N8550Q
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
FWD OTBD FA FLASHLIGHT WILL NOT TEST. REPLACED BATTERY IN FWD OTBD FA JUMPSEAT FLASHLIGHT IAW AMM 25-64-00.
FWD JUMPSEAT (FA) FLASHLIGHT DOES NOT TEST. R & R FLASHLIGHT IAW 25-64-00.
FOUR EMERGENCY LIGHTS INOPERATIVE. CHARGED BATTERY PACKS IAW AMM 33-51-06-610-802, & ACCOMPLISHED SATISFACTORY EMERGENCY LIGHTS OPS TESTED IAW AMM 33-51-00-710-801.
CEILING EMERGENCY EXIT SIGN BROKEN. R & R CEILING EMERG EXIT SIGN HOUSING ASSY IAW AMM 33-51-01.
R1 EMERGENCY LIGHTS INOP. R&R R1 EMERGENCY BATTERY PACK. REF AMM 33-51-06. OPS CHECK GOOD.
AFTER L2 DOOR SLIDE CONTAINER LOOSE; SLIDE NOT PROPERLY CONTAINED. <[01] INSPECTED L2 SERVICE DOOR SLIDE AND CONTAINER; TIGHTENED CONTAINER BOLTS AS PER AMM 25-66-01.
LOWER CUTOUT OF EXTERNAL POWER ACCESS DOOR SKIN HAS DELAMINATED DAMAGED<[01] PERFORMED HFEC OF AREA FOR CRACK MIGRATION PER 737 NDT PART 6 51-00-00 PROCEDURE 23 CRACK MIGRATED A .25 INCH BELOW MISSING MATERIAL;[02] PERFORMED HFEC OF TRIM OUT AREA PER 737 NDT PART 6 51-00-00 PROCEDURE 23 NO CRACKS FOUND.;[03] INSTALLED REPAIRED PARTS PER SRM 53-10-15-2R-4 REPAIR 4.;[04] SRM 53-10-15-2R-4-B00449 (REPAIR 4 - ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER - PERMANENT)
LEFT WING TO BODY OVERHEAT LIGHT ILLUMINATED DURING CLIMB. RAN QRH - LIGHT STAYED ILLUMINATED. LIGHT FLICKERED IN DESCENT AND EVENTUALLY EXTINGUISHED DURING ARRIVAL.<[01] T/S PER FIM 26-18 TASK 802 FOUND BITE CODE 14 STORED IN MEMORY. FOUND NO LEAKS OR EVIDENCE OF LEAKS ON LH LE BLEED. FOUND VOLTAGE OUT OF SPECIAL ON DETECTOR M268. R/R IAW AMM 26-18-02. OPS CK GOOD.;[02] SPECIAL SHOULD BE SPEC
#2 ENGINE AFT STRUT FAIRING AFT WEDGE FWD WEB HAS CRACK PROTRUDING FROM LAP AND EXTENDING INBOARD BEYOND THE RADIUS. CRACK MEASURES 1.3 INCHES.<[01] VERIFIED CRACK PER NDT 51-00-00 PROCEDURE 23.;[02] C/W EA M-23-154-01884-REPREF.
AFT ENTRY SLIDE SLIPPED OUT OF CONTAINER.<[01] REMOVED AND REINSTALLED AFT ENTRY EMERGENCY ESCAPE SLIDE ASSY INTO CONTAINER IAW MT 725-61-06 AE
RT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP<[01] R&R?D RT AFT EXTERIOR EMERGENCY EXIT LAMP PER REF AMM 33-51-04. OPS CHECK GOOD
CAPT SIDE AFT FA POSITION BOTH FLASHLIGHTS INOP LIGHTS WORK BUT NEED A SECURITY SEAL??<[01] REMOVED AND REPLACED FLASHLIGHT BATTERIES REF AMM 25-64-00. OPS CHECKS GOOD. SEALS REPLACED.
AFT SERVICE DOOR EMERGENCY LIGHTS INOP<[01] REMOVED AND REPLACED BATTERY PACK PER AMM 33-51-06;[02] OPS CHECKED GOOD PER AMM 33-51-06
FWD ENTRY EMERGENCY LIGHT BATTERY PACK IS INOP.<[01] R&R'D FWD ENTRY EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06.
(POSTDOCK TEST - CABIN PRESSURE LEAKAGE) AFT ENTRY DOOR FWD CORNER THRESHOLD SCUFF PLATE HAS EXCESSIVE PRESSURIZATION LEAK. LEAK COMING OUT OF EXPANSION SLOTS WITH STOP DRILL HOLES (2EA).<[01] R&R DOOR SCUFF PLATE;[02] R&R SCUFF PLATE PER AMM 53-11-01;[03] VERIFIED SCUFF PLATE RE-INSTALLED AND SEALED REF. C/A #2.;[04] REMOVED AND REINSTALLED AFT ENTRY DOOR SCUFF PLATE AND LEAK CHECKED IAW AMM 53-11-01 AND AMM 05-51-91. LEAK CHECK GOOD;[05] INSPECTION COMPLETE ON CORRECTIVE ACTION #4 FOR SATISFACTORY LEAK . SEE CORRECTIVE ACTION 1-3 FOR ALL OTHER MAINTENANCE.
CABIN FLOOR PANEL 221CF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] PANEL REPLACED WITH NEW FROM KIT 654A0004-1429. BN401684. OK TO CLOSE ON CLOSE-PANEL 221CF CARD (TTG8Q00MK04Y). NEW PANEL 141A5810-9 ITEM 200 VERIFIED WITH IPC 53-21-51-22B. FLOOR PANEL INSTALLED PER 5310-E-16414-NG AND AMM 53-21-00-400-801.
CABIN FLOOR PANEL 231MF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] RECEIVED SERVICEABLE PANEL FROM STOCK; PANEL TO BE INSTALLED ON TASK CARD: TTG8Q00MK042.;[02] C/W PART INFORMATION;[03] INSPECTED WORK PERFORMED IAW AMM 53-21-00.
CABIN FLOOR PANEL 231QF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] RECEIVED SERVICEABLE PANEL FROM STOCK; PANEL TO BE INSTALLED ON TASK CARD: TTG8Q00MK040.;[02] C/W PART INFORMATION;[03] INSPECTED WORK PERFORMED IAW AMM 53-21-00.
CABIN FLOOR PANEL 242RF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] CABIN FLOOR PANEL 242RF REPLACED; REF AMM 53-21-00;[02] INSPECTED WORK PERFORMED IAW AMM 53-21-00.
CABIN FLOOR PANEL 242SF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] CABIN FLOOR PANEL 242SF REPLACED; REF AMM 53-21-00.;[02] INSPECTED WORK PERFORMED IAW AMM 53-21-00.
CABIN FLOOR PANEL 242UF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] CABIN FLOOR PANEL 242UF REPLACED REF AMM 53-21-00;[02] INSPECTED WORK PERFORMED IAW AMM 53-21-00.
CABIN FLOOR PANEL 231YF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] RECEIVED SERVICEABLE PANEL FROM STOCK; PANEL TO BE INSTALLED ON TASK CARD: TTG8Q00MJZVM.;[02] C/W PART INFORMATION;[03] INSPECTED WORK PERFORMED IAW AMM 53-21-00.
CABIN FLOOR PANEL 231ZF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] RECEIVED SERVICEABLE PANEL FROM STOCK; PANEL TO BE INSTALLED ON TASK CARD: TTG8Q00MJZUY.;[02] C/W PART INFORMATION;[03] INSPECTED WORK PERFORMED IAW AMM 53-21-00.
CABIN FLOOR PANEL 231FF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] RECEIVED SERVICEABLE PANEL FROM STOCK; PANEL TO BE INSTALLED ON TASK CARD: TTG8Q00MK046;[02] PARTS UPDATE
CABIN FLOOR PANEL 231JF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] RECEIVED SERVICEABLE PANEL FROM STOCK; PANEL TO BE INSTALLED ON TASK CARD: TTG8Q00MK044;[02] PARTS UPDATE
CABIN FLOOR PANEL 242AF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] REMOVED AND REPLACED CABIN FLOOR PANEL 242AF PER AMM 53-21-00.
CABIN FLOOR PANEL 231TF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] RECEIVED SERVICEABLE PANEL FROM STOCK; PANEL TO BE INSTALLED ON TASK CARD: TTG8Q00MJZVT.;[02] PARTS UPDATE
CABIN FLOOR PANEL 231XF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] REMOVED AND REPLACED CABIN FLOOR PANEL 231XF PER AMM 53-21-00.;[02] C/W INSPECTION REQUIREMENTS.
CABIN FLOOR PANEL 221AF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] PANEL REPLACED WITH NEW FROM KIT 654A0004-1429. BN401684. OK TO CLOSE ON CLOSE-PANEL 221AF CARD (TTG8Q00MK052). NEW PANEL 141A5810-728 ITEM 85 VERIFIED WITH IPC 53-21-51-22B. FLOOR PANELS INSTALLED PER 5310-E-16414-NG AND AMM 53-21-00-400-801.
CABIN FLOOR PANEL 221BF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] PANEL REPLACED WITH NEW FROM KIT 654A0004-1429. BN401684. OK TO CLOSE ON CLOSE-PANEL 221BF CARD (TTG8Q00MK050). NEW PANEL 141A5810-729 ITEM 105 VERIFIED WITH IPC 53-21-51-22B. FLOOR PANEL INSTALLED PER 5310-E-16414-NG AND AMM 53-21-00-400-801.
CABIN FLOOR PANEL 221DF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] PANEL REPLACED WITH NEW FROM KIT 654A0004-1429. BN401684. OK TO CLOSE ON CLOSE-PANEL 221DF CARD (TTG8Q00MK04W). NEW PANEL 141A5810-303 ITEM 225 VERIFIED WITH IPC 53-21-51-22B. FLOOR PANEL INSTALLED PER 5310-E-16414-NG AND AMM 53-21-00-400-801.
CABIN FLOOR PANEL 221EF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] PANEL REPLACED WITH NEW FROM KIT 654A0004-1429. BN401684. OK TO CLOSE ON CLOSE-PANEL 221EF CARD (TTG8Q00MK04U). NEW PANEL 141A5810-249 ITEM 370 VERIFIED WITH IPC 53-21-51-22B. FLOOR PANEL INSTALLED PER 5310-E-16414-NG AND AMM 53-21-00-400-801.
CABIN FLOOR PANEL 221FF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] PANEL REPLACED WITH NEW FROM KIT 654A0004-1429. BN401684. OK TO CLOSE ON CLOSE-PANEL 221FF CARD (TTG8Q00MK04S). NEW PANEL 141A5810-157 ITEM 395 VERIFIED WITH IPC 53-21-51-22B. FLOOR PANEL INSTALLED PER 5310-E-16414-NG AND AMM 53-21-00-400-801.
CABIN FLOOR PANEL 221GF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] PANEL REPLACED WITH NEW FROM KIT 654A0004-1429. BN401684. OK TO CLOSE ON CLOSE-PANEL 221GF CARD (TTG8Q00MK04Q). NEW PANEL 141A5810-181 ITEM 420 VERIFIED WITH IPC 53-21-51-22B. FLOOR PANEL INSTALLED PER 5310-E-16414-NG AND AMM 53-21-00-400-801.
CABIN FLOOR PANEL 222DF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] PANEL REPLACED WITH NEW FROM KIT 654A0004-1429. BN401684. OK TO CLOSE ON CLOSE-PANEL 222DF CARD (TTG8Q00MK04L). NEW PANEL 141A5810-749 ITEM 270 VERIFIED WITH IPC 53-21-51-22B. FLOOR PANEL INSTALLED PER 5310-E-16414-NG AND AMM 53-21-00-400-801.
CABIN FLOOR PANEL 232AF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] REPLACED PASSENGER CABIN FLOOR PANEL IAW AMM 53-21-00. ON PANEL CLOSE CARD TASK #TTG8Q00MJZUG.;[02] C/W INSPECTION REQUIREMENT FOR INSTALLATION OF CABIN FLOOR PANEL 232AF IAW AMM 53-21-00
CABIN FLOOR PANEL 232BF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] REPLACED PASSENGER CABIN FLOOR PANEL IAW AMM 53-21-00. ON PANEL CLOSE CARD TASK #TTG8Q00MJZUE.;[02] C/W INSPECTION REQUIREMENTS OF REPLACEMENT OF CABIN FLOOR PANEL 232BF IAW AMM 53-21-00
CABIN FLOOR PANEL 231AF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] REPLACED PASSENGER CABIN FLOOR PANEL IAW AMM 53-21-00. ON PANEL CLOSE CARD TASK #TTG8Q00MK04C.;[02] C/W INSPECTION REQUIREMENT FOR REPLACEMENT OF PASSENGER CABIN FLOOR PANEL 231AF IAW AMM 53-21-00.
CABIN FLOOR PANEL 231BF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] REPLACED PASSENGER CABIN FLOOR PANEL IAW AMM 53-21-00. ON PANEL CLOSE CARD TASK #TTG8Q00MK04A.;[02] C/W
CABIN FLOOR PANEL 231CF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] REPLACED PASSENGER CABIN FLOOR PANEL IAW AMM 53-21-00. ON PANEL CLOSE CARD TASK #TTG8Q00MK048.;[02] C/W INSPECTION REQUIREMENT FOR REPLACED PASSENGER CABIN FLOOR PANEL IAW AMM 53-21-00
CABIN FLOOR PANEL 231RF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] REPLACED PASSENGER CABIN FLOOR PANEL IAW AMM 53-21-00. ON PANEL CLOSE CARD TASK #TTG8Q00MK03V.;[02] C/W INSPECTION REQUIREMENT FOR REPLACED PASSENGER CABIN FLOOR PANEL IAW AMM 53-21-00
CABIN FLOOR PANEL 242QF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] REPLACED PASSENGER CABIN FLOOR PANEL IAW AMM 53-21-00. ON PANEL CLOSE CARD TASK #TTG8Q00MK03Q.;[02] C/W INSPECTION REQUIREMENT FOR REPLACED PASSENGER CABIN FLOOR PANEL IAW AMM 53-21-00
CABIN FLOOR PANEL 242PF HAS MULTIPLE DENTS AND PULLING FIBERS<[01] REPLACED PASSENGER CABIN FLOOR PANEL IAW AMM 53-21-00. ON PANEL CLOSE CARD TASK #TTG8Q00MK035.
FLIGHT DECK PANEL 211AF DENTED AND DEFORMED<[01] LOCATED; DRILLED; TREATED AND PRIMED SERVICEABLE PANEL 211AF IAW SRM 51-40-05; AMM 51-21-21; AMM 51-21-72.;[02] PANEL 211AF TO BE INSTALLED WITH CARD TTG8Q00M2ZHC. REFERENCE CARD TTG8Q00MK06J FOR OK TO CLOSE.;[03] C/W INSP. PANEL 211AF TO BE INSTALLED WITH CARD TTG8Q00M2ZHC. REFERENCE CARD TTG8Q00MK06J FOR OK TO CLOSE.
#1 ENGINE I/B FAN COWL OIL DOOR ACCESS HOLE WEB CRACKED. (MARKED)<[01] REMOVED CRACKED WEB;[02] REJECT: CORRECTIVE ACTION #1 DOES NOT CONTAIN A REFERENCE USED FOR THE WORKED PERFORMED AS REQUIRED PER MPM 51.03.01. SEE FAULT TTG8Q00NB91V FOR REJECT.;[03] R/R CRACKED WEB PER SRM 51-40-02 AND CMM 71-13-30
FWD. CARGO COMPARTMENT RH TRANSITION ANGLE HAS AREAS OF SURFACE CORROSION AT STA.500-500D RBL 24.(MARKED)<[01] R/H TRANSITION ANGLE AT STA 500-500D IS OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2.;[02] R/H TRANSITION ANGLE WILL BE REMOVED AND REPLACED FROM STA 500A TO 500I REFERENCE NON ROUTINE CARD #TTG8Q00N5TLR FOR WORK TO BE ACCOMPLISHED.
AFT CARGO AFT CORNER SCUFFPLATE IS CRACKED.<[01] TO BE INSTALLED ON TTG8R007QB7A.;[02] CW
FWD. CARGO COMPARTMENT L/H TRANSITION ANGLE AT STA. 500-500C LBL 24 HAS CORROSION AT NUMEROUS NUT PLATE HOLES. (MARKED)<[01] CORROSION AT FASTENER HOLE AT BS 500+10 OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] CUT AND REMOVED L/H TRANSITION ANGLE FROM BS 480+9 - 500I PER SRM 53-00-53.;[03] LOCATED AND DRILLED NEW L/H TRANSITION ANGLE STA 500-500C PER SRM 53-00-53-1A-2;[04] LOCATED AND DRILLED NEW L/H TRANSITION ANGLE STA 480+9 TO STA 500I PER SRM 53-00-53-1A-2;[05] DEBURRED AND TREATED L/H TRANSITION ANGLE AND REPAIR PARTS STA. 480+9 TO 500I PER SRM 51-20-01;[06] INSPECTED THE WORK ON C/A #5; NO DEFECTS NOTED.;[07] LOCATED AND DRILLED NEW L/H TRANSITION ANGLE STA 480+9 TO STA 500I PER SRM 53-00-53-2R-5. LOCATED AND DRILLED 2 EA REPAIR SPLICE PIECES AT STA 480+9 AND STA 500D+13 PER SRM 53-00-53-2R-5;[08] C/W INSPECTION.;[09] PRIMED TRANSITION ANGLES AND REPAIR PARTS PER SRM 51-20-10. INSTALLED CLICK BOND NUT PLATES ON 21 SEPT. 2023 AT 19:30 HRS. PER SRM 51-40-10;[10] INSTALLED L/H TRANSITION ANGLE AND REPAIR PARTS FROM STA 480+9 TO 500I PER SRM 53-00-53-2R-5 PERFORMED PUSH TEST FOR ALL NEWLY INSTALLED NUT PLATES PER SRM 51-40-10. ALL TESTED GOOD.;[13] VERIFIED C/A #12.;[14] REPAIRED FWD CARGO L/H TRANSITION ANGLE FROM STA 480+9 TO 500I PER SRM 53-00-53-2R-5 AND EA M-22-153-01550.;[15] VERIFIED REPAIR COMPLETED;[16] VERIFIED REPAIR COMPLETED
FWD. CARGO COMPARTMENT FLOOR PANEL ATTACH ANGLE AT STA 500I RBL 24-LBL24 HAS SURFACE CORROSION. (MARKED)<[01] FWD CARGO AFT BULKHEAD LOWER ATTACH ANGLE IS OUT OF ALLOWABLE LIMITS PER SRM 53-30-08-1A-1.;[02] REMOVED AFT BULKHEAD LOWER ATTACH ANGLE PER SRM 51-40-02.;[03] R/R ATTACH ANGLE PER SRM 51-40-02
FWD. CARGO COMPARTMENT RH TRANSITION ANGLE HAS AREAS OF SURFACE CORROSION AT STA.500D-500I RBL 24.(MARKED)<[01] R/H TRANSITION ANGLE AT STA 500D TO 500I IS OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2.;[02] REMOVED R/H TRANSITION ANGLE FROM STA 500A TO 500I PER SRM 51-40-02.;[03] INSTALLED TRANSITION ANGLE PER SRM 51-40-02;[04] INSTALLED R/H TRANSITION ANGLE FROM STA 500A TO 500I PER SRM 51-40-02;[05] INSPECTION C/W;[06] INSPECTION C/W
FWD. CARGO COMPARTMENT L/H TRANSITION ANGLE AT STA. 500C-500I LBL 24 HAS CORROSION AT NUMEROUS NUT PLATE HOLES. (MARKED)<[01] CORROSION AT FASTENER HOLE AT BS 500E+10 OUT OF LIMITS PER SRM 53-00-53-1A-2.;[02] DAMAGE REMOVED AND REPAIRED ON NR#TTG8Q00N5VML PER SRM 53-00-52-2R-5;[03] C/W INSP .DAMAGE REMOVED AND REPAIRED ON NR#TTG8Q00N5VML PER SRM 53-00-52-2R-5;[04] DAMAGE REMOVED AND REPAIRED ON TTG8Q00N5VML PER SRM 53-00-53-2R-5.
PANEL 842CZ PANEL ASSEMBLY - EMERGENCY ESCAPE HATCH - COVER PLATE HAS A CRACK.<[01] REPLACED COVER PLATE PER AMM 52-22-51;[02] C/W INSPECTION
PANEL 843CZ PANEL ASSEMBLY - EMERGENCY ESCAPE HATCH - COVER PLATE IS CRACKED.<[01] REPLACED COVER PLATE PER AMM 52-22-51;[02] C/W INSPECTION
PANEL 833CZ PANEL ASSEMBLY - EMERGENCY ESCAPE HATCH - COVER PLATE HAS A CRACK.<[01] REPLACED COVER PLATE PER AMM 52-22-51;[02] C/W INSPECTION
PANEL 832CZ PANEL ASSY - EMERGENCY ESCAPE HATCH - COVER PLATE HAS A CRACK<[01] REPLACED COVER PLATE PER AMM 52-22-51;[02] C/W INSPECTION
FWD. CARGO COMPARTMENT TRANSITION ANGLE AT STA. 480+13 RBL 24 HAS SURFACE CORROSION.<[01] TRANSITION ANGLE FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. R/R TRANSITION ANGLE PER SRM 51-40-02;[02] C/W INSPECTION
FWD. CARGO COMPARTMENT TRANSITION ANGLE AT STA. 500+10 RBL 24 HAS SURFACE CORROSION.<[01] R/H TRANSITION ANGLE AT STA 500+10 IS OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2.;[02] R/R ANGLE PER SRM 51-40-02;[03] C/W INSPECTION
FWD. CARGO COMPARTMENT DOOR THRESHOLD (STA.440-480+12) HAS LIGHT SURFACE CORROSION. (MARKED)<[01] REMOVED DAMAGE FOUND TO BE WITHIN LIMITS PER SRM 53-00-3-1A-2. RESTORED FINISH PER AMM 51-21-72;[02] C/W INSPECTION
AFT CARGO R/H TRANSITION ANGLE STA 727E THRU 727F HAS CORROSION AT 3EA FASTENER HOLES<[01] PART BEING REPLACED F.S. 727 THRU F.S. 767; PART # 146A7502-52 ON NR# TTG8Q00N5E9F PER SRM 51-10-02;[02] C/W INSPECTION.
AFT CARGO R/H TRANSITION ANGLE STA 767 THRU 787 HAS CORROSION AROUND FASTENER HOLES.<[01] REMOVED SECTION OF RIGHT TRANSITION SHIELD FROM AIRCRAFT PER SRM 51-40-02. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1.;[02] VERIFIED WORK PERFORMED ON CORRECTIVE ACTION #1;[03] INSTALLED TRANSITION ANGLE PER SRM 51-40-02.
AFT CARGO R/H TRANSITION ANGLE STA 747 THRU 767 HAS CORROSION AROUND FASTENER HOLES.<[01] PART BEING REPLACED F.S. 727 THRU F.S. 767; PART # 146A7502-52 ON NR# TTG8Q00N5E9F PER SRM 51-10-02;[02] C/W INSPECTION.
AFT CARGO R/H TRANSITION ANGLE STA 727J THRU 747 HAS CORROSION AROUND FASTENER HOLES.<[01] PART BEING REPLACED F.S. 727 THRU F.S. 767; PART # 146A7502-52 ON NR# TTG8Q00N5E9F PER SRM 51-10-02;[02] C/W INSPECTION.
AFT CARGO R/H TRANSITION ANGLE STA 727I THRU 727J HAS CORROSION AROUND FASTENER HOLES.<[01] PART BEING REPLACED F.S. 727 THRU F.S. 767; PART # 146A7502-52 ON NR# TTG8Q00N5E9F PER SRM 51-10-02;[02] PART BEING REPLACED F.S. 727 THRU F.S. 767; PART # 146A7502-52 ON NR# TTG8Q00N5E9F PER SRM 51-10-02;[03] C/W INSPECTION.
AFT CARGO R/H TRANSITION ANGLE STA 727H THRU 727I HAS CORROSION AROUND FASTENER HOLES.<[01] PART BEING REPLACED F.S. 727 THRU F.S. 767; PART # 146A7502-52 ON NR# TTG8Q00N5E9F PER SRM 51-10-02;[02] C/W INSPECTION.
AFT CARGO R/H TRANSITION ANGLE STA 727G THRU 727H HAS CORROSION AT FASTENER HOLES.<[01] PART BEING REPLACED F.S. 727 THRU F.S. 767; PART # 146A7502-52 ON NR# TTG8Q00N5E9F PER SRM 51-10-02;[02] C/W INSPECTION.
AFT CARGO R/H TRANSITION ANGLE STA 727E -8 HAS CORROSION AT FASTENER HOLE.<[01] PART BEING REPLACED F.S. 727 THRU F.S. 767; PART # 146A7502-52 ON NR# TTG8Q00N5E9F PER SRM 51-10-02;[02] C/W INSPECTION.
FWD CARGO THRESHOLD FWD CORNER CASTING IS CRACKED.<[01] R/R FWD CARGO THRESHOLD FWD CORNER SCUFF PLATE PER AMM 53-11-02;[02] C/W INSPECTION.
AFT CARGO R/H TRANSITION ANGLE JUST AFT OF STA 727C HAS A HOLE.<[01] DAMAGE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] REMOVED R/H TRANSITION ANGLE FROM F.S. 727 TO F.S. 767 PER SRM 51-10-02;[03] VERIFIED WORK PERFORMED ON CORRECTIVE ACTIONS 1 & 2;[04] INSTALLED NEW TRANSITION ANGLE ASSEMBLY PER SRM 51-10-02.
R/H WING T/E WIGGLE PLATE IS CRACKED AT IRSS 220. MRKD<[01] REMOVED; DRILLED UP AND INSTALLED NEW WIGGLE PLATE PER SRM 51-40-02.
R/H WING T/E DEFLECTION CONTROL RIB I/B SIDE L-ANGLE IS CRACKED AT ATTACH FASTENERS. MRKD<[01] REMOVED CRACKED ANGLE.;[02] REJECT: CORRECTIVE ACTION #1 DOES NOT CONTAIN A REFERENCE USED FOR THE WORKED PERFORMED AS REQUIRED PER MPM 51.03.01. SEE FAULT TTG8Q00NB9U9 FOR REJECT.;[03] REMOVED CRACKED ANGLE PER SRM 51-40-02.;[04] VERIFIED CORRECTION OF REJECT FAULT IN C/A#2.;[05] DRILLED NEW ATTACH ANGLE AND INSTALLED NEW PER SRM 51-40-02
R/H WING T/E DEFLECTION CONTROL RIB UPPER FLANGE AND UPPER PANEL RIB ARE WORN FROM ATTACH BOLTS LOOSE AND WORKING. MRKD<[01] REMOVED LARGE AND SMALL SERRATED PLATES.;[02] REJECT: CORRECTIVE ACTION #1 DOES NOT CONTAIN A REFERENCE USED FOR THE WORKED PERFORMED AS REQUIRED PER MPM 51.03.01. SEE FAULT TTG8Q00NBACA FOR REJECT.;[03] REMOVED INBOARD AND OUTBOARD SERRATED PLATES PER SRM 51-40-02.;[04] REMOVED DAMAGE ON DEFLECTION CONTROL RIB UPPER TAB PER SRM 51-10-02 AND SRM 57-51-02-2R-4.;[05] VERIFIED CORRECTION FOR C/A #2 REJECTION. CORRECTION IS MADE IN C/A#3.;[06] ACCOMPLISHED HFEC HOLE PROBE AND SURFACE INSPECTION PER NDT PART 6 51-00-00 PROC. 16 AND PROC. 23 NO DEFECTS NOTED;[07] RH REPAIR DOUBLER SENT OUT TO ADVANTAGE AVIATION FOR HEAT TREAT<BR>AND CAD PLATE;[08] REF: SRM 57-51-02-2R4-4 FOR REPAIR DOUBLER;[09] C/W INSPECTION.;[10] LOCATED AND DRILLED REPAIR PARTS PER SRM 57-51-020-2R-4 AND 57-51-02-2R-1.;[11] C/W INSPECTION OF LOCATED AND DRILLED REPAIR PARTS PER SRM 57-51-020-2R-4 AND 57-51-02-2R-1.;[12] ALODINED AND PRIMED REPAIR PARTS PER SRM 51-20-01. OK TO INSTALL REPAIR PARTS PER SRM?S 57-51-02-2R-1 & 57-51-02-2R-4;[13] OK TO INSTALL REPAIR PARTS PER SRM?S 57-51-02-2R-1 & 57-51-02-2R-4;[14] INSTALLED REPAIR PARTS PER SRM?S 57-51-02-2R-1 & 57-51-02-2R-4;[15] VERIFIED 14. GREGORY BAXTER (TECHNICIAN); 18-SEP-2023 17:24 UTC<BR>INSTALLED REPAIR PARTS PER SRM?S 57-51-02-2R-1 & 57-51-02-2R-4;[16] REPAIRED PER SRM?S 57-51-02-2R-1 & 57-51-02-2R-4
FORWARD ENTRY SLIDE HAS EXTRA FABRIC HANGING LOOSE<[01] VERIFIED SECURITY OF L1 SLIDE PER AMM 25-66-01. OPS CHECK GOOD
FORWARD ENTRY DOOR SLIDE GIRT BAR AFT STOP NOT SECURE / [01] RESECURED FORWARD ENTRY DOOR AFT GIRT BAR STOP IAW SIP
FORWARD SERVICE DOOR GIRT BAR LOOSE / [01] RE-SECURED FWD SERVICE DOOR GIRT BAR IAW AMM 25-66-01; NO OTHER DEFECTS NOTED AT THIS TIME
LEFT BREAK PANEL ASSY HAS CRACK APPROXIMATELY 1 INCH LONG / [01] REMOVED AND REPLACED BREAK PANEL PER AMM 53-12-12. ALT; REF. SRM 51-40-02. (FASTENER).
RIGHT BREAK PANEL ASSY HAS CRACK APPROXIMATELY 2 INCHES LONG / [01] REMOVED AND REPLACED RIGHT BREAK PANEL PER AMM 53-12-12.ALT REF. SRM 51-40-02.
FWD GALLEY CAPT SIDE FLASHLIGHT FLASHING RED / [01] R & R FLASHLIGHT (ON CAPT SIDE)<BR>BATTERY PACK I.A.W S.I.P <BR>OPS CHCK GOOD.
FORWARD GALLEY GIRT BAR DIFFICULT TO SECURE IN UN-ARMED POSITIO. RIGHT SIDE OF RETAINING CLIP APEERS LOOSE. / [01] RE-SECURED FWD GALLEY SERVICE DOOR STOWAGE RETAINER PER MM 25-66-01
FWD INBOARD EMERGENCY FLASHLIGHT WILL NOT PUSH-TO-TEST / [01] R&R FLASHLIGHT AND BATTERY PER AMM 25-64-00. OPS CK GOOD
AT APPROXIMATELY 12;000 FEET ON ARRIAL INTO APPROACH; WE NOTICED AN ENG FAIL ON THE #1 EGT INDICATOR. IT APPEARED MOMENTARILY AND THEN CLEARED. SECONDS LATER; THE SAME ENG FAIL ANNUCIATION OCCURED. #1 EGT INDICATION WAS ERRATIC. THRUST LEVER CHANGES MADE NO CHANGES ON THE #1 ENGINE N1 INDICATOR. NO OTHER ABNORMAL INDICATIONS WERE PRESENT. QRH WAS COMPLIED WITH; ATC NOTIFIED; EMERGENCY DECLARED. BRAKING NORMAL. BRAKE COOLING CHARTS COMPLIED WITH (#1 ENGINE ENGINE PER QRH WAS SHUT DOWN IN-FLIGHT) / REMOVED AND REPLACED HMU IAW MT 773-21-10 REF LOGPAGE 1959778 FOR EEC REMOVAL AND INSTALLATIONPOS 1 PN OFF/ON; 442653 SN OFF; BECWF356 SN ON; BECW2207
L/H HORIZONTAL L/E FWD UPPER SLIDING SEAL CRACKED / REMOVED & REPLACED L/H HORIZONTAL L/E FWD UPPER SLIDING SEAL PER MM 53-31-31AMT 65828INSP 31326
LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED / REMOVED AND REPLACED LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31AMT 128968INSP 67932
FWD GALLEY INBOARD FLASH LIGHT SHOW RED WHEN TESTING ( CABIN EMERGENCY FLASHLIGHT HOLDERS/FLASHLIGHTS ) / DMA #0419509R&R FWD GALLEY INBD FLASHLIGHT BATTERY AND INSP STICKER AS PER MM25-64-00 CLR #76198
FORWARD CABIN OUTBOARD EMERGENCY FLASHLIGHT DID NOT TEST. RESET FLASHLIGHT IN HOLDER PER AMM.
LT LOWER EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.