N7714B
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.
86 reports on file, 2012-04-15 – 2019-09-06.
Part: GIRT BAR — DISPLACED (L1 DOOR) · airframe 51,955 hrs · 27,172 cycles
L1 DOOR SLIDE GIRT BAR DISPLACED. REPOSITIONED GIRT BAR AND SLIDE PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,954 hrs · 27,171 cycles
FORWARD RECESSED LIGHT, EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,954 hrs · 27,171 cycles
L2 DOOR LOWER EXIT LIGHT BULB INOP. RELAMPED LIGHT PER AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,954 hrs · 27,171 cycles
RT OVERWING FORWARD EXIT LIGHT BULB INOP. RELAMPED LIGHT PER AMM.
Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 51,954 hrs · 27,171 cycles
EMERGENCY EXIT LIGHT IN COCKPIT INOP. RELAMPED EMERGENCY EXIT LIGHT PER AMM.
Part: SHIELD — CORRODED (FUSELAGE) · airframe 51,954 hrs · 27,171 cycles
AFT CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS. 847 TO BS. 867, RBL 22. R&R SHIELD IAW SRM & DWG.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 51,954 hrs · 27,171 cycles
AFT CARGO BAY CARGO TRACK CORRODED BETWEEN BS. 787 TO BS. 867, RBL 13. R&R AFT CARGO BAY TRACK IAW SRM AND DWG.
Part: SPLICE — CORRODED (FUSELAGE) · airframe 51,954 hrs · 27,171 cycles
BULKHEAD FORWARD SIDE OF Y-CHORD CORRODED ON LOWER SIDE AT BS. 1016, LBL 1. R&R SPLICE IAW SRM AND DWG.
Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 51,954 hrs · 27,171 cycles
AFT CARGO BAY SUB WEB THRESHOLD UPPER SURFACE BETWEEN BS 800 TO BS 840, RBL 26. R&R SUB THRESHOLD IAW SRM & DWG.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 51,954 hrs · 27,171 cycles
AFT CARGO BAY ON LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 847, LBL 22. R&R SUPPORT IAW SRM AND DWG.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 51,954 hrs · 27,171 cycles
FORWARD CARGO BAY CORRODED FLOOR TO SIDEWALL SUPPORT BETWEEN BS. 420 TO BS. 500D, LBL 23. R&R SUPPORT ANGLE IAW SRM.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 51,954 hrs · 27,171 cycles
FORWARD CARGO BAY AFT BULKHEAD PANEL SUPPORT LOWER ANGLE CORRODED AT BS. 500D, BETWEEN RBL 21 TO LBL 21. REPAIRED ANGLE PER SRM & DWG.
Part: SHIELD — CORRODED (BS 420-440) · airframe 51,954 hrs · 27,171 cycles
FORWARD CARGO BAY SIDEWALL SHIELD CORRODED BETWEEN BS. 420 TO BS. 440, RBL 24. / R&R SHIELD IAW SRM AND DWG.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 51,954 hrs · 27,171 cycles
AFT CARGO BAY ON RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO BS. 767, RBL 22. R&R SUPPORT ANGLE IAW SRM AND DWG.
Part: ATTACH ANGLE — CRACKED (BS 500C) · airframe 51,954 hrs · 27,171 cycles
FORWARD CARGO BAY INTERCOSTAL ATTACH ANGLE CRACKED AT BS. 500C, FORWARD SIDE LBL 24. R & R THE ATTACH ANGLE IAW SRM & DWG.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 51,954 hrs · 27,171 cycles
FORWARD CARGO BAY INTERCOSTAL ATTACH ANGLE CRACKED AT BS. 500B, FORWARD SIDE LBL 24. R&R ANGLE IAW SRM & DWG.
Part: GUSSET — CRACKED (BS 500D) · airframe 51,954 hrs · 27,171 cycles
FORWARD CARGO BAY AFT BULKHEAD SUPPORT GUSSET CRACKED AT BS. 500D, STR. 19R. R&R GUSSET IAW SRM AND DWG.
Part: GUSSET — CRACKED (FUSELAGE) · airframe 51,954 hrs · 27,171 cycles
FORWARD CARGO BAY AFT BULKHEAD SUPPORT GUSSET CRACKED AT BS. 500D, STR. 19L. R&R GUSSET IAW SRM & DWG.
Part: BEAM — CRACKED (R1 DOOR) · airframe 51,954 hrs · 27,171 cycles
R1 DOOR #4 (LOWER) BEAM CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. / REPAIRED #4 (LOWER) BEAM PER WO.
Part: CREASE BEAM — CRACKED (BS 639-685) · airframe 51,954 hrs · 27,171 cycles
R/H CREASE BEAM INNER CHORD CRACKED AT FASTENER HOLE BETWEEN BS. 639 TO BS. 685, RBL 64. R&R CHORD PER SRM & DWG.
Part: FLOORBEAM — CRACKED (BS 540) · airframe 51,954 hrs · 27,171 cycles
FLOOR SUPPORT CRACKED AT BS. 540, BETWEEN RBL 0 TO RBL 1. R&R FLOOR SUPPORT PER SRM.
Part: FLAP — DELAMINATED (L/H WING) · airframe 53,316 hrs · 27,814 cycles
TRANSFERRED FROM LOGBOOK MX NOTE DEFECT NO 1026619 DTE 03302019 DEFERRED BY MDEF MDDR/TRACKING NO 48877 DEFECT: FOUND L/H WING O/B AFT FLAP INBD TRAILING EDGE DELAMINATE D. LOGBOOK ENTRY REQUIRED / PERMANENTLY REPAIRED DELAMINATION ON L/H WING O/B AFT FLAP INBD TRAILING EDGE PER SRM 57-53-01-2R-4 AND SRM 51-70-10-2R-4 56518C 4/2/19 INSP373 3APR19 LOGBOOK MEL CLEARING # 49887
Part: CLAMP — LOOSE (L1 DOOR) · airframe 49,964 hrs · 25,896 cycles
L1 DOOR GIRT BAR FITTINGS LOOSE. ADJUSTED MOUNT CLAMPS PER SIP.
Earlier reports · 2012–2018 · 63 reports
2018
Part: SLIDE — UNSECURE (L1 DOOR) · airframe 49,801 hrs · 25,787 cycles
L1 DOOR SLIDE FELL OUT INADVERTENTLY, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER MT.
Part: FAN — FAULTY (CABIN) · airframe 48,763 hrs · 25,130 cycles
AIR TURNBACK, DURING CLIMB THROUGH 5000FT. STRONG ELECTRICAL ODOR IN COCKPIT REMAINED THRU LANDING. R&R RECIRC FAN PER MM.
Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 47,572 hrs · 24,360 cycles
L1 DOOR EVAC SLIDE FAILED INSPECTION. R&R SLIDE PER MT.
Part: FITTING — LOOSE (R1 DOOR) · airframe 47,563 hrs · 24,355 cycles
R1 DOOR FORWARD GIRT BAR FLOOR FITTING LOOSE. SECURED FITTING IAW AMM.
2017
Part: BRACKET — OUT OF ADJUST (R1 DOOR GIRT BAR) · airframe 46,195 hrs · 23,489 cycles
R1 DOOR SLIDE GRIT BAR OUT OF ADJUST. ADJUSTED THE GIRT BAR BRACKETS IAW SIP.
Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 45,872 hrs · 23,283 cycles
L2 DOOR EMERGENCY ESCAPE SLIDE GAUGE PRESSURE LOW. R&R SLIDE PER MT.
Part: HOOK — LOOSE (L1 DOOR) · airframe 45,337 hrs · 22,936 cycles
L1 DOOR EMERGENCY EVAC SLIDE THE GIRT BAR RETAINING J HOOK LOOSE. SECURED J HOOK PER SRM AND MT.
Part: SENSOR — FAULTY (TE FLAP) · airframe 43,894 hrs · 22,082 cycles
DECLARED EMERGENCY, FLAPS WOULD NOT EXTEND. ON ALTERNATE FLAP EXTENSION, FLAP ASYMMETRY RESULTED IN A FLAPS LESS THAN 1 LANDING. R&R NR 8 FLAP SKEW SENSOR IAW AMM.
2016
Part: LENS — LOOSE (CABIN) · airframe 42,144 hrs · 21,073 cycles
AFT GALLEY RT OVERHEAD EXIT DOOR LENS LIGHT ASSEMBLY LOOSE. SECURED LIGHT ASSEMBLY IAW AMM.
Part: COVER — OUT OF ADJUST (CABIN) · airframe 42,144 hrs · 21,073 cycles
AFT EMERGENCY EXIT LIGHT BUTTON COVER SPRING OUT OF ADJUST. ADJUSTED COVER IAW AMM.
Part: BRACKET — LOOSE (R1 DOOR) · airframe 42,141 hrs · 21,071 cycles
R1 DOOR EMERGENCY EXIT SLIDE BAR RETAINING BRACKET LOOSE. SECURED BRACKET IAW MM SIP.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,848 hrs · 20,906 cycles
RIGHT AFT EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
FRAME CRACKED AT BS 907, STRINGER 8R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
FRAME CRACKED AT BS 907, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
FRAME CRACKED AT BS 480, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
RIGHT OTBD SEAT TRACK CORRODED, BETWEEN BS 837 - 887, RBL 45. R & R SEAT TRACK IAW SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
FRAME CRACKED AT BS 400, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
FRAME CRACKED AT BS 440, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
FRAME CRACKED AT BS 360, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
AFT CARGO STANCHION SUPPORT CLIP CRACKED AT BS 865, LBL 10. R & R CLIP IAW SRM & DWG.
Part: FRAME — CRACKED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
FRAME CRACKED AT BS 400, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
FRAME CRACKED AT BS 827, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
FRAME CRACKED AT BS 500C, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA & SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
FRAME CRACKED AT BS 440, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
FRAME CRACKED AT BS 727D, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
FRAME CRACKED AT BS 787, STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
CHORD CORRODED AT INTERCOSTAL BELOW AIR STAIR DOOR, BETWEEN BS 294.5 - 328, STRINGER 23L. REPAIRED CHORD IAW EA.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
CABIN FLOOR SUPPORT CORRODED AT BS 331, LBL 12. R & R SUPPORT IAW SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
INTERCOSTAL CRACKED BETWEEN BS 284 - 290, BL 0. R & R INTERCOSTAL IAW SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
INTERCOSTAL CRACKED AT BS 320, LBL 45. R & R INTERCOSTAL IAW SRM.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
INTERCOSTAL BELOW AIRSTAIR CORRODED, BETWEEN BS 312 - 328, STRINGER 23L. R & R INTERCOSTAL IAW SRM.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
FLOOR SUPPORT CORRODED BETWEEN BS 315 - 325, LBL 12. R & R SUPPORT IAW SRM.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
FORWARD ENTRY DOOR, LOWER INNER CHORD CORRODED, MOP SILL, NEAR LOWER AFT CORNER. R & R CHORD IAW DWG.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
AFT CARGO FLOOR SUPPORT CORRODED, BETWEEN BS 787 - 827, RBL 1. REPAIRED SUPPORT IAW EA.
Part: BRACKET — CRACKED (RT WING) · airframe 40,581 hrs · 20,178 cycles
RIGHT WING TE WAFFLE BRACKET CRACKED AT NR 2 ENG PYLON. R & R BRACKET IAW SRM.
Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
STRINGER CLIP CORRODED AT BS 887, STRINGER 22L. R & R CLIP IAW SRM & DWG.
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
STRINGER SPLICE CORRODED AT BS 887, STRINGER 22L. R & R SPLICE IAW SRM.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
AFT CARGO FLOOR TO SIDEWALL SUPPORT TRIM COVER ON THE LT SIDE CORRODED, BETWEEN BS 867 - 887. R & R SUPPORT IAW SRM & DWG.
Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 40,581 hrs · 20,178 cycles
FORWARD CARGO COMPARTMENT DOOR SUB THRESHOLD CORRODED, BETWEEN BS 440 - 592. R & R WEB IAW SRM & DWG.
2015
Part: LENS — DAMAGED (CABIN) · airframe 39,469 hrs · 19,543 cycles
FORWARD GALLEY RT EMER EXIT LENS DAMAGED. R & R LENS IAW SIP.
2014
Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,568 hrs · 16,172 cycles
LEFT OVERWING EMER LIGHT INOPERATIVE FWD OF SIDEWALL LIGHT. R & R LIGHT IAW AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,568 hrs · 16,172 cycles
RIGHT OVERWING EMER LIGHT INOPERATIVE AFT OF SIDEWALL LIGHT. R & R LIGHT IAW AMM.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,568 hrs · 16,172 cycles
LEFT EXTERNAL OVERWING EMER EXIT LIGHT INOPERATIVE. R & R LIGHT IAW MM.
Part: PANEL — DELAMINATED (RT WING) · airframe 33,568 hrs · 16,172 cycles
RIGHT WING PANEL 621MB CORNER DELAMINATED. REPAIRED PANEL IAW SRM.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 33,568 hrs · 16,172 cycles
SEAT TRACK OTBD FLANGE FWD INBD FLANGE AFT FASTENER HOLES CRACKED CHORD AT BS 727B, LBL 24.75. REPAIRED CHORD IAW ER & EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 33,568 hrs · 16,172 cycles
SEAT TRACK INBD FLANGE AFT FASTENER HOLE CHORD CRACKED AT BS 727B, RBL 45.5. REPAIRED CHORD IAW ER & EA.
Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 33,568 hrs · 16,172 cycles
LEFT WING TE COVE SEAL SUPPORT ANGLE CRACKED ABOVE NR 1 PYLON AFT TIP. R & R ANGLE IAW SRM.
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 33,568 hrs · 16,172 cycles
RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STATION 92.70 AT NR 1 & NR 3 VERTICAL STIFFENER. REPAIRED RIB IAW SRM.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 33,568 hrs · 16,172 cycles
CHORD ATTACH POINT STRINGER CRACKED AT BS 540, STRINGER 23L. REPAIRED STRINGER IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 33,568 hrs · 16,172 cycles
SEAT TRACK OTBD FLANGE FWD & AFT INBD FLANGE AFT FASTENER HOLES CRACKED AT BS 727B, LBL 45.5. REPAIRED CHORD IAW ER & EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 33,568 hrs · 16,172 cycles
FUSELAGE SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW ER & EA.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 33,568 hrs · 16,172 cycles
STRINGER CORRODED AT BS 537, STRINGER 23R. REPAIRED STRINGER IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 33,568 hrs · 16,172 cycles
SKIN CRACKED AT BS 540, BETWEEN STRINGER 22L TO STRINGER 23L. REPAIRED SKIN IAW ER & EA.
2013
Part: PLATE — CRACKED (LT WING) · airframe 31,327 hrs · 14,871 cycles
LT WING TE LOWER PANEL WIGGLE PLASTIC CRACKED AT ONE FASTENER LOCATION. R&R WIGGLE PLATE IAW SRM.
Part: COVER — LOOSE (ESCAPE ROPE) · airframe 29,813 hrs · 13,966 cycles
CAPT'S SIDE EMERGENCY EXIT ROW DOOR ESCAPE ROPE COVER ASSY LOOSE. RESECURED CAPTS SIDE EMERGENCY EXIT DOOR ESCAPE ROPE COVER ASSY.
2012
Part: COVER — LOOSE (CABIN) · airframe 28,564 hrs · 13,248 cycles
R2 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 27,091 hrs · 12,434 cycles
LEFT HORIZONTAL STABILIZER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,091 hrs · 12,434 cycles
R1 DOOR L-ANGLE CORRODED BETWEEN BS 297 TO BS 328, RBL 60. REMOVED AND REPLACED ANGLE PER SRM AND DWG.
Part: FRAME — CRACKED (FUSELAGE) · airframe 27,091 hrs · 12,434 cycles
FRAME CRACKED AT BS 500A+5.5, LBL 2. REPAIRED FRAME PER SRM.
Part: STRAP — MISSING (EMERGENCY EXIT) · airframe 27,091 hrs · 12,434 cycles
LT OVERWING EMERGENCY EXIT DOOR ASSISTANT STRAP INNER BOX MISSING FASTENER. INSTALLED STRAP ASSY PER MM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 27,091 hrs · 12,434 cycles
FRAME CRACKED AT BS 295. REPAIRED FRAME PER SRM.
Part: CONNECTOR — BROKEN (CABIN) · airframe 27,091 hrs · 12,434 cycles
LT OVERHEAD EMERGENCY EXIT LIGHT CONNECTOR BROKEN. REMOVED AND REPLACED CONNECTOR PER MM.
Part: SUPPORT BRACKET — CORRODED (GIRT BAR) · airframe 27,091 hrs · 12,434 cycles
L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR SUPPORT BRACKET CORRODED AT BS 344, LBL 58. REMOVED AND REPLACED BRACKET SRM.