Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR C1HA200776001Blades · damagedAFTER 1.4 EPR CHECK, WHICH WAS COMPLETELY NORMAL, POWER WAS ADVANCED ON ALL ENGINES. AT APPROXIMATELY 1.6 EPR AND 60 KTS THE NR 1 PACK TRIP LIGHT ILLUMINATED FOLLOWED BY THE ENGINE FAIL LIGHTS. ABORTED THE TAKEOFF AT THAT POINT THE FLIGHT ATTENDANT HEARD A SERSDR C1HA200676003Duct · disconnectedAT 3000' IN CLIMB, LOWER AFT BODY OVERHEAT LT ILLUMINATED. RAN COM 2, 3, 6, 5, AND LT EXTINGUISHED. RETURNED TO IND. FOUND DISCONNECTED AIR DUCT IN AFT BAG BIN. REPLACED COUPLER. FUNCTIONAL TEST WING ANTI-ICE SYS CHECKS NORMAL REF MM 30-13-00.SDR CIHA200676001Support Angle · corrodedCOCKPIT R-5 WINDOW FRAME CORRODED. REMOVED AND REPLACED COCKPIT R-5 WINDOW FRAME SUPPORT ANGLE IAW SRM 51-30-2 FIG 1.SDR C1HA200676002Attach Angle · corrodedFWD LWR FUSELAGE (DOG HOUSE) LT HORIZ WALKWAY AT BS 328 AT WL 169- UNDERSIDE IB SIDE OF WALKWAY SKIN WEB AT CHORD ATTACHMENT ANGLE HAS EXFOLIATION CORROSION. REMOVED AND REPLACED CHORD PN 65-19862-19 IAW SRM 51-30-2 FIG 7,11,15.SDR C1HA200476004Floorbeam · corrodedCORROSION ON FLOORBEAM STA 1010 LBL 0 - 15 LBL. CLEAN, TREAT & INSTALLED REPAIR DOUBLER.SDR C1HA200476005Floorbeam · corrodedCORROSION ON FLOORBEAM STA 1010 LBL 0 - 15 LBL. CLEANED, TREATED & INSTALLED REPAIR DOUBLER.SDR C1HA200476001Switch · out of adjustADVANCED POWER LEVERS ABOVE 1.4 EPR AND TAKEOFF WARNING SOUNDED. OPS CHECK SYSTEM PER AD 88-22-09-01 STEP 9. ADJUSTED FLAP SWITCH.