N7251
Registered owner: ACCELERATE AERIAL LLC, IL (owner ≠ operator)
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.
4 reports on file, 2021-12-01 – 2022-07-25.
Part: NONE — LEAKING (CTR FUEL TANK AT) · airframe 3,335 hrs · 1,182 cycles
AFTER FINAL REFUELLING, DETECTED FUEL LEAKAGE IN THE CENTER TANK ACCESS PANEL #1 (531AB). REMOVED AND REPLACED THE GASKET AND RING, CLAMP TANK ACCESS , AT POSITION 531AB.LEAK CHECK AFTER REFUELING --NO LEAKS FOUND.
Part: STRUCTURE — DAMAGED (MULTIPLE AREAS) · airframe 1,177 hrs · 436 cycles
REFERENCE 7504156 COMPLETED DAMAGE CUTOUT ON DENT R/H SIDE ...REF SRM 51-10-02...AWAITING AVO/EC/RA FOR FURTHER INSTRUCTIONS. HFEC INSPECTION REQUIRE AROUND THE CUTOUT. HFEC INSPECTION REQUIRE OF ALL REMOVED INITIAL FASTENERS. PERFORMED HFEC OF TRIM OUT REF 737 NDT PART 6 51-00-00 PROCEDURE MATERIAL ID# 2024-T3 .063 PO#9038308 STEP B - FABRICATION STEP 1 INSPECTION REQUIRED FOR MATERIAL ID VERIFIED MATERIAL ID. 23 & AVO 7251-21-11-28-01 STEP 1.A. NO DEFECTS NOTED. PER AVO# 7251-21-11-28-01. MATERIAL NOTED. REF: AVO #: 7251-21-11-28-01A, ITEM A, 9. APPROVED FABRICATION OF -1 REPAIR DOUBLER PER FIGURE 2 OF AVO # VERIFIED ACCOMPLISHMENT OF STEP 7 OF AVO 7251-21-11-28-01A VERIFIED STEPS 2, 5 AND 6 OF AVO # 7251-21-11-28-01A. VERIFIED ACCOMPLISHMENT OF STEP 1 AND 2 SECTION B OF AVO VERIFIED DAMAGE CUTOUT ON DENT R/H SIDE ...REF SRM 51-10-02.. VERIFIED ACCOMPLISHMENT OF STEP 5 AND 6 SECTION B OF AVO VERIFIED ACCOMPLISHMENT OF STEP 7 SECTION B OF AVO INSPECTED DOUBLER OK TO TREAT AND PRIME. CLEARED FOR OK TO INSTALL REPAIR PART AS PER 7251-21-11-28-01. (RE-FORM SKIN DENT TO ORIGINAL CONTOUR) 7251-21-11-28-01A (ENSURE ADDITIONAL DENT INFO AND LOCATION 7251-21-11-28-01A (EXTERNAL VISUAL AND UNDERLYING STRUCTURE 7251-21-11-28-01A (RE-FORM SKIN DENT TO ORIGINAL CONTOUR) AVO#7251-21-11-28-01A MATCH AND MEET CONDITIONS) NO DISCREPANCIES NOTED. INSP) NO DISCREPANCIES NOTED FABRICATED -1 REPAIR DOUBLER AND LOCATED PRODUCTION FASTENER PER PERFORMED HFEC INSPECTION OF REMOVED FASTENERS
Part: NONE — DAMAGED (MULTIPLE LOCATIO) · airframe 1,177 hrs · 436 cycles
AC 267 RIGHT WINGLET STRUCK UPPER SECTION OF RADOME, DAMAGE RUNS FROM 1OCLOCK TO 3OCLOCK 6 " FROM FUSELAGE PLUS DAMAGED 5 VORTEX GENERATORS ON CAPT SIDE, FO WINDSHIELD WIPER DAMAGED, R1 WINDOW SEAL SMALL DAMAGE TO RUBBER SEAL LOWER LEFT CORNER AND MIDDLE OF SEAL ON RIGHT SIDE. DENT ON FUSELAGE AT 1OCLOCK CAPT SIDE FWD OF LOWER RIGHT L1 WINDOW. CREASE AT 2 OCLOCK CAPT SIDE 4 " FROM RADOME EDGE ALLOWABLE DMG 1 FIG 103 G DENT DEPTH CAN BE A MAX OF .125". DENTS ARE MEASURED AT .130" AND .175" RESPECTIVELY. LOCKING FOR MX FERRY TO MCO UNLOCKED FOR UPDATES ADDED PHOTO OF DMG. AS PER SRM 53-10-01 ID 1 NOSE SKIN .063" THICK SEE FIG 5 ID 1 FOR CHEM-MILLED AREA. NOSE SKIN PART# 141A3810. AS PER SRM 53-10-01 ALLOWABLE DMG 1 REFER TO SRM 53-00-01 FOR ALLOWABLE DMG IN THIS AREA. AS PER SRM 53-00-01
Part: STRUCTURE — DENTED (STA200) · airframe 1,177 hrs · 436 cycles
UPON INSPECTION OF REPAIR IN NOSE AREA STA.200 R/H SIDE JUST UNDER WINDSHIED. A DENT WAS FOUND ABOUT 3" O/B OF CUTOUT(MARKED). REF. LOGPAGE 7514449 & AVO#7251-21-11-28-01. DENT WIDTH IS 0.70", LENGTH 0.50" ,& (DEPTH Y = 0.005") W/Y= 140 VERIFIED DENT MEASUREMENTS AND MAP OUT FOR ENGINEERING. .REF TO SRM 53-00-01. SEE PHOTO MAPOUT FOR ENGINEERING DISPOSITION. DAMAGE REPAIRED ON L/P 7515674 SEE LOG PAGE FOR ALL WORK ACCOMPLISHED VERIFIED DAMAGE REPAIRED ON L/P 7514449. INCORRECT L/P MENTIONED ON PREVIOUS UPDATE, DAMAGE REPAIRED ON L/P 7514449, SEE L/P FOR WORK ACCOMPLISHED