N940FR
Registered owner: DIAMOND RIM HOLDINGS LLC, AZ (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.
39 reports on file, 2006-12-10 – 2012-08-27.
Part: SKIN — DENTED (ZONE 400) · airframe 814,001 hrs
NR 1 ENGINE NOSE COWL INNER BARREL AT 9:30 POSITION HAS A DENT. REPAIRED IAW SRM 54-10-00, REPAIR 23, PARAGRAPH 2.A,B,C(1-3}, D, E(1 -2), F{1 -2), G AND H( 1-4).
Part: SKIN — DENTED (ZONE 400) · airframe 814,001 hrs
NR 1 ENGINE NOSE COWL INNER BARREL AT 9:00 POSITION HAS A DENT, REPAIRED IAW SRM 54-10-00, REPAIR 23, PARAGRAPH 2.A,B,C(1 -3), D, E(1 -2), F( 1-2), G AND H( 1-4).
Part: VALVE — INOPERATIVE (BRAKE SYSTEM) · airframe 24,801 hrs · 11,902 cycles
LEFT BRAKE PRESSURE INDICATION SHOWS ZERO PSI. R & R ALTERNATE BRAKE DIRECT DRIVE VALVE. OPS CHECK NORMAL REF AMM 32-43-35 PAGE BLOCK 401. TORQUE WRENCH F9TAB2197C CALIBRATION DUE 01/13. MEL CLEARED.
Part: EPSU — FAILED (EMERGENCY LIGHTS) · airframe 24,307 hrs · 11,638 cycles
CIDS 1 EPSU SYS TEST FAILS EPSU (10WL) FWD L/ DEU B (300RH1), R & R FAP DUE TO FAP NOT ACCEPTING CAM WRT AMM 23-73-12 PB 401. FAP LAYOUT SELECTION NOT CONFIGURED FOR CURRENT CABIN LAYOUT-CONT T/S. REINSTALLED ORIGINAL FAP IAW AMM 23-73-12 PB401 CLEANED AND TESTED EPSU FWD LT 10WL OPS TESTED GOOD IAW AMM 33-51-00-710-A.
Earlier reports · 2006–2011 · 35 reports
2011
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 23,465 hrs · 11,250 cycles
EMERGENCY EXIT LIGHTS AND ESCAPE PATH LIGHTS REMAINED ON DURING FLIGHT WITH SWITCH IN "NORM" POSITION- AND FAP AMBER NOTE "CHECK PAX RELATED FUNCTIONS" TROUBLESHOT REF TSM 33-51-00-810-881. CHECKED EPSU BATTERIES FOR CONDITION AND SECURITY. OPS TEST NORMAL IAW AMM 33-57, 00-710-004. NO PARTS WHERE CHANGED.
Part: RELAY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,991 hrs · 11,020 cycles
EMERGENCY EXIT LIGHTS FLICKERING ON TAKEOFF ROLL. R & R RELAY (8WL) REF ASM 33-51-00. OPS TEST OF THE EMERGENCY LIGHTS TEST GOOD REF AMM 33-51-00-710-001.
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 26,435 hrs · 10,953 cycles
PATHWAY EMERGENCY LIGHTS ON & OFF INTERMITTENTLY, EMERGENCY EXIT LIGHT ACFT LT OVERWING EXIT ON THROUGHOUT NIGHT. R & R EPSU EMERGENCY POWER SUPPLY UNIT 11WL WITH SERVICEABLE PART IAW AMM 33-51-38 PB 401, OPS CHECK GOOD.
2010
Part: BLANKING PLATE — CORRODED (ZONE 200) · airframe 17,064 hrs · 8,244 cycles
DURING C3 C-CHECK INSP NOTED L2 DOOR AFT GIRT BAR BLANKING PLATE CORRODED. MX INSTALLED NEW L2 DOOR AFT GIRT BAR BLANKING PLATE IAW AMM 52-13-31-400-007.
Part: BLANKING PLATE — CORRODED (ZONE 200) · airframe 17,064 hrs · 8,244 cycles
DURING C3 C-CHECK INSP NOTED R2 DOOR AFT GIRT BAR BLANKING PLATE CORRODED. MX INSTALLED NEW R2 DOOR AFT GIRT BAR BLANKING PLATE IAW AMM 52-13-31-400-007.
Part: BLANKING PLATE — CORRODED (ZONE 200) · airframe 17,064 hrs · 8,244 cycles
DURING C3 C-CHECK INSP NOTED L2 DOOR FWD GIRT BAR BLANKING PLATE CORRODED. MX INSTALLED NEW L2 DOOR FWD GIRT BAR BLANKING PLATE IAW AMM 52-13-31-400-007.
Part: BLANKING PLATE — CORRODED (ZONE 200) · airframe 17,064 hrs · 8,244 cycles
DURING C3 C-CHECK INSP NOTED R2 DOOR FWD GIRT BAR BLANKING PLATE CORRODED. MX INSTALLED NEW R2 DOOR FWD GIRT BAR BLANKING PLATE IAW AMM 52-13-31-400-007.
Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 17,064 hrs · 8,244 cycles
DURING C3 C-CHECK INSP NOTED FLOOR PANEL 261EF TOP GLASS LAYER IS DELAMINATED AFT LT SIDE. MX REPAIRED FLOOR PANEL IAW EA A9-53R-31605.
2009
Part: PLATE — CORRODED (ZONE 100) · airframe 17,064 hrs · 8,244 cycles
DURING C-3 C-CHECK INSP NOTED LT AFT SHEAR PLATE IS CORRODED ON NUT PLATE HOLES. MX REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11, SRM 51-21-11, SRM 51-44-11, SRM 51-75-12 AND EO A0-53EO-31434.
Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 17,064 hrs · 8,244 cycles
DURING C3 C CHECK INSP NOTED AFT R2 DOOR THRESHOLD AREA FLOOR PANEL 262FF HAS CORROSION AROUND ATTACHMENT HOLES AND TOP SURFACE. MX REPLACED PANEL 262FF IAW ROUTINE TASK CARD C534103-2.
Part: PLATE — CORRODED (R2 DOOR SILL) · airframe 17,064 hrs · 8,244 cycles
DURING C3 C-CHECK INSP NOTED R2 DOOR SILL PLATE INBD FASTENER HOLE FWD OF FRAME 68 IS CORRODED. MX REPAIRED FASTENER HOLE IAW SRM 53-41-14 FIGURE 201 REPAIR PRINCIPLE NR 5.
Part: SKIN — GOUGED (ZONE 200) · airframe 17,064 hrs · 8,244 cycles
DURING C3 C-CHECK INSP, NOTED SKIN GOUGED IN 3 SPOTS BETWEEN FRAME 52 AND FRAME 51 BETWEEN STRINGER 1 RT AND STRINGER 2 RT. MX REPAIRED FUSELAGE SKIN IAW SRM 53-00-11, FIG 204.
Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 17,064 hrs · 8,244 cycles
DURING C3 C-CHECK INSP NOTED FLOOR SUPPORT Y1292 FRAME 68 TO FRAME 69 OTBD FASTENER HOLE AT FRAME 68 CORRODED. MX REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-74-00, SRM 53-00-14, SRM 51-42-11, SRM 51-44-11 AND SRM 51-75-12.
Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 17,064 hrs · 8,244 cycles
DURING C3 C-CHECK INSP NOTED FLOORBEAM CORRODED AFT CABIN AT FRAME 67 Y1295. MX REMOVED AND REPLACED FLOORBEAM IAW SRM 51-74-00, SRM 53-00-14, SRM 51-42-11, SRM 51-44-11 AND SRM 51-75-12.
Part: PLATE — CORRODED (ZONE 100) · airframe 17,064 hrs · 8,244 cycles
DURING C-3 C-CHECK INSP, NOTED THE SHEAR PLATE CORRODED RT SIDE AFT CABIN UNDER GALLEY AT FRAME 70 Y1162. MX REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11 AND EO A0-53EO-31434.
Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 17,064 hrs · 8,244 cycles
DURING C3 C-CHECK INSP, NOTED FLOORBEAM CORRODED AFT CABIN AT FRAME 67 Y1295. MX REMOVED AND REPLACED FLOORBEAM IAW SRM 51-74-00, SRM 53-00-14, SRM 51-42-11, SRM 51-44-11 AND SRM 51-75-12.
Part: LINE — CHAFED (HYD SYSTEM) · airframe 16,019 hrs · 7,740 cycles
REFERENCE LOG PAGE 472314. CREW MADE AN AIR TURN BACK TO DEN DUE TO AN INDICATION FOR THE GREEN HYDRAULIC RESERVOIR LEVEL LOW. MAINTENANCE INSPECTED AND FOUND A GREEN HYDRAULIC SYSTEM PRESSURE PIPE WITH CHAFING DAMAGE AND A PIN HOLE. MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC PRESSURE LINE IAW AMM 29-11-49 PB 401 AND PERFORMED SATISFACTORY LEAK CHECK.
Part: SEAL — DISPLACED (FUEL SYSTEM) · airframe 15,861 hrs · 7,679 cycles
FUEL TRANSFERRED TO RT WING TANK DURING CTR PUMP OPERATION. MX FOUND SEAL FROM AFT FUEL SURGE ACCESS PANEL HAD MIGRATED INTO THE RT WING FUEL PUMP SUCTION VALVE. MX REPLACED THE PUMP SUCTION VALVE (PN D2825006400200)AND FUEL SURGE VALVE SEAL (PN 5725054220000) AND PERFORMED OPS AND LEAK CHECK IAW AMM 28-21-42-000-001.
Part: HOSE — LEAKING (BLEED PRESSURE) · airframe 15,513 hrs · 7,514 cycles
REF LOG PAGES 475705 AND 475708. DURING CLIMB OUT, PILOTS RECEIVED A WARNING FOR "AIR ENGINE 1 AND 2 BLEED FAULT" AND MADE AN AIR RETURN TO DEPARTURE. MX REMOVED AND REPLACED THE PRESSURE SENSE LINE AND PERFORMED OPS CHECK.
2008
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 11,767 hrs · 5,748 cycles
DURING C-CHECK INSP NOTED AFT PIT PANEL 152UG DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 11,767 hrs · 5,748 cycles
DURING C-CHECK INSP NOTED AFT PIT PANEL 151PE DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 11,767 hrs · 5,748 cycles
DURING C-CHECK INSP NOTED AFT PIT PANEL 151FE DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
Part: PANEL — DAMAGED (FUSELAGE) · airframe 11,767 hrs · 5,748 cycles
DURING C-CHECK INSP NOTED AFT PIT PANEL 151DE DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 11,767 hrs · 5,748 cycles
DURING C-CHECK INSP NOTED FWD PIT PANEL 131EG DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
Part: PANEL — DAMAGED (CARGO BAY) · airframe 11,767 hrs · 5,748 cycles
DURING C-CHECK INSP NOTED AFT PIT TRANSITION PANEL 151GE DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 11,767 hrs · 5,748 cycles
DURING C-CHECK INSP NOTED AFT PIT TRANSITION PANEL 151HE DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 11,767 hrs · 5,748 cycles
DURING C-CHECK INSP NOTED FWD PIT FLOOR PANEL 131CG DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 11,767 hrs · 5,748 cycles
DURING C-CHECK INSP NOTED AFT PIT FLOOR PANEL 151CE DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 11,767 hrs · 5,748 cycles
DURING C-CHECK INSP AFT PIT PANEL 161BF DAMAGED. MIANT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 11,767 hrs · 5,748 cycles
DURING C-CHECK INSP, NOTED AFT PIT PANEL 161CF DAMAGED. MAINT REMOVED DAMAGE AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 11,767 hrs · 5,748 cycles
DURING C-CHECK INSP NOTED AFT PIT PANEL 152WG DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 11,767 hrs · 5,748 cycles
DURING C-CHECK INSP, NOTED AFT PIT PANEL 162EF DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
Part: PANEL — DAMAGED (FUSELAGE) · airframe 11,767 hrs · 5,748 cycles
DURING C-CHECK INSP, NOTED AFT PIT PANEL 161NF DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)
Part: EPSU — INOPERATIVE (ZONE 200) · airframe 9,912 hrs · 4,851 cycles
DURING PERFORMANCE OF EPSU (12WL) FUNCTIONAL TEST, THE MECHANIC NOTED A POWER SUPPLY FAULT ON THE MDCU. THE EPSU WAS REPLACED, IAW AMM 33-51-38 PB 401 AND OPERATIONS CHECKED OKAY. PART TOTAL TIMES AND TOTAL CYCLES WILL BE PROVIDED AT A LATER DATE. REFERENCE LOG BOOK PAGE 308363, HOURS AND CYCLES FOR THE PART HAVE BEEN ADDED 01/11/08.
2006
Part: RIB — FAILED (PYLON) · airframe 5,775 hrs · 2,836 cycles
DURING C-1 CHECK, INSPECTION REPORTED RT PYLON RIB 9 FAILED HEAT TREATMENT TEST. READINGS BELOW 200. ACCOMPLISHED MODIFICATION (INSTALLATION OF RIB REINFORCEMENT KIT) PER EA A9-54R-11704.