N7705A
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.
58 reports on file, 2014-08-07 – 2019-08-13.
Part: SUPPORT — LOOSE (L1 GIRT BAR) · airframe 49,231 hrs · 24,011 cycles
L1 DOOR SLIDE GIRT BAR SUPPORT CLIP LOOSE. SECURED SUPPORT CLIP PER SRM.
Earlier reports · 2014–2018 · 57 reports
2018
Part: LIGHT — LOOSE (CABIN) · airframe 46,805 hrs · 22,532 cycles
EMERGENCY PATH LIGHT LOOSE NEAR ROW 8. R&R STRIP IAW AMM.
Part: RETAINER — BENT (L1 DOOR) · airframe 46,579 hrs · 22,389 cycles
L1 DOOR SLIDE GIRT BAR RETAINER BRACKET BENT. SECURED RETAINER PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,045 hrs · 22,057 cycles
FORWARD CABIN EGRESS LIGHT INOP. R&R BATTERY PACKS IAW AMM.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 46,045 hrs · 22,057 cycles
FORWARD CABIN EGRESS LIGHT INOP. R&R CHARGER IAW AMM.
Part: STRINGER — CRACKED (RT WING) · airframe 46,045 hrs · 22,057 cycles
RT WING INBOARD FIXED LEADING SKIN AFT STRINGER CRACKED AT OUTBOARD END JUST INBOARD OF PYLON. R&R STRINGER IAW DWG AND SRM.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 46,045 hrs · 22,057 cycles
SHEAR TIE CORRODED AT BS 360, STR 28L. R&R SHEAR TIE IAW SRM AND IAW EA.
Part: BEAM — CRACKED (R1 DOOR) · airframe 46,045 hrs · 22,057 cycles
R1 DOOR LOWER BEAM NR 4 HAS CRACKED IN RADIUS NEXT TO UPPER INBOARD BOLT HOLE. R&R NR 4 BEAM IAW DWG AND SRM.
Part: SKIN — CORRODED (FUSELAGE) · airframe 46,045 hrs · 22,057 cycles
LOWER EXTERNAL FUSELAGE SKIN CORRODED AT BS 1016, BETWEEN LBL 2 TO RBL 8. REPAIRED SKIN IAW SRM.
Part: SKIN — CORRODED (FUSELAGE) · airframe 46,045 hrs · 22,057 cycles
LOWER EXTERNAL FUSELAGE SKIN CORRODED BETWEEN BS 352 TO BS 358, BL 0. R&R SKIN IAW SRM AND EA.
Part: FLAP — DELAMINATED (RT WING) · airframe 45,100 hrs · 21,464 cycles
RT WING OUTBOARD AFT FLAP DELAMINATED ON THE INBOARD AFT CORNER ON THE TOP SIDE. R&R AFT FLAP PER AMM.
Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 45,100 hrs · 21,464 cycles
EMERGENCY EXIT LIGHTS BATTERY M1670 FAILED A CAPACITY TEST. R & R THE BATTERY PACK IAW MM.
Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 45,100 hrs · 21,464 cycles
EMERGENCY LIGHT BATTERY M1675 FAILED A CAPACITY TEST. R & R THE BATTERY IAW MM.
Part: BLADE — CRACKED (NR 1 ENG FAN) · airframe 45,100 hrs · 21,464 cycles
NR 1 ENGINE FAN BLADE NR 10 WAS FOUND CRACKED AT CONVEX SIDE. R & R THE FAN BLADE IAW MM.
2017
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,174 hrs · 20,325 cycles
RT LOWER OUTSIDE EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,174 hrs · 20,325 cycles
LT OVERWING EXIT OUTSIDE EMERGENCY LIGHT INOP. R&R BATTERY PACK PER MM.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 43,058 hrs · 20,255 cycles
RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. R&R LIGHT PER AMM.
Part: SLIDE — UNWANTED DEPLOY (R2 DOOR) · airframe 41,579 hrs · 19,433 cycles
R2 DOOR SLIDE DEPLOYED. R & R SLIDE IAW MT.
2016
Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 39,567 hrs · 18,272 cycles
AFT CARGO DOOR CUTOUT AFT CORNER SCUFF PLATE CRACKED. R & R SCUFF PLATE IAW AMM.
Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 39,567 hrs · 18,272 cycles
AFT CARGO DOOR CUTOUT FORWARD CORNER SCUFF PLATE CRACKED. R & R SCUFF PLATE IAW AMM.
Part: INTERCOSTAL — CORRODED (BS 747-767) · airframe 39,567 hrs · 18,272 cycles
RIGHT INTERCOSTAL CORRODED BETWEEN BS 747 - 767. R & R INTERCOSTAL IAW DWG AND SRM.
Part: STRAP — CORRODED (BS 1016) · airframe 39,567 hrs · 18,272 cycles
AFT WET AREA UPPER STRAP CORRODED BETWEEN BS 1016 TO 1016+ 14, LBL 3. R & R THE STRAP IAW SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,567 hrs · 18,272 cycles
SEAT TRACK CORRODED BETWEEN BS 727A-10 TO BS 727A-5, RBL 45. R & R SEAT TRACK IAW SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,567 hrs · 18,272 cycles
SEAT TRACK CORRODED BETWEEN BS 727E TO BS 727E+2, LBL 24. R & R SEAT TRACK IAW SRM.
Part: LIGHT — BROKEN (GALLEY) · airframe 39,567 hrs · 18,272 cycles
G-1 GALLEY EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. R & R THE LIGHT ASSEMBLY IAW AMM.
Part: SEAT TRACK — CORRODED (BS 727) · airframe 39,567 hrs · 18,272 cycles
SEAT TRACK CORRODED AT BS 727+10, LBL 24. R & R THE SEAT TRACK IAW SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 39,567 hrs · 18,272 cycles
FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME IAW EA.
Part: ANGLE — CRACKED (BS 787) · airframe 39,567 hrs · 18,272 cycles
AFT CARGO BAY RT FLOOR ZEE ANGLE CRACKED AT BS 787. R & R THE ZEE ANGLE IAW SRM.
Part: FRAME — CRACKED (BS 480) · airframe 39,567 hrs · 18,272 cycles
FRAME CRACKED AT BS 480, STRINGER 8R. REPAIRED THE FRAME IAW EA.
Part: GUSSET — CRACKED (BS 500D) · airframe 39,567 hrs · 18,272 cycles
FORWARD CARGO BAY GUSSET CRACKED AT BS 500D, STRINGER 19L. R & R THE GUSSET IAW DWG AND SRM.
Part: FRAME — CRACKED (BS 440) · airframe 39,567 hrs · 18,272 cycles
FRAME CRACKED AT BS 440, STRINGER 8R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 39,567 hrs · 18,272 cycles
FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (BS 500C) · airframe 39,567 hrs · 18,272 cycles
FRAME CRACKED AT BS 500C, STRINGER 8R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 39,567 hrs · 18,272 cycles
FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 39,567 hrs · 18,272 cycles
FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (BS 827) · airframe 39,567 hrs · 18,272 cycles
FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED THE FRAME IAW EA.
Part: FRAME — CRACKED (BS 727D) · airframe 39,567 hrs · 18,272 cycles
FRAME CRACKED AT BS 727D, STRINGER 8R. REPAIRED THE FRAME IAW EA.
Part: LENS — BROKEN (CABIN) · airframe 39,567 hrs · 18,272 cycles
FORWARD LAV, EMERGENCY EXIT LENS ON AFT SIDE OF LAV BROKEN. R & R LENS IAW AMM.
Part: RIVET — MISSING (FUSELAGE) · airframe 39,567 hrs · 18,272 cycles
PASSENGERS CABIN FLOOR STRUCTURE INNER CREASE BEAM CHORD VERTICAL FLANGE CLIP MISSING AT BS 639, STR 17R. INSTALLED RIVET IAW DWG AND SRM.
Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 39,567 hrs · 18,272 cycles
RIGHT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 25. REPAIRED WEB IAW SRM.
2015
Part: SKIN — CRACKED (LE SLAT) · airframe 35,325 hrs · 15,922 cycles
RIGHT WING NR 7 SLAT SKIN CRACKED ON LOWER SURFACE. REPAIRED SKIN IAW EA.
2014
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 32,939 hrs · 14,579 cycles
CREASE BEAM CORRODED AT BS 623 LBL 65. REPAIRED BEAM IAW ER & EA.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 32,939 hrs · 14,579 cycles
CREASE BEAM INNER CHORD CORRODED AT BS 643 RBL 65. REPAIRED CHORD IAW SRM & EA.
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 32,939 hrs · 14,579 cycles
RIGHT HORIZONTAL STABILIZER RIB AT STAB STATION 129.5, 3RD STIFFENER FROM FRONT SPAR CRACKED ON LOWER END. REPAIRED RIB IAW SRM.
Part: INSERT — BROKEN (FLOOR PANEL) · airframe 32,939 hrs · 14,579 cycles
FORWARD PAX CABIN FLOOR PANEL 221DF INSERT BROKEN. REPAIRED PANEL IAW SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 32,939 hrs · 14,579 cycles
FLOORBEAM UPPER CHORD CORRODED AT BS 328 BETWEEN RBL 11 TO RBL 57. REPAIRED CHORD IAW SRM.
Part: INSERT — BROKEN (FLOOR PANEL) · airframe 32,939 hrs · 14,579 cycles
AFT PAX CABIN FLOOR PANEL 241C INSERT BROKEN. REPAIRED PANEL IAW SRM.
Part: FLOOR PANEL — BROKEN (CABIN) · airframe 32,939 hrs · 14,579 cycles
FORWARD PAX CABIN FLOOR PANEL 221BF AFT OTBD CORNER BROKEN. REPAIRED PANEL IAW SRM.
Part: INSERT — BROKEN (FLOOR PANEL) · airframe 32,939 hrs · 14,579 cycles
FORWARD PAX CABIN FLOOR PANEL 221EF INSERT BROKEN. REPAIRED PANEL IAW SRM.
Part: FLOOR PANEL — BROKEN (CABIN) · airframe 32,939 hrs · 14,579 cycles
FORWARD PAX CABIN FLOOR PANEL 222BF INSERT BROKEN. REPAIRED PANEL IAW SRM.
Part: INSERT — BROKEN (FLOOR PANEL) · airframe 32,939 hrs · 14,579 cycles
AFT PAX CABIN FLOOR PANEL 241AEF INSERT BROKEN. REPAIRED PANEL IAW SRM.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 32,939 hrs · 14,579 cycles
LONGITUDINAL FLOORBEAM CHORD CRACKED AT BS 727B RBL 24.75. REPAIRED CHORD IAW ER & EA.
Part: BRACKET — CRACKED (L1 DOOR) · airframe 32,939 hrs · 14,579 cycles
L1 DOOR HOOK BRACKET AT FWD END UPPER HINGE CUT OUT FLAPPER HINGE SEAL CRACKED. R & R BRACKET IAW SRM.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,939 hrs · 14,579 cycles
FORWARD CARGO BULKHEAD CHORD CRACKED AT BS 540 STRINGER 22L. REPAIRED CHORD IAW EA.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,939 hrs · 14,579 cycles
FORWARD CARGO BULKHEAD CHORD CRACKED AT BS 540 STRINGER 22R. REPAIRED CHORD IAW EA.
Part: STRAP — CORRODED (FUSELAGE) · airframe 32,939 hrs · 14,579 cycles
FLOOR SHEAR WEB REINFORCEMENT STRAP CORRODED BETWEEN BS 1006 TO 1029 RBL 3. R & R STRAP IAW SRM & DWG.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,939 hrs · 14,579 cycles
LEFT OVERWING EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,939 hrs · 14,579 cycles
RIGHT OVERWING EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.