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 2021FA0000213Cowling · delaminatedLH ENGINE UPPER COWLING IS DELAMINATED FROM B/A LEAKS. TEXTRON AVIATION STRUCTURES ENGINEERING DOCUMENT DQ30702M1 DATED JULY 16, 2021.SDR IPXA2021072972243Skin · crackedNR 2 ENG PYLON PANEL 485AL OB UPPER AFT SKIN HAS A CRACK.REPAIRED FAIRING IAW SREO A300-5450-21297-I PERMANMENT REPAIR. NO 2 ENG PYLON PANEL 485AL OB UPPER AFT SKIN HAS A CRACK.REPAIRED FAIRING IAW SREO A300-5450-21297-I PERMANMENT REPAIR.SDR IPXA2021072271936Skin · crackedINSPECTION TYPE:C12CRACK DAMAGE WAS FOUND ON NO.1 PYLON OUTBD SKIN ASSEMBLY (P/N:311T2450-25) NEAR NAC STA 237.5PERFORM REPAIR I.A.W. BOEING SR 4-5188323591 AND UPS EO B767-5430-81058-ASDR CALA2021071201072Panel · missingPDA 3 #2 ENG STRUT PANEL 441DL MISSING ONE FASTENER. INSTALLED NEW FASTENER ON PANEL 441DL - REF IPC 54-52-03-01SDR SWIA2021081960417Skin · chafedRH UPPER TRANSCOWL OUTBOARD LEADING EDGE SKIN, INNER SURFACE UNDER LATCH DOUBLER IS CHAFFED. (C-CHECK RO 8/18/2021) REPAIRED RH UPPER TRANSCOWL OUTBOARD LEADING EDGE SKIN REF REO 670-54-21-1456 REV -A DATED 2021-08-12. COMPLIED WITH TASK CARD 51-900-10SDR DALA2021071203900Access Panel · crackedSHIP 3131 CRACK ACCESS PANEL 423DL ON RH PYLON. CORRECTIVE ACTION: REPAIRED ACCESS PANEL 423DL AT PYLON R/H AS PER ER/A #540187-14MA REV. ORIGINAL; A319 SRM TASK 54-52-11. (1869615)SDR REXA2021080600543Skin · gougedLEFT ENGINE LOWER AFT COWL HAS MULTIPLE GOUGES AND CHAFFED SPOTS JC:900 54-900-102 - REPAIRED DAMAGE AREAS TO L/H ENGINE LOWER AFT COWL IAW CRJ900 EANO. CRJ 954-11856SDR IPXA2021070871415Skin · crackedINSPECTION TYPE:C13CRACK DAMAGE WAS FOUND ON NO.2 PYLON INBD SKIN ASSEMBLY (P/N: 311T2450-25) NEAR NAC STA 237.5PERFORM REPAIR I.A.W. BOEING SR 4-5166544262 AND UPS EO B767-5430-80938-ASDR CALA2021070101008Skin · crackedPANEL IDENTIFIED ON R-315 AS "LEADING EDGE ABOVE PYLON" SKIN CRACKED IN CORNER(ON REPAIR RACK) FABRICATED NEW SKIN PANEL IAW DWG114N1802 REV L AND B757 BAC 530 0-2 REV J PARAGRAPH 8.2.1 FIG 3. INSTALLED WEBS AND SECURING BRACKETS IAW 51-40-02 PARAGRAPH 5 AND DSDR REXA2021080600544Skin · gougedRIGHT ENGINE LOWER AFT COWL HAS MULTIPLE CHAFED SPOTS AND GOUGES JC:900-54-900-102 - REPAIRED R/H ENGINE LOWER AFT CORE COWL IAW BOMBARDIER REO670-54-23-959 REV E, AND CRJ900 SRM 54-23-00.SDR V0XD20210716001Skin · crackedL/H ENGINE UPPER TRANSCOWL EXTERNAL SKIN AT FWD LATCH IS CRACKED. CORRECTIVE ACTION: CUTOUT DAMAGE, NDT, FABRICATED AND INSTALLED REPAIR PARTS IAW STS ENGINEERING EA# 72-20-21-116 REV IR, DATED 7/11/2021. WORK WAS PERFORMED ON AVMAX W/O:80943 W/C:4099SDR IPXA2021062871077Access Panel · crackedINSPECTION TYPE:A300ACCESS, PANEL 424AR EXTERNAL SURFACE WITH DENTREMOVED AND REPLACED 424AR P/N A7521502500300 IAW AMM 54-52-61-04-01SDR IPXA2021062370911Panel · crackedINSPECTION TYPE:A300PANEL RACK PANEL 413BL HAS A CRACKREPAIRED IAW 54-52-51-PARA 5.E FIGURE205SDR MK1Y20210614003Skin · damagedCORE COWL P/N 224-2302-545, S/N 3481001: SHOP FOUND THREE (3) DAMAGES IN INB’D EXTERNAL SKIN NAC STA 303.75 POSITION. THE DAMAGES ARE DESCRIBED AS FOLLOWS: M0186: 2.00” SCRATCH IN THE AFT EDGE OF THE EXTERNAL SKIN BETWEEN 5 AND 6 O’CLOCK POSITIONS. M0187: RIVSDR UIEA2021061101316Skin · dented# 2 ENG. INLET COWL HAS A DENT AT LOWER NOSE LIP AREA(<P>FOUND DENT WITH IN LIMITS 1.5 MINOR AXY BY .050 DEPTH EQUAL 30 PWER B767-300 SRM 54-13-01-1A-1. PERFORMED NKT, HFEC INSPECTION OF THE DENT AREA. NO CHECK INDICATION NOTED REF NDTM PART 6 51-00-01.<SDR FDEA202106111504Skin · corroded#1 PYLON I/B FWD HINGE PANEL LANDING IS EXFOLIATED REPAIRED DAMAGE IAW FEDEX EA # F-5430-T0362060 NACELLES/PYLONS - SKIN/PLATES/PANELS - #1 PYLON INBD SKIN PANEL, PP STA 120, INNER SURFACE, CORROSION REPAIR.SDR SWAA2021072681082Retainer · crackedCRACK SEAL RETAINER ACCESS PANEL 441AR ON RT ENGINE ; 2021-269599 / [01] REPLACED SEAL RETAINER ACCESS PANEL 441AR ON RT ENGINE IAW B737-700 SRM 51-40-02 TOOL USED CALIPER P/N: 500-197-30 S/N: A18234376 DUE DATE 30-JUL-21; [02] REPLACED SEAL RETAINER ACCESS PASDR DALA2021060803131Access Panel · damagedSHIP 3247 ELONGATED HOLE ACCESS PANEL 424CR ON RH PYLON. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 591929-14 REV.0 AND ER/A 591929-14 REV.ORIGINAL. (1832910)SDR IPXA2021062170854Landing · crackedINSPECTION TYPE:SEG#1 ENGINE PYLON PANEL 413BL FWD LANDING STRUCTURE IS CRACKED.REPAIR LANDING STRUCTURE IAW A300 SRM 54-50-00 CONFIG. 1SDR IPXA2021061770715Panel · crackedINSPECTION TYPE:SEG#2 ENGINE PYLON PANEL 423BL INSIDE SURFACE CRACKED AT CORNER AREAREPAIRED PANEL 423BL INNER CORNER AREA PER ARM 54-52-51 REPAIR 204SDR IPXA2021061770693Panel · crackedINSPECTION TYPE:SEG#2 ENG PYLON PNL 423BL FWD LANDING STRUCTURE CRACKEDWELDED REPAIR CRACK REINSTALLED PART IAW SRM 51-40-21SDR CALA2021053100764Panel · detachedPDA 1 LP 6301347, #2 ENGINE, INBOARD PYLON PANEL DEPARTED AIRCRAFT ON LANDING @ RSW. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN INSTALL NEW PANEL, ARRIVES AT 20:05 FLT 0401 INSTALL NEW PANEL, ARRIVES AT 20:05 FLT 0401 UPDATED MAA CODE FIX USING VENDOR MAA SCSDR IPXA2021061870722Landing · crackedINSPECTION TYPE:C#1 PYLON PANEL 413BL FWD LANDING STRUCTURE CRACKEDREPAIRED IAW SRM 54-50-00-101 FIG 107 ON VTMAE TRAVELER T21/1556922SDR SWIA2021081060301Skin · dentedRH LOWER TRANSCOWL OUTER SKIN DENT. 6 O€™CLOCK. (C-CHECK RO 8/9/2021) EVALUATED RH LOWER TRANSCOWL OUTER SKIN DENT. 6 O€™CLOCK DEPTH.036" LENGTH .300"WIDTH .300" FOUND TO BE OUT OF LIMITS DUE TO THE FACT ONLY ALLOWED A DEPTH OF .028" TOOL #TUC8531 DUESDR MK1Y20210519008Skin · corrodedDURING MAINTENANCE INSPECTION FOUND LARGE PITTING CORROSION AREA ON ENGINE #1 R/H CORE COWL EXTERNAL SKIN BETWEEN 2-6 O'CLOCK AND FIVE CRACKS AT APP. 2 O'CLOCK BELOW THE PRECOOLER.SDR MK1Y20210519004Skin · crackedDURING MAINTENANCE INSPECTION A CRACK OF APP. 1.10" FOUND ON ENGINE #1 L/H CORE COWL EXTERNAL SKIN AFT EDGE ON EXISTING FASTENER HOLES.SDR MK1Y20210519001Skin · damagedDURING MAINTENANCE INSPECTION CRACK OF APP. 1.14" FOUND AT AFT EDGE OF EXTERNAL SKIN ON 3/16" FASTENER HOLE.SDR 6PMR202105290001Skin · damagedAIRBORNE/PEMCO NON-ROUTINE 10830.0307 DISCREPANCY: #1 ENG. O/B CORE COWL, INTERNAL FWD. LOWER CORNER HAS DAMAGE. CORRECTIVE ACTION: ACCOMPLISHED REPAIR ON #1 ENGINE O/B CORE COWL, FIRESHIELD AT NAC STA 258.42 IAW ENGINEERING AUTHORIZAION PD 57-54-022 AND FAA SDR IPXA2021051769488Skin · crackedINSPECTION TYPE:SEG#1 ENG. PYLON HAS MULTIPLEREPAIRED IAW SRM 54-52-51SDR DALA2021051702726Skin · damagedSHIP 667 A.A. DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP AS FOLLOW; HOLE #3 SCRATCHES ON SKIN AND FITTING AT 9 OCLOCK POSITION, HOLE #5 CORROSION ON SKIN AND FITTING BETWEEN 1 AND 2 OCLOCK POSITION PER CARD. CORRECTIVE ACTION: SUMMARY: OF NRCSDR DALA2021052002804Access Door · missingSHIP 180 #2 ENGINE PYLON INBOARD SIDE STRUT ACCESS DOOR MISSING. REPLACED NACELLE STRUT ACCESS DOOR. (LP 7453271)SDR V0XD20210611002Skin · crackedL/H NACELLE LOWER COWLING PANEL 433AL HOUSING CRACKED. CORRECTIVE ACTION: PERFORMED REPAIR AT L/H LOWER NACELLE HOUSING FOR PANEL 433AL IAW STS EA 20-2021-109 REV IR, DATED 06/02/20201SDR V0XD20210611001Skin · crackedL/H NACELLE UPPER COWLING PANEL 433AL HOUSING CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED HOUSING FOR PANEL 433AL IAW CRJ 900 SRM 51-42-13 AND SRM 51-42-06.SDR UIEA2021050101041Fastener · worn#1 ENG PYLON HAS HYD RESERVOIR ACCESS PANELS WITH SMOKING RIVETS AT CLOSING LATCH POSITIONS ON I/B AND O/B SIDES (SAIL BOATS)(<DIV>REPLACED LOSSE FASTENERS AT #1 ENG PYLON BY ACCESS PANELS I/B AND O/B SIDE OF SAILBOATS PER B767-300 SRM 51-40-02-06-0.</DIV>)SDR IPXA2021061870721Landing · crackedINSPECTION TYPE:C#2 PYLON PANEL 423BL FWD LANDING STRUTURE CRACKEDREPAIRED IAW SRM 54-50-00-101 FIG 107 ON VTMAE TRAVELER T21/1556920SDR SWAA2021051967577Skin · chafed431 EL EXTERIOR CHAFED (MARKED) / NO APPLICABLE SRM ALLOWABLE DAMAGE FOR THIS PANEL. RPELACED PER SRM 51-10-02. PANEL INSTALLED ON SAM 565SSDR DALA2021050302502Skin · erodedSHIP 687 INITIAL INSPECTION: EROSION ON OUTB FAN COWL LEADING EDGE LOWER SECTION AT RH ENGINE. CORRECTIVE ACTION: SUMMARY OF N.R.C. 00288: OUTB FAN COWL LEADING EDGE LOWER SECTION AT RH ENGINE WAS REPAIRED PER B-757-200 S.R.M. (1793339)SDR IPXA2021050168830Skin · crackedINSPECTION TYPE:C12CRACK DAMAGE WAS FOUND ON NO.2 PYLON INBD SKIN ASSEMBLY(P/N:311T2450-25)NEAR NAC STA 237.5.PERFORM REPAIR I.A.W BOEING SR 4-5055536830 AND UPS EO B767-5430-80224-ASDR UIEA2021042200973Bolt · loose# 1 ENG HAS WIRE BUNDLE CLAMP NOT SECURED (BOLT MISSING) @ 11 O' CLOCK POS. JUST FWD OF MAIN HYD. LINE .(<P>REMOVED AND REPLACED MISSING BOLT PER MM 20-11-00.</P>)SDR DALA2021042202343Skin · damagedSHIP 667 .A. CORROSION AND SCRATCHES WERE FOUND ON HOLE #9 ON SKIN AND FITTING AT 9 O?CLOCK POSITION, SCRATCHES AND CORROSION WERE FOUND ON HOLE #10 ON SKIN AT 5 O?CLOCK POSITION PER CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00285: HOLES # 9 AND # 10 WERE REAMEDSDR DALA2021042202342Skin · damagedSHIP 672 (A.A)INITIAL INSPECTION:DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #1 SCRATCH ON FITTING BTW 8 TO 11 O CLOCK POSITION, HOLE #2 SCRATCH ON FITTING BTW 10 TO 11 OCLOCK POSITION, HOLE #4 CORROSION ON SKIN ANSDR DALA2021042202341Skin · damagedSHIP 672 GVI WAS ACCOMPLISHED IN RH DRAG FITTING HOLES #1, #2,#4, #5, #6, #7, #9 & #10. AND RESULTS ARE AS FOLLOW: HOLE #1 SKIN PRESENTS CORROSION AT 12: 00, 10:00 AND 06:30 CLOCK POSITIONS, SCRATCHES AT 11:00 OCLOCK POSITION, FITTING PRESENTS CORROSION AT 12:SDR SIMA202105110007Skin · chafedLH PYLON SKIN CHAFFED BETWEEN FR 67-68 AND STGR 7L-8L INSIDE 414DB-C/A-REPAIRED FUSELAGE SKIN INSIDE LH PYLON BETWEEN FRAMES 67-68 AND STRINGERS 7L-8L IAW EMB 145 SRM 53-31-01SDR UIEA2021042000939Skin · damagedINLET COWL ON # 2 ENG FOUND DAMAGED.(<P>REMOVED AND REPLACED # 2 ENG INLET COWL PER B767 AMM 71-11-01.<BR /></P>)SDR 9JLA2021041624289Skin · crackedTHE MAINTENANCE TEAM DISCOVERED DURING THE POSTFLIGHT CHECKLIST THE LEFT PYLON LOWER SHIN HAD A 3 INCH LONG CRACK. THE LEFT LOWER PYLON PANEL WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED ON THE PYLON PANEL. THE PANEL WAS REINSTALLED ONTO AIRCRAFT AND THESDR IPXA2021042168486Panel · crackedINSPECTION TYPE:A300#1 ENGINE PYLON PANEL 412BL HAS 4EA CRACKREPAIRED IAW SRM 54-52-51 FIG 205SDR IPXA2021042168485Skin · crackedINSPECTION TYPE:A300#2 ENGINE PYLON 423BL HAS 2EA CRACKREPAIRED IAW SRM 54-52-51 FIG 205SDR QXEA2021041100179Drain Mast · missingR/H NACELLE AFT I/B MLG DOOR P/N 85424003-001 DRAIN MAST FOUND MISSING . DRAIN MAST REQ REPAIR WITHIN 60 FH IAW DRAWING 85424003. 4/15/2021, REMOVED & REPLACED R/H NACELLE AFT I/B MLG DOOR DRAIN MAST. REF Q400 SRM 51-42-05-02-01 & DRAWING 85424003. PLACARD RSDR SWIA2021062859016Doubler · chafed*RH ENGINE UPPER TR COWL LATCH RECEPTICAL INTERNAL DOUBLER CHAFED THROUGH AT LEADING EDGE. (C-CHECK RO 6/22/2021) EVALUATED CHAFE DAMAGE AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED R/H ENGINE UPPER TR COWL INTERNAL DOUBLER. REF. REO 670-54-21-12SDR SWIA2021062859015Doubler · chafed*LH ENGINE LOWER TR COWL FWD LATCH RECEPTICAL INTERNAL DOUBLER CHAFED THROUGH AT LEADING EDGE. (C-CHECK RO 6/22/2021) EVALUATED CHAFE DAMAGE AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED L/H ENGINE LOWER TR COWL INTERNAL DOUBLER. REF. REO 670-54-
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