N384WA
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| ARROW AIR INC | Operator | on 2009-04-17 | Operator named in NTSB report |
Accident & incident history
Operated by ARROW AIR INC (per NTSB report)
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.
38 reports on file, 2008-10-02 – 2010-06-18.
Part: VANE — BROKEN (LT WING TE FLAP) · airframe 67,034 hrs · 13,312 cycles
INBOARD FLAP VANE TRAILING EDGE BROKEN OF LT WING. THIS NRC HAS BEEN COVERED BY ERA: DOCUMENT NUMBER 10-57-029 REVISION 1. CONDITION CHECK NORMAL AND JOB COMPLETED.
Part: SKIN — CORRODED (FUSELAGE) · airframe 67,034 hrs · 13,312 cycles
EXFOLIATION CORROSION ON CUTOUT SKIN EDGE OF LAVATORY SERVICE ACCESS DOOR STA: Y=410.5, X=2 TO X=-5. REPAIR SKIN IAW EGAT EI W2010A53B-1328 REV 00 AND REV 01. CONDITION CHECK NORMAL AND JOB COMPLETED.
Part: LONGERON — CORRODED (BS 939 L52) · airframe 67,034 hrs · 13,312 cycles
CORROSION ON LONGERON 52 OF FWD CARGO COMPARTMENT STA: Y=939. REPAIR CORROSION AREA IAW SRM 53-00-05 REPAIR TYPE 1 OF FIG 201 AND FIG 202. CONDITION CHECK NORMAL AND JOB COMPLETED.
Part: LONGERON — CORRODED (FUSELAGE) · airframe 67,034 hrs · 13,312 cycles
LONGERON 46R CORROSION STA Y=6-90--6-96 OF CENTER ACCESSORY COMPARTMENT. REPAIRED LONGERON IAW EI W2010A53B-1330 REV 00,01. CONDITION CHECK NORMAL AND JOB COMPLETED.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 67,034 hrs · 13,312 cycles
CORROSION ON MAIN DECK SEAT TRACK STA:Y=6-50, X=-6 . REPAIRED SEAT TRACK IAW SRM 53-00-52 REPAIR 1 FIG 201 REV 43. JOB COMPLETED AND CONDITION CHECK NORMAL.
Part: LONGERON — CORRODED (FUSELAGE) · airframe 67,034 hrs · 13,312 cycles
LONGERON 46R CORROSION OF CENTER CARGO LOWER SIDE AT STA 1721. ACCOMPLISH EI NO W2010A53B-1348 REV 00, 01, 02, 03, 04, COND CHECK SATISFACTORY.
Part: DOUBLER — CRACKED (CTR LG WW) · airframe 67,034 hrs · 13,312 cycles
CRACK ABOUT 2 INCHES ON CENTER L/G WHEEL WELL LT FORWARD OUTBOARD SIDE DOUBLER STA:Y=1384, X=31.5 (NRC:U05086). REPAIR THE DOUBLER OF STIFFENER AT CENTER GEAR WHEEL WELL LEFT KEEL WEB IAW EGAT EI: W2010A53B-1295. CONDITION CHECK NORMAL AND JOB COMPLETED.
Part: SUPPORT FITTING — CRACKED (NLG WW) · airframe 67,034 hrs · 13,312 cycles
CRACK - LT NLG SUPPORT FITTING CRACK 1 INCH AND RT NLG SUPPORT FITTING CRACK 0.75 INCH STA Y:595.
Part: STRUT — DAMAGED (CENTER LG) · airframe 66,293 hrs · 13,159 cycles
DUE TO HARD LANDING, INSP A PERFORMED AND FOUND CENTER LANDING GEAR STRUT DAMAGED. CENTER LANDING GEAR AND ADDITION BRAKES AND WHEELS REPLACED.
Part: BRACKET — DAMAGED (TE FLAP) · airframe 66,293 hrs · 13,159 cycles
DURING HARD LANDING INSP FOUND DAMAGE/DENT IN FLAP TRACK BRACKET. PER BOEING REPAIR REF 57-ED-269679, SRE-WLD-10-0001-02B THE BRACKET IS STRUCTURALLY ACCEPTABLE FOR CONT IN SERVICE WITH HFEC INSP EVERY C-CHECK NOT TO EXCEED 24MONTHS.
Part: VANE — DAMAGED (TE FLAP) · airframe 66,293 hrs · 13,159 cycles
DUE TO HARD LANDING, INSP A PERFORMED AND FOUND LT WING INBOARD FLAP-VANE AFT RT EDGE DAMAGED. DAMAGED SECTION TRIMMED OUT IAW BOEING APPROVAL REF SRE-WLD-10-0001-02B.
Part: MOUNT FITTING — CORRODED (PYLON) · airframe 66,293 hrs · 13,159 cycles
ENGINE PYLON FWD MOUNT TRUSS FITTING HAS CORROSION IN 2 AFT BOLT HOLES. REWORKED REPAIR IAW SERVICE GENERAL REPAIR DRAWING SG11540000.
Earlier reports · 2008–2009 · 26 reports
2009
Part: WHEEL — MISSING (NLG)
FLT 1457/17 AGT-SCL UPON POST FLIGHT INSPECTION FOUND LEFT NOSE WHEEL MISSING FROM AIRCRAFT.
2008
Part: STRUT — CHAFED (RT MLG)
CHAFING - DURING BRIDGE CHECK+4C CHECK, EGAT MECHANIC FOUND RT MAIN GEAR SHOCK STRUT UPPERSIDE HAD CHAFED L=3" AT STA Y=1240 (REFER TO EGAT NRC NO. U05124) IAW EGAT EI NR W2008A32B-1088 REV OO, EGAT EI NR W2008A32B-1088 REV 01 AND APPROVED RDR DATED 11/11/08.
Part: RIB — CRACKED (LT WING)
DURING BRIDGE CHK + C4 CHK, EGAT MECH FOUND LT WING FIXED LE INTERNAL SUPPORT RIB CRACK AT STA XORS=484. REPAIRED AREA IAW ENGINEERING INSTRUCTION W2008A57B-1288 REV 00 AND EI W2008A57B-1288 REV 01.
Part: SKIN — DAMAGED (BS 595-615)
DURING BRIDGE CHK + 4C, EGAT MECH FOUND FUSELAGE SKIN HAD WRINKLE FROM STA 595-615 AND STR 43R-47R. REPAIR FUSELAGE SKIN STA 595 TO STA 615 PER MD-11 SRM 53-20-00 FIG 11 REV 46.
Part: LONGERON — CORRODED (BS 1721 L44L)
DURING BRIDGE CHK + 4C CHECK, EGAT MECH FOUND LONGERON BASE CORRODED AT CENTER CARGO STA 1721 AND STR 44L. REMOVED CORRODED LONGERON SECTION, MANUFACTURED REPAIR PARTS PER SRM VOL 1 53-10-00 REV 40 AND REPAIRED DAMAGED AREA PER SRM VOL 1 53-10-00 REV 40.
Part: STANCHION — CORRODED (FWD CARGO BAY)
DURING BRIDGE CHK + 4C CHK, EGAT MECH FOUND FWD CARGO STA 6-73 STANCHION LWR END HAD CORROSION. REPAIRED CRACK AREA IAW ENGINEERING INSTRUCTION W2008A53B-1305 REV 00 AND EI W2008A53B-1305 REV 01, INSTALLED REPAIR STANCHION PER SRM VOL 2 51-35-01 REV 40.
Part: WEB — CRACKED (FUSELAGE)
DURING BRIDGE CHK + C4 CHK, EGAT MECH FOUND FWD CARGO COMP WEB UNDER FLOOR CRACKED AT STA 6-50. REPAIRED CRACK AREA IAW ENGINEERING INSTRUCTION W2008A53B-1315 REV 00 AND EI W2008A53B-1315 REV 01.
Part: RIB — CRACKED (LT WING)
CRACK- DURING BRIDGE CHECK + C4 CHECK, EGAT MECH FOUND LT WING FIXED L/E RIB CRACK ON FUELING PANEL OTBD LOWER SIDE AT XORS=538. REPAIRED CRACK AREA IAW ENGINEERING INSTRUCTION W2008A57B-1290 AND EI W2008A57B-1290 REV 01.
Part: SEAT TRACK — CRACKED (FUSELAGE)
DURING BRIDGE CHK + 4C CHK, EGAT MECH FOUND MAIN DECK SEAT TRACK CRACK AT STA 635 AND STR LBL 40. REPAIRED SEAT TRACK AREA PER MD-11F SRM VOL 1 51-21-01 REV 40.
Part: WEB — CRACKED (FUSELAGE)
DURING BRIDGE CHK + 4C CHK, EGAT MECH FOUND FWD CARGO COMP LONGERON L43L SUPPORT WEB CRACKED AT STA 6-60. REPAIRED CRACK IAW ENGINEERING INSTRUCTION W2008A53B-1314 REV 00 AND EI NO W2008A53B-1314 REV 01.
Part: ANGLE — CRACKED (LT WING)
DURING BRIDGE CHECK + 4C CHECK, EGAT MECH FOUND ANGLE OF LT WING FIXED L/E CRACK AT STA XORS=488. REPAIRED CRACK AREA IAW ENGINEERING INSTRUCTION W2008A57B-1301 REV 00 AND EI W2008A57B-1301 REV 01.
Part: SKIN — DAMAGED (RUDDER)
DURING BRIDGE CHECK + 4C CHECK, EGAT MECHANIC FOUND LWR RUDDER BROKEN ON THE LWR EDGE. REPAIRED SKIN DAMAGE AREA IAW ENGINEERING INSTRUCTION W2008A55B-1172 REV 01.
Part: SEAT TRACK — CORRODED (FUSELAGE)
DURING BRIDGE CHECK, MX FOUND M/D SEAT TRACK CORROSION AT Y465, X-27.5. REMOVED CORROSION PER MD-11F SRM 51-33-01 VOL 2 REV 40, REPAIRED SEAT TRACK PER MD-11F SRM 53-70-00 VOL 1 REV 40, REPLACED FASTENERS PER MD-11F SRM 51-33-01 VOL 2 REV 40.
Part: STRUCTURE — CRACKED (NR 3 NACELLE)
CORROSION - DURING BRIDGE CHECK, EGAT MECHANIC FOUND NR 3 ENG LT CORE COWL AFT FRAME CRACK AT 9 OâCLOCK POSITION. (REFER TO EGAT NRC U05049). REPAIRED IAW EI W2008A54B-1056 REV 00, AND EI 2008A54B-1056 REV 01.
Part: LONGERON — DAMAGED (FUSELAGE)
DURING BRIDGE CHECK, MX FOUND FUSELAGE FRAME AND LONGERON TO HAVE HEAT DAMAGE AT STA Y 6-90 TO Y 1139, L27L. REPAIRED IAW ENGINEERING INSTRUCTION W2008A53B-984 REV 00, W2008A53-984 REV 01, W2008A53B-984 REV 02, AND W2008A53B-984 REV 03 TO CLARIFICATION THE HEAT DAMAGED PARTS HAVE BEEN CONSIDERED AS SERVICEABLE AND CONTINUED USE.
Part: SKIN — CORRODED (CENTER WING SKIN)
DURING BRIDGE CHECK, MX FOUND CENTER WING TANK UPPER SKIN SURFACE CORROSION AT STA Y1229, X-100- -120. REPAIRED THE CENTER WING TANK UPPER SKIN CORROSION IAW EI W2008A57B-1061 REV.00
Part: FRAME — DAMAGED (FUSELAGE)
DURING BRIDGE CHECK, MX FOUND FUSELAGE FRAME AND LONGERON TO HAVE HEAT DAMAGE AT STA Y 6-90 TO Y 1139, L27L. OPEN
Part: SKIN — CORRODED (CENTER WING TANK)
DURING BRIDGE CHECK, MX FOUND CENTER WING TANK RT UPPER SKIN SURFACE CORROSION AT STA Y1150-1239, X-8 TO -120. REPAIRED CENTER WING TANK UPPER SKIN CORROSION AREA IAW ENGINEERING INSTRUCTION W2008A57B-1061 REV 00.
Part: FRAME — CRACKED (NR 3 NAC DOOR)
DURING BRIDGE CHECK, MX FOUND NR 3 ENGINE LT CORE COWL AFT FRAME CRACK AT 7 OâCLOCK POSITION. REPAIRED CRACK IAW ENGINEERING INSTRUCTION W2008A54B-1082 REV 00.
Part: FRAME — CRACKED (NR 3 COWLING)
DURING BRIDGE CHECK, MX FOUND NR 3 ENGINE LT CORE COWL AFT FRAME CRACK AT 9 OâCLOCK POSITION. OPEN
Part: SEAT TRACK — CORRODED (FUSELAGE)
DURING BRIDGE CHECK, MX FOUND M/D SEAT TRACK CORROSION AT STA Y466 TO Y470, X-58.5. REPAIR SEAT TRACK CORROSION IAW ENGINEERING INSTRUCTION W2008A53B-1092 REV 00, W2008A53B-1092 REV 01, AND W2008A53-1092 REV 02.
Part: SKIN — MISREPAIRED (TAILCONE)
DURING BRIDGE CHECK, MX FOUND TAILCONE SKIN RT FWD EDGE IMPROPER TRIM OUT AT STA Y2245. REPAIRED DAMAGED AREA IAW ENGINEERING INSTRUCTION W2008A53-119 REV 00 AND EI W2008A53B-119 REV 01.
Part: SKIN — CORRODED (CENTER WING TANK)
DURING BRIDGE CHECK, MX FOUND CENTER WING TANK LT UPPER SKIN SURFACE CORROSION AT STA Y1159-1239, X27-120. REPAIRED IAW ENGINEERING INSTRUCTION W2008A57B-106 REV 00.
Part: SKIN — DEFORMED (BS 595)
DURING BRIDGE CHK + 4C CHK, EGAT MECH FOUND NOSE GEAR TRUNNION FITTING SKIN DEFORMED AT STA Y=595, L50L, REFER TO EGAT NRC NR U05188. REMOVE TRUNNION FITTING AND DAMAGED DOUBLER PER MD-11F SRM VOL 2 51-35-01 REV 40. FABRICATED NEW DOUBLER IAW ENGINEERING INSTRUCTION W2008P53B-1311 REV 00. INSTALLED TRUNNION FITTING AND DOUBLER IAW EI W2008A53B-1308 REV 40.
Part: SEAT TRACK — CORRODED (FUSELAGE)
DURING BRIDGE CHECK, MECHANIC FOUND RT NR 1 DOOR LOWER SEAT TRACK CORROSION AT STA Y-430 TO Y-449. REMOVED CORROSION AND MEASURED REWORK AREA THICKNESS REF JOB CARD NO.300318. REPAIRED IAW ENGINEERING INSTRUCTION NR W2008A53B-1185 REV.01
Part: SEAT TRACK — WORN (FUSELAGE)
DURING BRIDGE CHECK, MECHANIC FOUND MAIN CABIN SEAT TRACK WORN AT STA Y-635, X-8.5. REPAIRED DAMAGE SEAT TRACK PER MD-11 SRM 53-70-00 FIG.1 VOL.1 REV.40.