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.

SDR DALA2020022311344Plate · missingTHE #2 ENG UPPER COWL HAS A PLATE MISSING ON THE INBOARD SIDE. MAINTENANCE ACCOMPLISHED A TIME LIMITED REPAIR, PER ER/A 547093-14MA AND DEFERRED THE PERMANENT REPAIR TO MONITOR TO BE ACCOMPLISHED WITHIN 10 CALENDER DAYS OF SECT 1 ACCOMPLISHMENT. MONITOR,#2 ENGFeb 20, 2020 · N948AT · Boeing 717200SDR DALA2020022301341Skin · damagedNBR 2 ENG UPPER COWL DAMAGED. REPLACED UPPER COWL ON NBR 2 ENG AS PER MD88 AMM 71-10. SEE LOG 6860834 FOR REF. A/C OK FOR SERVICE. DOOR, ENGINE, OFF 03-7110-9-0006 S/N 49644. (LP6860836)Feb 19, 2020 · N916DL · Doug MD88SDR IPXA2020021752207Panel · crackedINSPECTION TYPE:SEG#1 PYLON PANEL 413CL HAS CRACKREPAIRED PANEL 413CL IAW SRM 54-50-00.Feb 17, 2020 · N131UP · Airbus A300F4622RSDR IPXA2020021752206Panel · crackedINSPECTION TYPE:SEG#2 PYLON PNL 423CL HAS CRACKREPAIRED 432CL IAW SRM 54-50-00Feb 17, 2020 · N131UP · Airbus A300F4622RSDR RAIA2020022460001Skin · gougedL/H FUSELAGE SKIN HAS GOUGES INSIDE OF L/H PYLON BETWEEN FR 67-68.... REPAIRED PER ETD EO-EMB145-53-073-R1 AND ETD2020-145-005726Feb 16, 2020 · N21130 · Emb EMB145XRSDR CALA2020021600421Skin · crackedDURING ROTO INSP CRACK INDICATIONS NOTED AT PYLON (#13 FASTENER HOLE) RIGHT WING SKIN DRAG FITTINGS AREA, CRACK POSITION :- 7:O''CLOCK; CRACK DEPTH :- 0.323"; CRACK SIZE :- 0.030" REF. AAR N/R 9756220 SEE ECRA 5720-03164 R/H WING UPPER SKIN, FWD DRAG FITTINFeb 12, 2020 · N598UA · Boeing 757222SDR CALA2020021600420Skin · crackedDURING NDT HFEC ROTO INSPECTION OF #2 PYLON UPPER SKIN AT DRAG FITTING IAW NDTM PART 6, 51-00-16 CRACK INDICATIONS WERE FOUND AT HOLE #9 - CRACK POSITION :- 7:O''CLOCK; CRACK DEPTH :-0.315"; CRACK SIZE :-0.060" REF. AAR N/R 9756199 SEE ECRA 5720-03164 R/H WFeb 12, 2020 · N598UA · Boeing 757222SDR CALA2020021600419Skin · crackedDURING NDT HFEC ROTO INSPECTION OF #2 PYLON UPPER SKIN AT DRAG FITTING IAW NDTM PART 6, 51-00-16 CRACK INDICATIONS WERE FOUND AT HOLE #3 - CRACK POSITION :- 10:O''CLOCK; CRACK DEPTH :- 0.394"; CRACK SIZE :- 0.030" REF. AAR N/R 9756198 SEE ECRA 5720-03164 R/HFeb 12, 2020 · N598UA · Boeing 757222SDR CALA2020021200402Panel · missingPDA 2 ON INBOUND FLIGHT FUSELAGE INSPECTION FOUND PANEL 443CL MISSING FROM INBOARD SIDE OF RIGHT HAND ENGINE PYLON. #2 PYLON STRUT INBOARD PANEL 443CL MISSING. REFERENCE CDL 545310 54A. DISPATCH DESK: 59 E: 10-FEB-20- APPROVED #2 I/B PYLON STRUT AFT MOUNT ACFeb 10, 2020 · N780UA · Boeing 777222SDR DALA2020021100067Panel · detachedGROUND AGENT FOUND A PANEL HAD FALLEN FROM AREA OF NUMBER 1 ENGINE. PANEL WAS HOT TO TOUCH. DETERMINED TO BE THE LEFT PACK FAN BYPASS CHECK VALVE FLAPPER DOOR. (LP #7215891)Feb 9, 2020 · N981AT · Boeing 717200SDR CALA2020021200399Skin · damagedWHILE PERFORMING WALK AROUND, ON NO.2 ENGINE PYLON NEAR EXHAUST AREA FOUND PULLED PANEL, HEADS OF SCREWS UNABLE TO SECURE IT. PULLED PANEL IS LOCATED ON OUTBOARD AREA ON ENGINE NO.2 ENGINE UPON FURTHER INSPECTION, DIAMETER OF HOLES ON PANEL ARE ENLARGED CAUSINFeb 8, 2020 · N34137 · Boeing 757224SDR IPXA2020021452113Skin · crackedINSPECTION TYPE:C11CRACK ON SKIN ASSY (P/N: 311T2450-23) OF #2 PYLON INBD PNL#442AL CUTOUT EDGE.REPAIR I.A.W. BOEING SRID: 4-4687665939 AND UPS EO B767-5410-75495-A.Feb 5, 2020 · N326UP · Boeing 76734AFSDR SWIA2020021848705Skin · crackedLH ENGINE LOWER TRANSCOWL INNER PERFORARED SKIN SURFACE COMMON TO 'Z' STIFFENER HAS CRACK LOCATED AT LOWER HOLE. (C-CHECK) RO 2/14/2020 REPAIRED LH ENGINE LOWER TRANS COWL INNER SKIN.Jan 28, 2020 · N730SK · Cndair CL6002C10SDR SWIA2020040649937Fastener · wornCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD - COMPLY WITH PARAGRAPH (J) OF AD FOR THE LH PYLON BY REPLACING AFFECTED FASTENERS AND COLLARS, INCLUDING DOING ALL APPLICABLE RELATED INVESTIGATIVE AND CORRECTIVE ACTIONS, IN ACCORDANCE WITH THE ACCOMPLISHMENT INSTRUJan 23, 2020 · N753SK · Cndair CL6002C10SDR CALA2020012600223Skin · gougedNR 2 PYLON INBD SIDE HAD THREE GOUGES JUST ABOVE THE INBD T/R MOUNT . CHECKED LIMITS. AREA 3 WITHIN LIMITS, AREAS 1 AND 2 OUT OF LIMITS IAW B757-300 SRM 54-30-01 AD1 FIG 101, DETAIL I II. ACCOMPLISHED ECRA 5453-0118 TO AREAS 1 AND 2. NO FURTHER ACTION REQUJan 19, 2020 · N75853 · Boeing 757324SDR IPXA2020020311642Skin · crackedINSPECTION TYPE:C12CRACK ON #2 PYLON INBD SKIN ASSY (P/N : 311T2450-23) NEAR NAC 240.50REPAIR I.A.W BOEING SRID : 3-4623448622 AND UPS EO B767-5430-75336-AJan 17, 2020 · N315UP · Boeing 76734AFSDR SWIA2020021148420Skin · cracked*LH ENGINE UPPER TRANSCOWL HAS CRACK FWD OF FWD LATCH ASSY AND FASTENERS PULLED THROUGH STIFFENER AFT OF FWD LATCH ASSY. (C-CHECK) RO 2/07/2020 ORDERED AND RECEIVED SERVICEABLE LH/UPPER TRANSCOWL ASSEMBLY. SEE TRANS # 20073058, JOB 710202100, OPERATION 52Jan 9, 2020 · N746SK · Cndair CL6002C10SDR SWIA2020021148426Skin · chafed*LH ENGINE UPPER FAN COWL HAS CHAFE IN FORMER FROM CONTACT WITH INBOARD TR FEEDBACK ACTUATOR LVDT HARNESS. (C-CHECK) RO 2/07/2020 COMPLIED WITH REPAIR SRS742 PER SRM.Dec 31, 2019 · N746SK · Cndair CL6002C10SDR SWIA2019122647100Skin · chafedCHAFE ON THE RT ENGINE REINFORCEMENT PYLON SKIN FORWARD LEADING EDGE ASSEMBLY FROM THE RT PYLON I/B UPPER ROD END SAFETY WIRE. INSTALLED REPAIR DOUBLER ON RH ENG EINFORCEMENT PYLON SKIN FORWARD LEADING EDGE ASSEMBLY FROM THE R/H PYLON I/B UPPER ROD END REF EDec 20, 2019 · N132SY · Emb ERJ170200LRSDR DALA2019122703561Panel · missingDURING B-CHECK, MAINTENANCE FOUND THAT PANEL 330KB WAS MISSING. MAINTENANCE INSTALLED A NEW PANEL (MPN 5910412-151) IAW AMM 06-33.Dec 19, 2019 · N970AT · Boeing 717200SDR DALA2019122007473Skin · crackedCRACK INTERNAL SKIN INBOARD FAN COWL AFT AREA ON ENGINE 1 LOG-PAGE UPDATED. REPLACED FAN COWL ENG #1 I/B P/N 238-0302-513 S/N CU102 SERVICEABLE CONDITION THE INSTALLATION IS TO BE ACCOMPLISHED ON AMDS CARD 7832-2010-1R.Dec 19, 2019 · N346NB · Airbus A319114SDR DALA2020021401148Skin · damaged(AIRCRAFT 7004, L/P 1406821) WHILE CLOSING #1 FAN FOUND VISABLE DAMAGE TO LT OUTBD UPPER FAN COWL. CORRECTIVE ACTION: APPLIED PERMANENT REPAIR WITH REFERENCE TO B777 SRM 51-70-04-2R.Dec 17, 2019 · N863DA · Boeing 777232SDR REXA2019123041790Skin · crackedDAMAGE SEALS AND CRACK ON PYLON ACCESS PANELS SKIN 422CT AND 412CT. DAMAGE SEALS AND CRACKED SKIN ON PYLON ACCESS PANELS 422CT AND 412CT WERE REPLACED IAW SRM 51-42-06-001-001-A01 PAR. 6C, AND SRM 51-42-10-001-001-A01 PAR. 8C.Dec 14, 2019 · N930XJ · Cndair CL6002D24SDR DALA2019121607322Access Door · missingDURING SERVICE CHECK FOUND MISSING NACELLE STRUT ACCESS DOOR ON LT ENGINE INBOARD SIDE. MCO/PLAC REMOVED. (LP 6571998)Dec 13, 2019 · N171DN · Boeing 767332SDR YENA201912160701Skin · crackedFT # 526, TPA-JFK. #1 ENGINE INBOARD PYLON CRACK (REF ORIGINAL INSP LP 2766591-1); AEROMAN WO# 2019-414/1 WCC# 2019-414201 PERFORMED PROCEDURE TO LH PYLON IB UPPER SPAR LINK SPAR REPLACEMENT ALTERNATE TOOLING PER AEROMAN EA 54-50-76-19 REV 0(COVER 1 PART 1) ANDec 12, 2019 · N267JB · Emb ERJ190100IGWSDR SWIA2020020348143Skin · gouged*PANEL 432AB GOUGED/KNIFE EDGED AT THE TRAILING EDGE (MARKED) (C-CHECK) RO:1/29/2020REMOVED AND REPLACED WORN L/H ENGINE LOWER COWL 432AB AFT EDGE STRIP P/N 228-50081-107 REF. CRJ 200 CMM.Dec 12, 2019 · N487CA · Cndair CL6002B19SDR SWIA2020020348142Skin · gouged*PANEL 432AT GOUGED/KNIFE EDGED AT THE TRAILING EDGE (MARKED) (C-CHECK) RO:1/29/2020REMOVED AND REPLACED WORN L/H ENGINE UPPER COWL 432AT AFT EDGE STRIP P/N 228-50080-107 REF. CRJ 200 CMM.Dec 12, 2019 · N487CA · Cndair CL6002B19SDR SWIA2020020348108Skin · dentedLH ENGINE LOWER TRANSCOWL HAS DENT AT 6 O'CLOCK POSITION ( MARKED). PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK) RO:1/29/2020REPAIRED L/H LOWER TRANS COWL DENT BACKDec 6, 2019 · N487CA · Cndair CL6002B19SDR SWIA2020012147870Skin · chafedL/H ENGINE UPPER FAN COWL HAS CHAFFED MARLS ON TRAING EDGE OF COWL.432 AT (C-CHECK) RO:1/17/2020REMOVED AND REPLACED AFT EDGE STRIP ON COWL 432AT PER BOMBARDIER CMM.Dec 6, 2019 · N455CA · Cndair CL6002B19SDR SWIA2020012147869Skin · chafed* R/H SIDE UPPER FAN COWL HAS TRAILING EDGE WORN AND CHAFFED. 442AT (C-CHECK) RO:1/17/2020REMOVED AND REPLACED AFT EDGE STRIP ON COWL 442AT PER BOMBARDIER CMM.Dec 6, 2019 · N455CA · Cndair CL6002B19SDR FDEA201911263119Skin · gouged#1 ENG O/B CORECOWL AFT UPPER CHAFE STRIP GOUGED REMOVED AND REPLACED ATTACH BRACKET AND WEARSTRIP PER ROHR SRM 54-04-01, AND EA# 6-7110-T0351046 P1. TITLED: POWER PLANT - WING ENG COWL - #1 ENG OUTBD CORE COWL, WEAR PLATE SUPPORT, CHAFED.Nov 26, 2019 · N664FE · Airbus A300F4605RSDR U2RA2019121750001Doubler · corrodedCORROSION ON RIGHT ENGINE PYLON, INBOARD SIDE INTERIOR AT APPROXIMATELY POWERPLANT WATERLINE 140 POWERPPLANT STATION 152 TO 166, BEYOND ALLOWABLE LIMITS - ACCOMPLISHED CORROSION BLEND OUT REPAIR TO RIGHT ENGINE PYLON SKIN PER BOEING SERVICE REQUESTION SR 3-454Nov 25, 2019 · N567CA · Boeing 757223SDR A6WA2019112647037Skin · crackedPANEL 435AB HAS CRACKED AREA ON INSODE SKIN PANEL, AIRCRAFT REMOVED FROM SERVICE, REPAIR INNER SKIN IAW BOMBARDIER CMM 71-12-01 SRS0460Nov 24, 2019 · N411ZW · Cndair CL6002B19SDR U2RA201912190001Skin · corrodedCORROSION ON LEFT ENGINE PYLON INBOARD SIDE SKIN, ON INTERIOR, AT APPROXIMATELY POWERPLANT WATER LINE 140.94 POWERPLANT STATION 144.425 TO 170 - ACCOMPLISHED CORROSION BLEND OUT REPAIR TO LEFT ENGINE PYLON SKIN IN ACCORDANCE WITH BOEING SERVICE REQUEST SR 3-45Nov 21, 2019 · N567CA · Boeing 757223SDR GTIA2019111134775Skin · gouged"GOUGE FOUND CANTILEVER PYLON #1 RIB7-9 I/B DIMENSION L=36MM, W=15MM, D=PENETRATION THE SKIN & OST=0.80MM RAF01 2569250-1 OPENED-REVIEWED LTPR NRI 5000930755-0010.PERFORMED REPAIR AS PER EO 5450-1906 REV00 AND A3I RDAZ REQ 80701994-003-2019 ISSUE A. REPAIR INov 11, 2019 · N602NK · Airbus A320232SDR A6WA2019112647035Panel · crackedPANEL 433AB HAS A CRACK AIRCRAFT REMOVED FROM SERVICE REPLACED WITH SERVICEABLE PANEL 433AB REF CRJ200 SRM 52-41-02 REV 37.Nov 6, 2019 · N432AW · Cndair CL6002B19SDR SWIA2019122747362Skin · dentedSMALL DENT FOUND ON L/H ENGINE LOWER TRANSLATING COWL ABOUT 6 O'CLOCK POSITION. (MARKED WITH YELLOW PAINT) (C-CHECK) RO:12/24/2019 REPAIRED DAMAGE TO L/H ENGINE LOWER TRANS COWL NEAR 6 O'CLOCK POSITION REF. BOMBARDIER CMM REPAIR NO. SRS030.Nov 1, 2019 · N435SW · Cndair CL6002B19SDR DALA2019102506196Skin · cracked#1 ENG PYLON FWD LOWER SURFACE OPEN HOLE CUTOUT FOUND CRACK. REPAIRED PER ERA 582181-14. (LP 1331145)Oct 25, 2019 · N834MH · Boeing 767432ERSDR DALA2019102806199Access Door · erodedNO.2 PYLON AFT FAIRING I/B ACCESS DOOR L/E FOUND EROSION. REPAIRED PER SRM 51-70-04. (LP 1330747)Oct 25, 2019 · N831MH · Boeing 767432ERSDR DALA201910286196Skin · cracked#1 ENG PYLON FWD LOWER SURFACE OPEN HOLE CUTOUT FOUND CRACK. REPAIRED PER ERA 582181-14. (LP 1331145)Oct 25, 2019 · N834MH · Boeing 767432ERSDR DALA2019102306106Skin · crackedMTC TASK-#1 ENG FORWARD PYLON UPPER SURFACE OPEN HOLE CUTOUT FOUND CRACK. #1 ENG FORWARD PYLON UPPER SURFACE OPEN HOLE CUTOUT CRACK AREA REPAIRED AS PER PRI581828-14 REV.0. PRI581828-14 REV.0 COMPARED AND COMPLIED WITH ER/A581828-14AD REV.ORIGINAL. (LP1328042)Oct 23, 2019 · N834MH · Boeing 767432ERSDR 7C7A201910220513Access Panel · crackedCRACK DAMAGE OF L/H NACELLE ACCESS PANEL LANDING STRIP, P/N 85410182, AT XN 64.0 AND YN 8.48. THE PERMANENT REPAIR FOR CRACK DAMAGE TO L/H NACELLE ACCESS PANEL LANDING STRIP WILL ACCOMPLISHGED IAW DEHAVILLAND AIRCRAFT OF CANADA LIMITED RD 8-54-4224 ISSUE 1 DAOct 22, 2019 · N892EA · Dhav DHC8106SDR SIMA201910210002Skin · damagedLH COWL DMG FOUND DURG PRE FLIGHT.DAMAGE #1: LH LWR COWL 14.5" OTBD OF OIL SERV DOOR BOTTOM EDGE. PUNCTURE DUE TO BOLT ON CLAMP ON BLD TUBE BTWN ATS AND ATS VLV WITH CRACKS. CRACK L 1.5" WITH 2 LATERAL CRACKS OF 0.5" AND 0.25" FOR TOTAL W 0.75". PROTRUSION DEPOct 20, 2019 · N932AE · Emb EMB145LRSDR DALA2019102196016Skin · cracked#1 PYLON OB SIDE STRUT SKIN HAS 2" CRACK ABOVE 432AL. VERIFIED WITH HFEC SCAN TAG # 6741, CREATE EWO FOR REPAIR. REPAIRED #1 PYLON OB STRUT SKIN IAW ERA 581953-14 REV O. JOB COMPLETE. (LP1321034)Oct 18, 2019 · N156DL · Boeing 7673P6SDR DALA2019101805979Access Panel · crackedCRACK ACCESS PANEL 473AL ON LH PYLON. REPAIRED BY WELDS ACCESS PANEL 473AL LH PYLON AS PER ER/A PRI 582152-14 REV 0 PAGE 1 TO 7 ER/A NO 582152-14 REV ORIGINAL SHEET 1 TO 5.Oct 18, 2019 · N360NB · Airbus A319114SDR DALA2019101805980Access Panel · crackedCRACK ACCESS PANEL 483AL ON RH PYLON. REPAIRED BY WELDS ACCESS PANEL 483AL RH PYLON AS PER ER/A PRI 582212-14 REV 0 PAGE 1 TO 6 ER/A 582212-14 REV ORIGINAL SHEET 1 TO 6.Oct 18, 2019 · N360NB · Airbus A319114SDR ABXA201910316169Skin · crackedCRACK IN RIGHT ENGINE OUTBOARD CORE COWL LOWER LONGERON AT SECOND FROM AFT LATCH. THE CORE COWL WAS REPLACED. THE AIRPLANE WAS GROUNDED.Oct 16, 2019 · N312AA · Boeing 767223SDR DALA2019101765940Skin · crackedNUMBER 1 PYLON PANEL 436CR HAS HOLE ELONGATED , CRACKED ON INNER SKIN AND SPRING SEAL WORN (M) MOORE 350206 09/09/19 (ON REPAIR RACK). REPAIRED PYLON PANEL 436CR I/A/W ERA 581311-14 REV O. (LP1316822)Oct 15, 2019 · N156DL · Boeing 7673P6SDR DALA2019101105845Skin · bentNO. 2 ENG OUTBD CORE COWL 1ST LATCH HAS BENT SKIN ABOVE LATCH. MARKED. NO. 2 ENG OOUBOARD CORE COWL 1ST LATCH SKIN BENT ABOVE LATCH HAS BEEN REPAIRED PER ER/A 581524-14 REV-0 JOB COMPLETE (LP1309495)Oct 10, 2019 · N156DL · Boeing 7673P6SDR DALA2019101005828Access Panel · crackedCRACK ACCESS PANEL 413DL ON SKIN PLATE ON LT PYLON. REPAIRED BY WELDS ACCESS PANEL 413DL ON LH PYLON ASPER ER/A 540187-14MA REV ORIGINAL SECTION 1: PERMANENT REPAIR STEP 1 TO 7 AND A319 SRM TASK 54-52-11-300-004 PARAGRAPH 2.A, ITEM 1 STEPS (C) TO (K) FIGURE 00Oct 9, 2019 · N360NB · Airbus A319114
Back to JASC 5414