N42NC
Registered owner: CAPAIR INC, FL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| NORTHERN AIR CARGO LLC (NACA) | Operator | on 2005-06-15 | Operator named in NTSB report |
Accident & incident history
Operated by NORTHERN AIR CARGO 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.
24 reports on file, 2004-05-15 – 2006-03-29.
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,168 hrs · 25,453 cycles
KEELBEAM FRAME 25 THRU 27 HAS NUMEROUS AREAS LVL 1 CORROSION ON BOTH LWR SIDES & UPPER SIDE. REMOVED CORROSION ON KEELBEAM PER ATR-42 SRMM 51-21-45. EVALUATION DEPTH OF DAMAGE REMOVAL AREAS FOUND WEB PNLS TO BE OUT OF LIMITS PER SRM 53-57-70. REMOVED DAMAGE FROM SPECIAL STRINGERS 20L, 20R ON LWR SIDE OF KEELBEAM PER ATR-42 SRM 51-21-45 REV 76. FAB`D WEB PLATES OUT OF 7075-T6 .080". ALODINED PRIMED AND TOP COATED PER ATR-42 SRM 51-21-17 & 51-21-27. SPECIAL STRINGERS FOUND WITHIN LIMITS BY UT INSPECT PER ATR-42 SRM 53-51-00. ALODINED, PRIMED, AND TOP COATED PER ATR-42 SRM 51-21-17, 51-21-27. INSTALLED WEB PLATES PER ATR-42 SRM 51-25-01, 51-25-04.
Part: PANEL — GOUGED (LT NACELLE) · airframe 26,168 hrs · 25,453 cycles
LT NACELLE I/B REBATE PNL GOUGED ON LWR FLANGE. CLEANED DAMAGE AREA TO ACCESS DAMAGE. FOUND GOUGE LWR FWD CORNER .079" DEEP MAX AND CHAFFINGS .036" DEEP MAX. ORIG THICKNESS OF PART IS .079 PER ATR SRM 54-31-61 FIG 101 ITEM 5 REV 76. MAX ALLOWABLE DAMAGE PER ATR SRM CHAP 51-10-10 TABLE 1 REV 76 IS .004". FOUND DAMAGE BEYOND ALLOWABLE LIMITS. REMOVED RT I/B REBATE PNL IAW ATR 42 SRM CHAP 54-31-61 FIG 101 REV 76. MADE NEW REBATE PNL P/N S54310252201 USING 2024-0 .080". PNL HEAT TREATED TO 2024-T42 IAW ATR 42 SRM 51-23-01 PGA 18-19 REV76. ALODINED IAW ATR 42 SRM 51-21-17 REV 76. PRIMED IAW ATR 42 SRM 51-21-28 REV 76. INSTALLED RT I/B REBATE PNL IAW ATR 42 SRM 54-31-61 FIG 101 ITEM 5 REV 76, 51-25-01 REV
Part: PANEL — GOUGED (LT NACELLE) · airframe 26,168 hrs · 25,453 cycles
LT O/B NACELLE REBATE PNL IS CHAFFED. CLEANED DAMAGED AREA. FOUND GOUGE LWR FWD CORNER .046' DEEP MAX AND CHAFFING .015 DEEP MAX. ORIG THICKNESS OF PART IS .079" PER SRM 54-31-61 FIG 101. MAX ALLOWABLE DAMAGE PER ATR 42 SRM 51-10-10 TBL NR 1 IS .004, FOUND DAMAGE BEYOND ALLOWABLE LIMITS REMOVED RT O/B REBATE PNL IAW ATR 42 SRM 54-31-61 FIG 101. MADE NEW REBATE PNL P/B S54310252200 USING 2024-0 .080". PNL SENT FOR HEAT TREAT TO 2024-T42 IAW ATR 42 SRM 51-23-01 PGS 18-19 REV76. ALODINED IAW ATR 42 SRM 51-21-17 REV 76. PRIMED IAW ATR 42 SRM 51-21-28 REV 76. INSTALLED RT O/B REBATE PNL IAW ATR 42 SRM 54-31-61 FIG 101 IT NR 5 REV 76, ATR 42 SRM 51-25-01 REV 76, AND 51-25-04 REV 76. PRIMED AND TOP COATED REPA
Part: PANEL — GOUGED (RT NACELLE) · airframe 26,168 hrs · 25,453 cycles
RT NACELLE I/B REBATE PANEL IS GOUGED ON THE LOWER FLANGE. CLEANED DAMAGED AREA TO ASSESS DAMAGE. FOUND GOUGE AT LWR FWD CORNER TO BE .065" DEEP MAX AND CHAFFING TO BE .018" DEEP MAX. ORIGINAL THICKNESS OF PART IS .079" PER ATR 42 SRM CHAPTER 54-31-61 FIG 101 ITEM 5 REV 76. MAX ALLOWABLE DAMAGE PER ATR SRM CHAPTER 51-10-10 TABLE 1 REV 76 IS .004". FOUND DAMAGE TO BE BEYOND ALLOWABLE LIMITS. REMOVED RT I/B REBATE PANEL IAW ATR 42 SRM CHAPTER 54-31-61 FIG 101 REV 76. MADE NEW REBATE PANEL P/N S54310252200USING 2024-0 .080". PANEL HEAT TREATED TO TO 2024-T42 IAW ATR 42 SRM 51-23-01 PGA 18-19 REV76. ALODINED IAW ART 42 SRM 51-21-17 REV 76. PRIMED IAW ATR 42 SRM 51-21-28 REV 76. INSTALLED RT I/B REBATE PA
Part: PANEL — GOUGED (RT NACELLE) · airframe 26,168 hrs · 25,453 cycles
RT NACELLE O/B REBATE PNL IS CHAFFED. CLEANED DAMAGED AREA TO ASSESS DAMAGE. FOUND GOUGE AT LWR FWD CORNER .024" DEEP MAX AND CHAFFING .033" DEEP MAX. ORIG THICKNESS OF PART IS .079" PER ATR 42 SRM 54-31-61 FIG 101 IT#5. MAX ALLOWABLE DAMAGE PER ATR 42 SRM 51-10-10 TABLE 1 IS .004". FOUND DAMAGE BEYOND ALLOWABLE LIMITS. REMOVED RT O/B REBATE PNL IAW ATR 42 SRM 54-31-61 FIG 101. MADE NEW REBATE PNL P/B S54310252201 USING 2024-0 .080". PNL SENT FOR HEAT TREAT TO 2024-T42 IAW ATR 42 SRM 51-23-01 PGS 18-19 REV76. ALODINED IAW ATR 42 SRM 51-21-17 REV 76. PRIMED IAW ATR 42 SRM 51-21-28 REV 76. INSTALLED RT O/B REBATE PNL IAW ATR 42 SRM 54-31-61 FIG 101 IT NR 5 REV 76, ATR 42 SRM 51-25-01 REV 76, AND 51-25-0
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,168 hrs · 25,453 cycles
RT O/B SEAT TRACK FROM FR17-FR19 OUT OF LIMITS (CORROSION). REMOVED SEAT TRACK TRACK IAW 51-25-04 PG 27-28B REV 76. FABRICATED SEAT TRACK USING 946213 7075-T6511 AMS 22-200/HP10093-F IAW ATR42 SRM 53-00-00 FIG 437 SHEET 5 AND FIG 401 SHEET 1/2 REV 76. ALODINED, PRIMED, AND PAINTED IAW ATR 42 SRM 51-21-00/ 2B REV 76. INSTALLED IAW ATR 42 SRM 51-25-04 PG 13-14 REV 76. DRILLED NUT CLIP HOLES IAW ATR 42 SRM 51-25-02 PG 34-35 REV 76. ALODINED, PRIMED AND PAINTED NUT CLIP HOLES IAW ATR 42 SRM 51-21-00 PAR 2B.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,168 hrs · 25,453 cycles
LT O/B SEAT TRACK FROM FR 23-FR 29 OUT OF LIMITS (CORROSION). REMOVED SEAT TRACK TRACK IAW 51-25-04 PG 27-28B REV 76. FABRICATED SEAT TRACK USING 946213 7075-T6511 AMS 22-200/HP10093-F IAW ATR42 SRM 53-00-00 FIG 437 SHEET 5 AND FIG 401 SHEET 1/2 REV 76. ALODINED, PRIMED, AND PAINTED IAW ATR 42 SRM 51-21-00/ 2B REV 76. INSTALLED IAW ATR 42 SRM 51-25-04 PG 13-14 REV 76. DRILLED NUT CLIP HOLES IAW ATR 42 SRM 51-25-02 PG 34-35 REV 76. ALODINED, PRIMED AND PAINTED NUT CLIP HOLES IAW ATR 42 SRM 51-21-00 PAR 2B.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,168 hrs · 25,453 cycles
RT I/B SEAT TRACK FROM FR36-FR40 OUT OF LIMITS (CORROSION). REMOVED SEAT TRACK TRACK IAW 51-25-04 PG 27-28B REV 76. FABRICATED SEAT TRACK USING 946213 7075-T6511 AMS 22-200/HP10093-F IAW ATR42 SRM 53-00-00 FIG 437 SHEET 5 AND FIG 401 SHEET 1&2 REV 76. ALODINED, PRIMED, AND PAINTED IAW ATR 42 SRM 51-21-00/ 2B REV 76. INSTALLED IAW ATR 42 SRM 51-25-04 PG 13-14 REV 76. DRILLED NUT CLIP HOLES IAW ATR 42 SRM 51-25-02 PG 34-35 REV 76. ALODINED, PRIMED AND PAINTED NUT CLIP HOLES IAW ATR 42 SRM 51-21-00 PAR 2B.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,168 hrs · 25,453 cycles
LT I/B SEAT TRACK FROM FR 36 - FR 41 OUT OF LIMITS (CORROSION). REMOVED SEAT TRACK TRACK IAW 51-25-04 PG 27-28B REV 76. FABRICATED SEAT TRACK USING 946213 7075-T6511 AMS 22-200/HP10093-F IAW ATR42 SRM 53-00-00 FIG 437 SHEET 5 AND FIG 401 SHEET 1/2 REV 76. ALODINED, PRIMED, AND PAINTED IAW ATR 42 SRM 51-21-00/ 2B REV 76. INSTALLED IAW ATR 42 SRM 51-25-04 PG 13-14 REV 76. DRILLED NUT CLIP HOLES IAW ATR 42 SRM 51-25-02 PG 34-35 REV 76. ALODINED, PRIMED AND PAINTED NUT CLIP HOLES IAW ATR 42 SRM 51-21-00 PAR 2B.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,168 hrs · 25,453 cycles
LT I/B SEAT TRACK AT FR 26 OUT OF LIMITS (CORROSION). REMOVED SEAT TRACK TRACK IAW 51-25-04 PG 27-28B REV 76. FABRICATED SEAT TRACK USING 946213 7075-T6511 AMS 22-200/HP10093-F IAW ATR42 SRM 53-00-00 FIG 437 SHEET 5 AND FIG 401 SHEET 1/2 REV 76. ALODINED, PRIMED, AND PAINTED IAW ATR 42 SRM 51-21-00/ 2B REV 76. INSTALLED IAW ATR 42 SRM 51-25-04 PG 13-14 REV 76. DRILLED NUT CLIP HOLES IAW ATR 42 SRM 51-25-02 PG 34-35 REV 76. ALODINED, PRIMED AND PAINTED NUT CLIP HOLES IAW ATR 42 SRM 51-21-00 PAR 2B.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,128 hrs · 25,453 cycles
RT O/B SEAT TRACK FROM FR 36-FR 41 OUT OF LIMITS (CORROSION). REMOVED SEAT TRACK IAW 51-25-04 PG 27-28B REV 76. FABRICATED SEAT TRACK USING 946213 7075-T6511 AMS 22-200/HP10093-F IAW ATR42 SRM 53-00-00 FIG 437 SHEET 5 AND FIG 401 SHEET 1/2 REV 76. ALODINED, PRIMED, AND PAINTED IAW ATR 42 SRM 51-21-00/ 2B REV 76. INSTALLED IAW ATR 42 SRM 51-25-04 PG 13-14 REV 76. DRILLED NUT CLIP HOLES IAW ATR 42 SRM 51-25-02 PG 34-35 REV 76. ALODINED, PRIMED AND PAINTED NUT CLIP HOLES IAW ATR 42 SRM 51-21-00 PAR 2B.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,168 hrs · 25,453 cycles
RT I/B SEAT TRACK FROM FR 25-FR 26 OUT OF LIMITS (CORROSION). REMOVED SEAT TRACK TRACK IAW 51-25-04 PG 27-28B REV 76. FABRICATED SEAT TRACK USING 946213 7075-T6511 AMS 22-200/HP10093-F IAW ATR42 SRM 53-00-00 FIG 437 SHEET 5 AND FIG 401 SHEET 1/2 REV 76. ALODINED, PRIMED, AND PAINTED IAW ATR 42 SRM 51-21-00/ 2B REV 76. INSTALLED IAW ATR 42 SRM 51-25-04 PG 13-14 REV 76. DRILLED NUT CLIP HOLES IAW ATR 42 SRM 51-25-02 PG 34-35 REV 76. ALODINED, PRIMED AND PAINTED NUT CLIP HOLES IAW ATR 42 SRM 51-21-00 PAR 2B.
Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 26,168 hrs · 25,453 cycles
RT I/B SEAT TRACK AT FR 36 RUNOUT (FWD SIDE) OUT OF LIMITS (CORROSION). REMOVED SEAT TRACK TRACK IAW 51-25-04 PG 27-28B REV 76. FABRICATED SEAT TRACK USING 946213 7075-T6511 AMS 22-200/HP10093-F IAW ATR42 SRM 53-00-00 FIG 437 SHEET 5 AND FIG 401 SHEET 1/2 REV 76. ALODINED, PRIMED, AND PAINTED IAW ATR 42 SRM 51-21-00/ 2B REV 76. INSTALLED IAW ATR 42 SRM 51-25-04 PG 13-14 REV 76. DRILLED NUT CLIP HOLES IAW ATR 42 SRM 51-25-02 PG 34-35 REV 76. ALODINED, PRIMED AND PAINTED NUT CLIP HOLES IAW ATR 42 SRM 51-21-00 PAR 2B.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,168 hrs · 25,453 cycles
LT INBOARD SEAT TRACK FROM FR 17-FR 23 FOUND OUT OF LIMITS(CORROSION). REMOVED SEAT TRACK IAW ATR42 SRM 51-25-04 PG 27-28B REV 76. FABRICATED SEAT TRACK USING 946213:7075-T6511AMS 2Q-A-200/11P10093 IAW ATR 42 SRM 53-00-00-FIG 437 SHEET 5 AND FIGURE 401 SHEET 1/2 REV 76. ALODINED PRIMED AND PAINTED IAW ATR 42 SRM 51-21-00/2B REV76. INSTALLED IAW ATR 42 SRM 51-25 04 PG 13/14 REV76. LOCATED AND DRILLED NUT CLIPS HOLES IAW ATR42 SRM 51-25-02 PG 34/35 REV 76. ALODINED, PRIMED, AND PAINTED NUT CLIP HOLES IAW ATR 42 SRM 51-21-00 PAR 2B.
Part: SEAT TRACK — CORRODED (FUSLEAGE) · airframe 26,168 hrs · 25,453 cycles
LT O/B SEAT TRACK FROM FR 36 - FR 41 OUT OF LIMITS (CORROSION). REMOVED SEAT TRACK TRACK IAW 51-25-04 PG 27-28B REV 76. FABRICATED SEAT TRACK USING 946213 7075-T6511 AMS 22-200/HP10093-F IAW ATR42 SRM 53-00-00 FIG 437 SHEET 5 AND FIG 401 SHEET 1/2 REV 76. ALODINED, PRIMED, AND PAINTED IAW ATR 42 SRM 51-21-00/ 2B REV 76. INSTALLED IAW ATR 42 SRM 51-25-04 PG 13-14 REV 76. DRILLED NUT CLIP HOLES IAW ATR 42 SRM 51-25-02 PG 34-35 REV 76. ALODINED, PRIMED AND PAINTED NUT CLIP HOLES IAW ATR 42 SRM 51-21-00 PAR 2B.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,168 hrs · 25,453 cycles
LT I/B SEAT TRACK FROM FR35 - FR36 OUT OF LIMITS (CORROSION). REMOVED SEAT TRACK TRACK IAW 51-25-04 PG 27-28B REV 76. FABRICATED SEAT TRACK USING 946213 7075-T6511 AMS 22-200/HP10093-F IAW ATR42 SRM 53-00-00 FIG 437 SHEET 5 AND FIG 401 SHEET 1/2 REV 76. ALODINED, PRIMED, AND PAINTED IAW ATR 42 SRM 51-21-00/ 2B REV 76. INSTALLED IAW ATR 42 SRM 51-25-04 PG 13-14 REV 76. DRILLED NUT CLIP HOLES IAW ATR 42 SRM 51-25-02 PG 34-35 REV 76. ALODINED, PRIMED AND PAINTED NUT CLIP HOLES IAW ATR 42 SRM 51-21-00 PAR 2B.
Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,168 hrs · 25,453 cycles
AT FR 13 RT CREASE BEAM I/B ANGLE TOP SIDE, POST BLEND THICKNESS OUT OF LIMITS. REMOVED DAMAGE SECTION OF CREASE BEAM I/B ANGLE TOP SIDE. FAB`D REPLACEMENT SECTION OUT OF 7075-0 0.050 P7313G PER ATR42 SRM 53-11-50 ITEM 70 FIG 101 SHT 1 PG 105 REV76. PART HEATED TO 7075-T62 PER ATR 42 SRM 51-23-01 TABLE 7. PARTS FAB ALSO TO INCLUDE ATR 42 SRM 51-24-01 PG 1 REV 76. DRILLED UP PER ATR 42 SRM 51-25-01 REV 76. FAB REAR SPLICE OUT OF .079 7075-T6511 NTA44182 P04134 DRILLED UP PER ATR 42 SRM 53-31-50 FIG 407 REV 76. ALODINED, PRIMED, AND APPLIED TOP COAT TO SPLICE PER ATR 42 SRM 51-21-17 REV 76 AND 51-71-27 REV 76. INSTALLED FAB`D SECTION PER ATR 42 SRM 51-2501 FIG 14, ATR 42 SRM 53-31-50 FIG 402 REV 76. REPAIR PR
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,168 hrs · 25,453 cycles
RT O/B SEAT TRACK FROM FR 29 - FR 36 OUT OF LIMITS (CORROSION). REMOVED SEAT TRACK TRACK IAW 51-25-04 PG 27-28B REV 76. FABRICATED SEAT TRACK USING 946213 7075-T6511 AMS 22-200/HP10093-F IAW ATR42 SRM 53-00-00 FIG 437 SHEET 5 AND FIG 401 SHEET 1/2 REV 76. ALODINED, PRIMED, AND PAINTED IAW ATR 42 SRM 51-21-00/ 2B REV 76. INSTALLED IAW ATR 42 SRM 51-25-04 PG 13-14 REV 76. DRILLED NUT CLIP HOLES IAW ATR 42 SRM 51-25-02 PG 34-35 REV 76. ALODINED, PRIMED AND PAINTED NUT CLIP HOLES IAW ATR 42 SRM 51-21-00 PAR 2B.
Earlier reports · 2004–2005 · 6 reports
2005
Part: INDICATOR — INTERMITTENT (TRIM) · airframe 25,935 hrs · 25,283 cycles
TAKEOFF ABORTED DUE TO FLICKERING TAKEOFF CONFIGURATION AT 1 DEGREE DOWN TRIM. REPLACED TRIM POSITION INDICATOR. OP CHECKED GOOD. REF: JIC 27-15-81-RAI-10000.
Part: SWIVEL FITTING — BROKEN (HYD SYSTEM) · airframe 25,367 hrs · 24,845 cycles
HYDRAULIC BLUE LOW LEVEL LIGHT ON. RT OB SWIVEL FITTING FOUND BROKEN. REMOVED AND REPLACED WITH NEW FITTING. REF JIC 32-11-00-RAI-10020 TASK 1-3. BLED ALL MAIN LANDING GEAR BRAKES IAW ATR42 JIC 32-42-00-BLD-10010. SYSTEM OPS LEAK CHECKED GOOD.
Part: AILERON — LIGHTNING STRIKE (LT WING) · airframe 24,674 hrs · 24,330 cycles
LIGHTNING STRIKE KNOCKED OUT NR 1 ACW AND NR 1 ECU. BOTH WERE RESET SUCCESSFULLY. UPON INSPECTION, DISCOVERED THERE WAS DAMAGE TO LT AILERON. REPLACED LEFT AILERON ASSEMBLY AND OPS CHECKED GOOD.
2004
Part: CONTROL LEVER — SHORTED (MLG) · airframe 23,195 hrs · 23,201 cycles
LANDING GEAR WOULD NOT EXTEND NORMALLY. HAD TO USE MANUAL EXTENSION CONTROL. REPLACED LANDING GEAR CONTROL LEVER. OP CHECKED GOOD.
Part: HOSE — RUPTURED (LT MLG) · airframe 22,282 hrs · 22,620 cycles
GREEN HYDRAULIC SYSTEM LOW LEVEL INDICATION UPON GEAR RETRACTION AFTER TAKEOFF. REPLACED LEFT MAIN LANDING GEAR UP LINE AT ACTUATOR FOR BEING RUPTURED. CHECKED GOOD.
Part: RELAY — INOPERATIVE (MLG) · airframe 22,131 hrs · 22,524 cycles
LANDING GEAR WOULD NOT EXTEND WITH LEVER IN THE DOWN POSITION. GRAVITY EXTENSION PROCEDURE WAS USED. FOUND 14GA RELAY DEFECTIVE AND POOR WIRE RETENTION AT RELAY BASE. REPLACED 14GA RELAY AND RESET PINS. GEAR RETRACTION TEST GOOD MULTIPLE TIMES.