NEW PACIFIC AIRLINES, INC.
Also recorded as: NEW PACIFIC AIRLINES, NEW PACIFIC AIRLINES, INC., RAVN ALASKA
Accident & enforcement record
Events that happened, regardless of the operator's own reporting. Each links to its public source.
NTSB accidents & incidents
No NTSB accidents or incidents linked to this operator.
FAA enforcement actions
FAA enforcement records haven't been loaded into GroundCheck yet, so none can be shown — a gap in our data, not evidence of a clean enforcement history.
Maintenance disclosure history
Service Difficulty Reports are self-reported maintenance findings. The NUMBER of reports is not a measure of reliability — diligent operators file more, not fewer. These are shown for transparency, not as a negative signal.
635 reports on file — showing most recent 50.
FWD GALLEY EMERGENCY LIGHT INOP.
L4 DOOR FWD FRAME UPPER STOP FITTING IS GOUGED.
NR 2 ENGINE INBD THRUST REVERSER SLEEVE HAS A DENT 18 INCHES FROM TOP EDGE AND 15 INCHES FROM FWD EDGE.
LEFT MLG BODY DOOR OUTER SURFACE HEAT SHIELD COVER IS CRACKED AND DELAMINATED.
HIGH OIL CONSUMPTION AUTO SHUTDOWN ACTIVATED
R3 DOOR SLIDE LIGHT, O/H EXIT SIGN AND AISLE LIGHT SEATS 13DC, 15DC, 17DC, AND EXIT SIGN INOPERATIVE, NO TEST.
RIGHT UPPER SURFACE SKIN PATCH DE-BONDED.
RIGHT WING NR 6 SLAT TRAILING EDGE UPPER SKIN.
L3 DOOR EXIT IND SIGN INOPERATIVE.
AFT GALLLEY RIGHT SIDE EMERGENCY EXIT SIGN INOPERATIVE, WON'T TURN ON.
LEFT NACELLE REVERSE FLOW CHECK CONTROL LINE FOUND GOUGED.
RIGHT UPPER WING ACCESS PANEL 611KT FOUND DELAMINATED.
DENT ON FUSELAGE SKIN STA 846 BETWEEN S-4L AND S-5L.
RIGHT WINGTIP HAS LIGHTING STRIKE.
EVIDENCE OF DAMAGE AT EDGE OF CANOE PANEL 672HB.
DENT ON PREVIOUS BLEND ON FUSELAGE SKIN AT STA 481 BETWEEN STR 27L-28-L.
VERTICAL STABILIZER LH LOWER SIDE OF RUDDER HAS DENT
DENT ON FUSELAGE SKIN AT STA 531 BETWEEN STR 28L AND 28R
LH ENG OB LOWER BLOCKER FLAP #6 FROM 12 OCLOCK POSITION LOWER HINGE ATTACHEMENT PLATE HAS MISSING PIECE
DENT ON FUSELAGE SKIN STA 1697 BETWEEN S-18L AND S-19L.
R3 DOOR SLIDE LIGHT, O/H EXIT SIGN AND AISLE LIGHT SEATS 13DC, 15DC, 17DC INOP LIGHT ALONG WITH EXIT SIGN.
DURING INSTALLATING AFT 3 LH DOOR LINNERS FJOUND SLIDE LIGHT INDICATIO SWITCH BROKEN
AFT GALLEY R/H SIDE EMERGENCY EXIT MAKER INOP
EMERGENCY MARKER AT R3 DOOR INOPERATIVE.
DURING INSTALLING AFT 4 R/H DOOR LINERS FOUND SLIDE LIGHT INDICATOR SWITCH CONNECTOR BROKEN
DURING SCHEDULED "A" CK EVENT THE VERTICAL STABILIZER R/H FWD PANEL WAS FOUND DELAMINATED L=40", W=22" BETWEEN FSS195.390AND FSS 270.784. CORRECTIVE ACTION: PROCURED, LOCATED AND DRILLED NEW VERTICAL STAB R/H SIDE FIXED PANEL321CL PN: 175N20010U4 SN: 0004399709 IAW SRM 51-40-08, B757-200SRM 51-40-05, TREATED AND PRIMED HOLES FOR THE FASTENERS AND SURROUNDING EDGES ONPANEL 321CL IAW B757-200 SRM 51-20-01, OK TO INSTALL PANEL 321CLPN: 175N2001U4 SN: 0004399709
DURING SCHEDULED "A" CK EVENT THE VERTICAL STABILIZER R/H FWD PANEL WAS FOUND DELAMINATED L=40", W=22" BETWEEN FSS195.390AND FSS 270.784. CORRECTIVE ACTION: PROCURED, LOCATED AND DRILLED NEW VERTICAL STAB R/H SIDE FIXED PANEL321CL PN: 175N20010U4 SN: 0004399709 IAW B757-200 SRM 51-40-08, B757-200SRM 51-40-05, TREATED AND PRIMED HOLES FOR THE FASTENERS AND SURROUNDING EDGES ONPANEL 321CL IAW B757-200 SRM 51-20-01, OK TO INSTALL PANEL 321CL PN: 175N2001U4 SN: 0004399709
SKIN PANEL DELAMINATION
#2 ENG HYD PUMP CAUTION LIGHT CAME ON IN FLIGHT.
AUX BATT HOT WARNING LIGHT CAME ON MOMENTARILY TWICE ON INITIAL CLIMB OUT. WE FOLLOWED FLIGHT OPS READ FILE NO. 2504. TURNED AUX BATT SWITCH OFF.
CAPTS FMS SCREEN WENT BLANK. UNRESPONSIVE TO ANY INPUT.
LOUD SQUEAL COMING FROM THE CARGO DOOR. VERIFIED BY F/A.
NOSE WHEEL SHIMMY ON TAKEOFF.
#2 ITT GAUGE INTERMITTENTLY INOP
LAVATORY "FLUSH" INTERMITTENTLY INOP
RIGHT/FWD (R1) WINDSHIELD ARCHING IN FLIGHT, THEN SHATTERED. CORRECTIVE ACTION: REPLACED R1 WINDOW IAW B757-200 AMM 56-11-01, OPS CHECKED GOOD.
WHILE PERFORMING INSPECTIONS PER AD 2017-20-05, PARA (G), BOEING SB 757- A CRACK MEASURING 1.2" IN LENGTH WAS FOUND ON FUSELAGE SKIN PANEL P/N 141N3312-7 AT THE S-4R LAP SEAM BETWEEN BS 418 AND 439. DAMAGE WAS REPAIRED IAW BOEING MESSAGES C04-C04-25-0006-01C THROUGH -10B, 8100-9 DTD. 02/20/2025, REF. ID 202502150036-0004.
FLAP DRIVE CAUTION LIGHT ILLUMINATED AFTER TAKEOFF W/FLAPS SELECTED 5 DEGREES.
DURING A3 CHECK THE L4 DOOR OVERHEAD EMERGENCY LIGHT SWITCH DID WAS FOUND NOT TO WORK PER BOEING TASK CARD B757-LUMP-33-001-00-0. CORRECTIVE ACTION: REMOVED AND REPLACED EMERGENCY LIGHTS TEST SWITCH AT L4 DOOR PER B757 AMM 25-21-06-004-103, AMM 25-21-06-404-086. OPS CHECK GOOD PER B757 AMM 33-51-00-715-003.
LEFT MAIN GEAR DOOR HANGING DOWN 1 INCH IN CRUISE FLIGHT. F/A SAID THE DOOR CAME COMPLETELY UP DURING DESCENT.
CENTER AISLE MAIN ENTRANCE DOOR CEILING EMERGENCY EXIT SIGN INOP.
"ALT GEAR IND FAIL" ANNUNCIATOR CAME ON IN FLIGHT. RIGHT MAIN ALT LIGHT WAS INOP.
DISCREPANCY: #1 HYDRAULIC PUMP 'HOT CAUTION' LIGHT FLICKERING ON. CORRECTIVE ACTION: SWAPPED TO SECONDARY TEMP SENSOR ON #1 SPU AND REPLACED CANNON PLUG 2921-P1 AND OPS CHECKED GOOD IAW DASH-8-100 AMM 29-11-14.
RIGHT, #3 DE-ICE BOOT DOES NOT INFLATE. DE-ICE LIGHT DOES NOT ILLUMINATE.
RIGHT GEN CONT OFF ILLUMINATED ON TAKEOFF
DEICE BOOT FAILURE OF TAIL RHS OUTBOARD SECTION 6 RIGHT HAND SIDE - INDICATION LIGHT DOES NOT ILLUMINATE DURING OPERATION IN AUTO NOR IN MANUAL
#2 DC GEN CAUTION LIGHT ILLUMINATED. RESET FAILED.
#1 ENGINE INTAKE DEICE INOP
WEATHER RADAR FAILED IN FLIGHT IN BOTH AUTO AND MANUAL
SEVERAL EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE WHEN SWITCHED ON
Linked aircraft
No aircraft currently linked.