N821AL
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.
105 reports on file, 1997-02-08 – 2007-07-31.
Part: DUCT — FAILED (APU) · airframe 45,677 hrs · 67,561 cycles
NON-ETOPS FLIGHT 40 HNL - ITO, AFTER LANDING IN ITO THE CREW STARTED THE APU AND HAD A WING TO BODY OVERHEAT INDICATION. THE APU WAS SHUT DOWN. MAINTENANCE FOUND THE APU BLEED AIR DUCT HAD RUPTURED CAUSING THE OVERHEAT AND ALSO CAUSING THE APU FIRE EXTINGUISHER BOTTLE TO THERMAL DISCHARGE. THE APU WAS PLACED ON MEL AND THE AIRCRAFT RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THREE SECTIONS OF BLEED DUCT. MAINTENANCE ALSO REPLACED THE APU FIRE EXTINGUISHER BOTTLE PER AMM 26-22-11. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: ACTUATOR — MALFUNCTIONED (NLG) · airframe 45,444 hrs · 67,038 cycles
FLIGHT 90 HNL- KOA. ON APPROACH TO KOA WHEN THE CREW LOWED THE GEAR HANDLE, THE TWO MAIN GEAR SHOWED DOWN AND LOCKED BUT THE NOSE GEAR SHOWED UP AND CREW DIDNâT HEAR THE NLG EXTEND. AFTER APPROXIMATELY 20 SECONDS, THE NLG EXTENDED AND SHOWED DOWN AND LOCKED. CREW FLEW A LOW PASS TO HAVE ATC VISUALLY CHECK THAT ALL GEAR WERE DOWN. ATC REPORTED ALL GEAR DOWN AND CREW VERIFIED THE NLG WAS DOWN WHEN CHECKED THROUGH THE FLIGHT DECK VIEWING PORT. CREW LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS THEN FERRIED TO HNL WITH THE GEAR DOWN AND LOCK PINS INSTALLED. AIRCRAFT COMPLETED FERRY FLIGHT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NLG MODULAR PACKAGE AND NLG TRANSFER CYLINDER. AIRCRAFT FAIL
Part: SKIN PANEL — CRACKED (BS 947 S21-22L) · airframe 45,243 hrs · 66,578 cycles
WHILE PERFORMING INSPECTIONS TO COMPLY WITH AD 2005-13-30 A CRACK APPROX 3" LONG, LOCATED AT BS947 +15 BETWEEN STR 21L AND STR 22L WAS DISCOVERED. [SUP 05-22-07] CRACK APPROX 3 LONG, LOCATED AT BS 947 + 15 BETWEEN STR 21L AND STR 22L WAS REPAIRED IAW SRM 53-30-3 PROCEDURE VII. CUTOUT INSPECTED IAW NDT MANUAL PT. 6 51-00-00 FIG 23. FINAL REPAIR SIZE APPROX. 26 X 23.
Part: SKIN PANEL — CRACKED (BS 887 S23-24R) · airframe 45,243 hrs · 66,578 cycles
WHILE PERFORMING INSPECTIONS TO COMPLY WITH AD 2005-13 A CRACK APPROX 2" LONG WAS DISCOVERED AT BS887 +3 BETWEEN STR 23R AND STR 24R. [SUP 05-22-07] CRACK APPROX 2 LONG WAS REPAIRED AT BS 887 + 3 BETWEEN STR 23R AND STR 24R IAW SRM 53-30-3 PROCEDURE VII. CUTOUT INSPECTED IAW NDT MANUAL PT. 6 51-00-00 FIG 23. FINAL REPAIR SIZE APPROX. 12 X 10.
Part: FRAME — CRACKED (BS188) · airframe 45,243 hrs · 66,578 cycles
DURING INSPECTION OF THE BS 178 WEB, CRACKS WERE DISCOVERED ON THE BS 188 FRAME AT WL 207 ON BOTH LEFT AND RIGHT SIDES. LEFT SIDE CRACK IS APPROX 1.75 INCHES LONG. RIGHT SIDE CRACK IS APPROX. 2 INCHES LONG. [SUP 05-10-07] INTERIM REPAIR PERFORMED PER ECO 3650 PART I. CRACKS WERE STOP DRILLED AT BS 188 WL 207 LEFT AND RIGHT SIDES. RE-INSPECTION PER ECO 3650 PART II IS REQUIRED EVERY TWO WEEKS FOR 150 DAYS OR WHEN AIRCRAFT IS FERRIED TO FINAL DESTINATION. PERMANENT REPAIR REQUIRED PER ECO 3650 PART III IF AIRCRAFT IS TO BE USED AFTER FINAL FERRY FLIGHT OR 09/08/2007. 8110-3 RECEIVED ON 05/03/2007
Earlier reports · 1997–2006 · 100 reports
2006
Part: WIRE — BROKEN (LT FUEL SHUT OFF) · airframe 43,118 hrs · 61,748 cycles
NR 1 ENGINE SHUT DOWN WITHOUT CREW ACTION AFTER NORMAL START, DURING PUSHBACK. FUEL VALVE CLOSED LIGHT ILLUMINATED. REMOVED AND REPLACED THE LT FUEL SHUT OFF VALVE IAW MM 28-22-11, LEAK CHECK OKAY. THIS DID NOT FIX THE PROBLEM. FURTHER INVESTIGATION REVEALED TWO WIRES AT THE CONNECTOR FOR THE LEFT FUEL SHUT OFF VALVE BROKEN. REPAIRED BROKEN WIRES AT CONNECTOR, OPS CHECK OKAY. AIRCRAFT RETURNED TO SERVICE.
Part: SKIN PANEL — GOUGED (BS190 S19R) · airframe 42,950 hrs · 61,384 cycles
RIGHT HAND SIDE OF FUSELAGE GOUGED (3 LENGTH) AT BS 190 BELOW S19R. MAINTENANCE REPAIRED WITH FABRICATED .050 (2024-T3) EXTERNAL SKIN DOUBLER 9.5 X 6.75 INCHES PER ECO 5330.
2005
Part: SKIN — CORRODED (BS 998) · airframe 42,579 hrs · 60,613 cycles
SECTION 46 FUSELAGE SKIN WITH CORROSION AT BS 998.40, LBL 6.75.
Part: CLIP — CRACKED (BS 727) · airframe 42,579 hrs · 60,613 cycles
BULKHEAD BS 727, WL 202.6, RBL 10.0", CLIP UPPER CRACKED.
Part: SPAR — CORRODED (RT WING) · airframe 42,579 hrs · 60,613 cycles
RIGHT WING FRONT SPAR, LOWER CORD FWD FLANGE CORRODED AT SLAT STA 243.0 AND SLAT STA 254.0.
Part: CONNECTOR — DAMAGED (BLEED AIR)
NON-ETOPS ON TAXI AFTER LANDING THE CREW GOT AN APU FIRE WARNING LIGHT, COMPLETED APU FIRE CHECK LIST, SHUTDOWN APU AND DISCHARGED APU FIRE BOTTLE. FIRE WARNING LIGHT EXTINGUISHED. AIRCRAFT TAXIED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED APU FIRE BOTTLE AND FOUND NO EVIDENCE OF FIRE. FOUND A LEAK IN THE BLEED AIR DUCT CONNECTOR. THE CONNECTOR WAS REPLACED AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE.
Part: TIRE — FAILED (MLG)
NON-ETOPS FLT 68, HNL-ITO: ON TAKEOFF ROLL, FELT LIKE BOTH RIGHT MAIN LANDING GEAR TIRES BLEW. FOLLOWED BY AN EXTREME STRUCTURAL POUNDING COMING FROM THE RIGHT SIDE UNTIL SLOWED TO ABOUT 60KTS. DECLARED AN EMERGENCY. NO SMOKE OR FIRE. MAINTENANCE REMOVED AND REPLACED NR 3 AND NR 4 BRAKES AND MAIN LANDING GEAR TIRES. ALSO REMOVED AND REPLACED THE NR 1 & NR 2 BRAKES AND TIRES AS A PRECAUTION. COLLATERAL DAMAGE TO RIGHT FLAP, MAIN LANDING GEAR DOOR AND WING-TO-BODY FAIRING. AIRCRAFT NOT IN SERVICE AT THIS TIME. NUMEROUS PART REPLACEMENT AND CHECKS WERE ACCOMPLISHED. AIRCRAFT RETURNED TO SERVICE ON 6/7/05.
2004
Part: LINE — LEAKING (THRUST REVERSER)
FLT 46, HNL-ITO: HYDRAULIC FLUID QUANTITY DECREASING DURING GEAR RETRACTION. RETURNED TO HNL. UNEVENTFUL LANDING. WHILE ON GROUND, HYDRAULIC FLUID QUANTITY CONTINUED TO DECREASE SLOWLY. MAINTENANCE FOUND LEAKS AT THE NR 2 THRUST REVERSER LINE AND NR 4 SPOILER OUTBOARD ACTUATOR LINE AND B-NUT. REMOVED AND REPLACE THE NR 2 TR HYDRAULIC LINE. OPS AND LEAK CHECK OK. REMOVED AND REPLACED THE HYDRAULIC LINE AND B-NUT ON THE NR 4 SPOILER OUTBOARD ACTUATOR. OPS AND LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE.
Part: TRANSMITTER — FAILED (NR 2 ENGINE) · airframe 40,430 hrs · 55,774 cycles
ON TAKEOFF ROLL, THE NR 2 ENGINE OIL QUANTITY INDICATOR DROPPED TO ZERO. REJECTED TAKEOFF AND RETURNED TO THE GATE. DEFERRED THE NR 2 ENGINE OIL QUANTITY INDICATOR IAW MEL 79-1, CONTROL NR 0778B-10. SERVICED THE NR 2 ENGINE TO FULL AND INSTALLED PLACARDS ON AIRCRAFT AND LOG-BOOK. AIRCRAFT RETURNED TO SERVICE. REMOVED AND REPLACED THE NR 2 ENGINE OIL QUANTITY TRANSMITTER IAW AMM 79-31-11. OPS AND LEAK CHECK OK, PLACARDS REMOVED. AIRCRAFT RETURNED TO SERVICE.
Part: BYPASS SWITCH — FAULTY (NR 2 ENGINE)
NR 2 ENGINE OIL BYPASS LIGHT CAME ON. PERFORMED QRH PROCEDURES, ENGINE SHUTDOWN AND LANDED AT HNL. ACCOMPLISHED BREATHER PRESSURE CHECK PER FORM M-209. CHECK GOOD. DRAINED AND SERVICED OIL TANK AND GEARBOX. LEAK AND OPS CHECK GOOD. REPLACED THE NR 2 ENGINE OIL BYPASS SWITCH. RAN ENGINE, OPS CHECK OK. INSPECTED NR 2 ENGINE OIL FILTER AND REPLACED. IDLE RUN PERFORMED AND FILTER CHECKED CLEAN. MAINTENANCE DONE PER PW MM 72-00-00, PAGE 136. AIRCRAFT RETURNED TO SERVICE. (M)
2003
Part: WINDOW FRAME — CRACKED (FUSELAGE)
TRIMMED AREA AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED THREE FILLERS AND A REPAIR DOUBLER FROM 2024-T3 AS SHOWN IN FIGURE 1, MAINTAINING 2D EDGE MARGIN. MAINTAINED A MINIMUM .5 INCH OUTSIDE CORNER RADIUS AND MINIMUM 2.0 INSIDE CORNER RADIUS. FINISH ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OF BMS 10-79 TYPE III, PRIMER. INSTALLED FILLERS AND DOUBLERS WITH FASTENERS INDICATED IN FIGURES 1, 2, AND TABLE 1. APPLIED FILLET SEAL OF BMS 5-95 SEALANT AROUND EDGES OF REPAIR. REPAIR COMPLETED IAW ECO 3250, DEVIATION AL. AIRCRAFT RETURNED TO SERVICE. WINDOW FRAME P/N 65-458181, 65-46525, 65-46526 AND 65-46530, BS 360R UPPER, BS 380R, BS 400R, AND BS 460R. (M)
Part: WINDOW FRAME — CRACKED (FUSELAGE)
TRIMMED AREA AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED THREE FILLERS AND A REPAIR DOUBLER FROM 2024-T3 AS SHOWN IN FIGURE 1, MAINTAINING 2D EDGE MARGIN. MAINTAINED A MINIMUM .5 INCH OUTSIDE CORNER RADIUS AND MINIMUM 2 INCH INSIDE CORNER RADIUS. FINISH ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OF BMS 10-79 TYPE II, PRIMER. INSTALLED FILLERS AND DOUBLERS WITH FASTENERS INDICATED IN FIGURES 1, 2 AND TABLE 1. APPLIED FILLET SEAL OF BMS 5-95 SEALANT AROUND EDGES OF REPAIR. REPAIR COMPLETED IAW ECO 3250, DEVIATION A1. AIRCRAFT RETURNED TO SERVICE. WINDOW FRAME P/N 65-458181 BS 360L UPPER AND LOWER AND P/N 65-46525 BS 380L UPPER AND LOWER.(M)
Part: WINDOW FRAME — CRACKED (FUSELAGE)
TRIMMED AREA AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED THREE FILLERS AND A REPAIR DOUBLER FROM 2024-T3 AS SHOWN IN FIGURE 1, MAINTAINING 2D EDGE MARGIN. MAINTAINED A MINIMUM .5 INCH OUTSIDE CORNER RADIUS AND MINIMUM 2.0 INCH INSIDE CORNER RADIUS. FINISH ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OF MBS 10-79 TYPE III, PRIMER. INSTALLED FILLERS AND DOUBLERS WITH FASTENERS INDICATED IN FIGURES 1, 2 AND TABLE 1. APPLIED FILLET SEAL OF BMS 5-95 SEALANT AROUND EDGES OF REPAIR. REPAIR COMPLETED IAW ECO 3250, DEVIATION AI. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CRACKED (FUSELAGE)
REPAIRED FUSELAGE SKIN CRACK AT BS 767, STRINGER 19 RIGHT. CUTOUT AND REMOVED DAMAGED PORTION OF SKIN. VERIFIED CRACK REMOVED USING HFEC METHOD. FABRICATED AND INSTALLED A REPAIR FILLER AND PLATE FROM 2024-T3 MATERIAL IAW SRM 53-30-3, FIGURE 3. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
REPLACED FORWARD ENTRY DOOR POWER PACK DUE TO LOW VOLTAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: ENGINE — FAILED (NR 1)
AT CRUISE ALTITUDE, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED AND WOULD NOT GO OUT AT REDUCED THRUST SETTING. THE CREW SHUTDOWN THE NR 1 ENGINE AND LANDED AT HNL WITH NO FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. REMOVED AND REPLACED THE NR 1 ENGINE. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY PACK — DISCHARGED (PAX CABIN)
REPLACED LEFT AFT EMERGENCY EXIT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CRACKED (FUSELAGE)
CUT OUT DAMAGED SKIN AREA AT BS 520 MAINTAINING A .50 INCH MINIMUM RADIUS AND 2D EDGE MARGIN. VERIFIED EDGE OF TRIM USING HFEC METHOD. ENLARGED TRIMMED AREA BY .04 INCH AS AN INSURANCE CUT. FABRICATED TWO .063 INCH STRUCTURAL FILLERS AND A .071 INCH DOUBLER FROM 2024-T3 CLAD MATERIAL. FINISHED ALL BARE ALUMINUM WITH ALODINE AND TWO COATS BMS 10-11, TYPE 1 PRIMER. INSTALLED REPAIR PARTS, HI-LOCKS AND RIVETS WET WITH BMS 5-95 SEALANT BETWEEN THE FAYING SURFACES. APPLIED A FILLET SEAL OF BMS 5-95 AROUND THE EDGES. REPAIR COMPLETED IAW ECO 3324, FIURE 1. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CORRODED (FUSLEAGE)
CUTOUT DAMAGED SKIN ARE AT BS 908 MAINTAINING A .50 INCH MINIMUM RADIUS AND 2D EDGE MARGIN. VERIFIED CRACK REMOVED USING HFEC METHOD. ENLARGED TRIMMED AREA BY .04 INCH AS AN INSURANCE CUT. FABRICATED TWO STRUCTURAL FILLERS, A REPAIR FILLER, DOUBLER, AND TRIPLER FROM 2024-T3 CLAD MATERIAL. FINISHED ALL BARE ALUMINUM WITH ALODINE AND TWO COATS BMS 10-11, TYPE 1 PRIMER. INSTALLED REPAIR PARTS WET WITH BMS 5-95 SEALANT BETWEEN THE FRAYING SURFACES. APPLIED A FILLET SEAL OF BMS 5-95 AROUND THE EDGES. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 48, SHEET 55. AIRCRAFT RETURNED TO SERVICE. (M)
2002
Part: SKIN — CORRODED (FUSLEAGE)
CUTOUT AND REMOVED DAMAGED PORTION OF SKIN. HFEC INSPECTED THE EDGE OF TRIM. ENLARGED TRIMMED BY .04 INCH INSURANCE CUT. FABRICATED AND INSTALLED A .071 INCH REPAIR FILLER AND .080 INCH DOUBLER FROM CLAD SHEET 2024-T3 MATERIAL IAW SRM 53-30-3. FINISHED ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OF BMS 10-111 TYPE 1 PRIMER. REPAIR COMPLETED IAW ECO 3325. AIRCRAFT RETURNED TO SERVICE. (M)
Part: WINDOW FRAME — CRACKED (BS)
TRIMMED AREA AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED 3 EACH FILLERS AND A REPAIR DOUBLER FROM 2024-T3 AS SHOWN IN FIGURE 1, MAINTAINING 2D EDGE MARGIN. MAINTAINED A MINIMUM .5 INCH OUTSIDE CORNER RADIUS AND MINIMUM 2.0 INCH INSIDE CORNER RADIUS. FINISH ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OF MBS 10-79 TYPE III, PRIMER. INSTALLED FILLERS AND DOUBLERS WITH FASTENERS INDICATED IN FIGURES 1, 2 AND TABLE 1. APPLIED FILLET SEAL OF BMS 5-95 SEALANT AROUND EDGES OF REPAIR. REPAIR COMPLETED IAW ECO 3250, DEVIATION AI. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 2 FLOOR BATTERY PACK DUE TO LOW VOLTAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: STIFFENER — CRACKED (FUSELAGE)
REPAIRED CRACK AT BS 178, WI 184 LBL 5.7 VERTICAL CHORD. CUTOUT AND REMOVED DAMAGED PORTION OF SKIN AREA. VERIFIED CRACK REMOVED USING HFEC METHOD. FABRICATED AND INSTALLED A REPAIR ANGLE IAW SRM. AIRCRAFT RETURNED TO SERVICE.
Part: SKIN — CRACKED (FUSELAGE)
TRIMMED OUT DAMAGE SKIN AT BS 749 STRINGER 18R. HFEC EDGE OF TRIMMED AREA, NO DEFECTS NOTED.
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR FLOOR BATTERY PACK DUE TO LOW VOLTAGE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED FORWARD SERVICE DOOR IDENT LIGHT ASSEMBLY DUE TO INOPERATIVE. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED FORWARD SERVICE DOOR IDENT LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE.
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 5 EMERGENCY FLOOR LIGHT BATTERY PACKS DUE TO INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SKIN — CRACKED (FUSELAGE)
REPAIRED CRACK AT FS 965 (AFT ENTRY DOOR). CUTOUT AND REMOVED CRACK PORTION OF SKIN AROUND LOWER FORWARD AREA. PERFORMED HFEC INSPECTION AROUND CUT OUT AREA NO DEFECTS NOTED. FABRICATED AND INSTALLED A REPAIR FILLER AND PLATE IAW SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)
2001
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 5 AND NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M)
Part: INDICATOR — FALSE INDICATION (COCKPIT)
FLT 246 - HNL-ITO - DIVERT TO OGG, DURING CLIMB AT APPROX 200 FT PILOT NOTICED THE NR 1 ENGINE OIL TEMPERATURE GAUGE IN THE YELLOW BAND, 140 DEGREES. CONTINUED TO FL250 FT, POWER WAS REDUCED AND OIL TEMP INCREASED TO 150 DEGREES THEN WENT OFF SCALE MOMENTARILY. THE FUEL HEAT VALVE WAS CHECK, OIL TEMP BULB CANNON PLUG CLEANED, AND NR 1 AND NR 2 OIL TEMP GAUGED WERE SWAPPED FOR FURTHER TROUBLESHOOTING. THE ENGINE WAS THEN OPERATIONAL CHECKED AT TAKEOFF AND CRUISE POWER FOR SEVERAL MINUTES. ALL ENGINE PARAMETERS REPORTED NORMAL AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED CENTER AISLE EMERGENCY EXIT LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: FRAME — CRACKED (FUSELAGE)
IDENTIFIED CRACK AT FASTENER HOLE CAUSED BY A SHORT EDGE DISTANCE AT BS 1112 FRAME. TRIM OUT THE DAMAGED AREA OF FRAME, FABRICATED AND INSTALLED FILLER OF 056 INCH 7075-T6, FABRICATED AND INSTALLED 063 INCH REPAIR STRAP, CLEANED AND TREATED ALL EXPOSED AREAS IAW ECO 3202, 8110-3 APPROVAL RECEIVED. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SPAR — CRACKED (HORIZONTAL STAB)
IDENTIFIED CRACK AT LEFT HORIZONTAL STABILIZER CENTER SECTION REAR SPAR UPPER CHORD AFT UPPER CLEVIS LUG DURING SCHEDULED INSPECTION PER ECO 1384R6/SB 737-55-1033R1. (M)
2000
Part: BATTERY PACK — INOPERATIVE (CABIN)
REPLACED NR 2 AND NR 4 EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 6 FLOOR EMERGENCY LIGHT BATTERY PACK DUR TO INOP. OPS CK OK.A/C RETURNED TO SERVICE.
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 3 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — INOPERATIVE (PAX CABIN)
REPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED FORWARD SERVICE DOOR EXIT LIGHT ASSY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED FORWARD ENTRY DOOR EXIT LIGHT ASSY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED THE FORWARD AND AFT SERVICE DOOR EXIT LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
1999
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED FORWARD SERVICE DOOR EMERGENCY IDENTIFIER LIGHT ASSY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED FORWARD SERVICE DOOR LIGHT ASSY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED FORWARD AND AFT EXTERIOR EMERGENCY SLIDE LIGHT BATTERY PACKS DUE TO INOPERABLE. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X)
Part: BATTERY — DISCHARGED (CABIN)
REPLACED NR 6 FLOOR PROXIMITY LIGHT FAILED BATTERY TEST. REPLACED NR 6 FLOOR PROXIMITY LIGHT. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED LEFT AND RIGHT CENTER PASSENGER EMERGENCY BATTERY CARTRIDGE DUE TO INOPERABLE. OPS CHECK OKAY. AIRCRAFT RETURNED TO SERVICE. (X)
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED FOWARD ENTRY DOOR EMERGENCY EXIT LIGHT ASSY DUE TO DIM LIGHTS. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED AFT EMERGENCY CONTROL UNIT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED 1 THROUGH 6 FLOOR LIGHT EMERGENCY BATTERY PACKS DUE TO BEING INOPERABLE IN TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED BATTERY PACK FOR NR 5 FLOOR LIGHT ASSY DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (EMER EXIT)
REPLACED BATTERY PACK FOR AFT SERVICE DOOR EXIT IDENTIFIER LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (EMER EXIT)
REPLACED AFT SERVICE DOOR EXIT IDENTIFIER LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 1 POSITION 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 EMERGENCY EXIT LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED FORWARD SERVICE DOOR EMERGENCY IDENTIFIER DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (SERVICE DOORWAY)
REPLACED AFT SERVICE DOOR EXIT IDENTIFIER LIGHT ASSY. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LAMP — FAILED (CABIN)
RELAMPED AFT ENTRY DOOR SLIDE LIGHT DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
1998
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED POSITION NR 5 FLOOR PROX LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED BATTERY PACK FOR FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 5 POSITION BATTERY FOR FLOOR PROX LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOP (EMERGENCY EXIT)
REPLACED ENTRY SERVICE DOOR EMERGENCY EXIT IDENTIFIER DUE TO INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED ENTRY SERVICE DOOR EMERGENCY EXIT IDENTIFIER DUE TO INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED BATTERY PACK AT NR 1 POSITION EMERGENCY FLOOR LIGHT DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (SERVICE DOOR)
REPLACED FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT DUE TO INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED RIGHT EMERGENCY EXIT DOOR IDENTIFIER DO TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED BATTERY PACK AT THE RT EMERGENCY DOOR EXIT IDENTIFIER DO TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 5 POSITION FLOOR PROXIMITY EMERGENCY LIGHT BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 2 POSITION FLOOR PROXIMITY EMERGENCY LIGHT BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED NR 6 POSITION FLOOR PROXIMITY EMERGENCY LIGHT BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED BATTERY PACK AT NR 5 POSITION EMERGENCY FLOOR LIGHT DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (SERVICE DOOR)
REPLACED AFT SERVICE DOOR EXIT IDENTIFICATION LIGHT ASSY DUE TO ALL IS WELL LIGHT BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (SERVICE DOOR)
REPLACED FORWARD SERVICE DOOR EXIT IDENTIFICATION LIGHT ASSY DUE TO ALL IS WELL LIGHT BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
REPLACED FLOOR PROXIMITY LIGHT BATTERY PACK AT NR 5 POSITION DUE TO UNIT BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED FORWARD SERVICE DOOR EMERGENCY EXIT IDENTIFICATION LIGHT ASSY DUE TO BEING INOPERATIVE. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
REPLACED FLOOR PROXIMITY LIGHT ASSY AT NR 2 POSITION DUE TO UNIT BEING INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND NR 1 POSITION EMERGENCY FLOOR LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
ON SERVICE CHECK, FOUND AFT SERVICE DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 5 EMERGENCY FLOOR LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (PASSENGER CABIN)
ON SERVICE CHECK, FOUND POSITION NR 6 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 28,807:02 HOURS. TAC: 29,525. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK FOUND POSITION NR 2 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 28,807:02 HOURS. TAC: 29,525. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 28,807:02 HOURS. TAC: 29,525. (X)
Part: SIGN — INOPERATIVE (CABIN)
ON SERVICE CHECK, FOUND FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REPLACED IDENTIFIER ASSY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
1997
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND NR 5 POSITION EMERGENCY FLOOR LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SIGN — MALFUNCTIONED (CABIN)
ON SERVICE CHECK, FOUND THAT THE FORWARD SERVICE DOOR EMERGENCY LIGHT IDENTIFIER REMAINS ON WITH POWER TURNED OFF. REPLACED EMERGENCY EXIT LIGHT IDENTIFIER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND NR 4 POSITION 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 1 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 28,401:47 HOURS. TAC: 28,611. (X)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 28,401:47 HOURS. TAC: 28,611. (X)
Part: SIGN — INOPERATIVE (CABIN)
ON SERVICE CHECK, FOUND FORWARD SERVICE DOOR IDENTIFIER INOPERATIVE. REPLACED IDENTIFIER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 28,401:47 HOURS. TAC: 28,611. (X)
Part: SIGN — INOPERATIVE (CABIN)
ON SERVICE CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT IDENTIFIER INOP. REPLACED IDENTIFIER. EXIT LIGHT OPS CEHCK GOOD. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND NR 4 POSITION EMERGENCY FLOOR LAMP INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON SERVICE CHECK, FOUND NR 3 POSITION EMERGENCY FLOOR LAMP INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. (M)
Part: SIGN — INOPERATIVE (CABIN)
ON SERVICE CHECK, FOUND FORWARD SERVICE DOOR EMERGENCY EXIT IDENTIFIER LIGHT INOP. REPLACED IDENTIFIER. OPS CHECK GOOD. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ON DAILY CHECK, FOUND POSITION NR 6 FLOOR EMERGENCY LIGHT INOP. REPLACED LIGHT BATTERY PACK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)
Part: FLOOR BEAM — CORROSION (BS 328)
DURING HEAVY MAINTENANCE VISIT, DISCOVERED CORROSION ON BS 328 FLOOR BEAM UPPER CHORD AT LBL 11.0. REPAIRED PER ECO 2850 CORROSION BLEND-OUT. AIRCRAFT RETURNED TO SERVICE. TAT: 27,890.42 HOURS. TAC: 27,480. (X)
Part: BATTERY — DISCHARGED (CABIN)
DURING OVERNIGHT CHECK, REPLACED ROWS 1 AND 8 EMERGENCY FLOOR LIGHT BATTERIES DUE TO INOPERABLE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 27,527:38 HOURS. TAC: 26,659. (X)
Part: BATTERY — DISCHARGED (CABIN)
DURING OVERNIGHT CHECK, REPLACED ROW 22 EMERGENCY FLOOR LIGHT BATTERY DUE TO INOP. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 24,410:10 HOURS. TAC: 26,387. (X)
Part: BATTERY — DISCHARGED (CABIN)
DURING OVERNIGHT CHECK, REPLACED ROW 8 BATTERY FOR EMERGENCY FLOOR PROXIMITY LIGHT ASSY DUE TO INOPERABLE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 27,350:37 HOURS. TAC: 26,242. (X)
Part: BATTERY — DISCHARGED (CABIN)
DURING SERVICE CHECK, REPLACED ROW 17 BATTERY PACK FOR EMERGENCY FLOOR LIGHTING DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT REUTRNED TO SERVICE. TAT: 27,306:28 HOURS. TAC: 26,138. (X)
Part: ENGINE — FAILED (NR 2)
LIH/HNL - FLT 30 - PILOT REPORT. NR 2 ENGINE BEGAN VIBRATING AND FAILED AFTER TAKEOFF. DECLARED EMERGENCY, ALL CHECK LISTS COMPLETED. UNEVENTFUL LANDING AT LIHUE. REPLACED NR 2 ENGINE ASSY IAW FORMS M-211, M-212, M-213, M-214, AND M-215. AIRCRAFT RETURNED TO SERVICE. (X)