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 UIEA2018071601485Skin · chafedNR 2 PYLON FAN COWL SEGMENT SUPPORT BEAM UPPER SKIN CHAFED. ACCOMPLISHED BLENDOUT REPAIR ON NR 2 PYLON FAN COWL SEGMENT SUPPORT BEAM UPPER SKIN PER EA 767-5452-28-A7325IR.SDR IPXA2018080132252Skin · chafedINSPECTION TYPE:3C, RT O/B FWD PYLON LOWER SKIN IS CHAFED AT STA XDLE 330.2745. REMOVED, FABRICATED AND REPLACED L/E SKIN AT STA XLDE 330.2745 IAW DWG ARB2363 AND SRM 51-31-01 & 51-33-01. (MINOR)SDR SWAA2022022173910Stiffener · crackedLEFT PYLON AFT STRUT FAIRING HAS A CRACKED STIFFENER ABOVE FWD END OF THRUST TUBE. / FABRICATED REPLACEMENT PART PER BOEING DWG 313A2300 ID 003.INSTALLED PER SRM 51-40-02.SDR K11A2018112124007Skin · corrodedFUSELAGE EXTERIOR CORROSION. #2 ENGINE RIGHT SIDE ABOVE COWLING.SDR IPXA2018071631684Skin · crackedINSPECTION TYPE:4C, NR 1 ENG I/B LOWER AFT PYLON FAIRING MID SKIN CRACK REPAIR BETWEEN 2 FASTENERS PERMANENT REPAIR. REPARIED PER SREO A300-5450-32659-B.SDR IPXA2018071131595Rib · crackedINSPECTION TYPE:1C, NR 2 PYLON PANEL 423CL HAS 2 EA RIBS CRACKED. REPAIRED NR 2 PYLON PANEL 423CL IAW SRM 54-52-51 FIG 202.SDR DALA2018070304375Access Panel · damagedDURING INSPECTION FOUND EXPOSED MATERIAL ON ACCESS PANELS NBR 431ER AND 431EL OF ENGINE NR 1. ACCESS PANELS 431ER AND 431EL WERE REPAIRED PER SRM 51-70-05 REPAIR 10 AND SRM 51-70-05 REPAIR GENERAL PAR 4.SDR DALA2018070304373Access Panel · damagedDURING INSPECTION FOUND EXPOSED MATERIAL ON ACCESS PANEL NR 441EL OF ENGINE 2. ACCESS PANEL 441EL WAS REPAIRED PER SRM 51-70-05 REPAIR 10 AND SRM 51-70-05 REPAIR GENERAL.SDR REXA2018071800627Panel · chafedFAIRING PANEL 433 BB HAS CHAIFING AND CRACKED DOUBLER AT END OF PANEL (PR). REMOVED AND REPLACED FAIRING PANEL IAW SRM 51-42-06 AND 51-42-13.SDR K11A2018100373401Skin · corroded#1 PYLON TOP SIDE APPROX NAC STA 240 HAS CORROSIONSDR R61A201807090759Skin Panel · corrodedWHILE AIRCRAFT WAS IN FOR HEAVY MAINTENANCE, MAINTENANCE FOUND PANEL 419NR HAS CORROSION ON HINGE. MAINTENANCE REMOVED AND REPLACED PANEL 419NR PER AMM 54-50-22.SDR DALA2018062604225Panel · missingPANEL MISSING ON THE NR 1 ENGINE PYLON. INSTALLED A REPLACEMENT PANEL IAW AMM 20-10. OK FOR SERVICE.SDR KCSA201806231154Skin · crackedRIGHT PYLON INBD SIDE, AFT UPPER AREA OF OPENING FOR ACCESS PANEL 442AL. PYLON SKIN CRACKED.SDR UIEA2018062601256Skin · brokenCRACK AND BROKEN ON NR 4 PYLON RIGHT SIDE ACCESS DOOR SURROUND SKIN AND DOUBLER. REPAIR CRACK AREA IAW EI NO T2018A54M-2819 REV 1 2. JOB COMPLETED AND COND CHK NML.SDR R61A201806160698Access Panel · corrodedWHILE IN HEAVY CHECK - CORROSION NOTED DURING BLENDED OUT OF PANEL 429NR. REMOVED AND REPLACED PANEL PN: 170-34952-021 REF SRM 51-23-06.SDR KCSA201806121145Access Panel · crackedEVIDENCE OF CRACK ON NR 1 PYLON INBD SIDE ON LOWER LT CORNER OF ACCESS PANEL 452DR APPX MAC STA 282.SDR IPXA2018062093827Skin · crackedNR 1 PYLON LOWER AFT SKIN WAS CRACKED AT AFT DRAIN FITTING. REMOVED AND REPLACE THE SKIN IAW DWG A54515063, AND SRM 51-40-21.SDR IPXA2018061430665Panel · crackedINSPECTION TYPE:12YR, NR 2 PYLON O/B PANEL 424CR HAS CRACKED RIB (DISCREPANCY RACK). REPAIRED IAW SRM 54-52-51 FIG 202.SDR IPXA2018061430664Panel · wornINSPECTION TYPE:12YR, NR 2 PYLON O/B PANEL 424CR HAS WORN SCREW HOLE (DISCREPANCY RACK). REPAIRED IAW SRM 54-52-51 FIG 201.SDR DALA2018060103750Doubler · crackedDURING INSPECTION, A CRACKED INBD DOUBLER ON THE RT PYLON PPS 170. THE INBD DOUBLER WAS REPLACED IAW SRM 51-40-02-0G-0, AND DRAWING 313N3100.SDR DALA2018052803702Doubler · crackedCRACKED OUTBD DOUBLER ON RT PYLON STA PPS 170 (RT PYLON). REPLACED PER DWG 313N3100 REV. REMOVE AND INSTALLED PER SRM 51-40-02 PAR 7. LENGTH CRACKED WAS FOUND .521.SDR DALA2018052703717Fairing · crackedCRACKED LT PYLON AFT FIXED FAIRING, COMPLIED WITH EM 5450-01052 AND AD 2016-07-12 BY COMPLETING AMDS 5450-01052-03A AND 06A REFERENCE NR 13. ASSOCIATED AA 5450-01052.SDR IPXA2018060643312Skin · crackedNR 2 ENGINE, RT CORE COWL HAD A CRACK ON THE OUTER SKIN AT THE FWD LATCH. REPAIRED THE DAMAGE IAW EA 011-5430-01-A7295, REV I/R, AND EO MD11-5430-68739-A.SDR CALA2018060531311Skin · crackedNR 2 PYLON RT SIDE SKIN WAS FOUND CRACKED. REPAIRED IAW EC/R A 5430-02164, REV-.SDR UIEA201805160505Skin · damagedNR 1 ENGINE, LT CORE COWL FAIRING SKIN INTERIOR SURFACE AT THE UPPER AFT CUT-OUT SECTION FOUND DAMAGED. THE FAIRING SKIN WAS REPAIRED IAW SRM 54-45-01, REPAIR 11, REV 106.SDR UIEA201805160506Skin · damagedNR 2 ENGINE, RT CORE COWL FAIRING SKIN INTERIOR SURFACE ON THE UPPER AFT CUT-OUT SECTION FOUND DAMAGED. THE FAIRING SKIN WAS REPAIRED IAW SRM 54-45-01, REPAIR 11, REV 106.SDR UIEA201805160684Skin · scratchedNR 1 ENGINE, LT CORE COWL SKIN EXTERIOR SURFACES FOUND SCRATCHED. THE SCRATCHES WERE REMOVED AND FOUND WITHIN LIMITS IAW SRM 54-45-01-1A-1, FIG 101, TABLE 101, DETAIL II, REV 106.SDR UIEA201805160685Skin · scratchedNR 1 ENGINE, R CORE COWL SKIN EXTERIOR SURFACES SCRATCHED. SCRATCHES REMOVED AND FOUND WITHIN LIMITS IAW SRM 54-45-01-1A-1, FIG 101, TABLE 101, DETAIL II, REV 106.SDR UIEA201805160686Skin · scratchedNR 2 ENGINE, LT CORE COWL SKIN EXTERIOR SURFACES FOUND SCRATCHED. SCRATCHES REMOVED AND FOUND WITHIN LIMITS IAW SRM 54-45-01-1A-1, FIG 101, TABLE 101, DETAIL II, REV 106.SDR UIEA201805160688Skin · scratchedNR 2 ENGINE, RT CORE COWL SKIN EXTERIOR SURFACES FOUND SCRATCHES. SCRATCHES REMOVED AND FOUND WITHIN LIMITS IAW SRM 54-45-01-1A-1, FIG 101, TABLE 101, DETAIL II, REV 106.SDR UIEA2018042300760Skin · dentedNR 1 ENGINE, RT FAN COWL OUTER SKIN FOUND DENTED. REPAIRED IAW SRM 54-25-01, REPAIR 1, REV 106.SDR UIEA2018042300761Skin · dentedNR 1 ENGINE, RT FAN COWL OUTER SKIN FOUND DENTED. REPAIRED IAW SRM 54-25-01, REPAIR 1, REV 106.SDR UIEA201805160762Skin · dentedNR 1 ENGINE, RT FAN COWL OUTER SKIN FOUND DENTED. REPAIRED IAW SRM 54-25-01, REPAIR 1, REV 106.SDR UIEA201805160763Skin · dentedNR 2 ENGINE INLET COWL, LT OUTER SKIN FOUND DENTED. REPAIRED IAW SRM 54-15-01, REPAIR 9, REV 106.SDR UIEA201805160775Doubler · wornNR 2 ENGINE, LT CORE COWL AFT HAT FRAME REPAIR DOUBLERS FOUND WORN, LOCATED AT MID SECTION. THE REPAIR DOUBLER WAS REMOVED AND REPLACED IAW SRM 54-45-01, REPAIR 13, REV 31.SDR UIEA201805160776Skin · chafedNR 2 ENGINE, RT CORE COWL AFT HAT FRAME FOUND CHAFED, AT THE LOWER SECTION. REPAIRED IAW SRM 54-45-01, REPAIR 16, REV 31.SDR UIEA201805160800Skin · chafedNR 2 ENGINE, LT CORE COWL SECOND ZEE FRAME FROM FWD, FOUND CHAFED, ADJACENT TO HOLD OPEN ROD SECTION. REPAIRED IAW SRM 54-45-01, REPAIR 3, REV 31.SDR DALA2018050703186Panel · chafedLT PYLON IB UPPER SURFACE OF NACELLE FAIRING PANEL CHAFING LOWER WING SURFACE TO INCLUDE FUEL DOOR. REMOVED CHAFING FROM LT PYLON I/B UPPER SURFACE OF NACELLE FAIRING PANEL LWR WING SURFACE AND FUEL PANEL {DOOR}, FUEL PANEL FOUND IN LIMITS IAW SRM 57-20-01 AD SDR WVER201807160243Panel · gougedPANELS 443BB AND 443BT ARE GOUGED ON AFT END. REPAIRED PANELS 443BB AND 443BT IAW EXPRESS JET EC/TC`S EO CL600-2C10-54 L05664 AND EO CL6002C10-54-L05565.SDR SWAA2022021692141Panel · delaminated#1 PYLON PANEL 431DR AFT UPPER CORNER IS DELAM / REPAIRED #1 PYLON PANEL 431DR AFT UPPER CORNER I/A/W 737-700 SRM 51-70-04-2R-13 REV 64 PER 737-700 SRM 54-50-70-2R-2 REV 64.SDR UIEA2018042400783Skin · crackedNR 1 PYLON AT PANEL 416BR LANDING CRACKED THROUGH FASTENER HOLE. REPAIRED IAW EA 180129IR.SDR DALA2018041802602Skin · delaminatedDURING A SERVICE CHECK, FOUND THE NR 2 NACELLE SKIN DELAMINATED APPROXIMATELY 6 X 9 AND 6 X 3. REPAIRED IAW ERA 567774-14.SDR YENA201804140173Skin · chafedDURING HEAVY MAINTENANCE, THE NR 2 PYLON LOWER SKIN SURFACE FOUND CHAFED, INCLUDING THE HORIZONTAL DOUBLER AT RIB 5. REPAIRED THE NR 2 PYLON LOWER SKIN RIB 5 IAW SRM 54-51-12-283-003, 54-51-12-300-003, REO L21289, EC A18-277-01, AND RDAS 80441834-003-2018. CLSDR A8ZR20180823005Skin · dentedA DENT WAS FOUND ON THE NR 2 LOWER NACELLE SKIN AT XN 177.0 JUST ABOVE THE SKIN DOUBLER REPAIR THAT MEASURES 1.5"L X .75"W X .050"D. REFORMED TO NEW MEASUREMENT OF 1.7"L X 1.7"W X .011"D WITH NO CRACKS NOTED AND MATERIAL OFFSET TO COMPLY WITH SRM 54-00-16, ALSDR AALA2018051611002Skin · crackedLEFT PYLON LOUVERED PANEL LANDING CRACKED AT LOWER FORWARD END. REPAIRED PYLON SKIN IAW EA 279811.SDR IPXA2018041828709Panel · missingNR 2 ENGINE INBOARD PYLON MISSING PANEL 443HL. INSTALLED A NEW PANEL IAW MM 54-53-01. OK FOR SERVICE.SDR DALA2018041202379Skin · crackedCRACK ON UPPER SKIN APPROX STA Y=1421 AT RT PYLON TRAILING EDGE. TRAILING EDGE WAS REPAIRED PER DC9-MD80 SRM 53-01 FIG 2 SHEET 3 EXAMPLE C.SDR DALA2018041002356Skin · debondedNR 2 ENGINE AFT PYLON FAIRING FWD INBD SKIN IS DEBONDED. ACCOMPLISHED A PERMANENT REPAIR IAW ERA 369075-14MA, REV B.SDR IPXA2018041128462Panel · crackedINSPECTION TYPE: 1C, NR 1 PYLON PANEL 413CL HAS A CRACKED RIB. REPAIRED THE RIB IAW SRM 54-52-51. FA-B270ASDR CALA2018040501113Skin · damagedNR 2 PYLON PANEL 446AL SURROUND SKIN FOUND DAMAGED. THE SKIN WAS REPAIRED IAW ECRA 5450-02492, REV A, PART 1, ITEM A.
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