N734SA
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2018-10-11 – 2018-10-11 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2018-10-11 – 2018-10-11 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
F/A REQUESTS PLEASE CHECK SLIDE/GIRT AT AFT SVC DOOR<[01] REPOSITIONED SLIDE ASSY IAWMM 25-66-01 AND MT 725-61-06
L/H OVER WING EMERGENCY EXIT LIGHT INOP<[01] RELAMPED L/H OVER WING EMERGENCY EXIT WINDOW LIGHT PER AMM 33-21-00 OPS CHECKED GD.;[02] VERIFIED RELAMP/OPS CHECK REF AMM 33-21-00 AT LEFT OVER-WING EXIT ROW;[03] VERIFIED RELAMP/OPS CHECK REF AMM 33-21-00 AT LEFT OVER-WING EXIT ROW
EMERGENCY EXIT LIGHT INOP AT BULLNOSE ABOVE SEAT 14 CBA<[01] RAR SEAT 14ABC EMERGENCY AREA LIGHT IAW AMM 33-51-03;[02] CW INSP OF RR SEAT 14ABC EMERGENCY AREA LIGHT IAW AMM 33-51-03
EMERGENCY LIGHT LENS IS LOOSE AT SEAT 11-12 CBA<[01] REATTACHED SEAT 11-12ABC EMERGENCY LIGHT LENS IAW SIP;[02] CORRECTION AS FOLLOWS. REATTACHED SEAT 11-12 ABC EMERGENCY LIGHT LENS IAW AMM 33-51-03;[03] VERIFIED EMERGENCY LIGHT LENS @ ROWS 11-12 ABC AMM 33-51-03;[04] CW
L/H OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP<[01] REPLAMPED OVERWING EMERGENCY EXIT LIGHT IAW AMM 33-51-04
FWD GALLEY SERVICE DOOR SLIDE GAUGE NOT COMPLETELY VISIBLE. REPOSITIONED FWD GALLEY SERVICE DOOR SLIDE IN COMPARTMENT PER MT725-61-06
CLIP-DEFLECTION CONTROL RIB IS CRACKED AT L/H WING TRAILING PANEL JUST OUTBOARD OF NR 3 FLAP TRACK. REMOVED AND REPLACED CLIP-DEFLECTION CONTROL RIB AT L/H WING TRAILING PANEL JUST OUTBOARD OF NR 3 FLAP TRACK PER SRM 51-40-02.
LH OVERWING EMERGENCY EXIT LIGHT HAS ONE BULB INOP. / [01] RESCUED LH OVERWING EMERGENCY EXIT LIGHT IAW AMM 33-51-04
SUPPLEMENTAL INFORMATION: SLIDE OUT OF POSITION ; / [01] REPOSITION SLIDE TO LATCH VELCRO TO THE SLIDE CASE PER AMM 25-66-00
RH OUTBD AFT FLAP; DELAMINATED ON INBD UPPER SURFACE. (HONEYCOMB IS SHOWING) ; / [01] REMOVED RH OUTBOARD AFT FLAP ASSY. PER AMM 27-51-22.; [02] INSTALLED RH OUTBOARD AFT FLAP ASSY.PER AMM 27-51-22; [03] REMOVED AND REPLACED T/E O/B AFT FLAP TRACKS #1;2;3;4 PER M/M 27-51-26
PLACARD IN F/O SIDE EMERGENCY EXIT ROW KEEPS FALLING OFF. ; / R+R EMERGENCY EXIT SIGN PER AMM33-51-01
FLIGHT ATTENDANT REPORTS FORWARD SERVICE DOOR GIRT BAR RETAINING HOLDER/CLIP IS LOOSE. ; / SECURED BRACKET HARDWARE PER AMM 25-66-02.
R/H EMERGENCY EXIT DOOR LIGHT INOP ; / REMOVED AND REPLACED LIGHT ASSEMBLY FUSE REF AMM 33-21-00
FOUND CORROSION ON AFT CARGO AFT SCUFF PLATE PANEL. REMOVED AND INSTALLED NEW PLATE AT AFT CARGO COMPT REF B737700 SRM 5140020G0.
L/H STAB INSPAR RIB ASSY NO.4 AT STA 120.30 FWD LWR EDGE CRACKED / CUT OUT DAMAGE AREA; FABRICATED AND INSTALLED REPAIR AT L/H STAB RIB ASSY NO.4 STA 120.30 FWD LOWER EDGE PER RES-WI 2017205-5 REV P.1 AND IR AND SWA EA 21-155-00999 REV IR
MAIN CABIN FLOOR PANEL 241DF BOTTON SIDE COMPOSITE DAMAGE AT 3 LOCATION / CLEANED FLOOR PANEL 241DF. REMOVED DAMAGE NO CORE DAMAGE NO WATER FOUND. INSTALLED A PERMANENT REPAIR ON BOTTOM SIDE OF PANEL3 PLACERS AS PER B737 SRM 53-00-50-2R-1 MATERIAL USED PO# 1480720 PO# 1692653.
MAIN CABIN WL 208.1 STA 540 BETWEEN BL 0 TO RBL 24 CHANNEL CRACKED. REMOVED N REPLACED CHANNEL BL0 TO RBL 24 STA 540 MAIN CABIN WL 208.1 REF B737700 SRM 5140020G0 CHANNEL INTERCOS PART NO. 7530771
VERTICAL STAB DORSAL FIN FORWARDMOST RIB CRACKED. REMOVED AND REPLACED VERTICAL STAB DORSAL FIN FORWARDMOST RIB AS PER B737700 NDT PART 6 510000 PROC 23. BC 166317; SRM 5140020G0.
MAIN CABIN FLOOR PANEL 241AF TOP LAYER DELAMINATED / CLEANED AND REPAIRED SMALL AREAS OF TOP SURFACE DAMAGE ON MAIN CABIN FLOOR PANEL 241AF CAUSED BY CARPET REMOVAL AS PER B737 SRM 53-00-50-2R-1 MATERIALS USED PO# 1486720 AND PO#1692653
FOWARD CARGO LOWER DOOR CUT OUT AFT CONNER SCUFF PLATE IS CRACK RECIEVED SERVICEABLE REPAIRED AFT CONNER SCUFF PLATE PO# 1713374 AS PER B737 SRM 5330152R1 REPAIR 1. JL WELDING INC.
MAIN CABIN FLOOR PANEL 231XF TOP LAYER DELAMINATED / REPAIRED DAMAGED AREA AT MAIN CABIN FLOOR PANEL 231XF TOOP LAYER. REF B737-7 SRM 53-00-50-2R-1
CRACK INDICATION FOUND AT FASTENER AT R-1 DOOR CUTOUT BETWEEN STA 291.5 AND STA 294.5 BETWEEN STR 8R AND STR 9R. SEE FIG 4 AT FASTENER SHOWING TYPICAL CRACK. / ACCOMPLISHED INTERIM REPAIR PER RES-W1 2017205-2 REV P.1; P.2; IR AND EA 21-153-00875 IR AT R-1 DOOR CUT OUT BETWEEN STA 291.5 AND STA 294.5 BETWEEN STR 8R AND 9R.
L/H STAB INSPAR RIB ASSY NO. 5 AT STAB STA 129.50 STIFFENER NO. 3 CRACKED / REMOVED AND REPAIRED L/H HORIZONTAL STAB. NO.5 RIB AT STA 129.50 STIFFENER NO.3 AS PER B737-700 SRM 55-10-09-2R-4 REP 4 FIG 202 AND DWG NO. 55100003. REV B.
MAIN CABIN FLOOR PANEL 232SF TOP LAYER DELAMINATED / CLEANED AND REPAIRED PANEL #232SF AS PER B737-900 ER SRM 53-00-50-2R-1. MATERIALS USED FABRIC P/O #1480720 RESIN P/O 1692653
FWD CARGO COMPARTMENT FLOOR PANEL 120CF IS DETERIORATED REMOVED; FABRICATED & INSTALLED FLOOR PANEL #120CF FWD CARGO COMP. AS PER REF B737 700 AMM 255201201801
FWD CARGO COMPARTMENT FLOOR PANEL 120AF IS DETERIORATED REMOVED; FABRICATED & INSTALLED FLOOR PANEL #120AF FWD CARGO COMP AS PER REF B737 700 AMM 255201201801
RH HORIZONTAL STAB ILIZER LE FAIRING CRACKED @ RIB # 4 MKD DOT. REMOVED AND REPLACED RH HORIZONTAL STAB LE RIB # 4 AS PER B7377 SRM 514002OG0 AND DWG #186A1001.
RH HORIZONTAL STABILIZER LE FAIRING CRACKED @ RIB # 5 MKD DOT. REMOVED AND REPLACED RH HORIZONTAL STAB LE RIB #5 AS PER B7377 SRM 5140020G0 AND DWG#186A1001.
AFT CARGO COMPARTMENT FLOOR PANEL 140AF IS DETERIORATED REMOVED; FABRICATED AND INSTALLED FLOOR PANEL 140 AF AT AFT CARGO AS PER B737700 AMM 255210000801; AMM 255201201801 AND AMM 255210400801
AFT CARGO COMPARTMENT FLOOR PANEL 140BF IS DETERIORATED REMOVED; FABRICATED AND INSTALLED FLOOR PANEL 140BF AT AFT CARGO AS PER B737700 AMM 255210000801; AMM 255201201801 AND AMM 255210400801
LEFT WING REAR SPAR FIXED TE LOWER SUPPORT BRACKET CRACKED INB OF MLG FWD TRUNNION MKD DOT. REMOVED AND REPLACE PLATE ASSY-WIGGLE AT LT WING IB OF MLG TRUNNION PER BOEING 737700 SRM 5140020G0.
L/H MAIN WHEEL WELL PRESSURE PANEL UPPER SURFACE IS DISBONDED AT 665667; LBL 6670. WL 203. REMOVED AND INSTALLED NEW CUSP WEB PANEL; CUSP GUSSET AND SEALS AT LH MAIN WHEEL PRESSURE PANEL UPPER SURFACE STA 663.75 TO STA 685 LBL 6670 WL 203 IAW B737700 SRM 5140020G0.
EMERGENCY EXIT SIGN LOOSE. / TIGHTENED LOOSE SCREWS @ EMERGENCY EXIT SIGN PER AMM 20-50-11
CABIN CREW REPORTS FWD SERVICE DOOR SLIDE FALLING OUT. REPOSITIONED FWD SERVICE DOOR SLIDE, IAW WIC 725-61-06.
FWD ENTRY DOOR SLIDE LATCH ASSY DISENGAGED. R & R FWD ENTRY DOOR SLIDE, IAW WORK INSTRUCTION 725-61-06 ICT 551469 P/N OFF/ON 63550-101 S/NOFF 0426F, S/NON 0285F.
AFT SECTRON OF EGRESS LIGHTS INOP. R&R AFT LEFT BATTERY PACK, AS PER AMM 33-51-06.
EMERGENCY EXIT STRIP LIGHTING COVER LOOSE/OFF. ROW 6 L/H SIDE LENS MISSING 26975 BULL NOSE / INSTALLED LENS HOUSING ASSEMBLY PER MM.
EMERGENCY EXIT STRIP LIGHTING COVER LOOSE/OFF. ROW 6 L/H SIDE LENS MISSING 26975 BULL NOSE / INSTALLED LENS HOUSING ASSEMBLY PER MM.
FORWARD ENTRY CENTER EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW AMM.
R/H EMERGENCY EXIT AISLE LIGHTS INOP BETWEEN SEAT ROW 16 TO ROW 17. / R&R POWER SUPPLY IAW AMM.
R1 DOOR ESCAPE SLIDE EMERGENCY HANDLE COVER OUT OF POSITION. REPOSITIONED SLIDE IAW MT.
FORWARD LT EMERGENCY EXIT LIGHTS INOP AT LOCATION M1674. R&R BATTERY PACK IAW AMM.
ALL FORWARD R/H EMERGENCY EXIT LIGHTS INOP AT LOCATION M1675. R&R BATTERY PACK IAW AMM.
FLOOR PANEL 231YF APPEARS TO BE DISBONDING / REPAIRED FLOOR PANEL 231YF IAW AMM 53-21-00; SRM 53-00-50; AND DWG #144A5810-4
FLOOR PANEL 241EF APPEARS TO BE DISBONDING / REPAIRED 241EF IAW AMM 53-21-00; SRM 53-00-50; AND DWG# 144A5810-10
R2 DOOR EMERGENCY EXIT LIGHT HOUSING DAMAGED. R&R LIGHT HOUSING IAW AMM.
FLOOR PANEL 241BF APPEARS TO BE DISBONDING / REPAIRED FLOOR PANEL 241BF IAW AMM 53-21-00; SRM 53-00-50; AND DWG #144A5810-3T
CREASE BEAM WEB IS CRACKED AT LIGHTNING HOLE; BS 469 RBL 65; WL 208 / REMOVED CRACK ON CREASE BEAM WEB LIGHTNING HOLE EDGE AT BS 469; RBL 65; WL 208 IAW SRM 53-30-13-1A-1 STEP 4A (1)(A) & SRM 51-10-02-0G-0. AFTER EVALUATE REWORK AREA IT WAS FOUND WITHIN LIMITS IAW SRM 53-30-13-1A-1 STEP 4A (E)(A) FIG 103 DETAIL A. APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW 53-30-13-1A-1 STEPS 2C (1) & 2C(2). ACCOMPLISHED A HFEC INSP TO REWORKED AREA IAW 737 NDIM PT6 51-00-00 PROC 23; NO CRACKS NOTED.
PANEL 191D HAS A DELAMINATED DENT ON THE EXTERNAL SURFACE; IN THE CORE AREA. / DELAMINATED DENT ON THE EXTERNAL SURFACE HAS BEEN REPAIRED ON PANEL 191D IAW SRM 51-70-05-2R-2 59313U 05-09-19
LT MAIN WHEEL WELL PRESSURE PANEL UPPER SURFACE DEBONDED BETWEEN BS. 665 TO BS. 667, BETWEEN LBL 66 TO LBL 70. REPAIRED PANEL PER ER & EA.
SHEAR TIE CRACKED AT BS. 887 BETWEEN STR. 17L TO STR. 16L. R&R SHEAR TIE PER SRM & DWG.
***CORROSION*** ON L/H OVER WING EXIT LOWER SILL WEB ATTACH ANGLE BS 616-639 LBL68 WL221. / REMOVED AND REPLACED L/H OVERWING EXIT; LOWER SILL WEB ATTACH ANGLE WITH NEW ANGLE AT BS616-639 LBL 68 WL221 SRM 51-10-02-0G-0 SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 SRM 51-20-01-0G-0 BOEING DWG 411A2820 AND 411A2854 13656R 11MAY19
CREASE BEAM WEB CORRODED BETWEEN BS. 380 TO BS. 400, LBL 67. REPAIRED CREASE BEAM WEB IAW EA & ER.
CREASE BEAM INNER CHORD CORRODED BETWEEN BS. 618 TO BS. 664, LBL 65. R&R INNER CHORD IAW SRM AND DWG.
CREASE BEAM WEB UPPER ATTACH ANGLE CORRODED AT BS. 668, RBL 67. R&R ANGLE IAW SRM & DWG.
MAIN WHEEL WELL ON PRESSURE DECK SHEAR TIE CORRODED BETWEEN BS. 665 TO BS. 668, BETWEEN RBL 65 TO RBL 68. R&R SHEAR TIE PER SRM AND DWG.
CREASE BEAM INNER CHORD CORRODED BETWEEN BS. 673 TO BS. 727+5, RBL 65. REPAIRED INNER CHORD IAW SRM & DWG.
CREASE BEAM WEB CORRODED BETWEEN BS. 710 TO BS. 713, RBL 65. REPAIRED CREASE BEAM WEB IAW EA & ER.
MAIN WHEEL WELL ON PRESSURE DECK SHEAR TIE CORRODED BETWEEN BS. 665 TO BS. 668, BETWEEN LBL 65 TO LBL 68. R&R SHEAR TIE IAW SRM & DWG.
UNDERSIDE OF CREASE BEAM WEB CORRODED BETWEEN BS. 658 TO BS. 655, LBL 65. REPAIRED WEB PER EA AND ER.
STRAP CORRODED BETWEEN BS. 291 TO BS. 294, STR. 5R. R&R STRAP IAW SRM & DWG.
SEAT TRACK CORRODED BETWEEN BS. 578 TO BS. 727A+6.5, RBL 25. R&R SEAT TRACK IAW SRM AND DWG.
SEAT TRACK CORRODED BETWEEN BS. 552 TO BS. 727B, RBL 45. R&R SEAT TRACK SRM AND DWG.
SEAT TRACK CORRODED AT BS. 520, LBL 45. REPAIRED SEAT TRACK IAW SRM & DWG.
FRAME CRACKED AT BS. 312, STR. 5L, ABOVE UPPER SILL WEB. REPAIRED FRAME PER EA & ER.
CRACKED INTERCOSTAL AT BS 278 STR 14 R/H I/B SIDE. / REPAIRED CRACKED INTERCOSTAL BS 278 STR 14 R/H I/B SIDE IAW EA# 1-753-34896 REV IR AND ER# 19-03070 REV IR.
SEAT TRACK CORRODED BETWEEN BS. 407 TO BS. 471, LBL 45. R&R SEAT TRACK PER SRM & DWG.
COCKPIT FLOOR DAMAGED ON UPPER SURFACE BS257 270 RBL4-LBL 15 WL208. / REPAIRED DAMAGED COCKPIT FLOOR ON UPPER SURFACE BS 257-270 RBL 4- LBL 15 WL 208 PER EA 1-753-34787 REV IR AND ATS ER #19-02962 REV IR
EMERGENCY EXIT LIGHT DAMAGED ON G4 GALLEY. R&R LIGHT IAW AMM.
RT HORIZ STAB FWD UPPER SLIDE SEAL IS CRACKED. / REMOVED AND REPLACED R/H HORIZONTAL STAB UPPER FRONT SPAR CRACKED SLIDING SEAL IAW AMM 53-31-31-000-802 PAR 2D AND E AND 53-31-31-400-802 PAR 3EAND F. 57048U 08MAY19
LT HORIZONTAL STABILIZER LEADING EDGE CRACKED RIB AT LEADING EDGE STA. 150.20. R&R RIB IAW SRM AND DWG.
#1 ENGINE PYLON PANEL 431ER LWR CORNER IS DISBONDED. / #1 ENGINE BYLON PANEL 431ER WITH LOWER CORNER DISBOND WAS REPLACED WITH A SERVICEABLE PYLON PANEL PER SRM 51-10-02-0G-0 PARA 9.A.(1)
RT BIN EMERGENCY LIGHT LENSES DAMAGED AT ROW #11. R&R LENS IAW AMM & SIP.
AFT CARGO BAY FLOOR SPLICE STRAP AT BS727D+6 RBL10 TO LBL10 WL156 HAS AREAS OF CORROSION / RECIEVED NEW ACB FLOOR SPLICE STRAP FOR B.S 727D+6 ON PO# 724358 PART WILL BE INSTALLED ON CUST. CARD # JPANEL-141-CLOSE
AFT CARGO BAY FLOOR SPLICE STRAP AT BS772 RBL10 TO LBL10 WL156 HAS AREAS OF CORROSION / RECEIVED NEW ACB FLOOR SPLICE STRAP B.S 772 ON PO# 717082 NEW PART WILL BE INSTALLED ON CUST CARD # JPANEL-141-CLOSE
FORWARD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT BAFFLE CLIP CRACKED AT BS. 500C, LBL 24. R&R BAFFLE CLIP IAW SRM & DWG.
AFT CARGO BAY SHIELD CORRODED BETWEEN BS. 767 TO BS. 787, RBL 23. R&R SHIELD PER SRM AND DWG.
FORWARD CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT BAFFLE CLIP CRACKED AT BS. 500C, LBL 24. R&R BAFFLE CLIP IAW SRM & DWG.
AFT CARGO BAY VERTICAL WEB CORRODED BETWEEN BS. 927 TO BS. 947, RBL 3 ON FORWARD END. R&R VERTICAL WEB PER SRM & DWG.
RT BIN EMERGENCY LIGHT LENSES DAMAGED AT ROW #8. R&R LENS IAW AMM & SIP.
LT BIN EMERGENCY LIGHT LENSES DAMAGED AT ROW #4. R&R LENS IAW AMM & SIP.
LT BIN EMERGENCY LIGHT LENSES DAMAGED AT ROW #1. R&R LENS IAW AMM & SIP.
AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS. 747 TO BS. 807, LBL 23. R&R SUPPORT IAW SRM.
AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS. 727 TO BS. 767, RBL 23. R&R SUPPORT PLATE PER SRM AND DWG.
FORWARD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT BAFFLE CLIP CRACKED ON THE FORWARD SIDE AT BS. 500C, RBL 24. REPAIRED BAFFLE CLIP PER SRM AND DWG.
FORWARD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT BAFFLE CLIP CRACKED AT BS. 500B, LBL 24. R&R BAFFLE CLIP IAW SRM & DWG.
FORWARD CARGO BAY LT FLOOR TO SIDE WALL SUPPORT PLATE CORRODED BETWEEN BS. 500A TO BS. 500C, LBL 23. R&R SUPPORT IAW SRM.
LT BIN EMERGENCY LIGHT LENSES DAMAGED AT ROW #6. R&R LENS IAW AMM & SIP.
AFT CARGO BAY FLOOR SPLICE STRAP CORRODED AT BS. 887, BETWEEN RBL 10 TO LBL 10. R&R FLOOR SPLICE STRAP PER SRM.
AFT CARGO BAY VERTICAL WEB CORRODED BETWEEN BS. 827 TO BS. 847, RBL 6. R&R WEB PER SRM & DWG.
LT HORIZONTAL PRESSURE WEB CRACKED BETWEEN BS. 663 TO BS. 675, BETWEEN LBL 30 TO LBL 45. REPAIRED WEB IAW SRM.
FORWARD CARGO BAY, AFT BULKHEAD GUSSET CRACKED AT BS. 500D, STR. 19L. R&R GUSSET IAW SRM & DWG.
RT HORIZONTAL PRESSURE WEB CRACKED BETWEEN BS. 663 TO BS. 675, BETWEEN RBL 39 TO RBL 60. REPAIRED WEB IAW SRM.
RT WING UPPER T/E PANEL HORIZ SEAL RETAINER IS CRACKED; JUST AFT OF #2 PYLON. / REMOVED AND REPLAED R/H WING UPPER T/E PANEL CRACKED HORIZONTAL SEAL RETAINER AFT OF #2 PYLON IAW SOPM 20-50-01; SRM 51-40-02-0G-0 AND IPC 57-50-00-25. 57048U 02MAY19
VAPOR BARRIER ATTACH ANGLE CRACKED AT BS. 663, LBL 8. REPAIRED ANGLE PER ATS ER AND EA.
RT LOWER VAPOR BARRIER CRACKED AT BS. 663, BETWEEN RBL 45 TO RBL 55. R&R BARRIER IAW SRM & DWG.
LOWER L2 DOOR EXIT SIGNS DISCOLORED. R&R SIGNS IAW AMM.
L1 DOOR UPPER EMERGENCY LIGHT LENS DISCOLORED. R&R LENS IAW AMM.
R1 DOOR EXIT LIGHT COVERS DISCOLORED. R&R COVER IAW AMM.
R2 DOOR EMERGENCY LIGHT COVER DISCOLORED. R&R COVERS IAW AMM.
UPPER L2 DOOR EXIT SIGNS DISCOLORED. R&R SIGNS IAW AMM.
RT WING #8 SLAT CRACKED AROUND THE FASTENER AT LOWER SURFACE OF SLAT NOSE SKIN AT ACTUATOR RIBS. REPAIRED #8 SLAT IAW SRM.
L2 DOOR EMERGENCY LIGHT COVER DISCOLORED. R&R COVERS IAW AMM.
L1 DOOR LOWER EMERGENCY LIGHT LENS DISCOLORED. R&R LENS IAW AMM.
EXT LIGHT LENS NEAR L1 DOOR BROKEN. / R&R EXIT LIGHT LENS PER AMM.
R2 DOOR SLIDE PACK FELL FROM CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER MT.
AFT GALLEY CEILING EXIT "EXIT SALIDA" LIGHTS INOP. RESET CIRCUIT BREAKER P18-3 IAW AMM.
FORWARD GALLEY OVERWING EXIT "EXIT SALIDA" LIGHTS INOP. RESET CIRCUIT BREAKER P18-3 IAW AMM.
LT WING INBOARD AFT FLAP CREASED WITH A POSSIBLE CRACKED. R&R AFT FLAP IAW AMM.
LT INBOARD AFT FLAP CREASED WITH A POSSIBLE CRACK 21" INBOARD + 2 INCHES FROM TRAILING EDGE. R&R AFT FLAP IAW AMM.
LT WING INBOARD AFT FLAP CREASED WITH A POSSIBLE CRACK 21" INBOARD AND 2 INCHES FROM TRAILING EDGE. REPAIRED AFT FLAP IAW AMM.
LT WING NR 2 SLAT SKIN CRACKED AFT OF ACTUATOR. REPAIRED NR 2 SLAT SKIN PER EA.
RT EMERGENCY LIGHT COVER LOOSE AT ROW 3. SECURED COVER PER AMM.
RT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT LUG FITTING CORRODED. REPAIRED FITTING PER EA.
LT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT LUG FITTING CORRODED. REPAIRED FITTING PER EA.
SUPPLEMENTAL INFORMATION: FWD CORNER SECTION SCUFF PLATE OF THE AFT CARGO COMPARTMENT IS CRACKED. / REMOVED AND REPLACED REF AMM 53-11-02.
RT EMERGENCY EXIT LENS ASSEMBLY BROKEN AT ROW 18. R&R LENS PER SIP.
LEFT WING OTBD AFT FLAP DELAMINATED ON UPPER SURFACE. R & R THE AFT FLAP IAW AMM.
LEFT WING TO BODY FAIRINGS AFT EMERGENCY EXIT LIGHT LENS DIRTY. CLEANED THE LENS IAW SOPM.
GUSSET CRACKED AT BS 500D, STRINGER 19R. R & R THE GUSSET IAW SRM & DWG.
R1 DOOR SILL VERTICAL FLANGE TAPERED STRAP CORRODED BETWEEN BS 276 TO 298. R & R THE STRAP IAW SRM.
AFT CARGO BAY DOOR CUTOUT SURROUND STRUCTURE INTERCOSTAL WEB CORRODED AT BS 850, RBL 24.5. R & R THE WEB IAW DWG & SRM.
AFT EDGE OF COOLING FAN EXHAUST CUTOUT SKIN CRACKED AT BS 380, BETWEEN STR 28L TO STR 28R. REPAIRED SKIN PER EA.
AFT CARGO BAY DOOR SURROUND STRAP CORRODED AT BS 847, RBL 24.5. R & R THE STRAP IAW SRM.
AFT CARGO BAY SIDEWALL SUPPORT CORRODED BETWEEN BS 727C TO 767, RBL 24.5. R & R THE SIDEWALL SUPPORT IAW SRM.
AFT CARGO BAY DOOR CUTOUT SURROUND STRUCTURE AFT SHIELD CORRODED AT BS 857, RBL 24.5. R & R SHIELD IAW SRM.
AFT CARGO BAY SIDEWALL SUPPORT CORRODED BETWEEN BS 867 TO 917, RBL 24.5. R & R THE SIDEWALL SUPPORT IAW DWG.
AFT CARGO BAY SIDEWALL SUPPORT CORRODED BETWEEN BS 727D TO 807, LBL 24.5. R & R THE SIDEWALL SUPPORT IAW SRM.
AFT CARGO BAY DOOR CUTOUT SURROUND STRUCTURE BOTTOM STRAP CORRODED BETWEEN BS 787 TO 797, RBL 24.5. R & R THE STRAP IAW SRM.
AFT CARGO BAY DOOR CUTOUT SURROUND STRUCTURE FORWARD SHIELD CORRODED AT BS 787, RBL 24.5. R & R SHIELD IAW SRM.
FLOOR TO SIDEWALL SUPPORT SHIELD CORRODED BETWEEN BS 420 TO 440, RBL 25. R & R THE SUPPORT IAW SRM.
SIDEWALL PANEL SUPPORT ANGLE CRACKED AT BS 847, LBL 9. R & R SIDEWALL SUPPORT ANGLE IAW SRM.
AFT CARGO BAY FRAME ATTACH ANGLE CORRODED AT BS 767, RBL 24.5. R & R THE ATTACH ANGLE IAW SRM.
FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 492 TO 500A, RBL 25. R&R SIDEWALL SUPPORT IAW SRM.
LOWER BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN LBL 25 TO RBL 25. R & R THE SUPPORT ANGLE IAW SRM.
FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 400 TO 500D, LBL 25. R & R THE SUPPORT IAW SRM.
FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 500A TO BS. 500D, RBL 25. R & R THE SUPPORT IAW SRM.
RIGHT BULKHEAD SUPPORT ANGLE CORRODED AT BS 500D, RBL 25. R & R THE SUPPORT ANGLE IAW DWG AND SRM.
FLOOR SUPPORT CRACKED BETWEEN BS 277 TO 294.5, BL 0. R & R THE FLOOR SUPPORT IAW SRM AND DWG.
FLOORBEAM UPPER FLANGE TEE CORRODED AT BS 986, WL 208. REPAIRED THE FLOORBEAM TEE IAW ER.
FLOOR SUPPORT CRACKED BETWEEN BS 344 TO 360, RBL 12. REPAIRED THE FLOOR SUPPORT IAW SRM.
FORWARD CARGO BAY DOOR CUTOUT CENTER SCUFF PLATE CRACKED AT BS 450. REPAIRED THE SCUFF PLATE IAW EA.
LEFT WING LEADING EDGE NR 3 SLAT NOSE SKIN CRACKED AT ACTUATOR ATTACH FITTING. REPAIRED THE SKIN IAW SRM.
AFT LOWERED CEILING EMERGENCY EXIT LIGHT HOUSING CRACKED. R & R THE LIGHT IAW SOPM.
LT ABOVE OVERWING EMERGENCY LIGHT BATTERY PACK M1668 FAILED CHECK AT BS 500C. R&R BATTERY PACK IAW AMM.
LEFT EMERGENCY AISLE LIGHT BATTERY PACK M1670 FAILED CHECK. R & R THE BATTERY PACK IAW AMM.
EMERGENCY LIGHT BATTERY PACK M1668 FAILED CHECK AT BS 500C. R & R THE BATTERY PACK IAW AMM.
RIGHT CABIN EXIT LIGHT LENS MISSING BETWEEN ROWS 5 & 6. INSTALLED LENS IAW MM.
RT MID CABIN EMERGENCY EXIT LIGHT INOPERATIVE. R & R LIGHT IAW SIP.
R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR NOT FITTING. R&R SLIDE ASSEMBLY PER MT.
L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR NOT FITTING. R&R SLIDE ASSEMBLY PER MT.
AFT PRESS BULKHEAD AREA OF OIL CANNING AT BS 1016, BETWEEN BL 0 & STRINGER 3L, EXTEND FROM UPPER Y CHORD, 10" DOWN & OVER OUTER STRAP. REPAIRED BULKHEAD IAW SRM.
DURING CRUISE, CAPTAINS FWD WINDSHIELD L1 ARCED. R & R L1 WINDOW IAW MM.
LEFT MAIN WW LT ANGLE STIFFENER CRACKED AT BS 663 BULKHEAD FWD SIDE. R & R STIFFENER IAW SRM & DWG.
FORWARD SEAT TRACK TO SPLICE PLATE ATTACH FASTENER HOLES, INBOARD AFT & OUTBOARD FORWARD & AFT HOLES CRACKED AT BS 727B, RBL 25.75. REPAIRED SEAT TRACK IAW EA.
AFT SEAT TRACK TO FLOORBEAM ATTACH FASTENER HOLE, OUTBOARD FLANGE HOLE CRACKED AT BS 727B, RBL 25.75. REPAIRED SEAT TRACK IAW EA.
FORWARD SEAT TRACK TO SPLICE PLATE ATTACH FASTENER HOLES, INBD FWD & AFT, OTBD AFT HOLES CRACKED AT BS 727B, RBL 45.5. REPAIRED SEAT TRACK IAW EA.
FLOORBEAM CRACKED AT BS 727B, LBL 25.75. REPAIRED BEAM IAW EA.
FORWARD SEAT TRACK TO SPLICE PLATE ATTACH FASTENER HOLES, INBOARD & OUTBOARD AFT HOLES CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.
AFT SEAT TRACK TO FLOORBEAM, ATTACH FASTENER HOLES OUTBOARD FLANGE HOLE CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.
FRAME CRACKED AT BS 827, STRINGER 8L. REPAIRED FRAME IAW EA.
LEFT MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663, LBL 28. REPAIRED WEB IAW EA.
FUSELAGE FRAME CRACKED AT STATION 907, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 907, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 440, STRINGER 8L. REPAIRED FRAME IAW EA.
RIGHT WING NR 6 SLAT CRACKED AROUND FASTENERS THAT ATTACH THE ACTUATOR FITTING. REPAIRED NR 6 SLAT IAW SRM.
FRAME CRACKED AT BS 727B, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 520, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 500C, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 747, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 727D, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 400, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 380, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 827, STRINGER 8R. REPAIRED FRAME IAW EA.
SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW EA.
RIGHT HORIZONTAL STABILIZER RIB AT STAB STATION 92.70 CRACKED IN VERTICAL STIFFENER, 40" AFT OF FWD SPAR. REPAIRED RIB IAW SRM.
RIGHT HORIZONTAL STABILIZER RIB AT STAB STATION 92.70 CRACKED IN VERTICAL STIFFENER, 30" AFT OF FWD SPAR. REPAIRED RIB IAW SRM.
LEFT HORIZONTAL STABILIZER RIB AT STAB STATION 147.90 CRACKED IN VERTICAL STIFFENER, 30" AFT OF FWD SPAR. REPAIRED RIB IAW SRM.
NUMBER 3 RIGHT WINDOW FRAME AT E - F POST, AT SECOND LOWER CORNER HOLE CRACKED. REPAIRED POST IAW EA.
LEFT HORIZONTAL STABILIZER RIB CRACKED AT STAB STATION 101.90 IN VERTICAL STIFFENER & LOWER FLANGE 10" AFT OF FWD SPAR. REPAIRED RIB IAW EA.
SKIN CRACKED AT BS 540, LEFT SIDE. REPAIRED SKIN IAW EA.
RIGHT NR 1 FLIGHT DECK CRACKED IN UPPER OTBD CORNER. R & R FRAME IAW ACO.
LEFT HORIZONTAL STABILIZER RIB AT STAB STATION 101.90, CRACKED IN LOWER SURFACE 20" AFT OF FWD SPAR. REPAIRED RIB IAW EA.
RIGHT HORIZONTAL STABILIZER RIB AT STAB STATION 92.70, CRACKED IN VERTICAL STIFFENER, 20" AFT OF FWD SPAR. REPAIRED STIFFENER IAW AMM.
RIGHT HORIZONTAL STABILIZER RIB AT STAB STATION 92.70, CRACKED IN VERTICAL STIFFENER, 10" AFT OF FWD SPAR. REPAIRED STIFFENER IAW SRM.
RIGHT HORIZONTAL STABILIZER RIB AT STAB STATION 129.50 CRACKED IN VERTICAL STIFFENER, 10" AFT OF FWD SPAR. REPAIRED RIB IAW SRM.
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1670. R & R BATTERY PACK IAW WDM & AMM 6.
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R & R BATTERY PACK IAW WDM & AMM 6.
L1 DOOR EVAC SLIDE LOOSE. REPOSITIONED SLIDE IAW MM.
L2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW SIP.
SKIN CRACKED AT BS 540 BELOW STRINGER 22R. REPAIRED SKIN IAW EA.
SKIN CRACKED AT BS 540 BELOW STRINGER 22L. REPAIRED SKIN IAW EA.
BULKHEAD CHORD CRACKED AT BS 540 BELOW STRINGER 22L. REPAIRED CHORD IAW EA.
RIGHT LOWER OVERWING EMER EXIT LIGHTS BULB INOPERATIVE. RE LAMPED LIGHT IAW AMM.
LEFT LOWER OVERWING EMER EXIT LIGHT BULB INOPERATIVE. RE LAMPED LIGHT IAW AMM.
AFT CARGO DOOR CUT OUT LOWER AFT THRESHOLD CRACKED. REPAIRED THRESHOLD IAW EA.
LEFT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS IAW MM.
L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.
FWD CABIN EMERGENCY LIGHTS BATTERY PACKS FAILED CAPACITY CHECK. R & R BATTERY IAW MM.
AFT CABIN EMERGENCY LIGHTS BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY IAW MM.
FLANGE CRACKED AWAY WHERE INTERCOM PANEL DOOR MEETS FUSELAGE ON AFT FUSELAGE EDGE. REPAIRED SKIN IAW EA.
LT NR 3 FLIGHT DECK WINDOW FRAME ON E-F POST, SECOND LOWER CORNER FASTENER HOLE CRACKED. REPAIRED FRAME IAW SWA EA.
RT NR 3 FLIGHT DECK WINDOW FRAME ON E-F POST, SECOND LOWER CORNER FASTENER HOLE CRACKED. REPAIRED FRAME IAW SWA EA.
CENTER WING VERTICAL PRESSURE DECK WEB CRACKED AT STATION 663, BETWEEN RBL 36 - RBL 46. REPAIRED WEB IAW SRM.
LT WING TE PANEL ATTACH STRUCTURE WAFFLE PLATE CRACKED BEHIND NR 2 PYLON FAIRING. R&R FAIRING IAW SRM.
LT WING INBD MAIN FLAP DELAMINATED ON UPPER SURFACE. REPAIRED MAIN FLAP IAW SWA EA.
CRACK ON AFT CARGO DOOR FRAME BOTTOM MOD. FOUND CENTER SCUFF PLATE DAMAGES AT FWD EDGE 1" IN LENGTH X 1/16" WIDTH. OK TO CONTINUE PER EA 1-A53- 2389 PERFORM VISUAL INSPECTION EVERY 10 DAYS OR 100 FLT HRS FOR SPEED TAPE CONDITION. ACCOMPLISH
DECLARED EMERGENCY -- AFTER T/O, FELT VIBRATION DUE TO NR 2 LT MLG BLOWN TIRE. REMOVED AND REPLACED BOTH LT MLG TIRE/WHEEL ASSY'S PER MM.
RT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT PER AMM.
WINDSHIELD R1 ARCED AND SHATTERED. REMOVED AND REPLACED R1 WINDOW HEAT CONTROLLER PER MM.
DURING SCHEDULED HC1 CHECK, FOUND FWD EMERGENCY EXIT LIGHT BATTERY CHARGERS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.
DURING SCHEDULED HC1 CHECK, FOUND EEPLS DIRTY. CLEANED EEPLS PER MM.
DURING SCHEDULED HC1 CHECK, LT EMERGENCY EXIT LIGHTS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED HC1 CHECK, RT EMERGENCY EXIT LIGHTS FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOLDER LOOSE. SECURED HOLDER PER MT.
DURING SCHEDULED 12Y CHECK, FOUND RT CREASE BEAM ANGLE CORRODED AT BS 984, RBL 48. REPAIRED ANGLE IAW EA.
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME IAW EA.
DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT RT Z ANGLE CORRODED BETWEEN BS 727E TO BS 747. REMOVED AND REPLACED Z ANGLE IAW SRM.
DURING SCHEDULED 12Y CHECK, FOUND FORWARD CARGO DOOR CUTOUT WEB CORRODED. REMOVED AND REPLACED WEB IAW SRM.
DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT RT Z-ANGLE CORRODED BETWEEN BS 747 TO BS 767. REMOVED AND REPLACED Z-ANGLE IAW SRM.
DURING SCHEDULED 12Y CHECK, FOUND CREASE BEAM CORRODED AT BS 984, RBL 48. REMOVED AND REPLACED BEAM IAW SRM AND DWG.
DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.
DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, LBL 24. REPAIRED BEAM PER SRM.
DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD FITTING CORRODED. REMOVED AND REPLACED FITTING IAW SRM AND DWG.
DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, LBL 24. REPAIRED BEAM IAW SRM.
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER EA.
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867 STR 8R. REPAIRED FRAME PER EA.
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 787 STR 8L. REPAIRED FRAME PER EA.
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 747 STR 8L. REPAIRED FRAME PER EA.
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER EA.
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER EA.
DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM.
DURING SCHEDULED MV1 CHECK FOUND, RT EEPLS INOP AT ROW 7. REMOVED AND REPLACED EEPLS PER MM.
DURING SCHEDULED CV CHECK, FOUND RT EEPLS DELAMINATED BETWEEN ROW 6 TO ROW 8. REMOVED AND REPLACED EEPLS PER MM.
AIR TURNBACK - AT 41000FT ON CRUISE, LEFT BLEED TRIP OFF LIGHT ILLUMINATED A TOTAL OF 4 TIMES WITH SUCCESSFUL RESETS ON EACH OCCASION. RIGHT BLEED TRIP OFF LIGHT ALSO ILLUMINATED TWICE AND CABIN BEAN CLIMBING. RESET WAS SUCCESSFUL. REMOVED AND REPLACED PRECOOLER CONTROL VALVE SENSOR, NR 2 ENGINE PRECOOLER VALVE, AND AIR CONDITIONING ACCESSORY UNIT PER MM.
DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB ASSY PER MM.
DURING SCHEDULED 12Y CHECK, FOUND LT WING O/B FLAP I/B TRAILING EDGE DELAMINATED. REPAIRED FLAP PER SRM.
DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN BROKEN AT FWD BULKHEAD. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP DELAMINATED AT ROW 22. REMOVED AND REPLACED EEPLS PER MM.
DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION BEARING LUGS CORRODED. REPAIRED LUGS PER SWA EA.
DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION BEARING LUGS CORRODED. REPAIRED LUGS PER SWA EA.
FOUND L1 EMERGENCY EXIT DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.
L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.
L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
L2 DOOR EMERGENCY EVAC SLIDE WILL NOT ARM. REMOVED AND REPLACED EVAC SLIDE PER MM.
DURING SCHEDULED 8Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
DURING SCHEDULED 8Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 986.5, LBL 35. REPAIRED FLOORBEAM CHORD PER ER.
DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. R&R BATTERY PACK PER MM.
DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. R&R BATTERY PACKS PER MM.
DURING SCHEDULED HC2 CHECK, LH OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. R&R BATTERY PACK PER MM.
DURING SCHEDULED MV2 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED MV2 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.
DURING SCHEDULED HC1 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.
DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
DURING SCHEDULED MV3 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 4 DEF. SECURED LENS PER MM.
DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
R2 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM.
DURING SCHEDULED RON, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 3 AND 5 DEF. REMOVED AND REPLACED BATTERY PACK PER MM.
DURING SCHEDULED MV2 CHECK, FOUND RT AFT CABIN EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.
EEPLS LOOSE AT ROW 1. REMOVED AND REPLACED EEPLS FWD SECTION PER MM.
DURING SCHEDULED C1 CHECK, FOUND AFT SERVICE DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.
DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.
DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, RT ELEVATOR TAB FAILED FREE PLAY INSPECTION. REMOVED AND REPLACE RT ELEVATOR TAB NR 2 AND NR 4 HINGE HARDWARE AND BUSHINGS PER MM AND SWA SI.
DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, LT ELEVATOR TAB FAILED FREE PLAY INSPECTION. REMOVED AND REPLACED LT ELEVATOR TAB NR 2, NR 3 AND NR 4 HINGE HARDWARE AND BUSHINGS PER MM AND SWA SI.
DURING SCHEDULED C2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.
DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY LENGTH OUT OF ADJUST. REMOVED AND REPLACED SLIDE PER MM.
DURING SCHEDULED C3 CHECK, FOUND EEPLS COVER CRACKED AT FWD CABIN. REMOVED AND REPLACED EEPLS COVER PER MM.