N5209A
Registered owner: BANK OF UTAH TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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.
43 reports on file, 2023-02-24 – 2026-07-27.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 64,688 hrs · 41,070 cycles
RT SIDE OF AIRCRAFT EMERGENCY EXIT LIGHTS NOT WORKING DURING TEST. R & R RT SIDE EMERGENCY EXIT LIGHT BATTERY PACK REF AMM 33-51-06 OPS CHECK GOOD.
Part: SLIDE — DETACHED (ZONE 800) · airframe 63,863 hrs · 40,676 cycles
R1 DOOR SECAPE SLIDE DETACHED FROM COVER. ESCAPE SLIDE PACK INSTALLED IAW AMM 25-66-01 GOOD FOR SERVICE.
Part: WINDOW — LOOSE (SLIDE) · airframe 63,704 hrs · 40,595 cycles
L1 DOOR ESCAPE SLIDE VIEWING WINDOW LOOSE. SECURED L1 DOOR SLIDE VEIWING WINDOW REF SRM 51-30-10
Part: VIEW PORT — MISSING (ZONE 800 SLIDE) · airframe 63,457 hrs · 40,480 cycles
L1 DOOR SLIDE VIEWING WINDOW MISSING. OPEN
Earlier reports · 2023–2025 · 39 reports
2025
Part: VIEW PORT — MISSING (L1 DOOR SLIDE) · airframe 63,285 hrs · 40,397 cycles
L1 DOOR SLIDE VIEWING WINDOW MISSING. INSTALLED L1 DOOR SLIDE VIEWING WINDOW IAW AMM 25-52-01.
Part: SLIDE — NOT REPORTED (ZONE 800) · airframe 62,264 hrs · 39,875 cycles
R1 DOOR SLIDE UNUSABLE . R&R R1 SIDE IAW AMM 25-66-01 OK FOR SERVICE.
Part: SLIDE — DISLODGED (ZONE 800) · airframe 62,168 hrs · 39,829 cycles
UPON OPENING L-1 DOOR EMERGENCY ESCAPE SLIDE FELL OUT OF BUSTLE CONTAINER - RESOLUTION: INSTALLED NEW L1 DOOR SLIDE IAW AMM 25-66-01 OKAY FOR SERVICE THIS CLEARS MEL 52-16-1 MS=DDR# 131821
Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 62,111 hrs · 39,800 cycles
LEFT SIDE EMERGENCY LIGHT AND EXIT SIGN INOP. R&R LH SIDE EMERGENCY BATTERY PACK ASSY IAW AMM 33-51-06 OPERATIONAL CHECK GOOD.
Part: GIRT BAR — OUT OF ALIGNMENT (ZONE 800) · airframe 62,072 hrs · 39,779 cycles
R-1 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR NOT ALLIGNED WITH FLOOR GIRT BAR PAWLS. MARKED 09-45. (IN PROGRESS)
Part: BUSHING — WORN (ZONE 300) · airframe 62,072 hrs · 39,779 cycles
RIGHT HAND HORIZONTAL STABILIZER, THE FORWARD LOWER MOUNT BUSHINGS PLATING IS WORN. (120-109) - SUBMIT TO ENG, REMOVED FORWARD LOWER MOUNT BUSHINGS AT RIGHT HAND HORIZONTAL STABILIZER IAW BOEING SERVICE BULLETIN 737-55-1074 FIG. 4 PAGE 1 TO 3. REV. 2. DATE JULY 21/2017 PART 3. PERMANENT REPAIR STEP 5. INSPECTED THE JOINT, IAW EAR #08 RESPONSE STEP #2, PER SB 737-55-1074 REV 2: JULY 21, 2017. PART 3 - PERMANENT REPAIR, STEP 6. CORROSION NOTED. ACCOMPLISHED FILLING THE REPORT FORM FOR AFFECTED JOINT AS PER 737-NG-FTD-55-13002, JOINT DIMENSION REPORT IAW EAR #08 RESPONSE STEP 2. PERFORMED DAMAGE REMOVAL OF CORROSION IN THE BARE AREA AT RHS HOR. STAB. FRONT. SPAR LOWER LUG (BORE) UP TO NOMINAL SIZE DIAM: 1.326" IAW EAR #8 DATED 02/26/25 ENG RESPONSE STEP 6, 8 AND SB 737-55-1074 FIG 5.
Part: BUSHING — WORN (ZONE 300) · airframe 62,072 hrs · 39,779 cycles
LEFT HAND HORIZONTAL STABILIZER, THE AFT LOWER BUSHING HAS PLATING WORN. (120-112) - REMOVE AND REPLACE BUSHINGS, REMOVED AFT (REAR) LWR BUSHING AT LH HORIZONTAL STABILIZER IAW EAR #09 STEP 1. PER SB 737-55-1074 REV 2 JULY 21, 2017. FIGURE 7, SHEET 1 THRU 3. PERMANENT REPAIR PART 3, STEP 8. INSPECTED THE JOINT, IAW EAR #09 RESPONSE STEP 2, PER SB 737-55-1074 REV 2: JULY 21, 2017. PERMANENT REPAIR PART 3, STEP 11. CORROSION NOTED. ACCOMPLISHED FILLING THE REPORT FORM FOR AFFECTED JOINT AS PER 737-NG-FTD-55-13002, JOINT DIMENSION REPORT IAW EAR #09 RESPONSE STEP 2. PERFORMED DAMAGE REMOVAL OF CORROSION IN THE BORE AREA ONTO LH HOR. STAB. REAR SPAR LOWER LUG (BORE) UP TO NOMINAL SIZE DIAM: 1.951" IAW EAR ITEM #09 DATED: 02/06/25 ENG. RESPONSE STEP 6 THRU STEP 8 AND BOEING SB 737-55-1074 FIG. 10.
Part: LUG — GOUGED (ZONE 300) · airframe 62,072 hrs · 39,779 cycles
AIRCRAFT TAIL SECTION, RIGHT HAND HORIZONTAL STABILIZER, THE FORWARD UPPER MOUNT LUG HAS A GOUGE ON THE UPPER FORWARD SURFACE. . REMOVED DAMAGE ON TO AIRCRAFT TAIL SECTION R/H HORIZONTAL STABALIZER THE FWD UPPER MOUNT LUG ON THE UPPER FWD SURFACE IAW B737-800 BCF REV.22. SRM 51-10-02. PERFORMED DVI ON REWORKED AREA ON TO AIRCRAFT TAIL SECTION RT HORIZONTAL STABALIZER, THE FWD UPPER MOUNT LUG ON THE UPPER FWD SURFACE, NO FURTHER CRACKS OR OTHER DAMAGE NOTED IAW SRM 51-10-04 REV. 22. REQUEST NDT, PERFORM A HFEC SURFACE INSPECTION OF THE REWORKED AREA ENSURE NO CRACKS EXIST. HFEC SURFACE INSP. PER B-737 NDTM PT.6, 51-00-00, PROC.23, IAW EAR #7003121083, STEP #3. NO DEFECTS NOTED AT RH HORIZ. STAB. FWD UPPER MOUNT UPPER FWD SIDE REWORKED AREA. RESTORED SURFACE FINISH ON REWORKED AREA LOCATED AT RH SIDE HORIZONTAL STAB. THE FWD UPPER MOUNT LUG UPPER FWD SURFACE
Part: BUSHING — WORN (ZONE 300) · airframe 62,072 hrs · 39,779 cycles
LEFT HAND HORIZONTAL STABILIZER, THE AFT LOWER BUSHING HAS PLATING WORN. (120-112) - RESOLUTION: REMOVE AND REPLACE BUSHINGS, REMOVED AFT (REAR) LWR BUSHING AT LH HORIZONTAL STABILIZER IAW EAR #09 STEP 1. PER SB 737-55-1074 REV 2 JULY 21, 2017. FIGURE 7, SHEET 1 THRU 3. PERMANENT REPAIR PART 3, STEP 8. INSPECTED THE JOINT, IAW EAR #09 RESPONSE STEP 2, PER SB 737-55-1074 REV 2: JULY 21, 2017. PERMANENT REPAIR PART 3, STEP 11. CORROSION NOTED. ACCOMPLISHED FILLING THE REPORT FORM FOR AFFECTED JOINT AS PER 737-NG-FTD-55-13002, JOINT DIMENSION REPORT IAW EAR #09 RESPONSE STEP 2. PERFORMED DAMAGE REMOVAL OF CORROSION IN THE BORE AREA ONTO LH HOR. STAB. REAR SPAR LOWER LUG (BORE) UP TO NOMINAL SIZE DIAM: 1.951" IAW EAR ITEM #09 DATED: 02/06/25 ENG. RESPONSE STEP 6 THRU STEP 8 AND BOEING SB 737-55-1074 FIG. 10.
Part: BUNGEE CYLINDER — WORN (ZONE 300) · airframe 62,072 hrs · 39,779 cycles
RIGHT HAND HORIZONTAL STABILIZER AFT MOUNT, THE AFT FORWARD BUSHING HAS PLATING WORN. REMOVED THE RH REAR UPPER FWD BUSHING, IAW EAR# 08 RESPONSE STEP 1, PER SB 737-55-1074 REV 2: JULY 21, 2017. PERNAMENT REPAIR - PART 3. INSPECTED THE JOINT, IAW EAR#08 RESPONSE STEP 2, PER SB 737-55-1074 REV 2: JULY 21, 2017. PART 3 - PERNAMENT REPAIR, STEP 17. CORROSION NOTED.
Part: BUSHING — WORN (ZONE 300) · airframe 62,072 hrs · 39,779 cycles
WOLEFT HAND HORIZONTAL STABILIZER, THE AFT UPPER BUSHING HAS PLATING WORN. (120-117) - RESOLUTION: REMOVE AND REPLACE BUSHINGS. REMOVED AFT UPPER MOUNT BUSHINGS AT RH HORIZONTAL STABILIZER IAW BOEING SERVICE BULLETIN 737-55-1074 FIG. 4 PG. 1 TO PG 3 REV 2 JULY 21, 2017. FIGURE 7, SHEET 1 THRU 3. PERMANENT REPAIR PART 3, STEP 5. INSPECTED THE JOINT, IAW EAR #08 RESPONSE STEP 2, PER SB 737-55-1074 REV 2: JULY 21, 2017. PERMANENT REPAIR PART 3, STEP 10. SCRATCHES NOTED. ACCOMPLISHED FILLING THE REPORT FORM FOR AFFECTED JOINT AS PER 737-NG-FTD-55-13002, JOINT DIMENSION REPORT IAW EAR #08 RESPONSE STEP 2. PERFORMED DAMAGE REMOVAL OF CORROSION IN THE BORE AREA ONTO RHS HOR. STABILIZER REAR SPAR UPPER LUG (BORE) UP TO NOMINAL SIZE DIAM: 1.951" IAW EAR ITEM #08 DATED: 01/28/25 ENG. RESPONSE STEP 6 THRU STEP 8 AND BOEING SB 737-55-1074 FIG. 9.
Part: BUSHING — WORN (ZONE 300) · airframe 62,072 hrs · 39,779 cycles
RIGHT HAND HORIZONTAL STABILIZER, THE FORWARD LOWER MOUNT BUSHINGS PLATING IS WORN. (120-109) - RESOLUTION: SUBMIT TO ENG, REMOVED FORWARD LOWER MOUNT BUSHINGS AT RIGHT HAND HORIZONTAL STABILIZER IAW BOEING SERVICE BULLETIN 737-55-1074 FIG. 4 PAGE 1 TO 3. REV. 2. DATE JULY 21/2017 PART 3. PERMANENT REPAIR STEP 5. INSPECTED THE JOINT, IAW EAR #08 RESPONSE STEP #2, PER SB 737-55-1074 REV 2: JULY 21, 2017. PART 3 - PERMANENT REPAIR, STEP 6. CORROSION NOTED. ACCOMPLISHED FILLING THE REPORT FORM FOR AFFECTED JOINT AS PER 737-NG-FTD-55-13002, JOINT DIMENSION REPORT IAW EAR #08 RESPONSE STEP 2. PERFORMED DAMAGE REMOVAL OF CORROSION IN THE BARE AREA AT RHS HOR. STAB. FRONT. SPAR LOWER LUG (BORE) UP TO NOMINAL SIZE DIAM: 1.326" IAW EAR #8 DATED 02/26/25 ENG RESPONSE STEP 6, 8 AND SB 737-55-1074 FIG 5.
Part: BUSHING — WORN (ZONE 300) · airframe 67,072 hrs · 39,779 cycles
B000294 OFF AIRCRAFT PART, LEFT HAND HORIZONTAL STABILIZER, THE AFT MID BUSHING HAS PLATING WORN. REMOVE AND REPLACE BUSHINGS. REMOVED AFT (REAR) MID BUSHING AT LH HORIZONTAL STABILIZER, IAW EAR#09 STEP 1. PER SB 737-55-1074 REV 2 JULY 21, 2017. FIGURE 2, SHEET 1 THRU 3. PERMANENT REPAIR PART 3, STEP 8. INSPECTED THE JOINT, IAW EAR#09 RESPONSE STEP 2, PER SB 737-55-1074 REV 2: JULY 21, 2017. PART 3 - PERMANENT REPAIR, STEP 9. CORROSION NOTED. ACCOMPLISHED FILLING THE REPORT FORM FOR AFFECTED JOINT AS PER 737-NG-FTD-55-13002, JOINT DIMENSION REPORT IAW EAR #09 RESPONCE STEP 2. PERFORMED DAMAGE REMOVAL OF CORROSION IN THE BORE AREA ONTO LHS HOR. STAB. REAR SPAR MID FAILSAFE LUG (BORE) UP TO NOMINAL SIZE DIAM: 1.951" IAW EAR ITEM #09 DATED: 02/06/25 ENG RESPONSE STEP 6 THRU STEP 8 AND BOEING SB 737-55-1074 FIG. 8.
Part: BUSHING — WORN (ZONE 300) · airframe 62,072 hrs · 39,779 cycles
LEFT HAND HORIZONTAL STABILIZER, THE FORWARD LOWER BUSHING HAS PLATING WORN. REMOVED FWD LOWER MOUNT BUSHINGS AT L/H HORIZONTAL STABILIZER. IAW SERVICE BULLETIN 737-55-1074 FIG.4 PG.1 TO PG.3 REV 2. INSPECTED THE JOINT, IAW EAR#09 RESPONSE STEP 2, PER SB 737-55-1074 REV 2 PART 3 - PERMANENT REPAIR STEP 6. CORROSION NOTED. ACCOMPLISHED FILLING THE REPORT FORM FOR THE AFFECTED JOINT AS PER 737-NG-FTD-55-13002, JOINT DIMENSION REPORT IAW EAR#09 RESPONCE STEP 2. PERFORMED DAMAGE REMOVAL OF THE CORROSION IN THE BORE AREA ONTO LHS HOR. STAB. FRONT SPAR LOWER LUG (BORE) UP TO NOMINAL SIZE DIAM: 1.326" IAW EAR ITEM #09 DATED: 02/06/25 ENG RESPONSE STEP 6 THRU STEP 8 AND BOEING SB 737-55-1074 FIG. 5.
Part: BUSHING — WORN (ZONE 300) · airframe 62,072 hrs · 39,779 cycles
RIGHT HAND HORIZONTAL STABILIZER, THE FORWARD UPPER MOUNT BUSHINGS PLATING IS WORN. REMOVED FORWARD UPPER MOUNT BUSHINGS AT RIGHT HAND HORIZONTAL STABILIZER IAW BOEING SERVICE BULLETIN 737-55-1074. FIG. 4 PAG.1 TO 3. REV. 2 DATE, JULY 21/2017, PART 3, PERMANENT REPAIR STEP 5. INSPECTED THE JOINT, IAW EAR #03 RESPONSE STEP 2, PER SB 737-55-1074 REV 2: PART 3, PERMANENT REPAIR STEP 6. CORROSION NOTED. ACCOMPLISHED FILLING THE REPORT FORM FOR AFFECTED JOINT AS PER 737-NG-FTD-55-13002, JOINT DIMENSION REPORT IAW EAR #08 RESPONSE STEP 2. PERFORMED DAMAGE REMOVAL OF THE CORROSION IN THE BARE AREA ONTO THE RHS HOR. STAB. FRONT SPAR UPPER LUG (BORE) UP TO NOMINAL SIZE DIAM: 1.326", IAW EAR ITEM #08 ENG RESPONSE STEP 6 & 8, PER BOEING SB 737-55-1074 FIG. 5.
Part: BUSHING — WORN (ZONE 300) · airframe 62,072 hrs · 39,779 cycles
LEFT HAND HORIZONTAL STABILIZER, THE FORWARD UPPER BUSHING HAS PLATING WORN. REMOVED FORWARD UPPER BUSHING AT LEFT HAND HORIZONTAL STABILIZER IAW BOEING SERVICE BULLETIN 737-55-1074 FIG.4 PAG. 1 TO 3 REV. 2 DATE JULY 21/2017 PART 3 PERMANENT REPAIR STEP 5. INSPECTED THE JOINT, IAW EAR#09 RESPONSE STEP 2, PER SB 737-55-1074 REV 2: JULY 21, 2017. PART 3 - PERMANENT REPAIR STEP 6. CORROSION NOTED. PERFORMED DAMAGE REMOVAL OF THE CORROSION IN THE BORE AREA ONTO LHS HOR. STAB. FRONT SPAR UPPER LUG (BORE) UP TO NOMINAL SIZE DIAM: 1.326" IAW EAR ITEM #09 DATED: 02/06/25 ENG. RESPONSE STEP 6 THRU STEP 8 AND BOEING SB 737-55-1074 FIG.5.
Part: BUSHING — WORN (ZONE 300) · airframe 62,072 hrs · 39,779 cycles
RIGHT HAND HORIZONTAL STABILIZER, THE AFT MID MOUNT BUSHINGS PLATING IS WORN. REMOVED AFT MID MOUNT BUSHINGS AT R/H HORIZONTAL STABILIZER IAW BOEING SERVICE BULLETIN 737-55-1074 FIG 4 PG 1 TO 3 REV 2.
Part: BUSHING — WORN (ZONE 300) · airframe 62,072 hrs · 39,779 cycles
RIGHT HAND HORIZONTAL STABILIZER, THE AFT LOWER MOUNT BUSHINGS PLATING IS WORN. (120-107) - RESOLUTOIN: SUBMIT TO ENG. REMOVED AFT LOWER MOUNT BUSHINGS AT R/H HORIZONTAL STABILIZER. IAW BOEING SERVICE BULLETIN 737-55-1074 FIG.4 PG.1 TO PG.3 REV 2 DATE JULY 21-2017 PART 3 PERMANENT REPAIR STEP 5. INSPECTED THE JOINT IAW EAR#08 RESPONSE STEP 2, PER SB 737-55-1074 REV 2: JULY 21, 2017. PART 3 - PERMANENT REPAIR STEP 11. CORROSION NOTED. ACCOMPLISHED FILLING THE REPORT FORM FOR AFFECTED JOINT AS PER 737-NG-FTD-55-13002, JOINT DIMENSION REPORT IAW EAR #08 RESPONCE STEP 2. PERFORMED DAMAGE REMOVAL OF CORROSION IN THE BORE AREA ONTO RHS HOR. STAB. REAR SPAR LOWER LUG (BORE) UP TO NOMINAL SIZE DIAM: 1.951" IAW EAR ITEM #08 DATED:01-28-25 ENG. RESPONSE STEP 6 THRU STEP 8 AND BOEING SB 737-55-1074 FIG.10.
Part: SIGHT GLASS — CRAZED (ZONE 800) · airframe 62,072 hrs · 39,779 cycles
EMERGENCY SLIDE BUSSEL (1) BOTTLE SIGHT GLASS CRAZED AND DIRTY. REMOVED AND REPLACED ESCAPE SLIDE COVER (WINDOW) PER B737-800 AMM 20-30-11-910-801 REV 8S,
Part: SIGHT GLASS — CRAZED (ZONE 800) · airframe 62,072 hrs · 39,779 cycles
EMERGENCY ESCAPE SLIDE BUSSEL SIGHT GLASS IS DIRTY. CLEANED EMERGENCY ESCAPE SLIDE BUSSELL NR 2 GLASS PER AMM 20-30-81-410-801 REV85.
Part: STOP FITTING — UNSECURE (ZONE 200) · airframe 62,072 hrs · 39,779 cycles
OVERWING EMERGENCY EXIT DOORS (ALL). ALL DOOR STOPS ON FRAMES ARE NOT SECURED.VERIFICATION OF PROPER INSTALLATION REQUIRED. RESOLUTION: (IN PROGRESS)
Part: STOP FITTING — NO DISCREPANCY (ZONE 200) · airframe 62,072 hrs · 39,779 cycles
OVERWING EMERGENCY EXIT DOORS (832, 833, 843) DOOR STOPS INSTALLED PROPERTY IN REF B737-800 AMM 52-22-01-400-801 T/W ID: 19-987 D.D: 12FEB2025 83090/83963 SAA024 01FEB2025. OVERWING EMERGENCY EXIT DOOR (842) DOOR STOPS INSTALLED PROPERLY IN REF. B737-800 AMM 52-22-01-400-801 T/W ID: 19-1240 D.D: 04JUN2025
2024
Part: SLIDE — MISINSTALLED (ZONE 800) · airframe 61,628 hrs · 39,560 cycles
L-1 DOOR SLIDE IS NOT INSTALLED CORRECTLY. LOWER SUPPORT PIN NOT SEATED IN THE MOUNT. RESOLUTION: INSTALLED L1 ESCAPE SLIDE CORRECTLY INTO LOWER SUPPORT BRAKET. REF AMM 25-66-01.
Part: UNKNOWN — ODOR · airframe 60,985 hrs · 39,252 cycles
STRONG FUME ODOR @ FL400 FOLLOWED QRH DIVERTED TO ELP UNKNOWN SOURSCE. PERFORMED FIM TASK 21-00 TASK 806 COULD NOT REPEAT DISCREPANCY ON GROUND NO EVIDENCE OF REPORTED FUMES AC OK FOR SERVICE.
Part: DRAIN — CORRODED (FWD) · airframe 59,887 hrs · 38,777 cycles
CORROSION FOUND AROUND FWD DRAIN. REPAIR ACCOMPLISHED IAW ATS ER 24-01202 REV IR AND SCA TASK CARD ENG-53SCA-11321 REV 00.
2023
Part: UNKNOWN — UNKNOWN · airframe 57,624 hrs · 37,791 cycles
SUPPLEMENTAL: INCLUDED TOTAL TIME AND TOTAL CYCLES
Part: UNKNOWN — UNKNOWN
DEFECT JOB NO 802616 00229 WHILE LOCATING / DRILLING FWD CARGO AFT SHIELD FOUND SUPPORT STA 500A, STR 25L, WL 155, CRACKED. RESOLUTION: REMOVED AND INSTALLED FWD CARGO AFT SHIELD SUPPORT AT STA 500 A STR 25L, WL 155 IAW BOEING SRM 51-40-02-06-01 AND BOEING DWG # 143A7505 REV: D
Part: SHIELD — CORRODED · airframe 57,624 hrs · 37,791 cycles
DEFECT NR00130: RH SHIELD AFT OF FWD CARGO DOOR AT STA 490-500A RBL 25 WL 158. RESOLUTION: REMOVED AND INSTALLED NEW RH SHIELD AFT OF FWD CARGO DOOR AT STA 490-500A RBL 25 WL 158 IAW B737 SRM 51-40-02-0G-0 DWG 143A0080 REV. A. CORROSION DAMAGE ON RH SHIELD AFT OF FWD CARGO DOOR FOUND TO BE OUT OF LIMIT DUE TO NO SRM DAMAGE LIMITS FOR THIS PART.
Part: ANGLE — CORRODED · airframe 57,624 hrs · 37,791 cycles
DEFECT NR00227: CORROSION ON AFT CARGO COMPARTMENT ANGLE ATTACHED TO WEB BS 847-855 RBL 20. RESOLUTION: REMOVED DAMAGED AND REPLACED ATTACH ANGLE TO WEB BS 847-855 RBL 20 IAW BOEING DWG 146A8125-51, SRM 51-30-01-0G-0, 51-40-05-006-0.
Part: INTERCOSTAL — CRACKED (UNKNOWN) · airframe 57,624 hrs · 37,791 cycles
DEFECT NR00196: CRACKED EXPANDABLE INTERCOSTAL AT STA 540 RBL 6. RESOLUTION: REMOVED AND REPLACED INTERCOSTAL AT STA 540 TO RBL 6 IAW B737-800 SRM 51-40-02-0G AND DWG 143A5240.
Part: UNKNOWN — CORRODED · airframe 57,624 hrs · 37,791 cycles
DEFECT NR00193: L-1 DOOR MOP SILL HAS EVIDENCE OF SUSPECTED CORROSION AT FASTENER HOLE BETWEEN STA 270 AND 344 WL 208.1. (MARKED) - - - RESOLUTION: REPAIRED L-1 DOOR MOP SILL (INNER CORD) PER ATS ER 23-01284 REV 1R AND SCA ENG-53SCA-1114 REV 00. REPAIR IS A CAT B REPAIR AND MUST BE INSPECTED AS GIVEN IN PARAGRAPH 5, SRM 53-10-15-2R-8. 50,000 FLIGHT CYCLES FROM DELIVERY OF AIRPLANE OR 12,0000 FLIGHT CYLCES FROM REPAIR INSTALLTION WHICHEVER COMES FIRST. HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION OF THE INNER CORD AS SHOWN IN FIGURE 203/ REPAIR 8. LOW FREQUENCY EDDY CURRENT (LFEC) INSPECT ON THE INNER CORD AS SHOWN IN FIGURE 208/ REPAIR 8. DVI OF THE PART (2) REPAIR ANGLE AND STA 303.9 FRAME AT FRAME TO THE LOWER MAIN SILL INNER CORD JOINT. INTERVAL 12,000 FLIGHT CYCLES.
Part: BAFFLE — CRACKED · airframe 57,624 hrs · 37,791 cycles
DEFECT T/C 538160000 NR 00109: FWD CARGO BAFFLE STA 500G - 500H STR 25R CRAKCED. RESOLUTION: REMOVED AND INSTALLED REPLACEMENT BAFFLE FWD CARGO BAFFLE STA 500G-500H STR 25R IAW B737 SRM 51-40-02-0G-0 AND BOEING DWG #143A7505 REV. B.
Part: BAFFLE — CRACKED · airframe 57,624 hrs · 37,791 cycles
DEFECT T/C 538160000 NR00107: FWD CARGO BAFFLE STA 500E-500F STR 25R CRACKED. RESOLUTION: REMOVED AND INSTALLED REPLACEMENT FWD CARGO BAFFLE STA 500E-500F STR 25R IAW B737 SRM 51-40-02-0G-0 AND BOEING DWG #143A7505 REV. B.
Part: SHIELD — CORRODED · airframe 57,624 hrs · 37,791 cycles
DEFECT T/C 572100100 NR 00078: FWD CARGO SHIELD AT STA 420-440 RH SIDE STR 25 HAS CORROSION. RESOLUTION: REMOVED AND INSTALLED REPLACEMENT FWD CARGO SHIELD AT STA 420-440 RH SIDE STR 25 IAW B737 SRM 51-40-02-0G-0 AND BOEING DWG #143A0080 REV: -.
Part: CHANNEL — CORRODED · airframe 57,624 hrs · 37,791 cycles
DEFECT FWD CARGO ZEE CHANNEL RH SIDE STR 25 HAS CORROSION AROUND FASTENER HOLES FROM STA 500C - 500G+10 RESOLUTION: REMOVED AND INSTALLED REPLACEMENT FWD CARGO ZEE CHANNEL RH SUDE STR 25 STA 500A TO 500I IAW BOEING SRM 53-00-53-2R-5 AND BOEING DWG #143A7501 REV:-
Part: BAFFLE — DAMAGED · airframe 57,624 hrs · 37,791 cycles
DEFECT FWD CARGO BAY BAFFLE LH SIDE AT STATION 460 - STA480 IS DAMAGED. RESOLUTION: REMOVED AND INSTALLED REPLACEMENT FWD CARGO BAY BAFFLE LH SIDE AT STA460 - STA480 IAW BOEING SRM 51-40-02-06-0 AND BOEING DWG #143A7505 REV: -.
Part: CHANNEL — CORRODED · airframe 57,624 hrs · 37,791 cycles
DEFECT NR00074: AFT CARGO ZEE CHANNEL FROM STA 727D TO STA 807 LBL 25WL 160 HAS COORROSION. RESOLUTION: REMOVED AND REPLACED AFT CARGO ZEE CHANNEL FROM BS 727B + 11 TO BS 807 + 9.5, SPLICE LOCATIONS BS 727H TO 10 IAW B737 SRM 53-00-53-2R-5 AND BOEING DRAWING 146A7500 REV -.
Part: SHIELD — CORRODED · airframe 57,624 hrs · 37,791 cycles
DEFECT: AFT CARGO SHIELD AT STA 847-867 RBL25 WL162 HAS CORROSION. RESOLUTION: REMOVED DAMAGED AND REPLACED AFT CARGO SHIELD AT STA 847 TO 867 RBL 25 WL162 IAW B737 SRM 51-40-05-0G-0, 51-40-02-0G-0, BOEING DWG 146A8127-8.
Part: CHANNEL — CORRODED · airframe 57,624 hrs · 37,791 cycles
DEFECT JOB NO 802616 00073 CORROSION AFT ZEE CHANNEL FROM STA 727B +6" TO STA 767 RBL 25 WL 160 HAS CORROSION. RESOLUTION: REPAIRED AFT CARGO ZEE CHANNEL STA 727 +4 TO 767 RBL 25 PER SRM 53-00-53-2R-5 SPLICE LOCATION 727 F+10