N987HA
Registered owner: GOODMAN SETH A, IL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
109 reports on file, 1997-06-12 – 2012-12-27.
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 38,888 hrs · 40,813 cycles
CORROSION ON INSIDE OF SKIN, AROUND AIRSTAIR DOOR DRAIN BRACKET AND INBD INTERCOSTAL AT AFT SIDE OF DOOR HINGE, X=250, Y=49L, BETWEEN STRINGER 24 AND 25L. R & R INTERCOSTAL BETWEEN STRINGER 24 AND 25L AT X=250, Y=49L IAW SRM 51-10-00, 51-40-07, 51-40-10, 51-40-11, 51-42-05 AND RD 8-53-3450.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,685 hrs · 40,614 cycles
LEFT FORWARD EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED BULB ON FORWARD LEFT EGRESS EMERGENCY LIGHT.
Part: LINE — LEAKING (HYD SYSTEM) · airframe 38,417 hrs · 40,352 cycles
FLIGHT 2760, RETURNED TO FIELD DUE TO HYD SYS 1 FLUID LOSS. UPON ARRIVAL, THE INDICATION WAS 0 PERCENT. INSTALLED FLEX LINE.
Part: BATTERY — DISCHARGED (CABIN) · airframe 38,328 hrs · 40,262 cycles
FWD CEILING EMERGENCY LIGHT INOP. R2 FWD LT CEILING EMERGENCY POWER SUPPLY BATTERY PS3.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,328 hrs · 40,262 cycles
LT AFT EGRESS LIGHT OUT. R2 BULB.
Earlier reports · 1997–2011 · 104 reports
2011
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,811 hrs · 39,773 cycles
ALL EMERGENCY EXIT LIGHTS DEAD. R2 NR 3 AND NR 4 BATTERY PACKS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,370 hrs · 39,332 cycles
F/A POS LIGHT CONTROL EMERGENCY SWITCH LIGHT OUT. R2 BULB IN PB SWITCH LIGHT.
Part: FLASHLIGHT — LOW (CABIN) · airframe 37,142 hrs · 39,087 cycles
ONE FLIGHT DECK EMERGENCY FLASHLIGHT DIM. R2 1 EA FLIGHT DECK EMERGENCY FLASHLIGHT.
Part: BATTERY — WEAK (FLASHLIGHT) · airframe 36,849 hrs · 38,812 cycles
F/A FLASHLIGHT DIM. R2 BATTERIES.
Part: WIRE — EXPOSED (CABIN) · airframe 36,786 hrs · 38,758 cycles
EMER FLOOR LIGHT WIRING EXPOSED. MX RE-SECURED WIRING & RELAMPED.
Part: ESCAPE HATCH — DIRTY (COCKPIT) · airframe 36,668 hrs · 38,640 cycles
AIR LEAK ON COCKPIT ESCAPE HATCH. CLEANED, LUBED & INSTALLED HATCH.
Part: GAUGE — INACCURATE (COCKPIT) · airframe 36,621 hrs · 38,598 cycles
NR 1 NL GAUGE INACCURATE IN FLT. R2 NR 1 NL GAUGE.
Part: TAB — DAMAGED (RT ELEVATOR) · airframe 36,610 hrs · 38,588 cycles
RT ELEVATOR SPRING TAB T/E DAMAGED.
Part: SKIN — DEBONDED (TAILCONE) · airframe 36,609 hrs · 38,588 cycles
PERM REPAIR FOR A LARGE AREA DISBONDED ON TAIL CONE.
Part: SKIN — CRACKED (AILERON) · airframe 36,609 hrs · 38,588 cycles
RIGHT AILERON LOWER SKIN CRACKED AT INNER TRIM TAB HINGE CUTOUT.
Part: SKIN — DENTED (RUDDER) · airframe 36,609 hrs · 38,588 cycles
AFT RUDDER UPPER SKIN DENTED. REPAIRED AFT RUDDER UPPER SKIN IAW DASH 8 RO DHC 82-55-1101.
Part: EXHAUST DUCT — CRACKED (ZONE 400) · airframe 36,609 hrs · 38,588 cycles
RIGHT ENGINE EXHAUST OUTLET SHROUD ASSY INNER LINER CRACKED.
Part: SPOILER — DENTED (RT WING) · airframe 36,610 hrs · 38,588 cycles
RT INNER ROLL SPOILER UPPER SURFACE DENTED IN 2 EA AREAS. C/W PERMANENT REPAIR TO RT INNER ROLL SPOILER UPPER SURFACE IAW RO DHC82-27-1085.
Part: STRUCTURE — CHAFED (RT NACELLE) · airframe 36,610 hrs · 38,588 cycles
RT NACELLE OUTBOARD WHEEL HUMP CHAFED THRU 100 PERCENT. REMOVED AND REPLACED RT OUTBOARD WHEEL HUMP IAW DASH 8 SRM 51-42-05.
Part: PIN — BROKEN (NR 1 BRAKE) · airframe 36,567 hrs · 38,547 cycles
NR 1 BRAKE WEAR PIN BROKEN. RE-SECURED PIN.
Part: ESCAPE HATCH — UNSECURE (COCKPIT) · airframe 36,567 hrs · 38,547 cycles
COCKPIT HATCH IS UNLATCHED. INSPECTED & SECURED HATCH.
Part: BRAKE — LEAKING (NR 1) · airframe 36,561 hrs · 38,541 cycles
NR 1 BRAKE LEAKING. R2 NR 1 BRAKE ASSY.
Part: AUTOFEATHER SYS — MALFUNCTIONED (COCKPIT) · airframe 36,406 hrs · 38,386 cycles
AUTO FEATHER W/N ARM-RTG. MX PERFORMED CTR TRIM AND RUN TRIM ON BOTH ENGINES.
Part: FUEL CAP — LEAKING (FUEL SYSTEM) · airframe 36,396 hrs · 38,378 cycles
FUEL CAP BROKEN, FUEL DRIPPING FROM CONX. MX REPLACED FUEL CAP.
Part: CONNECTOR — DIRTY (AUTOFEATHER SYS) · airframe 36,396 hrs · 38,378 cycles
ATO-AUTO FEATHER DISARM T/O ROLL. CLEANED DEBRIS 1/2 SIG COND PLUGS, TAKEOFF POWER OPS NORMAL.
Part: PSU — UNSECURE (CABIN) · airframe 36,396 hrs · 38,378 cycles
ROW 9 LT PSU UNSECURED. RE-SECURED PSU.
Part: PSU — UNSECURE (CABIN) · airframe 36,329 hrs · 38,312 cycles
ROW 9A PSU HANGING DOWN. MX RE-SECURED PSU.
Part: HOOK AND LOOP — UNSECURE (EMERGENCY ROPE) · airframe 36,241 hrs · 38,237 cycles
EMERGENCY ROPE COVER NOT SECURED. MX SECURED VELCRO.
Part: SIGNAL COND UNIT — FAULTY (AUTOFEATHER SYS) · airframe 36,235 hrs · 28,230 cycles
AUTO FEATHER SYS DID NOT ARM ON T/O. MX REPLACED 6121-K5 RELAY AND BOTH SIGNAL CONDITIONING UNITS.
Part: RELAY — INOPERATIVE (AUTOFEATHER SYS) · airframe 36,203 hrs · 38,202 cycles
AUTO FEATHER DID NOT ARM, CREW ABORTED T/O AND RETURNED TO GATE. MX REPLACED RELAY 6121K5.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,154 hrs · 38,160 cycles
WHITE FLOOR LIGHT MARKER LIGHT 5DF INOP. MX RELAMPED.
Part: COVER — UNKNOWN (CABIN) · airframe 36,153 hrs · 38,160 cycles
FLOOR LIGHT MARKERS 3DF AND 6DF COVERED. MX RE-INSTALLED FLOOR LAMP COVERS.
Part: RELAY — FAILED (AUTOFEATHER SYS) · airframe 36,128 hrs · 38,140 cycles
AUTO FEATHER WOULD NOT TEST. MX REPLACED RELAY 6121K5.
Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 36,121 hrs · 38,136 cycles
AUTO FEATHER WILL NOT ARM, RETURNED TO GATE. MX OPS CHECK NORMAL.
Part: AUTOFEATHER SYS — MALFUNCTIONED · airframe 36,106 hrs · 38,125 cycles
AUTOFEATHER TEST FAILED. MX OPS CHECK GOOD.
Part: ENGINE — FIRE (NR 1) · airframe 36,082 hrs · 38,102 cycles
NR 1 ENG CAUGHT FIRE DURING START-UP, ENGINE FIRE BOTTLES WERE USED TO SUCCESSFULLY EXTINGUISH THE FIRE. MX C/W INSPECTION.
Part: LIGHT — INOPERATIVE (NR 2 STEP) · airframe 36,085 hrs · 38,105 cycles
NR 2 STEP LIGHT INOP. MX RE-LAMPED.
Part: BRAKE ASSY — LEAKING (NR 2 MLG) · airframe 35,944 hrs · 37,978 cycles
NR 2 MLG BRAKE LEAKING. MX REMOVED AND REPLACED NR 2 BRAKE ASSY.
Part: BELLCRANK — DEFECTIVE (NLG DOOR) · airframe 35,936 hrs · 37,969 cycles
NLG DOOR CTN WHEN SELECTED DOWN. MX R2 BELL CRANK ASSY.
Part: NACELLE — DAMAGED (RIGHT) · airframe 35,927 hrs · 37,960 cycles
DAMAGE TO RIGHT NACELLE. MX COMPLIED WITH PERMANENT REPAIR.
2010
Part: BRAKE ASSY — LEAKING (MLG) · airframe 35,819 hrs · 37,866 cycles
NR 1 BRAKE LEAKING. MX REPLACED NR 1 BRAKE ASSY, OPS AND LEAK CHECK GOOD.
Part: BRAKE — LEAKING (NR 3) · airframe 35,817 hrs · 37,865 cycles
NR 3 BRAKE LEAKING. MX REPLACED THE NUMBER THREE BRAKE.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,810 hrs · 37,860 cycles
TOP AIR STAIR DOOR LIGHT INOP. MX RELAMPED AIR STAIR DOOR LIGHT.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,774 hrs · 37,822 cycles
NR 2 EMERGENCY LIGHT INOP. MX R2 NR 2 BATTERY PACK.
Part: BATTERY PACK — DISCHARGED (CABIN)
NR 3 EMERGENCY LIGHTS BATTERY PACK DEAD. MX R2 NR 3 BATTERY PACK.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 35,763 hrs · 37,813 cycles
EMERGENCY LIGHTS UNCONTROLLABLE. MX REPLACED NR 1 POWER SUPPLY, OP CHECKS GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,610 hrs · 37,658 cycles
SEVERAL EMERGENCY LIGHTS IN CABIN INOP. MX RELAMPED.
Part: STRUT — CRACKED (ENTRY DOOR) · airframe 35,564 hrs · 37,616 cycles
UPPER FWD AIRSTAIR DOOR STRUT CRACKED. MX REMOVED AND REPLACED UPPER STRUT.
Part: BUSHING — MISSING (PAX DOOR) · airframe 35,564 hrs · 37,616 cycles
FWD LWR AIRSTAIR STRUT LOWER BUSHING MISSING. MX INSTALLED THE MISSING BUSHING IN PHX.
Part: COVER — DAMAGED (ESCAPE HATCH) · airframe 35,506 hrs · 37,558 cycles
CREW ESCAPE HATCH COVER DAMAGED. MX REMOVED AND REPLACED COVER.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,362 hrs · 37,416 cycles
RIGHT AFT EXT EMERGENCY LIGHT INOP. MX RELAMPED.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,250 hrs · 37,311 cycles
ROW 1 SIDEWALL EMERGENCY LIGHTS INOP. R2 NR 2 BATTERY PACK.
Part: SIGNAL COND UNIT — INOPERATIVE (AUTOFEATHER SYS) · airframe 35,203 hrs · 37,267 cycles
AUTOFEATHER W/N ENGAGE AUTOFEATHER WILL NOT ENGAGE (RTG). MX R & R NR 1 SIGNAL CONDITIONER UNIT.
Part: FLASHLIGHT — MISSING (COCKPIT) · airframe 35,152 hrs · 37,211 cycles
COCKPIT FLASHLIGHT MISSING. MX INSTALLED FLASHLIGHT.
Part: LIGHT — BROKEN (CABIN) · airframe 34,970 hrs · 37,015 cycles
ROW 4DF EMERGENCY EXIT LIGHT BROKEN. MX REMOVED AND REPLACED SIDE WALL EXIT IDENTIFIER, OPS GOOD.
Part: O-RING — CUT (HYDRAULIC SYS) · airframe 34,951 hrs · 36,996 cycles
ASH FLT 2850 YUM - PHX EXPERIENCED A COMPLETE LOSS OF NR 1 HYDRAULICS. THE CREW HAD THE AIRCRAFT TOWED TO THE GATE UPON LANDING IN PHX. MX FOUND AND REPLACED A CUT O-RING AT THE NR 1 HYDRAULIC PRESSURE TRANSDUCER.
Part: WIRE — LOOSE (CABIN) · airframe 34,912 hrs · 36,955 cycles
ROW 8/9DF LOOSE WRING ON TRACK LIGHTING. MX SECURED LOOSE WIRING.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,781 hrs · 36,827 cycles
AFT CABIN FLOOR TRACK LIGHT OUT. MX R2 BULB.
Part: STRIP — LOOSE (CABIN) · airframe 34,676 hrs · 36,728 cycles
FWD RT FLOOR EMERGENCY LIGHT STRIP LOOSE. MX RE-SECURED.
Part: COVER — BROKEN (CABIN) · airframe 34,612 hrs · 36,664 cycles
FORWARD EMERGENCY LIGHT TRACK COVER BROKEN. MX REPLACED TRACK COVER.
Part: TRACK — LOOSE (CABIN) · airframe 34,546 hrs · 36,602 cycles
FWD RT SECTION OF EMERGENCY LIGHT TRACK LOOSE. MX RE-SECURED LIGHT TRACK.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,525 hrs · 36,578 cycles
FWD 2ND RED EMERGENCY LIGHT OUT. MX RELAMPED FWD 2ND RED EMERGENCY LIGHT.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 34,488 hrs · 36,540 cycles
FLIGHT ATTENDANT FLASHLIGHT NOT FUNCTIONAL. MX REPLACED THE BATTERIES.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,017 hrs · 36,116 cycles
SEVERAL EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 5 EMERGENCY LIGHT BATTERY, OPS CHECK GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,808 hrs · 35,919 cycles
ONE RED LIGHT ON FLOOR EMERGENCY TRACK LIGHTING OUT. RELAMPED RED LIGHT ON FLOOR EMERGENCY TRACK LIGHTING, OPS CHECK GOOD.
2009
Part: UNKNOWN — ODOR (COCKPIT) · airframe 33,479 hrs · 35,623 cycles
ASH FLT 2857 PHX-FLG. ELECTRICAL BURNING SMELL FROM CAPT'S FLIGHT INSTRUMENTS. MX INSPECTED AND FOUND NO DEFECTS.
Part: SOCKET — DEFECTIVE (CABIN) · airframe 33,070 hrs · 35,237 cycles
ASH FLT 2852 FLG-PHX. BURNING SMELL COMING FROM OVERHEAD BIN 1DF. MX FOUND THE FWD CEILING LIGHT ON RT AFT CONNECTOR HAS MELTED AND CAUSING SMELL. MX REMOVED AND REPLACED SOCKET.
2007
Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,758 hrs · 31,256 cycles
ASH FLT 2907 PHX-GJT - PILOT REPORTED NO LIGHTED EXIT SIGNS IN CABIN. MX COULD NOT DUPLICATE, FUNCTIONAL CHECK GOOD.
Part: ACCESS PANEL — DAMAGED (FUSELAGE) · airframe 28,748 hrs · 31,246 cycles
RT SIDE FUSELAGE ACCESS PANEL FASTENER HOLE AT ST 25 IS DAMAGED AND ELONGATED, REPAIRED.
Part: SKIN — TORN (NR 2 NACELLE) · airframe 28,748 hrs · 31,246 cycles
FOUND DAMAGE TO THE NR 2 ENGINE NACELLE. DAMAGE IS A TEAR IN THE LOWER SKIN PANEL AND EXCEEDS THE LIMITS. MX PERFORMED REPAIR.
Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 28,748 hrs · 31,246 cycles
RT NR 1 FLAP TRACK HAS MINOR CORROSION, REPAIRED.
Part: STRUCTURE — DAMAGED (LT ELEVATOR) · airframe 28,612 hrs · 31,108 cycles
LIGHTNING STRIKE ON LT ELEVATOR TRAILER EDGE. COMPLIED WITH PERMANENT REPAIR AND CHECKED THE BALANCE OF THE ELEVATOR.
Part: STARTER GEN — MALFUNCTIONED (NR 1 ENGINE) · airframe 28,306 hrs · 20,784 cycles
ASH FLT 2860 FLG-PHX. DECLARED EMERGENCY FOR NR 1 ENGINE FIRE ON ENGINE SHUT DOWN. WHEN THE CREW WAS SHUTTING THE ENGINE DOWN THE CAPTAIN NOTICED SMOKE AND SPARKS COMING FROM THE NR 1 ENGINE. MX INSPECTED ENGINE AND FOUND NO EVIDENCE OF A FIRE, BUT FOUND THE DC STARTER GENERATOR IS BAD. THE DC STARTER GENERATOR IS WHAT CAUSED THE SMOKE AND SPARKS. MX IS CHANGING THE NR 1 DC STARTER GENERATOR.
Part: COVER — BROKEN (CABIN) · airframe 27,838 hrs · 30,299 cycles
ASH 2894 PHX. EMERGENCY PATH LIGHTING AT SEAT 1D COVER BROKEN. MX REPLACED COVER.
Part: DUCT — DIRTY (CABIN AIR) · airframe 27,619 hrs · 30,372 cycles
ASH 2858 FLG. UNCOMMANDED HEAT IN AUTO & MANUAL MODE OF THE AIR CONDITIONING PACK IN FLIGHT AND A POSSIBLE FIRE IN THE AFT EQUIPMENT BAY. MX INSPECTED AND FOUND IT TO BE DIRT.
Part: SOCKET — BURNED · airframe 27,597 hrs · 30,052 cycles
ASH 2805 PHX. AIRCRAFT WAS ON GROUND, CREW SMELLED SOMETHING BURNING. MX REMOVED AND REPLACED SOCKET.
Part: STRUT — BROKEN (PAX DOOR) · airframe 27,482 hrs · 29,935 cycles
ASH 2897 DRO - PASSENGER DOOR AFT STRUT BROKEN. REMOVED & REPLACED AFT UPPER STRUT.
Part: SEAT TRACK — DIRTY (FUSELAGE) · airframe 27,356 hrs · 29,801 cycles
ASH 2760 PHX. F/A JUMP SEAT DOES NOT AUTO RECLINE. MX CLEANED AND LUBED THE SEAT TRACKS, OPS CHECK GOOD.
Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 26,894 hrs · 29,388 cycles
ASH 2993 PHX - CREW REPORTED NUMEROUS FALSE LAV SMOKE WARNINGS WITH ENGINES RUNNING. MX REPLACED SMOKE DETECTOR.
Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 268,889 hrs · 29,378 cycles
ASH 2841 FLG. CREW REPORTED NUMEROUS FALSE SMOKE WARNING CALLS FROM THE LAV. MX REPLACED THE SMOKE DETECTOR.
2006
Part: SPU — FAILED (RT HYD SYS) · airframe 25,959 hrs · 28,493 cycles
ASH 2858 FLG. RIGHT HYDRAULIC SYSTEM FAILED IN FLIGHT. MX IS IN THE PROCESS OF TROUBLESHOOTING MX. REMOVED AND REPLACED SPU AND EDP.
Part: STARTER GEN — FAILED (NR 2) · airframe 25,186 hrs · 27,746 cycles
ASH 6255 PHX. NR 2 DC GEN CAUTION LIGHT AND HOT LIGHT, MAIN BATTERY WARNING ALONG WITH SMOKE FROM THE NACELLE. MX TROUBLESHOT TO THE DC STARTER GENERATOR. MX R2 STARTER GENERATOR AND STARTER CONTACTOR. OPS CHECK GOOD.
Part: PRESSURE SWITCH — MALFUNCTIONED (RUDDER PRESSURE) · airframe 24,892 hrs · 27,457 cycles
RUDDER PRESS ANNUNCIATOR DURING TAXI. MAINTENANCE REMOVED AND REPLACED NR 1 AND NR 2 PRESSURE SWITCHES.
Part: LIGHT — LOOSE (GALLEY) · airframe 24,609 hrs · 27,205 cycles
GALLEY EMERGENCY LIGHT STRIP WAS LOOSE. MX RESECURED THE LIGHT STRIP.
Part: SERVO — MALFUNCTIONED (AUTOPILOT) · airframe 24,343 hrs · 26,975 cycles
AUTO PILOT WILL NOT ENGAGE. MAINTENANCE REMOVED AND REPLACED THE AILERON SERVO.
Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 24,327 hrs · 26,961 cycles
ASH 6472 PHX - EMERGENCY ESCAPE PATH LIGHT COVER LOOSE. MAINTENANCE RESECURED LIGHT COVER.
Part: CONNECTOR — LOOSE (GUIDANCE COMP) · airframe 24,283 hrs · 26,924 cycles
LT YAW DAMPNER CHANNEL INOP IN FLIGHT. MX RESECURED THE NR 1 FLIGHT GUIDANCE COMPUTER CONNECTION AND THE SYSTEM OPS CHECKED GOOD.
Part: LIGHT — LOOSE (EMERGENCY LIGHT) · airframe 24,100 hrs · 26,767 cycles
EMERGENCY FLOOR PATH LIGHTING STRIP LOOSE. MAINTENANCE REMOVED AND REPLACED LIGHTING STRIP COVER.
Part: DIODE — FAILED (EMERGENCY LIGHT) · airframe 24,088 hrs · 26,752 cycles
FLOOR PROX ILLUMINATION EMERGENCY ESCAPE PATH LIGHTING INOP. MAINTENANCE REMOVED AND REPLACED FLOOR DIODE.
2005
Part: SIGN — LOOSE (EMERGENCY EXIT) · airframe 23,989 hrs · 26,662 cycles
SEAT 1C EMERGENCY EXIT SIGN HANGING DOWN. MAINTENANCE RE-SECURED THE SIGN.
Part: SWITCH — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,989 hrs · 26,662 cycles
F/A EMERGENCY LIGHT SWITCH INOP. MAINTENANCE TROUBLESHOT AND COULD NOT DUPLICATE, OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,901 hrs · 26,579 cycles
SEVEN OF THE EMERGENCY FLOOR PATH LIGHTS WERE INOP. CND. OPS CHECK GOOD.
Part: SELECTOR — MALFUNCTIONED (CABIN PRESSURE) · airframe 23,820 hrs · 26,507 cycles
ASH 6322 PHX. AIRCRAFT DIVERTED TO DRO WHEN THE CABIN WOULD NOT PRESSURIZE IN AUTO. MAINTENANCE REPLACED PRESSURE CONTROLLER, CONTROL PANEL AND STATIC SOURCE SELECTOR.
Part: ACM — SMOKE · airframe 23,292 hrs · 25,986 cycles
ASH 6377 PHX. SMOKE AND ASH IN THE CABIN AND COCKPIT. MX TROUBLESHOT AND FOUND THAT THE ACM WAS STARTING TO COME APART. MAINTENANCE REPLACED THE ACM.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,163 hrs · 25,868 cycles
ASH 6282 PHX. DURING PREFLIGHT, THE RIGHT EXT EMERGENCY LIGHTS WOULD NOT TURN OFF AFTER A SUCCESSFUL TEST WITHOUT THE APPLICATION OF GROUND POWER. MX CHANGED THE BATTERY PACK AND FOUND OPS TO BE NORMAL.
Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 23,110 hrs · 25,828 cycles
ASH 6370 YUM. THE NR 2 BAGGAGE COMP SMOKE DETECTOR INOP. REPLACED DETECTOR.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,449 hrs · 25,216 cycles
CREW REPORTED FWD WHITE LIGHT ESCAPE PATH INOP. MX REMOVED AND REPLACED ESCAPE PATH LIGHT.
Part: SIGN — DISLODGED (EMERGENCY EXIT) · airframe 22,205 hrs · 24,987 cycles
THE FORWARD EMERGENCY EXIT LIGHT FELL FROM ITS MOUNT. MAINTENANCE RE-ATTACHED THE SIGN.
Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 21,674 hrs · 24,521 cycles
ASH 6347 HMO PHX RETURNED TO THE FIELD DUE TO THE NR 2 HYD SYSTEM FAILED ON GEAR RETRACT. MAINTENANCE ARE IN THE PROCESS OF TROUBLESHOOTING. MAINTENANCE INSTALLED A TEMP FLEX LINE ON NR 2 HYD PRESS TRANSDUCER TO FLY THE AIRCRAFT BACK TO PHX. LATER THE FLEX LINE WAS REPLACED WITH THE PERMANENT HYD LINE. TEMP LINE P/N AE2460000E0200 (VARGA ENTERPRISES).
2004
Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 20,974 hrs · 23,896 cycles
ASH 7015 PHX DRO, EMERGENCY EXIT LIGHT DOES NOT GO OFF WITH SWITCH OFF OPERATION. REMOVED AND REPLACED FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH. CHECKED GOOD AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT.
Part: CONTROL UNIT — FAILED (NR 1 ENGINE) · airframe 20,528 hrs · 23,436 cycles
RETURNED TO THE GATE DUE TO AN UNCOMMANDED AUTOFEATHER OF NR 1 ENGINE. MEL'D AUTOFEATHER SYSTEM AFTER VERIFYING IT WAS AT FAULT. 7/21 MAINTENANCE REPLACED TSCU, OPS CHECKED GOOD.
2003
Part: SOCKET — OVERHEATED (CABIN LIGHT) · airframe 18,375 hrs · 21,223 cycles
CREW REPORTED SMOKE COMING FROM THE OVERHEAD CABIN LIGHT AT ROW 1 D/F. FOUND AFT LIGHT SOCKET OVERHEATED. REPLACED SOCKET.
Part: HYDRAULIC LINE — BURST (NOSE GEAR WELL) · airframe 18,068 hrs · 20,908 cycles
Lost number 2 hydraulic quantity in flight. Replaced nose gear up line.
2002
Part: LINE — MALFUNCTIONED (HYD SYSTEM) · airframe 16,893 hrs · 19,748 cycles
NR 2 HYDRAULIC CAUTION LIGHT CAME ON AND REMAINED ON AT GEAR RETRACTION, LANDING GEAR REMAINED IN TRANSIT. PREFORMED ALTERNATE EXTENSION. ON LANDING NR 2 HYDRAULIC PRESSURE RETURNED TO NORMAL. BLED AND SERVICED NR 2 HYDRAULIC SYSTEM. AIRCRAFT RELEASED FOR EVALUATION FLIGHT.
2000
Part: RELAY — INOPERATIVE (MLG) · airframe 11,770 hrs · 14,382 cycles
WHEN THE GEAR WAS SELECTED UP THE IT DID NOT RETRACT. AIRCRAFT RETURNED TO THE FIELD. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY BUT DID FIND INCORRECT GEAR INDICATION LIGHT SEQUENCING. REPLACED RELAY 3261-K13.
Part: SOCKET — ARCED (ROW 7) · airframe 11,279 hrs · 13,801 cycles
BETWEEN FLIGHTS A CABIN CEILING LIGHT AT ROW 7AC OVERHEAD BIN WAS REPORTED AS ARCING,SMOKING AND BURNING. REPLACED BULB SOCKET.
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 11,218 hrs · 13,730 cycles
NR 1 AND NR 3 EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOP. REPLACED BATTERY PACK 3351-PS2.
1998
Part: TIRE — FAILED (NLG)
MCO - FLT 3090 - LEFT NOSE TIRE DISINTEGRATED ON TAKEOFF AND DAMAGED LEFT NOSE GEAR DOOR, NOSE GEAR WIRE HARNESS AND DENTED FUSELAGE AFT OF GEAR WELL. REPLACES BOTH NOSE WHEEL ASSEMBLIES AND REPAIRED AFFECTED ITEMS. (M)
1997
Part: FORE RUDDER — CRACKED (VERTICAL STAB)
DISCREPANCY FOUND DURING A-CHECK. THE LOWER SURFACE OF FORE RUDDER WAS FOUND CRACKED. REPAIRED IAW EO8-27-97-925. (X)