2450-25) NEAR NAC STA 237.5. PERFORM REPAIR I.A.W UPS EO B767-5430-85116-ASDR IPXA2022102587510Access Panel · crackedINSPECTION TYPE:CENG #1 ACCESS PANEL 413BL HAS CRACKS.INSTALLED PANEL 413BL ON ACCESS 10Y IAW SRM 54-52-51SDR IPXA2022102587501Skin · crackedINSPECTION TYPE:SEG, #1 ENG PYLON LOWER AFT ACCESS PANEL 475AL AFT LH UPPER SKIN IS CRACKEDREPAIRED [WELDED] SKIN PER SERO EO NO A300-5420-21297-L THIS REPAIR IS CONSIDERED PERMANENT NO SUPPMENTAL INSP REQUIREDSDR IXXA2022102200002Access Panel · corroded# 2 PYLON ACCESS THRU PANEL 433GL INTERNAL SKIN LOWER SECTION AROUND PANEL HAS CORROSION.SDR IXXA2022101805Skin · corroded# 1 PYLON INBOARD SIDE INTERNAL SKIN AROUND PANEL 433LR HAS CORROSION IN MULTIPLE AREAS.SDR IXXA2022101804Skin · corrodedNUMBER 1 PYLON INBOARD SIDE FORWARD EXTERNAL SKIN REQUIRES REMOVAL FOR CORROSION.
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