N362NC
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.
32 reports on file, 2020-11-05 – 2022-09-17.
Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 61,522 hrs · 58,357 cycles
EMERGENCY EXIT LIGHTS FAILD TESTING DUE TO BATTERY PACK.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 61,521 hrs · 58,357 cycles
L1 DOOR INTERIONR AND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHTS FAILED FUNCTIONAL TESTING
Part: NONE — NONE · airframe 61,408 hrs · 58,268 cycles
SUPPLEMENTAL INFORMATION: REMOVED DAMAGE, PERFORMED NDT. FABBED AND INSTALLED REPAIR REF ASAP EO 53-22-037 AND B737-300 SRM AS REF IN EO. EO AND 8110-3 ON FILE.
Part: NONE — NONE · airframe 61,395 hrs · 58,257 cycles
SUPPLEMENTAL INFORMATION: REMOVED DAMAGE, PERFORMED HFEC, LOCATED AND FABBED DOUBLER WITH FILLER FROM .040 2024-T3. INSTALLED REPAIR DOUBLER WET WITH SEALANT. AFTER INSTALL COMPLETED, REPRIMED AND APPLIED CORROSION PREVENTIVE COMPOUND. REPAIR INSTALLED IN REF PEMCO EA PD37-53-3384 WITH NO DEVIATION. 8110-3 ON FILE WITH PEMCO EAPD37-53-3384
Part: NONE — NONE · airframe 61,096 hrs · 58,006 cycles
MAIN CABIN CENTER SEAT TRACK CRACKED STA 500B PLUS 3, FLAGGED AND MARKED AT FWD EDGE OF PALLET LOCK ASSY. SEE PWS AND PEMCO EO PD 37-53-3370 FOR DETAILS. REMOVED AND REPLACED SECTION OF SEAT TRACK, 8110-3 ATTACHED TO EO PD37-53-3370
Earlier reports · 2020–2021 · 27 reports
2021
Part: SUPPORT FITTING — CRACKED (LEFT WING) · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND LEFT WING AT MLG SYPPORT FITTING, HOLE #5 HAS A CRACK INDICATION IN CHORD LAYER. S/O 660006 N/R 38573
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND NUMBEROUS BULBS WERE OUT IN THE EMERGENCY EXIT LIGHTS ABOVE AND BELOW THE ENTRY DOORS. S/O 660006 N/R 38204.
Part: SKIN — CRACKED (L1 DOOR) · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND L1 DOOR AT UPPER HINGE, HOLE AT BS 303.9, STR. 10L HAS TWO CRACK INDICATIONS. S/O 660006 N/R 39632
Part: SKIN — CRACKED (L1 DOOR) · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND L1 DOOR FWD CORNER HAS CRACK INDICATION IN HOLE BS 304 - 6.5 INCHES, 2 INCHES DOWN FROM STR. 6L. S/O 660006 N/R 38447
Part: SKIN — CRACKED (LT WING) · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND L/H WING, I/B UPPER SKIN, HOLE "A" 75, AS A CRACK INDICATION. S/O 660006 N/R 38766
Part: SKIN — CRACKED (RT WING) · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND L/H WING, I/B UPPER SKIN, HOLE "B" 68, HAS A CRACK INDICATION. S/O 660006 N/R 38768
Part: SKIN — CRACKED (LT WING) · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND L/H WING, I/B UPPER SKIN, HOLE "A" 100, HAS A CRACK INDICATION. S/O 660006 N/R 38767
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND LEFT WING UPPER SKIN ON THE LOWER SURFACE AT WBL 174.7, THE SKIN HAS CORROSION 1" FWD OF T/E OF SKIN. S/O 660006 N/R 38756
Part: SUPPORT — CRACKED (RT WING) · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND RIGHT WING AFT 3678R WTB PANEL SUPPORT IS CHAFED AND CRACKED AT STA. 727 STR. 19 - 20R. S/O 660006 N/R 38690
Part: SUPPORT FITTING — CRACKED (RT MLG) · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MLG SUPPORT FITTING OF RIGHT WING AT HAS CRACK INDICATION IN HOLE #11 AND #12 IN REAR SPAR WEB LAYER. S/O 660006 N/R 38574
Part: SUPPORT — CRACKED (RT MLG WW) · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION, FOUND R/H MAIN LANDING W/W AFT BELLY CUTOUT RADIUS PANEL HAD A CRACKED PANEL SUPPORT. S/O 660006 N/R 38470
Part: FITTING — CORRODED (LT MLG) · corrosion level 2 · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION, FOUND LEFT MAIN LANDING GEAR FORWARD OUTBOARD LUG HAS SEVERE PITTING CORROSION. S/O 660006 N/R 38671
Part: ANGLE — CRACKED (LT WING TE FLAP) · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND L/H WING #3 FLAP FAIRING HAS TWO CRACKED INTERNAL "L" ANGLES. S/O 660006 N/R 38745
Part: PANEL — CORRODED (AILERON HINGE) · corrosion level 2 · airframe 58,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND R/H WING T/E AILERON, #3 AILERON HINGE FITTING, PANEL ATTACH BOLT HOLES HAVE CORROSION IN AND AROUND THEM. S/O 660006 N/R 38407
Part: ANGLE — DENTED (MAIN CARGO DOOR) · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND DENT IN FWD LWR ANGLE OF MAIN CARGO DOOR CUTOUT DOOR JAMB. S/O 660006 N/R 38238
Part: BRACKET — PUNCTURED (BS 344 S16L) · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND WEB BRACKET HAS A PUNCTURE AT BS 344, STR. 16L. S/O 660006 N/R 38669
Part: HINGE FITTING — CORRODED (RT AILERON) · corrosion level 2 · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND R/H WING T/E AILERON, #2 AILERON HINGE FITTING, PANEL ATTACH BOLT HOLES, HAVE CORROSION IN AND AROUND THEM. S/O 660006 N/R 38406
Part: FLOOR PANEL — CORRODED (AFT CARGO) · corrosion level 2 · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND AFT CARGO COMPARTMENT FLOOR PANEL 1534X HAS MULTIPLE AREAS OF SURFACE ETCH CORROSION. S/O 660006 N/R 38253
Part: STRUCTURE — DAMAGED (LT WING TE FLAP) · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND A DENT AND CRACK IN THE L/H TRAILING EDGE OF THE MID FLAP THAT WAS STOP DRILLED AND SEALED. S/O 660006 N/R 38151
Part: TRANSITION PANEL — CORRODED (AFT CARGO COMPT) · corrosion level 2 · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND AFT CARGO COMPARTMENT, BS 727D +10 - 790 LBL 24 TRANSITION PANEL HAS MULTIPLE AREAS OF CORROSION AND 2 EACH LOOSE FRAME ATTACH RIVETS. S/O 660006 N/R 38261
Part: SHEAR WEB — CRACKED (CARGO DOOR FRAME) · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND SHEAR WEB FRAME 592.4 OF FWD CARGO DOOR AFT FRAME IS CRACKED. S/O 660006 N/R 38630
Part: ATTACH ANGLE — CORRODED (AFT CARGO) · corrosion level 2 · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND MULTIPLE AREAS OF CORROSION ON FLOOR PANEL CROSS ATTACH ANGLE IN AFT CARGO COMPARTMENT AT BS947.5, LBL-24 - RBL-24. S/O 660006 N/R 38282
Part: ATTACH FITTING — CORRODED (RT MLG SUPPORT) · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND R/H MLG SUPPORT BEAM STABILIZER ATTACH FITTING HAS FRETTING ON BOTH LUG FACES. S/O 660006 N/R 39463
Part: TRANSITION PANEL — CORRODED (CARGO FLOOR) · corrosion level 2 · airframe 59,504 hrs · 56,339 cycles
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND TRANSITION PANEL IN AFT CARGO COMPARTMENT, AT BS 787 TO BS 947.5, LBL 24, HAS MULTIPLE AREAS OF CORROSION. S/O 660006 N/R 38264
2020
Part: FLAP SYSTEM — MALFUNCTIONED · airframe 59,004 hrs · 55,652 cycles
DISCREPANCY: MISSED APPROACH DUE TO FLAPS NOT DEPLOYING AND SPEED BRAKE NOT DEPLOYING. NO FLAP ASSYMETRY AND NO FLAP DISAGREE. CORRECTIVE ACTION: PERFORMED FLAP OPERATION CHECK & SPEED BRAKE OPERATIONAL CHECK WITH NO BINDING OR INABILITY TO MOVE HANDLES. INSPECTED EXPOSED CABLES FOR CONTAMINATION IN FWD E&E BAY & WHEEL WELL, NONE NOTED, REF B737-300 AMM 27-51-00-501 & 27-62-00-501.
Part: SKIN — CRACKED (FUSELAGE) · airframe 58,918 hrs · 55,582 cycles
DISCREPANCY: CRACK ON LEFT SIDE FUSELAGE, 14 INCHES FWD OF BS 500, 2.75 INCHES ABOVE S26L, 1.5 INCHES LONG. CUT OUT DAMAGE, FABBED DOUBLER AND INSTALLED, PER REF B737-300 SRM 53-00-01 REPAIR 31 DETAIL XIX AND PEMCO EA NR PD37-53-3220.
Part: START VALVE — INOPERATIVE (NR 2 ENGINE) · airframe 58,857 hrs · 55,532 cycles
DISCREPANCY: DURING CLIMB NR 2 ENGINE EGT LIGHT ILLUMINATED A/T DISCONNECT MANUAL THRUST REDUCTION. LARGE THRUST LEVER SPLIT FOR EQUAL THRUST. A/P & AT ILS ENGINE PERFORMANCE NORMAL. CORRECTIVE ACTION: PERFORMED VISUAL CHECK OF INLET AND EXHAUST, NO DEFECTS NOTED. CHECKED VSV ACTUATOR RIG VBV CABLE RIG. REPLACED START VALVE FOR NOT SEATING CLOSED & HAD PNEUMATIC LEAK. OPERATIONS CHECKED GOOD. PERFORMED POWER RUN TO 80 PERCENT N1, NO DEFECTS NOTED.