N7717D
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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.
77 reports on file, 2014-12-25 – 2020-12-06.
Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 48,673 hrs · 24,320 cycles
L2 AFT ENTRY DOOR SLIDE GIRT FALLS BELOW THE DOOR FRAME WHILE OPENING AND CLOSING (102-001). REMOVED L-2 DOOR SLIDE, ADJUSTED GIRT Z-FOLD TO LIFE THE GIRT ABOVE DOOR FRAME. REINSTALLED DOOR SLIDE AND TESTED FOUND OK, REF B737 AMM 25-66-01/400.
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 48,673 hrs · 24,320 cycles
R2 AFT ENTRY DOOR SLIDE GIRT FALLS BELOW DOOR FRAME WHILE OPENING AND CLOSING (102-002). REMOVED R-2 DOOR SLIDE READJUSTED GIRT Z-FOLD TO LIFE THE GIRT ABOVE DOOR FRAME. REINSTALLED DOOR SLIDE AND TESTED FOUND OK, REF B737 AMM 25-66-01/400.
Part: PLATE — CORRODED (AFT CARGO) · airframe 48,673 hrs · 24,320 cycles
***** CORROSION***** AFT CARGO COMPARTMENT BBETWEEN STA 727A AND STA 727B R/H SIDE;RBL 21 SIDEPLATE HAS SPOTS OF CORROSION AROUND FASTNER HOLES. (MKD 78-7). / FOUND DEEP CORROSION EXFOLIATION OUT OF LIMITS AT AFT CARGO COMPARTMENT SIDE PLATE 'Z' CHANNEL AROUND FASTENERS FROM STA 727 TO STA 767; RBL 21. REMOVED AND REPLACED AS PER REF B737-700 SRM 51-40-02-0G-0 AND DWG# 146A7502.
Part: FLOOR SUPPORT — CORRODED (FWD CARGO) · airframe 48,673 hrs · 24,320 cycles
** CORROSION ** FWD CARGO COMPMT. R/ H FLOOR SUPPORT Z CHANNEL AT S-25R STA 500 --500A MKD / REMOVED CORROSION FROM FWD CARGO R/H Z CHANNEL BETWEEN STA 500 & 500A STR 25R PER B737-700 SRM 51-10-02-0G-0. FOUND OUT OF LIMITS PER B737-700 SRM 53-00-53-1A-2 (CORROSION ALL THE WAY THRU). REMOVED & REPLACED Z CHANNEL (SHIELD) PER B737-700 SRM 51-40-02-0G-0 & DRWG # 143A0080.
Part: SHIELD — CORRODED (AFT CARGO) · airframe 48,673 hrs · 24,320 cycles
******CORROSION***** AFT CARGO COMPARTMENT R/H SIDE; BETWEEN STA 767 AND STA 787; SIDEPLATE HAS SPOTS OF CORROSION AROUND FASTNER HOLES. (MKD 78-10). / REMOVED AND REPLACED SIDEPLATE (SHIELD) AT AFT CARGO COMPARTMENT R/H SIDE BETWEEN STA 767 AND STA 727; RBL 21 AS PER REF B737-700 SRM 51-40-02-0G-0 AND DWG #146A8127
Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · airframe 48,673 hrs · 24,320 cycles
AFT CARGO COMPARTMENT STA 943; LBL 3.0; HAS CORROSION ON FLOOR SUPPORT . (MKD 78-19). WL 178. / FOUND DEEP CORROSION EXFOLIATION AT AFT CARGO COMPARTMENT BETWEEN STA 381 AND STA 947.5. REMOVED AND REPLACED AS PER REF B737-700 SRM 51-40-02-0G-0 A DWG #147A7501
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 48,673 hrs · 24,320 cycles
MAIN CABIN CENTER FLOOR PANEL NR 241EF UPPER SURFACE DELAMINATED MKD. CLEANED AND REPAIRED MAIN CABIN CENTER FLOOR PANEL 241EF AT UPPER SURFACE, REF B737 SRM 53-00-50-2R-1. MATERIALS USED RESIN PO NR 1692653 CAB-O-SIL-M5 PO NR 1614988.
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 48,673 hrs · 24,320 cycles
MAIN CABIN CENTER FLOOR PANEL NR 231XF UPPER SURFACE LAYERS DELAMINATED MKD. REPAIRED FLOOR PANEL 231XF UPPER SURFACE, REF B737-7 SRM 53-00-50-2R-1. MATERIAL USED PO: 1692653 AND PO: 1480720.
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 48,673 hrs · 24,320 cycles
MAIN CABIN FLOOR PANEL NR 232SF UPPER SURFACE LAYERS DELAMINATED MKD. REPAIRED FLOOR PANEL NR 232SF UPPER SURFACE, REF B737-7 SRM 53-00-50-2R-1 REPAIR NR 1. MATERIAL USED PO: 1480720 AND PO: 1692653.
Part: HOUSING — DAMAGED (EXIT SIGN) · airframe 48,673 hrs · 24,320 cycles
EXIT SIGN HOUSING IS DAMAGED AT AFT LOWER CEILING. REMOVED AND REPLACED EXIT SIGN HOUSING AT AFT LOWER CEILING, IAW B737-700 AMM 33-51-01-960-802.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 48,673 hrs · 24,320 cycles
MAIN CABIN FLOOR PANEL NR 241DF UPPER SURFACE LAYERS DELAMINATED MKD. REPAIRED FLOOR PANEL NR 241DF UPPER SURFACE, REF B737-7 SRM 53-00-50-2R-1 REPAIR NR 1. MATERIAL USED PO: 1480720 AND PO: 1692653.
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 48,673 hrs · 24,320 cycles
MAIN CENTER FLOOR PANEL NR 241FF UPPER SURFACE LAYERS DELAMINATED MKD. REPAIRED FLOOR PANEL NR 241FF UPPER SURFACE, REF B737-7 SRM 53-00-50-2R-1 REPAIR NR 1. MATERIAL USED PO 1480720 AND PO 1692653.
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 48,673 hrs · 24,320 cycles
MAIN CENTER FLOOR PANEL NR 241AF UPPER SURFACE LAYERS DELAMINATED MKD. REPAIRED FLOOR PANEL NR 241AF UPPER SURFACE, REF B737-700 SRM 53-00-50-2R-1. MATERIAL USED PO 1692653 AND PO 1480720.
Part: FLOOR PANEL — DETERIORATED (MAIN CABIN) · airframe 48,673 hrs · 24,320 cycles
MAIN CABIN CENTER FLOOR PANEL 242CF UPPER SURFACE LAYERS AREAS DETERIORATED, MARKED. CLEANED AND REPAIRED MAIN CABIN CENTER FLOOR PANEL 242CF, IN ACCORDANCE TO B737-7 SRM 53-00-50-2R-1. MATERIALS USED RESIN PO 169253 CA O SIL PO 1614988.
Part: SKIN — CRACKED (GRND POWER BOX) · airframe 48,673 hrs · 24,320 cycles
RIGHT FWD LOWER FUSELAGE EXTERNAL POWER COMPARTMENT CUTOUT CRACKED BELOW ACCESS DOOR LOWER HINGE, MARKED. ACCOMPLISHED PERMANENT REPAIR AT FUSELAGE BETWEEN STA 227 & STA 235 WL 176. ELECTRICAL GROUND POWER RECEPTACLES SURROUND DOUBLER BELOW ACCESS DOOR LOWER HINGE, PER SWA EA 20-153-02413 REV IR FIG 1 (RES# 2016450-1).
Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 48,655 hrs · 24,303 cycles
AFT LAVATORY SMOKE DETECTOR SOUNDED AS AN ALARM ON DESCENT 15 MINUTES FROM LANDING. "B" FLT ATTENDANT DID NOT SMELL SMOKE NOR DETECT ANY ABNORMAL HEAT ON THE FLOORS, WALLS, CEILING. AT THE GATE, THE "B" FLIGHT ATTENDANT SMELLED A SLIGHT ELECTRICAL ODOR COMING FROM THE GASPER OVER THE AFT ENTRY DOOR. R & R AFT LAV SMOKE DETECTOR, PER AMM 26-14-01.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,542 hrs · 23,621 cycles
EXTERIOR MAIN CABIN DOOR; & FWD EXIT SIGNS LIGHTS ARE INOP / REOVED AND REPLACED POWER SUPPLHY BATERY PACK M1675 NEAR THE FWD ENTRY DOOR. REF AMM 33-51-06. OPS CHECK GOOD.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,392 hrs · 23,542 cycles
EXTERIOR EMERGENCY LIGHT AFT OF THE AFT SERVICE DOOR IS INOP / REMOVED & REPLACED EMERGENCY BATTERY POWER SUPPLY M1672 AND EMERGENCY BATTERY PACK M1672 I.A.W. AMM 33-51-06. EMERGENCY LIGHT OPERATIONAL TEST GOOD.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 47,392 hrs · 23,542 cycles
EXTERIOR EMERGENCY LIGHT AFT OF THE AFT SERVICE DOOR IS INOP REMOVED & REPLACED EMERGENCY BATTERY POWER SUPPLY M1672 AND EMERGENCY BATTERY PACK M1672 I.A.W. AMM 33-51-06. EMERGENCY LIGHT OPERATIONAL TEST GOOD.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 47,392 hrs · 23,542 cycles
EXTERIOR EMERGENCY LIGHT AFT OF THE AFT SERVICE DOOR IS INOP / REMOVED & REPLACED EMERGENCY BATTERY POWER SUPPLY M1672 AND EMERGENCY BATTERY PACK M1672 I.A.W. AMM 33-51-06. EMERGENCY LIGHT OPERATIONAL TEST GOOD.
Earlier reports · 2014–2019 · 57 reports
2019
Part: STRAP — BROKEN (FLASHLIGHT) · airframe 43,706 hrs · 21,268 cycles
AFT EMERGENCY FLASHLIGHT STRAP BROKEN. R&R STRAP PER MM.
Part: TAIL CONE — DELAMINATED (FUSELAGE) · airframe 43,537 hrs · 21,165 cycles
UPPER SURFACE OF FUSELAGE TAIL CONE HAD MULTIPLE DENTS WITH SOME EXHIBITING EVIDENCE OF DELAMINATION. REPAIRED TAIL CONE PER SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,537 hrs · 21,165 cycles
AFT GALLEY G4 EXIT SIGN LIGHT INOP. RELAMPED LIGHT IAW MM.
Part: STRINGER — CRACKED (LT WING) · airframe 43,537 hrs · 21,165 cycles
LT WING STRINGER CRACKED 1.5" INBOARD OF PYLON ON FIXED LEADING EDGE. R&R STRINGER IAW SRM.
Part: BEAM — CRACKED (R1 DOOR) · airframe 43,537 hrs · 21,165 cycles
R1 DOOR NR 5 BEAM CRACKED IN RADIUS AT INBOARD AREA NEXT TO BOLD HOLE. R&R DOOR PER MM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,534 hrs · 21,165 cycles
PASSENGER CABIN NR 4 SEAT TRACK CORRODED BETWEEN BS 747+8 TO BS 747+12. R&R SEAT TRACK PER SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,534 hrs · 21,165 cycles
PASSENGER CABIN NR 4 SEAT TRACK CORRODED BETWEEN BS 767-2 TO BS 767+1. R&R SEAT TRACK PER SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,534 hrs · 21,165 cycles
PASSENGER CABIN NR 4 SEAT TRACK CORRODED BETWEEN BS 787 TO BS 787+15. R&R SEAT TRACK PER SRM.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 43,534 hrs · 21,165 cycles
PASSENGER CABIN NR 4 SEAT TRACK CORRODED AT BS 727E+4. R&R SEAT TRACK PER SRM.
2018
Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 43,372 hrs · 21,061 cycles
R1 DOOR GIRT BAR BLOCKED BY DEBRIS. REMOVED DEBRIS BLOCKING GIRT BAR PER SIP.
Part: TRANSMISSION — FAULTY (TE FLAP) · airframe 42,746 hrs · 20,680 cycles
DECLARED EMERGENCY, ON APPROACH, WHEN SELECTING FLAPS 5, LEFT TRAILING EDGE FLAP STAYED UP, RIGHT TRAILING EDGE FLAP INDICATED ABOUT 1/2 DEGREE EXTENDED. R&R NR 3 TRAILING EDGE FLAP TRANSMISSION IAW AMM.
Part: TRANSMISSION — FAULTY (TE FLAP) · airframe 42,746 hrs · 20,680 cycles
DECLARED EMERGENCY, ON APPROACH, WHEN SELECTING FLAPS 5, LEFT TRAILING EDGE FLAP STAYED UP, RIGHT TRAILING EDGE FLAP INDICATED ABOUT 1/2 DEGREE EXTENDED. R&R NR 4 TRAILING EDGE FLAP TRANSMISSION IAW AMM.
Part: RETAINING CLIP — OUT OF ADJUST (R1 DOOR) · airframe 41,467 hrs · 19,900 cycles
R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FELL OUT OF RETAINING CLIPS. ADJUSTED CLIPS IAW AMM.
Part: WEB — CRACKED (LT MLG WW) · airframe 40,749 hrs · 19,474 cycles
LT MAIN WHEEL WELL VERTICAL WEB CRACKED STA 663, BETWEEN LBL 32 TO LBL 45. REPAIRED WEB PER EA AND SRM.
2017
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 37,048 hrs · 17,322 cycles
RIGHT EMERGENCY EXIT LIGHT LENS COVER MISSING AT ROW 12. REPLACED THE LENS IAW AMM.
2016
Part: SHEAR TIE — CORRODED (BS 323) · airframe 36,816 hrs · 17,184 cycles
FRAME SHEAR TIE CORRODED AT BS 323.7, BETWEEN STRINGERS 21 - 23L. R & R THE SHEAR TIE IAW SRM AND DWG.
Part: FRAME — CORRODED (FUSELAGE) · airframe 36,816 hrs · 17,184 cycles
EQUIPMENT ELECTRONIC COMPARTMENT FRAME WEB CORRODED AT BS 323.7, BETWEEN STR 21L TO STR 23L. R&R WEB IAW SRM AND DWG.
Part: WEB — CRACKED (BS 344-360) · airframe 36,816 hrs · 17,184 cycles
WEB INTERCOSTAL CRACKED BETWEEN BS 344 TO 360, LBL 12. R & R WEB IAW SRM AND DWG.
Part: ANGLE — CRACKED (BS 400) · airframe 36,816 hrs · 17,184 cycles
ANGLE CRACKED AT BS 400, STRINGER 26L. R & R THE ANGLE IAW SRM.
Part: ANGLE — CRACKED (BS 500C) · airframe 36,816 hrs · 17,184 cycles
ANGLE CRACKED AT BS 500C, STRINGER 26R. R & R THE ANGLE IAW SRM.
Part: ANGLE — CRACKED (BS 500C) · airframe 36,816 hrs · 17,184 cycles
ANGLE CRACKED AT BS 500C, STRINGER 26L. R & R THE ANGLE IAW SRM.
Part: ANGLE — CRACKED (BS 500B) · airframe 36,816 hrs · 17,184 cycles
ANGLE CRACKED AT BS 500B, STRINGER 26R. R & R THE ANGLE IAW SRM.
Part: ANGLE — CRACKED (BS 277) · airframe 36,816 hrs · 17,184 cycles
ANGLE CRACKED AT BS 277, STRINGER 10R. R & R THE ANGLE IAW SRM.
Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 36,816 hrs · 17,184 cycles
MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, BETWEEN RBL 41.5 TO RBL42.5. REPAIRED WEB IAW SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,816 hrs · 17,184 cycles
WEB INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 45. REPLACED INTERCOSTAL IAW SRM AND DWG.
Part: ANGLE — CRACKED (BS 500B) · airframe 36,816 hrs · 17,184 cycles
ANGLE CRACKED AT BS 500B, STRINGER 26L. R & R THE ANGLE IAW SRM.
Part: SUPPORT — CORRODED (BS 480-500D) · airframe 36,816 hrs · 17,184 cycles
FORWARD CARGO BAY ZEE SUPPORT CORRODED BETWEEN BS 480 TO 500D, STRINGER 26L. R & R ZEE SUPPORT IAW SRM AND DWG.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,816 hrs · 17,184 cycles
WEB INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 31. R&R INTERCOSTAL IAW SRM AND DWG.
Part: SUPPORT — CORRODED (BS 747-767) · airframe 36,816 hrs · 17,184 cycles
AFT CARGO BAY SUPPORT ZEE CORRODED BETWEEN BS 747 TO 767, LBL 21.0. R & R THE SUPPORT ZEE IAW SRM AND DWG.
Part: ANGLE — CRACKED (BS 867) · airframe 36,816 hrs · 17,184 cycles
ANGLE CRACKED AT BS 867, STRINGER 26L. R & R THE ANGLE IAW SRM.
Part: SUPPORT — CRACKED (BS 727D) · airframe 36,816 hrs · 17,184 cycles
AFT CARGO BAY SUPPORT ZEE CRACKED AT BS 727D+3, LBL 21. REPAIRED THE SUPPORT ZEE IAW SRM AND DWG.
Part: STRAP — CORRODED (FUSELAGE) · airframe 36,816 hrs · 17,184 cycles
AFT CARGO COMPARTMENT STRAP CORRODED AT BS 887, BETWEEN STR 25R TO STR 26L. R&R STRAP IAW SRM AND DWG.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 36,816 hrs · 17,184 cycles
WEB INTERCOSTAL CRACKED BETWEEN BS 927 TO BS 947.5, STR 25R. R&R INTERCOSTAL IAW SRM AND DWG.
Part: GUSSET — CRACKED (FUSELAGE) · airframe 36,816 hrs · 17,184 cycles
FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS 500D, STR 19R. R&R GUSSET IAW SRM AND DWG.
Part: FITTING — CRACKED (BS 947) · airframe 36,816 hrs · 17,184 cycles
FUSELAGE STRINGER FITTING CRACKED AT BS 947.5, STRINGER 26L. R & R FITTING IAW SRM.
Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 36,816 hrs · 17,184 cycles
AFT GALLEY EXIT LIGHT LENS BROKEN. R & R LENS IAW MM.
Part: WIRE — BROKEN (CABIN) · airframe 36,816 hrs · 17,184 cycles
FORWARD GALLEY AREA EMERGENCY EXIT SIGN WIRE BROKEN. REPAIRED WIRE IAW SWPM.
Part: BEAM — CRACKED (R1 DOOR) · airframe 36,816 hrs · 17,184 cycles
R1 DOOR BEAM UNDER HANDLE BOX ASSEMBLY CRACKED IN RADIUS NEXT TO INBOARD FORWARD LOWER MOUNT BOLTS. REPAIRED BEAM PER EA.
Part: BEAM — CRACKED (R1 DOOR) · airframe 36,814 hrs · 17,183 cycles
R1 DOOR BEAM UNDER HANDLE BOX ASSEMBLY CRACKED IN RADIUS NEXT TO INBOARD FORWARD LOWER MOUNTING BOLTS. R & R THE BEAM IAW SRM AND DWG.
2015
Part: ENGINE — FAILED (RIGHT) · airframe 33,594 hrs · 15,353 cycles
AIR RETURN, INFLIGHT SHUTDOWN. NR 2 ENG LOUD BANG & SHUTDOWN. R & R NR 2 ENG IAW MT.
Part: SUPPORT FITTING — CORRODED (RT WING) · airframe 31,469 hrs · 14,126 cycles
RIGHT MLG FWD TRUNNION SUPPORT FITTING CORRODED. REPAIRED FITTING IAW EA.
Part: SUPPORT FITTING — CORRODED (LT WING) · airframe 31,469 hrs · 14,126 cycles
LEFT MLG FWD TRUNNION SUPPORT FITTING CORRODED. REPAIRED FITTING IAW EA.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,374 hrs · 13,527 cycles
L2 DOOR EMER EXIT LIGHT INOPERATIVE. R & R BULB IAW AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,374 hrs · 13,527 cycles
R1 DOOR EMER EVAC SLIDE LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.
Part: CONNECTOR — NOT SEATED (CABIN) · airframe 30,374 hrs · 13,527 cycles
R2 DOOR OVERHEAD EMER EXIT LIGHT INOPERATIVE. RESEATED CONNECTOR IAW SWPM & MM.
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 30,374 hrs · 13,527 cycles
RIGHT HORIZONTAL STABILIZER IN SPAR RIB AT STATION 129.50 3RD STIFFENER FROM THE FRONT CRACKED ON LOWER END. REPAIRED RIB IAW SRM.
Part: ATTACH ANGLE — BROKEN (RT WING) · airframe 30,374 hrs · 13,527 cycles
RIGHT WING INBD FWD TE PANEL AT DEFLECTION CONTROL RIB VERTICAL SUPPORT ANGLE OTBD ATTACH ANGLE BROKEN. R & R ANGLE IAW SRM.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 30,374 hrs · 13,527 cycles
FORWARD SEAT TRACK CRACKED AT BS 727B, LBL 45.5 OTBD FLANGE FWD HOLE. REPAIRED SEAT TRACK IAW ER & EA.
Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 30,374 hrs · 13,527 cycles
FLOOR PANEL 242UF LOWER SKIN OTBD EDGE CRACKED. REPAIRED FLOOR PANEL IAW SRM.
Part: POST — CRACKED (FUSELAGE) · airframe 30,374 hrs · 13,527 cycles
RIGHT NR 3 WINDOW FWD POST E - F FASTENER HOLE CRACKED. REPAIRED POST IAW EO.
Part: FLOOR PANEL — BROKEN (FUSELAGE) · airframe 30,374 hrs · 13,527 cycles
FLOOR PANEL 221GF FWD OTBD CORNER BROKEN OFF. REPAIRED PANEL IAW SRM.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 30,374 hrs · 13,527 cycles
FORWARD SEAT TRACK CRACKED AT BS 727B, LBL 25 OTBD FLANGE FWD & AFT HOLE, INBD FLANGE AFT HOLE. REPAIRED SEAT TRACK IAW ER & EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 30,374 hrs · 13,527 cycles
FORWARD SEAT TRACK CRACKED AT BS 727B, RBL 25 OTBD FLANGE FWD & AFT HOLES, INBD FLANGE FWD & AFT HOLES. REPAIRED SEAT TRACK IAW ER & EA.
Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 30,374 hrs · 13,527 cycles
FLOOR PANEL 241ABF LOWER SKIN OTBD EDGE CRACKED. REPAIRED FLOOR PANEL IAW SRM.
Part: ATTACH ANGLE — BROKEN (RT WING) · airframe 30,374 hrs · 13,527 cycles
RIGHT WING INBD FWD TE PANEL AT DEFLECTION CONTROL RIB VERTICAL SUPPORT ANGLE CTR ATTACH ANGLE BROKEN ON FWD SIDE. R & R ANGLE IAW SRM.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 30,374 hrs · 13,527 cycles
COCKPIT NR 1 LT WINDOW FRAME CRACKED FROM THE CORNER TO THE INTERIOR SURFACE. REPAIRED FRAME IAW ACO.
2014
Part: LENS — DIRTY (EXTERIOR) · airframe 30,374 hrs · 13,527 cycles
EXTERNAL EXIT LIGHT LENS DIRTY. CLEANED LENS IAW SOPM.