N732SW
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
363 reports on file, 2000-03-19 – 2022-12-20.
Part: TRAY — DISLODGED (SEAT 12D) · airframe 79,542 hrs · 46,984 cycles
ROW 12D TRAY TABLE IS DISLOCATED FROM THE ATTACHMENT ARM. REATTACHED SEAT 12D TRAY TABLE TO ATTACHMENT ARM IAW CMM 25-21-42.
Part: FLAP — DISCONNECTED (R1 DOOR SLIDE) · airframe 79,429 hrs · 46,905 cycles
CREW REPORTS FWD SERVICE DOOR MOUNTED SLIDE YELLOW FLAP ON RT SIDE NOT ATTACHED TO Z FOLD CORRECTLY. INSTALLED YELLOW FLAP TO DOOR SLIDE Z FOLD IAW MM 25-66-01; WITH NO OTHER DEFECTS.
Part: LIGHT — OUT OF POSITION (CABIN FLOOR) · airframe 78,454 hrs · 46,236 cycles
FRONT LEFT FLOOR PHOTO ILLUMINATION STRIP UNSTUCK FROM THE FLOOR / [01] RESECURED PHOTO ILLUMINATION STRIP PER CMM 25-00-66
Part: CIRCUIT BREAKER — POPPED (CABIN) · airframe 77,904 hrs · 45,867 cycles
SMOKE AND FUMES IN CABIN. QRH - SMOKE FIRE FUMES CHECK LIST COMPLETE. RETURN TO GATE / [01] C/W CONDITIONAL INSP AMM 05-51-56. FOUND RECIRC FAN CB POPPED. REF NONROUTINE TTG8Q00CYHKJ FOR FAN ASSY R&R
Part: PANEL — CRACKED (FUSELAGE) · airframe 77,643 hrs · 45,714 cycles
REF L/P 1995181; DAMAGE TO PANEL 194 GL ; MINOR CRACK (2ND) / [01] COMBINED THIS MINOR CRACK INTO THE FIRST CRACK PER ENGINEERING AND SRM 53-60-70-1A-1 FIG 104
Part: GIRT BAR — OUT OF POSITION (FWD SERVICE DOOR) · airframe 77,627 hrs · 45,703 cycles
FWD SERVICE DOOR SLIDE GIRT BAR NEEDS TO BE RESECURED / [01] REPOSITIONED GIRT BAR PER MM25-66-01.
Part: LIGHT — OUT OF POSITION · airframe 77,113 hrs · 45,387 cycles
RT. SIDE EMERGENCY EXIT LENS WONT STAY IN PLACE. / [01] REPLACED RT SIDE EMER. EXIT LIGHT ASSY PER AMM 33-51-04; CHECK GOOD.
Part: LIGHT — FAILED · airframe 76,749 hrs · 45,159 cycles
F/O SIDE EXIT SIGN FELL OFF IN THE EXIT ROW. ; / [01] RESECURED SIGN PER MM: 33-51-11.
Part: LIGHT — INOPERATIVE · airframe 76,650 hrs · 45,101 cycles
EMERGENCY LIGHT BATTERY?S FAILED CAPACITY TEST AT LOCATIONS M1672; M1673; M1669; M1670; M1668 ; EMERGENCY LIGHT ATTERY?S FAILED CAPACITY TEST AT LOCATIONS M1672; M1673; M1669; M1670; M1668 / [01] REPLACED EMERGENCY LIGHT BATTERY?S AT LOCATIONS M1672; M1673; M1669; M1670; M1668 PER AMM 33-51-06 WITH REFERENCE TO DWG 33500005; [02] C/W
Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 76,650 hrs · 45,101 cycles
HORIZONTAL STABILIZER L/H UPPER SLIDER SEAL CRACKED. REMOVED AND REPLACED L/H FWD UPPER SLIDING SEAL PER AMM 53-31-31
Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 76,650 hrs · 45,101 cycles
HORIZONTAL STABILIZER R/H UPPER SLIDER SEAL CRACKED. REMOVED AND REPLACED R/H FWD UPPER SLIDING SEAL PER AMM 53-31-31.
Earlier reports · 2000–2021 · 352 reports
2021
Part: PANEL — CRACKED (FUSELAGE)
FOUND 6 FASTENER HOLES WITH CRACKS. ; FOND 6 FASTENER HOLES WITH CRACKS ON 194E PANEL. / [01] REPLACED 194E PANEL
Part: SUPPORT WEB — CORRODED (BS 787-796) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON ACB FLOOR-TO-SIDEWALL SUPPORT WEB; BS 787-796; WL 160 ; / BLENDED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT WEB BS 787-792; RBL 22; WL 160. BLENDED 1'X1'X.020'; ORIGINAL THICKNESS IS .063'. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1.;INSTALLED NEW ACB FLOOR TO SIDEWALL SUPPORT WEB BS 787-792; RBL 22; WL 160 IAW SRM 51-40-02-0G-0; DWG# 146A8320.;LOCATED; DRILLED; DEBURRED NEW ACB FLOOR TO SIDEWALL SUPPORT WEB BS 787-792; RBL 22; WL 160 IAW SRM 51-40-05-0G-0; DWG# 146A8320. OK TO INSTALL;REMOVED SUPPORT WEB BS 787-792; RBL 22; WL 160 IAW SRM 51-40-02-0G-0;VERIFIED LOCATE; DRILL; DEBURR OF NEW ACB FLOOR TO SIDEWALL SUPPORT WEB IAW SRM 51-40-02 AND DWG 146A8320<BR>OK TO INSTALL;VERIFIED SRM REFS AND OUT OF LIMITS STATEMENT; VERIFIED REMOVAL OF PART PER SRM 51-40-02;VERIFIED ALL WORK COMPLETE;VERIFIED INSTALLATION OF NEW ACB FLOOR TO SIDEWALL SUPPORT WEB BS 787-792; RBL 22; WL 160 IAW SRM 51-40-02; DWG# 146A8320.
Part: WEB — CORRODED (BS 847-856) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON ACB FLOOR-TO-SIDEWALL SUPPORT WEB; BS 847-856; RBL 22; WL 160 ; / APPLIED A CHEMICAL CONVERSION COATING IAW SRM 51-20-01-0G-0 AND PRIMED NEW WEB IAW SOPM 20-41-02 AND DWG 146A8322; OK TO INSTALL;BLENDED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT WEB BS 847-856; RBL 22; WL 160. BLENDED 1'X1'X.020'; ORIGINAL THICKNESS IS .063'. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1.;EDITED MEASUREMENT TABLE;INSTALLED ACB FLOOR TO SIDEWALL SUPPORT WEB BS847 - BS856; RBL22; WL160 IAW SRM 51-40-02-0G-0 AND DWG 146A8321;LOCATED AND DRILLED NEW ACB FLOOR TO SIDEWALL SUPPORT WEB AT BS847 - BS856; RBL22; WL160 IAW SRM 51-40-05-0G-0 AND DWG 146A8321;OK TO INSTALL.;RECEIVED WEB IN FROM O.S.S; VERIFIED HEAT TREAT PER BAC5602 ON PO# 826173-SWA AND VERIFIED FABRICATION PER DWG 146A8322-12 ON PO# 826173-SWA;REMOVED SUPPORT WEB FROM BS 847-856; RBL 22; WL 160 IAW SRM 51-40-02-0G-0.
Part: GUSSET — CRACKED (BS 500D S22L) · airframe 74,727 hrs · 43,976 cycles
GUSSET AT BS 500D COMMON TO STR22L LBL53 WL170 IS CRACKED ; / ACCOMPLISHED STEP 8.;INSTALLED NEW GUSSET AT BS500D STR22L LBL53 WL170 IAW SRM 51-40-02 AND DWG #143A7902.;LOCATED; DRILLED; DEBURRED; APPLIED CHEMICAL CONVERSION COATING AND PRIMERED NEW GUSSET AT BS500D STR22L LBL53 WL170 IAW SRM 51-40-05 AND DWG #143A7902.;OK TO INSTALL NEW GUSSET AT BS500D STR22L LBL53 WL170.;PERFORMED RII INSPECTION ON INSTALLATION OF GUSSET.;RECEIVED FORMED GUSSET FROM OSS; PO# 826080.;REMOVED GUSSET BS 500D AT STR. 22L LBL 53; WL 170 PER SRM 51-40-02-0G-0.;VERIFIED INSTALLED NEW GUSSET AT BS500D STR22L LBL53 WL170 IAW SRM 51-40-02 AND DWG #143A7902.;VERIFIED RECEIVED FORMED GUSSET FROM OSS; PO# 826080.;OK TO INSTALL GIVEN.;UPDATED MEASUREMENT TABLE
Part: GUSSET — CRACKED (BS 500D S21L) · airframe 74,727 hrs · 43,976 cycles
GUSSET AT BS 500D COMMON TO STR21L LBL58 WL178 IS CRACKED ; / VERIFIED ALL WORK ACCOMPLISHED THIS CARD;VERIFIED INSTALLATION OF NEW GUSSET AT BS 500D STR-21L IAW SRM 51-40-02-0G-0 AND DWG 143A7902.;VERIFIED LOCATE AND DRILL OF NEW GUSSET AT BS 500D STR- 21L IAW SRM 51-40-05-0G-0 AND DWG 143A7902<BR><BR>OK TO INSTALL;INSTALLED NEW GUSSET AT BS 500D STR-21L IAW SRM 51-40-02-0G-0 AND DWG 143A7902.;LOCATED AND DRILLED NEW GUSSET AT BS 500D STR- 21L IAW SRM 51-40-05-0G-0 AND DWG 143A7902; OK TO INSTALL.;REMOVED DAMAGED GUSSET AT BS 500D STR-21L IAW SRM 51-40-02-0G-0.;UPDATED MEASUREMENTS TABLE
Part: GUSSET — CRACKED (BS 500D S19R) · airframe 74,727 hrs · 43,976 cycles
GUSSET AT BS500D COMMON TO STR19R IS CRACKED AT RBL60 WL192 ; / CERTIFIED STEP 8;LOCATED AND DRILLED NEW GUSSET FOR BS 500D STR 19 RBL 60 WL 192 IAW SRM 51-40-05-0G-0 OK TO INSTALL;REMOVED AND REPLACED CRACK DAMAGED GUSSET AT BS 500D STR 19 RBL 60 WL 192 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND BOEING DWG 143A7902 APPLIED CIC TO REPAIR AREA IAW AMM 51-21-91-620-802;REMOVED CRACK DAMAGED GUSSET AT BS 500D RBL 60 WL192 IAW SRM 51-40-02-0G-0;VERIFIED COMPLETE;VERIFIED INSPECTED AND OK TO INSTALL.;CORRECTED STEP 7 APPLIED CIC TO REPAIR AREA IAW AMM 51-21-91-620-802;INSTALLED NEW GUSSET AT BS 500D STR 19 LH LBL 60 WL 192 IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A7902 VERIFIED INSPECTED. INSTALLATION INSPECTED.;INSTALLED NEW GUSSET AT BS 500D STR 19 RBL60 WL 192 IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A7902;VERIFIED CIC APPLICATION AND INSTILLATION COMPLETE
Part: GUSSET — CRACKED (BS 500D S19L) · airframe 74,727 hrs · 43,976 cycles
GUSSET AT BS500D COMMON TO STR 19L IS CRACKED LBL 60; WL 192 ; / CERTIFIED FOR STEP 8;CORRECT STEP 7 APPLIED CIC TO REPAIR AREA IAW AMM 51-21-91-620-802;LOCATED AND DRILLED NEW GUSSET FOR BS 500D STR 19 LH WL 192 IAW SRM 51-40-05-0G-0 OK TO INSTALL;VERIFIED CORRECTIVE ACTION 1 AND 2; OK TO INSTALL GUSSET .;VERIFIED COMPLETE;INSTALLED NEW GUSSET AT BS 500D STR 19 LH LBL 60 WL 192 IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A7902;INSTALLED NEW GUSSET AT BS 500D STR 19 LH LBL 60 WL 192 IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A7902 VERIFIED INSPECTED.;INSTALLED NEW GUSSET AT BS 500D STR 19 LH LBL 60 WL 192 IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A7902 VERIFIED INSPECTED. VERIFIED INSTALLATION AND INSPECTED.;REMOVED AND REPLACED CRACK DAMAGED GUSSET AT BS 500D STR 19 LBL 60 WL 192 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND BOEING DWG 143A7902 APPLIED CIC TO REPAIR AREA IAW AMM 51-21-91-620-802;REMOVED CRACK DAMAGED GUSSET AT BS 500D STR 19 LH WL 192 IAW SRM 51-40-02-0G-0;VERIFIED CIC APPLICATION AND INSTALLATION COMPLETE
Part: SUPPORT — CORRODED (BS 947) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON AFT CARGO BAY AFT R/H BULKHEAD SUPPORT BS 947 RBL 24 WL 178 ; / EVALUATED CORROSION ON BULKHEAD SUPPORT BS 947 RBL 24 WL 178 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM. FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM REMOVED R/H BS 947 BULKHEAD SUPPORT PER SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW AFT CARGO BAY AFT R/H BULKHEAD SUPPORT BS947 RBL24 WL178 IAW SRM 51-40-05-0G-0; OK TO INSTALL VERIFIED LOCATED & DRILLED NEW AFT CARGO BAY AFT RT BULKHEAD SUPPORT BS947 RBL24 WL178 IAW SRM 51-40-05-0G-0. INSTALLED ACB RH BULKHEAD SUPPORT BS 947; RBL 21-41; WL 178 IAW SRM 51-40-02-0G-0; DWG# 149A8110; DWG#149A8117.
Part: SUPPORT ANGLE — CRACKED (BS 947) · airframe 74,727 hrs · 43,976 cycles
CRACKED WATER TANK SUPPORT ANGLE TO BS 947 BULKHEAD SUPPORT AT BS 947 LBL 11 WL 178 ; / INSTALLED NEW WATER TANK BULKHEAD SUPPORT ANGLE BS 947; LBL 11; WL 178 IAW SRM 51-40-02-0G-0; DWG# 149A8103.;LOCATED AND DRILLED NEW WATER TANK SUPPORT ANGLE TO BS947 BULKHEAD SUPPORT AT BS947 LBL11 WL178 IAW SRM 51-40-05-0G-0; OK TO INSTALL;VERIFIED LOCATED AND DRILLED NEW WATER TANK SUPPORT ANGLE TO BS947 BULKHEAD SUPPORT AT BS947 LBL11 WL178 IAW SRM 51-40-05-0G-0; OK TO INSTALL;VERIFIED ALL WORK COMPLETE;VERIFIED INSTALLATION OF NEW WATER TANK BULKHEAD SUPPORT ANGLE BS 947; LBL 11; WL 178 IAW SRM 51-40-02-0G-0; DWG# 149A8103;EVALUATED CRACK ON WATER TANK SUPPORT ANGLE FOUND TO BE OUT OF LIMITS FOUND OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS PER SRM 51-10-02-0G-0 REMOVED CRACKED ANGLE PER SRM 51-4-02-0G-0;UPDATED MEASUREMENT TABLE;VERIFIED
Part: CARGO TRACK — CORRODED (BS 927) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON RAIL AT AFT CARGO BAY BS927 RBL8 WL175. MARKED ; / CORRECTION REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS927 RBL8 WL175 NOT BS754;REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS754 RBL8 WL175 IN A 2'X.90' AREA; ORIGINAL THICKNESS .063; REMAINING THICKNESS .059; FOUND TO BE WITHOUT LIMITS IAW SRM 53-00-53-1A-2 PARA 4(A) 2 FIG.103 DEPTH GAGE ID ATS2473 S/N UNKNOWN; USED FOR MEASUREMENT;VERIFIED REFINISH;APPLIED CHEMICAL CONVERSION AND PRIMER TO BLENDED AREA IAW SRM51-20-01-0G-0 AND SOPM 20-41-02;CORRECTED BS927 FROM BS754;EVALUATION CONFIRMED; AT BS 927
Part: FLOOR SUPPORT — CORRODED (BS 927-947 RBL13) · airframe 74,727 hrs · 43,976 cycles
***CORROSION*** ON INTERCOSTAL AT AFT CARGO BAY BS927- BS947 RBL13 WL172. MARKED ; / INSTALLED NEW ACB INTERCOSTAL BS 927-947; LBL 13; WL 172 IAW SRM 51-40-02-0G-0; DWG# 147A7500;LOCATED; DRILLED; DEBURRED; APPLIED CHEMICAL CONVERSION COATING; AND PRIMED NEW ACB INTERCOSTAL BS 927-947; RBL 13; WL 172 IAW SRM 51-40-05-0G-0; DWG# 147A7500. OK TO INSTALL;RECEIVED FABRICATED INTERCOSTAL FROM OSS PO# 824879;VERIFIED DRILL UP; DEBURRING; AND CONVERSION COATING AND PRIMER. OK TO INSTALL.;VERIFIED MEASUREMENT TABLE; INTERCOSTAL FOUND TO BE OUT OF LIMITS AND REPLACEMENT PART PER SRM 51-10-02-0G;VERIFIED RECEIPT OF PART; MATERIAL TYPE/ THICKNESS/ TEMPER;EVALUATED CORROSION ON INTERCOSTAL BS927 TO BS947 RBL13 WL172 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;REMOVED INTERCOSTAL AT BS 947-927 RBL 13 W172 IAW SRM 51-40-02-0G-0;UPDATED MEASUREMENT TABLE;VERIFIED INSTALLATION OF NEW ACB INTERCOSTAL BS 927-947; LBL 13; WL 172 IAW SRM 51-40-02-0G-0; DWG# 147A7500
Part: CARGO TRACK — CORRODED (BS 754) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON RAIL AT AFT CARGO BAY BS754 LBL8 WL157. ; / COMPLETE;ET INSPECTED TRIM IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED.<BR><BR>IS000450 N500D;FABRICATED REPAIR SECTION OF RAIL AT AFT CARGO BAY BS727E - BS747+12 LBL8 WL157; MADE FROM BAC1509-100146#T76511 LOT#1458843-1 AND REPAIR SPLICE FROM SI#7530199 IAW SRM 53-00-53-2R-2 PARA 4 (I-O) OK TO INSTALL;INSTALLED RAIL SECTION AND SPLICES AT AFT CARGO BAY FROM BS727E+10 - BS747+12 LBL8 WL157 IAW SRM 53-00-53-2R-2 PARA 4 (P-S) AND DWG 146A7500;REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS754 LBL8 WL157 IN A 2'X.90' AREA; ORIGINAL THICKNESS .063; REMAINING THICKNESS .050; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARA 4(A) 2 FIG.103 DEPTH GAGE ID ATS2473 S/N UNKNOWN; USED FOR MEASUREMENT;REMOVED DAMAGE SECTION OF RAIL IN AFT CARGO BAY FROM BS727E+10 - BS747+12 IAW SRM 53-00-53-2R-2 PARA 4;REMOVED DAMAGE SECTION OF RAIL IN AFT CARGO BAY FROM BS727E+10 - BS747+12 LBL8 WL157 IAW SRM 53-00-53-2R-2;VERIFIED DAMAGE REMOVAL PER SRM;VERIFIED FABRICATION OF REPAIR SECTION PER SRM. VERIFIED OK TO INSTALL.;VERIFIED INSTALLATION OF RAIL SECTION AND SPLICES IAW SRM 53-00-53-2R-2 AND DWG 146A7500.;EVALUATION CONFIRMED
Part: CARGO TRACK — CORRODED (BS 747) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON TRACK TIEDOWN AT AFT CARGO BAY BS747 LBL17 WL157. ; / REMOVED CORROSION ON TOP SURFACE OF TRACK TIE DOWN; REMOVED 0.025 FROM MAX ALLOWABLE OF 0.020 IN 1'X1' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DEPTH GAUGE ID ATS1225 S/N UNKNOWN. TRACK TO BE REPLACED ON CUST CARD#TTG8Q0050UME; VERIFIED OUT OF LIMITS STATEMENT AND WORK TO BE ACCOMPLISHED ON CUST CARD# TTG8Q0050UME
Part: ANGLE — CRACKED (RT WING) · airframe 74,727 hrs · 43,976 cycles
RIGHT WING T/E PNL JUST AFT OF #2 PYLON VERT ANGLE IS CRACKED. ; / REMOVED AND REPLACED VERT ANGLE (FITTING; 115A2953-2) ON RIGHT WING T/E PANEL JUST AFT OF #2 PYLON IAW SRM 51-40-02-0G-0 PARA. 4 AND 9; AND AIPC 57-50-00-25.; VERIFIED REPLACEMENT OF VERT ANGLE (FITTING; 115A2953-2) ON RIGHT WING T/E PANEL JUST AFT OF #2 PYLON IAW SRM 51-40-02-0G-0 PARA. 4 AND 9; AND AIPC 57-50-00-25.
Part: CARGO TRACK — CORRODED (BS 727A) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON TRACK TIEDOWN AT AFT CARGO BAY BS727A LBL17 WL156. ; / REMOVED CORROSION ON TOP SURFACE OF TRACK TIE DOWN BS 727A LBL17 WL 156; REMOVED 0.025 FROM MAX ALLOWABLE OF 0.020 IN 1'X1' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DEPTH GAUGE ID ATS1225 S/N UNKNOWN. TRACK TO BE REPLACED ON CUST CARD#TTG8Q0050UME; VERIFIED OUT OF LIMITS STATEMENT AND WORK TO BE ACCOMPLISHED CUST CARD#TTG8Q0050UME
Part: SKIN — CORRODED (BS 674 RBL 4) · airframe 74,727 hrs · 43,976 cycles
CORROSION AROUND FWD FASTENER HOLE OF ADF #1 ANTENNA ; CORROSION ON ACFT SKIN AROUND FWD ; CENTER; FASTENER HOLE; OF ADF #1 ANTENNA BS 674; RBL 4; WL 308 / EVALUATED DAMAGE REMOVAL ON FUSELAGE SKIN AT BS 674; RBL 4; WL 308. MAX DEPTH OF DAMAGE REMOVAL FOUND TO BE 0.008'. DAMAGE FOUND TO BE OUT OF LIMITS PER ROW 44 SRM SUPPLEMENT ARM90-7023-01; REV B.;HFEC INSPECTED BLENDED AREAS PER 737NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS FOUND.;REFER TO EA 21-153-01387 SUMMARY REQUIREMENT; BARCODE: TTG8Q005EB1H.;REMOVED CORROSION ON AIRCRAFT SKIN AROUND FWD ; CENTER; FASTENER HOLE; OF ADF #1 ANTENNA AT BS 674; RBL 4; WL 308. DIMENSIONS OF DAMAGE REMOVAL FOUND TO BE 1' X 1' PER SRM 53-00-01-1A-1 AND ROW 44 SRM SUPPLEMENT ARM90-7023-01; REV B.;REQUEST NDI TO PERFORM HFEC INSPECTION OF BLENDED AREA ON AIRCRAFT SKIN AT BS 674; RBL 4; WL 308 TO VERIFY CRACK FREE CONDITION AND UT INSPECTION OF BLENDED AREA ON AIRCRAFT SKIN AT BS 674; RBL 4; WL 308 TO VERIFY REMAINING THICKNESS.;
Part: CARGO TRACK — CORRODED (BS 727D) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON TRACK TIEDOWN AT AFT CARGO BAY BS727D LBL17 WL156. ; / REMOVED CORROSION ON TOP SURFACE OF TRACK TIE DOWN BS 727D LBL 17 WL 156; REMOVED 0.025 FROM MAX ALLOWABLE OF 0.020 IN 1'X1' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DEPTH GAUGE ID ATS1225 S/N UNKNOWN. TRACK TO BE REPLACED ON CUST CARD#TTG8Q0050UME; VERIFIED OUT OF LIMITS STATEMENT AND WORK TO BE ACCOMPLISHED CUST CARD#TTG8Q0050UME
Part: ATTACH ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 74,727 hrs · 43,976 cycles
FWD SIDE OF BS 663 VAPOR BARRIER RH SIDE UPPER ATTACH ANGLE UPPER END CRACKED ; / ACCOMPLISHED STEPS 1 AND 2; VERIFIED STEPS 1 AND 2.
Part: SUPPORT — CORRODED (BS 727B-767) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727B - BS767 RBL21 WL157. ; / CORRECTIVE ACTION 9 WAS ENTERED IN ERROR CERTIFIED WORK PERFORMED FOR CORRECTIVE ACTION 11;OK TO INSTALL ACB RH FLOOR TO SIDEWALL SUPPORT BS727 TO BS 767.;REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 727B-767 RBL 21; DEEPEST DEPTH AT BS 747; REMOVED 0.015 FROM ORIG 0.040 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER ID4566A S/N UNKNOWN;VERIFIED INSTALLED- BS 947 BULKHEAD LOWER SUPPORT RBL 21 - LBL 7 PER SRM 51-40-02-0G-0 AND DWG # 149A8117 REV: -.;CARD COMPLETE;DAMAGE EVALUATED FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2;INSTALLED NEW RH FLOOR TO SIDEWALL SUPPORT BS727 TO BS767 IAW SRM51-40-02-0G-0 AND DWG 146A7500;LOCATED AND DRILLED NEW ACB RH FLOOR TO SIDEWALL SUPPORT BS727 TO BS767 IAW SRM 51-40-05-0G-0 SRM 51-40-02-0G-0;LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02; 51-40-05;OK TO INSTALL ACB RH FLOOR TO SIDEWALL SUPPORT BS727 TO BS 767;REMOVED ACB FLOOR TO SIDEWALL SUPPORT BS 727 TO 767 RH PER SRM 51-40-02-0G-0;VERIFIED INSTALLATION OF FLOOR TO SIDEWALL SUPPORT BS 727 - 767 IAW SRM 51-40-02-0G-0 AND DWG 146A7500.
Part: CARGO TRACK — CORRODED (BS 727D LBL 3) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON RAIL AT AFT CARGO BAY BS727D+6 LBL3 WL156. ; / APPLIED CHEMICAL CONVERSION COATING AND PRIMERED REPAIR PARTS @ BS 727D+6 LBL3 WL156 IAW SRM 53-00-53-2-2R.;ET INSPECTED CUT EDGE IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED.<BR><BR>CAL ID IS000450 N500D;INSTALLED REPAIR PARTS IN ACB BS727D+6 LBL3 WL156 IAW SRM 53-00-53-2R-2.;LOCATED; DRILLED; TRIMMED AND DEBURRED NEW REPAIR PARTS @ BS 727D+6 LBL3 WL156 IAW SRM 53-00-53-2R-2.;OK TO INSTALL REPAIR PARTS @ BS 727D+6 LBL3 WL156.;REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS727D+6 LBL3 WL156 IN A 2'X.90' AREA; ORIGINAL THICKNESS .063; REMAINING THICKNESS .053; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARA 4(A) 2 FIG.103 DEPTH GAGE ID ATS2473 S/N UNKNOWN; USED FOR MEASUREMENT;REMOVED RAIL UPPER JOGGLE IN A 3.1' AREA IN AFT CARGO BAY BS727D+6 LBL3 WL156 IAW SRM 53-00-53-2R-2;VERIFIED NDT WAS PREFORMED;VERIFIED DAMAGE REMOVAL PER SRM;VERIFIED FASTENER INSTALLATION;VERIFIED OK TO INSTALL NEW REPAIR PARTS;COMPLETE;EVALUATION AND ASSESSMENT CONFIRMED;VERIFIED; APPLIED CHEMICAL CONVERSION COATING AND PRIMERED REPAIR PARTS @ BS 727D+6 LBL3 WL156 IAW SRM 53-00-53-2-2R.;VERIFIED; LOCATED; DRILLED; TRIMMED AND DEBURRED NEW REPAIR PARTS @ BS 727D+6 LBL3 WL156 IAW SRM 53-00-53-2R-2.
Part: ATTACH ANGLE — CORRODED (BS 727D LBL 6) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON ATTACH ANGLE AT AFT CARGO BAY BS727D+10 LBL6 WL151. ; / CORRECTION TO STEP 7; SHOULD BE AMM NOT SRM.;INSTALLED ATTACH ANGLE BS 727D+ 10; LBL 6;WL 151 PER SRM51-40-02-0G-0; DWG 146A7730.;PRIMERED ATTACH ANGLE PER SRM 51-21-72-370-804; OK TO INSTALL.;REMOVED ATTACH ANGLE IN ACB BS 727D+10 LBL6 WL151 IAW SRM 51-40-02.;REFERENCE ESR:21-01944. FABRICATED ATTACH ANGLE AT BS727D+10; LBL6 WL151 USING BAC1493-672#7075-T62; LOT# 1370754-1; PER SRM 51-40-05-0G-0; DWG 146A7730; DWG 146A7734. APPLIED A CHEMICAL CONVERSION COATING PER AMM 51-21-41-370-802.;VERIFIED MEASUREMENT TABLE; ATTACH ANGLE FOUND TO BE OUT OF LIMITS AND REPLACEMENT PART PER SRM 51-10-02-0G;EVALUATED CORROSION ON ATTACH ANGLE BS727D+10 LBL6 WL151 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM51-10-02-0G-0;REMOVED ENGINEERING ROW DUE TO ENGINEERING NOT REQUIRED;UPDATED MEASUREMENT TABLE;VERIFIED PRIMERED ATTACH ANGLE PER AMM 51-21-72-370-804; OK TO INSTALL.;VERIFIED INSTALL OF ATTACH ANGLE BS 727D+ 10; LBL 6;WL 151 PER SRM51-40-02-0G-0; DWG 146A7730.;VERIFIED STEP 5.
Part: ATTACH ANGLE — CORRODED (BS 727D RBL 6) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON ATTACH ANGLE AT AFT CARGO BAY BS727D+10 RBL6 WL151. ; / PRIMERED ATTACH ANGLE PER SRM 51-21-72-370-804; OK TO INSTALL.;REMOVED ATTACH ANGLE IN ACB BS727D+10 RBL6 WL151 IAW SRM 51-40-02.;REFERENCE ESR: 21-01944; FABRICATED ATTACH ANGLE BS 727D+ 10 RBL6 WL151; USING BAC1493-672#7075-T62; LOT #1370754-1 PER SRM 51-40-05-0G-0; DWG 146A7734; DWG 146A7730; APPLIED A CHEMICAL CONVERSION COATING PER AMM 51-21-41-370-802.;VERIFIED MEASUREMENT TABLE; ATTACH ANGLE FOUND TO BE OUT OF LIMITS AND REPLACEMENT PART PER SRM 51-10-02-0G;CORRECTION TO STEP 7; SHOULD BE AMM NOT SRM.;EVALUATED CORROSION ON ATTACH ANGLE BS727D+10 RBL6 WL151 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;INSTALLED ATTACH ANGLE BS 727D + 10 RBL6 WL 151 PER SRM 51-40-02-0G-0; DWG 146A7730.;REMOVED ENGINEERING ROW DUE TO ENGINEERING NOT REQUIRED;UPDATED MEASUREMENT TABLE;VERIFIED PRIMERED ATTACH ANGLE PER AMM 51-21-72-370-804; OK TO INSTALL.;VERIFIED INSTALL OF ATTACH ANGLE BS 727D + 10 RBL6 WL 151 PER SRM 51-40-02-0G-0; DWG 146A7730.;VERIFIED STEP 5.
Part: CARGO TRACK — CORRODED (BS 727 RBL 3) · airframe 74,727 hrs · 43,976 cycles
***CORROSION*** ON RAIL AROUND FASTENER HOLE AT AFT CARGO BAY BS727+13 RBL3 WL156. ; / REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS727+13 RBL3 WL156 IN A 2'X.90' AREA; ORIGINAL THICKNESS .063; REMAINING THICKNESS .054; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARA 4(A) 2 FIG.103 DEPTH GAGE ID ATS2473 S/N UNKNOWN; USED FOR MEASUREMENT;REMOVED DAMAGE RAIL SECTION IN AFT CARGO BAY FROM BS727+4 - BS747+10 RBL3 WL156 IAW SRM 53-00-53-2R-2 PARA 4;VERIFIED DAMAGE REMOVAL PER SRM.;VERIFIED WORK TO BE ACCOMPLISHED ON CARD TTG8Q0050UMK;ALL OTHER WORK WILL BE PERFORMED ON FAULT # TTG8Q0050UMK;EVALUATION CONFIRMED
Part: INTERCOSTAL — CORRODED (BS 727A RBL 3) · airframe 74,727 hrs · 43,976 cycles
***CORROSION*** ON INTERCOSTAL AT AFT CARGO BAY BS727A+18 RBL3 WL150 ; / INSTALLED NEW INTERCOSTAL IN ACB BS727A+18 RBL3 WL150 IAW SRM 51-40-02 AND DWG #146A7510.;LOCATED; DRILLED; DEBURRED; AND APPLIED CHEMICAL CONVERSION COATING IAW SRM 51-40-05 AND DWG #146A7510.;PRIMERED NEW INTERCOSTAL @ BS727A+18 RBL3 WL150 IAW SRM 51-20-01-0G-0. OK TO INSTALL.;RECEIVED NEW INTERCOSTAL FOR ACB BS727A+18 RBL3 WL150 FROM OSS PO#824713-SWA.;REMOVED INTERCOSTAL IN ACB BS727A+18 RBL3 WL150 IAW SRM 51-40-02.;VERIFIED MEASUREMENT TABLE; INTERCOSTAL FOUND TO BE OUT OF LIMITS AND REPLACEMENT PART PER SRM 51-10-02-0G;EVALUATED CORROSION ON INTERCOSTAL BS727A+18 RBL3 WL150 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;UPDATED MEASUREMENT TABLE;VERIFIED RECEIVED NEW INTERCOSTAL FOR ACB BS727A+18 RBL3 WL150 FROM OSS PO#824713-SWA. AND VERIFIED LOCATED; DRILLED; DEBURRED; AND APPLIED CHEMICAL CONVERSION COATING IAW SRM 51-40-05 AND DWG #146A7510. VERIFIED APPLICATION OF PRIMER AND OK TO INSTALL;VERIFIED INSTALL OF NEW INTERCOSTAL IN ACB BS727A+18 RBL3 WL150 IAW SRM 51-40-02 AND DWG #146A7510.
Part: INTERCOSTAL — CORRODED (BS 727A LBL 17) · airframe 74,727 hrs · 43,976 cycles
***CORROSION*** ON INTERCOSTAL AT AFT CARGO BAY BS727A+2 LBL17 WL150 ; / INSTALLED NEW INTERCOSTAL IN ACB BS727A+2 LBL17 WL150 IAW SRM 51-40-02 AND DWG #146A7500.;LOCATED; DRILLED; AND DEBURRED NEW INTERCOSTAL AT BS 727A+2 LBL17 WL150 IAW SRM 51-40-05 AND DWG #146A7500. OK TO INSTALL.;RECEIVED NEW INTERCOSTAL FOR ACB BS727A+2 LBL17 WL150 PO #813866.;REMOVED INTERCOSTAL IN ACB BS727A+2 LBL17 WL150 IAW SRM 51-10-02;VERIFIED RECEIVED NEW INTERCOSTAL FOR ACB BS727A+2 LBL17 WL150 PO #813866. AND VERIFIED LOCATED; DRILLED; AND DEBURRED NEW INTERCOSTAL AT BS 727A+2 LBL17 WL150 IAW SRM 51-40-05 AND DWG #146A7500. OK TO INSTALL.;VERIFIED CORROSION ON INTERCOSTAL BS727+2 LBL17 WL150 IS OUT OF LIMITS AND REQUIRES REPLACEMENT DUE TO NO ALLOWABLE LIMITS IN THE SRM IAW SRM 51-10-02-0G.;EVALUATED CORROSION ON INTERCOSTAL BS727A+2 LBL17 WL150 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;UPDATED MEASUREMENT TABLE;VERIFIED INSTALL OF NEW INTERCOSTAL IN ACB BS727A+2 LBL17 WL150 IAW SRM 51-40-02 AND DWG #146A7500.
Part: ATTACH ANGLE — CRACKED (BS 633 BULKHEAD) · airframe 74,727 hrs · 43,976 cycles
FWD SIDE OF BS 663 VAPOR BARRIER RH SIDE UPPER ATTACH ANGLE UPPER END CRACKED ; / ACCOMPLISHED STEP 4 VERIFIED FASTENER INSTALLATION RII; COMPLETED ALL STEPS; VERIFIED EA IS COMPLETE (WIP 1)
Part: CARGO TRACK — CORRODED (BS 727D) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON RAIL AT AFT CARGO BAY BS727D+6 RBL8 WL156. ; / REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS727D+6 RBL8 WL156 IN A 2'X.90' AREA; ORIGINAL THICKNESS .063; REMAINING THICKNESS .051; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARA 4(A) 2 FIG.103 DEPTH GAGE ID ATS2473 S/N UNKNOWN; USED FOR MEASUREMENT;REMOVED DAMAGE SECTION OF RAIL IN AFT CARGO BAY AT BS727C+10-BS727E+10 RBL 8 WL 157 IAW SRM 53-00-53-2R-2. PARA 4;VERIFIED WORK TO BE ACCOMPLISHED ON CARD TTG8Q0050UMC;ALL OTHER WORK WILL BE ACCOMPLISHED ON FAULT #TTG8Q0050UMC;EVALUATION CONFIRMED
Part: CARGO TRACK — CORRODED (BS 727E) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON RAIL AROUND FASTENER HOLE AT AFT CARGO BAY BS727E+3 RBL8 WL157. ; / COMPLETED;ET INSPECTED TRIM IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED.<BR><BR>IS000450 N500D;INSTALLED RAIL SECTION AND SPLICES AT AFT CARGO BAY FROM BS727C+10 - BS727E+10 RBL8 WL157 IAW SRM 53-00-53-2R-2 PARA 4 (P-S) AND DWG 146A7500;LOCATED AND DRILLED REPAIR SECTION OF RAIL AT AFT CARGO BAY BS727C+10 - BS727E+10 RBL8 WL157 AND REPAIR SPLICES (2) EACH IAW SRM 53-00-53-2R-2 PARA 4 (I-O) OK TO INSTALL;RECEIVED CARGO RAIL FROM O.S.S; VERIFIED JOGGLED RAIL PER DWG 146A7503-4 ON PO# 824917-SWA AND VERIFIED DYE PENETRANT PER BAC5423 ON PO# 824917-SWA;REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS727E+3 RBL8 WL157 IN A 2'X.90' AREA; ORIGINAL THICKNESS .063; REMAINING THICKNESS .052; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARA 4(A) 2 FIG.103 DEPTH GAGE ID ATS2473 S/N UNKNOWN; USED FOR MEASUREMENT;REMOVED DAMAGE SECTION OF RAIL IN AFT CARGO BAY AT BS727C+10 - BS727E+10 RBL8 WL157 IAW SRM 53-00-53-2R-2;VERIFIED DAMAGE REMOVAL PER SRM;VERIFIED DAMAGE REMOVAL PER SRM;VERIFIED INSTALLATION OF RAIL SECTION AND SPLICES SRM 53-00-53-2R-2 AND DWG 146A7500.;VERIFIED LOCATION AND DRILLING OF REPAIR PARTS IAW SRM. VERIFIED OK TO INSTALL.;EVALUATION CONFIRMED
Part: CARGO TRACK — CORRODED (BS 727D) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON RAIL AT AFT CARGO BAY BS727D+6 RBL3 WL156. ; / COMPLETE;ET INSPECTED TRIM IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED.<BR><BR>IS000450 N500D;INSTALLED RAIL SECTION AND SPLICE AT AFT CARGO BAY FROM BS727+4 - BS747+10 RBL3 WL156 IAW SRM 53-00-53-2R-2 PARA 4 (P-S) AND DWG 146A7500;LOCATED AND DRILLED REPAIR SECTION OF RAIL AT AFT CARGO BAY BS727+4 - BS747+10 RBL3 WL156 AND REPAIR SPLICE IAW SRM 53-00-53-2R-2 PARA 4 (I-O) OK TO INSTALL;RECEIVED CARGO RAIL FROM O.S.S; VERIFIED JOGGLED RAIL PER DWG 146A7503-4 ON PO# 824918-SWA AND VERIFIED DYE PENETRANT PER BAC5423 ON PO# 824918-SWA;REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS727D+6 RBL3 WL156 IN A 2'X.90' AREA; ORIGINAL THICKNESS .063; REMAINING THICKNESS .053; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARA 4(A) 2 FIG.103 DEPTH GAGE ID ATS2473 S/N UNKNOWN; USED FOR MEASUREMENT;REMOVED DAMAGE SECTION OF RAIL IN AFT CARGO BAY FROM BS727+4 - BS747+10 RBL3 WL156 IAW SRM 53-00-53-2R-2;VERIFIED DAMAGE REMOVAL PER SRM;VERIFIED DAMAGE REMOVAL PER SRM.;VERIFIED INSTALLATION OF RAIL SECTION AND SPLICE IAW SRM 53-00-53-2R-2 AND DWG 146A7500.;VERIFIED LOCATION AND DRILLING OF RAIL SECTION PER SRM. VERIFIED OK TO INSTALL.;CORRECTED MATERIAL REMOVED FROM .015 TO .010;EVALUATION CONFIRMED
Part: CARGO TRACK — CORRODED (BS 727B) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON RAIL AROUND FASTENER HOLE AT AFT CARGO BAY BS727B+3 LBL12 WL156. ; / ADDING INSTALLATION REFERENCES TO STEP 10; ALSO USING DWG 146A7500 AND DWG 146A0061;CORRECTED LOCATION 727+4 TO 727B+10;ET INSPECTED CUT EDGE IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; ET INSPECTED HOLES IAW 737 NDTM PART 6 51-00-00 PROCEDURE 16; NO CRACKS NOTED.<BR><BR>CAL ID IS000450 N500D;INSTALLED RAIL AND REPAIR PARTS @ BS727B+3 LBL12 WL156 IAW SRM 53-00-53-2R-2.;LOCATED; DRILLED; TRIMMED; DEBURRED; APPLIED CHEMICAL CONVERSION COATING AND PRIMED REPAIR PARTS BS727+3 LBL12 WL156 IAW SRM 53-00-53-2R-2. OK TO INSTALL.;REQUEST HFEC INSPECTION ALONG CUT EDGES TO MAKE SURE THAT THERE ARE NO CRACKS IAW SRM 53-00-53-2R-2;REQUEST HFEC INSPECTION AT ALL REMOVED FASTENER LOCATIONS IAW SRM 53-00-53-2R-2.;REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS727B+3 LBL12 WL156 IN A 2'X.90' AREA; ORIGINAL THICKNESS .063; REMAINING THICKNESS .051; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARA 4(A) 2 FIG.103 DEPTH GAGE ID ATS2473 S/N UNKNOWN; USED FOR MEASUREMENT;REMOVED DAMAGE SECTION OF RAIL IN AFT CARGO BAY BS727+4 - BS727+10 LBL12 WL156 IAW SRM 53-00-53-2R-2;VERIFIED;VERIFIED DAMAGE REMOVAL PER SRM;VERIFIED DRILLED; DEBURRED; CHEM CONVERSION; PRIMER AND OK TO INSTALL.;CORRECTED TYPO CORRECTED BS LOCATION SHOULD BE 727B+10 NOT BS727+10;EVALUATION CONFIRMED;VERIFIED;VERIFIED INSTALLATION OF PARTS IAW SRM 53-00-53-2R-2; DWG 146A7500; 146A0061
Part: CARGO TRACK — CORRODED (BS 727B) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON TRACK TIEDOWN AT AFT CARGO BAY BS727B LBL17 WL156. ; / REMOVED CORROSION ON TOP SURFACE OF TRACK TIE DOWN BS 727B LBL17 WL 156; REMOVED 0.025 FROM MAX ALLOWABLE OF 0.020 IN 1'X1' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DEPTH GAUGE ID ATS1225 S/N UNKNOWN. TRACK TO BE REPLACED ON CUST CARD#TTG8Q0050UME; VERIFIED OUT OF LIMITS STATEMENT AND ALL WORK TO BE ACCOMPLISHED ON CARD # TTG8Q0050UME
Part: FLOOR SUPPORT — CORRODED (BS 727A) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS727A+18 LBL3 WL150 ; / CORRECTED LOCATION 727A TO 727B;INSTALLED NEW INTERCOSTAL IN ACB BS727+18 LBL3 WL150 IAW SRM 51-40-02 AND DWG #146A7510.;LOCATED; DRILLED; DEBURRED; APPLIED CHEMICAL CONVERSION COATING; AND PRIMERED REPAIR PARTS IAW SRM 51-40-05 AND DWG 146A7510. OK TO INSTALL;RECEIVED NEW INTERCOSTAL FOR ACB BS727A+18 LBL3 WL150 PO#786556.;REMOVED INTERCOSAL IN ACB BS 727A+18 LBL3 WL 150 IAW SRM 51-40-02.;VERIFIED;VERIFIED CORRECTED LOCATION 727A TO 727B;VERIFIED RECEIVED NEW INTERCOSTAL FOR ACB BS727A+18 LBL3 WL150 PO#786556. AND VERIFIED LOCATED; DRILLED; DEBURRED; APPLIED CHEMICAL CONVERSION COATING; AND PRIMERED REPAIR PARTS IAW SRM 51-40-05 AND DWG 146A7510. OK TO INSTALL;VERIFIED CORROSION IS OUT OF LIMITS AND REQUIRES REPLACEMENT DUE TO NO ALLOWABLE LIMITS IN SRM IAW SRM 51-10-02 OG-0.;EVALUATED CORROSION ON INTERCOSTAL AT BS727A+18 LBL3 WL150 WAS FOUND OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;UPDATED MEASUREMENT TABLE;VERIFIED INSTALL OF NEW INTERCOSTAL IN ACB BS727+18 LBL3 WL150 IAW SRM 51-40-02 AND DWG #146A7510.
Part: CARGO TRACK — CRACKED (BS 727E) · airframe 74,727 hrs · 43,976 cycles
CRACKED TRACK AT AFT CARGO BAY BS727E LBL17 WL156. ; / ASSIGNED PART TO JOB;EVALUATED CRACK ON CARGO TRACK BS 727E LBL 17 WL 156; CRACK FOUND TO BE 0.25 WITH ALLOWABLE DAMAGE OF 0.10. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;INSTALLED ACB CARGO TRACK BS727+4 TO BS867 LBL17 WL156 IAW SRM 51-40-02 AND DWG #146A7500.;LOCATED; DRILLED; AND DEBURRED ACB CARGO TRACK BS727+4 - BS 867; LBL17; WL 156 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG # 146A7500.;OK TO INSTALL ACB CARGO TRACK @ BS727+4 LBL17 WL156.;REMOVED ACB CARGO TRACK FROM BS727+4 - BS 867; LBL17; WL 156 IAW SRM 51-40-02-0G-0.;VERIFIED OUT OF LIMITS STATEMENT;OK TO INSTALL;UPDATED MEASUREMENT TABLE;VERIFIED LOCATED; DRILLED; AND DEBURRED ACB CARGO TRACK BS727+4 - BS 867; LBL17; WL 156 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG # 146A7500.;VERIFIED INSTALL OF ACB CARGO TRACK BS727+4 TO BS867 LBL17 WL156 IAW SRM 51-40-02 AND DWG #146A7500.
Part: SKIN — CORRODED (BS 702 RBL3) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON ACFT SKIN AROUND AFT LEFT FASTENER HOLE OF ADF # 1 ANTENNA ; CORROSION ON ACFT SKIN AROUND AFT; LEFT; FASTENER HOLE OF ADF #1 ANTENNA; BS 702; RBL 3; WL 308 / EVALUATED DAMAGE REMOVAL ON FUSELAGE SKIN AT BS 702; RBL 3; WL 308. MAX DEPTH OF DAMAGE REMOVAL FOUND TO BE 0.006'. DAMAGE FOUND TO BE OUT OF LIMITS PER ROW 44 SRM SUPPLEMENT ARM90-7023-01; REV B.;HFEC INSPECTED BLENDED AREA PER 737NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS FOUND.;REFER TO EA 21-153-01387 SUMMARY REQUIREMENT; BARCODE: TTG8Q005EB1H.;REFER TO FAULT TTG8Q0050L4B FOR REPAIR RESOLUTION.;REMOVED CORROSION ON AIRCRAFT SKIN AROUND AFT; LEFT FASTENER HOLE OF #1 ADF ANTENNA AT BS 702; RBL 3; WL 308. DAMAGE WAS REMOVED IN AN AREA OF 1' X 1' PER SRM 53-00-01-1A-1 AND ROW 44 SRM SUPPLEMENT ARM90-7023-01; REV B.
Part: CARGO TRACK — CORRODED (BS 727) · airframe 74,727 hrs · 43,976 cycles
***CORROSION*** ON RAIL AROUND FASTENER HOLE AT AFT CARGO BAY BS727+10 RBL3 WL156. ; / REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS727+10 RBL3 WL156 IN A 2'X.90' AREA; ORIGINAL THICKNESS .063; REMAINING THICKNESS .055; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARA 4(A) 2 FIG.103 DEPTH GAGE ID ATS2473 S/N UNKNOWN; USED FOR MEASUREMENT;REMOVED DAMAGE SECTION OF RAIL IN AFT CARGO BAY FROM BS727+4 - BS747+10 IAW SRM 53-00-53-2R-2 PARA 4;VERIFIED ALL PREVIOUS WORK ACCOMPLISHED AND DEFERRAL TO CARD# TTG8Q0050UMK;VERIFIED WORK TO BE ACCOMPLISHED ON CARD TTG8Q0050UMK;ALL OTHER WORK WILL BE ACCOMPLISHED ON FAULT # TTG8Q0050UMK;EVALUATION CONFIRMED
Part: ATTACH ANGLE — CRACKED (BS 663 BULKHEAD) · airframe 74,727 hrs · 43,976 cycles
FWD SIDE OF BS 663 VAPOR BARRIER RH SIDE UPPER ATTACH ANGLE UPPER END CRACKED. INSTALLED EWIS PROTECTION IAW AMM 20-60-07-913-801. REMOVED DAMAGE ON THE VAPOR BARRIER RH UPPER ATTACH ANGLE IAW SRM 57-10-10-2R-5. CONFORMED -1 REPLACEMENT ANGLE AND -2 SPLICE ANGLE PER SRM 57-10-10-2R-5 -1 REPLACEMENT ANGLE FABRICATED IAW SRM 57-10-10-2R REPAIR 5. REWORKED EDGES AND REPAIR PARTS IAW SRM 57-10-10-2R-5. DRILLED, TRIMMED & DEBAR REPAIR PARTS IAW SRM 57-1-10-10-2R-5. INSTALLED REPAIR IAW SRM 57-10-10-2R-5.
Part: CARGO TRACK — CORRODED (BS 754) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON RAIL AT AFT CARGO BAY BS754 RBL3 WL157. ; / REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS754 RBL3 WL157 IN A 2'X.90' AREA; ORIGINAL THICKNESS .063; REMAINING THICKNESS .053; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARA 4(A) 2 FIG.103 DEPTH GAGE ID ATS2473 S/N UNKNOWN; USED FOR MEASUREMENT;REMOVED DAMAGE SECTION OF RAIL IN AFT CARGO BAY FROM BS727+4 -BS747+10 RBL3 WL157 IAW SRM 53-00-53-2R-2 PARA 4;VERIFIED WORK TO BE ACCOMPLISHED ON CARD TTG8Q0050UMK;ALL OTHER WORK WILL BE PERFORMED ON FAULT # TTG8Q0050UMK;EVALUATION CONFIRMED
Part: SKIN — CORRODED (BS 674) · airframe 74,727 hrs · 43,976 cycles
CORROSION AROUND FWD FASTENER HOLE OF ADF #1 ANTENNA ; CORROSION ON ACFT SKIN AROUND FWD ; CENTER; FASTENER HOLE; OF ADF #1 ANTENNA BS 674; RBL 4; WL 308 / COMPLETED STEPS 4-8; COMPLETED AMT STEPS OF 21-153-01387-WIP1 (N732 - ATS(PAE) - REPAIR - FUSELAGE CROWN SKIN BLENDS AT ADF NO. 1 ANTENNA ATTACHMENT HOLES) [TTG8Q0056EMG].; STEP 12 FOD PROTECTION REMOVED. AREA CLEANED.
Part: SHIELD — CORRODED (BS 847-867 RBL21) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON AFT SHIELD AT AFT CARGO BAY BS847 - BS867 RBL21 WL163 ; / ADDED PART ASSIGNED TO JOB;EVALUATED CORROSION ON SHIELD BS 847-867 RBL 21 FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;INSTALLED NEW SHIELD ACB BS 847-867; RBL 21; WL 163 IN ACB IAW SRM 51-40-02-0G-0; DWG# 146A0081.;LOCATED; DRILLED; DEBURRED NEW SHIELD BS 847-867 RBL21 WL163 PER SRM51-40-05-0G-0; DWG 146A0081.;REMOVED AFT SHIELD AT AFT CARGO BAY BS 847-867 RBL21 WL163 PER SRM 51-40-02-0G-0.;VERIFIED ALL WORK COMPLETE;VERIFIED INSTALLATION OF NEW SHIELD IN ACB; BS 847-867; RBL 21; WL 163; IAW SRM 51-40-02-0G-0; DWG# 146A0081; REV C;DAMAGE FOUND TO BE OUT OF LIMITS; PART WILL BE REPLACED. PER SRM 51-10-02-0G-0;OK TO INSTALL NEW SHIELD BS 847-867; RBL 21; WL 163;OK TO INSTALL NEW SHIELD BS 847-867; RBL 21; WL 163 IN ACB;VERIFIED LOCATE; DRILLED; DEBURRED NEW SHIELD BS 847-867 RBL21 WL163 PER SRM51-40-05-0G-0; DWG 146A0081.
Part: FLOOR SUPPORT — CORRODED (BS 807 RBL 6) · airframe 74,727 hrs · 43,976 cycles
***CORROSION*** ON INTERCOSTAL AT AFT CARGO BAY BS807 RBL6 WL153. ; / APPLIED CHEMICAL CONVERSION COAT AND PRIMED TO FABRICATED PART I.A.W BOEING DWG 146A8132.OK TO INSTALL;CERTIFIED FOR STEP 3;INSTALLED NEW INTERCOSTAL BS 807-827; RBL 6; WL 153 IAW SRM 51-40-02-0G-0; DWG# 146A8130;RECEIVED INTERCOSTAL FROM FAB ON P.O #824835-SWA VERIFIED HEAT TREAT PER BAC5602 ON P;O #824835-SWA AND VERIFIED FAB PER DWG 146A8132-3 ON P.O #824835-SWA;REMOVED INTERCOSTAL BS 807-827; RBL6; WL 153 PER SRM 51-40-02-0G-0.;VERIFIED MEASUREMENT TABLE; INTERCOSTAL FOUND TO BE OUT OF LIMITS AND REPLACEMENT PART PER SRM 51-10-02-0G;EVALUATED CORROSION ON INTERCOSTAL BS807 RBL6 WL153 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-0G-0;LOCATED AND DRILLED NEW INTERCOSTAL AT ACB BS807 RBL6 WL153 I.A.W BOEING DWG 146A8130 AND SRM 51-40-05;UPDATED MEASUREMENT TABLE;UPDATED SRM REFERENCE TO 51-10-02-0G-0 IN CORRECTIVE ACTION 2;VERIFIED INSTALLATION OF NEW INTERCOSTAL BS 807-827; RBL 6; WL 153 IAW SRM 51-40-02-0G-0; DWG# 146A8130;VERIFIED STEPS 6;7; AND 8 OK TO INSTALL
Part: WEB — CORRODED (BS 809) · airframe 74,727 hrs · 43,976 cycles
***CORROSION*** ON WEB AT AFT CARGO BAY BS809 RBL19 WL159. ; / BS 847; RBL 19; WL 159 IAW SRM 51-40-02-0G-0.; [09] RECEIVED WEB PER P.O. #825119.; [10] VERIFIED STEP 9.; [11] RECEIVED WEB PER P.O. # 825689.; [12] LOCATED; DRILLED ;DEBURRED WEB PER SRM 51-40-05-0G-0; DWG 146A8120;DWG 146A8121. APPLIED A CHEMICAL CONVERSION COATING PER AMM 51-21-41-370-802.; [16] INSTALLED VERTICAL WEB BS 792-847 RBL 19;WL 159 PER SRM 51-40-02-0G-0; DWG 146A8120; DWG 146A8121
Part: CARGO TRACK — CORRODED (BS 934 LBL3) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS934 LBL3 WL179. ; / INSTALLED NEW ACB CARGO TRACK BS 887-947; LBL 3; WL 179 IAW SRM 51-40-02-0G-0; DWG# 147A7500.;LOCATED; DRILLED; AND DEBURRED NEW ACB CARGO TRACK BS 887-947; LBL 3; WL 179 IAW SRM 51-40-05-0G-0; DWG# 147A7500. OK TO INSTALL;VERIFIED DRILL UP AND DEBURR. OK TO INSTALL;VERIFIED INSTALLATION OF ACB TRACK BS887-947; LBL3; WL179. IAW SRM 51-40-02; DWG 147A7500;BLENDED CORROSION ON TRACK 1'X1' D=0.024' ORIGINAL THICKNESS 0.070 OUT OF LIMITS IAW SRM 53-00-53-1A-2 DET. 4C 2B;DAMAGE REMOVAL OUT OF LIMITS PER SRM 53-00-53-1A-2;REMOVED CARGO TRACK AT BS 947-887 LBL 3 WL 179 IAW SRM 51-40-02-0G-0;TOOL USED CALIPER ID ATS1317 S/N UNK DATE 06/2021;UPDATED DAMAGED TABLE;VERIFIED
Part: FLOOR SUPPORT — CORRODED (BS 848 RBL 6) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS848 RBL6 WL158. ; / APPLIED A CHEMICAL CONVERSION COATING AND PRIMED NEW INTERCOSTAL IAW BOEING DWG 146A8132 OK TO INSTALL;CORRECTED ITEM 6 LOCATED AND DRILLED NEW INTERCOSTAL AT ACB BS847 - BS867 RBL6 WL158 IAW BOEING DWG 146A8130;CORRECTION FROM ITEM 6; LOCATED AND DRILLED NEW INTERCOSTAL AT BS847- BS867 RBL6 WL158 IAW BOEING DWG 146A8130;CORRECTION LOCATED AND DRILLED NEW INTERCOSTAL AT BS847-BS867 RBL 6 WL158 IAW BOEING DWG 146A8130;INSTALLED NEW INTERCOSTAL BS 847-867 ; RBL 6; WL 153 IAW SRM 51-40-02-0G-0; DWG# 146A8130;LOCATED AND DRILLED NEW INTERCOSTAL AT ACB BS848 RBL6 WL158 IAW BOEING DWG 146A8130;RECEIVED NEW ACB INTERCOSTAL FROM FAB ON P;O#824809-SWA;VERIFIED FAB PER DWG 146A8132-5 ON P.O #824809-SWA;VERIFIED HEAT IAW BAC5602 ON P.O#824809-SWA;REMOVED INTERCOSTAL BS 847-867 RBL6 WL 158 PER SRM 51-40-02-0G-0.;VERIFIED MEASUREMENT TABLE; INTERCOSTAL FOUND TO BE OUT OF LIMITS AND REPLACEMENT PART PER SRM 51-10-02-0G;CORRECTION FROM ITEM 6 LOCATED AND DRILLED NEW INTERCOSTAL AT BS847-BS867 RBL 6 WL158 IAW BOEING DWG 146A8130;EVALUATED CORROSION ON INTERCOSTAL BS848 RBL6 WL158 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;UPDATED MEASUREMENT TABLE;VERIFIED INSTALLATION OF NEW INTERCOSTAL BS 847-867 ; RBL 6; WL 153 IAW SRM 51-40-02-0G-0; DWG# 146A8130;VERIFIED STEPS 5; 6; AND 7 OK TO INSTALL
Part: SUPPORT — CORRODED (BS 887-947) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS887 - BS947 RBL22 WL170. ; / INSTALLED NEW FLOOR TO SIDEWALL SUPPORT ABC BS 887-947; RBL 22; WL 170 IAW SRM 51-40-02-0G-0; DWG# 147A7500.;OK TO INSTALL NEW FLOOR TO SIDEWALL SUPPORT;OK TO INSTALL NEW FLOOR TO SIDEWALL SUPPORT; BS 887-947; RBL 22; WL 170;REMOVAL AND REPLACEMENT OF FLOOR TO SIDEWALL SUPPORT COMPLETE;REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 887-947 RBL 22; DEEPEST DEPTH AT BS 927 REMOVED 0.015 FROM ORIG 0.040 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USED MICROMETER ID4566A S/N UNKNOWN;DAMAGE EVALUATED FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2;LOCATED AND DRILLED NEW ACB FLOOR TO SIDEWALL SUPPORT BS887 TO BS 947 RH IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 DWG 147A7500;REMOVED ACB FLOOR TO SIDEWALL SUPPORT BS887-947 PER SRM 51-40-02-0G-0;VERIFIED INSTALLATION OF FLOOR TO SIDEWALL SUPPORT PER DWG 147A7500;VERIFIED LOCATE AND DRILLED NEW ACB FLOOR TO SIDEWALL SUPPORT BS887 TO BS 947 RH IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 DWG 147A7500.
Part: WEB — CORRODED (BS 807-832) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON SUBTHRESHOLD WEB AT AFT CARGO BAY BS807 - BS832 RBL25 WL169. ; / INSTALLED ACB SUB THRESHOLD WEB BS 794-847; RBL 25; WL 169 IAW SRM 51-40-02-0G-0; DWG# 146A8340.;LOCATED; DRILLED DEBURRED NEW SUBTHRESHOLD WEB; AFT CARGO BAY; BS 794- 847 RBL 25; WL 169; INSTALLED NUT PLATES PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 146A8340; DWG 146A8120.;OK TO INSTALL ACB SUB THRESHOLD WEB BS 794-847; RBL 25; WL 169;OK TO INSTALL ACB SUB THRESHOLD WEB BS 794-847; RBL 25; WL 169.;REMOVED AFT CARGO BAY SUBTHRESHOLD WEB BS 794-847 RBL25 WL 169 PER SRM 51-40-02-0G-0.;REMOVED CORROSION ON SUB THRESHOLD WEB BS 807-832 RBL 25. DEEPEST DEPTH AT BS 827 REMOVED 0.015 FROM ORIG 0.045 FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 USED MICROMETER ID4566A S/N UNKNOWN;VERIFIED ALL WORK COMPLETE;VERIFIED PROPER INSTALLATION OF ACB SUBTHRESHOLD WEB IAW SRM 51-40-02 AND DWG 146A8340;ASSIGNED PART TO JOB.;DAMAGE EVALUATED FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1;SUBTHRESHOLD WEB LOCATED AND DRILLED; NUT PLATES INSTALLED. IAW SRM51-40-02; 51-40-05; DWG 146A8340; 146A8120
Part: STRINGER CLIP — CORRODED (BS 737) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON STRINGER CLIP AT AFT CARGO BAY BS767 RBL15 WL151. FOUND OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM51-10-02-0G-0. REMOVED STRINGER CLIP IAW SRM 51-40-02-0G-0. FABRICATED STRINGER CLIP IAW SRM 51-40-05-0G-0, DWG146A1010, & DWG 146A1261. APPLIED A CHEMICAL CONVERSION COATING IAW SRM 51-21-41-370-802.PRIMED STINGER CLIP IAW SRM 51-21-72-370-804. INSTALLED STRINGER CLIP IAW SRM 51-40-02-0G-0 AND DWG 146A1261.
Part: FRAME — CORRODED (BS 947) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON FRAME AT AFT CARGO BAY BS947 LBL9 WL178. ; / EVALUATED CORROSION ON FRAME BS 947 LBL 9 WL 178. REMOVED 0.020 FROM ORIG 0.063 IN A 1'X2' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-07-1A-1 USED MICROMETER ID 4566A S/N UNKNOWN. FRAME TO BE REPLACED ON CUST CARD# TTG8Q0050GKX; VERIFIED CORROSION ON FRAME BS 947 LBL 9 WL 178. REMOVED 0.020 FROM ORIG 0.063 IN A 1'X2' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-07-1A-1 USED MICROMETER ID 4566A S/N UNKNOWN. FRAME TO BE REPLACED ON CUST CARD# TTG8Q0050GKX
Part: SUPPORT — CORRODED (BS 400-500D) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS400 - BS500D LBL24 WL157. ; / ALL STEPS COMPLETED;INSTALLED FCB LH FLOOR TO SIDEWALL SUPPORT BS400 TO BS500D IAW SRM51-40-02-0G-0 DWG143A7500;LOCATED AND DRILLED FCB FLOOR TO SIDEWALL SUPPORT LH BS400 TO 500D PER SRM 51-40-05-0G-0 SRM 51-40-02-0G-0 DWG 143A7500;OK TO INSTALL FCB LH FLOOR TO SIDEWALL; BS400 TO BS500D;REMOVED CORROSION FROM FCB L/H FLOOR TO SIDEWALL SUPPORT PLATE FROM BS 400 TO BS 500D NUMEROUS 1' X 1' AREAS REMOVED .010' FROM ORIGINAL THICKNESS OF .040 REMAINING THICKNESS OF .030' FOUND TO BE OUT OF LIMITS PER SRM-53-00-53-1A-2;REMOVED FCB L/H FLOOR TO SIDEWALL SUPPORT PLATE FROM BS 400 TO BS500D LBL24 WL157 PER SRM 51-40-02;USED MICROMETER ID#4566A S/N UNKNOWN;VERIFIED INSTALLATION OF FCB LH FLOOR TO SIDEWALL SUPPORT BS400 TO BS500D IAW SRM51-40-02-0G-0 DWG143A7500;VERIFIED LOCATE AND RILL OF FCB FLOOR TO SIDEWALL SUPPORT LH BS400 TO 500D PER SRM 51-40-05-0G-0 SRM 51-40-02-0G-0 DWG 143A7500;VERIFIED OK TO INSTALL;VERIFIED REMOVED CORROSION FROM FCB L/H FLOOR TO SIDEWALL SUPPORT PLATE FROM BS 400 TO BS 500D NUMEROUS 1' X 1' AREAS REMOVED .010' FROM ORIGINAL THICKNESS OF .040 REMAINING THICKNESS OF .030' FOUND TO BE OUT OF LIMITS PER SRM-53-00-53-1A-2
Part: ATTACH ANGLE — CRACKED (BS 500C) · airframe 74,727 hrs · 43,976 cycles
INTERCOSTAL ATTACH ANGLE CRACKED AT FWD CARGO BAY BS500C FWD SIDE LBL25 WL156. ; / REMOVED INTERCOSTAL ATTACH ANGLE IN FCB BS 500C FWD SIDE OF FRAME; LBL25; WL 156. LOCATED; DRILLED; DEBURRED; AND INSTALLED NEW ATTACH ANGLE IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG #143A7505.; VERIFIED INSTALLATION OF NEW ATTACH ANGLE PER SRM 51-40-02 AND DWG# 143A7505; VERIFIED ALL WORK; INCLUDING LOCATE; DRILL; DEBURR AND INSTALLATION OF NEW ATTACH ANGLE PER SRM 51-40-02 AND DWG 143A7505; NO FAULTS RAISED
Part: SUPPORT — CORRODED (BS 500A-500D) · airframe 74,727 hrs · 43,976 cycles
CORROSION IN MULTIPLE AREAS ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500A - BS500D RBL23 WL157. ; / OK TO INSTALL. NO OTHER DEFECTS NOTED IN GENERAL AREA.;INSTALLED FCB RH FLOOR TO SIDEWALL SUPPORT BS500A TO BS500D IAW SRM51-40-02-0G-0 DWG143A7500;LOCATED AND DRILLED FCB RH FLOOR TO SIDEWSLL SUPPORT BS 500A TO 500D PER SRM 51-40-05-0G-0 SRM 51-40-02-0G-0 ; DWG 143A7500;OK TO INSTALL FCB RH FLOOR TO SIDEWALL SUPPORT BS500A TO BS500D.;REMOVED CORROSION IN NUMEROUS 1'X1' AREAS FROM FCB R/H FLOOR TO SIDEWALL SUPPORT PLATE FROM BS500A TO BS500D RBL23 WL157 REMOVED 0.010 FROM ORIGINAL THICKNESS OF 0.040 REMAINING THICK OF 0.030 USING MICROMETER ID#4566A S/N UNKNOWN FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;REMOVED FCB R/H FLOOR TO SIDEWALL SUPPORT PLATE FROM BS500A TO BS500D RBL23 WL157 PER SRM 51-40-02;VERIFIED ALL STEPS COMPLETED;VERIFIED INSTALLATION FCB RH FLOOR TO SIDEWALL SUPPORT BS500A TO BS500D IAW SRM51-40-02-0G-0 DWG143A7500;VERIFIED LOCATE AND DRILL FCB RH FLOOR TO SIDEWSLL SUPPORT BS 500A TO 500D PER SRM 51-40-05-0G-0 SRM 51-40-02-0G-0 ; DWG 143A7500;VERIFIED REMOVED CORROSION IN NUMEROUS 1'X1' AREAS FROM FCB R/H FLOOR TO SIDEWALL SUPPORT PLATE FROM BS500A TO BS500D RBL23 WL157 REMOVED 0.010 FROM ORIGINAL THICKNESS OF 0.040 REMAINING THICK OF 0.030 USING MICROMETER ID#4566A S/N UNKNOWN FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2
Part: FLOORBEAM — CORRODED (BS 947) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT AT AFT CARGO BAY BS947 LBL8 TO RBL20 WL179. ; / INSTALLED AFT BULKHEAD TO FLOOR SUPPORT IN ACB BS 947; LBL 8 TO RBL 20; WL 179 IAW SRM 51-40-02-0G-0; DWG# 149A8110; DWG# 149A8117.;LOCATED AND DRILLED NEW AFT BULKHEAD TO FLOOR SUPPORT AT AFT CARGO BAY BS947 LBL8 TO RBL20 WL179 IAW SRM 51-40-05-0G-0; OK TO INSTALL;OK TO INSTALL NEW BULKHEAD TO FLOOR SUPPORT ACB BS 947. LBL 8 TO RBL 20; WL 179;VERIFIED LOCATED AND DRILLED NEW AFT BULKHEAD TO FLOOR SUPPORT AT AFT CARGO BAY BS947 LBL8 TO RBL20 WL179 IAW SRM 51-40-05-0G-0; OK TO INSTALL;VERIFIED ALL WORK ACCOMPLISHED;VERIFIED CORROSION ON BS947 AFT BULKHEAD TO FLOOR SUPPORT IS OUT OF LIMITS AND REQUIRES REPLACEMENT DUE TO NO ALLOWABLE LIMITS IN THE SRM IAW SRM 51-10-02-0G-0.;VERIFIED INSTALLATION OF AFT BULKHEAD TO FLOOR SUPPORT IN ACB BS 947; LBL 8 TO RBL 20; WL 179 IAW SRM 51-40-02-0G-0; DWG# 149A8110; DWG# 149A8117.;CORRECTED REFERENCE SHOULD BE SRM51-10-02-0G-0;EVALUATED CORROSION ON BS947 AFT BULKHEAD TO FLOOR SUPPORT; FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0G-0;REMOVED ACB AFT BULKHEAD TO FLOOR SUPPORT BS 947 LBL8 TO RBL20 PER SRM 51-40-02-0G-0;UPDATED DAMAGE TABLE
Part: FRAME — CORRODED (BS 947) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON FRAME AT AFT CARGO BAY BS947 RBL16 WL178. ; / EVALUATED CORROSION ON BS 947 FRAME RBL16 WL 178; FOUND 0.015 REMOVED FROM ORIG 0.063 IN A 1'X2' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-07-1A-1 USED MICROMETER ID4566A S/N UNKNOWN;LOCATED AND DRILLED NEW 947 FRAME STR 23R TO 23L PER SRM 51-40-05-0G-0 AND DRAWING 147A1047 OK TO INSTALL;REMOVED 947 BILGE FRAME STR 23R TO 23L PER SRM 51-40-02-0G-0;VERIFIED INSTALLED 947 FRAME STR 23R TO 23L PER SRM 51-40-02-0G-0 DWG 147A1047 DWG 147A0040 DWG 147A7410.;VERIFIED LOCATE AND DRILL OF NEW 947 FRAME PER SRM 51-40-05 AND DWG 147A1047; OK TO INSTALL;BEGAN INSTALLINGBS 947 FRAME PER SRM 51-40-02-0G-0 AND DWG 147A1047;INSTALLED 947 FRAME STR 23R TO 23L PER SRM 51-40-02-0G-0 DWG 147A1047 DWG 147A0040 DWG 147A7410;VERIFIED CORROSION ON BS 947 FRAME RBL16 WL 178; FOUND 0.015 REMOVED FROM ORIG 0.063 IN A 1'X2' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-07-1A-1 USED MICROMETER ID4566A S/N UNKNOWN
Part: INTERCOSTAL — CORRODED (BS 946) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS946 LBL3 WL172. ; / INSTALLED NEW ACB INTERCOSTAL BS 927-947; LBL 3; WL 172 IAW SRM 51-40-02-0G-0; DWG# 147A7500.;LOCATED; DRILLED; DEBURRED; APPLIED CHEMICAL CONVERSION COATING; AND PRIMED; NEW ACB INTERCOSTAL BS 927-947; LBL 3; WL 172 IAW SRM 51-40-05-0G-0; DWG# 147A7500; DWG# 147A7580. OK TO INSTALL;RECEIVED FABRICATED INTERCOSTAL FROM OSS PO#824877.;VERIFIED DRILL UP; DEBURR; CONVERSION COATING; AND PRIMER APPLICATION. OK TO INSTALL.;VERIFIED MEASUREMENT TABLE; INTERCOSTAL FOUND TO BE OUT OF LIMITS AND REPLACEMENT PART PER SRM 51-10-02-0G;VERIFIED RECEIPT OF PART; MATERIAL AND TEMPER;EVALUATED CORROSION ON INTERCOSTAL AT BS946 LBL3 WL172 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;REMOVED INTERCOSTAL AT BS 947-927 LBL 3 WL 172 IAW SRM 51-40-02-0G-0;UPDATED MEASUREMENT TABLE;VERIFIED INSTALLATION OF NEW ACB INTERCOSTAL BS 927-947; LBL 3; WL 172 IAW SRM 51-40-02-0G-0; DWG# 147A7500.
Part: SUPPORT — CORRODED (BS 867-887) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS867 - BS887 RBL21 WL169. ; / INSTALLED NEW FLOOR TO SIDEWALL SUPPORT ABC BS 867-887; RBL 21; WL 169 IAW SRM 51-40-02-0G-0; DWG# 146A7500.;OK TO INSTALL NEW FLOOR TO SIDEWALL SUPPORT;OK TO INSTALL NEW FLOOR TO SIDEWALL SUPPORT; BS 867-887; RBL 21; WL 169;REMOVAL AND REPLACEMENT COMPLETE;REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 867-887 RBL 21; DEEPEST DEPTH AT BS 877 REMOVED 0.015 FROM ORIG 0.040 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING MICROMETER ID4566A S/N UNKNOWN;VERIFIED INSTALLATION OF FLOOR TO SIDEWALL SUPPORT PER DWG 146A7500;DAMAGE EVALUATED FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2;LOCATED AND DRILLED NEW ACB RH FLOOR TO SIDEWALL SUPPORT BS867 TO BS887 IAW SRM51-40-05-0G-0; SRM 51-40-02-0G-0 DWG 146A7500;REMOVED ACB RH FLOOR TO SIDEWALL SUPPORT BS 867-887 PER SRM 51-40-02-0G-0;VERIFIED LOCATE AND DRILLED NEW ACB RH FLOOR TO SIDEWALL SUPPORT BS867 TO BS887 IAW SRM51-40-05-0G-0; SRM 51-40-02-0G-0 DWG 146A7500
Part: ATTACH ANGLE — CRACKED (BS 500B) · airframe 74,727 hrs · 43,976 cycles
INTERCOSTAL ATTACH ANGLE CRACKED AT FWD CARGO BAY BS500B FWD SIDE LBL25 WL156. ; / REMOVED DAMAGED INTERCOSTAL ATTACH ANGLE FCB BS 500B; LBL 25; WL 156. LOCATED; DRILLED; DEBURRED; AND INSTALLED NEW ATTACH ANGLE IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG # 143A7505; VERIFIED INSTALLATION OF NEW ATTACH ANGLE IAW SRM 51-40-02 AND DWG 143A7505; NO DEFECTS NOTED; VERIFIED REPLACEMENT; LOCATE; DRILL; AND DEBURR OF NEW ATTACH ANGLE IAW SRM 51-40-02; SRM 51-40-05-0G-0 AND DWG 143A7505
Part: WEB — CORRODED (BS 450-481) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON SUBTHRESHOLD WEB AT FWD CARGO BAY BS450 - BS481 RBL28 EL157. ; / INSTALLED NEW SUBTHRESHOLD WEB FCB BS440-492 RBL28 WL157 IAW SRM 51-40-02 AND DWG #143A8330;LOCATED; DRILLED; DEBURRED NEW SUBTHRESHOLD WEB FCB BS440-492 RBL 28; WL 157; INSTALLED NUT PLATES; PER SRM 51-40-02-0G-0;SRM 51-40-05-0G-0; DRAWING 143A8330.;OK TO INSTALL NEW SUBTHRESHOLD WEB FCB BS440-492 RBL28 WL157.;OK TO CLOSE FCB SUBTHRESHOLD WEB;REMOVED CORROSION ON SUBTHRESHOLD WEB IN NUMEROUS 1'X1' AREAS; REMOVED 0.010 FROM ORIG 0.045 FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1. USED MICROMETER ID4566A. S/N UNKNOWN;UPDATED PARTS TABLE;VERIFIED INSTALLATION OF NEW SUBTHRESHOLD WEB FCB BS440-492; RBL28; WL157; IAW SRM 51-40-02 AND DWG #143A8330;VERIFIED REMOVED CORROSION ON SUBTHRESHOLD WEB IN NUMEROUS 1'X1' AREAS; REMOVED 0.010 FROM ORIG 0.045 FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1. USED MICROMETER ID4566A. S/N UNKNOWN;VERIFIED ALL WORK COMPLETE;REMOVED FCB SUB THRESHOLD WEB PER SRM 51-40-02-OG-0;VERIFIED LOCATED; DRILLED; DEBURRED NEW SUBTHRESHOLD WEB FCB BS440-492 RBL 28; WL 157; INSTALLED NUT PLATES; PER SRM 51-40-02-0G-0;SRM 51-40-05-0G-0; DRAWING 143A8330.
Part: SUPPORT ANGLE — CORRODED (BS 500D RBL 24) · airframe 74,727 hrs · 43,976 cycles
CORROSION AT FWD CARGO BAY ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE BS500D RBL24 WL157. ; / EVALUATED CORROSION ON AFT BULKHEAD SUPPORT ANGLE BS 500D RBL 24 WL 157; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES TO BE REPLACED PER SRM 51-10-02-0G-0;INSTALLED FWD CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT ANGLE BS500D RBL24 WL157 IAW DWG 143A9481; DWG 143A7902 AND SRM 51-40-02-0G-0;LOCATED; DRILLED; DEBURRED NEW BULKHEAD SUPPORT ANGLE PER SRM 51-40-05-0G-0; DRAWING 143A7902; DRAWING 143A9481.;OK TO INSTALL RH BULKHEAD SUPPORT; BS 500D; RBL 24;REMOVED FCB AFT BULKHEAD SUPPORT BS 500D RBL 24 PER SRM 51-40-02-0G-0;VERIFIED INSTALLATION OF FWD CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT ANGLE BS500D RBL24 WL157 IAW DWG 143A9481; DWG 143A7902 AND SRM 51-40-02-0G-0;VERIFIED CARD COMPLETE;VERIFIED CORROSION ON AFT BULKHEAD SUPPORT ANGLE BS 500D RBL 24 WL 157; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES TO BE REPLACED PER SRM 51-10-02-0G-0;UPDATED PARTS TABLE;VERIFIED LOCATED; DRILLED; DEBURRED NEW BULKHEAD SUPPORT ANGLE PER SRM 51-40-05-0G-0; DRAWING 143A7902; DRAWING 143A9481.
Part: CARGO TRACK — CORRODED (BS 944 RBL 3) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON TRACK TIEDOWN AT AFT CARGO BAY BS944 LBL3 WL179. ; / VERIFIED CARGO TRACK TO BE IN LIMITS. TRACK WILL BE REPLACED ON FAULT #TTG8Q005GLQ.;DAMAGED REMOVED BS 944 LBL3 WL179 ON TRACK TIE DOWN FOUND OUT OF LIMITS DUE TRACK TO REPLACED 1'X1' D= 0.04' ORIGINAL THICKNESS 0.270 IAW SRM 53-00-53-1A-2 PAR. 4B 2 TOOL USED ATS1317 S/N UNK DATE 06/2021;DUE TO AFT CARGO TIE DOWN TRACK BEING FOUND OUT OF LIMITS TRACK WILL BE REMOVED AND REPLACED FROM BS 887 TO BS 947 LBL3 ON FAULT # TTG8Q0050GLQ;DUE TO CARGO TRACK BEING FOUND OUT OF LIMITS ON FAULT # TTGQQ0050GLQ CARGO TRACK WILL BE REMOVED AND REPLACED FROM BS 887 TO BS 947 LB3 ON FAULT #TTG8Q0050GLQ NO FURTHER ACTION REQUIRED ON THIS FAULT;REMOVED CORROSION ON AFT CARGO TIE DOWN TRACK AT BS 944 LBL3 WL 179 IN A 1' X 1' AREA REMOVED 0.04' ORIGINAL THICKNESS IS 0.270 FOUND TO BE IN LIMITS PER SRM 53-00-53-1A-2 MEASURING TOOL ID # 1317 S/N UNKNOWN;UPDATED DAMAGED TABLE
Part: SUPPORT ANGLE — CORRODED (BS 847-867) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON BULKHEAD TO FLOOR SUPPORT ANGLE AT AFT CARGO BAY BS847 - BS867 LBL13 WL163. ; / CARD COMPLETE;OK TO INSTILL ANGLE;OK TO INSTILL ANGLE GIVEN;VERIFIED INSTALLED ACB BULKHEAD TO FLOOR SUPPORT ANGLE BS847 TO BS867LBL13 WL 163 IAW SRM51-40-02-0G-0 AND DWG 149A8102;CERTIFIED;CORRECTED BS FROM BS 887 TO BS867 ON CORRECTIVE ACTION #2;EVALUATED CORROSION ON BULKHEAD TO FLOOR SUPPORT ANGLE BS847 TO BS887 LBL13 WL163 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;EVALUATION CONFIRMED;INSTALLED ACB BULKHEAD TO FLOOR SUPPORT ANGLE BS847 TO BS867LBL13 WL 163 IAW SRM51-40-02-0G-0 AND DWG 149A8102;LOCATED AND DRILLED NEW BULKHEAD TO FLOOR SUPPORT ANGLE ACB BS847 TO BS867 LBL13 IAW SRM 51-40-05-0G-0 SRM 5140-02-0G-0 DWG149A8102;UPDATED MEASUREMENT TABLE;VERIFIED LOCATE AND DRILLED NEW BULKHEAD TO FLOOR SUPPORT ANGLE ACB BS847 TO BS867 LBL13 IAW SRM 51-40-05-0G-0 SRM 5140-02-0G-0 DWG149A8102
Part: STRINGER CLIP — CORRODED (BS 787) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON STRINGER CLIP AT AFT CARGO BAY BS787 RBL6 WL153. ; / FABRICATED STRINGER CLIP AT BS787 RBL6 WL 153; USING BAC1493-878#7075T62; LOT #1459381-2 PER SRM 51-40-05-0G-0; DWG 146A8133; DWG 146A8130. APPLIED A CHEMICAL CONVERSION COATING PER AMM 51-21-41-370-802.;INSTALLED STRINGER CLIP PER SRM 51-40-02-0G-0; DWG 146A8130.;PRIMERED STRINGER CLIP PER SRM 51-21-72-370-804; OK TO INSTALL.;VERIFIED MEASUREMENT TABLE; STRINGER CLIP FOUND TO BE OUT OF LIMITS AND REPLACEMENT PART PER SRM 51-10-02-0G.;CORRECTION TO STEP7; SHOULD BE AMM NOT SRM.;EVALUATED CORROSION ON STRINGER CLIP AT BS787 RBL6 WL153 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM51-10-02-0G-0;REMOVED STRINGER CLIP BS 787; RBL6; WL 153 PER SRM 51-40-02-0G-0.;UPDATED MEASUREMENT TABLE;VERIFIED PRIMERED STRINGER CLIP PER AMM 51-21-72-370-804; OK TO INSTALL.;VERIFIED INSTALL OF STRINGER CLIP PER SRM 51-40-02-0G-0; DWG 146A8130.;VERIFIED STEP 5.
Part: ATTACH ANGLE — CORRODED (BS 787) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON ATTACH ANGLE AT AFT CARGO BAY BS787 LBL6 WL153. ; / FABRICATED ATTACH ANGLE AT BS 787 LBL6 WL153 USING BAC 1490-2815#7075-T62 LOT# 1455929-2 PER SRM 51-40-05-0G-0; DWG 146A1320; DWG 146A7810. APPLIED A CHEMICAL CONVERSION COATING PER AMM 51-21-41-370-802.;INSTALLED ATTACH ANGLE BS787 LBL 6; WL 153; PER SRM 51-40-02-0G-0; DWG 146A7810.;PRIMERED ATTACH ANGLE PER AMM 51-21-72-370-804; OK TO INSTALL.;RECEIVED EXTRUSION FROM HEAT TREAT; P.O. #824916;REMOVED ATTACH ANGLE AT BS 787 LBL6 WL153 PER SRM 51-40-02-0G-0.;VERIFIED MEASUREMENT TABLE; ATTACH ANGLE FOUND TO BE OUT OF LIMITS AND REPLACEMENT PART PER SRM 51-10-02-0G;EVALUATED CORROSION ON ATTACH ANGLE BS787 LBL6 WL153 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;UPDATED MEASUREMENT TABLE;VERIFIED PRIMERED ATTACH ANGLE PER AMM 51-21-72-370-804; OK TO INSTALL.;VERIFIED INSTALL OF ATTACH ANGLE BS787 LBL 6; WL 153; PER SRM 51-40-02-0G-0; DWG 146A7810.;VERIFIED STEPS 5 AND 6
Part: SHIELD — CORRODED (BS 767-787) · airframe 74,727 hrs · 43,976 cycles
***CORROSION*** ON FWD SHIELD AT AFT CARGO BAY BS767 - BS787 RBL22 WL157. ; / CARD COMPLETE;EVALUATED CORROSION ON SHIELD BS 767-787 RBL 22; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;INSTALLED NEW ACB FWD SHIELD BS 767-794; RBL 22; WL 157 IAW SRM 51-40-02-0G-0; DWG# 146A0081.;LOCATED ;DRILLED; DEBURRED NEW SHIELD BS 767-794 RBL22 WL157 PER SRM 51-40-05-0G-0; DWG 146A0081.;OK TO INSTALL ACB SHIELD BS 767-794; RBL 22; WL 157;REMOVED FWD SHIELD AT AFT CARGO BAY ;BS 767- 794 RBL22 WL 157 PER SRM 51-40-02-0G-0.;VERIFIED INSTALLED NEW ACB FWD SHIELD BS 767-794; RBL 22; WL 157 IAW SRM 51-40-02-0G-0; DWG# 146A0081.;DAMAGE FOUND TO BE OUT OF LIMITS; PART WILL BE REPLACED. PER SRM 51-10-02-0G-0;OK TO INSTALL ACB SHIELD BS 767-794; RBL 22; WL 157;VERIFIED LOCATE ;DRILLED; DEBURRED NEW SHIELD BS 767-794 RBL22 WL157 PER SRM 51-40-05-0G-0; DWG 146A0081.
Part: CARGO TRACK — CORRODED (BS 767) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON RAIL AT AFT CARGO BAY BS767+6 LBL3 WL157. ; / APPLIED CHEMICAL CONVERSION COATING AND PRIMERED BARE EDGES OF NEW REPAIR PARTS @ BS767+6 WL157 IAW SRM 53-00-53-2R-2.;CORRECTION RAIL AT AFT CARGO BAY BS767+6 LBL8 WL157 REINFORCEMENT ANGLE IS FOUND TO BE OUT OF LIMITS DUE TO NO SRM LIMITS; REPLACEMENT OF PART REQUIRED IAW SRM 51-10-02-0G-0 PARA 9;INSTALLED REPAIR PARTS IN ACB @ BS767+6 LBL3 WL157 IAW SRM 53-00-53-2R-2. REFERENCE TSR #2021002642;LOCATED; DRILLED; TRIMMED; AND DEBURRED NEW REPAIR PARTS @ BS767+6 LBL3 WL157 IAW SRM53-00-53-2R-2.;OK TO INSTALL REPAIR PARTS @ BS767+6 LBL3 WL 157.;RAIL AT AFT CARGO BAY BS767+6 LBL3 WL157 REINFORCEMENT ANGLE IS FOUND TO BE OUT OF LIMITS DUE TO NO SRM LIMITS; REPLACEMENT OF PART REQUIRED IAW SRM 51-10-02-0G-0 PARA 9;REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS767+6 LBL3 WL157 IN A 2'X.90' AREA; ORIGINAL THICKNESS .063; REMAINING THICKNESS .052; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARA 4 (A) 2 FIG. 103. DEPTH GAGE ID ATS2473 S/N UNKNOWN USED FOR MEASUREMENT;REMOVED REINFORCEMENT ANGLE AT BS767+6 LBL3 WL157 IAW SRM 51-40-02-0G-0;VERIFIED FASTENER INSTALLATION;VERIFIED OK TO INSTALL PARTS;VERIFIED; APPLIED CHEMICAL CONVERSION COATING AND PRIMERED BARE EDGES OF NEW REPAIR PARTS @ BS767+6 WL157 IAW SRM 53-00-53-2R-2.;VERIFIED; LOCATED; DRILLED; TRIMMED; AND DEBURRED NEW REPAIR PARTS @ BS767+6 LBL3 WL157 IAW SRM53-00-53-2R-2.;COMPLETE;RAIL AT REINFORCEMENT ANGLE EVALUATION CONFIRMED
Part: SUPPORT ANGLE — CORRODED (BS 500D RBL 23) · airframe 74,727 hrs · 43,976 cycles
***CORROSION*** ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT FWD CARGO BAY BS500D RBL23 WL157. ; / FOUND FCB AFT BULKEAD SUPPORT ANGLE BS500D RBL23 WL 157 OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM; FWD CARGO BAY AFT BULKHEAD FLOOR TO SIDEWALL SUPPORT ANGLE AT BS500D LBL20 WILL BE REMOVED AND REPLACED ON FAULT TTG8Q0050GGV; VERIFIED OUT OF LIMITS AND TO BE CORRECTED ON FAULT TTG8Q0050GGV
Part: CARGO TRACK — CORRODED (BS 767 LBL 8) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON RAIL AT AFT CARGO BAY BS767+6 LBL8 WL157. ; / APPLIED CHEMICAL CONVERSION COATING AND PRIMERED BARE EDGES OF NEW REPAIR PARTS @ BS767+6 LBL8 WL157 IAW SRM 53-00-53-2R-2.;CORRECTION RAIL AT AFT CARGO BAY BS767+6 LBL8 WL157 REINFORCEMENT ANGLE IS FOUND TO BE OUT OF LIMITS DUE TO NO SRM LIMITS; REPLACEMENT OF PART REQUIRED IAW SRM 51-10-02-0G-0 PARA 9;INSTALLED REPAIR PARTS IN ACB BS767+6 LBL8 WL157 IAW SRM 53-00-53-2R-2. REFERENCE TSR #2021002642;LOCATED; DRILLED; TRIMMED AND DEBURRED NEW REPAIR PARTS @ BS767+6 LBL8 WL157 IAW SRM 53-00-53-2R-2.;OK TO INSTALL REPAIR PARTS @ BS 767+6 LBL8 WL157.;RAIL AT AFT CARGO BAY BS767+6 LBL8 WL157 REINFORCEMENT ANGLE IS FOUND TO BE OUT OF LIMITS DUE TO NO SRM LIMITS; REPLACEMENT OF PART REQUIRED IAW SRM 51-10-02-0G-0 PARA 9;RAIL AT REINFORCEMENT ANGLE DAMAGE OUT OF LIMITS CONFIRMED;REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS767+6 LBL8 WL157 IN A 2'X.90' AREA; ORIGINAL THICKNESS .063; REMAINING THICKNESS .053; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 PARA 4(A) 2 FIG.103 DEPTH GAGE ID ATS2473 S/N UNKNOWN; USED FOR MEASUREMENT;REMOVED REINFORCEMENT ANGLE AT BS767+6 LBL8 WL157 IAW SRM 51-40-02-0G-0;VERIFIED OK TO INSTALL PARTS;VERIFIED REPAIR INSTALLATION;COMPLETE;VERIFIED; APPLIED CHEMICAL CONVERSION COATING AND PRIMERED BARE EDGES OF NEW REPAIR PARTS @ BS767+6 LBL8 WL157 IAW SRM 53-00-53-2R-2.;VERIFIED; LOCATED; DRILLED; TRIMMED AND DEBURRED NEW REPAIR PARTS @ BS767+6 LBL8 WL157 IAW SRM 53-00-53-2R-2.
Part: INTERCOSTAL — CORRODED (BS 928 RBL 3) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS928 RBL3 WL172. ; / INSTALLED NEW INTERCOSTAL ACB BS 927-947; RBL 3; WL 172 IAW SRM 51-40-02-0G-0; DWG# 147A7500.;LOCATED; DRILLED; AND DEBURRED NEW ACB INTERCOSTAL BS 927-947; RBL 3; WL 172 IAW SRM 51-40-05-0G-0; AND DWG# 147A7500. OK TO INSTALL;VERIFIED DRILL UP AND DEBURR. OK TO INSTALL;VERIFIED INSTALLATION OF INTERCOSTAL;EVALUATED CORROSION ON INTERCOASTAL AT BS928 RBL3 WL172 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;EVALUATION CONFIRMED;REMOVED INTERCOSTAL AT BS 947-927 RBL 3 WL 172 IAW SRM 51-40-02-0G-0;UPDATED MEASUREMENT TABLE
Part: FRAME — CORRODED (BS 947) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON FRAME AT AFT CARGO BAY BS947 RBL10 WL178. ; / EVALUATED CORROSION ON BS 947 FRAME RBL 10 WL 178; REMOVED 0.015 FROM ORIG 0.063 IN 1'X2' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-07-1A-1 USED MICROMETER ID4566A S/N UNKNOWN. FRAME TO BE REPLACED ON CUST CARD# TTG8Q0050GKX; VERIFIED CORROSION ON BS 947 FRAME RBL 10 WL 178; REMOVED 0.015 FROM ORIG 0.063 IN 1'X2' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-07-1A-1 USED MICROMETER ID4566A S/N UNKNOWN. FRAME TO BE REPLACED ON CUST CARD# TTG8Q0050GKX; FRAME TO BE REPLACED ON CUST CARD# TTG8Q0050GKX
Part: SHIELD — CORRODED (BS 420-440 RBL24) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON FWD SHIELD AT FWD CARGO BAY BS420 - BS440 RBL24 WL157. ; / ASSIGNED PART TO JOB;EVALUATED CORROSION ON SHIELD BS 420-440 RBL 24; FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;LOCATED; DRILLED; AND DEBURRED NEW SHIELD BS 420-440 RBL 24; WL 157 PER SRM 51-40-05-0G-0; DRAWING 143A0080.;OK TO INSTALL;OK TO INSTALL FWD SHIELD AT FWD CARGO BAY BS420 TO BS440 RBL24 WL157;REMOVED SHIELD BS 420-440 RBL 24 PER SRM 51-40-02-0G-0;VERIFIED INSTALLATIN OF FCB FWD SHIELD IAW SRM51-40-02; DWG 143A0080;VERIFIED CORROSION ON SHIELD BS 420-440 RBL 24; FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;INSTALLED FWD SHIELD AT FWD CARGO BAY BS420 TO BS440 RBL24 WL157 IAW SRM 51-40-02 AND DWG 143A0080;VERIFIED LOCATED; DRILLED; AND DEBURRED NEW SHIELD BS 420-440 RBL 24; WL 157 PER SRM 51-40-05-0G-0; DRAWING 143A0080.;VERIFIED CORROSION ON SHIELD BS 420-440 RBL 24; FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0
Part: SHIELD — CORRODED (BS 500-500A) · airframe 74,727 hrs · 43,976 cycles
***CORROSION*** ON AFT SHIELD AT FWD CARGO BAY BS500 - BS500A RBL24 WL157. ; / EVALUATED CORROSION ON SHIELD; FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;LOCATED ;DRILLED ; DEBURRED NEW SHIELD BS 492-500A RBL 24; WL157; INSTALLED NUTPLATES PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DRAWING 143A0080.;OK TO INSTALL;OK TO INSTALL AFT SHIELD AT FWD CARGO BAY BS500 TO BS500A RBL24 WL157;REMOVED SHIELD BS 500-500A RBL 24 PER SRM 51-40-02;USED MICROMETER ID4566A S/N UNKNOWN;VERIFIED INSTALLATION OF FCB AFT SHIELD IAW SRM 51-40-02; DWG 143A0080;VERIFIED CORROSION ON SHIELD; FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;VERIFIED FABRICATION OF NEW FCB SHIELD BS492 TO BS500 RBL23 IAW BOEING DRAWING 143A8126.;FABRICATED NEW FCB SHIELD BS492 TO BS 500 RBL23 IAW BEOING DRAWING 143A8126. REFER TO ATS BUILD SHEET 527244;INSTALLED AFT SHIELD AT FWD CARGO BAY BS500 TO BS500A RBL24 WL157 IAW SRM 51-40-02 AND DWG 143A0080;VERIFIED LOCATED ;DRILLED ; DEBURRED NEW SHIELD BS 492-500A RBL 24; WL157; INSTALLED NUTPLATES PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DRAWING 143A0080.
Part: SUPPORT ANGLE — CORRODED (BS 500D) · airframe 74,727 hrs · 43,976 cycles
***CORROSION*** ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT FWD CARGO BAY BS500D LBL20. ; WL157. / CARD COMPLETE;INSTALLED AFT BULKHEAD TO FLOOR SUPPORT ANGLE ATVFWD CARGO BAY BS500D LBL20 IAW DWG 143A9481; DWG 143A7902 AND SRM 51-40-02-0G-0;LOCATED; DRILLED DEBURRED NEW BULKHEAD TO FLOOR SUPPORT ANGLE BS 500D LBL 25 - RBL 25 PER SRM 51-40-05-0G-0; DWG 143A7902; DWG 143A9481.;OK TO INSTALL AFT BULKHEAD-TO-FLOOR SUPPORT; BS 500D; LBL 20;VERIFIED INSTALLATION OF AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT FWD CARGO BAY BS 500D LBL20 IAW DWG 143A9481; DWG 143A7902 AND SRM 51-40-02-0G-0;FWD CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT BS500D LBL20 WL157 WAS FOUND OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM PART MUST BE REPLACED DUE TO SRM 51-10-02-OG-0 REMOVED BULKHEAD SUPPORT ANGLE AT BS500D FROM LBL25 TO RBL25 PER SRM 51-40-02;UPDATED PARTS TABLE;VERIFIED LOCATED; DRILLED DEBURRED NEW BULKHEAD TO FLOOR SUPPORT ANGLE BS 500D LBL 25 - RBL 25 PER SRM 51-40-05-0G-0; DWG 143A7902; DWG 143A9481;VERIFIED FWD CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT BS500D LBL20 WL157 WAS FOUND OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM PART MUST BE REPLACED DUE TO SRM 51-10-02-OG-0 REMOVED BULKHEAD SUPPORT ANGLE AT BS500D FROM LBL25 TO RBL25 PER SRM 51-40-02
Part: CARGO TRACK — CORRODED (BS 764) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS764 LBL17 WL157. ; / REMOVED CORROSION ON TRACK AT FASTENER HOLE BS 764 LBL 17 WL 157; REMOVED 0.015 FROM ORIG .070 IN 1'X1' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. USED MICROMETER ID 4566A S/N UNKNOWN. TRACK TO BE REPLACED ON CUST CARD#TTG8Q0050UME; VERIFIED OUT OF LIMITS STATEMENT AND WORK TO BE ACCOMPLISHED ON CUST CARD# TTG8Q0050UME
Part: CARGO TRACK — CORRODED (BS 934 RBL 13) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON TRACK AROUND FASTENER HOLE AT AFT CARGO BAY BS934 RBL13 WL179. ; / INSTALLED NEW ACB CARGO TRACK BS 887-947; RBL 13; WL 179 IAW SRM 51-40-02-0G-0; DWG# 147A7500.;LOCATED; DRILLED; AND DEBURRED NEW ACB CARGO TRACK BS 887-947; RBL 13; WL 179 IAW SRM 51-40-05-0G-0; DWG# 147A7500. OK TO INSTALL;VERIFIED DRILL UP AND DEBURR. OK TO INSTALL;VERIFIED INSTALLATION OF ACB TRACK BS887-947; RBL13; WL179. IAW SRM 51-40-02; DWG 147A7500;DAMAGE REMOVED FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2;ON TRACK FLANGE BS 934 RBL13 WL179 DAMAGED REMOVED 1'X1' ORIGINAL THICKNESS 0.070' D=0.031 FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2 PAR. 4C 2B. TOOL USED ID ATS1317 S/N UNK DATE 06/2021;REMOVED CARGO TRACK AT BS 947-887 RBL 13 WL 179 IAW SRM 51-40-02-0G-0;UPDATED DAMAGED TABLE
Part: ATTACH ANGLE — CRACKED (BS 500C) · airframe 74,727 hrs · 43,976 cycles
INTERCOSTAL ATTACH ANGLE CRACKED AT FWD CARGO BAY BS500C AFT SIDE LBL25 WL156. ; / REMOVED INTERCOSTAL ATTACH ANGLE IN FCB BS500C AFT SIDE OF FRAME; LBL25; WL 156. LOCATED; DRILLED; DEBURRED; AND INSTALLED NEW ATTACH ANGLE IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG# 143A7505.; VERIFIED LOCATE; DRILL AND DEBURR OF NEW ATTACH ANGLE PER SRM 51-40-02; SRM 51-40-05; AND DWG 143A7505; VERIFIED INSTALLATION OF NEW ATTACH ANGLE PER SRM 51-40-02; SRM 51-40-05 AND DWG 143A7505; NO FAULTS RAISED
Part: SUPPORT ANGLE — CORRODED (BS 867-887 LBL9) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON BULKHEAD TO FLOOR SUPPORT ANGLE BS867 - BS887 LBL9 WL169. ; / INSTALLED BULKHEAD TO FLOOR SUPPORT ANGLE; BS 847-947 LBL9; WL 169 PER SRM 51-40-02-0G-0; DWG 149A8103; DWG 149A8104.;PRIMED AND PAINTED BULKHEAD TO FLOOR SUPPORT ANGLE PER DWG 149A8113; SOPM 20-41-02; INSTALLED NUT PLATES PER SRM 51-40-02-0G-0; OK TO INSTALL PART.;RECEIVED FORMED BULKHEAD SUPPORT ANGLE FROM OSS ON PO#825808 USING BAC 1503-1001145 2024-T3511 LOT# 1459916-1. LOCATED; DRILLED AND DEBURRED BULKHEAD SUPPORT ANGLE BS 867-947 LBL 9; WL 169; PER SRM 51-40-05-0G-0; DWG 149A8113.;RECEIVED PART FROM OSS PER P.O.#826249.;VERIFIED INSTALLATION OF BULKHEAD TO FLOOR SUPPORT ANGLE; BS 847-947 LBL9; WL 169 PER SRM 51-40-02-0G-0; DWG 149A8103; DWG 149A8104.;VERIFIED INSTALLATION OF BULKHEAD TO FLOOR SUPPORT ANGLE; PER SRM 51-40-02-0G-0; DWG 149A8103; DWG 149A8104.
Part: CARGO TRACK — CORRODED (BS 787 LBL 17) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON TRACK TIEDOWN AT AFT CARGO BAY BS787 LBL17 WL158. ; / REMOVED CORROSION ON TOP SURFACE OF TRACK TIE DOWN BS 787 LBL17 WL 158; REMOVED 0.025 FROM MAX ALLOWABLE OF 0.020 IN 1'X1' AREA FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DEPTH GAUGE ID ATS1225 S/N UNKNOWN. TRACK TO BE REPLACED ON CUST CARD#TTG8Q0050UME; VERIFIED OUT OF LIMITS STATEMENT AND WORK TO BE ACCOMPLISHED ON CUST CARD# TTG8Q0050UME
Part: FLOOR SUPPORT — CORRODED (BS 790 RBL 6) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON INTERCOSTAL AT AFT CARGO BAY BS790 RBL6 WL153. ; / INSTALLED NEW INTERCOSTAL BS 787-807; RBL 6; WL 153 IAW SRM 51-40-02-0G-0; DWG# 146A8130;LOCATED; DRILLED; AND DEBURRED NEW INTERCOSTAL BS 787-807; RBL 6; WL 153 IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG #146A8130. OK TO INSTALL.;REMOVED INTERCOSTAL BS 787-807 RBL6 WL 153 PER SRM 51-40-02-0G-0.;VERIFIED INTERCOSTAL CORROSION AT BS790 RBL6 WL153 IS OUT OF LIMITS AND REQUIRES REPLACEMENT DUE TO NO ALLOWABLE LIMITS IN SRM IAW SRM 51-10-020G-0;VERIFIED LOCATE; DRILL AND DEBURR OF INTERCOSTAL PER SRM 51-40-05 AND DWG #146A8130<BR>OK TO INSTALL;EVALUATED CORROSION ON INTERCOSTAL AT BS790 RBL6 WL153 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;UPDATED MEASUREMENT TABLE;VERIFIED INSTALLATION OF NEW INTERCOSTAL BS 787-807; RBL 6; WL 153 IAW SRM 51-40-02-0G-0; DWG# 146A8130
Part: SUPPORT — CORRODED (BS 727-807 LBL21) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS807 - BS727 LBL21 WL157. ; / INSTALLED NEW FLOOR TO SIDEWALL SUPPORT IN ACB BS 727-847 LBL21 WL157 IAW SRM 51-40-02 AND DWG #146A7500.;OK TO INSTALL NEW FLOOR TO SIDEWALL SUPPORT IN AFT CARGO BAY BS807-727 LBL21 WL157;OK TO INSTALL NEW FLOOR TO SIDEWALL SUPPORT IN AFT CARGO BAY BS807-727 LBL21 WL157.;REMOVED CORROSION ON L/H FLOOR TO SIDEWALL SUPPORT BS 727-807 LBL 21 WL 157 IN NUMEROUS 1'X1' AREAS; REMOVED 0.015 FROM ORIG 0.040 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. MICROMETER USED ID4566A S/N UNKNOWN;REMOVED OLD PART FROM PART ASSIGNED ROW;VERIFIED INSTALLED NEW FLOOR TO SIDEWALL SUPPORT IN ACB BS 727-847 LBL21 WL157 IAW SRM 51-40-02 AND DWG #146A7500.;VERIFIED VERIFIED INSTALLED NEW FLOOR TO SIDEWALL SUPPORT IN ACB BS 727-847 LBL21 WL157 IAW SRM 51-40-02 AND DWG #146A7500. <BR><BR>CARD COMPLETE;VERIFIED REMOVAL OF CORROSION ON L/H FLOOR TO SIDEWALL SUPPORT BS 727-807 LBL 21 WL 157 IN NUMEROUS 1'X1' AREAS; REMOVED 0.015 FROM ORIG 0.040 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. MICROMETER USED ID4566A S/N UNKNOWN;LOCATED AND DRILLED NEW ACB LH FLOOR TO SIDEWALL SUPPORT BS 727 TO BS847 IAW SRM 51-40-05-0G-0 SRM 51-40-02-0G-0;LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02; 51-40-05.;REMOVED ACB LH FLOOR TO SIDEWALL SUPPORT; BS 727 TO 847 PER SRM 51-40-02-0G-0
Part: STRINGER — CORRODED (BS 536 S26R) · airframe 74,727 hrs · 43,976 cycles
STR26R HAS CORROSION AT BS536 RBL23 WL152 ; / HFEC INSPECTED TRIMMED EDGE OF DAMAGE CUTOUT PER 737NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS FOUND.;UPDATED CORROSION MEASUREMENTS; EVALUATED CORROSION ON STRINGER 26 R/H BS 536; FOUND 0.020 REMOVED FROM ORIG 0.045 IN 1'X' AREA; FOUND TO BE OUT OF LIMITS PER SRM 53-00-03-1A-1; USED MICROMETER ID4566A S/N UNKOWN;VERIFIED RECEIPT OF PART; CUTOUT STR SECTION BS 500D +11 -538; STR 26R PER SRM 53-00-03 2R-1.;INSTALLED REPAIR PARTS AT STR-26R BS 500D+6' -540;APPLIED SEALING AROUND REPAIR AND CIC ON REPAIR AREA IAW SRM 53-00-03 REP.1; DWG 143A1215 & 143A3230.;LOCATED AND DRILLED REPAIR PARTS; APPLIED CHEMICAL CONVERSION STR-26 SECTION BS 500D+10' - 540 IAW SRM 53-00-03 REP.1;PERFORMED GVI AND NO ADDITIONAL DAMAGED FOUND;APPLIED PRIMER ON REPAIR PARTS AND REPAIR AREA STR-26R BS 500D+6' -540 IAW SRM 53-00-03 REP.1 AND OK TO INSTALL.;RECEIVED REPAIR PARTS FROM OSS VERIFIED HEAT TREATMENT AND FABRICATION NEW SECTION STR-26R MAT. USED 7075 T6 BARE 0.045' LOT#1451784 RO 824536-SWA IAW SRM 53-00-03 REP.1 DWG.143A3241 BAC5602; HAT SECTION MAT.USED 7075 T6 CLAD 0.050'LOT#1407037-1 RO 824537-SWA IAW SRM 53-00-03 REP.1 AND BAC 5602.;REMOVED DAMGED SECTION OF STR-26R AND INSTALLED NEW STR-26R SECTION AND SPLICE AT BS 500D+6'' - 540 IAW SRM 53-00-03 REP. 1
Part: STRINGER — CRACKED (BS 536 S25R) · airframe 74,727 hrs · 43,976 cycles
STR25R IS CRACKED AT BS536 RBL30 WL155 ; / REFER TO EA 21-153-01274 . UPDATED MEASUREMENT;VERIFIED LOCATE AND DRILLED NEW STR-25 SECTION;U CHANNEL & J- CHANNELS (2EA) AT BS 500D+6' - 540 AND APPLIED CHEMICAL CONVERSION COATING IAW AE 21-153-01274 AND SRM 53-00-03 REP.1.;VERIFIED RII STEPS COMPLETE.;VERIFIED REPAIRED STRINGER 25R AT BS 536 PER SWA EA # 21-153-01274.;VERIFIED APPLICATION OF CIC;VERIFIED PRIMER AND OK TO INSTALL.;VERIFIED; INSTALLED REPAIR PARTS AT BS 500D -540 STR-25R AND APPLIED SEALING AROUND REPAIR AREA IAW SRM 53-00-03 REP.1;DWG 143A1215;143A3230 & EA 21-153-01274;APPLIED CIC ON REPAIR AREA IAW SRM 53-00-03 REP. 1 AND EA 21-153-01274;APPLIED PRIMER ON REPAIR PARTS AND REPAIR AREA STR-25R BS 500D+6' - 540 IAW SRM 53-00-03 REP.1(LATE ENTRY);INSTALLED REPAIR PARTS AT BS 500D -540 STR-25R AND APPLIED SEALING AROUND REPAIR AREA IAW SRM 53-00-03 REP.1;DWG 143A1215;143A3230 & EA 21-153-01274;LOCATED AND DRILLED NEW STR-25 SECTION;U CHANNEL & J- CHANNELS (2EA) AT BS 500D+6' - 540 AND APPLIED CHEMICAL CONVERSION COATING IAW AE 21-153-01274 AND SRM 53-00-03 REP.1.;
Part: SEAT TRACK — CORRODED (BS 680-683 RBL45) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON TOP AND IN WELL OF SEAT TRACK CROWN BS 680-683 RBL 45 WL 208. ; / INSTALLED NEW SEAT TRACK BS 540-727B; RBL 45; WL 208 PER SRM 51-40-02-0G-0 AND BOEING DWG# 144A5300.;REAMED HOLES IN NEW SEAT TRACK STA 540-727B; RBL 45; WL 208 PER SRM 54-40-05-0G-0; SRM 51-40-02-0G-0; DWG# 144A5300; REV D. OK TO INSTALL.;REMOVED CORROSION ON TOP AND IN WELL OF SEAT TRACK CROWN STA 680-683; RBL 45; WL 208. MAX MATERIAL REMOVED WAS .025' .5' BY 2' ON TOP; .012' 1' BY 1' IN WELL. OUT OF LIMITS PER SRM 53-00-52-1A-1; SRM 51-10-02-0G-0. MEASURED DEPTH WITH DIAL DEPTH GAUGE ID# ATS2473; S/N UNKNOWN; EXPIRES 12/2021;REMOVED DAMAGED SEAT TRACK STA 540 TO 727B RBL 45 WL 208 PER SRM 51-40-02-0G-0;VERIFIED DAMAGED SEAT TRACK WAS REMOVED STA 540-727B; RBL 45; WL 208 PER SRM 51-40-02-0G-0.;VERIFIED DAMAGE REMOVAL AND OUT OF LIMITS;CERTIFIED CORRECTION;UPDATED DEPTH REMOVED.;UPDATED TO LEVEL 2 CORROSION. PART OUT OF LIMITS.;VERIFIED HOLES REAMED; AND OK TO INSTALL;VERIFIED INSTALLATION OF SEAT TRACK IAW SRM 51-40-02-0G-0; DWG# 144A5300
Part: STRINGER — CRACKED (BS 536 S23L) · airframe 74,727 hrs · 43,976 cycles
STR23L IS CRACKED AT BS536 LBL45 WL162 ; / HFEC INSPECTED TRIMMED EDGE OF DAMAGE CUTOUT PER 737NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS FOUND.;LOCATED AND DRILLED STRINGER AND HAT SECTION AT STR23L FROM BS500D+10 - BS540 IAW SRM 53-00-03-2R-1 PARA 4 STEPS (A-I) AND EA 21-153-01297;PERFORMED GVI OF REPAIR AREA IAW SRM 53-00-03-2R-1; NO ADDITIONAL FAULTS RAISED; OK TO INSTALL REPAIR PARTS;RII FUNCTION; VERIFIED ACCOMPLISHED STRINGER REPAIR STR23L AT BS 536 PER EA 21-153-01297 AND SRM 53-00-03-2R-1;RECEIVED STRINGER SECTION AND HAT SECTION FROM O.S.S; VERIFIED HEAT TREATED TO T6 CONDITION PER BAC5602 AND DYE PEN PER SOPM 20-20-02 ON PO# 824520-SWA;REFER TO EA 21-153-01297 SUMMARY REQUIREMENT; BARCODE: TTG8Q005DY9K.;REQUEST NDI FOR HFEC AT CUTOUT FOR CRACK FREE CONDITION PER SRM 53-00-03-2R-1.;VERIFIED ACCOMPLISHED STRINGER REPAIR STR23L AT BS 536 PER EA 21-153-01297 AND SRM 53-00-03-2R-1;VERIFIED (RII) INSTALLATION OF REPAIR PARTS AT BS 500D -540 STR-23L AND APPLICATION OF SEALANT AROUND REPAIR AREA IAW SRM 53-00-03 REP.1; DWG 143A1215; DWG 143A3230 & EA 21-153-01297 WIP2<BR><BR>VERIFIED APPLICATION OF CIC ON REPAIR AREA IAW SRM 53-00-03 REPAIR 1 AND EA 21-153-01297 WIP2;VERIFIED APPLICATION OF CIC;VERIFIED COMPLETION OF WORK IAW SRM 53-00-03-REPAIR 1 AND EA 21-153-01297 WIP1 AND -WIP2;VERIFIED CUTOUT STRINGER SECTION BS 500D +10; STR 23L PER SRM 53-00-03-2R-1.
Part: STRINGER — CRACKED (BS 536 S23R) · airframe 74,727 hrs · 43,976 cycles
STR23R IS CRACKED AT BS536 RBL45 WL162 ; / HFEC INSPECTED TRIMMED EDGE OF DAMAGE CUTOUT PER 737NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS FOUND.;PERFORMED GVI INSP; NO DEFECTS NOTED. VERIFIED PRIMER AND OK TO INSTALL PER SRM AND EA 21-153-01302.;RII FUNCTION;REPAIRED CRACK STRINGER AT STR-23R BS 536 PER SRM 53-00-03-2R-1 AND EA 21-153-01302;REFER TO EA 21-153-01302 SUMMARY REQUIREMENT; BARCODE: TTG8Q005E8R7.;VERIFIED;REPAIRED CRACK STRINGER AT STR-23R BS 536 PER SRM 53-00-03-2R-1 AND EA 21-153-01302;VERIFIED APPLICATION OF SEALANT AND CIC;VERIFIED CUTOUT OF STR SECTION BS 500D +10 - 538 STR 23R PER SRM SRM 53-00-03-2R-1.;VERIFIED NEW STRINGER SECTION AND SPLICE INSTALL PER SRM 53-00-03 REP 1 AND EA 21-153--01302.;APPLIED AT STR-23R BS 500D+6' -540 SEALING AROUND REPAIR AND CIC ON REPAIR AREA IAW SRM 53-00-03 REP.1 AND EA 21-153-01302 WIP2.;CORRECTIVE ACTIONS 6 & 7. REVIEWED R.O. 824531-SWA/ 824532-SWA. VERIFIED STRINGER SECTION / HAT CHANNEL PARTS FABRICATED; LOCATED AND DRILLED IAW 21-153-01302 AND SRM 53-00-23-2R-1 REPAIR 1.;CUTOUT STR SECTION BS 500D +10 - 538 STR 23R PER SRM SRM 53-00-03-2R-1.;FABRICATED REPAIR PARTS STR-23 SECTION AND HAT CHANNEL SECTION;LOCATED & DRILLED AND CHEMICAL CONVERSION COATING APPLIED IAW E/A 21-153-01302 AND SRM 53-00-03 REP.1;INSTALLED NEW STR-23 SECTION AND SPLICE AT BS 500D+6' - 540 IAW SRM 53-00-03 REP.1 AND EA 21-153-01302;PERFORMED GVI;
Part: STRINGER — CRACKED (BS 536 S27L) · airframe 74,727 hrs · 43,976 cycles
STR27L IS CRACKED AT BS536 LBL15 WL150 ; / HFEC INSPECTED TRIMMED EDGE OF DAMAGE CUTOUT PER 737NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS FOUND.;LOCATED; DRILLED; DEBURRED STRINGER SECTION AND HAT SECTION PER SRM 53-00-03-2R-1 REPAIR 1; STEPS 4; D;E;F;G;H; FIG 205; APPLIED A CHEMICAL CONVERSION COATING PER SRM 53-00-03-2R-1; STEP 4;I.;PERFORMED GVI OF REPAIR AREA IAW SRM 53-00-03-2R-1; NO FAULTS NOTED; OK TO INSTALL REPAIR PARTS;RECEIVED STRINGER SECTION; P.O.#824533. RECEIVED HAT SECTION ; P.O.# 824534.;VERIFIED CARD COMPLETE;VERIFIED; INSTALLED REPAIR PARTS AT BS 500D+6' -540 STR-27R AND APPLIED SEALING AROUND REPAIR AREA AND CIC IAW SRM 53-00-03 REP.1;DWG 143A1215;143A3230.;CUTOUT STR SECTION BS 500D +11 - 538; STR 27 L PER SRM 53-00-03-2R-1;;INSTALLED REPAIR PARTS AT BS 500D+6' -540 STR-27R AND APPLIED SEALING AROUND REPAIR AREA AND CIC IAW SRM 53-00-03 REP.1;DWG 143A1215;143A3230.;PERFORMED GVI ON REPAIR AREA AND NO ADDITIONAL DAMAGED FOUND; APPLIED PRIMER ON REPAIR PARTS AND REPAIR AREA IAW SRM 53-00-03 REP.1. OK TO INSTALL.;REQUEST NDI TO HFEC CUT SECTION FOR CRACK FREE CONDITION PER SRM 53-00-03-2R-1 STEP 4;C.;UPDATED MEASUREMENTS;VERIFIED CUTOUT OF STR SECTION BS 500D +11 - 538; STR 27 L PER SRM 53-00-03-2R-1;VERIFIED LOCATE DRILLED; DEBURRED STRINGER SECTION AND HAT SECTION PER SRM 53-00-03-2R-1 REPAIR 1; STEPS 4; D;E;F;G;H; FIG 205; APPLIED A CHEMICAL CONVERSION COATING PER SRM 53-00-03-2R-1; STEP 4;I.
Part: SEAT TRACK — CORRODED (BS 500D RBL45) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON TOP OF SEAT TRACK CROWN BS 500D+13.5 RBL 45 WL 208. ; / APPLIED ALUMIZED EPOXY PRIMER TO BLENDED AREAS ON TOP OF SEAT TRACK CROWN STA 500D+13.5; RBL 45; WL 208 PER SOPM 20-41-04.;APPLIED CHEMICAL CONVERSION COATING ON TOP OF SEAT TRACK CROWN STA 500D+13.5; RBL 45; WL 208 PER SRM 51-20-01-0G-0; SRM 53-00-52-1A-1.;EVALUATED CORROSION AND FOUND TO BE IN LIMITS PER SRM 53-00-52-1A-1.;REMOVED CORROSION ON TOP OF SEAT TRACK CROWN STA 500D+13.5; RBL 45; WL 208. MAX MATERIAL REMOVED WAS .009' .5' BY 2' ON TOP. IN LIMITS PER SRM 53-00-52-1A-1; SRM 51-10-02-0G-0. MEASURED DEPTH WITH DIAL DEPTH GAUGE ID# ATS1225; S/N UNKNOWN; EXPIRES 04/2022.;VERIFIED: APPLIED CHEMICAL CONVERSION COATING ON TOP OF SEAT TRACK CROWN STA 500D+13.5; RBL 45; WL 208 PER SRM 51-20-01-0G-0; SRM 53-00-52-1A-1.;VERIFIED APPLICATION OF ALUMINIZED PRIMER PER SOPM 20-41-04;VERIFIED DAMAGE REMOVAL AND DIMENSIONS;ADDED PART NUMBER TO MEASUREMENTS;COMPLETED;EVALUATED PER SRM 53-00-52-1A-1
Part: SEAT TRACK — DAMAGED (BS 520 LBL 45) · airframe 74,727 hrs · 43,976 cycles
MECHANICAL DAMAGE ON TOP OF SEAT TRACK CROWN BS 520 LBL 45 WL 208. ; / APPLIED CIC ON SEAT TRACK REPAIR AREA AND ALL REPAIR PARTS STA 500C+10-520; LBL 45; WL 208 PER SRM 53-00-52-2R4; AMM 51-21-91-620-802.;APPLIED BMS 8-283 TAPE TO THE TOP OF THE UPPER HORIZONTAL FLANGE OF THE ALUMINUM SEAT TRACK; STA 500C+10-520;LBL 45; WL 208 PER AMM 53-21-00-400-801; SRM 53-00-52-2R-4.;BLENDED MECHANICAL DAMAGE ON TOP OF SEAT TRACK CROWN STA 520; LBL 45; WL 208. MAX MATERIAL REMOVED WAS .026' .5' BY 2'. OUT OF LIMITS PER SRM 53-00-52-1A-1; SRM 51-10-02-0G-0. MEASURED DEPTH WITH DIAL DEPTH GAUGE ID# ATS1225; S/N UNKNOWN; EXPIRES 04/2022;CIC APPLIED IS FULLY CURED ON SEAT TRACK REPAIR STA 500C+10-520; LBL 45; WL 208 PER AMM 51-21-91-620-803.;HFEC ON TRIMMED EDGES OF SEAT TRACK REPAIR STA 500C+10-520; LBL 45; WL 208 IS NOR REQUIRED PER SRM 53-00-52-2R-4.;HFEC ON TRIMMED EDGES OF SEAT TRACK REPAIR STA 500C+10-520; LBL 45; WL 208 IS NOT REQUIRED PER SRM 53-00-52-2R-4.;HFEC ON TRIMMED EGDWS OF SEAT TRACK REPAIR STA 500C+10-520; LBL 45; WL 208 IS NOR REQUIRED PER SRM 53-00-52-2R-4.;HFEC INSP BLENDS IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED. EQUIP ID#: IS000450 S/N: N500D000M120071;HFEC INSPECTED HOLES COMMON TO SEAT TRACK SPLICE REPAIR PER NDTM PART 6; 51-00-00 PROCEDURE 16; NO CRACKS NOTED INSTALLED NEW REPAIR SEAT TRACK AND REPAIR CHANNEL FOR SEAT TRACK REPAIR BS 500C+10 - BS 520; LBL 45; WL 208 PER SRM 53-00-52-2R-4
Part: STRINGER — CRACKED (BS 536 S24R) · airframe 74,727 hrs · 43,976 cycles
STR24R IS CRACKED AT BS536; RBL39; WL158 ; / HFEC INSPECTED TRIMMED EDGE OF DAMAGE CUTOUT PER 737NDT PART 6 51-00-00 PROCEDURE 23. NO CRACKS FOUND.;VERIFIED INSTALLATION OF REPAIR PARTS AT STR-24R BS 500D+6' -540;APPLIED SEALING AROUND REPAIR AND CIC ON REPAIR AREA IAW SRM 53-00-03 REP.1; DWG 143A1215 & 143A3230.;VERIFIED PRIMER APPLICATION; PASSED. GVI OK TO INSTALL;VERIFIED RECEIPT OF PARTS; MATERIAL TYPE/ THICKNESS/ TEMPER; DRILL UP AND CONVERSION COATING APPLICATION. COMPLETED;CUTOUT STR SECTION ; BS 500D +12 - 538 STR 24R PER SRM 53-00-03 -2R-1.;INSTALLED REPAIR PARTS AT STR-24R BS 500D+6' -540;APPLIED SEALING AROUND REPAIR AND CIC ON REPAIR AREA IAW SRM 53-00-03 REP.1; DWG 143A1215 & 143A3230.;LOCATED AND DRILLED; GVI NO ADDITIONAL DAMAGED FOUND & CHEMICAL CONVERSION COATING APPLIED TO REPAIR PARTS IAW SRM 53-00-03 REP.1;RECEIVED REPAIR PARTS FROM OSS; REMOVED DAMGED SECTION OF STR-24R AND INSTALLED NEW STR-24R SECTION AND SPLICE AT BS 500D+6'' - 540 IAW SRM 53-00-03 REP. 1; DWG 143A1215;143A3230.;REQUEST NDI TO HFEC CUTOUT FOR CRACK FREE CONDITION PER SRM 53-00-03-2R-1 STEP 4;C
Part: STRINGER — CRACKED (BS 536 S25R) · airframe 74,727 hrs · 43,976 cycles
STR25R IS CRACKED AT BS536 RBL30 WL155 ; / COMPLETED STEPS 9-12; COMPLETED STEPS 1-13; VERIFIED FOD PROTECTION REMOVAL PER STEP 13
Part: STRINGER — CRACKED (BS 536 S23R) · airframe 74,727 hrs · 43,976 cycles
STR23R IS CRACKED AT BS536 RBL45 WL162 ; / COMPLETE STEP 6; VERIFIED STEPS 1-6 OF EA 21-153-01302 WIP2; VERIFIED EA 21-153-01302 STEPS 1-6 ARE COMPLETE WIP 2
Part: SEAT TRACK — CORRODED (BS 680-683 RBL25) · airframe 74,727 hrs · 43,976 cycles
CORROSION ON TOP AND IN WELL OF SEAT TRACK CROWN BS 680-683 RBL 25 WL 208. ; / .025' WAS ON TOP OF SEAT TRACK CROWN.;CHANGED TO LEVEL 2;INSTALLED NEW SEAT TRACK BS 540-727B; RBL 25; WL 208 PER SRM 51-40-02-0G-0 AND BOEING DRAWING 141A5300.;REMOVED CORROSION ON TOP AND IN WELL OF SEAT TRACK CROWN STA 680-683; RBL 25; WL 208. MAX MATERIAL REMOVED WAS .025' .5' BY 2'; .016' 1' BY 1' IN WELL. OUT OF LIMITS PER SRM 53-00-52-1A-1; SRM 51-10-02-0G-0. MEASURED DEPTH WITH DIAL DEPTH GAUGE ID# ATS2473; S/N UNKNOWN; EXPIRES 12/2021.;REMOVED DAMAGED SEAT TRACK AT STA 540-727B RBL 25 WL 208 PER SRM 50-40-02-0G-0.;UPDATED MEASUREMENTS. LOCATED AND DRILLED NEW SEAT TRACK BS 540-727B; RBL 25 PER SRM 51-40-05-0G-0 AND BOEING DWG# 144A5300. OK TO INSTALL NEW SEAT TRACK BS 540-727B; RBL 25.;VERIFIED DAMAGE REMOVAL AND OUT OF LIMITS;ADDED PART NUMBER TO MEASUREMENTS;VERIFIED LOCATED AND DRILLED NEW SEAT TRACK BS 540-727B; RBL 25 PER SRM 51-40-05-0G-0 AND BOEING DWG# 144A5300 AND OK TO INSTALL;VERIFIED INSTALLATION OF SEAT TRACK BS 540-727B; RBL 25; WL 208 PER SRM 51-40-02-0G-0 AND BOEING DRAWING 141A5300.;VERIFIED REMOVAL OF SEAT TRACK STA 540-727B; RBL 25; WL 208 PER SRM 51-40-02-0G-0.
Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 74,727 hrs · 43,976 cycles
RH HORIZONTAL STAB RIB ASSY 5 (STAB STA 129.50) STIFFENER 3 HAS A CRACK ON THE LOWER AREA ; / 12. APPLIED PRIMER TO REPAIR PARTS AND RIB BARE METAL IAW SRM 55-10-09-2R-4 STEP 4 L. OK TO INSTALL REPAIR PARTS.;13. INSTALLED REPAIR PARTS ON RIB 3RD STIFFENER AREA IAW SRM 55-10-09-2R-4 STEP 4 M THRU 4 R. QC REQUIRED TO VERIFY INSTALLATION.;14. INSTALLED INSPAR RIB ON RT HORIZONTAL STABILIZER AT STAB STATION 129.50 IAW SRM 51-40-02-0G-0 AND DWG #'S 182A1500; 182A3001 REPAIRED RH HORIZONTAL STAB RIB ASSY 5 (STAB STA 129.50) STIFFENER 3 LOWER AREA IAW SRM 55-10-09-2R-4;
Part: FLOOR PANEL — DAMAGED (PAX CABIN) · airframe 74,727 hrs · 43,976 cycles
PASSENGER CABIN FLOOR PANEL 232RF HAS DAMAGE ALONG AFT EDGE. ; / DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 232RF USING BMS 4-23TY2 LOT#1456675-1; INSTALLED INSERTS USING BMS 5-107 LOT# AKODP4051K; CURED WITH THERMOMETER ID: ATS1777 S/N: 34910028WS; PART MARKED IAW SRM 53-00-50-2R-0 PARA 1A(NOTE); 5S AND DWG 144A5810-4.; VERIFIED FABRICATION OF FLOOR PANEL 232RF IAW SRM 53-00-50-2R-0 PARA 1 A & DWG 144A5810-4; VERIFIED FLOOR PANEL FABRICATION PER SRM 53-00-50-2R-0.
Part: FLOOR PANEL — DAMAGED (PAX CABIN) · airframe 74,727 hrs · 43,976 cycles
PASSENGER CABIN FLOOR PANEL 241BF UPPER SURFACE HAS DAMAGE 49' FROM FWD EDGE; 4' FROM OB EDGE. MARKED ; / DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241BF USING BMS 4-23TY2 LOT#1456675-1; INSTALLED INSERTS USING BMS5-107 LOT#AK0HP5746K; CURED USING THERMOMETER ID:ATS1777 S/N 34910028WS; PART MARKED IAW SRM 53-00-50-2R-0 PARA 1A(NOTE); 5S AND DWG144A5810-37.; VERIFIED FABRICATION OF NEW FLOOR PANEL PER DWG 144A5810-37
Part: PRESSURE DECK — DENTED (BS 255) · airframe 74,727 hrs · 43,976 cycles
FLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. ; / EVALUATED FLIGHT DECK FLOOR DENTS AT BS 255; RBL 4 - LBL 14; WL 207.54. DENTS ON FLOOR FOUND TO BE GOUGED; THEREFORE; DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1. REPAIRED DAMAGED FLIGHT DECK FLOOR BS 255; RBL 4 - LBL 14; WL 207.54 PER EA M-21-153-00734 (SWA - REPAIR - FLIGHT DECK FLOOR WEB DENT REPAIR AT BS 260).;VERIFIED REPAIR WAS COMPLETED PER EA M-21-153-00734 (SWA - REPAIR - FLIGHT DECK FLOOR WEB DENT REPAIR AT BS 260).
Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 74,727 hrs · 43,976 cycles
M1674 AND M1675 EMERGENCY BATTERY PACKS FAILED CAPACITANCE TEST ; / PERFORMED SATISFACTORY INSTALLATION TEST OF BATTERY PACK AND BATTERY CHARGER AT LOCATIONS M1674 AND M1675 PER AMM 33-51-06-960-806 AND AMM 33-51-06-960-805;PERFORMED SATISFACTORY INSTALLATION TEST OF BATTERY PACK AND BATTERY CHARGER AT LOCATIONS M1674 AND M1675 PER AMM 33-51-06-960-806 AND AMM 33-51-06-960-805 QC VERIFIED.;REMOVED AND REPLACED BATTERY PACK AND BATTERY CHARGER AT LOCATION M1674 PER AMM 33-51-06-960-806 STEPS 5.E.(1)-(3) AND AMM 33-51-06-960-805 STEPS 4.D.(1)-(4);REPLACED BATTERY CHARGER AND BATTERY PACK IN LOCATION M1675 AS PER AMM 33-51-06-960-806 PARA 5. E. (1) THROUGH (3);REPLACED BATTERY CHARGER AND BATTERY PACK IN LOCATION M1675 AS PER AMM 33-51-06-960-806 PARA 5. E. (1) THROUGH (3); REMOVED AND REPLACED BATTERY PACK AND BATTERY CHARGER AT LOCATION M1674 PER AMM 33-51-06-960-806 STEPS 5.E.(1)-(3) AND AMM 33-51-06-960-805 STEPS 4.D.(1)-(4) QC VERIFIED.
Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 74,727 hrs · 43,976 cycles
M1674 AND M1675 EMERGENCY BATTERY PACKS FAILED CAPACITANCE TEST ; / PERFORMED SATISFACTORY INSTALLATION TEST OF BATTERY PACK AND BATTERY CHARGER AT LOCATIONS M1674 AND M1675 PER AMM 33-51-06-960-806 AND AMM 33-51-06-960-805;PERFORMED SATISFACTORY INSTALLATION TEST OF BATTERY PACK AND BATTERY CHARGER AT LOCATIONS M1674 AND M1675 PER AMM 33-51-06-960-806 AND AMM 33-51-06-960-805 QC VERIFIED.;REMOVED AND REPLACED BATTERY PACK AND BATTERY CHARGER AT LOCATION M1674 PER AMM 33-51-06-960-806 STEPS 5.E.(1)-(3) AND AMM 33-51-06-960-805 STEPS 4.D.(1)-(4);REPLACED BATTERY CHARGER AND BATTERY PACK IN LOCATION M1675 AS PER AMM 33-51-06-960-806 PARA 5. E. (1) THROUGH (3);REPLACED BATTERY CHARGER AND BATTERY PACK IN LOCATION M1675 AS PER AMM 33-51-06-960-806 PARA 5. E. (1) THROUGH (3); REMOVED AND REPLACED BATTERY PACK AND BATTERY CHARGER AT LOCATION M1674 PER AMM 33-51-06-960-806 STEPS 5.E.(1)-(3) AND AMM 33-51-06-960-805 STEPS 4.D.(1)-(4) QC VERIFIED.
Part: SLIDE — DISPLACED (EMERGENCY EXIT) · airframe 74,711 hrs · 43,964 cycles
EMERGENCY EXIT SLIDE HAD EXCESS SLIDE MATERIAL HANGING OUT OF ITS CONTAINER OF AFT ENTRY DOOR ; / REPOSITIONED AFT ENTRY DOOR ESCAPE SLIDE GIRT AS REQUIRED PER MT 725-61-06
Part: BRACKET — LOOSE (L1 DOOR) · airframe 74,585 hrs · 43,889 cycles
FA SAY GIRT BAR IS LOOSE BRACKET / RESECURED FASTENER E ON L1 DOOR GIRT BAR SUPPORT BRACKET REF S.I.P-
Part: SIGN — LOOSE (CABIN) · airframe 74,283 hrs · 43,720 cycles
MID CABIN EXIT COVER SIGN FELL OFF. ALL PARTS ACCOUNTED FOR / INSTALLED MID CABIN AFT CEILING EXIT SIGN PER SIP.
2020
Part: ESCAPE ROPE — LOOSE (LT OVERWING) · airframe 73,502 hrs · 43,259 cycles
LT OVERWING EMERGENCY EXIT ESCAPE ROPE NEEDS RESECURED. REINSTALLED LT OVERWING EXIT ESCAPE ROPE AND SECURED, REF AMM 25-61-10.
Part: SEAT TRACK — WORN (COCKPIT) · airframe 73,390 hrs · 43,190 cycles
CAPT`S FLT DECK SEAT AFT INBOARD SEAT TRACK WORN TO CK LIMITS. REMOVED AND REPLACED SEAT TRACK, PER AMM 25-11-11.
Part: SEAT TRACK — WORN (COCKPIT) · airframe 73,390 hrs · 43,190 cycles
F/O`S FLT DECK SEAT AFT INBOARD SEAT TRACK WORN TO CK LIMITS. REMOVED AND REPLACED SEAT TRACK, PER AMM 25-11-11.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 73,390 hrs · 43,190 cycles
INOPERABLE BULLNOSE EMERGENCY LIGHT AT SEAT 20ABC. RELAMPED, PER AMM 33-51-03.
Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 73,153 hrs · 43,046 cycles
EMERGENCY EXIT LIGHT LENS (OVER ROW 23/24 ABC) BROKEN / REATTACHED EMERGENCY LIGHT LENS TO BULL NOSE AT PASSENGER ROW 23 ABC IAW M/M 33-51-00 AIRCRAFT OK TO CONTINUE IN SERVICE.
Part: FLAP — BROKEN (CRGO DOOR HANDLE) · airframe 72,514 hrs · 42,652 cycles
TRANSFERRED FROM LOG PAGE 1345048. AFT CARGO DOOR HANDLE FLAPPER BROKEN / REMOVED AND REINSTALLED INTERIOR CARGO DOOR FABRIC AND DOOR HANDLE REF AMM 52-31-14 & 52-31-00 REMOVED AND REPLACED AFT CARGO DOOR HANDLE FLAPPER REF SRM 51-40-02 REF SA-M 326: A1081340
Part: STRUCTURE — DAMAGED (BS 727B RBL 46) · airframe 72,430 hrs · 42,603 cycles
DAMAGED/ELONGATED FASTNER HOLE @ BS 727B; RBL 45.50; POS #4 REFERENCE EA 20-153-00054. / (REF LP 0049247) COMPLIED WITH EA 20-153-00106; FOR WORK PERFORMED C/L # 35420
Part: STRUCTURE — DAMAGED (BS 727B) · airframe 72,430 hrs · 42,603 cycles
DAMAGED/ELONGATED FASTENER HOLE @ BS 727B; RBL 45.50 POS#4 REFERENCE EA 20-153-00054. / COMPLIED WITH EA 20-153-00106; FOR WORK PERFORMED
Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 72,124 hrs · 42,418 cycles
CENTER CABIN EXIT SIGN COVER CAME OFF. / RESECURED COVER PER SIP.
2019
Part: SENSOR — FAULTY (LE FLAP) · airframe 70,568 hrs · 41,448 cycles
DECLARED EMERGENCY, THE LE FLAPS TRANSIT AMBER LIGHT ILLUMINATED AFTER PLACING THE FLAP LEVER TO 1 DEGREE. THE A/C WAS AT 8.000' MSL AND 200 KIAS AND LEVEL. WE RAN THE QRH CHECKLIST LEADING EDGE FLAPS TRANSIT P. 9.12 WE LANDED WITH 15 DEGREES. UNEVENTFUL LANDING & TAXI. R&R #1 LEADING EDGE SLAT OUTBOARD SENSOR PER AMM.
Part: FAIRING — CRACKED (TE FLAP) · airframe 70,110 hrs · 41,124 cycles
LT WING #3 FLAP TRACK FORWARD FAIRING 542AB SCREW HOLE AT FORWARD MOUNT AREA COMPOSITE CRACKED. R&R FAIRING 542AB IAW SRM.
Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 70,110 hrs · 41,124 cycles
AFT CARGO DOOR CENTER SCUFF PLATE CRACKED. R&R SCUFF PLATE PER AMM.
Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 70,110 hrs · 41,124 cycles
AFT CARGO DOOR CENTER SCUFF PLATE FOUND CRACKED WHILE INSTALLING / REMOVED AND REPLACED SWEEPER SEAL PAN IAW SRM 51-40-02-0G-0 STEP 9. ATAG WN8772
Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 70,110 hrs · 41,124 cycles
PASSENGER CABIN FLOOR PANEL 242VF HAD DAMAGE AROUND CUTOUT FOR GALLEY FLOOR FITTING, BETWEEN BS. 887 TO BS. 1016. REPAIRED FLOOR BOARD PANEL 242-VF IAW SRM.
Part: FLOORBOARD — DELAMINATED (FUSELAGE) · airframe 70,110 hrs · 41,124 cycles
PASSENGER CABIN FLOORBOARD 242UF EDGE DELAMINATED BY FLOOR DRAINS, BETWEEN BS. 887 TO BS. 1016. REPAIRED FLOORBOARD 242UF IAW SRM.
Part: DOUBLER — CRACKED (WHEEL WELL LH) · airframe 70,110 hrs · 41,124 cycles
STA 663 L/H DUCT FEED THRU; DUCT SEAL ASSY DOUBLER IS CRACKED / REMOVED STA 663 L/H DUCT FEED THRU SEAL ASSY DOUBLER AND INSTALLED NEW DOUBLER IAW SRM 51-40-02-0G-0; AIPC 57-11-00-02 AND DWG:111A1512 REV - . ATG:WN4356.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 70,110 hrs · 41,124 cycles
LOWER ATTACH ANGLE HORIZONTAL FLANGE CRACKED AT STA 663 LBL 45 TO LBL 49. R&R REPAIR PARTS IAW EA.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 70,110 hrs · 41,124 cycles
CENTER SECTION WING BOX LOWER ATTACH ANGLE HORIZONTAL FLANGE CRACKED AT BS. 663, BETWEEN RBL 45 TO RBL 48. REPAIRED CENTER SECTION WING BOX IAW EA.
Part: STRINGER SPLICE — CORRODED (E&E) · airframe 70,110 hrs · 41,124 cycles
E&E COMPARTMENT BILGE AREA STA 344 - 380 STR 27R STRINGER SPLICE CORRODED / REMOVED AND REPLACED STRINGER SPLICE AT E/E COMPARTMENT STA 344-380; STR 27R ON NON ROUTINE CARD: 39560/1300/0014; DEFECT NO. X963254
Part: STRINGER SPLICE — CORRODED (E&E BAY) · airframe 70,110 hrs · 41,124 cycles
E&E COMPARTMENT BILGE AREA STA 344 TO 380 STRINGER SPLICE CORRODED_STR 28L / REPLACED STA 344 TO 380 STRINGER SPLICE AT 28L IS ACCOMPLISHED ON W/O X963253
Part: FLOOR SUPPORT — CORRODED (AFT CARGO BAY) · airframe 70,110 hrs · 41,124 cycles
AFT CARGO COMPARTMENT STA. 767+5' FLOOR SUPPORT RBL7.5' HAS CORROSION LOCATED UNDER THE FLOOR STRIP. / VERIFIED MAT. LOSS ON AFT CARGO STA 767+5' FLOOR SUPPORT INTERCOSTAL RBL 7.5' LOSS .048' ORIG .048 MAT REMAINING '0' 10% MAT. LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A-2 AAR TOOL 36308 DUE 19APR20 REMOVED & REPLACED INTERCOSTAL IAW SRM 51-40-02-06-0 & DWG 146A8130 REV- P/N 146A8132-1
Part: WEB — CORRODED (E&E BAY) · airframe 70,110 hrs · 41,124 cycles
ELECTRONICS AND EQUIPMENT COMPARTMENT WEB CORRODED AT BS. 358, LBL 8, ABOVE LOWER ATTACH ANGLE. / R&R WEB IAW DWG AND SRM.
Part: THRESHOLD — CORRODED (FLIGHT DECK FLOO) · airframe 70,110 hrs · 41,124 cycles
FLT DECK FLOOR; THRESHOLD PANEL 211AF CORROSION ON UNDERSIDE OF PANEL. / REMOVED CORROSION AT FLT DECK FLOOR REMOVABLE PNL 211 AF I.A.W SRM 51-10-02-0G-00. VERIFIED MATERIAL LOSS ORIGINAL .040 REMOVED .010 REMAIN .030 ALLOWABLE 10% FOUND OUT OF LIMITS USED AAR TOOL #18143 DUE 12/14/2019 I.A.W SRM 53-10-51-1A-1. DRILLED NEW PNL I.A.W SRM 51-40-05-0G-00 AND BOEING DWG 141A5133
Part: SPLICE — CORRODED (MAIN CABIN) · airframe 70,110 hrs · 41,124 cycles
PASSENGER CABIN AFT SERVICE STA 986 T-CAP IS CORRODED / REMOVED CORROSION ON A PREVIOUS REPAIRED T-TAP AT STA 986; ORIG 'T' IS .150 REMAINING .087; LOSS OF .063; OUT OUF LIMITS IAW SRM 53-70-15-1A-1 ALSO NO SRM LIMITS ON PREVIOUS REPAIR. REPLACED CORRODED T-CAP SECTION ONLY IAW AAR EA 190567 IR AND SWA EA 1-753-35045 REV IR P/N 147A5506-7
Part: BEAM — CORRODED (R2 DOOR) · airframe 70,110 hrs · 41,124 cycles
R2 DOOR CREASE BEAM WEB CORRODED. R&R BEAM WEB IAW SRM, EA, AND DWG.
Part: SPAR WEB — CORRODED (RT WING) · airframe 70,110 hrs · 41,124 cycles
RH WING. IRSS 145; AFT SPAR WEB HAS CORROSION AT UPPER AND LOWER GROUNDING POINTS FOR AFT BOOST PUMP / REMOVED CORRSION ON UPPER AND LOWER GROUNDING POINTS ON THE REAR SPAR AFT BOOST PUMP. LOWER BLEND EXCEEDED .100. OUT OF LIMITS IAW SRM 57-20-10-1A-3. REPAIRED IAW AAR EA 190451 IR AND SWA EA 1-757-16368 REV IR REAR SPAR WEB P/N 112A1104-4 ATAG U00132 A78261; A85915; A80511 A78682
Part: FRAME — CRACKED (FWD ENTRY DOOR () · airframe 70,110 hrs · 41,124 cycles
L-1 DOOR AFT FRAME UPPER LOCATOR IS CRACKED / REMOVED AND INSTALLED NEW L-1 DOOR AFT FRAME UPPER LOCATOR I/A/W CMM 52-16-12 A-TAG # N10612
Part: FRAME — CRACKED (FWD ENTRY DOOR () · airframe 70,110 hrs · 41,124 cycles
L-1 DOOR AFT FRAME LOWER LOCATOR IS CRACKED / REMOVED AND INSTALLED L-1 DOOR AFT FRAME LOWER LOCATOR I/A/W CMM 52-16-12 PG 710; 711 A-TAG #A76617
Part: ANGLE — CRACKED (MAIN CABIN) · airframe 70,110 hrs · 41,124 cycles
PASSENGER CABIN; STA 663+3; RBL 65; HORIZONTAL PRESSURE DECK DOUBLER ANGLE HAS CORROSION ON UPPER LIP. / REMOVED CORROSION ON THE UPPER LIP OF THE HORIZONTAL PRESSURE DECK DOUBLER ANGLE AT STA 663 + 3 RBL 65. VERIFIED MATERIAL LOSS. 0RIG 'T' .063. REMAINING .062. LOSS OF .001. SRM HAS NO LIMITS IN THIS AREA. REPAIRED IAW AAR EA 190565 IR AND SWA EA 1-757-1632 REV IR
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 70,110 hrs · 41,124 cycles
CABIN FLOORBOARD 242AF HAS NUMEROUS FIBER PLYS MISSING ON UPPER SURFACE. / REPAIRED FLOORBOARD 242 AF UPPER SURFACE IAW SRM 53-00-50-2R-1; PG'S 1;2;3 STEPS 3 (A-M).
Part: GIRT BAR — DEFORMED (R2 DOOR) · airframe 70,110 hrs · 41,124 cycles
R2 DOOR SLIDE AFT RETAINER CLIP FOR GIRT BAR DEFORMED. R&R GIRT BAR IAW SRM.
Part: DOUBLER — CORRODED (MAIN CABIN) · airframe 70,110 hrs · 41,124 cycles
PASSENGE CABIN; STA 663+3; LBL 65; HORIZONTAL PRESURE DECK DOUBLER ANGLE HAS CORROSION AROUND FASTNERS / REMOVED CORROSION IAW B737-700 SRM 51-10-02. ORIGINAL MATERIAL THICKNESS = .063' AFTER BLENDING .060' REMAINS = .003' MATERIAL LOSS. REPAIRED IAW EA 190566 IR AND EA 1-757-16364 REV IR.
Part: RETAINER — CRACKED (LT WING) · airframe 70,110 hrs · 41,124 cycles
LEFT WING LWR INBD FIXED TE PNL 551GB SEAL RETAINER CRACKED AT OTBD END. / REMOVED AND REPLACED LEFT WING LOWER IN BOARD FIXED TRAILING EDGE PANEL SEAL RETAINER FOR PANEL # 551GB IAW BOEING DWG 115A2714 REV -. ATAG WN4613
Part: DOUBLER — CRACKED (EXT PWR DOOR CUT) · airframe 70,110 hrs · 41,124 cycles
EXTERNAL FUSELAGE; EXTERNAL POWER RECEPTACLE DOOR CUTOUT; AFT LOWER CORNER; FLANGE DOUBLER IS CRACKED / TRIMMED OUT DAMAGED AREA OF FLANGE DOUBLER AT EXTERNAL POWER RECEPTACLE CUTOUT FWD LWR CORNER PERFORMED HFEC INSPECTION WITH NO DEFECTS NOTED; AND RESTORED FINISH IN REWORKED AREA IAW SRM 53-10-15-1A-4
Part: BUMPER — CRACKED (SERVICE DOOR) · airframe 70,110 hrs · 41,124 cycles
AFT SERVICE DOOR SLIDE ENDCAP BUMPER CRACKED. R&R ENDCAP PER SRM.
Part: RETAINER — DEFORMED (L2 DOOR) · airframe 70,110 hrs · 41,124 cycles
L2 DOOR SLIDE AFT RETAINER CLIP FOR GIRT BAR DEFORMED. R&R RETAINER IAW SRM.
Part: RETAINER — CRACKED (VERTICAL STAB) · airframe 70,110 hrs · 41,124 cycles
VERT STAB PNL 323BL AFT RETAINER STRIP CRACKED IN 2 PLACES. / REMOVED AND REPLACED DAMAGED AFT RETAINER STIP ON VERT STAB PNL 323BL. RTAINER STRIP PN 172A6125-US ATAG A76603. IAW B-737 SRM 51-40-02-0G-0 AND B-DRAWING 172A6121 REV: A.
Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 70,110 hrs · 41,124 cycles
CREASE BEAM CORD CORRODED. R&R CREASE BEAM IAW SRM AND DWG
Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 70,110 hrs · 41,124 cycles
R/H CABIN STOWBIN EMERGENCY LIGHT LENS LOOSE BETWEEN ROW 7 TO ROW 9. / R&R LENS IAW AMM.
Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 70,110 hrs · 41,124 cycles
L/H CABIN STOWBIN EMERGENCY LIGHT LENS LOOSE BETWEEN ROW 6 TO ROW 8. R&R LENS IAW AMM.
Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 70,110 hrs · 41,124 cycles
L\H HORIZONTAL STAB AT FWD TERMINAL FITTING LOWER SLIDING SEAL CRACKED. / REMOVED AND REPLACED L/H HORIZONTAL STAB LOWER FWD SLIDING SEAL; PLATE; AND FITTING I/A/W 737 AMM 53-31-31-400-801; BOEING DWG 181A8012 REV. A; AND 737-700 SRM 51-40-02-0G-0 ATAG'S A82207; A81365; AND N10627
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 70,110 hrs · 41,124 cycles
KEEL BEAM STIFFENER ON FORWARD SIDE VAPOR BARRIER CRACKED AT BS. 663, RBL 6.30. R&R STIFFENER IAW SRM, DWG, & EA.
Part: DOOR FRAME — CRACKED (L1 DOOR) · airframe 70,110 hrs · 41,124 cycles
L1 DOOR AFT FRAME LOWER EDGE CRACKED IN RADIUS INBOARD OF STOP PIN FITTING. R&R AFT FRAME IAW SRM AND DWG.
Part: STRINGER SPLICE — CORRODED (BS 344-380) · airframe 70,110 hrs · 41,124 cycles
EQUIPMENT AND ELECTRONICS COMPARTMENT BILGE AREA STRINGER SPLICE CORRODED BETWEEN BS. 344 TO BS. 380, STR. 27R. R & R STRINGER SPLICE IAW SRM & DWG.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,110 hrs · 41,124 cycles
STRINGER CLIP CRACKED AT BS. 294.5, STR. 13L. R&R STRINGER CLIP IAW DWG AND SRM.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 70,110 hrs · 41,124 cycles
L/H HORIZONTAL STABILIZER LEADING EDGE PANEL 341B, STARTING INBOARD TO OUTBOARD 6TH RIB CRACKED. R&R RIB ASSEMBLY IAW DWG, SRM, AND AMM.
Part: STRINGER CLIP — CRACKED (BS 261) · airframe 70,110 hrs · 41,124 cycles
STRINGER SUPPORT CLIP CRACKED IN RADIUS AT BS. 261, STR. 10L. / R&R CLIP IAW SRM AND DWG.
Part: FLOOR PANEL — CORRODED (FWD CARGO BAY) · airframe 70,110 hrs · 41,124 cycles
FORWARD CARGO PIT FLOOR PANEL 120BF UPPER SURFACE LEFT SIDE EDGE HAS CORROSION / FOUND PANEL 120BF TO BE OUT OF LIMITS WITH MORE THAT 30% DAMAGE DUE TO WORN/WARPED SURFACE IAW SRM 53-00-53-1A-1 STEP 5. VERIFIED RECEIVED REPLACEMENT FLOOR PANEL P/.N 453A1610-4 ATAG WN3993. IAW AIPC 25-52-10-01
Part: SKIN — CORRODED (E&E BAY) · airframe 70,110 hrs · 41,124 cycles
E&E COMPARTMENT STA 360 STR 26L HAS SPOT OF CORROSION / REMOVED CORROSION IN E & E COMPARTMENT AT STA 360 STR 26L VERIFIED MATERIAL LOSS. ORIG 'T' IS .071; REMAINING .068. LOSS OF .003. SRM HAS NO LIMITS IN THIS AREA. REPAIRED IAW AAR EA 190442 IR AND SWA EA 1-753-35043 REV IR
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 70,110 hrs · 41,124 cycles
EQUIPMENT & ELECTRONICS COMPARTMENT BILGE AREA STRINGER SPLICE CORRODED BETWEEN BS. 344 TO BS. 380, STR. 28L. R&R STRINGER SPLICE IAW SRM AND DWG.
Part: STRAP — DAMAGED (RT EMERGEN EXIT) · airframe 70,110 hrs · 41,124 cycles
R/H EMERGENCY EXIT HATCH ESCAPE STRAP HOOK ASSEMBLY CORRODED. R&R STRAP IAW AMM.
Part: FLOOR PANEL — CORRODED (AFT CARGO BAY) · airframe 70,110 hrs · 41,124 cycles
AFT CARGO COMPARTMENT MID FLOOR PANEL #140CF HAS CORROSION. / FOUND PANEL 140CF TO BE OUT OF LIMITS MORE THAT 30% OF PANL DUE TO WORN WARPED SURFACE IAW SRM 53-00-53-1A-1. VERIFIED RECEIVED REPLACEMENT PANEL 140CF P/N 453A2610-2 ATAG WN1465 IAW AIPC 25-52-10-02
Part: STIFFENER — CRACKED (BS 663 BULKHEAD) · airframe 70,110 hrs · 41,124 cycles
VAPOR BARRIER KEEL BEAM STIFFENER CRACKED ON AFT SIDE OF BS. 663, RBL 6.30. / R&R STIFFENER IAW SRM AND DWG.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 70,110 hrs · 41,124 cycles
STRINGER CLIP CRACKED AT BS. 277, STR. 10R. R&R STRINGER CLIP IAW DWG & SRM.
Part: INTERCOSTAL — CRACKED (AFT CARGO BAY) · airframe 70,110 hrs · 41,124 cycles
AFT CARGO COMPARTMENT STA 947.5 -1' RBL 21.50 UNDER R/H Z ANGLE ON OUTBD BOTTOM SIDE INTERCOASTAL HAS A 3' LONG CRACK AS MARKED / REMOVED AND REPLACED AFT CARGO INTERCOSTAL STA 927-947 SRM 21.5 IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 & SWG 146A7508 REV C. FABRICATED INTERCOSTAL ON BACKSHOP W/O 39562-1600-0001 TREATED & PRIMED IAW AMM 51-21-72-370-809 & SRM 51-20-01-0G-0.
Part: FLOOR SUPPORT — CORRODED (BS 747) · airframe 70,110 hrs · 41,124 cycles
AFT CARGO COMPARTMENT BILGE AREA FLOOR SUPPORT ANGLE CORRODED AT BS. 747+15, RBL 19.5. / R&R STRINGER CLIP IAW SRM.
Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 70,110 hrs · 41,124 cycles
AFT CARGO COMPARTMENT FWD SHIELD HAS CORROSION ON THE UNDERSIDE._STA. 787 RBL 20.5 ' / REMOVED DAMAGE IN AFT CARGO FWD SHIELD IAW SRM 51-10-02-060 ORIG. MAT .063' MAT . LOSS .009' MAT. REMAINING .054'. OUTOF LIMITS IAW SRM 53-00-53-1A-2 AAR TOOL 36644 DUE 19-SEP-19. REMOVED AND REPLACED AFT CARGO FWD SHIELD STA 767-787 IAW SRM 51-40-02-0G0; SRM 51-40-05-0G-0. DWG 146A0081 REV C.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,110 hrs · 41,124 cycles
FLOOR SUPPORT BEAM CORRODED. R&R FLOORBEAM REPAIR CHANNEL IAW EQ.
Part: SUPPORT ANGLE — CRACKED (AFT CARGO BAY) · airframe 70,110 hrs · 41,124 cycles
AFT CARGO COMPARTMENT STA 867- 2'; LBL 10' LOWER SUPPORT ANGLE BRACKET FOR WASTE WATER BULKHEAD FRAME IS CRACKED AS MARKED / REMOVED & REPLACED AFT CARGO STA 867-2 LBL10 LOWER SUPPORT ANGLE BRACKET IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 & DWG 149A8109 REV B
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,110 hrs · 41,124 cycles
FLOOR SUPPORT BEAM CORRODED. R&R FLOOR SUPPORT BEAM PER SRM.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 70,110 hrs · 41,124 cycles
FLOOR SUPPORT BEAM CORRODED. R&R FLOORBEAM IAW SRM
Part: ANGLE — CRACKED (LT WING) · airframe 70,110 hrs · 41,124 cycles
LH WING; 2.5' INBOARD OF DEFLECTION RIB; LATERAL WEB IS CRACKED IN UPPER FLANGE COMMON TO O/B FASTNER / L/H WING 2.5' I/B OF DFLECTION RIB; REMOVED AND REPLACED LATERAL WEB (ANGLE) PN 115A2156047-770529-ATAG WN3234; IAW SRM 51-40-02-0G-0 AND BOEING DWG 115A2156 REV D AND DWG 115A2512 REV B.
Part: FLOORBEAM — CORRODED (AFT CARGO BAY) · airframe 70,110 hrs · 41,124 cycles
AFT CARGO COMPARTMENT FWD SCREW HOLES ON THE RIGHT OF THE FIRST TIE DOWN HAS CORROSION INSIDE. LOCATION 15' TO THE RIGHT OF BL0. / REMOVED CORROSION ON SCREW HOLES ON AFT CARGO TRACK TIE DOWN STA 727A RBL 13.5 IAW SRM 51-10-02-0G-0. VERIFIED MAT. LOSS .020' ORIG MAT .070' MAT. REMAINING .050' OUT OF LIMITS IAW SRM 53-00-53-1A-2 AAR TOOL 36308 DUE 19APR20. AFT CARGO FLOOR TRACK/BEAM REMOVED & REPLACED STA 727-887 RBL 13.5' P/N 146A7501-25
Part: RETAINER — CRACKED (LT WING) · airframe 70,110 hrs · 41,124 cycles
LH WING 10' INBOARD OF DEFLECTION RIB; CURVED SEAL RETAINER ON AFT SIDE OF LONGITUDINAL WEB IS CRACKED AT LOWER FASTNER HOLE / L/H WING I/B OF DEFLECTION RIB; REMOVED AND REPLACED CURVED SEAL RETAINER (WEB) PN 115A2982-9; IAW BOEING DWG 115A2930 REV- ATAG A72167; AND SRM 51-40-00-0G-0 & BOEING DWG 115A2900 REV E.
Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 70,110 hrs · 41,124 cycles
AFT CARGO COMPARMENT RH Z ANGLE HAS CORROSION FROM STA. 727 TO STA. 767._RBL 29.5' / REMOVED DAMAGE ORIG MAT .040 MAT LOSS .040' MAT REMAINING 0.00' FOUND OUT OF LIMITS IAW B737-700 SRM 53-00-53-1A-2. FABRICATED & INSTALLED RH 'Z' ANGLE IAW SWG PL 146A7502 REV.A & SRM 51-40-02-0G-0 146A7502-2
Part: TIE DOWN — CORRODED (AFT CARGO BAY) · airframe 70,110 hrs · 41,124 cycles
AFT CARGO COMPARTMENT 2ND FLOOR TIE DOWN ON THE LH SIDE AFT NUT PLATE HAS CORROSION ON THE AFT OUTBD. / REMOVED & REPLACED AFT CARGO 2ND FLOOR TIE DOWN L/H SIDE AFT NUT PLATE IAW B 737-700 SRM 51-40-02-0G-0
Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 70,110 hrs · 41,124 cycles
AFT CARGO COMPARTMENT LH 'Z' ANGLE AT STA. 727B+15' HAS A SPOT OF CORROSION. / REMOVED CORROSION ON LH Z ANGLE IN AFT PIT STA 727 BHS IAW SRM 51-10-02-0G-0. MAT LOSS .015' ORIG MAT .040' MAT. REMAINING .025' OUT OF LIMITS IAW SRM 53-00-53-1A-2. AAR TOOL 36308 DUE 19-APR-20. REMOVED + REPLACED AFT CARGO LH Z ANGLE STA 727-847 IAW SRM 53-00-53-1A-2; 53-00-53-2R-6 SRM 51-40-02--0G-0. DWG 146A7500 REV A + SRM 51-40-05-0G-0. TREATED + PRIMED ZANGLE IAW AMM 51-21-72-370-804 + SRM 51-20-01-0G-0
Part: WEB — CORRODED (AFT CARGO THRESH) · airframe 70,110 hrs · 41,124 cycles
AFT CARGO DOOR UNDER CENTER TRESHOLD BETWEEN STA 847 AND 787+6.50 TRESHOLD WEB SKIN HAS SEVERAL AREAS OF CORROSION AS MARKED TOP SURFACE / REMOVED DAMAGE ON THRESHOLD WEB (IAW SRM 51-10-02-0G-0) ORIG MAT. .050' MAT LOSS .030' MAT REMAINING .020' FOUND OUT OF LIMITS IAW B737-700 SRM 53-00-53-1A-2. INSTALLED NEW THRESHOLD WEB IN AFT CARGO AT STA 847 AND 787 + 6.50 IAW B737-700 SRM 51-40-02-0G-0
Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 70,110 hrs · 41,124 cycles
MLG HORIZONTAL PRESSURE DECK CRACKED AT BS. 665, RBL41. R&R WEB CUTOUT PER SRM.
Part: PRESSURE PANEL — CRACKED (LT M LG WW) · airframe 70,110 hrs · 41,124 cycles
LT HORIZONTAL PRESSURE WEB FASTENER HOLES CRACKED AT BS. 663, LBL 30. REPAIRED WEB PER EA.
Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 70,110 hrs · 41,124 cycles
MLG HORIZONTAL PRESSURE DECK CRACKED AT BS. 671, RBL 42. REPAIRED WEB CUTOUT PER SRM.
Part: MOUNT — BROKEN (R2 DOOR) · airframe 70,110 hrs · 41,124 cycles
R2 DOOR AFT SLIDE BRACKET UPPER ISOLATION MOUNT BROKEN. R&R UPPER ISOLATION MOUNT IAW SRM.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 70,110 hrs · 41,124 cycles
R2 DOOR CUTOUT FORWARD FRAME JUST ABOVE LOWER LATCH RECEIVER EVIDENCE OF CRACK IN CURVE OF FRAME. R&R FRAME IAW SRM AND DWG.
Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 70,110 hrs · 41,124 cycles
MLG HORIZONTAL PRESSURE DECK CRACKED AT BS. 665, RBL 39. R&R WEB CUTOUT PER SRM.
Part: BEAM — CRACKED (R1 DOOR) · airframe 70,110 hrs · 41,124 cycles
R1 DOOR LOWER BEAM #4 CRACKED. R&R #4 BEAM IAW SRM AND DWG.
Part: REPAIR — DETERIORATED (BULKHEAD WEB) · airframe 70,110 hrs · 41,124 cycles
L/H VAPOR BARRIER EXISTING REPAIR DETERIORATED AT BS. 663, REQUIRING COMPOSITE REPAIR. REPAIRED L/H VAPOR BARRIER WEB IAW SRM.
Part: BULKHEAD WEB — CRACKED (BS 1016) · airframe 70,110 hrs · 41,124 cycles
AFT PRESSURE BULKHEAD WEB LAP SPLICE CRACKED AT BS. 1016, STR. 7R, BETWEEN FIRST AND SECOND TEAR STRAPS. REPAIRED DOUBLER IAW EA.
Part: BATTERY PACK — FAILED (CABIN) · airframe 70,110 hrs · 41,124 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1674. R&R BATTERY PACK AND POWER SUPPLY PER MM.
Part: ROD END — BROKEN (L1 DOOR) · airframe 69,713 hrs · 40,869 cycles
AFTER FLIGHT, L1 DOOR WOULD NOT OPEN. FOUND L1 DOOR LOWER ROD END ON ROD FROM HANDLE MECHANISM TO LOWER TORQUE TUBE BROKEN. R&R ROD END PER SIP.
Part: SKIN — CRACKED (RT WING) · airframe 69,685 hrs · 40,851 cycles
RT WING LEADING EDGE PANEL UNDERLYING STRUCTURE CRACKED AT UPPER AFT OUTBOARD CORNER OF PANEL INBOARD OF CORNER AT HOLE 4. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (RT WING) · airframe 69,685 hrs · 40,851 cycles
RT WING LEADING EDGE PANEL UNDERLYING STRUCTURE CRACKED AT UPPER AFT OUTBOARD CORNER OF PANEL FORWARD OF THE CORNER AT HOLE 15. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (RT WING) · airframe 69,685 hrs · 40,851 cycles
RT WING LEADING EDGE PANEL UNDERLYING STRUCTURE CRACKED AT UPPER AFT OUTBOARD CORNER OF PANEL FORWARD OF THE CORNER AT HOLE 12. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (RT WING) · airframe 69,685 hrs · 40,851 cycles
RT WING LEADING EDGE PANEL UNDERLYING STRUCTURE CRACKED AT UPPER AFT OUTBOARD CORNER OF PANEL FORWARD OF THE CORNER AT HOLE 5. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (RT WING) · airframe 69,685 hrs · 40,851 cycles
RT WING LEADING EDGE PANEL UNDERLYING STRUCTURE CRACKED AT UPPER AFT OUTBOARD CORNER OF PANEL FORWARD OF THE CORNER AT HOLE 3. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (RT WING) · airframe 69,685 hrs · 40,851 cycles
RT WING LEADING EDGE PANEL UNDERLYING STRUCTURE CRACKED AT UPPER AFT OUTBOARD CORNER OF PANEL FORWARD OF THE CORNER AT HOLE 7. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (RT WING) · airframe 69,685 hrs · 40,851 cycles
RT WING LEADING EDGE PANEL UNDERLYING STRUCTURE CRACKED AT UPPER AFT OUTBOARD CORNER OF PANEL FORWARD OF THE CORNER AT HOLE 11. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (RT WING) · airframe 69,685 hrs · 40,851 cycles
RT WING LEADING EDGE PANEL UNDERLYING STRUCTURE CRACKED AT UPPER AFT OUTBOARD CORNER OF PANEL FORWARD OF THE CORNER AT HOLE 4. REPAIRED SKIN PER EA.
Part: SKIN PANEL — CRACKED (RT WING) · airframe 69,685 hrs · 40,851 cycles
15TH COUNTERSUNK HOLE INBOARD OF THE RT WING SKIN PANEL UPPER AFT OUTBOARD CORNER CRACKED. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (RT WING) · airframe 69,685 hrs · 40,851 cycles
RT WING LEADING EDGE PANEL UNDERLYING STRUCTURE CRACKED AT UPPER AFT OUTBOARD CORNER OF PANEL INBOARD OF CORNER AT HOLE 10. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (RT WING) · airframe 69,685 hrs · 40,851 cycles
RT WING LEADING EDGE PANEL UNDERLYING STRUCTURE CRACKED AT UPPER AFT OUTBOARD CORNER OF PANEL INBOARD OF CORNER AT HOLE 2. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (RT WING) · airframe 69,685 hrs · 40,851 cycles
3RD COUNTERSUNK HOLE FORWARD OF THE RT WING SKIN PANEL UPPER AFT OUTBOARD CORNER CRACKED. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (RT WING) · airframe 69,685 hrs · 40,851 cycles
RT WING LEADING EDGE PANEL UNDERLYING STRUCTURE CRACKED AT UPPER AFT OUTBOARD CORNER OF PANEL FORWARD OF THE CORNER AT HOLE 8. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (RT WING) · airframe 69,685 hrs · 40,851 cycles
RT WING LEADING EDGE PANEL UNDERLYING STRUCTURE CRACKED AT UPPER AFT OUTBOARD CORNER OF PANEL FORWARD OF THE CORNER AT HOLE 2. REPAIRED SKIN PER EA.
Part: SKIN — CRACKED (RT WING) · airframe 69,685 hrs · 40,851 cycles
RT WING LEADING EDGE PANEL UNDERLYING STRUCTURE CRACKED AT UPPER AFT OUTBOARD CORNER OF PANEL INBOARD OF CORNER AT HOLE 6. REPAIRED SKIN PER EA.
2018
Part: WEDGE — DEBONDED (RH INBD MAIN FLA) · airframe 68,381 hrs · 40,000 cycles
RIGHT INBOARD MAINFLAP OUTBOARD WEDGE PANEL IS SPLIT; DISBONDED AT TRAILING EDGE. / REMOVED & REPLACED RIGHT INBOARD MAIN FLAP OUTBOARD WEDGE PANEL . I.A.W. SRM 51-40-02
Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,365 hrs · 39,986 cycles
LT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.
Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,365 hrs · 39,986 cycles
RT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED FITTING PER EA.
Part: PANEL — CRACKED (LT WING) · airframe 68,365 hrs · 39,986 cycles
LT MLG LT UPPER TRAILING EDGE PNL CLIP CRACKED / REMOVED AND REPLACED LT MLG UPPER TRAILING_EDGE PANEL CLIP PER SRM 51-40-02
Part: PANEL — CRACKED (RT WING) · airframe 68,365 hrs · 39,986 cycles
RT MLG RT UPPER TRAIL EDGE PNL CLIP CRACKED / R/R'ED RT MLG RT UPPER TRAILING EDGE PANEL CLIP PER SRM 51-40-02
Part: LINE — LEAKING (AC BAY) · airframe 66,969 hrs · 39,095 cycles
DIVERSION/DECLARED EMERGENCY, AUTO FAIL LIGHT ON PRESS CONTROLLER, SWITCHED TO ALT AND AGAIN AUTOFAIL, SWITCHED TO MAN AND CONTROLLED FOR ABOUT 5 MIN AND THEN CABIN ALT STARTED CLIMBING. FOUND WATER FILTER SUPPLY LINER LEAKING ABOVE OUTFLOW VALVE. R&R LINE IAW MM.
Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 66,951 hrs · 39,085 cycles
DECLARED EMERGENCY, AUTO FAIL & ALT ON PRES PANEL ILLUMINATED AT 380 MSL AFTER A FEW SECONDS ALT LIGHT WENT OUT SWITCHED TO MANUAL AUT FLOW VALVE FULL CLOSED CABIN STILL CONTINUED TO CLIMB; O2 MASKS DEPLOYED AFTER OPENING / PAX O2 SWITCH NOTED DASHED LINES ON FLT&LND ALT WINDOWS. R&R NR 1 CABIN PRESSURE CONTROLLER PER MM.
Part: OUTFLOW VALVE — FAULTY (AC BAY) · airframe 66,951 hrs · 39,085 cycles
DECLARED EMERGENCY, AUTO FAIL & ALT ON PRES PANEL ILLUMINATED AT 380 MSL AFTER A FEW SECONDS ALT LIGHT WENT OUT SWITCHED TO MANUAL AUT FLOW VALVE FULL CLOSED CABIN STILL CONTINUED TO CLIMB; O2 MASKS DEPLOYED AFTER OPENING, PAX O2 SWITCH NOTED DASHED LINES ON FLT&LND ALT WINDOWS. R&R CABIN OUTFLOW VALVE PER MM.
Part: CONTROLLER — FAULTY (AC BAY) · airframe 66,951 hrs · 39,085 cycles
DECLARED EMERGENCY, AUTO FAIL & ALT ON PRES PANEL ILLUMINATED AT 380 MSL AFTER A FEW SECONDS ALT LIGHT WENT OUT SWITCHED TO MANUAL AUT FLOW VALVE FULL CLOSED CABIN STILL CONTINUED TO CLIMB; O2 MASKS DEPLOYED AFTER OPENING / PAX O2 SWITCH NOTED DASHED LINES ON FLT&LND ALT WINDOWS. R&R NR 2 CABIN PRESSURE CONTROLLER PER MM.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 66,951 hrs · 39,085 cycles
R1 DOOR SURROUND STRUCTURE "STUB FRAME" CRACKED AT BS 290, BETWEEN STR 5R TO STR 9R. R&R STUB FRAME IAW SRM AND DWG.
Part: SEAL — CRACKED (RH HOR STAB) · airframe 66,240 hrs · 38,645 cycles
RH HORIZONTAL STAB. FWD UPPER SLIDER IS CRACKED / R&R RH HORIZONTAL STAB. FWD UPPER SLIDER REF AMM 53-31-31.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 66,240 hrs · 38,645 cycles
EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT M1669. R & R THE BATTERY PACK IAW AMM.
Part: SIGN — LOOSE (CABIN) · airframe 65,907 hrs · 38,451 cycles
RT OVERWING LOWER EXIT SIGN LOOSE. SECURED SIGN PER SIP.
2017
Part: LENS — LOOSE (CABIN) · airframe 65,103 hrs · 37,939 cycles
RT OVERWING EMERGENCY EXIT LOWER EXIT SIGN LENS LOOSE. INSTALLED LENS ASSEMBLY PER AMM.
Part: PANEL — DELAMINATED (LH PYLON) · airframe 65,082 hrs · 37,925 cycles
PANEL 431ER ON #1 ENGINE INBOARD PYLON; (THRUST REVERSER STRUT FAIRING PANEL) IS DELAMINATED; ON LOWER FWD CORNER; THROUGH SEVERAL LAYERS AND MEASURES 4 1/2' X 3'; OUT OF ALLOWABLE DAMAGE LIMITS IN SRM 54-50-70-1A-2 PARAGRAPH 4.C. (1) (D) / REFERENCE L/P 0247618 REMOVED DISCREPANT PANEL 431ER INSTALLED SERVICEABLE PANEL IAW AMM 51-40-04. CLOSING #23045.
Part: BRACKET — INOPERATIVE (L1 DOOR) · airframe 64,875 hrs · 37,794 cycles
L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LATCH INOP. R&R BRACKET IAW MM.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 64,424 hrs · 37,506 cycles
EMERGENCY EXIT AISLE LIGHT LENS MISSING. REPLACED THE LENS IAW MM.
Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 64,171 hrs · 37,351 cycles
EMERGENCY LIGHT BATTERIES FAILED A CAPACITY TEST AT LOCATION M1670. R & R THE BATTERY IAW AMM AND DWG.
Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 64,171 hrs · 37,351 cycles
EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1672. R & R THE BATTERY IAW AMM AND DWG.
Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 64,171 hrs · 37,351 cycles
EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATION M1673. R & R THE BATTERY IAW AMM AND DWG.
Part: WEDGE — DELAMINATED (LH INBD FLAP) · airframe 64,171 hrs · 37,351 cycles
LEFT WING INBD MAIN FLAP OUTBD WEDGE CORNER LOWER SKIN HAS A DELAMINATION MEASURING 3.5 IN WIDE BY 8IN LONG. / REMOVED AND REPLACED INBD MAIN LH FLAP WEDGE PN# 113A2500-13 IAW SRM 51-40-02 AND 51-10-02
Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 63,782 hrs · 37,129 cycles
CRACK ON CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT / PAIRED BY WELDING CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW EA NO.1-A53-2076- REV.11.
Part: PLATE — CRACKED (LEFT WING) · airframe 63,782 hrs · 37,129 cycles
BROKEN WIGGLE PLATE ON TRAILLING EDGE ACCESS PANEL 551GB AT LT WING / REPLACED WIGGLET PLATE ON TRAILING EDGE ACCESS PANEL 551GB AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING #115A2001 REV 0
Part: FLOOR PANEL — CRACKED (AFT CARGO THRESH) · airframe 63,782 hrs · 37,129 cycles
CRACK ON AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT / AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT REPAIRED BY WELDS IAW EA NO. 1-A53-2076- REV. 11
Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 63,782 hrs · 37,129 cycles
CRACK ON CENTER SCUFF PLATE AT FWD CARGO COMPARTMENT / REPAIRED BY WELDING CENTER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW EA NO.1-A53-2076 REV.11
Part: ANGLE — BROKEN (RT WING) · airframe 63,782 hrs · 37,129 cycles
BROKEN ANGLE LOCATED ON ACCESS PANEL #651FB AT RT WING / REPLACED ANGLE (BRAKET) LOCATED ON ACCESS PANEL #651FB AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 DUE TO NOT FOUND ALLOWABLE DAMAGE IN SRM B737-700 FOR CRACK
Part: ANGLE — CRACKED (RT WING) · airframe 63,782 hrs · 37,129 cycles
RIGHT WING TRAILING EDGE AREA ANGLE CRACKED AT ORSS 290. R & R THE ANGLE IAW SRM AND DWG.
Part: ANGLE — CRACKED (LT WING TE) · airframe 63,782 hrs · 37,129 cycles
LEFT WING TRAILING EDGE AREA ANGLE CRACKED AT ORSS 290. R & R THE ANGLE IAW AND DWG.
Part: LIGHT — BROKEN (CABIN) · airframe 63,782 hrs · 37,129 cycles
EMERGENCY EXIT LIGHT BROKEN AT SIDEWALL PANEL 232YHM. R&R LIGHT ASSY PER MM.
Part: SUPPORT — CRACKED (BS 907-927) · airframe 63,782 hrs · 37,129 cycles
AFT CARGO BAY ANGLE SUPPORT CRACKED BETWEEN BS 907 TO 927, BETWEEN STRINGERS 25 TO 27R. R & R THE SUPPORT IAW SRM AND DWG.
Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 63,782 hrs · 37,129 cycles
RIGHT AFT EXIT LIGHT LENS BROKEN. R & R THE LENS IAW MM.
Part: FRAME — CRACKED (BS 727) · airframe 63,782 hrs · 37,129 cycles
RIGHT FUSELAGE FRAME CRACKED AT BS 727, WL 200. REPAIRED THE FRAME IAW EA.
Part: LENS — DELAMINATED (EMERGENCY LIGHT) · airframe 63,782 hrs · 37,129 cycles
RIGHT OVERHEAD STOWAGE BIN EMERGENCY LIGHT LENS DELAMINATED AT ROW 5. R & R THE LENS IAW AMM.
Part: LIGHT — BROKEN (CABIN FLOOR) · airframe 63,782 hrs · 37,129 cycles
EMERGENCY LIGHT STRIP BROKEN. R & R THE EMERGENCY LIGHT IAW MM.
Part: SKIN — DELAMINATED (TAILCONE) · airframe 63,782 hrs · 37,129 cycles
RIGHT TAIL CONE SKIN DELAMINATED AT BS 1156 +9. REPAIRED SKIN IAW SRM.
Part: SKIN — CRACKED (NR 6 SLAT) · airframe 63,782 hrs · 37,129 cycles
NR 6 L/E SLAT LOWER SKIN CRACKED AT ACTUATOR CUTOUT. R & R THE SLAT IAW MM.
Part: SKIN — CRACKED (LT WING SLAT) · airframe 63,782 hrs · 37,129 cycles
LEFT WING NR 3 SLAT SKIN CRACKED LOWER ACTUATOR AREA. REPAIRED THE SKIN IAW SRM.
Part: SKIN — CRACKED (NR 4 SLAT) · airframe 63,782 hrs · 37,129 cycles
NR 4 L/E SLAT LOWER SKIN CRACKED AT ACTUATOR CUTOUT. R & R THE SLAT IAW MM.
2016
Part: COVER — MISSING (EXIT SIGN) · airframe 60,476 hrs · 35,150 cycles
R2 DOOR EMER EXIT SIGN COVER MISSING. R & R SIGN IAW AMM.
Part: LIGHT — LOOSE (CABIN) · airframe 60,244 hrs · 35,018 cycles
LEFT BULLNOSE EMER LIGHT LOOSE AT ROW 4. SECURED LIGHT ASSEMBLY IAW AMM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 60,244 hrs · 35,018 cycles
LEFT FORWARD CABIN BATTERY PACK FAILED CAPACITY FUNCTION CHECK. R & R BATTERY PACK IAW AMM.
Part: BATTERY — FAILED (CABIN) · airframe 60,244 hrs · 35,018 cycles
RIGHT FWD CABIN BATTERY PACK FAILED CAPACITY FUNCTION CHECK. R & R BATTERY IAW AMM.
2015
Part: LENS — MISSING (CABIN) · airframe 58,268 hrs · 33,857 cycles
LEFT EMER EXIT LENS MISSING. INSTALLED LENS IAW SIP.
Part: SIGN — UNSECURE (CABIN) · airframe 58,074 hrs · 33,738 cycles
FORWARD GALLEY LOWER EMER EXIT SIGN FELL OFF ON TAKEOFF. R & R SIGN AMM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,524 hrs · 33,429 cycles
LEFT BULLNOSE EMER LIGHT INOPERATIVE BETWEEN ROW 5 - 6. R & R BATTERY PACK IAW MM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,524 hrs · 33,429 cycles
FRAME WEB CRACKED AT BS 259, STRINGER 9L. REPAIRED WEB IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,524 hrs · 33,429 cycles
FUSELAGE FRAME CRACKED AT STATION 747, STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 57,524 hrs · 33,429 cycles
RIGHT HORIZONTAL STABILIZER RIB 92.70, NR 1 VERTICAL STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.
Part: FRAME — CRACKED (BS 867) · airframe 57,524 hrs · 33,429 cycles
FOUND THE FUSELAGE FRAME CRACKED AT BS 867, STRINGER 8L. REPAIRED THE FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,524 hrs · 33,429 cycles
FUSELAGE FRAME CRACKED AT STATION 360, STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,524 hrs · 33,429 cycles
FRAME WEB CRACKED AT BS 727B, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (BS 747) · airframe 57,524 hrs · 33,429 cycles
FOUND THE FUSELAGE FRAME CRACKED AT BS 747, STRINGER 8L. REPAIRED THE FRAME IAW EA.
Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 57,524 hrs · 33,429 cycles
RIGHT HORIZONTAL STABILIZER RIB 92.70, NR 2 VERTICAL STIFFENER CRACKED. REPAIRED STIFFENER IAW EA.
Part: STRINGER CLIP — CRACKED (BS 360) · airframe 57,524 hrs · 33,429 cycles
FOUND THE STRINGER CLIP CRACKED AT BS 360, S8R. R & R THE STRINGER CLIP IAW SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,524 hrs · 33,429 cycles
FUSELAGE FRAME CRACKED AT STATION 727D, STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,524 hrs · 33,429 cycles
FRAME CRACKED AT BS 907, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (BS 787) · airframe 57,524 hrs · 33,429 cycles
FOUND THE FUSELAGE FRAME CRACKED AT BS 787, STRINGERS 8 - 9R. REPAIRED THE FRAME IAW EA.
Part: FRAME — CRACKED (BS 360) · airframe 57,524 hrs · 33,429 cycles
FOUND THE FUSELAGE FRAME CRACKED AT BS 360, STRINGER 9R. REPAIRED THE FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,524 hrs · 33,429 cycles
FRAME CRACKED AT BS 787, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,524 hrs · 33,429 cycles
STRINGER CLIP CRACKED AT STATION 360, STRINGER 8R. R & R CLIP IAW SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,524 hrs · 33,429 cycles
FUSELAGE FRAME CRACKED AT STATION 500A, STRINGER 8R - 9A. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,524 hrs · 33,429 cycles
FUSELAGE FRAME CRACKED AT STATION 787, STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,524 hrs · 33,429 cycles
FRAME CRACKED AT BS 827, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,524 hrs · 33,429 cycles
FUSELAGE FRAME CRACKED AT STATION 727D, STRINGER 8L. REPAIRED FRAME IAW EA.
Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 57,524 hrs · 33,429 cycles
RIGHT HORIZONTAL STABILIZER RIB 92.70, NR 3 VERTICAL STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,524 hrs · 33,429 cycles
FUSELAGE FRAME CRACKED AT STATION 867, STRINGER 8R - 9R. REPAIRED FRAME IAW EA.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 57,524 hrs · 33,429 cycles
RIGHT NR 1 WINDOW FRAME UPPER OTBD CORNER CRACKED. REPAIRED FRAME IAW ACO.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,524 hrs · 33,429 cycles
LEFT HORIZONTAL STAB RIB CRACKED AT AFT SPAR STATION 111.10. R & R RIB IAW SRM.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,524 hrs · 33,429 cycles
FORWARD SEAT TRACK OTBD FLANGE, FWD & AFT HOLES & INBD FLANGE, FWD & AFT HOLES CRACKED AT BS 727B, LBL 45.5. REPAIRED FLANGE IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,524 hrs · 33,429 cycles
FORWARD SEAT TRACK OTBD FLANGE, FWD & AFT HOLES & INBD FLANGE, AFT HOLE CRACKED AT BS 727B, LBL 24.75. REPAIRED FLANGE IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,524 hrs · 33,429 cycles
FORWARD SEAT TRACK OTBD FLANGE, FWD HOLE CRACKED AT BS 727B, RBL 45.5. REPAIRED FLANGE IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 57,524 hrs · 33,429 cycles
CABIN SEAT TRACK CRACKED AT STATION 727B, RBL 24.75. REPAIRED TRACK IAW EA.
Part: SKIN — CRACKED (LE SLAT) · airframe 57,524 hrs · 33,429 cycles
RIGHT WING NR 7 SLAT, LE SLAT NOSE SKIN AT ACTUATOR RIB, LOWER SURFACE CRACKED AT SLAT STATION 322.71. REPAIRED SKIN IAW SRM.
Part: POST — CRACKED (FUSELAGE) · airframe 57,524 hrs · 33,429 cycles
NUMBER 3 LT COCKPIT WINDOW POST CRACKED. R & R POST IAW SRM.
Part: COVER — MISSING (EXIT SIGN) · airframe 56,654 hrs · 32,937 cycles
RIGHT EMER EXIT SIGN COVER MISSING. INSTALLED COVER IAW AMM.
Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 56,204 hrs · 32,670 cycles
RIGHT WING AFT UPPER TE PANEL BETWEEN NR 7 & 8 SPOILERS AFT SUPPORT BRACKET CRACKED AT UPPER OTBD FASTENER. R & R BRACKET IAW SRM.
Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 56,204 hrs · 32,670 cycles
RIGHT WING AFT UPPER TE PANEL BETWEEN NR 7 & 8 SPOILERS AFT SUPPORT BRACKET TO DEFLECTOR BAR ATTACH BRACKET CRACKED AT UPPER FASTENER. R & R BRACKET IAW DWG & SRM.
Part: FAIRING — CRACKED (TE FLAP) · airframe 56,204 hrs · 32,670 cycles
RIGHT WING OTBD AFT FLAP NR 2 TRACK LOWER FAIRING CRACKED. R & R FAIRING IAW SRM.
2014
Part: LENS — MISSING (COCKPIT) · airframe 55,942 hrs · 32,526 cycles
COCKPIT EMER EXIT LIGHT, NOT ARMED, ANNUNCIATOR LENS MISSING. R & R LIGHT IAW MM.
Part: LENS — MISSING (COCKPIT) · airframe 55,942 hrs · 32,526 cycles
COCKPIT EMER EXIT LIGHT, NOT ARMED, ANNUNCIATOR MISSING LENS. R & R LIGHT IAW MM.
Part: CONTROL UNIT — FAULTY (COCKPIT) · airframe 55,093 hrs · 32,044 cycles
CLICKING WITH AN ELEC SMELL COMING FROM BEHIND FIRST OFFICER'S RT SHOULDER. R & R STANDBY POWER CONTROL UNIT IAW MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,516 hrs · 31,700 cycles
LEFT OVERWING EMER EXIT EXTERIOR LIGHT INOPERATIVE. RECHARGED BATTERY PACK IAW AMM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,516 hrs · 31,700 cycles
LEFT OVERWING EMER EXIT INTERIOR LIGHT INOPERATIVE. RECHARGED BATTERY PACK IAW AMM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,516 hrs · 31,700 cycles
LEFT OVERWING EXTERIOR EMER EXIT LIGHT INOPERATIVE. CHARGED BATTERY PACK IAW AMM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,516 hrs · 31,700 cycles
LEFT OVERWING EMER EXIT LIGHT INOPERATIVE. CHARGED BATTERY PACK IAW AMM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,516 hrs · 31,700 cycles
LEFT OVERHEAD STOW BIN EMER LIGHT INOPERATIVE AT ROW 6. CHARGED BATTERY PACK IAW AMM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 54,516 hrs · 31,700 cycles
RIGHT STOW BIN EMER LIGHT INOPERATIVE AT ROW 13. R & R BATTERY IAW MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,516 hrs · 31,700 cycles
SKIN CRACKED AT BS 540 STRINGER 22R. REPAIRED SKIN IAW EA.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,516 hrs · 31,700 cycles
SKIN CRACKED AT BS 540 STRINGER 22R. REPAIRED SKIN IAW EA.
2013
Part: EEC — FAULTY (NR 2 ENGINE) · airframe 52,184 hrs · 30,341 cycles
INFLIGHT SHUTDOWN, AIR TURN BACK NR 2 ENG AUTO SHUT DOWN IN FLIGHT WOULD NOT RE-START. R & R NR 2 ENG EEC & WIRE HARNESS IAW MM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 50,615 hrs · 29,380 cycles
RIGHT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT STA 520. R & R BATTERY IAW MM.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 50,615 hrs · 29,380 cycles
EVIDENCE OF CORROSION FOUND INSIDE AND AFT OF MAIN E & E ENTRY AT STA 360+3, STR 28R. R & R STRINGER IAW SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 50,615 hrs · 29,380 cycles
FLOORBEAM INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 47. R & R INTERCOSTAL IAW SRM.
Part: LENS — CRACKED (CABIN) · airframe 50,615 hrs · 29,380 cycles
LEFT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT LENSES CRACKED BETWEEN ROW 1 TO ROW 23. R & R LENSES IAW MM.
Part: LENS — CRACKED (CABIN) · airframe 50,615 hrs · 29,380 cycles
RIGHT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHTS CRACKED BETWEEN ROW 3 TO ROW 22. R & R LENSES IAW MM.
Part: COVER — LOOSE (CABIN) · airframe 49,847 hrs · 28,908 cycles
EMERGENCY EXIT ROW LIGHT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY PER AMM.
Part: TRIM PANEL — CRACKED (L1 DOOR) · airframe 49,534 hrs · 28,718 cycles
LOWER FLAPPER DOOR OF L1 DOOR HAS TRIM CRACKED IN TWO PLACES. SECURED BACKING TRIM PLATE COVER AS REQUIRED PER MM.
2012
Part: LIGHT — LOOSE (CABIN) · airframe 48,987 hrs · 28,385 cycles
FWD PAX CALL LIGHT LENS WILL NOT STAY ON LIGHT ASSY. REPLACED LIGHT ASSY AFT OF COCKPIT DOOR ON CEILING PANEL AS PER AMM. OPS CHECK GOOD.
Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 48,947 hrs · 28,357 cycles
AIR TURNBACK-- NR 2 OIL FILTER BYPASS LIGHT ILLUMINATED ON DEPARTURE. EXTINGUISHED WHEN POWER REDUCED BELOW APPROX 30 PERCENT N1. POWER ADVANCED TO APPROX 45-55 PERCENT N1 AND LIGHT BACK ON. EXTINGUISHED AGAIN WITH POWER REDUCED. REMOVED AND REPLACED NR 2 ENGINE PER MT.
Part: LIGHT — LOOSE (CABIN) · airframe 47,897 hrs · 27,682 cycles
EEPLS LOOSE AT ROW 8. SECURED EEPLS PER AMM.
Part: BRACKET — LOOSE (GIRT BAR) · airframe 47,897 hrs · 27,682 cycles
R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED BRACKET ASSY PER MM.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 46,946 hrs · 27,114 cycles
AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER M/M.
Part: LENS — LOOSE (CABIN) · airframe 46,238 hrs · 26,697 cycles
BULL NOSE AT ROW 13 RT EMERGENCY LIGHT LENS IS LOOSE. SECURED LENS PER AMM.
Part: LENS — LOOSE (CABIN) · airframe 46,238 hrs · 26,697 cycles
BULL NOSE AT ROW 9 LT EMERGENCY LIGHT LENS IS LOOSE. SECURED LENS PER AMM.
2011
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,050 hrs · 25,435 cycles
DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,050 hrs · 25,435 cycles
DURING SCHEDULED 12Y CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 44,050 hrs · 25,435 cycles
DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR FRAME CRACKED AT BS 294.5, STR 17R. REPAIRED FRAME PER SRM AND EA.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,050 hrs · 25,435 cycles
DURING SCHEDULED 12Y CHECK, FOUND OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 9 TO ROW 11. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 44,050 hrs · 25,435 cycles
DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RECONNECTED CONNECTOR PER WDM.
Part: LENS — LOOSE (EVAC SLIDE) · airframe 44,050 hrs · 25,435 cycles
DURING SCHEDULED 12Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE LENS LOOSE. SECURED LENS PER MM.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 44,050 hrs · 25,435 cycles
DURING SCHEDULED 12Y CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,050 hrs · 25,435 cycles
DURING SCHEDULED 12Y CHECK, FOUND OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 3 TO ROW 7. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 44,050 hrs · 25,435 cycles
DURING SCHEDULED 12Y CHECK, FOUND SKIN CRACKED AT BS 207, RBL 4.5. REPAIRED SKIN IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 44,050 hrs · 25,435 cycles
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME IAW EA.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 44,050 hrs · 25,435 cycles
DURING SCHEDULED 12Y CHECK, FOUND FRAME ANGLE CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED ANGLE PER EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 44,050 hrs · 25,435 cycles
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 44,050 hrs · 25,435 cycles
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 44,050 hrs · 25,435 cycles
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 44,050 hrs · 25,435 cycles
DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME IAW EA.
Part: BATTERY — FAILED (CABIN) · airframe 43,287 hrs · 24,988 cycles
DURING SCHEDULED HC2 CHECK, LT AFT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.
Part: BATTERY — FAILED (CABIN) · airframe 43,287 hrs · 24,988 cycles
DURING SCHEDULED HC2 CHECK, RT AFT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.
Part: BATTERY — FAILED (CABIN) · airframe 43,287 hrs · 24,988 cycles
DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.
2010
Part: VALVE — FAULTY (HYDRAULIC SYS) · airframe 40,268 hrs · 23,217 cycles
DECLARED EMERGENCY - TOTAL LOSS OF "B" SYSTEM HYDRAULICS AT FIRST FLAP POSITIONING. REMOVED AND REPLACED FLOW LIMITING HYDRAULIC VALVE PER MM.
Part: COVER — BROKEN (CABIN) · airframe 39,585 hrs · 22,814 cycles
R2 DOOR EMERGENCY EXIT LIGHT SIGN COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.
2009
Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,602 hrs · 22,233 cycles
EMERGENCY LIGHT INOP AT ROW 16 ABC. RELAMPED PER MM.
Part: WEB — CRACKED (FUSELAGE) · airframe 37,102 hrs · 21,323 cycles
DURING SCHEDULED 10Y CHECK, FOUND LT WHEEL WELL WEB CRACKED AT BS 663, RBL 34. REPAIRED WEB PER AAR EA.
Part: FITTING — CRACKED (CENTER WING) · airframe 37,102 hrs · 21,323 cycles
DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX, UPPER DECK, UPPER CHORD BRACKET CRACKED AT BS 547, RBL 7. REPAIRED FITTING PER SRM.
Part: WEB — CRACKED (FUSELAGE) · airframe 37,102 hrs · 21,323 cycles
DURING SCHEDULED 10Y CHECK, FOUND LT WHEEL WELL WEB CRACKED AT BS 663, LBL 34. REPAIRED WEB PER AAR EA.
Part: FITTING — CRACKED (CENTER WING) · airframe 37,102 hrs · 21,323 cycles
DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX, UPPER DECK, UPPER CHORD BRACKET CRACKED BETWEEN BS 542 TO BS 548, LBL 15. REPAIRED FITTING PER SRM.
Part: SKIN — CRACKED (LE SLAT) · airframe 37,102 hrs · 21,323 cycles
DURING SCHEDULED 10Y CHECK, FOUND RT WING NR 8 SLAT CRACKED ON LOWER SURFACE. REMOVED AND REPLACED SLAT PER MM.
Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 37,101 hrs · 21,323 cycles
DURING SCHEDULED 10Y CHECK, FOUND CABIN EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.
Part: SIGN — BROKEN (CABIN) · airframe 35,843 hrs · 20,579 cycles
L1 DOOR EMERGNECY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.
Part: LUG — CORRODED (LT MLG) · airframe 35,747 hrs · 20,518 cycles
DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.
Part: LUG — CORRODED (RT MLG) · airframe 35,747 hrs · 20,518 cycles
DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.
2008
Part: ENGINE — FAILED (LEFT) · airframe 33,319 hrs · 19,023 cycles
DIVERSION, ON CLIMB AT 12000' HEARD A POP/BANG NOISE ACCOMPANIED BY LOUD WHIRRING NOISE. MAXIMUM VIBRATION ON NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE PER MT.
2007
Part: GLOWSTRIP — LOOSE (CABIN) · airframe 31,987 hrs · 18,179 cycles
EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 DEF. REMOVED AND REPLACED STRIP PER MM.
Part: SKIN — CRACKED (FUSELAGE) · airframe 30,477 hrs · 17,304 cycles
DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE SKIN CRACKED AT EXTERNAL POWER RECEPTACLE CUTOUT AFT END. REPAIRED SKIN PER SWA EA.
Part: FLOORBEAM — CORRODED (BS 903) · airframe 30,477 hrs · 17,304 cycles
DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 903, RBL 8. REPAIRED FLOORBEAM PER SRM.
2006
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 27,289 hrs · 15,493 cycles
DURING SCHEDULED HC1 CHECK, RT OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: GLOWSTRIP — WORN (CABIN) · airframe 27,289 hrs · 15,493 cycles
DURING SCHEDULED HC1 CHECK, FOUND LT AFT CABIN EEPLS PHOTOLUMINESCENT STRIP WORN. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP PER MM.
Part: FAN — FAULTY (A/C DISTRIB BAY) · airframe 25,683 hrs · 14,578 cycles
SMOKE SMELL IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM.
Part: FAN — SEIZED (CABIN AIR) · airframe 25,079 hrs · 14,233 cycles
ODOR IN CABIN. FOUND GASPER FAN SEIZED. REMOVED AND REPLACED FAN PER MM.
2005
Part: SLIDE — FAULTY (L1 DOOR) · airframe 22,292 hrs · 12,726 cycles
L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATING LOW. REMOVED AND REPLACED SLIDE PER MM.
2004
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 19,795 hrs · 11,349 cycles
DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASSY PER MM.
Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 19,521 hrs · 11,195 cycles
DURING SPV, FOUND 2 EACH OVERWING EMERGENCY EXIT LIGHT LENS, LOOSE. SECURED LIGHT LENS PER MM.
Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 19,001 hrs · 10,879 cycles
DURING SCHEDULED C1 CHECK, EMERGENCY EXIT LIGHT BATTERIES FAILED TEST. REMOVED AND REPLACED EMERGENCY EXIT BATTERIES PER MM.
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 19,001 hrs · 10,879 cycles
DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.
2003
Part: COVER — CRACKED (CABIN) · airframe 16,446 hrs · 9,486 cycles
DURING SCHEDULED C3 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS 3, 4, AND 23. REMOVED AND REPLACED TRACK COVERS PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,789 hrs · 8,529 cycles
DURING SCHEDULED SERVICE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.
Part: COVER — CRACKED (CABIN) · airframe 14,104 hrs · 8,164 cycles
DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED (5 EA) IN AFT CABIN. REMOVED AND REPLACED EEPLS COVERS PER MM.
2002
Part: SLIDE — OUT OF ADJUST (AFT SVC DOOR) · airframe 12,908 hrs · 7,527 cycles
DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.
Part: HOOK — LOOSE (FWD ENTRY DOOR) · airframe 12,679 hrs · 7,400 cycles
FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.
Part: BUSHING — WORN (LT ELEVATOR) · airframe 11,499 hrs · 6,748 cycles
DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, FOUND LT ELEVATOR TAB HINGE ATTACH POINTS NR 2, NR 3 AND NR 4 WORN. REMOVED AND REPLACED HARDWARE AND BUSHINGS PER MM.
Part: BUSHING — WORN (RT ELEVATOR) · airframe 11,499 hrs · 6,748 cycles
DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, FOUND RT ELEVATOR TAB HINGE ATTACH POINTS NR 2 AND NR 4 WORN. REMOVED AND REPLACED HARDWARE AND BUSHINGS PER MM.
Part: COALESCER BAG — CONTAMINATED (A/C BAY) · airframe 10,645 hrs · 6,231 cycles
F/A REPORTED ELECTRICAL/RUBBERIZED SMELL COMING FROM AIR COND IN MAIN CABIN DURING FLIGHT. REMOVED AND REPLACED RT AIR CONDITIONING COALESCER BAG.
2001
Part: BULKHEAD — CANNING (FUSELAGE) · airframe 8,834 hrs · 5,158 cycles
DURING SCHEDULED SERVICE CHECK, SI 1157-53 FOUND AFT PRESS BULKHEAD OIL CANNED, BETWEEN STR 2R & 3R. REPAIRED BULKHEAD PER SWA RA 1-753-2705.
Part: BRACKET — LOOSE (FWD ENTRY DOOR) · airframe 8,349 hrs · 4,855 cycles
DURING SCHEDULED BC4 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE ON CONTAINER. SECURED EVAC SLIDE BRACKET PER MM.
Part: GROUND WIRE — LOOSE (CABIN) · airframe 7,500 hrs · 4,369 cycles
DURING SCHEDULED PM CHECK, FOUND EXIT LIGHT INOP AT FWD CEILING. SECURED GROUND WIRE AT CEILING GROUNDING BLOCK PER MM.
Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 5,777 hrs · 3,420 cycles
FWD SECTION LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.
2000
Part: SLIDE — LOOSE (PAX DOOR)
FWD ENTRY DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.