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 UIEA2017071401222Skin · damagedNR 2 ENGINE OTBD CORE COWL OUTER SKIN FWD UPPER CORNER IS CRACKED AND BENT. REPAIRED IAW EO 1971A139.SDR IPXA2017072219610Skin · dentedINSPECTION TYPE: C-12, NR 2 PYLON INBD SIDE SKIN PANEL DENTED. REPAIRED IAW EO B757-5430-64999-ASDR IPXA2017072119586Skin · chafedINSPECTION TYPE: 1C, THE NR 1 ENGINE INLET COWL AFT WEB CHAFED ADJACENT TO SENSE LINE ELBOW FITTING, 9:00 O`CLOCK POSITION. REPAIRED THE WEB IAW SRM 54-15-02, REPAIR 13.SDR UIEA2017071201160Acoustic Liner · dentedNR 1 ENGINE NOSE COWL INLET ACOUSTIC HAVE MULTIPLE DENTS IN SEVERAL PLACES. REPAIRED NR 1 ENGINE NOSE COWL INLET ACOUSTIC IAW SRM 54-12-01 REPAIR 3 7.11 FIG 201.SDR SWAA2022012640877Panel · delaminatedFWD TOP CORNER DELAMINATED ON L/H PYLON ACCESS PANEL 434AL / REPAIRED FWD TOP CORNER L/H PYLON ACCESS PANEL 434AL I.A.W SRM 54-50-70-1A-3; I.A.W SRM 51-70-04-2R-6.SDR SWAA2022012640878Panel · delaminatedAFT BOTTOM CORNER DELAMINATED ON L/H PYLON ACCESS PANEL 434BL / AFT BOTTOM CORNER DELAMINATED ON L/H PYLON ACCESS PANEL 434 BL REPAINED IAW SRM 54-50-70-2R-3 AND IAW SRM 51-70-04-2R-13.SDR IPXA2017071319268Skin · crackedINSPECTION TYPE: C10, CRACK FOUND ON THE INBD SIDE SKIN AND DOUBLER OF THE NR 2 PYLON. REPAIRED IAW EO B767-5430-64819-A.SDR JJBA20170703008Skin · crackedCRACK FOUND ON LT NACELLE JUST ABOVE FWD MLG DOOR. DAMAGE CUT OUT AND DOUBLER FABRICATED IAW RD 8-54-874.SDR EE4Y201706263824Cowling · delaminatedENGINE NR 2, OUTBOARD FAN COWL, FWD EDGE WITH DELAMINATION. REPAIRED AS STATED IN ENGINEERING ORDER NR EOD-32S-54-0159-R00.SDR SWIA2017072543573Skin · chafedLEFT AFT CORE COWL IS CHAFED ON THE OUTBOARD EDGE WHERE IT CONTACTS THE FORWARD UPPER AND LOWER CORE COWLS. REPAIRED THE DAMAGED AREA IAW SRM.SDR COEA2017062102900Landing · chafedHEAVY CHECK COE/MAJOR REPAIR, RT NACELLE INBOARD REBATE LANDING FOR LATERAL PANEL 485AL IS CHAFED. LEVEL 2, REPAIRED PER SRAS PCE-1146/17. 11649 DATED 7/13/2017.SDR DALA2017062204923Skin · dentedDENT ON RIGHT UPPER SKIN STATION 1364 AT RIGHT PYLON. COMPLIED WITH ERA 559786-14, REV O.SDR IPXA2017071819479Skin · crackedINSPECTION TYPE: 3C, NR 3 ENGINE INLET NOSE COWL SKIN CRACKED AROUND FASTENERS, 8:00 POSITION. REMOVED AND REPLACED THE 3 INLET COWL IAW AMM 71-11-01.SDR GTIA2017061402005Cowling · delaminatedNR 2 ENGINE INBD FAN COWL HAS DELAMINATION. LENGTH 11MM X 11MM. PERFORMED FILLER PLATE REPAIR IAW EO 5414-1711SDR UIEA2017061301017Skin · damagedNR 1 PYLON BLEND DAMAGE UNDER THE 431 BT PANEL INBD OF SUPPORT FITTING. REPAIRED THE PYLON IAW EA 170189.SDR UIEA2017061201004Skin · delaminatedDURING A WALK AROUND, THE NR 2 ENGINE FAN COWL HAS AN AREA OF DELAMINATION. REMOVED, AND REPAIRED IAW AMM 71-11-04-714-001-400. INSTALLED IAW AMM 71-11-04/401.SDR P5CA2017061300183Skin · chafedNR 4 ENGINE LT CORE COWL INNER FACE FWD & NR 2 CHANNEL REPAIR DOUBLER FOUND CHAFED. REPAIRED IAW SRM 54-45-022R-1, FIG 201.SDR P5CA2017061300185Skin · damagedNR 3 ENGINE RT CORE COWL OUTER FACE AFT UPPER CORNER CHAFED WITH A HOLE AT LOWER OF SPRING SOFT. REPAIRED IAW SRM 54-45-01-2R, REPAIR 7, FIG 202.SDR UIEA2017060800980Skin · scratchedNR 2 ENGINE, RT CORE COWL SCRATCHED IN THE MIDDLE. SCRATCH SMOOTHED IAW SRM 51-10-02, NDT CHECKED IAW D634T301, PART 6 51-00-19, NO CRACKS FOUND. THICKNESS MEASURED IAW D 634T301, PART 4 51-00-10, & FOUND WITH IN LIMITS IAW SRM 54-42-01.SDR UIEA2017060800984Skin · dentedNR 1 ENGINE FAN COWLS HAVE DENTS IN SOME PLACES. THE DENTS WERE FILLED WITH COMPOUND IAW MM 54-21-01 & REPAINTED IAW MM 51-21-10.SDR UIEA2017060800985Skin · dentedNR 2 ENGINE FAN COWLS HAVE DENTS IN SOME PLACES. DENTS FILLED WITH COMPOUND IAW MM 54-21-01 & REPAINTED IAW MM 51-21-10.SDR UIEA2017060800986Skin · scratchedNR 2 ENGINE CORE COWLS SCRATCHED IN SOME PLACES. SCRATCHES SMOOTHED IAW MM 51-10-02, NDT CHECKED IAW D634T301, PART 651-00-10, FOUND WITHIN LIMITS PER SRM 54-42-01.</P>)SDR UIEA2017041700598Skin · wornNR 2 ENGINE, LT CORE COWL FAIRING SKIN INTERIOR AREA FOUND WORN LOCATED AT UPPER AFT CUT-OUT. THE FAIRING SKIN WAS REPAIRED IAW SRM 54-45-01-2R-11, REPAIR 11, REV 103.SDR UIEA2017050900733Skin · scratchedNR 1 ENGINE LT CORE COWL EXTERIOR SKIN FOUND SCRATCHED. SCRATCHES BLENDED OUT AND FOUND WITHIN LIMIT IAW SRM 54-42-01-1A-1, FIG 101, NOTE B, DETAIL III, REV 104.SDR UIEA2017060500941Panel · missingPANEL 461AL ON THE NR 2 PYLON OTBD DISCOVERED MISSING DURING WALK AROUND INSPECTION. INSTALLED A TEMPORARY PANEL IAW EO 4454A089.SDR IXXA20170802263Skin · crackedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. NR 1 PYLON INBOUND SKIN HAS A CHAFE MARK AT THE UPPER CONTACT POINT WITH THE WING LEADING EDGE. REMOVED AND REPLACED THE NR 1 PYLON INBOUND SKIN IAW DRAWING 313T200 AND SRM 51-40-02, PARAGRAPH 7.SDR DALA2017052604283Doubler · wornLEFT ENGINE PYLON INBOARD SIDE AT NACSTA 102 AFT SIDE HAD A DOUBLER THAT IS WORN. REMOVED AND REPLACED THE REPAIR DOUBLER IAW SRM 54-51-02, REPAIR 1.SDR SWIA201743422Skin · dentedMULTIPLE DENTS ON THE LEFT ENGINE LOWER FAN COWL. FOUND TO BE OUT OF LIMITS AND REPAIRED IAW SRM.SDR GTIA2017051801916Skin · debondedFOUND THE NR 1 ENGINE INBD FAN COWL SKIN DISBONDED. 23.5L X 14W. PERFORMED FILLER PLATE REPAIR IAW EO 5414-1709.SDR KO0R201705180015Panel · crackedNR 3 PYLON PANEL 487AR VENT DUCT HAS A CRACKED CORNER.SDR IPXA2017052717593Panel · gougedINSPECTION TYPE: 1C, NR 3 PYLON PANEL 487BL GOUGED AT VENT. REPAIRED THE PANEL IAW EA 011-5450-01-A6802, REV IR, AND EO MD11-5450-64348-A.SDR DALA2017051704033Skin · chafedNR 1 ENGINE UPPER PYLON PANEL 431AT LEADING EDGE AREA CHAFED ON SKIN. REMOVED DAMAGE FROM PANEL AND FOUND TO BE OUT OF LIMITS IAW SRM 54- 51-01 FIG. 101. REMOVED THE PANEL, FABRICATED A NEW PANEL AND INSTALLED IAW DWG 311N3510 & SRM 51-40-02.SDR FDEA201705131461Access Panel · crackedNR 2 ENGINE PYLON ACCESS PANEL 457CT SKIN CRACKED AT YID 425.30. REPAIRED THE ACCESS PANEL IAW EA 8-5480-T0333228.SDR P5CA2017050500108Skin · wornNR 1 NACELLE LT CORE COWL INTERIOR AFT UPPER SKIN FOUND WORN. REPAIRED IAW SRM 51-40-02, REV 104.SDR P5CA2017050600114Skin · erodedNR 1 ENG NOSE COWL EXTERIOR SKIN AFT OF NOSE COWL LIP FOUND EROSION CIRCUMFERENTIALLY. NR 1 NOSE COWL EXTERIOR SKIN AFT OF NOSE COWL LIP REPAIRED IAW SRM 54-12-01-2R-11 REPAIR 11, REV 104, AND PAINTED IAW AMM 51-21-10, REV 120.SDR P5CA2017050700118Skin · dentedRIGHT NACELLE O/B CORE COWL BELOW PRECOOLER EXHAUST, FOUND A DENT. FOUND WITHIN LIMITS IAW SRM 54-42-01-1A-1, FIG.101, REV 104.SDR P5CA2017050800124Fastener · wornNR 1 NACELLE RT CORE COWL EXTERIOR AFT UPPER SKIN FOUND WITH TWO FASTENER HEADS WORN. REMOVED AND REPLACED THE FASTENERS IAW SRM 51-40-02, REV 104.SDR P5CA2017050800125Skin · scratchedNR 1 NACELLE, RT CORE COWL EXTERIOR SKIN WITH SCRATCHES. MINOR SCRATCHES REMOVED IAW SRM 51-10-02, REV 104. FOUND WITHIN LIMIT IAW SRM 54-42-01-1A-1, FIG 101, REV 104.SDR 7C7A2017050500323Skin · dentedDENTS ON LT NACELLE OUTBOARD COWLING 413ALSDR CALA2017050101199Skin · crackedNR 2 PYLON RT SKIN FOUND CRACKED AT PANEL 426BR. CUTOUT POSITION NR 2 PYLON RT SKIN AT PANEL 426BR CUTOUT CRACKED AND REPAIRED IAW SRM 54-53-01, REPAIR 6, FIG 201.SDR JJBA20170419022Deck Plate · chafedUPPER DECK ON LT NACELLE CHAFED THROUGH BY FINGERNAIL. DAMAGE CUT OUT.SDR IPXA2017041816236Skin · crackedINSPECTION TYPE: C10, CRACK ON INBD SIDE SKIN AND DOUBLER OF THE NR 2 ENGINE PYLON. REPAIRED IAW EO B767-5430-63922-A.SDR SWAA2022012106689Seal · crackedBROKEN SEAL RETAINER ACCESS PANEL #431AR ON ENGINE 1 / REPLACED SEAL RETAINER ACCESS PANEL #431AR ON ENGINE 1 IAW SRM B737-700 51-40-02 AND 51-10-02 ITEM 9SDR SWAA2022012106690Seal · brokenBROKEN RETAINER STRIP ACCESS PANEL #431AL ON ENGINE 1 / REPLACED RETAINER STRIP ACCESS PANEL #431AL ON ENGINE #1 IAW B737-700 SRM 51-10-02 PARAGRAPH 9 B737-700 SRM 51-40-02SDR SWAA2022012106691Seal · brokenBROKEN RETAINER SEALS ACCESS PANEL #441AT ON ENGINE 2 (2E/A) / REPLACED RETAINER SEALS ON ACCESS PANEL #441AT AT ENGINE #2 (2E/A) IAW SRM 737-700 51-10-02 ITEM 9 AND SRM B737-700 51-40-02-0G-0 REV 61SDR QXEA2017050200336Stiffener · crackedLT NACELLE AFT FAIRING PNL 414AR AFT BOTTOM ANGLE CRACKED. REMOVED AFT BOTTOM STIFFENER PN 85414249-102 FROM AFT FAIRING PNL 414AR REF SRM 51-42-05. INSTALLED NEW AFT BOTTOM STIFFENER PN 85414249-102 ON AFT FAIRING PNL 414AR, REF SRM 51-42-05.SDR SWAA2022011906677Retainer · crackedCRACK SEAL RETAINER ON ACCESS PANEL #441AL ON ENGINE 2 / REPLACED SEAL RETAINER ON ACCESS PANEL #441AL ON ENGINE #2 IAW SRM 737-700 51-40-02 AND SRM 737-700 51-10-02 ITEM 9SDR SWAA2022011981543Seal Plate · brokenBROKEN SEAL PLATE LOCATED STRUT ACCESS PANEL #441AR ON ENGINE 2 / REPLACED SEAL PLATE LOCATED STRUT ACCESS PANEL #441AR ON ENGINE #2 IAW B737-700 SRM 51-10-02 ITEM 9SDR SWAA2022011981540Seal Plate · brokenBROKEN SEAL PLATE LOCATED STRUT ACCESS PANEL #431AL ON ENGINE 1 / REPLACED SEAL PLATE LOCATED STRUT ACCESS PANEL #431AL ON ENGINE 1 IAW B737-700 SRM 51-10-02 ITEM #9SDR SWAA2022011981541Seal Plate · brokenBROKEN SEAL PLATE LOCATED STRUT ACCESS PANEL #431AR ON ENGINE 1 / REPLACED SEAL PLATE LOCATED STRUT ACCESS PANEL #431 AR ON ENGINE 1 IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9
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