N8708Q
Registered owner: SOUTHWEST AIRLINES CO, TX (owner ≠ operator)
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.
57 reports on file, 2021-02-26 – 2026-08-21.
Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 22,107 hrs · 10,323 cycles
BOTH AFT GALLEY FLASHLIGHTS INOPERATIVE. R & R THE FLASHLIGHTS IAW AMM 25-64-00.
Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 22,107 hrs · 10,323 cycles
BOTH AFT GALLEY FLASHLIGHTS INOPERATIVE. R & R THE AFT GALLEY FLASHLIGHTS IAW AMM 25-64-00.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 22,099 hrs · 10,319 cycles
M1675 BATTERY NOT RETAINING CHARGE REMOVED, REPLACED AND PERFORMED GOOD INSTALLATION TEST OF M1675 BATTERY CHARGER IAW AMM 33-51-06-960-803, M1675 BATTERY PACK NOW PROPERLY CHARGES AND RETAINS CHARGE.
Part: ELEC CONNECTOR — DISCONNECTED (ZONE 200) · airframe 22,099 hrs · 10,319 cycles
COCKPIT EMERGENCY LIGHT INOPERATIVE, PERFORMED GOOD CONTINUITY CHECK OF CONNECTOR D2992 TO GROUND. PERFORMED POWER CHECK FROM D 2970 - NO POWER AT CONNECTOR D2992. ACCESSED FWD BULLNOSE PANEL - PERFORMED VISUAL INSPECTION OF EMERGENCY LIGHT BATTERY PACK M1675 - FOUND CONNECTOR D10750 NOT CONNECTED. RECONNECTED CONNECTOR D10750 TO BATTERY PACK M1675 AND PERFORMED GOOD EMERGENCY LIGHTS TEST IAW AMM: 33-51-06-960-802 AND WDM 33-51-12 AND AMM 25-21-71-000-803.
Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 22,099 hrs · 10,319 cycles
LEFT BS 663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER LBL 11 WL 167.68. TTG8Q01DE7GB.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 22,099 hrs · 10,319 cycles
COCKPIT FLOOR PANEL 211AF REQUIRES REPLACEMENT. COCKPIT FLOOR PANEL 211AF REPLACEMENT IAW SRM 51-40-05-0G-0 AND DWG 141A5133 REV: C.
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 22,099 hrs · 10,319 cycles
CRACKED FLOOR SUPPORT, BS 380-400 LBL 14 WL 208. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, AND DWG 143A5400, REV-.
Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 22,099 hrs · 10,319 cycles
L/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER LBL11 WL167.68 CRACK FOUND TO BE OUT OF LIMITS AS PER SRM 57-10-10-1A-2. REPAIRED L/H BS663 UPPER ATTACH ANGLE ON VAPOR BARRIER LBL 6-12 WL167.68 IAW AE-M-26-157-01142. COMPLETE. TTG8Q01DN1H7CK TO BE ACCOMPLISHED ON TTG8Q01DN1H7 RII BUYBACK TO BE ACCOMPLISHED ON TTG8Q01DN1H7
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 22,099 hrs · 10,319 cycles
CORRODED FLOOR SUPPORT, BS 949, LBL 49, WL 208. R & R THE FLOOR SUPPORT IAW SRM 51-10-02-0G-0 51-40-02-0G-0, & DWG 147A5650, REV A.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 22,099 hrs · 10,319 cycles
CORROSION ON FLOORBEAM, BS 947, RBL 49, WL 208. REMOVED CORROSION ON FLOORBEAM UPPER FLANGE 1 X 1 AREA ORIGINAL MATERIAL THICKNESS IS 0.150" LOWEST MATERIAL THICKNESS IS 0.120" DAMAGE FOUND TO BE OUT LIMITS ON UPPER TEE ANGLE TO BE REPAIRED ALONG THE FULL UPPER FLANGE IAW SRM 53-70-51-2R, REPAIR 5, PARA 2.B, ALTERNATIVE 1. ALL REPAIR TO BE PERFORMED AND RECORDED ON CCN TTG8Q01DE4K3.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 22,099 hrs · 10,319 cycles
CORROSION ON FLOOR SUPPORT BS 947 RBL 49 WL 208. REMOVED AND REPLACED FLOOR SUPPORT BS 947, RBL 49, WL 208 IAW SRM 51-40-02-0G-0, AND DWG 147A5650, REV-.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 22,099 hrs · 10,319 cycles
CORROSION ON FLOORBEAM, BS 947, LBL 49, WL 208. REMOVED AND REPLACED UPPER FLANGE OF THE BS 947 FLOORBEAM FROM LBL 50 - RBL 50, WL208 AND REPAIRED IAW SRM 53-70-51-2R, REPAIR 5, PAR 2.B ALTERNATIVE 1.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 22,099 hrs · 10,319 cycles
CORROSION ON FLOORBEAM BS 947 LBL 24 WL 208. REMOVED CORROSION ON FLOOR BEAM UPPER FLANGE BS947 LBL24 WL208 1"X1" AREA ORIGINAL MATERIAL THICKNESS IS 0.150" LOWEST MATERIAL THICKNESS IS 0.120" DAMAGE FOUND TO BE OUT LIMITS BS947 UPPER T-CHORD TO BE REPAIRED ALONG THE FULL UPPER FLANGE I.A.W SRM 53-70-51-2R-REPAIR 5 PAR 2.B ALTERNATIVE 1. ALL REPAIR TO BE PERFORM AND RECORDED ON CCN TTG8Q01DE4K3.
Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 22,099 hrs · 10,319 cycles
FCB FWD CORNER SCUFF PLATE CRACKED (MARKED) REPAIRED FCB FWD CORNER SCUFF PLATE IAW 53-30-15-2R-1 REPAIR 1 SRM 51-40-05. CORNER SCUFF PLATE WILL BE INSTALLED ON CUSTOMER CARD # TTG8Q01DC94Y VERIFIED CORRECTIVE ACTION 1
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 22,099 hrs · 10,319 cycles
CORROSION ON FLOOR SUPPORT BS 949, LBL 26, WL 208. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, & DWG 147A5650, REV A.
Part: INSERT — DAMAGED (FLOOR PANEL) · airframe 22,099 hrs · 10,319 cycles
DAMAGED UPPER INSERT ON CABIN FLOOR PANEL 242VF. THE FLOOR PANEL 242VF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0, PARA 8,.A.1.
Part: PANEL — CRACKED (ZONE 500) · airframe 22,099 hrs · 10,319 cycles
PANEL 511AT CRACKED. REPAIRED PANEL 511AT IAW SRM 51-70-05-2R-6.
Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 21,790 hrs · 10,184 cycles
ONE FORWARD EMERGENCY FLASHLIGHT WILL NOT TEST. REMOVED AND REPLACED FLASHLIGHT BATTERY ON THE FORWARD EMERGENCY FLASHLIGHT IAW AMM 25-64-00.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 21,453 hrs · 10,019 cycles
BATTERY PACK M1675 FOR THE FWD LT EMERGENCY LIGHTS FOUND INOPERATIVE. REMOVED AND REPLACED IAW AMM 33-51-06-960-802.
Earlier reports · 2021–2025 · 38 reports
2025
Part: LENS — MISSING (ZONE 200) · airframe 20,198 hrs · 9,435 cycles
EMERGENCY LIGHT LENS ON CEILING PANEL ABOVE ROW 21 DEF MISSING. INSTALLED NEW EMERGENCY LIGHT LENS IAW AMM 33-51-03.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 19,835 hrs · 9,245 cycles
RIGHT ENTRY DOOR INTERIOR AND EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. R & R THE BATTERY PACK AT M2816 POSITION PER AMM 33-51-06.
Part: LENS — DAMAGED (ZONE 200) · airframe 19,042 hrs · 8,859 cycles
EMERGENCY LIGHT LENS NEAR AFT LIFE RAFT IS DAMAGED. REMOVED AND INSTALLED NEW EMERGENCY LIGHT LENS PER SIP
Part: HANDLE — LOOSE (ZONE 800) · airframe 18,847 hrs · 8,754 cycles
FORWARD GALLEY SERVICE DOOR ASSIST HANDLE IS LOOSE<[01] TIGHTENED FORWARD ENTRY DOOR ASSIST HANDLE IAW AMM 52-11-31-400-801-MAX.;[02] TASK C/W
Part: HANDLE — LOOSE (ZONE 800) · airframe 18,847 hrs · 8,754 cycles
FORWARD ENTRY DOOR ASSIST HANDLE IS LOOSE<[01] TIGHTENED FORWARD ENTRY DOOR ASSIST HANDLE IAW AMM 52-11-31-400-801-MAX.;[02] TASK C/W
Part: GLOWSTRIP — DETERIORATED (ZONE 200) · airframe 18,769 hrs · 8,717 cycles
DUE TO REPORTS OF PHOTOLUMINESCENT STRIP LOCATED ON CENTER ISLE F/O'S SIDE FROM ROW 1 - 5 NOT GLOWING AS BRIGHT AS ADJACENT STRIPS; REPLACE THIS SECTION PER AMM 33-51-15.
Part: GLOWSTRIP — DETERIORATED (ZONE 200) · airframe 18,764 hrs · 8,715 cycles
FIRST 5 SEATS OF EMERGENCY CARPET GLOW STRIP ON F/O'S SIDE IS NOT GLOWING. CW CLEANING OF FLOOR PHOTOLUMINESCENT STRIP PER AMM 33-51-15 OPS CK GOOD.
Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 18,298 hrs · 8,511 cycles
FOUND PORTION OF RH OVERWING EMERGENCY EXIT LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY BACK AND POWER SUPPLY AT POSITION M1671 IN REF TO AMM 33-51-06. OPS CHECK GOOD AT THIS TIME.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 18,298 hrs · 8,511 cycles
FOUND PORTION OF RH OVERWING EMERGENCY EXIT LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY BACK AND POWER SUPPLY AT POSITION M1671 IN REF TO AMM 33-51-06. OPS CHECK GOOD AT THIS TIME.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 17,934 hrs · 8,316 cycles
AFT RH EXTERNAL EMERGENCY LITE AND SIDEWALL EMERGENCY LITE AT ROW 15D INOP <[01]. REPLACED M01671 BATTERY PACK AND CHARGER PER AMM 33-51-06.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 17,715 hrs · 8,216 cycles
RIGHT OWE AFT EMERGENCY EXIT LIGHT IS INOP <[01]. TROBLESHOOTING RIGHT OWE AFT EMERGENCY LIGHT INOP; FOUND ALL LIGHT ASSOCIATED WITH BATTERY PACK M1671 ARE INOP; REMOVED AND REPLACED BATTERY PACK M1671; PERFORMED GOOD TEST PER AMM 33-51-06-960-802; [02] VERIFIED JOB COMPLETE.
Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 17,666 hrs · 8,195 cycles
FWD GALLEY F/A EMER. FLASHLIGHT(LEFT) INOP <[01]. PERFORMED OPS CHECK AMM 25-64-00 OPS CHECK GOOD.
2024
Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 16,550 hrs · 7,637 cycles
FWD F/A STATION I/B FLASHLIGHT INOP<[01] R/R FWD FA STATION I/B FLASHLIGHT PER AMM 25-64-00 OPS CHK GOOD
Part: HEAT SHIELD — CRACKED (ZONE 400) · airframe 16,241 hrs · 7,481 cycles
#2 ENGINE STRUT AFT HEAT SHIELD SKIN HAS A LARGE CRACK #2 ENGINE STRUT AFT HEAT SHIELD SKIN HAS A LARGE CRACK REF. SRM 54-50-70-1A-3 ALLOWABLE DAMAGE LIMITS 4(B)<[01] REPAIRED #2 ENG AFT FAIRING PLUME SUPPRESSOR PER SRM 54-50-70-2R-7. DVI REQUIRED EVERY 30 DAYS FOR 3 MONTHS THEN 120 DAYS AFTER 3 MONTHS.;[02] VERIFIED C/A #1
2023
Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 12,787 hrs · 5,693 cycles
MULTIPLE FWD RH CABIN EMERGENCY LIGHTS OUT<[01] REMOVED AND REMPLACED R/H BATTERY PACK AND PACK;CHARGER ASSY I.A.W AMM 33-51-06-960-802<BR>I TAG:WN33986<BR>I TAG:WN33992<BR>OPS CHECKS:GOOD;[02] REMOVED AND REMPLACED R/H BATTERY PACK AND PACK;CHARGER ASSY I.A.W AMM 33-51-06-960-802<BR>A TAG:WN33986<BR>A TAG:WN33992<BR>OPS CHECKS:GOOD;[03] VERIFIED STEP 1 AND 2<BR>AUDIT C/W
Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 12,787 hrs · 5,693 cycles
MULTIPLE FWD LH CABIN EMERGENCY LIGHTS OUT<[01] REMOVED AND REMPLACED L/H POWER SUPPLY-BATTERY PACK I.A.W AMM 33-51-06-960-802<BR>I TAG:WN33989<BR>OPS CHECKS:GOOD;[02] REMOVED AND REMPLACED L/H POWER SUPPLY-BATTERY PACK I.A.W AMM 33-51-06-960-802<BR>I TAG:WN33986<BR>OPS CHECKS:GOOD;[03] REMOVED AND REMPLACED L/H POWER SUPPLY-BATTERY PACK I.A.W AMM 33-51-06-960-802<BR>A TAG:WN33986<BR>OPS CHECKS:GOOD;[04] VERIFIED STEPS 1-3<BR>AUDIT C/W
Part: SEAL — DELAMINATED (ZN 300 STABILIZE) · airframe 12,787 hrs · 5,693 cycles
RH HORIZONTAL STAB TRAILING EDGE SEAL P/N 185A1621-122 CORNER IS TORN AND DELAMINATED<[01] REPLACED RH HORIZONTAL STAB TE SEAL P/N 185A1621-122 (ACCESS PANEL 344DB) IAW AMM 55-05-03-210-813 STEP 13. H. (3);[02] REPLACED RH HORIZONTAL STAB TE SEAL P/N 185A1621-122 (ACCESS PANEL 344DB) IAW AMM 55-05-03-210-813 STEP 13. H. (3)<BR><BR>A TAG#: WN6715;[03] C/W<BR>AUDIT C/W
Part: FLOOR PANEL — CORRODED (ZN 100 FUS LOWER) · airframe 12,787 hrs · 5,693 cycles
(A204 DOT 59) FWD CARGO FLOOR PANEL 120DF HAS LIGHT SURFACE CORROSION ALONG RH EDGE ON UPPER AND LOWER SURFACE.<[01] FABRICATED NEW FLOOR PANEL C/W;[02] FABRICATED NEW FLOOR PANEL C/W;[03] AUDIT C/W.
Part: FLOOR PANEL — CORRODED (ZN 100 FUS LOWER) · airframe 12,787 hrs · 5,693 cycles
185-010 AFT CARGO FLOOR PANEL 140DF HAS CORROSION ON BOTH SIDE OF DOOR OPENING<[01] REMOVED CORROSION AT AFT CARGO FLOOR PNL 140DF VERIFIED MATERIAL LOSS ;LOSS IS OVER 3.0 IN LENGTH IS OUT OF LIMITS I/A/W SRM 53-00-53-1A-1 STEP 5 A.B;[02] VERIFIED STEP 1;[03] OK TO TREAT AND PRIME .;[04] TREATED AND PRIMED I/A/W AMM 51-21-72-370-804 AND SRM 51-20-01-0G-0;[05] C/W;[06] VERIFIED ITEM 5<BR>AUDIT C/W
Part: ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 12,787 hrs · 5,693 cycles
A 221 DOT 17; AFT CARGO COMPARTMENT BETWEEN STA 767 AND 787 +6' L ANGLE THAT TIES INTERCOSTAL TO FWD FLOOR SHIELD IS CORRODED IN SEVERAL AREAS AS MARKED<[01] VERIFIED PART USING ATAG WN33472 P/N 146A8125-53 AND DWG 146A0081 REV:A STARTED LOCATING AND DRILLING L ANGLE IAW SRM 51-40-02-0G-0;[02] VERIFIED STEP 1;[03] C/W<BR>AUDIT C/W;[04] C/W<BR>AUDIT C/W
Part: SHIELD — CORRODED (ZN 100 FUS LOWER) · airframe 12,787 hrs · 5,693 cycles
A 221 DOT 13; AFT CARGO COMPARTMENT BETWEEN STA 847 AND 867 AFT FLOOR SHIELD IS CORRODED 4EA AREAS TOP SKIN AS MARKED<[01] AUDIT CW
Part: ANGLE — CORRODED (ZN 100 FUS LOWER) · airframe 12,787 hrs · 5,693 cycles
A 221 DOT 20; AFT CARGO COMPARTMENT BETWEEN STA 787 AND 727F TOP AND BOTTOM SKIN OF THE L/H/S ZEE ANGLE IS CORRODED IN SEVERAL AREAS AS MARKED<[01] REMOVED CORROSION VISUALLY INSPECTED CORRODED ARE WITH 10X MAGNIFIER<BR>NO DEFECTS NOTED I.A.W SRM 53-00-53-1A-2;[02] VERIFIED MATERIAL LOSE :<BR>BETWEEN STA727F-727H ORGINAL .040 REMOVED .004 REMAIN .0036 FOUND WITHIN LIMITS .<BR>BETWEEN STA 727H-727I RGINAL .040 REMOVED .007 REMAIN .033<BR>FOUND OUT OF LIMITS.<BR>BETWEEN STA727I-STA787 ORGINAL .040 REMOVED.004 REMAIN .036 FOUND WITHIN LIMITS USED AAR TOOL # 36649 DUE 07/25/2024 I.A.W SRM 53-00-53-1A-2 AND SRM53-60-53-0I-2;[03] VERIFIED ITEM 1&2;[04] REMOVED DAMAGED AREA OF L/H ZEE ANGLE BETWEEN STA 727G+10' - 727J+10' IAW B737-8 SRM 53-00-53-2R-6 PAR. 4 STEP B;[12] STARTED FABRICATING 'Z' ANGLE IAW SRM 53-00-53-2R-6;[13] FABRICATED 'Z' ANGLE AND SPLICES IAW SRM 53-00-5R-2R-6;[18] INSTALLED 'Z' ANGLE AND SPLICES IAW SRM 53-00-53-2R-6.;[19] VERIFIED ITEM 18;[20] OK TO APPLY CIC.;[21] APPLIED CIC ON AFT CARGO COMPARTMENT ON L/H/S ZEE ANGLE I.A.W AMM 51-21-91-701;[22] GLUED ON NUT PLATES ON AFT CARGO COMPARTMENT ON L/H/S ZEE ANGLE REPAIR I.A.W SRM 51-40-10-2R-0.<BR><BR>NOTE: GLUED APPLICATION TIME: 10:30 AM.;[23] REMOVED ELASTIC FROM N/P'S. CURE COMPLETE;[24] REPAIRED Z ANGLE C/W;[25] REMOVED ELASTIC FROM N/P'S. CURE COMPLETE. COMPLETED PUSH TEST IAW SRM 51-40-10-2R-0 TOOL #42641 CAL DUE 01/09/24;[26] VERIFIED STEPS 23-25.<BR>AUDIT C/W.
Part: SHIELD — CORRODED (ZN 100 FUS LOWER) · airframe 12,787 hrs · 5,693 cycles
A 221 DOT 16; AFT CARGO COMPARTMENT BETWEEN STA 767 AND 787 +6' FWD FLOOR SHIELD HAS SEVERAL AREAS OF CORROSION TOP AND BOTTOM SKIN AS MARKED<[01] C/W<BR>AUDIT C/W;[02] UPDATED PARTS INFO;[03] C/W<BR>AUDIT C/W
Part: BATTERY PACK — INOPERATIVE (ZN 100 FUS LOWER) · airframe 12,787 hrs · 5,693 cycles
(A204 DOT 5) PASSENGER CABIN. EMERGENCY WHITE LIGHT IS INOP IN COVE CEILING PANELS AT SEAT 15CB; AND 23ABC<[01] DURING TROUBLESHOOTING OF EMERGENCY WHITE AISLE LIGHT AT SEAT 15CB AND 23 ABC FOUND BAD POWER SUPPLY AT STA 727C +13 WL212 LBL68 (M1670) IAW WDM 33-51-13 PAGE 101 SHEET 1.;[02] REMOVED BATTERY PACK IN POWER SUPPLY M1670 IAW AMM 33-51-06-960-802 STEP 4D.(1) UP TO (4).;[03] REMOVED POWER SUPPLY IN M1670 IAW AMM 33-51-06-960-806 STEP 5E.1 UP TO 4.(A)(B)(C).;[04] OK TO INSTALL POWER SUPPLY;[05] INSTALLED NEW POWER SUPPLY AND BATTERY PACK IN M1670 IAW AMM 33-51-06-960-806 STEP 5E.4.(D)(E)(F) AND AMM 33-51-06-960-802 STEP 4D.(5). PENDING FOR OPS CHECK. <BR><BR>A-TAG# WN33102<BR>A-TAG# WN33252;[06] STEP 5 C/W;[07] ACCOMPLISHED OPS CHECKS OF AISLE LIGHTS 15CB AND 23ABC IAW AMM'S 33-51-06-960-802 AND 33-51-06-960-802 OPS CHECKS GOOD;[08] REMOVED POWER SUPPLY IN M1670 IAW AMM 33-51-06-960-803 STEP 5E.1 UP TO 4.(A)(B)(C)(D);[09] INSTALLED NEW POWER SUPPLY AND BATTERY PACK IN M1670 IAW AMM 33-51-06-960-803 STEP 5E.4.(D)(E)(F) AND AMM 33-51-06-960-802 STEP 4D.(5). PENDING FOR OPS CHECK.;[10] ACCOMPLISHED OPS CHECKS OF AISLE LIGHTS 15CB AND 23ABC IAW AMM'S 33-51-06-960-802 AND 33-51-06-960-803 OPS CHECKS GOOD;[11] VERIFIED STEP 7-10<BR>AUDIT C/W;[12] JOB COMPLETE<BR>AUDIT C/W;[13] JOB COMPLETE<BR>AUDIT C/W
Part: POWER SUPPLY — INOPERATIVE (ZN 100 FUS LOWER) · airframe 12,787 hrs · 5,693 cycles
(A204 DOT 5) PASSENGER CABIN. EMERGENCY WHITE LIGHT IS INOP IN COVE CEILING PANELS AT SEAT 15CB; AND 23ABC<[01] DURING TROUBLESHOOTING OF EMERGENCY WHITE AISLE LIGHT AT SEAT 15CB AND 23 ABC FOUND BAD POWER SUPPLY AT STA 727C +13 WL212 LBL68 (M1670) IAW WDM 33-51-13 PAGE 101 SHEET 1.;[02] REMOVED BATTERY PACK IN POWER SUPPLY M1670 IAW AMM 33-51-06-960-802 STEP 4D.(1) UP TO (4).;[03] REMOVED POWER SUPPLY IN M1670 IAW AMM 33-51-06-960-806 STEP 5E.1 UP TO 4.(A)(B)(C).;[04] OK TO INSTALL POWER SUPPLY;[05] INSTALLED NEW POWER SUPPLY AND BATTERY PACK IN M1670 IAW AMM 33-51-06-960-806 STEP 5E.4.(D)(E)(F) AND AMM 33-51-06-960-802 STEP 4D.(5). PENDING FOR OPS CHECK. <BR><BR>A-TAG# WN33102<BR>A-TAG# WN33252;[06] STEP 5 C/W;[07] ACCOMPLISHED OPS CHECKS OF AISLE LIGHTS 15CB AND 23ABC IAW AMM'S 33-51-06-960-802 AND 33-51-06-960-802 OPS CHECKS GOOD;[08] REMOVED POWER SUPPLY IN M1670 IAW AMM 33-51-06-960-803 STEP 5E.1 UP TO 4.(A)(B)(C)(D);[09] INSTALLED NEW POWER SUPPLY AND BATTERY PACK IN M1670 IAW AMM 33-51-06-960-803 STEP 5E.4.(D)(E)(F) AND AMM 33-51-06-960-802 STEP 4D.(5). PENDING FOR OPS CHECK.;[10] ACCOMPLISHED OPS CHECKS OF AISLE LIGHTS 15CB AND 23ABC IAW AMM'S 33-51-06-960-802 AND 33-51-06-960-803 OPS CHECKS GOOD;[11] VERIFIED STEP 7-10<BR>AUDIT C/W;[12] JOB COMPLETE<BR>AUDIT C/W;[13] JOB COMPLETE<BR>AUDIT C/W
Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 12,232 hrs · 5,422 cycles
EMERGENCY LIGHTS NEAR AFT SVC DOOR INOP.<[01] REMOVED AND REPLACED AFT RH BATTEY PACK IN REF TO AMM 33-51-06. OPS CHECK GOOD.
Part: GIRT BAR — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 11,942 hrs · 5,274 cycles
FWD SERVICE DOOR RIGHT SLIDE HOOK LOOSE<[01] ADJUSTED FWD SERVICE DOOR GIRT BAR HOOK REF AMM 25-66-01.
Part: SIGN — DETACHED (ZN 200 FUS TOP) · airframe 11,889 hrs · 5,246 cycles
EXIT SIGN DETACHED<[01] REATTACHED EXIT SIGN PER SIP
Part: FLASHLIGHT — FAILED (ZN 200 FUS TOP) · airframe 11,214 hrs · 4,879 cycles
FLIGHT DECK FLAS LIGHT RED LED ILLUMINATED DURING TEST<[01] R AND R FLT DECK EMERGENCY FLASHLIGHT AND CKS OK REF AMM 25-64-00. MEL/PLAC REMOVED
2022
Part: BRACKET — POPPED (ZN 800 DOOR) · airframe 10,908 hrs · 4,739 cycles
AFT GALLEY SVC DOOR GIRT BAR IS VERY LOOSE. IT KEEPS POPPING OUT<[01] TIGHTENED GIRT BAR ATTACH BRACKET PER SIP;[02] CHANGED FAULT SOURCE FROM MECHANIC TO PILOT AND FOUND BY TO PILOT'S EMPLOYEE NUMBER PER TELECONFERENCE WITH JASON RIVET E86976
Part: BRACKET — TIGHT (ZN 200 FUS TOP) · airframe 10,908 hrs · 4,739 cycles
FWD SVC DOOR GIRT BAR IS EXCESSIVELY TIGHT<[01] TIGHTENED GIRT BAR ATTACH BRACKET PER SIP.;[02] CHANGED FAULT SOURCE FROM MECHANIC TO PILOT AND FOUND BY TO PILOT'S EMPLOYEE NUMBER OF PILOT PER TELECONFERENCE WITH JASON RIVET E86976
Part: FRAME — CRACKED (#2 ENG IB FAN CO) · airframe 9,057 hrs · 3,836 cycles
#2 ENG IB FAN COWL HAS CRACKED FRAME / [01] REMOVED COWL;[02] R+R #2 ENG I/B FAN COWL PER 71-11-04
Part: BATTERY PACK — INOPERATIVE (L/H CABIN) · airframe 8,894 hrs · 3,780 cycles
AFT LEFT EMERGENCY EXIT LIGHTS INOP / [01] R&R AFT EMERGENCY LIGHT BATTERY PACK ASSY PER AMM 33-51-06. OPS CHK NORMAL
2021
Part: COVER — MISSING (ESCAPE STRAP) · airframe 2,491 hrs · 5,547 cycles
ESCAPE STRAP COVER ON CAPT SIDE AFT OVERWING EXIT VELCRO ON CAP MISSING OK TO CONT PER MEL 25-10-01 SP1B TK# 110929 ( NON-ESSENTIAL EQUIPMENT & FURNISHINGS; NEF ITEMS LISTED IN MEL APPENDIX 25-10 NON-ESSENTIAL EQUIPMENT & FURNISHINGS (NEF) ) /
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 5,375 hrs · 2,398 cycles
EMERGENCY EXIT LIGHT COVER MISSING ON AFT RIDE SIDE EMERGENCY WING EXIT. / REPLACED EMERGENCY EXIT LIGHT COVER IAW AMM 33-51-01
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 5,122 hrs · 2,255 cycles
CABIN FLOOR PANEL 232 SF HAS EDGE DAMAGE / REMOVED AND RE- INSTALLED CABIN FLOOR PANEL 232SF PER AMM 53-21-00.SEE SA-M 326: A1303251
Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 5,122 hrs · 2,255 cycles
CABIN FLOOR PANEL 231YF HAS EDGE DAMAGED (MARKED) / REPAIRED FLOOR BOARD PANEL 231YF PER SRM 53-00-50-2R-10
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 5,119 hrs · 2,254 cycles
FAILED BATTERY PACK CAPICITY CHECK 33-51-06. POSITIONS FWD L/HRH; MID CABIN LH; AFT CABIN RH / REMOVED AND REPLACED BATTERIES PER MM 33-51-06