N817AL
Registered owner: ZIPLINE INTERNATIONAL INC, CA (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.
117 reports on file, 1997-07-21 – 2007-10-28.
Part: SKIN — CRACKED (FUSELAGE) · airframe 47,546 hrs · 70,583 cycles
IN THE PROCESS OF ECO 3512, NDT INSPECTION DISCOVERED THE AFT CARGO DOOR CUTOUT AFT FRAME CRACKED. REPLACED THE FRAME IN ACCORDANCE WITH ECO 3512.
Earlier reports · 1997–2006 · 116 reports
2006
Part: PUMP — MALFUNCTIONED (FUEL BOOST) · airframe 46,299 hrs · 67,709 cycles
AFTER LEVELING OFF AT 21,000 FEET, THE NR 2 FORWARD FUEL BOOST PUMP LIGHT BEGAN FLICKERING ON AND OFF. THE CREW REVIEWED THEIR QRH AND CONTACTED MAINTENANCE CONTROL. MAINTENANCE CONTROL ADVISED THE CREW TO RETURN TO HNL DUE TO NO MAINTENANCE PERSONNEL IN HILO. THE CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE CHECKED THE AIRCRAFT AND PLACED THE NR 2 FORWARD FUEL BOOST PUMP ON MEL 28-1-1B. AIRCRAFT WAS RETURNED TO SERVICE.
2005
Part: LINE — OBSTRUCTED (PT2 SENSE)
CARGO FLT 820 HNL-OGG. AT CRUISE, CREW NOTED NR 1 ENGINE EPR 0.30 LESS THAN NR 2 ENGINE. N1 AND N2 SAME ON BOTH ENGINES. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED DEBRIS FROM THE NR 1 PT2 SENSE LINE PER AMM 72-00-00 AND RETURNED THE AIRCRAFT TO SERVICE.
Part: TRANSMITTER — DEFECTIVE (NR 1 EPR)
FLT 850 HNL - ITO. ON TAKEOFF, NUMBER 1 ENGINE PRESSURE RATIO INDICATION STOPPED INCREASING AT 170 WHILE THE NUMBER 2 ENGINE INDICATION OPERATED NORMALLY. CREW ABORTED TAKEOFF AT 80 KNOTS. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE EPR TRANSMITTER AND PERFORMED AN ENGINE HIGH POWER RUN UP WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.
2004
Part: LINE — LOOSE (NR 1 ENGINE)
NR 1 ENGINE WILL NOT REACH TAKEOFF POWER; REPORTED BY CREW. MAINTENANCE TROUBLE SHOOTING FOUND THE AFT PT7 LINE LOOSE. SECURED THE LINE; RAN ENGINE TO POWER. ALL PARAMETERS, OPS AND LEAK CHECK GOOD. SYSTEM CHECK OK. AIRCRAFT RETURNED TO SERVICE.
Part: DUCT — FAILED (NR 2 ENGINE) · airframe 43,855 hrs · 61,917 cycles
DURING CLIMB-OUT, THE NR 2 ENGINE OVERHEAT LIGHT CAME ON. RETURNED TO HNL. REMOVED AND REPLACED THE NR 2 ENGINE NOSE-COWL ANTI-ICE DUCT DUE TO LEAK AT THE BELLOWS. LEAK CHECK OK, AIRCRAFT RETURNED TO SERVICE.
Part: INDICATOR — FAILED (VERT SPEED) · airframe 43,831 hrs · 61,860 cycles
CAPTAINS VERTICAL SPEED INDICATOR INOPERATIVE. RETURN TO HNL. REPLACED VERTICAL SPEED INDICATOR, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: PITOT TUBE — CONTAMINATED (AIRSPEED) · airframe 43,721 hrs · 61,600 cycles
CAPTAINS AND FIRST OFFICERS AIRSPEED INDICATORS READ 20 KTS DIFFERENCE. RETURNED TO HNL. REMOVED FOD FROM PITOT TUBE, SYS OPS & LEAK CHECK GOOD IAW AMM 34-11-00. AIRCRAFT RETURNED TO SERVICE.
2003
Part: SKIN — CRACKED (FUSELAGE)
TRIMMED OUT DAMAGED AREA. VERIFIED CRACK FREE USING HFEC INSPECTION. FABRICATED REPAIR DOUBLER FORM 2024-T3. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAIR PARTS PER SRM 53-30-3, FIGURE 1. APPLIED FILLET SEAL WITH BMS 5-95 SEALANT AROUND EDGES OF REPAIR. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW ECO 3361. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CRACKED (FUSELAGE)
CUT OUT DAMAGED AREA. VERIFIED CRACK FREE USING HFEC. FABRICATED REPAIR PLATE. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAIR PARTS USING FASTENERS IDENTIFIED IN TABLE II. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)
REPLACED NR 2 FLOOR EMERGENCY LIGHT ASSEMBLY DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
2002
Part: APU — FAILED (APU BAY)
JUST AFTER TAKEOFF THE APU OVERSPEED LIGHT CAME ON AND THE APU SHUTDOWN. THE AIRCRAFT RETURNED AND LANDED, WITH NO FURTHER INCIDENT. REPLACED THE APU ACCESSORY UNIT AND THE THREE SPEED SWITCH. GROUND OPS CHECK GOOD AND AN OVERWEIGHT LANDING CHECK WAS COMPLETED. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: FLAP TRACK — DAMAGED (TE FLAPS)
FLAP TRACK ATTACHMENT FITTING HOLE ELONGATED. REPAIRED AND AIRCRAFT RETURNED TO SERVICE.
Part: SKIN — CRACKED (FUSELAGE)
BS 380 STRING 15R CRACK ON FUS SKIN. HFEC INSP EDGES ON CUTOUT, .040 IN INSUR CUT, FAB 2024-T3, CLAD SHEET .032 IN FILLER, .050 IN FILLER, AND .050 DOUBLER, MAINTAINING 2D MIN EDGE MARGIN, 2.0 INCH MIN INSIDE CORNER AND .5 IN MIN OUTSIDE CORNER RADIUS WITH CHAMF EDGES PRE-FORMED TO MATCH CONTOUR OF FUSELAGE. SURFACES TREATED WITH CHEMICAL CONVER COATING, TWO COATS, BMS 10-79, TYPE III PRIMER. INSTALL PARTS USING BACB30FP6AAT EXIST HI-LOK LOCATIONS. BACR15BB6AD ATTACH .032 FILLER TO SKIN POCKET, BACR15BB6D AT FASTENER LOCATIONS WET WITH BMS 5-95 SEALANT BETWEEN FAYING SURFACES. APPLIED BMS5-95 FILLET SEAL AROUND EDGES AND APPLIED CORROSION INHIBITING COMPOUND TO INTERN SURFACES. AC RETURNED TO SERVICE.
Part: LINE — OBSTRUCTED (NR 1 ENGINE)
DURING CLIMB THE NR 1 ENGINE EGT INDICATED 600 DEGREES C WITH THRUST LEVER 4 INCHES AHEAD OF THE NR 2 ENGINE THRUST LEVER. THE NR 1 ENGINE EPR WAS 1.73 AND THE NR 2 ENGINE EPR WAS 1.83. THE FLIGHT RETURNED AND LANDED WITH NO FURTHER INCIDENT. (ETOPS A/C ON NON ETOPS FLIGHT) MAINTENANCE INSPECTED THE NR 1 ENGINE AND REMOVED AN OBSTRUCTION IN THE PT2. POWER ASSURANCE CHECK WAS COMPLETED AT BOTH TAKEOFF AND CLIMB POWER SETTINGS. NO DEFECTS WERE NOTED AND THE AIRCRAFT RETURNED TO SERVICE.
Part: TRANSMITTER — INOPERATIVE (NR 1 ENGINE)
NR 1 ENGINE EPR DROPPED OFF ON CLIMB OUT OF 7,000 FEET. NR 1 ENGINE EPR WAS 1.73 AND NR 2 ENGINE EPR WAS 1.85. BOTH THE NR 1 AND NR 2 ENGINES NR 1 WAS 89 PERCENT AND NR 2 WAS 92 PERCENT. THE AIRCRAFT RETURNED AND LANDED IN HNL WITH NO FURTHER INCIDENT. (ETOPS A/C OR NON ETOPS FLIGHT) MAINTENANCE INSPECTED THE NR 1 ENGINE AND PURGED THE PT2 AND PT7 LINES. THE NR 1 ENGINE EPR TRANSMITTER WAS REPLACED IAW MM. A HIGH POWER RUN AND POWER ASSURANCE CHECK WAS COMPLETED ON THE NR 1 ENGINE. NO DISCREPANCIES WERE NOTED AND THE AIRCRAFT RETURNED TO SERVICE.
Part: SKIN — CRACKED (FUSELAGE)
IDENTIFIED A TWO INCH CRACK ON FUSELAGE SKIN AT BS274 STRINGER 15R. TRIMMED OUT DAMAGED SKIN, HFEC EDGE OF TRIMMED AREA WITH NO DEFECTS NOTED, FABRICATED FILLER AND DOUBLER. INSTALLED REPAIR PARTS IAW SRM. AIRCRAFT RETURNED TO SERVICE.
Part: SKIN — CRACKED (FUSELAGE)
IDENTIFIED A TWO AND A HALF INCH CRACK ON FUSELAGE SKIN AT BS 942 STRINGER 24R. TRIMMED OUT DAMAGED SKIN, HFEC EDGE OF TRIMMED AREA WITH NO DEFECTS NOTED, FABRICATED TWO EACH FILLER AND TWO EACH DOUBLER. INSTALLED REPAIR PARTS IAW SRM. AIRCRAFT RETURNED TO SERVICE.
Part: SKIN — CRACKED (FUSELAGE)
IDENTIFIED A TWO INCH CRACK ON FUSELAGE SKIN AT BS962 STRINGER 21L. TRIMMED OUT DAMAGED SKIN, HFEC EDGE OF TRIMMED AREA WITH NO DEFECTS NOTED, FABRICATED A FILLER AND DOUBLER. INSTALLED REPAIR PARTS IAW SRM. AIRCRAFT RETURNED TO SERVICE.
Part: SKIN — CRACKED (FUSELAGE)
IDENTIFIED ONE INCH CRACK ON FUSELAGE SKIN AT BS 277 STRINGER 11L. TRIMMED OUT DAMAGED SKIN, HFEC EDGE OF TRIMMED AREA WITH NO DEFECTS NOTED, FABRICATED A FILLER AND DOUBLER. INSTALLED REPAIR PARTS IAW SRM. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED FORWARD ENTRY DOOR IDENTIFIER POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE.
Part: LIGHT — DAMAGED (CABIN)
REPLACED FORWARD ENTRY DOOR IDENTIFIER LIGHT ASSEMBLY DUE TO DAMAGE. OPS CHECK, OK. AIRCRAFT RETURNED TO SERVICE.
Part: WIRE HARNESS — WORN (APU)
ENROUTE , THE APU SHUTDOWN DUE TO AN OVERSPEED. THE AIRCRAFT RETURNED WITHOUT FURTHER INCIDENT. MAINTENANCE RESTARTED THE APU AND CONDUCTED AN OPERATIONAL CHECK OF THE UNIT. THE OPERATIONAL CHECK WAS GOOD AND AN OVERWEIGHT LANDING INSPECTION WAS COMPLETED. THE AIRCRAFT WAS RELEASED AND RESTRICTED TO SERVICE DUE TO HF INTERFERENCE WITH THE APU OPERATION. INSPECTED THE APU WIRING AND REPAIRED A BROKEN/WORN HARNESS AT THE APU TACH GENERATOR. GROUND OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE.
Part: BATTERY PACK — INOPERATIVE (PAX CABIN)
REPLACED NR 2 FLOOR PATH EMERGENCY EXIT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
2001
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 2 FLOOR PROXIMATELY EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CORRODED (FUSELAGE)
DISCOVERED BULGING AT BS 1088, S-20R FUSELAGE SKIN. REMOVED THE CORRODED PORTION OF THE STRAP, FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER. RECEIVED 8110-3 APPROVAL. AIRCRAFT RETURNED TO SERVICE. (M)
Part: WINDOW FRAME — CRACKED (FUSELAGE)
PERFORMED WINDOW CORNER FASTENER HOLE INSPECTION PER S/B 737-53A1177R6 AND DISCOVERED DEFECTS IN NUMEROUS AREAS AT LT FUSELAGE WINDOW CORNERS; 2 BETWEEN BS 500-520 AND 33 BETWEEN BS 727-907, RT FUSELAGE WINDOW CORNERS; 8 BETWEEN BS 360-540 AND 1 AT BS 727A-727B FOR A TOTAL OF 44 DEFECTS NOTED AT WINDOW CORNERS UTILIZING HFEC METHOD. OVERSIZED FASTENER HOLE AND INSTALLED RIVET OR OVERSIZE HI-LOCK. THE FASTENER HOLES WITH THE 44 DEFECTS WERE OVERSIZED UNTIL THE INDICATIONS WENT AWAY OR REPAIRED WINDOW BY TRIMMING OUT CRACKED HOLES. INSTALLED FILLER, FABRICATED AND INSTALLED REPAIR DOUBLER, REPAIR TRIPLER, AND SPLICE PLATES. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CORRODED (LT WING)
DISCOVERED CORROSION ON LEFT LOWER WING SURFACE, WS 500. REMOVED CORROSION, CONFIRMED REMOVAL OF CORROSION, FLAP PEENED REWORKED AREAS PER SOPM 20-10-03. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CORRODED (LT WING)
DISCOVERED CORROSION AT LEFT LOWER WING SURFACE, WS 515.5. REMOVED CORROSION, CONFIRMED REMOVAL OF CORROSION, FLAP PEENED REWORKED AREAS PER SOPM 20-10-03. AIRCRAFT RETURNED TO SERVICE. (M)
Part: PRESSURE SWITCH — FAULTY (NR 1 ENGINE)
FLT 953 - ITO-HNL - DURING A NON-ETOPS QC CARGO FLIGHT, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT CAME ON. SHUTDOWN THE NR 1 ENGINE AND DECLARED AN EMERGENCY. UNEVENTFUL LANDING AT HNL. REMOVED AND REPLACED THE OIL BYPASS SWITCH IAW MM 79-35-011-4. INSPECTED AND REPLACED THE MAIN OIL FILTER. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 1 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — INOPERATIVE (PAX CABIN)
REPLACED NR 1 FLOOR EMERGENCY LGIHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: CSD — FAILED (NR 1 ENGINE)
FLT 915 - HNL-LIH - DURING FLIGHT, THE LOW OIL PRESSURE LIGHT CAME ON AND THE NR 1 ENGINE CSD GENERATOR WAS DISCONNECTED AQ MAINTENANCE WAS CONTACTED AND ADVISED PILOT TO RETURN TO HNL. AIRCRAFT RETURNED TO HNL AND BLOCKED IN T 0154 HOURS WITH NO FURTHER INCIDENT. THE CSD WAS REMOVED AND REPLACED PER MM 24-11-11 AND FORM M137. LEAK AND OPERATIONS CHECK WAS GOOD WITH NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: SKIN — DAMAGED (FUSELAGE)
FOUND FUSELAGE SKIN WRINKLE BETWEEN BS 663.75 AND BS 706, S13L AND S16L. (M)
Part: SKIN — DAMAGED (FUSELAGE)
FUSELAGE SKIN WRINKLE BETWEEN BS 663.75 AND BS 706, S13 AND S16. (M)
Part: FRAME — CRACKED (FUSELAGE)
FUSELAGE BS 727, STRINGER 18A LEFT OUTBOARD CHORD DETECTED CRACK BY METHOD OF HFEC INSPECTION. (M)
Part: FRAME — CRACKED (FUSELAGE)
FOUND FUSELAGE BS 727, STRINGER 18A RIGHT OUTBOARD CHORD DETECTED CRACK BY METHOD OF HFEC INSPECTION. (M)
Part: SKIN — CRACKED (FUSELAGE)
DURING HARD LANDING INSPECTION, DISCOVERED 2 INCHES CRACK AT BS 540, STRINGER 1R AND 2R, VERIFIED BY USING HFEC. (M)
Part: PRESSURE PANEL — CRACKED (FUSELAGE)
FOUND CRACK NOTED AT LEFT UPPER CORNER NLG PRESSURE PANEL. CONFIRMED CRACK BY UTILIZING HFEC METHOD. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 2 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 1 AND NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: DOOR — CRACKED (CARGO BAY)
IDENTIFIED CRACKS AT 3.25 INCH PROPAGATING FROM ONE RIVET TO ADJACENT RIVET ON MAIN CARGO DOOR AT BS 430, 2 INCHES BELOW STRINGER 14L CONFIRMED BY UTILIZING HFEC AND VISUAL METHOD. TRIM OUT THE CRACK DAMAGE, FABRICATED FILLERS FROM 2024-T3, FABRICATED EXTERNAL DOUBLER ONE GAUGE THICKER THAN DOOR LOWER OUTER SKIN, AND INSTALLED FASTENERS PER SRM 51-30-2. IN ACCORDANCE WITH ECO 3211, RECEIVED 8110-3 APPROVAL. (M)
2000
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 4 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SELECTOR VALVE — LEAKING (MLG)
FLT 248 - LIH-HNL - CLIMBING THROUGH 10,000 FT, BOTH MAIN GEAR RED AND GREEN LIGHTS ILLUMINATED WITH THE LANDING GEAR HANDLE IN THE OFF POSITION. AFTER REVIEWING THE ISSUE, THE LANDING GEAR HANDLE WAS PLACED TO DOWN AND ALL THREE GEARS INDICATED DOWN AND LOCKED. THE GEAR WAS THEN RAISED AND ALL THREE GEARS INDICATED UP AND LOCKED. THE LANDING GEAR HANDLE WAS LEFT IN THE UP POSITION UNTIL THE GEAR WAS LOWERED FOR LANDING. T/S MLG SYSTEM PER MM 32-31-0. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE. LEAK AND OPS CHECK OK. RETRACTION CHECK OK PER MM 32-31-51/401 AND 32-32-0/501. SYTEM CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — INOPERATIVE (PAX CABIN)
REPLACED NR 2 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED NR 3 FLOOR EMERGENCY LIGHT BATTERY PACK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — INOPERATIVE (CABIN)
REPLACED NR 6 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: DOOR FRAME — DAMAGED (FUSELAGE)
REPAIRED MAIN CARGO DOOR CUTOUT FRAME LEFT SIDE STATION 500, WBL 264.5 BY BLENDOUT OF ELONGATED FRAME HOLE IAW ECO 3145. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CORRODED (RT WING AILERON)
REPAIRED RIGHT AILERON CONTROL QUADRANT AT WING STATION 519 BY BLENDOUT AND TREATING CORROSION IAW ECO 3147. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — INOPERATIVE (CABIN)
REPLACED FORWARD EXIT IDENTIFIER POWER PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED NR 2 FLOOR PROXIMITY LIGHT ASSY DO TO NO TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
1999
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED FORWARD SERVICE DOOR EXIT IDENTIFIER DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 2 FLOOR PROXIMITY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERABLE (CABIN)
REPLACED NR 5 FLOOR PROXIMITY LIGHT ASSY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 1 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 5 FLOOR PROXIMITY LIGHT ASSY BATTERY PACK DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (PAX DOOR)
REPLACED FORWARD ENTRY DOOR EXIT IDENTIFIER LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED RIGHT OVERWING EXIT IDENTIFIER LIGHT ASSY DUE TO NOT SHUTTING OFF. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED POSITION 1, 2, 3 AND 4 EMERGENCY FLOOR BATTERY PACKS DUE TO LOW VOLTAGE. OPS CHECKS OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: POWER PACK — INOPERATIVE (CABIN)
REPLACED RIGHT OVERWING EMERGENCY POWER PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY — DISCHARGED (CABIN)
REPLACED NR 1 SEAT EMERGENCY ASSEMBLY BATTERY DUE TO NO TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY — DISCHARGED (CABIN)
REPLACED BATTERY PACK FOR FLOOR PROX AISLE LIGHT NR 2 AND NR 3 DUE AS WELL LIGHT INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY — DISCHARGED (CABIN)
REPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)
1998
Part: BATTERY — DISCHARGED (CABIN)
REPLACED EMERGENCY FLOOR LIGHT BATTERY PACK FOR POSITIONS NR 2 AND NR 5 DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY — DISCHARGED (CABIN)
REPLACED FORWARD PASSENGER DOOR EMERGENCY EXIT IDENTIFIER DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY — DISCHARGED (CABIN)
NR 1 AND NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK INOP. REMOVED AND REPLACED NR 1 AND NR 6 EMERGENCY FLOOR BATTERY PACK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY — DISCHARGED (CABIN)
REPLACED THE FLOOR PROXIMITY EMERGENCY LIGHT BATTERIES FOR POSITIONS, NR 1, NR 2 NR 3 AND NR 5 FOR LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (PAX DOOR)
REPLACED FORWARD ENTRY DOOR EXIT IDENTIFIER LIGHT ASSY DUE INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (PAX DOOR)
REPLACED FORWARD ENTRY DOOR EXIT IDENTIFIER BATTERY PACK DUE INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 4 FLOOR PROX LIGHT BATTERY PACK DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED THE BATTERY PACK IN THE NR 2 AND NR 5 POSITION EMERGENCY PROXIMITY FLOOR LIGHTS. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (SERVICE DOOR)
REPLACED LT O/W, FORWARD SVC DOOR EXIT IDENTIFIER DUE TO INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (SERVICE DOOR)
REPLACED LT O/W, FORWARD SVC DOOR LIGHT IDENTIFIER DUE TO INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (PAX DOOR)
REPLACED FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER DUE TO INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BUSHING — WORN (TE FLAP)
ON LANDING, AIRCRAFT ROLLS TO THE LEFT 30 DEGREES WITH GEAR DOWN AND FLAPS 15. REPLACED NR 1 AND NR 2 FLAP JACKSCREW GIMBAL BUSHINGS. GROUND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED THE BATTERY PACK IN THE NR 4 POSITION EMERGENCY PROXIMITY FLOOR LIGHT. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — INOPERATIVE (CABIN)
REPLACED LEFT FORWARD ENTRY DOOR EXIT IDENTIFIER. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 1 POSITION EMERGENCY PATH LIGHT ASSY BATTERY PACK DUE TO BEING INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 3 POSITION EMERGENCY PATH LIGHT ASSY BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 5 POSITION EMERGENCY PATH LIGHT ASSY BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 6 POSITION EMERGENCY PATH LIGHT ASSY BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: WEB — CRACKED (BS 664)
FOUND 2 INCH CRACK AT BS 664 AND 39.5 INCHES TO THE RIGHT OF BL. VERIFIED BY HFEC. REPAIRED CRACK PER ECO 2917. AIRCRAFT RETURNED TO SERVICE. (M)
Part: WEB — CRACKED (BS 664)
FOUND 2 INCH CRACK AT BS 664 AND 52 INCHES TO THE RIGHT OF BL. VERIFIED BY HFEC. REPAIRED CRACK PER ECO 2917. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 2 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO BATTERY LAMPS NOT ILLUMINATING. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 4 EMERGENCY FLOOR LIGHT BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 3 POSITION EMERGENCY EXIT LIGHT ASSY BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSY BATTERY PACK DUE TO INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSY DUE TO INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 5 POSITION EMERGENCY EXIT LIGHT ASSY BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED FORWARD SERVICE DOOR EXIT IDENTIFICATION LIGHT ASSY DUE TO INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED BATTERY PACK ON NR 5 FLOOR EMERGENCY LIGHT DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED BATTERY PACK ON NR 1 FLOOR EMERGENCY LIGHT DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED BATTERY PACK ON NR 1 FLOOR EMERGENCY LIGHT DUE TO BEING INOPERATIVE. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X)
Part: SKIN — CRACKED (BS 767)
SKIN CRACK, APPROXIMATELY .75 INCH LONG, NOTED AT BS 767 AND STRINGER 18L. CONFIRMED WITH HFEC. REPAIRED SKIN IAW BOEING SRM 53-30-3 FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 3 EMERGENCY FLOOR LIGHT INOP, REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHT INOP, REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 3 EMERGENCY FLOOR LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
ON SERVICE CHECK, FOUND FORWARD DOOR EMERGENCY EXIT LIGHT INOPERABLE. REPLACED IDENTIFIER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 33,777:16 HOURS. TAC: 40,326. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND RIGHT OVERWING EMERGENCY SLIDE LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 33,534:51 HOURS. TAC: 39,782.
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 33,513:04 HOURS. TAC: 39,735. (X)
Part: SIGN — INOPERATIVE (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED FLOOR LIGHT ASSY, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 33,513:14 HOURS. TAC: 39,735. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 33,513:04 HOURS. TAC: 39,735. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 1 EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 33,513:04 HOURS. TAC: 39,735. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 3 EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 33,513:04 HOURS. TAC: 39,735. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 33,483:34 HOURS. TAC: 39,664. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 33,483:34 HOURS. TAC: 39,664. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 5 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 33,483:34 HOURS. TAC: 39,664. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 1 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 33,483:34 HOURS. TAC: 39,664. (X)
1997
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND AFT ENTRY EMERGENCY LIGHT BLINKING. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 33,269:05 HOURS. TAC: 39,185. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND NR 4 EMERGENCY FLOOR LIGHT BATTERY WEAK. REPLACE BATTERY PACK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON DAILY CHECK, FOUND NR 6 POSITION FLOOR EMERGENCY LIGHT INOP. REPLACED LIGHT BATTERY PACK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY — DISCHARGED (CABIN)
DURING OVERNIGHT CHECK, REPLACED BATTERY FOR ROW 1 EMERGENCY FLOOR PROX LIGHT ASSY DUE TO INOP. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: STIFFENER — CRACKED (CARGO DOOR)
FLT 77 - ITO-HNL - LOUD NOISE AND VIBRATION FROM MAIN CARGO DOOR IN FLIGHT. REPLACED TWO CRACKED ANGLE BRACKETS (STIFFENERS) PER SRM 51-10-1. LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
DURING OVERNIGHT CHECK, REPLACED AFT ENTRY AND SERVICE EMERGENCY BATTERY POWER SUPPLY DUE TO INOPERABLE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 32,451:34 HOURS. TAC: 37,325. (X)
Part: BATTERY — DISCHARGED (CABIN)
DURING OVERNIGHT CHECK, REPLACED BATTERY FOR AFT EMERGENCY SLIDE LIGHT DUE TO INOPERABLE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 32,390;53 HOURS. TAC: 37,186. (X)