JASC 5597

System/component code · Stabilizer System Wiring

Service difficulty reports
14
FAA table
Page 52

From the FAA's JASC code table (October 2008), the codes service difficulty reports use.

What it covers

For reports indicating a problem with wiring specific to the Stabilizer Systems.

Service difficulty reports · 14

Reports filed under 5597, newest first.

19982026
Service difficulty reports filed under 5597 per year, 1998–2026: 14 reports
19982
20031
20041
20051
20071
20192
20202
20211
20221
20231
20261
SDR IPXA2026080187673Angle · corrodedLEFT HORIZONTAL STAB REAR SPAR TO ELEVATOR FRONT SPAR BONDING WIRE AND ATTACH BRACKETS HAVE CORROSION AT OTBD SIDE OF OTBD HINGE. INSTALLED ONE ANGLE IAW SRM 51-40-02-0G-0 & AMM 20-11-00-912-001.Jul 21, 2026 · N438UP · Boeing 75724APFSDR DALA2023111409357Unknown · unknownSHIP 3119 BROKEN BONDING PLATE HINGE ARM 2 ON RH ELEVATOR. CORRECTIVE ACTION: REPLACED BONDING PLATE HINGE ARM 2 ON RH ELEVATOR AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0063093)Nov 13, 2023 · N319NB · Airbus A319114SDR AALA202301039353Bonding Jumper · damagedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ELEVATOR HAS DAMAGED BONDING STRAP. REPLACED RIGHT HAND ELEVATOR BONDING STRAP JUST OUT BOARD OF ELEVATOR ACTUATOR FITTING. BOND CHECK GOOD PER AMM 20-28-00.Dec 21, 2022 · N104NN · Airbus A321231SDR QXEA2021052100256Wire Harness · out of positionDURING E-28-0007 FUEL QUANTITY HARNESS INSPECTION, FOUND RIGHT GROUND SPOILER HARNESS P0746 TY-WRAPPED TO THE FUEL QUANTITY HARNESS. REMOVED P0746 FROM THE FUEL QUANTITY HARNESS AND SECURED THE FUEL QUANTITY HARNESS AND HARNESS P0746 IAW E175 AMM 28-41-06-400-May 19, 2021 · N636QX · Emb ERJ170200LRSDR SWIA202054443Bonding Wire · corrodedRT ELEVATOR INBOARD HINGE BONDING WIRE HARDWARE IS CORRODED AND OUTBOARD HINGE BOLT AND ANTI ROTATION HARDWARE ARE CORRODED. C-CHECK RO 11/24/2020. REMOVE AND REPLACED CORRODED HARDWARE AT INBOARD HINGE BONDING WIRE AND OUTBOARD HINGE BOLT AND ANTI ROTATION Nov 12, 2020 · N928EV · Cndair CL6002B19SDR SWIA202054442Bonding Wire · corrodedLT ELEVATOR INBOARD HINGE BONDING WIRE HARDWARE IS CORRODED AND OUTBOARD HINGE BOLT AND ANTI ROTATION HARDWARE ARE CORRODED. C-CHECK RO 11/24/2020. REPLACED LT ELEVATOR INBOARD HINGE BONDING WIRE HARDWARE, OUTBOARD HINGE BOLT AND NUT AND ANTI ROTATION HARDWANov 12, 2020 · N928EV · Cndair CL6002B19SDR SWIA202002248802Bonding Jumper · corrodedRIGHT ELEVATOR #4 HINGE ATTACH HARDWARE AND BONDING JUMPER HARDWARE ALSO SAFETY KEEPER HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED RIGHT ELEVATOR # 4 HINGE HARDWARE CLEANED & REMOVED CORRISION FROM BONDING JUMPER AND SAFETY KEEPER HARDWADec 11, 2019 · N465SW · Cndair CL6002B19SDR SWIA202002248799Bonding Jumper · corrodedRIGHT ELEVATOR #1 HINGE ATTACH HARDWARE AND BONDING JUMPER HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED R/H ELEVATOR HINGE #1 ATTACHED HARDWARE AND BONDING JUMPER HARDWARE IAW CRJ-200. STS TORQUE WRENCH # 3816 , DUE 05-APR-20. REMOVED ADec 11, 2019 · N465SW · Cndair CL6002B19SDR DXTA200702651Wire · damagedH-STAB FAIL ANNUNCIATOR LIGHT ILLUMINATED IN FLIGHT. TROUBLESHOT SYSTEM FOUND TOO LARGE OF AN OHM SPLIT AT C/P 473 OF CONTROLLER, TRACED WIRING BACK TO TB061 STILL HAD LARGE SPLIT OHM DIFFERENCE. REMOVED LT STAB LEADING EDGE, REPAIRED CONNECTIONS AT TB060 ANDec 4, 2007 · N153QS · Beech 400ASDR 2006FA0000072Wire · shortedWHILE TROUBLESHOOTING INTERMITTENT UPPER BEACON CIRCUIT BREAKER FAULT, DISCOVERED LT ELEVATOR CONTROL CABLE HAD TORN THROUGH WIRING CONDUIT IN VERTICAL STABILIZER. THE CABLE WORE THROUGH THE CONDUIT AND SHORTED OUT THE WIRING FOR THE UPPER BEACON. REPAIRED WOct 15, 2005 · N601KF · Cndair CL6013ASDR AUS20040173Wire · wrong part(AUS) RT ELEVATOR TRIM TAB HINGE WIRE MANUFACTURED FROM MILD STEEL. RT TRIM TAB FREEPLAY 7.366MM (0.290IN) AND LT TRIM TAB FREEPLAY 9.829MM (0.387IN). MAXIMUM FREEPLAY 2.133MM (0.084IN). PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART.Feb 23, 2004 · Beech 95C55SDR 03FDEA00377Wire Harness · burnedHORIZONTAL STABILIZER CENTER SECTION TOP- WIRE BUNDLE AT THE RT INBOARD SIDE, INSIDE THE AFT FUSELAGE COMPT, FOUND BURNED AND DAMAGED DURING FSC RETURN-TO-SERVICE TEST.Apr 2, 2003 · N585FE · Doug MD11SDR CA980818002Wire · failed(CAN) LEFT ELEVATOR HORN HEAT CAUTION LIGHT ON DURING CLIMB. DUE TO FORECAST ICING CONDITIONS, AIRCRAFT RETURNED TO BASE. A WIRE BETWEEN CONNECTORS J3 AND J5 WAS FOUND BURNT AND OPEN. PART TC: 39,154.Jul 14, 1998 · Dhav DHC8102SDR 98ZZZX2446Wire · failedDURING LEVEL FLIGHT, A PITCH UP MOTION OCCURRED. UPON LANDING, THE LT FORWARD UPPER STREAMLINE TAIL WIRE HAD HAD AN APPARENT TENSION FAILURE AT MID-SPAN. ALL 8 TAIL WIRES WERE REPLACED ABOUT 2 YRS AND 100 HRS TIS AGO. THESE WIRES WERE PURCHASED FROM THE BELJun 5, 1998 · N9849B · Blanca 14192

Other codes in chapter 55 · 26

See all 26 codes in chapter 55