N5479A
Registered owner: BANK OF UTAH TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Richard F. Groger | Operator | on 2007-09-01 | Operator named in NTSB report |
Accident & incident history
Operated by Richard F. Groger (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.
48 reports on file, 2022-05-20 – 2026-07-28.
Part: SKIN — CORRODED (ZONE 200) · airframe 63,558 hrs · 411,955 cycles
W/O 96513 NR00050: -FUSELAGE SKIN, BS 727 - 907, S14R - S17R, CORROSION AND SCRIBE LINE. PERFORMED EA 53-0375 5479A, FUSELAGE SKIN BS 727 - 907, S14R. CORROSION AND SCRIBE LINE REPAIRED.
Part: SKIN — CORRODED (ZONE 200) · airframe 63,558 hrs · 41,195 cycles
FUSELAGE SKIN, BS 727 TO 887, S4L - CORRODED REPAIR. PERFORMED EA 53-0313, FUSELAGE SKIN REPAIR BS 727 - 887 STR.4L REPAIRED.
Part: SKIN — DAMAGED (ZONE 100) · airframe 63,558 hrs · 41,195 cycles
FUSELAGE SKIN, BS 351 TO 380, S23R TO S25R, CORROSION AND SCRIBE LINE. PERFORMED ENGINEERING TASK CARD NUMBER ENG-53SCA-11906 N5479A FUSELAGE SKIN STA 351 TO 380 - S23R TO S25R CORROSION SCRIBE LINE REPAIR.
Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 63,558 hrs · 41,195 cycles
FWD ENTRY AREA LH SIDE EMERGENCY LIGHT BATTERY PACK IS INOP.(OBSERVED WHILE PERFORMING FINAL CHECKS WITH ITEM 7-44). REPLACED AND TESTED FWD ENTRY AREA LH POWER SUPPLY BATTERY PACK IAW AMM 33-51-06-960-805 REV 89 DATED 02-15-2026 SATISFACTORY CONDITION.
Part: LAP JOINT — CRACKED (ZONE 200) · airframe 63,558 hrs · 41,195 cycles
EXTERNAL FUSELAGE, LAP JOINT AT STRINGER 14R, BS 727I+2, LOWER SKIN CRACKED. THIS CONDITION WAS FOUND DURING THE HFEC HOLE PROBE INSPECTION PER EO COO-EO-2026-24361. PERFORMED PERMANENT REPAIR AT EXTERNAL SKIN SECTION BETWEEN BS 727H & BS 727J, STRINGERS 13R & 16R DUE TO THE CRACK IAW EO COO-EO-2026-24361-R05, REV 5.
Part: SKIN — CORRODED (ZONE 200) · airframe 63,558 hrs · 41,195 cycles
UPPER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN BS 887 - 1016, STRINGER 4L, CORRODED. PERFORMED PERMANENT REPAIR AT EXTERNAL FUSELAGE SKIN PANEL FROM BS 887 - 1006, STRINGER 14L DUE TO CORROSION IAW EO COO-EO-2026-24383-R01, AND RDR 1 COO-SCA-26-0063-12B, AND SCA ENGINEERING AUTHORIZATION 53-0306.
Part: SKIN — CORRODED (ZONE 100) · airframe 63,558 hrs · 41,195 cycles
LOWER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN AT STA 361, STA 418, STRA 442 ON STR-24R SKIN WITH CORROSION. PERFORMED PERMANENT REPAIR LOWER FUSELAGE EXTERNAL SKIN SECTION FROM STA 360 TO STA 540 ON STRG-24RH DUE TO SKIN PANEL WITH CORROSION AND SCRIBE LINE IAW COOPESA E.O #COO-EO-2026-24369-R03 REV 03 (07-15-2026)RDR #C00-SCA-26-0068-15B(07-11-2026)FAA FORM REF ID 202606230006-0005 (07-15-2026) FIRST AND SECOND STAGE APPROVAL FAA FOM 8100-9 REF ID:202606230006-0007 (07-10-2026) FIRST STAGE APPROVAL THIS REPAIR IS AMOC AT PARAGRAPH (G) OF AD2010-26-06 FAA FORM 8100-9 REF ID 202606230006-0006 CONTINUE ON TASK 6
Part: SKIN — DAMAGED (ZONE 100) · airframe 63,558 hrs · 41,195 cycles
LOWER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN AT STA 421 ON STR-24R SKIN WITH SCRIBE LINE. PERFORMED PERMANENT REPAIR LOWER FUSELAGE EXTERNAL SKIN SECTION FROM STA 360 TO STA 540 ON STRG-24RH DUE TO SKIN PANEL WITH CORROSION AND SCRIBE LINE IAW COOPESA E.O #COO-EO-2026-24369-R03 REV 03 (07-15-2026)RDR #C00-SCA-26-0068-15B(07-11-2026)FAA FORM 8100-9 REF ID 202606230006-0005 (07-15-2026) FIRST AND SECOND STAGE APPROVAL FAA FOM 8100-9 REF ID:202606230006-0007 (07-10-2026) FIRST STAGE APPROVAL THIS REPAIR IS AMOC AT PARAGRAPH (G) OF AD2010-26-06 CONTINUE ON TASK 7
Part: SKIN — CORRODED (ZONE 200) · airframe 63,558 hrs · 41,195 cycles
UPPER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN FROM STA 360 TO STA 540 ON STR-14R SKIN WITH CORROSION. PERFORMED PERMANENT REPAIR AT STA 43 FROM STA 360 TO 540 BETWEEN STR 14 RH AND STR24 RH EXTERNAL SKIN PANEL WITH CORROSION AND SCRIBE LINE IAW COOPESA EO# 2026 -24381- R02 (07/27/2026).
Part: SKIN — CORRODED (ZONE 100) · airframe 63,558 hrs · 41,195 cycles
LOWER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN FROM STA 500D TO STA 500F ON STR-24R SKIN WITH CORROSION. PERFORMED PERMANENT REPAIR AT LOWER FUSELAGE EXTERNAL SKIN SECTION FROM STA 360 TO STA 540 ON STRG 24RH DUE TO SKIN PANEL WITH CORROSION AND SCRIBLE LINE IAW COOPESA EO.#COO-EO-2026-24369-R03 REV 3(07-15-2026)RDR #COO-SCA-26-0068-15B(07-11-2026) FAA FORM 100-9 REF ID 202606230006-0005 (07-10-2026) FIRST AND SECOND STAGE APPROVAL FAA FORM 8100-9 REF ID 202606230006-0007(07-10-2026) FIRST STAGE APPROVAL THIS IS AMOR OF PARAGRAPH (9) OF AD2010-26-06 CONTINUE ON TASK 6
Part: SKIN — DAMAGED (ZONE 200) · airframe 63,558 hrs · 41,195 cycles
UPPER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN AT STA 500I + 18.375 ON STR-4L SKIN WITH SCRIBE LINES. PERFRORMED PERMANENT REPAIR AT BS 500I THRU BS 540 BETWEEN STR.2L AND 6L OVER EXISTING REPAIR. BS 500I +11 INCG=HES TO BS 520 + 8 INCHES BETWEEN STR. 3L AND STR.5L. DUE TO SCRIBE LINE IAW COOPESA E0#COO-EO-2026-24354-R01-REV.01 07/08/2026. FAA FORM 8100-9 REFID: 202606250024-0005 07/29/2026 AUTHORIZED BY SCA ENGINEERING TASK CARD #ENG-53SCA-11910 REV.00 07/31/2026 AND NEW FAA 8100-9 MUST BE ISSUED WITHIN 24 MONTHS DUE 07/29/2028, THIS IS AMOC OF PARA(G) OF A.D. 2010-26-06.
Part: SKIN — CORRODED (ZONE 200) · airframe 63,558 hrs · 41,195 cycles
UPPER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN FROM STA 360 TO STA 540 ON STR-14R SKIN WITH CORROSION. PERFORMED PERMANENT REPAIR AT SECTION 43 FROM BS 360 - 540 STR 4R EXTERNAL FUSELAGE SKIN PANEL DUE TO CORROSION REPAIR IAW EO 000-EO-2026-24311-R03 REV 03, ENGINEERING AUTHORIZATION 53-0317 REV 00. FUSELAGE SKIN REPAIR BETWEEN BS 420 AND 460 S3R AND S6R FAA FORM 8100-9 REF ID 20260414-0050-0012 (FIRST STAGE APPROVAL)DATED: 07/29/2026 CONTINUE ON TASK #15.
Part: SKIN — CORRODED (ZONE 100) · airframe 63,558 hrs · 41,195 cycles
LOWER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN FROM STA 500D TO STA 500F ON STR-24R SKIN WITH CORROSION. - - MRO EMP# Â 5323-PERFORMED PERMANENT REPAIR AT LOWER FUSELAGE EXTERNAL SKIN SECTION FROM STA 360 TO STA 540 ON STRG 24RH DUE TO SKIN PANEL WITH CORROSION AND SCRIBLE LINE IAW COOPESA EO.#COO-EO-2026-24369-R03 REV 3(07-15-2026)RDR #COO-SCA-26-0068-15B(07-11-2026) FAA FORM 100-9 REF ID 202606230006-0005 (07-10-2026) FIRST AND SECOND STAGE APPROVAL FAA FORM 8100-9 REF ID 202606230006-0007(07-10-2026) FIRST STAGE APPROVAL THIS IS AMOR OF PARAGRAPH (9) OF AD2010-26-06 CONTINUE ON TASK 6
Part: SKIN — CORRODED (ZONE 200) · airframe 63,558 hrs · 41,195 cycles
UPPER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN AT STA 727 TO STA 887 ON STR-14R SKIN WITH CORROSION AND SCRIBE LINES. PERFORMED PERMANENT REPAIR AT EXTENRAL SKIN SECTION FROM STA 727 TO STA 887 BETWEEN STR-14R AND STR-17RH DUE TO CORROSION AND SCRIBE LINE IAW COOPESA E.O#COO-2026-24361-R05 REV 5 (07-22-2026) RDR #COO-SCA-26-0065-33B 53-0315 REV 00 . FUSELAGE SKIN INFORCING REPAIR BETWEEN BS 727C AND BS 727E S-13R AND S-25R
Part: SKIN — DAMAGED (ZONE 200) · airframe 63,558 hrs · 41,195 cycles
UPPER FUSELAGE EXTERNAL SKIN SECTION LAP JOINT LOWER SKIN AT STA 727C ON STR-4L SKIN WITH SCRIBE LINE. PERFORMED PERMANENT REPAIR AT EXTERNAL SKIN SECTION FROM B575B+13" TO BS727C+9" BETWEEN STR-2L AND STR6L DUE TO SCRIBE LINE IAW COOPESA EO COO-EO-2026-24295-R04 REV 04 (07-13-2026) FAA 8100-9 REFERENCE ID:202604140172-0005(FIRST STAGE APPROVAL) THIS IS A AMOC TO PARAGRAPH (G) OF AD2010-26-06 NEW FAA FORM MUST BE ISSUE WITHIN 24 MONTHS FROM THE DATE (07-01-2026) AND ENGINEERING TASK CARD ENG-53SCA-1194.
Part: LENS — DAMAGED (SLIDE COVER) · airframe 63,558 hrs · 41,195 cycles
L1 FWD ENTRY DOOR ESCAPE SLIDE COVER WITH LENS DAMAGED.
Part: RETAINER — LOOSE (GIRT BAR) · airframe 63,558 hrs · 41,195 cycles
L1 FWD ENTRY DOOR ESCAPE SLIDE GIRT BAR RETAINER CLIPS HAVE THE RIVETS LOOSE.
Part: COWL DOOR — UNLATCHED (ZONE 400) · airframe 63,555 hrs · 41,194 cycles
ABNORMAL ACFT VIBRATION AFTER TAKEOFF. ACFT REQUIRED SUBSTANTIAL RT AILERON TO MAINTAIN WINGS LEVEL. RETURNED TO LAL. POST FLT REVEALED NR 1 ENG COWL UNLATCHED INFLT. ACFT INSPECTED & REPAIRED EXCEPT FOR NR 42 & 43. COMPONENTS REPLACED: NR 2 FUEL HOSE, NR 3 HYD PUMP DRAIN LINE, NR 4 IDG DRAIN LINE, NR 5 HYD PRESSURE HOSE, NR 6 STARTER DUCT SUPPORT LINK, NR 7 INBD T/R PORT CAP, NR 8 J5 HARNESS, NR 9 LOWER FANCASE DETECTION ASSY, NR 10 LT FAN COWL, NR 11 RT FAN COWL, NR 13 THUMBNAIL FAIRING, NR 19 INLET COWL, NR 20 HFEC PERFORMED ON COWL ATTACHMENT FITTINGS, NR 21 OTBD FANCOWL ATTACHMENT FITTING, NR 51 REPLACED EEC.
Part: SLIDE — DETACHED (ZONE 800) · airframe 63,388 hrs · 41,114 cycles
FOUND L1 DOOR OPEN, SLIDE RESTING ON MAINTENANCE STAND. MAIN CABIN EXIT/SLIDE L-1 DOOR SLIDE INOPERATIVE OR MISSING PROVIDED R1 OPERATES NORMALLY. REPLACED L1 ESCAPE SLIDE IAW AMM 25-66-01, GOOD FOR SERVICE, THIS CLEARS MEL, 52-16-1.
Part: WINDOW — OVERTEMP (ZONE 200) · airframe 63,203 hrs · 41,027 cycles
R3 WINDOW VERY HOT TO THE TOUCH ( ELECTRICALLY HEATED WINDSHIELDS; NO. 3 WINDOW HEAT SYSTEM(S) . REF GMM/MTI MDDR#136262 WINDOW OVERHEAT OVER REF AMM 30-41-00 REF LOG PAGE 829340 ITEM #1 R/H #3 WINDOW R&R THIUS CLEARS MEL 30-11-4 MDDR#136261
Earlier reports · 2022–2025 · 28 reports
2025
Part: ENGINE — FIRE (NR 2) · airframe 63,199 hrs · 41,023 cycles
AFTER ENGINE SHUTDOWN NUMBER TWO ENGINE FLARED UP OUTISDE OF PLUG, HAND HELD FIRE EXTINGUSHER WAS APPLIED TO SUPPRESS FIRE. REMOVED & REPLACED #2 ENG PER TASK CARD 710000000 W/O# 101157. LEAK AND OPS TEST GOOD. OK FOR SERVICE.
Part: SMOKE DETECTOR — MALFUNCTIONED (ZONE 200) · airframe 67,979 hrs · 40,833 cycles
SMOKE ALARM WENT OFF WHEN WE WERE ON BASE TO FINAL LAVATORY SMOKE DETECTION SYSTEMS. REPLACED LAVATORY SMOKE DETECTOR IAW AMM 26-14-01, OPS CHECK GOOD,
Part: NUT — UNDERTORQUED (OIL TANK) · airframe 62,084 hrs · 40,489 cycles
DURING CLIMB OUT, OIL QUANTITY IN #2 ENGINE DECREASED TO ZERO, DID NOT MOVE FROM ZERO FOR REST OF FLIGHT, ALL OTHER INDICATIONS REMAINED NORMAL. RETORQUED ENGINE OILTANK OIL IN COUPLING NUT IAW AMM 79-11-01, PERFORMED IDLE LEAK CHECK 3A AND PART POWER LEAK CHECK 3B IAW B737 AMM 71-00-00, NO LEAKS NOTED. EMERGENCY DECLARDED. RETORQUED ENGINE OILTANK OIL IN COUPLING NUT IAW B737 AMM 79-11-01, PERFORMED IDLE LEAK CHECK 3A AND PART POWER LEAK CHECK 3B IAW B737 AMM 71-00-00, NO LEAKS NOTED.
Part: LAMP — INOPERATIVE (ZONE 200) · airframe 61,381 hrs · 40,175 cycles
DEFECT 782438: RH EMERGENCY LAMP OUT. - - RESOLUTION: REMOVED AND REPLACED RH EMERGENCY LAMP IAW B737 AMM 33-51-04-960-801 OPS TEST OK AT THIS TIME.
Part: SLIDE — OUT OF POSITION (ZONE 800) · airframe 61,167 hrs · 40,078 cycles
DEFECT 732333: L1 DOOR SLIDE PACKAGE OUT OF POSITION. - - RESOLUTION: (IN PROGRESS)
2024
Part: FLAP SYSTEM — MALFUNCTIONED · airframe 60,081 hrs · 39,577 cycles
DEFECT : APON APPROCH AT FLAPS 30 AND THEN FLAPS 15 AIRSPEED LOW AURAL WARNING SOUNDED UNABLE TO CONFIGURE FOR NORMAL LANDING. (EMERGENCY DECLARED) - - RESOLUTION: AIRSPEED WARNING AND CONFIG PROBLEMS FOUND TO BE FROM DDG PROCEDURE NOT FOLLOWED CORRECTLY FOR MEL 27-4-7. STALL WARNING ASYMMERTY MODE C/B FOUND TO NOT BE PULLED AND COLLARED ALONG WITH LIGHT BULBS STILL INSTALLED IN THE FORWARD PANEL INDICATION LIGHTS. DDG# 27-04-02-03 NOW C/W
Part: FIRE WARNING — FALSE INDICATION (MLG) · airframe 59,682 hrs · 3,931 cycles
#3 BRAKE FIRE / OVERHEAT AFTER A FLAPS 15 LDG W REF 150 KTS.AND REVERSER SLOW & STIFF IN DEPLOYING. THRUST REVERSER LEVERS VERY STIFF AND SLOW IN DEPLOYING TR'S IN ABQ. REMOVED AND REPLACED R/H MLG AXLE IAW AMM 32-11-45. OK FOR SERVICE. REF LOG PAGE 723662 ITEM #2 FOR RESOLUTION FOR T/R DEPLOYMENT. PERFORMED FIM 78-31 TASK 801 EAU BITE FOUND FAULT DIR CONT VALVE SENSOR ON BOTH ENGS. PERFORMED FIM 78-31 TASK 811 STOW FAULT - DIRECTIONAL CONT VALVE SENSOR. OPS CHECK GOOD CLEANED CONNECTORS, CLEARED FAULTS COULD NO DUPLICATE.
Part: FLOORBEAM — CORRODED (BS 772 R-LBL21) · airframe 39,209 hrs · 59,276 cycles
AFT CARGO COMPARTMENT @STA. 772 BETWEEN RBL 21 AND LBL 21 FLOOR TEE SUPPORT WITH CORROSION. REPALCED FLOOR SUPPORT TEE.
Part: ACCESS DOOR — CORRODED (RT WING) · corrosion level 2 · airframe 59,276 hrs · 39,209 cycles
RIGHT WING, MAIN TANK ACCESS DOOR 632MB WITH CORROSION. REPLACED DOOR
Part: WEB — CRACKED (BS 540 LBL 35) · airframe 59,276 hrs · 39,209 cycles
UPPER FUSELAGE MAIN CARGO CABIN AREA AT STA 540 LBL 35 TRANSVERSAL FLOOR SUPPORT WEB WITH CRACK. REPLACED FLOOR SUPPORT WEB.
Part: WEB — CRACKED (BS 540 RBL 31) · airframe 59,276 hrs · 39,209 cycles
UPPER FUSELAGE MAIN CARGO CABIN AREA AT STA 540 RBL 31 TRANSVERSAL FLOOR SUPPORT WEB WITH CRACK. REPLACED FLOOR SUPPORT WEB.
Part: WEB — CRACKED (BS 540 LBL 48) · airframe 59,276 hrs · 39,209 cycles
UPPER FUSELAGE MAIN CARGO CABIN AREA AT STA 540, WL 208, LBL 48 TRANSVERSAL FLOOR SUPPORT WEB WITH CRACK. REPALCED FLOOR SUPPORT WEB.
Part: ANGLE — CRACKED (BS 867 RBL 16) · airframe 59,276 hrs · 39,209 cycles
LOWER FUSELAGE AFT CARGO COMPARTMENT, AT STA 867 RBL 16, VERTICAL SUPPORT LOWER ANGLE LIGHT WITH CRACK. REPLACED ANGLE PN# 149A8109U114 LOCATED AT STA. 867 RBL 16 IAW B737-800 BCF SRM 51-10-02-06-0 PAR.P AND REF. AIPC B737-800 53-42-51-06
Part: SUPPORT ANGLE — DAMAGED (PAX DOOR) · airframe 59,276 hrs · 39,209 cycles
UPPER FUSELAGE FWD ENTRY DOOR TORQUE TUBE ACCESS STRUCTURE WITH ELONGED HOLE. REPLACED STRUCTURE SUPPORT ANGLE
Part: SUPPORT BRACKET — CRACKED (LT WING SPAR) · airframe 59,276 hrs · 39,209 cycles
LH WING REAR SPAR AT RSS 207 SUPPORT WITH RACK . REPLACED SUPPORT BRACKET CLIP ASSY P/N 115A5552-1 IAW B737-800 BCF SRM 51-10-02 PARA. 9 AND REFERENCE AIPC 57-50-00-23 SHEET 001
Part: TEE ANGLE — CORRODED (ACCESS PANEL) · airframe 59,276 hrs · 39,209 cycles
LOWER FUSELAGE, COMMON TO ACCESS PANEL #193AL, AFT CURVED ANGLE AND LOWER TEE ANGLE WITH CORROSION AND WEAR AT SEVERAL PLACES. REPLACED ANGLES
Part: FLOORBEAM — CORRODED (BS 727I) · corrosion level 2 · airframe 59,276 hrs · 39,209 cycles
AFT CARGO COMPARTMENT AT STA 727I+10"BETWEEN RBL 12"-LBL 21"FLOOR SUPPORT TEE WITH CORROSION. REPALCED FLOOR SUPPORT TEE
Part: DOUBLER — CRACKED (FUSELAGE) · airframe 59,276 hrs · 39,209 cycles
LOWER FUSELAGE EXTERNAL POWER RECEPTACLE DOOR CUTOUT AREA INTERNAL DOUBLER CRACKED. REPLACED INTERNAL DOUBLER PN: 141A3722-12
2022
Part: FLANGE — CORRODED · airframe 54,921 hrs · 37,263 cycles
SUPPLEMENTAL: CORROSION AT FLOOR SUPPORT UPPER CHORD FLANGE. CAUSE OF CORROSION: MOISTURE.
Part: BATTERY PACK — INOPERATIVE · airframe 54,921 hrs · 37,263 cycles
DEFECT 690301: FWD LH & RH EMER LIGHT BATTERY PACKS INOP. RESOLUTION: PERFORMED INSTALLATION POWER SUPPLY BATTERY PACK FWD LH AND RH ZONE IAW AMM TASK 33-51-06-960-805. OPERATYIONL TEST GOOD IAW AMM SUBTASK 33-51-06-710-004.
Part: BATTERY PACK — INOPERATIVE · airframe 54,921 hrs · 37,263 cycles
WORK ODER 61170: FWD AND RH EMER LIGHT BATTERY PACKS INOP. RESOLUTION: (IN PROGRESS)
Part: BATTERY PACK — INOPERATIVE · airframe 54,921 hrs · 37,263 cycles
SUPPLEMENT SCNA20221003116: WORK ORDER NR-00183: FWD LH & RH EMER LIGHT BATTERY PACKS INOP. RESOLUTION: PERFORMED INSTALLATION POWER SUPPLY BATTERY PACK FWD LH AND RH ZONE IAW AMM TASK 33-51-06-960-805. OPERATYIONL TEST GOOD IAW AMM SUBTASK 33-51-06-710-004.
Part: BATTERY PACK — INOPERATIVE · airframe 54,921 hrs · 37,263 cycles
WORK ORDER 61170: FWD LH & RH EMER LIGHT BATTERY PACKS INOP. RESOLUTION: (IN PROGRESS)
Part: STRAP — CRACKED · airframe 54,921 hrs · 37,263 cycles
DEFECT: FOUND STRAP DAMAGED UNDER EXTERNAL SKIN AT STA 1138 RH. BEHIND PANEL 343AT SLIDING SEAL (STRAP N/N REF 148A8713-8) RESOLUTION: 7/10/2022 - REMOVED AND REPLACED STRAP UNDER EXTERNAL SKIN STA1138 RH BEHIND PANEL 343AT SLIDING SEAL PO # 511743-1 IAW ATS CR 22-01910 REV 1R AND SCA EA 53-0118.
Part: SKIN PANEL — CRACKED · airframe 54,921 hrs · 37,263 cycles
DEFECT: EXTERNAL SKIN DAMAGE WAS FOUND TO BE DAMAGED AT STA 1138 RH BEHIND PANEL 343AT SLIDING SEAL. RESOLUTION: 7/10/2022 - ACCOMPLISHED REPAIR TO EXTERNAL SKIN AT STA 138 RH BEHIND PANEL 343AT SLIDING SEAL IAW ATS CR 22-01896 AND ENG-57SCA-10984.
Part: FLOOR SUPPORT — CRACKED · airframe 54,921 hrs · 37,263 cycles
DEFECT: BAFFLE CRACKED AT BS500A-500B R/H SIDE. RESOLUTION: REMOVED AND REPLACED BAFFLE AT BS500A-500B R/H SIDE IN ACCORDANCE WITH B737 SRM 51-40-02-04-0 PART B.
Part: FLOOR SUPPORT — CORRODED · airframe 54,921 hrs · 37,263 cycles
DEFECT: CORROSION AT FLOOR SUPPORT STA 986.5 4IN INBD OF L2. RESOLUTION: CORROSION DAMAGE ON 986.5 FLOOR BEAM FOUND TO BE OUT OF LIMITS PER B737 SRM 53-70-51-1A-1. REMOVED DAMAGE FROM FLOOR BEAM BSTA 986.5, FWD FLANGE DIMENSIONS: 1.150" X .900", B737-SRM 51-10-02-04-0. REPAIRED FLOOR BEAM PER ATS ER 22-01786 REV 1R AND SCA ENG-53SCA-10977 REV 00.
Part: SPAR — CRACKED · airframe 54,921 hrs · 37,263 cycles
DEFECT: CORROSION. RH WING, FWD OF FWD SPAR HAS CORROSION WHERE REFUELING PANEL LATCH CONTACTS STRUCTURE, WS 372 APPROX. (MARKED). RESOLUTION: 7/09/2022 REPAIRED RH WING FWD SPAR AT REFUELING PANEL LATCH AREA IAW SCA ENG-57SCA-10983 AND ATS ENGINEERING 22-01773 REV 1R THIS IS TIME LIMITED REPAIR REPLACE REPAIR WITHIN 24 MONTHS NOT TO EXCEED 3000 CYCLES.