N568WN
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.
96 reports on file, 2015-05-30 – 2019-11-25.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,637 hrs · 27,647 cycles
SUPPLEMENTAL INFORMATION, LT EMERGENCY LIGHTING ON OVERHEAD BIN BULLNOSE INOP AT ROW 9. R&R BATTERY PACK PER AMM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,637 hrs · 27,647 cycles
SUPPLEMENTAL INFORMATION, LT EMERGENCY LIGHTING ON OVERHEAD BIN BULLNOSE INOP AT ROW 7. R&R BATTERY PACK PER AMM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,637 hrs · 27,647 cycles
SUPPLEMENTAL INFORMATION, LT EMERGENCY LIGHTING ON OVERHEAD BIN BULLNOSE INOP AT ROW 14. R&R BATTERY PACK PER AMM.
Part: RETAINER — CRACKED (RT WING) · airframe 55,773 hrs · 27,078 cycles
RIGHT WING FIXED T/E I/B BULKHEAD ASSY. SEAL RETAINER IS CRACKED / R/H WING; FIXED T/E I/B BULKHEAD. REMOVED AND REPLACED SEAL RETAINER IAW B737 SRM 51-40-02-0G-0
Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 55,773 hrs · 27,078 cycles
EMERGENCY EXIT LIGHT LOCATED ON THE G1 GALLEY BROKEN. / R&R CONTACT SPLICE IAW SWPM & AMM.
Part: RAIL — INCORRECT (AFT CARGO COMPT) · airframe 55,773 hrs · 27,078 cycles
DTIP - PREVIOUS OPERATOR INSTALLED REPAIR ON AFT CARGO RAIL AT BS 767; RBL 3.0 IS NON-CONFORMING & REQUIRES REMOVAL & INSTALLATION OF NEW REPAIR PER CUSTOMER REQUEST. / REMOVED OLD REPAIR OF AFT CARGO RAIL BS 767 RBL 3 IAW B737-700 SRM 51-40-02-0G-0. INSTALLED NEW REPAIR AT AFT CARGO RAIL BS 767 RBL 3 IAW B737-700 SRM 53-00-53-2R-2 AND EA: 1-A53-4982 REV:3
Part: SUPPORT — CRACKED (VERTICAL STAB) · airframe 55,773 hrs · 27,078 cycles
VERTICAL STABILIZER RIB LATERAL SUPPORT CRACKED AT BS. 1018, BETWEEN LBL 10 TO RBL 10. / R&R SUPPORT IAW DWG & SRM.
Part: FLAP — DELAMINATED (LT WING) · airframe 55,773 hrs · 27,078 cycles
LT OUTBOARD AFT FLAP, AFT INBOARD CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM.
Part: ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 55,773 hrs · 27,078 cycles
REAR SPAR VERTICAL PRESSURE DECK CRACKED AT BS. 663, BETWEEN RBL 25 TO RBL 45. REPAIRED ANGLE IAW EA.
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 55,773 hrs · 27,078 cycles
RH MAIN CABIN FLOOR ACCESS PANEL #222AF TOP LAYER IS MISSING IN SEVERAL AREAS. / EVALUATED; PREPPED; CLEANED AND REPAIRED UPPER SURFACE DAMAGE TO SKIN PLY ON FLOORBAORD 222AF IAW B737 SRM 53-00-50-2R-1; PAR 3 9A;C;E-F; K1;L1;M1) REV 68/
Part: FLOOR PANEL — PULLED (MAIN CABIN) · airframe 34,428 hrs · 20,768 cycles
CABIN FLOORBOARD 231XF UPPER SURFACE HAS PULLED FIBE / REPLACED CABIN FLOORBOARD 231 X F BY FABRICATION I.A.W. B737-700 SRM 53-00-50-2R-0 TABLE 204 REV. 68 AND BAC 3085 REV. E AND BOEING DWG # 144A5810-126 REV A (MP1345) (A40400) (A71226)
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 55,773 hrs · 27,078 cycles
LH MAIN CABIN FLOOR ACCESS PANEL #221CF TOP LAYER IS COMING OFF. / REPAIRED CABIN FLOOR PANEL #221CF I.A.W B737-700 SRM'S 53-00-50-2R-0 REV. 68 & 53-00-50-2R-1
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 55,773 hrs · 27,078 cycles
L2 CREASE BEAM INNER CHORD UPPER FLANGE CORRODED AROUND NUT PLATES BETWEEN BS. 958 TO BS. 985, LBL 51.8. R&R INNER CHORD IAW SRM & DWG.
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 55,773 hrs · 27,078 cycles
PASSENGER CABIN FLOOR BOARD 232SF HAS A PUNCTURE WITH DELAM ON UPPER SURFACE 1.5' FROM FORWARD EDGE AND 5' FROM INBOARD EDGE / REPAIRED PUNCTURE W/ DELAM ON UPPER SURFACE 1.5' FROM FWD EDGE & 5' FROM INBOARD EDGE ON PASSENGER CABIN FLOOR BOARD 232 SF IAW B 737 SRM 53-00-50-2R-2 REV 68
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 55,773 hrs · 27,078 cycles
AFT CABIN FLOORBOARD 242UF HAS MISSING FIBERS ON TOP SIDE. / REPAIRED AFT CABIN FLOOR BOARD 242UF ON TOP SIDE IAW B737-700 SRM 53-00-50-2R-1 AND 51-00-05 NDT P4; BOND CHECKED (A09236) (A36551) C
Part: CREASE BEAM — CORRODED (BS 958-985) · airframe 55,773 hrs · 27,078 cycles
R2 CREASE BEAM INNER CHORD UPPER FLANGE CORRODED BETWEEN BS. 958 TO BS. 985, RBL 51, AROUND NUT PLATES. R&R CREASE BEAMS IAW DWG AND SRM.
Part: FLOORBOARD — DAMAGED (CABIN) · airframe 55,773 hrs · 27,078 cycles
PASSENGER CABIN FLOORBOARD 241AF HAD A FIBER DAMAGE ON UPPER SURFACE ALONG LENGTH OF PANEL. R&R FLOORBOARD 241AF IAW SRM & DWG.
Part: SHEAR WEB — CORRODED (MAIN CABIN) · airframe 55,773 hrs · 27,078 cycles
CABIN FLOOR WEB AT STA 1006+11' LBL 19 WL 208 CORRODED ON TOP SURFACE / ACCOMPLISHED BLEND REPAIR ON FLOOR SUPPORT STRUCTURE SHEAR WEB AT STA 1020 LBL 19 TO 27 I..A.W E.A 190593 IR AND SEA 1-753-35278 REV IR.
Part: BAFFLE — CORRODED (FWD CARGO BAY) · airframe 55,773 hrs · 27,078 cycles
FWD CARGO COMPARTMENT BAFFLE AT STA 500C TO 500D LBL 21 CORRODED. / REMOVED CORROSION IAW SRM 51-10-02-0G0 VISUAL INSPECTON WITH A 10X MAG G LOSS NO DEFECTS ORIGINA .032 REMAININ .025 LOSS .007 FOUND TO BE OUT LOF LIMITS IAW SRM 53-00-53-1A-2 FIG 103. REMVOED AND REPLACED FWD CARGO BAFFLE @ STA 500C TO 500D LBL 21. IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A7505 SHT 9 REV:A. TOOL 32351 CAL 12-27-19.
Part: INTERCOSTAL — CORRODED (BS 767-787) · airframe 55,773 hrs · 27,078 cycles
AFT CARGO COMPARTMENT INTERCOSTAL CORRODED BETWEEN BS. 767 TO BS. 787, RBL 20. REPAIRED INTERCOSTAL IAW DWG & SRM.
Part: FLOORBEAM — CORRODED (BS 986) · airframe 55,773 hrs · 27,078 cycles
CABIN FLOOR STRUCTURE "T" CAP UPPER AND LOWER SURFACE CORRODED AT NUTPLATE HOLES BS. 986, RBL 43. / REPAIRED FLOOR BEAM UPPER T-CAP IAW EA.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 55,773 hrs · 27,078 cycles
FORWARD WET AREA, FLOOR STRUCTURE R1 DOOR Z ANGLE CORRODED AT BS. 291+5. R&R R1 DOOR LOWER SILL CREASE BEAM ANGLE IAW SRM AND DWG.
Part: ATTACH BRACKET — CRACKED (LT WING) · airframe 55,773 hrs · 27,078 cycles
LT WING; I/B FIXED T/E PANEL 551FB; MOUNT ANGLE IS BROKEN . (STREAMER) / REMOVED ATTACH BRACKET P/N 287A9152-23 @ L/H WING; I/B FIXED; T/E PANEL 551FB. LOCATED & DRILLED NEW BRACKET. INSTALLED NEW BRACKET. ALL ACTIONS ARE IAW B737 SRM'S 51-40-02-0G-0; 51-40-05-0G-0; 51-40-06-0G-0; & BOEING DWG #115A2710 REV B
Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 55,773 hrs · 27,078 cycles
LT WING AFT SPAR FIXED PANEL BETWEEN #5 SPOILER AND GROUND SPOILER SUPPORT ANGLE CRACKED ON FORWARD SIDE. R&R SUPPORT ANGLE IAW DWG.
Part: SUPPORT RIB — CRACKED (LT WING) · airframe 55,773 hrs · 27,078 cycles
LT WING AFT SPAR FIXED PANEL BETWEEN #5 SPOILER AND GROUND SPOILER SUPPORT RIB CRACKED IN RADIUS. R&R SUPPORT RIB IAW DWG & SRM.
Part: ANGLE — CORRODED (BS 747-847) · airframe 55,773 hrs · 27,078 cycles
AFT CARGO PIT LEFT ZEE ANGLE CORRODED UPPER SURFACE BETWEEN BS. 747 TO BS. 847, LBL 21. / REPAIRED Z ANGLE IAW SRM & DWG.
Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 55,773 hrs · 27,078 cycles
AFT CARGO PIT R/H Z ANGLE BETWEEN STA 727E+6' TO 767 RBL 21 HAS CORROSION UPPER SURFACE / REMOVED CORROSION ON R/H Z ANGLE STA 727E TO 767 RBC 21. IAW SRM 51-10-02-0G-0. MEASURED 100% MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2. REMOVED AND REPLACED Z-ANGLE IAW SRM 51-40-02-0G-0 AND BOEING DWG - 146A7502 REV A. RH SIZE STA. 727TO STA 767 RBL 21 146A 7502-2
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 55,773 hrs · 27,078 cycles
AFT CARGO PIT LOWER SILL WEB CORRODED UPPER SURFACE BETWEEN BS. 787+18 TO BS. 847, RBL 27. R&R WEB IAW SRM & DWG.
Part: ATTACH BRACKET — CRACKED (AFT CARGO BAY) · airframe 55,773 hrs · 27,078 cycles
AFT CARGO PIT ATTACH BRACKET STA 867-2' ON WASTE TANK VERTICAL SUPPORT LBL 10 AT FLOOR LEVEL CRACKED / INSTALLED NEW AFT CARGO PIT ATTACHE BRACKET STA 867-2' ON WASTE TANK VERTICAL SUPPORT LBL 10 AT FLOOR LEVEL IAW SRM B737NG SRM 51-40-02-0G-0; DWG 149A8102 REV A PN 149A8109-114 ATAG A68260
Part: SUPPORT — CRACKED (RT WING) · airframe 55,773 hrs · 27,078 cycles
RIGHT WING AFT SPAR; 7' OTBD OF FUSELAGE SIDE OF BODY; UPPER WING PANEL SUPPORT ATTACH CLIP; CRACKED THROUGH. / REMOVED & REPLACED CRACKED ATTACH CLIP R/H WING AFT SPAR; 7' OTBD OF FUSELAGE SIDE OF BODY; UPPER WING PANEL SUPPORT IAW BOEING DWG # 115A2000 REV. - B; B737 SRM 51-40-02-0G0 A TAG # A93212.
Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 55,773 hrs · 27,078 cycles
FWD CARGO AFT CORNER SCUFF PLATE CRACKED / REPAIRED AFT CORNER SCUFF PLATE IAW E.A. 1-A53-2076 REV 11
Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 55,773 hrs · 27,078 cycles
FWD CARGO FWD CORNER SCUFF PLATE IS CRACKED / REPAIRED FORWARD CORNER SCUFF PLATE IAW E.A. 1-A53-2076 REV 11
Part: FINGER DOUBLER — CRACKED (LT WING) · airframe 55,773 hrs · 27,078 cycles
(NO DOT-18) LEFT WING AFT SPAR; LOCATED JUST INBOARD OF #1 ENGINE LINES. FINGER PLATE LOOSE AND CRACKED. / REMOVED LEFT WING AFT SPAR FINGER PLATE IAW SRM 51-40-02-0G-0. VERIFIED NEW PT 115A2781-13 IAW BOEING DRAWING 115A2714 REV A FRAME 2 AND BOEING ENGINEERING INFORMATION DELIVERY. INSTALLED NEW FINGER PLATE IAW SRM 51-40-02-06-0 AND 51-10-01-06-0. TREATED AND PRIMED IAW AMM 51-21-41-370-803 AND 51-21-72-370-804. RESTORED DECORATIVE FINISH IAW AMM 51-21-99-300-801. ATAG: WN34025
Part: SUPPORT FITTING — CRACKED (RT WING) · airframe 55,773 hrs · 27,078 cycles
RT WING UPPER FIXED TRAILING EDGE 10" INBOARD OF DEFLECTION CONTROL RIB, UPPER PANEL SUPPORT CLIP CRACKED. R&R SUPPORT CLIP IAW SRM & DWG.
Part: SHIELD — CORRODED (FUSELAGE) · airframe 55,773 hrs · 27,078 cycles
FORWARD CARGO COMPARTMENT R/H FLOOR SHIELD CORRODED AROUND FASTENER HOLES BETWEEN BS. 420 TO BS. 440. R&R SHIELD IAW SRM & DWG.
Part: VAPOR BARRIER — CRACKED (LT WHEEL WELL) · airframe 55,773 hrs · 27,078 cycles
LH MAIN WHEEL VAPOR BARRIER BULKHEAD EXISTING REPAIR DELAMED. / ACCOMPLISHED COMPOSITE BOND REPAIR ON LH STA 663 VAPOR BARRIER BULKHEAD I.A.W. SRM 51-70-04-2R-10 REV 68
Part: ANGLE — CORRODED (BS 500A-500D) · airframe 55,773 hrs · 27,078 cycles
FORWARD CARGO COMPARTMENT LEFT Z-ANGLE CORRODED AROUND FASTENER HOLES BETWEEN BS 500A TO 500D. R & R THE LT Z-ANGLE IAW SRM AND DWG.
Part: PANEL — DELAMINATED (LT WING) · airframe 55,773 hrs · 27,078 cycles
L/H WING LWR L/E PANEL 521WB INNER SURFACE FWD OUTBD CORNER MISSING PIECE OF COMPOSITE AND DELAMINATING / REPAIRED DAMAGE ON PANEL 521WB; APPLIED RESIN SWEEP TO REPAIR AREA AND CURED. RESTORED DECORATIVE FINISH. IAW B737-700 SRM 51-70-04-2R-13 REV 68; B737 AMM 51-21-99-300-801 REV 68
Part: GUSSET — CRACKED (FUSELAGE) · airframe 55,773 hrs · 27,078 cycles
FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS. 500D, STR. 19L. R&R GUSSET IAW DWG & SRM.
Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 55,773 hrs · 27,078 cycles
AFT CARGO PIT COVER PLATE FOR FLOOR PANEL 140CF CORRODED LOWER SURFACE / VERIFY LIMITS FOR AFT CARGO PIT COVER PLATE FOR FLOOR PANEL 140CF NO LIMITS GIVEN IN THE SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0. P;C. VERIFIED NEW PART IAW IPC 25-52-10-02 PART #453A2611-2. PLACED PART BACK ON RACK.
Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 55,773 hrs · 27,078 cycles
FWD CARGO PIT FLOOR PANEL 120AF HAS CORROSION UPPER SURFACE AT NET TIE DOWN PLATE & FWD EDGE / REMOVED CORROSION ON FWD CARGO FLOORPANEL 120AF UPPER SURFACE @ NET TIEDOWN IAW SRM 51-10-02-0G. VISUAL INSPECTION WITH A 10X MAG GLASS; NO DEFECTS- ORIGINAL .071' REMAIN .062' LOSS OF .009' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1. RECEIVED NEW FLOOR BOARD 120AF IAW AIPC 25-52-10-01; ITEM 223 P/N 453A1610-14 ATAG WN4101 TOOL 36644 CAL 19SEP19
Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 55,773 hrs · 27,078 cycles
AFT CARGO PIT FLOOR PANEL 140BF HAS CORROSION ON EDGES ON UPPER SURFACE / VERIFIED NEW FLOOR PNL 140 BF IAW IPC 25-52-10-02 PART# 453A2610-32 ATAG WN9914. FLOOR PNL WILL BE INSTALLED ON SOUTHWEST CARD 39747/1600/0012; JPANEL-141-CLOSE. REMOVED AND REPLACED PNL ON SHELF ATAG- WN9914
Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 55,773 hrs · 27,078 cycles
FWD CARGO PIT FLOOR PANEL 120CF HAS CORROSION UPPER SURFACE AFT EDGE / REMOVED CORROSION FROM FWD CARGO FLOOR PANEL 120CF ON AFT EDGE BELOW SRM 51-10-02-0G-0 PAR 15. ORIG 'T' .071'; .067' .004' LOSS 48' LONG FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 103 TOOL AAR 32351 DUE 12/27/19. VERIFIED NEW PANEL 453A1610-32 SI 7253766 A-TAG #WN1848 IAW AIPC 25-52-10-01 PART CHANGE OUT ON SHELF. PN 453A1610-32
Part: SHIELD — CORRODED (FWD CARGO BAY) · airframe 55,773 hrs · 27,078 cycles
FWD CARGO COMP.RH FLOOR SHIELD CORROSION AROUND FASTNER HOLES STA.490-500A / REMOVED CORROSION IAW SRM 51-10-02-0G-0 100% LOSS OF MATERIAL. REMOVED AND REPLACED FWD CARGO FLOOR SHIELD @ STA 490 TO 500A IAW SRM 51-40-02-0G-0 AND BOE8ING DWG 143A0080 SHT 11 REV:- P/N 143A8126-19
Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 55,773 hrs · 27,078 cycles
RT HORIZONTAL STABILIZER INSPAR RIB, STAB. STA. 120.30, VERTICAL STIFFENERS #3 CRACKED APPROXIMATELY 1" ABOVE RIB LOWER FLANGE. REPAIRED STIFFENER IAW SRM.
Part: RETAINER — CORRODED (RT WING) · airframe 55,773 hrs · 27,078 cycles
R/H WING REFUEL PANEL 621GB SEAL RETAINER HAS MINOR CORROSION / RETAINER FOUND WITH 100% MATERIAL LOSS. FABRICATED NEW P/N 116A8504-8 RETAINER FROM 7075-T6 X. 040' MATERIAL IAW DRAWING 116A8504 REV B. INSTALLED NEW RETAINER IAW 737 AMM 20-50-11-910-801 TABLE 204.
Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 55,773 hrs · 27,078 cycles
RT HORIZONTAL STABILIZER INSPAR RIB, STAB. STA. 120.30, VERTICAL STIFFENER #2 CRACKED. REPAIRED STIFFENER IAW SRM.
Part: BONDING JUMPER — FRAYED (EMERGENCY EXIT) · airframe 55,773 hrs · 27,078 cycles
RT EMERGENCY EXIT HATCH BONDING JUMPER FRAYED. R&R BONDING JUMPER IAW AMM.
Part: PANEL — DELAMINATED (RT WING) · airframe 55,773 hrs · 27,078 cycles
R/H WING LWR L/E PANEL 621VB FWD INDB CORNER DELAMINATED AT EROSION STRIP / EVALUATED PREPPED CLEANED AND REPAIRED DELAM DAMAGE AT FWD IND CORNER ON PANEL 621 VB IAW B 737 SRM 51-70-04 PAR 4 (A-E) REV 68
Part: SKIN — CRACKED (LT WING SLAT) · airframe 55,773 hrs · 27,078 cycles
LEFT WING #1 SLAT L/E NOSE SKIN @ ACTUATOR FTG ATTACH FASTENER HOLE; CRACK; MRK'D. / REPAIRD L/H WING #1 SEAT LEADING EDGE SKIN IAW B 737-700 SRM S7-42-01-2R-8
Part: CLEVIS — CRACKED (LT WING) · airframe 55,473 hrs · 26,885 cycles
LEFT WING DEFLECTION CONTROL RIB LOWER ATTACH POINT FOR THE WING SUPPORT ROD IS CRACKED OFF / ACCOMPLISHED A PERMANENT REPAIR REF EA NO: 1-A57-1997.
Part: BEAM — CRACKED (R1 DOOR) · airframe 55,469 hrs · 26,882 cycles
R1 DOOR HANDLE BOX LOWER BEAM CRACKED ON FORWARD OUTBOARD RADIUS. R&R R1 DOOR PER MM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 55,139 hrs · 26,681 cycles
R1 DOOR OUTSIDE EMERGENCY LIGHT TEST FAILED. R&R BATTERY PACK M1674 PER AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 55,139 hrs · 26,681 cycles
L1 DOOR UPPER EMERGENCY EXIT SIGN LIGHTS FAILED TEST. R&R BATTERY PACK M1674 PER AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 55,139 hrs · 26,681 cycles
RT EMERGENCY LIGHTS TEST FAILED BETWEEN ROW 3 TO ROW 6. R&R BATTERY PACK M1674 PER AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 55,139 hrs · 26,681 cycles
OVERHEAD BINS EXIT SIGN TEST FAILED. R&R BATTERY PACK M1674 PER AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 55,139 hrs · 26,681 cycles
LOWER EXIT SIGN IN FRONT OF G1 GALLEY TEST FAILED. R&R BATTERY PACK M1674 PER AMM.
Earlier reports · 2015–2018 · 39 reports
2018
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,752 hrs · 25,832 cycles
FRAME CRACKED AT BS 727E, BETWEEN STR 22L TO STR 23L. REPAIRED ANGLE IAW BOEING MESSAGE.
Part: LIGHT — LOOSE (CABIN) · airframe 53,603 hrs · 25,734 cycles
RT EMERGENCY FLOOR LIGHTING LOOSE AT ROW 1. R&R LIGHT PER CMM.
Part: VAPOR BARRIER — CRACKED (LT WHEEL WELL) · airframe 53,209 hrs · 25,474 cycles
CRACK IN VAPOR BARRIER LOWER LEFT; LEFT MAIN GEAR WHEEL WELL NEAR HYDRAULIC FUSE DECAL. (BETWEEN LBL 32.5 AND LBL 40.) / APPLIED INTERIM PATCH REPAIR TO 15' CRACK PER EA 1-757-15510. REPAIR APPLIED TO FWD SIDE OF VAPOR BARRIER. FOR DEFERRAL INFORMATION; SEE SRM 57-10-10-2R-2 PAR. 2.C. REPETITIVE INSPECTION REQUIRED:
Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 52,374 hrs · 24,927 cycles
L1 DOOR SLIDE GAUGE READS LOW. R&R SLIDE PER MT.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 51,872 hrs · 24,602 cycles
R1 DOOR EXIT LIGHT LENS MISSING. INSTALLED A NEW LENS IAW MM.
Part: LAMP — INOPERATIVE (ROW 17) · airframe 51,634 hrs · 24,440 cycles
LEFT EMERGENCY LIGHT INOPERATIVE AT SEAT ROW 17. REPLACED THE LAMPS IAW AMM.
Part: SWITCH — FAULTY (EMERGENCY LIGHTS) · airframe 51,570 hrs · 24,399 cycles
EMERGENCY LIGHT SWITCH FAULTY. R & R THE SWITCH IAW WDM & AMM.
Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 51,376 hrs · 24,280 cycles
FORWARD GALLEY LT EMERGENCY LIGHT BATTERY PACK FAILED A DEEP CYCLE CHECK. R & R THE BATTERY IAW AMM.
2017
Part: BATTERY — DISCHARGED (CABIN) · airframe 49,363 hrs · 22,983 cycles
L2 OVERHEAD DOOR EMERGENCY EXIT SIGN INOP. R&R BATTERY PER AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,363 hrs · 22,983 cycles
R2 DOOR EMERGENCY EXIT LIGHT INOP. R&R LIGHT ASSEMBLY PER MM.
Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 49,363 hrs · 22,983 cycles
R2 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. / R&R LIGHT PER AMM.
Part: DOUBLER — CRACKED (LOWER EXT FUSELA) · airframe 49,228 hrs · 22,894 cycles
GROUND POWER RECEPTACLE SURROUND DOUBLER IS CRACKED / CUT OUT DAMAGE AT GROUND POWER RECEPTACLE DOUBLES; NOT VERIFIED NO FURTHER DEFECTSNOTED. INSTALLED DOUBLE REPAIR IAW SRM 53-10-15-2R-4
Part: HANDLE — CRACKED (EMERGENCY EXIT) · airframe 49,228 hrs · 22,894 cycles
LT OVER WING EMERGENCY EXIT UPPER PULL HANDLE AND COVER PANEL 833 BZ CRACKED. R&R HANDLE ASSEMBLY IAW SOPM.
Part: STRAP — FRAYED (EMERGENCY EXIT) · airframe 49,228 hrs · 22,894 cycles
LT OVER WING EMERGENCY EXIT DOOR RED DOOR OPEN ASSIST STRAP FRAYED. R&R STRAP IAW SOPM.
Part: RAIL — CORRODED (FUSELAGE) · airframe 49,228 hrs · 22,894 cycles
FWD CARGO AFT BULK HEAD LWR RAIL AT STA 500D IS CORRODED / REMOVED AND REPLACED 1EA FWD CARGO AFT BULKHEAD LWR RAIL @ STA. 500D IAW B737 SRM 51-40-02-06 AND DWG 143A9481 SHEET 10
Part: STRAP — FRAYED (EMERGENCY EXIT) · airframe 49,228 hrs · 22,894 cycles
RT OVER WING EMERGENCY EXIT DOOR RED DOOR ASSIST STRAP FRAYED. R&R STRAP IAW SOPM.
Part: SUPPORT — BROKEN (FUSELAGE) · airframe 49,228 hrs · 22,894 cycles
RIGHT AC BAY AT STA 663 FAIRING SUPPORT ANGLE BROKEN AT AFT ATTACH FLANGE / REMOVED AND REPLACED BROKEN SUPPORT AND CLIP AT RH AC BAY STA663 IAWSRM51-40-02-0G-0STEP 7A AND DWG#149A7210
Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,228 hrs · 22,894 cycles
LT EMERGENCY LIGHT BULB INOP AT ROW 20. R&R BULB IAW AMM.
Part: RETAINER — LOOSE (R2 GIRT BAR) · airframe 47,827 hrs · 22,070 cycles
R2 DOOR SLIDE GIRT BAR RETAINER FOUND LOOSE. SECURED THE RETAINER IAW AMM.
2016
Part: BATTERY — FAILED (CABIN) · airframe 44,779 hrs · 20,263 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672. R & R BATTERY IAW AMM.
Part: BATTERY — FAILED (CABIN) · airframe 44,779 hrs · 20,263 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R & R BATTERY IAW AMM.
2015
Part: BATTERY — BROKEN (CABIN) · airframe 42,736 hrs · 19,047 cycles
LEFT EMER EXIT CEILING LIGHT BATTERY BROKEN AT M1668. R & R BATTERY IAW MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,714 hrs · 19,034 cycles
RIGHT OVERWING FWD EMER THRESHOLD LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 42,714 hrs · 19,034 cycles
R2 DOOR EMER EVAC SLIDE GIRT OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.
Part: LENS — LOOSE (CABIN) · airframe 42,714 hrs · 19,034 cycles
RIGHT OVERHEAD BIN EMERGENCY LIGHT LENS LOOSE AT ROW 6. SECURED LIGHT IAW SOPM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,714 hrs · 19,034 cycles
EMERGENCY LIGHT INOPERATIVE AT L732. RELAMPED LIGHT IAW AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,714 hrs · 19,034 cycles
EMERGENCY LIGHT INOPERATIVE AT L1063. RELAMPED LIGHT IAW AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,714 hrs · 19,034 cycles
EMERGENCY LIGHT INOPERATIVE AT L733. RELAMPED LIGHT IAW AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,714 hrs · 19,034 cycles
EMERGENCY LIGHT INOPERATIVE AT L6. RELAMPED LIGHT IAW AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,714 hrs · 19,034 cycles
EMERGENCY LIGHT INOPERATIVE AT L731. RELAMPED LIGHT IAW AMM.
Part: BATTERY PACK — BROKEN (CABIN) · airframe 42,714 hrs · 19,034 cycles
M1675 EMERGENCY BATTERY CHARGER BROKEN AT BS 328, STRINGER 1L. R & R BATTERY PACK IAW AMM.
Part: LATCH — BROKEN (L1 DOOR) · airframe 42,714 hrs · 19,034 cycles
L1 DOOR EMER EVAC SLIDE SHROUD LATCH BROKEN. R & R LATCH IAW SRM.
Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 42,714 hrs · 19,034 cycles
RIGHT MLG LOWER TRUNNION FITTING FACES CORRODED. R & R FITTING IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 42,714 hrs · 19,034 cycles
AFT CARGO FRAME CRACKED AT BS 727A, LBL 19. REPAIRED FRAME IAW EA.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,714 hrs · 19,034 cycles
INTERCOSTAL CRACKED AT STATION 927 TO 947, RBL 20. R & R INTERCOSTAL IAW SRM.
Part: PLATE — CORRODED (FUSELAGE) · airframe 42,714 hrs · 19,034 cycles
AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 907 - 927, RBL 21. R & R PLATE IAW SRM & DWG.
Part: FRAME — CRACKED (FUSELAGE) · airframe 42,714 hrs · 19,034 cycles
FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 42,714 hrs · 19,034 cycles
FRAME CRACKED AT BS 827, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 42,714 hrs · 19,034 cycles
FRAME CRACKED AT BS 500A, STRINGER 8R. REPAIRED FRAME IAW EA.