JASC 5414
Service difficulty reports · 4,361
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 EE4Y20110278Skin · corrodedENGINE NR1, PYLON AFT FIXED FAIRING, OTBD AND INBD LATERAL SKIN PANEL WITH CORROSION. NOTE: THE PANELS' CORROSION REQUIRES A MAJOR REPAIR.SDR P5CA2011051100043Access Panel · damagedNUMBER 1 ENGINE STRUT FAIRING ACCESS PANEL 452EL HAS FASTENER HOLE ELONGATED. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A54B-1025.SDR P5CA2011051000016Access Panel · damagedCHAFING DAMAGE ON NR 1 ENGINE NACELLE STRUT, INBOARD AFT SIDE OF ACCESS PLATE 452FR. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A54B-958.SDR P5CA2011051000015Panel · damagedWEAR DAMAGE FOUND ON FASTENER HOLE OF NUMBER 4 ENGINE STRUT FAIRING PANEL 482EL. ACCOMPLISHED PERMANENT REPAIR IAW EI T2011A54B-1001 DATED 22APRIL11.SDR KCSA111112Skin · crackedNR 4 PYLON UPPER SKIN HAS 3 EA CRACK INDICATIONS BETWEEN NAC STA 213 AND NAC STA 216.SDR KCSA111111Skin · crackedNR 2 PYLON UPPER SKIN HAS A .5 INCH CRACK AT NAC STA 221.SDR KCSA111110Skin · crackedNR 1 PYLON UPPER SKIN HAS A .5 INCH CRACK AT NAC STA 222.SDR ZZDA2011431Skin · crackedLEFT ENG APRON NR 2 COWL LATCH LOWER CUTOUT, CRACKED. ACCOMPLISHED LOWER CUTOUT DOUBLER REPAIR PER TRA 17-54-TR00129.SDR DALA1130359866Fastener · loosePYLON NR 1 UPPER SURFACE SKIN HAS 8EA LOOSE FASTENERS AT I/B OF AFT ENG MOUNT. REMOVED 4EA FASTENERS LOOSE IAW DC9 SRM 51-30-2. FOUND CRACK AT 1EA FASTENER HOLE. REPAIR CRACK 54-01 FIG 2 SHEET 2. RESHOOT 4EA REMAINING LOOSE FASTENERS IAW DC9 SRM 51-30-2.SDR IPXA11M66264Skin · looseNR 2 ENG PYLON SKIN LOOSE RIVETS. REPAIRED IAW EO MD11-5410-42470-A.SDR A6WA201140423Panel · chafedLT PYLON PANEL 412DB SEPARATES KNIFE EDGE. R & R FWD SEPARATOR, BLENDED AFT SEPERATOR TO WITHIN LIMITS IAW SRM 51-42-06, 51-42-13, 54-10-00 AND 51-12-00.SDR A6WA201140285Skin · dentedOUTER SKIN DENTED ON 435AT UPPER CORE COWL. REPAIR DENTED DAMAGE ON OUTER SKIN UPPER CORE COWL.SDR FDEA201104151495Skin · misrepairedNR 2 ENGINE PYLON FOUND AN EXISTING REPAIR ON RT SIDE OF PYLON SKIN, Y= 2075. FOUND NOT CARRIED OUT IN ACCORDANCE WITH APPROVED DATA. REPAIR REMOVED AND NEW REPAIR INSTALLED AS PER E.A. 1-5410-143549. E.O. 1-5100-7-5001 A5 PART 1. REPAIR CLASSIFIED AS MAJSDR FDEA201104151494Skin · misrepairedNR 2 ENGINE PYLON FOUND AN REPAIR ON RT SIDE OF PYLON SKIN, Y= 2300. FOUND NOT CARRIED OUT IN ACCORDANCE WITH APPROVED DATA. EXISTING REPAIR REMOVED AND NEW REPAIR INSTALLED AS PER FEDEX E.A. 1-5410-143549. E.O. 1-5100-7-5001 A5 PART 1. REPAIR CLASSIFIED SDR CA110415001Skin · delaminated(CAN) LT UPPER FWD NACELLE COVER PANEL STARTED DELAMINATING AND TEARING BACK WHILE IN FLIGHT. PASSENGERS NOTIFIED THE FLIGHT CREW AND THE ACFT LANDED WITHOUT INCIDENT. ANOTHER PANEL WAS INSTALLED AND ACFT RETURNED TO SERVICE.SDR A6WA201140424Skin · chafedLT LOWER CORE COWL CHAFED ON OUTER SKIN NEXT TO DOUBLE LATCH, C/W CMM 71-12-01.SDR UIEA2011041000242Skin · crackedENGINE COWLING - NR 4 RT ENGINE CORE COWL OUTER SKIN - CRACK - REPAIR - DURING MX WALKAROUND, MX FOUND A CRACK ON THE NR 4 RT CORE COWL OUTER SKIN. THE CIRCUMFERENTIAL CRACK IS APPROX 1 IN LONG. THE LENGTH OF THE CRACK EXCEEDS THE SRM LIMITS. (DISPOSITION ISDR IPXA11566109Skin · gougedINSPECTION TYPE: MOD NR 2 PYLON INBD SIDE GOUGE ON PYLON EXTERNAL SKIN 4.5" AFT OF T/R HINGE. REPAIRED IAW ER 11-02315, AND EO B757-5450-42265-A.SDR FDEA201104051324Skin · corrodedNR 1 PYLON, OTBD SIDE FWD SKIN HAS CORROSION IN PANEL 433AL CUTOUT AREA AT PP STA 107.00. EVALUATE AND RECTIFY. NR 1 PYLON OTBD SIDE FWD SKIN CUTOUT FLANGE CORROSION AT PP STA 107.00. REPAIRED IAW EA F-5450-135888. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-SDR IPXA11566083Doubler · gougedINSPECTION TYPE:MOD, RT AFT FAIRING STRUCTURE FWD RT NUTPLATE SPLICE MACHINED DOUBLER IS GOUGED ON THE TOP INBD SIDE AND CHANGED ON THE OTBD SIDE. REMOVE, FABRICATED AND INSTALL IAW DWG 313N5025, AND SRM 51-40-02.SDR KCSA111092Skin · crackedNR 1 PYLON EXTERIOR SKIN APPROX NAC STA 221 LEFT, HALF MOON CUTOUT SCREW HOLE CRACKED.SDR DHLA201100042Skin · wornNR 4 ENG INLET NACELLE COWL UPPER SKIN WORN STA, YN 147.000 AT 12 O'CLOCK POS. PERFORMED MAJOR REPAIR IAW SRM 71-5-2, FIG 2, SHEET 1,2,3. REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED AREA & FABRICATED SKIN & SPLICE IAW SRM 71-5-2 FIG 2, SHEET 1,2,3. HSDR EIAA2011032Skin · tornNR 3 PYLON SKIN TORN NAC STA 190.0. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 471-54-293-2.SDR FDEA201103301247Skin · damagedNR 3 ENGINE NOSE COWL O/B T/E SKIN DAMAGED AT 4:30 POAITION. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER, AND INSTALLED REPAIR PARTS IAW SRM 51-10-1, 51-30-2, 54-30-3 FIG 8.SDR UIEA2011032900233Panel · wornNR 3 ENGINE PYLON PANEL NR 472QR BOLT HOSE WORN. (REPAIR IAW EGAT EZ T2P011A54B-688)SDR UIEA2011032900232Panel · wornNR 2 ENGINE PYLON PANEL NR 462QR BOLT HOLES WORN. (REPAIR IAW EGAT E2 NR T2Q11A54B-687)SDR KO0R2011F00078Skin · crackedNR 3 PYLON INBD SIDE LOWER EDGE CRACKED (MIGRATED INTO DOUBLER).SDR A6WA201140302Skin · damagedINSPECT QEC FOR DAMAGE INCURED WHEN ENGINE STAND BROKE AND REPAIR AS NECESSARY- FIXED CORE COWL OUTER SKIN AND STIFFENER DAMAGED WHEN REAR MOUNT BROKE DURING TRANSITION ON TRUCK. REPAIRED ENGINE ASSY CF34-381, SN 873714. FIXED CORE COWL OUTER SKIN AND STIFFESDR KCSA111088Skin · gougedNR 4 PYLON I/B SKIN GOUGED UNDER FIRESHIELD AT NAC STA 217.SDR KCSA111077Skin · crackedNR 1 PYLON TOP SKIN CRACKED AT AFT EDGE NAC STA 222, LBL 1, .5 INCHSDR KCSA111076Skin · crackedNR 2 PYLON TOP SKIN CRACKED AT FASTENER HOLE RBL 2 NAC STA 221, .5 INCH.SDR KCSA111071Skin · crackedNR 4 PYLON TOP SKIN HAS TWO .5 INCH CRACKS AT NAC STA 222.SDR KCSA111068Strap · crackedNR 2 PYLON HAS TWO .5 INCH CRACKS IN THE SKIN STRAP AT THE TOP OF THE PYLON, LT SIDE NAC STA 221.9SDR KCSA111067Strap · crackedNR 1 PYLON HAS A .3 INCH CRACK IN THE TOP SKIN STRAP AFT ROW LT SIDE NAC STA 221.9SDR KCSA111066Strap · crackedNR 4 PYLON HAS A .2 INCH CRACK IN THE CAP SKIN STRAP AFT FASTENER ROW, RT SIDE NAC STA 221.9SDR USAA2011040491322Skin · crackedCLT - Q5/QX6 - CRACK ON RIGHT PYLON SKIN AT ACCESS PANEL CUTOUT 5828R UPPER CORNER. REPAIRED RIGHT PYLON SKIN AT ACCESS PANEL CUTOUT 5828R UPPER CORNER IAW TYPICAL REPAIR B737-5430-10-0054.SDR USAA2011033191301Skin · crackedCLT - Q5/QX6 - CRACK ON OUTBOARD SIDE OF NR 2 ENGINE PYLON SKIN AT LOWER FORWARD CORNER OF PANEL 5823R. REPAIRED OUTBOARD SIDE OF NR 2 ENGINE PYLON SKIN AT LOWER FORWARD CORNER OF PANEL 5823R IAW EA 102766 & B737 SRM 51-40-02 & 51-10-02.SDR IPXA1665734Skin · crackedINSPECTION TYPE:C, NR 2 PYLON - ACCESS PANEL 442AL CUTOUT SKIN CRACKED APP. 2 " LONG. NR 2 PYLON ACCESS PNL 442AL CUTOUT SKIN REPAIRED IAW R54-54-36993 & 767-5430-42012, CRACK LENGTH 2", CRACK STOP AT FASTENER HOLE, THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIRSDR UALA2012031601731Fastener · faultyPYLON ACCESS PANEL 443BL HAS 3 SCREWS AND 3 INDICATORS THAT NEED REPLACING. REPLACED FASTENERS AND REINSTALLED PANEL.SDR A6WA201140186Skin · chafedLT LOWER COWL CHAFED BY FWD LATCHES DAMAGED WITHIN BLENDABLE LIMITS AND REPAIRED IAW REO 601R-71-12-2326.SDR UIEA2011031400184Access Panel · worn1 FASTENER HOLE WORN OUT ON NR 3 STRUT. ENG-TO-WING FAIRING ACCESS PANEL 472 EL. (REPAIR IAW E NR T2011A54B-563, REV 00 AND REV. 01.)SDR JR2R2011031300087Skin · crackedHINGE LINE FAIRING PNL 443BB/433BT CRACKED. FABRICATED HINGE FAIRING SKIN IAW CRJ 900 SRM 51-42-36.SDR A6WA201140185Skin · erodedLT ENGINE NOSE COWL LIP SKIN PITTED & ERODED. REPAIRED LT ENGINE NOSE INLET COWL LIP SKIN IAW REO 601R-71-61-2532, REV C.SDR FDEA201103070895Panel · crackedNR 2 STRUT OTBD SIDE PRECOOLER EXHAUST LOUVER PANEL 443CR HAS CRACK ALONG LOWER VANE AREA APPROX 1 INCH IN LENGTH. CRACKED LOUVER R & R IAW AMM 20-11-00. REPAIR IS CLASSIFIED AS MINOR.SDR UALA2011030701120Panel · dentedPANEL 423BL HAS 2 DENTS IN PYLON SKIN PANEL. TOP DENT IS 4X 2.75D-.0625 DEEP, LOWER DENT IS 4 X 3-. 0125 DEEP. BOTH DENTS WERE WITHIN RATIO FOR CARRY FORWARD TO THE NEXT 'C' CHECK 26SEPT2012 BUT NOT TO EXCEED 04NOV, 2012 (20 MONTH LIMIT OR PTC 25306) PER SRM.SDR U2RA464M85463Access Panel · crackedNR 4 PYLON UPPER L/E CAP FAIRING HINGE IS CRACKED 2 PLACES ON OTBD SIDE.SDR DALA1115239877Doubler · crackedCRACK ON REPAIR DOUBLER AT PYLON 2 AFT APRON SECTION WEB IN FRONT OF AFT MOUNT FITTING INSIDE ACCESS 8206A. REMOVED REPAIR DOUBLER IAW DC-9 SRM 51-30-5 PARA 8. HFEC INSPECTION PREV STOP DRILL NO PROGRESSION NOTED. FABBED REPAIR IAW SRM 54-01 FIG 2 SHEET 2 DSDR UALA2011030100996Panel · crackedON WALKAROUND FOUND CRACKED PANEL ON PYLON PANEL 437AR ON INBD SIDE OF NR 1 ENG. CRACK MEASURES 3.250 LONG. REPLACED PYLON PANEL 437AR.SDR UALA2011022800966Panel · peelingNR 1 AFT OTBD PYLON FAIRING PANEL AT NAC STATION 352.80 HAS METAL OVERLAY PEELING UP. MEASURES 3 INCH BY 4.5 INCH ACP TEMP REPAIR PER EVA UAL 80580, PANEL SECURE. REMOVED NR 1 OUTBOARD PYLON PNL 313T3381-203 AND ROUTED TO SHOP 273. REMOVED AND REPLACED 4299SDR V0XR20110225003Skin Panel · corroded(V0XR) SKIN LOCATED BELOW RIGHT FINGERNAIL FOUND TO BE CORRODED BEYOND LIMITS. REPLACED SKIN PER DASH8-100 SRM 51-10-00, 51-40-00, 51-40-11. FABRICATED PARTS FROM DASH8-100 DRAWINGS FOR STIFFNER RIBS.
Back to JASC 5414