N743SW
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.
263 reports on file, 1999-01-16 – 2020-02-16.
Part: RADOME — DAMAGED (NOSE) · airframe 73,478 hrs · 43,468 cycles
**NOSE RADOME HAS COMPOSITE DAMAGE. / REMOVED AND REPLACED NOSE RADOME IAW AMM 53-52-00-400-801 STEPS 3.F(4)(7) AND G.(1)-(4);(6);(7);(9);(11)(H);(I);(J);(12);(14)-(16) (POS:ONLY; TAG NO:N/A; P/N OFF:1001002-7; S/N OFF:0309151; P/N ON:1001002-2; S/N ON:0402271C)
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,478 hrs · 43,468 cycles
EMERGENCY BATTERY PACKS IN POWER SUPPLIES M1669 WOULD NOT CHARGE. / R&R BATTERY PACK IAW AMM.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,478 hrs · 43,468 cycles
EMERGENCY BATTERY PACKS IN POWER SUPPLIES M1672 WOULD NOT CHARGE. / R&R BATTERY PACK IAW AMM.
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 73,478 hrs · 43,468 cycles
EMERGENCY BATTERY PACKS IN POWER SUPPLIES M1674 WOULD NOT CHARGE. / R&R BATTERY PACK IAW AMM.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,478 hrs · 43,468 cycles
EMERGENCY BATTERY PACKS IN POWER SUPPLIES M1675 WOULD NOT CHARGE. / R&R BATTERY PACK IAW AMM.
Part: DOUBLER — CORRODED (VHF ANTENNA) · airframe 73,478 hrs · 43,468 cycles
***CORROSION*** DOUBLER UNDER THE VHF ANTENNA AT STATION 727D + 10; BL 0; WL 150 HAS CORROSION. / REMOVED CORROSION FROM EXTERIOR SURFACE UNDER THE VHF ANTENNA AT BS 727D+10 BL 0 WL 150 PER SRM 51-10-02. REMOVED IN AREA OF 5.4' X 3.0' X .002' AND FOUND TO BE OUT DUE TO NO LIMITS SRM 51-10-02 #9. REPAIRED DAMAGE AT BS 727D+10; BL 0 WL 150 IAW ATS ER 20-01812 IR + SWA EA 1-753-36572 IR
Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 73,478 hrs · 43,468 cycles
FWD CARGO DOOR FORWARD CORNER THRESHOLD IS CRACKED / LOCATED AND DRILLED NEW REPLACEMENT SCUFF PLATE PART# 143A8331-3; PO# 777241; IAW-SRM-51-40-05-0G-0; DWG 143A8330; 80603U 2/11/20
Part: SKIN — CORRODED (BS 889) · airframe 73,478 hrs · 43,468 cycles
FUSELAGE EXTERNAL SKIN CORRODED AT BS. 889, BL 0. / REPAIRED SKIN IAW ER AND EA.
Part: ANGLE — CORRODED (BS 219) · airframe 73,478 hrs · 43,468 cycles
CLIP ANGLE CORRODED AT BS. 219, RBL 15. / REPAIRED ANGLE IAW ER AND EA.
Part: SKIN — CORRODED (BS 887) · airframe 73,478 hrs · 43,468 cycles
EVAL PEELING PAINT CORROSION AT BS 887 BL 0 WL 159 / REPAIRED DAMAGE AT BS 887 BL 0 ON SKIN IAW ATS ER 20-01674 REV IR AND SWA EA 1-753-36547 IR
Part: SKIN — CORRODED (BS 1016 BL0) · airframe 73,478 hrs · 43,468 cycles
EXTERIOR SKIN HAS PEELING PAINT (CORROSION) AT BS 1016 BL 0 AROUND DRAIN WL 186 / REPAIRED FUSELAGE SKIN AT STA 1016 BL 0 AROUND DRAIN WL 186 IAW EA 1-753-36560 REV IR AND ER 20-01675 REV IR. APPLIED DENT DOT TO AFFECTED AREA IAW SWA MPM 52.03.01.02 PAR. 3.
Part: STRAP — DAMAGED (TE FLAP FAIRING) · airframe 73,478 hrs · 43,468 cycles
#6 FLAP FAIRING AFT TAIL CONE SPLICE STRAP HAS DAMAGED HOLES / REMOVED AND REPLACED WITH NEW SPLICE STRAPS ON #6 FLAP FAIRING AFT TAIL CONE USING 2024 T3 .063 LOT # 5086648-1 IAW SRM 51-40-05; SRM 51-40-02 AND DWG 113A9352
Part: BAFFLE — CRACKED (BS 460-480) · airframe 73,478 hrs · 43,468 cycles
FORWARD CARGO COMPARTMENT L/H SIDE BAFFLE CRACKED BETWEEN BS. 460 TO BS. 480, LBL 21. / R&R BAFFLE PER SRM AND DWG.
Part: BAFFLE — CRACKED (BS 500B-500C) · airframe 73,478 hrs · 43,468 cycles
FORWARD CARGO COMPARTMENT L/H SIDE BAFFLE CRACKED BETWEEN BS. 500B TO BS. 500C, LBL 21. / R&R BAFFLE PER SRM AND DWG.
Part: BAFFLE — CRACKED (BS 440-460) · airframe 73,478 hrs · 43,468 cycles
FORWARD CARGO COMPARTMENT L/H SIDE BAFFLE CRACKED BETWEEN BS. 440 TO BS. 460, LBL 21. / R&R BAFFLE PER SRM & DWG.
Part: BAFFLE — CRACKED (BS 500C-500D) · airframe 73,478 hrs · 43,468 cycles
FWD CARGO COMPARTMENT L/H SIDE BAFFLE AT STA 500C-500D WL155 LBL21 IS CRACKED / FWD CARGO COMPARTMENT L/H BAFFLE AT STA 500C - 500D WL 155 LBL 21 IS CRACKED; REMOVED AND REPLACED WITH NEW PART ITEM # 143A7503-5; P.O. # 750993/6 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; AND BOEING DRAWING. 92679U 01/31/2020.
Part: BAFFLE — CRACKED (BS 500-500A) · airframe 73,478 hrs · 43,468 cycles
FORWARD CARGO COMPARTMENT L/H SIDE BAFFLE CRACKED BETWEEN BS. 500 TO BS. 500A. / R&R BAFFLE PER SRM & DWG.
Part: BAFFLE — CRACKED (BS 500A-500B) · airframe 73,478 hrs · 43,468 cycles
FORWARD CARGO COMPARTMENT L/H SIDE BAFFLE CRACKED BETWEEN BS. 500A TO BS. 500B, LBL 21. / R&R BAFFLE PER SRM AND DWG.
Part: WEB — CORRODED (BS 792-847) · airframe 73,478 hrs · 43,468 cycles
AFT CARGO COMPARTMENT LOWER SILL VERTICAL WEB CORRODED BETWEEN BS. 792 TO BS. 847, RBL 25. / R&R WEB IAW SRM AND DWG.
Part: DOUBLER — CORRODED (AIRPHONE ANTENNA) · airframe 73,478 hrs · 43,468 cycles
***CORROSION*** FWD CARGO COMPARTMENT AIRPHONE ANTENNA DOUBLER BS 500+8 BL0 WL 150 / REMOVED DAMAGED AIRPHONE ANTENNA DOUBLER AT FWD CARGO; STA 500+8 BL 0 & INSTALLED NEW DOUBLER P/N 7530980 PO 779986 IAW SRM 51-40-02-0G-0; DWG 143A3230 81146U 2/2/20
Part: ACCESS PANEL — DELAMINATED (LT WING) · airframe 73,478 hrs · 43,468 cycles
L/H WING LEADING EDGE ACCESS PANEL 521MB DELAMINATED AT CENTER OF THE PANEL. / REPAIRED PANEL IAW SRM.
Part: BEAM — CRACKED (R1 DOOR) · airframe 73,478 hrs · 43,468 cycles
R1 DOOR #5 BEAM CRACKED. / R&R DOOR IAW AMM.
Part: SHIELD — CORRODED (BS 492-500A) · airframe 73,478 hrs · 43,468 cycles
FORWARD CARGO RH AFT DOOR SHIELD CORRODED BETWEEN BS. 492 TO BS. 500A, RBL 24. / R&R SHIELD IAW SRM AND DWG.
Part: STRAP — CORRODED (AFT CARGO) · airframe 73,478 hrs · 43,468 cycles
***CORROSION*** AFT CARGO DOOR STRAP STA 767 - 867 RBL 19 WL 156 / CORROSION ON AFT CARGO DOOR CUTOUT STRAP BS 767-867 RBL 19 WL 156 FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 FIG 103 DETAIL J. REMOVED; LOCATED; DRILLED AND INSTALLED NEW STRAP PER SRM 51-40-02; SRM 51-40-05 AND BOEING DRAWING 146A8120
Part: STRAP — CORRODED (AFT CARGO) · airframe 73,478 hrs · 43,468 cycles
***CORROSION*** AFT CARGO FLOOR STRAP STA 887 LBL 15 - RBL 17 WL 160 / AFT CARGO FLOOR STRAP STA 887 LBL 15 - RBL 17 WL 160 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS STATEMENT IN SRM; REMOVED DAMAGED FLOOR STRAP & INSTALLED NEW STRAP IAW SRM 51-40-02-0G-0; DWG 146A7500 81146U 2/14/20
Part: STIFFENER — CORRODED (BS 1030 S2L-R) · airframe 73,478 hrs · 43,468 cycles
***CORROSION*** ON 'L' ANGLE BRACKET AT STA 1030; BETWEEN STR2L AND 2R; LBL 9 - RBL 9 (EXTERNAL) WL 302 / REMOVED AND REPLACED STIFFNER ON STA. 1030; BETWEEN STR 2L AND 2R IN REFERENCE TO BDW #148A3110 AND SRM 51-40-02-0G-0 P/N 69-69859-2 OUT OF LIMITS DUE TO NO SRM LIMITS
Part: CARGO TRACK — CORRODED (AFT CARGO BAY) · airframe 73,478 hrs · 43,468 cycles
***CORROSION*** AFT CARGO LH FLOOR RAIL STA 887 - 947 LBL 3 WL 160 / AFT CARGO L/H FLOOR RAIL STA. 887-STA. 947 LBL 3 WL 160 HAS CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 PAGE 6 4.(A) FIGURE 103 DETAIL D. REMOVED AND REPLACED NEW PART; P.N. 147A7501-13; ITEM # 7530392; P.O.# 779986/2 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; AND BOEING DRAWING 147A7500 REV. C. 92679U 02-08-2020
Part: SHIELD — CORRODED (FWD CARGO) · airframe 73,478 hrs · 43,468 cycles
FORWARD CARGO RH FORWARD DOOR SHIELD CORRODED BETWEEN BS. 420 TO BS. 440, RBL 24. / R&R SHIELD IAW SRM AND DWG.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 73,478 hrs · 43,468 cycles
AFT CARGO INTERCOSTAL AUXILIARY SILL CORRODED BETWEEN BS. 767 TO BS. 787, RBL 7. / R&R INTERCOSTAL IAW SRM & DWG.
Part: CHANNEL — CORRODED (BS 727-767) · airframe 73,478 hrs · 43,468 cycles
AFT CARGO RH ZEE CHANNEL CORRODED BETWEEN BS. 727 TO BS. 767, RBL 22. / R&R ZEE CHANNEL IAW SRM AND DWG.
Part: CHANNEL — CORRODED (BS 400-500D) · airframe 73,478 hrs · 43,468 cycles
FORWARD CARGO L/H ZEE CHANNEL CORRODED BETWEEN BS. 400 TO BS. 500D, LBL 24. / R&R ZEE CHANNEL PER SRM AND DWG.
Part: THRESHOLD — CORRODED (BS 792-849) · airframe 73,478 hrs · 43,468 cycles
AFT CARGO THRESHOLD CORRODED BETWEEN BS. 792 TO BS. 849, RBL 27. / R&R WEB IAW DWG & SRM.
Part: SHIELD — CORRODED (BS 849-867) · airframe 73,478 hrs · 43,468 cycles
AFT CARGO DOOR AFT SHIELD CORRODED BETWEEN BS. 849 TO BS. 867. / R&R SHIELD IAW SRM AND DWG.
Part: CHANNEL — CORRODED (BS 867-947) · airframe 73,478 hrs · 43,468 cycles
AFT CARGO RH ZEE CHANNEL CORRODED BETWEEN BS. 867 TO BS. 947, RBL 22. / R&R ZEE CHANNEL IAW SRM AND DWG.
Part: BULKHEAD — CORRODED (BS 947) · airframe 73,478 hrs · 43,468 cycles
AFT CARGO LOWER AFT BULKHEAD CORRODED AT BS. 947, BETWEEN LBL 15 TO RBL 17. / R&R BULKHEAD IAW SRM AND DWG
Part: CHANNEL — CORRODED (BS 727-849) · airframe 73,478 hrs · 43,468 cycles
AFT CARGO L/H ZEE CHANNEL CORRODED BETWEEN BS. 727 TO BS. 849, LBL 22. / R&R ZEE CHANNEL PER SRM & DWG.
Part: SHIELD — CORRODED (BS 767-792) · airframe 73,478 hrs · 43,468 cycles
AFT CARGO DOOR FORWARD SHIELD BETWEEN BS. 767 TO BS. 792, RBL 22. / R&R SHIELD IAW SRM AND DWG.
Part: THRESHOLD — CORRODED (BS 792-849 RBL27) · airframe 73,478 hrs · 43,468 cycles
CORROSION AFT CARGO THRESHOLD STA 792 - 849 RBL 27 WL 156 / REMOVED CORROSION IN AN AREA OF 1.8' X .8' X .011 DEEP; FOUND TO BE OUT OF LIMITS DUE TO NO ESTABLISHED SRM LIMITS; REMOVED WEB BS 792-849 RBL 27; LOCATED AND DRILLED NEW WEB; INSTALLED WEB IAW DWG 146A8340 & SRM 51-40-02
Part: SKIN — CORRODED (BS 905-927) · airframe 73,478 hrs · 43,468 cycles
FUSELAGE SKIN AROUND THE WATER SERVICE DOOR CORRODED BETWEEN BS. 905 TO BS. 927, BETWEEN STR. 28R TO STR. 26R. / REPAIRED SKIN PER ER AND EA.
Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 73,478 hrs · 43,468 cycles
AFT CARGO AFT CORNER SCUFF PLATE CRACKED / REPAIRED AFT CARGO AFT CORNER SCUFF PLATE IAW EA NO: 1-A53-2076 REV 11
Part: SKIN — CORRODED (BS 927 S23-25L) · airframe 73,478 hrs · 43,468 cycles
***CORROSION*** ON THE EXTERIOR FUSELAGE SKIN STA 927 BETWEEN STR 23L TO 25L WL 153 / REMOVED CORROSION ON EXTERIOR FUSELAGE SKIN @ STA. 927 BETWEEN STR. 23L TO STR 25L; WL 153 IN AREA OF. 16.0'L X 4.0'W X .003'D OUT OF LIMITS PER SRM 53-00-01-1A-1. REPAIRED DAMAGE PER ER# 20-01507 REV IR AND EA# 1-A753-36525 REV IR
Part: STRIP — DAMAGED (AFT CARGO) · airframe 73,478 hrs · 43,468 cycles
AFT CARGO FWD FLOOR PANEL 140AF FWD SUPPORT CAPSTRIP DAMAGED / RECEIVED NEW PART ITEM 7253171 P.O. 779727. OK TO INSTALL INSP 389 2-13-20 INSTALLED CAPSTRIP AT AFT CARGO FWD FLOOR PANEL 140 AF FWD SUPPORT; IAW SOPM 20-50-01. 59189U 02-13-20
Part: DOUBLER — CRACKED (BS 663 BULKHEAD) · airframe 73,478 hrs · 43,468 cycles
STA 663 L/H VAPOR BARRIER WEB GSE DUCT DOUBLER LBL15 WL155 IS CRACKED / RECEIVED NEW STA 663 L/H VAPOR BARRIER WEB GSE DUCT DOUBLER AT LBL 15 WL 155 ITEM 7570583 P.O. # 778796 MPN 111A1512UI. LOCATED AND DRILLED NEW DOUBLER IAW SRM 51-40-05-0G-0 AND DWG 111A1512 REV.-. 92058U 01/28/20
Part: SKIN — CORRODED (BS 917) · airframe 73,478 hrs · 43,468 cycles
FUSELAGE SKIN AROUND LAV VENT CORRODED AT BS. 917, BETWEEN STR. 21L TO STR. 22L. / REPAIRED SKIN PER SRM, ER, AND EA.
Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 73,478 hrs · 43,468 cycles
LEFT MAIN WHEEL WELL HORIZONTAL PRESSURE DECK WEB CRACKED AT BS. 663+2, LBL 32. / REPAIRED WEB IAW SRM.
Part: BARRIER — DISLODGED (CENTER WING) · airframe 73,478 hrs · 43,468 cycles
*CUSTOMER REQUEST*REPAIR BS 663 LOWER VAPOR BARRIER L/H (EXISTING REPAIR AT LBL 12 WL 150 IS DISBANDED.) / REPAIRED DAMAGE A LBL 12 AND WL 150 ON BS 663.75 LOWER VAPOR L/H IAW 737 SRM 57-10-10-2R-2 AND SRM 51-70-04-2R-10 AND SRM 51-70-04-2R-0
Part: SKIN — CORRODED (BS 972) · airframe 73,478 hrs · 43,468 cycles
FUSELAGE SKIN AROUND BODY DRAIN CORRODED AT BS. 972, BETWEEN STR. 26L TO STR. 27L. / REPAIRED SKIN PER SRM, ER, AND EA.
Part: FLOORBOARD — DAMAGED (NOT REPORTED) · airframe 73,478 hrs · 43,468 cycles
FLOOR BOARD 242BF HAS DAMAGE ON FWD OUTBD CORNER. / FLOOR BOARD 242BF DAMAGE ON FWD OUTBD CORNER REPAIRED IAW SRM 53-00-50-2R-6. DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4F. NO DELAMINATION ALLOWED
Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 73,478 hrs · 43,468 cycles
LEFT HAND OUTBOARD AFT FLAP INBOARD TRAILING EDGE DELAMINATED / REPAIRED DELAMINATION DAMAGE ON I/B TRAILING EDGE OF L/H O/B AFT FLAP IAW 737 57-53-01-2R-4 AND SRM 51-70-10-2R-4 AND SRM 51-70-10-2R-0
Earlier reports · 1999–2019 · 214 reports
2019
Part: ACTUATOR — FAULTY (NLG LOCK) · airframe 73,243 hrs · 43,310 cycles
DIVERSION-------------------ON TAKE OFF, LANDING GEAR LEVER MOVED TO UP, ALL GEAR CAME UP. ALL LIGHTS OUT. WHEN LANDING GEAR LEVER WAS MOVED TO OFF, THE NOSE GEAR EXTENDED AND BOTH RED AND GREEN "NOSE GEAR" LIGHTS ILLUMINATED. / R&R NOSE LANDING GEAR LOCK ACTUATOR PER AMM.
Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 71,792 hrs · 42,412 cycles
R1 DOOR SLIDE GAUGE WINDOW OUT OF POSITION. REPOSITIONED SLIDE PER MT.
Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 71,001 hrs · 41,920 cycles
R1 DOOR SLIDE PRESSURE GAUGE SAT EVERY LOW IN SLIDE CASE WINDOW. REPOSITIONED SLIDE IAW MT.
Part: BATTERY PACK — FAILED (CABIN) · airframe 70,082 hrs · 41,320 cycles
EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M1670. R&R BATTERY PACK PER MM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 70,082 hrs · 41,320 cycles
EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M1675. R&R BATTERY PACK PER MM.
Part: FLAP — DELAMINATED (RT WING) · airframe 70,082 hrs · 41,320 cycles
RT WING OUTBOARD TRAILING EDGE AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 70,082 hrs · 41,320 cycles
EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M1672. R&R BATTERY PACK PER MM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 70,082 hrs · 41,320 cycles
EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M1669. R&R BATTERY PACK PER MM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 70,082 hrs · 41,320 cycles
EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PACK PER MM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 70,082 hrs · 41,320 cycles
EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M1668. R&R BATTERY PACK PER MM.
Part: FLAP — DELAMINATED (RT WING) · airframe 70,082 hrs · 41,320 cycles
RT WING OUTBOARD TRAILING EDGE AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 70,082 hrs · 41,320 cycles
EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M1674. R&R BATTERY PACK PER MM.
2018
Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 69,342 hrs · 40,830 cycles
R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 68,465 hrs · 40,237 cycles
R1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
Part: RIB — CRACKED (LT MLG DOOR) · airframe 67,921 hrs · 39,891 cycles
LT MAIN GEAR MIDDLE DOOR STIFFENER RIB CRACKED AT LOWER FORWARD OF ATTACH BRACKET. R&R DOOR IAW AMM.
Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 67,744 hrs · 39,773 cycles
LT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.
Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 67,744 hrs · 39,773 cycles
RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.
Part: GIRT BAR — LOOSE (R2 DOOR SLIDE) · airframe 67,377 hrs · 39,532 cycles
R2 DOOR SLIDE GIRT BAR RESTRAINT ATTACHMENT LOOSE. REPAIRED THE GIRT BAR ASSEMBLY PER EA.
Part: LIGHT — BROKEN (CABIN) · airframe 66,833 hrs · 39,193 cycles
CENTER CABIN OVERHEAD EMERGENCY EXIT LIGHT BROKEN. R&R LIGHT IAW AMM.
Part: SUPPORT CHANNEL — CRACKED (LT WING) · airframe 66,833 hrs · 39,193 cycles
LT WING AFT PANEL SUPPORT CHANNEL FOR PANEL 561AB CRACKED ON INBOARD AFT EDGE. R&R CHANNEL IAW SRM.
Part: BRACKET — CRACKED (BS 663) · airframe 66,833 hrs · 39,193 cycles
FORWARD SIDE DIAGONAL BRACKET CRACKED AT BS 663, IN INBOARD END. R & R BRACKET IAW SRM AND DWG.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 66,833 hrs · 39,193 cycles
FORWARD VERTICAL ANGLE CRACKED AT BS 663, RBL 6.15. R&R STIFFENER IAW SRM AND DWG.
Part: BULKHEAD — DELAMINATED (BS 663) · airframe 66,833 hrs · 39,193 cycles
BULKHEAD DELAMINATED AT BS 663. REPAIRED THE BULKHEAD IAW SRM.
2017
Part: RIB — BUCKLED (HORIZONTAL STAB) · airframe 66,833 hrs · 39,193 cycles
RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB WEB BUCKLED AT HSS 150.5. R & R RIB IAW SRM AND DWG.
Part: CHANNEL — CORRODED (BS 360) · airframe 66,833 hrs · 39,193 cycles
E&E BAY CHANNEL TIE CORRODED AT BS 360, RBL 10. R & R THECHANNEL TIE IAW SRM AND DWG.
Part: SKIN — CORRODED (FUSELAGE) · airframe 66,833 hrs · 39,193 cycles
E&E COMPARTMENT SKIN CORRODED BETWEEN BS 350 TO BS 360, BETWEEN RBL 10 TO LBL 10. REPAIRED SKIN IAW EA.
Part: RIB — BUCKLED (HORIZONTAL STAB) · airframe 66,833 hrs · 39,193 cycles
RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB WEB BUCKLED AT BS 142. R & R THE RIB IAW SRM AND DWG.
Part: SUPPORT ANGLE — CRACKED (RT MLG WW) · airframe 66,833 hrs · 39,193 cycles
VAPOR BARRIER SUPPORT ANGLE CRACKED AT BS 663, RBL 9. REPAIRED BARRIER IAW EA.
Part: SUPPORT ANGLE — CRACKED (LT MLG WW) · airframe 66,833 hrs · 39,193 cycles
CENTER WING SECTION VAPOR BARRIER SUPPORT ANGLE CRACKED AT BS 663, LBL 8. REPAIRED ANGLE IAW EA.
Part: RETAINER — CORRODED (FUSELAGE) · airframe 65,745 hrs · 38,472 cycles
UPPER SURFACE OF PRESSURE DECK RETAINER CORRODED AT BS 669, RBL 62. R&R RETAINER IAW SRM & DWG.
Part: STRAP — CRACKED (CARGO DOOR) · airframe 65,745 hrs · 38,472 cycles
FORWARD CARGO BAY DOOR SUPPORT STRAP CRACKED AT BS 440. R&R STRAP IAW SRM.
Part: SKIN — CRACKED (LE SLAT) · airframe 65,745 hrs · 38,472 cycles
LT WING NR 3 SLAT LEADING EDGE NOSE SKIN CRACKED AT ACTUATOR ATTACH RIB. REPAIRED SKIN IAW SRM.
Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 65,745 hrs · 38,472 cycles
RT WHEEL WELL BEADED WEB CRACKED AT BS 663.75+15, BETWEEN RBL 30 TO RBL 63. REPAIRED WEB PER ER & EA.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 65,745 hrs · 38,472 cycles
STIFFENER CRACKED AT BS 663 JUST OUTBOARD OF LT PACK EXHAUST. REMOVED STIFFENER PER SRM & DWG.
Part: SUPPORT ANGLE — CRACKED (LT WNG TO BDY) · airframe 64,074 hrs · 37,500 cycles
LEFT FORWARD WING TO BODY FAIRING FORWARD CENTER SUPPORT ANGLE CRACKED. R & R THE SUPPORT ANGLE IAW SRM.
Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 64,074 hrs · 37,500 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1975. R & R THE BATTERY IAW MM.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 64,074 hrs · 37,500 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669. R & R THE BATTERY PACK IAW MM.
2016
Part: SLIDE — LOOSE (CABIN) · airframe 62,980 hrs · 36,862 cycles
L2 DOOR SLIDE SKIRT LOOSE. SECURED SLIDE ASSEMBLY IAW SIP.
Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 62,672 hrs · 36,683 cycles
L2 DOOR EMERGENCY ESCAPE SLIDE OUT OF POSITION. REPOSITIONED SLIDE ASSEMBLY IAW AMM.
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 62,579 hrs · 36,629 cycles
R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MAINTENANCE.
Part: DOOR — CRACKED (RT MLG) · airframe 61,957 hrs · 36,258 cycles
RT MLG CENTER SHOCK STRUT DOOR CRACKED. R & R DOOR IAW AMM.
Part: LENS — UNSECURE (EXIT SIGN) · airframe 60,254 hrs · 35,286 cycles
OVERWING CEILING EMER EXIT SIGN LIGHT LENS FELL OFF. REINSTALLED LENS IAW SIP.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 60,232 hrs · 35,273 cycles
LOWER SIDEWALL, RT EMER EXIT SIGN, LIGHT BULB INOPERATIVE. RELAMPED SIGN IAW AMM.
2015
Part: PLATE — CRACKED (LT WING) · airframe 60,232 hrs · 35,273 cycles
LEFT WING TE PANEL 551GB, WIGGLE PLATE CRACKED. R & R WIGGLE PLATE IAW SRM & DWG.
Part: PLATE — CRACKED (RT WING) · airframe 60,232 hrs · 35,273 cycles
RIGHT WING TE PANEL 651GB, CRACKED WIGGLE PLATE. R & R WIGGLE PLATE IAW SRM & DWG.
Part: WEB — CORRODED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
FUSELAGE WEB CORRODED AT STATION 986 - 1016, RBL 38. REPAIRED WEB IAW SRM.
Part: GUSSET — CRACKED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
GUSSET CRACKED AT STATION 500D, STRINGER 21L. R & R GUSSET IAW SRM.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
L1 DOOR THRESHOLD SUPPORT Z ANGLE CORRODED, BETWEEN BS 312 - 344. REPAIRED Z ANGLE IAW SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
FLOORBEAM CORRODED AT STATION 986, BL 0 TO RBL 53. REPAIRED BEAM IAW SRM.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
RIGHT CREASE BEAM CORRODED AT STATION 300 - 324. REPAIRED BEAM IAW SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
FLOORBEAM CORRODED AT STATION 986, BL 0 TO LBL 53. REPAIRED BEAM IAW SRM.
Part: ATTACH FITTING — CORRODED (GIRT BAR) · airframe 60,232 hrs · 35,273 cycles
L1 DOOR SLIDE FWD GIRT BAR ATTACH FITTING CORRODED. R & R FITTING IAW SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
INTERCOSTAL CRACKED AT STATION 312 - 328, RBL 30. R & R INTERCOSTAL IAW SRM.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
LEFT CREASE BEAM CORRODED AT STATION 947 - 990. REPAIRED BEAM IAW SRM.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
RIGHT CREASE BEAM CORRODED AT STATION 947 - 987, RBL 53. REPAIRED BEAM IAW SRM.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
AFT CARGO BAY FLOOR SUPPORT TIE DOWN FITTING, CORRODED AT BS 747 LT. R & R FLOOR SUPPORT IAW SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
INTERCOSTAL CRACKED AT STATION 344 - 360, RBL 12. R & R INTERCOSTAL IAW SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
MAIN CABIN FLOORBEAM, CORRODED AT BS 294, BETWEEN BL 0 TO RBL 10. REPAIRED FLOORBEAM IAW SRM.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
LEFT CREASE BEAM CORRODED AT STATION 308 - 357. REPAIRED BEAM IAW SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
INTERCOSTAL CRACKED AT STATION 312 - 324, LBL 48. R & R INTERCOSTAL IAW SRM.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
RIGHT CREASE BEAM CORRODED AT STATION 294 - 355. REPAIRED BEAM IAW SRM.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
AFT CARGO BAY FLOOR SUPPORT CORRODED, BETWEEN BS 727 - 727B+3, BETWEEN STRINGER 26L - 25L. R & R SUPPORT IAW SRM & DWG.
Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
AFT CARGO BAY FLOOR STRUCTURE CORRODED, BETWEEN BS 727 - 727B. REPAIRED FLOOR STRUCTURE IAW SRM.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
AFT CARGO BAY, LT Z ANGLE CORRODED, BETWEEN BS 727D - 827. R & R Z ANGLE IAW SRM.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
FORWARD CARGO PIT FLOOR SUPPORT CORRODED AT BS 500C. R & R FLOOR SUPPORT IAW SRM.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
AFT CARGO BAY RT Z ANGLE CORRODED, BETWEEN BS 727 - 76. R & R Z ANGLE IAW SRM & DWG.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
FORWARD CARGO BAY, FLOOR SUPPORT TIE DOWN FITTING CORRODED, AT BS 727D, LBL 17.50. R & R SUPPORT IAW SRM.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
AFT CARGO BAY FLOOR SUPPORT TIE DOWN FITTING, CORRODED AT BS 790 LT. R & R FLOOR SUPPORT IAW SRM.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
FORWARD CARGO PIT, Z ANGLE CORRODED AT BS 500C. R & R Z ANGLE IAW SRM.
Part: SHIELD — CORRODED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
FORWARD CARGO COMPARTMENT FLOOR SHIELD CORRODED, AT BS 420 RT SIDE WEB AT CARGO FLOOR LINE. R & R FLOOR SHIELD IAW SRM & DWG.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
AFT CARGO BAY FLOOR SUPPORT STRUCTURE CORRODED, BETWEEN BS 767 - 787, STRINGER 25R. R & R SUPPORT IAW SRM & DWG.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 60,232 hrs · 35,273 cycles
FORWARD CARGO DOOR CUT OUT DOOR, SILL WEB CORRODED. R & R SILL WEB IAW SRM & DWG.
Part: ANGLE — CRACKED (RT MLG WW) · airframe 58,991 hrs · 34,531 cycles
RIGHT WW BULKHEAD L ANGLE CRACKED AT BS 663. R & R L ANGLE IAW DWG.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,991 hrs · 34,531 cycles
FRAME CRACKED AT BS 867, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,991 hrs · 34,531 cycles
FRAME CRACKED AT BS 400, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,991 hrs · 34,531 cycles
FRAME CRACKED AT BS 480, STRINGER 8R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,991 hrs · 34,531 cycles
FRAME CRACKED AT BS 787, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 58,991 hrs · 34,531 cycles
FRAME CRACKED AT BS 727B, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: POST — CRACKED (FUSELAGE) · airframe 58,991 hrs · 34,531 cycles
NUMBER 3 LEFT FLIGHT DECK WINDOW FRAME ON E - F POST, SECOND LOWER CORNER FASTENER CRACKED. REPAIRED POST IAW EA.
Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 58,438 hrs · 34,214 cycles
L2 DOOR EMER EVAC SLIDE PRESS LOW. R & R SLIDE IAW MT.
Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 58,353 hrs · 34,165 cycles
R2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.
Part: BATTERY PACK — FAILED (CABIN) · airframe 58,006 hrs · 33,961 cycles
FORWARD CABIN EMER BATTERY PACKS FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 58,006 hrs · 33,961 cycles
AFT CABIN EMER BATTERY PACKS FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.
Part: SLIDE — UNSECURE (L1 DOOR) · airframe 57,630 hrs · 33,744 cycles
L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER, DID NOT DEPLOY & STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.
2014
Part: SLIDE — UNSECURE (L1 DOOR) · airframe 55,944 hrs · 32,789 cycles
L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY & STILL OPERATIONAL. REINSTALLED SLIDE IAW TC.
Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 54,543 hrs · 32,006 cycles
LEFT OVERWING EMERGENCY EXIT SIGN COVER LOOSE. R & R COVER IAW MM.
Part: LIGHT — INOPERATIVE (R2 DOOR) · airframe 54,543 hrs · 32,006 cycles
R2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW MM.
Part: STRIP — DELAMINATED (CABIN) · airframe 54,369 hrs · 31,908 cycles
RT EEPLS STRIP DELAMINATED. R & R LT EEPLS STRIP ASSEMBLY.
Part: STRIP — DELAMINATED (CABIN) · airframe 54,369 hrs · 31,908 cycles
LT EEPLS STRIP DELAMINATED. R & R LT EEPLS STRIP ASSEMBLY.
Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 54,369 hrs · 31,908 cycles
RIGHT WW VERTICAL PRESS WEB CRACKED AT BS 663, BETWEEN RBL 29 TO RBL 42. REPAIRED WEB IAW EA.
Part: DOUBLER — CRACKED (LT MLG WW) · airframe 54,369 hrs · 31,908 cycles
LT WW VERTICAL PRESS WEB DOUBLER CRACKED AT BS 663, LBL 41. REPAIRED DOUBLER IAW SRM.
2013
Part: FLAP — DELAMINATED (LT WING) · airframe 53,660 hrs · 31,475 cycles
LT WING OTBD AFT FLAP DELAMINATED ON TE APPROXIMATELY 9" FROM INBD CORNER. R & R AFT FLAP SA-M.
Part: SKIN — CRACKED (RT WING) · airframe 53,655 hrs · 31,474 cycles
NR 5 LE SLAT HAS CRACKED AT ACTUATOR ATTACH CUTOUT. REPAIRED SLAT IAW SWA EA.
Part: SLAT — CRACKED (LT WING) · airframe 53,655 hrs · 31,474 cycles
LT WING NR 2 SLAT CRACKED THRU A FASTENER AT THE ACTUATOR ATTACH POINT. R & R SLAT IAW MM.
Part: BRACKET — CRACKED (LT WING) · airframe 53,655 hrs · 31,474 cycles
LT WING AFT SPAR BULB SEAL BRACKET CRACKED ABOVE WING PANEL 551GB. R & R BRACKET IAW SRM.
Part: FLAP — DELAMINATED (LT WING) · airframe 53,655 hrs · 31,474 cycles
LT WING OTBD AFT FLAP DELAMINATED AT TE AREA. REPAIRED IAW SWA EA.
Part: CONNECTOR — BROKEN (CABIN) · airframe 53,279 hrs · 31,261 cycles
RT PASSENGER CABIN EMERGENCY AISLE LIGHT CONNECTOR BROKEN AT STATION 752. R & R CONNECTOR IAW WDM & MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,279 hrs · 31,261 cycles
LT STOW BIN MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE BETWEEN ROW 9 TO ROW 12. R & R BATTERY PACK IAW MM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 53,279 hrs · 31,261 cycles
RT STOW BIN MOUNTED EMERGENCY LIGHTS INOPERATIVE BETWEEN ROWS 3 TO ROW 6. R & R BATTERY IAW AMM.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,279 hrs · 31,261 cycles
LT NR 1 WINDOW FRAME CRACKED AT UPPER OTBD CORNER. R & R FRAME IAW ACO.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 53,279 hrs · 31,261 cycles
CABIN FLOOR STRUCTURE ATTACH ANGLE CRACKED AT STATION 727B, RBL 45.5. R & R ANGLE IAW SRM & DRAWING.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,279 hrs · 31,261 cycles
SEAT TRACK CRACKED AT STATION 727B, RBL 45.5. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,279 hrs · 31,261 cycles
SEAT TRACK CRACKED AT STATION 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,279 hrs · 31,261 cycles
SEAT TRACK CRACKED AT STATION 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 53,279 hrs · 31,261 cycles
SEAT TRACK CRACKED AT STATION 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,279 hrs · 31,261 cycles
FLIGHT DECK FRAME WEB CRACKED AT STATION 259.5, STRINGER 9R. REPAIRED WEB IAW EA.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 53,279 hrs · 31,261 cycles
LT HORIZONTAL STAB RIB AT STATION 92.70 CRACKED AT 2ND FROM FWD VERTICAL STIFFENER. REPAIRED RIB IAW SRM.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 53,279 hrs · 31,261 cycles
LT HORIZONTAL STAB RIB AT STATION 129.5 CRACKED AT 3RD FROM FWD VERTICAL STIFFENER. REPAIRED RIB IAW SRM.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 53,279 hrs · 31,261 cycles
LT HORIZONTAL STAB RIB AT STATION 92.70 CRACKED AT 3RD FROM FWD VERTICAL STIFFENER. REPAIRED RIB IAW SRM.
Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 53,279 hrs · 31,261 cycles
RT HORIZONTAL STAB RIB CRACKED AT STATION 92.70 AT 3RD FROM FWD VERTICAL STIFFENER. REPAIRED STIFFENER IAW SRM.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 53,279 hrs · 31,261 cycles
LT HORIZONTAL STABILIZER RIB AT STATION 92.70 CRACKED ON LOWER FLANGE NEAR MOST FWD VERTICAL STIFFENER. REPAIRED RIB IAW EA.
Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 53,279 hrs · 31,261 cycles
RT HORIZONTAL STAB RIB CRACKED AT STATION 92.70 AT FWD VERTICAL STIFFENER. REPAIRED STIFFENER IAW SRM.
Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 53,279 hrs · 31,261 cycles
RT HORIZONTAL STAB RIB CRACKED AT STATION 92.70 AT 2ND FROM FWD VERTICAL STIFFENER. R & R STIFFENER IAW SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,279 hrs · 31,261 cycles
FRAME CRACKED AT STATION 500A, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,279 hrs · 31,261 cycles
FRAME CRACKED AT STATION 747, STRINGER 8R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,279 hrs · 31,261 cycles
FRAME CRACKED AT STATION 480, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,279 hrs · 31,261 cycles
FRAME CRACKED AT STATION 907,STRINGER 8R. R & R FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,279 hrs · 31,261 cycles
FRAME CRACKED AT STATION 400, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,279 hrs · 31,261 cycles
FRAME CRACKED AT STATION 380, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,279 hrs · 31,261 cycles
FRAME CRACKED AT STATION 500A, STRINGER 8R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,279 hrs · 31,261 cycles
FRAME CRACKED AT STATION 727B, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,279 hrs · 31,261 cycles
FRAME CRACKED AT STATION 440, STRINGER 8L. REPAIRED FRAME IAW SW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,279 hrs · 31,261 cycles
FRAME CRACKED AT STATION 480, STRINGER 8R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,279 hrs · 31,261 cycles
FRAME CRACKED AT STATION 727B, STRINGER 8R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,279 hrs · 31,261 cycles
FRAME CRACKED AT STATION 787, STRINGER 8R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 53,279 hrs · 31,261 cycles
FRAME CRACKED AT STATION 500C, STRINGER 8R. REPAIRED FRAME IAW EA.
Part: LIGHT — INOPERATIVE (LT WING) · airframe 53,279 hrs · 31,261 cycles
LT WING EMERGENCY LIGHT INOPERATIVE. R & R LIGHT IAW MM.
Part: LIGHT — INOPERATIVE (RT WING) · airframe 53,279 hrs · 31,261 cycles
RT WING EMERGENCY LIGHT INOPERATIVE. R &R LIGHT IAW MM.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 51,666 hrs · 30,310 cycles
FLIGHT DECK NR 3 WINDOW FRAME RIGHT SIDE CRACKED AT SECOND LOWER FWD CORNER FASTENER HOLE COMMON TO THE E-F POST. REPAIRED FRAME PER EA.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 51,666 hrs · 30,310 cycles
LEFT NR 1 WINDOW FRAME CRACKED AT THE UPPER AFT CORNER. REPAIRED FRAME IAW EA.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 51,666 hrs · 30,310 cycles
FLIGHT DECK NR 3 WINDOW FRAME LEFT SIDE CRACKED AT THE SECOND LOWER FWD CORNER FASTENER HOLE COMMON TO THE E-F POST. REPAIRED FRAME PER EA.
Part: FRAME — CRACKED (NR 2 COWLING) · airframe 51,666 hrs · 30,310 cycles
NR 2 ENGINE FAN FRAME B1 FLANGE CRACKED AT UPPER LEFT FIRE DETECTOR LOWER MOUNT. REMOVED AND REPLACED NR 2 ENGINE INBD FAN COWL PER M/M.
Part: RUB STRIP — CRACKED (NR 1 PYLON) · airframe 51,301 hrs · 30,101 cycles
RUBSTRIP'S ON PANEL'S 431AL & 431AR ARE CRACKED. REMOVED AND REPLACED RUBSTRIPS PER SRM.
2012
Part: FLAP — DELAMINATED (LT WING) · airframe 49,488 hrs · 28,962 cycles
LEFT WING O/B AFT FLAP INBOARD AFT CORNER DELAMINATED ON UPPER SIDE. REPAIRED AFT FLAP IAW SRM.
Part: FITTING — LOOSE (GIRT BAR) · airframe 49,488 hrs · 28,962 cycles
R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING IAW AMM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 49,488 hrs · 28,962 cycles
RIGHT HORIZONTAL STABILIZER LOWER SKIN AT STA 147. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 49,488 hrs · 28,962 cycles
RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101. REPAIRED SKIN IAW SRM & EA.
Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 49,488 hrs · 28,962 cycles
LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147. REPAIRED SKIN IAW SRM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,368 hrs · 27,700 cycles
DURING SCHEDULED MV2 CHECK FOUND, L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
2011
Part: SKIN — CRACKED (HORIZ STAB) · airframe 47,236 hrs · 27,623 cycles
DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED AT STA 101.90. REPAIRED SKIN IAW SRM.
Part: LIGHT — WORN (CABIN) · airframe 47,236 hrs · 27,623 cycles
DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS WORN BETWEEN ROW 1 TO ROW 2. REMOVED AND REPLACED EEPLS PER MM.
Part: HOOK — LOOSE (GIRT BAR) · airframe 46,118 hrs · 26,979 cycles
DURING SCHEDULED CV CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK IAW MM.
Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 46,118 hrs · 26,979 cycles
DURING SCHEDULED CV CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.
Part: LENS — CRACKED (R1 DOOR) · airframe 46,118 hrs · 26,979 cycles
DURING SCHEDULED CV CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE COVER LENS CRACKED. REMOVED AND REPLACED LENS PER MT AND MM.
Part: LIGHT — LOOSE (CABIN) · airframe 45,924 hrs · 26,869 cycles
L1 DOOR EEPLS LENS LOOSE. REMOVED AND REPLACED EEPLS IAW EA.
Part: ELEVATOR — PUNCTURED (RIGHT) · airframe 45,132 hrs · 26,405 cycles
DURING SCHEDULED MV2 CHECK FOUND, RT ELEVATOR PUNCTURED. REMOVED AND REPLACED ELEVATOR PER MM.
Part: COVER — BROKEN (CABIN) · airframe 44,746 hrs · 26,196 cycles
FWD EEPLS COVER BROKEN. REMOVED AND REPLACED COVER PER MM.
2010
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 40,278 hrs · 23,608 cycles
DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 460, RBL 8. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: FITTING — CORRODED (GIRT BAR) · airframe 40,278 hrs · 23,608 cycles
DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.
Part: LIGHT — BROKEN (CABIN) · airframe 40,278 hrs · 23,608 cycles
DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 40,278 hrs · 23,608 cycles
DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 32.40. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 40,278 hrs · 23,608 cycles
DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 6.14. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: LENS — CRACKED (CABIN) · airframe 40,278 hrs · 23,608 cycles
DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.
Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 40,278 hrs · 23,608 cycles
DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 54.60. REMOVED AND REPLACED SHEAR TIE PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 40,278 hrs · 23,608 cycles
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 40,278 hrs · 23,608 cycles
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 40,278 hrs · 23,608 cycles
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 40,278 hrs · 23,608 cycles
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER EA.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,278 hrs · 23,608 cycles
DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 40,278 hrs · 23,608 cycles
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER EA.
2009
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 40,278 hrs · 23,608 cycles
DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 974 TO BS 992, RBL 50. REPAIRED BEAM PER SRM.
Part: ACTUATOR — FAULTY (NLG) · airframe 38,334 hrs · 22,370 cycles
DIVERSION / DECLARED EMERGENCY. AFTER T/O FROM MDW NOTICED HIGH VIBRATION FROM NLG OBSERVED NOSE GEAR WOULD NOT RETRACT, RECYCLED LANDING GEAR AND GOT NORMAL INDICATION. DIVERTED TO BWI. REMOVED AND REPLACED NOSE GEAR LOCK ACTUATOR AND NOSE GEAR LOCK VALVE ACTUATOR PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,293 hrs · 21,731 cycles
DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT BULBS INOP. RELAMPED PER MM.
Part: FITTING — CRACKED (CENTER WING) · airframe 37,202 hrs · 21,675 cycles
DURING SCHEDULED 10Y CHECK, FOUND LT WING CENTER BOX SHEAR FITTING CRACKED AT BS 540, LBL 40. REMOVED AND REPLACED FITTING PER SRM.
Part: FITTING — CRACKED (CENTER WING) · airframe 37,202 hrs · 21,675 cycles
DURING SCHEDULED 10Y CHECK, FOUND RT WING CENTER BOX SHEAR FITTING CRACKED AT BS 540, RBL 32. REMOVED AND REPLACED FITTING PER SRM.
Part: FITTING — CRACKED (CENTER WING) · airframe 37,202 hrs · 21,675 cycles
DURING SCHEDULED 10Y CHECK, FOUND LT WING CENTER BOX SHEAR FITTING CRACKED AT BS 540, LBL 6. REMOVED AND REPLACED FITTING PER SRM.
Part: FITTING — CRACKED (CENTER WING) · airframe 37,202 hrs · 21,675 cycles
DURING SCHEDULED 10Y CHECK, FOUND RT WING CENTER BOX SHEAR FITTING CRACKED AT BS 540, RBL 54. REMOVED AND REPLACED FITTING PER SRM.
Part: FITTING — CRACKED (CENTER WING) · airframe 37,202 hrs · 21,675 cycles
DURING SCHEDULED 10Y CHECK, FOUND RT WING CENTER BOX SHEAR FITTING CRACKED AT BS 540, RBL 15. REMOVED AND REPLACED FITTING PER SRM.
Part: FITTING — CRACKED (CENTER WING) · airframe 37,202 hrs · 21,675 cycles
DURING SCHEDULED 10Y CHECK, FOUND LT WING CENTER BOX SHEAR FITTING CRACKED AT BS 540, LBL 15. REMOVED AND REPLACED FITTING PER SRM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,122 hrs · 21,637 cycles
DURING SCHEDULED CV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.
2008
Part: GASPER FAN — FAULTY (E&E BAY) · airframe 35,588 hrs · 20,713 cycles
DURING FLIGHT GASPER FAN MADE A LOUD GRINDING NOISE. REMOVED AND REPLACED GASPER FAN PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,026 hrs · 20,386 cycles
DURING SCHEDULED MV2 CHECK, FOUND RT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: FITTING — CORRODED (LT WING) · airframe 34,947 hrs · 20,345 cycles
DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG CORRODED. REPAIRED FITTING PER SWA EA.
Part: FITTING — CORRODED (RT WING) · airframe 34,947 hrs · 20,345 cycles
DURING SCHEDULED MV2 CHECK, FOUND RIGHT MLG TRUNNION FITTING LUG CORRODED. REPAIRED FITTING PER SWA EA.
Part: LUG — CORRODED (RT MLG) · airframe 34,947 hrs · 20,345 cycles
DURING SCHEDULED MV2 CHECK, FOUND RIGHT MLG TRUNNION LUG CORRODED. REPAIRED LUG PER SWA EA.
Part: LUG — CORRODED (LT MLG) · airframe 34,947 hrs · 20,345 cycles
DURING SCHEDULED MV2 CHECK, FOUND LEFT MLG TRUNNION LUG CORRODED. REPAIRED LUG PER SWA EA.
2007
Part: ENGINE — FAILED (NR 2) · airframe 32,596 hrs · 18,897 cycles
AIR TURNBACK/DECLARED EMERGENCY/INFLIGHT SHUTDOWN NR 2 ENGINE FAILED ON CLIMBOUT. REMOVED AND REPLACED NR 2 ENGINE PER MT.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 29,839 hrs · 17,281 cycles
DURING SCHEDULED 8Y CHECK, FOUND R1 DOOR CUTOUT FWD LOWER FRAME CRACKED AT BS 295, RBL 54. REPAIRED FRAME PER SRM.
Part: FITTING — CORRODED (FUSELAGE) · airframe 29,839 hrs · 17,281 cycles
DURING SCHEDULED 8Y CHECK, FOUND INTERCOSTAL FITTING CORRODED AT BS 288 TO BS 294, RBL 19. REPAIRED FITTING PER SWA EA.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,839 hrs · 17,281 cycles
DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 39. REPAIRED FLOORBEAM PER SRM.
2006
Part: BATTERY PACK — FAILED (CABIN) · airframe 28,710 hrs · 16,655 cycles
DURING SCHEDULED HC1 CHECK, RT OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: STIFFENER — CRACKED (MLG W/W) · airframe 28,710 hrs · 16,655 cycles
DURING SCHEDULED HC1 CHECK, FOUND RT FWD MLG W/W STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER PER SRM.
Part: BATTERY — FAILED (CABIN) · airframe 28,710 hrs · 16,655 cycles
DURING SCHEDULED HC1 CHECK, RT AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 26,337 hrs · 15,287 cycles
DURING SCHEDULED HC2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP INBOARD T/E DELAMINATED. REPAIRED FLAP PER SWA EA.
Part: LIGHT — MISSING (CABIN) · airframe 26,337 hrs · 15,287 cycles
DURING SCHEDULED HC2 CHECK, FOUND EEPLS STRIP MISSING AT ROW 3 DEF. INSTALLED EEPLS PER MM.
Part: LIGHT — CRACKED (CABIN) · airframe 26,337 hrs · 15,287 cycles
DURING SCHEDULED HC2 CHECK, FOUND FWD RIGHT EMERGENCY EXIT LIGHT ASSY CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.
Part: SLIDE — DISLODGED (L1 DOOR) · airframe 25,866 hrs · 15,024 cycles
L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.
2005
Part: STRIP — DAMAGED (CABIN) · airframe 25,085 hrs · 14,616 cycles
DURING SCHEDULED MV2 CHECK, FOUND PHOTOLUMINESCENT STRIP DAMAGED AT FWD END. REMOVED AND REPLACED STRIP PER MM.
Part: SLIDE — OUT OF ADJUST (L1 & R2 DOOR) · airframe 23,876 hrs · 13,927 cycles
DURING SCHEDULED HC1 CHECK, FOUND L1 & R2 DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM.
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 22,828 hrs · 13,353 cycles
R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. RE-INSTALLED SLIDE PER MM.
Part: BATTERY — INTERMITTENT (EMERGENCY LIGHT) · airframe 22,615 hrs · 13,235 cycles
CABIN EMERGENCY BULLNOSE LIGHTS INTERMITTENT DURING FLIGHT. REMOVED AND REPLACED BULLNOSE LIGHTS BATTERY PACK PER MM.
Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 22,549 hrs · 13,195 cycles
R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR SLIDE PER MM.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,221 hrs · 13,003 cycles
DURING SCHEDULED RON, FOUND FWD LT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.
2004
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,339 hrs · 10,850 cycles
DURING SCHEDULED 5Y CHECK, FOUND FWD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
2003
Part: ROD END — WORN (RT ELEVATOR) · airframe 16,655 hrs · 9,911 cycles
DURING SCHEDULED C4 CHECK, SWA SI 11038-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB ROD END HARDWARE PER MM.
Part: COVER — CRACKED (CABIN) · airframe 166,555 hrs · 9,911 cycles
DURING SCHEDULED C4 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED IN CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM.
2002
Part: TAB — VIBRATION (BOTH ELEVATORS) · airframe 12,987 hrs · 7,912 cycles
DURING CRUISE NOTICED A VERY HIGH FREQUENCY VIBRATION, COULD BE FELT IN ALL CONTROLS AS WELL AS ALL SURFACES IN COCKPIT. REMOVED AND REPLACED BOTH ELEVATOR TRIM TABS PER MM.
Part: BUSHING — WORN (LT ELEVATOR) · airframe 11,957 hrs · 7,331 cycles
DURING SCHEDULED C4 CHECK, SWA SI 11075-55, FOUND LT ELEVATOR TAB NR 3 AND NR 4 HINGES WORN. REMOVED AND REPLACED TAB BUSHINGS PER MM.
Part: BUSHING — WORN (RT ELEVATOR) · airframe 11,957 hrs · 7,331 cycles
DURING SCHEDULED C4 CHECK, SWA SI 11075-55, FOUND RT ELEVATOR TAB NR 2 HINGE WORN. REMOVED AND REPLACED NR 2 HINGE BUSHING PER MM.
Part: COVER — CRACKED (CABIN) · airframe 11,945 hrs · 7,325 cycles
DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 8. REMOVED AND REPLACED COVER PER MM.
Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 11,100 hrs · 6,832 cycles
FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.
Part: SLIDE — OUT OF ADJ (ENTRY DOOR) · airframe 10,857 hrs · 6,685 cycles
DURING SCHEDULED C3 CHECK, FOUND FWD SVC AND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT PLAY OUT OF ADJUST. ADJUSTED SLIDE PER MM.
2001
Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,825 hrs · 6,661 cycles
DURING SCHEDULED PM CHECK, FOUND 12 EEPLS INOP. RECONNECTED EEPLS WIRING AND REMOVED AND REPLACED LIGHT TRACKS PER MM.
Part: BULKHEAD — CANNING (FUSELAGE) · airframe 10,124 hrs · 6,240 cycles
DURING SCHEDULED SERVICE CHECK, (SI 11152-53) FOUND AFT SIDE BS 1016 BULKHEAD HAS MULTIPLE DAMAGE, DENTS AND OIL CANNING BETWEEN LT & RT STRINGERS 1 & 4, ABOVE FIRST STRAP & BELOW 2ND STRAP. MX FERRY TO PAE FOR BAC EVALUATION. OCT 21, 2001 REPAIRED BULKHEAD PER BOEING DOCUMENT 6-1171-RE-1013.
Part: WIRE — EXPOSED (CABIN) · airframe 9,165 hrs · 5,689 cycles
EEPLS WIRES EXPOSED AT ROW 8. SECURED EEPLS WIRES PER MM.
Part: COVER — CRACKED (CABIN) · airframe 8,560 hrs · 5,294 cycles
DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT VARIOUS LOCATIONS FROM ROW 1 TO ROW 19. R&R TRACK COVERS PER MM.
Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 7,683 hrs · 4,794 cycles
FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EVAC SLIDE ASSY PER MM.
2000
Part: SLIDE — DISLODGED (PAX DOOR) · airframe 6,588 hrs · 4,114 cycles
DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY SAGGING. ADJUSTED SLIDE ASSY PER MM.
Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 5,652 hrs · 3,543 cycles
DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE GIRT ASSY OUT OF ADJUST. RE-INSTALLED SLIDE ASSY PER MM.
Part: COVER — CRACKED (ROW 1)
DURING SCHEDULED C4 CHECK, FOUND EEPLS TRACK COVER TRACK CRACKED AT ROW 1. REMOVED AND REPLACED TRACK COVER PER MM.
1999
Part: SLIDE — OUT OF POSITION (SERVICE DOOR)
DURING SCHEDULED BC3 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE PRESSURE IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.
Part: LINK — BROKEN (RT MLG)
RT MLG SEVERE VIBRATION ON LANDING. UPPER TORSION LINK BROKE. BOEING, ENGINEERING, QC AND SWA MX ALL ON SITE. INCIDENT STILL UNDER INVESTIGATION.
Part: BATTERY CHARGER — INOP (CABIN)
DURING SCHEDULED CHECK, FOUND CABIN MID FLOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED CHARGER/BATTERY UNIT AND OP CHECKED PER BOEING M/M.
Part: BATTERY CHARGER — INOP (CABIN)
DURING SCHEDULED RON CHECK, FOUND MID CABIN FLOOR LIGHTS INOP. REPLACED CHARGER/BATTERY ASSEMBLY PER BOEING MM.