N462AW

Part: SKIN — DAMAGED (BS 409) · airframe 37,656 hrs · 36,317 cycles

SCRIBE MARKS TOP FUSELAGE FS 409.00+80 +4.5 TO 409+80+7 S0+2R TO S0.2L ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SCRIBE MARKS TOP FUSELAGE FS 409.00+80 +4.5 TO 409+80+7 S0+2R TO S0.2L,AT ORIGINAL THICKNESS OF 0.058Ï¿½ BLEND MEASURED 2.0Ï¿½L X 1.5Ï¿½W X .005Ï¿½D. LOSS 0.005Ï¿½ REMAINING 0.053Ï¿½. WHERE CHEM MILLED THICKNESS IS 0.045Ï¿½ BLEND IS 3.5Ï¿½L X 2.0Ï¿½W X 0.002Ï¿½D. REMAINING 0.043Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. BLENDS ARE WITHIN LIMITS AND ALL WORK ACCOMPLISHED IAW ASAP EA# AWAC-CRJ253-01618 REV B DATED 4/29/2021. DTE HAS BEEN COMPLETED AND DTA IS REQUIRED TO BE COMPLETED WITHIN 12 MONTHS.

Part: SKIN — CRACKED (BS 589-621) · airframe 37,656 hrs · 36,317 cycles

DURING EDDY CURRENT INSPECTION OF CUT-LINE OF PREVIOUS REPAIR OF SKIN AT FS589.00 Ï¿½ FS621.00 BETWEEN STR 23L AND STR 27L, 1 INDICATION NOTED EMANATING FROM CUT-LINE ADJACENT TO STR 23L 1.0Ï¿½ FORWARD OF FRAME AT FS605 MEASURING 0.175" FWD OF FS605 AND BELOW STR23L ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED REPAIR CUT-OUT ADJACENT TO STR 23L FORWARD OF FS605.00+1.0 BY REMOVING EXISTING REPAIR AND INSTALLING NEW DOUBLER AND TRIPLER IAW ASAP EA# AWAC-CRJ253-01611 REV IR DATED 5/10/2021

Part: SKIN — CORRODED (LEFT WING) · corrosion level 2 · airframe 37,656 hrs · 36,317 cycles

LEFT WING LOWER WING PLANK ACCESS HOLE CUT-OUT AT PANEL 540BB HAS FRETTING CORROSION AT SEVERAL LOCATIONS AROUND CIRCUMFERENCE. INITIATE AWAC E06/021-457 CURRENT REVISION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED FRETTING CORROSION ON INBOARD (P1) AND OUTBOARD (P2) FLANGE OF PANEL 540BB ACCESS HOLE. P1) 10.200Ï¿½L X 0.500Ï¿½W X 0.016Ï¿½ D, REMAINING 0.166Ï¿½. P2) 8.400Ï¿½L X 0.500Ï¿½W X 0.011Ï¿½D, REMAINING 0.171Ï¿½. BLENDED AREAS WITHIN LIMITS, HFEC PERFORMED WITH NO INDICATIONS ROTO PEENED AND PROTECTIVE FINISH RESTORED, REF EO#E06/021/457 REV D DATED12/20/2018 AND REO 601-57-21-030 REV L DATED 2014/02/05.

Part: RETAINER — GOUGED (RT WINDSHEILD) · airframe 37,656 hrs · 36,317 cycles

STRAP JUST ABOVE FRONT RIGHT WINDSHIELD OUTBOARD VERTICAL RETAINER HAS A GOUGE WL 128.85 RBL 1. AIRCRAFT REMOVED FROM SERVICE BLENDED DAMAGE TO A SMOOTH CONTOUR, PERFORMED HFEC WITH NO INDICATIONS, ROTO PEENED REWORK AREA AND APPLIED PROTECTIVE FINISH IAW REO 601R-53-11-3686 REV.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 37,656 hrs · 36,317 cycles

RIGHT LOWER WING PLANK ACCESS HOLE CUT-OUT AT PANEL 640BB HAS FRETTING CORROSION AT 2 LOCATIONS AROUND CIRCUMFERENCE. INITIATE AWAC E06/021-457 CURRENT REVISION. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED FRETTING CORROSION ON INBOARD (P1) & OUTBOARD (P2) FLANGE OF PANEL 640BB ACCESS HOLE AT 2 LOCATIONS, P1) 6.800Ï¿½ X 0.500 X 0.007Ï¿½D REM 0.175Ï¿½. P2) 9.100Ï¿½L X 0.500Ï¿½W X 0.003Ï¿½ D, REMAINING 0.179Ï¿½. BLENDED AREA WITHIN LIMITS, HFEC PERFORMED WITH NO INDICATIONS ROTO PEENED AND PROTECTIVE FINISH RESTORED, REF EO# E06/021/457 REV D DATED12/20/2018 AND REO 601-57-21-030 REV L DATED 2014/02/05.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 37,656 hrs · 36,317 cycles

RIGHT LOWER WING PLANK ACCESS HOLE CUT-OUT AT PANEL 640CB HAS 2 INDICATIONS AT FWD I/B ARC. INITIATE AWAC E06/021-457 CURRENT REVISION. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED INDICATIONS ON INBOARD FLANGE OF PANEL 640CB ACCESS HOLE, MEASURING 6.100Ï¿½L X 0.500Ï¿½W X 0.019Ï¿½ D, REMAINING 0.163Ï¿½. BLENDED AREA WITHIN LIMITS, HFEC PERFORMED WITH NO INDICATIONS ROTO PEENED AND PROTECTIVE FINISH RESTORED, REF EO#E06/021/457 REV D DATED12/20/2018 AND REO 601-57-21-030 REV L DATED 2014/02/05

Part: SKIN — CORRODED (BS 409) · corrosion level 2 · airframe 37,656 hrs · 36,317 cycles

CORROSION TOP FUSELAGE FS 409.00+80 +4 S 0+3L ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION TOP FUSELAGE FS 409.00+80 +4 S 0+3L, 2.5Ï¿½L X 1.0Ï¿½W X .003Ï¿½D. ORIGINAL MATERIAL 0.045Ï¿½, LOSS 0.003Ï¿½ REMAINING 0.042Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. BLEND IS WITHIN LIMITS AND ALL WORK ACCOMPLISHED IAW ASAP EA# AWAC-CRJ253-01618 REV B DATED 4/29/2021. DTE HAS BEEN COMPLETED AND DTA IS REQUIRED TO BE COMPLETED WITHIN 12 MONTHS.

Part: SKIN — CORRODED (BS 409) · corrosion level 2 · airframe 37,656 hrs · 36,317 cycles

CORROSION TOP FUSELAGE FS 409.00+80 +2.5 S 0+3R ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION TOP FUSELAGE FS 409.00+80 +2.5 S 0+3R, 4.0Ï¿½L X 5.0Ï¿½W X .005Ï¿½D. ORIGINAL MATERIAL 0.058Ï¿½, LOSS 0.005Ï¿½ REMAINING 0.053Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. BLEND IS WITHIN LIMITS AND ALL WORK ACCOMPLISHED IAW ASAP EA# AWAC-CRJ253-01618 REV B DATED 4/29/2021. DTE HAS BEEN COMPLETED AND DTA IS REQUIRED TO BE COMPLETED WITHIN 12 MONTHS.

Part: ANGLE — CORRODED (LT WING) · corrosion level 2 · airframe 37,656 hrs · 36,317 cycles

LEFT WING REAR SPAR AT WS 53-60 INBOARD DOUBLER/ ANGLE HAS CORROSION AROUND UPPER AND LOWER ELECTRICAL CONNECTOR HOLES. ***AIRCRAFT REMOVED FROM SERVICE*** FOUND AND BLENDED CORROSION IN 3 PLACES ON LEFT WING REAR SPAR AT WS 53-60 INBOARD ANGLE. P1) 5.800Ï¿½L X 0.900Ï¿½W X 0.003Ï¿½D P2) 1.500Ï¿½L X 4.700Ï¿½W X 0.001Ï¿½D P3) 0.100Ï¿½L X 2.000Ï¿½W X 0.003Ï¿½D. ORIGINAL THICKNESS 0.080Ï¿½. ALL BLENDS WITHIN LIMITS IAW ASAP EA# AWAC-CRJ257-01613REV IR DATED 4/26/2021

Part: RIB — CORRODED (S53.60) · corrosion level 2 · airframe 37,656 hrs · 36,317 cycles

RIGHT WING REAR SPAR RIB AT WS 53.60 INBOARD DOUBLER HAS CORROSION AROUND UPPER AND LOWER ELECTRICAL CONNECTOR HOLES AND AROUND NUTPLATE HOLES (3 EACH). ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM RIGHT WING REAR SPAR RIB AT WS 53.60 INBOARD DOUBLER, UPPER AND LOWER ELECTRICAL CONNECTOR HOLES AND AROUND NUTPLATE HOLES (3 EACH), ALL BLENDS WITHIN LIMITS, PROTECTIVE FINISH REINSTALLED. ALL WORK ACCOMPLISHED IAW ASAP EA# AWAC-CRJ257-01614 REV IR DATED 4/26/2021. DTE IS COMPLETED NO DTA REQUIRED.

Part: ANGLE — CORRODED (RT WING) · corrosion level 2 · airframe 37,656 hrs · 36,317 cycles

RIGHT WING REAR SPAR WS 53.60 INBOARD UPPER ANGLE HAS CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION FROM RIGHT WING REAR SPAR WS 53.60 INBOARD UPPER ANGLE BLENDS WITHIN LIMITS IAW ASAP EA# AWAC-CRJ257-01616 REV IR DATED 4/27/2021. DTE IS COMPLETED NO DTA REQUIRED.

Part: WEB — CORRODED (RT WING) · corrosion level 2 · airframe 37,656 hrs · 36,317 cycles

RIGHT WING REAR SPAR RIB AT WS 53.60 AFT UPPER ANGLE HAS CORROSION. ***AIRCRAFT WAS REMOVED FROM SERVICE*** REMOVED CORROSION ON R/H WING REAR SPAR AT WS 53.60 AFT WEB, ARE MEASURES 1.50Ï¿½L X 0.10Ï¿½W X 0.004Ï¿½D, ORIGINAL THICKNESS 0.050Ï¿½, REMAINING 0.046Ï¿½. WITHIN LIMITS, IAW ASAP EA# AWAC-CRJ257-01615REV A DATED 4/27/2021.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 37,656 hrs · 36,317 cycles

LEFT WING REAR SPAR RIB AT WS 48.30 HAS CORROSION BELOW UPPER LIGHTING HOLE. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON LH WING REAR SPAR AT WS 48.30 BELOW UPPER LIGHTING HOLE, MEASUREMENTS ARE 0.800"L X 0.700"W X 0.002"D. REMAINING THICKNESS IS 0.048". REPAIR WITHIN LIMITS REF ASAP ES# AWAC-CRJ257-01612 REV IR DATED 4/26/2021.

Part: STRAP — DAMAGED (RT WINGLET) · airframe 37,656 hrs · 36,317 cycles

RIGHT WING TIP WHERE PANEL 671JT ATTACHES HAS SCRIBE MARKS ON THE UPPER AND LOWER SURFACES, 9 AREAS IN ALL. ***AIRCRAFT REMOVED FROM SERVICE***1) LOWER RT WINGLET DOUBLER, PN 600-10380-64 REPAIRED IAW ASAP EA# AWAC-CRJ257-01620 REV A DATED 5/5/2021. FCBS IS NOT AFFECTED. NO DTA IS REQUIRED.2) UPPER RT WINGLET DOUBLER, PN 600-10380-60 REPAIRED IAW ASAP EA# AWAC-CRJ257-01621 REV A DATED 5/5/2021. FCBS IS NOT AFFECTED. NO DTA IS REQUIRED.3) FWD LWR OB FAIRING RT WINGLET STRAP PN 600-10388, REPAIRED IAW ASAP EA# AWAC-CRJ257-01622 REV IR DATED 5/2/2021. FCBS IS NOT AFFECTED. NO DTA IS REQUIRED4) LWR OB SKIN, RT WINGLET STRAP, PN 600-15108-5, REPAIRED IAW ASAP EA# AWAC-CRJ257-01623 REV IR DATED 5/2/2021. FCBS IS NOT AFFECTED. NO DTA IS REQUIRED.5) FWD IB FAIRING RT WINGLET STRAP, PN 600-10388, REPAIRED IAW ASAP EA# AWAC-CRJ257-01624 REV IR DATED 5/2/2021. FCBS IS NOT AFFECTED. NO DTA IS REQUIRED.6) LWR IB SKIN RT WINGLET STRAP PN 600-15108-18, REPAIRED IAW ASAP EA# AWAC-CRJ257-01625 REV IR DATED 5/2/2021. FCBS IS NOT AFFECTED. NO DTA IS REQUIRED.7) FWD ON SKIN RT WINGLET STRAP PN 600-15108-7, REPAIRED IAW ASAP EA# AWAC-CRJ257-01626 REV IR DATED 5/2/2021. FCBS IS NOT AFFECTED. NO DTA IS REQUIRED.8) FWD IB SKING RT WINGLET STRAP PN 600-15108-16, REPAIRED IAW ASAP EA# AWAC-CRJ257-01627 REV IR DATED 5/2/2021. FCBS IS NOT AFFECTED. NO DTA IS REQUIRED.9) LWR LE RT WINGLET BRACKET PN 600-15111, REPAIRED IAW ASAP EA# AWAC-CRJ257-01628 REV IR DATED 5/2/2021. FCBS IS NOT AFFECTED. NO DTA IS REQUIRED.BLENDS (ALL WITHIN LIMITS), THICKNESS CHECKS AND HFEC (NO INDICATIONS NOTED) COMPLIED WITH IAW APPLICABLE EAÏ¿½S.

Part: SKIN — DENTED (BS 580 S30L) · airframe 37,656 hrs · 36,617 cycles

AFT FUSELAGE SKIN DENT AT FS580.0 AND STR L20+2.5. ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED DENT AT FS580 LEFT HAND AT STR 20+2.5, PERFORMED HFEC NO INDICATIONS NOTED. REPAIR WITHIN LIMITS REF ASAP EA# AWAC-CRJ253-01608 REV A DATED 4/22/2021.

Part: SKIN — DENTED (BS 672 S23R) · airframe 37,656 hrs · 36,317 cycles

AFT FUSELAGE SKIN DENT FS 672.20+2 AND S23+3R ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED DENT AT FS672.20+2 AND S23+2R IAW ASAP EA# AWAC CRJ253-01606 REV IR DATED 4/27/2021.

Part: SKIN — DENTED (BS 691 S23L) · airframe 37,656 hrs · 36,317 cycles

AFT FUSELAGE SKIN DENT AT FS 691.0 STR 23+2L ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED FUSELAGE DENT AT FS 691.0 STR 23+2L TO ORIGINAL CONTOUR IAW ASAP EA# AWAC-CRJ253-01607 REV IR DATED 4/21/2021.

Part: SKIN — DENTED (BS 636-638 L26L) · airframe 37,656 hrs · 36,317 cycles

AFT FUSELAGE SKIN DENT FS 636-638 STR 26+1.5 TO 26+3L ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED 2 DENTS TO ORIGINAL CONTOUR AT FS636-638 STR 26+1.5 TO 26+3L IAW ASAP EA# AWAC CRJ253-01609 REV IR DATED 04/21/2021.

Part: SKIN — DENTED (BS 654.S22L) · airframe 37,656 hrs · 36,317 cycles

AFT FUSELAGE SKIN DENT FS654.50+8 STR22+3.5L ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED DENT AT AFT FUSELAGE SKIN DENT FS654.50+8 STR22+3.5L IAW CRJ SRM 53-00-31 REPAIR #3 REV 38.

Part: SKIN — DENTED (BS 692) · airframe 37,656 hrs · 36,317 cycles

AFT FUSELAGE SKIN DENT LH FS692.5 STR 23+4L ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED DENT AT LH FS693.5 AND STR 23+4L IAW ASAP ENGINEERING REV IR DATED 4/21/2021

Part: CONTROL HANDLE — FAULTED (LD GEAR CONTROL) · airframe 37,476 hrs · 36,124 cycles

AFTER TAKEOFF RECEIVED A SKID INBD CAUTION MSG FOLLOWED BY PARKING BRAKE SOV CAUTION MSG GEAR WOULD NOT RETRACT. Q/W QRH. AFTER SELECTING GEAR DOWN ALL MESSAGES CLEARED. NO GEAR DISAGREE MSG AND ALL INDICATIONS GREEN. GEAR HANDLE WAS IN UP FOR APPROX 7 MIN. AIRCRAFT REMOVED FROM SERVICE. R & R LANDING GEAR CONTROL HANDLE IAW AMM 32-31-01. OPS CHECK GOOD.

Part: IDG — MALFUNCTIONED (NR 3 ENGINE) · airframe 36,653 hrs · 35,291 cycles

SUPPLEMENTAL, RECEIVED NR 2 GEN CAUTION MESSAGE WITH DISCONNECT INDICATION, ALSO RECEIVED RIGHT WINDOW HEAT CAUTION MESSAGE AIRCRAFT REMOVED FROM SERVICE. COMPLIED WITH M ACTION FOR MEL 24-11-01-01 AND PLACED IDG GEN NR 2 ON MEL. PERFORMED FIM RESET PROCEDURE FOR WINDOW MESSAGE. MESSAGE CLEARED. R&R RIGHT ENGINE IDG REF AMM 24-11-01. OPS CHECK GOOD. LEAK CHECK GOOD. REMOVED PLACARD. REMOVED FROM MEL. SN OFF 1851/4765 SN ON 1800/4682.

Part: PANEL — DAMAGED (HORIZ STAB) · airframe 35,333 hrs · 34,063 cycles

PANEL 342BB HAS ONE DAMAGED FASTENER HOLE.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 35,333 hrs · 34,063 cycles

PRESSURE FLOOR INTERCOSTAL AT FS 484 RBL 27-RBL 36 IS CRACKED AT O/B SIDE REPAIRED PRESSURE FLOOR INTERCOSTAL AT FS 484 RBL 27 - RBL 36 IAW ASAP EA#: AWAC-CRJ253-01224 REV IR

Part: FLOORBEAM — CRACKED (BS 484) · airframe 35,333 hrs · 34,063 cycles

PRESSURE FLOOR INTERCOSTAL AT FS 484 LBL27-LBL36 IS CRACKED O/B SIDE REPAIRED PRESSURE FLOOR INTERCOSTAL AT FS 484 LBL27-LBL36 IAW ASAP EA# AWAC-CRJ253-01225 REV 1R

Part: INTERCOSTAL — CRACKED (BS 340-349) · airframe 35,333 hrs · 34,063 cycles

PAX DOOR UPPER FOWARD INTERCOSTAL CRACKED REMOVED AND REPLACED PAX DOOR UPPER FWD INTERCOSTAL IAW CRJ 200 SRM 51-42-06 AND 51-42-21

Part: INTERCOSTAL — CRACKED (BS 310-320) · airframe 35,333 hrs · 34,063 cycles

PASSENGER DOOR UPPER AFT INTERCOSTAL CRACKED REMOVED AND REPLACED PASSENGER DOOR UPPER AFT INTERCOSTAL IAW CRJ 200 SRM 51-42-06 + 51-42-21

Part: BRACKET — CRACKED (BS 625.3) · airframe 35,333 hrs · 34,063 cycles

AFT CARGO DOOR BEAM MEMBER AFT BRACKET CRACKED REMOVED AND REPLACED AFT CARGO DOOR BEAM MEMBER AFT BRAKCET IAW CRJ 200 SRM 51-42-21

Part: RETAINER — CRACKED (BS 605-640) · airframe 35,333 hrs · 34,063 cycles

PANEL 422AT HAS CRACKED SEAL RETAINER REPAIRED CRACKED SEAL RETAINER ON PANEL 422AT IAW CRJ 200 SRM 51-71-59

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 35,333 hrs · 34,063 cycles

BAGGAGE DOOR LINTEL INTERCOSTAL CRACKED REPAIRED LINTEL INTERCOSTAL IAW BOMBARDIER REO# 601R-53-61-1230 REV F

Part: SHIM — DAMAGED (BS 621) · airframe 35,333 hrs · 34,063 cycles

GS621 APB REPAIR AT BAGGAGE DOOR LINTEL, POCKET SHIM DAMAGED AT ONE OFF NON REPAIR BLIND FASTENER USED TO ATTACH POST TO BULKHEAD LINERS. REPLACED LINTEL FITTING REPAIR POCKET SHIM IAW REO 601R-53-61-1230 REV-F.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 35,333 hrs · 34,063 cycles

RBL9 SEAT TRACK CORRODED. REPLACED RBL9 SEAT TRACK #4 IAW CRJ200 AMM 53-01-11-000-802 AND 53-01-11-400-802.

Part: STIFFENER — CRACKED (BS 409 BULKHEAD) · airframe 35,333 hrs · 34,063 cycles

FS409+128 BULKHEAD VERTICAL POST AT LBL 18.0 O/B STIFFENER IS CRACKED AT BOTTOM FASTENER HOLE. REPAIRED VERTICAL POST STIFFENER IAW REO 601R-53-41-056 REV-E.

Part: SEAT TRACK — CORRODED (BS 409-559) · corrosion level 2 · airframe 35,333 hrs · 34,063 cycles

LBL9 SEAT TRACK #3 CORRODED. REPLACED SEAT TRACK IAW CRJ200 AMM 53-01-11-000-802, 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 35,333 hrs · 34,063 cycles

LBL9 SEAT TRACK #4 CORRODED AT FS559.00+4 TO 559.00+86. REPLACED SEAT TRACK IAW CRJ200 AMM 53-01-11-000-802, 53-01-11-400-802.

Part: STIFFENER — CRACKED (BS 621 BULKHEAD) · airframe 35,333 hrs · 34,063 cycles

FS621.00 APB HORIZONTAL STIFFENER O/B OF LBL36.20 IS CRACKED. REPLACED STIFFENER IAW CRJ 200 SRM 51-42-06.

Part: CHANNEL — CRACKED (BS 718) · airframe 35,333 hrs · 34,063 cycles

CHANNEL BEHIND HYD. SYS. 2 PRESSURE/RETURN MANIFOLD IS CRACKED. REPAIRED CHANNEL IAW REO 601R-53-62-031 REV-A.

Part: VERTICAL SUPPORT — CRACKED (BS 409) · airframe 35,333 hrs · 34,063 cycles

STA 409+128 VERTICAL POST CRACKED IN RADIUS. REPLACED VERTICAL POST IAW REO601R-53-41-889 REV-D AND CRJ200 SRM 51-42-06.

Part: RIB — CRACKED (RT WING) · airframe 35,333 hrs · 34,063 cycles

RH WING LEADING EDGE 630JL RIB IS CRACKED AT WS 247.95 REMOVED AND REPLACED RH WING LEADING EDGE RIB AT WS 247-95 IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-10

Part: VERTICAL SUPPORT — CRACKED (BS 409) · airframe 35,333 hrs · 34,063 cycles

STA 409+128 BL0, VERTICAL POST HAS A CRACK ON L/H SIDE AFT ANGLE, WL69. REPLACED VERTICAL POST IAW REO 601R-53-41-899 REV-D, CRJ200 SRM 51-42-06.

Part: DOOR FRAME — CRACKED (BS 605) · airframe 35,333 hrs · 34,063 cycles

AFT CARGO DOOR CUTOUT FRAME AT STR 9L HAS 2 CRACKS. REPAIRED FRAME IAW REO 601R-53-61-5214 REV-A.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 35,333 hrs · 34,063 cycles

SEAT TRACK #4 HAS CORROSION THE ENTIRE LENGTH OF THE TRACK, RBL9 REMOVED AND REPLACED #4 SEAT TRACK AT RBL 9 IAW CRJ 200 AMM 53-01-11

Part: RETAINER — CRACKED (BS 654-672) · airframe 35,333 hrs · 34,063 cycles

PANEL 442BT CRACKED SEAL RETAINER REMOVED AND REPLACED CRACKED SEAL RETAINER IAW CRJ 200 SRM 51-42-06

Part: SEAT TRACK — CORRODED (BS 349-379) · corrosion level 2 · airframe 35,333 hrs · 34,063 cycles

SEAT TRACK #1 RBL 9 HAS CORROSION THE ENTIRE LENGTH OF THE TRACK REMOVED AND REPLACED SEAT TRACK #1 LOCATION RBL9 IAW CRJ 200 AMM 53-01-11

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 35,333 hrs · 34,063 cycles

PRESSURE FLOOR SUPPORT INTERCOSTAL OUTBD CLIP AT FS484 RBL 36 CRACKED. REPLACED

Part: ANGLE — CRACKED (BS 280) · airframe 35,333 hrs · 34,063 cycles

PREVIOUS REPAIR ANGLE AFT FACE OF STA 280 AND RBL 12 CRACKED. REPLACED

Part: SKIN — CRACKED (PAX DOOR) · airframe 35,333 hrs · 34,063 cycles

PAX DOOR LOWER CLOSE OUT SKIN IS CRACKED UNDER TOP FOLDING STEP. REPAIRED

Part: ANGLE — CRACKED (BS 473) · airframe 35,333 hrs · 34,063 cycles

RH OVER WING BL 45 FS 473 REINFORCING ANGLE CRACKED. REPLACED

Part: ANGLE — CRACKED (BS 473) · airframe 35,333 hrs · 34,063 cycles

LH OVER WING BL 45 FS 473 REINFORCING ANGLE CRACKED. REPLACED

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 35,333 hrs · 34,063 cycles

AFT PRESSURE BULKHEAD FORWARD FACE HAS A CRACK EXTENDING FROM THE TOP END OF THE CARGO DOOR TRACK AS LBL 27.50 UPWARD APPROX. .75INCH. REPAIR

Part: BULKHEAD WEB — DAMAGED (BS 621) · airframe 34,719 hrs · 33,474 cycles

CHAFING MARKS ON AFT PRESSURE BULKEAD REQUIRING BLEND REPAIRS PER GREO601R-53-61-2155 AND DOUBLER REPAIRS PER GREO 601R-53-61-1285

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 33,457 hrs · 32,286 cycles

FLAPS FAILED WHEN SELECTING FLAPS OUT OF ZERO. PERFORMED A RESET PROCEDURE IAW 98-18G, BOX 12. FLAPS RESET. R & R THE LEFT AND RIGHT BPSU IAW AMM 27-51-10-05, OPS CHECKED GOOD, R & R THE FECU IAW AMM 27-51-05-05, OPS CHECKED GOOD, COMPLIED WITH 270261. ALL OPS CHECKS GOOD. ACFT OK FOR SERVICE.

Part: BPSU — MALFUNCTIONED (TE FLAP) · airframe 33,457 hrs · 32,286 cycles

FLAPS FAIL WHEN SELECTING FLAPS OUT OF ZERO. PERFORMED RESET PROCEDURE IAW SUP 98-18G BOX 12, FLAPS RESET. R&R LEFT AND RIGHT BPSU'S PER AMM 27-51-10-05, OPS CHECK GOOD. R&R FECU PER AMM 27-51-05-05, OPS CHECK GOOD. ALL OPS CHECK GOOD, A/C OK FOR SERVICE.

Part: ECU — MALFUNCTIONED (TE FLAP) · airframe 33,457 hrs · 32,286 cycles

FLAP FAIL CAUTION MESSAGE ON FINAL APPROACH WHEN FLAPS SELECTED ZERO TO 8 DEGREES. C/W QRH, LANDED WITHOUT INCIDENT. PERFORMED RESET PROCEDURE IAW SUP 98-18G BOX 12, FLAPS RESET. R&R LEFT AND RIGHT BPSU'S PER AMM 27-51-10-05 OPS CHECK GOOD R&R FECU PER AMM 27-51-05-05 OPS CHECK GOOD C/W. ALL OPS CHECK. GOOD A/C OK FOR SERVICE.

Part: BEAM — DAMAGED (BS 574-621) · airframe 32,644 hrs · 31,437 cycles

DURING RON MAINTENANCE THE CARGO DOOR BEAM WAS FOUND DAMAGED FROM CARGO DOOR ASSIST CABLE.

Part: RISER PANEL — CRACKED (PAX DOOR) · airframe 32,031 hrs · 30,876 cycles

PAX DOOR AFT RISER PANEL IS CRACKED BY THIRD STEP.

Part: FRAME — CRACKED (BS 333) · airframe 32,031 hrs · 30,876 cycles

FRAME BS 333 CRACKED FROM TOOLING HOLE BETWEEN STRINGER 0 AND 1L.

Part: FRAME — CORRODED (BS 310) · corrosion level 2 · airframe 32,031 hrs · 30,876 cycles

FRAME BS 310 HAS CORROSION ON THE FWD AND AFT SIDE BETWEEN STRINGERS 22R AND 23R

Part: HINGE — GOUGED (PAX DOOR) · airframe 32,031 hrs · 30,876 cycles

PAX DOOR PIANO HINGE ON FUSELAGE SIDE IS GOUGED AT MOST AFT LUG LANDING.

Part: INTERCOSTAL — CRACKED (BULKHEAD) · airframe 32,031 hrs · 30,876 cycles

REAR PRESSURE BULKHEAD LT INTERCOSTAL OTBD ANGLE IS CRACKED.

Part: CLEAT — CORRODED (DOOR SILL) · corrosion level 2 · airframe 32,031 hrs · 30,876 cycles

PAX DOOR LOWER SILL FWD CLEAT HAS CORROSION.

Part: CARGO TRACK — DAMAGED (BS 559) · corrosion level 2 · airframe 32,031 hrs · 30,876 cycles

CARGO TRACK IS CORRODED AND GOUGED AT BS 559+80 - 559+96, LBL 9.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · corrosion level 2 · airframe 32,031 hrs · 30,876 cycles

AFT CARGO FLOOR SUPPORT HAS CORROSION LBL 28 BS 559+80 - 621.

Part: SEAT TRACK — CORRODED (BS 544-599) · corrosion level 2 · airframe 32,031 hrs · 30,876 cycles

LEFT SIDEWALL SEAT TRACK HAS CORROSION BETWEEN BS 544 - 559+80 IN THE CABIN.

Part: CARGO TRACK — DAMAGED (BS 559) · corrosion level 2 · airframe 32,031 hrs · 30,876 cycles

CARGO TRACK CORRODED AND GOUGED.

Part: DOOR SILL — CORRODED (BS 310-349) · corrosion level 2 · airframe 32,031 hrs · 30,876 cycles

PAX DOOR LOWER SILL LOWER ANGLE HAS CORROSION ON THE INBD AND OTBD SIDE BETWEEN BS 310 AND 349.

Part: CARGO TRACK — DAMAGED (BS 559) · corrosion level 2 · airframe 32,031 hrs · 30,876 cycles

CARGO TRACK IS CORRODED AND GOUGED AT BS 559+80 TO 559+96, RBL 9.

Part: STIFFENER — CRACKED (NR 1 EXHAUST) · airframe 32,031 hrs · 30,876 cycles

NR 1 ENGINE EXHAUST NOZZLE 436AL ACCESS PANEL CAM LOCK SOCKET STIFFENER CRACKED. REPLACED THE STIFFENER IAW SRM 51-42-06.

Part: ANGLE — CRACKED · airframe 32,031 hrs · 30,876 cycles

OBLIQUE ANGLE INBD OF STRINGER 14 INTERCOSTAL IN AEB IS CRACKED. REPLACED THE ANGLE IAW SRM 51-42-21, 53-61-17, 51-41-11, AND 51-25-16.

Part: BRACKET — CRACKED (BS 449) · airframe 32,031 hrs · 30,876 cycles

LEFT LONGERON ASSY BRACKET FOR OVERWING ACCESS PANEL AT BS 449.85 IS CRACKED.

Part: BRACKET — CRACKED (BS 461) · airframe 32,031 hrs · 30,876 cycles

RIGHT LONGERON ASSY SUPPORT BRACKET FOR OVERWING ACCESS PANEL AT BS 461 IS CRACKED

Part: BRACKET — CRACKED (BS 449) · airframe 32,031 hrs · 30,876 cycles

1014336-1000-0035 - RH LONGERON SUPPORT BRACKET FOR OVERWING ACCESS PANEL AT BS 449.85 IS CRACKED

Part: FRAME — CORRODED (BS 333) · corrosion level 2 · airframe 32,031 hrs · 30,876 cycles

FRAME BS 333 CORRODED BETWEEN STRINGERS 25L AND 25R. REPLACED THE FRAME IAW EA 253-00679 REV-IR.

Part: STRAP — CORRODED (BS 559) · corrosion level 2 · airframe 32,031 hrs · 30,876 cycles

MAIN CABIN FLOORBEAM STRAP CORRODED. REPLACED THE STRAP IAW EA 253-00680, REV IR.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 31,888 hrs · 30,743 cycles

FIVE MINUTES AFTER TURNING PACKS ON, RECEIVED A SMOKE TOILET CAUTION & RT PACK HIGH TEMP CAUTION MESSAGES. FOLLOWED BY SMOKE IN THE CABIN. R & R THE RT ACM IAW AMM 21-61-10. RAN FOR 30 MINUTES. OPS AND LEAK CHECKED GOOD IAW 289621/3. R & R THE TEMP SWITCH IAW 289621/2, AND IAW AMM 21-61-25. OPS CHECKED GOOD.

Part: SEAT BELT — UNKNOWN (COCKPIT) · airframe 29,920 hrs · 28,921 cycles

FIRST OFFICER'S HARNESS, SEAT BELT, REPLACE WITH NEW RELEASE.

Part: HANDLE — FAILED (SERVICE DOOR) · airframe 29,561 hrs · 28,599 cycles

SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. CLEANED AND LUBRICATED SERVICE DOOR OUTER HANDLE, NO FIX. APPEARS HANDLE BINDING ON INNER SLEEVE. REPLACED OUTER HANDLE AND ANCHOR ASSY, REF CMM 52-41-01, OPS CHECK GOOD. THIS CLEARS MEL.

Part: WIRE HARNESS — DEFECTIVE (MLG) · airframe 29,411 hrs · 28,450 cycles

FLIGHT 3925 REC ANTI-SKID OTBD MESSAGE, ABORTED TAKEOFF AT 100 KNOTS, BTMS READS 10-8-10-3. INSPECTED GEAR HARNESS, NO DEFECTS FOUND. TIGHTENED RT OTBD ANTI-SKID HARNESS CONNECTOR. COMPLIED WITH ASCU BITE TEST & OPERATIONS TESTS, ALL PASSED. CLEANED HARNESS CONNECTORS. ANTI-SKID CHECKED GOOD IAW AMM 32-44-00.

Part: INDICATOR — LEAKING (APU) · airframe 29,317 hrs · 28,363 cycles

FLIGHT 3847 STRONG FUEL SMELL IN REAR OF CABIN. PRIOR CREW REPORTS APU HUNG START. INSPECTED APU, FOUND DIFF PRESS INDICATOR LEAKING FUEL IAW 296975 3. LOG 296975 3 REF 975/2 APU FUEL LEAK. COMPLIED WITH CM ACTION. PLACARDED & PLACED ON MEL. M/C FUEL FILTER BOWL DELTA P INDICATOR LEAKING. R & R APU FUEL CONTROL IAW AMM 49-31-01. OPERATIONS CHECKED GOOD. REMOVED FROM MEL & REMOVED PLACARD.

Part: HANDLE — LACK OF LUBE (SERVICE DOOR) · airframe 28,744 hrs · 27,807 cycles

SERVICE DOOR WILL NOT OPEN FROM OUTSIDE, HANDLE WILL NOT SPRING OUT TO OPEN THE DOOR. REMOVED OUTER HANDLE, CLEANED & LUBED HANDLE HOUSING IAW AMM 52-41-0. RE-INSTALLED OUTER HANDLE. OPERATIONS CHECKED GOOD.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 28,487 hrs · 27,541 cycles

LEFT PACK IN MANUAL OR AUTO, PACK OVER TEMPS, CREW REPORTED BURNING SMELL. INSPECTED DUCTING IN AFT EQUIPMENT BAY, NO LEAKS NOTED. NO BURNING SMELL IN AFT EQUIPMENT BAY OR COCKPIT, REF LP 261965 4 FOR MEL. R & R THE NR 1 ACM IAW AMM 21-51-10. LEAK & OPERATIONS CHECK COMPLIED WITH. REMOVED PLACARD & FROM MEL.

Part: AILERON — TIGHT · airframe 28,275 hrs · 27,331 cycles

AILERON CONTROL FEELS TIGHTER THAN USUAL ON FLIGHT CONTROLS. CHECK IN BOTH DIRECTIONS, FEELS EVEN TIGHTER TO THE RT, HYD PUMPS ON & OFF.

Part: FITTING — CRACKED (CARGO BAY) · airframe 26,411 hrs · 25,610 cycles

AFT BAGGAGE COMPARTMENT CURTAIN SUPPORT BAR AFT LOWER CLIP IS CRACKED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,248 hrs · 26,318 cycles

AFT SIDE OF FS 621 INTERCOSTAL AT STRINGER 14L CRACKED.

Part: MOUNT BRACKET — CRACKED (FUSELAGE) · airframe 27,248 hrs · 26,318 cycles

GND POWER RECP MOUNT BRACKET CRACKED.

Part: DRAG ANGLE — CRACKED (LT WING) · airframe 27,248 hrs · 26,318 cycles

LEFT BATTERY RIB DRAG ANGLE & ATTACHING CLIP CRACKED.

Part: BRACKET — CRACKED (SERVICE DOOR) · airframe 27,248 hrs · 26,318 cycles

SERVICE DOOR INNER HANDLE STOP BRACKET CRACKED.

Part: MOUNT — CRACKED (LT COWLING) · airframe 27,248 hrs · 26,318 cycles

LEFT ENG NOSE ACCESS COWL MOUNT IS CRACKED.

Part: SHROUD — DAMAGED (RT AILERON) · airframe 27,248 hrs · 26,318 cycles

RIGHT AILERON UPPER & LOWER FIXED SHROUDS ARE WORN & CHAFED IN MULTIPLE PLACES.

Part: SUPPORT — CRACKED (ESCAPE HATCH) · airframe 27,248 hrs · 26,318 cycles

CREW ESCAPE HATCH LT HINGE POINT CUT OUT SUPPORT IS CRACKED.

Part: STIFFENER — CRACKED (TAILPIPE) · airframe 27,248 hrs · 26,318 cycles

LT TAIL PIPE FAIRING HAS CRACK IN STIFFENER NEAR THE POSITION.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 27,248 hrs · 26,318 cycles

PAX DOOR AFT DRAG ANGLE CRACKED.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 27,248 hrs · 26,318 cycles

LT & RT WINDSHIELD POST SUPPORTS ARE CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,248 hrs · 26,318 cycles

RPB FS 621.00 RT OBLIQUE ANGLE CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,248 hrs · 26,318 cycles

CLIPS AT LBL 9 & RBL 9 ON FS 280 FLOORBEAM ARE CRACKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,248 hrs · 26,318 cycles

55304-2000-0086 CARGO COMPARTMENT FLOOR SEAT TRACK BETWEEN FS 559+112 - 574.00 & RBL 9 IS CORRODED.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 27,248 hrs · 26,318 cycles

FS 280.00 STRINGER 3L CLIP IS CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,248 hrs · 26,318 cycles

BATHTUB FITTING CRACKED AT RBL 9 FS 461.00.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 27,248 hrs · 26,318 cycles

PAX DOOR OUTER HANDLE CRACKED.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 27,248 hrs · 26,318 cycles

CARGO BAY FLOOR TRACKS BETWEEN FS 605 & 621, LBL 9 CORRODED.

Part: DRAG ANGLE — CRACKED (RT WING) · airframe 27,248 hrs · 26,318 cycles

RIGHT MLG WW BATTERY RIB DRAG ANGLE CRACKED.

Part: MOUNT BRACKET — CRACKED (PAX DOOR) · airframe 27,248 hrs · 26,318 cycles

PAX DOOR POWER ASSIST MOTOR MOUNT BRACKET CRACKED.

Part: ATTACH FITTING — CRACKED (CARGO DOOR) · airframe 27,248 hrs · 26,318 cycles

CARGO DOOR UPPER FWD ATTACH FITTING CRACKED.

Part: APU — ODOR (APU BAY) · airframe 27,098 hrs · 26,170 cycles

STARTED APU ON APPROACH WITH DISTINCT FUEL ODOR. SHUT DOWN APU LANDED WITHOUT APU ON.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 25,540 hrs · 24,684 cycles

FIRST OFFICERS’ WINDSHIELD OUTER PANE CRACKED IN CRUISE & OBSERVED INTERNAL ARCING AT FL290. COMPLIED WITH QRH, DECLARED AN EMER & DIVERTED. CABIN PRESS REMAINED IN CONTROL & DID NOT LAND OVERWEIGHT. R & R FIRST OFFICER`S WINDSHIELD IAW AMM 56-11-01. PRESS & LEAK CHECKED GOOD.

Part: SHUTOFF VALVE — OUT OF POSITION (CABIN PRESSURE) · airframe 25,363 hrs · 24,522 cycles

AT ACFT ALTITUDE 11000 CABIN ALTITUDE CLIMBED TO ABOVE 8500 FT & AMBER CAUTION APPEARED. CABIN CONTINUED TO CLIMB TO SLIGHTLY ABOVE 10000 FT &THE CAUTION CHANGED TO A WARNING. DECLARED EMERGENCY & LANDED PHL, SCHEDULED STN. NOTICED OTBD EXHAUST SOV WAS IN THE OPEN POSITION. CLOSED VLV HANDLE INTO POSITION CLOSED TO COMPLIED WITH MEL IAW AWAC SUPP 13-014.

Part: HINGE FITTING — GOUGED (RUDDER) · airframe 22,639 hrs · 21,868 cycles

LOWER CENTER HINGE ON RUDDER HAS TOOL GOUGES IN LUG. REMOVED AND REPLACED HINGE FITTINGS P/N 600-21098-3.

Part: STRUCTURE — GOUGED (FUSELAGE) · airframe 22,639 hrs · 21,868 cycles

AEB DOOR CUTOUT STRUCTURE HAS GOUGE ON LEFT SIDE AT FS 700. REMOVED DAMAGE AND INSTALLED FILLER & DOUBLER IAW REO 601R-53-61-4896.

Part: SILL — CORRODED (FUSELAGE) · airframe 22,639 hrs · 21,868 cycles

RIGHT FLOOR SILL IN CARGO BAY FROM FS 589 TO 621 HAS CORROSION IN 8 PLACES. REPAIRED DAMAGE BY BLENDING IAW REO 601R-53-61-4892.

Part: SKIN — DENTED (FUSELAGE) · airframe 22,639 hrs · 21,868 cycles

FUSELAGE SKIN DENT BELOW CARGO DOOR CUTOUT. REPAIRED FUSELAGE SKIN DENT IAW REO 601R-53-61-4865.

Part: HINGE — CHAFED (TE FLAP) · airframe 22,639 hrs · 21,868 cycles

RIGHT O/B FLAP O/B HINGE ARM IS CHAFED AT HINGE BOX CONNECTION. REPAIRED RIGHT O/B FLAP O/B HINGE ARM AT HINGE BOX CONNECTION IAW REO 601R-57-21-1918.

Part: SILL — CORRODED (FUSELAGE) · airframe 22,639 hrs · 21,868 cycles

CORROSION ON LEFT O/B FLOOR SILL BY CARGO DOOR ENTRANCE. REPAIRED CARGO BAY FLOOR SILL IAW BOMBARDIER REO 601R-53-61-690 REV D.

Part: NUT PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,639 hrs · 21,868 cycles

CORROSION ON & UNDER NUT PLATES AT FS 620 RBL 16 & RBL 39. COMPLIED WITH REO 601R-53-61-4690 & REO 601R-53-61-117 REV C.

Part: SKIN — DENTED (FUSELAGE) · airframe 22,639 hrs · 21,868 cycles

PROTRUDING DENT ON RIGHT LOWER FUSELAGE EXTERIOR SKIN AT APPROX FS 668 STR 23R. REPAIRED IAW REO 601R-53-61-4885.

Part: FRAME — CRACKED (EXHAUST FAIRING) · airframe 22,639 hrs · 21,868 cycles

RIGHT EXHAUST FAIRING 2ND FRAME FROM FRONT CHAFED & CRACKED. REMOVED AND REPLACED FRAME P/N 228-50181-849 ON RIGHT EXHAUST FAIRING IAW CMM 20-40-11 & 20-42-06.

Part: BRACKET — CRACKED · airframe 22,639 hrs · 21,868 cycles

A/C GROUND RECEPTACLE BRACKET CRACKED O/B FWD & I/B AFT. REMOVED AND REPLACED BRACKET P/N 600-33283-33 IAW SRM 51-42-13 & 51-42-21.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,639 hrs · 21,868 cycles

LEFT OBLIQUE ANGLE IS CRACKED. REMOVED AND REPLACED OBLIQUE ANGLE P/N 601-35012-51 IAW CRJ 200 SRM 51-42-21.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,639 hrs · 21,868 cycles

CORROSION ON TIE DOWN CLEAT NEAR FS 584 & LBL 10. REMOVED AND REPLACED CLEAT P/N 601R38663-21 IAW CRJ 200 SRM 51-41-02.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 22,639 hrs · 21,868 cycles

BRAKE PRESSURE TRANSDUCER BRACKET IN RIGHT MLG WHEEL WELL IS CRACKED. REMOVED AND REPLACED BRACKET P/N 601R75262-157 IAW CRJ SRM 51-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,639 hrs · 21,868 cycles

UNDER FLOOR CLIP ANGLES AT FS 484 & RBL 27 & 36 ARE CRACKED. REMOVED AND REPLACED CLIPS IAW GREO 601R-53-41-059 REV B & SRM 51-40-11.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 22,639 hrs · 21,868 cycles

11 EA TOOL AND SCREW MARKS ON FWD SIDE OF 621 BULKHEAD. REPAIRED 7EA AREA ON FS 621 BULKHEAD IAW REO 601R-53-61-2155 & 4 EA AREAS IAW REO 601R-53-61-1285 REV D.

Part: COWLING — CHAFED (LEFT) · airframe 22,639 hrs · 21,868 cycles

INNER CORE COWL LEFT LOWER #434AB HAS 4 CHAFE /DENT AREAS, 2 OF THE DENTS THAT WERE OUT OF LIMITS WERE LESS THAN 6" & REQUIRED REO. FOLLOWED REO 601R-71-12-4166 WHICH SAID TO FOLLOW CMM 71-12-01 REPAIR ORDER SRS046 TO REPAIR DAMAGE AREAS THAT WERE OUT OF LIMITS. 1 CHAFE WAS IN LIMITS & BLENDED SMOOTH & 3 DENTS REPAIRED.

Part: VANE — CHAFED (TE FLAP) · airframe 22,639 hrs · 21,868 cycles

RIGHT I/B FLAP VANE L/E IS CHAFED FROM ALL 3 STOPS. BLEND I/B & O/B STOP AREAS AND FOUND TO BE WITHIN LIMITS IAW BOMBARDIER REO 601R-57-52-004 REV D CENTER L/E VANE REMOVED AND REPLACED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 22,639 hrs · 21,868 cycles

CLIP ANGLE CRACKED BELOW CARGO FLOOR SILL. REMOVED & REPLACED CRACKED CLIP WITH SERVICEABLE DUPLICATED CLIP IAW CRJ 200 SRM 51-21-11, 51-23-00, 51-24-16, 51-24-36, 51-25-06, 51-25-16, 51-40-11, 51-42-21.

Part: STRIKER — DAMAGED (PAX DOOR) · airframe 22,639 hrs · 21,868 cycles

PAX DOOR AFT SEAL STRIKER IS DAMAGED AT UPPER FITTING. REMOVED AND REPLACED STRIKER, REPAIR DOUBLER IAW REO 601R-53-22-033 REV C.

Part: ISOLATOR — CRACKED (FUSELAGE) · airframe 22,639 hrs · 21,868 cycles

1 EA ISOLATOR ON FWD LEFT SIDE OF FS 621 BULKHEAD IS CRACKED. REMOVED UNSERVICEABLE ISOLATOR AND INSTALLED SERVICEABLE ISOLATOR BRACKET ON FWD SIDE OF FS 621 BULKHEAD IAW CRJ 200 SRM 51-42-06 AND 51-40-11.

Part: TRUNNION — DAMAGED (RT MLG) · airframe 22,639 hrs · 21,868 cycles

DURING COLD WORKING PROCESS FOUND 1 EACH OVERSIZED HOLE ON LEFT & 2 EA ON RIGHT LOWER MLG TRUNNION FLANGE. REPAIRED 1EA OVERSIZED HOLE ON LEFT & 2EA ON RIGHT LOWER MLG TRUNNION FLANGES IAW BOMBARDIER REO 601R-57-21-1911 & REO 601R-57-21-1912.

Part: LONGERON CLIP — CRACKED (FUSELAGE) · airframe 22,639 hrs · 21,868 cycles

UNDER FLOOR LONGERON CLIP ANGLES AT APPROX FS 484 LBL 27 AND LBL 36 ARE CRACKED 2 TOTAL. REMOVED AND REPLACED CLIPS.

Part: DIODE — FAILED (THRUST REVERSER) · airframe 20,539 hrs · 19,803 cycles

RECEIVED RT THRUST REVERSER UNLOCK CAUTION MESSAGE, TESTED AFTER ROTATION INDICATION ONLY. NO PERFORMANCE CHANGE. COMPLIED WITH QRH MESSAGE PERSISTED. R & R DIODE MODULE TB207-7-2CR7KE IAW WIRE MANUAL 78-30-00. THRUST REVERSERS OPS CHECKED GOOD IAW 78-30-00.

Part: WARNING MESSAGE — ILLUMINATED (THRUST REVERSER) · airframe 20,478 hrs · 19,750 cycles

ON CLIMB OUT, RECEIVED RT THRUST REVERSER UNLOCK MESSAGE. COMPLIED WITH QRH, SELECTED EMERGENCY STOW, RT THRUST REVERSER UNLOCK MESSAGE PERSISTS, WITH THRUST LEVER AT IDLE, FELT SLIGHT VIBRATION IN AIRFRAME, NO ABNORMAL N1 OR N2 VIBRATION INDICATIONS. VIBRATION FELT ON CLIMB OUT AT 290 KTS AND VIBRATION STILL FELT. COMPLIED WITH QRH & SHUT DOWN RIGHT ENGINE, ENGINE WAS SHUT DOWN FOR APPROX 40 MINUTES, OIL PRESSURE READ APPROX 1 PSI WHILE ENGINE WAS WINDMILLING. PERFORMED ENGINE RUN, NOTED NO ABNORMAL VIBRATIONS. OPS CHECKED GOOD.

Part: SKIN — CHAFED (RT NACELLE) · airframe 18,268 hrs · 17,365 cycles

RT LOWER CORE COWL T/E CHAFED. REPAIRED IAW REO 601R-71-12-3276.

Part: HINGE — DAMAGED (RUDDER) · airframe 18,268 hrs · 17,365 cycles

DURING BEARING REMOVAL UPPER HALF OF RUDDER LWR CENTER HINGE WAS DAMAGED. REPAIRED HINGE HALF IAW REO 601R-55-31-212.

Part: ATTACH ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 18,268 hrs · 17,365 cycles

ANGLE AT 621 BULKHEAD THAT IS ATTACHED TO CARGO DOOR CURTAIN ROD CRACKED. REMOVED UNSERVICEABLE ANGLE FABRICATED. INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-21 & SRM 51-42-10.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 18,268 hrs · 17,365 cycles

LT INBD FLAP VANE INBD END IS CHAFED FROM STOPS. LT INBD FLAP VANE END L/E WAS DETERMINED TO BE OUT OF LIMITS IAW REO 601R-57-52-004, REV C. REMOVED AND INSTALLED NEW SERVICEABLE L/E SKIN ON FLAP VANE IAW REO 601R-57-52-1730.

Part: DRAG ANGLE — UNKNOWN (VERTICAL STAB) · airframe 18,268 hrs · 17,365 cycles

REPAIRED VERTICAL STAB DRAG ANGLE 601R-55-32-075E. COMPLIED AWAC WC 4DMI15089 AND REO 601R-55-32-075, REV E. PERMANENT REPAIR TO VERTICAL STAB DRAG ANGLE DIAPHRAGM.

Part: SUPPORT BRACKET — CRACKED (BS 574) · airframe 18,268 hrs · 17,365 cycles

CARGO BAY DOOR FWD TRACK LOWER SUPPORT BRACKET CRACKED. REMOVED CRACKED LOWER SUPPORT BRACKET AND INSTALLED NEW SUPPORT BRACKET IAW SRM 51-42-06.

Part: PANEL — GOUGED (RT WING TE FLAP) · airframe 18,268 hrs · 17,365 cycles

PANEL 692BB GOUGED. REMOVED GOUGED GUIDE PLATE FROM PANLE 692BB AND INSTALLED NEW SERVICEABLE GUIDE PLATE IAW SRM 51-42-06.

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 18,268 hrs · 17,365 cycles

LT MLG DOOR L/E 1 FILLER CHAFED FROM PREVIOUS REPAIR. INSTALLED SERVICEABLE 1 FILLER IAW REO 601R-52-82-034, REV C.

Part: STRIP — CHAFED (RT NACELLE) · airframe 18,268 hrs · 17,365 cycles

RT ENG UPPER NOSE COWL AFT SEAL STRIP IS KNIFE EDGED. REMOVED UNSERVICEABLE AFT EDGE STRIP & REPLACED WITH SERVICEABLE AFT EDGE STRIP IAW CMM 71-14-01-300-814-A01.

Part: FITTING — CHAFED (RT WING TE FLAP) · airframe 18,268 hrs · 17,365 cycles

PANEL 697BB GUIDE FITTING CHAFED AND DAMAGED. REMOVED DAMAGED GUIDE EDGE A ON PANEL 697BB AND INSTALLED NEW SERVICEABLE GUIDE IAW SRM 51-42-06.

Part: SKIN — CHAFED (LT AILERON) · corrosion level 1 · airframe 18,268 hrs · 17,365 cycles

LT AILERON UPPER L/E IS CHAFED. BLENDED LEFT AILERON UPPER L/E DAMAGE WITHIN ALLOWABLE LIMITS IAW REO 601R-57-60-013, ALODINED, PRIMED AND PAINTED IAW SRM 51-21-11, 51-25-06 AND 51-25-16.

Part: SKIN — CHAFED (RT AILERON) · airframe 18,268 hrs · 17,365 cycles

RT AILERON FIXED L/E TOP AND BOTTOM HAVE CHAFE DAMAGE 6 EA PLACES. BLENDED RT AILERON FIXED L/E TOP AND BOTTOM, DAMAGE WITHIN ALLOWABLE LIMITS IAW REO 601R-57-60-013, ALODINED, PRIMED AND PAINTED IAW SRM 51-21-11, 51-25-06 AND 51-25-16.

Part: SKIN — CHAFED (RT NACELLE) · airframe 18,268 hrs · 17,365 cycles

RT UPPER CORE COWL T/E CHAFED. REPAIRED UPPER CORE COWL T/E IAW REO 61R-71-12-3276.

Part: HINGE — GOUGED (RT WING TE FLAP) · airframe 18,268 hrs · 17,365 cycles

RT INBD FLAP OTBD HINGE BOX ATTACH LUG GOUGED (HINGE ARM TO HINGE BOX LUG) BLENDED (.008") IAW REO 601R-57-54-192.

Part: BRACKET — CRACKED (PAX DOOR ASSIST) · airframe 18,268 hrs · 17,365 cycles

PAX DOOR PWR ASSIST MOTOR MOUNTING BRACKET CRACKED AT LOWER RADIUS. REMOVED DAMAGED BRACKET AND REPLACED WITH NEW SERVICEABLE BRACKET PN 601R3177457.

Part: ACCESS PANEL — CHAFED (RT WING) · airframe 18,268 hrs · 17,365 cycles

ACCESS PANELS 699CB AND 699AB HAVE CHAFING DAMAGE FROM SEAL BLENDED AILERON LOWER ACCESS PANELS 699AB AND 699CB IAW SRM 51-12-00 WITHIN LIMITS IAW REO 601R-57-60-020.

Part: FITTING — CHAFED (LT WING TE FLAP) · airframe 18,268 hrs · 17,365 cycles

LT WING OTBD FLAP ALIGNMENT FITTING IS CHAFED. BLENDED LT WING OTBD FLAP ALIGNMENT FITTING REMOVING .025" MATERIAL IAW SRM 51-12-00 AND REO 601R-57-51-143. THIS IS ALLOWABLE DAMAGE.

Part: TRACK — GOUGED (CARGO DOOR) · airframe 18,268 hrs · 17,365 cycles

CARGO DOOR AFT TRACK GOUGED. BLENDED GOUGED AREA OF THE CARGO DOOR AFT TRACK. REMOVING .055" LEAVING .215" MATERIAL IAW REO 601R-53-62-024 WITHIN LIMITS.

Part: FITTING — CHAFED (LT WING TE FLAP) · airframe 18,268 hrs · 17,365 cycles

LT OTBD FLAP ALIGNMENT FITTING CHAFED NEXT TO ROLLER. BLENDED MINOR CHAFE ON LT OTBD FLAP ALIGNMENT FITTING IAW REO 601R-57-53-864.

Part: ATTACH BRACKET — CHAFED (RT WING TE FLAP) · airframe 18,268 hrs · 17,365 cycles

RT OTBD FLAP ROLLER GUIDE ATTACH CRACKED AND GUIDE FITTING HAVE CHAFE AND GOUGE DAMAGE. BLENDED RT OTBD GUIDE ATTACHED BRACKET AND RT OTBD FLAP GUIDE FITTING IWA 601R-57-51-143.

Part: HINGE FITTING — CHAFED (RT WING TE FLAP) · airframe 18,268 hrs · 17,365 cycles

RT INBD FLAP ZB HINGE ARM ATTACH LUGS HAVE MINOR CHAFING FROM FAIRINGS 2 PLACES. BLENDED RT INBD FLAP INBD AND OTBD AFT LUGS. REMOVEING .005" MATERIAL FROM EACH LUG ARE WITHIN LIMITS IAW REO 601R-57-52-1536.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 18,268 hrs · 17,365 cycles

RT INBD FLAP VANE L/E CHAFED AT INBD CTR AND OTBD SECTIONS BLENDED CHAFE AREAS ON THE RT INBD FLAP VANE L/E AT INBD, CTR AND OTBD SECTIONS ALL 3 AREAS WITHIN LIMITS IAW REO 601R-57-52-004.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 18,268 hrs · 17,365 cycles

LT INBD FLAP VANE CHAFED FROM STOPS AT CTR AND OTBD LOCATIONS. BLENDED MINOR CHAFE MARKS AT LT INBD FLAP VANE CTR AND OTBD LOCATIONS. CTR AND OTBD CHAFES WITHIN ALLOWABLE LIMITS IAW 601R-57-52-004.

Part: SUPPORT — CRACKED (PAX DOOR) · airframe 18,268 hrs · 17,365 cycles

SUPPORT FOR 832 CT CRACKED. PAX DOOR AFT STAIR SIDE PANEL AT 2ND STEP WHEN OPEN. REPAIRED DAMAGE TO SUPPORT FOR 832CT (AFT SIDE) IAW REO 601R-52-11-702.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 18,268 hrs · 17,365 cycles

SUPPORT FOR PAX DOOR BRACKET (832CT) CRACKED IN RADIUS, PAX DOOR FWD STAIR SIDE PANEL 2ND STEP WHEN OPEN. REPAIRED DAMAGE TO SUPPORT FOR 832CT (FWD SIDE) IAW REO 601R-52-11-702.

Part: HINGE FITTING — GOUGED (PAX DOOR) · airframe 18,268 hrs · 17,365 cycles

PAX DOOR HINGE LUG NR 3, 4 AND 25 (DOOR SIDE) HAS MINOR GOUGES BLENDED OUT MINOR GOUGES IAW SRM 51-12-00. FOUND TO BE WITHIN LIMITS IAW REO 601R-52-11-1347, TYPE 1 DISPOSITION.

Part: VALVE — MALFUNCTIONED (COMPUSTER DRAIN) · airframe 17,241 hrs · 16,310 cycles

APU WOULD NOT START ON 1ST ATTEMPT, STRONG ODOR OF JET FUEL, BLEEDS REMAINED ON ENGINE BLEEDS. RAN APU SEVERAL TIMES, NO PROBLEMS STARTING, APU, NO LEAKS NOTED, R & R BOTH PACK COALESCER BAGS IAW AMM 21, R & R APU FUEL COMBUSTOR DRAIN VALVE IAW AMM 49, RAN APU AND BOTH ENGINES WITH BOTH PACKS SELECTED FOR SEVERAL MINUTES, WITH HOT AND COLD SELECTED, NO ODORS.

Part: UNKNOWN — ODOR (CABIN) · airframe 16,940 hrs · 16,000 cycles

APU WOULD NOT START IN FLIGHT. AFTER LANDING APU STARTED & FUEL ODOR NOTED IN CABIN RT AFTER START, THEN DISSAPATED SHORTLY AFTERWARDS. INSPECTED APU, FOUND NO FUEL LEAKS. RAN APU FOR 20 MINUTES, NO ODOR NOTED. OK FOR SERVICE.

Part: COALESCER BAG — DIRTY (A/C SYSTEM) · airframe 16,910 hrs · 15,968 cycles

STRONG FUEL ODOR IN CABIN ON APPROACH. BEFORE APU START AND BEFORE FLAPS AND GEAR. INSPECTED FUEL SHROUD DRAINS, APU BOX AND AFT EQUIPMENT BAY NO LEAKS FOUND. R & R LT AND RT COALESCERS IAW AMM 21-51-13. OPS CHECK GOOD AT THIS TIME. NO FUEL LEAKS NOTED ON ENGINES.

Part: OVERHEAT LOOP — DAMAGED (RT MLG WW) · airframe 14,001 hrs · 12,971 cycles

AT CRUISE ALTITUDE, RECEIVED MLG BAY OVERHEAT FAIL CAUTION MESSAGE INTERMITTENTLY. FOLLOWED BY MLG BAY OVERHEAT WARNING MESSAGE WITH TRIPLE CHIME. C/W QRH, BTMS 1-1-1-1. REMOVED AND REPLACED RT WHEEL WELL LOOP IAW AMM 26-14-00. OPS CHECK GOOD. (K)

Part: FITTING — CRACKED (BS 621 BULKHEAD) · airframe 13,605 hrs · 12,588 cycles

CRACK FOUND ON REAR PRESSURE BULKHEAD AT LINTEL FITTING LOCATION. REAR PRESSURE BULKHEAD REPAIRED AT LINTEL FITTING LOCATION IAW REO 601R-53-61-1230 REV D. (K)

Part: BULKHEAD — DAMAGED (BS 280) · airframe 13,605 hrs · 12,588 cycles

2 RIVET DAMAGE AND SCRATCH FOUND ON FWD COMPARTMENT PRESSURE BULKHEAD FS 280.00, RBL 9.0, WL 94.50. FWD COMPARTMENT PRESSURE BULKHEAD FS 280, RBL 9 WL 94.50. REPAIRED IAW REO 601R-53-11-1677, REV A . (K)

Part: BULKHEAD — CRACKED (BS 202) · airframe 13,605 hrs · 12,588 cycles

FWD PRESSURE BULKHEAD FS 202.75, LBL 23.71 CRACKED. FWD PRESSURE BULKHEAD FS 202.75, LBL 23.71, REPAIRED IAW REO 601R-53-11-1681. (K)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 13,605 hrs · 12,588 cycles

DURING MODIFICATION OF THE ENGINE BEAM REWORK LT AND RT SKIN AND SKIN DOUBLER IN ORDER TO ELIMINATE ATTACHMENT AT DISCREPANT FASTENER LOCATION DUE TO FALLING CONDITION ON ANGLE PN 601R350073-3 AND -4. REWORK ON LT AND RT SKIN AND SKIN DOUBLER PERFORMED IAW MODSUM NO TC 601R17262, STEP 4. (K)

Part: THROTTLE CABLE — OBSTRUCTED (LT NACELLE) · airframe 13,605 hrs · 12,588 cycles

DURING MODIFICATION OF THE ENGINE SUPPORT BEAM REWORK ON RT AND LT UPPER AND LOWER PYLON TO FUSELAGE FITTING TO ELIMINATE HOW EDGE DISTANCE AND FOULING CONDITION WITH THE TROTTLE CABLE. REWORK ON RT LAND LT UPPER AND LOWER PYLON TO FUSELAGE FITTING C/O MODSUM TC601R17262, STEP 9. (K)

Part: STRUCTURE — CRACKED (RT NACELLE) · airframe 13,605 hrs · 12,588 cycles

RT ENG NOSE INLET COWL BRIDGING PIECE FOUND CRACKED. RT ENG NOSE COWL BRIDGING PIECE REPLACED IAW CMM 20-41-04. (K)

Part: SKIN — CRACKED (FUSELAGE) · airframe 13,605 hrs · 12,588 cycles

DURING MODIFICATION OF THE ENGINE SUPPORT BEAM, REWORK LT AND RT SKIN AND SKIN DOUBLER IN ORDER TO ELIMINATE EXISTING CRACK IN INTERNAL DOUBLER. REWORK LT AND RT SKIN AND SKIN DOUBLER C/O IAW MODSUM NR TC 601R17262.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 13,605 hrs · 12,588 cycles

RT INTERCOSTAL CLIP FS 621-625 ADJACENT TO STR 14 CRACKED. RT INTERCOSTAL CLIP FS 621-625 ADJACENT TO STR 14 REPLACED IAW SRM 51-42-06 AND 51-42-21. (K)

Part: FLOORBEAM — CRACKED (BS 280)

CRACK ON FLOORBEAM CLIP FS 280, LBL 9, INBD AND OTBD. FLOORBEAM CLIP REPLACED ON FS 280, LBL 9 INBD AND OTBD. (K)

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 13,605 hrs · 12,588 cycles

INTERCOSTAL CLIP CRACKED AT FS 484, LBL 27. INTERCOSTAL CLIP REPLACED AT FS 484, LBL 27 SRM 51-42-06 AND ARM 51-42-20. (K)

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 13,605 hrs · 12,588 cycles

LT INTERCOSTAL FS 621-625 ADJACENT TO STR 14 CRACKED. LT INTERCOSTAL FS 621-625 ADJACENT TO STR 14 REPLACED IAW SRM 51-42-06 AND 51-42-21. (K)

Part: ANGLE — CRACKED (BS 280) · airframe 13,605 hrs · 12,588 cycles

FS 280 UPPER ANGLE CRACKED AT LBL 9. FL 280 UPPER ANGLE REPAIR IAW REO 601R-53-11-138 REV NC. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 13,605 hrs · 12,588 cycles

CRACK FOUND ON INTERCOSTAL FS 484, LBL 36. REPAIR PERFORMED ON INTERCOSTAL FS 484, LBL 36 IAW REO 601R 53-41-59 REV A. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 13,605 hrs · 12,588 cycles

CRACK FOUND ON INTERCOSTAL FS 484, RBL 36. REPAIR PERFORMED ON INTERCOSTAL FS 484, RBL 36, IAW REO 601R-53-41-059 REV A. (K)

Part: FLOORBEAM — CORRODED (BS 280) · airframe 13,605 hrs · 12,588 cycles

FS 280.0 FLOORBEAM CRACKED AT RBL 9.0 LOWER RADIUS FS 280.0 FLOORBEAM AT RBL 9.0 REPAIR CARRIED OUT IAW REO 601R-53-11-171, REV D. SCHEME B. (K)

Part: BRACKET — CRACKED (DOOR SILL) · airframe 13,605 hrs · 12,588 cycles

CARGO DOOR FLOOR SILL CRACKED AT FWD STOW PLATE BRACKET (CRACK LENGTH .500) CARGO DOOR FLOOR SILL AT FWD STOW PLATE BRACKET REPAIRED IAW REO 601R-53-61-1741. (K)

Part: FLEX DRIVE — CORRODED (TE FLAP) · airframe 13,709 hrs · 12,686 cycles

FLEXSHAFT ON FLAP FOUND WITH HEAVY CORROSION ON 70 PERCENT OF THE COIL SURFACE AND SEIZED IN ACTUATOR. B-NUT FOUND IMPROPERLY TORQUED AT THE SEIZED END. SUBSEQUENT DAMAGE ON TERMINAL. C/A IN PROGRESS. (K)

Part: LINE — BROKEN (NR 1 HYD SYSTEM) · airframe 12,601 hrs · 11,625 cycles

HYDRAULICS 1 LOW PRESSURE MSG. CW QRH NR 1 HYD PRESSURE AT ZERO PSI AND NR 1 HYD QUANTITY SHOWS AMBER DASHES. DIVERTED TO CRW. FLIGHT TIME AT ZERO PSI WAS 46 MINUTES. 1B PUMP OPERATED FOR 2 MINUTES. FOUND BROKEN LINE ON NR 1 NYD SYSTEM FROM EDP TO CASE DRAIN FILTER. R&R LINE IAW AMM 29-10-00. OPS AND LEAK CHECK GOOD..

Part: CONNECTOR — LOOSE (FIRE LOOP) · airframe 10,710 hrs · 9,813 cycles

INTERMITTENT MLG BAY OVERHEAT FAULT THEN MLG BAY OVER HEAT INDICATION DIVERTED TO SCE. BRAKE TEMPS INDICATED NORMAL AT ALL TIMES (01 ON ALL FOUR). SECURED LOOSE CONNECTION ON RT MLG BAY FIRELOOP. REPAIRED BROKEN CONNECTION ON LT MLG FIRELOOP. COMPLIED WITH FUNCTION TEST IAW AMM 26-14-00 PARA B (1) AND (2) FAULTS. (A)

Part: LANDING GEAR — MALFUNCTIONED · airframe 10,491 hrs · 9,604 cycles

AFTER TAKEOFF UPON GEAR RETRACTION NOSE GEAR SHOWED DOWN WITH GEAR DISAGREE, COMPLIED WITH QRH, PERFORMED MANUAL GEAR EXTENSION, RETURNED TO ROS. (M)

Part: STRUCTURE — DAMAGED (LT WING) · airframe 10,491 hrs · 9,604 cycles

WINDSHEAR DURING LANDING LEFT WING PUSHED UP AND RIGHT WINGSTRIP SCRAPED RUNWAY. (M)

Part: PITOT SYSTEM — CONTAMINATED (PITOT/STATIC SYS) · airframe 10,232 hrs · 9,364 cycles

ON TAKEOFF ROLL STANDBY IAS READS -0- KNOTS, REJECTED TAKEOFF AT ABOUT 85 KNOTS, MAX BTMS = 8,7,6,6. NOTE: NO HES/RTO INSPECTION REQUIRED. FOUND WATER IN THE STANDBY PITOT/STATIC SYSTEM. PERFORMED CONTAMINATION REMOVAL OF THE STANDBY PITOT/ STATIC SYSTEM. PERFORMED LEAK CHECK OF P3 SYSTEM IAW AMM 34-11-00. OPS CHECK GOOD. (K)

Part: CONTROL UNIT — FAILED (PITCH TRIM)

CAUTION MESSAGE INFLIGHT, STAB TRIM, MACH TRIM, AUTOPILOT TRIM NOSE DOWN. PITCH STUCK AT 6.0. WHEN AUTOPILOT DISENGAGED AT 1000` AGL ALL MESSAGES DISAPPEARED PITCH TRIM WAS OPERATIONAL. HSTCU FAIL, REMOVED AND REPLACED HSTCU IAW 27-41-01, NO FAULTS NOTED. OPS CHECK GOOD. (M)

Part: FLOORBEAM — CRACKED (BS 621) · airframe 8,681 hrs · 7,865 cycles

LT FS 621 FLOOR SUPPORT ANGLE CRACKED APPROX .2 INCH LONG. MAINTENANCE CUT OUT DAMAGED AREA AND INSTALLED REPAIR ANGLE IAW REO 601R-53-61-117. (K)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 8,681 hrs · 7,865 cycles

RT FS 621 FLOOR SUPPORT ANGLE APPROX .2 INCH LONG. MAINTENANCE REMOVED DAMAGED AREA AND INSTALLED REPAIR ANGLE IAW REO 601R-53-61-117. (K)

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 8,681 hrs · 7,865 cycles

HYDRAULIC PRESSURE TRANSDUCER HAT CHANNEL (PN 601R75262-159) CRACKED APPROX .2 INCH LONG IN LT MLG WHEEL WELL CEILING. MAINTENANCE REMOVED AND REPLACED CHANNEL PN 601R75262-159 IAW SRM 51-42-06. (K)

Part: TRANSDUCER — CRACKED (HYD PRESSURE) · airframe 8,681 hrs · 7,865 cycles

HYDRAULIC PRESSURE TRANSDUCER (PN 610R75262-157) CRACKED APPROX .2 INCH LONG INRT MLG WHEEL WELL CEILING. MAINTENANCE REMOVED CRACKED HAT CHANNEL AND INSTALLED SERVICEABLE HAT CHANNEL PN 601R75262-157 IAW SRM 51-42-06. (K)

Part: BRACKET — CRACKED (RT MLG WW) · airframe 8,681 hrs · 7,865 cycles

HYDRAULIC LINE Z-BRACKET (PN 601R75262-153) CRACKED APPROX .1 INCH LONG IN RT MLG WHEEL WELL. MAINTENANCE REMOVED AND REPLACED BRACKET (PN 601R75262-153) IAW SRM 51-42-06. (K)

Part: FLOORBEAM — CRACKED (BS 484) · airframe 8,681 hrs · 7,865 cycles

LT FS 484 ANGLE IS CRACKED AT LBL 36 AND 27 APPROX 1.4 INCH L. MAINTENANCE REPAIRED LT FS 484 IAW REO AND SRM. (K)

Part: CHANNEL — CRACKED (CARGO DOOR) · airframe 8,681 hrs · 7,865 cycles

CARGO DOOR FWD TRACK C-CHANNEL HAS A .5 INCH LONG CRACK WL. (K)

Part: FLOORBEAM — CRACKED (BS 484) · airframe 8,681 hrs · 7,865 cycles

RT FS 484 ANGLE IS CRACKED AT RBL 27 AND 36 APPROX 1.4 INCH L. MAINTENANCE REPAIRED RT FS 484 ANGLES AT RBL 27 AND RBL 36 IAW REO 601R-53-41-059 AND BSC STANDARD REPAIR 601R-53-0030A. (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 8,681 hrs · 7,865 cycles

PAX DOOR AFT DRAG ANGLE CRACKED JUST ABOVE ASSIST MOTOR PULLEY BRACKET. MAINTENANCE CUT OUT DAMAGED AREA AND INSTALLED REPAIR ANGLE IAW REO 601R-52-11-513. (K)

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 8,681 hrs · 7,865 cycles

LT FS 625 OBLIQUE ANGLE IS CRACKED APPROX 1 INCH L. MAINTENANCE REMOVED AND REPLACED ANGLE IAW SRM 51-42-06, 51-42-21 AND REO 601R-53-61-422. (K)

Part: CONTROL UNIT — UNKNOWN (HORIZONTAL STAB) · airframe 7,207 hrs · 6,455 cycles

STAB CHANNEL 1 INOP STATUS MESSAGE IN FLIGHT, COULD NOT RESET. AIR RETURN TO DEPARTURE. REMOVED AND RETURNED HSTCU IAW AMM 27-41-01. OPS CHECK GOOD. (K)

Part: IDG — MALFUNCTIONED (NR 1)

IDG NR 1 CAUTION MESSAGE ON TAKEOFF ROLL. ABORTED TAKEOFF AT LESS THAN 40 KNOTS. BTMS TEMPS WERE 2-2-3-2. REMOVED AND REPLACED IDG NR 1, OPS CHECK GOOD, IAW 24-11-01. LEAK AND OPS CHECK GOOD. (M)

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 3,682 hrs · 6,141 cycles

CHANNEL OF MAIN UNDERCARRIAGE AND UPLOCK APRON BENT AND CRACKED. REPAIRED IAW EO. (K)