JASC 5410
Service difficulty reports · 4,110
Reports filed under 5410 · Nacelle/Pylon, Main Frame, 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 = '5410' 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 = '5410' 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 CALA2025012100163Plate · corrodedLH PYLON SPIGOT FITTING CORRODED ON INNER BEARING SURFACE. REMOVED AND REPLACED LH PYLON SPIGOT FITTING PLATE IAW A319 SRM 54-51-12-300-002.SDR CALA2025012100162Spar · crackedR/H PYLON O/B SLIDE SPAR DOUBLER HAS CRACK. R & R R/H PYLON O/B SPAR IAW A320 SRM 51-75-12-911-001.SDR AALA202501210467Spigot · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON SPIGOT FITTING BETWEEN PYLON RIB 7 AND 8. REPLACED SPIGOT FITTING PER SRM 54-51-12.SDR AALA202502194193Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON SPIGOT FITTING RECEPTACLE. REPLACED SPIGOT FITING PER SRM 54-51-12.SDR JR2R20250117994Acoustic Panel · nicked#1 ENG INLET COWL INNER BARREL LOWER ACOUSTIC PANEL HAS 3 NICKS.SDR DALA2025011700417Drag Fitting · crackedSHIP 694 A.D.//A.A. CRACK INDICATION ON OPEN HOLE # 1 ON FITTING BTW 12-1 O CLOCK POSITION FROM LH ENG DRAG FTG CLAMP-UP. (IN REF: CARD 5720-01100-04A JOB # 081-0001 STEP 14). CORRECTIVE ACTION: SUMMARY OF NRC 251: CRACK INDICATION ON OPEN HOLE # 1 ON FITTING SDR UIEA2025011000022Fire Seal · damagedENGINE 2 LH CORE COWL (427AL), ZONE CC5, FIRE SHIELD WITH SEALANT DAMAGE.(<P>ENGINE 2 LH CORE COWL (427AL), ZONE CC5, FIRE SHIELD SEALANT WAS RESTORED IAW AMM 78-31-00-308-072-H00. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025011000024Fire Seal · wornENGINE #1 NACELLE STRUT FIRE SEAL ON NAC STA 256 INBOARD AND OUTBOARD SIDE WITH WEAR.(<P>ENGINE #1 NACELLE STRUT FIRE SEAL ON NAC STA 256 INBOARD AND OUTBOARD SIDE WAS REPLACED IAW SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED</P>)SDR VNAA20250121003Fan Cowl · dentedTRFKE00AP6E2:EA23-C9-54-0795-PERM REPAIR BEFORE 19,894.41 FH - DOOR ASSY, FAN COWL, LWR (LH)ORRECTIVE ACTION: SUMMARY: DOOR ASSY, FAN COWL, LWR (LH) WAS REPAIRED PER REO 670-54-14-1012. REV. B. AND REO 690-54-14-761 REV -- (P1).SDR SWAA2025011585220Fairing · crackedPER M-23-154-01884-TLD; #1 ENGINE PYLON AFT STRUT SUPPORT FAIRING REPAIR REQUIRED<[01] REMOVED AND REPLACED #1 ENGINE PYLON AFT STRUT SUPPORT FAIRING ASSY PER SRM 51-40-05 AND SRM 51-40-02.<BR>TOPCOAT OF NEW PYLON SUPPORT IS REQUIREDSDR SWAA2025012384772Strut · delaminatedRIGHT WING LOWER FIXED LEADING EDGE; WING STATION 204.25; INBOARD OF NACELLE STRUT; HAS A DELAMINATION AT THE TRAILING EDGE. MARKED.<[01] REPAIRED PER SRM 51-70-06-2R-1; DETAIL E. REFERENCE TSR# 202500299 FOR CLARIFICATION ON ALTERNATE USE OF RESIN P/N.;[02] CSDR IPXA2025013160750Hinge Fitting · damaged#1 ENG INBD FAN COWL AFT HINGE ARM CHAFFED. VERIFIED INSTALLATION OF NEW HINGE FITTING USING EXISTING FASTENERS IAW A300-600 SRM 51-40-21 WITH SEALANT P/N 04-001-0114, BATCH 0004321398 IAW A300-600 SRM 51-76-10.SDR IPXA2025020649678Duct · crackedFAULT: STR-540-#2 ENGINE PRECOOLER AIR DUCT CRACKED DOT# 110-71 JP-110. ACCOMPLISHED PERMANENT REPAIR PER EO-92575-REQ1 AND VTMAE EA 300-3611-27-A3759 REV-. REVIEWEDSDR R61A2025010400016Inlet · crackedDURING HEAVY CHECK L/H PYLON PRE COOLER INLET DUCT BRACKET SUPPORT FOUND CRACKED. REMOVED AND REPLACED BRACKET IAW AMM 36-11-08SDR AALA202501178830Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON INBOARD LOWER POSITION SHACKLES BOLT AT PYLON RIB 4. REPLACED BOLT PER TASK CARD 26C42554028.SDR AALA202501175170Spigot · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON LOWER SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12.SDR AALA202501172938Spigot · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON LOWER SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12.SDR SWAA2025012487079Bracket · damaged[DOT: Z048] RIGHT WING L/E CAVITY INBD OF PYLON HAS PNEUMATIC DUCT INBD SUPPORT BRACKET HAS ELONGATED HOLE. (STREAMER ATTACH)<[01] REMOVED & REPLACED R/W L/E I/B BLEED AIR SUPPORT BRACKET ASSY PN: 212A1214-9ATSMRO BN: 562974 IAW B737-800 SRM 51-40-02 & BAC DWGSDR UIEA2024122901190Panel · loose#2 ENGINE I/B CORECOWL HINGES DAMAGED, DIFFICULT TO OPEN AND CLOSE. REQUIRES EVALUATION.(<P>EVALUATED AND FOUND SKIRT PANEL WITH LOOSE AND MISSING FASTENERS. LOCATED AND INSTALLED NEW FASTENERS IAW SRM 51-40-02-06. OPS CHECK GOOD.</P>)SDR AALA202502255964Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON MEASURES OF CORROSION ARE L= 12.200INCH, W=1.300INCH, D=0.003INCH. MAINTENANCE REPLACED SPIGOT FITTING ON LH PYLON IAW AMM 54-51-41-000-001-A, A319 SRM 54-51-12-300-001 AND AMM 54-5SDR AALA202502258786Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FITTING BORE OF PYLON SPIGOT RECEPTACLE IN RH PYLON MEASURES OF CORROSION ARE L=12.00INCH, W=1.27INCH, D=0.003INCH. MAINTENANCE REPLACED SPIGOT FITTING ON RH PYLON IAW AMM 54-51-41-000-001-A, A319 SRM 54-51-12-300-001 ANSDR DALA2024122612010Heat Shield · damagedSHIP 3308 ELONGATED FASTENER HOLES COMMON TO AN EXISTING REPAIR WAS FOUND ON THE #2 ENGINE LAPF LOWER HEAT SHIELD. CORRECTIVE ACTION: REPAIRED PER ERA 623079-14. (0725383)SDR AALA202501025363Transition Panel · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT HHAND WING UPPER TRANSITION PANEL JUST AFT OF PYLON LOWER WEB IS CRACKED AT OUTBOARD UPPER CORNER. REMOVED AND REPLACED LOWER WEB AT RIGHT HAND WING UPPER TRANSITION PANEL JUST AFT OF PYLON-B. PER B737-NG AIPC 57-50-00--36A,SDR AALA202502034794Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON L=14.2 INCH W=1.34 INCH D=0.006 INCH. MAINTENANCE REPLACED LOWER SPIGOT FITTING BTW RIB 4 TO RIB 5 LH PYLON IAW A320 SRM 54-51-12-300-001.SDR AALA202502030804Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON L=13.6 INCH W=1.32 INCH D=0.007 INCH. MAINTENANCE REPLACED LOWER SPIGOT FITTING BTW RIB 4 TO RIB 5 RH PYLON IAW A320 SRM 54-51-12-300-00.SDR DALA2024122011856Fairing · crackedSHIP 3307 FOUND CRACK ON #1 ENG LOWER AFT PYLON FAIRING LOWER SKIN. CORRECTIVE ACTION: REPAIRED PER ERA 622965-14 REV ORIGINAL. (0718107)SDR CALA2024121301493Latch · malfunctioned#2 ENGINE O/B FAN COWL ,LATCH SAFETY ASSEMBLY FOUND NOT HOOKED UP AT LOWER END OF FAN COWL. VERIFIED INSTALLATION HARDWARE, AND RESECURED #2 ENGINE O/B FAN COWL SAFETY LATCH REF SOPM 20-50-01 AND AIPC 71-11-06-01. OPS CHECKED GOOD.SDR 3EJA828JS121024Cowling · detachedDESCENDING THROUGH FL200 HEARD VERY LOUD BANG FOLLOWED BY LEFT ENGINE FAILURE. AFTER ARRIVING AT SIGNATURE I FOUND THE LEFT ENGINE COWLING HAD FALLEN OFF THE AIRCRAFT.SDR DALA2024121111622Fitting · damagedSHIP 3165 DAMAGE WAS FOUND ON THE NO.1 PYLON FORWARD SPIGOT FITTING. CORRECTIVE ACTION: COMPLIED WITH ER/A 31-622911. (0704015)SDR DALA2024121111612Frame Angle · crackedCRACK ON FRAME CLIP (ENGINE PYLON SUPPORT BULKHEAD) IN STA Y=1022 AT L7 LH. SUMMARY OF NRC 00536: FRAME CLIP (ENGINE PYLON SUPPORT BULKHEAD) IN STA Y=1022 AT L7 LH WAS REPAIRED PER ERA 622468-14 REV ORIGINAL. (LP #0703045)SDR SWAA2025011483538Inlet · pulled#2 ENGINE INLET COWL LIP SKIN OUTER AFT ROW MULTIPLE FASTENERS DO NOT FLUSH WITH THE SKIN AT POSITION FROM 1 O'CLOCK TO 2 O'CLOCK POSITION.<[01] RECIEVED NEW/SERVICEABLE #2 ENGINE INLET COWL PN: 314M2100-503 SN: 3117001. INLET COWL INSTALLED ON CARD #TTG8Q00S7SDR UIEA2024120301163Latch · brokenENG #2 NACELLE STRUT, INBOARD ACCESS PANEL WITH LATCH BROKEN.(<P>REMOVED DAMAGED LATCH AT ENG #2, NACELLE STRUT INBOARD ACCESS PANEL AREA, LOCATED, CLEANED, TRIMMED, SECURED, ADJUSTED, SAFETY WIRE, INSTALLED NEW LATCH AS REQUIRED AT ENG #2 NACELLE STRUT, INBOASDR AALA202412303276Stiffener · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT PYLON OUTBD CUTOUT FRAME IS CRACKED AT UPPER MIDDLE SECTION. REPLACED STIFFENER ASSEMBLY PER SRM B787-A-51-43-05-03A-010A-A.SDR AALA202412232154Bracket · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED CROSSOVER BEAM BRACKET ON LEFT HAND PYLON. REPLACED BEAM BRACKET PER AMM 78-32-44.SDR FDEA202411291753Fitting · gouged#1 ENG WERE OB SHEAR TIE (FWD OF SKIRT BEAM) HAS CHAFFED INTO THE FWD BULKHEAD OF TORQUE BOX. DURING CURRENT HMV CHECK IN INDIANAPOLIS, IN (IND), MAINTENANCE DISCOVERED CHAFE AND GOUGE DAMAGE TO THE LH PYLON AFT ENGINE MOUNT BULKHEAD FITTING, P/N 311T2261SDR CALA2024120201383Door · missingPDA 2 #1 ENGINE RH INBOARD TR MID PANEL 416FR HINGE AND SMALL DOOR ASSY FOUND MISSING ON ARRIVAL SEE LP 3042567. MISSING COMPONENT APPROX 6X3 INCHES, METALLIC IN CONSTRUCTION. A/C LANDED ON RUNWAY 1R AND AIRPORT OPS ADVISES RUNWAY CHECKED NO DEBRIS WAS FOUND SDR UIEA2024112801126Fairing · damagedENG #2 AFT FAIRING WITH SEVERAL SCREWS MISSING(<P>LOCATED, CLEANED, PREPARED, SECURED AND INSTALLED MISSING HARDWARE AT #2 ENG, AFT FAIRING, PER BOEING 767-300 SRM 51-40-02-0G-0. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024112801125Fairing · damagedENG #1 AFT FAIRING WITH SERVERAL SCREW MISSING(<P>LOCATED, CLEANED, PREPARED, SECURED AND INSTALLED MISSING FASTENER AT ENG #1, AFT FAIRING PER BOEING 767-300 SRM 51-40-02-0H-0. NO FURTHER DEFECTS NOTED</P>)SDR FDEA202411271750Door · delaminatedRH PYLON PNL# 447BL FOUND WITH MISSING TOP FIBERGLASS SKIN PLYS MISSING AND PAINTED OVER. REPAIRED TOP SKIN ON RH PYLON (PNL#447BL/MPN: 313T3341-9110) IN REF. TO 767 SRM 54-52-70- 2R FIG. 201 SHEET 4, AND 767 SRM: 51-70-08. THIS IS A MAJOR REPAIR. SEE JPF FSDR UIEA2024112201099Skate Angle · crackedCRACK ON LH SKATE ANGLE ON STRUT #2 (FOUND DURING SEALANT REMOVAL)(<P>A SEGMENT OF THE SKATE WITH CRACK WAS REMOVED, AND THE NEW SEGMENT WAS MANUFACTURED AND INSTALLED IAW FVCI CONTROL EO 24190-2. NO FURTHER DEFECTS NOTED.</P>)SDR DALA2024112711246Fitting · corrodedSHIP 3145 CORROSION SPIGOT FITTING RECEPTACLE BORE ON RH PYLON. CORRECTIVE ACTION: REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON PER A319 SRM 54-51-12-300-001, AND A319 SRM 51-44-11-801. (0680425)SDR CALA2024112202921Door · missingPDA 2 FOUND DOOR NACELLE ASSY. ON E2 SIDE ALSO MISSING. REF. L/P 9904036 ON LOCATION 436/446. REQUESTING CDL DEFERRAL PER CDL 54C. DEFERRED PER CDL 54C. COMPLIED WITH DDP. INSTALLED PLACARD.SDR DALA2024112111124Junction Box · crackedSHIP 3166 FWD OTBRD CORNER OF #2 PYLON ELECTRICAL JUNCTION BOX CRACKED. CORRECTIVE ACTION: REPAIRED PER A319 SRM 54-50-00. (0670518)SDR SWIA2025010601120Doubler · crackedTHERE APPEARS TO BE A CRACK IN THE LH ENGINE PYLON DOUBLER BEHIND THE HYDRAULIC PRESSURE LINE QD FITTING (C-CHECK RO 12/21/2024) (FILED CLOSED)REMOVED AND REPLACED WITH NEW DOUBLER ON LH ENGINE PYLON DOUBLER BEHIND THE HYDRAULIC PRESSURE LINE QD FITTING. REF.SDR DALA2024112111120Fitting · corrodedSHIP 3136 CORROSION SPIGOT FITTING RECEPTACLE BORE ON RH PYLON. CORRECTIVE ACTION: REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON AS PER A319 SRM 54-51-12-300-001. (0669385)SDR IXXA20241120001Rub Strip · worn#1 ENGINE I/B CORE COWL L/E INTERNAL RUB STRIP WORN AND PEELED BACK AT LOWER ENDSDR IXXA20241511002Bracket · excess playBRACKET ASSY. - PYLON HOLD OPEN ROD.SDR IXXA20241114008Frame · gouged#2 ENG CORE COWL O/B INSIDE 2ND FRAME LOWER FROM AFT HAS GOUGE. REPAIRED WITH 8110-3.SDR DALA2024111410963Fitting · corrodedSHIP 3145 CORROSION SPIGOT FITTING RECEPTACLE BORE ON LH PYLON. CORRECTIVE ACTION: REPLACED SPIGOT FITTING RECEPTACLE AND FASTENERS ON LH PYLON AS PER A319 SRM 54-51-12-300-001 AND AS PER A320 FAM AMM54-51-41-400-001-A. (0658391)SDR IXXA20241113001Attach Bracket · broken#2 PYLON, IB SIDE, ATTACH BRACKET FOR FAIRING 447DB IS BROKEN. REQUIRED 8110-3 DUE TO CHEMICAL CONVERSION IN LIEU OF SULFURIC ACID ANODIZING.
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