N7822A
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2017-02-11 – 2017-02-11 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2017-02-11 – 2017-02-11 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
L2 GIRT BAR DOOR BRACKET LOOSE. R&R RIVET PER SIP.
FWD ENTRY DOOR GIRT BAR J-HOOKS LOOSE <[01]. ADJUSTED J-HOOKS ON FWD ENTRY DOOR ESCAPE SLIDE FOR GIRT BAR REF. AMM 52-11-00 OPS CHECK GOOD.
EMERGENCY LIGHTS ON UPON ARRIVAL. CYCLED AFT EMERGENCY SWITCH TO OFF ; OPS CHKD OK IAW MM 33-51-00.
FORWARD GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. R/R BATTERY PER AMM 25-64-00.
PANEL 193AL HAS 3.6' CRACK ON UPPER AFT CORNER FROM CONTACT WITH GEAR DOOR <[01]. COMPLIED WITH EA 25-153-01017 INSTRUCTIONS FOR INSPECTION; CLEANING AND TAPING.; [02] CHANGED FAILURE TYPE AND EDITED MEASUREMENTS; [03] CHANGED RII AND MAJOR REPAIR BACK TO 'NO'.
ELECTRICAL BURNING SMELL ON FLIGHT DECK AND FOLLOWED THROUGH CABIN THEN A FEW MINUTES LATER; LEFT PACK TRIP OFF ANNUNCIATOR LIGHT CAME ON <[01] FOUND ACM LH SEIZED. R/R LH ACM PER AMM 21-51-04; OPS OK.
AFT SERVICE DOOR SLIDE BAR HOLDER NUT PLATE BROKEN.<[01] INSTALLED NEW NUT PLATE; @0530 REQUIRES CURE TIME OF 1 HOUR.;[02] NUT PLATE IS FULLY INSTALLED IAW SRM 51-40-10.
PASSENGER CABIN SEAT RECLINES AT SEAT 11B EMERGENCY EXIT ROW<[01] ADJUSTED RECLINE AT 11B PER CMM 25-23-46.
SEAT 11B RECLINING AT EMERGENCY EXIT<[01] READJUSTED SEAT 11B RECLINE LOCK RING AT EMERGENCY EXIT PER CMM 25-21-42
AFT ENTRY DOOR GIRT BAR BRACKET LOOSE<[01] TIGHTEND BRACKET PER SIP
L/H HORIZONTAL LOWER SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED LOWER SLIDER PER AMM 53-31-31.
L/H HORIZONTAL UPPER SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED SLIDER PER AMM 53-31-31.
LH AFT EXTERIOR EMER EXIT LIGHT OUT<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-04-960-801-NG (SLIDE/OVERWING LIGHT - LAMP REPLACEMENT - PERMANENT)]
FWD ENTRY EMER SLIDE CASING CAME LOOSE WHEN OPENING DOOR<[01] ACCOMPLISHED MT 725-61-06 REM/INSTL PER M/M 25-66-01
AFT LEFT SERVICE DOOR SLIDE EXPOSED<[01] ADJUSTED AFT SERVICE DOOR SLIDE GIRT BAR AND FLAP; REF AMM 25-66-01. A/C OK FOR SERVICE
OUT OF ROUND HOLE WITH ADJACENT GOUGE TO FLANGE SURFACE; LH HORIZONTAL STAB RIB AT STAB STA 129.50; LOWER OB FLANGE 23.5' FROM FWD EDGE.<[01] REPAIRED DAMAGE IAW EA 23-155-02777
FCB SUB THRESHHOLD WEB IS CORRODED FROM BS 480+1 - 460+11; RBL 32; WL 32 CORRECT WL 157<[01] UPDATED STEP 5;[02] UPDATED STEP 6;[03] UPDATED STEP 6 AND 7;[04] SRM 53-30-15-1A-1 FOUND TO BE APPLICABLE; BLENDED MULTIPLE CORROSION AT FBC SUB THRESHOLD WEB BS 480+1 - 460+11; RBL 32; WL 157; WORK AREA; L 1.5' X W 1.0' X D 0.009'; ORIGINAL THICKNESS 0.045'; REMAINING THICKNESS 0.039; DEEPEST FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15-1A-1; USE DEPTH GAUGE ID:ATS401 DUE:10/23; REMOVED SUB THRESHOLD FCB FROM BS 440 TO BS 492; IAW SRM 51-40-02-0G-0; INSTALLED NUTPLATES ON NEW SUBTHRESHOLD WEB IAW SRM 51-40-02-0G-0 AND DWG 143A8330; ID: 0013; REV: A ; APPLIED BMS 10-11 TYPE 2 ANAMEL IAW SOPM 20-41-02; APPLIED CIC IAW AMM 51-21-91-620-802; INSTALLED NEW SUB THRESHOLD ON FCB BETWEEN BS 440 TO BS 492; RBL 32; WL 157 IAW SRM 51-40-02-0G-0 AND DWG 143A8330; ID:: 0015; REV: A;[05] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 4 AND MEASUREMENT TABLE.
AFT CARGO BAY; AFT CORNER SCUFF PLATE CRACKED<[01] UPDATED STEP 5.;[02] COMPLETED STEP 5.;[03] COMPLETED STEP 6.;[04] REMOVED PROTECTIVE COATINGS FROM SCUFF PLATE PRIOR TO WELDING PER SRM 53-60-15-2R-1 PARAGRAPH 4.B. (2) AND SOPM 20-30-02. WELDED CRACKED RADIUS OF SCUFF PLATE PER SRM 53-30-15-2R-1 PARAGRAPH 4.B. (4). PT INSPECTED AREA IAW SOPM 20-20-02. SANDED THE WELD REPAIR AREA PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(5). APPLIED CHEMICAL CONVERSION COATING IAW SOPM 20-43-03. APPLIED TWO COATS OF BMS 10-11 TY1 PRIMER IAW AMM 51-21-72-370-804.;[05] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 4.
L/W T/E PANEL 551GB AFT SEAL RETAINER IS CRACKED<[01] REPLACED L/W T/E PANEL 551GB AFT SEAL RETAINER PER AMM 20-50-11.;[02] CORRECTION: REPLACED L/W T/E PANEL 551GB AFT SEAL RETAINER PER AMM 20-50-11.;[03] CORRECTION: REPLACED L/W T/E PANEL 551GB AFT SEAL RETAINER PER AMM 20-50-11.<BR>SCREWGUN ID: ATS2589 EXP:08/2024;[04] UPDATED INSTALLED PART SIGN OFF;[05] UPDATED INSTALLED PART SIGN OFF;[06] VERIFIED CORRECTIVE ACTION 1-5
CORROSION ON FRAME CHORD AT AREA AFT OF FWD CARGO BAY BS500D RBL8 WL151.<[01] VERIFIED CORROSION REMOVED; THE REQUESTED NDT INSPECTIONS IS FOR ENGINEERING SUPPORT.;[02] COMPLETED STEP 6.;[03] REJECTED: SEE TTG8Q00NJT8E AND TTG8Q00NJTH5;[04] ACCOMPLISHED EA 23-153-02719 (N7822A - ATS(PAE) - REPAIR TO FAILSAFE CHORD BS 500D WL 151;[05] VERIFIED.<BR>VERIFIED MEASUREMENTS.
CRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-22R WL172. MARKED<[01] UPDATED STEPS 2-3;[02] UPDATED STEPS 6-8;[03] PARTIAL STEPS 6-7-8;[04] PARTIAL UPDATE STEPS 6 AND 7;[05] COMPLETED STEP 7 AND 8.;[06] STEP 3 COMPLETE;[07] REMOVED DAMAGED STR SECTION BETWEEN BS 500D+10 AND BS 540 S-22R; REPAIRED STRINGER 22R SRM 53-00-03-2R-1 AND EA#23-153-02702;[08] VERIFIED MEASUREMENT TABLE.;[09] VERIFIED CORRECTIVE ACTION 7.
LEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 129.50; 3RD VERTICAL STIFFENER IS CRACKED.<[01] SRM 55-10-09-2R-4 STEP 4. E. INSPECTION FOUND DAMAGE ADJACENT TO REPAIR AREA; GENERATED TTG8Q00NBZEC; SEE SUB-STEP 9.;[02] REPAIR OF L/H HORIZONTAL STAB INSPAR RIB 3RD VERTICAL STIFFENER AT STAB STA 129.50 AND OUT OF ROUND HOLE ON LOWER FLANG ACCOMPLISHED ON FAULT TTG8Q00NBZEC REFERANCE EA 23-155-02777;[03] ?REFER TO FAULT TTG8Q00NBZEC WHERE EA 23-155-02777 WAS ADDED AS A SUBTASK?;[04] VERIFIED CORRECTIVE ACTION COMPLETE. VERIFIED MEASUREMENT TABLE.
LH HORIZONTAL STABILIZER LOWER SKIN - .7' CRACK FOUND 27' FROM FWD EDGE AT RIB STA 184.70<[01] REPAIRED PER EA 23-155-02717 WITH REPETITIVE INSPECTION PROGRAM DEFINED IN EA 23-155-02717-INSP.';[02] TASK CARD COMPLETE.
LH HORIZONTAL STABILIZER LOWER SKIN - .7' CRACK FOUND 18' FROM FWD EDGE AT RIB STA 193.90<[01] REFER TO FAULT TTG8Q00N5DVD WHERE EA 23-155-02717 WAS ADDED AS A SUBTASK;[02] VERIFIED CORRECTIVE ACTION 1
WING CENTER SECTION HAS A CRACKED BREAK PANEL AT BS 540; LBL 1; WL 207<[01] UPDATED STEPS 1;2;[02] UPDATED STEP 3;[03] UPDATED STEP 3 ADDED REFERENCE;[04] CERTIFIED CHANGE TO STEP 3;[05] UDATED STEP 4 INSTALLED BREAK PANEL;[06] UPDATED MEASUREMENT TABLE;[07] UPDATED PARTS;[08] TASK COMPLETE
WING CENTER SECTION HAS A CRACKED CABLE INTERCOSTAL ATTACH ANGLE AT BS 685+7; RBL 24; WL 203<[01] UPDATED STEPS 1-4;[02] INSTALLED NEW ANGLE AT BS 685+7; RBL 24; WL 203 PER SRM 51-40-02-0G-0 AND DWG 273A9110;[03] VERIFIED CORRECTIVE ACTION #2.<BR>VERIFIED MEASUREMENTS.
WING CENTER SECTION HAS A CRACKED CABLE INTERCOSTAL ATTACH ANGLE AT BS 685+7; LBL 24; WL 203<[01] UPDATED STEPS 1-4;[02] INSTALLED NEW ANGLE AT BS 685+7; LBL 24; WL 203 PER SRM 51-40-02-0G-0 AND DWG 273A9110;[03] VERIFIED CORRECTIVE ACTION #2.<BR>VERIFIED MEASUREMENTS.
LH HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 111.10; 3RD VERTICAL STIFFENER IS CRACKED.<[01] UPDATED STEP 2;[02] REPAIRED L/H HORIZONTAL STABILIZER INSPAR RIB; (STAB. STA. 111.10) 3RD VERTICAL STIFFENER IAW SRM 55-10-09-2R-4.;[03] VERIFIED STEPS 4 & 5 AND MEASUREMENT TABLE
FED CUTOUT SURROUND STRUCTURE - CRACK ON UPPER CHORD FRAME ASSY BS 312 STR-5L<[01] REQUEST NDI TO VERIFY CRACK AND IF CRACKED MARK ENDS OF CRACK BS 312 STR 5L UPPER RADIUS OF FRAME;[02] ACCOMPLISHED HFEC SURFACE SCAN IAW 737 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23. CRACK CONFIRMED; MEASURED AT L: 0.2' MARKED.<BR><BR>EQUIPMENT USED: NORTEC 600 ID: ATS1465 CAL DUE: 09/2023;[03] UPDATED MEASUREMENT TABLE;[04] REPAIRED CRACK BS 312 STR 5L ON M-22-153-01244; TTG8Q00N56CS;[05] VERIFIED COMPLETION OF CORRECTIVE ACTIONS 4 AND MEASUREMENT TABLE.
HORIZONTAL PRESSURE DECK CRACKED BS664.5; WL 202; LBL52 APPROX 1 INCH IN LENGTH. MARKED WITH BLACK SHARPIE.<[01] REPAIRED HORIZONTAL BEADED PRESSURE DECK WEB BETWEEN STA 663.75 TO 675 LBL 30 TO LBL 60 PER SRM 53-40-51-2R-2. FIG. 203.;[02] VERIFIED CORRECTIVE ACTION #1;[03] REPAIRED CRACK IN HORIZONTAL PRESSURE DECK BS 664.5; WL 202; LBL 52 PER SRM 53-40-51-2R-2.
RIGHT WING T/E ORSS 280 TRANSVERSE WEB O/B L-CLIP ATTACHED TO DEFLECTION CONTROL RIB IS CRACKED<[01] PARTIAL UPDATE STEPS 1 AND 2;[02] COMPLETED STEPS 1 AND 2;[03] TASK COMPLETE.
RIGHT WING T/E VERTICAL SEAL RETAINER IS CRACKED AT ORSS 268 JUST ABOVE AFT PYLON FAIRING TIP<[01] REMOVED AND REPLACED RIGHT WING T/E VERTICAL SEAL RETAINER IAW SRM 51-40-02-0G-0;[02] JOB COMPLETE.;[03] VERIFIED MEASUREMENTS.
DURING DESCENT AT APPROXIMATELY 27;000 FEET CREW NOTICE ABNORMAL SMELL THROUGHOUT COCKPIT AND CABIN. SMELL DESCRIBED AS WAXY OR OILY.<[01] COMPLIED WITH SMOKE AND FUMES CONDITIONAL INSPECTION PER MM O5-51-56. FOUND A HYD SYSTEM SERVICED T0 96% AND B SYSTEM AT 106%. DRAINED AND SERVICED PER AMM 12-12-00. REPLACED A&B RESERVOIR CROSS FITTING CHECK VALVES PER AMM 29-09-04. REPLACED RECIRC FAN FILTER PER MM 21-25-01 AND WATER SEPARATOR SOCKS PER MM 21-51-05.
F/A REPORTS L1 GIRT BAR LOOSE<[01] RESECURED GIRT BAR BRACKET PER SIP
LEFT WING- AFT FLAP DEFLECTION SUPPORT BEAM UPPER BRACKET CRACKED<[01] ACCOMPLISHED OF L/H WING AFT FLAP FIXED TRAILING EDGE DEFLECTION SUPPORT BEAM UPPER TAB PER SRM 57-51-02-2R-3 REPAIR 3.
RIGHT WING - AFT FLAP DEFLECTION BEAM UPPER TAB CRACKED.<[01] REMOVED DAMAGED UPPER TAB FROM DEFLECTION CONTROL RIB; LOCATED AND DRILLED REPAIR PART PER SRM 57-51-02-2R REPAIR 3.;[02] REPAIRED RH WING AFT FLAP DEFLECTION BEAM UPPER TAB IAW SRM 57-51-02-2R-3
RIGHT WING - FIXED LOWER TE PANEL WIGGLE PLATE OTB OF #6 FLAP SUPPORT CRACKED.<[01] REMOVED AND REPLACED RIGHT WING T/E PANEL WIGGLE PLATE PER AMM 57-50-02.;[02] REMOVED AND REPLACED RIGHT WING T/E PANEL WIGGLE PLATE PER AMM 57-50-02.
LEFT WING-AFT TRAILING EDGE UPPER PANEL SUPPORT BRACKET CRACKED JUST OUTBOARD OF #3 FLAP TRACK<[01] REMOVED AND REPLACED LEFT WING-AFT TRAILING EDGE UPPER PANEL SUPPORT BRACKET PER SRM 51-40-02.
MULTIPLE EMERGENCY LIGHT BATTERIES FAILED CAPACITY CHECK.<[01] PERFORMED DEEP CYCLE AND RECHECKED CAPACITY FOR FAILED BATTERIES IAW AMM 33-51-06. FOUND BATTERY AT M1672 TO BE THE ONLY ONE TO FAIL AFTER DEEP CYCLE. REMOVED AND REPLACED BATTERY AT M1672 LOCATION REFERENCING AMM 33-51-06. OPS CHECK GOOD.
DURING INTERNAL DVI ON NOSE RADOME FOUND A 3 CRACK AT THE 10 O CLOCK POSITION LOOKING FROM AFT.<[01] REMOVED 14 OUT OF 16 RADOME BOLTS.;[02] R/R NOSE RADOME PER AMM 53-52-00.
EMERGENCY EXIT SIGN LOOSE OVER WING EXIT AIRCRAFT RIGHT / [01] REINSTALLED EMERGENCY LIGHT COVER AT OVER WING EXIT SIGN PER AMM 33-51-04
R/H OVERWING EXTERIOR EMERGENCY LIGHT INOP ; / [01] RELAMPED R/H EXTERIOR OVERWING EMERGENCY EXIT LIGHT IAW B737 AMM 33-51-04.
PANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES. ; / [01] REPLACED PANEL 193B PER SRM 51-40-02
SUPPLEMENTAL INFORMATION: FWD ENTRY DOOR SLIDE GIRT BAR HARD TO RELEASE FROM FROM FLOOR ATTACHMENTS ; / [01] REMOVED DEBRIS FROM FWD ENTRY DOOR GIRT BAR FLOOR ATTACH POINTS PER SIP AND LUBED LATCHES
FRONT ENTRY EMERGENCY SLIDE DETACHED FROM ITS COMPARTMENT AFTER FLIGHT ATTENDANT CORRECTLY SECURED GIRT BAR FROM ITS ARMED POSITION. FRONT ENTRY DOOR WAS UNABLE TO BE FULLY OPENED ; / [01] CW MT 725-61-06
EMERGENCY EXIT AISLE LIGHTS AT SEAT ROWS 9CBA AND 17CBA ARE INOP ; / [01] REMOVED; REPLACED AND PERFORMED GOOD OPERATIONAL CHECK OF EMERGENCY EXITS AISLE LIGHT LAMPS AT SEAT ROWS 9CBA AND 17CBA PER AMM 33-51-03-960-801; [02] VERIFIED REMOVED; REPLACED AND PERFORMED GOOD OPERATIONAL CHECK OF EMERGENCY EXITS AISLE LIGHT LAMPS AT SEAT ROWS 9CBA AND 17CBA PER AMM 33-51-03-960-801.
RIGHT OVERDOOR EXIT SIGN DOES NOT ILLUMINATE; OTHER LIGHTS RELATED TO M1675 BATT PACK OPERATE CORRECTLY. ; / [01] FOUND 7822 CAME IN WITH D40042J CONNECTOR PART NUMBER BACC65AK221P SHOULD BE BACC65AK211P PER WDM EQUIPMENT LIST. CONNECTOR DID NOT MATE PROPERLY WITH THE PLUG-SIDE CONNECTOR AND THUS WOULD HAVE ONLY WORKED INTERMITTENTLY. REMOVED AND REPLACED D40042J INSTALLING CORRECT PN CONNECTOR PER WDM 33-1-12 AND SWPM 20-72-24. PERFORMED A GOOD OPS CHECK OF L1063 PER AMM 33-51-00-710-801; [02] VERIFIED CORRECTIVE ACTION 1. CHECKS GOOD.
LEFT EMERGENCY LIGHTING SYSTEM GROUND ILLUMINATION LIGHT DOES NOT ILLUMINATE ; / [01] RELAMPED LEFT GROUND ILLUMINATION LIGHT; LIGHT STILL DOES NOT ILLUMINATE PER TASK 33-51-04-960-801<BR>.; [02] VERIFIED RELAMPED LEFT GROUND ILLUMINATION LIGHT; LIGHT STILL DOES NOT ILLUMINATE PER TASK 33-51-04-960-801; [03] UPON FURTHER INVESTIGATION; FOUND CONN D10716 DISCONNECTED FROM EMERGENCY EXIT LIGHT BATT PACK M1670. CONNECTED D10716 PER SWPM 20-60-06. PERFORMED GOOD TEST OF EMERGENCY LIGHTING GROUND ILLUMINATION LIGHTS PER AMM 33-51-00-710-801.<BR>ACCESSED AND RESTORED AIR RETURN GRILLE AT STA 727C+13 WL 212 LBL 68 PER AMM 21-23-03-000-801 AND AMM 21-23-03-400-802;
SUPPLEMENTAL INFORMATION: AFT CARGO BAY ANGLE CRACKED BS 867 LBL 15 WL 156 ; / [01] UPDATED MEASUREMENTS; [02] LOCATED AND DRILLED ANGLE BS 867 LBL 15 WL 156; OK TO INSTALL PER SRM 51-40-02-0G-0 AND DWG 149A8102; [03] REMOVED CRACKED CLIP BS 867 LBL 15 WL 156 PER SRM 51-40-02-0G-0; [04] AFT CARGO BAY CRACKED ANGLE BS 867 LBL 15 WL 156 FOUND OUT OF LIMITS DUE TO NO LIMITS ESTABLISHED IN SRM; [05] LOCATED AND DRILLED ANGLE BS 867 LBL 15 WL 156; OK TO INSTALL PER SRM 51-40-02-0G-0 AND DWG 149A8102; [06] VERIFIED CORRECTIVE ACTIONS 2-5. OK TO INSTALL.; [07] INSTALLED ACB ANGLE BS 867 LBL 15 WL 156 PER DWG 149A8102 ;DWG 149A8104 AND SRM 51-40-02-0G-0; [08] VERIFIED INSTALLED ACB ANGLE BS 867 LBL 15 WL 156 PER DWG 149A8102 ;DWG 149A8104 AND SRM 51-40-02-0G-0
ACB R/H FLOOR TO SIDEWALL SUPPORT BS 887-947 HAS OVERSIZED HOLES AT SPLICE LOCATION BS 887 RBL 25 WL 156 ; / [01] REMOVED ACB FLOOR TO SIDEWALL SUPPORT AT BS887 - BS947; RBL25; WL156 PER SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED ACB FLOOR TO SIDEWALL SUPPORT AT BS887 - BS947; RBL25; WL156 PER SRM 51-40-05-0G-0 AND DWG 147A7500; [03] NEW FLOOR TO SIDEWALL SUPPORT BS 887-847 RBL 25 TO BE INSTALLED ON CUST CARD# TTG8Q006DC17; [04] VERIFIED CORRECTIVE ACTION 2 & 3.
FWD CARGO BAY BULKHEAD R/H SIDEWALL SUPPORT ANGLE AT 500D LOWER FLANGE I/B FASTENER HOLE ELONGATED ; / [01] ELONGATED HOLE FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [02] VERIFIED OUT OF LIMITS; [03] REMOVED FWD CARGO BAY BULKHEAD SUPPORT ANGLE AT BS 500D STR 18R TO 26R PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED NEW FCB BULKHEAD SUPPORT ANGLE P/N: 143A9485Y34 LOT #1464138-1 AT BS 500D STR 18R TO 26R IAW. SRM 51-40-05 DWG 143A7902 ID:0174 REV:- .; [05] RECEIVED PART; [06] VERIFIED CORRECTIVE ACTION ENTRY 5.; [07] OK TO INSTALL BULKHEAD BS 500D STR 18R TO 26R; [08] VERIFIED OK TO INSTALL BULKHEAD BS 500D STR 18R TO 26R; [09] INSTALLED FWD CARGO BAY BULKHEAD R/H SIDEWALL SUPPORT ANGLE AT BS 500D STR 18R TO 26R PER SRM 51-40-02-0G-0; DWG 143A7902 AND DWG 143A9481; [10] VERIFIED INSTALLED FWD CARGO BAY BULKHEAD R/H SIDEWALL SUPPORT ANGLE AT BS 500D STR 18R TO 26R PER SRM 51-40-02-0G-0; DWG 143A7902 AND DWG 143A9481
FWD CARGO BAY BULKHEAD L/H SIDEWALL SUPPORT ANGLE AT 500D LOWER FLANGE I/B FASTENER HOLE ELONGATED ; / [01] ELONGATED HOLE FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [02] VERIFIED OUT OF LIMITS; [03] REMOVED FWD CARGO BAY BULKHEAD SUPPORT ANGLE AT BS 500D STR 18L TO 26L; [04] REMOVED FWD CARGO BAY BULKHEAD SUPPORT ANGLE AT BS 500D STR 18L TO 26L PER SRM 51-40-02-0G-0; [05] LOCATED AND DRILLED NEW FCB BULKHEAD SUPPORT ANGLE P/N: 143A9485U30 LOT:1463858-1 AT BS 500D STR 18L TO IAW. SRM 51-40-05 AND DWG: 143A7902 ID:0174 REV:-; [06] VERIFIED CORRECTIVE ACTION ENTRY 5.; [07] OK TO INSTALL BULKHEAD BS 500D STR 18L TO 26L; [08] VERIFIED OK TO INSTALL BULKHEAD BS 500D STR 18L TO 26L; [09] INSTALLED FWD CARGO BAY BULKHEAD L/H SIDEWALL SUPPORT ANGLE AT BS 500D STR 18L TO STR 26L PER SRM 51-40-02-0G-0 DWG 143A7902 AND DWG 143A9481; [10] VERIFIED INSTALLED FWD CARGO BAY BULKHEAD L/H SIDEWALL SUPPORT ANGLE AT BS 500D STR 18L TO STR 26L PER SRM 51-40-02-0G-0 DWG 143A7902 AND DWG 143A9481
FORWARD CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. WELDED CRACKED FCB AFT CORNER SCUFF PLATE PER SRM 53-30-15-2R-1 PARA 4. B.(2) AND (4) ACCOMPLISHED FPI INSPECTION TO SCUFF PLATE IAW BOEING SOPM 20-20-02. NO CRACKS NOTED. SANDED REPAIR WELD AREA IAW SRM 53-30-15-2R-1 PARA 4.B.(5) SCUFF PLATE WAS REPAIRED PER SRM 53-30-15-2R-1 PARA 4. B. (2) AND (4). SCUFF PLATE WILL BE INSTALLED ON FAULT TTG8Q003G2EG VERIFIED COMPLETION OF STEP 7.
PANEL 191AL INNER SURFACE; FWD LOWER CORNER IS CRACKED AT CORE ; / [01] IDENTIFIED PANEL 191AL IAW SRM 53-30-70-0I-1.FIG 2; ITEM [1]. FOUND DAMAGE AT 3' FROM FWD EDGE; 2'FROM LOWER EDGE TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-30-70-1A-1.PARA 4.A.(1). REQUIRES REPAIR PER SRM 51-70-05-2R-1 IAW SRM 53-30-70-2R-1.TABLE 201.<BR>REMOVED APPROX. 3'X3' DAMAGED PLIES IAW SRM 51-70-05-2R-1.PARA 4.A-B.; [02] VALIDATED APPLICABILITY OF SRM 51-70-05-2R-1 IAW SRM 53-30-70-2R-1.; [03] INSPECTED AND VERIFIED CORRECTIVE ACTION ITEMS 1 AND 2. OKAY TO PROCEED PER SRM 51-70-05-2R-1.; [04] APPLIED VACUUM BAG FOR MOISTURE REMOVAL; CHECKED FOR LEAKS. LEAK CHECK GOOD. SET TO CURE USING HEATCON ID:ATS532 S/N:15092117 IAW SRM 51-70-05-2R-1.PARA 4.B.; [05] COMPLETED MOISTURE REMOVAL; NO CONTAMINATION NOTED; REMOVED VACUUM BAG; FABRICATED REPAIR PLIES OUT OF BMS 8-79 ST 120 LOT#1458373-1; BMS 8-79 ST 1581 LOT#1466502-1; AND BMS 5-129 GR5 LOT#1464324-2; INSTALLED; VACUUM BAGGED; CHECKED FOR LEAKS AND SET TO CURE USING HEATCON HOTBONDER ID:ATS532 S/N:15092117 IAW SRM 51-70-05-2R-1 PAR 4B-E.; [06] CURED; UNBAGGED; LIGHTLY SANDED; AND CLEANED REPAIR PLIES IAW SRM 51-70-05-2R-1 PAR 4E-G.; [07] VERIFIED CORRECTIVE ACTIONS 4-6; [08] UT INSPECTED POST CURE IAW 737 NDTM PART 4 51-00-02; NO DISBONDS NOTED. EQUIP ID#: ATS2341 S/N: 190848104; [09] REFINISHED REPAIR AREA IAW SRM 51-70-05-2R-1 PAR 4G AND AMM 51-21-99-300-802 PAR 3C(1).<BR><BR>COMPLETED SRM REPAIR 51-70-05-2R-1.; [10] VERIFIED CORRECTIVE ACTION 9
SEAT TRACK ATTACH ANGLE FOR SADDLE CRACKED BS 500D-520 LBL 45 WL205 ; / [01] LOCATED AND DRILLED HOLES ON NEW SEAT TRACK ANGLE FOR SADDLE BS 500D-520 LBL 45 WL 205 IAW SRM 51-40-05 AND DWG 143A5410 ID:0013 REV:B.; [02] CORRECTION FOR CORRECT DWG: DWG 143A5034 ID:006 REV:A; [03] VERIFIED STEP 1AND 2; [04] UPDATED MEASUREMENT TABLE; [05] VERIFIED LOCATE AND DRILL OF NEW ANGLE FOR SADDLE; BS 500D-520; LBL 45; WL 205; PER SRM 51-40-05 AND DWG 143A5410; OK TO INSTALL; [06] INSTALLED NEW ANGLE FOR SADDLE AT BS 500-520; LBL 45; WL 205 DWG 143A5034<BR>ID:006 REV:A.; [07] UPDATED PARTS TABLE; [08] VERIFIED STEP 6; [09] VERIFIED INSTALLED NEW ANGLE FOR SADDLE AT BS 500-520; LBL 45; WL 205 DWG 143A5034 ID:006 REV:A. AND SRM 51-40-02-0G-0; [10] ADDED REFERENCE SRM 51-40-02
CRACK ON END OF STRINGER 26 LEFT B.S. 520+17. ; / REMOVED DAMAGED AREA S-26L BS 500D+10'-540 IAW SRM 53-00-03-2R-1 REP.1; [02] REQUIRED NDI INSPECTION S-26L BS 500D+10' CUT OUT CRACK FREE IAW SRM 53-00-03-2R-1 REP.1 RECEIVED STR REPAIR SECTION FROM OSS FABRICATED FROM 7075-0 .045 LOT #1464744-1 HEAT TREATED TO T6 CONDITION ON SWA PO# 835676 REPAIR HAT SECTION RECEIVED FROM OSS FABRICATED FROM 7075-0 .050 LOT #1457313-101 HEAT TREATED TO T6 CONDITION ON SWA PO#835675 ALL DATED 03 SEP 21;TRIMMED LOCATED AND DRILLED NEW STR AND HAT SECTION FOR STR REPAIR AT STR 26L BS 500D+10 TO 540 APPLIED CHEMICAL CONVERSION COAT TO PARTS AND REPAIR AREA ALL IAW SRM 53-00-03-2R-1 STEPS 4 E F G H AND I FIG 205 OK TO PRIME INSTALLED STR REPAIR AT STR 26 L/H BS 500D+10 TO 540 APPLIED FAY SEAL AND CIC ALL IAW SRM 53-00-03-2R-1 STEPS 4 K AND L AND BOEING DWG 143A3230
CORROSION ON INTERCOSTAL AT B.S. 500D+1; L.B.L. 7; W.L. 151. ; / [01] CORROSION ON INTERCOSTAL WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-04-1A-1 FIGURE 102 DETAIL E.; [02] VERIFIED DAMAGE OUT LIMITS PER SRM 53-00-04-1A-1; [03] LOCATED AND DRILLED NEW INTERCOSTAL P/N 143A9803-15 IAW SRM 51-40-05-0G-0 AND DWG 143A7902. OK TO INSTALL.; [04] VERIFIED LOCATED AND DRILLED NEW INTERCOSTAL P/N 143A9803-15 IAW SRM 51-40-05-0G-0 AND DWG 143A7902. OK TO INSTALL.; [05] INSTALLED NEW INTERCOSTAL P/N 143A9803-15 IAW SRM 51-40-05-0G-0 AND DWG 143A7902.; [06] AND SRM 51-40-02-0G-0; [07] VERIFIED INTERCOSTAL INSTALLED PER SRM 51-40-05-0G-0 AND DWG 143A7902 AND SRM 51-40-02-0G-0; [08] UPDATED MEASUREMENTS; [09] TASK COMPLETE
CRACKED UPPER ANGLE ON SUPPORT WEB BS 927-947 BL 0 WL 208 ; / [01] REMOVED UPPER ANGLE FROM WEB SUPPORT BS 927-947 BL 0 WL 208 PER SRM 51-40-02; [02] LOCATED AND DRILLED NEW UPPER ANGLE ON SUPPORT WEB BS 927-947 BL 0 WL 208 PER SRM 51-40-05-0G-0 AND DWG 147A5430. OK TO INSTALL.; [03] VERIFIED LOCATION AND DRILL UP PER SRM 51-40-05 AND DWG 147A5430; [04] INSTALLED NEW UPPER ANGLE ON SUPPORT WEB BS 927-947 BL 0 WL 208 PER SRM 51-40-02-0G-0 AND DWG 147A5400.; [05] CORRECTION- VERIFIED LOCATION AND DRILL UP PER SRM 51-40-05 AND DWG 147A5430. OK TO INSTALL; [06] VERIFIED INSTALLATION UPPER ANGLE ON SUPPORT WEB BS 927-947 BL 0 WL 208 PER SRM 51-40-02 AND DWG 147A5400; [07] TASK COMPLETE
CRACKED FLOOR SUPPORT BS 344-360 BL 0 WL 208 ; / [01] ET INSPECTED SUSPECTED CRACK IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; VERIFIED CRACK EXISTS.<BR>CAL ID IS000450 N500D; [02] REMOVED INTERCOSTAL AT BS344-360 BL0 WL 208; PER SRM 51-40-02. LOCATED AND DRILLED NEW INTERCOSTAL PER SRM 51-40-05 AND DWG141A5400. REQUEST OK TO INSTALL.; [03] VERIFIED LOCATION AND DRILL UP PER SRM 51-40-05 AND DWG 141A5400. FLOORBOARD HOLES STILL REQUIRED; [04] INSTALL NEW INTERCOSTAL BS 344-360 BL 0 WL208 IAW SRM 51-40-02 AND DWG 141A5400; [05] VERIFIED INSTALLATION AND DRILLING OF FLOORBOARD HOLES IN INTERCOSTAL PER SRM 51-40-02 AND DWG 141A5400.
CRACKED FLOOR SUPPORT BS 277-294 BL 0 WL 208 ; / [01] REMOVED CRACKED SUPPORT AT BS 277-294 BL0 WL 208; LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-40-02 SRM 51-40-05. REQUEST OKAY TO INSTALL; [02] VERIFIED REMOVED CRACKED SUPPORT AT BS 277-294 BL0 WL 208; LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-40-02 SRM 51-40-05. REQUEST OKAY TO INSTALL; [03] INSTALLED NEW INTERCOSTAL PER SRM 51-40-02 AND DWG 141A5400; [04] VERIFIED INSTALLATION OF NEW INTERCOSTAL PER SRM 51-40-02 AND DWG 141A5400; [05] VERIFIED INSTALLATION OF NEW INTERCOSTAL PER SRM 51-40-02 AND DWG 141A5400
CORROSION ON BS 986 FLOOR BEAM UPPER CHORD LBL 44 WL 208 ; / [01] WORK COMPLETED ON CARD NO. M-21-153-00612 (2529).; [02] VERIFIED WORK COMPLETED ON CARD NO. M-21-153-00612 (2529).
CORROSION ON BS 986 FLOOR BEAM UPPER CHORD RBL 44 WL 208 ; / [01] REMOVED CORROSION ON BS986 FLOOR BEAM UPPER CHORD RBL44 WL208 IN AREA OF 0.9' BY 1.1' BY A DEPTH OF 0.065' PER SRM 51-10-02-0G-0 AND SRM 53-70-51-1A-1. OUT OF LIMITS PER SRM 53-70-51-1A-1.; [02] VERIFIED REMOVED CORROSION ON BS986 FLOOR BEAM UPPER CHORD RBL44 WL208 IN AREA OF 0.9' BY 1.1' BY A DEPTH OF 0.065' PER SRM 51-10-02-0G-0 AND SRM 53-70-51-1A-1. OUT OF LIMITS PER SRM 53-70-51-1A-1.; [03] REMOVED ANGLE UNDER MOPSILL BS 986-1001 RBL 44 WL 207 FOR ACCESS PER SRM 51-40-02-0G-0.; [04] REMOVED ANGLE UNDER MOPSILL BS 967-986 RBL 48 WL 207 FOR ACCESS PER SRM 51-40-02-0G-0.; ALL I.A.W 53-70-51-2R-4 STEP 4.G-4.M.OK TO INSTALL.; [13] FABRICATED REPAIR PARTS ITEMS(1)T-CHORD1EA;(2)ANGLE 2EA;(3)ANGLE 2EA;(4)STRAP 2EA;PARTS OBTAINED FROM SOUTHWEST KIT BS986 SI#7530799;APPLIED CHEMICAL CONVERSION COATING AND PRIMED REPAIR PARTS AND BARE SURFACE OF THE REWORKED AREAS ALL I.A.W SRM 53-70-51-2R-4 STEP 4.G-4.M.OK TO INSTALL; [INSTALLED INTERCOSTAL, ITEM(8)2EA CORNER FITTINGS, ITEM (6) FILLERS 2EA BS986-1006 RBL38 WL208-WL200 I.A.W SRM 53-70-51-2R-4 STEP 4.N,O AND BOEING DWG 147A5730
CORROSION ON FLOOR TO SIDEWALL SUPPORT FROM STA 727 TO STA 767; RBL 22; WL 154. ; / [01] UPDATED MEASUREMENTS; [02] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLE PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [03] UPDATED STATEMENT OF CORRECTIVE ACTION BLOCK 1. CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [04] UPDATED STATEMENT OF CORRECTIVE ACTION BLOCKS 2 AND 3. CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [05] VERIFIED CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [06] REMOVED ACB FLOOR TO SIDEWALL SUPPORT AT BS727 - BS767; RBL22; WL154 PER SRM 51-40-02-0G-0; [07] LOCATED AND DRILLED ACB FLOOR TO SIDEWALL SUPPORT AT BS727 - BS767; RBL22; WL154 PER SRM 51-40-05-0G-0 AND DWG 146A7500; [08] VERIFIED CORRECTIVE ACTION 7.; [09] OK TO INSTALL RH FLOOR-TO-SIDEWALL SUPPORT; [10] INSTALLED FLOOR TO SIDEWALL SUPPORT BS 727 TO 767; RBL22; WL154 IAW SRM 51-40-02 AND DWG 146A0061; DWG 146A7502 AND DWG 146A7502; [11] VERIFIED INSTALLATION OF RH FLOOR-TO-SIDEWALL SUPPORT; BS 727-767; RBL 22; WL 154; PER SRM 51-40-02 AND DWG 146A0061 AND DWG 146A7502; [12] VERIFIED ALL WORK COMPLETE THIS TASK
CORROSION ON AFT CARGO BAY DOOR CUT-OUT FWD SHIELD FROM STA 767 TOO STA 787+7; RBL22; WL 154 ; / [01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [02] VERIFIED CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [03] REMOVED ACB FWD SHIELD AT BS767 - BS787; RBL22; WL154 PER SRM 51-40-02-0G-0; [04] LOCATED/DRILLED ACB FWD SHIELD AT BS767 - BS787; RBL22; WL154 PER SRM 51-40-05-0G-0 AND DWG 146A0081; [05] VERIFIED CORRECTIVE ACTION ENTRY 4.; [06] OK TO INSTALL; [07] OK TO INSTALL; [08] INSTALLED PER SRM 51-40-02-0G-0 AND DWG 146A0081; [09] UPDATED PART USE; [10] INSTALLED AFT CARGO BAY FWD SHIELD BS 767 TO 792 RBL 22 WL 154 PER SRM 51-40-02-0G-0 AND DWG 146A0081; [11] VERIFIED INSTALLATION OF ACB FWD SHIELD; BS 767-792; RBL 22; WL 154; PER SRM 51-40-02 AND DWG 146A0081; [12] VERIFIED ALL WORK COMPLETE THIS TASK
CORROSION ON FLOOR TO SIDEWALL SUPPORT FROM STA 727 TO STA 847; LBL 22; WL 154 ; / [01] UPDATED MEASUREMENTS; [02] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [03] VERIFIED CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL D; [04] REMOVED ACB FLOOR TO SIDEWALL SUPPORT AT BS727 - BS847; LBL22; WL154 PER SRM 51-40-02-0G-0; [05] FABRICATED; LOCATED AND APPLIED CHEMICAL CONVERSION COATING TO ACB FLOOR TO SIDEWALL SUPPORT AT BS727 - BS847 AND SPLICE REPAIR AT BS727E+8 - BS 727E+18 USING BAC1496-377#7075T62 LOT#1467164-1 PER SRM 51-40-05-0G AND DWG 146A7500; SRM 53-00-53-2R-5; AMM 51-21-41-370-80; [11] VERIFIED APPLIED PRIMER TO FLOOR TO SIDEWALL SUPPORT PER AMM 51-21-72-370-804.; PER SRM 51-40-02 AND DWG 146A7502; [18] ALL WORK COMPLETE; [19] VERIFIED ALL WORK COMPLETE; [20] THE CORRECT SELECT REF IS 53-00-53-2R-5-A00957. NO FOLLOW ON REQUIREMENTS REQUIRED.; [21] CERTIFY STEP 20
#1 ENGINE O/B T/R AFT FIRE SEAL LABRYNTH BRACKET ON PYLON IS CRACKED ; #1 ENGINE O TR AFT FIRE SEAL LARYNTH RACKET ON PYLON IS CRACKED / [01] REMOVED AND REPLACED #1 ENG O/B T/R AFT FIRE SEAL LABRYNTH BRACKET ON PYLON PER SRM 51-40-02-0G-0 STEP 4. AND PER IPC 54-54-00-03; [02] CERTIFIED ACTION 1; [03] VERIFIED INSTALLATION OF #1 ENG O/B T/R AFT FIRE SEAL LABYRINTH BRACKET ON PYLON PER SRM 51-40-02-0G-0 STEP 4. AND PER IPC 54-54-00-03; [04] CORRECTED MESURMENTS; [05] TASK COMPLETE
WHILE ACCOMPLISHING HFEC INSPECTION, FOUND A 1 INCH CRACK AT BS 673 RBL 40 WL 203, COMMON TO THE HORIZONTAL PRESSURE DECK WEB. REMOVED ADDITIONAL 0.040IN FROM EDGE OF THE WEB CUTOUT IAW SRM 53-40-51-2R-2 PAR 4.D(4). VERIFIED .040' INSURANCE CUT AND PERFORMED DVI INSPECTION IAW SRM 53-40-51-2R-2, NO DEFECTS OR DAMAGE NOTED FABRICATED A DOUBLER AND STIFFENERS AND WEB. LOCATED AND DRILLED ALL REPAIR PARTS IAW SRM 53-40-51-2R-2. INSTALLED ALL FASTENERS TO REPAIR IAW SRM 53-40-51-2R-2.
CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT STA 867+15; RBL 22; WL 157 ; / [01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL D.; [02] VERIFIED CORROSION OUT OF LIMITS PER SRM 53-00-53-1A-2; [03] UPDATED MEASUREMENT; [04] VERIFIED UPDATED MEASUREMENTS; [05] REMOVED ACB FLOOR TO SIDEWALL SUPPORT AT BS867 - BS887; RBL22; WL157 PER SRM 51-40-02-0G-0; [06] LOCATED AND DRILLED ACB FLOOR TO SIDEWALL SUPPORT AT BS867 - BS887; RBL22; WL157 PER SRM 51-40-05-0G-0 AND DWG 146A7500; [07] VERIFIED CORRECTIVE ACTION 6.; [08] OK TO INSTALL.; [09] OK TO INSTALL; [10] INSTALLED FLOOR TO SIDEWALL SUPPORT AT BS 887- 867 RBL 22 WL 156 IAW SRM 51-40-02-0G-0 AND DWG 147A7500; 146A7502;147A0060.; [11] VERIFIED INSTALLED FLOOR TO SIDEWALL SUPPORT AT BS 887- 867 RBL 22 WL 156 IAW SRM 51-40-02-0G-0 AND DWG 147A7500; 146A7502;147A0060.
AFT CARGO SIDEWALL SUPPORT BRACKET CRACKED, BS 947, RBL 40, WL 200. REMOVED THE SUPPORT BRACKET IAW SRM 51-40-02-0G-0. FABRICATED, LOCATED, DRILLED, & CHEMICAL CONVERSION COAT, PRIMER AND NUTPLATE INSTALLATION IAW SRM 51-40-05-0G-0;51-40-02-0G-0 AND DWGS 149A9490, 149A9491. INSTALLED THE NEW SUPPORT BRACKET IAW SRM 51-40-02, DWGS 149A9490, 149A9491, 147A9109, 147A0060 AND AIPC 53-11-51-01.
CORROSION NEAR FASTENER HOLE ON BULKHEAD FLANGE UPPER SURFACE AT BS 260 RBL 9.5 WL 208. ; / [01] REMOVED CORROSION NEAR FASTENER HOLE BS260 RBL9.5 WL208 1'X1' AREA I.A.W SRM 51-10-02-0G-0; [02] REMOVED NUTPLATE BS260 RBL10 WL208 I.A.W SRM 51-40-02-0G-0; [03] VERIFIED CORROSION REMOVED PER SRM 51-10-02.; [04] REQUEST UT INSPECTION;HFEC OPEN HOLE INSPECTION AND HFEC SURFACE INSPECTION.; [05] UT INSPECTED BLEND IAW 737 NDTM PART 4 51-00-00 PROCEDURE 2; LOWEST THICKNESS = 0.089'<BR>ET INSPECTED BLEND AND HOLE IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23 AND PROCEDURE 16; NO CRACKS NOTED.<BR>CAL ID IS000450 N500D<BR>CAL ID ATS2031 E650; [06] REQUEST G.V.I OF THE DAMAGED AREA; ADJACENT AND UNDERLYING STRUCTURES TO VERIFY NO ADDITIONAL DAMAGE; [07] ACCOMPLISHED GVI; NO ADDITIONAL DAMAGE AT REPAIR AREA; ADJACENT AND UNDERLYING STRUCTURE; OK TO PROCEED. PER SRM 51-10-02.; [08] EDIT TO CORRECTIVE ACTION #5:<BR>ERRANTLY WROTE 0.089' AS REMAINING THICKNESS.<BR><BR>REMAINING THICKNESS IS ACTUALLY 0.087'; [09] VERIFIED COMPLETION OF EA 21-153-02555; [10] VERIFIED ALL STEPS ARE COMPLETE.; [11] VERIFIED ALL RII STEPS ARE COMPLETE.
AFT CARGO SIDEWALL SUPPORT BRACKET STA 727; RBL-22; WL-156; HAS SURFACE CORROSION. ; / [01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO NO DAMAGE IS ALLOWED AT THIS LOCATION PER SRM 53-40-08-1A-3 FIGURE 102.; [02] VERIFIED CORROSION OUT OF LIMITS PER SRM 53-40-08-1A-3; [03] REMOVED SIDEWALL SUPPORT BRACKET BS 727 RBL 22 WL 156 IAW SRM 51-40-02-0G-0; [04] LOCATED; DRILLED; DEBURRED NEW AFT CARGO SIDEWALL SUPPORT BRACKET BS 727 RBL22 WL 156 IAW SRM 51-40-05. OK TO INSTALL; [05] VERIFIED LOCATE; DRILL AND DEBURR OF NEW ACB SIDEWALL SUPPORT BRACKET; BS 727; RBL 22 WL 156; PER SRM 51-40-05; OK TO INSTALL; [06] INSTALLED NEW AFT CARGO SIDEWALL SUPPORT BRACKET BS 727 RBL22 WL 156 IAW SRM 51-40-02 AND DWG 144A2600; [07] VERIFIED INSTALLATION OF NEW AFT CARGO SIDEWALL SUPPORT BRACKET BS 727 RBL22 WL 156 IAW SRM 51-40-02 AND DWG 144A2600.
AFT CARGO SIDEWALL SUPPORT BRACKET STA 727; LBL-26; WL-157; HAS SURFACE CORROSION ; / [01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO NO DAMAGE IS ALLOWED AT THIS LOCATION PER SRM 53-40-08-1A-3 FIGURE 102.; [02] VERIFIED CORROSION OUT OF LIMITS PER SRM 53-40-08-1A-3; [03] REMOVED SIDEWALL SUPPORT BRACKET BS 727 LBL 26 WL 156 IAW SRM 51-40-02-0G-0; [04] LOCATED; DRILLED; DEBURRED NEW AFT CARGO SIDEWALL SUPPORT BRACKET BS 727 LBL26 WL 157 IAW SRM 51-40-05. OK TO INSTALL; [05] VERIFIED LOCATE; DRILL AND DEBURR OF NEW ACB SIDEWALL SUPPORT BRACKET; BS 727; LBL 26 WL 157; PER SRM 51-40-05; OK TO INSTALL; [06] INSTALLED NEW AFT CARGO SIDEWALL SUPPORT BRACKET BS 727 LBL26 WL 157 IAW SRM 51-40-02 AND DWG 144A2600; [07] VERIFIED INSTALLATION OF NEW AFT CARGO SIDEWALL SUPPORT BRACKET BS 727 LBL26 WL 157 IAW SRM 51-40-02 AND DWG 144A2600.
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A - BS500D RBL23 WL156. ; / [01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL D.; [02] VERIFIED DAMAGE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [03] REMOVED FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY 500A TO BS 500D RBL 23 WL 156 PER SRM 51-40-02-0G-0; [04] RECEIVED NEW FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY N/P: 143A7501U186 LOT:1465888-1 PO NUMBER:833400. LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A - BS500D RBL23 WL156 IAW SRM 51-40-02 AND DWG 143A7500 ID: 0017 REV:A; [05] RECEIVED PART; [06] VERIFIED LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A - BS500D RBL23 WL156 IAW SRM 51-40-02 AND DWG 143A7500 ID: 0017 REV:A.; [07] OK TO INSTALL FLOOR TO SIDEWALL SUPPORT; [08] OK TO INSTALL FLOOR TO SIDEWALL SUPPORT GIVEN.; [09] INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A - BS500D RBL23 WL156 IAW SRM 51-40-02 AND DWG 143A7500 ID: 0017 REV:A.; [10] VERIFIED INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A - BS500D RBL23 WL156 IAW SRM 51-40-02 AND DWG 143A7500 ID: 0017 REV:A.
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS400 TO BS420 LBL23 WL156. ; / CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIG 103 DETAIL REMOVED FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS 400 TO BS 420 LBL 23 WL 156 PER SRM 51-40-02-0G-0 FABRICATED NEW FLOOR TO SIDEWALL SUPPORT BS 396 TO 500D L/H; AND SPLICE REPAIR BS 480 TO 500 L/H FROM EXTRUSION CLAD BAC1496-444#7075T62 LOT# 1466509-1 PER SRM 53-00-53-2R-5; SRM51-40-05-0G-0; AND DWG 143A7501LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT AND SPLICE REPAIR PER PER SRM 53-00-53-2R-5; SRM51-40-05-0G-0; AND DWG 143A7501] INSTALLED SPLICE REPAIR PER SRM 53-00-53--2R-5 AND DWG 143A7501] INSTALLED FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BS 396 TO500D LBL 23 WL 156 PER SRM 51-40-02-0G-0; AND DWG 143A7500
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS411 RBL24 WL156. ; / [01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMIT DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL D.; [02] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2.; [03] UPDATED MEASUREMENTS; [04] REMOVED FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS 396 TO 420 PER SRM 51-40-02-0G-0; [05] FABRICATED FCB FLOOR TO SIDEWALL SUPPORT BS 400-420; RBL 24 WL 156 IAW SRM 50-40-05 DWG# 143A7501. APPLIED CHEMICAL CONVERSION COATING IAW SRM 51-20-01. REQUEST OK TO APPLY PRIMER.; [06] VERIFIED FABRICATED FCB FLOOR TO SIDEWALL SUPPORT BS 400-420; RBL 24 WL 156 IAW SRM 50-40-05 AND DWG# 143A7501.<BR>VERIFIED APPLIED CHEMICAL CONVERSION COATING IAW SRM 51-20-01.<BR>VERIFIED OK TO PRIME.; [07] APPLIED PRIMER IAW SOPM 20-41-02; [08] VERIFIED CORRECTIVE ACTION ENTRY 7.; [09] OK TO INSTALL FCB RH FLOOR TO SIDEWALL SUPPORT BS 396 - 420; [10] OK TO INSTALL FCB RH FLOOR TO SIDEWALL SUPPORT BS 396-420 GIVEN.; [11] INSTALLED FCB RH FLOOR TO SIDEWALL SUPPORT ; BS 396-420; RBL24; IAW SRM 51-40-02-0G-0; DWG143A7500.; [12] VERIFIED INSTALLED FCB RH FLOOR TO SIDEWALL SUPPORT ; BS 396-420; RBL24; IAW SRM 51-40-02-0G-0; DWG143A7500.
CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT AT FWD CARGO BAY BS500D LBL23 TO RBL23 WL156. ; / [01] CORROSION ON SUPPORT FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SPM.; [02] VERIFIED NO LIMITS; REPAIR BY REPLACEMENT OF PART.; [03] CORROSION ON SUPPORT FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [04] UPDATED MEASUREMENTS; [05] REMOVED AFT BULKHEAD TO FLOOR SUPPORT AT FWD CARGO BAY BS 500D LBL 23 TO RBL 23 WL 153 PER SRM 51-40-02-0G-0; [06] LOCATED/DRILL AFT BULKHEAD TO FLOOR SUPPORT AT FCB BS500D; LBL23 - RBL23; WL 156 PER SRM 51-40-05-0G-0 AND DWG 143A9481; DWG 143A7902; [07] VERIFIED CORRECTIVE ACTION ENTRY 6.; [08] OK TO INSTALL LOWER BULKHEAD BS 500D; [09] VERIFIED OK TO INSTALL REPLACEMENT SUPPORT BS 500D LBL 23 TO RBL 23 WL 156; [10] INSTALLED FWD CARGO BAY LOWER BULKHEAD SUPPORT ANGLE BS 500D LBL 23 TO RBL 23 WL 156 PER SRM 51-40-02-0G-0; DWG 143A9481; AND DWG 143A7902; [11] VERIFIED INSTALLED FWD CARGO BAY LOWER BULKHEAD SUPPORT ANGLE BS 500D LBL 23 TO RBL 23 WL 156 PER SRM 51-40-02-0G-0; DWG 143A9481; AND DWG 143A7902
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500C TO BS500C+6 LBL23 WL156. ; / [01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL D. NEW FLOOR TO SIDEWALL SUPPORT FROM BS 396 TO BS 500D LBL 24 WL 156 WILL BE INSTALLED ON FAULT TTG8Q00687YP.; [02] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; REPLACEMENT ON TTG8Q00687YP; JOB COMPLETE.
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A+10 TO BS500A+15 LBL23 WL156. ; / [01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL D. NEW FLOOR TO SIDEWALL SUPPORT FROM BS 396 TO BS 500D LBL 24 WL 156 WILL BE INSTALLED ON FAULT TTG8Q00687YP.; [02] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; REPLACEMENT ON TTG8Q00687YP; JOB COMPLETE.
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS499 LBL24 WL156. ; / [01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL D. NEW FLOOR TO SIDEWALL SUPPORT FROM BS 396 TO BS 500D LBL 24 WL 156 WILL BE INSTALLED ON FAULT TTG8Q00687YP.; [02] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; REPLACEMENT ON TTG8Q00687YP; JOB COMPLETE.
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS496 LBL24 WL156. ; / [01] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL D. NEW FLOOR TO SIDEWALL SUPPORT FROM BS 396 TO BS 500D LBL 24 WL 156 ON FAULT TTG8Q00687YP.; [02] CORROSION ON SUPPORT WAS FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLES PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL D. NEW FLOOR TO SIDEWALL SUPPORT FROM BS 396 TO BS 500D LBL 24 WL 156 WILL BE INSTALLED ON FAULT TTG8Q00687YP.; [03] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; REPLACEMENT ON TTG8Q00687YP; JOB COMPLETE.
CORROSION ON AFT SHIELD AT FWD CARGO BAY BS500 - BS500A RBL23 WL156. ; / [01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [02] VERIFIED NO LIMITS IN THE SRM.; [03] REMOVED AFT SHIELD AT FWD CARGO BAY BS 500 TO 500A RBL 23 WL 156 PER SRM 51-40-02-0G-0; [04] RECEIVED NEW AFT SHIELD AT FWD CARGO BAY N/P: 143A8126U31ATSMRO LOT:1467243-1 PO NUMBER: 835328. LOCATED; DRILLED AND COUNTERSANK NEW AFT SHIELD AT FWD CARGO BAY BS500 - BS500A RBL23 WL156 IAW SRM 51-40-02 AND DWG 143A0080 ID:0019 REV:-; [05] RECEIVED PART; [06] VERIFIED LOCATED; DRILLED AND COUNTERSANK NEW AFT SHIELD AT FWD CARGO BAY BS500 - BS500A RBL23 WL156 IAW SRM 51-40-02 AND DWG 143A0080 ID:0019 REV:- .; [07] OK TO INSTALL.; [08] VERIFIED OK TO INSTALL; [09] INSTALLED NEW AFT SHIELD AT FWD CARGO BAY BS500 - BS500A RBL23 WL156 IAW SRM 51-40-02 AND DWG 143A0080; [10] VERIFIED INSTALLED NEW AFT SHIELD AT FWD CARGO BAY BS500 - BS500A RBL23 WL156 IAW SRM 51-40-02 AND DWG 143A0080.; [11] VERIFIED ALL STEPS COMPLETE.
CORROSION ON TRACK TIEDOWN AT FWD CARGO BAY BS436 RBL13 WL156. ; / [01] CORROSION ON TRACK WAS FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 10% OF THE MATERIAL WAS REMOVED PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL G; TRACK WILL BE REPLACED ON FAULT TTG8Q00687ZQ.; [02] CORROSION ON TRACK WAS FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 10% OF THE MATERIAL WAS REMOVED PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL G; TRACK WILL BE REPLACED ON FAULT TTG8Q00687ZQ.; [03] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; REPLACEMENT ON TTG8Q00687ZQ; CARD COMPLETE.
CORROSION ON TRACK TIEDOWN AT FWD CARGO BAY BS420 RBL13 WL156. ; / [01] UPDATED MEASUREMENTS; [02] CORROSION ON TRACK WAS FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 10% OF THE MATERIAL WAS REMOVED PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL G; TRACK WILL BE REPLACED ON FAULT TTG8Q00687ZQ.; [03] CORROSION ON TRACK WAS FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 10% OF THE MATERIAL WAS REMOVED PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL G; TRACK WILL BE REPLACED ON FAULT TTG8Q00687ZQ.; [04] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; REPLACEMENT ON TTG8Q00687ZQ; CARD COMPLETE.
CORROSION ON TRACK TIEDOWN AT FWD CARGO BAY BS400 RBL13 WL156. ; / [01] CORROSION ON TRACK WAS FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 10% OF THE MATERIAL WAS REMOVED PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL G; TRACK WILL BE REPLACED ON FAULT TTG8Q00687ZQ.; [02] CORROSION ON TRACK WAS FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 10% OF THE MATERIAL WAS REMOVED PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL G; TRACK WILL BE REPLACED ON FAULT TTG8Q00687ZQ.; [03] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; REPLACEMENT ON TTG8Q00687ZQ; CARD COMPLETE.
CORROSION ON FWD SHIELD AT FWD CARGO BAY BS420 - BS440 RBL23 WL156. ; / [01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [02] VERIFIED NO LIMITS; REPAIR BY REPLACEMENT OF PART.; [03] REMOVED FWD SHIELD AT FWD CARGO BAY BS 420 TO BS 440 RBL23 WL156 PER SRM 51-40-02-0G-0; [04] LOCATED AND DRILLED FCB FWD SHIELD BS 420-440; RBL 23 IAW SRM 51-40-05; DWG# 143A0080.; [05] VERIFIED CORRECTIVE ACTION ITEMS 3 AND 4; [06] OK TO INSTALL FCB RH FWD SHIELD; BS 420-440. RBL23.; [07] VERIFIED OK TO INSTALL; [08] INSTALLED FCB RH FWD SHIELD;BS 420-440; RBL23 IAW SRM 51-40-02-0G-0; DWG 143A0080; [09] VERIFIED INSTALLED FCB RH FWD SHIELD;BS 420-440; RBL23 IAW SRM 51-40-02-0G-0; DWG 143A0080
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500 RBL24 WL156. ; / [01] CORROSION ON SUPPORT/SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. NEW SHIELD WILL BE INSTALLED ON FAULT TTG8Q00686P2.; [02] VERIFIED NO LIMITS; REPLACEMENT ON TTG8Q00686P2; CARD COMPLETE.
CORROSION ON TRACK TIEDOWN AT FWD CARGO BAY BS500B RBL13 WL156. ; / [01] CORROSION ON TRACK WAS FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 10% OF THE MATERIAL WAS REMOVED PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL G; TRACK WILL BE REPLACED ON FAULT TTG8Q00687ZQ.; [02] CORROSION ON TRACK WAS FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 10% OF THE MATERIAL WAS REMOVED PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL G; TRACK WILL BE REPLACED ON FAULT TTG8Q00687ZQ.; [03] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; REPLACEMENT ON TTG8Q00687ZQ; CARD COMPLETE.
CORROSION ON TRACK TIEDOWN AT FWD CARGO BAY BS500C+16 RBL13 WL156. ; / [01] CORROSION ON TRACK WAS FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 10% OF THE MATERIAL WAS REMOVED PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL G; TRACK WILL BE REPLACED ON FAULT TTG8Q00687ZQ.; [02] CORROSION ON TRACK WAS FOUND TO BE OUT OF LIMITS DUE TO MORE THAN 10% OF THE MATERIAL WAS REMOVED PER SRM 53-00-53-1A-2 FIGURE 103 DETAIL G; TRACK WILL BE REPLACED ON FAULT TTG8Q00687ZQ.; [03] VERIFIED OUT OF LIMITS PER SRM 53-00-53-1A-2; REPLACEMENT ON TTG8Q00687ZQ; CARD COMPLETE.
CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C AFT SIDE RBL25 WL155. ; / [01] CRACK FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.; [02] VERIFIED OUT OF LIMITS DUE TO NO SRM LIMITS; [03] LOCATED AND DRILLED NEW ANGLE P/N: 143A7502U154 LOT: 1456906-4 . IAW SRM 51-40-05 AND DWG:143A7505 ID: 0010 REV:A REQUEST OK TO INSTALL; [04] VERIFIED CORRECTIVE ACTION 3. OK TO INSTALL.; [05] INSTALLED NEW ANGLE P/N: 143A7502U154 LOT: 1456906-4 . IAW SRM 51-40-02 AND DWG:143A7505 ID: 0010 REV:A; [06] VERIFIED INSTALLED NEW ANGLE P/N: 143A7502U154 LOT: 1456906-4 . IAW SRM 51-40-02 AND DWG:143A7505 ID: 0010 REV:A; [07] VERIFIED ALL STEPS COMPLETE.
CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 LBL25 WL155. ; / [01] FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [02] VERIFIED OUT OF LIMITS DUE TO NO SRM LIMITS; [03] LOCATED AND DRILLED NEW ANGLE P/N: 143A7502U155 LOT: 1458822-5 . IAW SRM 51-40-05 AND DWG:143A7505 ID: 0002 REV:B REQUEST OK TO INSTALL; [04] VERIFIED CORRECTIVE ACTION 3. OK TO INSTALL INTERCOSTAL ATTACH ANGLE (CLIP) IN FCB BS 400 LBL 25 WL 155.; [05] INSTALLED NEW ANGLE P/N: 143A7502U155 LOT:1458822-5 . IAW SRM 51-40-02 AND DWG:143A7505 ID: 0002 REV:B.; [06] VERIFIED INSTALLED NEW ANGLE P/N: 143A7502U155 LOT:1458822-5 . IAW SRM 51-40-02 AND DWG:143A7505 ID: 0002 REV:B.; [07] VERIFIED ALL STEPS COMPLETE.
CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 RBL25 WL155. ; / [01] FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [02] VERIFIED OUT OF LIMITS DUE TO NO SRM LIMITS; [03] LOCATED AND DRILLED NEW ANGLE P/N 143A7502U154 LOT 1448645-4 IAW DWG 143A7505 ID:0002 REV:B REQUEST OK TO INSTALL.; [04] VERIFIED LOCATED AND DRILLED NEW ANGLE P/N 143A7502U154 LOT 1448645-4 IAW DWG 143A7505 ID:0002 REV:B.<BR>VERIFIED OK TO INSTALL.; [05] INSTALLED NEW ANGLE P/N 143A7502U154 LOT 1448645-4 IAW SRM 51-40-02 DWG 143A7505 ID:0002 REV:B; [06] VERIFIED INSTALLED NEW ANGLE P/N 143A7502U154 LOT 1448645-4 IAW SRM 51-40-02 DWG 143A7505.; [07] VERIFIED ALL STEPS COMPLETE.
CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C AFT SIDE LBL25 WL155. ; / [01] FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [02] VERIFIED OUT OF LIMITS DUE TO NO SRM LIMITS; [03] LOCATED AND DRILLED NEW ANGLE P/N: 143A7502U155 LOT: 1458822-5 . IAW SRM 51-40-05 AND DWG:143A7505 ID: 0009 REV:A REQUEST OK TO INSTALL; [04] VERIFIED LOCATED AND DRILLED NEW ANGLE P/N: 143A7502U155 LOT: 1458822-5 . IAW SRM 51-40-05 AND DWG:143A7505 ID: 0009 REV:A.<BR>VERIFIED OK TO INSTALL;.; [05] INSTALLED NEW ANGLE P/N: 143A7502U155 LOT: 1458822-5 . IAW SRM 51-40-02 AND DWG:143A7505 ID: 0009 REV:A; [06] VERIFIED INSTALLED NEW ANGLE P/N: 143A7502U155 LOT: 1458822-5 . IAW SRM 51-40-02 AND DWG:143A7505 ID: 0009 REV:A.; [07] VERIFIED ALL STEPS COMPLETE.
CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C FWD SIDE LBL25 WL155. ; / [01] FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [02] VERIFIED OUT OF LIMITS DUE TO NO SRM LIMITS; [03] LOCATED AND DRILLED NEW ANGLE P/N: 143A7502U159 LOT: 1461470 . IAW SRM 51-40-05 AND DWG:143A7505 ID: 0005 REV:B REQUEST OK TO INSTALL; [04] UPDATED PART RECEIVING.; [05] VERIFIED LOCATED AND DRILLED NEW ANGLE P/N: 143A7502U159 LOT: 1461470 . IAW SRM 51-40-05 AND DWG:143A7505 ID: 0005 REV:B. <BR>VERIFIED OK TO INSTALL.; [06] INSTALLED NEW ANGLE P/N: 143A7502U159 LOT: 1461470 . IAW SRM 51-40-02 AND DWG:143A7505 ID: 0005 REV:B; [07] VERIFIED INSTALLED NEW ANGLE P/N: 143A7502U159 LOT: 1461470 . IAW SRM 51-40-02 AND DWG:143A7505 ID: 0005 REV:B.; [08] VERIFIED ALL STEPS COMPLETE.
CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500B FWD SIDE LBL25 WL155. ; / [01] FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM; [02] VERIFIED OUT OF LIMITS DUE TO NO SRM LIMITS; [03] LOCATED AND DRILLED NEW ANGLE P/N: 143A7502U159 LOT: 1461470 . IAW SRM 51-40-05 AND DWG:143A7505 ID: 0005 REV:B REQUEST OK TO INSTALL; [04] UPDATED PART RECEIVING.; [05] VERIFIED CORRECTIVE ACTION 3. OK TO INSTALL.; [06] VERIFIED OK TO INSTALL.; [07] INSTALLED NEW ANGLE P/N: 143A7502U159 LOT: 1461470 . IAW SRM 51-40-02 AND DWG:143A7505 ID: 0005 REV:B; [08] VERIFIED INSTALLED NEW ANGLE P/N: 143A7502U159 LOT: 1461470 . IAW SRM 51-40-02 AND DWG:143A7505 ID: 0005 REV:B; [09] VERIFIED ALL STEPS COMPLETE.
CRACKED TRACK AT FWD CARGO BAY BS460 RBL13 WL155. ; / [01] CRACK ON TRACK IS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2; [02] VERIFIED CRACK ON TRACK IS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2; [03] REMOVED FCB TRACK BS 396-500D; RBL 13 IAW SRM 51-40-02. <BR>LOCATED AND DRILLED NEW TRACK PER SRM 51-40-05; DWG# 143A7500 ID 05.; [04] VERIFIED CORRECTIVE ACTION ITEM 3; [05] REQUEST OK TO INSTALL.; [06] VERIFIED OK TO INSTALL FCB TRACK BS396-500D RBL13.; [07] INSTALLED FCB TRACK BS 396-500D; RBL 13; WL 155 IAW SRM 51-40-02; DWG# 143A7500 ID 05.; [08] VERIFIED INSTALLED FCB TRACK BS 396-500D; RBL 13; WL 155 IAW SRM 51-40-02; DWG# 143A7500 ID 05.; [09] VERIFIED ALL STEPS COMPLETE.
FLOOR PANEL 221GF FWD OUTBD CORNER CRACKED. REPLACED FLOOR PANEL 221GF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-68 ITEM 370.
FWD SERVICE DOOR LOWER BEAM CRACKED AT I/B SIDE OF RADIUS ; / [01] WORK COMPLETED ON RO NO P0972344-1.; [02] VERIFIED WORK ACCOMPLISHED ON RO# P0972344-1
CORROSION ON FUSELAGE EXTERIOR SKIN AT STA 1084 THROUGH STA 1090 AND LBL 12 THROUGH RBL6 ; / [01] UPDATED TABLE 1-13 ; 15 AND 16; [02] STRIPPED EXTERIOR FINISH PER AMM 51-21-11-150-801; [03] REMOVED 21 FASTENERS PER SRM 51-40-02-0G-0; [04] BLENDED CORROSION 19'X4' PER SRM 53-00-01-1A-1; [05] VERIFIED REMOVAL OF FASTENERS PER SRM 51-40-02 AND BLENDING OF CORROSION PER SRM 53-00-01-1A-1; [06] UT INSPECTED SKIN BLENDOUT AREA IAW B737 NDTM P4; 51-00-00 PROC 2. REMAINING MAT. 0.077 TOOL ID ATS2341; E650; [07] HFEC INSPECTED SKIN BLENDOUT AREA; IAW B737 NDTM P6; 51-00-00 PROC 23. NO CRACKS NOTED. TOOL ID ATS1465; N600; [08] ACCOMPLISHED HFEC HOLE INSPECTION TO OPEN FASTENERS REMOVED IN BLENDOUT AREA IAW B737 NDTM P6; 51-00-00 PROC 16. NO CRACKS NOTED. TOOL ID ATS1465; N600; TOOL ID ATS1411; MINIMITE; [09] ACCOMPLISHED HFEC COUNTERSINK INSP TO COUNTERSINKS IN BLENDOUT AREA IAW B737 NDTM P6; 53-30-00 PROC 3. NO CRACKS NOTED. TOOL ID ATS1465; N600; TOOL ID ATS1411; MINIMITE; [10] BLEND MEASURES 19'X4'X.003' ORIGINAL THICKNESS .080'; .077' FOUND OUT OF LIMITS DUE TO BLEND EXCEEDING 3 IN 10 FASTENERS PER SRM 53-00-01-1A-1 FIG D; [11] VERIFIED OUT OF LIMITS PER SRM 53-00-01-1A-1; [12] UPDATE TABLE; [13] REFER TO EA 21-153-02672 SUMMARY REQUIREMENT; BARCODE: TTG8Q006M0GH;
RIGHT MLG SUPPORT BEAM ;LOWER O/B STABILIZER LINK CRACKED APPOX 1 INCH LONG . CRACK IS LOCATED AT FWD SIDE LUG NEAR ATTACHMENT POINT. ; / [01] REMOVED AND REPLACED THE R/H MLG SUPPORT BEAM LOWER STABILIZER LINK REF AMM 57-15-00
RT MLG FWD TRUNNION SUPPORT FITTING ; RT MLG FWD TRUNNION SUPPORT FITTING; LOWER O/B LUG; I/B FACE HAS EVIDENCE OF CORROSION / REPAIRED AS PER EA-1-A57-3246 REV 12
R1 DOOR SLIDE LENSE COVER MISSING REF LP# 1811387 MEL 25-10-01 AUTH# 13799 ; / INSTALLED R1 DOOR SLIDE COVER PER AMM 20-30-11.
EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01675 ; / REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LOCATION M01675 PER AMM 33-51-06
LEFT HORIZONTAL STABILIZER LOWER SLIDING SEAL BENT ; /
LEFT HORIZONTAL STABILIZER UPPER SLIDING SEAL CRACKED ; /
AFT CARGO CENTER THRESHOLD HAS AFT CORNER CURLED/BENT UP APPROXIMATELY .1875 X .1875. / REMOVED AND REPLACED CENTER SCUFF PLATE REF AMM 53-11-02.
FORWARD GALLEY CEILING PANEL LOOSE. RESECURED FORWARD CEILING EMERGENCY EXIT SIGN PANEL, AS PER AMM 33-51-01.
EMERGENCY LIGHTS ON ROW 7 A/B/C AND 9 A/B/C INOPERABLE. REMOVED & REPLACED BATTERY AT LOC M2335. OPS CK GOOD, REF AMM 33-51-06 AT ROWS 7 A/B/C, 9 A/B/C, & .14 A/B/C
FORWARD R/H SIDE AISLE PHOTOLUMINESCENT STRIP NOT SECURED. / SECURED PHOTOLUMINESCENT STRIP PER SIP.
FORWARD ENTRY DOOR EMERGENCY LIGHT COVER BROKEN OFF. / R&R LIGHT PER AMM.
R/H SIDE FUSELAGE SKIN INNER SURFACE AROUND HOLES CORRODED STA 667, RBL 70. / REPAIRED SKIN IAW EA.
KICK FITTING PN 112A1513-2 IS CORRODED AND REQUIRES REPLACEMENT. THIS NRC IS FOR CORROSION REPORTING PURPOSE. STA 666; RBL 73; WL 190 / FITTING WAS REPLACED BY BOEING AOG TEAM ON FRR-8. CORROSION FINDING # 20217.
FUSELAGE INNER SURFACE OF SKIN AROUND HOLES CORRODED AT BS. 667, LBL 70. / REPAIRED SKIN PER EA.
LEFT HAND PICKLE IS CRACKED AT STA 663. / THE LH PICKLE FORK FRAME P/N 144A2410-7 WAS REMOVED AND REPLACED BY BOEING AOG UNDER AGREEMENT SWA-RE-1906934 IN VCV. REF. SWA EA 1-753-35957 REV IR FOR DETAILS OF THE BOEING AOG VISIT AND FOR DOCUMENTATION OF ASSOCIATED REPAIRS.
REF LOG PAGE 1102696 LEFT HAND PICKLEFORK CRACKED AT STA 663 / THE LH PICKLE FORK FRAME P/N 144A2410-7 WAS REMOVED AND REPLACED BY BOEING AOG UNDER AGREEMENT SWA-RE-1906934 IN VCV. REF. SWA EA 1-753-35957 REV IR FOR DETAILS OF THE BOEING AOG VISIT AND FOR DOCUMENTATION OF ASSOCIATED REPAIRS. CLEARING# 5812
L/H PICKLE FORK IS CRACKED AT STATION 663. / COMPLIED WITH EA 1-753-35800; ACCOMPLISH PERMANENT REPAIR OR REPLACEMENT OF DISCREPANT PARTS WITHIN 1 NON-REVENUE FERRY FLIGHT FLIGHT CYCLE FROM DAL-VCV. CONDITIONS FOR FERRY-KNOWN OR FORCAST TURBULANCE IS AVOIDED; FLIGHT IS NON-REVENUE WITH NO PASSENGERS AND NO-REVENUE CARGO-MINIMUM CREW. REFERENCE LP 1102699
R1 DOOR EMERGENCY EXIT LIGHT ON GALLEY INOP AT M1674. R&R BATTERY PACK PER AMM.
LT WING LWR L/E PNL 521FB FWD O/B CORNER HAS CRACK FROM FASTENER HOLE TO EDGE / REMOVED PANEL 521FB FROM AIRCRAFT IAW SOPM 20-50-01 59402U 22SEP19 8119C 22SEP19 LT WING LWR L/E PNL 521FB FWD O/B CORNER CRACK WAS REPAIRED IAW SRM 51-70-05-22-6 20021C 24SEP19 INSTALLED LT WING LWR L/E PNL 521FB PER SRM 2050-01
R1 DOOR EMERGENCY SLIDE LIGHT INOP AT M1674. R&R BATTERY PACK PER AMM.
RT EMERGENCY AISLE LIGHTS INOP BETWEEN SEAT ROWS 3 TO ROW 6. R&R BATTERY PACK PER AMM.
LOWER EMERGENCY LIGHT INOP. CONNECTED CONNECTOR PER WDM.
AISLE LIGHT AT 13R INOP. CONNECTED CONNECTOR PER WDM.
AFT GALLEY DOOR PANEL; 844DZ; AFT ATTACH BRACKET IS CRACKED. / REPLACED AFT GALLEY DOOR PANEL; 844DZ; AFT ATTACH BRACKET IAW SRM 51-40-02-0G-0.
SUPPORT CHANNEL CORRODED BETWEEN BS 259 TO BS 270, BETWEEN LBL 2.8 TO RBL 2.8. R&R SUPPORT CHANNEL IAW DWG AND SRM.
***CORROSION*** BS 540FRAME BETWEEN STR 8 AND 9 R/H RBL 58 WL 272. / REPAIRED DAMAGE ON BS 540 FRAME BETWEEN STR 8 AND 9 R/H; RBL. 58; WL 272 PER ER 19-04625 REV IR AND EA # 1-753-35582 REV IR.
BS 312 FRAME CRACKED AT END RADIUS ABOVE FWD ENTRY DOOR UPPER SILL WEB. / REPAIRED BS 312 FRAME AT END RADIUS ABOVE FWD ENTRY DOOR UPPER SILL WEB. PER ER# 19-04626 AND EA# 1-753-35556; REV IR.
LATERAL INTERCOSTAL CORRODED AT BS 270, BETWEEN LBL 7.5 TO RBL 7.5. FORWARD FLANGE AROUND NUTPLATE. REMOVED INTERCOSTAL PER SRM & EA.
R2 DOOR MOP SILL CORRODED BETWEEN BS 960 TO BS 986, RBL 54. R&R MOPSILL IAW SRM & DWG.
OUTBOARD OF MOP SILL ANGLE CRACKED AT BS 293, RBL 53. R&R ANGLE IAW EA AND SRM.
***CORROSION*** ON FWD SERVICE DOOR THRESHOLD SUPPORT ANGLE BS 308-325 RBL55 WL208. / REMOVED AND REPLACED FWD SERVICE DOOR THRESHOLD SUPPORT ANGLE-CHORD BS291.5-328 RBL55 WL208 IAW SRM 51-40-05-0G-0 SRM 51-40-02-0G-0 AND BOEING DWG 141A6310
CABIN PANEL 242UF HAS DAMAGED INSERTS. / CABIN FLOOR PANEL 242UF WITH DAMAGED INSERTS WAS REPAIRED IAW SRM 53-00-50-2R-1 59702U 09/02/19
SEAT TRACK CROWN CORRODED AT BS 500C+8-10 TO BS 520, LBL 25. REPAIRED SEAT TRACK IAW SRM & DWG.
SEAT TRACK CROWN CORRODED BETWEEN BS 540 TO BS 727B, LBL 25. R&R SEAT TRACK CROWN IAW SRM & DWG.
SEAT TRACK CROWN CORRODED BETWEEN BS 540 TO BS 727B, RBL 45. R&R SEAT TRACK IAW SRM, AMM, & DWG.
FLOOR SUPPORT CRACKED BETWEEN BS 312 TO BS 328, RBL 30.5. R&R FLOOR SUPPORT IAW SRM AND DWG.
FLOOR SUPPORT CRACKED BETWEEN BS 312 TO BS 328, LBL 45. R&R INTERCOSTAL IAW SRM AND DWG.
FLOOR SUPPORT CRACKED BETWEEN BS 328 TO BS 344, LBL 45. R&R FLOOR SUPPORT IAW SRM AND DWG.
AFT CARGO BAY, LOWER BULKHEAD SUPPORT ANGLE CORRODED AT BS 947, BETWEEN LBL 10 TO RBL 20. R&R ANGLE IAW SRM & DWG.
AFT CARGO BAY; R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS AREAS OF CORROSION BS727 TO BS767 RBL23 WL156 / REMOVED & REPLACED ACB R/H FLOOR TO SIDEWALL SUPPORT PLATE BS 727-767; RBL 23; WL 156 IAW SRM 51-40-02; SRM 51-40-05; DWG #146A7500
AFT CARGO BAY INTERCOSTAL ANGLE BELOW SHIELD BS 767- 787 RBL 23 WL 156 IS CORRODED / INSTERCOSTAL ANGLE BELOW SHIELD BS 767-787 RBL 23 WL156 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM. REMOVED REPLACED INTERCOSTAL ANGLE PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 146A8123.
AFT CARGO BAY SHIELD FORWARD OF CARGO DOOR CORRODED BETWEEN BS 767 TO BS 787, RBL 23. R&R SHIELD PER SRM & DWG.
AFT CARGO BAY, LT FLOOR TO SIDEWALL SUPPORT PLATE HAD AREAS CORRODED BETWEEN BS 727 TO BS 847, LBL 23. R&R SUPPORT IAW SRM & DWG.
AFT CARGO BAY CARGO FLOOR SPLICE STRAP CORRODED AT BS 887, BETWEEN RBL 10 TO LBL 10. R&R SPLICE STRAP IAW SRM & DWG.
AFT CARGO BAY, VERTICAL WEB CORRODED BETWEEN BS 787 TO BS 807, RBL 6. R&R VERTICAL WEB PER SRM & DWG.
AFT CARGO BAY, VERTICAL WEB CORRODED BETWEEN BS 807 TO BS 827, RBL 6. R&R VERTICAL WEB PER SRM & DWG.
FWD CARGO BAY AFT BULKHEAD GUSSET IS CRACKED AT BS500D STR19L / REMOVED AND REPLACED FWD CARGO BAY AFT BULKHEAD GUSSET @ BS 500D STR19L IAW SRM 51-40-05; SRM 51-40-02; AND DWG 143A7902
FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 500A TO BS 500B, RBL 23. R&R SUPPORT IAW SRM & DWG.
FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS 440 TO BS 480, RBL 27. R&R WEB PER SRM & DWG.
FWD CARGO BAY AFT BULKHEAD GUSSET IS CRACKED AT BS500D STR19R / REMOVED AND REPLACED FWD CARGO BAY AFT BULKHEAD GUSSET @ BS500D STR19R IAW SRM 51-40-02; SRM 51-40-05 AND DWG 143A7902.
RT WING TRAILING EDGE WIGGLE PLATE CRACKED AT RSS 293. R&R WIGGLE PLATE IAW SRM.
RIGHT WING TRAILING EDGE WIGGLE PLATE JUST O/B OF SWING DOWN PANEL CRACKED / REMOVED WIGGLE PLATE RIGH WING JUST O/B OF SWING DOWN PANEL IAW SRM 51-40-02-0G-01 89813U 08-31-19 LEAD 286 8/31/19 REPLACED WIGGLE PLATE RIGHT WING TRAILING EDGE JUST O/B OF SWING DOWN PANEL. IAW SRM 51-40-02-0G-0 89813U 09-01-19 FASTENERS IAW AIPC 57-50-00-22
AT LEFT WING TRAILING EDGE NUT PLATE BEAM BELOW #5 SPOILER PANEL IS CRACKED / REMOVED AND REPLACED NUT PLATE BEAM AT LEFT WING TRAILING EDGE; BELOW #5 SPOILER PANEL IAW SRM 51-40-02-G0-0 AND DRAWINGS 115A3758; 115A3712 59796C 30AUG19
#3 CANOE FAIRING 542BB HAS A CRACKED INNER SKIN BELOW LINKAGE / #3 CANOE FAIRING 542BB WITH A CRACKED INNER SKIN BELOW LINKAGE WAS REPAIRED PER SWA EA 1-757-16542 REV IR AND ATS ER# 19-04575 REV IR DATED 10-SEP-19
VAPOR BARRIER CRACKED AT BS 663, BETWEEN LBL 8 TO LBL 75. R&R VAPOR BARRIER PER SRM & DWG.
RIGHT WING AFT TRAILING EDGE SEAL SUPPORT CRACKED / REMOVED AND REPLACED RIGHT WING AFT TRAILING EDGE SEAL SUPPORT PER SRM 51-40-02 AND MM 20-50-11
AIR CONDITIONING DISTRIBUTION BAY, FLOORBEAM CRACKED AT BS. 540, BETWEEN L/H AND R/H OF BL 0. R&R INTERCOSTAL PER SRM.
FLOORBEAM INTERCOSTAL BROKEN BETWEEN BS 312 TO BS 328 LT SIDE. R&R INTERCOSTAL IAW SRM.
LT EMERGENCY EXIT SIDEWALL LIGHT INOP. R&R LIGHT ASSEMBLY IAW AMM.
FLOORBEAM WEB CRACKED BETWEEN BS 500A TO BS 500B, STR 26R. REPAIRED WEB IAW SRM.
FUSELAGE L/H FWD WING TO BODY FARING AFT SUPPORT BRACKET CRACKED. / REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-40-02
TRAILING EDGE FIXED PANEL 651GB FORWARD PANEL SUPPORT CRACKED. (WIGGLE PLATE.) / REMOVED AND REPLACED PER SRM 51-40-02
RT EMERGENCY EXIT AFT LIGHT INOP. SECURED HARNESS IAW WDM.
CCO 57-52-0048; LEFT HAND INBOARD FLAP CARRIAGE; OUTBOARD LOWER MOUNT BOLT HOLE IS NOT TRUE AND ROUND. / REMOVED AND REPLACED #4 INBOARD FLAP CARRIAGE IAW CCO 57-52-0048. REPLACED WITH SERVICABLE CARRIAGE. POS: 4 TAG/GRB NO.: 29420 P/N OFF: 113A2800-3 S/NON OFF: 7822 #4 P/N ON: 113A2800-3B S/N ON: 3H2326
WING TO BODY FAIRING 195BR HAS AREA OF DELAMINATION AT TOP AFT END. / REPAIRED WING TO BODY FAIRING 195BR AT TOP AFT END I/A/W SRM 51-70-04-SR-1 PAR 4-B-F REV 62
LT MAIN WHEEL WELL VERTICAL STIFFENER CRACKED AT BS 663, LBL 25. R&R STIFFENER IAW SRM AND DWG.
R\H HORZ STAB PANEL 343AB HAS METAL BLADE SEAL CRACKED. / REMOVED AND REPLACED STAB PNL SEAL ON PNL 343AB IAW SOPM 20-50-01 STEP 3F.
AFT CARGO PIT AFT CORNER SCUFF PLATE CRACKED / CRACKED AFT CARGO PIT AFT CORNER WELDED ON W/O 36201-1000-0001 AND SA EA 1-A53-2076 REV 11
LEFT WHEEL WELL; STATION 663; LBL 16; HORSESHOE ANGLE ABOVE THE LEFT PACK EXHAUST IS CRACKED ON THE INBOARD ANGLE. / REMPOVED AND INSTALLED NEW HORSESHOE ANGLE IN THE LEFT WHEEL WELL; STATION 663 AT PACK EXHAUST DUCT IAW DWG 111A1000 AND IAW SRM 51-40-02-0G
RIGHT WHEEL WELL; STATION 663; RBL 16; HORSESHOE ANGLE ABOVE THE RIGHT PACK EXHAUST DUCT; IS CRACKED ON THE INBOARD FLANGE. / REMOVED AND INSTALLED NEW HORSESHOE ANGLE ON THE RIGHT WHEEL WELL; STATION 663 AT EXHAUST DUCT IAW DWG 111A1000 AND IAWSRM 51-40-02-0G ATAG#GW0931
LT WING NR 1 SLAT LOWER SURFACE OF THE LEADING EDGE NOSE SKIN AT ACTUATOR CRACKED. REPAIRED SKIN IAW SRM.
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R&R LIGHT PER AMM.
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1670. R&R LIGHT PER AMM.
L2 DOOR EXIT LIGHT INOP. RELAMPED LIGHT PER MM.
MID CABIN OVERHEAD EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.
EMERGENCY LIGHTING BATTERY PACK M1672 FAILED CAPACITY CHECK. R&R BATTERY PACK PER AMM.
EMERGENCY LIGHTING BATTERY PACK M1669 FAILED CAPACITY CHECK. R&R BATTERY PACK PER AMM.
L1 DOOR EMERGENCY SLIDE LIGHT LENS LOOSE. R & R THE LENS IAW AMM.
RIGHT AFT SERVICE DOOR EMER EXIT LIGHT INOPERATIVE. R & R BATTERY CHARGER IAW MM.
LEFT FWD GALLEY BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.
FORWARD SERVICE DOOR EMER LIGHT INOPERATIVE. FOUND CONNECTOR LOOSE, RE-SEATED CONNECTOR IAW WDM & AMM.
FRAME CRACKED AT BS 480, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 440, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 400, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 360, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 747, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 727D, STRINGER 8R. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 787, STRINGER 8R. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 727A, STRINGER 8L. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 480, STRINGER 8L. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 360, STINGER 8L. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 400, STRINGER 8L. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 440, STRINGER 8L. REPAIRED FRAME IAW EA.
FUSELAGE FRAME CRACKED AT BS 787, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 727D, STRINGER 8L. REPAIRED FRAME IAW EA.
R2 DOOR EMER EVAC SLIDE SKIRT WORN. R & R SLIDE IAW CARD.
R2 DOOR EMER EVAC SLIDE GIRT BAR QUICK RELEASE RETAINER CLIP BROKEN. R & R CLIP IAW AMM.
LEFT EMER EXIT HATCH ESCAPE STRAP HOOK CORRODED. R & R STRAP IAW AMM.
R1 DOOR FWD FRAME LOWER STUB BEAM CRACKED AT INBD HOLE AT WL 208. REPAIRED STUB BEAM IAW ER & EA.
RIGHT EMER EXIT HATCH ESCAPE STRAP HOOK. R & R STRAP IAW AMM.
FORWARD CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 420 TO 440, BETWEEN STRINGER 24L TO 25L. R & R SUPPORT IAW SRM & DWG.
INTERCOSTAL CRACKED BETWEEN BS 277 TO 294.5, UNDER FLOOR ACCESS PANEL 221AF. R & R INTERCOSTAL IAW SRM.