N411ZW

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,686 hrs · 42,772 cycles

16 EA BLENDED AREAS P11 TO P26 FOUND OUT OF LIMITS ON FLOOR BEAM RAIL AT FS559+121 TO FS621 LBL27. REMOVED AND REPLACED 1EA FLOOR BEAM RAIL (P/N; N126-1577-56830), 4EA BEAM (P/N; 600-35031-307, 600-35031-308, 600-35031-309, AND 600-35031-310), AND 1EA BEAM DOUBLER (P/N: 600-35139-7) ON FLOOR SUPPORT STRUCTURE AT FS559+121 TO FS621 AT LBL27. IAW CRJ-200 SRM 51-42-06 AND 51-42-21 REV39.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,686 hrs · 42,772 cycles

FLOOR SUPPORT STRUCTURE HAS SEVERAL AREAS WITH CORROSION BETWEEN FS559+80 AND FS621 LBL9. AIRCRAFT REMOVED FROM SERVICE. BLENDED AND EVALUATED 28 AREAS OF CORROSION BETWEEN FS559 TO FS621 LBL8 TO LBL10 FOUND TO BE STRUCTURALLY ACCEPTABLE IAW REO 601R-53-00-005, REV B DATED 2011/01/06. REMOVED AND REPLACED FLOOR SUPPORT STRUCTURE FOR 1 AREA OUT OF LIMITS, AT FS559+121 TO FS621. 2EA BEAMS OB P/N 600-35031-307, IB BEAM P/N 600-35031-308. IAW CRJ-200 SRM 51-42-06, AND 51-42-21 REV 39.

Part: SKIN — ERODED (ZONE 600) · airframe 44,686 hrs · 42,772 cycles

RH OUTBOARD LEADING EDGE SKIN P/N 601R12074-4 OUT OF LIMITS AFTER EROSION REMOVAL. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED RH OUTBOARD LEADING EDGE P/N 601R12074-4 AT WS350.348 TO WS389.00. REF CRJ-200 SRM 51-42-06, AND 51-42-13 REV 39. UPPER EDGING P/N 601R12076-6, LOWER EDGING P/N 601R12076-8.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,686 hrs · 42,772 cycles

BLENDED AREA FOUND OUT OF LIMITS ON FLOOR SUPPORT AT FS559 RBL9. AIRCRAFT REMOVED FROM SERVICE REPAIRED AREA ON FLOOR SUPPORT STRUCTURE AT FS559 AND RBL9 IAW MHIRJ REO 601R-53-41-3255 REV--. DATED 2024-09-18.

Part: FLOOR SUPPORT — DAMAGED (ZONE 200) · airframe 44,686 hrs · 42,772 cycles

20144 327672 453-170-500 Ï¿½ MFG50317. 74.45MHRS FLOOR SILL AT FS513+9 LBL42 TOOL MARK ON PRESSURE FLOOR SILL PANEL AT FS513+9 LBL42. AIRCRAFT REMOVED FROM SERVICE PERFORMED REPAIR ON PRESSURE FLOOR SILL PANEL AT FS513+9 AND LBL42. ALL WORK WAS PERFORMED IAW BOMBARDIER REO# 601R-53-41-3246 REV--. ALL WORK PERFORMED UNDER AERSALE WORK ORDER 004393, CARD NO. 20144, TT: 44,686:36 TC: 42,772.

Part: TRIM PANEL — CRACKED (ZONE 200) · airframe 46,096 hrs · 43,568 cycles

TRIM EDGE FOUND BROKEN AND CORRODED ON WARDROBE AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED TRIM EDGE ON WARDROBE IAW CMM 25-20-52 REV 8, AND CRJ200 SRM 51-22-00 REV 39.

Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 44,686 hrs · 42,772 cycles

PILOTS SEAT TRACK LH FWD SECTION MISSING HI-LITE FASTENERS REMOVED AND REPLACED PILOT SEAT TRACK P/N 601R41082-11 REF CRJ200 SRM 51-41-02 REV39. ALL WORK PERFORMED UNDER AERSALE WORK ORDER 004393 CARD NO. 20078. TT: 44,686:36, TC: 42,772 AIRCRAFT REMOVED FROM SERVICE 20078 327672 453-220-500 HRS 50.15 N411ZW PILOTS SEAT TRACK LH FWD SECTION MISSING HI-LITE FASTENERS REMOVED AND REPLACED PILOT SEAT TRACK P/N 601R41082-11 REF CRJ200 SRM 51-41-02 REV39. ALL WORK PERFORMED UNDER AERSALE WORK ORDER 004393 CARD NO. 20078. TT: 44,686:36, TC: 42,772

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,686 hrs · 42,772 cycles

FLOOR SILL AT FS559+14 RBL42 BLEND AREA P3 ON RH FLOOR SILL AT FS559+14 RBL42 OUT OF LIMITS. REMOVED AND REPLACED INTERCOSTAL P/N 601R38842-3 AT FS559.00 TO FS559+16 RBL42. ALL WORK WAS PERFORMED IAW SRM 51-42-06 REV 39, CRJ200 SRM 51-40-20 REV 39. ALL WORK PERFORMED UNDER AERSALE WORK ORDER 004393, CARD NO. 20163, TT: 44,686:36 TC: 42,772. AIRCRAFT REMOVED FROM SERVICE 20163 327672 453-170-500 Ï¿½ 74.45MHRS FLOOR SILL AT FS559+14 RBL42 BLEND AREA P3 ON RH FLOOR SILL AT FS559+14 RBL42 OUT OF LIMITS. REMOVED AND REPLACED INTERCOSTAL AT FS559.00 TO FS559+16 RBL42. ALL WORK WAS PERFORMED IAW SRM 51-42-06 REV 39, SRM 51-40-20 REV 39.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 44,686 hrs · 42,772 cycles

CRACKED FLOOR STRUCTURE AT FS153 LBL30 AND WL79.50. AIRCRAFT REMOVED FROM SERVICE. REMOVED ANGLE P/N 601R75251-13.CUT AWAY CRACKED PORTION OF FLOOR PANEL 601R33101-117. & LOWER FLANGE BRACKET P/N 601R75251-13.BETWEEN FS559-621 LBL27 FABRICATED AND INSTALLED DOUBLER,FILLER AND ANGLE IWA WITH REO# 601R52-11-111 REV NC. PERFORMED HFEC WITH NO INDICATIONS.RESTORED PROTECTIVE FINISH. WORK PERFORMED UNDER AERSALE WORK ORDER 004390, CARD NO. 20097, TT: 44,686:36 TC: 42,772.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,686 hrs · 42,772 cycles

CORROSION ON FLOOR STRUCTURE RH STRAP PN 601R31025-29 AT FS 559.00 AND RBL27 - 36. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND INSTALLED FLOOR STRUCTURE RH STRAP PN 601R31025-29 AT FS 559.00 AND RBL27 - 36 WITH FABRICATED NEW STRAP WITH MATERIAL 7075-T6, THICKNESS 0.050Ï¿½. DIMENSIONS L= 37.5Ï¿½ X W= 5.25Ï¿½. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM 53-00-00 REV 39, SRM 53-41-43 REV 39, SRM 51-40-11 REV 39, SRM 51-42-06 REV 39, SRM 51-24-21 REV 39 AND SRM 51-42-20 REV 39. WORK PERFORMED UNDER AERSALE WORK ORDER 004393, CARD NO. 20146, TT: 44,686:36 TC: 42,772.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,686 hrs · 42,772 cycles

SEAT TRACK PN 20276-288-0-0 AT FS364.00 TO 559.00 +80 LHS HAS CORROSION AT NUMEROUS LOCATIONS. AIRCRAFT REMOVED FROM SERVICE REPLACED WITH A NEW SEAT TRACK PN 20276-288-0-0 AT FS544.00 TO FS599.00 LHS. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 AMM 53-01-11 REV 66. WORK PERFORMED UNDER AERSALE WORK ORDER 004393, CARD NO. 20140, TT: 44686:36 TC: 42772.

Part: STRAP — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,686 hrs · 42,772 cycles

CORROSION ON FLOOR STRAP L/H AT FS559.00 AND LBL27-36. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED 1EA STRAP PN 601R31025-29 ON FLOOR STRAP L/H AT FS559.00 AND LBL27 TO 36. IAW CRJ-200 SRM 51-42-06 REV 36. . PERFORMED HFEC WITH NO INDICATIONS. RESTORED SURFACE FINISH. WORK PERFORMED UNDER AERSALE WORK ORDER 004393, CARD NO. 20145, TT: 44,686;36 TC: 42,772

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,686 hrs · 42,772 cycles

SEAT TRACK PN 20276-288-0-0 AT FS544.00 TO 559.00 RHS HAS CORROSION AT NUMEROUS LOCATIONS. AIRCRAFT REMOVED FROM SERVICE. REPLACED WITH A NEW SEAT TRACK PN 20276-288-0-0 AT FS544.00 TO FS599.00 RHS. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 AMM 53-01-11 REV 66. WORK PERFORMED UNDER AERSALE WORK ORDER 004393, CARD NO. 20141, TT: 44686:36 TC: 42772.

Part: CONTROL LEVER — FAILED (FLAP SYS) · airframe 44,460 hrs · 42,516 cycles

ON APPROACH RECEIVED FLAP FAIL AT 20 DEGREES. AIRCRAFT REMOVED FROM SERVICE. TROUBLESHOT PER FIM SUPP. 98-018I. REMOVED AND REPLACED FLAP CONTROL LEVER IAW AMM SUPP. 09-038A. OPS CHECKS GOOD. REMOVED PLACARD + FROM MEL.

Part: DRIVE UNIT — UNKNOWN (MLG BAY) · airframe 43,832 hrs · 41,801 cycles

RECIEVED FLAPS FAIL CAUTION MSG FLAPS FAIL AT 20* IN FLIGHT. PERFORMED FLAP RESET PROCEDURES IAW AWAC SUP 09-018I BOX 12 FLAPS RESET ********AIRCRAFT REMOVED FROM SERVICE******** R&R FLAP PDU

Part: PROXIMITY SENSOR — NONE (MAIN AVIONICS CO) · airframe 43,641 hrs · 41,603 cycles

AFTER DROPPING LDG GEAR 5MIN LATER NOSE DOOR OPEN WARN MSG ANTI SKID IB/OB CAU MSG AND PARK BRAKE SOV/ PROX SYS CAU MSGS. C/W QRH LANDED NORMAL. TAXIED OFF RUNWAY. GOT TOWED TO GATE. HAD 3 GREENS BUT PULLED EMER GEAR RELASE HANDLE PER QRH. ******AIRCRAFT REMOVED FROM SERVICE*********** R&R PSEU IAW AMM 32-61-01 PERF OPS CK IAW AMM 32-61-00 PERF ANTISKID SYS OPS CK IAW AMM 32-44-01 OPS CK GOOD INSP GEAR MANUL SYS IAW AWAC SUP 18-077 OPS CK GOOD P/N: 8-648-08, S/N OFF: C454, S/N ON: C345 ARW

Part: NONE — NONE · airframe 41,803 hrs · 39,850 cycles

ON CLIMB OUT, HEARD LOUD SQUEAL FROM PAX DOOR AREA. ABOVE 11,000' COULD NOT MAINTAIN CABIN PRESSURE. PACKS NORMAL, DOOR INDICATIONS NORMAL. DIVERTED TO MKE. ***AIRCRAFT REMOVED FROM SERVICE*** R/R PAX DOOR SEAL PER AWA SUP 21-023 AND AMM 52-11-10 OPS AND PRESSURIZATION CHECK GOOD AT THIS TIME.

Part: SKIN — DENTED (LT GRND SPOILER) · airframe 39,877 hrs · 37,883 cycles

LEFT WING, I/B GROUND SPOILER LOWER SURFACE HAS ROCK DAMAGE. AIRCRAFT REMOVED FROM SERVICE REPAIRED LEFT WING I/B GROUND SPOILER IAW EA# AWAC-CRJ257-01402 REV-IR.

Part: FLOOR SUPPORT — DAMAGED (BS 574-621) · airframe 39,877 hrs · 37,883 cycles

FLOOR SILL AT CARGO DOOR HAS SEVERAL ELONGATED HOLES AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED FLOOR SILL AT CARGO DOOR IAW BOMB. REO 601R-53-61-690 REV. D

Part: POST — CRACKED (BS 409) · airframe 39,877 hrs · 37,883 cycles

BS 409+128 VERTICLE POST AT RBL 18 WAS CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE VERTICLE POST IAW REO 601R-53-41-889.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 39,877 hrs · 37,883 cycles

PASSENGER DOOR EDGE MEMBER CRACKED ON FWD SIDE OF DOOR AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED EDGE MEMBER IAW CRJ-200 SRM 51-42-06 AND 51-42-10

Part: ANGLE — DAMAGED (SERVICE DOOR) · airframe 39,878 hrs · 37,884 cycles

SUPPLEMENTAL INFORMATION, INSIDE OF SERVICE DOOR HAS SEVERAL IMPROPERLY INSTALLED AND MISSING FASTENERS AND DAMAGED ANGLES AT FS 342.00, WL 73.50 TO WL 93.50. AIRCRAFT REMOVED FROM SERVICE. REPAIRED SERVICE DOOR IAW SRM 51-42-06, 51-42-10, 51-42-21 AND 51-42-22.

Part: ANGLE — DAMAGED (SERVICE DOOR) · airframe 39,877 hrs · 37,883 cycles

INSIDE SERVICE DOOR HAS SEVERAL IMPROPERLY INSTALLED AND MISSING FASTENERS AND DAMAGE ANGLE AT FS 342.00 WL 73.5 AND WL93.50 AIRCRAFT REMOVED FROM SERVICE REPAIRED SERVICE DOOR IAW CRJ 200 SRM 51-42-06 51-42-10 51-42-21 AND 51-42-22

Part: DOUBLER — CRACKED (EXHAUST) · airframe 39,877 hrs · 37,883 cycles

436AL HAS CRACKED DOUBLER AT MOUNTING HOLE PANEL AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED DOUBLER AT MOUNTING HOLE ON PANEL 436AL IAW BOMB. CMM 20-42-06

Part: DOUBLER — CORRODED (BS 310-319) · corrosion level 2 · airframe 39,877 hrs · 37,883 cycles

R/H FLOOR SILL GALLEY SHOOT BOLT MOUNT BETWEEN FS310 AND FS319 HAS CORROSION AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED R/H FLOOR SILL GALLEY MOUNT IAW CRJ 200 SRM 51-42-06

Part: FLOOR SUPPORT — CORRODED (BS 319) · corrosion level 2 · airframe 39,877 hrs · 37,883 cycles

RIGHT FLOOR SILL CORRODED AT FS 319.00. AIRCRAFT REMOVED FROM SERVICE REPLACED FLOOR SILL IAW CRJ200 SRM 51-42-06.

Part: SKIN — CRACKED (NACELLE) · airframe 39,877 hrs · 37,883 cycles

PANEL 435AB HAS CRACKED AREA ON INSODE SKIN PANEL, AIRCRAFT REMOVED FROM SERVICE, REPAIR INNER SKIN IAW BOMBARDIER CMM 71-12-01 SRS0460

Part: RETAINER — CRACKED (PAX DOOR) · airframe 39,877 hrs · 37,883 cycles

SUPPLEMENTAL INFORMATION, PASSENGER DOOR LOWER CENTER SEAL RETAINER DAMAGED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED PASSENGER DOOR SEAL RETAINER IAW SUPP 18-014A.

Part: ATTACH ANGLE — CRACKED (BS 621) · airframe 39,877 hrs · 37,883 cycles

CARGO BEAM MEMBER AFT ATTACH ANGLE CRACKED, AIRCRAFT REMOVED FROM SERVICE, REMOVED AND REPLACED CRACKED ANGLE ON CARGO BEAM MEMBER IAW CRJ 200 SRM 51-42-21

Part: SEAL — CHAFED (COWLING) · airframe 39,877 hrs · 37,883 cycles

SUPPLEMENTAL INFORMATION, PANEL 432AT ACCESS COWL HAS CHAFED AFT SEAL. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED AFT EDGE STRIP IAW CMM 71-14-01.

Part: BRACKET — CRACKED (BS 193-210) · airframe 39,877 hrs · 37,883 cycles

BRACKET FOR EXTERNAL SERVICE BOX CRACKED INSIDE PANEL 122CR AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED BRACKET IAW CRJ 200 SRM 51-42-06 AND SRM 51-41-02

Part: WINDSHIELD — FAILED (FIRST OFFICER'S) · airframe 37,901 hrs · 36,000 cycles

FIRST OFFICER`S WINDSHIELD SHATTERED IN FLIGHT. COMPLIED WITH QRH.

Part: ANGLE — CRACKED (ASSIST MOTOR) · airframe 36,765 hrs · 34,831 cycles

PAX DOOR ASSIST MOTOR LOWER ANGLE CRACKED.

Part: RETAINER — CRACKED (DOOR SEAL) · airframe 36,765 hrs · 34,831 cycles

PAX DOOR LOWER FWD SEAL RETAINER CRACKED.

Part: PLUG — MISSING (BS 222 SKIN) · airframe 36,765 hrs · 34,831 cycles

FUSELAGE SKIN CUT OUT AT BS 222, STRINGER 22L HAS MISSING FREEZE PLUG FOR CHEEK PANEL 131AL.

Part: SKIN — TORN (FUSELAGE) · airframe 36,765 hrs · 34,831 cycles

PAX DOOR CUTOUT FWD LOWER CORNER SKIN TORN.

Part: SEAL — CRACKED (LT SPOILER) · airframe 36,765 hrs · 34,831 cycles

LEFT FLT SPOILER INBD SPRING SEAL IS CRACKED.

Part: BRACKET — CRACKED (BS 700-718) · airframe 36,765 hrs · 34,831 cycles

AFT ACCESSORY BAY, HYDRAULIC SYSTEM NR 2 PRESSURE AND RETURN MANIFOLD MOUNT BRACKET CRACKED.

Part: ANGLE — CRACKED (BS 621-625) · airframe 36,765 hrs · 34,831 cycles

ANGLE CRACKED AT THE INBD SIDE OF STRINGER 14L IN THE AFT EQUIPMENT BAY.

Part: SEAL — CRACKED (RT SPOILER) · airframe 36,765 hrs · 34,831 cycles

RIGHT FLT SPOILER CENTER SPRING SEAL IS CRACKED.

Part: ANGLE — CRACKED (BS 621-625) · airframe 36,765 hrs · 34,831 cycles

ANGLE CRACKED AT THE INBD SIDE OF BS 625.3, STRINGER 13L IN THE AFT EQUIPMENT BAY AFT OF PRESSURE BULKHEAD.

Part: BRACKET — BROKEN (TRANSDUCER) · airframe 36,765 hrs · 34,831 cycles

RIGHT MLG BRAKE APPLICATION PRESSURE TRANSDUCER MOUNTING BRACKET BROKEN IN THE R/H MLG WHEEL WELL FS530 AND RBL23.

Part: ANGLE — CRACKED (BS 625) · airframe 36,765 hrs · 34,831 cycles

ANGLE CRACKED AT THE INBD SIDE OF FRAME BS 625.3, STRINGER 13R IN THE AFT EQUIPMENT BAY, JUST AFT OF 621 BULKHEAD.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 36,765 hrs · 34,831 cycles

1014984 3000-0026 - AFT ACCESSORY BAY INTERCOSTAL AT FS621-FS625 AT STRL13L CRACKED

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 36,765 hrs · 34,831 cycles

AFT ACCESSORY BAY INTERCOSTAL AT BS 621 - 625, STRINGER 15L IS CRACKED

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 36,765 hrs · 34,831 cycles

AFT ACCESSORY BAY INTERCOSTAL AT BS 621 - 625, STRINGER 14L CRACKED.

Part: STATIC WICK — CRACKED (RT AILERON) · airframe 36,765 hrs · 34,831 cycles

RIGHT AILERON STATIC WICK BASE IS CRACKED.

Part: FLOORBEAM — CORRODED (BS 620) · corrosion level 2 · airframe 36,765 hrs · 34,831 cycles

FLOORBEAM ANGLE AT BS 621 HAS CORROSION BETWEEN LBL 9 AND LBL 27 IN THE CARGO BAY.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 36,765 hrs · 34,831 cycles

AFT ACCESSORY BAY INTERCOSTAL AT BS 621 - 625, STRINGER 16L IS CRACKED.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 36,765 hrs · 34,831 cycles

LEFT SIDE OVER WING ACCESS PNL ATTACH BRACKET AT FS461 IS CRACKED.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 36,765 hrs · 34,831 cycles

LEFT SIDE OVER WING ACCESS PNL ATTACH BRACKET AT FS449 IS CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 36,765 hrs · 34,831 cycles

APU SKID ASSY PLATFORM LT SIDE BRACE AT ABOUT LBL18 UPPER O/B ANGLE BRACKET IS CRACKED IN THE AFT EQUIPMENT BAY.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 36,765 hrs · 34,831 cycles

LT FLOOR SILL IS CRACKED AT FS589 IN THE CARGO BAY.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 36,765 hrs · 34,831 cycles

RIGHT SIDE OVER WING ACCESS PNL ATTACH BRACKET AT FS468 IS CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 36,765 hrs · 34,831 cycles

ANGLE CLIP IS CRACKED AT THE O/B SIDE OF RBL27 AT FS484 IN CABIN BELOW THE FLOOR.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 36,765 hrs · 34,831 cycles

ANGLE CLIP IS CRACKED AT THE I/B SIDE OF RBL36 AT FS 484 IN THE CABIN BELOW THE FLOOR.

Part: PANEL — CRACKED (PAX DOOR) · airframe 36,765 hrs · 34,831 cycles

PAX DOOR UPPER PANEL AFT CORNER HAS A POSSIBLE CRACK.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 36,765 hrs · 34,831 cycles

LEFT SIDE OVER WING ACCESS PNL ATTACH BRACKET AT FS468 IS CRACKED.

Part: FITTING — CRACKED (COCKPIT) · airframe 36,765 hrs · 34,831 cycles

FLIGHT DECK WINDSHIELD CENTER POST LOWER LEFT FITTING IS CRACKED (NDT HAS VERIFIED)

Part: PDU — FAILED (THRUST REVERSER) · airframe 36,696 hrs · 34,763 cycles

DURING TAKEOFF ROLL, ABOVE 80 KNOTS, RECEIVED A RIGHT THRUST REVERSER MESSAGE, FOLLOWED BY AN UNLOCK MESSAGE, FOLLOWED BY AN EMERERGENCY STOW LIGHT. ABORTED TAKEOFF. R & R THE RT THRUST REVERSER PDU, FOUND BAD FLEX LOCK SWITCH.

Part: NONE — NONE · airframe 36,509 hrs · 34,571 cycles

4921 EMERGENCY FLOOR LIGHTS AT TOW 7 AND 8 NOT ILLUMINATING OPS CHECK GOOD IAW AMM 33-51-00

Part: AUTOPILOT SYS — INOPERATIVE · airframe 35,273 hrs · 33,412 cycles

AIRCRAFT EXPERIENCED SUBSTANTIAL UNCOMMANDED YAW AT 10,000 FEET IN SMOOTH AIR. AUTOPILOT DID NOT DISENGAGE AFTER 2 EPISODES. C/W QRH, DISCONNECTED AND AUTOPILOT AND YD NO FURTHER UNCOMMANDED YAW.

Part: LIGHT — MISSING (CABIN) · airframe 33,223 hrs · 31,512 cycles

LAST 4 FT OF EMER LIGHT STRIPS MISSING. ALSO MISSING ORANGE ARROWS AT LAST STRIP THAT IS THERE.

Part: SHUTOFF VALVE — STICKS (ANTI-ICE SYSTEM) · airframe 33,154 hrs · 31,448 cycles

ON CLIMB OUT AT FL 6000', RECEIVED LT WING ANTI-ICE CAUTION, FOLLOWED QRH, SELECTED STANDBY. MSG WENT OUT & RETURNED WITHIN A MINUTE. SELECTED 14TH STAGE ISO VLV OPEN, MSG WENT AWAY, LEFT ICING LANDED, DECLARED AN EMER. COMPLIED WITH FIM 30-10-00. FOUND LT WING MSOV INTERMITTENTLY STICKING CLOSED. R & R VLV IAW AMM 30-12-04. OPERATIONS CHECK FAILED. R & R LT BLEED AIR SOV IAW AMM 30-12-04, NO FIX, LT WING ANTI-ICE VERIFIED, WORKS IN STANDBY MODE. R & R RELAY K1HA IAW 30-11. OPERATIONS CHECKED GOOD.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

DURING INSTALLATION OF PANEL 131AL, THE FREEZE PLUG AT HOLE 15 PULLED OUT, REPAIRED.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

DURING INSTALLATION OF PANEL 131AL, THE FREEZE PLUG AT HOLE 32 PULLED OUT, REPAIRED.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

DURING INSTALLATION OF PANEL 131AL, THE FREEZE PLUG AT HOLE 22 PULLED OUT, REPAIRED.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

DURING INSTALLATION OF PANEL 131AL, THE FREEZE PLUG AT HOLE 28 PULLED OUT, REPAIRED.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

DURING INSTALLATION OF PANEL 131AL, THE FREEZE PLUG AT HOLE 12 PULLED OUT, REPAIRED.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

DURING INSTALLATION OF PANEL 131AL, THE FREEZE PLUG AT HOLE 17 PULLED OUT, REPAIRED.

Part: WEB — CRACKED (RT MLG WW) · airframe 32,640 hrs · 30,973 cycles

RIGHT MLG WW UPPER WEB DAMAGED DURING GEAR SWING, REPAIRED.

Part: SEAL DEPRESSOR — GOUGED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

SERVICE DOOR CUT OUT SEAL DEPRESSOR IS GOUGED ON AFT SIDE, APPROX 12" FROM UPPER AFT CORNER.

Part: SEAL DEPRESSOR — GOUGED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

GALLEY SERVICE DOOR, UPPER PRESS SEAL DEPRESSOR IS GOUGED IN SEVERAL AREAS.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

INTERCOSTAL JUST TO THE LT OF STRINGER 27 HAS CORROSION, BETWEEN FRAMES 349 & 364, REPAIRED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

INTERCOSTAL ON TOP OF STRINGER 26L HAS CORROSION, BETWEEN FRAMES 349 & 364, REPAIRED.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

LEFT GUSSET ON TOP OF FRAME 364 AT STRINGER 26L HAS CORROSION, REPAIRED.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,640 hrs · 30,973 cycles

INTERNAL SKIN DOUBLER AROUND POTABLE WATER DRAIN LINE HAS CORROSION, BETWEEN FRAMES 349 & 333, REPLACED.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

LONGERON ON STRINGER 25L HAS CORROSION ON THE OTBD SIDE, BETWEEN FRAMES 349 & 364, REPAIRED.

Part: BEAM — CRACKED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

FS 409.00+128 VERTICAL BEAM, RBL 27 INBD LOWER CORNER IS CRACKED, REPAIRED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

INTERCOSTAL JUST TO THE RT OF STRINGER 27 HAS CORROSION, BETWEEN FRAMES 364 & 349, REPAIRED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

FRAME 319.70 HAS CORROSION ON THE FWD SIDE, BETWEEN STRINGER 22R & 23R, REPAIRED.

Part: ANGLE — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 32,640 hrs · 30,973 cycles

SERVICE DOOR LOWER SILL ANGLE IS CORRODED, REPLACED.

Part: FITTING — CRACKED (NLG WW) · airframe 32,640 hrs · 30,973 cycles

NOSE LANDING GEAR WELL RT TOP AT FS 193.00, CLIP CRACKED, REPAIRED.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

GROUND ACFT SERVICE PANEL, LOWER MOUNT, HINGE DOUBLER CRACKED, REPLACED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,640 hrs · 30,973 cycles

INTERCOSTAL ON TOP OF STRINGER 25R, CORROSION ON BOTH THE INBD & OTBD SIDES, BETWEEN FRAME 364 & 349, REPAIRED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,640 hrs · 30,973 cycles

FORWARD SIDE OF FRAME 364 HAS CORROSION, BETWEEN STRINGER 25L & 22R. REPLACED FRAME SECTOR.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,640 hrs · 30,973 cycles

FLOORBEAM END & TAB HAS CORROSION ON THE TOP & BOTTOM SIDES, JUST INBD OF THE SERVICE DOOR OPENING, REPAIRED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,640 hrs · 30,973 cycles

FRAME 349 HAS NUMEROUS CORROSION SPOTS ON THE FWD & AFT SIDES, BETWEEN STRINGER 25L - 20R, REPAIRED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,640 hrs · 30,973 cycles

INTERCOSTAL JUST TO THE RT OF STRINGER 27 HAS CORROSION, BETWEEN FRAMES 394 & 409, REPAIRED.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 32,640 hrs · 30,973 cycles

RIGHT HORIZONTAL LE RIB AT INBD STATION BL 6.0 HAS SMALL CRACK, .250 IN LENGTH, REPAIRED.

Part: TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,640 hrs · 30,973 cycles

LBL 9 TIE DOWN TRACK AT FS 559.00+112 HAS CORROSION, REPLACED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 32,640 hrs · 30,973 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED ADJACENT TO ASSIST CABLE PULLEY BRACKET, REPLACED.

Part: SKIN — CHAFED (RT AILERON) · airframe 32,640 hrs · 30,973 cycles

RIGHT AILERON, UPPER FIXED LE SKIN CHAFED. R & R RT AILERON, FIXED UPPER SKIN IAW SRM 51-42-06 & SUPPLEMENT 13-055B.

Part: STIFFENER — CRACKED (LT JET PIPE) · airframe 32,640 hrs · 30,973 cycles

LEFT JET PIPE FAIRING, CRACKED AT FWD INNER SUPPORT RING. REPAIRED LT EXHAUST NOZZLE FAIRING FWD STIFFENER IAW CMM 78-11-00-300-810-A01 REPAIR SRS 042.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,640 hrs · 30,973 cycles

RIGHT WINDSCREEN, INBD SHOOT BOLT FITTING HAS CORROSION COMING OUT OF SHOOT BOLT HOLE ON FLOORBEAM 349, BETWEEN RBL 9 & RBL 27, REPLACED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

EXTERIOR LOWER SKIN IS CREASED AT APPROX FS 598, BETWEEN STRINGERS 23L & 24L, REPAIRED.

Part: SKIN — CHAFED (TE FLAP) · airframe 32,241 hrs · 31,113 cycles

LEFT OTBD FLAP, UPPER SKIN INBD END HAS SMALL CHAFE, REPAIRED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

BATHTUB FITTING IS CRACKED AT FS 461, OTBD SIDE OF RBL 9, IN CABIN. R & R.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 32,640 hrs · 30,973 cycles

TIE DOWN TRACK FS 559.00+80 TO 559+96, LBL 27 IS CORRODED. R & R.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,640 hrs · 30,973 cycles

LEFT SIDEWALL SEAT TRACK, STICK 2 HAS CORROSION, IN CABIN. R & R.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 32,640 hrs · 30,973 cycles

TIE DOWN TRACK AT RBL 9 AT FS 559.00+90 HAS CORROSION. R & R.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

STRINGER 3L, INBD & OTBD CLIPS ARE CRACKED, JUST AFT OF THE 280 BULKHEAD. R & R CLIPS.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

CARGO BAY DOOR OPENING OVERHEAD BEAM, AFT INBD ANGLE BRACKET AT THE AFT PRESS BULKHEAD, IS CRACKED. R & R.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,640 hrs · 30,973 cycles

LEFT SIDEWALL SEAT TRACK, STICK 6 HAS CORROSION & IS CHAFED, IN CABIN. R & R.

Part: FITTING — CRACKED (COCKPIT) · airframe 32,640 hrs · 30,973 cycles

RIGHT WINDSHIELD SIDE POST, LOWER AFT ANGLE FITTING IS CRACKED AT WL 110, IN THE FLIGHT DECK. R & R.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 32,640 hrs · 30,973 cycles

TIE DOWN TRACK AT RBL 27, FS 559.00+80 HAS CORROSION, R & R.

Part: FITTING — CRACKED (COCKPIT) · airframe 32,640 hrs · 30,973 cycles

LEFT WINDSHIELD SIDE POST, LOWER AFT ANGLE FITTING IS CRACKED AT WL 110, IN THE FLIGHT DECK. R & R.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 32,640 hrs · 30,973 cycles

TIE DOWN TRACK AT RBL 9, FS 559.00+112 HAS CORROSION. R & R.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 32,640 hrs · 30,973 cycles

CARGO TIE DOWN TRACK AT FS 615.00, LBL 9 HAS CORROSION. R & R.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 32,640 hrs · 30,973 cycles

CARGO TIE DOWN TRACK AT FS 559.00+90, LBL 9 HAS CORROSION. R & R.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

FLOORBEAM FS 280, UPPER ANGLE IS CRACKED JUST OTBD OF RBL 9, IN CABIN.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

ANGLE CLIP IS CRACKED AT THE OTBD SIDE OF RBL 9 & FLOORBEAM 280, IN CABIN.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

CARGO DOOR SILL CRACKED AT FS 605.00. REPAIRED IAW REO 601R-53-61-433.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,640 hrs · 30,973 cycles

LEFT AISLE SEAT TRACK STICK 5 HAS CORROSION, IN CABIN.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,640 hrs · 30,973 cycles

LEFT AISLE SEAT TRACK STICK 1 HAS CORROSION, IN CABIN.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

ANGLE CLIP IS CRACKED AT THE OTBD SIDE OF LBL 27 AT FS 484, IN CABIN. R & R.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,640 hrs · 30,973 cycles

ANGLE CLIP IS CRACKED AT THE INBD SIDE OF LBL 36 AT FS 484, IN CABIN.

Part: CARBON SEAL — DEFECTIVE (LT ENGINE) · airframe 32,414 hrs · 30,758 cycles

RECEIVED LT ENG OIL PRESS WARNING ENROUTE. WARNING WAS INTERMITTENT. ENG LEFT AT IDLE FOR DURATION OF FLIGHT. COMPLIED WITH QRH. LOWEST KNOWN OIL PRESS WAS 29 PSI. LOW OIL PRESS WARNING LASTED NO LONGER THAN 10 SECONDS. PERFORMED CONSUMPTION RUN & FOUND IDG CARBON SEAL TO BE BAD. R & R IDG CARBON SEAL IAW AWAC 05-018E. LEAK CHECK, OPERATIONS CHECK & CONSUMPTION RUN GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,576 hrs · 29,947 cycles

FLIGHT NUMBER 3926. EMERGENCY LIGHTS WILL NOT ILLUMINATE. R & R FOUR EMERGENCY LIGHT BATTERY PACKS IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 30,693 hrs · 29,117 cycles

REF LP 273644 1 PAX DOOR AFT CLOSING FRAME CRACKED.

Part: UNKNOWN — MALFUNCTIONED (NLG STEERING) · airframe 30,648 hrs · 29,078 cycles

AIRCRAFT YAWED LEFT AFTER BRAKE RELEASE ON TAKEOFF. UNABLE TO CORRECT WITH FULL RT RUDDER. ABORTED TAKEOFF APPROX 35 KNTS. BTMS = 2-1-2-3. NOSE TIRE PRESSURES ARE GOOD, NO DEFECTS NOTED ON TORQUE LINKS. RUDDER PEDAL RVDT DOTS LINE UP, NWS OPERATIONS CHECKED GOOD IAW AMM 32-51-00.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 30,591 hrs · 29,022 cycles

ON APPROACH, APU DID NOT LIGHT OFF, ABORTED START & RE-STARTED AFTER 2 MINUTES. COCKPIT & CABIN FILLED WITH EXCESSIVE FUEL ODOR, SHUTDOWN APU & FUEL ODOR CLEARED.

Part: SKIN — DENTED (BS 672) · airframe 28,044 hrs · 26,568 cycles

LEFT EXTERNAL SKIN HAS TWO PROTRUDING DENTS AT FS 672, STR 19L. COLD WORKED DENTS BACK TO ALLOWABLE LIMITS IAW EA- 15-2013-464, REV A.

Part: RETAINER — DENTED (CARGO DOOR) · airframe 28,044 hrs · 26,568 cycles

CARGO DOOR SEAL RETAINERS DENTED AT UPPER AFT, BOTTOM AFT, AND BOTTOM MID SECTIONS. REMOVED AND INSTALLED NEW RETAINERS, UPPER AFT, BOTTOM AFT AND BOTTOM CENTER.

Part: SKIN — DAMAGED (BS 634) · airframe 28,044 hrs · 26,568 cycles

SKIN DAMAGED AT FS 634, STR 24L. PERFORMED REPAIR ON LT AFT SKIN IAW REO 601R-53-61-5033, REV A.

Part: SKIN — DENTED (BS 625.3-640) · airframe 28,044 hrs · 26,568 cycles

TWO PROTRUDING DENTS IN FUSELAGE SKIN AT FS 625.3 BETWEEN STR 26L & STR 25L. REPAIRED SKIN IAW REO 601R-53-61-5068, REV-.

Part: GROUND STUD — CORRODED (BS 589) · airframe 28,044 hrs · 26,568 cycles

GROUND STUDS ON FRAME 589, BETWEEN 17R AND 19R HAVE CORROSION AROUND STUDS. BLENDED FRAME, FOUND TO BE WITHIN LIMITS AND R & R ANGLE AT STR 17 FWD AND AFT OF FRAME 589.

Part: SKIN — GOUGED (LT NACELLE) · airframe 28,044 hrs · 26,568 cycles

LEFT LOWER CORE COWL HAS GOUGE FROM BLOCKER DOOR ON OUTER SKIN JUST AFT OF FWD LATCHES. COMPLIED WITH EA 15-2013-463 BY BLEND OUT DAMAGE AND INSTALL DOUBLER.

Part: RIB — CRACKED (LT WING WW) · airframe 28,044 hrs · 26,568 cycles

LEFT W/W BATT RIB CRACKED AT AFT CORNER. INSTALL DOUBLER REPAIR IAW REO 601R-57-51-046, REV B.

Part: CLEAT — DAMAGED (PAX DOOR) · airframe 28,044 hrs · 26,568 cycles

PAX DOOR AFT CLEAT BRACKET BLENDED OUT OF SERVICEABLE LIMITS. R & R AFT CLEAT BRACKET.

Part: MOUNT FITTING — CORRODED (BS 310-349) · corrosion level 2 · airframe 28,044 hrs · 26,568 cycles

MOUNTING PLATES FOR CONNECTORS JIMB & J2MB ARE CORRODED. REMOVED UNSERVICEABLE BRACKET CONNECTOR & REPLACED WITH 2 EA 601R31771-1 IAW SRM 51-42-06.

Part: BRACKET — CRACKED (ACCUMULATOR) · airframe 28,044 hrs · 26,568 cycles

HYD NR 3 BRAKE ACCUMULATOR FWD/OB MOUNT BRACKET CRACKED. R & R WITH NEW IAW SRM.

Part: SKIN — CHAFED (RT MLG DOOR) · airframe 28,044 hrs · 26,568 cycles

RIGHT MLG DOOR INNER SKIN HAS GOUGE AND 2 CHAFED RIVETS. R & R INNER SKIN ON RT MLG DOOR.

Part: RIB — CRACKED (RT WING WW) · airframe 28,044 hrs · 26,568 cycles

RT W/W BATTERY RIB CRACKED. REPAIRED RT BATTERY RIB IAW REO 601R-57-51-046, REV B.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 28,044 hrs · 26,568 cycles

LT SIDE SEAT TRACK CORRODED AT FS 559+77. REPLACED SECTION OF SEAT TRACK FROM 546 TO 559+80 IAW SRM , AMM AND REO 601R-53-00-485.

Part: FAIRING — DAMAGED · airframe 28,044 hrs · 26,568 cycles

CENTER ATTACH FITTINGS FOR BELLY FAIRING 193AB HAVE ELONGATED HOLES. R & R IAW SRM 51-41-02.

Part: SKIN — DAMAGED (RT NACELLE) · airframe 28,044 hrs · 26,568 cycles

RT LOWER CORE COWL ALIGNMENT HOLES ELONGATED. FABRICATED AND INSTALL 2 EA DOUBLER FOR RT LOWER CORE COWL ALIGNMENT HOLES.

Part: FLOOR SUPPORT — CORRODED (BS 450-559) · corrosion level 2 · airframe 28,044 hrs · 26,568 cycles

LEFT OTBD FLOOR SUPPORT HAS CORROSION NEAR FS 450 - 559. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06 , REPAIRED IAW SRM 51-42-06.

Part: DRAG ANGLE — CRACKED (RT MLG WW) · airframe 28,044 hrs · 26,568 cycles

RIGHT W/W DRAG ANGLE CRACKED AT FWD & AFT CORNERS. R & R DRAG ANGLE WITH SERVICEABLE IAW SRM 51-40-11 & SRM 51-42-21.

Part: FLOORBEAM — CORRODED (BS 589) · corrosion level 2 · airframe 28,044 hrs · 26,568 cycles

FLOORBEAM FS 589, RBL 36 TO RBL 18 HAS CORROSION. REMOVED CORROSION FROM FLOORBEAM AND R & R FLOORBEAM CAP.

Part: SUPPORT BRACKET — CRACKED (BS 718) · airframe 28,044 hrs · 26,568 cycles

NR 2 HYD RETURN MANIFOLD ASSY SUPPORT BRACKET CRACKED AT LOWER AFT CORNER. CUTOUT DAMAGED SECTION OF BRACKET AND INSTALLED FABRICATED ANGLE IAW REO 601R-53-62-031, REV A.

Part: DRAG ANGLE — CRACKED (BS 489-499) · airframe 28,044 hrs · 26,568 cycles

LEFT WW DRAG ANGLE COMMON TO BATTERY RIB CRACKED. R & R WITH SERVICEABLE PART IAW SRM 51-42-21.

Part: BRACKET — BROKEN (BS 574-589) · airframe 28,044 hrs · 26,568 cycles

CARGO DOOR SILL FWD FOLDING STEP BRACKET BROKEN. R & R CARGO DOOR SILL FWD BRACKET IAW SRM 51-42-20.

Part: STRUCTURE — DAMAGED (BS 621) · airframe 28,044 hrs · 26,568 cycles

SIX RIVET HEADS HAVE SCREW DAMAGE. REMOVED DAMAGED FASTENERS AND INSTALLED NEW FASTENERS IAW SRM 42-06.

Part: HEAT SHIELD — CRACKED (EXHAUST PIPE) · airframe 28,044 hrs · 26,568 cycles

RT JET PIPE HEAT SHIELD CRACKED BETWEEN SECOND AND THIRD STIFFENERS. REPAIRED IAW CMM 78-11-00.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 28,044 hrs · 26,568 cycles

FS 621, BULKHEAD HAS SCREW DAMAGE. BLENDED DAMAGE TO SMOOTH.

Part: TRUNNION — DAMAGED (RT WING) · airframe 26,406 hrs · 24,959 cycles

DURING COLD WORKING OF THE FASTENER HOLES OF THE MLG TRUNNION LOWER FLANGE FOUND 1 EA OVER SIZED HOLES ON RT SIDE. REPAIRED OVERSIZED HOLES ON RIGHT LOWER MLG TRUNNION FLANGE IAW BOMBARDIER REO 601R-57-21-1864 REV -.

Part: FLAP — DENTED (LT WING) · airframe 26,406 hrs · 24,959 cycles

LEFT I/B FLAP DENTED AT TRAILING EDGE FO PANEL 583BB. REPAIRED IAW BOMBARDIER REO 601R-57-52-2011.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 26,406 hrs · 24,959 cycles

CARGO BAY DOOR SUPPORT BRACKET HAS CRACKED SUPPORT ANGLE ON 621 BULKHEAD. REMOVED UNSERVICEABLE ANGLE AND REPLACED WITH SERVICEABLE ANGLE, FABRICATED FROM MATERIAL 2024 T3 .040 IAW CRJ 200 SRM 51-24-21, 51-42-21.

Part: CONTROL HANDLE — INOPERATIVE (MLG) · airframe 25,244 hrs · 23,822 cycles

AFTER TAKE OFF, SELECTED GEAR UP. RECEIVED ANTI-SKID INBD CAUTION, AND PARK BRAKE SOV CAUTION MESSAGES. GEAR DID NOT MOVE. NO GEAR DISAGREE MESSAGE DISPLAYED. R & R LANDING GEAR CONTROL HANDLE IAW AMM 32-31-01. OPS CHECKED GOOD. GEAR RETRACTION/EXTENSION WAS ACCOMPLISHED REF AMM 32-31-01.

Part: CHECK VALVE — FAILED (A/C PACK) · airframe 23,945 hrs · 22,536 cycles

AFTER LANDING, STRONG SMOKE ODOR IN COCKPIT FOLLOWED BY LT PACK HIGH TEMP CAUTION MESSAGE, FOLLOWED BY SMOKE TOILET CAUTION MESSAGE. COMPLIED WITH QRH. ACTUAL SMOKE AND TEMP MESSAGE REMOVED. FOUND LT PACK FAN BYPASS CHECK VALVE, RAM AIR CHECK VALVE MISSING BOTH FLAPPER DOORS. R & R FAN BYPASS CHECK VALVE REF AMM 21-52-07. OPS CHECKED GOOD. NO ODOR PRESENT.

Part: SWITCH — FAILED (PITCH TRIM) · airframe 23,782 hrs · 22,366 cycles

MACH TRIM & STAB TRIM CAUTION MESSAGES CLIMBING THROUGH 12,000 FT. RAN QRH, WOULD NOT RESET. LANDED AT 45,000 LBS, SPEED 150 KTS, TOUCHDOWN APPROXIMATELY 200 FPM. R & R PITCH TRIM DISCONNECT SWITCH.

Part: FLOORBEAM — CRACKED (FS 280) · airframe 23,519 hrs · 22,105 cycles

FLOORBEAM CRACKED AT THE 280 BULKHEAD, RBL 9. REPAIRED FLOORBEAM IAW REO 601R-53-11-136, 601R-53-11-2225 AND 601R-53-11-171.

Part: LUG — GOUGED (HORIZONTAL STAB) · airframe 23,519 hrs · 22,105 cycles

HORIZONTAL STAB LT OTBD LUG GOUGED. BLENDED DAMAGED AREA NDT INSPECTED FLAP PEENED, ALODINED, PRIMED IAW REO 601R-55-11-391.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 23,519 hrs · 22,105 cycles

PAX DOOR HANDLE IS CRACKED. R & R PAX DOOR HANDLE, PN 601R-31763-1.

Part: BRACKET — CRACKED (BS 574) · airframe 23,519 hrs · 22,105 cycles

LOWER U-BRACKET AT FS 574 CRACKED. REMOVED DAMAGED U-BRACKET AND INSTALLED NEW CHANNEL PN 601R-35050-25 IAW SRM 51-42-06, 51-40-11, 51-25-16.

Part: BEAM — CORRODED (BS 605-621) · corrosion level 2 · airframe 23,519 hrs · 22,105 cycles

SEVERAL SCREW HOLES ON THE RBL 27 BEAM HAVE LIGHT CORROSION FROM FS 605 TO 621. REMOVED OUT OF LIMITS PORTION OF BEAM AND SPLICED IN NEW BEAM IAW SRM 53-00-43.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,519 hrs · 22,105 cycles

FLOORBEAM IS CRACKED AT BS 280 BULKHEAD. LT SIDE IS JUST OTBD OF LBL9. R & R DAMAGED IAW REO 601R-53-11-171 & 601R-53-11-138.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 23,519 hrs · 22,105 cycles

RT INBD FLAP VANE CHAFED 2 EA PLACES. BLENDED OTBD CHAFED AREA, ALODINED, PRIMED AND TOP COATED AND APPLIED TEFLON COATING IAW REO 601R-57-52-004. REMOVED INBD L/E SKIN, INSTALLED NEW SKIN PN 601R14303-54 AND TOP COATED IAW SRM 51-42-13, 51-23-00, 51-25-16.

Part: FLOORBEAM — CORRODED (BS 559.0+112) · corrosion level 2 · airframe 23,519 hrs · 22,105 cycles

BS 559.0+112 LBL 27 FLOORBEAM CAP CORRODED. R & R LBL 27 FLOORBEAM CAP IAW FORM 412 AND SRM.

Part: ACCESS PANEL — CHAFED (LT WING) · airframe 23,519 hrs · 22,105 cycles

FLAP ACCESS PANEL 584AB CHAFED PN 601R14003-23. REPAIR IAW REO 601R-31-52-1799.

Part: STIFFENER — CRACKED (EXHAUST) · airframe 23,519 hrs · 22,105 cycles

CRACKED FWD STIFFENER ON PANEL 446L, REPAIRED CRACKED STIFFENER IAW CMM 78-11-00-997-022-A07.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 23,519 hrs · 22,105 cycles

FUEL PANEL 510AB CUT OUT HAS FRETTING CORROSION. BLENDED AREAS OF FRETTING .003 MAX REMOVED CPX-7, REF 326, CAL DUE 6/14/12 NDT INSPECTED, ROTO PENNED, SANDED, ALODINED AND PRIMED IAW REO 601R-57-21-030.

Part: DOOR — CHAFED (MLG LT DOOR) · airframe 23,519 hrs · 22,105 cycles

LT MLG DOOR IS CHAFED. BLENDED CHAFING IAW REO`S.

Part: SKIN — GOUGED (RT NACELLE) · airframe 23,519 hrs · 22,105 cycles

RT LOWER CORE COWL INNER SKIN GOUGED 3EA SEATS 85-3. REPAIRED 3 EA LOCATION ON RT LWR INNER CORE COWL SKIN IAW CMM 71-12-01. REPAIR NR SRS046.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 23,519 hrs · 22,105 cycles

LT INBD FLAP VANE L/E CAPS CHAFED INBD 601R14303-53 CENTER 601R14303-39, OTBD 601R14303-43. REPLACED INBD IAW SRM 51-42-13. REPAIR OTBD AND CENTER IAW REO 601R-57-52-004.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 23,519 hrs · 22,105 cycles

SEAT TRACK ON LT SIDE CORRODED. REMOVED AND INSTALLED NEW SERVICEABLE SECTION OF SEAT TRACK IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 364-424) · airframe 23,519 hrs · 22,105 cycles

SEAT TRACK ON RT SIDE CORRODED. REMOVED AND INSTALLED NEW SERVICEABLE SECTION OF SEAT TRACK AMM 53-01-11.

Part: ACCESS PANEL — CHAFED (LT WING) · airframe 23,519 hrs · 22,105 cycles

AILERON LOWER ACCESS PANEL 559AB HAS CHAFE DAMAGE. BLENDED CHAFED AREA ON AILERON LOWER ACCESS PANEL IAW SRM 51-12-00. REMOVED .009 OF MAT, MAT THICKNESS .081 REMAINS ORIGINAL THICKNESS .090 REMAINING MAT IS WHAT INSERVICEABLE LIMITS IAW REO 601R-57-60-020.

Part: ANGLE — CRACKED (BS 625) · airframe 23,519 hrs · 22,105 cycles

RT OBLIQUE ANGLE AT FS 625.00 CRACKED. R & R IAW REO 601R-53-61-422 AND SRM 51-40-11, 51-42-21, 51-42-06.

Part: SILL — CORRODED (BS 473.15-529) · airframe 23,519 hrs · 22,105 cycles

RT FLOOR SILL BETWEEN FS 473.15 AND FS 529.00 HAS CORROSION REMOVED. CORROSION & RESTORED FINISH IAW REO 601R-53-41-666.

Part: SKIN — DENTED (BS 605 S24-26R) · airframe 22,041 hrs · 20,530 cycles

FUSELAGE SKIN DENTED AT FS 605 AND STR 25L. REPAIRED IAW REO 601R-53-61-3984.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 20,562 hrs · 19,014 cycles

RT FLIGHT SPOILER CAUTION MESSAGE ASSOCIATED WITH ACFT ROLLED LT. C/W QRH SPOILER DID NOT DEPLOY. FOUND RT SECU`S SYS TEST AND BYTE TEST GOOD. BOTH RT FLT SPOILER PCU`S ELECT AND OPS TEST GOOD. RT OTBD SPOILERONS PCU HAD HIGH RESISTANCE, REQ PCU IAW AMM 27-62. OPS CK TESTED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (SPOILERS) · airframe 20,525 hrs · 18,974 cycles

RT FLIGHT SPOILER CAUTION MESSAGE ASSOCIATED WITH ACFT ROLLED LT. C/W QRH SPOILER DID NOT DEPLOY. C/A IN PROGRESS.

Part: INTERCOSTAL — CRACKED (DOOR) · airframe 18,990 hrs · 17,382 cycles

AFT COMP DOOR RT UPPER INTERCOSTAL IS CRACKED. AFT COMPT DOOR UPPER INTERCOSTAL REPLACED IAW SRM 51-42-06. (K)

Part: FITTING — CRACKED (FAIRING VENT) · airframe 18,990 hrs · 17,382 cycles

LEFT TAILPIPE FAIRING VENT FITTING ASSY CRACKED. LT TAIL PIPE FAIRING VENT FITTING ASSY REPLACED IAW SRM 51-42-06. (K)

Part: CAM — WORN (FLAP BUTTE DOOR) · airframe 18,990 hrs · 17,382 cycles

LT WING OTBD FLAP, OTBD FLAP BUTTE DOOR CAM WORN. LT WING OTBD FLAP, OTBD BUTTE DOOR CAM REPLACED IAW REO 601R-57-53-016, REV NC. (K)

Part: ANGLE — CRACKED (BS 559) · airframe 18,990 hrs · 17,382 cycles

LOWER RT CAP ANGLE OF THE PRESSURE BULKHEAD IS CRACKED FS 669. LOWER RT CAP ANGLE AND PRESSURE BLKHD STRUCTURE AT FS 559 REPAIRED IAW REO 601R-53-41-260 REV D AND REO 601R-53-41-609 REV A DEVIATION D. (K)

Part: BULKHEAD — CRACKED (BS 621) · airframe 18,990 hrs · 17,382 cycles

AFT PRESSURE BULKHEAD WEB ABOVE CARGO DOOR TRACK IS CRACKED AT FS 621, LBL 27.5, WL 130. CUT OUT ON DAMAGE PORTION OF WEB ABOVE CARGO DOOR TRACK AT FS 621, LBL 27.5, WL 130. NDT PERFORMED ON CUT OUT WET INSTALLATION OF PIECES IAW REO 601R-53-61-1541, REV B. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 18,990 hrs · 17,382 cycles

CRACK FOUND ON INTERCOSTAL FS 484, RBL 36. INTERCOSTAL AT FS 484, RBL 36 REPAIRED IAW REO 601R-53-41-059, REV B. (K)

Part: HINGE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 18,990 hrs · 17,382 cycles

PAX DOOR TOP FOLDING STEP UPPER HINGE AND SCREWS FOUND CORRODED. PAX DOOR TOP FOLDING STEP UPPER HINGE AND SCREWS REPLACED IAW AMM TASK 52-11-00-430-004. (K)

Part: LONGERON — CORRODED (PAX DOOR) · airframe 18,990 hrs · 17,382 cycles

PAX DOOR LOWER LONGERON IS CORRODED PAX DOOR ENTRANCE LOWER LONGERON, CORROSION REMOVED IAW SRM 51-21-06. (K)

Part: PRESSURE BLKHD — CRACKED (BS 621) · airframe 18,990 hrs · 17,382 cycles

REAR PRESSURE BULKHEAD WEB IS CRACKED AT THE LINTEL LOCATION FS 621, LBL 46, WL 110. CUT OUT ON WEB AT FS 621, LBL 46, WL 110 NDT PERMORMED ON CUTO OUT, WET INSTALLATION OF ALL PIECES FABRICATED IAW REO 601R-53-61-1230, REV D. (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 18,990 hrs · 17,382 cycles

PASSENGER DOOR AFT DRAG STAIR ANGLE CRACK. PASSENGER DOOR AFT DRAG ANGLE, REPAIRED IAW REO 601R-52-11-513, REV A. (K)

Part: BRACKET — CRACKED (BS 528.56) · airframe 18,990 hrs · 17,382 cycles

LT MLG BAY HYD SUPPORT BRACKET AT FS 528.56 BTW LBL 18 AND LBL 27 CRACKED. LT MLG BAY HYD SUPPORT BRACKET REPLACED IAW SRM 51-42-06.

Part: BRACKET — CRACKED (BS 528.56) · airframe 18,990 hrs · 17,382 cycles

RT MLG BAY HYD SUPPORT BRACKET AT F/S 528.56 BTW RBL 18.0 AND RBL 27.0 CRACKED. REPLACED IAW SRM 51-42-06. (K)

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 18,990 hrs · 17,382 cycles

INTERCOSTAL CLIP AT FS 484, RBL 27, WL 71 IS CRACKED .300" LONG. INTERCOSTAL CLIP AT FS 484, RBL 27, WL 71 REPLACED IAW SRM 51-42-21. (K)

Part: BRACKET — CRACKED (LT NACELLE) · airframe 18,990 hrs · 17,382 cycles

LT ENG AT 6 O`CLOCK POSITION BRACKET CRACKED FOR T/R ORANGE HARNESS. LT ENG AT 6 O`CLOCK BRACKET FOR T/R ORANGE HARNESS REPLACED IAW SRM 51-42-06. (K)

Part: ANGLE — CRACKED (BS 559) · airframe 18,990 hrs · 17,382 cycles

LOWER CAP ANGLE OF THE PRESSURE BLKHD IS CRACKED .400" L, LT SIDE. LOWER CAP ANGLE OF THE PRESSURE BLKHD AND PRESSURE BLKHD STRUCTURE AT FS 559 LT SIDE REPAIRED REO 601R-53-41-260, REV D AND REO 601R-53-41-609 REV A DEVIATION D. (K)

Part: SKIN — DAMAGED (BS 228) · airframe 18,990 hrs · 17,382 cycles

FASTENER HOLES IN FWD FUSELAGE ACCESS DOOR SURROUND DOUBLER F/S 228.00, STR 19-20 DAMAGED FASTENER HOLES IN FWD FUSELAGE ACCESS DOOR SURROUND DOUBLER AT FS 228, STR 19-20 LT SIDE REPAIRED IAW REO 601R-53-11-162, REV B.

Part: HANDLE — CRACKED (AVIONICS DOOR) · airframe 18,990 hrs · 17,382 cycles

MAIN AVIONIC DOOR HANDLE HSG FOUND CRACK. MAIN AVIONIC DOOR HANDLE HSG REPLACED. (K)

Part: HANDLE — CRACKED (CARGO DOOR) · airframe 18,990 hrs · 17,382 cycles

CARGO DOOR HANDLE HSG FOUND CRACK CARGO DOOR HANDLE HSG REPLACED IAW SRM 51-42-21 AND DWG NR PL601R35027, REV AY. (K)

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 17,152 hrs · 15,596 cycles

LOG 192917/4 WHEN BATTERY MASTER SELECTED ON OXYGEN MASK FELL PASS OXY PBA INDICATES OFF.

Part: RUDDER PEDAL — INOPERATIVE · airframe 15,427 hrs · 13,934 cycles

NO DIRECTIONAL CONTROL ON TAKEOFF WITH RUDDER PEDALS. ABORTED TAKEOFF. AIRSPEED NOT REGISTERED. BRAKE TEMPS 4,3,2,4. PERFORMED TAXI TEST WITH CREW ASSISTANCE IAW 09-20-00 AT 60 KNOTS. NO DEFECTS NOTED. A/C GOOD FOR SERVICE. (K)

Part: SEAL — MISSING (FAIRING)

DURING CRUISE INTERMITTENT VIBRATION AT 280 KNOT FOR APPROX 5 SECONDS. ALL ENGINE PARAMETERS WERE NORMAL. APPLIED SEALANT TO WING TO FUSELAGE FAIRING AS REQUIRED IAW CRJ AMM 51-23-00 AS REQUIRED. (M)

Part: ANGLE — CORRODED (BS 461)

RIGHT PRESSURE FLOOR SILL PLATE ANGLE AT FS 461, RBL 43 CORRODED APPROX .750 INCH DIAMETER. MAINTENANCE FOUND CORROSION TO BE LIGHT. REMOVED APPROX .002 INCH MATERIAL IAW CRJ 200 SRM 51-21-06 3B 1-5. (M)

Part: ANGLE — CORRODED (BS 499)

LT PRESSURE FLOOR SILL PLATE ANGLE AT FS 499.0, LBL 43 CORRODED APPROX .750 INCH DIAMETER. MAINTENANCE FOUND CORROSION TO BE LIGHT. REMOVED APPROX .022 INCH MATERIAL IAW CRJ SRM 51-21-06 3B 1-5. (M)

Part: ANGLE — CORRODED (BS 499)

FOUND RIGHT PRESSURE FLOOR SILL PLATE ANGLE AT FS 499, RBL 43 CORRODED, APPROX .750 INCH DIAMETER. MAINTENANCE FOUND CORROSION TO BE LIGHT REMOVED APPROX .002 INCH MATERIAL IAW CRJ SRM 51-21-06 3B 1-5. (M)

Part: ANGLE — CORRODED (BS 544)

LEFT PRESSURE FLOOR SILL PLATE ANGLE AT FS 544, LBL 43 CORRODED APPROX .750 INCH DIAMETER. MAINTENANCE FOUND CORROSION TO BE LIGHT. REMOVED APPROX .002 INCH MATERIAL IAW CRJ SRM 51-21-06 3B 1-5. (M)

Part: BRACKET — CORRODED (BS 319)

FOUND SERVICE DOOR LOWER SILL JOINT BRACKET P/N 601R38335-1 CORRODED AT FS 319.70 WL 73. MAINTENANCE REPLACED LOWER SILL JOINT ANGLE ON SERVICE DOOR IAW CRJ 200 SRM 51-42-06, 51-42-21 AND BSC EO 601R-53-13486. (M)

Part: SKIN — DENTED (LT TE FLAP)

LEFT INBOARD FLAP UPPER SKIN DENTED 15 INCHES FROM INBOARD EDGE, 7 INCHES FROM TRAILING EDGE APPROX 1.25 INCH LONG BY 1 INCH WIDE BY .022 INCH DEEP. MAINTENANCE REPAIRED LT INBOARD FLAP UPPER SKIN USING NON-FLUSH REPAIR IAW CRJ 200 SRM 57-52-00 REPAIR NR 03. (M)

Part: PANEL — CRACKED (PAX DOOR)

PAX DOOR STAIR AFT SIDE PANEL IS CRACKED IN ZONES 2 AND 3 APPROX .250 INCH LONG IN RADIUS. MAINTENANCE REPAIRED ZONES 2 AND 3 ON PAX DOOR AFT SIDE PANEL IAW BOMBARDIER REO 601R-52-11-702 AND BSC EO 601R-52-13410. (M)

Part: PANEL — CRACKED (PAX DOOR)

PAX DOOR STAIR FORWARD SIDE PANEL IS CRACKED IN ZONE 2 AND 3 APPROX .250 INCH LONG IN RADIUS. MAINTENANCE REPAIRED ZONES 2 AND 3 ON PAX DOOR FORWARD SIDE PANEL IAW BOMBARDIER REO 601R-52-11-702 AND BSC EO 601R-52-13411A. (M)

Part: FLOORBEAM — CRACKED (BS 280)

FOUND FS 280 FLOORBEAM CLIP AT RBL 9.0, INBOARD, IS CRACKED IN RADIUS APPROX .50 INCH LONG. (M) MAINTENANCE REMOVED CRACKED SLIP AND INSTALLED NEW CLIP P/N 601R31113-58 IAW BSC SR 601R-53-0057A AND CRJ SRM 51-42-21. (M)

Part: FLOORBEAM — CRACKED (BS 280)

FOUND FS 280 FLOORBEAM CLIP AT RBL 9.0, OUTBOARD, IS CRACKED IN RADIUS APPROX .50 INCH LONG. (M) MAINTENANCE REMOVED CRACKED CLIP AND INSTALLED NEW CLIP P/N 601R31113-58 IAW BSC SR 601R-53-0057A AND CRJ SRM 51-42-13, 51-42-21. (M)

Part: FLOORBEAM — CRACKED (BS 280)

FOUND FS 280 FLOOR SUPPORT BEAM CLIP AT LBL 9.0, INBOARD, IS CRACKED IN RADIUS APPROX .50 INCH LONG. (M)

Part: FLOORBEAM — CRACKED (BS 280)

FOUND FS 280 FLOORBEAM CLIP AT LBL 9.0, OUTBOARD, IS CRACKED IN RADIUS APPROX .50 INCH LONG. MAINTENANCE REMOVED CRACKED CLIP AND INSTALLED NEW CLIP P/N 601R31113-57, IAW BSC SR 601R-53-0057A, CRJ SRM 51-42-13, AND 51-42-21. (M)

Part: FLOOR SUPPORT — CRACKED (FS 280)

FS 280 FLOOR SUPPORT BEAM CLIP AT LBL 9, INBOARD, IS CRACKED IN RADIUS APPROX .50 INCH LONG. MAINTENANCE CRACKED CLIP AND INSTALLED NEW CLIP P/N 601R31113-57 IAW BSC SR 601R-53-0057A AND CRJ SRM 51-42-21. (M)

Part: BULKHEAD — CORRODED (BS 280)

PILOTS BULKHEAD FS 280 HAS CORROSION APPROX .010 INCH DEEP BETWEEN LBL 9.0 AND RBL 9.0 AT WL 73.10. (M) MAINTENANCE INSTALLED NEW ANGLE IAW CRJ SRM 51-42-06 AND 51-42-13. (M)

Part: ANGLE — CRACKED (BS 621-625)

FOUND LEFT AND RIGHT FS 621 TO 625 OBLIQUE ANGLES ARE CRACKED. MAINTENANCE REMOVED CRACKED ANGLES AND INSTALLED NEW ANGLES P/N 601R-35012-51, 601-35012-52 IAW CRJ SRM 51-42-06. (M)

Part: FLOORBEAM — CRACKED (BS 484)

FOUND LEFT SIDE UNDER FLOORBEAM HAS A CRACKED ATTACH ANGLE AT THE OUTBOARD SIDE OF LBL 27, FS 484, WL 70.73. (M) MAINTENANCE REMOVED CRACKED ANGLE, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW BSC SR 601R-53-0029B. (M)

Part: FLOORBEAM — CRACKED (BS 484)

RIGHT SIDE UNDER FLOORBEAM HAS A CRACKED ATTACH ANGLE AT THE OUTBOARD SIDE OF RBL 27, FS 484, WL 70.73. (M) MAINTENANCE PERFORMED REPAIR TO RT SIDE FLOOR SUPPORT INTERCOSTAL ATTACH ANGLE OUTBOARD SIDE OF RBL 27 FS 484 IAW BSC SR 601R-53-0029B AND CRJ 200 SRM 51-42-21. (M)

Part: UNKNOWN — UNKNOWN

LONGITUDINAL OSCILLATIONS BEGAN CLIMBING THRU APPROX 26,000 FT FOR APPROX 30 SECONDS OSCILLATIONS RETURNED IN LEVEL CRUISE FLIGHT AT 33,000 WITH AUTOPILTO ON OR OFF. OSCILLATION STOPPED WHEN BEGAN DESCENT.

Part: BOLT — LOOSE (NLG DOOR) · airframe 21,056 hrs · 10,632 cycles

INTERMITTENT VIBRATION IN AIRCRAFT, FLIGHT CONTROL AND ENGINE INDICATIONS NORMAL. INSPECTED ALL DOOR AND SEALS, PRIMARY AND SECONDARY FLIGHT CONTROLS, MLG AND NLG DOORS, ALL FAIRINGS, WHEEL BINS, RAM AIR SOV, APU INLET DOOR, ACM`S, RADOM, WING TO FUSELAGE MOUNTS AND ALL ANTENNAS. FOUND AFT NLG DOOR RT BOLT LOOSE AND TIGHTENED IAW AMM32-20. FOUND BELLY FAIRING SEALANT CRACKED AND RESEALED IAW 53-50. (K)

Part: IDG — FAILED (RIGHT) · airframe 11,986 hrs · 10,565 cycles

DURING TAKEOFF IDG CAUTION MESSAGE FOLLOWED BY GEN NR 2 CAUTION MESSAGE, ABORTED TAKEOFF. REMOVED AND REPLACED IDG NR 2 IAW AMM. OPS CHECK GOOD. (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR)

FOUND PAX DOOR AFT DRAG ANGLE IS CRACKED. MAINTENANCE REPAIRED PAX DOOR AFT DRAG ANGLE BY CUTTING AWAY DAMAGED SECTION OF ANGLE AND INSTALLING REPAIR ANGLE AND SPLICES IAW REO 601R-53-11-513 REV A. (M)

Part: IDG — LACK OF LUBE (NR 2)

ON TAKEOFF ROLL, IDG NR 2 CAS MESSAGE FOLLOWED BY `GEN NR 2 OFF` CAUTION MESSAGE. ABORTED TAKEOFF AT 60 KNOTS AND COMPLIED WITH QRH. GEN RN 2 RESET. FOUND IDG NR 2 OIL QUANTITY LOW. RESERVICED IAW AMM 12-13-24. ENGINE RUN OPS CHECK GOOD AT THIS TIME. ABORTED TAKEOFF AIRSPEED WITH LIMITS. (M)

Part: CABLE — BROKEN (PAX DOOR) · airframe 10,385 hrs · 9,022 cycles

INFLIGHT AT 10,000 FT F/A REPORTED LOUD POP BOARDING DOOR AND SAFE INDICATES SECOND STEP RED. NO ASSOCIATED PAX DOOR WARNING AND CAUTION MESSAGE. FOUND BROKEN CABLE REMOVED AND REPLACED ICE DOOR CABLE ON DOOR PRESS. VLV IAW AMM, INSPECTED DOOR OUTER HANDLE FOR CRACKS AND OTHER DAMAGE, NO DAMAGE NOTED. (K)

Part: SENSOR — OUT OF ADJUST (RT MLG)

FOUND RED WARNING GEAR DISAGREE ON TAKEOFF RIGHT MLG DID NOT SHOW UP LOCKED COMPLIED WITH QRH, ALL THREE GEAR EXTENDED. TIGHTENED RIGHT MLG UPLOCK TARGET AND ADJUSTED SENSOR TO TARGET CLEARANCE TO .085 INCH REF AMM 22-32-05. PERFORMED GEAR SWING. OPS CHECK GOOD AT THIS TIME. (M)

Part: HANDLE — OUT OF POSITION (MLG) · airframe 9,862 hrs · 8,559 cycles

AFTER TAKEOFF, ROTATION GEAR DISAGREE RED WARNING MESSAGE CAME ON, WAITED 20-30 SECONDS, LOOKED AT GEAR HANDLE, IT SEEMED WAS NOT UP ALL THE WAY. RECYCLED LANDING GEAR HANDLE AND GEAR CAME UP. PULLED OUT QRH, C/W ALSO CHECK HYD PRESSURE WAS NORMAL. (K)

Part: ACM — MALFUNCTIONED (RIGHT)

RT PACK OVER PRESSURIZE ON BLEED SWITCH OVER, AND WOULD NOT RESET, AIR RETURN. REMOVED AND REPLACED RT AIR CYCLE MACHINE IAW AMM 21-51-10, OPS CHECK NORMAL. (M)

Part: MANIFOLD — CHAFED (APU) · airframe 7,622 hrs · 6,521 cycles

STRONG ODOR OF JET FUEL IS PRESENT WITH PACKS ON WHILE ON GROUND. FOUND APU PRIMARY MANIFOLD CHAFED THROUGH BY STARTER CONTROL VALVE. REPLACED MANIFOLD IAW AMM AND REPOSITIONED CONTROL VALVE. GROUND RAN AND LEAK AND OPS CHECK GOOD. (K)

Part: PLUG — DAMAGED (FUSELAGE)

MWC - 170 PANEL 131AL HAS DAMAGED FREEZE PLUG AT NR 2 IN CLOCKWISE POSITION, EXCEEDS DIAMETER OF .343 INCH PER BOMBARDIER REO 601R-53-11-162. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND LEFT FS 621 ANGLE IS CRACKED. REPAIRED LEFT FS 621 ANGLE IAW BOMBARDIER, INC REC 601R-53-61-117 REV B B4 INSTALLING REPAIR ANGLE. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND RIGHT FS 621 ANGLE IS CRACKED. REPAIRED RIGHT FS 621 ANGLE IAW BOMBARDIER REO 601R-53-61-117 REV B BY INSTALLING REPAIR ANGLE. (M)

Part: ACCESS DOOR — CORRODED (LT WING FUEL)

LT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 12.245 HAS MINOR FRETTING ON FAYING SURFACE LESS THAN .010 INCH DEEP. PERFORMED A MAJOR REPAIR BY REMOVING FRETTING IAW BOMBARDIER, INC REO 601R-57-21-030 REV D. (M)

Part: SKIN — CORRODED (LT WING)

FOUND LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT AT WS 163 HAS MINOR FRETTING ON FAYING SURFACE. LESS THAN .008 INCH DEEP. PERFORMED A MAJOR REPAIR BY REMOVING FRETTING IAW BOMBARDIER, INC REO 601R-57-21-030 REV D. (M)

Part: ANGLE — CRACKED (FUSELAGE)

LEFT SIDE 484 ANGLE IS CRACKED AT INTERCOSTAL FLANGE AT LBL 36. (M)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 7,483 hrs · 6,398 cycles

LT SIDE 484 ANGLE IS CRACKED AT INTERCOSTAL FLANGE AT LBL 36. REPAIRED LT SIDE 484 ANGLE AT LBL 36 IAW REO. (K)

Part: SENSOR — MALFUNCTIONED (TE FLAPS)

FLAPS FAIL MASTER CAUTION DURING FLAP RETRACTION DURING TAKEOFF 17 DEGREE SETTING. REMOVED AND REPLACED LEFT BPSU REF AMM 27-51-10. OPS CHECK GOOD. (M)

Part: STRIKER — DAMAGED (PAX DOOR)

PASSENGER DOOR SEAL STRIKER IS DAMAGED AT FS 310 AND FS 349 AT MIDDLE LATCH LOCATION. REPAIRED PASSENGER DOOR SEAL STRIKER AT FS 310 AND 349 IAW REO 601R-52-11-008 ISSUE B. (M)

Part: ADG — WILL NOT TEST (ELECTRICAL)

MAINTENANCE CHECK FLIGHT REQUIRED FOR ADG DEPLOY INFLIGHT FUNCTION TEST. REMOVED AND REPLACED ADG (S/N OFF: 0598) (S/N ON:0736). PERFORMED ADG FLIGHT TEST, TEST OK. ADG COMPONENT REPAIR SHOP TEAR-DOWN FINDINGS, NO FAULT FOUND (NFF).