N706DN
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.
18 reports on file, 2009-11-25 – 2019-06-11.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 49,400 hrs · 4,474 cycles
OVERHEAD EMERGENCY EXIT LIGHTS AT ROWS 50 AND 52 ON RH INOP. R & R EMERGENCY LIGHT POWER SUPPLY & BATTERY PACK M33409. OPS CK GOOD. OK FOR SVC. WORK ACCOMPLISHED IAW AMM 33-51.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 48,617 hrs · 4,402 cycles
GALLEY R4 OVERHEAD EXIT SIGN LENS IS MISSING. REPLACED GALLEY R4 EXIT LENS. LP 5532402
Part: BRACKET — BROKEN (T/R CROSS TIE) · airframe 48,446 hrs · 4,389 cycles
(AIRCRAFT 7106, L/P 1013189) ON NUMBER 1 ENGINE CHANGE FOUND THE THRUST REVERSER CROSS TIE ASSY. BRACKET BROKEN AND STOPS CRACKED. REPLACED CROSSTIE BRACKETS AND STOPS ON NUMBER 1 ENGINE.
Part: BATTERY — DISCHARGED (R4 DOOR) · airframe 48,295 hrs · 4,374 cycles
DOOR 4R EPAS GREEN LIGHT INOPERATIVE. REPLACED EPAS 9 VOLT BACK UP BATTERY. LP 4982731
Earlier reports · 2009–2018 · 14 reports
2018
Part: FRAME — CRACKED (LT PYLON) · airframe 47,647 hrs · 4,297 cycles
LT PYLON AFT FAIRING O/B AREA FRAME AFT OF PANEL 434BL FOUND CRACKED AS MARKED. LT PYLON AFT FAIRING O/B AREA NR 5 FRAME CARRIED OUT REPAIR AS PER PRI ER/A 572027-14 REV 0 AND REV 1. AWAITING FOR FINAL ER/A. COMPARED WITH PRI ER/A 572027-14 REV 0 AND REV 1, FINAL ER/A 572027-14AD SECT I. REV. ORIGINAL FOUND IN COMPLIANCE.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 47,631 hrs · 4,295 cycles
(AIRCRAFT 7106, L/P 0776316) MTC TASK - STA 424 TO STA 445 , S-46L TO S-47L , LWR FX SKIN AREA FOUND WITH TWO ADJACENT BLEND-OUTS. EXISTING BLEND-OUTS AT THE NOTED LOCATION EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-01-1A-1, ALLOWABLE DAMAGE 1, FIG 102 REV 77. ORIGINAL SKIN THK=0.070", MATERIAL REMOVED=0.047" AND REMAINING SKIN THK=0.023". DAMAGED AREA TRIMMED OUT AND EXTERNAL DOUBLER REPAIR CARRIED OUT AS PER SRM 53-00-01, REPAIR 7, FIG 202. REPAIR EMBODIMENT AT AIRCRAFT TOTAL FLIGHT CYCLES OF 4295 AND TOTAL FLIGHT HOURS OF 47631.37. THIS REPAIR IS A CATEGORY "B" REPAIR AND REQUIRED REPEAT INSPECTION PER SRM 53-00-01, REPAIR 7, TABLE 204. WITH ZERO-TIMED NOT CARRIED OPUT ON INITIAL FASTENER HOLES AT CRITICAL ROW, INSPECTION THRESHOLD AT 30,000 TOTAL FLIGHT CYCLES FROM THE TIME AIRPLANE WAS DELIVERED OR 16,000 FLIGHT CYCLES FROM THE TIME REPAIR INSTALLED, WHICHEVER COMES LATER. METHOD:HFEC AND DETAILED VISUAL.INTERVAL:16,000 FLIGHT CYCLES. IDENTIFIED REPAIR WITH LOG PAGE NUMBER PER PS:900-5-1 , NO.4.
2017
Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 42,729 hrs · 3,885 cycles
EMERGENCY LIGHT LENS IS DAMAGED. REPLACED THE LENS COVER . OPS CHECKED GOOD, OK FOR SERVICE.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 42,565 hrs · 3,871 cycles
EMERGENCY LIGHT BATTERY PACKS M33404 AND M33409 FAILED FUNCTIONAL CAPACITY CHECK IAW W/C 0591-1204. R & R THE BATTERY PACKS IAW AMM 33-51.
Part: BULB — MISSING (EMERGENCY LIGHT) · airframe 42,339 hrs · 3,852 cycles
SEAT 11B MISSING EMERGENCY PROXIMITY LENS AND BULBS. REPLACED BULBS AND LENS.
Part: LENS — UNSECURE (EMERGENCY LIGHTS) · airframe 40,636 hrs · 3,700 cycles
EMERGENCY LIGHT LENS LOOSE. SECURED THE LENS.
Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 40,636 hrs · 3,700 cycles
EMERGENCY LIGHT LENS LOOSE. SECURED THE LENS.
Part: LENS — DAMAGED (EMERGENCY LIGHTS) · airframe 39,896 hrs · 3,631 cycles
EMERGENCY LIGHT LENS DAMAGED. REPLACED THE LENS.
Part: LENS — DAMAGED (EMERGENCY LIGHTS) · airframe 39,896 hrs · 3,631 cycles
EMERGENCY LIGHT LENS DAMAGED. REPLACED THE LENS.
2016
Part: BEARING — MIGRATED (TE FLAP) · airframe 38,510 hrs · 3,504 cycles
LT WING NR 2 FLAP TRACK AFT DRIVE FITTING BEARING MIGRATION. MIGRATION BEARING AT LT WING NR 2 FLAP TRACK AFT FAIRING AFT DRIVE FITTING REMOVED AS PER BSOPM 20-50-03 REV 107 IAW CMM 57-26-60 REPAIR 9-1 REV 23 HOLE MEASURED DIA. 1.1898" ALLOWABLE HOLE DIA. 1.1875" - DIA. 1.1885". OVERSIZED HOLE REWORKED AND FOUND WITHIN LIMIT AS PER CMM 57-26-60 REPAIR 9-2 REV 23. EXISTING HOLE DIA. 1.1898" , FINAL HOLE DIA. 1.248", MAXIMUM ALLOWABLE DIA. 1.2485". REPAIR SLEEVES BUSHING 02 EA FABRICATED BY MACHINING AND INSTALLED AS PER BSOPM 20-50-03 REV 107 IAW CMM 57-26-60 REPAIR 9-2 REV 23. NEW BEARING INSTALLED AS PER BSOPM 20-50-03 REV 107 IAW CMM 57-26-60 REPAIR 9-1 REV 23. LT WING NR 2 FLAP TRACK AFT FAIRING AFT DRIVE FITTING REMOVED AND REINSTALLED AS PER AMM 27-51-22.
Part: FLAP TRACK — CORRODED (RT WING TE FLAP) · airframe 38,223 hrs · 3,477 cycles
RIGHT INBD MAIN FLAP OUTBD TRACK SUPPORT FITTING BORE CORROSION FOUND. CORROSION CAN NOT BE REMOVED AT MAX DIAMETER FOR FITTING REPLACEMENT.
2012
Part: BATTERY PACK — INOPERATIVE (R3 DOOR SLIDE) · airframe 18,764 hrs · 1,691 cycles
R3 DOOR EPAS BATTERY STATUS LIGHT IS INOPERATIVE, NOT FLASHING GREEN WITH DOOR ARMED. REPLACED R3 DOOR EPAS BATTERY PACK. OPS CHECKED GOOD IAW AMM.
2009
Part: ENGINE — FAILED (NR1) · airframe 2,881 hrs · 253 cycles
NR 1 ENG FAILED BORO INSP/C NBR 1 ENG REPLACED. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.
Part: LINE — CRACKED (NR 1 ENGINE) · airframe 2,693 hrs · 238 cycles
ON ARRIVAL FLT CREW REPORTED A FUEL IMBALANCE DURING FLIGHT. MTC NOTICED FUEL LEAKAGE FROM NR 1 ENG. FOUND THE VSV MUSCLE SUPPLY LINE CRACKED IN THE FLEXIBLE PORTION ON THE RT UPPER AREA WHERE IT PLUGS INTO THE RT 2.5 BLEED VLV. REMOVED LINE AWAITING SAME FROM ATL. INSTALLED REPLACEMENT LINE, NEED ENG RUN FOR LEAK CHECK. PERFORMED TEST 5 ENGINE IDLE LEAK CHECK AND TEST 14 FUEL ACTUATOR TEST - ALL TEST PASSED. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.