N494HA
Registered owner: HAWAIIAN AIRLINES INC, HI (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Hawaiian Airlines | Operator | 2023-11-30 – 2023-11-30 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
FA'S REPORT EMERGENCY EXIT LIGHTS. INTERMITTENATLY FLASHING WHEN ACFT IS DESCENDING. GROUNDED - YES. REPLACED EMERGENCY LIGHT SWITCH S1-177 IAW SSM 33-51-0-101. OPS CHECK GOOD. OK TO CONTINUE SERVICE.
ATB- FA REPORTS THREE LOUD SOUNDS COMING FROM MAIN CABIN DOOR DURING CLIMB OUT. CABIN PRESSURE INDICATING NORMAL. GROUNDED - YES. CLEANED MAIN DOOR SEAL. CONDITION OF SEAL GOOD. PERFORMED CABIN PRESSURIZATION TO DP OF 7 PSI TWICE. IAW WITH AMM 213000-780801. NO NOISE DETECTED. OK FOR SERVICE.
OVERWING EMERGENCY LIGHT INOPERATIVE. GROUNDED - YES. REMOVED AND REPLACED OVERWING EMERGENCY BATTERY IAW AMM 33-51-06. OPS CHECK GOOD. OK FOR SERVICE.
FORWARD SERVICE DOOR ESCAPE SLIDE UNSERVICEABLE, REQ'S REPLACEMENT. GROUNDED - YES. FWD SERVICE DOOR ESCAPE SLIDE REMOVED AND REPLACED. SECURITY & OPS CK GOOD IAW AMM 25-61-01. AC OKAY FOR SERVICE.
"ANTISKID L FAIL" ON LANDING ROLL OUT LEFT MAIN LANDING GEAR OUTER TIRE POPPED. REMOVED AND REPLACED #1&2 MLG (LH) TIRES PER AMM 32-41-01. AWAITING ANTISKID RESOLUTION.
LEFT LANDING GEAR DID NOT RETRACT WITH GEAR HANDLE UP ON TAKEOFF UNTIL 1300FT WITH A LOUD THUD. GEAR UNSAFE LIGHT ON. TROUBLE SHOT- FOUND L/H MLG ACTUATOR BYPASSING DURING GEAR SWING. REMOVED LH MLG RETRACT CYLINDER PER AMM 32-33-01-000-801. INSTALLED LH MLG RETRACT ACTUATOR CYLINDER PER AMM 32-33-01OPS AND LEAK CHECK GOOD. GEAR SWING CHECK GOOD.
LH SIDE CABIN WINDOW: WINDOW #16 HAS CORROSION. FWD SIDE OF WINDOW (MARKED)M66 SUBMITTED. REPAIRED PER E105-494100-PERM.
FIRE DETECT LEFT FAIL MESSAGE RECEIVED FOUR SEPERATE TIMES DURING TAXI OUT. REMOVED AND REPLACED WIRE # 7324012016W18 AND 7324012017W18 DUE TO WIRES CHAFFING AT T-10321-1 AND T-1032-2 PER AMM 71-50-00. PERFORMED ENG 1 FIRE DETECTION OPS TEST. OPS TEST GOOD. PERFORMED ENGINE RUN NO FIRE DETECT LEFT FAIL MESSAGE.
MILDUE SMELL IN COCKPIT. PERFORMED PACK BURNOUT PER AMM 21-54-00 AND REMOVED AND REPLACED COALESCER BAGS PER AMM 21-54-08, OPS, LEAK, SECURITY CHECKS GOOD. NO DEFECTS OR SMELL NOTED, OK FOR SERVICE.
ATB - COMPRESSOR STALL ON TAKE OFF. PER FLIGHT CREW, NEED SHUTDOWN NO 2 ENGINE AND RETURNING TO HNL. WILL REQUIRE AN ENGINE CHANGE [TURBINE BLADE DAMAGED]. REF LP 916301/1 FOR ENGINE REPLACEMENT REF T/C E1128-717-72-003-INSTALL. OK FOR SVC. OPS/ LEAK CHK GOOD.
ATB - LEFT ENGINE COMPRESSOR STALL // OPENED #1 ENG COWLING REMOVED BREATHER OUTLET TO FOM REMOVED PANEL 412DL TO FOM INSPECTED MASTER MAGNETIC CHIP DETECTOR NO PARTICLES FOUND MECH 16989 3/18/2022 FOUND DAMAGED COMPRESSOR ROTOR BLADES & STATOR VANES. REMOVED AND REPLACED #1 ENG PER W/O 219374 S/N OFF 13235 S/N ON 13438
EMER EQ - EMERGENCY EXITS LIGHTS @ROW 18 INOP // REMOVED AND REPLACED BATTTERY PACK (B5-230) PER AMM 33-51-03. OPS CHECK GOOD. OK FOR SERVICE.
C CHECK MAJOR REPAIR - CRACK IN LH FUSELAGE FRAME GUSSET AT STA 1022, L-7L // REPAIRED PER SR#3-5198890164
C CHECK MAJOR REPAIR - DURING ROUTINE MAINTENANCE TASKS, A CRACK IN THE FUSELAGE AT STATION 1022 AT LONGERON L-14L, AND WAS FOUND ON BOTH THE SKIN (PN 5936436-101) AND ON THE FINGER DOUBLER (PN 5936436-39) BELOW. A 3.8 INCH X 1.1 INCH SECTION WAS CUT OUT OF THE SKIN AND A 3.5 INCHES X 0.5" // REPAIRED PER E105-494063-PERM
EMER EQ - AFT DOOR SEAL HISSING/LEAKING // REMOVED AND REPLACED AFT DOOR HINGE PIN UPPER SIDE PER AMM 52-12-03. LEAK CHECK GOOD PER AMM 21-30-00-790-801. OK FOR SERVICE.
ATB - DUAL FMS FAIL DURING CLIMB RESULTING IN AIR TURN BACK. // PERFORMED FIM TASK 34-63 TASK 830, FMS DUAL FAIL - ALL RTS TESTS PASS - OK FOR SVC.
INFLIGHT, RT ENG SYS FAIL. TROUBLESHOT FAULT THROUGH MCDU EEC-2 AND FOUND FAULT TO BE N2 PROBE ELECTRICAL CH-B. REMOVED AND REPLACED N2 SPEED PROBE PER FIM 77-12 TASK802. PERFORMED ENGINE AND LEAK CHECK. NO LEAKS/NO FAULTS. FAULT CODE; 771202
OPEN - RH WING MOVEABLE VANE UPPER SURFACE DENT/CORROSION. VERIFY FILLER MATERIAL IS 7075T6.016. HFEC INSPECTION COMPLETED FOR CRACKS, NO CRACKS VERIFIED DOUBLER MATERIAL IS 7075T6.020. FABRICATED DOUBLER PER SRM 57-53-01-R2-1/ OK TO INSTALL. INSTALLED DOUBLER PER SRM 57-53-01-2R-1. PAINT PENDING. PAINTED PER SRM 51-22-01. REPAIRED PER E105-C10308-TER.
ON ILS W/ AUTO PILOT ON #2 AT 800 FT FLT DIR ROLL BAR DISAPPEARED & AUTO PILOT KICK OFF. RAW DATA OK. // REMOVED AND REPLACED FCC #2 PER BOEING 717 AMM 22-01-03. PERFORMED FCC #2 RTS TEST PER BOEING 717 AMM 22-00-00. CHECK OK.
CORROSION ON LEFT WING LOWER SURFACE AT XRS 261 STR RS. MARKED AS 6. CLEANED AND TREATED PER SRM 51-10-04. PRIMED AND PAINTED PER SRM 51-22-01.
CORROSION ON LEFT WING LOWER SURFACE AT XRS 295 STR RS MARKED AS 9. CLEANED AND TREATED PER SRM 51-10-04. PRIMED AND PAINTED PER SRM 51-22-01.
CORROSION ON LEFT WING LOWER SURFACE AT XRS 293 STR RS. MARKED AS 7. CLEANED AND TREATED PER SRM 51-10-04. PRIMED AND PAINTED PER SRM 51-22-01.
ON APPROACH IN NAV, AUTOPILOT ENGAGED, ACFT MADE UNCOMMENTED LT TURN. ONCE ESTABLISHED ON FINAL APPROACH AUTOPILOT FAILED & FD DISAPPEARED. REMOVED & REPLACED THE NR 1 FCC AS A PRECAUTION, RTS GOOD, NO FAULTS NOTED IAW AMM 22-01-03.
AIR TURN BACK, AFTER DEPARTURE, FMS 1 FAIL OCCURRED AND RESET. FMS 2 FAIL THEN HAPPENED AND RESET. FINALLY, FMS DUAL FAIL AND RESET SHORTLY AFTERWARD. PERFORMED FIM TASK 34-63 TASK 830 - FMS NR 1 AND NR 2 (VIA NR 1 AND NR 2 RESPECTIVELY) PASS TESTS - REMOVED VIA NR 1 AND VIA NR 2, INSPECTED CONNECTION, AND REINSTALLED VIA NR 1 AND NR 2 - NO ANOMALIES NOTED - PERFORMED RTS PER MM 31-43-00 - ALL TESTS PASS - OK FOR SERVICE.
NR 2 ENGINE COMPRESSOR STALL. REMOVED AND REPLACED NR 2 ENGINE.