AMERIJET INTERNATIONAL INC

Sanction: $17,334 · case closed 2019-12-12

Sanction: $200,000 · case closed 2019-12-12

Sanction: $8,800 · case closed 2013-03-29

Sanction: $37,500 · case closed 2013-02-08

Part: HYDRAULIC LINE — LEAKING (RIGHT ENGINE) · airframe 112,339 hrs · 21,294 cycles

RIGHT ENGINE OVERHEAT EICAS MESSAGE DURING FLIGHT. PRECAUTIONARY ENGINE SHUT DOWN, AND DEVIATION.

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 104,733 hrs · 38,945 cycles

DURING A SERVICE CHECK, EMERGENCY LIGHT LOCATED AT DOOR SIGN AND LAVATORY INOP.

Part: TURBINE — DAMAGED (LT ENGINE) · airframe 120,634 hrs · 23,493 cycles

LEFT ENGINE FAILURE DURING FLIGHT. AFTER INSPECTION FOUND HOT SECTION DAMAGE.

Part: GEARBOX — FAULTED (NR 2 ENGINE) · airframe 261 hrs · 46 cycles

ON FLIGHT 99 FROM ICN TO ANC, TEN MINUTES INTO THE FLIGHT, THE FLIGHT CREW REPORTED A HIGH ENGINE VIBRATION ON #2 ENGINE, FOLLOWED BY RELATED FIRE WARNING. THE CREW PROCEEDED TO DISCHARGE BOTH FIRE BOTTLES AND PERFORMED EMERGENCY PROCEDURES, RETURNING TO ICN AND LANDING WITH SINGLE ENGINE. EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. AFTER LANDING, ENGINE DAMAGED WAS DISCOVERED. MANUFACTURERS WERE CONTACTED FOR EVALUATION AND CAUSE OF FAILURE. #2 ENGINE GEARBOX FAILURE IS SUSPECTED AT THIS TIME.

Part: CONTROL PANEL — INTERMITTENT (COCKPIT) · airframe 63,131 hrs · 44,360 cycles

AS THE CREW WERE APPROACHING TOP CLIMB OF FLIGHT LEVEL 380, THE CREW RECEIVED A MASTER WARNING,FOLLOWED BY A FIRE BELL, EICAS MESSAGE OF "MAIN DECK CARGO FIRE" AND THE MAIN DECK ZONES THAT WERE SENSING SMOKE ENUNCIATED. THE CREW PROCEEDED TO COMMENCE THE QRH CHECKLIST FOR MAIN DECK CARGO FIRE . DURING COMMENCEMENT OF THE CHECKLIST , PRIOR TO REACHING STEP #6, THE FIRE BELL, MASTER WARNING AND MAIN DECK AFFECTED ZONES SILENCED AND ASSOCIATED WARNINGS EXTINGUISHED. AS A PRECAUTION, THE CREW DECIDED TO DIVERT BACK TO MIA. DURING THE DIVERSION, THE CREW ASK THE FLIGHT MECHANIC TO VISUALLY ASSESS THE SITUATION THROUGH THE SMOKE BARRIER DOOR WINDOW. THE MECHANIC ADVISED THAT THERE WERE NO SIGNS OF FIRE, SMOKE. THE CREW DECIDED NOT TO DECLARE AN EMERGENCY. THE AIRPLANE LANDED WITHOUT FURTHER ISSUE. NO FURTHER WARNING MESSAGES WERE RECEIVED DURING DESCEND, APPROACH, AND LANDING.

Part: FITTING — WORN (RUDDER PCA) · airframe 100,829 hrs · 17,651 cycles

UPPER RUDDER PCA INPUT FITTING HAS PLAY.REMOVED, REPAIRED, AND REINSTALLED UPPER RUDDER PCA INPUT FITTING IAW B767 AMM 27-21-02 AND AMES REA47411REA05 REV. IR.

Part: HYDRAULIC SYSTEM — LOW PRESSURE (C SYSTEM) · airframe 93,226 hrs · 44,638 cycles

AFTER GEAR DOWN AND FLAPS AT 2" C HYDRAULIC PRESSURE AT 2990

Part: BRACKET — CRACKED (LT COWLING) · airframe 85,819 hrs · 26,355 cycles

L/H AFT PRECOOLER MOUNT BRACKET CRACKED VIEWED BENEATH #2 L/H CORE COWL. REMOVED AND REPLACED L/H AFT PRECOOLER MOUNT BRACKET IAW B767 SRM 51-40-02 PARA 9 AND IAW 47404FAB04.

Part: TEE FITTING — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 85,819 hrs · 26,355 cycles

CORROSION ON INTERIOR "T" SECTION OF ALC DOOR 10" FROM AFT EDGE, 24" FROM TOP EDGE.REMOVED AND REPLACED INTERIOR "T" SECTION OF ALC 3RD FROM TOP USING 140T2604-3 IAW BOEING DWG# 140T2604.

Part: WEB — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 85,819 hrs · 26,355 cycles

ALC DOOR HAS LIGHT CORROSION AT INTERIOR PANEL MOUNTING SCREW LOCATIONS.REPLACED SKIN ON ALC DOOR IAW B767 51-40-02 PAR 4 BOEING DWG 140T2640 AND DOC 47404FAB02

Part: WEB — CRACKED (NR 2 PYLON) · airframe 85,819 hrs · 26,355 cycles

NUMBER 2 PYLON - WEB AND BRACKET THAT NOSE COWL ANTI-ICE DUCT ATTACHES TO AT FORWARD END OF PYLON AT PASS THRU ARE WORN/BROKEN.REPLACE WORE BRACKET IAW B767 SRM 51-40-02, NEW WEB REPLACEMENT DONE ON AMES REA 47404FAB01 ON #2 PYLON FWD END.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 85,819 hrs · 26,355 cycles

STRINGER SPLICE AT STA. 434 S31R CORRODED.REMOVED AND REPLACED CORRODED SPLICE AT STA 434 S31R IAW B767 SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N2380 DISCREPANCY: AFT CARGO STRINGER 36R HAS CORROSION AT STA-1355. CORRECTIVE ACTION: REMOVED, FABRICATED AND REPLACED STRINGER SECTIONS IAW B767-200 SRM 51-40-02 AND SRM 53-00-03, REPAIR 2 TYPE III.

Part: SKIN — CRACKED (FUSELAGE) · airframe 85,819 hrs · 26,355 cycles

AFT R/H EXTERIOR FUSELAGE SKIN IS CRACKED STA 1654.5 BETWEEN STRINGERS 4R-5R. (VERIFIED WITH HFEC SURFACE SCAN).REPAIRED EXTERIOR FUSELAGE SKIN STA 1654.5 S3R-S8R IAW B767 SRM 53-80-01 REPAIR 4.

Part: INLET — DAMAGED (NR 2 ENGINE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2768N93 DISCREPANCY: P/R-MESA SUPPORT TASK; #2 ENGINE INLET COWL REPAIR AT 5:30 POSITION (AFT LOOKING FWD) REQUIRES ENGINEERING EVALUATION REF FVCI EO 20113-2 CORRECTIVE ACTION: COMPLIED WITH FVCI E.O. 20113-2 (ATTACHED SEE ATTACHED 8110-3)

Part: FRAME — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE DISCREPANCY: CORROSION ON AFT CARGO FRAME WEB STA-1270 AFT FACE BETWEEN STR-29R AND STR-32R. CORRECTIVE ACTION: REMOVED, FABRICATED WEB (7075-T6 .100) AND SPLICE PLATE (7075-T6 .125), INSTALLED WEB AND SPLICE PLATE. REMOVED AND REINSTALLED SEAL DEPRESSOR, DOOR STOP FITTINGS, SUPPORT BRACKETS AND "L" ANGLES AT STA-1270 STR-28R - STR-32R. ALL WORK ACCOMPLISHED IAW B767-200 SRM 51-40-02, 51-10-02, 51-40-05, 51-40-04, 51-20-01, SOPM 20-41-02 AND F.V.C E.O.#19309.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N498 DISCREPANCY: AFT LOWER CARGO HAS CORROSION APROX. S-36 STA-1131 BELOW POWER DRIVE 1R INTERNAL. CORRECTIVE ACTION: REMOVED, FABRICATED AND INSTALLED AFT CARGO STRINGER 36R BETWEEN STA 1087 TO STA 1143 IAW B767-200 SRM 53-60-03 FIG.201, PG 201 AND B767-200 SRM 53-00-03 REPAIR 2.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N316 DISCREPANCY: FWD CARGO STRINGER 39R FROM FWD FACE BULKHEAD TO STA-764. CORRECTIVE ACTION: REMOVED, FABRICATED AND REPLACED STRINGER SECTION AT FWD CARGO BETWEEN STA-730 - STA-784 S-39R IAW B767-200 SRM 53-00-03 REPAIR 2. AND SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N2956 DISCREPANCY: SEAT TRACK FLANGE AT LBL-78 CORRODED FROM STA-1087 - STA-1109 ON I/B SIDE. CORRECTIVE ACTION: REMOVED, FABRICATED, AND INSTALLED SEAT TRACK SECTION FROM STA-1087 - STA-1109, LBL-78 IAW B767 SRM 51-40-02, 51-40-05 AND 53-00-52.

Part: SLAT — CORRODED (RT WING) · corrosion level 2 · airframe 85,819 hrs · 26,355 cycles

NUMBER 7 SLAT - LOWER LEADING EDGE HAS BULGE 93 INCHES FROM OUTBOARD END AND 7 INCHES FROM TRAILING EDGE.REPAIRED #7 SLAT LOWER LEADING EDGE IAW REA# 47404REA02

Part: STRINGER — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N3148 DISCREPANCY: AFT CARGO, STRINGER 39R AND STRINGER SPLICE CORRODED AT APPROX STA-1287 - STA-1307. CORRECTIVE ACTION: REMOVED, FABRICATED, REPLACED STRINGER AND STRINGER SPLICE AT 39R AT STATION 1287 - 1307 IAW B767-200 SRM 51-40-02, 51-40-05, AND 53-00-03 TYPE III, REPAIR 2.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N1601 DISCREPANCY: CORROSION ON STRINGER 36L FROM STA-434 - STA-478. CORRECTIVE ACTION: REMOVED, FABRICATED, INSTALLED REPAIRS AT STA-434 - SAT-478, STR36L IAW B767-200 SRM 51-40-05, 53-00-03 REPAIR 2, E.O.#19330 REV.A AND E.O.#19365.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N2078 DISCREPANCY: CORROSION ON AFT CARGO DOOR SILL WEB STA-1270 - STA-1285, STR-33 R/H. CORRECTIVE ACTION: REMOVED, FABRICATED NEW WEB IAW FVCI E.O.# 19544 AND INSTALLED IAW BOEING 767-200 SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N3163 DISCPREPANCY: AFT CARGO STRINGER 39L IS CRACKED APPROX. AT STA 1307. CORRECTIVE ACTION: REMOVED CRACKED STRINGER 39L, FABRICATED, AND INSTALLED STRINGER REPAIRS AT STA-1253 - 1275 AND STA-1307 - 1329 IAW B767-200 SRM 53-00-03. REPAIR #2 FIG. 201 SHT 5 TYPE III.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBNORNE/PEMCO NON-ROUTINE 2387N3147 DISCREPANCY: AFT CARGO WEB BETWEEN STA-1285 - STA-1329 LBL 35-38. CORRECTIVE ACTION: REMOVED, FABRIACATED AND REPLACED AFT CARGO WEB BETWEEN STA-1285 - STA-1329 LBL 35-38 IAW B767-200 SRM 51-40-02, 53-60-53,51-30-01.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N2744 DISCREPANCY: AFT CARGO DOOR CUT-OUT BEAR STRAP CORRODED STA-1250 - STA-1307, STR-38R - STR-31R. REQUEST EA. CORRECTIVE ACTION: COMPLIED WITH AFT CARGO DOOR CUT-OUT BEAR STRAP (REPAIR) STA-1250 - STA-1307, STR-38R - STR-31R IAW E.A.# PD67-55-070.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N1528 DISCREPANCY: AFT CARGO BEAR STARP CORRODED AT STA.1285 - STA-1307, STR-34R STR-35R. CORRECTIVE ACTION: BEAR STRAP FROM STA 1250 - STA-1307 AND STR-32R -STR-38R WAS REPAIRED ON N/R 2387N2744 AND IAW E.A.#PD67-53-070.

Part: SKIN — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N608 DISCREPANCY: EXTERNAL SKIN CORRODED BENEATH DOUBLER STATION 1285, STR-36R. CORRECTIVE ACTION: EXTERNAL FUSELAGE SKIN AT STA-1285, STR-36R REPAIR ACCOMPLISHED ON N/R CARD 2387N2744 AND E.O. PD67-53-070.

Part: FRAME — CRACKED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N3078 DISCREPANCY: AFT CARGO FRAME WEB CRACKED AT STA-1153 RBL-18. CORRECTIVE ACTION: REMOVED, FABRICATED, AND INSTALLED FRAME WEB AT AFT CARGO STA-1153, RBL-44 TO LBL-44 IAW B767-200 SRM 51-40-05, 51-30-01 AND 51-40-02.

Part: SPAR — CORRODED (RT WING) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N3013 DISCREPANCY: RIGHT WING, APPRX WS-933 UPPER SPAR T/E SPAR CORRODED. CORRECTIVE ACTION: COMPLIED WITH FLIGHT VEHICLES CONSULTING INC.. E.O.# 19552 REV.B FOR RIGHT WING , APPROX WS-933 UPPER SPAR T/E SPAR.

Part: SPAR — CORRODED (RT WING) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N3014 DISCREPANCY: RIGHT WING STA-933 LOWER SPAR T/E SPAR CORRODED. CORRECTIVE ACTION: REPAIRED IAW F.V.C E.O.#19553 REV.IR.

Part: SPAR — CORRODED (RT WING) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N2980 DISCREPANCY: R/H WING, T/E UPPPER SPAR AT APPRX WS-442 HAS CORROSION. CORRECTIVE ACTION: REMOVED CORRSION AT R/H WING UPPER T/E SPAR WS-442 AND REPAIRED IAW E.O.#19350.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N2982 DISCREPANCY: AFT CARGO STRINGER 36R CORRODED BETWEEN STA-1373 - STA-1461. CORRECTIVE ACTION: REMOVED AND REPLACED AFT CARGO STRINGER 36R BETWEEN STA-1373 - STA-1461 IAW B767-200 SRM 53-00-03.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N2965 DISCRREPANCY: FWD CARGO STRINGER 35R CORRODED AT STA-780. CORRECTIVE ACTION: REMOVED DAMAGE STRINGER SECTION AND INSTALLED STRINGER REPAIR IAW B767-200 SRM 53-00-03 REPAIR #2 DETAIL III.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRRBORNE/PEMCO NON-ROUTINE 2387N2976 DISCREPANCY: FWD CARGO STR-36L CORRODED AT APPROX STA-594. CORRECTIVE ACTION: REMOVED DAMAGED STRINGER SECTION AND INSTALLED STRINGER REPAIR AT STA-578 -STA-600 IAW SRM 53-00-03 REPAIR 2 DETAIL III.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N3191 DISCRPANCY: WHILE ACCOMPLISHING N/R 2387N2982 FOUND PREVIUOS DAMAGE AT STA-1395 - STA-1415, STR-36R. DAMAGE WAS COVERED UP WITH BONDO. CORRECTIVE ACTION: REWORKED AND REPAIRED AREA AT AFT CARGO EXTERNAL FUSELAGE SKIN BETWEEN STA-1395 - STAS-1415, STRINGER 36R IAW F.V.C E.O# 20038 REV. IR

Part: SPAR CAP — CORRODED (LT WING) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N3021 DISCREPANCY: DURING "OK TO INSTALL" L/H AILERON FOUND CORROSION ON WING REAR SPAR UPPER CAP AT W.S.906.2 FWD OF AILERON I/B MOST HINGE FITTING. CORRECTIVE ACTION: REMOVED CORROSION ON L/H AILERON ON WING REAR UPPER SPAR CAP AT W.S. 906.2 FWD OF AILERON I/B MOST HINGE FITTING IAW SRM 57-51-02. MATERIAL 0.120, MATERIAL LOSS 0.050, REMAINING MATERIAL THICKNESS 0.070. FOUND TO BE OUT-OF-LIMITS IAW B767-200 SRM 57-51-02. REPAIRED IAW E.O.#19560.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N2950 DISCREPANCY: AFT CARGO, STR 37R HAS CORROSION AT STA.1297. CORRECTIVE ACTION: REMOVED, FABRICATED AND REPLACED 37R AT STATION 1297 IAW B767 SRM 53-00-03 REPAIR 2.

Part: FRAME — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,799 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N3190 DISCREPANCY: MAIN CABIN FRAME OUTTER FLANGE AT STA-1480, STR-18 R/H IS CORRODED. CORRECTIVE ACTIN: REMOVED CORROSION AT MAIN FRAME STA-1480, FOUND TO OUT-OF-LIMITS IAW SRM 53-00-07 FIG.101. REMOVED, FABRICATED AND INSTALLED NEW FRAME AT MAIN CABIN STA 1480 IAW SRM 51-40-02, TRAVELERS NR#2387N3228/NR#2387N3229.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO DISCREPANCY: CORROSION ON AFT CARGO SILL WEB STA-1270 - STA-1285, STR-33 R/H. CORRECTIVE ACTION: REMOVED, FABRICATED NEW WEB IAW FVCI E.O. 19544 AND INSTALLED IAW BOEING 767-200 SRM 51-40-02.

Part: SKIN — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N318 DISCREPANCY: FWD CARGO-LOWER BILGE AREA CORRODED AT STA 698 BETWEEN S36R-S35R. CORRECTIVE ACTION: REWORKED AND REPAIRED AREA AT FWD CARGO - LOWER BILGE STA 698 S36R-S35R IAW B767-200 SRM 53-00-01 REPAIR 12.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N314 DISCREPANCY: FWD CARGO STRINGER CORRODED, FWD OF BULHEAD STA 764 AT S36R. CORRECTIVE ACTION: REMOVED AND REPLACED DAMAGE STRINGER S36R FROM STA-638 TO STA-784 IAW B767-200SRM 53-00-03 REPAIR #2 AND E.O. 47359REA10.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2768N42 DISCREPANCY: (PR 604284) BULK CARGO EXISTING REPAIR AT STA 1394 TO STA 1407 BETWEEN S25R TO 27R REQUIRES ENGINEERING EVALUATION CORRECTIVE ACTION: BULK CARGO EXISTING REPAIR @ STA 1394 TO STA 1407 BETWEEN S25R TO 27R WAS FOUND TO BE INCORRECT PER B767 SRM 53-00-01 REPAIR 33 AND CORROSION WAS FOUND ON OUTER SURFACE OF DOUBLER, TRIPLER, AND FILLER. REMOVED AND REPLACED IAW B767 SRM 53-00-01 REPAIR 33

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N2192 DISCREPANCY: MAIN DECK STA-786 - STA-996, LBL-54.75, CORRODED SEAT TRACK OUT-OF-LIMITS. CORRECTIVE ACTION: EVALUATED DAMAGE, REMOVED DAMAGE AND REPAIRED AT DECK STA-786 - STA-996. LBL 54.75 SEAT TARCK, O/B FLANGE L=10FT W=1.25, I/B FLANGE L=6FT W=1.40, AFT I/B FLANGE IAW BOEING 767-200 E.O. #CS-22215-009.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N2186 DISCREPANCY: MAIN DECK STA-786 - STA-996, RBL-74.75, CORRODED SEAT TARCK OUT-OF-LIMITS. CORRECTIVE ACTION: EVALUATED DAMAGE , REMOVED DAMAGE AND INSTALLED REPAIRS IAW E.O.# CS-22215-009.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N2187 DISCREPANCY: MAIN DECK STA-786 - STA-996, RBL 54.75, CORRODED SEAT TARCK OUT-OF-LIMITS. CORRECTIVE ACTION: EVALUATED DAMAGE, REMOVED DAMAGE AND INSTALLED REPAIRS IAW E.O.#CS-22215-009.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N2188 DISCREPANCY: MAIN DECK STA-786 - STA-996, RBL 33, CORRODED SEAT TRACK OUT-OF-LIMITS. CORRECTIVE ACTION EVALUATED DAMAGE, REMOVED DAMAGE AND INSTALLED REPAIRS IAW E.O.#CS-22215-009.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N2189 DISCREPANCY: MAIN DECK STA-786 - STA-996, RBL-11, CORRODED SEAT TRACK OUT-OF-LIMITS. CORRECTIVE ACTION: EVALUATED DAMAGE, REMOVED DAMAGE AND INSTALLED REPAIRS IAW E.O.#CS-22215-009.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,799 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N2190 DISCREPANCY: MAIN DECK STA-786 - STA-996, LBL 11, CORRODED SEAT TRACK OUT-OF-LIMITS. CORRECTIVE ACTION: EVALUATED REWORK DAMAGE AT SEAT TRACK FLANGE, FOUND TO BE OUT -OF -LIMITS, REPAIRED MAIN SEAT TRACK FLANGE I/B AND O/B AT STA 786 - STA 996, LBL 11 IAW E.O.# CS-22213-009.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 89,451 hrs · 43,779 cycles

AIRBORNE/PEMCO NON-ROUTINE 2387N2191 DISCREPANCY: EVALUATED DAMAGE, REMOVED DAMAGE AND REPAIRED AT MAIN DEACK STA-786 - STA-996, LBL 33, I/B FLANGE (2 EACH)L=7FT 6IN W=1.25, L=8FT 6IN W= 1.25 O/B FLANGE L=9IN W=1.25, L=6FT W=1.25 IAW E.O.#CS-22215-009.