N8601C
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| ROLF E. IVERSON LTD. | Operator | on 1982-08-22 | Operator named in NTSB report |
Accident & incident history
Operated by ROLF E. IVERSON LTD. (per NTSB report)
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.
130 reports on file, 2012-06-05 – 2024-04-21.
Part: RETAINER — LOOSE (SLIDE COVER) · airframe 40,329 hrs · 18,725 cycles
FSD SLIDE PACK COVER FWD RETAINER LOOSE (MARKED)<[01] REMOVED AND REPLACED LOOSE FASTENERS ON FSD SLIDE PACK COVER FWD RETAINER PER SRM 51-40-02-0G-0 STEP 4.;[02] VERIFIED
Part: SHIELD — CRACKED (NR 1 FAN COWL) · airframe 40,329 hrs · 18,725 cycles
#1 ENGINE I/B FAN COWL OIL DOOR SHEILD HAS A CRACK<[01] REMOVE AND INSTALL NEW SHIELD ON #1 ENINE I/B FAN COWL STRUCTURE IAW SRM 51-40-02-0G-0 AND CMM 71-13-30;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
Part: SHIELD — CRACKED (NR 2 FAN COWL) · airframe 40,329 hrs · 18,725 cycles
#2 ENGINE O/B FAN COWL OIL DOOR SHEILD HAS A CRACK<[01] REMOVE AND INSTALL NEW SHIELD ON #2 ENINE O/B FAN COWL STRUCTURE IAW SRM 51-40-02-0G-0 AND CMM 71-13-30;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
Part: LIGHT — INOPERATIVE (ROWS 16FED-18CBA) · airframe 40,322 hrs · 18,721 cycles
EPL PATHWAYS STRIPS AT ROWS 16FED AND 18CBA INOP.<[01] REMOVED AND REPLACED EPL PATHWAYS STRIPS AT ROWS 16FED AND 18CBA IN REF. DWG 417A5775.;[02] VERIFIED REPLACEMENT
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 40,322 hrs · 18,721 cycles
LAVATORY A EXIT SIGN TO L-1 DOOR LENS MISSING<[01] INSTALLED LAVATORY A EXIT SIGN TO L-1 DOOR LENS; B 737-800 AMM 33-5101-860-802;[02] INSTALLED LAVATORY A EXIT SIGN TO L-1 DOOR LENS; B 737-800 AMM 33-51-01-860-802;[03] STEP 1 EIE. VERIFIED CORRECTED STEP 2.;[04] STEPS 1; 2; AND 3 ENTERED IN ERROR.;[05] INSTALLED LAVATORY A EXIT SIGN TO L-1 DOOR LENS; B 737-800 AMM 33-51-01-960-802;[06] VERIFIED STEP 5.
Part: BATTERY PACK — INOPERATIVE (EMERGNECY LIGHTS) · airframe 40,322 hrs · 18,721 cycles
MULTIPLE LIGHTS FOUND INOP INSIDE CABIN AND ON EXTERIOR DURING OPERATIONAL CHECK MULTIPLE EMERGENCY LIGHTS FOUND INOP INSIDE CABIN AND ON EXTERIOR DURING OPERATIONAL CHECK<[01] REPLACED BATTERY PACKS ASSEMBLIES AT EMERGENCY LIGHTS POWER SUPPLY ASSEMBLIES M01671 AND M1627. REPLACED 1 (EA) FUSES AT EMERGENCY EXIT POWER SUPPLY ASSEMBLIES M1694 AND M1695. REPLACED ALSO 1 BATTERY PACK AT M1694 POWER SUPPLY ASSY. REFERENCE B 737 AMM 33-51-06-960-805. EMERGENCY LIGHTS OPERATINAL TEST PASSED. B737 AMM 33-51-00-710-801.;[02] VERIFIED STEP #1
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 40,322 hrs · 18,721 cycles
MAIN CABIN FLOOR PANEL 221DF HAS UPPER SURFACE DELAMINATED.<[01] FOUND MAIN CABIN FLOOR PANEL 221DF OUT OF LIMITS PER BOEING 737-800 SRM 53-00-50-1A-1. REMOVED AND REPLACED FLOOR PANEL PER BOEING 737-800 AMM 53-21-00-400-801.<BR><BR>TOOL: SCREW GUN B/C 176016. CALIBRATION DUE DATE 07-JUN-2024;[02] VERIFIED STEP 1
Part: HANDLE — CHAFED (SERVICE DOOR) · airframe 40,322 hrs · 18,721 cycles
FWD GALLEY SERVICE DOOR HANDLE CAM PLATE HAS CHAFING MARK<[01] REMOVED AND REPLACED FWD GALLEY SERVICE DOOR HANDLE CAM PLATE PER B737 SOPM 20-50-01;[02] VERIFIED STEP 1
Part: MOUNT — BROKEN (DOOR SLIDE) · airframe 40,322 hrs · 18,721 cycles
FWD GALLEY SERVICE DOOR SLIDE AFT MOUNT HAS SHOCK MOUNT BROKEN<[01] REMOVED AND REPLACED FWD GALLEY SERVICE DOOR SLIDE AFT SHOCKMOUNT P/N BACS14K2 PO#1291885 AS PER SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1
Part: FASTENER — INOPERATIVE (SERVICE DOOR) · airframe 40,322 hrs · 18,721 cycles
FWD GALLEY SERVICE DOOR FIFTH BEAM CENTER SECTION BLIND FASTENER HAS SHREDDED<[01] REMOVED AND INSTALLED FASTENERS AT FWD GALLEY SERVICE DOOR FIFTH BEAM CENTER SECTION REF USED SRM 51-40-02-0G-0 STEP 4.B(1) AND DWG#141A5616;[02] VERIFIED R/R
Part: ATTACH BRACKET — CRACKED (BS 500G) · airframe 40,322 hrs · 18,721 cycles
FORWARD CARGO COMPARTEMENT INTERCOSTAL BFRACKET ATTACH CRACKED AT STA 500G R/H<[01] REMOVED AND REPLACED AT FORWARD CARGO COMPARTEMENT INTERCOSTAL CLIP FROM STA 500G R/H SIDE PER REF SRM 51-4-02-0G-0;[02] VERIFIED STEP # 1
Part: ATTACH BRACKET — CRACKED (BS 500H) · airframe 40,322 hrs · 18,721 cycles
FORWARD CARGO COMPARTMENT INTERCOSTAL BRACKET ATTACH CRAKED AT STA 500H AFT SIDE UNDER 'Z' CHANNEL.<[01] REMOVED AND REPLACED AT FORWARD CARGO COMPARTMENT INTERCOSTAL CLIP FROM STA 500H AFT SIDE UNDER 'Z' CHANNEL PER REF SRM 51-40-02-0G-0;[02] VERIFIED STEP # 1
Part: STRINGER — CRACKED (BS 500I S25R) · airframe 40,322 hrs · 18,721 cycles
FORWAD CARGO COMPARTMENT STA 500I R/H STRINGER 25 CLICK ATTAC IS CRACKED FORWARD CARGO COMPARTMENT STA 500I R/H STRINGER CLIP ATTACH IS CRACKED<[01] REMOVED AND REPLACED AT FORWAD CARGO COMPARTMENT STRINGER CLIP FROM STA 500I PER REF SRM 51-40-02-0G-0;[02] VERIFIED STEP # 1
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 40,322 hrs · 18,721 cycles
MAIN CABIN FLOOR PANEL#241D UPPER SURFACE FOUND DELAMINATED<[01] FOUND CABIN FLOOR PANEL 241D OUT OF LIMITS AS PER SRM 53-00-50-1A-1. RECEIVED NEW FLOOR PANEL. REF. CLOSING CARD TTG8Q00RDDMA.
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 40,322 hrs · 18,721 cycles
MAIN CABIN STA. 890 FLOOR PANEL#242SF UPPER SURFACE FOUND DELAMINATED<[01] FOUND FLOOR PANEL 242SF OUT OF LIMITS AS PER SRM 53-00-50-1A-1. RECEIVED NEW PANEL. REF. CLOSING CARD TTG8Q00RDFXP.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 40,322 hrs · 18,721 cycles
MAIN CABIN STA.887 FLOOR PANEL#241ZF UPPER SURFACE FOUND DELAMINATED<[01] FOUND CABIN FLOOR PANEL 241ZF OUT OF LIMITS AS PER SRM 53-00-50-1A-1. RECEIVED NEW FLOOR PANEL. REF. CLOSING CARD TTG8Q00RDFD4.;[02] VERIFIED STEP 1
Part: FLOOR PANEL — DELAMINATED (AFT CABIN) · airframe 40,322 hrs · 18,721 cycles
AFT MAIN CABIN FLOOR PANEL#242D UPPER SURFACE FOUND DELAMINATED<[01] FOUND CABIN FLOOR PANEL 242D OUT OF LIMITS PER BOEING 737-800 SRM 53-00-50-1A-1. RECEIVED NEW FLOOR PANEL. REF. CLOSING CARD TTG8Q00RDDKR.;[02] VERIFIED RECEIVED
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 40,322 hrs · 18,721 cycles
MAIN CABIN AFT WET AREA STA.960 PANEL#241ABF UPPER SURFACE FOUND DELAMINATED<[01] REPLACED MAIN CABIN FLOOR 241ABF AT AFT CABIN WET AREA PER BOEING 737-800 SRM 53-00-50-1A-1;[02] VERIFIED REPLACED
Part: FLOOR PANEL — DELAMINATED (AFT CABIN) · airframe 40,322 hrs · 18,721 cycles
MAIN CABIN AFT WET AREA STA. 890 PANEL#241YF UPPER SURFACE FOUND DELAMINATED<[01] FOUND CABIN FLOOR PANEL 241YF OUT OF LIMITS AS PER SRM 53-00-50-1A-1. RECEIVED NEW FLOOR PANEL. REF. CLOSING CARD TTG8Q00RDFDT.
Part: FLOOR PANEL — DELAMINATED (AFT CABIN) · airframe 40,322 hrs · 18,721 cycles
MAIN CABIN AFT WET AREA STA. 890 PANEL#241XF UPPER SURFACE FOUND DELAMINATED<[01] FOUND CABIN FLOOR PANEL 241XF OUT OF LIMITS PER BOEING 737-800 SRM 53-00-50-1A-1. RECEIVED NEW FLOOR. REF. CLOSING CARD TTG8Q00RDDKX;[02] VERIFIED RECEIVED
Part: STRAP — CRACKED (BS 540) · airframe 40,322 hrs · 18,721 cycles
MAIN CABIN FLOOR STRAP CRACKED AT STA.540 LBL2.<[01] REMOVED AND REPLACED FLOOR STRAP AT MAIN CABIN STA 540 LBL12' REF B-737-800 SRM 51-40-02-0G-0;[02] VERIFIED R/R
Part: FLOOR SUPPORT — CRACKED (BS 380-400 LBL15) · airframe 40,322 hrs · 18,721 cycles
MAIN CABIN FLOOR STRUCTURE INTERCOSTAL BETWEEN STA 380 AND 400 LBL 15' IS CRACK AT UPPER SURFACE MKD (107-004)<[01] REMOVED AND REPLACED INTERCOSTAL UPPER CHORD AT MAIN CABIN FLOOR STRUCTURE BETWEEN STA 380 AND 400 LBL 15' AS PER BOEING 737-800 SRM 51-40-02-0G-0;DWG:143A5400;[02] RII- VERIFIED REMOVED AND REPLACED INTERCOSTAL
Part: FLOOR SUPPORT — CORRODED (BS 947) · airframe 40,322 hrs · 18,721 cycles
AFT WET AREA FLOOR STRUCTURE HAS SURFACE CORROSION AROUND FASTENER HOLE AT STA 947 LBL 4<[01] SUMMARY: REMOVED CORROSION AT AFT WET FLOOR STRUCTURE AROUND FASTENER HOLE STA 947 LBL4: AS PER REF B/737 SRM 51-10-02-0G-0.IAW B737 NDT P. 4; 51-00-00 PROC. 3. MIN THICKNESS .144';<BR>EQUIP: OLYMPUS 27MG CAL DUE: 4/24 B/C 172139.FABRICATED REPAIR PART ( STRAP ) .MATERIAL USED 7075 T6 .100 P/O 2010612 AS PER REF B/737 SRM 53-70-51-2R-8 FIG 203. ALTERNATIVE 1.INSTALLED REPAIR PART ON AFT WET AREA FLOOR STRUCTURE STA 947 LBL4' AS PER REF B/737 SRM 53-70- 51-2R -8 REPAIR 8 FIG 203 ALTERNATIVE 1.MIXED 0870B002BMS 16:00 03/06/24.FILLED BLENDED AREA AS PER REF B/737 SRM 51-70-01-2R-0 REPAIR GENERAL .PARR 4 D.;[02] VERIFIED STEP 1
Part: FRAME — CRACKED (BS 312 LBL 33) · airframe 40,322 hrs · 18,721 cycles
FWD CABIN STA 312 LBL 33 FRAME CRACKED ON TOP OF DOOR CUTOUT<[01] ACCOMPLISHED FWD CABIN STA 312 LBL-33 FRAME CRACK ON TOP OF DOOR CUTOUT P/N 141A1134-5 REF CARD#M-22-153-01244/9151210;[02] ACCOMPLISHED FWD CABIN STA 312 LBL 33 FRAME CRACK.
Part: FLOOR PANEL — DEFORMED (MAIN CABIN) · airframe 40,322 hrs · 18,721 cycles
PANEL 231AF HAS LARGE DEFORMATIONS OVER SURFACE<[01] REPLACED MAIN CABIN FLOOR PANEL 231AF PER BOEING 737-800 SRM 53-00-53-1A-1<BR>PO 2059779;[02] VERIFIED
Part: FLOOR SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 40,322 hrs · 18,721 cycles
PASSENGER COMPARTMENT B/W STA 294-312 INTERCOSTAL HAS CORROSION IN AT FLOOR PANEL ATTAC HOLE LBL 12'.<[01] REMOVED AND REPLACED NEW INTERCOSTAL P/N 141A5690UIATSMRO P.O #2058779 AT PASSENGER COMPARTMENT STA 294-312 LBL 12 AS PER SRM 51-40-02-0G-0. DWG 141A5600 ID 0006;[02] VERIFIED R/R
Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 39,950 hrs · 18,518 cycles
EMERGENCY LIGHT BATTERY PACK M1673 NOT CHARGING AT AFT GALLEY AREA OVERHEAD<[01] R&R?D CHARGER AND BATTERY PACK PER AMM 33-51-06
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,898 hrs · 18,487 cycles
AFT ENTRY DOOR EMERGENCY LIGHT (SLIDE/OVERWING LIGHT) INOP.<[01] RELAMPED AFT ENTRY EMERGENCY LIGHT ( SLIDE/OVERWING LIGHT) IAW AMM 33-51-04. OPS CHECK GOOD.
Earlier reports · 2012–2023 · 102 reports
2023
Part: DOOR FRAME — CRACKED (ZN 100 FUS LOWER) · airframe 39,579 hrs · 18,304 cycles
EXT. POWER DOOR FRAME CRACKED AT APPROX 6OCLOCK POSITION.<[01] REMOVED DAMAGED SECTION OF SURROUND DOUBLER PER SRM 53-10-15-2R-4; REPAIR 4;[02] ACCOMPLISHED HFEC OF CUTOUT PER NDT PART 6; 51-00-00 PROCEDURE 23. NO DEFECTS FOUND.;[03] REPAIRED PER SRM 53-10-15-2R-4 REPAIR 4
2022
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,189 hrs · 16,389 cycles
OVER WING EXIT EMERGENCY LIGHT R/H INOP. / [01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06 ( STA 663 R/H ) PART # INSTALLED D71701 S/N 299537. P/N OFF D717-01 S/N 211201
Part: OIL SYSTEM — LOW PRESSURE (NR 2 ENGINE) · airframe 36,188 hrs · 16,388 cycles
AT FL370 NR 2 ENGINE OIL QTY AND PRESSURE STEADILY DROPPED TO ZERO; WITH ASSOCIATED ALERTS. COMPLIED WITH QRH PROCEDURES UP TO ENGINE SHUT DOWN. REMOVED AND REPLACED THE NR 2 ENGINE IAW 771-00-01 (LINE 12).
Part: NONE — INOPERATIVE (PAX CABIN) · airframe 35,401 hrs · 15,933 cycles
4 EMERGENCY LIGHTS OUT ON MID LEFT SIDE OF AIRPLANE / [01] R/R M1676 EMERGENCY EXIT BATT PACK IAW AMM 33-51-06. OPS CHECK GOOD.
Part: SLIDER — CRACKED (R/H HORIZ. STAB.) · airframe 34,860 hrs · 15,636 cycles
RIGHT UPPER HORIZONTAL STABILIZER TO BODY SLIDER IS CRACKED. / [01] REMOVED AND REPLACED BODY SLIDER PER AMM 51-31-31;[02] AMM 53-31-31
Part: SLIDER — CRACKED (L/H HORIZ. STAB.) · airframe 34,860 hrs · 15,636 cycles
LEFT UPPER HORIZONTAL STABILIZER TO BODY SLIDER IS CRACKED. / [01] R&R LEFT UPPER SLIDER PER AMM 53-31-31.
Part: BATTERY PACK — INOPERATIVE · airframe 33,836 hrs · 15,057 cycles
R/H EMERGENCY LIGHTS. 2 R/H EMERGENCY LIGHTS OUT ON R/H VALANCE / [01] REPLACED EMERGENCY LIGHT BATTERY PACK AND CHARGER OPS CHECKS GOOD PER MM 33-51-06;[02] VERIFIED REPLACEMENT OF BATTERY PACK PER AMM 33-51-06.
Part: TRANSITION PANEL — DAMAGED (AFT CARGO BAY) · airframe 33,836 hrs · 15,057 cycles
R/H AFT CARGO TRANSITION ANGLE (SHIELD) AT STA 767 - STA 792 DAMAGED. / [01] REMOVED R/H AFT CARGO TRANSITION ANGLE (SHIELD) AT STA 767 - STA 792 .;[02] LOCATED AND DRILLED NEW PART PER SRM 51-40-05.;[03] INSP C/W FOR NEW PART DRILLING.;[04] REMOVED AND REPLACED R/H AFT CARGO TRANSITION ANGLE (SHIELD) AT STA 767 - STA 792 PER SRM 51-40-02;[05] REMOVED AND REPLACED R/H AFT CARGO TRANSITION ANGLE (SHIELD) AT STA 767 - STA 792 PER SRM 51-40-02. INSPECTION C/W.;[06] PARTS UPDATE ONLY;[07] FAULT IS COMPLETE
Part: BEAM — BROKEN (RH WING) · airframe 33,836 hrs · 15,057 cycles
RIGHT WING TRAILING EDGE BEAM ASSY. PN: 115A3758-34 IS BROKEN. / [01] REMOVED AND REPLACED PER SRM 51-40-02;[02] WORK ACCOMPLISHED PER SRM 51-40-02.NO DEFECT.;[03] FOUND PANEL NOT LINING UP WITH NEW BEAM ASSY. REMOVED AND REPLACED BEAM ASSY WITH A NEW BEAM ASSY PER SRM 51-40-02.;[04] FOUND PANEL NOT LINING UP WITH NEW BEAM ASSY. REMOVED AND REPLACED BEAM ASSY WITH A NEW BEAM ASSY PER SRM 51-40-02.;[05] REINSTALLED PANEL 661AB PER SOPM 20-50-01.;[06] VERIFIED CORRECTIVE ACTION STEP #5;[07] C/W INSPECTION. SEE INDIVIDUAL STEPS FOR WORK ACCOMPLISHED
Part: FLOOR PANEL — DELAMINATED (CABIN FLOOR) · airframe 33,836 hrs · 15,057 cycles
CABIN FLOOR PANEL 231DF IS DELAMINATED/DAMAGED AT APPX BL 0; JUST AFT OF STA 420. / [01] R&R FLOOR ACCESS PANEL PER AMM 53-21-00.;[02] PANEL NOT REPLACED YET;[03] CERTIFY STEP;[04] R&R FLOOR BOARD PNL# 231DF PER AMM 53-21-00.
Part: INTERCOSTAL — CRACKED · airframe 33,836 hrs · 15,057 cycles
CENTER SECTION STA. 540 LBL-0 TO LBL24.5 FLOOR BOARD NUT-PLATE CHANNEL CRACKED. / [01] REMOVED AND REPLACED INTERCOSTAL AT STA. 540 LBL-0 TO LBL24.5 PER SRM 51-40-02
Part: NONE — CRACKED (RH WING) · airframe 33,836 hrs · 15,057 cycles
RT WING FLAP DEFLECTION RIB PLATE CRACKED (MARKED) / [01] REMOVED DAMAGED DEFLECTION RIB TAB PER SRM 57-51-02-2R-3 REPAIR 3;[02] ACCOMPLISHED NDT ON DAMAGE REMOVAL. NO DEFECTS NOTED PER NDT MANUAL PART 6 CH51-00-00 PROCEDURE 23.;[03] TOOL UPDATE.;[04] ROTO PEENED PER SOPM 20-10-03 FIG 2-2;[05] INSPECTED AREA FOR ROTO PEEN;[06] LOCATED AND DRILLED UP REPAIR TEE AND RADIUS FILLER PER SRM 57-51-02-2R-3. PARTS OK TO INSTALL.;[07] VERIFIED LOCATION AND DRILLED PART IS C/W;[08] INSTALLED REPAIR TEE AND RADIUS FILLER PER SRM 57-51-02-2R-3.;[09] VERIFIED RADIUS FILLER AND TEE INSTALLED PER 57-51-02-2R-3.;[10] PARTS UPDATE ONLY;[11] PARTS UPDATE ONLY;[12] REPAIRED RT WING FIXED TRAILING EDGE DEFLECTION CONTROL RIB UPPER TAB (PLATE) IAW SRM 57-51-02-2R-3;[13] RII-INSPECTED WORK ACCOMPLISHED IN CORRECTIVE ACTION #12. JAMES KNOTTS (TECHNICIAN); 25-MAR-2022 00:50 UTC REPAIRED RT WING FIXED TRAILING EDGE DEFLECTION CONTROL RIB UPPER TAB (PLATE) IAW SRM 57-51-02-2R-3;[14] CLEARANCE CHECK GOOD. SEE ATTACHED SIGN OFFS FOR ALL WORK PERFORMED.;[15] C/W INSPECTION. SEE INDIVIDUAL STEPS FOR WORK ACCOMPLISHED
Part: SUPPORT BRACKET — BROKEN · airframe 33,836 hrs · 15,057 cycles
ABOVE THE LEFT HAND MAIN GEAR AFT TRUNNION; THE SUPPORT BRACKET FOR THE WIRE HARNESS GUIDE THROUGH ASSEMBLY IS BROKEN. PICTURES ATTACHED / [01] R&R SUPPORT BRACKET IAW SRM 51-40-02;[02] C/W BRACKET REMOVAL AND INSTALLATION.;[03] R&R SUPPORT BRACKET IAW SRM 51-40-02
Part: BALANCE WEIGHT — CORRODED (LH WING) · airframe 33,836 hrs · 15,057 cycles
ON THE LEFT WING LEADING EDGE OTBD END; THE BALLAST WEIGHTS HAVE EVIDENCE OF CORROSION. / [01] COMPLIED WITH EA M-22-157-00365.;[02] C/W EA M -22-157-00365
Part: PANEL — PULLED (LH WING) · airframe 33,836 hrs · 15,057 cycles
LT WING PANEL 543EB HAS SEVERAL PULLED THROUGH FASTENERS. / [01] REMOVED OLD TAIL CONE AND PICKED UP HOLES IN NEW TAIL CONE 543EB PER SRM 51-40-02-0G-0.;[02] VERIFIED;[03] INSTALLED AFT TAIL CONE FAIRING ONTO CANOE PER AMM 27-51-28-400-802.;[04] C/W INSPECTION
Part: LIGHT — INOPERATIVE · airframe 33,836 hrs · 15,057 cycles
CEILING LIGHT AT ROW 10DEF HAS SEGMENT OUT. / [01] R&R'D CEILING LIGHT AT ROW 10DEF; OP CK GOOD IAW AMM 33-22-00.
Part: PANEL — CRACKED (LH WING) · airframe 33,836 hrs · 15,057 cycles
LEFT WING PANEL 561BB HAS CRACKS AROUND NUMEROUS FASTENER HOLES. / [01] REPAIRED FASTENER HOLES PER SRM 51-70-04 REPAIR #9.;[02] VERIFIED REPAIR;[03] REPAIRED PER SRM 51-70-04 REPAIR #9. RESTORED FINISH PER M/M 51-21-99 AND M/M 51-21-81.;[04] INSPECTED WORK PERFORMED IN C/A #3
Part: LIGHT — INOPERATIVE · airframe 33,836 hrs · 15,057 cycles
CROSS-BIN LIGHT AT ROW 8ABC HAS SEGMENT OUT. / [01] R&R'D CROSS BIN LIGHT AT ROW 8ABC; OP CK GOOD IAW AMM 33-22-00.;[02] INSPECTED CROSS BIN LIGHT AT ROW 8ABC; OP CK GOOD
Part: PANEL — CRACKED (LH WING) · airframe 33,836 hrs · 15,057 cycles
LEFT WING PANEL 561AB HAS CRACKS AROUND NUMEROUS FASTENER HOLES. / [01] REPAIRED PER SRM 51-70-04 REPAIR #9.;[02] INSPECTED WORK PERFORMED IN CORRECTIVE ACTION #1. NICHOLAS DEBUS (TECHNICIAN); 11-MAR-2022 20:41 UTC REPAIRED PER SRM 51-70-04 REPAIR #9.;[03] REPAIRED FASTENER HOLES PER SRM 51-70-04 REPAIR#9.;[04] INSPECTED THE REPAIRED FASTENER HOLES PER SRM 51-70-04 REPAIR#9.NO DEFECT.
Part: PANEL — CRACKED (LH WING) · airframe 33,836 hrs · 15,057 cycles
LEFT WING PANEL 561CB HAS CRACKS AROUND NUMEROUS FASTENER HOLES. / [01] REPAIRED PER SRM 51-70-04 REPAIR #9.;[02] INSPECTED WORK PERFORMED IN CORRECTIVE ACTION #1. NICHOLAS (TECHNICIAN); 11-MAR-2022 20:36 UTC REPAIRED PER SRM 51-70-04 REPAIR #9.;[03] INSPECTED STEP 1 & 2;[04] CERTIFY STEPS
Part: LIGHT — INCORRECT · airframe 33,836 hrs · 15,057 cycles
CROSS-BIN LIGHT AT ROW 14ABC HAS SEGMENTS OUT / [01] CROSS BIN LIGHT NOT FOUND AT ROW 14ABC ONLY WIRING BETWEEN SEGMENTS IAW AIPC 33-21-51-74.;[02] INADVERTENTLY CROSS REFERENCED CROSS-BIN LIGHT WITH SIDEWALL LIGHT AT SAME POSITION WHICH DID NOT EXIST PER THE AIPC 33-21-51-74.;[03] CERTIFYING THE INITIAL INCORRECT WORK PERFORMED.;[04] R&R'D CROSS BIN LIGHT AT ROW 14ABC IAW AMM 33-22-00.;[05] INSPECTED INSTALL REQUIRES OPS CHECK;[06] PERFORMED OPS CHECK PER AMM 33-22-00. OPS CHECK GOOD.
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 33,589 hrs · 14,916 cycles
EMERGENCY LIGHTS AT SEATS 6; 10; AND 14DEF INOP ; / [01] R AND R?D EMERGENCY LIGHTS BATTERY PACK FOR SEATS 6;10;AND14DEF. IAW AMM 33-51-06
2021
Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 14,239 hrs · 32,297 cycles
L1 DOOR EMERGENCY SLIDE PULLED OUT / REPACKED L1 EMERGENCY SLIDE IAW AMM 25-66-01-400-804.
Part: BULKHEAD WEB — CRACKED (BS 663)
RIGHT WHEEL WELL VAPOR BARRIER CRACKED AT BS 663.75 RBL32 DAMAGE MEASURES 6' LONG AND IS LOCATED 6' UP FROM BOTTOM SURFACE.REFERNCE SA-M 943T # 010683. PERFORMED INTERIM REPAIR PER SRM 57-10-10-1A-2 & EA: REPAIR-57EA-05646REPETITIVE ACTION REQUIRED: DO A DETAILED VISUAL INSPECTION OF THE REPAIR AREA AT 1200 FLIGHT CYCLES INTERVALS OR MORE FREQUENTLY. MAKE SURE THE CRACK HAS NOT GROWN PAST THE INTERIM SEAL. REFER TO SRM 57-10-10-1A-2 IF CRACK HAS GROWN /
Part: SCUFF PLATE — CRACKED (FWD CARGO)
FWD CARGO CENTER SCUFF PLATE HAS A DENT WITH A CRACK IN IT. / REMOVED AND REPLACED FWD CARGO CENTER SCUFF PLATE REF AMM 53-11-02.
Part: TRUNNION — CORRODED (RT MLG)
RT. MLG FWD TRUNNION SUPPORT FITTING; LOWER OB LUG (#3) OUTER FACE HAS EVIDENCE OF CORROSION. / REPAIRED PER EA NO: 1-A57-3246 REV 12
2020
Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 29,041 hrs · 12,492 cycles
RIGHT HORIZONTAL STABILIZER UPPER FORWARD SLIDING SEAL CRACKED / REMOVED AND REPLACED RIGHT HOIZONTAL STABILIZER UPPER FORWARD SLIDNG SEAL PER AMM 53-31-31INSP 50310
Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 29,041 hrs · 12,492 cycles
LEFT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL CRACKED / REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL PER AMM 53-31-31INSP 50310
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,376 hrs · 11,707 cycles
EMERGENCY LIGHT BETWEEN L/H OVER WING DOORS INOPERATIVE. / R&R BATTERY PACK IAW AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,376 hrs · 11,707 cycles
EMERGENCY LIGHT BETWEEN R/H OVER WING DOORS INSIDE CABIN INOPERATIVE AT BS. 616. / R&R LIGHT ASSEMBLY IAW AMM.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,376 hrs · 11,707 cycles
EMERGENCY LIGHT BETWEEN L/H OVER WING DOORS INOPERATIVE. / RELAMPED BULB IAW AMM.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,376 hrs · 11,707 cycles
EMERGENCY LIGHT BATTERY PACKS M2335 INOPERATIVE. / R&R BATTERY PACK IAW AMM.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,376 hrs · 11,707 cycles
EMERGENCY LIGHT BATTERY PACKS M1675 INOPERATIVE. / R&R BATTERY PACK IAW AMM.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,376 hrs · 11,707 cycles
EMERGENCY LIGHT BATTERY PACKS M2816 INOPERATIVE. / R&R BATTERY PACK IAW AMM.
Part: BAFFLE — CRACKED (BS 500D-500E) · airframe 27,833 hrs · 11,911 cycles
FWD CARGO COMPARTMENT R/H SIDE BAFFLE AT STA 500D-500E RBL21 WL155 IS CRACKED / REMOVED OLD BAFFLE AT FWD COMPARTMENT R/H SIDE AT STA 500D-500E RBL 21 WL 155 IAW SRM 51-40-02-0G-0. LOCATED; DRILLED AND INSTALLED NEW BAFFLE ITEM 143A7510-22 P.O.# 782373 IAW SRM 51-40-05-0G-0. SRM 51-40-02-0G-0 AND DWG 143A7505 REV.- 0092058U 02/18/20
Part: BAFFLE — CRACKED (BS 500B-500C) · airframe 27,833 hrs · 11,911 cycles
FWD CARGO COMPARTMENT R/H SIDE BAFFLE AT STA 500B-500C RBL21 WL155 IS CRACKED / REMOVED OLD BAFFLE AT FWD CARGO COMPARTMENT R/H AT STA 500B-500C RBL 21 WL 155 IAW SRM 51-40-02-0G-0. LOCATED; DRILLED; AND INSTALLED NEW BAFFLE ITEM 143A7510-22 P.O.# 782373 IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 143A7505 REV.- 0092058U 02/18/20
Part: GUSSET — CRACKED (BS 500I S19R) · airframe 27,833 hrs · 11,911 cycles
GUSSET AT STRT 19 BS 500I WL 155 CRACKED / REMOVED AND REPLACED GUSSET AT STA 500I; WL 155; STR 19; P/N 143A9481-5; IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A7902 59326U 2/17/20
Part: SKIN — DEBONDED (LT WING TE FLAP) · airframe 27,833 hrs · 11,911 cycles
*CUSTOMER REQUEST* LT WING OTBD AFT FLAP DISBOND AT INBD AFT EDGE LOWER SKIN / REPAIRED DISBONDED EDGE ON L/H WING O/B AFT FLAP AT I/B AFT LOWER SKIN IAW 737 SRM 51-70-10-2R-0 AND SRM 57-53-01-2R-14. DISBOND WAS FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-53-01-1A-5 PARA 4
Part: FLOOR SUPPORT — CRACKED (BS 276-294) · airframe 27,833 hrs · 11,911 cycles
FLOOR SUPPORT CRACKED AT STA278; BL0; WL207 / REMOVED AND REPLACED FLOOR SUPPORT (INTERCOSTAL) ON MAIN CABIN FLOOR STRUCTURE FROM STA 276 TO STA 294.5 BL 0 WL 207 I.A.W SRM 51-40-02-0G-0 AND DWG 141A5400; 59600U 02-11-20
Part: FLOOR SUPPORT — CRACKED (BS 276-295) · airframe 27,376 hrs · 11,707 cycles
FLOOR SUPPORT CRACKED BETWEEN BS. 276 TO BS. 294.5, BL 0. / R&R FLOOR SUPPORT (INTERCOSTAL) IAW SRM AND DWG.
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,833 hrs · 11,911 cycles
CABIN FLOOR PANEL 221GF HAS DAMAGE TO LOWER SURFACE. REPAIRED DAMAGE TO LOWER SURFACE ON CABIN FLOOR PANEL 221GF IAW SRM 53-00-50-2R-6. DAMAGE WAS BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1. DAMAGE WAS WITHIN 3.0' OF EDGE. 80733U 19FEB20
Part: CHANNEL — CORRODED (BS 500B-500I) · airframe 27,833 hrs · 11,911 cycles
***CORROSION*** ON CARGO FLOOR TO SIDEWALL SUPPORT AT STA 500B+12 - 500I; LBL22; WL155 / AFTER EVALUATION OF CORROSION DAMAGE FOUND TO BE OUT OF LIMITS DUE TO 100% MATERIAL LOSS FROM EDGES OF MULTIPLE FASTENER HOLES IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED FWD CARGO L/H ZEE CHANNEL FROM B.S. 500C-500I IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A7500
Part: SUPPORT — CORRODED (BS 500B-500I) · airframe 27,833 hrs · 11,911 cycles
***CORROSION*** ON CARGO FLOOR TO SIDEWALL SUPPORT AT STA 500B+8 - 500I; RBL22; WL155 / CORROSION ON CARGO FLOOR TO SIDEWALL AT BS 500B+8-500I RBL 22 WL 155 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED SIDEWALL SUPPORT PER SRM 53-00-53-2R-5; SRM 51-40-02 SRM 51-40-05 AND BOEING DRAWING 143A7501. SIDEWALL SUPPORT SPLICE LOCATED AT BS 500E-500F RBL 22 WL 155
Part: CREASE BEAM — CORRODED (BS 316-328) · airframe 27,833 hrs · 11,911 cycles
CORROSION ON FWD GALLEY DOOR I/B CREASE BEAM CORD (MOP SEAL) STA316+10 -328; RBL60; WL207 / CORROSION ON FWD GALLEY I/B CREASE BEAM @ STA. 316+10 -328; RBL 60; WL 207 MEASURED 6.0'L X 1.0'W X .011'D. FOUND OUT OF LIMITS PER SRM 53-10-15-1A-2. CORROSION REWORKED PER ER # 20-01685 REV IR AND EA # SWA EC/TC REPAIR-53EA-07822 REV IR
Part: SCUFF PLATE — BROKEN (FWD CARGO) · airframe 27,833 hrs · 11,911 cycles
FWD CARGO AFT SCUFF PLATE IS BROKEN AT CURVED AREA / RECEIVED FWD CARGO DOOR AFT SCUFF PLATE ITEM P/N 143A8331 P.O.# 746334
Part: SUPPORT — CORRODED (BS 500I) · airframe 27,833 hrs · 11,911 cycles
***CORROSION*** ON 500I BULKHEAD LOWER SUPPORT ('L' ANGLE)LBL20 - RBL20; WL155 / AFTER EVALUATION OF CORROSION DAMAGE FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM IAW SRM 51-10-02-0G-0. REMOVED AND REPLACED LOWER BULKHEAD SUPPORT AT B.S. 500I LBL 20 TO RBL 20 WL 155 IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A9401
Part: CREASE BEAM — CORRODED (BS 951-992) · airframe 27,833 hrs · 11,911 cycles
**CORROSION** ON AFT ENTRY DOOR INBOARD CREASE BEAM CORD; LOCATED BETWEEN STA. 951 AND STA. 992.8; LBL 50; AND WL 208.1. / REPAIRED INBOARD CREASE BEAM AT STA. 951-992.8 LBL 50 WL 208.1 IAW EA REPAIR-53EA-07829 REV 1 AND ER 20-01718 REV IR
Part: WEB — CORRODED (FWD CARGO) · airframe 27,833 hrs · 11,911 cycles
***CORROSION*** MULTIPLE AREAS OF CORROSION ON THE FWD CARGO SUB THRESHOLD WEB FROM STA 449 - 485 WL 156 AT THE FWD CARGO DOOR CUTOUT RBL 31 / FWD CARGO SUB THRESHOLD WEB @ STA 449-485 WL 156 FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15-1A-1. REMOVED AND REPLACED FWD CARGO DOOR LOWER SUB THRESHOLD WEB IAW SRM 51-40-02 AND DWG 143A8330 PO# 766674
Part: CREASE BEAM — CORRODED (BS 951-992) · airframe 27,833 hrs · 11,911 cycles
**CORROSION** ON AFT GALLEY DOOR INBOARD CREASE BEAM CORD; LOCTED BETWEEN STA. 951 AND STA. 992.8; RBL 50; AND WL 208.1 / AFT GALLEY DOOR LRW MAIN SILL R/H INNER CHORD AT BS 962-984 FOUND TO BE OUT OF LIMITS MORE THAN 3 FASTENERS IN A GROUP IAW SRM 53-70-15-1A-1. REPAIRED IAW ATS ER 20-01719 IR & SWA EA REPAIR-53EA-07833 REV 1
Part: ANGLE — CORRODED (BS 500I) · airframe 27,833 hrs · 11,911 cycles
***CORROSION*** ON 500I BULKHEAD RIGHT HAND SUPPORT ('L' ANGLE)RBL22; WL155 / REMOVED AND REPLACED R/H BULKHEAD SUPPORT 'L' ANGLE STA 500I; RBL 22; WL 155 P/N 143A9485-34; ITEM# 7530202 I.A.W SRM 51-40-01-0G-0 AND BOEING DWG 143A9481 12A 59326U 2/17/20
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 27,833 hrs · 11,911 cycles
CABIN FLOOR PANEL 221FF HAS DAMAGE TO LOWER SURFACE. REPAIRED DAMAGE TO LOWER SURFACE ON CABIN FLOOR PANEL 221FF IAW SRM 53-00-50-2R-1. DAMAGE WAS BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4B.(1) DAMAGE WAS GREATER THAN ONE PLY IN DEPTH. 80733U 18FEB2020
Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 27,833 hrs · 11,911 cycles
FLOOR PANEL 241E HAS UPPER SURFACE DAMAGE. REPAIRED FLOOR PANEL 241E IAW SRM 53-00-50-2R-0. DAMAGE DETERMINED TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1; PARA 4B(1). A MAXIMUM OF ONE PLY IN DEPTH. 57795U 19FEB2020
Part: WEB — CORRODED (BS 794-847) · airframe 27,833 hrs · 11,911 cycles
**CORROSION**AT AFT CARGO DOOR SUB THRESHOLD WEB BETWEEN STA. 794.37 AND 847.00 @ WL 159; RBL 25. / CORROSION ON AFT CARGO DOOR SUB THRESHOLD WEB BETWEEN STA 794.37 AND 847 WL 159 RBL 25 WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1. REMOVED OLD WEB IAW SRM 51-40-02-0G-0. LOCATED. DRILLED. COUNTERSUNK AND INSTALLED WEB ITEM 7531818 P.O. # 782301 IAW SRM 51-40-05-0G-0. SRM 51-40-08-0G-0; SRM 51-40-02-0G-0 AND DWG 146A8120. 92058U 02/17/20
Part: BRACKET — CRACKED (BS 867) · airframe 27,833 hrs · 11,911 cycles
CRACKED BRACKET IN AFT CARGO COMPARTMENT LOCATED AT STA. 867; LBL 13; WL 143 . / REMOVED AND REPLACED CRACKET BS 867 LBL 13 WL 143 WITH REPLACEMENT P.O# 743769 IAW SRM 51-40-02-0G-0 DRG# 149A8102. 57309U 2/16/20
Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 27,833 hrs · 11,911 cycles
AFT CARGO DOOR AFT CORNER SCUFF PLATE HAS A CRACK ON FWD SIDE / RECEIVED AFT CARGO DOOR AFT CORNER SCUFF PLATE ITEM 7530659 P.O.# 778503. 92058U 02/17/20
Part: SCUFF PLATE — BROKEN (AFT CARGO) · airframe 27,833 hrs · 11,911 cycles
AFT CARGO DOOR FWD CORNER SCUFF PLATE IS BROKEN / RECEIVED AFT CARGO DOOR FORWARD SCUFF PLATE ITEM 7530220 P.O.# 771944. 92058U 02/17/20
Part: WEB — CORRODED (BS 794-847) · airframe 27,376 hrs · 11,707 cycles
AFT CARGO DOOR SUB THRESHOLD WEB CORRODED BETWEEN BS. 794.37 TO BS. 847, RBL 25. / R&R WEB IAW SRM AND DWG.
Part: WEB — CORRODED (THRESHOLD) · airframe 27,376 hrs · 11,707 cycles
FORWARD CARGO SUB THRESHOLD WEB CORRODED BETWEEN BS. 449 TO BS. 485, RBL 31. / R&R WEB IAW SRM AND DWG.
Part: CHANNEL — CORRODED (BS 500B-500I) · airframe 27,376 hrs · 11,707 cycles
CARGO FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 500B+12 TO BS. 500I, LBL 22. / R&R ZEE CHANNEL IAW SRM AND DWG.
Part: CREASE BEAM — CORRODED (BS 951-992) · airframe 27,376 hrs · 11,707 cycles
AFT ENTRY DOOR INBOARD CREASE BEAM CHORD CORRODED BETWEEN BS. 951 TO BS. 992.8, LBL 50. / REPAIRED INBOARD CREASE BEAM IAW EA AND ER.
Part: CREASE BEAM — CORRODED (BS 316-328) · airframe 27,376 hrs · 11,707 cycles
FORWARD GALLEY DOOR INBOARD CREASE BEAM CHORD (MOP SEAL) CORRODED BETWEEN BS. 316+10 TO BS. 328, RBL 60. / REPAIRED CREASE BEAM PER ER.
Part: BULKHEAD WEB — DAMAGED (BS 663) · airframe 27,376 hrs · 11,707 cycles
VAPOR BARRIER HAD TEMPORARY REPAIR THAT WAS PEELING AT APPROXIMATELY BS. 663, RBL 30. / REPAIRED VAPOR BARRIER PER SRM.
Part: SUPPORT ANGLE — CORRODED (BS 500I) · airframe 27,376 hrs · 11,707 cycles
BULKHEAD RIGHT HAND SUPPORT "L" ANGLE CORRODED AT BS. 500I, RBL 22. / R&R R/H BULKHEAD SUPPORT "L" IAW SRM AND DWG.
Part: GUSSET — CRACKED (BS 500I) · airframe 27,376 hrs · 11,707 cycles
GUSSET CRACKED AT BS. 500I, STR 19. / R&R GUSSET IAW SRM AND DWG.
Part: SUPPORT — CORRODED (BS 500B-500I) · airframe 27,376 hrs · 11,707 cycles
CARGO FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 500B+8 TO BS. 500I, RBL 22. / R&R SIDEWALL SUPPORT PER SRM AND DWG.
Part: CREASE BEAM — CORRODED (BS 951-992) · airframe 27,376 hrs · 11,707 cycles
AFT GALLEY DOOR INBOARD CREASE BEAM CHORD CORRODED BETWEEN BS. 951 TO BS. 992.8, RBL 50. / REPAIRED CHORD IAW SRM AND ER.
2019
Part: INTERCOSTAL — CRACKED (FWD CARGO BAY) · airframe 27,062 hrs · 11,569 cycles
RT ECNTER INTERCOSTAL FLOOR SUPPORT CRACKED ABOVE FWD CARGO AIR CONDITIONING BAY AT STA. 540 / REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02 AND SRM 51-10-02AMT 56504
Part: SIGN — LOOSE (CABIN) · airframe 25,739 hrs · 10,962 cycles
CEILING MOUNT OVERWING EXIT SIGN LOOSE. R&R LIGHT ASSEMBLY PER AMM.
2018
Part: SIGN — LOOSE (CABIN) · airframe 23,066 hrs · 9,784 cycles
MID CABIN CEILING EXIT SIGN LOOSE. SECURED SIGN PER SIP.
Part: VAPOR BARRIER — CRACKED (WHEEL WELL RH) · airframe 22,904 hrs · 9,708 cycles
RIGHT WHEEL WELL VAPOR BARRIER CRACKED AT BS 663.75 RBL32 DAMAGE MEASURES 6' LONG AND IS LOCATED 6' UP FROM BOTTOM SURFACE. / REF SA-M 943T # V010683. PERFORMED INTERIM REPAIR PER SRM 57-10-10-1A-2 & EA: REPAIR-57EA-05646
Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 22,781 hrs · 9,654 cycles
L2 DOOR EVAC SLIDE OUT OF ADJUST. REPOSITIONED SLIDE ASSY PER MM.
Part: TRANSMITTER — FAULTY (HYDRAULIC SYS) · airframe 22,426 hrs · 9,511 cycles
A HYDRAULIC QUANTITY DROPPED TO 73% AND INTO FLIGHT 1:30 A SYSTEM QUANTITY SHOWED 86% AND WHEN GEAR DOWN A QUANTITY SHOWED 94%. R&R A SYSTEM QUANTITY TRANSMITTER IAW AMM.
Part: FLOORBOARD — PULLED (FUSELAGE) · airframe 21,209 hrs · 9,001 cycles
PAX CABIN FLOOR BOARD 241AF; UPPER SURFACE MIDSECTION FWD TO AFT; MULTIPLE AREAS OF FIBERGLASS THREAD PULLED OUT. / FABRICATED PAX CABIN FLOOR BOARD 241AF IAW B737-800 SRM 53-00-50-2R-0 REV 61 TABLE 204; DWG 144A5810-127 REV- AND BAC 5085 SECTION 8;4;2.1 AND 8.4.2.2. REV E. A17483 A86613 A86111
Part: FLOOR PANEL — PULLED (MAIN CABIN) · airframe 21,209 hrs · 9,001 cycles
PAX CABIN FLOOR BOARD 232SF; UPPER SURFACE OTBD EDGE ADJACENT AND BELOW RH AFT OVERWING EXIT; FIBERGLASS THREADS PULLED OUT. / REPAIRED PAX CABIN FLOORBOARD 2325F OF TOP PLY DAMAGE ONLY IAW B737-800 SRM 53-00-50-2R-1 REV 61 AND B737-800 SRM 53-00-50-2R-0 REPAIR GENERAL REV 61. A51273; A26386
Part: ANGLE — CORRODED (BS 727H-797) · airframe 20,634 hrs · 8,728 cycles
AFT CARGO BAY ZEE ANGLE CORRODED BETWEEN BS 797 TO 727H, LBL 22. R & R THE ANGLE IAW SRM.
Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 21,209 hrs · 9,001 cycles
AFT CARGO COMPARTMENT STA 797-727H LBL 22; Z ANGLE IS CORRODED. / REMOVED CORROSION BY BLENDING VERIFIED W/ 10X. MAX LOSS FOUND TO BE .006' ORIG 'T' .040' REMAINING .034'. FOUND TO BE 'OUT OF LIMITS' IAW SRM 53-00-53-1A-2 TOOL # 36649 CAL DUE 7/5/18 REMOVED AFT CARGO ZEE ANGLE LBL 22 @ STA. 727H - 797. VERIFIED MATERIAL TO BE P/N BAC1496-377 7075 T6. FABRICATED REPAIR PARTS; TREATED + PRIMED FABRICATED PARTS. ASSEMBLED NEW ZEE ANGLE & REPAIR SPLICES. INSTALLED NEW SECTION OF ZEE + REPAIR SPLICES IAW SRM 53-00-53-2R-5; APPLIED CIC IAW AMM 51-00-59-201
Part: ANGLE — CORRODED (BS 500F-500G) · airframe 20,634 hrs · 8,728 cycles
FORWARD CARGO BAY LEFT ZEE ANGLE CORRODED BETWEEN BS 500F TO 500G. R & R THE ANGLE IAW SRM.
Part: ANGLE — CORRODED (FWD CARGO BAY) · airframe 21,209 hrs · 9,001 cycles
FORWARD CARGO PIT; LEFT 'Z' ANGEL; HAS CORROSION FROM STA 500F TO 500G [MARKED] / FWD CARGO PIT LEFT 'Z' ANGEL HAS CORROSION FROM STA 500F-500G BLENDED CORROSION AND FOUND ORIG T TO BE .040' REMAINING .032' REMOVED .008' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 REMOVED AND REPLACED 'Z' ANGLE FROM STA 500C-500I IAW SRM 53-00-53-2R-5 REPAIR 5
Part: SKIN — DELAMINATED (LT WING) · airframe 21,209 hrs · 9,001 cycles
LH OUTBD FLAP INBD CORNER LOWER SURFACE DELAMED. (MARKDED) / REPAIRED DELAMINATION ON L/H OUTBD FLAP INBD CORNER LOWER SURFACE PER B 737 SRM 51-70-10-2R-0
Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 20,950 hrs · 8,877 cycles
LEFT EMERGENCY LIGHT LENS FAILED. SECURED THE LENS IAW SIP.
2017
Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 19,697 hrs · 8,301 cycles
RH HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED / REMOVED & REPLACED R/H STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31
Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 19,697 hrs · 8,301 cycles
LH HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED / REMOVED AND REPLACED L/H FWD UPPER STAB SLIDING SEAL PER AMM 53-31-31
Part: LAMP — INOPERATIVE (EXTERIOR) · airframe 19,299 hrs · 8,119 cycles
L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.
Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 18,474 hrs · 7,767 cycles
L2 DOOR SLIDE OUT OF ADJUST. SECURED THE SLIDE ASSY IAW MM.
Part: COVER — DAMAGED (L2 DOOR SLIDE) · airframe 18,040 hrs · 7,589 cycles
L2 DOOR SLIDE COVER DAMAGED. R & R THE COVER IAW MT.
Part: COVER — DAMAGED (L2 DOOR SLIDE) · airframe 18,187 hrs · 7,647 cycles
L2 DOOR SLIDE COMPARTMENT DAMAGED. R & R THE COVER IAW MM.
Part: HOLDER — BROKEN (L2 DOOR GIRT BAR) · airframe 18,187 hrs · 7,647 cycles
L2 DOOR SLIDE GIRT BAR HOLDER BROKEN. R&R HOLDER IAW MT.
Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 178,180 hrs · 7,494 cycles
EMERGENCY LIGHT MISSING PROTECTIVE COVERING BETWEEN ROWS 2 TO 12. INSTALLED STRIP IAW AMM.
2016
Part: FLASHLIGHT — NOT SEATED (AFT CABIN) · airframe 16,952 hrs · 7,130 cycles
AFT F/A'S EMERGENCY FLASHLIGHT WILL NOT TEST. RESEATED FLASHLIGHT IN THE MOUNT. OPS CHECKED GOOD IAW MM.
Part: BATTERY PACK — FAILED (CABIN) · airframe 15,783 hrs · 6,594 cycles
EMERGENCY LIGHTS BATTERY PACK FAILED CAPACITY CHECK AT M1672. R&R BATTERY PACK PER DWG.
Part: BATTERY PACK — FAILED (CABIN) · airframe 15,783 hrs · 6,594 cycles
EMERGENCY LIGHTS BATTERY PACK FAILED CAPACITY CHECK AT M1675. R&R BATTERY PACK PER DWG.
Part: BATTERY PACK — FAILED (CABIN) · airframe 15,783 hrs · 6,594 cycles
EMERGENCY LIGHTS BATTERY PACK FAILED CAPACITY CHECK AT M1670. R&R BATTERY PACK PER DWG.
Part: ANGLE — CRACKED (RT WING) · airframe 15,783 hrs · 6,594 cycles
RT WING TRAILING EDGE UPPER FIXED PANEL WEB ANGLE CRACKED. R&R ANGLE PER SRM.
Part: LIGHT — BROKEN (CABIN) · airframe 14,768 hrs · 6,172 cycles
EMERGENCY LIGHT BROKEN AT ROW 25 DEF. R & R LENS IAW MM.
Part: LENS — BROKEN (CABIN) · airframe 14,628 hrs · 6,113 cycles
EMERGENCY EXIT LIGHT LENS COVER BROKEN, BETWEEN ROW 5 - 27. R & R LENS IAW MM.
2014
Part: LENS — MISSING (CABIN) · airframe 9,387 hrs · 3,850 cycles
RIGHT EMER LIGHT CLEAR LENS COVER MISSING AT ROW 10. INSTALLED COVER IAW MM.
2013
Part: SLIDE — UNSECURE (R2 DOOR) · airframe 5,447 hrs · 2,122 cycles
R2 DOOR EMERGENCY EVAC SLIDE ATTACHMENT LOOSE. SECURED SLIDE IAW SIP.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,624 hrs · 1,799 cycles
FWD ENTRY EMERGENCY EXIT LIGHT INOPERATIVE. R & R LIGHT IAW MM.
Part: FAN — FAILED (AC BAY) · airframe 4,990 hrs · 1,946 cycles
AIR TURN BACK SMOKE & FUMES PLASTIC BURNING SMELL ON CLIMB OUT. FOUND RT RECIRC FAN FAILED. R & R RT RECIRC FAN IAW MM.
Part: SIGN — LOOSE (CABIN) · airframe 3,414 hrs · 1,330 cycles
OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER M/M.
Part: LENS — LOOSE (CABIN) · airframe 3,175 hrs · 1,227 cycles
MID CABIN EMERGENCY EXIT SIGN LIGHT LENS LOOSE. SECURED LENS IAW M/M.
2012
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 9 hrs · 8 cycles
FORWARD O/B FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.