N891EA

Part: DEICE SYSTEM — LOW PRESSURE (ZONE 300) · airframe 55,870 hrs · 59,255 cycles

DEICE BOOT FAILURE OF TAIL RHS OUTBOARD SECTION 6 RIGHT HAND SIDE - INDICATION LIGHT DOES NOT ILLUMINATE DURING OPERATION IN AUTO NOR IN MANUAL

Part: DEICE SYSTEM — LOW PRESSURE (ZONE 400) · airframe 55,811 hrs · 59,204 cycles

#1 ENGINE INTAKE DEICE INOP

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 54,799 hrs · 58,467 cycles

L/H AFT EMERGENCY "EXIT' SIGN DOES NOT ILLUMINATE. REPINNED CONNECTOR FOR LH AFT CABIN EMERGENCY EXIT LIGHT. OPS CHECKED OK. REF DHC-8-100 MM 20-45-06 AND 33-52-00.

Part: UNKNOWN — DETACHED (UNKNOWN) · airframe 54,326 hrs · 58,019 cycles

EMER EXIT PLACARD OVER MAIN CABIN ENTRY FELL OFF. RE-ATTACHED PER AMM 33-00

Part: GENERATOR — FAILED · airframe 54,210 hrs · 57,858 cycles

#2 AC GEN HOT CAUTION LIGHT CAME ON

Part: CONTACTOR — FAILED · airframe 54,031 hrs · 57,654 cycles

UN-COMMANDED ENGINE #1 MOTORING AFTER A DC BUSS CAUTION LIGHT. REPLACED A FAILED RELAY STUCK CLOSED.

Part: CONTROL BOX — FAILED · airframe 53,871 hrs · 57,520 cycles

EMERGENCY LIGHTS IN CABIN ILLUMINATED DURING TAXI WITH PROPELLERS IN MIN. REPLACED EMERGENCY LIGHT CONTROL BOX

Part: CONTROL BOX — MALFUNCTIONED · airframe 53,780 hrs · 57,433 cycles

EMERGENCY LIGHTS CONTINUOUSLY ON WITH EMER LIGHTS SWITCH IN ARM

Part: BATTERY PACK — DISCHARGED · airframe 53,780 hrs · 57,433 cycles

IN FLIGHT....EMERGENCY LIGHTS IN CABIN WOULD RANDOMLY COME ON FOR ABOUT 5 MINUTES THEN SHUT OFF.

Part: SOLENOID VALVE — FAILED (ZONE 600) · airframe 53,722 hrs · 57,382 cycles

ROLL SPLR OUTBD CAUTION LIGHT ILLUMINATED AFTER SELECTING "FLIGHT" OUTBD ROLL SPOILERS REMAINED DOWN AT IDLE WITH "FLIGHT" SELECTED. R/R R/H #1 ROLL SPOILER LIFT DUMP SOLENOID VALVE.

Part: ANTENNA — FAILED (VHF) · airframe 53,607 hrs · 57,266 cycles

AFTER DEPARTING ANC CREW DISCOVERED #1 COM NOT WORKING. R&R #1 VHF COMM ANTENNA

Part: HORN — FAILED (LT ELEVATOR) · airframe 53,542 hrs · 57,209 cycles

LEFT ELEVATOR HORN HEAT CAUTION LIGHT ON WHEN ELV HORN HEAT ON.

Part: WARNING LIGHT — FALSE ACTIVATION (HYD PUMP) · airframe 53,498 hrs · 57,184 cycles

#1 STANDBY HYDRAULIC PUMP HOT LIGHT INTERMITTENTLY FLASHING ON TAXI. REPINNED IAW AMM 29-11-17.

Part: PUMP — FAULTED (HYD SYS STNDBY) · airframe 53,498 hrs · 57,184 cycles

NR 1 STBY HYD PUMP HOT LIGHT INTERMITTENLY FLASHING ON TAXI. T/S STBY HYS PUMP, FOUND HARD FAULT ON STBY HYS PUMP OINS A/B OVERTEMP SWITCH MOVED TO PIN E/F OVERTIEMP SWITCH IAW AMM 29-11-17

Part: AUTOPILOT SYS — FAILED

AFCS&AUTO PILOT FAIL IN FLIGHT

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 53,325 hrs · 57,022 cycles

CORROSION FOUND ON L/H INBOARD SEAT TRACK BTW STA X526 TO X592. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 526-600) · corrosion level 3 · airframe 53,325 hrs · 57,022 cycles

CORROSION R/H INBOARD SEAT TRACK BTW STA X526 - 600

Part: FRAME — CRACKED (BS 136 S15A) · airframe 53,325 hrs · 57,022 cycles

FRAME CRACK @ STA X136 ABOVE STR 15A

Part: LONGERON — CRACKED (RT NACELLE) · airframe 49,764 hrs · 53,819 cycles

CRACK DAMAGE TO RH NACELLE I/B UPPER NACELLE LONGERON P/N 85410209 AROUND EYE BOLT.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 49,265 hrs · 53,358 cycles

2 DENTS ON LEFT HAND FUSELAGE BETWEEN STATION X277-X285 ABOVE AND BELOW STRINGER 11P. RD 8-53-16128 WAS ISSUED AND PROVIDES PREMANENT ALLOWANCE FOR MULTIPLE DENT DAMAGE TO THE LEFT HAND SIDE FUSELAGE SKIN PANELS(P/N 85320281 AND 85320313) BETWEEN X270.50 - X291.40 AND STRINGERS 10P - 12P.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 49,265 hrs · 53,358 cycles

SCRATCH IN BELLY FUSELAGE SKIN.

Part: FLAP TRACK — CORRODED (LT NR 5) · corrosion level 2 · airframe 49,265 hrs · 53,358 cycles

CORROSION DAMAGE TO LEFT HAND #5 FLAP TRACK ASSEMBLY, INBOARD HALF

Part: SKIN — DENTED (RUDDER) · airframe 49,265 hrs · 53,358 cycles

DENT ON L/H SKIN OF FORE RUDDER BTW RIB 11 - 12 AND AFT OF REAR SPAR

Part: SKIN — DENTED (BS 151-167) · airframe 49,265 hrs · 53,358 cycles

DENTS IN BOTTOM FUSELAGE SKIN

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 49,265 hrs · 53,358 cycles

MULTIPLE DENTS IN FUSELAGE SKIN PANELS 85320281 AND 85320313.

Part: CONTROL BOX — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,936 hrs · 49,581 cycles

EMERGENCY LIGHTS CONTROL BOX INOPERATIVE. REMOVED AND REPLACE THE EMERGENCY LIGHT CONTROL BOX IAW 33-51-00.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 45,355 hrs · 48,949 cycles

FWD FUSELAGE ACCESS HOLE 122AR UPPER FWD CORNER SCREW HOLE ELONGATED.

Part: SKIN — DENTED (BS 324) · airframe 45,355 hrs · 48,949 cycles

TWO DENTS ON FUSELAGE SKIN, ONE AT BS 324.5, 1.5 INCHES ABOVE STRINGER 4L AND ONE AT BS 324.5, 2.5 INCHES ABOVE STRINGER 4L.

Part: SKIN — DENTED (VERTICAL STAB) · airframe 45,355 hrs · 48,949 cycles

VERTICAL STABILIZER, LT SKIN DENTED

Part: PANEL — CHAFED (FUSELAGE) · airframe 45,355 hrs · 48,949 cycles

WEAR DAMAGE ON LT WING TO FUSELAGE PANEL ALONG THE LOWER EDGE.

Part: SKIN — DENTED (LT NACELLE) · airframe 45,355 hrs · 48,949 cycles

DENTS ON LT NACELLE OUTBOARD COWLING 413AL

Part: SKIN — DENTED (FUSELAGE) · airframe 45,355 hrs · 48,949 cycles

MULTIPLE DENTS FOUND ON SKIN BTW STA X590 TO X600 & BTW STR 23S AND 24S.

Part: PANEL — CORRODED (ZONE 600) · airframe 45,355 hrs · 48,949 cycles

CORROSION IN COUNTERSINK SCREW HOLES OF STRESS PANEL.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,355 hrs · 48,949 cycles

ON RT FUSELAGE BETWEEEN STA X488.00 AND 532.00 STR 30S FOUND CORRODED.

Part: SKIN — DENTED (RUDDER) · airframe 45,355 hrs · 48,949 cycles

DENT FOUND ON LT SKIN OF TRAILING RUDDER BETWEEN RIBS 25-26, AFT OF REAR SPAR

Part: SKIN — DENTED (RUDDER) · airframe 45,355 hrs · 48,949 cycles

DENT FOUND ON LTH TRAILING RUDDER BETWEEN RIBS 13-14, AT FRONT SPAR

Part: SKIN — DENTED (RUDDER) · airframe 45,355 hrs · 48,949 cycles

DENT FOUND ON THE RT SKIN OF TRAILING RUDDER BETWEEN RIBS 22-23, AFT OF FRONT SPAR

Part: SKIN — DENTED (RUDDER) · airframe 45,355 hrs · 48,949 cycles

DENT FOUND ON LT SKIN OF TRAILING RUDDER BETWEEN RIBS 7-8, AFT OF FRONT SPAR

Part: STRAP — CHAFED (BS 253) · airframe 45,355 hrs · 48,949 cycles

MAIN ENTRANCE, AFT FRAME STRAP CHAFED AT BS 252.3 AND FLOOR LEVEL 100.3

Part: SKIN — DENTED (RUDDER) · airframe 45,355 hrs · 48,949 cycles

DENT FOUND ON THE RT SKIN OF TRAILING RUDDER BETWEEN RIBS 6-7 ONE INCH AFT OF FRONT SPAR

Part: FRAME — CHAFED (BS 387) · airframe 45,355 hrs · 48,949 cycles

LEFT FWD LOWER MAIN FRAME CHAFED.

Part: SKIN — DENTED (RUDDER) · airframe 45,355 hrs · 48,949 cycles

DENT FOUND ON LT SKIN OF TRAILING RUDDER BETWEEN RIBS 26-27 AND BETWEEN FRONT SPAR AND REAR SPAR

Part: SKIN — DENTED (RUDDER) · airframe 45,355 hrs · 48,949 cycles

DENT FOUND ON RT SKIN OF TRAILING RUDDER BTW RIBS 6-7 AT ONE INCH AFT OF REAR SPAR

Part: SKIN — DENTED (RUDDER) · airframe 45,355 hrs · 48,949 cycles

DENT FOUND ON RT SKIN OF TRAILING RUDDER BETWEEN RIBS 5-6, 7 INCHES AFT OF FRONT SPAR

Part: TAB — DENTED (RT ELEVATOR) · airframe 45,355 hrs · 48,949 cycles

RIGHT ELEVATOR SPRING TAB BETWEEN YH6 AND YH16 DENTED.

Part: ACTUATOR — DAMAGED (PROPELLER) · airframe 44,160 hrs · 47,437 cycles

NR 1 ENGINE OIL PRESSURE DROPPED BELOW 40 PSI AND THE NR 1 ENGINE WAS SHUTDOWN. R & R THE NR 1 PROPELLER ACTUATOR DUE TO DOME PISTON SEALING SURFACE DAMAGED IAW CMM 61-13-02.

Part: SEAL — FAILED (PROP SHAFT) · airframe 44,125 hrs · 47,434 cycles

SHUT DOWN NR 1 ENGINE DUE TO LOW OIL PRESSURE, DETERMINED LEAK AT PROP SHAFT SEAL.

Part: WIRE — DAMAGED (IGNITION SYS) · airframe 41,334 hrs · 44,026 cycles

SCC-1430L AVIONICS COOLING FAN INOP. (FIRE/SMOKE INFLIGHT AIR TURNBACK). AVIONICS COOLING FAN DEFERRED AND THEN REPLACED WHEN AIRCRAFT RETURNED TO BASE. UPON FURTHER INVESTIGATION FOUND NR 2 ENGINE AUTO IGNITION SYSTEM INOP. REPAIRED WIRE 20004A20 IN 2 PLACES, ONE AT 2' BEHIND NR 2 NH INDICATOR. ANOTHER AT CLOSET CEILING UNDER PA AMP WERE IT RUBBED THROUGH. TEST GOOD MM# 74-00-00. AUTO IGNITION WIRES ARE BELIEVED TO BE THE ORIGINAL CAUSE OF THE SMOKE IN CABIN.

Part: SKIN PANEL — DENTED (RT NACELLE) · airframe 41,261 hrs · 43,945 cycles

DENT DAMAGE TO RH NACELLE COWL DOOR/ACCESS DOOR BETWEEN XN80.10 AND XN88.05. REPAIRED WITH DOUBLER PATCH IAW ECO 008.54-15.05

Part: WEB — CRACKED (LT NACELLE) · airframe 41,261 hrs · 43,945 cycles

CRACK DAMAGE TO LT FWD FLANGED WEB ON ENGINE HORSECOLLAR ASSY PN 85410012-001. REPAIRED WITH DOUBLER PATCH IAW ECO 008.54-15.02

Part: WEB — CRACKED (LT NACELLE) · airframe 41,261 hrs · 43,945 cycles

CRACK DAMAGE ON LT ENGINE HORSECOLLAR AFT WEB PN 85410012-001. REMOVED DAMAGE AND APPLIED DOUBLERS IAW ECO 008.54-15.02

Part: MOUNT BRACKET — CRACKED (ZONE 400) · airframe 41,261 hrs · 43,945 cycles

CRACK DAMAGE TO I/B TRACK MOUNT IN 2 PLACES. WELDED REPAIR IAW BOMBARDIER RD 8-78-149.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 41,261 hrs · 43,945 cycles

CRACK DAMAGE TO LT SIDEWALL BOX VERTICAL Z MEMBER. REMOVED DAMAGES PORTION REPAIRED IAW ECO 008.53-15.44

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 41,261 hrs · 43,945 cycles

DENT DAMAGE TO RT AFT FUSELAGE STA 581 STR 25S - 26S. REPAIRED WITH PERMANENT DENT ALLOWANCE IAW ECO 008.53-15.38

Part: FRAME — CORRODED (LT NACELLE) · corrosion level 2 · airframe 41,261 hrs · 43,945 cycles

AFT LOWER FRAME ON LT FINGERNAIL CORRODED REPAIRED FRAME STRUCTURE WITH NEW PARTS IAW SRM 51-42-05. WP449 WC 4067

Part: ACCESS DOOR — DENTED (LT NACELLE) · airframe 41,261 hrs · 43,945 cycles

DENT DAMAGE TO LT NACELLE ACCESS DOOR 415AL ABOVE MIDDLE LATCH. ALLOWANCE OF DENT DAMAGE IAW ECO 008.54-15.03

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 41,261 hrs · 43,945 cycles

DENT DAMAGE TO REAR FUSELAGE OUT OF LIMITS FOR SRM OR GENERIC REPAIRS. REPAIRED DENT IAW ECO 008.53-15.42

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,261 hrs · 43,945 cycles

CORROSION DAMAGE TO STR 31 AT FUSELAGE STATION X195. REMOVED AND REPLACED TENSION ANGLE AND BLENDED STRINGER IAW SRM 51-42-16.

Part: SKIN PANEL — DENTED (VERTICAL STAB) · airframe 41,261 hrs · 43,945 cycles

DENT DAMAGE TO RT SIDE OF VERTICAL STABILIZER SKIN PANEL 85530011. DENT ALLOWANCE REPAIRED IAW ECO 008.55-15.01

Part: SKIN PANEL — DENTED (RT ELEVATOR) · airframe 41,261 hrs · 43,945 cycles

RT ELEVATOR TAILING EDGE SKIN DENTED NEAR STATIC WIC. REPLACED ELEVATOR TRAILING SKIN IAW SRM 51-42-45 AND DWG 85520058, DWG 85520179.

Part: SKIN PANEL — DENTED (VERTICAL STAB) · airframe 41,261 hrs · 43,945 cycles

DENT DAMAGE TO LT VERTICAL STABILIZER LOWER SKIN PANEL FRONT SPAR AND MAIN SPAR AND RIB NR 7. REPAIRED WITH PERMANENT DENT ALLOWANCE IAW ECO 008-55-15.02

Part: LUG — WORN (RUDDER) · airframe 41,261 hrs · 43,945 cycles

FORE RUDDER UPPER AND LOWER ACTUATOR LUGS WORN. BLENDED LUGS ON FORE RUDDER HINGE ASSSEMBLY IAW BOMBARDIER RD 8-55-128.

Part: SKIN PANEL — DENTED (RUDDER) · airframe 41,261 hrs · 43,945 cycles

DENT DAMAGE TO RT FORE RUDDER PN 85540001-003. REPAIRED WITH PERMANENT DENT ALLOWANCE IAW ECO 008.27-15.01

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 41,261 hrs · 43,945 cycles

DENT DAMAGE TO LT FUSELAGE SKIN PANEL 85320313. REPAIRED WITH PERMANENT DENT ALLOWANCE IAW ECO 008-53-15.41

Part: SKIN — GOUGED (TE FLAP) · airframe 41,261 hrs · 43,945 cycles

GOUGE DAMAGE TO TOP LT OUTBOARD FLAP SKIN AND FLAP STRINGER NR 2 APPLIED PATCH REPAIR IAW ECO 008.27-15.02

Part: SKIN PANEL — DENTED (LT AILERON) · airframe 41,261 hrs · 43,945 cycles

DENT DAMAGE TO LT AILERON TOP SKIN BETWEEN AILERON FRONT SPAR AND REAR SPAR. PERMANENT ALLOWANCE FOR DENT DAMAGE REPAIRED IAW ECO 008.27-15.03

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 41,261 hrs · 43,945 cycles

DENT DAMAGE TO RT FUSELAGE SKIN PANEL PN 85310533. REPAIRED WITH PERMANENT DENT ALLOWANCE IAW ECO 008.53-15.43

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 41,261 hrs · 43,945 cycles

DENT DAMAGE TO LT FUSELAGE SKIN PANEL 85330103, X600 - X606 STR 27P-28P. REPAIRED PERMANENT DENT ALLOWANCE IAW ECO 008.53-15.39

Part: SKIN PANEL — CORRODED (LT NACELLE) · corrosion level 2 · airframe 41,261 hrs · 43,945 cycles

CORROSION DAMAGE TO LT NACELLE SKIN OUTBOARD SKIN REMOVED AND REPLACED IAW SRM 51-42-45.

Part: TAB HINGE — DENTED (LT AILERON) · airframe 41,261 hrs · 43,945 cycles

DENT DAMAGE TO AILERON TAB HINGE 85740059 YW435.30. HINGE REWORKED TO TAKE OVERSIZE BUSHING IAW ECO 008.27-15.04

Part: INTERCOSTAL — CRACKED (RT WING) · airframe 41,261 hrs · 43,945 cycles

GEAR WELL CRACKED HAND PUMP STORAGE BRACKET. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-42-05 WP 449 WC 9009

Part: FRAME — CHAFED (FUSELAGE) · airframe 41,261 hrs · 43,945 cycles

CHAFE DAMAGE TO LT FRONT SPAR FRAME PN 85320882 AND 85320883. REPAIRED BY PERMANENT CHAFE ALLOWANCE IAW ECO 008.53-15.40

Part: SKIN PANEL — DENTED (PAX DOOR) · airframe 41,261 hrs · 43,945 cycles

DENT DAMAGE TO PAX DOOR OUTER SKIN PANEL 85210021. PERMANENT ALLOWANCE IAW ECO 008.52-15.02

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 41,261 hrs · 43,945 cycles

NLG BOS SIDEWALL CRACKED VERTICAL Z MEMBER RT. CUT AND REMOVE DAMAGED PORTION OF THE MEMBER, NDT ENSURE REMAINING STRUCTURE IS CRACK FREE, INSTALL REPAIR CHANNEL AND REPRODUCTION BARE AREAS IAW 8-53-1676. ECO 008.53-15.48

Part: SKIN PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 41,261 hrs · 43,945 cycles

CORROSION DAMAGE AT 277 LOCATIONS ON STRESS PANELS 524AT PN 85710023 SN FI18355, 624AT PN 85710023-004 SN F18343, 524CT PN 85710025-003 SN FI8337D, 521AT PN 85711101-003 SN FI8331, 523AT PN 85711094 SN FI6335-2, 623AT PN 85711094-003 SN F18337-2, 522AT PN 85711802-005 SN F1489321, 622AT PN 85711802-005 SN F1489331, 524BT PN 85710024-003 SN F18337C, 624BT PN 85710024-004 SN F118341C. REPAIRED CORROSION IAW BOMBARDIER RD 8-57-1420, 8-57-2673.

Part: SMOKE DETECTOR — FALSE ACTIVATION (ZONE 200) · airframe 40,933 hrs · 43,589 cycles

SMOKE LIGHT. UNABLE TO VERIFY PROBLEM, TESTED OK WITH SMOKE AND CHECKED ALL CONNECTIONS, REPLACED THE LAMP BEACON IN BOTH SMOKE DETECTORS AND GROUND TEST GOOD IAW MM 26-12-01.

Part: SMOKE DETECTOR — DEFECTIVE (ZONE 200) · airframe 40,871 hrs · 43,527 cycles

SMOKE WARNING LIGHT ILLUMINATED INTERMITTENTLY DURING FLIGHT. REMOVED AND REPLACED THE NR 1 AND 2 SMOKE DETECTORS IAW AMM 26-12-01 OPS CHECKED GOOD. OK FOR SERVICE.

Part: SMOKE DETECTOR — FALSE INDICATION (ZONE 200) · airframe 40,511 hrs · 43,151 cycles

SMOKE WARNING LIGHT ILLUMINATED ON DESCENT INTO SCC. WAS ON FOR 2 MINUTES THEN EXTINGUISHED.

Part: SWITCH — DEFECTIVE (SPOILER) · airframe 39,861 hrs · 42,418 cycles

FLIGHT SPOILER 1 PUSH OFF LIGHT ILLUMINATED IN FLIGHT. R & R LT & RT INBD SPOILER CLUTCH SWITCHES IAW MM 27-14-38. OPERATIONS CHECKED GOOD. OK FOR CONTINUED SERVICE.

Part: SKIN — CRACKED (LT AILERON) · airframe 39,351 hrs · 41,712 cycles

LEFT AILERON LOWER SKIN FOUND CRACKED AT AFT EDGE AROUND OTBD SPRING TAB HINGE AT SAT YW 47. REPAIR WITH PATCH AT AFT EDGE AROUND OTBD SPRING TAB HINGE AREA YW 471 IAW RD 8-27-017 REV 2.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 39,351 hrs · 41,712 cycles

DENT DAMAGE TO AFT FUSELAGE LOWER SKIN PANEL 85530014 LOCATED AFT OF ACCESS DOOR AT MID SPAR BETWEEN STRINGER 29P - 29S. REPAIRED WITH PATCH IAW 8-55-2680.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 39,351 hrs · 41,712 cycles

DENT AT X 291.4 - X 333.3, STRINGER 30P & 31P. REPAIRED TO RD 8-53-13611.

Part: STOP FITTING — CHAFED (ZONE 200) · airframe 39,351 hrs · 41,712 cycles

AT CARGO DOOR SURROUND STRUCTURE BOTH UPPER DOOR STOP FITTINGS FOUND CHAFED. REPAIRED IAW RD 8-53-7447 & WC 53-5764.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,351 hrs · 41,712 cycles

CORROSION FOUND AT FRAME BETWEEN STRINGER 21P - 22P, STATION 545.0. REMOVED CORROSION IAW SRM CARD 53-3005.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,351 hrs · 41,712 cycles

CORROSION FOUND AT FRAME BETWEEN STRINGER 21 - 22 RT SIDE SAT 539. REMOVED CORROSION IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 39,351 hrs · 41,712 cycles

CORROSION FOUND AT WEB STATION 649.897, BL 9.25, REMOVED IAW SRM WORK CARD 53-3002.