# JASC 1410: Hoses and Tubes - Type: JASC system/component code (FAA) - ATA chapter: 14 Hardware - Title in the code table: HOSES AND TUBES - Service difficulty reports: 23 - FAA code table: https://www.faa.gov/sites/faa.gov/files/JASC_Code.pdf#page=14 - Page: https://openairdocs.org/jasc/1410 ## What it covers For reports indicating a problem with any aircraft or engine hose or that are not associated a specific aircraft system. ## Service difficulty reports (23) - [SDR 1SMA20221214001](https://openairdocs.org/sdr/1SMA20221214001), Dec 14, 2022: Piper PA31350. HOSE. LEAKING. DURING CRUISE FLIGHT, THE PILOT NOTICED THE RIGHT ENGINE OIL PRESSURE SUDDENLY INDICATED 0 PSI. THE NEAREST AIRPORT WAS (N35475) - [SDR 2022FA0000254](https://openairdocs.org/sdr/2022FA0000254), May 10, 2022: Piper PA44180. HOSE. BUCKLED. DURING TAKE OFF ROLL, THE PILOT REPORTED LOSS OF POWER - ABORTED TAKEOFF. TROUBLESHOT AND FOUND THE AERODUCT HOSE P/N: 6 (N360LU) - [SDR HXXC2022031422](https://openairdocs.org/sdr/HXXC2022031422), Mar 12, 2022: Beech A100. HYDRAULIC LINE. CORRODED. PILOT RH BRAKE FAILED WHILE TAXIING. FOUND 1/4" ALUMINUM LINE BELOW FLOOR CORRODED PIN HOLE. (N479AK) - [SDR 2022FA0000119](https://openairdocs.org/sdr/2022FA0000119), Feb 18, 2022: Cessna 525. FUEL LINE. CRACKED. AS TOLD BY MAINTENANCE TECHNICIAN JEFF SHAW: CREW REPORTED THE ENGINE HAD GENERATOR FAIL WITH VIBRATION FOLLOWED BY ENGI (N741CC) - [SDR 9JLA2021120722965](https://openairdocs.org/sdr/9JLA2021120722965), Dec 1, 2021: Gulstm GIV. HYDRAULIC LINE. LEAKING. THE MAINTENANCE TEAM REPORTED THAT DURING POSTFLIGHT CHECKS FINDING THE LEFT AILERON ACTUATOR HOSE LEAKING FLUID. THE MA (N120SB) - [SDR CA111117024](https://openairdocs.org/sdr/CA111117024), Nov 17, 2011: HOSE. INACCURATE. (CAN) PART WAS RECEIVED NEW FROM AN AMERICAN VENDOR. PART WAS MFG BY VENDOR AND MARKED WITH THE ACFT MFG PN ONLY. VENDOR - [SDR CA111117023](https://openairdocs.org/sdr/CA111117023), Nov 17, 2011: HOSE. INACCURATE. (CAN) PART WAS RECEIVED NEW FROM AN AMERICAN VENDOR. PART WAS MFG BY VENDOR AND MARKED WITH THE ACFT MFG PN ONLY. VENDOR - [SDR CA111117022](https://openairdocs.org/sdr/CA111117022), Nov 17, 2011: HOSE. INACCURATE. (CAN) PART WAS RECEIVED NEW FROM AN AMERICAN VENDOR. PART WAS MANUFACTURED BY VENDOR AND MARKED WITH THE ACFT MFG PN ONL - [SDR CA111117021](https://openairdocs.org/sdr/CA111117021), Nov 17, 2011: HOSE. INACCURATE. (CAN) PART WAS RECEIVED NEW FROM AN AMERICAN VENDOR. PART WAS MANUFACTURED BY VENDOR AND MARKED WITH THE ACFT MFG PN ONL - [SDR CA111117020](https://openairdocs.org/sdr/CA111117020), Nov 17, 2011: HOSE. INACCURATE. (CAN) PART WAS RECEIVED NEW FROM AN AMERICAN VENDOR. PART WAS MANUFACTURED BY VENDOR AND MARKED WITH THE ACFT MFG PN ONL - [SDR CA111117018](https://openairdocs.org/sdr/CA111117018), Nov 17, 2011: HOSE. INACCURATE. (CAN) PART WAS RECEIVED NEW FROM AN AMERICAN VENDOR. PART WAS MFG BY VENDOR AND MARKED WITH THE ACFT PN ONLY. VENDOR IS - [SDR CA111117012](https://openairdocs.org/sdr/CA111117012), Nov 17, 2011: HOSE. INACCURATE. (CAN) PART WAS RECEIVED NEW FROM AN AMERICAN VENDOR. PART WAS MFG BY VENDOR AND MARKED WITH THE ACFT MFG PN ONLY. THIS S - [SDR QMLR10082009](https://openairdocs.org/sdr/QMLR10082009), Oct 8, 2009: Bell 412. HOSE. MISMANUFACTURED. RECEIVED FROM INVENTORY NEW HOSE ASSY AND ATTEMPTED TO INSTALL. HOSE HAS A STRAIGHT NR 10 CONNECTION ON ONE END AND A 90 - [SDR 2006FA0000407](https://openairdocs.org/sdr/2006FA0000407), Apr 14, 2006: Piper PA32R301T. HOSE. DETERIORATED. PARTIAL POWER LOSS, TWO CYLINDERS DROPPED OUT, CAUSED BY SMALL PARTICLES OF RUBBER HOSE FROM UPPER DECK AIR REFERENCE LI (N126LM) - [SDR CA050817008](https://openairdocs.org/sdr/CA050817008), Jul 19, 2005: Cndair CL6002B19. BLOCK. WORN. (CAN) DURING AN INSPECTION AME FOUND DAMAGE ON NR 2 HYDRAULIC CASE DRAINLINE UPSTREAM OF RESERVOIR. DAMAGE CAUSED BY WOR - [SDR CA050817007](https://openairdocs.org/sdr/CA050817007), Jul 19, 2005: Cndair CL6002B19. BLOCK. WORN. (CAN) DURING AN INSPECTION AME FOUND DAMAGE ON NR 2 HYDRAULIC SUCTION LINE UPSTREAM OF RESERVOIR DAMAGE CAUSED BY WORN F - [SDR 2004FA0000843](https://openairdocs.org/sdr/2004FA0000843), Oct 22, 2004: Beech E90. HOSE. DETERIORATED. DURING CLIMB OUT, OIL PRESSURE ON BOTH ENGINES DROPPED TO APPROXIMATELY 50 PSI WITH SLIGHT SURGING. AUTOFEATHER WAS ENGA (N3741M) - [SDR PG9R97903](https://openairdocs.org/sdr/PG9R97903), Oct 21, 2004: Doug MD900. LINE. LEAKING. FOUND TO BE LEAKING A SMALL QUANTITY OF OIL/ REPLACED OIL HOSE ASSY. (K) (N368PA) - [SDR UXCR200400002](https://openairdocs.org/sdr/UXCR200400002), Aug 26, 2004: Piper PA46350P. HOSE. FLAKING. DURING CLIMB TO ALTITUDE, THE ENGINE EXHIBITED A ROUGH RUNNING CONDITION THAT NECESSITATED A REDUCTION IN POWER REQUIRIN (N4128K) - [SDR GTIA040726](https://openairdocs.org/sdr/GTIA040726), Aug 17, 2004: Doug DC983. B-NUT. LOOSE. DTW - FOUND FORWARD CABIN HAS A HEAVY FUEL ODOR, AFT CABIN IS FINE. FOUND B-NUT LOOSE AT FORWARD AUX TANK VENT FITTING D (N832NK) - [SDR 2004FA0000608](https://openairdocs.org/sdr/2004FA0000608), Jun 25, 2004: Gulstm GV. LINE. LOOSE. AT FL 410 RECEIVED A CABIN PRESSURE LOW (RED) MESSAGE ON YTHE CAS. AIRCRAFT INITIATED EDM APPROX. FL 380 CAS MESSAGE EXT (N300K) - [SDR 2004FA0000334](https://openairdocs.org/sdr/2004FA0000334), Mar 3, 2004: Amtr VORTEX. HOSE. IMPROPER PART. THE VACUUM LINE GOING TO THE FUEL PNEUMATIC PUMP HAD AN IRREGULAR PART INSTALLED. THE MM REQUIRES A HARD, NON-COLLAPSIBL (N96XV) - [SDR 2003FA0000771](https://openairdocs.org/sdr/2003FA0000771), Jul 18, 2003: Stbros SD360300. LINE. BROKEN. AIRCRAFT WAS CROSSING THE NORTH ATLANTIC BETWEEN GREENLAND AND ICELAND AND ONCE THEY REACHED CRUSING ALTITUDE THE LEFT E ## Other codes in chapter 14 - [JASC 1400](https://openairdocs.org/jasc/1400): Miscellaneous Hardware (42 reports) - [JASC 1420](https://openairdocs.org/jasc/1420): Electrical Connectors (215 reports) - [JASC 1430](https://openairdocs.org/jasc/1430): Fasteners (705 reports) - [JASC 1497](https://openairdocs.org/jasc/1497): Miscellaneous Wiring (9 reports) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.