N565WN
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SOUTHWEST AIRLINES CO | Operator | 2016-04-14 – 2016-04-14 | Operator named in NTSB report |
| SOUTHWEST AIRLINES, CO. (SWAA) | Operator | 2016-04-14 – 2016-04-14 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
AT FL250 CABIN PRESSURE DROPPED TO -4000 PSI; ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09-11 NO DEFECTS NOTED. PRESSURIZED AIRCRAFT TO 4.5 PSID NO ABNORMAL LEAKS NOTED IAW MM 21-31-00. PERFORMED PRESSURIZATION DECAY TEST TWICE WITH DECAY TIMES TO BE 119 SECS. PERFORMED BOTH PRESSURE CONTROLLER BITE TEST IAW MM 21-31-01 & FOUND SEVERAL LEGS WITH LOW INFLOW, HIGH LEAKAGE FOUND ON SEVERAL RANDOM FLT LEGS. R & R NR 1 ENG. HIGH STAGE REGULATOR IAW AMM 36-11-07, LEAK & OPS CHECK DUE. R & R NR 2 ENG. HIGH STAGE REGULATOR IAW AMM 36-11-07, LEAK & OPS CHECK DUE. R & R NR 2 ENG. HIGH STAGE VALVE IAW AMM 36-11-06, LEAK & OPS CHECK DUE. R & R NR 1 ENG. HIGH STAGE VALVE IAW AMM 36-11-06, LEAK & OPS CHECK DUE. COMPLETED OPS CHECKS IAW AMM 36-11-06 AND AMM 36-11-07.
AT FL250 CABIN PRESSURE DROPPED TO -4000 PSI, ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09-11, NO DEFECTS NOTED. PRESSURIZED ACFT TO 4.5 PSID, NO ABNORMAL LEAKS NOTED IAW MM 21-31-00. PERFORMED PRESSURIZATION DECAY TEST TWICE WITH DECAY TIMES TO BE 119 SECONDS. PERFORMED BOTH PRESSURE CONTROLLER BITE TEST IAW MM 21-31-01 & FOUND SEVERAL LEGS WITH LOW INFLOW, HIGH LEAKAGE FOUND ON SEVERAL RANDOM FLT LEGS. R & R NR 1 ENG. HIGH STAGE REGULATOR IAW AMM 36-11-07, LEAK & OPS CHECK DUE. R & R NR 2 ENG. HIGH STAGE REGULATOR IAW AMM 36-11-07, LEAK & OPS CHECK DUE. R & R NR 2 ENG. HIGH STAGE VALVE IAW AMM 36-11-06, LEAK & OPS CHECK DUE. R & R NR 1 ENG HIGH STAGE VALVE IAW AMM 36-11-06, LEAK & OPS CHECK DUE. COMPLETED OPS CHECKS IAW AMM 36-11-06 & AMM 36-11-07.
AT FL250 CABIN PRESSURE DROPPED TO -4000 PSI; ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09-11, NO DEFECTS NOTED. PRESSURIZED ACFT TO 4.5 PSID, NO ABNORMAL LEAKS NOTED IAW MM 21-31-00. PERFORMED PRESSURIZATION DECAY TEST TWICE WITH DECAY TIMES TO BE 119 SECS. PERFORMED BOTH PRESSURE CONTROLLER BITE TEST IAW MM 21-31-01 & FOUND SEVERAL LEGS WITH LOW INFLOW, HIGH LEAKAGE FOUND ON SEVERAL RANDOM FLT LEGS. R & R NR 1 ENG. HIGH STAGE REGULATOR IAW AMM 36-11-07, LEAK & OPS CHECK DUE. R & R NR 2 ENG HIGH STAGE REGULATOR IAW AMM 36-11-07, LEAK & OPS CHECK DUE. R & R NR 2 ENG HIGH STAGE VALVE IAW AMM 36-11-06, LEAK & OPS CHECK DUE. R & R NR 1 ENG HIGH STAGE VALVE IAW AMM 36-11-06, LEAK & OPS CHECK DUE. COMPLETED OPS CHECKS IAW AMM 36-11-06, & AMM 36-11-07.
AT FL250 CABIN PRESSURE DROPPED TO -4000 PSI; ALT HORN SOUNDED. RAN QRH PRESSURE WAS CONTROLLED IN MANUAL. INSPECTED BOTH CARGO DOOR PRESSURE SEALS IAW MM 52-09-11, NO DEFECTS NOTED. PRESSURIZED ACFT TO 4.5 PSID, NO ABNORMAL LEAKS NOTED IAW MM 21-31-00. ALSO PERFORMED PRESSURIZATION DECAY TEST TWICE WITH DECAY TIMES TO BE 119 SECS. PERFORMED BOTH PRESSURE CONTROLLER BITE TEST IAW MM 21-31-01, & FOUND SEVERAL LEGS WITH LOW INFLOW, HIGH LEAKAGE FOUNDS ON SEVERAL RANDOM FLIGHT LEGS. R & R NR 1 ENG HIGH STAGE REGULATOR IAW AMM 36-11-07, LEAK & OPS CHECK DUE. R & R NR 2 ENG HIGH STAGE REGULATOR IAW AMM 36-11-07, LEAK & OPS CHECK DUE. R & R NR 2 ENG HIGH STAGE VALVE IAW AMM 36-11-06, LEAK & OPS CHECK DUE. R & R NR 1 ENG HIGH STAGE VALVE IAW AMM 36-11-06, LEAK AND OPS CHECK DUE. COMPLETED OPS CHECKS IAW AMM 36-11-06, & AMM 36-11-07.
LEFT OVERWING EMERGENCY EXIT DOOR HANDLE HOUSING MISSING SCREW LEFT OVERWING EMERGENCY EXIT DOOR HANDLE HOUSING MISSING SCREW. REPLACED LT OVERWING EMERGENCY EXIT DOOR HANDLE HOUSING SCREW IAW AMM 12-25-22.
TRAILING EDGE FLAPS INOPERATIVE. FIM 27-59 TASK 808 CARRIED OUT. OHMED FOR CONTINUITY, SHORTS, INSULATION RESISTANCE & DAR TEST IAW WDM 27-53-21. NO FINDINGS. REPLACED FSEU IAW AMM 27-51-01. OPS CHECKED GOOD.
AFTER PUTTING FLAP LEVER TO 5 THE FLAPS DID NOT EXTEND. WE NOTICED A VERY SMALL SPLIT IN THE TRAILING EDGE FLAPS. LE DEVICES WERE EXTENDED WITH THE ALTERNATE FLAP SWITCH PER QRH. THE LANDING WAS NORMAL AND UNEVENTFUL. R&R #8 FLAP SKEW SENSOR PER AMM 27-59-01.
AS WE WERE ABOUT TO SELECT FLAPS 1 (210KTS) WE NOTICED THE FLAP GAUGE INDICATING ZERO - ONE ON RT SIDE. WHEN WE SELECTED F1 THE FLAPS/SLATS DID NOT EXTEND. SELECTED F5, SAME RESULT. RETURNED FLAP HANDLE TO ZERO CHECKED CIRCUIT BREAKERS, ALL IN, AND EXECUTED TRAILING EDGE FLAPS UP LANDING CHECKLIST QRH 9.34-9.36 COMPLIED WITH, VREF 163 VTARGET 168. COMPLIED WITH FSEU BITE IAW FIM 27-51 TASK 801, NO CURRENT FAULTS FOUND. FOUND INTERMITTENT INACTIVE FAULT 27-53257. INSPECTED TRAILING EDGE FLAP DRIVE SYS IAW AMM 27-51-00, NO DEFECTS FOUND. PERFORMED TRAILING EDGE OPS CHECK IAW AMM 27-51-00 NO DEFECTS FOUND. AC OK FOR SERVICE.
AFT ENTRY DOOR SLIDE EXCESSIVE FABRIC<[01] REPOSITIONED AFT ENTRY SKIRT SLIDE PER AMM 25-66-01 AND TASK MT 725-61-06.
CREW REPORTS OVER WING EMERGENCY EXIT INDICATOR LIGHT INOP. REMOVED AND REPLACED EXIT INDICATOR SIGN PER AMM 33-51-01.
L/H OVER WING EMERGENCY EXIT LIGHT LENS COVER MISSING<[01] INSTALLED L/H OVER WING EMERGENCY EXIT LUGHT LENS COVER PER SIP
FWD ENTRY DOOR SLIDE SHROUD NOT INSTALLED PROPERLY AT BOTTOM CENTER OF SHROUD<[01] INSTALLED CORRECTLY FWD ENTRY DOOR-SLIDE IAW AMM 25-66-01-400-801.;[02] INSTALLED CORRECTLY FWD ENTRY DOOR-SLIDE IAW AMM 25-66-01/401-MT 725-61-06.;[03] VERIFIED CORRECTIVE ACTION ITEM 2; CARD COMPLETE.
EMERGENCY LIGHT L1065 INOP APROX STA 480 LEFT<[01] RELAMPED EMERGENCY LIGHT L1065 APROX STA 480 LEFT; PERFORMED GOOD TEST PER AMM 33-51-03-960-801;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
EMERGENCY EXIT CEILING LIGHT L1419 INOP.<[01] PERFORMED TROUBLESHOOTING FOUND CONNECTOR D40038J DISCONNECT. RECONNECTED CONNECTOR D40038P FOR THE EMERGENCY LIGHT L1419 PER SWPM 20-63-02. PERFORMED GOOD OPERATIONAL TEST PER AMM 33-51-00-710-801;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.
PASSENGER CABIN SEAT TRACK AFT FASTENER HEAD HAS A CRACK AT BS 727B; RBL 24.75. (MARKED)<[01] FINISHED PER EA-25-153-00101;[02] VERIFIED CORRECTIVE ACTION COMPLETE
RT HAND FWD UPPER TRACK ASSY FOR PANEL 343AT CRACKED.<[01] REMOVED AND REPLACED RT HAND FWD UPPER TRACK ASSY FOR PANEL 343AT IAW AMM 27-41-31-400-802.; [02] VERIFIED CORRECTIVE ACTION ENTRY 1.
FCB FWD CORNER SCUFF PLATE CRACKED<[01] REPAIRED IAW SRM 53-30-15-2R-1; NDI CRACK FREE; FCB FWD CORNER SCUFF PLATE;[02] VERIFIED ALL STEPS; CORRECTION ACTION ITEM 1; MEASUREMENT FIELD COMPLETE; CARD COMPLETE.
ACB AFT CORNER SCUFF PLATE CRACKED<[01] VERIFIED
ACB FWD CORNER SCUFF PLATE CRACKED<[01] VERIFIED
BS540 FLOOR SUPPORT (PANEL BREAK) IS CRACKED LBL1; WL208<[01] REMOVED AND REPLACED FLOOR SUPPORT (PANEL BREAK) BS540 LBL1 TO LBL24 IAW SRM 51-40-02 AND DWG 143A0060 ID:0002 REV: B<BR>INSTALLED PANEL 231UF IAW AMM 53-21-00-400-801;[02] CORRECTIVE ACTION COMPLETED.
BS540 FLOOR SUPPORT (PANEL BREAK) IS CRACKED RBL1; WL208<[01] REOMOVED AND REPLACED NEW FLOOR SUPPORT (PANEL BREAK) BS540 RBL1 TO RBL24 IAW SRM 51-40-02 AND DWG 143A0060 ID:0002 REV: B;[02] VERIFIED CORRECTIVE ACTION 1
PASSENGER CABIN FLOOR PANEL 231XF HAS AREAS OF PULLED STRANDS<[01] PASSENGER CABIN FLOOR PANEL 231XF WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 144A5810 ID:0007.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
PASSENGER CABIN FLOOR PANEL 241FF HAS AREAS OF PULLED STRANDS<[01] FOUND DAMAGE TO PANEL 241FF BE BEYOND ECONOMICAL REPAIR; FABRICATED NEW FLOOR PANEL FROM BMS 4-17 TY 6 LOT 1583459-1; INSTALLED INSERTS WITH BMS 5-107 LOT AK4BA2601A/A; CURED INSERTS AND PART MARKED IAW SRM 53-00-50-2R-0 PARA 1.A NOTE; PARA 4 AND 5.S; TABLE 204 AND BOEING DWG 114A5810-22;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
PASSENGER CABIN FLOOR PANEL 241EF HAS AREAS OF PULLED STRANDS<[01] FOUND DAMAGE TO PANEL 241EF BE BEYOND ECONOMICAL REPAIR; FABRICATED NEW FLOOR PANEL FROM BMS 4-17 TY 6 LOT 1583459-1; INSTALLED INSERTS WITH BMS 5-107 LOT AK4BA2601A/A; CURED INSERTS AND PART MARKED IAW SRM 53-00-50-2R-0 PARA 1.A NOTE; PARA 4 AND 5.S; TABLE 204 AND BOEING DWG 114A5810-129;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
PASSENGER CABIN FLOOR PANEL 241DF HAS AREAS OF PULLED STRANDS<[01] PASSENGER CABIN FLOOR PANEL 241DF; WITH AREAS OF PULLED STRANDS; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL; DUE TO THE EXTENT OF ALL OF THE DAMAGE; IAW SRM 53-00-50-2R-0.;[02] WORK COMPLETED.;[03] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
PASSENGER CABIN FLOOR PANEL 241BF HAS AREAS OF PULLED STRANDS<[01] PASSENGER CABIN FLOOR PANEL 241BF WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 144A5810 ID:0018.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
PASSENGER CABIN FLOOR PANEL 231ZF HAS AREAS OF PULLED STRANDS<[01] PASSENGER CABIN FLOOR PANEL 231ZF WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 144A5810 ID:0020.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
PASSENGER CABIN FLOOR PANEL 231YF HAS AREAS OF PULLED STRANDS<[01] PASSENGER CABIN FLOOR PANEL 231YF WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 144A5810 ID:0017.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
GRAB ASSIST HANDLE BROKEN FWD ENTRY DOOR<[01] RE SECURED PER SIP NO DEFECTS NOTED.
F/O SIDE EXIT SIGN AT FOOT LEVEL FELL OFF AND COULDNT BE REATTACHED<[01] RE-ATTACHED LIGHT LENS PER AMM 33-51-01
EMERGENCY EXIT LIGHT COVER MISSING F/O SIDE OVERWING EXIT LOWER LENS<[01] INSTALLED LIGHT COVER F/O SIDE EMERGENCY EXIT LIGHT PER AMM 33-51-04
ROW 12DEF EMERGENCY EXIT FWD LIGHT ASSY COVER IS MISSING<[01] INSTALLED EMERGENCY LIGHT LENS COVER AT ROW 12 DEF FWD LIGHT ASSY IAW AMM 33-51-01.
FLAP ASYMMETRY DISCOVERED DURING CRUISE BY SPLIT NEEDLES ON FLAP GAUGE. RT FLAP SHOWED FULL UP; LT FLAP WAS BETWEEN UP AND 1. VERIFIED ASYMMETRY BY CONFIGURING EARLY ON ARRIVAL. FLAPS DID NOT MOVE. PERFORMED A TRAILING FLAPS UP LANDING. VREF/VTARGET WAS 170/175. AUTOBRAKES 3 SELECTED. LANDING WAS SMOOTH & DIDNT FEEL AUTOBRAKING UNTIL 150 KTS. RAN BRAKE COOLING FOR 160 KTS AND PARKED AT GATE FOR COOLING. AFTER LANDING NOTICED FLAP GAUGE READING BOTH FLAPS FULL UP LIKE NORMAL. ALSO NOTED HYD SYS B WAS AT 73% RF.<[01] REF AD-HOC FOR FLAP LOCK OUT (TTG8Q00MJMKL)<BR>FLAP #2 SKEW SENSOR R/R; TERMINATED PIN D40024J; AND R/R CONNECTOR D40024P/J. OPS CHECK GOOD PER AMM 27-51-00.
FLAP ASYMMETRY DISCOVERED DURING CRUISE BY SPLIT NEEDLES ON FLAP GAUGE. RT FLAP SHOWED FULL UP; LT FLAP WAS BETWEEN UP AND 1. VERIFIED ASYMMETRY BY CONFIGURING EARLY ON ARRIVAL. FLAPS DID NOT MOVE. PERFORMED A TRAILING FLAPS UP LANDING. VREF/VTARGET WAS 170/175. AUTOBRAKES 3 SELECTED. LANDING WAS SMOOTH & DIDNT FEEL AUTOBRAKING UNTIL 150 KTS. RAN BRAKE COOLING FOR 160 KTS AND PARKED AT GATE FOR COOLING. AFTER LANDING NOTICED FLAP GAUGE READING BOTH FLAPS FULL UP LIKE NORMAL. ALSO NOTED HYD SYS B WAS AT 73% RF.<[01] REF AD-HOC FOR FLAP LOCK OUT (TTG8Q00MJMKL)<BR>FLAP #2 SKEW SENSOR R/R; TERMINATED PIN D40024J; AND R/R CONNECTOR D40024P/J. OPS CHECK GOOD PER AMM 27-51-00.
AT CRUISE NOTICED A SMALL SPLIT ON THE FLAP GAUGE. RIGHT FLAP AT 0 LEFT FLAP AT .2. ON CONFIGURATION FOR LANDING FLAPS 1 SELECTED WITH NO MOVEMENT OF THE FLAPS. LED'S DID NOT MOVE EITHER. SAME WHEN FLAPS 5 WAS SELECTED. QRH WAS RUN WE LANDED WITH FULL LED'S AND 0 TRAILING EDGE FLAPS<[01] PERFORMED FSEU BITE PER FIM 27-51- TASK 801; FAULTING THE #1 SKEW. CLEANED AND RESEATED #1 FLAP SKEW SENSOR PER AMM 27-59-01. CHECKED SKEW SENSOR READINGS IN AHM; ALL WITHIN LIMITS. CYCLED FLAPS SEVERAL TIMES; NO FAULTS NOTE. A/C OK FOR SERVICE.
ON DECENT #2 ENGINE OIL QTY DROPPED TO 21% ON DECENT #2 ENGINE OIL QTY DROPPED TO 21%.WHEN THRUST LEVER WAS MOVED FORWARD THE QTY DROPPED TO 19% WE KEPT THE #2 THRUST LEVER AT IDLE FOR THE REST OF THE DECENT & APPROACH. THE #2 OIL QTY REACHED 11% ON SHORT FINAL.THE #2 OIL PRESSURE READ NORMAL THROUGHOUT .<[01] DRY MOTORED #2 ENGINE FOUND OIL SPRAYING FROM #2 ENGINE STARTER. R&R ENGINE #2 STARTER PER AMM 80-11-01.OPS AND LEAK CHECK GOOD. REPLENISHED #2 ENGINE OIL WITH 16 QUARTS.
SELECTED FLAPS 5; ONE FLAP STAYED AT ZERO; OTHER FLAP STOPPED AT LESS THEN 1.<[01] UPDATING PARTS TRANSACTION;[02] PERFORMED PARTS TRANSACTION ONLY;[03] FSEU FAULTED SKEW SENSOR 1. REPLACED SKEW SENSOR 1 REF. AMM 27-59-01. OPS CHECKS GOOD.
ON APPROACH WITH FLAPS 5 SELECTED FLAPS LOCKED OUT BETWEEN 1 AND UP. SMOOTH NORMAL LANDING.<[01] R&R RH FLAP POSITION TRANSMITTER IAW AMM 27-58-01. OPS CHECK GOOD. NO DEFECTS NOTED.
RUDDER CONDUCTIVE FRAME PREVIOUS REPAIR SPLICE STRIP PEELED BACK; LH SIDE AT TE.<[01] INSTALLED NEW SPLICE STRIP AND VERIFIED CONDUCTIVITY LESS THAN 0.01 OHM IAW SRM 55-40-01-2R-2.;[02] NO CHANGE TO WEIGHT AND BALANCE. NO ADDITIONAL MATERIAL ADDED; MATERIAL INSTALLED EQUAL TO MATERIAL REMOVED.;[03] ADDED REFERENCE AND DAMAGE RECORD
MULTIPLE CABIN EMERGENCY LIGHT INOP<[01] FOUND CABIN EMERGENCY LIGHTS INOP AT 6C 8D 9C 12C 13D 18D. R/R POWER SUPPLY AND BATTERY PACK AT 7A ALONG THE SIDEWALL NEAR FLOOR; LIGHTS OPS GOOD AT 6C 8D 9C.<BR>SLAVED IN POWER SUPPLY AND BATTERY PACK AT 11A 12F 17A ALONG THE SIDEWALL NEAR FLOOR AND BOTH NEAR THE AFT ENTRY DOOR NO HELP; BACK TO ORIGINAL CONFIG. EMERGENCY LIGHTS AT 12C 13D 18D INOP. AWD IAW B737 AMM 33-51-06.;[02] -AS PER WDM33-51-13-5 T/SHOOTING C/OUT;FOUND D11328 AND D11330 PLUG NOT PROPERLY CONNECTED ; RECONNECTED IT; OPS CHKED GOOD FOR 12C;13D EMERGENCY LT.<BR>-FOUND WIRE OPEN AT BEHIND PIN 16/D10744 PLUG; TERMINATED PIN PER SWPM 20-60-00 AND OPS CHKED GOOD FOR 18D EMERGENCY L/T.<BR>-ALL EMERGENCY L/T OPS CHKED GOOD PER AMM 33-51-00;[03] AS PER WDM33-51-13-5 T/SHOOTING C/OUT;FOUND D11328 AND D11330 PLUG NOT PROPERLY CONNECTED ; RECONNECTED IT; OPS CHKED GOOD FOR 12C;13D EMERGENCY LT. <BR>-FOUND WIRE OPEN AT BEHIND PIN 16/D10744 PLUG; TERMINATED PIN PER SWPM 20-60-00 AND OPS CHKED GOOD FOR 18D EMERGENCY L/T. <BR>-ALL EMERGENCY L/T OPS CHKED GOOD PER AMM 33-51-00
AISLE LIGHT AT STA727E+13 RBL29 AND AFT SERVICE DOOR SLIDE LIGHT DO NOT ILLUMINATE DURING INSTALLATION TEST OF M1672 BATTERY<[01] **FOUND CONNECTOR D11336 DISCONNECTED. CONNECTED D11336 PER SWPM 20-61-28 AND PERFORMED GOOD TEST OF AISLE LIGHT AT 727E+13 RBL29 PER AMM 33-51-04-960-801; STEP 2.F.(2).<BR>**REPLACED LAMP FOR AFT SERVICE DOOR SLIDE LIGHT AND PERFORMED GOOD TEST PER AMM 33-51-04-960-801.;[02] CORRECTION TO AISLE LIGHT FUNCTIONAL REFERENCE: GOOD TEST OF AISLE LIGHT PER AMM 33-51-03-960-801; STEP 2.D.(2).;[03] VERIFIED CORRECTIVE ACTION 1 AND 2.
NEED TO RELOCATE FLOOR PANEL #241FF INSERT (1 EACH) DUE TO REPAIRED INSTALLED ON THE FLOORBEAM AT BS727+6 LBL 45.57.<[01] FABRICATED NEW FLOOR PANEL 241FF USING BMS 4-17TY6 LOT#1514505-1; INSTALLED ALL INSERTS EXCEPT P12 TO BE RELOCATED USING BMS 5-107 LOT#AK2KP8383K IAW SRM 53-00-50-2R-0 PARA 1A.(NOTE); 4; 5.S AND BOEING DWG 144A5810-22;[02] CURED ALL INSERTS USING HEAT LAMP IAW SRM 53-00-50-2R-0 PARA 5.S.<BR><BR>THERMOMETER ID: ATS2209 / CAL DUE DATE' 10/2023<BR><BR>COMPLETED ALL STEPS OF EA 23-153-00384-WIP1 WITH NO DEVIATIONS NOTED.;[03] COMPLETED STEP 1 OF EA 23-153-00384-WIP2 WITH NO DEVIATIONS NOTED.;[04] REFER TO EA 23-153-00384 SUMMARY REQUIREMENT; BARCODE: TTG8Q00HPR44;[05] COMPLETED ALL STEPS OF EA 23-153-00384.;[06] JOB COMPLETE.
1 EACH WIRE IS PULLED OUT OF GROUND BLOCK BEHIND AFT LAV; JUST FWD OF BS 1006 ON L/H SIDEWALL<[01] RETERMINATED WIRE W3142-0451-18 TO GD3778 PER WDM 33-51-14.;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] RETERMINATED WIRE W3142-0451-18 TO GD3778 PER WDM 33-51-14; AND PERFOMED GOOD TEST OF AFT LH ESCAPE SLIDE LIGHT PER AMM 33-51-04-960-801 STEP 2.F.(2);[04] EDITED STEP 1 PER QC COMPLETE;[05] CERTIFYIG ACTION ITEMS 3 AND 4.;[06] COMPLETED STEP 1;[07] ALL WORK COMPLETE.;[08] VERIFIED REQUIRED CORRECTIVE ACTIONS COMPLETED.
BAFFLE UNDER L/H FLOOR TO SIDEWALL SUPPORT BS 400-420 LBL 25 IS CRACKED<[01] REMOVED BAFFLE UNDER FLOOR TO SIDEWALL SUPPORT BS 400-420 LBL 25 PER SRM 51-40-02-0G-0.;[02] CRACK BAFFLE UNDER L/H FLOOR TO SIDEWALL SUPPORT BS 400-420 LBL 25 WITH NEXT DIMENSIONS L=0.142 TOOL USED ID: ATS1317; SN: UNKNOWN; DATE:08/2022; DUE:08/2023 FOUND TO BE OUT LIMITS I.A.W SRM 53-30-53-0L-2 FOR IDENTIFICATION AND SRM 53-00-053-1A-2 FOR ALLOWABLE DAMAGE IT WILL BE REPAIRABLE BY REPLACEMENT I.A.W SRM 51-10-02-0G PAR 9C .;[03] LOCATED AND DRILLED NEW BAFFLE UNDER L/H FLOOR TO SIDEWALL SUPPORT BS 400-420 LBL 25 I.A.W SRM 51-40-05-0G-0 AND DWG 143A7500.AND OK TO INSTALL.;[04] VERIFIED MEASUREMENTS<BR>VERIFIED CORRECTIVE ACTION #2; 3;[05] INSTALLED NEW BAFFLE UNDER L/H FLOOR TO SIDEWALL SUPPORT BS 400-420 LBL 25 I.A.W SRM 51-40-02-0G-0 AND DWG 143A7500.;[06] VERIFIED CORRECTIVE ACTION #5
FLOOR PANEL 232RF UPPER SKIN PREVIOUS REPAIR IS DISBONDED. (MARKED)<[01] IDENTIFIED FLOOR PANEL 232RF MATERIAL IAW SRM 53-00-50-0I-1 FIG 4 TABLE 4<BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4B<BR><BR>DUE TO EXTENT OF DAMAGE FABRICATED NEW 232RF FLOOR PANEL FROM BMS4-23 TYPE 2 LOT#1508290-1; INSTALLED INSERTS USING BMS5-107 LOT#1513635-1 AND CURED USING HEATLAMPS AND THERMOMETER ATS2208 CAL DUE DATE 10/2023 IAW SRM 53-00-50-2R-0 PARA 1A(NOTE) AND BOEING DWG 144A5810-17;[02] INSPECTED AND VERIFIED CORRECTIVE ACTIONS. JOB COMPLETE.<BR><BR>VERIFIED MEASUREMENTS TABLE.
FLOOR PANEL 242CF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] IDENTIFIED PANEL 241CF MATERIAL IAW SRM 53-00-50-0I-1 FIG 4 TABLE 4 AND DWG: 144A5810 ID: 0019.<BR><BR>PANEL IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.C AND 4.F.<BR><BR>OK TO FABRICATE A NEW PANEL IAW SRM 53-00-50-2R-0 PARA 1.A.;[02] UPDATED MEASUREMENTS;[03] FABRICATED NEW FLOOR PANEL AND LOCATED INSERT HOLES USING BMS4-17 TYVI LOT#1496139-1 IAW SRM 53-00-50-2R-0 PARAGRAPH 5.S(1) (A-C) AND BAC DWG 144A5810 ID:0019.;[04] FINISHED FABRICATION OF FLOOR PANEL. INSTALLED 26EA INSERTS USING BMS 5-107 LOT: 1513635-1<BR>CURED RESIN USING THERMOMETER ATS2209 DUE: 10/2023 AND PART MARKED PANEL IAW SRM 53-00-50-2R-0 PARA 5.S.(1). ALONG WITH DWG 144A5810 SHEET 19.;[05] INSPECTED AND VERIFIED CORRECTIVE ACTIONS. JOB COMPLETE.<BR><BR>VERIFIED MEASUREMENTS TABLE.
FLOOR PANEL 241FF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] PART/MATERIAL IDENTIFIED PER SRM 53-00-50-0I-1 FIG 4 TABLE 4 LOW TRAFFIC<BR>NUMEROUS PULLED STRANDS DENTS & HEAL STRIKES EXCEEDS ALLOWABLE DAMAGE LIMITS & IS BEYOND ECONOMICAL REPAIR . AS GIVEN IN SRM 53-00-50-1A-1 PARA 4 B. C. D. & F.<BR>PANEL REPLACEMENT WILL BE ACCOMPLISHED PER SRM 53-00-50-2R-0 PARA 1. A. NOTE:;[02] FABRICATED NEW FLOOR PANEL 241FF USING BMS 4-17 TY6 LOT#1486491-1; INSTALLED INSERTS USING BMS 5-107 LOT#1513635-1; CURED WITH HEAT LAMPS AND THERMOMETER ID: ATS2209 DUE: 10/23; AND PART MARKED IAW SRM 53-00-50-2R-0 PARA 1.A. NOTE.5. S AND BDWG 144A5810-22.;[03] INSPECTED AND VERIFIED CORRECTIVE ACTIONS. JOB COMPLETE.<BR><BR>VERIFIED MEASUREMENTS TABLE.
FLOOR PANEL 242DF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] IDENTIFIED PANEL 242DF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 4; TABLE 4; AND DWG DOC: 144A5800 ID: 0004. <BR><BR>PANEL IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR. 4.C. & F. <BR><BR>OK TO FABRICATE NEW PANEL FOLLOWING SRM 53-00-50-2R-0 PAR. 1.A.;[02] UPDATED MEASUREMENTS;[03] CORRECTION TO CORRECTIVE ACTION 1: ' AND DWG DOC: 144A5800 ID: 0004'; TO SAY; ' AND DWG DOC: 144A5800 ID: 0011.';[04] UPDATED MEASUREMENTS;[05] FABRICATED NEW FLOORBOARD USING BMS4-17 TY VI LOT# 1496139-1 SANDED EDGES AND CLEANED IAW SRM 53-00-50-2R-0 PAR. 4.A.(1)<BR><BR>LOCATED AND UPSIZED INSERT HOLE LOCATIONS AND CLEANED (42EA) TO FACILITATE FOR INSERT INSTALL IAW SRM 53-00-50-2R-0 PAR. 5.S.(1)(A)-(D) AND DWG: 144A5810 ID: 0016;[06] INSTALLED INSERTS USING BMS 5-107 LOT#1513635-1; CURED WITH HEAT LAMPS AND THERMOMETER ID: ATS2209 DUE: 10/23; AND PART MARKED IAW SRM 53-00-50-2R-0 PARA 5.S AND BDWG 144A5810-16;[07] EDIT CORRECTIVE ACTIONS 1 AND 3: DRAWING USED FOR ID IS 144A5810 ID: 0016;[08] INSPECTED AND VERIFIED CORRECTIVE ACTIONS. JOB COMPLETE.<BR><BR>VERIFIED MEASUREMENTS TABLE.
FLOOR PANEL 231XF UPPER SURFACE HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] IDENTIFIED PANEL 231XF MATERIAL IAW SRM 53-00-50-0I-1 FIG 4 TABLE 4 AND DWG: 144A5810 ID: 0007.<BR><BR>PANEL IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.C AND 4.F.<BR><BR>OK TO FABRICATE A NEW PANEL IAW SRM 53-00-50-2R-0 PARA 1.A.;[02] UPDATED MEASUREMENTS;[03] FABRICATED NEW FLOOR PANEL AND LOCATED INSERT HOLES USING BMS4-17 TYVI LOT#1496139-1 IAW SRM 53-00-50-2R-0 PARAGRAPH 5.S(1) (A-C) AND BAC DWG 144A5810 ID:0007.;[04] FINISHED FABRICATION OF FLOOR PANEL 231XF; INSERTS INSTALLED USING BMS5-107 LOT#1513635-1 AND CURED USING HEAT LAMP AND THERMOMETER ATS2208 CAL DUE DATE 10/2023 IAW SRM 51-70-05-2R-0 PARA 1A(NOTE) AND BOEING DWG 144A5810-7;[05] INSPECTED AND VERIFIED CORRECTIVE ACTIONS. JOB COMPLETE.<BR><BR>VERIFIED MEASUREMENTS TABLE.
CORROSION ON FWD CARGO BAY ATTACH BRACKET AT BS 480 BETWEEN STRINGER 23L-24L.<[01] THE STRUCTURAL ITEM DOES NOT HAVE ALLOWABLE DAMAGE ENTRIES . THEREFORE HAS TO BE REPAIRED BY REPLACEMENT PER REF SRM 51-10-02-0G-0<BR><BR>FABRICATED NEW BRACKET FROM MATERIAL 6013T4#0.040'' LOT NBR 1404467-1 PER REF DWG NBR 417A2106;[02] VERIFIED CORRECTIVE ACTION 1.;[03] RECEIVED BRACKET FROM OSS HFAB53-BR-151 PO NBR 903645<BR><BR>LOCATED AND DRILLED NEW BRACKET PER REF SRM 51-40-05 AND DWG NBR 417A2106<BR><BR>OK TO APPLY PRIME;[04] VERIFIED CORRECTIVE ACTION STEP 3. VERIFIED OK TO PRIME.;[05] APPLIED PRIME AT BRACKET PER REF AMM 51-21-99;[06] REMOVED AND REPLACED BRACKET PER REF SRM 51-40-02 AND DWG NBR 417A2106;[07] VERIFIED CORRECTIVE ACTION STEP 6.;[08] VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
CORROSION ON FWD CARGO BAY R/H AFT BULKHEAD TO SIDEWALL ANGLE AT BS 500D RBL 27.5; RBL 31; RBL 34; RBL 34; RBL 35; RBL 37; RBL 46; RBL 48; RBL 51. CORROSION ON FWD CARGO BAY R/H AFT BULKHEAD TO SIDEWALL ANGLE AT BS 500D RBL 27.5 RBL 31 RBL 34 RBL 35 RBL 37 RBL 46 RBL 48 RBL 51<[01] VERIFIED APPLICABILITY SRM 53-30-08-01-1 FOR IDENTIFICATION AND SRM 53-30-08-1A-1 FOR ALLOWABLE DAMAGE.<BR><BR>REMOVED CORROSION IAW SRM 51-10-02.<BR><BR>EVALUATED DAMAGE REMOVAL AT BLENDED AREA L=1'' W=0.800' ORIGINAL THICKNESS= 0.071'; REMAINING =0.055'; MATERIAL LOSS= 0.016'; MAX MAT REMOVE ALLOWABLE =0.015' FOUND TO BE OUT OF LIMITS IAW SRM 53-30-08-1A-1 PARA 4A (2) FIG 103 DETAIL C.<BR>TOOL ID: ATS2826 S/N: UNKNOWN DUE:01/2024.;[02] VERIFIED CORRECTIVE ACTION1 AND STEPS 1-8.;[03] THIS FAUL WILL BE ACOMPLISHED ON CARD TTG8Q00H706P;[04] VERIFIED CORRECTIVE ACTIONS STEP 1-8 AND CORRECTIVE ACTION 3.
CORROSION ON AFT CARGO BAY BRACKET AT BS 947+1 LBL 2.<[01] THE STRUCTURAL ITEM DOES NOT HAVE ALLOWABLE DAMAGE ENTRIES .THEREFORE HAS TO BE REPAIRED BY REPLACEMENT PER REF SRM 51-10-02-0G-0;[02] REMOVED BRACKET LOCATED BETWEEN BS 947 - RBL3; LBL3 IAW SRM 51-40-02.<BR>BRACKET FORMED FROM MATERIAL 7075T0# 0.063' LOT: 1477375-1 IAW SRM 51-30-01 AND DWG#147A9100 REV: D. FORMED BRACKET IT WILL BE SENT TO O.S.S FOR HEAT TREATMENT AT T62.;[03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2.;[04] RECEIVED BRACKET HFAB53-BR-011 FROM OSS PO NBR 903477<BR><BR>LOCATED AND DRILLED NEW BRACKET PER REF SRM 51-40-05<BR><BR>OK TO APPLY CHEMICAL CONVERSION COATING AND PRIME ON BRACKET;[05] VERIFIED CORRECTIVE ACTION STEP 4. VERIFIED OK TO CHEMICAL CONVERT AND PRIME.;[06] APPLIED CHEMICAL CONVERSION COATING AND PRIMER AT DISCREPANCY AREA PER REF SRM 51-20-01 AND SOPM 20-41-02 <BR><BR>OK TO INSTALL NEW BRACKET.;[07] VERIFIED CORRECTIVE ACTION STEP 6. VERIFIED OK TO INSTALL NEW BRACKET.;[08] INSTALLED BRACKET AT BS 947+1 LBL 2. PER REF SRM 51-40-02 AND DWG NBR 147A7500;[09] VERIFIED CORRECTION ACTION STEP 8.;[10] VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
CORROSION ON STRINGER CLIP AT BS 420 STR 2R<[01] REMOVED CLIP AT BS 420 STR 2R; SRM 51-40-02;[02] LOCATED AND DRILLED NEW STRINGER CLIP AT BS 420 STR 2R IAW B 737-700 SRM 51-40-05-0G-0 DWG 143A112.- OK TO INSTALL.;[03] THIS PART DOES NOT HAVE ENTRY ON THE LOWER ALLOWABLE DAMAGE LIMITS THERE FOR IT HAS TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02 STEP 9;[04] VERIFIED CORRECTIVE ACTION 1-3 OK TO INSTALL;[05] INSTALLED STRINGER CLIP AT BS 420 STR 2R PER REF SRM 51-40-02 AND DWG 143A112;[06] VERIFIED CORRECTIVE ACTION 5 AND MEASUREMENT TABLE.
CORROSION ON AFT CARGO BAY WATER TANK SUPPORT AT BS 947+2 LBL 10.<[01] REMOVED CORROSION AT DISCREPANCY AREA L=1 W=.5 PER REF SRM 51-10-02-0G-0;[02] VERIFIED CORRECTIVE ACTION 1.;[08] REMOVED ADDITIONAL DAMAGE AT DISCREPANCY AREA . TOTAL AREA REMOVED L=2.2' W=1.9' AFTER FURTHER INVESTIGATION NO ALLOWABLE DAMAGE FOUND ON SRM. PART TO BE REPAIR BY REPLACEMENT PER SRM 51-10-02 PARAGRAPH 9.;[09] VERIFIED CORRECTIVE ACTION 8.;[10] RECEIVED NEW INTERCOSTAL P/N 147A7410-19;LOCATED AND DRILLED IAW SRM 51-40-05;AND DWG#147A7410 REV E;OK TO INSTALL.;[12] INSTALLED NEW INTERCOSTAL ON AFT CARGO WATER TANK SUPPORT AT BS 947 TO BS 967;IAW SRM 51-40-02 AND DWG#147A7410 REV E.ALL MAINTENANCE ACTION ARE COMPLETED REQUIRE FINAL BUY OFF.
CRACK ON FWD CARGO BAY GUSSET AT BS 500D STRINGER 19R.<[01] DAMAGE FOUND AT FWD CARGO BAY GUSSET BS 500D STR-19R FOUND TO BE OUT OF LIMIT DUE TO NO LIMTE ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR.9C;[02] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT FIELD;[03] REMOVED FWD CARGO BAY GUSSET AT BS 500D STRINGER 19R IAW SRM 51-40-02;[04] LOCATED AND DRILLED FWD CARGO BAY NEW GUSSET AT BS 500D STRINGER 19R P/N143A9481-5 IAW SRM 51-40-05 AND DWG 143A9481 REV A ;OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION STEP 4. VERIFIED OK TO INSTALL.;[06] INSTALLED ON FWD CARGO BAY NEW GUSSET AT BS 500D STRINGER 19R P/N143A9481-5 IAW SRM 51-40-02AND DWG 143A7902 REV:;[07] VERIFIED CORRECTIVE ACTION STEP 6.;[08] VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
CRACK ON FWD CARGO BAY GUSSET AT BS 500D STRINGER 19L.<[01] DAMAGE FOUND AT FWD CARGO BAY GUSSET BS 500D STR-19L FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR.9C.;[02] VERIFIED CORRECTIVE ACTION #1 AND MEASUREMENT FIELD;[03] REMOVED FWD CARGO BAY GUSSET AT BS 500D STRINGER 19L IAW SRM 51-40-02;[04] LOCATED AND DRILLED FWD CARGO BAY NEW GUSSET AT BS 500D STRINGER 19L P/N143A9481-6 IAW SRM 51-40-05 AND DWG 143A9481 REV A ;OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION STEP 4. VERIFIED OK TO INSTALL.;[06] INSTALLED ON FWD CARGO BAY NEW GUSSET AT BS 500D STRINGER 19L P/N143A9481-6 IAW SRM 51-40-02AND DWG 143A7902 REV:;[07] VERIFIED CORRECTIVE ACTION STEP 6.;[08] VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
CORROSION ON PASSENGER CABIN FRAME ATTACH ANGLE AT BS 277 STRINGER 1.(MARKED)<[01] EVALUATED DAMAGE ON PASSENGER CABIN FRAME ATTACH ANGLE AT BS277 S-1 FOUND TO BE OUT OF LIMITS DUE NO LIMITS IN SRM PART WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] REMOVED ATTACH ANGLE ON PASSENGER CABIN FRAME BS277 S-1 IAW SRM 51-40-02-0G-0;[03] FABRICATED ANGLE FROM MATERIAL BAC1490-64#7075T62 LOT# 1516715-1; LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-05-0G-0; DWG 141A1251; APPLIED CHEMICAL CONVERSION COATING IAW SRM 51-20-01-0G-0; OK TO PRIMER;[04] VERIFIED CORRECTIVE ACTION 3.;[05] APPLIED PRIMER ON NEW ANGLE IAW SOPM 20-41-02; OK TOINSTALL;[06] VERIFIED CORRECTIVE ACTION 5; OK TO INSTALL AND THE MEASURUEMENT TABLE;[07] INSTALLED ATTACH ANGLE ON PASSENGER CABIN FRAME BS277 S-1 IAW SRM 51-40-02-0G-0 DWG 141A0741; CARD IS COMPLETED;[08] VERIFIED CORRECTIVE ACTION 7.;[09] VERIFIED CORRECTIVE ACTION 1 AND THE MEASUREMENT TABLE.
CORROSION ON PASSENGER CABIN DOOR WEB ATTACH ANGLE AT BS 348+10 STRINGER 13L.(MARKED)<[01] REMOVED CORROSION ON PASSENGER CABIN DOOR WEB ATTACH ANGLE AT BS 348+10 S-13L REWORKED AREA: L=1.7' W=.800' IAW SRM 51-10-02-0G-0;[02] VERIFIED CORRECTIVE ACTION 1.;[03] EVALUATED DAMAGE ON PASSENGER CABIN DOOR WEB ATTACH ANGLE AT BS 348+10 S-13L AFTER FURTHER EVALUATION FOUND TO BE OUT OF LIMITS; DUE NOT LIMITS IN SRM PART WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0;[04] REMOVED ON PASSENGER CABIN DOOR WEB ATTACH ANGLE AT BS 348+10 S-13L IAW SRM 51-40-02-0G-0;[05] FORMED ANGLE CLIP FROM MATERIAL 7075-T0 0.050' LOT# 1439128-1; IAW DWG 141A8163; REQ SEND TO OSS FOR HT TR T0 TO T62;[06] VERIFIED CORRECTIVE ACTIONS 3 AND 5.;[07] CORRECTED ACTION STEP 5: LOT# 1474582-1;[08] RECIVED ANGLE CLIP FORMED FROM OSS HT TR T62; LOT# 1516735-1 CUSTOMER RO NO 902793-SWA; LOCATED AND DRILLED FORMED PART IAW SRM 51-40-05-0G-0 DWG 141A8163; APPLIED CHEMICAL CONVERSION COATING IAW SRM 51-20-01-0G-0 OK TO PRIMER;[09] VERIFIED CORRECTIVE ACTION 8- OK TO PRIME.;[10] APPLIED PRIMER ON ANGLE CLIP IAW SOPM 20-41-02; OK TO INSTALL;[11] VERIFIED CORRECTIVE ACTION 10- OK TO INSTALL.;[12] INSTALLED ON PASSENGER CABIN DOOR WEB ATTACH ANGLE AT BS 348+10 S-13L IAW SRM 51-40-02-0G-0 DWG 141A8190; CARD IS COMPLETED;[13] VERIFIED MEASUREMENT TABLE.;[14] VERIFIED CORRECTIVE ACTION 12.
CORROSION ON PASSENGER CABIN DOOR WEB ATTACH ANGLE AT BS 295 STRINGER 12L.(MARKED)<[01] EVALUATED DAMAGE ON PASSENGER CABIN DOOR WEB ATTACH ANGLE AT BS 295 S-12L AFTER FURTHER EVALUATION FOUND TO BE OUT OF LIMITS; DUE NOT LIMITS IN SRM PART WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] REMOVED PASSENGER CABIN DOOR WEB ATTACH ANGLE AT BS 295 S-12L IAW SRM 51-40-02-0G-0;[03] VERIFIED STEP 2 AND VERIFIED MEASUREMENT FIELD;[04] REFER TO FAULT TTG8Q00H7MSH WHERE EA 23-153-00290 WAS ADDED AS A SUBTASK;[05] LOCATED AND DRILLED NEW DOOR STOP INTERCOSTAL CLIP IAW SRM 51-40-05-0G-0 AND DRAWING#141A8184 REFER TO EA# 23-153-00290-WIP1 STEP 3.<BR>OK TO TREAT AND PRIME.;[06] VERIFIED CORRECTIVE ACTIONS STEPS 4;5; OK TO TREAT AND PRIME GIVEN.;[07] APPLIED CHEMICAL CONVERSION COATING AND PRIME ON NEW DOOR STOP INTERCOSTAL CLIP IAW AMM 51-21-41-370-802 AND AMM 51-21-72-370-804.;[08] OK TO INSTALL NEW PART;[09] VERIFIED CORRECTIVE ACTION STEPS 7 AND 8. VERIFIED OK TO INSTALL.;[10] INSTALLED NEW PASSENGER CABIN DOOR WEB ATTACH ANGLE AT BS 295 S-12L; IAW SRM 51-40-02-0G-0 DWG 141A8180; CARD IS COMPLETED;[11] VERIFIED CORRECTIVE ACTION STEP 10.;[12] REPLACEMENT OF WEB ATTACH ANGLE ACCOMPLISHED IAW 23-153-00290 (N565WN - ATS(PAE) - REPAIR - FWD DOORSTOP INTERCOSTAL CLIPS AT BS 294.5; STR 9L & STR 12L ? MATERIAL SUBSTITUTION);[13] VERIFIED CORRECTIVE ACTION ITEMS AND MEASUREMENT FIELDS; CARD COMPLETE.
CORROSION ON CABIN SEAT TRACK RBL45.4 BS 727B+6; BS 727C+17; BS 727D+10; BS 727E+7.5; BS 747+18; BS 787+10; BS 807+10; BS 847+13; BS 867+5.<[01] CORROSION ON CABIN SEAT TRACK RBL45.4 BS 727B+6; BS 727C+17; BS 727D+10; BS 727E+7.5; BS 747+18; BS 787+10; BS 807+10; BS 847+13; BS 867+5 WILL BE ACCOMPLISHED ON CUSTOMER CARD TTG8Q00H7SLD.;[02] VERIFIED CORRECTIVE ACTION 1
CORROSION ON PASSENGER CABIN DOOR WEB ATTACH ANGLE AT BS 295 STRINGER 9L.(MARKED)<[01] EVALUATED DAMAGE ON PASSENGER CABIN DOOR WEB ATTACH ANGLE AT BS 295 S-9L AFTER FURTHER EVALUATION FOUND TO BE OUT OF LIMITS; DUE NOT LIMITS IN SRM PART WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] REMOVED ATTACH ANGLE PASSENGER CABIN DOOR WEB AT BS 295 S-9L IAW SRM 51-40-02-0G-0;[03] VERIFIED STEP 2 AND VERIFIED MEASUREMENT FIELD;[04] ROUTED BAC1506-3633#7075T6511 LOT# 738969 TO MACHINE SHOP FOR MACHINING OF THE 141A8184-1 CLIP AND 141A8184-22 CLIP.;[05] REFER TO EA# 23-153-00290-WIP1 FOR PART FABRICATION REQUIREMENTS.;[06] LOCATED AND DRILLED NEW DOOR STOP INTERCOSTAL CLIP IAW SRM 51-40-05-0G-0 AND DRAWING#141A8184 REFER TO EA# 23-153-00290-WIP1 STEP 4.<BR>OK TO TREAT AND PRIME.;[12] VERIFIED CORRECTIVE ACTION STEP 11.;[13] REPLACEMENT OF WEB ATTACH ANGLES ACCOMPLISHED IAW 23-153-00290 (N565WN - ATS(PAE) - REPAIR - FWD DOORSTOP INTERCOSTAL CLIPS AT BS 294.5; STR 9L & STR 12L ? MATERIAL SUBSTITUTION);
CORR0SION AFT CARGO FLOOR SUB THRESHOLD WEB BS807-BS847 RBL 25<[01] VERIFIED APPLICABILITY IAW SRM 53-60-15-0L-1 FOR IDENTIFICATION AND SRM 53-60-15-1A-1 FOR ALLOWABLE DAMAGE.<BR>REMOVED CORROSION ON AFT CARGO BAY DOOR CUT-OUT SUB-THRESHOLD WEB<BR>FROM BS 807 TO BS847 RBL 25;[02] EVALUATED BLENDED AREA L=2.400' W=1.200' ORIGINAL THICKNESS 0.045' REMAINING 0.029' LOSS 0.016'; MAX MAT REMOVED ALLOWED 0.004'; WAS FOUND OUT LIMITS IAW SRM 53-60-15-1A-1 TABLE 101 PARA 4G (2) FIG 103 DETAIL D.<BR>TOOL ID: ATS1672 S/N: 65092939 DUE:03/2023;[03] INSPECTED ACTION 1;2;[04] RECEIVED SUB THRESHOLD WEB WITH P/N 146A8123-25 LOT: 1515672-1. <BR>LOCATED AND DRILLED WEN LOCATED BTW. BS794.37 - 847 RBL 21 - RBL27 WL 152 IAW SRM 51-40-05 DWG# 146A8340 REV: B .<BR> OK TO INSTALL NUT PLATES.;[05] VERIFIED CORRECTIVE ACTION 4.;[06] INSTALLED NUT PLATES ON AFT SUB-THRESHOLD WEB IAW SRM 51-40-02 & DWG# 146A8340. ALL MAINTENANCE ACTION ARE COMPLETE REQUEST FINAL BUY OFF.;[07] UPDATED PART NUMBER;[08] PARTS INFO UPDATE;[09] VERIFIED CORRECTIVE ACTION 8 AND MEASUREMENT TABLE.
CORR0SION AFT CARGO TRACK TIE BS727D RBL2<[01] VERIFIED APPLICABILITY PER REF SRM 53-60-53-0I-2 AND SRM 53-00-53-1A-2<BR><BR>REMOVED DAMAGE AT DISCREPANCY AREA PER REF SRM 53-00-53-1A-2 L=2.5<BR>W=.900;[02] VERIFIED CORRECTIVE ACTION 1.;[03] REQUIRE NDI TO VERIFY FOR CRACK FREE CONDITION AND REMAINING;TICKNESS VERIFICATION.;[04] ACCOMPLISHED HFEC SURFACE CRACK IAW 737 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23.<BR>NO CRACKS NOTED.<BR><BR>ACCOMPLISHED UT THICKNESS INSPECTION IAW 737 NDTM PART 4 CHAPTER 51-00-00 PROCEDURE 2.<BR>REMAINING MATERIAL THICKNESS 0.053' ADJACENT 0.063'<BR><BR>EQUIPMENT USED: <BR>-NORTEC 600 ID: ATS1465 CAL DUE: 09/2023<BR>-EPOCH 650 ID: ATS2031 CAL DUE: 03/2023;[12] LOCATED AND DRILLED AFT CARGO BAY FLOOR SUPPORT AT BS727D RBL2 PER SRM 53-00-53-2R-2 REPAIR 2 FIG. 203.;[13] LOCATED AND DRILLED REINFORCING CHANNEL MADE FROM 53100004-001; LOT#1513707-1 AT AFT CARGO BAY FLOOR SUPPORT BS727D RBL2 PER SRM 53-00-53-2R-2 REPAIR 2 FIG. 203.OK TO TREAT AND PRIME THE CUT OUT;[17] INSTALLED REPAIR ANGLE AT AFT CARGO BEY FLOOR SUPPORT BS727D RBL2 PER SRM 53-00-53-2R-2 REPAIR 2 FIG. 203;
SLAT #7 LOWER L/E SKIN AT ACTUATOR SUPPORT RIB ATTACH POINT HAS PROTRUDING FASTENER HEADS.<[01] REMOVED PANEL 624DB AT SLAT #7 IAW SRM 51-40-02.;[02] REMOVED AND REPLACED FASTENERS AT SLAT #7 LOWER L/E SKIN AT ACTUATOR SUPPORT RIB ATTACH POINT IAW SRM 57-42-01-2R-8.<BR>OK TO CLOSE PANEL 624DB.;[03] VERIFIED CORRECTIVE ACTION 2. PRIOR TO CLOSING PANEL 624DB SEE STEP 1.;[04] VERIFIED MEASUREMENT TABLE.;[05] STEP 1 COMPLETE.;[06] VERIFIED STEP 2.;[07] REINSTALLED PANEL 624DB AT SLAT #7 IAW SRM 51-40-02<BR>SCREW GUN ID PER2267 S/N 1703476 CAL DUE 02/2023;[08] VERIFIED CORRECTIVE ACTION 7.
CRACK ON FWD CARGO BAY END OF STRINGER AT BS 540 STRINGER 26R.<[01] CUT AND REMOVED THE DAMAGED PART OF STRINGER 26R BETWEEN BS 500D+10 AND BS 540 IAW SRM 53-00-03-2R-1 REPAIR 1;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REQUEST NDI TO DO A HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION OF THE REPAIR AREA TO MAKE SURE THAT ALL OF THE DAMAGE IS REMOVED. REFER TO 737 NDT PART 6; 51-00-00; FIGURE 4.;[04] NDT HFEC INSPECTED THE REPAIR AREA IAW 737 NDTM PART 6 51-00-00 PROC 23. <BR>NO CRACKS NOTED <BR>EQUIP USED: NORTEC 500D IS000681 DUE 02/23;[EQUIP USED: NORTEC 500D ID: IS000681 DUE 02/23 MINIMITE ID: MM12030Z012384 DUE 07/23;[06] RECEIVED STR 26R -7 REPLACEMENT STRINGER SECTION FORMED AT MACHINE SHOP MATERIAL USED 7075T0 ; 0.045' CLAD LOT # 1381192-1 ; HEAT TREATED TO T62 AND DYE PENETRANT INSPECTED ON CUSTOMER R/O # 901827-SWA . <BR>AND RECEIVED -1 HAT SECTION SPLICE FORMED AT MACHINE SHOP FROM 7075T0 # 0.050' CLAD LOT # 1474582-1 HEAT TREATED TO T6 AND DYE PENETRANT INSPECTED ON CUSTOMER R/O # 901825-SWA ; FABRICATED LOCATED ; DRILLED AND APPLIED A CHEMICAL CONVERSION COATING TO ALL REPAIR PARTS IAW SRM 53-00-03-2R-1 REPAIR 1 APPLIED PRIMER TO ALL REPAIR PARTS AND REWORKED AREAS IAW SRM 53-00-03-2R-1 REPAIR 1 ; INSTALLED ALL REPAIR PARTS AT FCB STRINGER 26R BETWEEN BS 500D AND 540 ; APPLIED A FILLET SEAL AND CIC AT THE REPAIR AREA IAW SRM 53-00-03-2R-1 REPAIR 1
CRACK ON FWD CARGO BAY END OF STRINGER AT BS 540 STRINGER 25R.<[01] CUT AND REMOVED THE DAMAGED PART OF STRINGER 25R BETWEEN BS 500D+10 AND BS 540 IAW SRM 53-00-03-2R-1 REPAIR 1;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REPAIRED FWD CARGO BAY STRINGER AT BS 500D - 540 IAW SRM 53-00-03-2R-1 REPAIR 1 AND ER: 23-153-00233-WIP1;[04] VERIFIED CORRECTIVE ACTION 3.;[05] 'THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 (REPAIR 1) AND EA 23-153-00233'.;[06] VERIFIED CORRECTIVE ACTION ITEMS AND MEASUREMENT FIELDS; EXCEPT FOR ITEM 4 EXISTING REPAIR (BLANK);[07] UPDATED MEASUREMENTS;[08] UPDATED MEASUREMENT TABLE ; ALL MAINTENANCE ITEMS COMPLETE;[09] VERIFIED CORRECTIVE ACTIONS 7 AND 8
CRACK ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT ATTACH ANGLE AT LBL 25 BS 400.<[01] REMOVED FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT ATTACH ANGLE AT LBL 25 BS 400 PER SRM 51-40-02-0G-0.;[02] CRACK ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT ATTACH ANGLE AT LBL 25 BS 400 WITH NEXT DIMENSIONS L=0.130 TOOL USED ID: ATS1317; SN: UNKNOWN; DATE:08/2022; DUE:08/2023 FOUND TO BE OUT LIMITS DUE TO NO ALLOWABLE DAMAGE IN SRM; IT WILL BE REPAIRABLE BY REPLACEMENT I.A.W SRM 51-10-02-0G PAR 9C.;[03] LOCATED AND DRILLED NEW ATTACH ANGLE ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 25 BS 400 I.A.W SRM 51-40-05-0G-0 AND DWG 143A7505.AND OK TO INSTALL.;[04] VERIFIED MEASUREMENTS<BR>VERIFIED CORRECTIVE ACTION #2; 3;[05] INSTALLED NEW ATTACH ANGLE ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 25 BS 400 I.A.W SRM 51-40-02-0G-0 AND DWG 143A7505.;[06] VERIFIED CORRECTIVE ACTION #5
LT HORIZ FORWARD UPPER SLIDE SEAL CRACKED.<[01] REMOVED AND REPLACED LT HORIZ FORWARD UPPER SLIDE SEAL IAW AMM 53-31-31-000-802 AND AMM 53-31-31-400-802.;[02] VERIFIED CORRECTIVE ACTION 1.
SLAT #5 HAS DISBONDED FILLER MATERIAL AT INNER T/E O/B CORNER.<[01] #5 SLAT WAS REPLACED ON FAULT TTG8Q00H6ZBY;[02] VERIFIED. TASK CARD COMPLETE.
CORROSION ON FWD CARGO BAY AFT DOOR SHIELD AT RBL 22 BS 480+16; BS 480+18; BS 500+2; BS 500+6; BS 500+10; BS 500+14; BS 500+19.<[01] THIS PART DOES NOT HAVE ALLOWABLE DAMAGE LIMITS. IT HAS TO BE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G. STEP 9.;[02] VERIFIED CORRECTIVE ACTION 1.;[03] REPLACED ;LOCATED AND DRILLED NEW FWD CARGO BAY AFT DOOR SHIELD PER REF SRM 51-40-05 AND DWG NBR 143A8126.;[04] VERIFIED CORRECTIVE ACTION STEP 3. VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 22 BS 500A+14; BS 500A+18; BS 500B+6; BS 500B+14; BS 500C+2; BS 500C+6; BS 500C+12.<[01] VERIFIED APPLICABILITY SRM 53-60-53-01-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE.<BR><BR>REMOVED CORROSION ON FWD CARGO BAY FLOOR TON SIDEWALL SUPPORT AT RBL 22 500A+14 IAW SRM 51-10-02.<BR> <BR>EVALUATED DAMAGE REMOVAL AT BLENDED AREA L=1.000'' W=0.700' ORIGINAL THICKNESS 0.040' REMAINING 0.022' LOSS 0.018'; MAX MAT REMOVE ALLOWABLE 0.004'; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARA 4A (2) FIG 103 DETAIL D.<BR>TOOL ID: ATS1225 S/N: UNKNOWN DUE:08/2023<BR><BR>STEPS 1-7 PARTIAL COMPLETED;[02] VERIFIED STEPS 1-7 AND CORRECTIVE ACTION 1.;[03] FABRICATED; LOCATED AND DRILLED FLOOR TO SIDEWALL SUPPORT FROM BS 500A TO BS 500D AT RBL 22; USING MATERIAL BAC1496-444#7075T62 LOT 1501239-1 IAW SRM 51-40-05-0G-0 AND DWG 143A7501.<BR>OK TO CHEMICAL CONVERSION COATING AND PRIMER.;[04] VERIFIED CORRECTIVE ACTION 3 AND STEPS 1-7.;[05] VERIFIED MEASURUEENT TABLE.;[06] APPLIED CHEMICAL CONVERSION AND COATING PRIMER ON SIDEWALL SUPPORT IAW SRM 51-20-01 AND SOPM 20-41-02;[07] VERIFIED CORRECTIVE ACTION 6.
CORROSION ON FWD CARGO BAY THRESHOLD AT RBL 28 BS 440+10; BS 440+13; BS 440+17; BS 440+18; BS 440+19; BS 460; BS 460+2; BS 460+4.<[01] IDENTIFICATION SRM 53-30-15-01-1 AND ALLOWABLE DAMAGE SRM 53-30-15-1A-1 ARE APPLICABLE. EVALUATED CORROSION ON FWD CARGO BAY THRESHOLD AT RBL 28 BS 440+10 L=1.4' W=.5' D=.011'. FOUND TO BE OUT OF LIMITS. ORIGINAL THICKNESS .045' REMAINING THICKNESS .034' PER SRM 53-30-15-1A-1 STEPS 4.G.(2) FIGURE 103 DETAIL D. DEPTH GAUGE USED ID: ATS400 SN: UNKNOWN DUE: 09/2023.;[02] VERIFIED CORRECTIVE ACTION 1 AND STEPS 1-7.;[03] THIS JOB CARD WAS BE ACCOMPLISHED ON CUSTOMER CARD [TTG8Q00H707T].;[04] VERIFIED CORRECTIVE ACTION #3 AND MEASUREMENT FIELD;[05] NEW PART WILL BE INSTALLED WITH CUSTOMER CARD # TTG8Q004B87Y;[06] VERIFIED CORRECTIVE ACTION #5
CORROSION ON FWD CARGO BAY THRESHOLD AT RBL 28 BS 460+9; BS 460+13; BS 460+16; BS 460+18; BS 480+1.<[01] IDENTIFICAION SRM 53-30-15-01-1 AND ALLOWABLE DAMAGE SRM 53-30-15-1A-1 ARE APPLICABLE.;[02] EVALUATED CORROSION ON FWD CARGO BAY THRESHOLD AT RBL 28 BS 460+16 L=1.2' W=1' D=.012'. FOUND TO BE OUT OF LIMITS. ORIGINAL THICKNESS .045' REMAINING THICKNESS .033' PER SRM 53-30-15-1A-1 STEPS 4.G.(2) FIGURE 103 DETAIL D. DEPTH GAUGE USED ID: ATS400 SN: UNKNOWN DUE: 09/2023.;[03] VERIFIED STEPS 1-5 AND CORRECTIVE ACTIONS 1AND 2.;[04] LOCATED AND DRILLED NEW FWD CARGO BAY THRESHOLD AT RBL 28 BS 440-BS 493 P/N 143A8122-10 I.A.W SRM 51-40-05-0G-0 AND DWG 143A8122. THIS JOB CARD WILL BE ACCOMPLISHED ON CUSTOMER CARD [TTG8Q004B87Y] FOR THE APPLY ENAMEL; CORROSION INHIBITING COMPOUND AND INSTALLATION.;[05] VERIFIED CORRECTIVE ACTION #4 AND MEASUREMENT FIELD;[06] CARD COMPLETE
CORR0SION FLOOR TO SIDEWALL SUPPORT BS727+5; BS727A+10; BS727B+2-BS727C+14; BS727D+2; BS727D+8-BS767 RBL22<[01] PARTIAL STEPS #1- 7.;[02] VERIFIED APPLICABILITY SRM 53-60-53-0I-2 IDENTIFICATION 2 AND SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2.;[03] CORRECTED STEP# 5 WL156.;[04] VERIFIED STEPS 1-7 AND CORRECTIVE ACTION 2.;[05] RECEIVED EXTRUSION BAC1496-377 LOT. 1515191-1.<BR>LOCATED AND DRILLED BTW. BS 727 - BS 767 RBL 23 WL 156 IAW SRM 51-40-05 AND DWG# 146A7500; DWG# 146A7502 REV: A.<BR>OK TO APPLY TREAT AND PRIME.;[06] VERIFIED CORRECTIVE ACTION STEP 5.VERIFIED OK TO TREAT AND PRIME.;[07] APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON NEW FLOOR TO SIDEWALL SUPPORT AND INSTALLED NUT PLATES IAW SRM 51-20-01 AND SOPM 20-41-02. AND SRM 51-40-02 AND DWG# 146A7502 REV:A;[08] VERIFIED CORRECTIVE ACTION STEP 7. VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
CORR0SION FLOOR TO SIDEWALL SUPPORT BS727+15-BS727A+2; BS727A+10-BS727B; BS727C+2-BS727C+10; BS727D+2-BS727D+8; BS727E+6-BS767+8 LBL22<[01] PARTIAL STEP 1TO 10;[02] VERIFIED APPLICABILITY OF SRM 53-00-53-1A-2 ALLOWABLE DAMAGE;[03] VERIFIED STEPS 1-10 AND CORRECTIVE ACTION 2.;[04] VERIFIED MEASUREMENT TABLE.;[05] FABRICATED;LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT AT LBL22;BS727 TO BS847;AND SPLICE SIDEPLATE BETWEEN BS727E-BS747;MATERIAL USED BAC1496-377#7075T62;LOT#1508577-1;IAW SRM 53-00-53-2R-5 REPAIR 5 FIG 202;SRM 51-40-05 AND DGW#146A7502 REV.A.OK TO TREAT AND PRIME.;[06] VERIFIED CORRECTIVE ACTION STEP 5. VERIFIED OK TO TREAT AND PRIME.;[07] APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON FLOOR TO SIDEWALL AT ACB LBL22;BS727 TO BS847.- IAW 737-700; AMM 51-21-72-370-804; AMM 51-21-41-370-802. OK TO INSTALL ZEE CHANNEL SIDEPLATES AND SPLICE SIDEPLATE.;[08] VERIFIED CORRECTIVE ACTION 7. OK TO ASSEMBLE L/H FLOOR TO SIDEWALL SUPPORT;[09] INSTALLED NUT PLATES ON FLOOR TO SIDEWALL SUPPORT BTW BS 727 - BS 847 LBL22 IAW SRM 51-40-02 & DWG# 146A7502 REV: A.<BR>INSTALLED SPLICE SIDE PLATE LOCATED BTW. BS 727E - 747 IAW SRM 53-00-53-2R-6 REPAIR 6 TABLE 201 ITEM [2].;[10] VERIFIED CORRECTIVE ACTION 9.
CORR0SION AFT CARGO TRACK TIE BS927+17 RBL 14<[01] VERIFIED APLICABILITY SRM 53-70-53-01-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE<BR><BR>REMOVED CORROSION ON AFT CARGO TRACK TIE BS927+17 RBL 14<BR>DIMENSIONS L=0.700' W=0.800' MAX.MAT.LOSS 0.021';<BR>ORIGINAL THICKNESS IS .140' REMAINING THICKNESS 0.119'<BR>MAX.MAT.REMOVED ALLOWABLE 0.040'<BR> FOUND TO BE WITHIN LIMITS PER SRM 53-00-53-1A-2.<BR><BR>USED TOOL ID: ATS1738 DATE DUE: 10/2023 S/N UNKNOWN<BR>OK CHEMICAL CONVERSION AND PRIMER;[02] VERIFIED CORRECTIVE ACTION ITEM; OK FOR CHEMICAL CONVERSION AND PRIMER.;[03] APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON AFT CARGO TRACK TIE BS927+17 RBL 14 - IAW 737-700; AMM 51-21-72-370-804; AMM 51-21-41-370-80;[04] VERIFIED CORRECTIVE ACTION 3 AND MEASUREMENT TABLE.
CORR0SION AFT CARGO FLOOR TO SIDEWALL SUPPORT BS887+11 RBL23<[01] SRM 53-60-53-0I-2 IDENTIFICATION AND SRM 53-00-53-1A-2 ALLOWABLE DAMAGE ARE APPLICABLE.;[02] REMOVED CORROSION ON AFT CARGO FLOOR TO SIDEWALL SUPPORT BS887+11 RBL23; MEASURE: L=0.070'; W=0.060'; D=0.005'; ORIGINAL TICKNESS IS 0.040'; REMAINING TICKNESS IS 0.035'; FOUND AREA OUT OF LIMITS; IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2 PARAG.4A (2) DETAIL D FIG.103<BR><BR>TOOL USED: ATS1672; DUE:03/2023.;[03] VERIFIED CORRECTIVE ACTION ITEM 1-2.;[04] RECEIVED EXTRUSION BAC1496-377 LOT. 1503760-1.<BR>LOCATED AND DRILLED BTW. BS 887 - BS 947 RBL 23 WL 156 IAW SRM 51-40-05 AND DWG# 147A7500; DWG# 147A7501 REV: A. <BR>OK TO APPLY TREAT AND PRIME.;[05] VERIFIED CORRECTIVE ACTION STEP 4.;[06] APPLIED CHEMICAL CONVERSION AND PRIMER ON NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-20-01 AND SOPM 20-41-02.<BR>OK TO INSTALL NUT PLATES.;[07] VERIFIED CORRECTIVE ACTION STEP 6. VERIIFIED OK TO INSTALL NUTPLATES.;[08] INSTALLED NUT PLATES ON AFT CARGO FLOOR TO SIDEWALL SUPPORT BTW. BS 887 - BS 947 IAW SRM 51-40-02 AND DWG# 147A7501 REV: A. <BR>ALL MAINTENANCE ACTION ARE COMPLETE REQUEST FINAL BUY OFF.;[09] VERIFIED CORRECTIVE ACTION STEP 8. VERIFIED MEASUREMENT TABLE AND TASK CARD COMPLETE.
CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 25 BS 480+6.<[01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS OF FCB FLOOR TO SIDEWALL SUPPORT LBL 25 WL 156 IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2.;[02] REMOVED CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 25 WL 156 BS 480+6 DIMENSIONS L=1' W= 0.750 DEPTH:0.011' IAW SRM 51-10-02 PARAGRAPH 15 EVALUATED REWORKED AREA ORIGINAL MATERIAL THICKNESS 0.040' REMAINING THICKNESS: 0.029' AND FOUND TO BE OUT LIMITS; ALLOWABLE DAMAGE IAW SRM 53-00-53-1A-2 TOOL USED ID ATS2739 S/N A22004232 DUE 04/2023;[03] ACCOMPLISHED WORK AT CUST SISTEM ID TTG8Q00H706B;[04] VERIFIED CORRECTIVE ACTIONS 1-3.;[05] VERIFIED MEASUREMENT TABLE.
CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 25 BS 480+13; BS 500+10; BS 500+14; BS 500+18; BS 500A+2; BS 500A+6; BS 500A+10; BS 500A+14; BS 500A+18.<[01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS OF FCB FLOOR TO SIDEWALL SUPPORT LBL 25 WL 156 IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2.;[02] FABRICATED LOCATED AND DRILLED REPLACEMENT FLOOR TO SIDEWALL SUPPORT USING BAC1496-444#7075T62 LOT:1501239-1 IAW SRM 51-40-05-0G-0; AND DWG 143A7501 REV: B. FABRICATED FLOOR TO SIDEWALL SUPPORT SPLICE REPAIR AT BETWEEN B/S 480 TO BS 500' USING BAC1496-444#7075T62 LOT:1501239-1 IAW SRM 53-00-53-2R-6 AND SRM 51-40-05.;[03] VERIFIED STEPS 1-9 COMPLETE.;[04] OK TO CHEMICAL CONVERSION AND PRIMER ON FABRICATED SIDEWALL SUPPORT AND PLICE;[05] VERIFIED STEP 4.;[06] APPLIED CHEMICAL CONVERSION COATING AND PRIMER<BR>ON FLOOR TO SIDEWALL SUPPORT AND SPLICE<BR>IAW SRM 51-20-01 AND SOPM 20-41-02 OK TO INSTALL SPLICE;[07] INSPECTED ACTION 6; OK TO INSTALL;[08] NEW PART WILL BE INSTALLED WITH CUSTOMER CARD # TTG8Q004B87Y;[09] VERIFIED CORRECTIVE ACTION #6 AND MEASUREMENT FIELD
CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 24 BS 400+10; BS 400+14.<[01] VERIFIED APPLICABILITY SRM 53-30-53-01-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE.<BR>REMOVED CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 24BS 400+10 ADN BS 400+14.<BR>FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARA 4A (2) FIG 103 DETAIL D.<BR>TOOL ID: ATS1225 S/N: UNKNOWN DUE:08/2023;[02] VERIFIED PARTIAL STEPS 1 AND 2 AND CORRECTIVE ACTION 1.;[03] FABRICATED; LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT AT RBL 24 BS 400 TO BS 420 WITH NEXT MATERIAL USED BAC1496-444#7075T62 LOT 1515896-1 I.A.W SRM 51-40-05-0G-0 AND DWG 143A7501 AND APPLIED CHEMICAL CONVERSION COATING I.A.W SRM 51-20-01;OK TO PRIME.;[04] VERIFIED CORRECTIVE ACTION 3. OK TO PRIME.;[05] APPLIED PRIMER ON NEW FLOOR TO SIDEWALL SUPPORT. PER SRM 20-41-02;[06] VERIFIED CORRECTIVE ACTION 5 AND MEASUREMENT TABLE.
CORROSION ON FWD CARGO BAY AFT R/H LOWER BULKHEAD SUPPORT AT BS 500D RBL 25.<[01] VERIFIED APPLICABILITY SRM 53-30-08-01-1 FOR IDENTIFICATION AND SRM 53-30-08-1A-1 FOR ALLOWABLE DAMAGE.<BR><BR>EVALUATED DAMAGE REMOVAL AT BLENDED AREA L=1'' W=0.800' ORIGINAL THICKNESS= 0.071'; REMAINING =0.052'; MATERIAL LOSS= 0.019'; MAX MAT REMOVE ALLOWABLE =0.015'; FOUND TO BE OUT OF LIMITS<BR> IAW SRM 53-30-08-1A-1 PARA 4A (2) FIG 103 DETAIL C.<BR>TOOL ID: ATS2826 S/N: UNKNOWN DUE:01/2024.;[02] VERIFIED CORRECTIVE ACTION 1.;[03] REPLACED WITH NEW PART 143A9485Y34 LOT 1488903-1 <BR>LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG 149A7502;[04] NEW PART WILL BE INSTALLED WITH CUSTOMER CARD # TTG8Q004B87Y;[05] VERIFIED CORRECTIVE ACTION #3; 4 AND MEASUREMENT FIELD
CORR0SION AFT CARGO FWD SHEILD BS767-BS787+2 RBL22<[01] DAMANGE FOUND ON ACB FWD SHIELD BS767-BS787+2 RBL22 WL164 P/N 146A8127-12 FOUND TO BE OUT OF LIMIT IAW SRM PART WILL BE REPAIRED BY REMPLACEMENT IAW SRM 51-10-02-0G-0 PAR. 9C;[02] LOCATED AND DRILLED NEW FWD SHIELD PN#146A8127U12 FROM BS767-BS797 RBL 22 IAW SRM 51-40-02 AND IAW DWG#146A0081;[03] VERIFIED CORRECTIVE ACTION ITEM 1-2.;[04] ALL MAINTENANCE ACTION ARE COMPLETED WITH CARD#TTG8Q004CCW1.REQUIRE FINAL BUY OFF;[05] MEASUREMENT FIELD ITEM 17 INCORRECT; NOT .400'; SHOULD BE .000'.;[06] VERIFIED CORRECTIVE ACTION ITEMS AND MEASUREMENT FIELDS; CARD COMPLETE.
CORR0SION AFT CARGO TRACK TIE BS787; BS 787+3 LBL18<[01] PARTIAL STEP 1 AND 2;[02] VERIFIED CORRECTIVE ACTION ITEMS; OK FOR CHEMICAL CONVERSION AND PRIMER.;[03] APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON AFT CARGO TRACK TIE BS787; BS 787+3 LBL18.- IAW 737-700; AMM 51-21-72-370-804; AMM 51-21-41-370-80;[04] VERIFIED CORRECTIVE ACTION 3 AND MEASUREMENT TABLE.
RT HORIZ FORWARD LOWER SLIDE SEAL CRACKED<[01] REMOVED AND REPLACED RT HORIZ FORWARD LOWER SLIDE SEAL IAW AMM 53-31-31-000-803 AND AMM 53-31-31-400-803.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE
CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 25 BS 500C+2; BS 500C+14.<[01] COMPLETE STEP 1-2;[02] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS OF FCB FLOOR TO SIDEWALL SUPPORT LBL 25 WL 156 IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2.;[03] ACCOMPLISHED WORK AT CUST SISTEM ID TTG8Q00H706B;[04] VERIFIED STEPS 1 AND 2. AND CORRECTIVE ACTIONS 1-3. VERIFIED MEASUREMENT TABLE.
RIGHT WING COMPOSITE FIXED LEADING EDGE UPPER SURFACE IS DELAMINATED FROM OFSS 655 TO OFSS 683.<[01] IDENTIFIED R/H O/B UPPER FIXED LEADING EDGE MATERIAL ACCORDING TO SRM 57-41-01-0I-3; FIG. 4; TABLE 4; ITEM 1; AND FIG. 8; TABLE 8. <BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1; PARA'S 2.B AND 4.B.(5); AND FIG. 101. <BR><BR>AREAS TO BE REPAIRED ACCORDING TO SRM 51-70-05-2R-4; AS REQUIRED BY SRM 57-41-01-2R-1; PARA'S 2.F; 4.B.(1); AND TABLE 201.<BR><BR>STRIPPED UPPER SURFACE PAINTS/PRIMERS; REMOVED LOWER SURFACE BONDED ALUMINUM FOIL; REMOVED DELAMINATED PLIES AND CORE TO A REGULAR SHAPE THRU BOTH BOTH FACESHEETS; APPROX. 51' FROM O/B END; AND 8' FROM THE FWD EDGE; TAP TESTED AREAS (NO DISBONDS NOTED); REMOVED CONTAMINANTS FROM REPAIR AREA; ALL ACCORDING TO SRM 51-70-05-2R-4; PARA'S 4.A AND 4.B.; AND SRM 51-70-14-2R-3. PARA. 4.A.(2).(B).;[12] FABRICATED ALUMINUM FOIL REPAIR PLY FROM BMS 8-289 LOT#1507307-1; INSTALLED WITH BMS 5-128 LOT#JH2FAL7046; VACUUM BAGGED; LEAK CHECK GOOD; CURED; UNBAGGED AND TRIMMED EXCESS MATERIAL IAW SRM 51-70-14-2R-3 PARA 4(3-5)(11)(A-L) AND BOEING DWG 116A5411 FL11.<BR>APPLIED ALUMINUM TAPE 3M Y425 LOT#1514681-1 ACROSS FWD EDGE IAW BOEING DWG 116A5411 FL 11.<BR>REFINISHED OUTER SURFACE IAW SRM 51-70-05-2R-4 PARA 4.M.<BR><BR>THERMOMETER ID:ATS2208 CAL DUE 10/2023<BR>VACUUM GAUGE ID:ATS2441 CAL DUE 08/2023<BR>MULTIMETER ID:ATS1658 CAL DUE 03/2023;[13] VERIFIED CORRECTIVE ACTION #12
#2 ENGINE PYLON INBOARD AFT FIRE WALL BRACKET HORIZONTAL FLANGE IS BROKEN<[01] REMOVED #2 ENGINE PYLON INBOARD AFT FIRE WALL BRACKET IAW SRM 51-40-02-0G-0 STEP 5.;[02] #2 ENGINE PYLON INSTALLED SERVICEABLE INBOARD AFT FIRE WALL BRACKET IAW SRM 51-40-02-0G-0 STEP 5.;[03] #2 ENGINE PYLON INSTALLED SERVICEABLE INBOARD AFT FIRE WALL BRACKET IAW SRM 51-40-02-0G-0 STEP 5.;[04] CORRECTIVE ACTION STEP 2 ENTERED IN ERROR; BRACKET INSTALLATION ACCOMPLISHED ON CORRECTIVE ACTION STEP 3;[05] VERIFIED CORRECTIVE ACTION 3.
PANEL 561BB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<[01] IDENTIFIED PART AND MATERIAL IAW SRM 57-51-01-0I-1 FIGURES 1+3; TABLE 3; ITEM [9].<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 PAR 4.B (5).<BR>A PERMANENT REPAIR WILL BE ACCOMPLISHED IAW SRM 51-70-04-2R-9 AS DIRECTED PER SRM 57-51-01-2R-1 PAR 4.B (2) AND TABLE 202.;06] CURED SLURRY; SANDED FLUSH; CLEANED REPAIR AREA; FABRICATED REPAIR PLIES FROM BMS9-3 STYLE 1581 LOT NUMBER 1513216-1; INSTALLED PLIES WITH BMS8-301 TYPE 1 LOT NUMBER JH2EAA8895; VACUUM BAGGED; VERIFIED A SATISFACTORY 5X5 USING VACUUM GAUGE ID: ATS2107 DUE: 04/2023; CURED PLIES UNDER A HEAT LAMP USING THERMOMETER ID: ATS2208 DUE: 10/2023; UNBAGGED PLIES AND LIGHTLY SANDED PLIES; WORK PERFORMED IAW SRM 51-70-04-2R-9 PARAGRAPH 4.F-M AND P.
CRACK IN LH HORIZ STAB LWR SKIN; STAB STA 193.9. INBD FASTENER ROW; 25' FROM L/E. .5' IN LENGTH. FOUND USING HFEC INSPECTION METHOD. MARKED.<[01] CUT AND REMOVED THE DAMAGED AREA OF THE LH HORIZ STAB LWR SKIN; STA 193.9. IAW SRM 55-10-01-2R-11 REPAIR 11;[02] VERIFIED CORRECTIVE ACTION 1;[03] REQUEST NDI TO HFEC INSPECT CUT EDGES FOR CRACK FREE CONDITION;[04] ACCOMPLISHED HFEC SURFACE SCAN OF CUT EDGES IAW 737 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23.<BR>NO CRACKS NOTED.<BR><BR>EQUIPMENT USED: NORTEC 600 ID: ATS1465 CAL DUE: 09/2023;[05] FABRICATED -1 DOUBLER FROM 2024T3 # 0.080' CLAD LOT# 1497191-1 FOR LH HORIZ LWR SKIN; STAB STA 193.9 IAW SRM 55-10-01-2R-11 REPAIR 11 ; OK TO TREAT AND PRIME;[06] REJECTION - MULTIPLE SITE DAMAGE REPAIR REQUIRES HFEC NDT INSPECTION OF OUTER ROW HOLES PER SRM 55-10-01-2R-11 REPAIR 11 STEP 4. F. (5). DO NOT PROCEED WITH FABRICATION.;[07] REQUEST NDI TO HFEC INSPECT OF OUTER ROW HOLES PER SRM 55-10-01-2R-11 REPAIR 11 STEP 4. F. (5);[09] VERIFIED CORRECTIVE ACTION ITEM 5 AFTER HOLES NDT HFEC COMPLETED; OK TO TREAT AND PRIME FABRICATED DOUBLER.;[10] APPLIED A CHEMICAL CONVERSION COATING AND PRIMER TO THE -1 DOUBLER AND ALL REWORKED AREAS AT LH HORIZ STAB LWR SKIN; STAB STA 193.9 PER SRM 55-10-01-2R-11 REPAIR 11 ; OK TO INSTALL;[11] VERIFIED CORRECTIVE ACTION 10.;[12] INSTALLED REPAIR PART IAW SRM 55-10-01-2R-11 REPAIR 11
CRACK IN RH HORIZ STAB LWR SKIN; STAB STA 193.9 INBD FASTENER ROW; 17' FROM L/E; 1.2' IN LENGTH. FOUND USING HFEC INSPECTION METHOD. MARKED.<[01] SRM 55-10-01-0I-4 IDENTIFICATION 4 AND SRM 55-10-01-2R-11 REPAIR 11 ARE APPLICABLE TO THIS A/C;[02] CUT AND REMOVED THE DAMAGED AREA OF THE SKIN BY 2.6'LX1.0'W IAW SRM 55-10-01-2R-11 REPAIR 11;[03] VERIFIED CORRECTIVE ACTION 1 AND 2;[04] REQUESTED HFEC INSPECTION OF THE CUT EDGE TO MAKE SURE THAT ALL THE DAMAGE IS REMOVED IAW SRM 55-10-01-2R-11 REPAIR 11 STEP 4D(1)(A);[05] ACCOMPLISHED HFEC SURFACE SCAN OF CUT EDGES IAW 737 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23.<BR>NO CRACKS NOTED.<BR><BR>EQUIPMENT USED: NORTEC 600 ID: ATS1465 CAL DUE: 09/2023;[06] FABRICATED -1 REPAIR DOUBLER FROM 2024T3#0.080' CLAD LOT#1497191-1. TREATED IAW SRM 55-10-01-2R-11 REPAIR 11. OK TO PRIME;[07] VERIFIED CORRECTIVE ACTION ITEM 6; OK TO PRIME.;[08] APPLIED BMS 10-79 PRIMER TO REPAIR PART AND REWORKED AREA IAW SRM 55-10-01-2R-11 REPAIR 11.....OK TO INSTALL;[09] VERIFIED CORRECTIVE ACTION ITEM 8; OK TO INSTALL.;[10] INSTALLED REPAIR PART IAW SRM 55-10-01-2R-11 REPAIR 11;[11] RII VERIFIED CORRECTIVE ACTION ITEM 10.;[12] APPLIED FILLET SEAL AROUND THE EDGES OF -1 DOUBLER AND APPLIED FINISH IAW SRM 55-10-01-2R-11.;[13] VERIFIED CORRECTIVE ACTION 12 AND MEASUREMENT TABLE.
LEFT HAND HORIZONTAL STABILIZER INSPAR RIB; AT STABILIZER STATION 111.10; 4TH VERTICAL STIFFENER IS CRACKED.<[01] HFEC REQUEST TO VERIFY CRACK ON L/H HORIZONTAL STAB INSPAR RIB AT STAB. STA. 111.10 4TH VERTICAL STIFFENER;[02] VERIFIED CRACK IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23 TOOL# IS000680 CAL. DUE 04/2023.;[03] REMOVED THE DAMAGED PART AT LH HORIZONTAL STABILIZER STA 111.10 RIB 4HT VERTICAL STIFFENER IAW SRM 55-10-09-2R-4;[04] HFEC REQUEST ON THE CUT OUT EDGES; WEB AND EXISTING FASTENERS HOLES WITHIN THE REPAIR AREA TO ENSURE NO CRACKS EXIST.;[07] FABRICATED REPAIR PARTS (1) T-SECTION FROM 60-5872 7075 T76511 LOT# 1449876-1 (2) ANGLE FROM BAC 1490-2793 7075 T62 CLAD LOT# 1442205-1 (3) SHIM FROM 7075 T6 0.040' CLAD LOT# 1463598-1; APPLIED CHEMICAL CONVERSION COATING IAW SRM 55-10-09-2R-4 OK TO PRIME.;[08] PERFORMED GVI OF ALL AREAS WITHIN THE REPAIR AREA; NO DEFECTS NOTED; IAW SRM 55-10-09-2R-4.;[09] VERIFIED CORRECTIVE ACTIONS 7 AND 8.;[10] PRIMED REPAIR PARTS AND COMMON AREA IAW SRM 55-10-09-2R-4 OK TO INSTALL.;[11] VERIFIED CORRECTIVE ACTION 10.;[12] INSTALLED REPAIR PARTS AT LH HORIZONTAL STABILIZER STA 111.10 RIB 4TH VERTICAL STIFFENER IAW SRM 55-10-09-2R-4;[13] VERIFIED CORRECTIVE ACTION 12.;[14] VERIFIED COMPLETION.
CRACK IN LH HORIZ STAB LWR SKIN; STAB STA 193.9. INBD FASTENER ROW; 17' FROM L/E. .6' IN LENGTH. FOUND USING HFEC INSPECTION METHOD. MARKED.<[01] CUT AND REMOVED THE DAMAGED AREA OF THE LH HORIZ STAB LWR SKIN; STA 193.9. IAW SRM 55-10-01-2R-11 REPAIR 11;[02] VERIFIED CORRECTIVE ACTION 1;[03] REQUEST NDI TO HFEC INSPECT CUT EDGES FOR CRACK FREE CONDITION;[04] ACCOMPLISHED HFEC SURFACE SCAN OF CUT EDGES IAW 737 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23.<BR>NO CRACKS NOTED.<BR><BR>EQUIPMENT USED: NORTEC 600 ID: ATS1465 CAL DUE: 09/2023;[05] CRACK IN LH HORIZ STAB LWR SKIN; STAB STA 193.9. INBD FASTENER ROW; 17' FROM L/E. .6' IN LENGTH WILL BE REPAIRED ON FAULT [TTG8Q00H2644];[06] ALL RII REQUIREMENTS HAVE BEEN MET.;[07] VERIFIED CORRECTIVE ACTION ITEMS AND MEASUREMENT FIELDS; CARD COMPLETE.
EMERGENCY AISLE LIGHTS AT 12CBA & 14CBA INOPERATIVE. R & R THE BATTERY PACK M1670 IAW AMM 33-51-06. OPS CHECKED GOOD.
EMERGENCY EXIT LIGHTS POWERED BY BATTERY POWER SUPPLY M01673 ARE INOP / [01] OPENED AFT LOWERED CEILING PANEL IAW AMM 33-51-06-960-805 STEP 4E(3)(E);[02] REMOVED AND REPLACED AND OPS CHECKED AFT LH EMERGENCY LIGHT BATTERY IAW AMM 33-51-06-960-805 PAGES 1-11 OPS CHECK GOOD;[03] VERIFIED STEP 1 AND 2 C/W<BR><BR>OK TO CLOSE AFT LOWERED CEILING PANEL;[04] CLOSED AFT LOWERED CEILING PANEL AND INSTALL SECURITY SEAL IAW AMM 33-51-06-960-805 STEP 4F(4);[05] ALL WORK C/W<BR>AUDIT C/W
DOT A-24-1 MID CABIN FLOOR PANEL 231ZF HAS COMPOSITE PULLED FIBERS ON UPPER SIDE. / [01] EVALUATED AND FOUND DAMAGE TO UPPER SURFACE TO BE REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2R-1 STEPS 3 A;C;E;F.<BR>VERIFIED REPAIR MATERIALS AS GLASS--(A10269); RESIN--(A141868) IAW SRM 53-00-50-2R-1 TABLE 201<BR>NEED OK TO BOND;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEPS 3 K-M. TAP TEST GOOD. TOOLING AAR30347 DUE 4-30-23;[04] REPAIRED DAMAGE TO UPPER SURFACE FLOOR BOARD IAW SRM 53-00-50-2R-0 REPAIR GENERAL AND SRM 53-00-50-2R-1 REPAIR 1. TAP TEST GOOD.;[05] VERIFIED STEPS 3-4
DOT A-24-5 MID CABIN FLOOR PANEL 232SF HAS COMPOSITE PULLED FIBERS ON UPPER SIDE. / [01] EVALUATED AND FOUND DAMAGE TO UPPER SURFACE TO BE REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2R-1 STEPS 3 A;C;E;F.<BR>VERIFIED REPAIR MATERIALS AS GLASS--(A10269); RESIN--(A141868) IAW SRM 53-00-50-2R-1 TABLE 201<BR>NEED OK TO BOND;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEPS 3 K-M. TAP TEST GOOD. TOOLING AAR30347 DUE 4-30-23;[04] REPAIRED DAMAGE TO UPPER SURFACE FLOOR BOARD IAW SRM 53-00-50-2R-0 REPAIR GENERAL AND SRM 53-00-50-2R-1 REPAIR 1. TAP TEST GOOD.;[05] VERIFIED STEPS 3-4
DOT A-24-6 MID CABIN FLOOR PANEL 242BF HAS COMPOSITE PULLED FIBERS ON UPPER SIDE. / [01] EVALUATED DAMAGE; UPPER SURFACE IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1. TAP TEST GOOD; NO DELAMINATION NOTED. <BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS A;C;E; AND F. <BR> <BR>VERIFIED REPAIR MATERIALS IAW B737 SRM 53-00-50-2R-1 TABLE 201; FIBERGLASS CLOTH BMS9-3 (A10269); RESIN EPOCAST 50A (A141868)<BR><BR>REQUIRES OKAY TO BOND REPAIR.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEP 3 K-M. CURED AT 150 DEGREES (OVEN B0-06 EXP 11-8-22).;[04] REPAIRED MID CABIN FLOOR PANEL 242BF UPPER SIDE IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.;[05] VERIFIED STEPS 3-4
DOT A-24-2 MID CABIN FLOOR PANEL 241AF HAS COMPOSITE PULLED FIBERS ON UPPER SIDE. / [01] EVALUATED AND FOUND MISSING PLIES OVER MAJORITY OF UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A; C; E-F.<BR><BR>VERIFIED MATERIAL IAW SRM 53-00-50-2R-1 TABLE 201. RESIN (A141868); FABRIC (A10269).<BR><BR>REQUESTING OK TO BOND;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEP 3 K-M. CURED AT 150 DEGREES (AAR 30347 EXP 4-30-22). TAP TEST GOOD.;[04] REPAIRED MID CABIN FLOOR PANEL 241AF ON UPPER SIDE IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.;[05] VERIFIED STEPS 3-4
DOT A-24-3 MID CABIN FLOOR PANEL 232RF HAS COMPOSITE PULLED FIBERS ON UPPER SIDE. / [01] EVALUATED AND FOUND MISSING PLIES OVER MAJORITY OF UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A; C; E-F.<BR><BR>VERIFIED MATERIAL IAW SRM 53-00-50-2R-1 TABLE 201. RESIN (A141868); FABRIC (A10269).<BR><BR>REQUESTING OK TO BOND;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEP 3 K-M. CURED AT 150 DEGREES (AAR 30347 EXP 4-30-22). TAP TEST GOOD.;[04] REPAIRED MID CABIN FLOOR PANEL 232RF ON UPPER SIDE IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.;[05] VERIFIED STEPS 3-4
DOT A-24-4 MID CABIN FLOOR PANEL 242AF HAS COMPOSITE PULLED FIBERS ON UPPER SIDE. / [01] EVALUATED DAMAGE; UPPER SURFACE IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1. TAP TEST GOOD; NO DELAMINATION NOTED. <BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS A;C;E; AND F. <BR> <BR>VERIFIED REPAIR MATERIALS IAW B737 SRM 53-00-50-2R-1 TABLE 201; FIBERGLASS CLOTH BMS9-3 (A10269); RESIN EPOCAST 50A (A141868)<BR><BR>REQUIRES OKAY TO BOND REPAIR.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR PLIES IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS K; L; AND M. TAP TEST GOOD.;[04] REPAIRED CABIN FLOOR PANEL 242AF UPPER SURFACE IAW B737 SRM 53-00-50-2R-1 REPAIR 1.;[05] VERIFIED STEPS 3-4
CRACK FOUND ON UPPER ATTACH ANGLE AT STA 663 OUTBOARD SIDE OF RBL 45 WL 193. VERIFIED WITH HFEC / [01] REMOVED DRAIN COVER I.A.W SRM 51-40-02-0G-0;[02] REMOVED ELEC PLUGS COVER AT W/W R/H AFT OF 663 CEILING I.A.W SRM 51-40-02-0G-0;[03] REMOVED GROUND SPOILER VALVE MOUNT I.A.W SRM 51-40-02-0G-0;[04] RECEIVED FORMED AND HEAT TREATED -1 AND -2 REPAIR ANGLES FROM BACKSHOP IAW E/A 22-157-02626-WIP1 STEP 7A. BACKSHOP W/O# 44093-6000-0001;[05] VERIFIED STEP 4;[06] BLADDER SEALS REMOVED FOR REPAIR;[07] OK TO INSTALL ITEMS REMOVED ION STEPS 1; 3; AND 6;[08] INSTALLED DRAIN COVER; GROUND SPOILER VALVE MOUNT; AND BLADDER SEALS IAW SRM 51-40-02 AND BOEING DWG 111A1000 REV A;[09] VERIFIED STEP 8 C/W;[10] OK GIVEN TO REINSTALL REMOVED ELEC PLUGS COVER;[11] REINSTALLED ELEC PLUGS COVER I.A.W SRM 51-40-02-0G-0;[12] VERIFIED STEP 11 C/W;[13] ACCOMPLISHED FUEL LEAK CHECK OF CNT TANK FASTENERS IAW AMM 28-11-00-210-801<BR>LEAK CHECK GOOD;[14] VERIFIED STEP 13 C/W;[15] VERFIED REPAIR IS COMPLETE IAW EA 22-157-02626;[16] VERIFIED STEP 15 C/W; JOB COMPLETE; AUDIT C/W
CRACK FOUND ON UPPER ATTACH ANGLE AT STA 663 OUTBOARD SIDE OF LBL 45 WL 193. VERIFIED WITH HFEC / [01] DISPLACED WIRING BONDLE AFT SIDE OF REPAIR AREA IAW SRM 51-40-02-0G-0;[02] VERIFIED STEP 1 C/W;[03] ACCOMPLISHED FUEL LEAK CHECK OF CNT TANK FASTENERS IAW AMM 28-11-00-210-801<BR>LEAK CHECK GOOD;[04] VERIFIED STEP 3 C/W;[05] REINSTALLED DISPLACED WIRE BUNDLE AFT OF REPAIR AREA (MAIN WHEEL WELL) IAW SWPM 20-10-12 PARA D;[06] VERIFIED STEP 5 C/W;;[07] VERIFIED UPPED ATTACH ANGLE AT STA 663 LBL 45 WAS REPAIRED IAW EA 22-157-02625;[08] VERIFIED ITEM 7<BR>AUDIT C/W
RT OVERWING EXIT DOOR SERVICE LIGHT IS BURNT OUT @ 11 CB / [01] RELAMPED RT OVER WING EXIT DOOR SERVICE LIGHT AT 11CB IAW 737 AMM 33-51-01;[02] INSPECTED
FWD SERVICE DOOR /FWD GALLEY LOWER WALL EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE DURING TEST / [01] REMOVED AND REPLACED R 1 DOOR ON GALLEY WALL EMERGENCY EXIT LIGHTED SIGN ASSEMBLY NO HELP REF AMM 33-51-01;[02] R&R R1 DOOR EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-51-06
LEFT OVER WING EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE DURING TEST LOWER WALL / [01] R&R LH OVER WING DOOR EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-51-06
FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP ; / [01] REVAMPED FORWARD SERVICE DOOR SLIDE EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK GOOD
FWD SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP ; / [01] RELAMPED IAW AMM 33-51-03
AFT ENTRY SLIDE FELL OUT OF THE COMPARTMENT ; / [01] REINSTALLED AFT ENTRY SLIDE PER MT725-61-06. VPN-5A3307-7; S/N-BNG30126
L/H O/W EXIT ASSIST STRAP BOX MISSING HARDWARE. / INSTALLED L/H O/W EXIT ASSIST STRAP BOX HARDWARE. PER AMM 52-22-51
L/H O/W EXIT HANDLE LOOSE / INSTALLED L/H O/W EXIT HANDLE PER AMM 52-22-51
AFT GALLEY DOOR SLIDE GIRT HANGING LOW. / INSTALLED AFT GALLEY DOOR SLIDE PER AMM 25-66-01 AND MT#725-61-06
FWD LAV EMERGENCY EXIT LIGHT WIRING BUNDLE (A/C SIDE) HAS A LOOSE WIRE AT THE GROUND BLOCK / INSTALLED NEW CONTACT ON WIRE W4142-0152-20 AND RETERMINATED INTO GD3782-DC PER WDM 33-51-21 AND SWPM 20-90-15. PERFORMED GOOD CONTINUITY CHECK FOR WIRE W4142-0152-20 AS DOCUMENTED ON 57897U 10JAN21 SA-M326: A1289300. TEST WILL BE PERFORMED ON NRC: U260310. 57897U 10JAN21.
***CORROSION*** ON STRINGER CLIP AT AFT CARGO BAY BS767 S-19R WL191. MARKED / REMOVED AND REPLACED ACB STR CLIP AT BS767 STR19R WL191 DUE NO ALLOWABLE LIMIT IN THE SRM FOR THIS ITEM; IAW SRM 51-40-02-0G-1; AND DWG # 146A1261
***CORROSION*** ON STRINGER CLIP AT AFT CARGO BAY BS767 RBL15 WL152. / REMOVED AND REPLACED ACB STR CLIP BS767 STR 26R DUE TO NO ALLOWABLE LIMIT FOUND IN THE SRM FOR THIS ITEM; IAW SRM 51-40-02-0G-1 DWG # 146A1261
BENT RAIL AT AFT CARGO BAY BS747 LBL3 WL156. MARKED / A.C.B. RAIL AT BS 747; LBL 3; WL 156 REPAIRED IAW SRM 53-00-53-2R-2. ALTERNATIVES 1. FIG 203.
***CORROSION*** ON SHEAR TIE AT AFT CARGO BAY BS867 LBL11 WL160. / REMOVED AND REPLACED SHEAR TIE AT ACB BS 867 LBL 11 WL 160 IAW SRM 51-40-02-0G-0 DWG 146A3230
***CORROSION*** ON ATTACH ANGLE AT AFT CARGO BAY BS747 RBL6 WL151. / REMOVED CORROSION ON ATTACH ANGLE FOUND TO BE OUT OF LIMITS MORE 50% MAT. LOSS ACB BS 747 RBL 6 WL 151; REMOVED FABRICATED; LOCATED DRILLED AND INSTALLED ATTACH ANGLE AT ACB BS 747 RBL 6 PER SRM 53-00-53-1A-2; 51-40-02 DWG 146A1320 DWG 146A7810
***CORROSION*** ON SHEAR TIE AT AFT CARGO BAY BS747 RBL8 WL150. / SHEAR TIE AT BS 747; RBL8; WL150. MATERIAL LOSS MORE THAN 50%. FOUND TO BE OUT OF LIMITS PER SRM 53-00-07-1A-1. LOCATED; DRILLED AND INSTALLED NEW SHEAR TIE ITEM: HFAB53-ST-012. PO# 812597/1 AND PO# 812598/1 IAW SRM 51-40-05; SRM 51-40-02. DWG # 146A3230 AND DWG # 146A1260.
***CORROSION*** ON WEB AT AFT CARGO BAY BS790 RBL19 WL157. / REMOVED ADN REPLACED WEB AT ACB BS 790 RBL 19 WL 157 IAW SRM 51-40-02-0G-0 DWG 146A8320
***CORROSION*** ON FLOOR SUPPORT SPLICE AT AFT CARGO BAY BS767 RBL13 WL156. REJECTED DUE TO CORROSION HAS NOT BEEN TOTALLY REMOVED. / REMOVED AND REPLACED FLOOR SUPPORT SPLICE AT ACB BS767 WL156 PER SRM 51-40-02 AND FLOOR SUPPORT SPLICE AT ACB BS767 RBL13 WL156 PER SRM 51-40-02 AND 146A7500
***CORROSION*** ON STRINGER CLIP AT AFT CARGO BAY BS927 LBL5 WL171. / REMOVED AND REPLACED ACB STR CLIP AT BS927 STR27L DUE TO NO ALLOWABLE LIMIT FOUND FOR THIS ITEM; IAW SRM 51-40-02-0G-0 AND DWG # 147A0040
***CORROSION*** ON STRINGER CLIP AT AFT CARGO BAY BS747 RBL15 WL152. / REMOVED AND REPLACED ACB STR CLIP AT BS 747 STR 26R DUE TO NO ALLOWABLE LIMIT FOUND FOR THIS ITEM.; IAW SRM 51-40-02-0G-0 AND DWG # 146A1260
***CORROSION*** ACB AFT RT BULKHEAD SUPPORT; BS 947; S-21R TO S-25R WL 181 / CORROSION ACB AFT RT BULKHEAD SUPPORT ANGLE; BS 947; S-21R TO S-25R WL 181 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. THE STRUCTURAL ITEMS THAT DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT. IAW SRM 51-10-02 PAR 9C. REMOVED AND REPLACED ACB AFT RT BULKHEAD SUPPORT ANGLE BS 947 S-21R - S-25R; PN # 149A8118-28 IAW SRM 51-40-02 AND IAW DWG # 149A8117 AND IAW DWG # 149A8118
***CORROSION*** ACB AFT CTR BULKHEAD SUPPORT; BS 947; LBL10 TO RBL22 / CORROSION ON ACB AFT CENTER BULKHEAD SUPPORT ANGLE; BS 947; LBL 10 TO RBL 22 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. THE STRUCTURAL ITEMS THAT DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 PAR 9C. REMOVED AND REPLACED ACB AFT CENTER BULKHEAD SUPPORT ANGLE PN # 149A8118-29 IAW SRM 51-40-02; IAW DWG # 149A8117 AND IAW DWG # 149A8110
***CORROSION*** ACB RT FLOOR TO SIDEWALL SUPPORT. BS727+4 TO BS767; RBL21; WL157 / REMOVED ADN REPLACED ACB R/H FLOOR TO SIDEWALL SUPPORT AT BS 727+4 TO BS767; RBL21 IAW SRM 51-40-02-0G-1 DWG 146A7500
***CORROSION*** ACB FWD SHIELD. BS767 TO BS787; RBL21; WL157 / REMOVED AND INSTALLED ACB FWD SHIELD AT BS 767 TO BS 787; RBL 21; WL157 ITEM # 7531132 IAW SRM 51-10-02-0G-0; SRM 51-40-2-0G-2; DWG# 146A0081.
GUSSET AT BS 500D STR 19 R/H IS CRACKED / REMOVED AND INSTALLED NEW GUSSET AT BS 500D STR 19 R/H I.A.W. SRM 51-40-02-0G-0; DWG 143A7902 88302U 13JAN21
GUSSET AT BS 500D STR 19 L/H IS CRACKED / REMOVED AND INSTALLED NEW GUSSET AT BS 500D STR 19 L/H I.A.W. SRM 51-40-02-0G-0; DWG NO 143A7902. 88302U 13JAN21
***CORROSION*** ACB DOOR SURROUND STRUCTURE FWD STRAP; ALONG FWD EDGE. 8' IN LENGTH; BS793.5; BETWEEN S-24R AND S-25R; WL159; RBL27. / REMOVED AND INSTALLED NEW ACB DOOR SURROUND STRUCTURE F.W.D. STRAP; BETWEEN S-17R AND S-27R; BS 793.5; WL 159; RBL 27; ITEM # 7531466; PO # 812463 IAW SRM 53-60-15-0I-1; SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG # 146A8208; DWG # 146A8200
***CORROSION*** ON FLOOR BEAM UPPER SURFACE AT B.S. 986.5; W.L. 208.1; R.B.L. 30-43. / REPAIRED CORROSION ON FLOOR BEAM UPPER SURFACE AT BS 986.5 WL 208.1; RBL 30-43 IAW EA 1-A53-8241 REV 3.
L/W LOWER TRAILING EDGE CAVITY HAS NUTPLATE BROKEN OFF AT RSS 273; O/B OF AFT PYLON FAIRING. / REMOVED AND REPLACED L/H LOWER TRAILING EDGE CAVITY WIGGLE PLATE AT RSS 273 O/B OF AFT PYLON FAIRING I.A.W SRM 51-40-02-0G-0 AND DRAWING # 115A2001. AND 115A2714. WIGGLE PLATE P/N. 115A2781-9.
***CORROSION*** ON FLOOR BEAM UPPER SURFACE AT B.S. 986.5; W.L. 208.1; L.B.L. 27-42. / REPAIRED CORROSION ON THE FLOOR BEAM UPPER SURFACE OF BS 986.5; WL 208.1. WL 27-42. IAW EA 1-A53-8241 REV 3
CRACKED INTERCOSTAL AT B.S. 277-294.5; W.L. 208.1; R.B.L. 1. / REMOVED & REPLACED INTERCOSTAL AT BS 277-294.5 WL208.1 RBL1 IAW DWG 414A5400 & SRM 51-40-02-0G-0
CRACK IN RADIUS OF FRAME AT B.S. 312 JUST ABOVE FORWARD ENTRY DOOR CUT OUT. / REPAIRED FRAME BS312 JUST ABOVE FWD ENTRY DOOR CUTOUT PER SWA EA 21-153-00078 REV IR (ATS ER 21-01024 REV IR)
***CORROSION*** ON B.S. 328 FLOOR BEAM; UPPER SURFACE; W.L. 208.1; R.B.L. 47. / FLOOR BEAM AT BS 329; UPPER SURFACE; W.L. 208.1; RBL 47 REPAIRED IAW ATS ER 21-01022; REV IR; DATED 18-JAN-2021 AND PER EA NO: 21-153-00121 REV IR. 55981U 19JAN21
FLOOR SUPPORT AT BS 540 BL 0 TO RBL 23 WL 207 CRACKED / REMOVED AND REPLACED FLOOR SUPPORT AT BS 540 BL 0 TO RBL 23 WL 207 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG #143A0060
TAILCONE 542EB OUTER SKIN IS DISBONDED JUST AFT OF DRAIN HOLE. / REMOVED AND REPLACED NEW TAIL CONE 542EB: PN# 113A9352-1; PO# 811848 IAW SRM 51-40-05; IAW SRM 51-40-02 AND IAW DWG# 113A9300
FLOOR SUPPORT CRACKED AT BS 663 RBL 63 WL 207 / REMOVED & REPLACED FLOOR SUPPORT AT BS 663 RBL 63 WL 207 P/N 144A5702-6 IAW DRW 144A3701 & SRM 51-40-02-0G-0
FWD FLOOR PANEL 222AF IS DELAMINATED ON THE UPPER SKIN / FWD FLOOR PANEL 222AF WITH DELAMINATED UPPER SKIN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9.A.(1)
AFT FLOOR PANEL 241AAF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / REPAIRED DAMAGE TO FLOOR PANEL 241AAF UPPER SKIN IAW SRM 53-00-50-2R-1.
AFT FLOOR PANEL 242WF UPPER SKIN HAS AREAS OF PULLED STRANDS. / AFT FLOOR PANEL 242WF WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.(1)
FLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. / REPAIRED FLIGHT DECK FLOOR AT BS 250 TO BS 270 RBL4 - LBL14 WL207.54 IAW EA 1-A53-33179 REV 1 AND DWG 141A0631
B.S. 663 LOWER COMPOSITE BULK HEAD RIGHT HAND UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 7; W.L. 164. / ACCOMPLISHED PERMANENT REPAIR AT BS 663 LOWER COMPOSITE BULK HEAD RIGHT HAND UPPER ATTACH ANGLE AT RBL 7; WL.164 I.A.W SRM. 57-20-20-2R-5. FIG. 202 SHEET #4. DETAIL B.
FWD FLOOR PANEL 221EF UPPER SKIN PREVIOUS REPAIR IS DISBONDED. / FWD FLOOR PANEL 221EF WITH DISBONDED PREVIOUS REPAIR ON UPPER SKIN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.(1).
AFT FLOOR PANEL 242VF LOWER SKIN HAS AREAS OF DAMAGE. (MARKED) / REPAIRED AREAS OF DAMAGE ON LOWER SKIN OF AFT FLOOR PANEL 242VF IAW SRM 53-00-50-2R-1.
AFT FLOOR PANEL 242VF HAS AREAS OF PULLED STRANDS. (MARKED) / REPAIRED AREAS OF PULLED STRANDS ON AFT FLOOR PANEL 242VF IAW SRM 53-00-50-2R-1.
AFT FLOOR PANEL 242UF HAS AREAS OF PULLED STRANDS. (MARKED) / REPAIRED DAMAGE TO FLOOR PANEL 242UF IAW SRM 53-00-50-2R-1
AFT FLOOR PANEL 242TF HAS AREAS OF PULLED STRANDS. (MARKED) / REPAIRED AREAS OF PULLED STRANDS ON AFT FLOOR PANEL 242TF IAW SRM 53-00-50-2R-1.
AFT FLOOR PANEL 241AEF UPPER SKIN HAS AREAS OF DAMAGE. (MARKED) / REPAIRED DAMAGE TO FLOORPANEL 241 AEF UPPER SKIN IAW SRM 53-00-50-2R-1
AFT FLOOR PANEL 241ADF LOWER SKIN HAS AREAS OF DAMAGE. (MARKED) / AFT FLOOR PANEL 241ADF WITH LOWER SKIN HAS AREAS OF DAMAGE WAS REPAIRED IAW SRM 53-00-50-2R-1; SRM 53-00-50-2R-4.
AFT FLOOR PANEL 241ACF UPPER SKIN HAS AN AREA OF PULLED STRANDS ALONG THE AFT EDGE. / AFT FLOOR PANEL 241ACF WITH UPPER SKIN HAS AN AREA OF PULLED STRANDS ALONG THE AFT EDGE WAS REPAIRED IAW SRM 53-00-50-2R-1.
AFT FLOOR PANEL 241ABF UPPER SKIN HAS AN AREA OF PULLED STRANDS ALONG THE AFT EDGE. / AFT FLOOR PANEL 241ABF WITH UPPER SKIN HAS AN AREA OF PULLED STRANDS ALONG THE AFT EDGE WAS REPAIRED IAW SRM 53-00-50-2R-1
FWD FLOOR PANEL 221DF HAS A LARGE PREVIOUS REPAIR THAT IS DISBONDED. / FWD FLOOR PANEL 221DF WITH LARGE DISBONDED PREVIOUS REPAIR WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.(1).
PANEL 193AR HAS INNER SURFACE CHAFING DAMAGE ON EDGEBAND / PANEL 193AR INNER SURFACE CHAFFING DAMAGE ON EDGEBAND WAS REPAIRED IAW SRM 51-70-05-2R-6
EXTERNAL POWER ACCESS DOOR IS BENT / REMOVED AND REPLACED EXTERNAL POWER ACCESS DOOR DUE TO NO ALLOWABLE LIMIT FOUND IN THE SRM FOR THIS ITEM IAW SOPM 20-50-01 AND DWG # 141A8701
FWD FLOOR PANEL 221GF FWD O/B CORNER TANG IS BROKEN. / FWD FLOOR PANEL 221GF WITH FWD O/B CORNER BROKEN TANG WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9.A.(1)
FWD FLOOR PANEL 221BF AFT O/B TANG IS BROKEN OFF. / FWD FLOOR PANEL 221BF WITH AFT O/B TANG BROKEN OFF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9.A.(1).
#2 ENGINE PYLON OUTBOARD SKATE ANGLE IS CRACKED / #2 ENGINE PYLON OUTBOARD SKATE ANGLE WAS REPAIRED IAW ATS ER #20-03701 REV IR DATED 16DEC20 AND EA 20-154-02506 REV IR
L/H MLG FWD TRUNNION FITTING-UPPER INBOARD LUG OUTER FACE HAS CORROSION / SPOT FACED UPPER INBD LUG OUTER FACE PER E.A. 1-A57-3246 AND INSTALLED NEW BUSHING PER MT 757-RCB-04-01 AND EA 1-A57-3246. D&M ENTERPRISES A/R W.O. # SSR#1223
L/H MLG FWD TRUNNION FITTING-LOWER INBOARD LUG BORE DIMENSION OUT OF TOLERANCE. DOES NOT MEET NOMINAL SIZE DIMENSIONS. / LINE REAMED LOWER INBD LUG PER E.A. 1-A57-3246 AND INSTALLED NEW BUSHING PER MT 757-RCB-04-01 AND EA 1-A57-3246 REF. D&M ENTERPRISES A/R W.O. #SSR1223
L/H MLG FWD TRUNNION FITTING-UPPER INBOARD LUG BORE DIAMETER OUT OF TOLERANCE. DOES NOT MEAT NOMINAL SIZE DIMENSIONS. / LINE REAMED UPPER INBD LUG PER E.A. 1-A57-3246 AND INSTALLED NEW BUSHING PER MT 757-RCB-04-01 AND EA 1-A57-3246. REF. D&M ENTERPRISES A/R W.O.#SSR1223
L/H MLG FWD TRUNNION FITTING-LOWER OUTBOARD LUG BORE DIMENSIONS OUT OF TOLERANCE. DOES NOT MEET NOMINAL SIZE DIMENSIONS / LINE REAMED LOWER OUTBD LUG PER E.A. 1-A57-3246 AND INSTALLED NEW BUSHING PER MT 757-RCB-04-01 AND EA. 1-A57-3246 REF. D&M ENTERPRISES A/R W.O. #SSR1223
L/H MLG FWD TRUNNION FITTING-UPPER OUTBOARD LUG BORE DIMENSION OUT OF TLERANCE. DOES NOT MEET NOMINAL SIZE DIMENSIONS / LINE REAMED UPPER OUTBD LUG PER E.A. 1-A57-3246 AND INSTALLED NEW BUSHING PER MT 757-RCB-04-01 AND E.A. 1-A57-3246 REF. D&M ENTERPRISES A/R W.O. #SSR1223
R/H MLG FWD TRUNNION LOWER OUTBOARD BORE OUT OF TOLERANCE / LINE REAMED LOWER OUTBD LUG BORE PER E.A 1-A57-3246 AND INSTALLED NEW BUSHINGS PER MT 757-RCB-04-01 AND E.A. 1-A57-3246 REF. D&M ENTERPRISES A/R SSR# 1224
R/H MLG FWD TRUNNION LOWER INBOARD BORE OUT OF TOLERANCE / LINE REAMED LOWER INBD LUG BORE PER E.A. 1-A57-3246 AND INSTALLED NEW BUSHING PER MT757-RCB-04-01 AND E.A. 1-A57-3246.
R/H MLG FWD TRUNNION UPPER OUTBOARD BORE OUT OF TOLERANCE / LINE REAMED UPPER OUTBD LUG BORE PER EA.1-A57-3246 AND INSTALLED NEW BUSHING PER MT 757-RCB-04-01 AND E.A.1-A57-3246 REF. D&M ENTERPRISES A/R W.O.SSR#1224
R/H MLG FWD TRUNNION UPPER INBOARD BORE OUT OF TOLERANCE / LINE REAMED UPPER INBD LUG BORE PER E.A. 1-A57-3246 AND INSTALLED NEW BUSHING PER MT 757-RCB-04-01 AND EA 1-A57-3246 REF. D&M ENTERPRISES A/R W.O.SSR#1224
AFT SERVICE DOOR EXTERIOR FAM EMERGENCY LIGHT INOP. / RTND CHARGER & BATTERY EQUIP #M1672 PER MM 33-51-06
DECLARED EMERGENCY, UPON INITIAL FLAP EXTENSION ONLY 1/2 DEGREES OF FLAPS CAME OUT. ALSO THERE WAS AN ASYMMETRY CONDITION. LEADING EDGE. DEVICES DID NOT EXTEND. FOLLOWED QRH PROCEDURES FOR TRACKING EDGE FLAP / ASYMMETRY LEADING US TO TRACKING EDGE FLAPS UP LANDING EXTENDED LEADING EDGE DEUCES THROUGH ALT FLAP EXTENSION PROCEDURES REF 167 KTS TARGET 173 KTS. DIVERTED & FOLLOWED BRAKE COOLING PROCEDURES. / R&R CONNECTOR PLUG AT NR 8 SKEW SENSOR AS PRECAUTIONARY PER SWPM.
R2 DOOR SLIDE WAS BELOW SERVICEABLE LIMIT. R&R SLIDE IAW MT.
OVER WING EMERGENCY EXIT DOOR ON CAPTAINS SIDE LOWER HANDLE AND COVER ASSEMBLY BROKEN. / INSTALLED MISSING HARDWARE IAW SIP.
DECLARED EMERGENCY--------------------------------------------------WHILE DESCENDING THROUGH 30,000 / FT. CABIN RATE INCREASED AT 4000 FPM OR GREATER. CABIN CLIMBED THROUGH 10,000 FT. PERFORMED A RAPID DEPRESSURIZATION DESCENT AND ACCOMPLISHED THE QRC "CABIN ALT WARNING, RAPID DEPRESSURIZATION" AND THE QRH RAPID DEPRESSURIZATION CHECKLIST. / R&R AFT OUTFLOW VALVE IAW AMM.
L/H EMERGENCY LIGHT COVER FELL OFF AT ROW 14. / SECURED COVER PER SIP.
FORWARD CABIN, EMERGENCY EXIT LIGHTS COMMON TO M1675 WERE NOT OPERATING CORRECTLY. / R&R BATTERY PACK IAW AMM.
FORWARD CABIN, EMERGENCY EXIT LIGHTS COMMON TO M1675 WERE NOT OPERATING CORRECTLY. / R&R POWER SUPPLY IAW AMM.
CUSTOMER REQUEST: (F.B.) AFT CARGO COMPARTMENT INTERCOSTAL BS 787-807 AT S-27R IS CORRODED. WL 156 / INTERCOSTAL WAS FOUND TO HAVE 100% MATERIAL LOSS. REMOVED AND REPLACED NTERCOSTAL AT STA 787-807 STR 27R IAW BOEING DWG #146A8130 REV: B AND SRM 51-40-02-0G-0. APPLIED CIC TO THE NEW INTERCOSTAL IAW AMM 51-21-91-620-802 PARAGRAPH 3.C. P/N 146A8132-17
LH VAPOR BARRIER HORIZNAL STIFFNER AT LBL 6-30 AND AT STA.663 CRACKED / REMOVED HORIZ STIFFENER AT BS 663; LBL 6 TO 3D IAW SRM 51-40-02-0G-0. FABRICATAED NEW STIFFENER IAW EA 190941 REV. IR AND SWA EA 1-757-16681 REV. IR. INSTALLED NEW STIFFENER IAW SRM 51-40-02-0G-0 AND BOEING DWG. 111A1000 REV. B.
UPPER VAPOR BARRIER FORWARD SUPPORT ANGLE, CENTER FUEL TANK CRACKED AT BS. 663, LBL 7. / REPAIRED ANGLE IAW SRM.
L/H CREASE BEAM AT FORWARD ENTRY, CORRODED FROM LOWER FORWARD CUTOUT TO AFT LOWER CUTOUT. / R&R L-1 CREASE BEAM CHORD IAW SRM & DWG.
RW PANEL 651 GB HAS A CRACK ON FWD O/B SIDE OF BRACKET MARKED IN RED. / DAMAGED BRACKET TO RW PANEL 651GB REMOVED AND REPLACED NEW IAW B-737 SRM 51-40-02-0G-0. NEW PART FASTENER LOCATIONS LOCATED AND DRILLED IAW B-737 SRM 51-40-05-0G-0; SRM 51-40-06-0G-0; & 51-40-08-0G-0 A-TAG FT2583
RT WING; LWR L/E PANEL 621DB HAS THREE CORNERS DELAMINATED. / VERIFIED NEW PART #116A9110Y30 FOR RIGHT WING; LOWER L/E PANEL 621DB; ATAG# FT2584. LOCATED; DRILLED; COUNTERSUNK NEW FASTENER LOCATIONS IN BLANK PANEL IAW SRM 51-40-05-0G-0 AND SRM 51-40-08-0G-0
L/H WING LOWER LEADING EDGE PANEL 521JB HAD ONE CORNER DELAMINATED. / REPAIRED PANEL 521JB IAW SRM.
AFT CARGO FLOOR PANEL 140DF HAS CORROSION FWD LOWER EDGE / FABRICATECD NEW FLOOR PANEL 140DF IAW IPC 25-52-10-02 AND BOEING DWG 453A2610 REV: B. EA 190924 REV. P1 CANCELLED
RUDDER BALANCE WEIGHT HAS HEAVY CORROSION ON FWD SIDE._RUDDER STATION 151.17; 17.05 INCHES FWD OF HINGE C/L / REMOVED & REPLACED RUDDER BALANCE WEIGHT IAW CMM 55-40-09 DISASSEMBLY & ASSEMBLY P/N 173A5103-1
AFT ENTRY DOOR PANEL 834DZ AFT BRACKET CRACKED / REMOVED & REPLACED BROKEN L2 DOOR PANEL 834DZ AFT BRACKET W NEW PN 411A2129-548 IAW AIPC 52-13-21-10 & SRM 51-40-02-0G & ATAG # A60238
COMPOSITE REPAIR LAYER DELAMINATED ON THE TOP SURFACE OF THE CABIN FLOOR PANEL 221GF, FORWARD INBOARD CORNER BETWEEN BS. 270 TO BS. 420. / REPAIRED FLOOR BOARD PANEL #221GF IAW SRM.
AFT GALLEY DOOR PANEL 844DZ AFT BRACKET CRACKED / REMOVED & REPLACED BROKEN R2 DOOR PANEL 844DZ W/ NEW BRACKET PN 411A2129-547 IAW AIPC 52-41-31-10 SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 ATAG# A60235
R2 CREASE BEAM INNER CHORD CORRODED ON UPPER SURFACE BETWEEN BS. 887+6 TO BS. 1016, RBL 51. / R&R R-2 CREASE BEAM IAW DWG & SRM.
WIRE BROKEN AT GROUND BLOCK GD03778S BS. 1006. / REPAIRED W-3142-0452-20 IAW WDM.
RH ENGINE STRUT BOX ASSEMBLY AFT END EXTERNAL SURFACES ARE CORRODED AT NAC STA 273-282; NAC LBL 3-7; NAC WL 119-130. / REMOVED CORROSION FROM #2 PYLON STRUT ASSY.; AFT END; I/B LOWER FITTING IAW SRM 51-10-02-0G-0. ORIGINAL 'T' .125'; REMAINING 'T' .108'; LOSS OF .017'. DAMAGE OUT OF LIMITS IAW SRM 54-50-71-1A-2. REPAIRED AREA IAW EA 190926 REV. IR AND SWA EA 1-754-2457 REV. IR.
RH WING TRAILING EDGE FLAP WELL LOWER SIDE WIGGLE PLATE IS CRACKED AT RSS 270. / REPLACED WIGGLE PLATE ASSEMBLY AT TRAILING EDGE FLAP RSS 270 IAW SRM 51-40-02-0G-0 + 51-40-05-0G-0.
RH ENGINE STRUT AFT FAIRING (PN 313-2060-928; SN 889301001) FRAME LATERAL RESTRAINT FITTING INSTALLATION IS CORRODED AT NAC STA 283; NAC LBL 4; NAC WL 122. / REMOVED CORROSION ON R/H ENGINE STRUT AFT FAIRING FRAME INTERNAL RESTRAINT FITTING IAW B 737 SRM 51-10-02-0G-0 ITEM 15. MATERIAL REMOVAL NOT ALLOWABLE OUT OF LIMITS IAW NDT PUBLISHED DOCUMENTS. REMOVED AND REPLACED FITTING P/N 313A2312-3 IAW B737 SRM 51-40-82-0G-0 AND IPC 54-52-01-01 FIG ITEM 40.
RIGHT PYLON PANEL 441EL LOWER INTERNAL MATING SURFACE HAS AREA OF CORROSION / REMOVED CORROSION FROM RT PYLON PANEL 441EL IAW SRM 51-10-02-0G-0. ORIGINAL 'T' .110' AND .170'; REMAINING 'T' .107' AND .152' LOSS OF .003' AND .018'. REPAIRED PANEL IAW EA 190911 REV. IR AND SWA EA# 1-754-2455 REV. IR. NO FURTHER ACTION REQUIRED.
L/H WING TRAILING EDGE FLAP WELL LOWER SIDE WIGGLE PLATE CRACKED AT RSS. 270. / R&R WIGGLE PLATE E PLATE IAW SRM & AMM.
DECLARED EMERGENCY----------------------------------------------------MOVED FLAP HANDLE TO 5. NO FLAP MOVEMENT FLAP INDICATOR SHOWED A SPLIT. NO FLAP LANDING. GROSS WEIGHT 122.9, MAX BRAKE, MAX REVERSE AT 182 KNOTS. / R&R #8 FLAP SKEW SENSOR IAW AMM.
R1 DOOR SLIDE GIRT BAR LOOSE. ADJUSTED GIRT BAR HOLDER IAW AMM.
AIR TURNBACK, UPON FLAP RETRACTION AMBER LEADING EDGE FLAP TRANSIT LIGHT REMAINED ILLUMINATED OVERHEAD LEADING EDGE DEVICE PANEL INDICATED #1 LEADING EDGE FLAP EXTENDED NO ROLL EXPERIENCED. R&R #1 FLAP EXTEND PROXIMITY SENSOR PER AMM.
FORWARD MEGAPHONE WEAK. R&R BATTERIES PER SIP.
COCKPIT EXIT LIGHT INOP. R&R BATTERY PACK M1675 PER AMM.
RT OVERWING ALL EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK M1669 PER AMM.
RT EMERGENCY EXIT BULLNOSE LIGHTS INOP BETWEEN ROW 11 TO ROW 13. R&R BATTERY PACK PER AMM.
L2 DOOR EMERGENCY EXIT SLIDE LIGHT INOP. R&R BATTERY PACK PER AMM.
LOWER AFT EMERGENCY EXIT SIGN INOP. R&R BATTERY PACK PER AMM.
L1 DOOR EMERGENCY SLIDE EXIT LIGHT INOP. R&R BATTERY PACK M1675 PER AMM.
R2 DOOR EXIT LIGHT ABOVE DOOR INOP. R&R BATTERY PACK PER AMM.
FORWARD EXIT LIGHT INOP. R&R BATTERY PACK M1675 PER AMM.
FORWARD ENTRY DOOR LOWER EXIT LIGHT INOP. R&R BATTERY PACK M1675 PER AMM.
LT EMERGENCY EXIT BULLNOSE LIGHTS INOP BETWEEN ROW 4 TO ROW 23. R&R BATTERY PACK PER AMM.
L2 DOOR EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK PER AMM.
AFT CARGO BAY VERTICAL BULKHEAD STATION AT BS 947 LBL 12 IS CRACKED / NO ALLOWABLE DAMAGE FOUND IN SRM; REMOVED AND REPLACED AFT CARGO BAY VERTICAL BULKHEAD BRACKET AT B.S. 947 LBL 12 IAW SOPM 20-50-01 AND BOEING DRAWING 149A8118 SH 14 AND IPC 53-11-51-01 92819U 20FEB19
FWD CARGO BAY AFT CORNER SCUFF PLATE IS BROKEN IN HALF / LOCATED AND DRILLED REPLACEMENT AFT CORNER SCUFF PLATE IN FWD CARGO BAY IAW DRAWING 143A8331. INSTALLATION WILL BE PERFORMED ON CUSTOMER CARD NBR 753-140-00-01Y 80570U 18FEB19
FWD CARGO BAY FWD CORNER SCUFF PLATE IS BROKEN IN HALF / LOCATED AND DRILLED REPLACEMENT SCUFF PLATE IN FWD CARGO BAY FWD CORNER IAW DRAWING 143A8331. INSTALLATION WILL BE PERFORMED ON CUSTOMER CARD NBR 753-140-00-01Y 80570U 18FEB19
SEAT TRACK CORRODED BETWEEN AT BS 540 TO BS 727B, LBL 45. R&R SEAT TRACK IAW SRM AND DWG.
PASSENGER CABIN SEAT TRACK CORRODED BETWEEN BS 540 TO BS 727B, LBL 24.5. R&R SEAT TRACK IAW SRM AND DWG.
PASSENGER CABIN SEAT TRACK CORRODED BETWEEN BS 540 TO BS 727B, RBL 24.5. R&R SEAT TRACK IAW DWG & SRM.
PASSENGER CABIN SEAT TRACK CORRODED BETWEEN BS 540 TO BS 727B, RBL 45. R&R SEAT TRACK IAW DWG & SRM.
EMERGENCY EXIT HATCH R/H SIDE FORWARD SIDE AT EMERGENCY EXIT SIGN LIGHT CONNECTION BROKEN. R&R CONNECTOR PER SWPM & WDM.
***CORROSION*** FUSELAGE CROWN EXTERNAL SKIN; BS 978 TO BS 1002; IN STR 1 FASTENER HOLES / FUSELAGE CROWN SKIN AT BS 978 TO BS 1002; STR 1 WAS REPAIRED IAW ATS ER 19-01789 REV IR DATED 20FEB19 AND EA 1-753-34224 REV IR
AFT CARGO BAY SIDE WALL SUPPORT CORRODED BETWEEN BS 727 TO BS 847, LT SIDE WL 156. REPAIRED SPLICE PER SRM AND DWG.
FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO BS 794, RBL 17. R&R SUPPORT IAW SRM AND DWG.
FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 867 TO BS 887, RBL 17. R&R SUPPORT IAW SRM AND DWG.
FORWARD CARGO RT SIDE FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D, RBL 25. R&R SUPPORT IAW SRM AND DWG.
FORWARD CARGO, FLOOR TO AFT BULKHEAD SUPPORT CORRODED AT BS 500D, BETWEEN RBL 25 TO LBL 25. R&R SUPPORT IAW SRM AND DWG.
FORWARD CARGO LT SIDE FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 400 TO BS 500D, LBL 25. REPAIRED SUPPORT IAW SRM AND DWG.
FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 847 TO BS 867, RBL 17. R&R SUPPORT IAW SRM & DWG.
FLOOR PANEL SPLICE STRIP CORRODED AT BS 887, BETWEEN LBL 17 TO RBL 17. R&R SPLICE STRIP IAW SRM AND DWG.
AFT CARGO BAY WALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 22. R&R SUPPORT IAW SRM & DWG.
AFT CARGO BAY SIDE WALL SUPPORT CORRODED BETWEEN BS 727 TO BS 847, LT SIDE WL 156. REPAIRED SUPPORT PER SRM AND DWG.
R1 DOOR NR 4 (LOWER) BEAM CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. R&R DOOR PER AMM.
RT WING NR 7 SLAT NOSE SKIN AT ACTUATOR RIB CRACKED AROUND THE FASTENER. REPAIRED SKIN IAW SRM.
RT WING NR 8 SLAT NOSE SKIN AT ACTUATOR RIB CRACKED AROUND THE FASTENER. REPAIRED SKIN IAW SRM.
LT WING FORWARD WING TO BODY FAIRING FORWARD UPPER ATTACH BRACKET CRACKED. R&R BRACKET PER SRM.
LT OVERWING EXIT DOOR HANDLE COVER CRACKED. R&R COVER PER AMM.
R2 DOOR SLIDE LOW PRESSURE. R&R SLIDE IAW MT.
DIVERSION/DECLARED EMERGENCY, ELECTRICAL SMELL IN AFT GALLEY AT FL 290. R&R RECIRCULATION FAN PER AMM.
R1 DOOR GIRT BAR LOOSE IN BRACKETS. SECURED BRACKET IAW AMM.
LEFT WING INBD LEADING EDGE PANEL 511AT DELAMINATED AT AFT OUTBD CORNER / REPAIRED PER SRM 51-30-10
L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW WO & MT.
ON DOWNWIND, SELECTED FLAP S 5. NOTICED FLAPS DID NOT EXTEND AND THERE WAS A VERY SMALL FLAP SPLIT. RECYCLED FLAPS BACK TO 0 THEN 5 AGAIN WITH NO CHANGE PROCEEDED IAW THE QRH AND DID A FLAPS UP LANDING WITH LED'S EXTENDED. AN EMERGENCY WAS DECLARED. R & R THE NR 3 FLAP SENSOR IAW AMM.
RAPID DEPRESSURIZATION AT FL 390 PRESSURE CONTROLLER BLANKED. MASKS DEPLOYED. NO AUTO FAIL LIGHT. DIVERTED AND DECLARED AN EMERGENCY. R & R THE CABIN PRESSURE SELECTOR PANEL IAW AMM.
LT SIDEWALL EMERGENCY EXIT CONNECTOR BROKEN. R&R CONNECTOR IAW SWPM & AMM.
L1 DOOR EMERGENCY EVAC SLIDE GIRT OUT OF POSITION. REPOSITIONED SLIDE ASSEMBLY IAW MT.
R1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.
OVERWING EMER EGRESS LIGHT INOPERATIVE. R & R BATTERY IAW AMM.
AFT ENTRY CEILING EMER EXIT LIGHT LOWER LENS MISSING. INSTALLED LENS IAW AMM.
RIGHT OVERWING EMER EXIT LIGHT INOPERATIVE. R & R BATTERY PACK IAW AMM.
RIGHT EEPLS CONNECTOR INOPERATIVE AT BS 641.9. SECURED CONNECTOR IAW AMM.
R1 DOOR EMER EXIT LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM.
R1 DOOR FWD FRAME LOWER CORNER CRACKED BS 295, WL 208 AT LOWER INBD FASTENER. R & R FRAME IAW EA.
RIGHT HORIZONTAL STABILIZER RIB 92.7 NR 3 STIFFENER LOWER SECTION CRACKED. REPAIRED RIB IAW SRM.
RIGHT HORIZONTAL STABILIZER RIB 92.7, NR 2 STIFFENER LOWER SECTION CRACKED. REPAIRED RIB IAW SRM.
RIGHT WING LOWER TE WAFFLE PLATE CRACKED JUST INBD OF NR 2 PYLON. R & R WAFFLE PLATE IAW SRM.
LEFT WING TRANSVERSE WEB CRACKED AT OTBD END JUST INBD OF PROGRAM ROLLER SUPPORT ARM ATTACH POINT. R & R WEB IAW SRM.
RIGHT WING UPPER TE SUPPORT ANGLE CRACKED AT TRANSVERSE WEB ATTACH POINT. R & R WEB IAW SRM.
LEFT WING TRANSVERSE WEB OTBD ATTACH ANGLE CRACKED AT PROGRAM ROLLER SUPPORT ARM ATTACH POINT. R & R ANGLE IAW SRM & DWG.
LEFT WING UPPER TE SUPPORT ANGLE CRACKED AT TRANSVERSE WEB LOWER ATTACH POINT. R & R ANGLE IAW SRM.
FRAME CRACKED AT BS 867, STRINGER 8L. REPAIRED FRAME IAW EA.
FRAME CRACKED AT BS 400, STRINGER 8R. REPAIRED FRAME IAW EA.
CENTER WING FWD SEAT TRACK INBD AFT HOLE CRACKED AT BS 727B, RBL 45.5. REPAIRED SEAT TRACK IAW EA & ER.
CENTER WING FWD SEAT TRACK INBD FWD HOLE CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA & ER.
VERTICAL PRESS WEB CRACKED AT BS 663, LBL 36. REPAIRED WEB IAW SRM.
CENTER BELLY DRAIN EXTERIOR DOUBLER CORRODED AT BS 727, WL 148.5. R & R DOUBLER IAW SRM & DWG.
CENTER BELLY DRAIN EXTERIOR DOUBLER CORRODED AT BS 727A, WL 148.5. R & R DOUBLER IAW SRM & DWG.
STRINGER CLIP CORRODED AT BS 1006, STRINGER 11L. R & R CLIP IAW SRM.