N774SW
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.
290 reports on file, 2001-09-03 – 2022-12-13.
Part: PANEL — DAMAGED (WNG-BDY FAIRING) · airframe 72,453 hrs · 43,099 cycles
WING TO BODY FAIRING PANEL 193B HAS ELONGATED & CRACKED HOLES. R & R THE FAIRING PANEL 193B IAW AMM.53-51-21.
Part: LIGHT — INOPERATIVE (PAX CABIN) · airframe 70,869 hrs · 42,027 cycles
FO SIDE EMERGENCY EXIT WINDOW LIGHT INOP (WING) / [01] OK TO CONTINUE PER MEL 33-2-03 SP1B C/W. R AND R BULB AND FUSE FO SIDE EMERGENCY EXIT WINDOW LIGHT IAW AMM 33-51-04
Part: BRACKET — CRACKED (L/H WING) · airframe 70,806 hrs · 41,985 cycles
I/B T/E SUPPORT BRACKET FOR PANEL 551EB L/H WING IS CRACK. / [01] REMOVED I/B TRAILING EDGE SUPPORT BRACKET FOR ACCESS PANEL 551 EB AS PER BOEING 737 SRM 51-40-02;[02] VERIFIED STEP 1.;[03] CORRECTION: REMOVED AND REPLACED I/B TRAILING EDGE SUPPORT BRACKET(CLIP ASSY) P/N 115A5552-1 AS PER B737 SRM 51-40-02-0G-0.;[04] VERIFIED 3;COMPLETE
Part: GIRT LACING — OUT OF ADJUST (L1 DOOR) · airframe 70,806 hrs · 41,985 cycles
CUSTOMER REQUEST- L1 DOOR SLIDE HAS EXCESSIVE GIRT HANGING DOWN. / [01] READJUSTED L1 DOOR SLIDE GIRT REF B737 AMM 25-66-01-400-803;[02] VERIFIED 1;COMPLETE
Part: ANGLE — CRACKED (FUSELAGE) · airframe 70,806 hrs · 41,985 cycles
SUPPORT ANGLE AT VAPOR BARRIER LH STA 663 CRACKED / [01] LOCATED AND DRILLED NEW SUPPORT ANGLE AT VAPOR BARRIER L/H STA 663 PER REF B737-700 SRM51-40-05-0G-0.;[02] VERIFIED STEP 1. OK TO TREAT AND PRIMER.;[03] TREATED AND PRIMED NEW HOLES ON NEW ANGLE PER REF B737-700 AMM 51-21-41-370-802 AND AMM 51-21-72-370-804.;[04] LOCATED AND DRILLED NEW SUPPORT ANGLE;TREATED AND PRIMED NEW HOLES AT VAPOR BARRIER L/H STA 663 PER REF B737-700 SRM51-40-05-0G-0.;[05] LOCATED AND DRILLED NEW SUPPORT ANGLE;TREATED AND PRIMED NEW HOLES AT VAPOR BARRIER L/H STA 663; INSTALLATION OF THIS SUPPORT ANGLE IS ACCOMPLISHED ON CARD (TTG8Q00CGDYE) PER REF B737-700 SRM51-40-05-0G-0.;[06] VERIFIED STEPS 3;4 AND 5.
Part: VAPOR BARRIER — CRACKED (CENTER WING) · airframe 70,806 hrs · 41,985 cycles
L/H STA 663 VAPOR BARRIER CRACKED AT LBL 10 LOWER CORNER. STOP DRILL CRACK AS PER B737 SRM 51-70-04-2R-10; ACCOMPLISH DRY OUT ON DAMAGE AREA OF L/H VAPOR BARRIER FOUND NO WATER AS PER B737 SRM 51-70-04-2R-0 SECTION 4-D-9; REPAIRED 9' CRACK ON THE L/H VAPOR BARRIER WITH A PERMANENT REPAIR AS PER B737 SRM 51-70-04-2R-10 AND REPAIRED A 6' INTERIM REPAIR IN THE SAME LOCATION .TOTAL CRACK SIZE 15' AS PER B737 SRM 57-10-10-1A-2 SECTION 2-C-4 AT STA 663 LBL 10' LOWER CORNER.PERFORMED TAP TEST ON REPAIRED AREA; FOUND NO DELAMINATION AS PER B737 NDT 51-05-01 SECTION (5);ON THE INTERIM REPAIR DO A VISUAL INSPECTION OF THE REPAIRED AREA AT 1200 FLIGHT CYCLE INTERVALS OR MORE FREQUENTLY AS PER B737 SRM 57-10-10-1A-2 SECTION 2-C-(4);
Earlier reports · 2001–2021 · 284 reports
2021
Part: LENS — BROKEN (CABIN)
CUSTOMER WALK: FORWARD CABIN EMERGENCY EXIT LENS FALLING WONT STAY UP CLIP LOCK BROKEN. ; / [01] SECURED FORWARD CABIN EMERGENCY EXIT LENS AS PER B737 AMM 33-51-01-960-801; [02] STEP 1 VERIFIED
Part: SCUFF PLATE — CRACKED (FUSELAGE)
AFT CARGO CENTER SCUFF PLATE CRACKED ; AFT CARGO CENTER SCFF PLATE CRACKED / [01] RECEIVED NEW SCUFF PLATE PART #146A8342-8 TO BE INSTALLED ON WORK ORDER #TTG8Q0032BDK; [02] VERIFIED STEP # 1.
Part: SLIDE — OUT OF POSITION (R2 DOOR)
R2 DOOR SIDE SCURT TOUCHING SCUFF PLATE WHEN CLOSED ; / [01] REPOSITIONED R2 DOOR SLIDE SKIRT PER B737 AMM 25-66-01-400-803; [02] VERIFIED STEP 1.
Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 69,284 hrs · 41,071 cycles
R1 DOOR EXTERIOR EMERGENCY LIGHT INOP. ; / [01] RELAMPED R1 DOOR EXTERIOR EMERGENCY LIGHT AS PER REF. B737 AMM 33-51-04-960-801. TEST OK; [02] VERIFIED STEP 1.
Part: NONE — MISSING (CABIN) · airframe 69,284 hrs · 41,071 cycles
EMERGENCY EXIT SIGN LENS MISSING AT G4 GALLEY ; / [01] REPLACED EMERGENCY EXIT SIGN LIGHT ASSEMBLY AND PERFORMED TEST FOR NEW ASSEMBLY AS PER B737 AMM 33-51-01960-802. TEST OK.; [02] VERIFIED STEP 1
Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,284 hrs · 41,071 cycles
EMERGENCY OVERHEAD BIN LIGHTS INOP AT POSITIONS: 14L/H THRU 23L/H AND 22R/H. ; / [01] WORK TO BE ACCOMPLISHED IN ITEM TTG8Q0096A91; OPS CHECK FOUND NORMAL AS PER B737 AMM 33-51-06-960-805.; [02] VERIFIED
Part: NONE — INOPERATIVE · airframe 69,284 hrs · 41,071 cycles
R2 DOOR UPPER EMERGENCY INDICATOR EXIT SIGN INOP. ; / [01] WORK TO BE ACCOMPLISHED IN ITEM TTG8Q0096A91; OPS CHECK FOUND NORMAL AS PER B737 AMM 33-51-06-960-805.; [02] VERIFOED
Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 69,284 hrs · 41,071 cycles
L2 DOOR EXTERIOR EMERGENCY LIGHT INOP. ; / [01] WORK TO BE ACCOMPLISHED IN ITEM TTG8Q009A91; OPS CHECK FOUND NORMAL AS PER B737 AMM 33-51-06-960-805.; [02] VERIFIED
Part: SIGN — BURNED OUT (CABIN) · airframe 69,284 hrs · 41,071 cycles
R/H OVER-WING EMERGENCY EXIT INDICATOR SIGN HAS 1 BULB BURNED OUT. ; / [01] REPLACED EXIT SIGN; LAMP AT R/H OVER WING INDICATOR; AS PER B737 AMM 33-51-01-960-801; TEST FOUND NORMAL.; [02] VERIFIED NORMAL
Part: SKIN — INOPERATIVE (CABIN) · airframe 69,284 hrs · 41,071 cycles
L2 DOOR LOWER EMERGENCY INDICATOR EXIT SIGN INOP. ; / [01] PERFORMED BATTERY PACK REPLACEMENT AT M1673 L2 DOOR (S/N ON: 36688) ; AND ACCOMPLISHED OPS CHECK AS PER B737 AMM 33-51-06-960-805; TEST FOUND NORMAL.; [02] VERIFIED COMPLETE
Part: DOUBLER — CORRODED (FUSELAGE) · airframe 69,284 hrs · 41,071 cycles
FOUND CORROSION AT FWD CARGO COMP BILGE AREA M2134 'NATS AIRPHONE ANTENNA' DOBBLER BETWEEN STA 500 AND 500A STGR 28L AND STGR 28R .INSTALLED PROTECTION OF EWIS AT FWD CARGO IAW AMM 20-60-07-913-801. REMOVED EXTERIOR COVER DOUBLE PLATE ATTACHED WITH 6 (EA) FASTENERS IAW SRM 51-40-02-0G-0. REMOVED ANTENNA DOBBLER AT FWD CARGO BILGE AREA IAW SRM 51-40-02-0G-0. INSTALLED NEW DOUBLEIAW SRM 51-40-02-0G-0 IPC 53-42-00-24 & DWG 143A3233. INSTALLED COVER REMOVED ON STEP #2 IAW SRM 51-40-02-0G-0. REMOVED PROTECTION OF EWIS INSTALLED ON STEP #1 IAW AMM 20-60-07-913-801. REMOVED AND REPLACED DOUBLE IAW SRM 51-40-02-0G-0 IPC 53-42-00-24 AND DWG 143A3233.
Part: NONE — MISSING (CABIN) · airframe 69,284 hrs · 41,071 cycles
EMERGENCY EXIT DOOR L & R SIDE INDICATOR ASSY -LIGHTED EXIT FOUND MISSING ; / [01] INSTALLED EMERGENCY EXIT DOOR L/H SIDE AND R/H SIDE INDICATOR ASSY LIGHT AS PER BOEING 737-700 AMM 33-51-01-960-801.; [02] VERIFIED INSTALL. TEST ON CARD TTG8Q0033A01
Part: INTERCOSTAL — CRACKED (ENG 2) · airframe 69,284 hrs · 41,071 cycles
ENG 2 O/B FAN COWL INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL AT NR 2 ENGINE O/B FAN COWL IAW SRM 51-40-02-0G-0.
Part: ACCESS PANEL — DELAMINATED (NR 2 NACELLE) · airframe 69,284 hrs · 41,071 cycles
NR 2 PYLON ACCESS PANEL 431ER EDGE DELAMINATED. PREPARED PANEL 431ER FOR REPAIR OF THE FIBER GLASS IAW SRM 51-70-062R-7. REPAIRED AT PANEL 431ER IAW SRM 51-70-06-2R-7. RESTORED FINISH AT #2 PYLON ACCESS PANEL 431ER IAW AMM 51-21-73-370-803.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 69,284 hrs · 41,071 cycles
CORROSION ON AFT CARGO BAY BILGE FRAME SUPPORT UPPER FLANGE BS 787, S26R. REMOVED CORROSION IAW SRM 51-10-02-0G-0. EVALUATED REWORKED AREA ORG MAT 0.088 MAT REMOVED 0.042 MAT REMAINING 0.046 FOUND TO BE OUT OF LIMITS IAW B737-7 SRM 53-00-53-1A-2 REMOVED AT AFT CARGO COMPARMENT THE BILGE FRAME SUPPORT UPPER FLANGE FROM STA 787 TO STA 860 OF R/H SIDE STR 26R IN REF B 737-700 SRM 51-40-02-0G-0 VERIFIED 4COMPLETE LOCATED AND DRILLED NEW BILGE FRAME SUPPORT UPPER FLANGE AT AFT CARGO COMPARMENT FROM STA 787 TO 860 STR 26 R/H SIDE IN REF B 737-700 51-40-05-0G-0. INSTALLED 100% AFT CARGO FRAME SUPPORT FROM STA 787 TO STA 867 AS PER B737-700 SRM 51-40-02-0G-0 AND DWG# 146A8120.
Part: CHANNEL — CORRODED (AFT CARGO BAY) · airframe 69,284 hrs · 41,071 cycles
CORROSION ON AFT CARGO COMPARTMENT R/H FLOOR SUPPORT Z CHANNEL NUTPLATES BETWEEN BS 767 & 787. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP. ON REWORKED AREA IAW NDT PART 4 51-00-00 PROC. 3. MIN THICKNESS .028'. EVALUATED REWORKED AREA ORG MAT 0.040 MAT REMAINING 0.028 MAT REMOVED 0.012 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1. FABRICATED A NEW Z-CHANNEL SECTION, LOCATED & DRILLED IAW SRM 51-40-05-0G-0 & DWG 146QA7500. TREATED & PRIMED CHANNEL IAW AMM=51-00-58-201 & AMM 51-21-72-370-802. INSTALLED NUT PLATES IAW SRM 51-40-02-0G-0. CHANNEL INSTALLED ON ITEM TTG8Q004ECQV.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 69,284 hrs · 41,071 cycles
CORROSION FOUND AFT FUSELAGE INTERNAL STINGER 27L, BS 1006 & 1016. REMOVED CORROSION AT AFT FUSELAGE & FOUND OUT OF LIMITS DUE TO ITS ALL THE WAY THROUGH STRINGER BLOWN OUT IAW SRM 51-10-02-0G-0. FABRICATED A NEW STRINGER IAW SRM 53-00-03-2R-1, FIGURE 205. LOCATED & DRILLED REPAIR PARTS FOR STRINGER IAW SRM 53-00-03-2R-1, TREATED & PRIMED ALL REPAIR PARTS IAW AMM-51-00-58-201 & AMM-51-21-72-370-801 PARTIALLY INSTALLED FASTENERS IAW SRM 51-40-02-0G-01. INSTALLED 100% STRINGER REPAIR IAW SRM 51-40-02-0G-0.
Part: HINGE — CORRODED (ZONE 100) · airframe 69,284 hrs · 41,071 cycles
CORROSION AT UPPER FUSELAGE UNDER VERTICAL FIN AREA BETWEEN VERTICAL STAB. FWD HINGE & AFT HINGE. OTBD S1L & 1R. REMOVED CORROSION AT UPPER FUSELAGE UNDER VERTICAL FIN AREA IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP. ON REWORKED AREAS IAW NDT PART 4 51-00-00, PROCEDURE 3. MIN. THICKNESS 0.062'. EVALUATED REWORKED AREA ORG MAT 0.068 MAT REMAINING 0.062 MAT REMOVED 0.006 FOUND TO BE WITH IN LIMITS IAW SRM 53-00-01-1A-5. INSTALLED NEW FASTENERS REMOVED FOR ACCESS AT REWORKED AREA IAW SRM 51-40-02-0G-0, TREATED AND PRIMED REWORKED AREA IAW AMM 51-00-58-201 & AMM 51-21-72-370-802.
Part: PANEL — DELAMINATED (FUSELAGE) · airframe 69,284 hrs · 41,071 cycles
PANEL 192BL HAS EDGES DELAMINATED IN TWO SPOTS. REMOVED DAMAGED PLIES & PREPARED THE DAMAGED AREA TO APPLY FABRIC REPAIR PLIES NO WATER NOTE AT ACCESS PANEL 192BL IAW SRM 51-70-04-2R-10 PARAGRAPH 4 B & C. APPLIED FABRIC REPAIR PLIES AT ACCESS PANEL 192BL IAW SRM 51-70-04-2R-10 PARAGRAPH 4 D, E, F & G. PERFORMED VISUAL INSPECTION & TAP TEST INSP AROUND REPAIR AREA, NO DELAMINATION NOTE & NO MATERIAL COMPOSITE DAMAGE IAW NDT PART 1 51-05-01 PARA 5. APPLIED FINISH ON REPAIR AREA AT ACCESS PANEL 192BL IAW SRM 53-40-70-2R-1 & SRM 51-70-04-2R-10 PARAGRAPH 4 H. APPLIED FABRIC REPAIR PLIES AL DAMAGED AREA ON ACCESS PANEL 192BL SRM 53-40-70-2R-1 & SRM 51-70-04-2R-10.
Part: STIFFENER — CRACKED (LH HOR STAB) · airframe 69,284 hrs · 41,071 cycles
LEFT HORIZONTAL STAILIZER INSPAR RIB ASSY #4 STIFFENER #2 LOWER CRACK NOTED. PERFORMED HFEC INSP ON STIFFENER#2 LOWER CHORD IAW B737 NDT P6 51-00-00 PROC.23; 2EA CRACKS NOTED. PERFORMED ROTO INSP ON STIFFENER#2 LOWER 8EA EXISTING HOLES IAW NDT P6 51-00-00 PROC.16; CRACKS NOTED ON 2EA HOLES. REMOVED CRACK HOLES RIB #4 STIFFENER #2 I/B AND O/B LOWER FLESH IAW B737 SRM 55-10-09-2R-REPAIR 5.; [04] VERIFIED STEP 3 (DAMAGE REMOVAL).; [05] PERFORMED HFEC INSP ON CUT OUT IAW B737 NDT P6 51-00-00 PROC.23; NO CRACKS
Part: STIFFENER — CRACKED (LH HOR STAB) · airframe 69,284 hrs · 41,071 cycles
LEFT HORIZONTAL STAILIZER INSPAR RI ASSY #4 STIFFENER #4 LOWER CRACK NOTED / REMOVED DAMAGED AT LT HORIZONTAL STAB #4 RIB #4 STIFFENER LOWER IAW 7 SRM 55-10-09-2R REPAIR 4. NO CRACKS NOTED. INSTALLED REPAIR AT#4 RIB STIFFENERS #4 AT L/H HORIZONTAL STAB IAW B737 SRM55-10-09-R2 REPAIR 4. CORRECTION: VERIFIED STEPS 1 5 AND 8. RII STEPS VERIFIED ALL STEPS VERIFIED.
Part: WEB — CRACKED (CENTER WING) · airframe 69,284 hrs · 41,071 cycles
CRACK FOUND AT EXTERNAL WHEEL WELL WEB LOCATED AT RT SIDE STA 663 BETWEEN RBL 31.83 & RBL 40.00. CRACK LENGTH : 0.512'. / [01] INSTALLED EWIS PROTECTION AT EXTERNAL WHEEL WEB AT R/H SIDE STA 663 BETWEEN RBL 31.83 AND RBL 40.00 IN REFERENCE B-737 AMM20-60-07-913-801;[38] COMPLETED VERTICAL PRESSURE DECK WEB REPAIR AT RT SIDE STA 663 BETWEEN RBL 31.83 & RBL 40.0 AS PER B737-700 SRM 57-10-10-2R-3.; [39] VERIFIED FINAL STATEMENT; [40] REPAIR COMPLETED AT RT SIDE STA 663 BETWEEN RBL 31.83 AND RBL 40.0 AS PER B737-700 SRM 57-10-10-2R-3.
Part: RIB — CRACKED (VERTICAL STAB) · airframe 69,284 hrs · 41,071 cycles
DORSAL FIN FWD RIB CRACKED ; / [01] REMOVED DORSAL FIN FWD RIB AS PER B737-700 SRM 5-40-02-0G-0; [02] LOCATED AND DRILLED NEW RIB ASSEMBLY AS PER B737-700 SRM 51-40-05-0G-0; [03] VERIFIED STEP 2. OK TO INSTALL ON DORSAL FUN.; [04] INSTALLED NEW RIB AT DORSAL FIN AS PER B737-700 SRM 51-40-02-0G-0; [05] REMOVED DORSAL FIN FWD RIB AS PER B737-700 SRM 5-40-02-0G-0. LOCATED AND DRILLED NEW RIB ASSEMBLY AS PER B737-700 SRM 51-40-05-0G-0. INSTALLED NEW RIB AT DORSAL FIN AS PER B737-700 SRM 51-40-02-0G-0.; [06] VERIFIED STEPS 4 AND 5.
Part: PANEL — DELAMINATED (ENG 2) · airframe 69,284 hrs · 41,071 cycles
NO-2 PYLON ACCESS PANEL 441EL EDGE AREA DELAMINATED MKD DOT ; / [01] PREPARED FOR REPAIR AT PANEL 441 EL AS PER B737-700 SRM. 51-70-06-2R-7; [02] VERIFIED STEP 1; OK TO INSTALL REPAIR PLIES; [03] REPAIRED AT PANEL 441 EL AS PER B737-700 SRM 51-70-06-2R-7 MATERIAL USED PO. 1731939 AND PO. 1694548; [04] VERIFIED STEP 3; [05] RESTORED FINISH AT ACCESS PANEL 441EL IAW B 737-7 AMM51-21-73-370-803.; [06] SUMMARY=PREPARED FOR REPAIR AT PANEL 441 EL AS PER B737-700 SRM. 51-70-06-2R-7 REPAIRED AT PANEL 441 EL AS PER B737-700 SRM 51-70-06-2R-7 MATERIAL USED PO. 1731939 AND PO. 1694548 RESTORED FINISH AT ACCESS PANEL 441EL IAW B 737-7 AMM51-21-73-370-803.; [07] VERIFIED STEPS #5 AND #6. N/R FINALIZED.
Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,284 hrs · 41,071 cycles
FWD CARGO R/H STA 500D S-19R GUSSET BRACKET CRACK. ; / [01] REMOVED GUSSET AT FWD CARGO R/H SAT 500D S-19 B737-700 ARM 51-40 -02 0G-0; [02] LOCATED HOLE NEW GUSSET PER B737-700 IN REF SRM 51-40)05; [03] VERIFIED NEW GUSSET DRILL; OK TO INSTALL; [04] INSTALLED GUSSE BRACKET AT FWD CARGO R/H STA 500D PER B 737-700 IN REF.SRM 51-40-02; [05] VERIFIED INSTALL; [06] CORRECTION SRM 51-40-02-0G-0
Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,284 hrs · 41,071 cycles
FWD CARGO L/H STA 500D S-19L GUSSET BRACKET CRACK. ; / [01] REMOVED GUSSET AT FWD CARGO DOOR L/H STA 500D S19L B737-700 ARM 51-40-02-0G-0; [02] LOCATED. HOLE AND NEW GUSSET B737-700 SRM 51-40-05-0G-0; [03] VERIFIED DRILL OF NEW; OK TO INSTALL; [04] INSTALLED GUSSET BRACKET AT FWD CARGO L/H STA. 500 D PER.B 737-700 IN REF. SRM 51-40 -02; [05] VERIFIED INSTALL <BR>CORRECTION SRM 51-40-02-0G-0
Part: SKIN — CORRODED (FUSELAGE) · airframe 69,284 hrs · 41,071 cycles
LIGHT CORROSION AT AFT PRESSURE DOME FWD SIDE BS 1016, CIRCUMFERENTIAL SKIN SPLICE BETWEEN STRINGERS 26L TO 26R. REMOVED SKIN ATTACH RIVETS AT AFT PRESSURE DOME IAW SRM 53-80-08-1A-1 CORROSION FOUND OUT OF LIMITS IAW SRM 53-80-08-1A-1. REMOVED SPLICE ANGLE IAW SRM 51-40-02-0G-0. FABRICATED SPLICE ANGLE & HEAT TREATMENT IAW DWG 148A2216, & SRM 51-40-05-G-0. TREATED AND PRIMED NEW SPLICE ANGLE IAW AMM 51-21-52-370-804 & SRM 51-20-01-0G-0. INSTALLED RIVETS IAW DWG 147A0070. REINSTALLED BOLTS IAW SRM 51-40-04-0G-0 TABLE B FIG (1). INSTALLED STRINGER TIE IAW SRM 51-40-02-0G-0. SEALED FASTENERS IAW SOPM 20-50-19.
Part: STIFFENER — CRACKED (L/H HORIZ. STAB.) · airframe 69,284 hrs · 41,071 cycles
LEFT HORIZONTAL STAB INSPAR RIB NR 4, STIFFENER 3 LOWER AREA CRACKED. REMOVED DAMAGED IAW SRM 55-10-09-2R, REPAIR 4. PERFORMED HFEC INSP ON STIFFENER IAW NDT P6 51-00-00 PROC.23, CRACK NOTED. PERFORMED ROTO INSP ON STIFFENER IAW NDT P6 51-00-00 PROC.16 NO CRACKS NOTED. REMOVED CRACK IAW SRM 55-10-09-2R, REPAIR 4. PREFOMED ROUGHNESS OF 63MICRO INCHES RA AND INITIAL PART 125 MICRO INCHES IAW SRM 55-10-09-R2 R 5. LOCATED AND DRILLED A REPAIR SRM 51-40--05 0G-0. TREATED AND PRIMED AREA IAW AMM 51-21-41-370-802 AND AMM51-21-72-370-802. INSTALLED NEW REPAIR RIB $ STIFFENER #3 SRM 51-40-02-0G-0.
Part: STIFFENER — CRACKED (R/H HORIZ. STAB.) · airframe 69,284 hrs · 41,071 cycles
RIGHT HORIZONTAL STABILIZER INSPAR RIB ASSY. #4 (STAB STA 120.30); STIFFENER #3 LOWER AREA CRACK NOTED. REMOVED CRACK IAW SRM 55-10-09-2R REPAIR 4. PERFORMED HFEC INSP ON REWORKED AREA WEB IAW B737 NDT P6 51-00-00 PROC.23 CRACK NOTED. PERFORMED ROTO INSP ON REWORKED AREA 4EA EXISTING HOLES AT LOWER CHORD IAW NDT P6 51-00-00 PROC.16, CRACK NOTED ON 1EA HOLE. FABRICATED NEW ANGLE AT #4 RIB STIFFENERS #3 IAW SRM 55-10-09-2R REPAIR 5. LOCATED AND DRILLED REPAIR IAW SRM 51-40-05-0G-0. FABRICATED FILLER IAW SRM 55-10-09-2R-REPAIR 5.TREATED AND PRIMED NEW REPAIR ANGLE IAW AMM 51-21-41-370-801 & AMM 51-21-72-370-804. INSTALLED REPAIR IAW SRM 51-40-02-0G-0 AND SRM 55-10-09-2R-5 REPAIR 5.
Part: STIFFENER — CRACKED (R/H HORIZ. STAB.) · airframe 69,284 hrs · 41,071 cycles
RIGHT HORIZONTAL STAB INSPAR RIB 4, HSS 120.30. STIFFENER 4 LOWER AREA CRACKED. REMOVED CRACK IAW SRM 55-10-09-2R REPAIR 4. HFEC INSP IAW NDT P6 51-00-00 PROC.23 CRACK NOTED. ROTO INSP IAW NDT P6 51-00-00 PROC.16 CRACK NOTED. REMOVED CRACK ON WEB & HOLE IAW SRM 55-10 09-2R, REPAIR 5. SURFACE ROUGHNESS OF 63 MICROINCHES RA ON CUT EDGES & ROUGHNESS OF 125 MICROINCHES RA ON PART IAW SRM 55-10-09-2R REPAIR 5. FABRICATED NEW ANGLE.IAW SRM 55-10-09-2R REPAIR 5. LOCATED & DRILLED NEW REPAIR IAW SRM 51-40-05-0G-0. FABRICATED FILLER IAW SRM 55-10-09-2R REPAIR 5. TREATED & PRIMED NEW REPAIR ANGLE IAW AMM 51-21-41-370-801 & AMM 51-21-72-370-804. INSTALLED REPAIR IAW SRM 51-40-02-0G-0 & SRM 55-10-09-2R-5 REPAIR 5.
Part: STIFFENER — CRACKED (RH HOR STAB) · airframe 69,284 hrs · 41,071 cycles
RIGHT HORIZONTAL STAB INSPAR RIB ASSY NR 4 HSS 120.30. STIFFENER #2 LOWER AREA CRACK NOTED. REMOVED CRACK ON STIFFENER 2 RIB 4 RT HORIZONTAL STAB IAW SRM 55-10-09 -2R REPAIR4. VERIFIED STEP 1 PERFORMED ROTO INSP ON REWORKED AREA 4EA EXISTING HOLES AT LOWER CHORD IAW NDT P6 51-00-00 PROC.16 CRACK NOTED ON 1EA HOLE. PERFORMED HFEC INSP ON REWORKED AREA WEB IAW NDT P6 51-00-00 PROC.23 CRACK NOTED. REMOVED CRACK ON WED AND HOLE AT 4 RIB STIFFENER 2 IAW SRM 55-10 09-2R REPAIR 5.
Part: CHANNEL — CORRODED · airframe 69,284 hrs · 41,071 cycles
AFT CARGO BILGE AREA; R/H SIDE 'Z' CHANNEL FROM BS 727 TO 767. REMOVED CORROSION BILGE AREA R/H Z CHANEL IAW SRM 51-10-02-0G-0. PERFORMED UT THIKNESS INSP. ON REWORKED AREA IAW NDT PART 4 51-00-00 PROC. 3. MIN THICKNESS .030'. ORIGINAL THICKNESS 0.040'' AFTER REWORKED AREA MINIMUM MAT FOUND 0.030; MAT LOST 0.10'' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103 DETAILS A, B, C, D AND E. FABRICATED NEW Z CHANNEL. TREATED AND PRIMED NEW Z CHANNEL AMM 51-00-58-201 & AMM 51-21-72-370-802. INSTALLED NEW NUT PLATES ON NEW Z- CHANNEL IAW SRM 51-40-02-0G-0. INSTALLED ON ITEM #TTG8Q002YTJ0 AFT CARGO MOD.
Part: WEB — CRACKED (AFT CABIN) · airframe 69,284 hrs · 41,071 cycles
AFT WET AREA FLOOR WEB AT BS 1016+8', RBL 30 CRACKED. REMOVED AFT WET AREA FLOOR WEB IAW SRM 51-40-02-G-0. LOCATED AND DRILLED A NEW WEB IAW SRM 51-40-05-0G-0. FABRICATED A NEW WEB IAW SRM 53-70-51-01-1, WEBS & STRAPS DWG 147A5744. TREATED AND PRIMED THE NEW WEB IAW AMM 51-21-72-370-801 & AMM 51-00-58-201. INSTALLED FASTENERS ON AFT WET AREA IAW SRM 51-40-02-0G-0 AND DWG #147A5730 PARTIALLY ISTALLED FASTENERS AT AFT WET AREA RT FLOOR WEB IAW SRM 51-40-02-0G-0 AND DWG #147A5730.
Part: CHANNEL — CORRODED (AFT CARGO BAY) · airframe 69,284 hrs · 41,071 cycles
CORROSION ON AFT CARGO BILGE AREA, LT SIDE ZEE CHANNEL, BS 727D+9 - 847. REMOVED CORROSION IAW SRM 51-51-10-02-0G-0. PERFORMED UT THIKNESS INSP. ON REWORKED AREA IAW NDT PART 4 51-00-00 PROC. 4. MIN THICKNESS .035'. ORIGINAL THICKNESS 0.040'' AFTER REWORKED AREA MINIMUM MAT FOUND 0.035 MAT LOST 0.005'', FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103, DETAILS A, B, C, D, & E NEW Z-CHANNEL TO BE INSTALLED ON WORK CARD TTG8Q004ECQV.
Part: PANEL — DELAMINATED (FUSELAGE) · airframe 69,284 hrs · 41,071 cycles
ACCESS PANEL 193D AFT EDGE DELAMINATED. / [01] PREPARED FOR REPAIR PLIES THE AREA AT PANEL 193D AS PER B737-700 SRM51-70-04-2R-9; [02] OK TO INSTALL REPAIR.; [03] REPAIRED AT PANEL 193 D AS PER B737-700 SRM 51-70-04-2R-9 . MATERIAL USED PO.1731939 AND PO. 1694548; [04] VERIFIED STEP 3.; [05] RESTORED FINISH AT ACCESS PANEL 193D IAW B 737-7 AMM51-21-73-370-803.; [06] RESTORED FINISH AT ACCESS PANEL 193D IAW B 737-7 AMM51-21-73-370-803.; [07] SUMMARY=PREPARED FOR REPAIR PLIES THE AREA AT PANEL 193D AS PER B737-700 SRM51-70-04-2R-9 REPAIRED AT PANEL 193 D AS PER B737-700 SRM 51-70-04-2R-9 . MATERIAL USED PO.1731939 AND PO. 1694548 RESTORED FINISH AT ACCESS PANEL 193D IAW B 737-7 AMM51-21-73-370-803..
Part: STIFFENER — CRACKED (L/H HORIZ. STAB.) · airframe 69,284 hrs · 41,071 cycles
LEFT HORIZONTAL STABILIZER INSPAR RIB 5, STIFFENER 3 LOWER AREA, CRACK NOTED. REMOVED PAINT FOR ACCESS FASTENER UPPER AND LOWER SKIN IAW AMM 51-21-11-150-801. REMOVED STAB NR 5 RIB IAW SRM 51-40-02-0G-0. REMOVED CRACK FROM NR 5 RIB STIFFENER 3 IAW SRM 55-10-09-2R REPAIR 4. .PERFORMED HFEC INSP ON RIB NR 5 STIFFENER 3 CUT OUT IAW NDT P6 51-00-00 PRC 23. LOCATED AND DRILLED NEW REPAIR RIB STIFFENER IAW SRM 51=40-05=0G-0. TREATED AND PRIMED AREA IAW AMM51-21-41-370-802 AND AMM51-21-72-370-802. INSTALLED REPAIR IAW SRM 51-40-002-0G-0. VERIFIED ITEM 14. PAINT RESTORE FOR STEP ONE AND L/H HORIZONTAL STAB #5 RIB INSTALLATION ACCOMPLISH ON FAULT TTG8Q006RDS2 VERIFIED STEP 19. VERIFIED STEP 17.
Part: SPLICE — CORRODED (AFT CARGO BAY) · airframe 69,284 hrs · 41,071 cycles
AFT CARGO BILGE AREA; FLOOR-PANEL SPLICE AT STA#727D+5; SPOTS OF CORROSION. DOT#208-16<REMOVED CORROSION AT AFT CARGO BILGE AREA FLOOR PANEL SPLICE AT STA 727.5 CORROSION IS ALL THE WAY THROUGH THE TEE IS OUT OF LIMITS IAW B737-7 SRM 51-10-02-0G-0 CORROSION OUT OF LIMITS RECEIVED NEW TEE IT WILL BE INSTALLED ON WORK CARD TTG8Q004ECQV
Part: STIFFENER — CRACKED (LH HOR STAB) · airframe 69,284 hrs · 41,071 cycles
REMOVE LEFT HAND HORIZONTAL STABILIZER IN SPAR RIB ASSY #5 FOR ACCESS TO STIFFENER #3 REPAIR. ; REMOVE LEFT HAND HORIZONTAL STAILIZER IN SPAR RI ASSY #5 FOR ACCESS TO STIFFENER #3 REPAIR. / [01] REMOVED L/H HORIZONTAL STAB IN SPAR RIB #5 STIFFENERS #3 IAW B737 SRM 51-40-020G-0.; [02] LATE ENTRY REMOVED PAINT FOR ACCESS TO FASTENER AT UPPER AND LOWER SKIN TO GAIN ACCESS TO REMOVE L/H HORIZONTAL STAB RIB #5 IAW AMM51-21-11-150-801.; [03] VERIFIED STEP 1 AND 2.; [04] OK TO INSTALL #5 RIB.; [05] PARTIALLY INSTALLED L/H # 5 RIB INSTALLED 70% OF FASTENERS IAW SRM 51-40-02-0G-0.
Part: STRUCTURE — CORRODED (AFT CARGO BAY) · airframe 69,284 hrs · 41,071 cycles
CORROSION ON AFT CARGO BILGE AREA; FLOOR STRUCTURE BETWEEN BS 727- 727A, LBL 4 - RBL 8. AROUND FASTENER HOLES. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP IAW NDT P4 51-00-00 PROC.3; MIN THK. NOTED 0.051'. EVALUATED REWORKED AREA ORG MAT 0.063 MAT REMAINING 0.051 MAT REMOVED 0.013 FOUND TO BE OUT OF LIMITS IAW SRM-53-00-53-1A-2. CUTOUT DAMAGE IAW SRM 53-00-53-2R-2, REPAIR 2 STEPS 4 & 5. LOCATED AND DRILLED NEW REPAIR IAW SRM 51-40-05. TREATED AND PRIMED IAW AMM 51-00-58-201 AND AMM 51-21 -72 -370-802. INSTALLED NEW PARTS IAW SRM 51-40-02-0G -0.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 69,284 hrs · 41,071 cycles
CABIN FLOOR INTERCOSTAL AT ABOUT BL-0 BETWEEN STA 380-400 UPPER SURFACE CRACKED ; / [01] REMOVED UPPER ANGLE AT CABIN FLOOR INTERCOSTAL ABOUT BL-0 BETWEEN STATION 380 & 400 AS PER SRM 51-40-02-G-0.; [02] LOCATED AND DRILLED NEW ANGLE AS PER SRM 51-40-05-0G-0.; [03] OK TO INSTALL NEW ANGLE; [04] INSTALLED NEW ANGLE AT CABIN FLOOR INTERCOSTAL ABOUT BL-0 BETWEEN STATION 380 & 400 AS PER SRM 51-40-02-0G-0 & DWG 143A5400.; [05] VERIFIED STEP 4; [06] C/W
Part: PANEL — DEFORMED (CABIN) · airframe 69,284 hrs · 41,071 cycles
PANEL 211AF OUT OF SHAPE. LOCATED AND DRILLED NEW PART REF B-737-700 SRM 41-40-05-0G-0; [02] VERIFIED NEW PART.INSTALLATION ON CARD TTG8Q002YL6X
Part: CHANNEL — CORRODED (AFT CARGO BAY) · airframe 69,284 hrs · 41,071 cycles
AFT CARGO BILGE AREA; R/H SIDE 'Z' CHANNEL FROM STA#867 TO STA#887; SPOTS OF CORROSION AROUND FASTENER HOLES. REMOVED CORROSION AFT CARGO BILGE AREA R/HZ CHANNEL. FOUND OUT LIMITS EXFOLIATION CORROSION AREA IAW SRM 51-10-02-0G-0 VERIFIED 1 PERFORMED UT THIKNESS INSP. ON REWORKED AREA @ AFT CARGO BILGE AREA R/H SIDE Z-CHANNEL IAW NDT PART 4 51-00-00 PROC. 3. MIN THICKNESS .026'. ORIGINAL THICKNESS 0.040'' AFTER REWORKED AREA MINIMUM MAT FOUND 0.026 MAT LOST 0.14'. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 FIG 103 DETAILS A, B, C, D, & E. NEW Z-CHANNEL TO BE INSTALLED ON ITEM# TTQ004ECQV.
Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 69,284 hrs · 41,071 cycles
AFT CARGO BILGE AREA; FLOOR-PANEL SPLICE AT STA#772 CORROSION. REMOVED CORROSION AFT CARGO BILGE AREA FLOOR PANEL SPLICE AT STA772IAW B737 SRM51-10-02-0G-0. VERIFIED 1 PERFORMED UT THICKNESS INSP. ON REWORKED AREA @ AFT CARGO BILGE AREA FLOOR-PANEL SPLICE @ STA 772 IAW B737 NDT PART 4 51-00-00 PROC. 3. MIN THICKNESS .028'. EVALUATED REWORKED AREA ORG MAT 0.070 MAT REMAINING 0.028 MAT LOST 0.042 FOUND TO BE OUT OF LIMITS IAW B 737-7 SRM 53-00-53-1A-2 RECEIVED NEW TEE ANGLE PART #146A9401-4 TO BE INSTALLED ON WORK CARD #TTG8Q004ECQV.
Part: BLOCKER DOOR — EXPOSED (ENG 2) · airframe 69,284 hrs · 41,071 cycles
ENGINE #2 TR BLOCKER DOORS 6; 7; 8 ;9 COMPOSITE MATERIAL EXPOSED CLOSE TO SUPPORT FITTING. PERFORMED VISUAL INSPECTION AND TAP TEST NO DELAMINATION FOUND IAW PART 1 51-05-01 ONLY FOUND POTTING MISSING. PREPARED AREAS TO APPLY POTTING AT ENG #2 T\R ON BLOCK DOORS 6, 7, 8 & 9 IAW SRM 54-30-01-2R-4 PARAGRAPH 4.B. APPLIED POTTING AND SEALED AT ENG #2 T\R ON BLOCK DOORS IAW SRM 54-30-01-2R-4.
Part: PANEL — DELAMINATED (CABIN) · airframe 69,284 hrs · 41,071 cycles
PANEL 241XF DELAMINATED ; / [01] REMOVED DAMAGED AREA AND PREPARED AREA FOR REPAIR AT PANEL 241XF AS PER B737 SRM 53-00-50-2R-1; [02] REPAIRED DAMAGED AREA AT PANEL 241XF AS PER B737 SRM 53-00-50-2R-1; [03] REPAIRED DELAMINATED AREA AT PANEL 241XF AS PER B737 SRM 53-00-50-2R-1; [04] (RII) VERIFIED STEPS #1 AND #3.; [05] (RII) FINAL INSPECTION; DELAMINATED AREA REPAIRED.
Part: PANEL — DELAMINATED (FUSELAGE) · airframe 69,284 hrs · 41,071 cycles
PANEL 221BF DELAMINATED ; / [01] REMOVED DAMAGED AREA AND PREPARED AREA FOR REPAIR AT PANEL 221BF AS PER B737 SRM 53-00-50-2R-1; [02] REPAIRED DAMAGED AREA AT PANEL 221BF AS PER B737 SRM 53-00-50-2R-1; [03] REPAIRED DELAMINATED AREA AT PANEL 221BF AS PER B737 SRM 53-00-50-2R-1; [04] (RII) VERIFIED STEPS #1 AND #3.; [05] FINAL INSPECTION; DELAMINATION REPAIRED.
Part: ANGLE — BROKEN (ENG 1) · airframe 69,284 hrs · 41,071 cycles
NO. 1 ENGINE PRIMARY NOZZLE ASSEMBLY; UPPER L/H AFT NOZZLE FENCE ANGLE BROKEN OFF ; / [01] REMOVED # 1 ENGINE PRIMARY NOZZLE ASSEMBLY; UPPER L/H AFT FENCE ANGLE PER REFERENCE B-737 SRM 51-40-02-0G-0; [02] INSTALLED #1 ENGINE PRIMARY NOZZLE ASSEMBLY UPPER L/H AFT FENCE ANGLE IN REFERENCE B737 SRM 51-40-01-0G-0; [03] CORRECTION STEP 2 SRM 51-40-02-0G-0; [04] REMOVED AND REPLACED # 1 ENGINE PRIMARY NOZZLE ASSEMBLY; UPPER L/H AFT NOZZLE FENCE ANGLE IN REFERENCE B-737 SRM 51-40-20 0G-0; [05] VERIFIED STEP 4
Part: NONE — DELAMINATED (FUSELAGE) · airframe 69,284 hrs · 41,071 cycles
LH AIR CONDITIONING BAY EXHAUST DUCT BASE CORNER DELAMINATED ; / [01] PREPARED AREA FOR REPAIR AT PANEL L/H AIR CONDITIONING BAY EXHAUST DUCT BASE CORNER; AS PER B737- SRM 51-70-06-2R-6; [02] VERIFIED STEP 1; OK TO INSTALL REPAIR; [03] REPAIRED AT L/H AIR CONDITIONING BAY EXHAUST DUCT BASE ;AS PER B737 SRM 51-7006-2R-6MATERIAL USED PO. 1731939 AND PO. 1694548; [04] VERIFIED STEP 3
Part: PANEL — ELONGATED (FUSELAGE) · airframe 69,284 hrs · 41,071 cycles
FOUND SEVERAL FASTENER HOLES ELONGATED ON PANEL 194E ; / [01] PREPARED ON DAMAGED AREA ON PANEL 194E FOR REPAIR AS PER B737 SRM 51-70-04-2R-9 PARAGRAPH 4.C.; [02] VERIFIED PREPARATION<BR>OK TO INSTALL REPAIR; [03] REPAIRED DAMAGED AREA ON PANEL #194E AS PER B737 SRM 53-60-70-2R-1 AND SRM 51-70-04-2R-9 PARAGRAPH 4.D;E;F. MATERIALS USED; P/O#1731939 AND P/O#1690463; [04] VERIFIED REPAIR <BR>OK TO PAINT; [05] PAINTED PANEL 194E AS PER B737 AMM 51-21-99-300-802. MATERIALS USED WHITE PAINT P/O#1729487; [06] VERIFIED PAINT AND FINAL REPAIR STATEMENT
Part: PANEL — CRACKED (FUSELAGE) · airframe 69,284 hrs · 41,071 cycles
ACCESS PANEL 193D AFT EDGE SEVERAL FASTENER HOLES CRACKED . ; / [01] CORRECTION FOR REFERENCE SRM 51-70-04-2R-9; [02] REPAIRED AT PANEL 193D AS PER B737- 700 SRM. 51-70-04-2R-9 .MATERIAL USED PO.1731939 AND PO 1694548; [03] VERIFIED ITEM 1 AND 2.; [04] RESTORED FINISH AT ACCESS PANEL 193D IAW B 737-7 AMM51-21-73-370-803.; [05] SUMMARY=REPAIRED AT PANEL 193D AS PER B737- 700 SRM. 51-70-04-2R-9 .MATERIAL USED PO.1731939 AND PO 1694548 RESTORED FINISH AT ACCESS PANEL 193D IAW B 737-7 AMM51-21-73-370-803.; [06] VERIFIED STEPS 4 AND 5. N/R FINALIZED.; [07] CORRECTION.<BR>REFERENCE USED IS B737-700<BR>SRM 53-60-70-2R-1; [08] CORRECTION.<BR>REFERENCE USED IS B737-700<BR>SRM 53-60-70-2R-1
Part: PANEL — CRACKED (FUSELAGE) · airframe 69,284 hrs · 41,071 cycles
PANEL 194E FWD EDGE 2EA FASTENER HOLES CRACKED. ; / [01] PERFORMED NDT INSPECTION ON PANEL #194E AS PER B737 NDTM 51-05-01 AND FOUND NO WATER; OIL; FUEL; OR OTHER UNWANTED MATERIAL.; [02] PREPARED DAMAGED AREA ON PANEL 194E FOR REPAIR AS PER B737 SRM 53-60-70-2R-1 AND SRM 51-70-04-2R-9 PARAGRAPH 4.C; [03] VERIFIED PREPARATION<BR>OK TO INSTALL REPAIR; [04] REPAIRED DAMAGED AREA ON PANEL #194E AS PER B737 SRM 53-60-70-2R-1 AND SRM 51-70-04-2R-9 PARAGRAPH 4.D;E;F. MATERIALS USED; P/O#1731939 AND P/O#1690463; [05] VERIFIED REPAIR<BR>OK TO PAINT; [06] PAINTED PANEL 194E AS PER B737 AMM 51-21-99-300-802. MATERIALS USED WHITE PAINT P/O#1729487; [07] VERIFIED PAINT AND FINAL STATEMENT STEP 4
Part: NONE — OUT OF TOLERANCE (L1 DOOR) · airframe 69,284 hrs · 41,071 cycles
L-1 DOOR SLIDE BOTH GIRT BAR RETAINER CLIPS ARE WEEK OVER DIMENSION LIMIT ; / [01] REMOVED AND REPLACED (2EA ) RETAINER CLIPS AT L-1 DOOR SLIDE GIRT BAR LOCATION AS PER B737-700 SRM 51-40-02-0G-0.; [02] VERIFIED INSTALLATION; [03] REMOVED AND REPLACED RETAINER CLIPS AT L-1 DOOR SLIDE GIRT BAR LOCATION AS PER B737-700 SRM 51-40-02-0G-0.; [04] PENDING SUBTASK; [05] CLEARING FINAL AMT ROW THAT REMAINS OPEN ALL MAINTENANCE PREVIOUSLY COMPLETED
Part: PANEL — CORRODED (FUSELAGE) · airframe 69,284 hrs · 41,071 cycles
PANEL 145AL GROUND WIRE SCREW EDGES (DOOR SIDE) SHOW SURFACE CORROSION. REMOVED PANEL 145AL IAW SRM 51-40-02-0G-0. REMOVED CORROSION AT PANEL 145AL GROUND WIRE SCREW EDGES IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS ON REWORKED AREA IAW NDTM PART 4 51-00-00 PROCEDURE 3 MINIMUM FOUND: 0.024' FOUND OUT OF LIMIT IAW SRM 52-40-01-1A-4 FIGURE 103 DETAIL D. INSTALLED NEW DOOR PANEL (145AL) IAW SRM 51-40-02-0G-0.
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 69,280 hrs · 41,070 cycles
FWD ENTRY EMERGENCY LIGHTS INOP ; / [01] R&R'D FWD ENTRY BATTERY PACK PER AMM 33-51-06. OPS CHECKED GOOD
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 69,280 hrs · 41,070 cycles
FWD ENTRY EMERGENCY LIGHTS INOP ; / [01] R&R'D FWD ENTRY BATTERY PACK PER AMM 33-51-06. OPS CHECKED GOOD
Part: NONE — DELAMINATED (L/H WING) · airframe 69,280 hrs · 41,070 cycles
LT WING O/B AFT FLAP IS DELAMINATES ON THE I/B LOWER CORNER. ; /
2020
Part: SLIDE — LOOSE (R1 DOOR) · airframe 68,658 hrs · 40,673 cycles
R1 DOOR SLIDE PACK WAS SAGGING. REPACKED SLIDE DOOR ASSEMBLY IAW MT.
Part: SLIDE — LOOSE (R1 DOOR) · airframe 68,648 hrs · 40,667 cycles
R1 DOOR EVAC SLIDE WAS SAGGING. REPACKED SLIDE ASSEMBLY IAW AMM AND MT.
2019
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 67,739 hrs · 40,105 cycles
3 EACH CABIN EMERGENCY LIGHT BATTERY PACKS FAIL CAPACITY TEST. R&R BATTERY PACKS AT POSITIONS M01672, M01670, AND M01669 PER AMM.
Part: HANDLE — LOOSE (LT OVERWING EXIT) · airframe 67,739 hrs · 40,105 cycles
L/H OVERWING EMERGENCY EXIT RELEASE HANDLE IS LOOSE. TIGHTENED RELEASE HANDLE PER AMM.
Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,440 hrs · 39,902 cycles
RT MAIN LANDING GEAR, FORWARD TRUNNION FITTING, INBOARD LOWER, OUT LUG FACE CORRODED. REPAIRED LUG FACE PER EA.
Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,440 hrs · 39,902 cycles
RT MAIN LANDING GEAR, FORWARD TRUNNION FITTING, UPPER OUTBOARD, OUTER LUG FACE CORRODED. REPAIRED LUG FACE PER EA.
Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,440 hrs · 39,902 cycles
RT MAIN LANDING GEAR, FORWARD TRUNNION FITTING, INBOARD LOWER, INNER LUG FACE CORRODED. REPAIRED LUG FACE PER SRM.
Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,440 hrs · 39,902 cycles
RT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER OUTBOARD LUG BORE CORRODED. REPAIRED LUG BORE PER EA.
Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,440 hrs · 39,902 cycles
LT MAIN LANDING GEAR, FORWARD TRUNNION FITTING, UPPER OUTBOARD, OUTER LUG FACE CORRODED. REPAIRED LUG FACE PER EA.
Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,440 hrs · 39,902 cycles
RT MAIN LANDING GEAR, FORWARD TRUNNION FITTING, OUTBOARD LOWER, OUTER LUG FACE CORRODED. REPAIRED LUG FACE PER EA.
Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,440 hrs · 39,902 cycles
LT MAIN LANDING GEAR, FORWARD TRUNNION FITTING, LOWER INBOARD OUTER LUG FACE CORRODED. REPAIRED LUG FACE PER EA.
Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,440 hrs · 39,902 cycles
LT MAIN LANDING GEAR FORWARD TRUNNION FITTING, LOWER OUTBOARD, OUTER LUG FACE CORRODED. REPAIRED LUG FACE PER EA.
Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,440 hrs · 39,902 cycles
RT MAIN LANDING GEAR, FORWARD TRUNNION FITTING, OUTBOARD LOWER, INNER LUG FACE CORRODED. REPAIRED LUG FACE PER SRM.
Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,440 hrs · 39,902 cycles
LT MAIN LANDING GEAR, FORWARD TRUNNION FITTING, LOWER OUTBOARD INNER LUG FACE CORRODED. REPAIRED LUG FACE PER SRM.
Part: LUG — CORRODED (LT MLG TRUNNION) · airframe 67,440 hrs · 39,902 cycles
LT MAIN LANDING GEAR, FORWARD TRUNNION FITTING, LOWER INBOARD, INNER FACE LUG CORRODED. REPAIRED LUG FACE PER SRM.
Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,440 hrs · 39,902 cycles
RT MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD LUG BORE FITTING CORRODED. REPAIRED LUG BORE PER EA.
Part: LUG — CORRODED (RT MLG TRUNNION) · airframe 67,440 hrs · 39,902 cycles
RT MAIN LANDING GEAR, FORWARD TRUNNION FITTING, INBOARD UPPER, OUTER LUG FACE CORRODED. REPAIRED LUG FACE PER EA.
Part: BRACKET — BROKEN (RT WING) · airframe 66,405 hrs · 39,209 cycles
RIGHT INBOARD FLAP BRAKET BROKEN / R&R INBOARD FLAP #6 CONTROL ARM BRACKET PER AMM 51-40-02
Part: FUSE — BLOWN (CABIN) · airframe 66,335 hrs · 39,170 cycles
OVER L2 DOOR EXIT SIGN INOP. R&R POWER SUPPLY FUSE PER AMM.
Part: FUSE — BLOWN (CABIN) · airframe 66,335 hrs · 39,170 cycles
AFT GALLEY EMERGENCY EXIT SIGN INOP. R&R POWER SUPPLY FUSE PER AMM.
Part: LIGHT — DIM (CABIN) · airframe 66,335 hrs · 39,170 cycles
LT EMERGENCY AISLE LIGHT VERY DIM AT SEAT 20. R&R LAMP IAW AMM.
Part: BULKHEAD — CANNING (FUSELAGE) · airframe 66,335 hrs · 39,170 cycles
AFT PRESSURE BULKHEAD OIL CANNING AT BS. 1016, BETWEEN BL 0 AND RBL 53. REPAIRED WEB IAW ER AND EA.
Part: MEGAPHONE — FAULTY (CABIN) · airframe 65,712 hrs · 38,767 cycles
AFT MEGAPHONE FAULTY. R&R AFT MEGAPHONE PER AMM.
Part: BATTERY — DISCHARGED (MEGAPHONE) · airframe 65,712 hrs · 38,767 cycles
AFT MEGAPHONE FAULTY. INSTALLED BATTERY PER MM.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 65,636 hrs · 38,710 cycles
RT EMERGENCY EGRESS LIGHT FUSE BEHIND FLAP INOP. RELAMPED LIGHT IAW AMM.
Part: VANE — CRACKED (RT ENGINE) · airframe 635,327 hrs · 38,516 cycles
DURING BOROSCOPE INSPECTION FOUND APPROXIMATELY 3 CRACKED ON STAGE 1 LOWER PRESSURE TURBINE NGV 1 SEG W/4 VANES CRACKED 3 SEG. R&R NR 2 ENGINE PER MT.
2018
Part: FAIRING — DELAMINATED (LWR FUSELAGE) · airframe 65,131 hrs · 38,403 cycles
PANEL 191FL HAS DELAM PEICE FLAPPING NEAR KRUEGER FLAP / R&R PANEL 191 FL PER AMM 53-51-21 CL #24156
Part: WINDOW — SHORTED (COCKPIT) · airframe 64,201 hrs · 37,820 cycles
DESCENDING THROUGH 10,000, R1 WINDOW HEAT SHORTED OUT. R&R R1 WINDOW IAW AMM.
Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 63,505 hrs · 37,387 cycles
FWD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED / REPAIRED FWD CARGO BAY FWD CORNER SCUFF PLATE IAW EA 1-A53-2076 REV 11
Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 63,505 hrs · 37,387 cycles
AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED / REMOVED AND REPAIRED AFT CARGO BAY AFT CORNER SCUFF PLATE IAW EA 1-A53-2076 REV 11
Part: INTERCOSTAL — CRACKED (AFT CARGO BAY) · airframe 63,505 hrs · 37,387 cycles
WATER TANK INTERCOSTAL ATTACK BRACKET CRACKED BS 947 LBL9 / REMOVED DISCREPANCY ATTACH BRACKET PER SRM 51-40-02-0G-0 89263C 07JUN18 AND REPLACED. WATER TANK INTERCOSTAL ATTACH BRACKET AT BS 947 LBL 9 IAW SRM 51-40-02-0G-0 AND DWG 149A8103
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
FLOOR TO BULKHEAD ATTACH SUPPORT ANGLE CRACKED AT BS 867, LBL 10. R&R ANGLE IAW DWG AND SRM.
Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT SHIELD CORRODED BETWEEN BS 767 TO BS 787, RBL 20. R&R VERTICAL WEB IAW SRM AND DWG.
Part: SKIN — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
FUSELAGE SKIN CORRODED AT BS 887, BETWEEN STR 23L TO STR 23R. REPAIRED SKIN PER EA AND ER.
Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 63,505 hrs · 37,387 cycles
PANEL 193B HAS A DELAMINATED AREA ON THE EXTERNAL SURFACE / REPAIRED PANEL 193B DELAMINATION ON EXTERNAL SURFACE IAW SRM 51-70-05-2R-2 PARA. 4. AND SRM 51-70-05-2R-0 55974U 12JUN18
Part: TIE DOWN — CORRODED (CARGO BAY) · airframe 63,505 hrs · 37,387 cycles
AFT CARGO TRACK TIE DOWN CORRODED AT BS 727A, LBL 16. R&R TIE DOWN IAW SRM AND DWG.
Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
HORIZONTAL PRESSURE DECK WEB CRACKED AT BS 665, RBL 39. REPAIRED WEB IAW EA.
Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
AFT CARGO RT FLOOR TO SIDEWALL SUPPORT SHIELD CORRODED BETWEEN BS 767 TO BS 787. R&R SHIELD IAW SRM AND DWG.
Part: ANGLE — CORRODED (LOWER INT FUSELA) · airframe 63,505 hrs · 37,387 cycles
***CORROSION*** AFT CARGO; POTABLE WATER SERVICE PAN; AFT SUPPORT ANGLE; BS 918; RBL 10 / AFT SUPPORT ANGLE FROM ACB POTABLE WATER SERVICE PAN AT BS 918 RBL10 FOUND TO BE OUT OF LIMITS DUE NO ALLOWABLE DAMAGE IN SRM. REMOVED AND REPLACED AFT SUPPORT ANGLE AT ACB POTABLE WATER SERVICE PAN BS 918 RBL 10 IAW SRM 51-40-02-0G-0 AND DWG 147A7221
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
FORWARD CARGO BAY ON AFT BULKHEAD CENTER PANEL LOWER SUPPORT CORRODED AT BS 500D, BETWEEN LBL 24 TO RBL 24. R&R SUPPORT IAW DWG AND SRM.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
AFT CARGO FLOOR TO AFT WALL SUPPORT ANGLE CORRODED AT BS 947, BETWEEN LBL 9 TO RBL 17. R&R ANGLE PER SRM AND DWG.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 494 TO BS 500A, RBL 24. R&R SUPPORT IAW SRM AND DWG.
Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
AFT CARGO DOORWAY LOWER THRESHOLD WEB CORRODED BETWEEN BS 795 TO BS 847, RBL 23. R&R WEB IAW SRM.
Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
HORIZONTAL PRESSURE DECK WEB CRACKED AT BS. 669, RBL 43. REPAIRED WEB IAW EA.
Part: FRAME — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
AFT CARGO FRAME UPPER FLANGE CORRODED AT BS 947, LBL 9. REPAIRED FLANGE IAW ER AND EA.
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
AFT CARGO LT SIDEWALL SUPPORT ANGLE CORRODED AT BS 727D, BETWEEN STR 23L TO STR 25L. R&R ANGLE IAW SRM AND DWG.
Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
AFT CARGO LT FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 727 TO BS 847. R&R SUPPORT PLATE IAW DWG AND SRM.
Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,505 hrs · 37,387 cycles
AFT CARGO RT FLOOR TRACK CORRODED BETWEEN BS 727 TO BS 778, RBL 14. R&R TRACK IAW SRM AND DWG.
Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
HORIZONTAL PRESSURE DECK WEB CRACKED AT BS 665, RBL 41. REPAIRED WEB IAW EA.
Part: SUPPORT — CRACKED (CABIN) · airframe 63,505 hrs · 37,387 cycles
FLOORBOARD SUPPORT IS CRACKED AT BS 540; RBL1; WL207 / REMOVED AND REPLACED FLOOR BOARD SUPPORT AT BS 540; RBL 1; WL207 PER REF B737 SRM 51-40-02 AND IPC 53-31-00-05 92462U 08JUNE18
Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 63,505 hrs · 37,387 cycles
***CORROSION*** AFT CARGO LH SIDEWALL SUPPORT ANGLE; BS 787; STR 24L TO STR 25L / NO DAMAGE LIMITS IN SRM FOR AFT CARGO LH SIDEWALL SUPPORT ANGLE B.S. 787; STR24L TO STR 25L PART WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR 9C; REMOVED DAMAGED SIDEWALL SUPPORT ANGLE; FABRICATED NEW SUPPORT ANGLE AND INSTALLED SUPPORT ANGLE IAW BOEING DRAWING 146A9403; BOEING DRAWING 146A 1262 AND SRM 51-40-02
Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
AFT CARGO RT FLOOR TO SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 727 TO BS 767, RBL 21. R&R SUPPORT PER SRM & AMM.
Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 63,505 hrs · 37,387 cycles
***CORROSION*** IN FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT B.S. 400-500D; L.B.L. 24. / UPON FURTHER INVESTIGATION FOUND FLOOR TO SIDEWALL SUPPORT IN FCB AT BS 400-500D; LBL 24 OUT OF LIMITS IAW 53-0053-1A-2 REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BS400-500D; LBL 24 AND SPLICE PLATE BS490 LOT # 1337671-4 IAW SRM. 53-30-53-01-2; SRM 53-00-53-1A-2; SRM 53-00-53-2R-5; BOE DWG #143A7500; SRM 51-40-05-0G-0.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
FLOORBEAM CRACKED AT BS 328, RBL 25. REPAIRED FLOORBEAM IAW SRM.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D, RBL 24. R&R SUPPORT IAW SRM & DWG.
Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 63,505 hrs · 37,387 cycles
PANEL 193D HAS A DELAMINATED DENT ON THE EXTERIOR SKIN AT 6.75' FROM THE O/B EDGE 14' FROM THE FWD EDGE / PANEL 1930 DELAMINATED DENT ON THE EXTERIOR SKIN AT 6.75' FROM THE O/B EDGE 14' FROM THE FWD EDGE REPAIRED IAW SRM 51-70-05-2R-2 20549U 06/08/18
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
R1 DOOR STUB FRAME CRACKED AT BS 294.5, WL 209. REPAIRED STUB FRAME PER ER AND EA.
Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
FORWARD SERVICE DOOR MOPSILL ATTACH ANGLE FOR THRESHOLD SUPPORT CORRODED. R&R ANGLE IAW SRM & DWG.
Part: INTERCOSTAL — CRACKED (CABIN) · airframe 63,505 hrs · 37,387 cycles
CRACKED INTERCOSTAL AT B.S. 277-294;.B.L. 0. / REMOVED AND REPLACED CRACKED INTERCOSTAL AT B.S 277-294; B.L.0. WITH ITEM # 141A5410 U3AAR IAW BOE DWG # 141A5400 AND SRM 51-40-02-0G-0
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
FORWARD ENTRY DOOR MOP SILL CORRODED BETWEEN BS 294 TO BS 360. R&R MOP SILL IAW SRM AND DWG.
Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
SHEAR WEB CORRODED AT BS 1016, BETWEEN BL 0 TO LBL 45. R&R SHEAR WEB IAW SRM AND DWG.
Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
FORWARD SERVICE DOOR THRESHOLD CRACKED. REPAIRED THRESHOLD IAW EA.
Part: FAIRING — BROKEN (LOWER EXT FUSELA) · airframe 63,505 hrs · 37,387 cycles
FAIRING 191FL FWD UPPER CUT-OUT CORNER IS BROKEN OFF . (MARKED) / REPAIRED FAIRING 191FL PNL FWD UPPER CUT-OUT CORNER PER SRM 51-70-05-2R-6 & LOCATED; DRILLED & COUNTERSUNK FASTENER HOLE PER DWG # 149A7103 & 51-40-05-0G-0
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,505 hrs · 37,387 cycles
FWD CABIN FLOOR BOARD 222CF HAS DAMAGED UPPER SKIN ON AFT EDGE / REPAIRED DAMAGED UPPER SKIN ON AFT EDGE OF FWD CABIN FLOOR BOARD 222CF IAW SRM 53-00-50-2R-9. 57066U 06/04/18
Part: SPLICE STRAP — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
SPLICE STRAP CORRODED BETWEEN BS 1016 TO BS 1028, RBL 3. R&R SPLICE STRAP PER SRM AND DWG.
Part: SPLICE STRAP — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
SPLICE STRAP CORRODED BETWEEN BS 1016 TO BS 1028, LBL 3. R&R SPLICE STRAP IAW SRM AND DWG.
Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
FORWARD ENTRY DOOR GIRT BAR SUPPORT FITTING CORRODED AT BS 344. R&R FITTING IAW SRM AND DWG.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
FORWARD SERVICE DOOR MOP SILL CORRODED BETWEEN BS 294 TO BS 328. R&R MOP SILL IAW SRM & DWG.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 1. R&R INTERCOSTAL IAW DWG AND SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 16. R&R INTERCOSTAL IAW DWG AND SRM.
Part: FLOOR PANEL — BROKEN (CABIN) · airframe 63,505 hrs · 37,387 cycles
AFT CABIN FLOOR BOARD 242XF IS BROKEN / DUE TO THE EXTENT OF DAMAGE; REPLACED PANEL 242XF WITH NEW PART IAW SRM 51-10-02-0G-0 PAR 9 AND AIPC 53-21-00-26 ITEM 220
Part: INTERCOSTAL — CRACKED (CABIN) · airframe 63,505 hrs · 37,387 cycles
CRACKED INTERCOSTAL AT B.S. 312-328; L.B.L. 47; W.L. 208.1. / REMOVED AND REPLACED CRACKED INTERCOSTAL AT BS 312-328; LBL 47; WL 208.1 WITH ITEM # 141A5410-12 IAW BOE DWG # 141A5400 AND SRM 51-40-02-0G-0
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
FLOORBEAM CORRODED AT BS 986, BETWEEN RBL 40 TO RBL 45. REPAIRED FLOORBEAM IAW SRM.
Part: ANGLE — CORRODED (FED THRESHOLD) · airframe 63,505 hrs · 37,387 cycles
FWD ENTRY DOOR 'Z' ANGLE FOR THRESHOLD SUPPORT IS CORRODED. / REPAIRED PER EA EA 1-753-32814 REV IR AND ER 18-02944 REV. IR.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 63,505 hrs · 37,387 cycles
AFT CABIN FLOOR BOARD 242RF UPPER SURFACE PLIES ARE DAMAGED / REPAIRED DAMAGE TO UPPER SURFACE PLIES ON AFT CABIN FLOOR BOARD 242RF IAW SRM 53-00-50-2R-1. 56749U 01JUN18
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
AFT ENTRY DOOR MOP SILL CORRODED BETWEEN BS 947 TO BS 992. R&R MOPSILL IAW SRM AND DWG.
Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
L1 DOOR GIRT BAR SUPPORT FITTING CORRODED AT BS 312. R&R FITTING IAW SRM AND DWG.
Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
SHEAR WEB CORRODED AT BS 1011, RBL 40. R&R SHEAR WEB IAW SRM AND DWG.
Part: SPLICE STRAP — CRACKED (LT WING) · airframe 63,505 hrs · 37,387 cycles
LT WING INBOARD LEADING EDGE STRAKELET SPLICE STRAP CRACKED. R&R STRAP IAW SRM AND DWG.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
R2 DOOR MOP SILL, UPPER SURFACE CORRODED BETWEEN BS 947 TO BS 992. R&R MOPSILL PER SRM AND DWG.
Part: INTERCOSTAL — CRACKED (CABIN) · airframe 63,505 hrs · 37,387 cycles
CRACKED INTERCOSTAL AT B.S. 328-344; L.B.L. 47; W.L. 208.1. / REMOVED AND REPLACED CRACKED INTERCOSTAL AT BS 328-344; LBL 47; WL 208.1 WITH ITEM # 141A5410-16 IAW BOE DWG # 141A5400 AND SRM 51-40-02-0G-0
Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
FORWARD ENTRY DOOR MOPSILL ATTACH ANGLE FOR THRESHOLD SUPPORT CORRODED. R&R ANGLE IAW SRM AND DWG.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 35. R&R INTERCOSTAL IAW SRM AND DWG.
Part: BALANCE WEIGHT — CORRODED (AILERON LH) · airframe 63,505 hrs · 37,387 cycles
***CORROSION*** (L/H WING) I/B AILERON BAY; AILERON BALANCE WEIGHT HAS CORROSION; SECOND FROM I/B. / REMOVED AND REPLACED THE L/H WING I/B AILERON BAY; AILERON BALANCE WEIGHT (SECOND FROM I/B) PER SOPM 20-50-01. 6888U 31MAY'18
Part: STRIP — CRACKED (RT WING) · airframe 63,505 hrs · 37,387 cycles
RT WING WIGGLE STRIP ABOVE NR 6 FLAP TRACK CRACKED. R&R WIGGLE STRIP IAW SRM.
Part: DOUBLER — CRACKED (FUSELAGE) · airframe 63,505 hrs · 37,387 cycles
GROUND POWER DOOR CUTOUT DOUBLE CRACKED. REPAIRED DOUBLER PER SRM.
2017
Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 60,810 hrs · 35,721 cycles
LT WHEEL WELL PRESSURE DECK WEB CRACKED AT BS 664, LBL 31. REPAIRED WEB PER EA.
Part: SLIDER — CRACKED (HORIZONTAL STAB) · airframe 60,099 hrs · 35,281 cycles
RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDER CRACKED. / R&R SLIDER IAW AMM 53-31-31
Part: SLIDER — CRACKED (HORIZONTAL STAB) · airframe 60,099 hrs · 35,281 cycles
LEFT HORIZONTAL STABILIZER UPPER LEADING EDGE SLIDER CRACKED. / R&R SLIDER IAW AMM 53-31-31
2016
Part: SEAL — CRACKED (BS 663) · airframe 58,732 hrs · 34,474 cycles
RH MLG WHEEL WELL VAPOR BARRIER SEAL CRACKED AT BS 663, RBL 14. REPAIRED VAPOR BARRIER IAW EA.
Part: SEAL — CRACKED (BS 663) · airframe 58,732 hrs · 34,474 cycles
RH MLG WHEEL WELL VAPOR BARRIER SEAL CRACKED AT BS 663, RBL 12. REPAIRED VAPOR BARRIER IAW EA.
Part: BRACKET — CRACKED (LT WING TE FLAP) · airframe 57,892 hrs · 33,978 cycles
LEFT WING FLAP DEFLECTION ROLLER BEAM I\B SIDE ANGLE BRACKET CRACKED. R & R THE BRACKET IAW SRM.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 57,892 hrs · 33,978 cycles
EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01675. R & R BATTERY PACK IAW DWG.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,369 hrs · 33,653 cycles
LEFT EMERGENCY LIGHTS INOPERATIVE BETWEEN BS 603 TO BS 727C. R & R BATTERY PACK IAW AMM.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 57,369 hrs · 33,653 cycles
LEFT BULKHEAD ANGLE CRACKED AT BS 727, WL 192. REPAIRED ANGLE IAW EA.
Part: FRAME — CRACKED (BS 727D) · airframe 57,369 hrs · 33,653 cycles
FRAME CRACKED AT BS 727D, STRINGER 8R. REPAIRED THE FRAME IAW EA.
Part: FRAME — CRACKED (BS 827) · airframe 57,369 hrs · 33,653 cycles
FRAME CRACKED AT BS 827, STRINGER 8L. REPAIRED THE FRAME IAW EA.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,369 hrs · 33,653 cycles
SEAT TRACK CORRODED BETWEEN BS 480 TO BS 520, LBL 24. R & R SEAT TRACK IAW SRM.
Part: FRAME — CRACKED (BS 787) · airframe 57,369 hrs · 33,653 cycles
FRAME CRACKED AT BS 787, STRINGER 8L. REPAIRED THE FRAME IAW EA.
Part: FRAME — CRACKED (BS 727D) · airframe 57,369 hrs · 33,653 cycles
FRAME CRACKED AT BS 727D, STRINGER 8L. REPAIRED THE FRAME IAW EA.
Part: FRAME — CRACKED (BS 500C) · airframe 57,369 hrs · 33,653 cycles
FRAME CRACKED AT BS 500C, STRINGER 8L. REPAIRED THE FRAME IAW EA.
Part: FRAME — CRACKED (BS 500A) · airframe 57,369 hrs · 33,653 cycles
FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED THE FRAME IAW EA.
Part: FRAME — CRACKED (BS 380) · airframe 57,369 hrs · 33,653 cycles
FRAME CRACKED AT BS 380, STRINGER 8L. REPAIRED THE FRAME IAW EA.
Part: FRAME — CRACKED (BS 480) · airframe 57,369 hrs · 33,653 cycles
FRAME CRACKED AT BS 480, STRINGER 8L. REPAIRED THE FRAME IAW EA.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 57,369 hrs · 33,653 cycles
PASSENGER SEAT TRACK CORRODED BETWEEN BS 706+17 TO BS 727+17, RBL 45.57. R & R SEAT TRACK IAW SRM.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,369 hrs · 33,653 cycles
STRINGER CLIP CRACKED AT BS 360, STR 8R. R & R CLIP IAW SRM.
Part: FRAME — CRACKED (BS 360) · airframe 57,369 hrs · 33,653 cycles
FRAME CRACKED AT BS 360, STRINGER 8R. REPAIRED THE FRAME IAW EA.
Part: FRAME — CRACKED (BS 727) · airframe 57,369 hrs · 33,653 cycles
RIGHT BULKHEAD FRAME WEB AND INNER CHORD CRACKED BS 727, WL 200 LOWER FASTENER HOLE. REPAIRED THE FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 57,369 hrs · 33,653 cycles
FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (BS 747) · airframe 57,369 hrs · 33,653 cycles
FRAME CRACKED AT BS 747, STRINGER 8R. REPAIRED THE FRAME IAW EA.
Part: FRAME — CRACKED (BS 727) · airframe 57,369 hrs · 33,653 cycles
LEFT LOWER FRAME WEB CRACKED AT BS 727, WL 200. REPAIRED THE FRAME WEB IAW EA.
Part: FRAME — CRACKED (BS 480) · airframe 57,369 hrs · 33,653 cycles
FRAME CRACKED AT BS 480, STRINGER 8R. REPAIRED THE FRAME IAW EA.
Part: BULKHEAD — CRACKED (BS 727) · airframe 57,369 hrs · 33,653 cycles
RIGHT BULKHEAD WEB AND INNER CHORD CRACKED AT BS 727, WL 200 LOWER FASTENER HOLE. REPAIRED BULKHEAD WEB IAW EA.
Part: SKIN — CRACKED (LE SLAT) · airframe 57,369 hrs · 33,653 cycles
RIGHT WING NR 7 L/E SLAT NOSE SKIN CRACKED AT ACTUATOR RIB. REPAIRED SKIN IAW SRM.
Part: HOLDER — LOOSE (L1 DOOR) · airframe 55,931 hrs · 32,848 cycles
L1 DOOR EMER SLIDE GIRT BAR HOLDERS LOOSE. SECURED GIRT BAR IAW AMM.
Part: HOLDER — LOOSE (R1 DOOR) · airframe 55,931 hrs · 32,848 cycles
R1 DOOR FWD GIRT BAR HOLDER LOOSE. SECURED GIRT BAR IAW AMM.
2015
Part: POST — CRACKED (FUSELAGE) · airframe 55,363 hrs · 32,526 cycles
RIGHT NR 3 WINDOW POST, 3RD FROM BOTTOM FASTENER CRACKED. REPAIRED POST IAW ACO.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,363 hrs · 32,526 cycles
LEFT NR 3 WINDOW POST 3RD FROM BOTTOM FASTENER HOLE CRACKED. R & R FRAME IAW EA.
Part: POST — CRACKED (FUSELAGE) · airframe 55,363 hrs · 32,526 cycles
RIGHT NR 3 WINDOW POST 2ND FROM BOTTOM FASTENER HOLE CRACKED. REPAIRED POST IAW ACO.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,363 hrs · 32,526 cycles
LEFT NR 1 WINDOW FRAME CRACKED IN UPPER OTBD CORNER. REPAIRED FRAME IAW ACO.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 55,363 hrs · 32,526 cycles
RIGHT NR 1 WINDOW FRAME CRACKED IN UPPER OTBD CORNER. REPAIRED FRAME IAW ACO.
Part: ACM — FAILED (LEFT) · airframe 53,718 hrs · 31,554 cycles
THE LEFT A/C PACK TRIPPED WITH AN ODOR. R & R THE LT AIR CYCLE MACHINE IAW MM.
Part: FUSE — BLOWN (CABIN) · airframe 52,684 hrs · 30,963 cycles
R1 DOOR FLOOR EMER EXIT LIGHT INOPERATIVE. R & R FUSE IAW AMM.
2014
Part: BATTERY — DISCHARGED (CABIN) · airframe 51,553 hrs · 30,312 cycles
EMERGENCY LIGHTS FAILED CAPACITY CHECK. R & R M1674 BATTERY IAW MM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 51,553 hrs · 30,312 cycles
EMERGENCY LIGHTS FAILED CAPACITY CHECK. R & R M1673 BATTERY IAW MM.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 50,488 hrs · 29,682 cycles
LEFT HORIZONTAL STABILIZER STATION 101.9 RIB LOWER INBD FLANGE 9 INCHES AFT OF LE CRACKED. REPAIRED FLANGE IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,488 hrs · 29,682 cycles
SEAT TRACK CRACKED AT BS 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EA.
Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 50,488 hrs · 29,682 cycles
RIGHT HORIZONTAL STAB STIFFENER CRACKED AT STATION 92.70. REPAIRED STIFFENER IAW SRM.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,488 hrs · 29,682 cycles
SEAT TRACK CRACKED AT BS 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EA.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,488 hrs · 29,682 cycles
SEAT TRACK CRACKED AT BS 727B, RBL 45.5. REPAIRED SEAT TRACK IAW EA.
Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 50,488 hrs · 29,682 cycles
RIGHT HORIZONTAL STAB STIFFENER CRACKED AT STATION 129.50. REPAIRED STIFFENER IAW SRM.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,488 hrs · 29,682 cycles
SEAT TRACK CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 50,199 hrs · 29,506 cycles
LEFT HORIZONTAL STABILIZER STATION 175.5 FWD OTBD HOLE IN RIB CRACKED. REPAIRED RIB IAW EA.
2013
Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 47,658 hrs · 28,033 cycles
R2 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. R&R SLIDE IAW MT.
Part: BATTERY — FAILED (CABIN) · airframe 47,192 hrs · 27,755 cycles
RT EMERGENCY BATTERIES FAILED CAPACITY TEST. R&R BATTERIES IAW AMM.
2012
Part: SLIDE — LOOSE (R1 DOOR) · airframe 43,895 hrs · 25,788 cycles
R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,761 hrs · 25,712 cycles
AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 772, RBL 8. REPAIRED SUPPORT IAW EA.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,761 hrs · 25,712 cycles
AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 772, LBL 3. REPAIRED SUPPORT IAW EA.
Part: RIB — CRACKED (LT HORIZ STAB) · airframe 43,761 hrs · 25,712 cycles
LEFT HORIZONTAL STABILIZER RIB CRACKED AT STA 92.70. REPAIRED RIB PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,761 hrs · 25,712 cycles
FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME IAW EA.
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 43,761 hrs · 25,712 cycles
RIGHT HORIZONTAL STABILIZER INSPAR RIB CRACKED AT STA 92.70. REMOVED AND REPLACED RIB PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,761 hrs · 25,712 cycles
FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,761 hrs · 25,712 cycles
FRAME CRACKED AT BS 867, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,761 hrs · 25,712 cycles
CABIN FRAME CRACKED AT BS 787, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,761 hrs · 25,712 cycles
FRAME CRACKED AT BS 827, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,761 hrs · 25,712 cycles
FRAME CRACKED AT BS 867, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME IAW EA.
Part: SUPPORT FITTING — CORRODED (L1 DOOR) · airframe 43,761 hrs · 25,712 cycles
L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR SUPPORT FITTING CORRODED. REMOVED AND REPLACED FITTING ASSY PER SRM.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,761 hrs · 25,712 cycles
FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME IAW EA.
Part: FRAME — CRACKED (FUSELAGE) · airframe 43,761 hrs · 25,712 cycles
FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME IAW EA.
Part: WEB — CORRODED (FUSELAGE) · airframe 43,761 hrs · 25,712 cycles
WEB CORRODED BETWEEN BS 794 TO BS 833, BETWEEN RBL 21 TO RBL 27. REMOVED AND REPLACED WEB PER SRM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,761 hrs · 25,712 cycles
RIGHT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED ON THE REAR SPAR BETWEEN STA 98 TO STA 96. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,761 hrs · 25,712 cycles
RIGHT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED AT STA 83.50. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,761 hrs · 25,712 cycles
LEFT HORIZONTAL STABILIZER LOWER SURFACE CRACKED AT STAB STA 101.90. REPAIRED SKIN PER SRM.
Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 43,761 hrs · 25,712 cycles
LEFT HORIZONTAL STABILIZER LOWER SURFACE CRACKED AT STAB STA 120.30. REPAIRED SKIN PER SRM.
Part: SPAR — CRACKED (LT HORIZ STAB) · airframe 43,761 hrs · 25,712 cycles
LEFT HORIZONTAL STABILIZER REAR SPAR CRACKED AT STA 120.30. REPAIRED SPAR IAW SRM.
Part: SPAR — CRACKED (LT HORIZ STAB) · airframe 43,761 hrs · 25,712 cycles
LEFT HORIZONTAL STABILIZER REAR SPAR CRACKED AT STA 92.70. REPAIRED SPAR IAW SRM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,454 hrs · 25,530 cycles
RIGHT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED AT STA 142-15. REPAIRED PER SKIN SRM.
Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 43,454 hrs · 25,530 cycles
RIGHT HORIZONTAL STABILIZER INSPAR SKIN CRACKED AT L/E STA 142-15. REPAIRED SKIN PER SRM.
Part: LIGHT — DAMAGED (CABIN) · airframe 43,091 hrs · 25,336 cycles
RT EEPLS DAMAGED AT ROW 15. REMOVED AND REPLACED EEPLS PER MM.
2011
Part: WINDOW — ARCED (COCKPIT) · airframe 42,092 hrs · 24,751 cycles
R1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW AND WINDOW HEAT CONTROLLER PER MM.
Part: BATTERY — FAILED (CABIN) · airframe 40,752 hrs · 23,953 cycles
DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER MM.
Part: BATTERY — FAILED (CABIN) · airframe 40,752 hrs · 23,953 cycles
DURING SCHEDULED HC2 CHECK, RT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER MM.
Part: GASPER FAN — FAULTY (AC BAY) · airframe 39,251 hrs · 23,071 cycles
DIVERSION / EMERGENCY DECLARED, ELECTRICAL SMELL IN CABIN. REMOVED AND REPLACED A/C GASPER FAN PER MM.
2010
Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,292 hrs · 22,526 cycles
FWD EEPLS INOP. REMOVED AND REPLACED EEPLS PER MM.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 37,071 hrs · 21,809 cycles
DURING SCHEDULED 10Y CHECK, FOUND INTERCOSTAL CORRODED UNDER COCKPIT THRESHOLD AT BS 270, BETWEEN RBL 12 TO LBL 10. REPAIRED INTERCOSTAL PER EA.
Part: WEB — CRACKED (CENTER WING BOX) · airframe 37,071 hrs · 21,809 cycles
DURING SCHEDULED 10Y CHECK, FOUND VERTICAL WEB CRACKED AT BS 663, RBL 42. REPAIRED WEB PER EA.
Part: WEB — CRACKED (CENTER WING BOX) · airframe 37,071 hrs · 21,809 cycles
DURING SCHEDULED 10Y CHECK, FOUND VERTICAL WEB CRACKED AT BS 663, LBL 40. REPAIRED WEB PER EA.
Part: WEB — CRACKED (CENTER WING BOX) · airframe 37,071 hrs · 21,809 cycles
DURING SCHEDULED 10Y CHECK, FOUND VERTICAL WEB CRACKED AT BS 663, LBL 27. REPAIRED WEB PER EA.
Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 37,071 hrs · 21,809 cycles
DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX VERTICAL STIFFENER CRACKED AT BS 547, LBL 15. REMOVED AND REPLACED ANGLE PER SRM.
Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 37,071 hrs · 21,809 cycles
DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX VERTICAL STIFFENER CRACKED AT BS 547, LBL 32. REMOVED AND REPLACED ANGLE PER SRM.
Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 37,071 hrs · 21,809 cycles
DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX VERTICAL STIFFENER CRACKED AT BS 547, RBL 41. REMOVED AND REPLACED ANGLE PER SRM.
Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 37,071 hrs · 21,809 cycles
DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX VERTICAL STIFFENER CRACKED AT BS 547, LBL 41. REMOVED AND REPLACED ANGLE PER SRM.
Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 37,071 hrs · 21,809 cycles
DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX VERTICAL STIFFENER CRACKED AT BS 547, RBL 32. REMOVED AND REPLACED ANGLE PER SRM.
Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 37,071 hrs · 21,809 cycles
DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX VERTICAL STIFFENER CRACKED AT BS 547, RBL 15. REMOVED AND REPLACED ANGLE PER SRM.
Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 37,071 hrs · 21,809 cycles
DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX VERTICAL STIFFENER CRACKED AT BS 547, LBL 6. REMOVED AND REPLACED ANGLE PER SRM.
Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 37,071 hrs · 21,809 cycles
DURING SCHEDULED 10Y CHECK, FOUND CENTER WING BOX VERTICAL STIFFENER CRACKED AT BS 547, RBL 6. REMOVED AND REPLACED ANGLE PER SRM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,813 hrs · 21,036 cycles
DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT HATCH LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,357 hrs · 20,764 cycles
DURING SCHEDULED CV CHECK, FOUND RT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP BETWEEN ROW 5 TO ROW 6. RELAMPED PER MM.
2009
Part: RELIEF VALVE — FAULTY (CABIN PRESSURE) · airframe 34,709 hrs · 20,372 cycles
DIVERSION - ON TAKEOFF AIRCRAFT WOULD NOT PRESSURIZE NORMAL. OUTFLOW VALVE CLOSED. REMOVED AND REPLACED NEGATIVE PRESSURE RELIEF VALVE PER MM.
Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 34,466 hrs · 20,222 cycles
DURING SCHEDULED MV2 CHECK, FOUND RIGHT MLG FWD TRUNNION SUPPORT FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.
Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 34,466 hrs · 20,222 cycles
DURING SCHEDULED MV2 CHECK, FOUND LEFT MLG FWD TRUNNION SUPPORT FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA.
Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 34,178 hrs · 20,037 cycles
R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF POSITION. REPOSITIONED SLIDE PER MM.
Part: FITTING — OBSTRUCTED (L1 DOOR) · airframe 33,814 hrs · 19,805 cycles
DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR NOT ABLE TO ARM. REMOVED DEBRIS FROM FITTINGS PER MM.
Part: LENS — BROKEN (CABIN) · airframe 32,570 hrs · 19,059 cycles
DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 32,471 hrs · 18,999 cycles
DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.
Part: TRACK — DAMAGED (CABIN) · airframe 31,910 hrs · 18,641 cycles
DURING SCHEDULED HC2 CHECK, FOUND EEPLS TRACK DAMAGED. REMOVED AND REPLACED EEPLS PER MM.
2008
Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 30,116 hrs · 17,578 cycles
L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 29,634 hrs · 17,283 cycles
DURING SCHEDULED HC1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,165 hrs · 16,389 cycles
DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 28,156 hrs · 16,384 cycles
LEFT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 28,156 hrs · 16,384 cycles
LEFT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.
2007
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,666 hrs · 16,084 cycles
DURING SCHEDULED MV3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 27,262 hrs · 15,842 cycles
DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT LIGHT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 25,939 hrs · 15,065 cycles
R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 35,939 hrs · 15,065 cycles
R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.
Part: BOTTLE — LOW PRESSURE (L2 DOOR SLIDE) · airframe 25,231 hrs · 14,650 cycles
DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM.
2006
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,188 hrs · 14,050 cycles
DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,148 hrs · 13,480 cycles
RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,139 hrs · 13,425 cycles
RT OVERWING EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,080 hrs · 13,442 cycles
DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT EXTERIOR LIGHT INOP AT LT AFT FUSELAGE. REMOVED AND REPLACED LIGHT BULB PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,290 hrs · 12,989 cycles
DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: SIGN — LOOSE (CABIN) · airframe 21,514 hrs · 12,551 cycles
RT OVERWING EMERGENCY EXIT SIGN LOOSE. R&R LIGHT ASSY PER MM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,929 hrs · 9,949 cycles
DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.
2005
Part: BULB — INOPERATIVE (FUSELAGE) · airframe 19,871 hrs · 11,647 cycles
DURING SCHEDULED RON CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.
Part: COVER — LOOSE (CABIN) · airframe 19,629 hrs · 11,506 cycles
EEPLS TRACK COVER LOOSE AT FWD END. SECURED COVER PER MM.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,656 hrs · 10,946 cycles
DURING SCHEDULED 5Y CHECK, FOUND RT OVERWING EXIT EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,573 hrs · 10,333 cycles
DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 17,404 hrs · 10,223 cycles
DURING SCHEDULED RON, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.
Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 17,384 hrs · 10,222 cycles
DURING SCHEDULED RON, FOUND FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM.
Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 17,338 hrs · 10,200 cycles
DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.
2004
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,078 hrs · 9,438 cycles
DURING SCHEDULED MV2 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.
Part: COVER — CRACKED (ROW 8 - 12) · airframe 15,022 hrs · 8,807 cycles
DURING SCHEDULED MV2 CHECK, FOUND EEPLS LIGHT COVERS AT ROW 8 ABC, ROW 12 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVERS PER MM.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,957 hrs · 8,777 cycles
DURING SCHEDULED RON, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.
Part: BULKHEAD — CANNING (FUSELAGE) · airframe 13,759 hrs · 8,098 cycles
DURING SCHEDULED C4 CHECK, FOUND BS 1016 BULKHEAD PRESS BULKHEAD OIL CANNED AT STR 26. REPAIRED BULKHEAD PER SWA EA.
Part: COFFEEMAKER — FAULTY (AFT GALLEY) · airframe 13,593 hrs · 8,006 cycles
F/A REPORTED SMELLING SMOKE IN AFT GALLEY AREA. TRACED ELECTRICAL BURNT ODOR TO COFFEEMAKER. PULLED COFFEEMAKER CB NO FURTHER ODOR. REMOVED AND REPLACED NR 2 COFFEEMAKER PER MM.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 13,239 hrs · 7,821 cycles
DURING SCHEDULED MS CHECK, FOUND OVERHEAD RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED OVERWING EMERGENCY EXIT LIGHT BATTERY PER MM.
2003
Part: SLIDE — DISLODGED (R2 DOOR) · airframe 12,374 hrs · 7,306 cycles
R2 DOOR EVACUATION SLIDE FALLING OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.
Part: SLIDE — OUT OF ADJUST (ENTRY DOOR) · airframe 11,651 hrs · 6,880 cycles
DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.
Part: SLIDE — UNSERVICEABLE (AFT ENTRY DOOR) · airframe 11,398 hrs · 6,742 cycles
AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 11,097 hrs · 6,586 cycles
DURING SCHEDULED RON, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.
Part: LIGHT — INOPERATIVE (ROW 8 & 15) · airframe 10,637 hrs · 6,324 cycles
DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP BETWEEN ROW 8 & ROW 15. REPAIRED WIRE AT D1072 CONNECTOR PER MM.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 9,683 hrs · 5,759 cycles
DURING SCHEDULED RON, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER AND BATTERY PER MM.
2002
Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 8,526 hrs · 5,100 cycles
FWD ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.
Part: BUSHING — WORN (RT ELEVATOR) · airframe 7,959 hrs · 4,782 cycles
DURING SCHEDULED SERVICE CHECK, SWA SI 11038-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB HARDWARE AND BUSHINGS AT NR 2, NR 3 AND NR 4 HINGE ATTACH POINTS PER MM.
Part: SLIDE — OUT OF ADJUST (FWD SVC DOOR) · airframe 7,041 hrs · 4,220 cycles
FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.
Part: BUSHING — WORN (ELEVATORS) · airframe 6,688 hrs · 4,024 cycles
DURING SCHEDULED C2 CHECK, SI 11038-55, BOTH LT AND RT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 4 HINGE BUSHINGS ON LT AND RT TABS PER MM.
2001
Part: SLIDE — OUT OF ADJ (GALLEY DOOR) · airframe 4,328 hrs · 2,609 cycles
DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EVAC SLIDES OUT OF ADJUST AT BOTH GALLEY DOORS. ADJUSTED EVAC SLIDES PER MM.
Part: COVER — CRACKED (CABIN) · airframe 4,328 hrs · 2,609 cycles
DURING SCHEDULED C4 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED. R&R EEPLS COVERS PER MM.